AVIONES DESGRACIA B 47 f 86 %H2OX7/

Page 1

DEPARTMENT OF THE AIR FORCE HEADQUARTERS AIR FORCE SAFETY CENTER

AFSC/CV 9700 G Avenue SE, Suite 240 Kirtland AFB NM 87117-5670

3 1 0 T Z~GO FERNANDO DE MONREAL CLAVIJO

Mr. John Greenewald, Jr. ·.-.

·.·.

Dear Mr. Greenewald, Jr. In reply to your 28 September 2000 request, attached are the releasable portions of the 5 February 1958 B-47B/F-86L aircraft mishap report. Some pages may be difficult to read, but these copies are the best possible. Portions of the safety investigation report have been redacted. They are not releasable for the following reasons: a. The safety investigating board's analysis, findings, and recommendations are exempt from disclosure under the United States Code, Title 5, Section 552(b)(5), and Department of Defense Regulation (DODR) 5400.7/Air Force Supplement C3.2.1.5. Release of this information would have a stifling effect on the free and frank expression of ideas and opinions of Air Force officials. Privacy information regarding other individuals referred to in the report is also exempt. b. The statements of witnesses giving unsworn testimony before the safety investigating board, as well as any direct or implied references to such testimony, are exempt from disclosure under the United States Code, Title 5, Section 552(b)(5), and DODR 5400.7/Air Force Supplement C3.2.1.5. In order to promote full disclosure, witnesses are promised by the mishap investigation board that their testimony will be used solely for mishap prevention and for no other purpose. This promise of confidentiality is made in order to encourage witnesses to disclose to the investigating board everything they know about the mishap even though the statements they make may be against their personal interest or possibly incriminating. c. Information from the Life Sciences Report is exempt from release under the United States Code, Title 5, Sections 552(b)(5) and (6), and DODR 5400.7/Air Force Supplement C3.2.1.5 and C3.2.1.6. Disclosure of this information would result in an unwarranted invasion of personal privacy.

In addition to the federal regulations cited above, our denial of release is supported by case law which clearly establishes the Air Force' s privilege against release of safety board deliberations, analysis, and recommendations. Landmark cases include, Machin v. Zuckert, 316 F.2d 336 (D.C. Cir), cert. denied, 375 U.S. 896 (1963); United States v. Weber Aircraft Com., 465 U.S. 792 (1984); and Badhwar v. United States Department of the Air Force, 829 F.2d 182 (D.C. Cir. 1987). Release of these portions of the safety report, even though the report is old, would jeopardize a significant government interest by inhibiting its ability to conduct future safety investigations of Air Force aircraft mishaps. Disclosure of this information would be contrary to the promises of confidentiality extended to witnesses and investigators. There was no time limit placed on this promise, and such a disclosure could set a precedent that would result in a weakening of the process whereby the Air Force gathers and evaluates safety information in future aircraft mishaps. The decreased ability of the Air Force to gather and evaluate safety information would result in the increased loss of aircraft and crewmembers and ultimately have a detrimental effect on national security. Pursuant to his authority, when a mishap report is deemed historical, the Air Force Chief of Safety can, under certain circumstances, release the safety board' s findings. He has done so in this case. Should you decide that an appeal to this decision is necessary, you must write to the Secretary of the Air Force within 60 calendar days from the date of this letter. Include in the appeal your reasons for reconsideration and attach a copy of this letter. Address your letter as follows: Secretary of the Air Force THRU: HQ AFSC/JAR 9700 G Avenue SE, Suite 236B Kirtland AFB NM 87117-5670 Federal regulation provides that the cost of search and reproduction be assessed to the requester. The total in this instance has been waived. We have no other information responsive to your request. I hope this information is helpful. Sincerely

~~one!, Vice Commander

Attachment: KC-97G Aircraft Mishap Report, 29 Oct 57

USAF

r\ ..

tt. ; !r. .r: :; .:, , ;:,~ ~ ~~­ fir~ . oirfromc failure, bailout, 1pin . dt ~" ~ "r·:

10. ALTITUDE of oircro-ft oOo•c

oecurrcd

:19

· . HUnter

·--·,

351

·

..

·.

I. AIRFIELD DATA. i-IU IN (o) OR (b) AS APPLICABLE. (F<>r tcoploncs · · opplieablc. Oi~.euu ln Section M.) If .occidc~t oecurrcd on' oir~rt: (b) II occident ~c~rrcd off airport : cl ..otion at teen< of o«:lt-~L.I~~\-~-

. lc~gth

of ;~nwoy in vn:_ _ · _ _ ft .

Was aircraft toling off, approaching or moneu"cr ing to lar::f7

Hcodi~~ ~f ru~~·ey in un ___ dr:srcu Fidd clcvation_. _ _ _ _ ft. MSL

If yu.. stotc airport involve-d .. _ _ _ ___ ___

Type of runway turlaec ; (Ched)

For cithu airport mentioned in lib above :

Yn__

-- - - - --

If no, state nearest airport suitable for landing tl1is oircroft .J-it!Il~J:

J ),

Co.,cu:tc__

A1phalt __

S~e airport type. (i. c .. AF. A, N, CG, !'C, P) __{';f__ ..

Other_

(Specify) ___ _

Distoncc, airport

t:

Nc .:s_

accidcnL_A.2N.__milu. Heading of runway in

;.1]_ _ _______ .~ . -i -

P

uu~n_Q___ _dc ~u tc l.

lr:~_; ~ .:. : . r..~~wm~~~~~~~~~-~----------------~------------------ Magnetic bearing, oirport to oecidcnt..JJ_B__ degrc:u.

Airport c:le¥o1ion _

_

J. ASSIGNMENT AND STATUS CODE c + ,; .., , cf oc ' ;,;.

N/A I. OPERATOR (Person at controls at time of accident)

a. LAST NAME I Jr., II, etc .)

FIRST NAME

MIDDLE NAME

Clarence Arville

13

J\.l.!l

56

Pilot

FIRST NAME

MIDDLE NAME

··I

t \.]"

\

.

~

•

S<!ction D-FL YIHG EXPERIENCE OF PILOT! S I INVOLVED

1. '>NAS OPERATOk 0~1 INSTRUMEtJTS

··- ... -··· ..._... ---.. -..·-·--·-----..·-----1 ,q

TIM~

OF ACCIDENT OR JMMED1~.Hl Y BEFORL !-·- ·--··-·- ···--- -·---·---......--............... ..

.. _·----

(C.,mplc•-: ·'~"'· 1 1 +hrou~h ··: ,;· for -:n~h --~~,.-:,:;;·~·b·~-,-~-,~~-)

T

I'.SSIGNED DUTf ON FLIGHT ORDfR

co.i>.1i:cir ··

~~~sr· ~ . ?tl.ci t (Lo <l llomd

.

(lod Nome)

~ · ·,.:i~CP..':rT'CI.io·~· ) (Lmt ~lomd ;

.... t:/A __ .1 _... _F/A_ .. . __ ;_ _____'.J)J:, ____.... ___· -~;~..:...:.____~ 1

..___ ----·-

.. __

--------..l......--------'-----

· - - -- - - - - - -.. +-····

Section E-PERSONNEL INVOLVED . - - - - . . - - - · - - - - - -- - - · - - - ·(,..ln_,..c_l_u__d_i....::."9 operator and all othr.r pcn'.:.\n\ , ...,J\cthcr in plane or not ) Duly c!

h.nc of occ: idc nt

Nome { lo1t nomt. rir1f, Grode, Serial Number end Component or Sc rv ,cc)

Typ<

ORGANIZATIONAL ASSIGNMENT

Aero

Rating

p

No::!. .

'· I• TDR'r•'l•til•d1 Yu. .• _ . NoX_ Attadl copy ol r•quorl .

W~4

FiGhter D1terceptor leston ~~, South c~roli

Sczction H-DAMAGE DESCRIB& ERIEFlY EXTENT OF DAMAGE TO AIRCRAFT AND ANY PROPERtY DAMAGE INCURRED •

.I

·"

'Aircraft totally destroyed

Sec:tion K-CONDITIONS AFFECTING ACCIDENT

Sec:tlon J-ACCIDENT TYPE Chc:d one: occident type as "Primary." Che.:k all othtrs applicable as

~~r-~~------------------·------1 -~---+-··s_.•_c_o_n_d_o~ry~.'-'----------------~--~--·----------------------------~

Section L-CAUSE FACTOR ANALYSIS (S<e AFM b7-5 for definition•) (P) , ond thon contributory co~~~--ioclor-;-Ti:fih~ moybc~pjicable. NOTE: Contributory couu facto" may appear in some mojor cote gory as primary co"'u:, i. c .-both primary and contributing cause: factors may bt: .. Operator error." OPERA ~-OR

~~;-O-;-- ---·-·TI;c·~~~~; ~;~ti~-~- -;Jth~-;i~~jt" ~-;-it,--,~~~;;;-~~~~~cr hchni·~uc ; inod~quotc

-------·----~--

~~~~~~!ro~dur~~-~~-~!~ jud9':~~~··

by

Right preparation :

p~~~~~~-_:~~~~~-f oi~~~~~~~ -~~":~~~idcnt .

Error comm itted by any mt"mbcr of the: flight crew uc~pt opuotor(1.} .

- -- - - - - - - ---------- - ----.. - -----------------------------------·-----1

lncd~quoh~ ucrciJc of command : inodtquoh supuviston of a •rcrcw\, opuotion1, maintenance other f1o1ndicM s~o~ppg r t•ng flying ope.~cti?r'li ; i.node.q~o~otc s... puvision of t r, iniflg , ~'< · I Incl. IP's & AC't

i lmptopu repair. suvicc , inspcdion or instullotio~ of aircraft comp:)n~nh , path or systems : inodtq'-lote

· --t-~~~~~~~-~~~~~~--~~-~--~~'!.~~~~~~~~--~~~~~~-~-~:~-~-~~~~-~~~-~-~ ····· ······ ··--..-·------..--- - -·-----------1 .- EHo11 committed by other than Ottcrt:w , supt:H·isory or motntcnonct: pct,onncl. lndudu GCA, Weot~<r .

Towc:t, Communicotloni, lnstollot.ons ond ony othu • i.l ppott •ng personnel . de .

11------- ----------------·---------·-·_,______,__,_______ _···· --··--· ·---·---.. --·- -----·--· j Failure or molfuncflun of

.

. .

the oid,omc, t:ng•nt or ony othcr sy,tcm, componcnt or occu•o"l ol the

·------!L~~~~~~~-- ~-~:·_ ....... - - ----·--·· -----------·· -... . .. -·- ---·.. -·- --- .....____. ___ --·- ---· ··---- ------·---------! Any 1"\0ifwnct•on. tnodcq~<~acy or ob,cnu of ou bo"" and . or g,r .. oy• tqutpmcnt ot focilitiu. includ.ng i

dcf,cic:nctcs and hoaord1 (If rwn ... oyi, to•t•oys. op•ons. o•tl t wn~ . dear tones. etc..

" 'j' _.. ____ . ·· ··- ·--

.. . ·------ ---.. .. _ .. .

.. .... ... ... ......

. ..... .. .- ··-·-·-·.. ·- - ···--------·-· - ·- - ..------ ·---

( Rcductd wisibihty , •cin!l . twrbw!cnc.c , thund( 1\lorrn, , ,~,~doc.c ••t~d . .... nd, cfoft , lo- cc i ltn~ . ~tc: • .

-;--

..

- ----- ~·

-·- --

~- ·--- -~

. -·

'--

~

. ·-· -----

...... ....... ... ..

MIS(E-'... ! . ANEOU~ (O; lOITJQNS : l! wJ •:~ o k'!'~ . ~• ~ vd ~-;-...- to'!J.tf, c.ho" . r•cocP-.th.. hyp?uo:l. ·. r" "~o bt.guc . de .

c:•u.t s. or c.u•d•hom '"n&,..Jcrul rc Lt p P mo r t ur CO"'" •t:.utory co ... ,c h.1ct r.rr~ of N\.ltt r.)t,..-c Docr.pt•on cA A,c;ulcnt rcquirtd l,f Sc-r.tu:tn M.

dtto.lcd duc.ropf!On uf O(h

fiNOIHG!.

J..<<;tf•OI'I

I uporoh:

palf.J9roph

fQt

S\!ction M-INSTRUCTIONS FOR COMPLETING NARRATIVE DESCRIPTION OF ACCIDENT THl · · ~~ ... R~ATIVE DESCRIPTIOt~ ' Will INCLUDE THE FOlLOWING lt·lFORM,.TION PAEP,..P.ED 01~ SEP,o.~-'TE SHEETS C>F P.o.PEP AND .A TT .. c,;en TO THE J..F FORM 1•

•

A co~c. i u: nn n of·v~ · ·'

... .. ~·..,r, : .. h~d '~''' ""'~ '"CUtTH•u,..co ., chron r"J II)gtcol vrdr:• ul thr: n.ght ffo ..... to~I.GP.' fo tr""''~'~:J ~ ; J')n •• /~ bt: p1ts~"h: d : d~~t . hmf! ol'ld JH>tnf o~ .-:r, r.: turf.: , typt ol c.lr.oranct. ITIIH•on. d~st,,.,afiO'I , ht)ur, :~f ~uti , ET€ . pos •f ion •cport,, wr.IJ+u:r . "''

•.c

2. INVESTIGATION AND ANALYS IS (Su .o.FM b2-S)

n.,

ttchon wdl YOI'f U'l con•('nt OC.C~Idt ;ICJ fo the compluity of tl..c oc.c.idr.nt and tht: ut~:nt t)f th,. ..... ut iCjahol"! . Dr~~"d'"9 upo" th'! nofurr of'"'' oc.c.idr.td, Mporoh PfJf09roph\ \hould d~\c.r i bf' th~ ua,.,inotion , onoly1•1 ond l ind•ns1 ol ony or oil o' the lollow •nq , oorcroft '="9 ' ~'~<1 : o •rfr11mt and ••ructuru: control ty\tc"' ; clccfHtol tyth:t"''' ; hydraulic •y•h:m: flight inshurncnh : noo;•~ot•onol oids and nir holt focdihu : '.lde.qu?ty of comrnond and \taR 1.upcro;is•on of operation, and tra•n•ng ; odcquoty of moinhnoncr prouduru, iPtlpll:cho" ond ''O"I i n~ ; vr.•f dllrd•vu end SOP •. and any othu fudor~ pcdir.e.nt to the octidrnt. l"f o"d d i,cuu any "' i olotion~o .

n.,.,,

···-· o · Th iJ "dion w•ll fitt the: 1i9"ifi ~ ·•nf factual defc:rmHHJfion\ ruulti:-.g from invcshgot ion of the oc.c•drnt. Separate poragr-:~ph1 wifl be u1ed to enumerate the following : primary coutc of the oc:cidcrd ; each c:ontribu!ing c:oule foc.tor of the ocCident : YOfluus ddicic:nc:•u or •nodcquociu o( equip• mcr'lt, proceduru, operations. momtenoncc, supervi1ion, locildiu. etc., whicJ..~Ithough not direct contribuhng laclcu, to this occ: idt:nl, ore horards to softdy ol flight : various considerof•ons f'IOf cloued 01 contributory cou1u of th~ occident but implcm~ntoflon or installation of which would hovt

~: ::~:0;~-io~~i:::~- ,1hs:::~~~.~~:y_-:~~:~·~~~~.~:·~;-~::~:~n::~~:;;d~ . ~-. -.~!_~:-!~_ :.:!:. ~ '!. __

nus icthon wiiJ Contain, 1n C:OnCISC onr4 cfucct sfot(mcnts, 0 f1shng of ~ .'1":'cd10 officer or board, ... ,11 prevent r~c.urre"'ce of ••m•lor fypt: occ•denh and l.mj-h

fu:

...:_: ·:

.

-~

·--=-- __ _. .. __~_:____ _

.

__..!

'~OII~chve OC.fiOn\ whu:h, 1ft the 0p1n10n of fh~ lft'tUfigoflng

ddic:u1:nc•n c.tt:d '" "F•nd•ngs" of the •nve1t.got.on .

_______________ _R-~~r~t~:~-~#~~- -:~tr~.~&~r~~fo1J Yr: ED--·--·-----~ H aJ ~~~QR..QAN45)6 ONJ.·1

THE FOLLOWING WILL lol.ldOi<. Ali<CRAFi ACCILJENij IAi' FORM l•j

J._

RFOJ.IAWIJ'IG.-~LL .J!L~TACHED

~-' '

.f'

TO nEPoRrs OF

1.

~

Norralivc

.

~Jmo A.lt.e!D~ ~Ht':/~)lVti~BLE

~

duc•i~~ion of Aceidcnt ~~:.~;:n:,- --. -t--- -~:T ~~-:-~rocccdings

r;t;J

2.

X

AF Fo•m 14A·----- ------------~~

~

X

AF Form 148

4.

X I

Af

6.

X

Statements of crcw mcmbcrs and witnen••...lwh~-~·~.i~•-~-1--+1-X-1-op_p_o_r_tu_n_it_y_ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _

X

Scc;tion G, Item b)

------ _ ________ (;) ___

~orm 5, Piiotlsi onvoivcd ISec Sec. 0, licm ;;)

·--

S.oO~-.-n-t_o_f_c_o_n_tr_o_l-to_w_c_r_o__p_c_r_o_to_r_l1-)----------i

~~/+tcmcnt of runway control officer

t-~TX IS!:!::r.:o! of ...,•!-er 1.-::<e:!cr 18.1

6.

e

Liot of Tec.J.nicol Orders not complied with ISu

I .

..

.

20.

X

Statement of damage to private property

21.

X

Mop sho•ing geoJrophic:ol loeaiion of occident

22.

X

DO 36SF (Form F)

Diagram of Kc:ftc of oec:id&ftt

23.

X

AF Form 14C

IX

AF Fotm 1~0

I DO Form 781-1

Statement o-r

T{)"'"'

DO Form 781-1

statenent Q.f

TDS"

t---

- - -·

9.

X

10.

X

II.

X

Photograph& (identified)

2~- I

12.

X

lndn to AF Form 14 oltoohmcnll

25.

/A

Af Form 14E

13.

lx

NOTE: Determine Security olunificotion of report& I if applic.ablc)

26.

/A /A

AF Form

I

d~clining the

~ Tronscnph of comn"1Urt1tnf•ons rc:corcl•ng&

00 Form 175 or AF Form Ill 1Clearance J

··I X

X

or stohments

19.

1-~C.::..:'--f----.c,_--:.,_----------------

7.

j Statements of rebuttal

27

----~

7

-

l~F

AF TO 29 (Unsatisfactory Report)

--

I. I

~

i

:I '""""' o41tltnt t( Ihit lu• ""'Y ~~

Ab

••o4

Pate 4

• •• 1

REf'ORT OF AF AIRCRAFT

.

lc"" ;" occoulontt with AF Reg. 62-14 one! Af Manual 6i-&, "Airc~afl .A.ccidcrn Pr<Ycnlic~t-lnvuli!alion-Rcp<>rlin! .~ Fill in all Of>OC<I !>PPliooblc. If .oddilionol 1poc:i: i1 nudcd, ocldi~-1 "'•cl(•) and ldc,t~y by proper tc~on letter and wb~ecticn numb,.

u,.·ll>it

wte

Section A-GENERAL IN

RMATION . !l..occidtnf occurred on oi• port. identify,

EOFF

10. ALTITUDE of airc;o!.

Hunter, C"'1. . "-IRFI EL D DATA.

FILL IN (o) OR (b ) "-S APPLICABLE. (For scapi OflU

D i\c. U~t.

'a pplicab le.

in St- d ion M.)

If occide nt o:-curr<d on ai rpo rt: ~t .ng th

of run•ay in usc ___ ________ ft.

Head ing of runwa y in uu: __ ___ dc.grc:u

! (b)

If occident occuucd off o1irport: elevation at scene of acc:tf . ___

I

Wen oircraH to~ing off. opprooc.hing or moneuvc1ing to lond7

I

.Fidd clcvoli on. _ ·····-- --· ·-· ·--.11. M5L Type of runw ay \u docc : (Chcd. }

Conc rt!c ..

fire, airframe fail..,rc: , occurred

08: 35

i

A•pholl __ _

Yes__

No.x_

If yes, tfote a irport involved .. --------- --··---· .•.. . --...... ··-····---.. --··-- __ _ _ _ --·- -

11 no, 1lole ntorul airport suiloblt for londin9 thi, aircraft _______ ,

H-.mter

A1'l3~ -·-· -- - ·-

For either oirpcrt mentioned in II b above :

l i

( 5p.c ify)

J5 J_9_~__________ft. MSL

Stale airport type (i. t., AF. A, N. CG, PC, P) ___ ___ ;:..f_ ____ Didonct, a irport to occident.. Magnetic bearing, oirpori to

_

illLmiles. Heading of runway in use_. ~'ZQ ___ dcgreu.

accident_~.)-~.... degrees.

Airport dc:vation_ ..b..~- ---ft. MSL

3. ASSIGNMENT AND 5TATU5 CODE at lime of accident .

SA.C-C-C

LING RE UIRED Ofo>' f.AA 14~~, ~~IP.F F< C.2- l ti. ·- ----·--··--·- - -- --··-·------ --· ··-··· - ---···: COMPONENT

...Richr.r.>i:N~ . HQ'{?.L<LJ~·1L __ __ __ R~o1

or

j c. A5SI GNEO DUTY ON FLIG HT ORDf.K

R·~~!-~~~!-···- ·--------·-· ---~-~~~----· ~p- · ----~--- -~-~---- ---~ !~.~!~~cify)

I

ASSIGN Eel ORG ANiiArtON- -- --·

: Su bc:ommond or AF ~ A.r o ~ ~•li OI'J

s..;.c

,

2.!2

t-----· - =~- --:-c- _ _....._ ___ - -

ATTAC HED

\V. ng

b2 3 AJJ

:

i

~ Squadron or Unit

r Group

I Sq!Jodra'R"'~-,

Group

··- ---- - "--- ·· -- - - - ---- ~ ----FOR FLYING S ubcon>rT~O•\J or A.F Au D·.:!~ :wtng

O~G A NIZ A TI O:-l

i

NUMBER

··----) H~ . i .JJ.&\E_ _ . ____ .14-31+5J\

b. f 0 5I;ION IN ;.IRt"l.AF T AT TI NIE OF ACC IDENT Fr ::.l'\ f or lt: h StoY..

l 5ERY ICE

------·

l

- -- ---- --

I Bct.c

).9 BVI ! if/A - -.a-.------: 30BS stead -------....J.-.---·------- ___ .l_I Rome __ __ _ _ _ _ _ r:· 1·

·-: .

: r;

I • ;

J

{"

I

llntt

Sou:

._1·

.. •

2..4F . : I o23 AJ) I 19 m N/ A ,-,30BS Horne stead . ... -· c. -· ·-- ----·---·----"--- ---- - - - ·-· - --.... ·-- _ __1___: ___ -·- ... -- __j_ ·------·----·-··-·· · . ORIG INA L "-ER OIIAtJTICAL RA TING< 9· PHS ENT "-ERON"-UTICAL R"-TING Jh. INSTRUMENT CARD 1•. AFSC "'"o.;:;;..n Ri;Ce iv·w I Ar-<0 D"'TE iU:<.~iVlO ! _ Gre-=~ I . 1245A SAC :/• ·.:_ i - - ·-- .. - ··'.

t-----~·:c:--::-:-·c::·.-:~-c.---·-- --

I

___ ___ . _ __

I

j

..

lypc

1

.

Pflmory. ..

~- -~~~ i;)?~ --~an . ~9_5~. __._ __D_•~_o.l~·~r~.:.•."... 6_..~.PY.__2~_ _o~_'r ___

CP

;~

Otltct ~ Spc cif yJ

• j S.quorircm _ ~..c .

ATT ACh E[!

L

_

?!\F. .

vl:; Ar ~IV.TIOI<

J u;.J _

f ·) P. FLYING ; Sub <<.mtT",anJ vr Af· \ .A11 O• .,•U<1n I

_ S\C

.

2t-:;:

. O?.h.J! r-<~At /,(i(:JN,.l. Uii(AL RA T1r ;(.

;.'ID

O A ~E

P.f(f •VE::J

P_lt_ - ~ ~~- .. ~~5=~-.

.

j Win~ I

-~2 3 .

~

.......J..

1,H

Un•t

__!_.30 B$ . - ·· ..

..l9 ...

ISq uo dt <;l\

( Gt(.l~.>p

or Untt

I

T· ~·

. \a !. t .e..

THAN rwn PI LOE ARc II<Y OLVlD (fLIGtH CREIIII ) REPORT 5"-ME

!HP!:le t>'~-~:c>).,_______________~ j B<uc ~ :iv!: ~ stead

; .~ ·· ..:F·sc ·

1h ltJSTRUMEtH CARD

_~ _. r.~:~ . . ---~ ~~~-- ~;.;.2~- -- ~-... .-..!. ... -~':!.~ .:!_!:~~::.:::-:..b.·..~~~

; BoH

'

. _4,9 _ . , .. . .. H/..\ . .. . L JO _p$

p;.-<;~r-<: AEWONAUT ICAl ~ATING ~. ti!.l D.>."r E RECEIVED

... . ... .

12_45A

:

.-: :..;_

,c·:: ..••.-

Pnmo•y

I Ovt.,

·· ·· ·- · ··-·· ··12)!;.J! .,

'j

"J{·

L . ___ ·- · _ ... --:: - •..J.' INFORM .. Tiurl HOIJIRHJ IN 5ECT10r~ (.

s~ction E-PERSONNEL INVOLVED

:

1-----1--------_l·~ ~ ~~ NOTE: If c><lditionol spoe< is r<quir<d to list oil personnel involved , ottoch add itional shut.

S(tction F-WEATHER Ceiling

I

Visibilit~

·- Lf --· -·· lQ_-

I :;~T'Oire:!Kion

I

(At time and plae< of accident) and Velocity

J Te::~aFture

I

o·e= ~~nl

~-

I

All. Setting ,

1lY 1"1'=>)-j "\. • i') "1019 If w~rotnt.r , 1ncludin5 wind condition&, was o foetor ift the oecident, oHoeh ltahmcnt of wc:othcr officer .

Other Wco~hcr Condition'

..

fj

Sectloa b.-ENGINEERING DATA: :; -,:, · -.. -.;,ct ~----------------------~~----------~--------~--~---------1. Damage :

J.

(Chcc~ oot) "Ocslroyid__

Subs'Ltio)L.

Minor_

N~n._

r '

'

2. Wqs aircrafi damaged bey..nd ccoiu,.;,ical repoir7 Yu - . Nox.

~ii.im~tcd nu~b.cr ~:f ~irc.cl _"';'"hours fo~ rc~ if oppl,ic~blc_.l57Jt.•'..n •C~;, of d~os•.': ~ir. crolt• . .-~486.00.~- .

<4. Fin befo re

occ•d~nt_:__ ~ Fur

after occedcnt ._ ..

h

F1rc: d1d not

occYr,.X. ~~·

O.d csplos,on o.cc".u7 Yu.:--

Na_~

....:.._} . .

t

o. H~w ,;,o~ 1.0: ..Ot ~;;,plied with ai tin~ ol occident?.-26-···_ ·__; i,Vr.b. numbers ond titles o~ scpo~atc s).ut) 1: ----'--..,....;-.-. _____.:...____----1 7. ··~lot your ·aa.. prcvi~u;ly' oubmittcd

1. h

6

UR l.•i•a ~Ubmitt'tJ

.:01

D

UR Oft ony ·roc-tor

o '""'' olthi• occiclc•17

f-:--:-· . . .

. .. ' . .

AF: 1'r~:M$ 6 14

,.;,,1•••• ~.1101• er 11-u ,,,;. .. ,

~- li TOR r<quuld7

lnvolnd in lt.io occident? Yes .•. _

Yes~ -· ..

'1'1!1.-- No._.J:; Altuch copy of rtQuul "-

.,,..~

No .• • ;:

N~...:.:

(If "Yu" aHo<h copy)

--~----------------~

u·R ftvmhcf_~....~:. --·-·-··--·

··

I

... .

v•-·~~··~

bY 'an

. .

Section H-DAMAGE

. . .·

.

. (', /

~ J.- J./.'? ~.

1 . RiEF:.Y· EXTENT OF DAMAGE TO AIRCRAFT AND ANY ,RO~ERTY OAMAGF. IN~UI:RE-------O. - - - ---1'

is considered

ec.:~nomically

repairable. ;Further evaluation iu to be

A:M·~c~ <te6m. · Right side of fuselage from .awroximntely otntion

870

1)[~:-:J-.

-~. 18 excesaivel;f d..alD!iged~ An forms and bulkheads are broken in this e.r28. " R~E;.'n.t ·: borizon.t a.land ·v ertical atabiiizers extensivdy da.znllged: Right ;rir.g np:prc:r:il:a?.tcly Station' 1555· 1;() 595; . eic:essi7Yely damaged. 'fue rear Spe.n is broken in tvo. Upper and.: lover st::-ess plates are torn and buckled. Right drop tonk deJDolior"ed. Ntu.1bcr 6 engine torn loose at rear mount, tail cone dama.ged sligbt.iy. Right aelcron o.nd fla:Peron <le.maeed. .Left drop: tank je'!tsoned and unrecovered at present. Sectio n l{-CCN DITI ONS AFFECTING .:.CC!J;l';, ··-:-

Section J-ACCIDENT TYI'E occidc~f type as "Primary_ ." Chcc~ all athcn applicable a•

Chr:d on r.

''Secondary."

·

Section L-CAUSE FACTOR ANALYSIS {Sec AFM bl-5 lot definitions) primary coun foetor (P). onith-~;-;;nfribwJory ·~~-UlC factors (C) that may be: app ii~J,J;_--- ·--- - ----NOTE: Contributory eouu foc:torl may opp.:or in lome mojor:. r.ahgory as pr imary cow ~t. i. c.-both p ri ma ry and contributing c.oule

factors

be "Optro!or error."

----'----'---- ---·.,-----~--;-~· ---:-----:--~-- ----.---·-·-.--- -- · ------ · ------ -- !

Incorrect operation of the a ir craft or ih systems ; improp1:1 hchn•que : in~d c:quo t c fi ight prc:po•ofion : improper ptouduru ; faulty judgment, etc., by pcnon(s) at contro ls of o;rcroft o' t.mc of occident.

e,or comm itted by any mcmb.:r

or the

Aight

CICW

u c rpl o;--•. rot a! {\).

lnodc:quotc U¢teisc of command ; inodcquc:.tt •upcr.,.is ion of o irc.rc- '"' \, opc•ot ion1 .

othtr fun-~ti ons 1upporfing flyln9 ot'cral ;u"' ; i~•uUc~uuic tuJ.~t"•• ;l; .... ., u: tru;.,, ,,':S · ";.,_ \ : .. .::.

;r·, t. ;...('.;

---··----·--·- -·-----..-!----·--· ..-------· - '" ..... - ··--------------.. ---··-.. - -- -.. --. ... -- - _, ___ ·--· - - - - -·- ·

lmprop~r fCpolt , U:I VICC, in1opcction Of in\follation o( o itet oft cum ron cnh . pOtfi 01 \ Y'•'Cm'l.; inudcquol c

___.. __________ ._____ _______ _____

or _____ improper _____._________.___ ,_ .

_ ____

cornpl ioncC' with utabli,hcd maintcnunce prtu:cdu tu. __ . . , , , ,_ , _._

Erro11 committed by other than oirctcw , wpC'n·i,ory or mointcnc.nc.c p C' ru.. ·

t l.

lncb d t , GCA , Wc-othc• .

ions., ln~. tollot io n' ond ony othu 1ouppotl ing pc:nonnc-1 , rtc. ___________________,,____ ., -----..-+--.To•u, . --- -Communicat - ---..--.... .. __ _________ , _____________........... ............ - ··--- - _, __ _-- __,_, ___ ___ ___ ..

I

Failu re or malfunction of the a irfr ame , eng ine or any other 'Y'tcm . componcr.t

01

occU\CIJ' of the

. oirctaft , etc.

i An y rnolfunct•on , •nodc:quocy or ub1cncc of

011

bo•c ond or o u ... a 1 , c- qu.pmc-n~ or foc:!d,t, , ,ndudin<J

~ dcfic•cnciu and hotordJ of rwnwoy\ , toa i ... oy• , apron• , owc:r;un\ cl r o•

zon CI . et c.

; Rtd '-! ctd wi , ib illty , ~c : n, . tucbwlc:ncc: . thundu,totm,, U.ttfoct • ind , .. ind, o lclt , ,lu ... C.lll,ng , dt. . . j ... --- _,_ __ __ .....

... ..

-···· ·· ··- .. --·-·---.. ···· ·-· -.. ···· ·-- .. ·-r-. -· ····-··-·---·--.. -·--·· .

S12dion M-IHSTRUCliONS FOR COMPLETING NAIIRAiiVF. PHCRIPTIOH OF ACCIDENT THf ''IJ-"RRAT I'IE DtS(RIPT ~ IJN" Wli.l •TTA CIIEn TO TH( M FCRM

1•

l~l(lUD~

THE FOLLC'oX'ING

lll~OPI-IATI(';N

PRfPARfO Or< SF.PA~ATE SHHTS Or PA'fR AND

A co,. t i•c rv:urott vt d u :J H'?b :. :.htd ll'lc.tt !tnd c.•tc.wrn,tnncu i" duonol.,gt co l otdr.t c.f the f), 9 ht 1, 0 ,.,., tt:.~h!')U to t~ 1 ,.,, ,H,t 10 "' .,.. 11J be dotr , ftmc nnd potnt ol d " r·c : turt , t ·( pt of dt:otonu, ml\\ton. df!st inc;tion , hi'Ju't of furl . ETE- f!Ot• t 10 , r~pojrh . .. , 0 thtr. rf c .

1.'-,,

2.

lliVE~TIGATION

AND ANALY:iiS (S« .o.FM 62-Sj

Thu ucfton will vory in contr:nt occ:ordtng to th~ comple,•ty of the. occidc.nt and the ufcnt ol the ,,.,.~:,hgot•on . Oc.ptnd•ng upon th, na ture of the I"Jccid,.nt , tt~Otl')ft paragraph• 1hould duc,;bc th.: uai'Tiinofion , 'll"'olytis I'Jnd findtng' of on~ or oil ..,f the foll')wtng : OH<. t oft ~"9•flc:\ ; Otllromt and lftucfUtt\ ; Confrof \y\ftm : t:fc:t:.fr tc oJ \ "f\!tm; hydrouftc. 1y1hm ; flight instrumf'flft : ftC1"' 190t!Onul oith ond oir bou foctfdof"t ; oJ~qUOI'",y of COn"ttnond ond ttoH lupcr"'•IIOn of flying opuot•on\ ond fro•ning : adequacy of moinhno'lc.t proccduru, 11\lpedto,. tone' tro~ru:"\g: unit dirtcfi'-'u of'ld SOP1, ol'd ony <..thr.r fodot \ pt t flfltnf to '"t: occ i d~nt . L;,f and di,cuu any violations.

J. FINDINGS (S« AFM 61-5 lor d<to;l, of p•u<nlofooni Th is s~dion will li't tht 1ignificont factual dctc:rtnrnofiont ruult ing from invufiCJof•on of the: occ•d,nt . Scporoh F-oOtogr op ht ,.,jlf be utc:d to tniJ · -=-•.Hue. (I( ;~c ou.;dcn ;; cod, t.on;r iOr.dir.g cou1c: fuc;or of the: 6ccu::irnt : vcwou' cit:l~t.lf:nc•u or rnodcquocic:t ot tqu•P · rncnt . pror..rdur~l. opuot:oru. "'oin~cnonce, 1upuvition, focilitiu, ffc .. ... hich ,Jthou9h not dir,.-;f co"*"bvttng fa ctors t'J tht~ oc cl'j~nt, arc hatorch fo lofdy of night : VOf i">UI COMidttofiOnl I'IOf clautd 01 C.Onfribufory COUU\ of th~ CIC.Cidtnf but !tnpftmtnfof.on Of intto!Jofion o( which would ftovr d~crtand or minimized lht probability of the: occidt:nt hovin~ occurred. /'

,,., ,u :. th• fv!!v .. ;"'! · Y~;mu•1

..... -·- - - - - - ·-- ---..- --- - - ------ - ·····- ·-·-·-- -- --·····----···-r · ··---- --- --·---- -- -- ·----·• . RECOMMENDATIONS (Su AFM 61-S lor d<toilt of pru<ntotion) This u:c.t ion _.j!! c.onlorn. ;, concin and duect stotcmtnh, a listina of the oniccr or DoorC , •iii prevent rtc.urrtnct of simiior f y pt: occicienh ~nd t

RECORDER '<; CHECKLIST FOR

~-------------- -----&fit~r~l~~:-R· M-~"'' THE FOLLOWING WILL BE ATTACHED TO All R MAJOR AIRCRtfl A~CtDEtlli ·(~f_) )'QA~ ~)

odion~o wh ici.,. ' " thr. opin iort o~ lht ,,..,.,Jigot in! 1 clfc.d '" "' hnd rngs ·· of the '""'c:stigof1on.

THE AF FORM 1-4

r\fG ~·riK1;l~tJ.rR-E~P- ------------~ THE FOLLOWING '<will BE ATTACHED TO REPQkrS OF ·• r MAJOR·'"'CC'IDENTS WHEN APPLICABLE .. --·o - -·· -

--

·---------------1

AF Form 5, Pilot(•) involv<d (Stc S<e. D,ltem 15)

Stoftmcnt of weothu fortcadtr

Stotcmenh of ere:-... mcmbcr1 and witncstcl (when available)

Stohrnc:nh of rcbutiol or ttatc:mcnh declining the opportunity

u.t of Tce~nicol Orders nol compli•d Section G, llcm o)

Tronseriph of comrnwnicotiona r~cord i ng1

wit~

(Sec

DO Form 175 or AF Form II) (Clear on«)

lndu to AF Form 1<4 attachrncnh NOTE: Dct.,minc S<curily (if applicable)

claui~eali on

of reports

being t.ontlcuc:d, ferried, etc., at+ach cop&C3 of co. · meu.ogcs 1howing soinins ond laaing organizations

Sec:tion N-AUTHENTICATION . (NAME AND ~RADEl •

..

••

I

rliSTOI11 OF FLIGHT

,\? Jet (B-47) No.: 51-2349, hereafter known as Ivory 2 1 depllrted Homestead Air Force Base, Florida., on 4 FebrWI.ry 1958, at 21512, on a roun.:!r?bin IFR flight ple:.n tc Homestead AFB. This aircraft 't(aS N'Lirr.ber 2 of Ivery Cell, a 2-ship !light, !rom the 19th Bomb iving M Jet (;iAC) 1 i:wol nd. in Operation Southern f'~lle as directed by Second Air Farce Operations Order 300-57. ':'he purJ?CSc of this mission was a USCM for the 19th Bombard.":lent ~·ling, involving chaff drop and max.irD'.L":l fighter ut tc-.cY.s :in the simulated enenw area, 2-ir refueling, t.nC. "' ::. tr ~--11ge t.:-crget radr.r run, AJ' Form l'i5 for Ivery 2 requested (in the Remarks Section) tbat flight p1an inforrr,;:;.tion "not be passed to tr.e 20th, 30th 31st .37th or 5th Air Division" (sic). 19th Bc:::b \"ling aircrews were specifically briefed that no fighter attacks were to be made outside. simul::.ted enenv territory, i.e,, not south of the targe:. at Jlg_d fg.t,ejoA.

--.

Virg_~, ~___..

Although 2AF Operations Orders 500-57 speci!i~ that attacks would not be made Southern Belle B-47's except

on, sequcnt}.J published J5AD .Jar. 51.1), authorizing fiehter intercepts to ?;s within the 35th AD area

0

'!'he !1 ight of Ivory Cell frcm Horr..estead Air Force Base through tr.;.. t .:;.rgo:t <: r<)ct was l.inc·.-ent!'·.ll 2.r.d ii.s br:!."!fed. All tactics up to the IP 1-1ere normal; at the I?, Ivory 2 obto>j ned !-.is spc-.ci!"lg from Ivory 1 for an in:\ividtwl bomb run by doglegging and, at bombs away tin;r; 1 Ivory 2 mlnules be~ind Ivory :. • IFF settJ.r.g~ were as briefed with was hrory l squ~•,kl.ng 2 aftf;::- tombs away end Ivory 2 on standblC, throughout the mission. Ivory 1 was responsiblti for all positioD rep~rts, ae briefed. :

4±

•

Bombs away time~ for Ivory 1 and 2 were 045oiZ aad 0455Z (5 F$b 58) respectively. Both aircraft reduced speed from 460 to 426 KTS TAS 2 minutes pa~t the target Lnd descended to 34,000 r~et ~ld 35,000 res~":ti'.r~l:':l e:!.ti~~":~!"~ ~~t

!.b

29.;.~2 11 !!g ..

~v~~ ~ ~~vt'r c~ught. up t.tri. t.h

Ivery 1 after bomb~ away although he did attempt to decrease his intenal elight.ly by holding 430 KTS TAS ( approx:inuttely) for a !!hort distance afJ.er level off from poet-target descellt. l'fQry l proee~ded o.n course as briefed on a 200° TH t:;, his turning point (TP) sout.'lea.et of the Sav~&rmah Rinr PNject (SRP), ~nd thence on course on • 220° TH to a point weat of s~varu1ah, Georgi&. At 053~2, Ivory 1 r~ported to Ivory 2 that he had just. been under fighter att.ar."lt by a eingle fighter aeen to a ro&ch :.:'.rom left to rigti t.

(Cont 1d)

Hi st ory of Fl ight

At 0 53.3Z approxilllateJ.y, Ivory 1 he.a.rd a ¥~t.ia~ trfill!:'mis!!ie. !rom Ivory 2 ~!! Guard channel (UHF), stating that he had bsen hit by another aircraft. The c:G-pilot o! Ivory 1 repor:t ed eeeing a !la:~h o! !ire at his 5 o•c:lock .position s ome distmce behind &n:!. ':~lightly above~ . · Ivory 1 .made a .!!mall tun to star- · . b;.:.id, th:nt d~cided he coUld be of ':nc h~lp to Ivory 2, and proceeded oa c:ouniJ t o Ho~s tead . Ivory 2, afte r bomb!! away and descent to .35 ,OCOfeet, overshot hi:! checkpoi!tt ·. at Char lotte, North Cuolina, and turrted south i.t a point 11 NM we:~t of Charlott ~; at leaet one !"lther easteH,y turn to approxi.m&tely 1700 TH wu made to miss the Sa.\"<Hmah River Project, and in !let· doing, Ivory 2 agaia overshot his TP southeast of the Savannah River Project; at this point Ivory 2 t urned southwest to 2250 TH and continued on this track until the time of the colli sion. At 053l~Z, Ivory 2, having jU8t heard Ivory 1 report a fighter attack, a lso saw a figh t er passing close underneath from le!t to right. Shortly thereaft er , at approximately 05332, Ivor,r 2 was hit b7 an F-86L (Pt~ Gold 2) and called Mayday over G1lard channel. The crew of .' I\rory 2 felt 1. eevere yaw to the left on impact; both pilot:! saw an explosion and observed No. 6 engine to hang at a 45° angle noee up; the #6 thrattle could not be !topcocked but the engine was s uccessfully shut down by pulling the firebutton. Ivory 2 bega...-1 ar. i.Inmediata dese ent and elow leit tUl"l'l to hold airspeed -which -nad de cr~ased t o 210K IAS ; the pilots then nctic~d the right wing tank rf.i ~ mis sing and ele c ted to jettison the left win£ tank in a clear area deeigna ted. by th~ n~'"i igs.tc r. !..fter ccn~ac~ ~~ th H~-ttar 7c;··i:Q~ ~d ltAJ::l CCN >. Ivory 2 rr~ de a s l owi d~1c ending approach t c H\mter Air Force Base; being high on the final apj:roach and p1.lling excessive power, a left turn -!;_ ,j the east wa s ~~d~ , the un i t j ettisoned of! Tybee Beach southeast o! Hunte~ A)r FOTce Base , and anot her l eft turn to 2?0°, ending in a euccessful landing at Hunter.Air Force Base, The damage to Ivory 2 wae major and extensive but t he cre1.,r wa e unaware of the full extent of the damage until after they / landed. Th ~ weath er in the Savannah area at the time o! the mid-air collision was VFR in !~arkness h1th a full moon. Visibility on th~ ground and in the a ir wae Gxceptionallr go od. Heavy contrails were reported by the fighters du ring th~i r inte rcept s of Ivory 1 and Ivory 2. 0

At 0508<: 1 5 February 1958, G<>ld Flight., :1 flight of three F-861 aircr aft, ":: !' sc~ar:b led upon. instructions receiv .3tl from the 35th Air Division (D) to intercept tra ck number PLl, sub:>t.:qt:<!r::.:!Y cl-<ingcd to PN17. Til! flight wa.~ ~.:i · amble. .:' op a hea<ii.ne of ?70 d~g!"f'!!l 1"-·,- !k:Ungw;..y, th~ 792.~d Airc:-a!t :cn :~,: ol and Haz·ning SqU!j.dron 1 based at North ;:!k.-. .:-lee ten Ai:r Station, Nerth Charlest on , Sout r, Carolina. The fH ght. ~:a:: ai rbo rne at 0513Z and made a routine radio report to The dut.y d.b-ect or e:! tc.li lish-.:d positi v~ radar contact and a::< sumeci control. on c.n ass:J..gned t.act.iC.:i.J. l're(juency. Tne flight was <Urected to co ntinue c li;ubine on " he;;.ding of 2?0 degreee to an altitude of 30 1 000 feet , clirr.bing a t mili : :"r;• pc·J~r to 15,000 feet and then in aft~r-ourner to 30 , 000 , Shortly .-. rt"r pa :>t~ill g through 11,000 feet the flight w ·.., ~). ven an in-t ra il t urn t o :h· :·:;rj;t to a heading of 360 degrees. Durini: t~.~:; clirr.b the night was ::.ain t :d.:! ~ ng an in--t.:-ail separ11tion of a!Jproxi.rr.ately !ive r::i"l.e s by r ad :;r. !'r;t I li. .;h t 'h:.i.s ad vi ~ed that the ta.rg~:t w;;.s tracking b~: t.ween 120 to 1 90 ,: .;: gre e!l ;<.:IG was Cit an altitude of !.bout 34,000 fer-.J:::;ol ~ fii ;-:ht wae d ir e cted tc le vel off F:.':. 35,000 feet • Ht!ndngwA.y .

•'. :?.

•..

S'Jl. d

O ~: e

F~';c ~ r1

•.r.rc'.lii:h :-:J, 'JOC , tne f l ight wa!l tu.rne:i

in-p.~.·~ ·ct~

~' L<rL~~d i<V.<=.cf.

l··-:~·.~ ~~

~l~ r::!

:.:. ~

V'!r:to r of 2'70 1egre'::5 ., An in-place turn r ~· nint\j' "'.. · ~.s :~ 1:0':. :.:t~l:!:!'C. :·- ~ iT.. r: uts tht! int~rcert..vrs 1~-ne. abrea!5t

_ ;-.·. ~-ta•j ;:1' ::n '";,., :c :-· :· .;,c e c r : ~ l.:>n fc: . : t. i •X•. For a ta.rget pa:ssine right '.o ~:c::: :'~ !.r1 t:-.i .o •:\ s-,, t he ~! ; !..erceptor:; !!hould t-'! L'1 an. ech~1.on

·: ,.,u. ,

•

Histerr o! Flight '

.

(Cont'~)

formation to the left with approximately five miles separation. • in tr.i:s caee -.:Aa necGs:;itatP.d CJ' .;.

.

::..:.t~

Tho tu.rn

det;;ct!.lln be.::ause ot a weak target.

. radar ~turn at the c:ontrolling radar site, The three fighters .,.-er'l d1rP.cted to displace themselves to gain the proper interval:, and these inetruction:~ were acknowledged b;y the pilots, The director theu in!~nned Gold One that ti1e target was thirty-!i ve degree! right at thirty-f:l. va iniles. Shortly th~r e­ a!'ter, Gold One wa.s instructed t~ ttu-n further left to a heading of 260 degree e. •. Upon rolling out on thia heading, Gold One asked the c::.r ' .;t• .;o~ how many bogies were in the track. The director informed ths fiight that .· two bogie_s were reported tv be iri the track, but that he_was painting only · one. In addition, he informed the flight tha.t thia waa a weak pick-up. The director then in11tructed G9ld Flight to turn further le!t to 250 · degrees. When Gold one called steady on 250 degrees, the director informed him that the target ~as about 40 degrees right at 25 miles. At this time Gold One called a contact at about 25 degrees left at 25 miles. After verifying the heading of Gold One, the director informed him that the target was 50 degrees right at 21 miles. A !ew se:onda later the director informed Gold One that the target was 50 degrees right at 19 ~iles. C~ld One had a radar contact at 40 degrees right at 16 miles. The director informed Gold One that this contact was his target. At this time the target wae called 40 degree~ right at 18 miles far Gold Two and 35 de gree~ right at 25 miles for G<>ld Three. Gold One called "Judy" at appro::Cu•.a. tely 15 miles and took over the remainder of his intercept. Gold Two had ~ radar contact at 50 degrees right at 15, and a few seconds later Gold Three contacted the target at 50 degrees right at 17 miles. Gold Two too k a "Judy" soon ·<:1ereafter. Gold Thr ee called "Jud;r" at 13 miles out with the target 40 degrees riJht, Very soon thereafter Gold One reported the target was appa.rentl;r turning. The director stated that the target appeared tc. be turning slightly to the sc:>ut.h,.,~st b•Jt that he ~sn•t getting ':cry good paints. All three inter~eptor pilots then stated that they were in a tail chase, Gold One stated that he was going to make an identific"lticn j:-.3.!':~ . Gold One advised the director wten nls radar indicated ten seconds prior to computed rocket impact and started his break-aw~y. r.n)n One re po; tcd the targst to be at about 35,500 feeti ealled "splash", ;;:-.:::. pasAed approximately 500 feet below and slightly behind the target aircraft., 0 During this break-awa;r, Go).d One initiated a gentle turn to the right to an assigned heading of 090 degrees. As the turn progr~s s e d he gradually increased his angle o! bank to a maXimum cf 60 degree~. Approximately one minute ,md thirteen seconds after Gold One- calJ.ed "Splash", Gold T"..:o callod, "T'went.y :;econ<1s" > advi:ling the director that hie r:tr!a::indicated 20 seconds prior tu the computed rocket impact time, Approximately 34 seconds later, a.t about 053JZ, the collision occurred. The total elapsed time between Gold One ' s transmission or "splash" to the coJ.lision was approximately one minute and forty seconds . The times indicated above were obtained from a magnetic tape recnrdinB of tht intercept mission . This tape was made at Hemingway, the ground contrc l intercilpt static:.~. responsible for th~ control of the mission. Tne times are felt to be rea.,onably correct :~ince the tap~!! ran con;; tantly during t hi e particuh.r mission, The a.ct:-.11ll time of impact was dete ned a mike "click" audible on the recordin

l

~

LJ {IIC.L/J SS; FlED

Hist~T.J . or Flight.

1

(Cont 1 d)

· All three fighters had during tha latter pa.r t. ,.r t he ~:..,~c~: :·r:-t ·~ ('. (·•J .' "lightly frC~m t-h~ find heading~! ?50 d~g=-~~:: g!.~~r: ::; t~.:: ;::;c.:. ~.-:: ;-. :;;:.l~ bne3~u in a right at· t he time o! the colli!!h n anc ob~er·, ?::: £:-. !l :, -ph:.ion at hit! four.· o'clOck p~:;ition shortly before rolling eut on hi s

:tun

h_ell~ine of 090 d~gre·~~.

G<>ld One returned to Charleston AFB !or l andi:l£;, a:1d C-<Jld TJ.:r ·.•c r~r.:ai n-: _; 11.t t he scene of the accident looking for narer. or ot ~1er inriicatio:-l!l o! eurvi vors. He remained as long ;tS fuel permi t ~-ed ;tnd t heh r e t un~ed tc Charle s t on AFB for landing. The we~th er at Charleston at the time of th~ a::ident was o!fi: ia~ly re p~rted as hi gh scatte r ed , visibility 15 mile s, Th,.. al tb~· te:- !i~t: i.ng ·,;<>r 30.17. Pilots in t his and previous flights re ported exc e ptior.alJy geed

, ___ ,

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IWVFSTIGATTON AND

A~~YSIS

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·B-u7B 51-231.!9 ,: Hepcat 39 ·' Ivory 2 in a cell of two aircraft, l<ir.ded :; t E<mter Air Fc:-::c Ea::e, ~-eor-gia 7 e.t Ol26E on 5 February 1993. Sufficient time elapsed after the mid-air collision had occurred until the B-47 made a safe landing at •Hunter to allow two meroters. of the accident investi ting bOard to 'meet the aircr:tft after landing.

A diagnosis of damage revealed the following: The first point of impact on the B-47 was on the rear of the right rri.ng, just at the aft tip of the drop tank. The wing was crushed inward to a point approximately three feet from the trailing edge and approxiwa:ely trree feet acrosso Red and blue paint marks on the right sice of the impact area indicate the F-86 was in a right bank of approxi:nately 30°. The F-06 left wing made the first contact rd.th the B-u7. The sta~dard Air Force insignia is painted on the top of this wing. The outb:Jard eight feet of the F-8& s left wing was c severed at this point; along wl t.h the F-3 6 drop tank and the B-h 7 drop tank . Impr;t shock broke the <.~t main spar in the right wing • in the B-47. Shock also C<Jused the aft mount of the #0 engine to hre:<lk and the engine !rung at a IIS'"J angle .• nose up. A section of the F-~6 left wing scraped across ~ he top of the B-L7 wing and circumscnbed"•an arc in scratches tack around tmvards the e:rJ?enr,:;ge of the 3-~7. It !;tru~k the aft right portion nf t:.he fuselaeF:l and vertical stablizer. The right horizontal stablize~ was struck from the front ~-a heavy object~ either a portion of the F-g6 wing o~ the wing " c~:;ter section . Thl s is berne out by the fact that the wing center section and the inbo~rd 6 feet of each wing separated from the f::~ela"e, presumably at j_mpact " -re r~:ained in one piece, and struck the ground soMe two mHes fro~n the ::~ain ''reckage. Both main landing wheels were found Hith this ~.:enter 'dn r; section and black rubber m;:;rks were found near the hole in the B--4 7 Tflrizontal stabilizer. A piece identified as a portion of the F-86 left ving (outboard leading edge) was found imbedded in the tical s blizer the rudder st cf the B-47.

()

with

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. .•

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.

FINDINGS

1. The prima~ cause of the accident was operator error o~ the part of the F-861 pilot in that he.collided into the rear of 4~other aircraft in flight during a visual breakaway from an intercept att.'ick U..'1der condi t:!..ons ~f excellent visibility.

'.

..... •

••

2. A possible contrjbuting cause of the•accrdent is materiel failure. The historJ of radar malfunction in this partict:rar F-861 • coupled with the very nature or the collision point up a possible e:-roneoua scope presentation which could lead the pilot to continue unaware on his radar run until dar~erously near the target.

..

3;

..

.

A possible contributtng cause of the accident is P-ilot

hypoxia which might have caused the pilot to disregard the "passage of time before initiating his breakaway after reaching the twenty seconds to go point. :

.

4. The fighter attacks vere autho:r;iz;d by• CINCSAC to

• '-,. ·· /

CINCNORAD. • •

Even eo, the B-47 ere~ vas not briefed to expect attacks in the collision area. AlthOugh not directly contributary to""the accident, this fact ir>.!.linuates a lack of complete co.ordination in the scheduling of fighter intercepts on. SAC aircraft. • 0 •

5. The B-47 pilots vere not in contact with GCI nor did the 2!F Operations Order require it, hence they were unaware of the intercept 'before vi~ally Bighting the fighters. 6. Th~ B-47 personnel were admit'tit!dly not familiar with the nature and appe~ance o! all-veatMr fighter pa!!ees and the methode UBed in controlling these pa.eeeB. ·

6

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Special Haruiling Rcqui.r1:!d in lccordance vi th Pa.ragraplul 49 and 52, .lYR 62-lh.

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. .. '. ! ··. 7•. The board could. find no record of Hemingvay GCl' 11 b:~:rlng . utilized height finder ra.dar eqUipment 1n .det·e·rmining the h•1ight and . COmpoSition of .,PN 17 itrack, even 'though erose-tell information frariJ. . Basketvool GCI :site did not eti:;:nuate the .distance apart of tvo . reported ·targets~ . · · . . ·. .. ~

'

8 :. :r11~ Pilot or ~g Gold 2 ~~~ not ..,;;aring glove! and therefor.,

.(

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tru.ffe"i'·~

severe frost bite after bail out: Further,·he vas•un!amiliar time of useful c,ol,leci~1sriese at 35,000 feet without_ · · · ox;rgen. · · · · · ·.

With the e.xpecteq

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.

MADISON .

Colonel, USAF · Prei1dent

1 · ~~

,·.

~el

USAF

~

·

Major,

USAF

Accident Investigator

c/bdL r~ &.u4 DONALD F. KNE.JU.E Captain, USAF

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DETACHMENT 4 _26th Weather Squadron United States Air Force :Hunter Air ·Force Base, Georgia

.

19 February 19.58

TO:

Who It- May Concern ·

I certifY that the following weather observations are c orrec t as taken from the teletype weather sequences or WBA N Form lQs for the time s indicated.

05/2JOOE

/-ll 15 mi vis

/t 10

100 ¢1 /-~ 15

o6/ooooE

Hi Thin Scattered 15

/~ 10

E 40 ~ /10 0 ~ 15

06/0lOOE

Clear 15 mi vis

/~ 10

40 ¢ E 100

06/0200E

Clear 15 mi vis

E 100 c 10

40 ¢ N 70

ES Ti.'!!e

CharlestonS.

Hunter AFB.

Aug-<Jsta Ga .,

c.

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15

Lt. Col. , USAF

Commander

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20 pages of life sciences withheld.

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AIP.C!lAFT

MAIHTENAN~E

IEPORT · Accid ... t .. Preve'ntion-lnvcsli~t.ion-Repoftins"

accordance with .AF : Res. 62-'14 orwl AF :Manual 62-6,

wh.. AF Aircroft Accident/lnci<hnt Involves lnoclcquacy, Mcilfu..C.tion. or Foilur. of Af Mote riel.··:···

Section A-GENERAL. INF~RMATION\. of accident ,.

5 m-1 rrE

52-10108

F-86t-5o

Comp·l~c · the

Hunter AFB 1 Ga.

4.

fepiA

]. Date lost overhaul

2. Totol airtrome hours

695:05

54

~orhouling

A\:C:5~SORI!!~

following when material failure, inodcquocy or malfunction ore known or wspcc+cd cause facton.

:I·• .~~ of JoJr Force acceptonco

2~ Oct

•

2D

6A.35M

: Scctlo11 I-AIRCRAFT. HISTORY, AIRFRAME COMPONENTS AND AIRCRAFT

·. .Y .

• I

Base invostiroting oC:C:Ident

4. l'locc of

Aircroft Nr.

Typo ond moclcl of oir"-raft involved

.~:5 'rebi-Uary se : : o~3J!z ·.

,

1 Harch 19)7 ~

5. Aircraft houn Iince overhaul

activity

7. Ai,rcraft hours at lost perio~ic irupcction

Dole ond type

8th Periodic

272:05

F AT Frc1;no, Calif

2D Oct

57

I. Nome, pori number and position on aircraft of port contributing to accident

62?:35·

Hot Applicable

• 9. Is port ovoiloblo for analysis? NO_

f!/A

YES_

(II yes) Where locoted 12. Date port last overhaulod

I I. Oaf< port lost installed

Dote of Air Force occcptoncc of pod

N/A

N/A

H/A

15. Total flight hours of p;,rt at lost in.~oclion

14. Totol flight hours of port

Las(· overhaul activity

'N/A

H/A

N/A

.,

Section C-FIRES AND EXPLOSIONS I. Did fire occur?

YES~

Before impocl_

1f yea,

di~ewn

NO_

2. Did uplosion occur?

Alfor impocL.A

Before impact_

in Section F.

YEs.L

NO_

Afterempoci__J

3. Wos aircraft fire detection

system octivofod 7 YES_ NOJl. (II yu, give type ond manufacturer)

If yn. di•cuss in Soclion F.

4. Was aircraft fiud fire c:dinguis.hing system uscd7 (If yes, givo type and manufocluror)

NO __l

Se~tion

YES__

Ef!ectivo_

lncf!ectivr_ __

QuantitY-·---- .. - .

0-POWER PLANT HISTORY

Complete the followins when applicable for c:nginu, afterburners, propellers. turbo-supcrchargus, hcl:eoptcr rotors and/or any other power r.lont componcnh involved. U1c a separate colt~mn for each component. Complete a scporotc column for each engine when specific c"ginc 1) involved, or occident couM factor involving cnsinc (s) is undetermined. Name of component 2. Location (if opplicoble)No, I, 2,

]. Moclel or Port Number

•

4. S~riol rlum~r (if applicable)

1~/A

5. Manulocturor (or licensee)

•

4. Total hours 7. Num.b cr of major owcrhauls I. Hourt since ~ost moior outhoul 9. Dote of lent overhaul

.

--:----:-·-·--------.- ·~; ;-:---- -----:-- ..·-·-·--------·-ll·-·---·-..--·-·---·--~-·- ·---- ·----1 ---·-------·----1

I 2. Ho1.U1 '•t\Cr latt •ndollcd

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·------·--··--------+-·-·------··-·-----+----·--·-----+-------· ---~--------·.. -~

n: Date ofl.,.i pe:iw: ~~~~:"_• .L . :'~J~-------~;-------- J. -·. - -- ·- -·-·-·--·- ·--1-·-..---..--·- ----t---------·--l J.f. T'19C- oflo·d pctiodic in,p.cc:tion

i

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J· · · -------r-----I --------------- ---- -OAT.~<

ON FAILED ENGINES

- - -----····-----·--·--·------- -- ----··-··T- - - - -- -- -fngi"~ fodorl

I

Pr iot fo failu~e of sceond trHJtnt

Prior to fail_, ,, of Ftrst cngtnc

--[·j.~:~~-~-~--~-~~-~~~:·:--~~-~~--r ~:;:: --~ ~~1 '

:.::::·:.s~~:-===~~~ - r~·

---=1-::/A -~ ~~~ua•t:___ ___:___-__j ___ :):. -1

9. Oil tcmperatur<

~

II. Cyli•der head tcmpcrature

l::

12. Fll<l mixturc sctti•g

I

- - -_-----~===-~-

·- -- ·-

"o<,

__

REMA~KS

of ~ird tng i"c

~" lif"' - - - -- _

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--- -· ---- -- --- ------- --- - - - f

p,;0 , to fa ilurt

--- ------------·

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. :_------~---------~~---_-t----- -----·---------~

1;/A

-------+---;-'-:/w;A.___ -+-------+--------+--

u Ul

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13. Fuel pressure 14. Fucl flow 15. Carburetor preheat setting

I

16. Carburetor air h:mpuohuc

-

-+-----l---=---J

1 - - - - - - - - - + - · - -+t - - - + - - - - - l - - - - - - - - - - f 17 . Othcr

19.

R. P. M.

Exhaust gas tcmpe;::::-----1--- J: j

20 • Emergc•cy fuel control •citing

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• •

18 . Percent

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A

I

--- - - r· - - - - - - - - - - - - - - - - l

·1. - •

~----------~------·L--+-----------~---------~-----~ 21. Aftcrburner settings • j

,_./A

0 oc "' ::::> ....

-~M;-

22 . f--A--fter-bur--ncr--cyc-lid--posilio-n

1-2-l_._A_n_ti_-i_c_•_s_ta_t_u_s- - - - - - - --fi 2<4 . Inlet Krccn position

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25. Othcr

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Section F-'AIRCRAFT MAINTENANCE OFFICER'S ANALYSIS Describe difficulii"cs involved and relationship of the various components oboYe to the occident. Include any add itional information or opiniort of possible value to future technical analysis of this report. Continuation on plain paper shcch should be attoc:hed wht"n neeeuory.

IIo f e.i l ed co11:ponent s

1. 2.

No

~ y<:tP.J~S

failure noted

AIRCRAFT

AF

1

:~i'~ 6

14 C

Ptc•iaus cditiont of this form rnoy be used.

M.~<INTENANC~

OFFICER (lignotvreJ

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- L I certify that a eurrey of the d.amage to F-86L, No.. 52' 10lo8~ was accomplished _to 'the most pract~ca.l. eXtent possible Wld. the following estimate inade: · , a.

Airframe:

l~ d~stroyed - no repairs possible.

b. A~P.Q. SysteJM: P_OSSible.

c.

1~ damage - no repairs possible.

Armament and Electronics:'

1~

damage - no repairs

2. Aircraft was completely destroyed by impact and rire. The loss to the United States Air Force for this accident is estimated at $587,493.00.

~~) Major USAF Maintenance Officer

•

•

•

•

•

•

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•

UN C.L/1$:5 1 F 1£1J

·'""'"·.,.&,r

MAINTENANCE OFFICER'S RE

Vic this form in occordonce with AF Re,. 62-14 and AF Manual 62-5, "Aircraft Accident l're'l'tntion-lnvtltigotiC<~-Reporting';

whc" Af Aircraft Acdclcnt/lrKidcnt ln•olvcs lna~cqvocy, Molfuncti011, or Failure of AF Materiel.

1

Section A-GENERAL INFORt-tATIOH 3. Aircraft Nr.

2. Type ond modtl of

I. Date of occident

5 February

4. Place of. occident 5. Sese invu!igoling NM NE ~JlV ani. oc c~~nl , .

5

aircraft involved

0533Qf.

B-47D

Hunt~r-AF!J, Gn.

Ga., 35 H

51-2349

Section I-AIRCRAFT HISTORY, AIRFRAME COMPONENTS AND AIRCRAFT ACCESSORIES DATA Complete the followin9 when matcric:l failure, iMdcq.,ocy or malfunction arc inown or 111\pcctcd cause facton.

I. Dole of Air Force acceptance of oircrolt

). Dote la1t ovtrhaul

2. Total airframe houn

1650:15

28 Jruruar-J 1953 4. Onrhaulin! activity

23 October 1957

5. Aircraft houn tinct anrhoul

6. Do!< o"d ly p< of lo•l

triadic in• p•etion

Lockheed Aircraft Corp

~· ~-~·~ __i_c_t+_~~~-,__Ga_.__________,_____a_a_._o_5______________~____#_B__rrr ______________~ 7. Aircrafl hours at last puiodic in1peclion

8. Name, part number and poaition on aircroll of part cantrib,.;in9 to accident

N/A

1562:10

!I!1AH .i,.•

• 9. It part crtOilablt lor cnalyoit7 NO_A_

N/A

YES_

Ill

yu) Wh•r ..locat•d

~------------------------------r--------------------------------r--------------------------12. Date pari lo1l ov<rhoulcd II. Dale part lad in•lollcd 10. Date of Air Force acceplancc of part

N/A 1•.

ll. Lo,t overhaul activity

N/A

N/A

Total Ri9ht hou" of pari

, •

---

15. Total Righ t hou rs of port ot Iot.t inspection

!-;/A

H/A

•section C-FIRES AND EXPLOSIONS YES..:_

I. Did fire occur? Before impod_

NO.....!

.

2. Did uplo1ion occur?

After impact_

B.lore impact__ , •

YES_

NOJ

• If yn, discuss in•section F. • If yn, di~eun in Section F. •• 4. Was aircraft fixed fire u .tinguishing syshm uscd7 NO....X YES_ . Effective_ Ill

3, Was a ircr aft fire dchc... io n

1y1ltm cct ivoltd 1 • YES_ · NO.L 111 yu~ 9 ive lyps and ma nula cturcr l

Alter impact_

yu, give type and manufacturer)

lncffcct iv~~• ··

Section D-POWER PLANT HISTORY Complete the follow ing when applicable for engines, afterburners, propellers, turbo·supuc:harsc rs, hdtcoptcr roto rs a nd/or an y o th e r po-:cr r,lan_t componcnh involved. Usc a uporotc column it)r each component. Complete o separa te colum, for each t:ns• nc when 1pccific cn;•nc s) tnvolvcd, or occident cau" factor in.,olving cngin~(l) is undetermined. • o

"'

I. Nome of component

•

2. Location I if applicablt) No.I, 2, etc .

..... ... ' 4 - - - - - - - - - - - t - - - - - - - - - - i

Not Il.pplic; lh.~e

•· Serial N•mbcr (if opplicoblcj

----------~---~---·

5. Manufoc.turcr {or liccnJcc)

~-----------------------+-----·-·----~--------------!-------------~---------·-~------- ~ ~---~

..

6. Total ho•ra 7. Number of tnojor O¥crhoul1

a. Hours Iince

lalt Mojor o..-uhawl

'

t . Dote of loot overhaul 10. Ovcrhc.l activity

r------ ---------·--·

N ACCOR D.f.NCE Wr!J"4 ~i1'9 & 5 2 P..F R r3.:.

I). .Dole lo•t innollcd

·--·--·-<··- ·----···"" 1). Cote of Ia• I poriodic ::.pccti: .....

L!!'.

I

/

14

"'-;

··--- --·+-··--·-- -~~----.--------·-·+· ·----------4------·-·----t

I -r--·· -··___________._______'_ ____.,.! ____,.,..--·------+-·--·------·---····-- + -·..·----

·--···-----

0

1-I.-.-T-,-pc-c.l-~lo-,-,-pc--,i-od.-ic-i-n•..pc._ct_io.-n--·~----·- ·- .. - ..--·--+l·-·----·-----·-- · i-~:·--·---------....;. -...::..---·-···-··--- -

·-·--·-·.. --···· ----

1--·--- ·-···-·---------·-..·----·· i·-- ..... _____ , _, .. _______ .-;..._ . -- - -.. ···---.--·-·----··--·· ·-···--- ..,.... ___ ..... --· - - -.. +- - --·---- ·-----· .J s. f..Jc.l { rypc or octof\4: II I 1

··.

~ra-~~

14 C

P,.viout edition• of tl.i1 lor"' may be u.. cl.

.·•

Sectlow I-POWER P'LANT OP'ERAT

·-- ·--·--·----- -·-c-·---c+-·· - - - -----------·--r·-·---------..,-· - - - - - - - - · l ) . !.llitudc fo<luro(s) 2. Timo iofcr•ml bctwoto failuru:

1. Seq••••• of failure(s) by OO«IIe po•i+ioo (l. I, etc. )

I For "'"ltiplo failures)

occu,ccl

::/:.. ·- ------- --··- ----···.

•

•

Engtne fcrd011

DATA ON FAILE:l ENGINES

•

Prior to foilurt

of

~;,.,

•• , ;••

rrior to failure of ICf.Oftd cr~giftt

Prior to fo ilo.,c ol +herd cngi,.c

REMARKS

s. It P. M. 6. Moftifold prcnvrc

•

7. Tor que read ing'

Not

I. Oil prusurr

•

9. Oil tcmpcrot~rc

..,z

I 0. Oil quootity

•

;:::

~

II , Cyliodcr head !cmpcra!urc

...u0""

12 . Fuel mi1turc sdtin!l

""

I J. Fuc I pressure

w

•

14. F.,.l Row 15. Carburetor preheat JCtliog 16. Carburetor air hrnpcrafure

•

17. Other 18. P<rc<ot !l P. M.

19. E1hawd gos temperature

e

1-

w

..""

6 ::>

22. Altcrburnc r cyclid position

1-

23. Anti-icc status 2~ .

Inlet Krccn posit ion

.

•

25. Other

S~etion F-AIRCR~FT

MAINTENANCE OFf·ICER'S ANALYSIS

Describe difficulties involved and relationship of the various componcnh abo¥c to the accident. Include any cdditionol information or opi"ion of po11iblc value to future tcc.hnieal anoly,is of this report. Continwotion on plain paper sheets 1hould be oHaehcd when ncccuory.

.

{\

.

I

&;~1-:;J,Uttle_

DOHAJ...D F. ii.1!EALE, C.AJ'TAn; , FSAF AIRCRAFT MAINTENANCE OFFICER {oisnaturc)

v

•

CERTIFICATE OF DAMAGE l. I certify that a survey :>f the damage to B-47B, No. 51_2349, was accomplished to the most practical extent possible and :the following estimate made:

.

a.

60%

Airframe:

d~~ge

- repairs possible.

b. A.•P .G. Systel!lS: 2C1f:, d.e.In..age - 8r::Jf, of total parts ca."1 be returned to ::>en'i ceable condition after depot and/ or factor~· teardmm and inspection.

c. Antament and Electronics: 1()1;1, damage - 9Cfj, total component parts can be returned to serviceable condition after depot and/or factory tea.rd.c·'\o/'!2 E~.nd inspection. 2. The loss to the United States Air Force for this accident is estimated at $163,486.00. Tr~s figure is based on unit cost as set forth in T.O. 00-25-30 dated 10 September 1957· No estimate of the manhours requu·-~d to ret·.trn those component parts which might be used again to ser-riceable condition can be made because the requirement for teardown and inspection of all parts must be done at depot and/or factory level.

~

()

l...l.

k ·

y~~ • -, s-t·~~SEPH HO-JNACKI

~jor USAF Maintenance Officer

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0

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FORM 781-2 WRITE-UPS AliT) '.::0RR~ITVE ACTION ON AIRCntu"':' 51-2349A FOR T'r..E lAST FIVE (5) FLIGHI'S :NR.

SYSTEM

1

16

10 JANUARY 1958

CORRECTIVE AC..:'IOl"

UHF Radio iLo:perativ'2 20 mi nutes after

G/F

takeoff Xnitter extremely weak after two hours and receiver out. OMNI receiver OK. Received call from Atlanta center on Channel

#9· 2

15

3

7

#4 EGT inoperative at times and reads 2G0° lower );han ot her when operating.

C/ F

Intakes not inspected

C/ F

14 JANUARY 1958

1

17

2

A.";<,C-27 UHF radio very noisy but ranee is good now (static )

C/ F

radar modulator trip o:ut, vould not reset.

C/ F

GlL"lllery

See Fonn 257

3 4

16

5

7

Xmitter (UEF) reported weak in traffic pattern at F.ST . r~ta kes

C/ F

c/F

not inspected.

20 JANUARY 1955 1

15

A/ C' s turn und slip inst. turn needle i:10pera t i ve.

Replaced I r;d .

2

14

Sextant mow1t l ite in repr cockpit vill not wo:::-k

Replaced blub

I

UHF

3

Remove RT-176 (55 -266 ) . Replaced RE- 178

rec eiver inoperative

(8752) ..,.).

15

#l e:ncine Ol l pressure r<:ads 6 lbs at Ll.S'fo at 36, 500 '

2<:1

16

UHF

!~e~r2: i ..;e!·

•.!!:.a:1e_ed. tlu·ee

::£:..s not

Adjusted

JAlfUARY .:. )52. ext. :·e!!'lely ·...reak. t.·l~ mes

;~nd

Ea.s ·ceen

rcc.:eptior~

!;t ill

i!:tiH'C' \' C: 'i .

C/F

2

(' / ~ "I •

.S :;e

.:: ·~-~l

l.r9

::a..!-..d.l ir:.;

i·:Pr~. 1 ~ 2-:. :.;. .

(_) f.j

'L!·t';~ . ;,

eked ;:.:ood, dn;.ineL \.."a ter .:.; ut cf :.ra!l.smi t r.er.

an.d. ~ 2,

•

.,.

e !ffi

.

,...,,,.,~4

V~.:J

. u:.•rt

1 FErlRUA.'W 1958

CO.PJ\ECTIVE ACTION

1 .'

14

Engine starter sel. sv. does not click into position on engine #5 and /#5.

C/F

2

15

Forward main does not pass through intermediate indication when eear lowered.

C/F

3

14

Lite-C.P. Sextant inoperative. NOTE: Insufficient maintenance at staging base to correct gear orrite-up. Write-up was kno·wn to be in ~ safe condition by crew.

C/F

•'

•

2

S~ec~al n~~dl~cg

0

wit!:

A.l1'R 62 -14 .

U fJ C. LA S 5 1 F I E]J

• CERTIFICATE

No red diagonal discrepancies were listed in the DD Form 781-2 for this flight an Aircraft Number 51-2349.

~~r~ OONALD F. lU'reA!E

Ca:pta.:in, USAF

Maintenance Officer

"

.

®

•

. '>..:.

; ~·

,.

~

'. . : .. ,~ .

Section I-PROCEDURES ASSOCIATED WITH LEAVING AIRCRAFT (Check one as " Primary,"

others applicable as "Secondary.")

s

p

Heat

X X

Cold Ccntrifusol force Lack of time Prtuure c:hangn

Hypoxia

X

nt

Vtttigo-or icntotion Decompression Ainichcu Fatigue

"l'ucked __

Feet fint_ __ Ejection sccrt upward..!.....

Ejection seal downward__

Sucked_ out _b_y 1lip 1lreom. Cockpit escape hcrtch_ .

Caplu_l_e..,No1cwhccl welL _

Gunner'• ucope hatch _ _

Other (Describe!-------- - - - --

- -·- -

Chute hornell

None~

Handle pvllcd loou ...__

Rear cockpit _ __

Risht 1ccrt_

loo~eor

Bottom ucope hatch. __

Left seaL--

twilled__

btendins les'--

Aft bomb bay_

Blown out by uplo1ion_

- - -·- · - - - -- -- - - - ··--- ··------- --

E..tendins amu~.-

TO STRAIGHTEN BODY BEFORE PULLING RIPCORD

fF.;;.;,...-_.c___ __

IN FINDING OR PULLING RIPCORD

Front Cockpit_ _

Woill or main "l"ope hertel.__ _F orwordor main_b<>mb bay____

--------

Rolled on bacL_

Injured or wounded _

Glowu worn__

I to s___

II to 25 .. ....

Other (Explain) _ __ _

Al BETWEEN LEAVING PLANE AND PULLING RIPCORD (in second•)

• Fed down_~

6to 10 ......

Abowe 60. -··· On bock _ __

down __

26 to 60~- -

Unknown . __ _

On face __ _ _

Tumbl ins-

Severe X

Modercrt•-···

Slipp<ns chute_ _ Turnins body to loc;e drift ..... . OiuiftcU.--~--

N®'-C4 ..

-p

u.,on~oeiowlftUI. ___

HypoliG.- ·· -

Fro1tbitc.. -~ - e

Oth&r (Ducribc in Sec. H) _-- ----- - - ··-·-- ·-··--·-· ·- ·····----- ·-···· ·· ----· ·--·-····--· 12. ATIITUDE AT LANG•:..<G •

Sidcwo~ lA":fOIHG EQVIYAlfi'iT TO

Verticol...! _

· IQ-.15 ft. free falL!..

Rolled forward _

_

dout• -~---- . .ft•

1._20 ft . free foiL _ __

Rollcd bockwordJ: . .

Fell fCNword. _

t.t...,l.d by chute.. . _

A"-c 20 ft . free fai L __ :

fell backward ...._

O!hcr (Duc;ibcl.- --- ·--'-

hllto left_.

.........

e

~ection

1-PitCX:EDUAES (Continued)

:-;l;,_

IS. OIFF!<:UU 'f IN COU.APSE OF CMIOPY AND ULU•SE OF HARNE:.S IN '.VATER : eu~ •lu

'"004 hard to r..-lca\t

(,1

J<Jm~'"9

f?duff! ol ~u•d r-: 1 ,~~

0'

Ca~"~ory collop,r.d .... . th

14.

FUNCTIO~HNG

'lltnd ).indt:rt~

•

ll!ffor•t

lnJU''t or u~"~ct:~,tcl.,..,.u, -d,.l~·1 •d ,_Uor•,

""''cf-lon ·vn t£,.plou, '" Srr.. H)

No'"!

r.J,f.l" ~, 1 1ty

•Jih~r

{ i.>f!sertb .. J

OF CHUTE

Section C-ltESULTS TO PARACHUTIST

INJURIES

I. FRACTURES

Crontol

Vertebra

••

Clov•cl~

1---------- ---- -

r--· R;b'----·-- ---- ____ ----~ ---

- ---+ - -- - ~

~~-'-w_r;_ sl_____ __ _ __

_

.

-~nki<~_!___!!_L ___

I

_Oth<o - -- - · --- - - ---· -· ___

t··-

I

!

!

···-- - - ·· ...

I

.+---- i -- --+---+----I ----A~~-~~~-~_!_£~~·-~~-~~-----I

1---+---- - ~- __ J j__ j_ ____

I !I

_Locroat;a~"· mai•>~

__ :._-~~:~bplao~-·~ S<o"-~~-l

j ____

_l __

!

1

--1

_._jL...,_..l, _ _

.__i

... If above informot•on not available , uplotn '"Section H

t-- - - - -------- -----· - -------

-

S. V:::::::.::ie:.:sr.ess

Yu

- . -- . - -~ Stn•r number of doys hospitolned -- -- ----- __ __ ! ____________ ________________________--!

... · ---------- -

NoX

-------------·-·----- -Etplo in couu- of '"Jury"' full dttoil ,

Uilng

u"!:lltd spocc under Section H , or additional shu:h as ncc:c:ssary

Section D-AERIAL CONDITIONS

- - - - - - - -----

---------

---------- --------.- -- - -

1 ATTITUDE OF AIRCRAFT AT TIME OF BAILOUT

L<v<l

lnvut<d

Dov< Left spiral

0 - ~ .. ~~!LOUT, 35 ~DgO

2 APPROXIMATE HEIGHT ABOVE IN FEET AT TIME OF JUMP

~U R~AC~S OF AIRCRAFT AT TJME .O~- - IN KNOT$

•

9

, , r.ol Ct1

..

Right bani__

L.lt bani Right spiral. __

Unknown_ ~ -

·4. APPRC'<'I.IATE FP.EE AIR C:"'TEMPERATURE: - --:"'

1

... . • Fahrenheit

Section £-SURFACE CONDITIONS AT POINT OF LANDING I. LAND

Type: of h:'r~in:

Flat X

Mounta in ous

Ground conditions;

Salt

Oitchei or gulli•H

Ground obstructions:

Trees _ _

-------2.

k< _

Hilly ___

~i;pp<ry

Stone~,

Power linu

bouldceu .

Desert

Hard .~

Swamp ____ Rody ___

Bushu___ _

Build;ngt ____

HEIGHT AT WHICI-' PARACHUTIST FIRST DE i ERMINED ACTUAL LANDING SITE: (Fed) ..

Oth<r ( Duoribc ) ....

Othu (Duoribe) ________

Non<~-

.

Oth<r (Duoo;~<)

\drJ:!]0_k1L.

~-----------------------~-------------------------------------------------4 3. WATER CONDITIONS !!/A Fouh.

Salt .

Approximal< d<pth (lui)

Calm ___ __

Appoa•imatc t<mpuatur< (° F.)

Wavu (H<;ght , Fed) ___ _______ ____ .. .. -----·- · --------- - --

-;-rnomy-o~-z;-;;~{;~~-;-S).-:-fr:-:-~~------~~FACE

Choppy __

AIR TEMPERATURE ( • F.) __ _ __?.Q_____

_

Section F-EQUIPMENT

- --~: ·:~~:'-t.-'--- ---------~-4_1_1._._--_--_ _21 b. Automuttc opcni"9 device:

lt ...x_ ____S_ea_t_t-'-y'-p-•____Ba_o_l_t-'-yp'-•-J._._-_ _o_t_h_,_,..:.(_D_.._.,_,;_b_<;_)_-_-_._-_ __C::·9:_-----

Available : YuX._

-------------------·---------- . c. Type har"n"

---- ----

a.;d <<lea••'-' ..

•. Pool N"n:bor (F1om

Losl ---~. ?.1?..~~- -

No .......

Snap and V rins .. __

---- __ .

No.X.

U.. d: Yu .... No ......

.. .. .

Page

2

/

Section F-EQUIPMEHT (Continued l . ,,ROTtCTIVE HELMET Avoiloblr: Yu~- No .. . .. Used : Yes .. .:~. Typo: (c. 5·· Pl. PIA. 1''. etc.] _ .__ _ Visor ottocl.ccl:

Yu~

No.......

Yu . ~ No .. .. .. When loll between ejecti on !ft. l a:1din1

loll:

_E:_~- ---- --.... . .... ........ .

No .-..

Visor up_X__

-(thlnksTf-~i~s--81'\:cr .. r.hut~

Visor down ___.

Wos helmet Riled by quoli~ecl pcriOnncl (Eaploin in Scclion H]:

Oxygen mosk fadcncd : Yes .. ~

Yu~

Oc' E'!:td)

No.. ...

No .. _

- - -- ·· · ···--- ..- - -.··· ·-·----..... . ...- - - ----·-------- - - - -- - --=::--;;--,1 3. EMERGENCY BAILOUT Oay!en available : Yetle_

No _ .. _

Used : Yes......

No_~-

No ..JC..

Foiled: y.,_

Recharged (Dot e )._2_0

.J ~~-- 5

4. PINGHY Available: Yu.~.. No ...... Used : Yu ... ~ No ... .. Failed: Yu.. No . Type . .......... .... 9..:.?.A -· r-------------------------------------------·~-----------------------

5. ANTI-EXPOSURE SUIT A•oiloble : Yu .... .

No~

b. MAE WEST A•oiloble : Yu X.

Used : Yu .._ _

No ....

Used · Ye._ __ No..... No. .Z.

At who! point inflotedL .......... - ......... 7. SURVIVAL KITS Available : YuX.. 3. FOOTGEAR

No___

Uud : Yu . ..X

No ....

Adequate (E.ploin in Section H) : Yu . X

No____

Shou ....... Boots. ~

Type _ _____ - - ·----- - -·--- .. . __ _

No .... .

Oil!iculty in inflating : Yu.

Nc ....

low quarter oalords__

Failed: Yes._ ...

Foiled : Yes .. _

Flying boots .. ..

No _ ._

Type .. . . 1r;::;.~L ..

-

Other (Describe) . .. .. .. .. .. ......... - ............. ........ ·- ......._

9. OTHER list ih:ms

of

Hunting knife anci fl ash li t;ht.

sptc:iol or ptnoftol cquipmutt used.

l11t oil rtems lud during borlout. 10. WERE UR's SUBMITTE07

l'u

Hunting 'knife and flash li F,ht.

No .:l!;..

II " l'es, " Iill items.. ·- ··- ... ·-

Section G-TRAINIHG AND I. W ..t..S CHUTE HARNESS FITTED !l' OU .4.li<IEO PARACHUTE PERSONNEL7

------ -

- - --

1. WAS THE FIT OF THE HARNESS SATISFACTORY FC'R THIS 8AILOUT1

~REPARATION (If not, e•plorn in Sect ion H)

(II not, uplo;n in Section H)

Ground Troining ( Horne11 rigs, tumbling , etc.) :x:_

3. PltE\' IOUS PARACHUTE TRAINING: lcetvr<s X ous e;ecnoN SEAT TRAINU;G: lcc ~t.I ICS X

Practic e CJCd ions X

_.

Y<sX.. Yes X

No .

No

Number of p re vious

None

Numbll! r of prcv iou\ e ject io ns

Section H-ADDITIONAL COMMENTS, CRITICISMS' AND _____ _ _.. ____ ..._.._____ ____ .. .......... .... ....... ...-------· _ ___ ___

-

--

__ _ - -- - · - .. - --

0

None

X

RECOMMENDATION S .. .. .. . .

nforrr 1t1on " duircd rcgord•ng the ncccu •t y fo , such cqu•pmcnt os flas~llghh, stgnol muron, Very p•stol , ~and fiar n , knt fc , Side ar ms, or thcr •tcmt. Add any recommendations you may hove for training and cqu•pmcnt. specifically in regard to h:chniquc • of ba ilo ut from h igh peed cJ itcroft . Valid cr itic ism on u isting equ ipment is invited .

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.. SPECIAL NUl·!BER

HF.A.IQUARTERS 38TH Am DIVISION (MC) United States Air Force Hunter Air Force Base_. Ga.

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. Verbal Order Commander 5 Feb 58,

12 February 10"

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3. is confiiT.Jed, Follt"1Wing named Officer Organizat ions i ndicated, SAC, Ar~, are appointed membe~s of the 2nd Bomb Wing Aircraft Accident Investigating Board meeting at th' call of the ?resident to investigate all Accidents or incidents resulting ir: t>Jajo~ damr.ge to aircraft and such accident/incidents which are determined by the Co!~ander to require investigating b:,.· a B0<1rd of Off ice~s, o..~d occur on vr in the vicinity of Hunter AFB, Ga. I!l the event of the 1-'resir:l.ent or Recorder are absent, the Senior member present will act ns ?resident. ~;d the '-TU.1iior rrember \·:ill act as Rccurder. A Quol·wn will consiGt of four (4) members including at least one (1) Director of Safety, One (1) hlot One (l) Engr Officer and One (1) Flight Surgeon., Exigencies of the Service ?reclude the isstta.'1ce of orders in advance. Authority. AFR 62 -14, SAC Sup 1 to A"R .. 62 -14 and /•.FR 11-1 J.nd Verbal r1rder Conuna.'lder Hq_ 35th 1\ir Di vision. Any ex::.sting order in conflict with this 0rder a.re hereby rescinded. COL · :-: ·L ~./:"'SC· L

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OPERATIONS Clearance and Reservice of Interceptor Aircraft on Active Air Defense and Scramble and Recovery Training Missions 1~ c~•trol

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To outline procedures for expediting air traffic operational agreements for fighter-interceptor aircraft participating in active air defense missions. In addition, it prescribes development and coordination of operational agreement" to extend the range b.Y reservicing fighter-interceptor aircraft at appropriate pservicing or recovery bassse This regulation appllea t' recovery bases located within the continental limits of the United States.

clearance,

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2. ~. It is not the intent of this regulation to establisl: a requirement for complete turn-around facilities at every alternate

recovery base. Operational agreomants should be effected to provide reservice or complete turn-around for fiehter-interceptor aircraft wW are within the normal capabilities of the recovery base concerned. & ever, this does not preclude pre-positioning certain items deemad appz priate to facilitate reservlcing at recovery bases. Such items will 1 supplied from currvnt assets and authorizations of the comcand Jirectj the recovery and reservicing operation. War Reserve Material aasets • not be moved trom authorized base locations unless approved ~ this h( quarters.

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Waiver *of Reguirementa.*

a. The pil&t of an interceptor aircraft is not required to J a flight clearance, DD Form 175, when scrombled from an airfield havit Air Force or Naval activity, provided: (1)

The interceptor(s) aircraft is scrambled on an actb defense mission, or

(2)

A eei'amble and recovery training miaaion; and

(a), Interceptor{s) aircraft reme.ina under control c ADC Ali80ol system, and

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Except for emergencies, recovery 1B to 'b!i accOJ ni~ht origin or at a reeov "q 1 where an operat1oncl agree:nent is in effuct, a1

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OPERATIONS Clearance and Reservica of Interceptor Aircraft on Active Air Defense and Scramble and Recovery Tre.ining Missions lc Pl1,.nn,..,. To oYtlin~ procedures for expedi Ung air trafi'ic ccn.troi cleo.rancs·,. by operational !!gree!!!:!?nts ·r or !"ighter-int9roeptor aircraft participating in active air defense missions. In addition,

it prescribes development and coordination of operational agreementa to eA~end the range by reservicing fighter-interc~ptor aircraft at appropriata FSServicing or recovery basGs~ This regulation applies to recovery bases located within the continental limits of the United States a 2. ~. It is not the intent of this regulation to establish a requirement for complete turn-arour..d facilities at every alternate

recovery base. Operational agreements should be effected to provide reaervice or complete turn-around for fighter-interceptor aircraft which are within the normal capabilities of the recovery base concerned. However, this does not preclude pre-positionlng certain items deemad appropriate to facilitate reservlcing at recovery bases. Such items will be supplied from current assets ~nd author1~.ations of the co~~nd directing the recovery and reservicing operationo Har Reserve Material assets will not be moved from authorized base locations unless approved by this headquarters.

*

-----·-·

4.

Waiver *pf Regyirernentg.*

*

a. The pilot of an interceptor aircraft is not required to file a !'light clearance, DD Form 175, when scrambled from an airfield haviog an Air Force or Naval activity, provided:

(1) The interceptor(s) aircraft is scrambled on an active air defense mission, or (2)

A scramble and recovery training mission; and

(a). Interceptor(a) aircraft remains under control of the ADC AG&W system, and (b)

All interceptor aircraft involv~d have operational communications and oavigational.equipment; and

(c)

Pilot makes necesa~ contact with the control tower prior to take-off and landing, and

(d)

Except for emergencies, rocover.y io to ba accomplished at the base of flight oricin or at a recovery base • 'Where an operat1oncJ. agreo:nent is in effoct, an1

•

* FOR THF; COHM/\NOF..R:

s/t JOHN H. KONOSKY

DISTRIBUT IONi A

Colonel, USAF

Director of Operations

(ADC-6841-7}

2

THIS IS A CERTIFIED TRUE EXTRACT COPY:

<!If.~ Captain, USAF A01909520 Ass 1 t Operations Officer

SPECIAL HA

G REQUIRED

IN ACCORDANCE WI

R 49 & 52 AFR 62- 14

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l?[':·;:?_'i.rhe following

1. · · r:r.;;~-538-R~placement ' !

.

2• 3. 4. 5. 6. 7-

8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21 • 22. 23. 24. 25. 26. 27.

or west1ilglouse Generator. . IF-86-534-Replacement of L/gear control switch. IF-86-549-Inst ~ manual overide sw. nadar recorder. I1'-86-:<549Ai. " II . " " " " IF..:86-55l-Change to single safety pin in ejection sys. IF-86-552-Inst. of temp recordi ng equipment. IF-86-559-Inst. of M&5-MA6 lap be.lts. IF-86-560-Inst. of MD-10 t~y slip indicator. IF-86-561-Inst. of alternator and gen. cooling air screens. IF-89-562 (not listed in index) new T.O. coming out. IF-86-567-Replacemen~s · of relays. IF-86-569-Replacement of tail light spacers and lamps. IF-86-575-Insp. and mod. teleflex gear box. IF-86D-538A-Ins+.. of standard receptacle standard inverter. IF-86L-5o6-Insp. for and if necessary of inst. auto pilot master sw. IF-86L-507-Inst. of guard over throttle telese:·opic rod. IF-86L-517-Bework o! ID-250 indicator sys. IF-86L-521-Revision of AIC-10 interphone ¥ad. IF-86L-524-El.imination radio noise pick-up. 5A9-2-3-501-Mod. of AIO flt controller. . a>6:.5-9-501-Replacement of brushcover band on jack and heintz inverter. llP3-2-2-501-Inst. of M-71-one sec. delay cart. in M4 initiators. 2J-J47-54l-Replacement fuel nozzle assy. 2J-J47-268-Replacement reheat control valve. 2J-J47-505-Rework of annular transition liner outer band. 2J-J47-527-Inst. of starter-gen. lead cover. IF-86-558-Replacement of vickers hyd. pump.

The reasons for non-compliance are as follovs:

1.

PE. insp. or eng. removal.

2.

No kit auto dist.

3· Kits not on hand. 4. Kits not on hand. 5. 6. 7.

8.

9.

10. 11.

12.

13. 14. 15. 16. 17.

18. lY.

No kit auto dist. Kits on order. Complete kit not on hand. Complete kit not on hand. Held in abeyance. (Info by TWX) Kits-oo b-and .PE.- .. insp. Lamps oo order. Nex~ PE. insp. Kits on order - next PE. Kit on hand 1 PE. insp. Held in abeyance f'arts on ~ P.!. !oap . Parts oo order. Parts oo order.

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21.

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24.

On order.· .• . As schedUled. oy WRAMA.. · Parts on order. . . . ' No

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25. Kits held in abe~ance. 26. Kits on order. 27. Pumps on hand PE. insp.

£'??'~)

RO~ W. CAMBLIN Major, USAF

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,Tb,e :rollov1Jlg T.o;i,j have not been ~ ~~ Yith on B-47B ~-

~l-2349~

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·1'he fcillov1Jlg T.O~'s ~complied rlth on Engin~s l, 2 1

· T.o. 2J-J47-522

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MOdification of Fuel Pressure Control Valves

T.O •. 2J-J47-546

T.O.

'

Modification of Main Fuel Regulator Oil Inl.et and Outlet

l.B-47-905

Revision of Door Latch and Electrica.l Wiring MUll I..s.nding Gear Door

T.O. J.B-47-914

Installation of

Stowage Provisions for T-19B or

T-249 T~o.

11Bl2-3-3-5o8

Replacement of Hand Crank Assy

T.O. 11Bl2-6-l-501

Variation Changes Modification, Polar Nav Controls

T.O. llB12-7-2-509

Installation of Memory Point SVitch Stop

T.O. llB21-2-9-507

Modification to Prevent Burning of Cathode Ray Tube Screen

T.O. 11B21-2-9-509

Installation of Dust Cover for Periscope Assy Indicator Azimuth and Range

T.O. 12R2-2ARC27-502 Replacement of Vibration Isolators on M:>untillg T.o. 13Al-2-513 T.O.

Modification of Shoulder Harness Loop Ends

lB-47-752

Installation of Wave Guide to Coaxia.l Adapter

T.O. 1B-47-8o4

Inspection of U2 Rack l£1ck Assy

T.O. lB-47-890

Installation of Separate FCS External Power Prcwisions

T.O. lB-47E-536

Aa.c'IItliii Pump Circuit Breaker Replacellimt

T.O. 11P3-3-2-5o6

Installation of

!'.0.

11P3-2-2-501

T.O. l.B-47-1001

M-73 Cartridge in M-3 In1 tiatore

Inste.lla.tion of M-71 One Second Delay Csr-..ridge in

-M-4 Initiators Empennage Anti-Icing Sensing Line Revision

The reasons .for non-ecmpllance are as follovs: 'l'.O.

2J-J47-522

Depot

Level Ma.intenence

Req-~-dance

Special Handling vitl:. Pr.ra,c;tr.apha 49

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On Or<ler

T.o. 13AJ.-2-513

On Order

T.O. l.B-47-752

:Hot Applicable to B-47 #51-2349

T.O. l.B-47-8o4

Not Applicable to B-47 #51-2349

T.o. l.B-47-890

Te~ic~l

T.o. l.B-47E-536 .

Depot

T.O. llP3-3-2-5o6

Aircraft Not Available When Scheduled -

On

T.O. llP3-2-2-501

Aircraft Not Available When Scheduled -

On Refl~

T.O. l.B-47-1001

On Order

Order Not Received

Level Complianae

Lu~~ OONALD F. KNEALE Captain,

USAF

Maintenance Officer

Reflex

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Oebrge ll~C:o~,, issi~tailt~ Cl!ii,ma ofric~r, 'Runt~ .

. :.Air. Fore~ Base, Georgia iditij. on 8 · Febrilary, 1958 1 :<ins~ct the area. ;

·.: . ,.:.'of: the crastLof

en F-86 ijet 'rfSbte:i from 'chltrJ..~ston Air 'Force Ease·~ .

_,:::.; gC}ut;~ : cafoiiDa; whlch ~ad'

oqc::uTred Con ·5 ::e~rU8.~·y> l958.

The :results ·.

were: . 1. Hora~e Waters cf Sylvania, Georgia vas interviewed con.. cerning. a small portion of the -F-86 which· fell uwn his property~ i He· vas satisfied th!i.t no d.anis.ge had resulted directly or iildirectly and · he did sign a "'B.iver: of possible claims against the government •.

2. Mr. Bruce Hurst, Rt 3, Pox 65, Sylvania, Georgia was i.riterviewed concerning the major portion of 'the F-86 which crashed ilito his property. Inspection revealed that the plane had landed into and. destroyed soine of' a corn field:, and that a. few trees had been scorched by the heat of the crash • . Also. as result of heavy machinery being moved upon n portion of the fiel~, the. ground was greatly compacted 1.ri a.rea.s of norma!. cc"l:'n :pl&nt.i.ng. This heavy machinery also broke the main post to the gate of the entrance of Mr. Hurst's property. The extent of damage cannot be accurately determined until planting is att~mpted, but it should not exceed one hundred dollars ($100.00).

a

3. Mr. Bod-...•ell of Gair Woodlands Corp., Savannah Bank Bldg., Savannah, Georgia was in~erviewed concerning a portion of the F-86 which landed on property of the (:Orpcration. He stated that a fiel,d report indicated that no damage had resulted from the crash, and that Mr. Earl, the president 1 w.:;.uld. sign a .,.'B.iVf:r of pose.ible claimD against the government as scon as he returnei from his current illness.

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· : · ' te '; 38• (B . 47)' d

!f Fe~ 1958 . . OnlY·:·tbe.t .

P,ug.·.GOld··

f·<L86L) : . .

tranacribed~

, . Pug. Gold'. 's_:·trari'mellicms

· ·;·:· ~~m;· ~~~~r::to>~r.~:r~;::~~~-·;~~~~:~e~)_.·, .collision -has .. b~n

. C:'&t~ :'by a

·v111 be

indi-

"a" ancfri.igb.t:. p<>8:ttiOZ1 i nUinbei'~ : ~i' a transmissions ·e.:r-e·· .

· indicat-.d b:r: e.n "R" ••

•. ·L ·

Gl. -

Hemin~y

H

-

Roger, Gold Flight, read

Gl

-

Roger, five by1 a.:Uborn~, vectorinS 270, cl:lmbing buster to 20, squawking three .nonDe.l.. · · · ·

Control, Pug Gold.

you

five by.

Hcnr ~?.

Roger, let's ccintinue your climb and · go to button 8. return this channel.

H

G:.

-

Ro~:r, Gold Flight 1 button

G2

-

Gold Tvo.

G3

I! no contact,

8 - ( tvelve second pause).

Gold Three,

Gl

-

Hemingway, Pug Gold, butt-on eight.

H

-

Reger, Gold, read

Gl

-

Roger, five by.

II

-

Roger, Gold Flight. tive?

Gl

-

That's affirmative.

H

-

'IYo 1

G2

-

Tally-ho.

H

-

Three, you tied-on to tvo7

G3

-

Tally-h..>.

H

-

Roger, let 'a go up to 30,000 feet. fift~en, gat~ the rest of the way.

Gl

-

Roger, going bl.lSter t.o !1ft~en and gate to twenty--, gate to thirty-- (twelve eecond pau.ae), Go.~d

H

YQU

five by.

Understand

Hov me?

a~wking

three normal.

Affirma-

you tied-on to one 7

Fl.ight,

~et'

e go gate up to thirty thousand.

Gl

-

Roger, you want ua to go nowt

H

-

Roger.

Special Handling <=--o.u.o.,., v1 th pare.graphe 49~--....-

Let 'e climb buster to about

ji

~

.:. ·

, .. .

·'-'

i. '

:·:

..

:,

''G2 .

. ··~

~

Rc'~r/· Tiro'• bc»:hUng·on~·. :·)':.

.;

\•,

:.~.

·;

How 's it coming tbreet

j

G3

Roger -:- (nineteen secem.:l paua~).

G2

Tvo going gata - (!:ixty e~acoald pause).

E:

1:...-o, yvu. tied on to one nov?

H

Roger.

G3

·I 'hree has tally-ho.

H

Roger.

Gl

One pass ing angels e leven.

H

Roger .

Gl

What's cur range to target nov?

H

Roger . The target i s being cross told to us from Bas ~:etwool present time . He's about a hundred and five miles out from Charleston.

Gl

Roger .

H

Gold Flight,

Gl

Rogsr Gol·i Flight._, :in·-t:rail etarboard to three eix zero.

G2

Roger Two .

G3

Three,

H

Gold Flight, at present time he seems to be tracking about one eighty to one nine.ty heading.

Gl

Gol d, Roger.

H

We have him at tirlrty-one point four angels. He's probably up about thi rty-four. Suggest you go up to about thirty-five angela pre s ent time.

Gl

Reger, Gold w1ll c l :1.mb to tb1rty-t'ive angela - (t'ive second pause).

H

What angel e now one?

Gl

GoB. one ang-el!! seventeen.

H

Roge r.

Three an b!o ?

V.'hat

altitude one?

l~t's

t urn in-t=ail starboard to three six zero.

2 Syec1l:ll F.andling P.e vi tb pal'tt.(T,r l!l.pb.s 49

-:,, ,._

...

··,_ (··, . . .

pl~. : I'~~t~ing ra~.- ~ai ·~ktn . . ..-..

. . ·. .~ . . "l

:. .

'.

-~

.: .

.!. ·• ..

Gi. i:·"·::'...t:· · -:

:-: .~·

:.- - - _,;~

-~·

, i .!l···

'' G2 ··

. .

·,

. R~

G3 !".

; ·-- ·: -::-. -

'•;_.">.

;;. G:f .- , ~

.

.•

~:-

Three -

. .•·

,.

,:

(~tt-1'1ve se~ond pauae) • .•.

steady~ .

-~~-

.

·.

.

' ... '· ' ·. -·

.~

·.

'--,_ ' - .

:··- .

<J

~ .; ':·-

R

Roger two - (thirteen &~cond i)e.\lae ).. . ,

G3

Three steady.

..

.

H

..

-

.

·:

Roger three · ~ · (five se~ond pause) . - . What . angels now, one?

Gl

Gold one passing angels twenty-three •

H

Roger - (e:E";V'€Ilt-een s~cond pause) - One you continue yo\U" turn to two seven zero.

Gl

Roger, two seven zero for one.

H

That's for one only. Roger, let's make that two seven zero tor all of Gold Flight, and two and three you can displace yourselves

..

That in-trail?

cf'f to the le:rt. Gl

Roger, wderstand you w.nt that to be an in-P-ace turn.

H

R!)ger, let's mtike it in-:place now to tvo seven.

G2

'I'Yo tu.rning nov., th:r-ee.

G3

Roger - (twenty-one e~ccnd pause).

Gl

Gold one steady two seven zero.

G2

Two steady.

H

Roger one, you shauld have hill about thirty-five degrees starboard now at th1rty-f1V1!: milea.

Gl

Gold one, Roger.

H

-

What angels now, ooe?

Gl

Gold one, angels three

G2

Tiro backing of:r.

G3

Rog.

H

One contiiiUe yo..rr: turn to about two six zero. •

ze~o.

3 .~q_ui:n:rd

and

52, U

in Ac~ordance P~ 62-14. tJCL-A~SJF 1€1)

..

~

,. .

':.' ··.· , \ '

-One Roge ·· ,

Gl ·

tvo , eix zero • .

.•. g .-· · ' 1,

.·• · · ·

. G3

i.

Rog •

. ; af· .· .· .:·..~ - ~ .

~

Gold one ste8.dy bogies iR lit? ner~,

track.

tY.J

si:t

zero.

.. ., ,

liav

Winy

fighters . - uh - bow .mny

..

. . {thl:;Je secan<i ·pa\lsej Should ~. -~- {garbled). ' .. ·

r· ... ;., Olll.y ·s-at· -

tvo

bogies · 1n the

·.. ··· Gl

-

Roger, they fiying elose formation?

H;

-

Roger, l' m onl.y :painting, cme and be's comilig in rs.the I' ~,. ~ ?.l.g:;;:cnow. Gold Flight let's all turn port to two six zero.

G2

Roger two.

G3

And three.

H

Gold Flight make that all port to tYO fhre ~ere.

Gl

noger, Gold .tr.Light in :place tvo 1'1ve zero.

G2

-

Roger tvo.

G3

Three.

Gl

One steady tvo five zero.

H

Roger, \i"hen steady t-..-o 'five zaro, one, you'll have b.i:m about forty degrees starboaz~ at twenty-five miles.

Gl

One Roger, no joy - (five second pause) - One has a :paint, a paint about tventy-five degr~~s port at twenty-five.

H

Roger, it' a him ~ (three second pause) - Say age.in, port?

Gl

-

Affirmati~.

H

-

Roge:~; you should be heading two :five zero.

Gl

-

Roger I'm steady tv.o fiwe zero.

Affirmative?

H

Roger, you should have him about :forty degrees, make it 1'1t'ty degrees to your ste.rboa.rd about twenty-one miles.

Gl

Roger, no joy.

G3

Angel.s one?

Gl

•

Roge::-·, one level angels, level three f1 ve.

H

Say again, please .

Gl

One 1e level angE:l£ three fl ve.

4 Special

HaJldl~quired ani

vi th par~_ra~ha

) ~,

in Ac c ordance AFR 62-14.

I.J /1)

CL-f) ~5 IF I f?b

·.Y"'~~*~~.~,~\;l''~if~n,~·nt'l.:.:r: ...,, ·, , ·'' ·

~(~·~ }. · ·::·!._ .[{"';-~--~--?.,

, ("

::::~..-; yvu ano-..u.a have ~ -.bo)lt !if'ty .~egre:ee , . · . . · · ·· .. ·· ~-- . ·:.: ,· . .-·

niilet~. ' -. ~:-;·• ·,.,: _; :.: ·,. . .. ~ :-. .: _ ·:·· ~•

, o .••'

. ··r :Gl · . ~ . _. Thli.t ., s ,' &tt~ru.t~;ve. ·,y.::y;t,4·-·? ·_ ~t ~.~:~een. i• -·.; : .

>

,·: -

·, .-,,/: .. :· :

'...·c.~~ 'h

o

I"' ,

· ~t~s h1.m -

o

,• ' '

,: · •

..

~oW:: at • .<. ..

;i

''• ·•..~: ··,·, •', '

!

0

_:-- .

; _ •••.. ·

•,

:,

.< :·\:

;;/~~.{·.::: · :~· ' ••

' ... . ~

(seven. seeon~(pe.uee) .:. TwO ~ :sboul~ ba"le-hill !arty

de~es'· starboard at aboU-t · e'ighteezi. ::' '· ·, ,,. · ·

~0~~

·.

I haV&. a . eontacir &bOut ·.torty : degre~·~.~

,

no joy·.

·' .

' ·

·;

·

· ·

. :.. :

.. . : -~-:. . -: .

~~

·ab,o ut tventt-five miles !c;tr

Roger

three~

~· thirty~:t'ive

degrees

·etarbo&z~tl. ·

.·.

no : Joy• .

.

'

Twc, YoU'~ . about seventeen Su~ out.

starboard.

Gl

erie has a "judy".;

H.

Roger 1 "judy'' far one •

. Gl

'· : ·

iltai7boar.4

Look about .thirty degrees

I have a fly down indication.

H

Say again.

Gl

Disregard.

1I ·

Tlio 1 you have a contact yet?

G2

Negative.

H

Understand "judy" f-::Jr t>ro?

G2

Negative t-..-o.

H

Roger.

G2

I am, two.

G3

Three ai':firm.

H

Roger. You should have him about fifty degrees starboard at abot:.": fifteen miles - (th-~e second pause) - Two, any luck?

G2

Two, roger contact.

H

Roger, contact. sixteen.

G3

Three turning in (gcbled.

H

One, you still llave your judy?

Gl

One Roger - ( t:n second pause).

H

Three, you eho·v ld be about fifty degrees starboard now at seventeen.

G3

Three 1 Roger, h!l8 a contact.

No ccnta.ct, no joy.

You heading tv.o five zero two and three?

Three you got him about fit'ty degrees starboard at Perhaps incorrect).

5

R~ · in Ae:co:rdance • 52 AFF. 62-14.

Special HandlirJg vi th paragraphs 49

1

AJC..LA SS1 F lf?D

·.a .·· ' ~

1{ :

-

. .Ro~r,

y

re-!

has a contact.

: ~~· ~ :. Two. c~~rting ' .H·:

. nay

.· 02 ·' .,;_ , •. '1'vCl

port.

again •

~anvertms port.

Roger - (nine •second pa~e ).

Three lost contact. Roger th..'"'ee, J-'CU should be s.bo-.rt thi...........een m:Ues out about forty degrees starboard now. G3

Roger, tb...."""ee ba.6 a "Judy''.

H

Roger 1 three ha5 "judy'' - (seventeen second pause) • have a "judy" 7

G2

TW'o affirm.

H

Roger, may be, Geld Flight. We'~ not gettir.g a very good paint on him. He looks like he's turning probably to the sol..r."tlr,.-est a lit t le, to the starboard.

G3

Roger, three.

G3

Two, do you have tally-ho three, nine o'clock position?

G2

Roger, gotcha boy - (sevenken second delay).

Gl

One ' s in a tail chase.

R

Roger, one,

G2

Same-o for tvo.

G3

Same-o

Gl

Gold one will make en ID,

H

Roger.

Gl

One has ten seconds to go.

H

Roger, one.

Gl

He is about a.ogeJ.I;

H

Roger, tmdt:!rstani thirty-five point :f'ive.

Gl

One "splash" .

H

Roger~

fo~ th-~e.

lflt 's

b~ak

thirty~fi ve

sta.r·boa.:'j 7.ero nine zero.

6 Special Randling vi th paragraphs 49

point five.

'lW 1 do you

..

, ;

Gl G2

Roger starboard zero n irie zero. -

Which vay you ·breaking!

Roger, starboard 090.

Gl

G2

.·.·::

G3

-

Three's turning in.

G2

-

Ro~r boy. brea.k-o!f.

G3

-

Negati~,

G2

-

Rog.

H

If' you l ook like. you got a real good one Jim, I'll

it' s a tail chase.

(Hemingway monitor came on the air) Hemingway testing - 1, 2,

3, 4,

5, 5, 4 - (six s e cond pause). G2

-

I knov it.

G3

H

'Ynis guy's ree.lly going.

-

G2

Gol1 tvo, you still

c hasL~?

'I\ro, I'm still after· h:illl.

H

-

Ro g ~

G2

-

Two's about tventy 8econds • .

H

-

Roger tvo.

"Click" (This click -.res !"co:r:led 34 seconds after Gold Two's tre.nsmission of "tvent y seconds" • ) G3

-

TW'o ::io you re ad -- (five second pause).

H

-

Gold Flight be advised I m not getting very good paints on you or the t arge t right now so i f 1 t 's any .• uh - i f you suspect any - dl - sug-

ge s t you keep heads up. G3

-

Be.aketwool (S IC), th~re vas an explosion or something. This is -Gold Two -- was a bright flash. I can •t read Gold Two.

H

-

Say again Gold Tiro.

G3

-

Gold

II

-

You nay you have a mid-air c-.ollisian?

G3

-

Roger,

Tb.~e,

Gold.

~ee

here.

It's a mid-air collision.

!1ayday, May:iay.

H

Roger un:ierate.n d o

Cl

Hey, Gold

Tl~ee , ~

that Cold Tvo7

7 Spec t al r.ll.I1dllr: Yith pan.gre.phs

i :red 111 Al~cordance 52 , AFF. 62-14,

' at ~ · :_ ROger, :t~ . - :uh

~ -~aw: ; an e~~~ tUBO~ ; fu.~ :be hit 'the A7?

G3 J:~: , :~fu.; I .l::im't - (r~ secao.a::Pa~). ·.The . ;,,:~~;- ., ~. ~=~~t oohiln•. •. : _... . ··-:-·

G~

- ~ ~,

... ,. r - :·.

;-

.

.._.

..- ·- •.. · ·:

:· ~.

.

•'weii;

..·. G3 ~

·Reker;

.

.

.

.

'

H Gl

- ..

. ...

;_ !Lf l <., ..: ·· t·T~~-~,

~

Roger. · ·.WelJ.., don't ;tly vhe_re·Yoti'll hit his. ps:raehute •

ri:m

out the . ~i• . .

:-

< Gl . · - ,

.

B,-47is gcme, I have

~y,

GOld

'

-

.:;

One • •

Roger, Go:!A. Gne, go MaYaay :please. -

Roger, what 's our pigeons now?

H

Roger, I have you about seventy-five miles out.

Gl

Roger.

G3

Basketvooa. (SIC), Gold Th..-.oee, here, I'm in a starboard orbit over the scene, over. (three second pause)

R

Gold One, you're siXty miles out now.

H

Roger One, go ahead.

Gl

H

Gold one is on ma;yday.

I' 11 s quavk me.yday, and ve don't vant to fly right around the area lbere be bail-- -, where he might have bailed out. We might fly into his parachute. -

On~ and three e.ll Sq'.lB.Yking me.J"3"y?

Roger --- (four second pauee). ma.yday~

Gl

One is squavking

Roger.

G3

Thr-ee is ma.yday, affirmative.

Shortly after this, Gold One returned to Charleston .AFB for landing. Gold Three continued to orbit the scene, pinpointing fires on the ground and looking for flares or other evidence of survivors. He remained in the area a.a long as fuel permitted and then proceeded to Charles-ten £or landing.

8 1n Accordance 52, AF'R 62-14.

quir~d

l~ \

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N

~

~

t

lli ~

......

~

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