NATO Tiger Meet 2016 by David Parody

NATO TIGER MEET

2016

Zaragoza, Spain, May 2016 Photo Essay by David M Parody 1

Aircraft data supplied by Wikipedia as are line images. Aircraft registrations supplied by Daniel Ferro. All photography ÂŠ DM Parody 2016

Order of Battle M1-24 Superhind Mi-17 HIP Gazelle Huey Puma E3-Sentry E2-Hawkeye C130 Hercules Mirage 2000 Rafale Gripen Tornado F16 Fighting Falcon f18 Hornet Eurofighter Typhoon Casa C-212 Canadaur CL-215 Beech 1900/Dausault Flacon LearjeT 35A/Cessna Citation V Boeing 747/Airbus A330 Airframe registrations

4 10 12 16 18 20 24 28 34 42 52 62 68 98 112 128 130 132 134 136

9 11 15 17 19 23 27 33 41 51 61 67 97 111 127 129 131 133 135 139

Mil Mi-24 Sup

> Czech Air Force : 221 LtBVr : Namest

per Hind

General characteristics Crew: 2–3: pilot, weapons system officer and technician (optional) Capacity: 8 troops or 4 stretchers or 2400 kg (5,291 lb) cargo on an external sling Length: 17.5 m (57 ft 4 in) Rotor diameter: 17.3 m (56 ft 7 in) Wingspan: 6.5 m (21 ft 3 in) Height: 6.5 m (21 ft 3 in) Disc area: 235 m2 (2,530 ft2) Empty weight: 8,500 kg (18,740 lb) Max. takeoff weight: 12,000 kg (26,500 lb) Powerplant: 2 × Isotov TV3-117 turbines, 1,600 kW (2,200 hp) each Performance Maximum speed: 335 km/h (208 mph) Range: 450 km (280 miles) Service ceiling: 4,900 m (16076 ft)

> Czech Air Force : 221 LtBVr : Namest

Mi-17 HiP

> Czech Air Force : 221 LtBVr : Namest GENERAL CHARACTERISTICS Crew: Three – two pilots and one engineer Capacity: 30 troops or 12 stretchers or 4,000 kg (8,820 lb) cargo internally /5,000 kg (11,023 lb) externally slung. Length: 18.465 m (60 ft 7 in) Rotor diameter: 21.25 m (69 ft 10½ in) Height: 4.76 m (15 ft 7¼ in) Disc area: 356 m² (3,834 ft²) Empty weight: 7,489 kg (16,510 lb) Loaded weight: 11,100 kg (24,470 lb) Max. takeoff weight: 13,000 kg (28,660 lb) Powerplant: 2 × Klimov TV3-117VM turboshafts, 1,633 kW (2,190 shp) each Performance Maximum speed: 250 km/h (135 knots, 155 mph) Range: 465 km (251 nmi, 289 mi) (standard fuel) Service ceiling: 6,000 m (19,690 ft) Rate of climb: 8 m/s[citation needed] (1,575 ft/min)

Aérospatiale General characteristics Crew: 2 Capacity: 3 Passengers Length: 11.97 m (39 ft 0 in) Main rotor diameter: 10.5 m (34 ft 6 in) Height: 3.15 m (10 ft 3 in) Main rotor area: 86.5 m2 (931 ft2) Empty weight: 908 kg (2,002 lb) Gross weight: 1,800 kg (3,970 lb) Powerplant: 1 × Turbomeca Astazou IIIA turboshaft, 440 kW (590 hp) Performance Maximum speed: 310 km/h (193 mph) Cruising speed: 264 km/h (164 mph) Range: 670 km (416 miles) Service ceiling: 5,000 m (16,405 ft) Rate of climb: 9 m/s (1,770 ft/min)

> French Army

e Gazelle

> French Army

> Italian Ai

Bell UH-1N Tw

General characteristics Crew: 4 (pilot, co-pilot, crew chief, gunner) Capacity: 6-8 combat-equipped troops, or equivalent cargo Length: 57 ft 8 in (12.69 m) Rotor diameter: 48 ft 0 in (14.6 m) Height: 14 ft 5 in (4.4 m) Disc area: 1,808 ft² (168.0 m²) Empty weight: 6,100 lb (2,765 kg) Useful load: 4,400 lb (1,996 kg) Max. takeoff weight: 10,500 lb (4,763 kg) Powerplant: 2 × Pratt & Whitney Canada T400-CP-400 turboshaft, 900 shp (671 kW), (total 1,250 shp; 932 kW) each Performance Maximum speed: 130 knots (135 mph, 220 km/h) Cruise speed: 110 knots (126 mph, 207.3 km/h) Range: 248 nmi (286 mi, 460 km) Service ceiling: 17,300 ft (5,273 m) 16

ir Force : 12 Gruppo : Gioia del Colle

win Huey

> R

Aérospatiale

General characteristics Crew: 3 Capacity: 16 passengers Length: 18.15 m (59 ft 6½ in) Rotor diameter: 15.00 m (49 ft 2½ in) Height: 5.14 m (16 ft 10½ in) Disc area: 177.0 m² (1,905 ft²) Empty weight: 3,536 kg (7,795 lb) Max takeoff weight: 7,000 kg (15,430 lb) Powerplant: 2× Turbomeca Turmo IVC turboshafts, 1,175 kW (1,575 hp) each Performance Never exceed speed: 273 km/h (147 knots, 169 mph) Maximum speed: 257 km/h (138 knots, 159 mph) Cruise speed: 248 km/h (134 knots, 154 mph) econ cruise Range: 580 km (313 nm, 360 mi) Service ceiling: 4,800 m (15,750 ft) Rate of climb: 7.1 m/s (1,400 ft/min)

Royal Air Force : 230 Sqn : RAF Benson

e Puma

Boeing E-3 Se

> NATO : 1 AEW&CS : MOB Geilenkirchen

entry

General characteristics Crew: Flight crew: 4 (aircraft commander, pilot, navigator, flight engineer) Mission crew: 13–19 Length: 152 ft 11 in (46.61 m) Wingspan: 145 ft 9 in (44.42 m) Height: 41 ft 4 in (12.6 m) Wing area: 3,050 ft2 (283.4 m2) Empty weight: 185,000 lb (73,480 kg) Loaded weight: 344,000 lb (with aerial refueling) (156,036 kg) Max. takeoff weight: 347,000 lb (157.397 kg) Powerplant: 4 × Pratt and Whitney TF33-PW-100A turbofan, 21,500 lbf (93 kN) each Performance Maximum speed: 530 mph (855 km/h, 461 knots) Range: 4,000 nmi (7,400 km) (8 hr) Service ceiling: 41,000 ft (12,500 m)

> NATO : 1 AEW&CS : MOB Geilenkirchen

E-2 Hawkeye

> French Navy

General characteristics Crew: Five: Pilot, Copilot, Radar Officer (RO), Combat Information Center Officer (CICO), Aircraft Control Officer (ACO) Length: 57 ft 8.75 in (17.60 m) Wingspan: 80 ft 7 in (24.56 m) Height: 18 ft 3.75 in (5.58 m) Wing area: 700 ft2[80] (65 m2) Empty weight: 40,200 lb (18,090 kg) Loaded weight: 43,068 lb (19,536 kg) Max. takeoff weight: 57,500 lb (26,083 kg) Powerplant: 2 Ă&#x2014; Allison / Rolls-Royce T56-A-427 (E-2C), T56-A-427A (E-2D) turboprop, 5,100 shp (3,800 kW) each Performance Maximum speed: 350 knots (648 km/h or 402 MPH) Cruise speed: 256 knots (474 km/h or 294 MPH) Ferry range: 1,462 nmi (2,708 km or 1,682 mi) Endurance: 6 hr Service ceiling: 34,700 ft (10,576 m) Wing loading: 72.7 lb/ft2 (355 kg/m2)

> French Navy

C-130 Hercul

les

> Belgian Air Force

General characteristics Crew: five (two pilots, navigator, flight engineer and loadmaster) Capacity: C-130E/H/J cargo hold: length, 40 feet (12.19 m); width, 119 inches (3.02 m); height, 9 feet (2.74 m). Rear ramp: length, 123 inches (3.12 m); width, 119 inches (3.02 m) C-130J-30 cargo hold: length, 55 feet (16.76 m); width, 119 inches (3.02 m); height, 9 feet (2.74 m). Rear ramp: length, 123 inches (3.12 m); width, 119 inches (3.02 m) 92 passengers or 64 airborne troops or 74 litter patients with 5 medical crew or 6 pallets or 2–3 Humvees or 2 M113 armored personnel carriers Payload: 45,000 lb (20,400 kg) Length: 97 ft 9 in (29.8 m) Wingspan: 132 ft 7 in (40.4 m) Height: 38 ft 3 in (11.6 m) Wing area: 1,745 ft² (162.1 m²) Empty weight: 75,800 lb (34,400 kg) Useful load: 72,000 lb (33,000 kg) Max. takeoff weight: 155,000 lb (70,300 kg) Powerplant: 4 × Allison T56-A-15 turboprops, 4,590 shp (3,430 kW) each Propellers: 4 propellers Propeller diameter: 13.5 ft (4.1 m) Performance Maximum speed: 320 knots (366 mph, 592 km/h) at 20,000 ft (6,060 m) Cruise speed: 292 kts (336 mph, 540 km/h) Range: 2,050 nmi (2,360 mi, 3,800 km) Service ceiling: 33,000 ft (10,060 m) empty;[81] 23,000 ft (7,077 m) with 42,000 pounds (19,090 kilograms) payload () Rate of climb: 1,830 ft/min (9.3 m/s) Takeoff distance: 3,586 ft (1,093 m) at 155,000 lb (70,300 kg) max gross weight;[80] 1,400 ft (427 m) at 80,000 lb (36,300 kg) gross weight

> Belgian Air Force

> Spanish : Ejercito del aire

Dassault Mir

General characteristics Crew: 1 Length: 14.36 m (47 ft 1 in) Wingspan: 9.13 m (29 ft) Height: 5.20 m (17 ft) Wing area: 41 m² (441.3 ft²) Empty weight: 7,500 kg (16,350 lb) Loaded weight: 13,800 kg (30,420 lb) Max. takeoff weight: 17,000 kg (37,500 lb) Powerplant: 1 × SNECMA M53-P2 afterburning turbofan Dry thrust: 64.3 kN (14,500 lbf) Thrust with afterburner: 95.1 kN (21,400 lbf) Performance Maximum speed: Mach 2.2 (2,530+ km/h, 1,500+ mph) at high altitude/ 1,110 km/h (690 mph) at low altitude Range: 1,550 km (837 nmi, 963 mi) with drop tanks Ferry range: 3,335 km (1,800 nmi, 2,073 mi) with auxiliary fuel Service ceiling: 17,060 m (59,000 ft) Rate of climb: 285 m/s (56,000 ft/min) Wing loading: 337 kg/m² (69 lb/ft²) Thrust/weight: 0.7 at loaded weight

French Air Force : ECE 5/330 : Araxos

rage 2000

French Air Force : ECE 5/330 : Araxos

Dassault Raf

General characteristics Crew: 1–2 Length: 15.27 m (50.1 ft) Wingspan: 10.80 m (35.4 ft) Height: 5.34 m (17.5 ft) Wing area: 45.7 m² (492 ft²) Empty weight: 10,300 kilograms (22,700 lb) (B)[69][246] 9,850 kilograms (21,720 lb) (C) () Loaded weight: 15,000 kilograms (33,000 lb) () Max. takeoff weight: 24,500 kilograms (54,000 lb) (B/C/D) () Powerplant: 2 × Snecma M88-2 turbofans Dry thrust: 50.04 kN (11,250 lbf) each Thrust with afterburner: 75.62 kN (17,000 lbf) each Fuel capacity: 4,700 kg (10,360 lb) internal Performance Maximum speed: High altitude: Mach 1.8 (1,912 km/h, 1,032 knots) Low altitude: Mach 1.1 (1,390 km/h, 750 knots) Supercruise: Up to Mach 1.4[citation needed] Range: 3,700+ km (2,000+ nmi) with 3 drop tanks Combat radius: 1,852+ km (1,000+ nmi) on penetration mission Service ceiling: 15,235 m (50,000 ft) Rate of climb: 304.8+ m/s (60,000+ ft/min) Wing loading: 328 kg/m² (67.1 lb/ft²) Thrust/weight: 0.988 (100% fuel, 2 EM A2A missile, 2 IR A2A missile) version B Maximum g-load: +9/–3.6

> French Navy : 11F : BAN Landiviseau

fale

> French Navy : 11F : BAN Landiviseau

> C

Saab JAS 39 G

General characteristics Crew: 1 (2 for JAS 39D) Payload: 5,300 kg (11,700 lb) Length: 14.1 m (46 ft 3 in); two-seater: 14.8 m (48 ft 5 in) Wingspan: 8.4 m (27 ft 7 in) Height: 4.5 m (14 ft 9 in) Wing area: 30.0 m² (323 ft²) Empty weight: 6,800 kg[337] (14,990 lb) Loaded weight: 8,500 kg (18,700 lb) Max. takeoff weight: 14,000 kg (31,000 lb) Powerplant: 1 × Volvo RM12 afterburning turbofan Dry thrust: 54 kN (12,100 lbf) Thrust with afterburner: 80.5 kN (18,100 lbf) Wheel track: 2.4 m (7 ft 10 in) 52

Czech

Air Force : 221 TL : Caslav AFB

Gripen

Performance Maximum speed: Mach 2 (2,204 km/h (1,190 kn; 1,370 mph)) at high altitude Combat radius: 800 km (497 mi, 432 nmi) Ferry range: 3,200 km (1,983 mi) with drop tanks Service ceiling: 15,240 m (50,000 ft) Wing loading: 283 kg/m² (58 lb/ft²) Thrust/weight: 0.97 Maximum g-load: +9 g

> C

Czech

Air Force : 221 TL : Caslav AFB

> C

Czech

Air Force : 221 TL : Caslav AFB

> Hunga

arian Air Force : 59/1 Sqn : Kecskemet

> Hunga

arian Air Force : 59/1 Sqn : Kecskemet

Panavia Torn

> Luftwaffe : Schleswig AB

nado ECR

General characteristics Crew: 2 Length: 16.72 m (54 ft 10 in) Wingspan: 13.91 m at 25° wing sweep, 8.60 m at 67° wing sweep (45.6 ft / 28.2 ft) Height: 5.95 m (19.5 ft) Wing area: 26.6 m2 (286 ft2) Empty weight: 13,890 kg (30,620 lb[248]) Loaded weight: 20,240 kg (44,620 lb[249]) Max. takeoff weight: 28,000 kg (61,700 lb) Powerplant: 2 × Turbo-Union RB199-34R Mk 103 afterburning turbofans Dry thrust: 43.8 kN (9,850 lbf) each Thrust with afterburner: 76.8 kN (17,270 lbf) each Performance Maximum speed: Mach 2.2 (2,400 km/h, 1,490 mph) at 9,000 m (30,000 ft) altitude; 800 knots, 1,482 km/h, 921 mph indicated airspeed near sea level Range: 1,390 km (870 mi) for typical combat mission Ferry range: 3,890 km (2,417 mi) with four external drop tanks Service ceiling: 15,240 m (50,000 ft) Rate of climb: 76.7 m/s (15,100 ft/min) Thrust/weight: 0.77 63

> Luftwaffe : Schleswig AB

> Tur

F-16 Fighting General characteristics Crew: 1 Length: 49 ft 5 in (15.06 m) Wingspan: 32 ft 8 in (9.96 m) Height: 16 ft (4.88 m) Wing area: 300 ft² (27.87 m²) Airfoil: NACA 64A204 root and tip Empty weight: 18,900 lb (8,570 kg) Loaded weight: 26,500 lb (12,000 kg) Max. takeoff weight: 42,300 lb (19,200 kg) Powerplant: 1 × General Electric F110-GE-129 (for F-16C/D Block 30-40-50) afterburning turbofan Dry thrust: 17,155 lbf (76.3 kN) Thrust with afterburner: 28,600 lbf (127 kN) Internal fuel: 7,000 pounds (3,200 kg)[2] Performance Maximum speed: At sea level: Mach 1.2 (915 mph, 1,470 km/h)[66] At altitude: Mach 2[2] (1,320 mph, 2,120 km/h) clean configuration Combat radius: 340 mi (295 nmi, 550 km) on a hi-lo-hi mission with four 1,000 lb (450 kg) bombs Ferry range: 2,280 nmi (2,620 mi, 4,220 km) with drop tanks Service ceiling: 50,000+ ft[2] (15,240+ m) Rate of climb: 50,000 ft/min (254 m/s) Wing loading: 88.3 lb/ft² (431 kg/m²) Thrust/weight: 1.095 (1.24 with loaded weight & 50% internal fuel)[232] Maximum g-load: +9.0 g

rkish Air Force : 192 Filo : Balikesir

g Falcon

> Belgi

ian Air Force : 31 smd : Kleine Brogel

> Belgi

ian Air Force : 31 smd : Kleine Brogel

> Belgian Air Force

> Greek Air Force : 335 Mira : Araxos

> Royal Norwe

egian Air Force : 338 Sky : MAS Orland

> Royal Norwe

egian Air Force : 338 Sky : MAS Orland

> Royal Norwe

egian Air Force : 338 Sky : MAS Orland

> Polish A

Air Force : 6 ELT : Poznan-Krzesiny AB

> Polish A

Air Force : 6 ELT : Poznan-Krzesiny AB

> Polish A

Air Force : 6 ELT : Poznan-Krzesiny AB

> Tur

rkish Air Force : 192 Filo : Balikesir

> Tur

rkish Air Force : 192 Filo : Balikesir

> Tur

rkish Air Force : 192 Filo : Balikesir

> Spanish Eje

F/A-18 Horne General characteristics

Crew: F/A-18C: 1, F/A-18D: 2 (pilot and weapons system officer) Length: 56 ft (17.1 m) Wingspan: 40 ft (12.3 m) Height: 15 ft 4 in (4.7 m) Wing area: 400 ft² (38 m²) Airfoil: NACA 65A005 mod root, 65A003.5 mod tip Empty weight: 23,000 lb (10,400 kg) Loaded weight: 36,970 lb (16,770 kg) Max. takeoff weight: 51,900 lb (23,500 kg) Powerplant: 2 × General Electric F404-GE-402 turbofans

ercito del aire : Ala 15 : BA Zaragoza

Performance Maximum speed: High altitude: Mach 1.8 (1,034 knots, 1,190 mph, 1,915 km/h) at 40,000 ft (12,190 m) Low altitude: Mach 1.2 (795 knots, 915 mph, 1,473 km/h)[141] Range: 1,089 nmi (1,250 miles, 2,000 km) with only two AIM-9s Combat radius: 400 nmi (460 mi (740 km)) on air-air mission Ferry range: 1,800 nmi (2,070 mi (3,330 km)) Service ceiling: 50,000 ft (15,240 m) Rate of climb: 50,000 ft/min (254 m/s) Wing loading: 93 lb/ftÂ˛ (454 kg/mÂ˛) Thrust/weight: 0.96 (1.13 with loaded weight & 50% internal fuel)

> Swi

100

iss Air Force : Staffel 11 : Meiringen

101

> Swi

102

iss Air Force : Staffel 11 : Meiringen

103

> Swi

104

iss Air Force : Staffel 11 : Meiringen

105

> Swi

106

iss Air Force : Staffel 11 : Meiringen

107

> Spanish Eje

108

ercito del aire : Ala 15 : BA Zaragoza

109

> Spanish Eje

110

ercito del aire : Ala 15 : BA Zaragoza

111

Eurofighter General characteristics Crew: 1 (operational aircraft) or 2 (training aircraft) Length: 15.96 m (52.4 ft) Wingspan: 10.95 m (35.9 ft) Height: 5.28 m (17.3 ft) Wing area: 51.2 m²[330] (551 sq ft) Empty weight: 11,000 kg[331][N 6] (24,250 lb) Loaded weight: 16,000 kg[332][N 7] (35,270 lb) Max. takeoff weight: 23,500 kg[330] (51,800 lb) Powerplant: 2 × Eurojet EJ200 afterburning turbofan Dry thrust: 60 kN (13,490 lbf) each Thrust with afterburner: >90 kN[331][333] (20,230 lbf) each Fuel capacity: 5,000 kg (11,020 lb) internal[334][335] Performance Maximum speed: At altitude: Mach 2 class[336] (2,495 km/h or 1,550 mph)[337][338] At sea level: Mach 1.25[329] (1,470 km/h or 910 mph)[339] Supercruise: Mach 1.5[136] Range: 2,900 km (1,800 mi) Combat radius: (with 3 external 1,000 l tanks) Ground attack, lo-lo-lo: 601 km (325 nmi) Ground attack, hi-lo-hi: 1,389 km (750 nmi) Air defence with 3-hr combat air patrol: 185 km (100 nmi) Air defence with 10-min. loiter: 1,389 km (750 nmi) [330][340] Ferry range: >3,790 km (2,350 mi with 3 drop tanks) Service ceiling: 19,812 m (65,000 ft[341][342]) Rate of climb: >315 m/s[343] (62,000 ft/min[344]) Wing loading: 312 kg/m²[330] (63.9 lb/ft²) Thrust/weight: 1.15 (interceptor configuration)[330] Maximum g-load: +9/−3 g[345] Brakes-off to Take-off acceleration: <8 sec Brakes-off to supersonic acceleration: <30 s Brakes-off to Mach 1.6 at 11,000 m (36,000 ft): <150

112

> Luftwaffe : TaktLwG 74 : Neuburg

r Typhoon

113

114

> Luftwaffe : TaktLwG 74 : Neuburg

115

116

> Luftwaffe : TaktLwG 74 : Neuburg

117

118

> Luftwaffe : TaktLwG 74 : Neuburg

119

120

> Italian Air Force

121

> Spanish E

122

Ejercito del aire : 142 Esc : Albacete

123

> Spanish E

124

Ejercito del aire : 142 Esc : Albacete

125

> Spanish E

126

Ejercito del aire : 142 Esc : Albacete

127

CASA C-212 Av

General characteristics Crew: Two (pilot and co-pilot) Capacity: 26 passengers (civil version), 24 paratroops or 2,700 kg (5,952 lb) cargo Length: 16.20 m (53 ft 1¾ in) Wingspan: 20.28 m (66 ft 6½ in) Height: 6.30 m (20 ft 8 in) Wing area: 41.0 m² (441 ft²) Airfoil: NACA 653-218 Aspect ratio: 10.0:1 Empty weight: 3,780 kg (8,333 lb) Max. takeoff weight: 7,700 kg (16,975 lb) Powerplant: 2 × Garrett AiResearch TPE-331-10R-513C turboprop engines, 617 kW (900 shp) each Performance Maximum speed: 370 km/h (200 kts, 230 mph) Cruise speed: 300 km/h (162 knots, 186 mph) (econ cruise) Stall speed: 145 km/h (78 knots, 90 mph) Range: 1,811 km (978 nmi, 1,125 miles) econ cruise, max fuel Service ceiling: 7,925 m (26,000 ft) Rate of climb: 8.3 m/s (1,630 ft/min) 128

viocar

129

Canadair CL-2

General characteristics Crew: two pilots Capacity: 18 passengers (utility version) Payload: 5,346 litres (1,176 Imp gal) of water or 5,444 kg (12,000 lb) of chemicals Length: 19.82 m (65 ft 0½ in) Wingspan: 28.60 m (93 ft 10 in) Height: 8.98 m (29 ft 6 in[22]) Wing area: 100.3 m² (1,080 ft²) Empty weight: 12,065 kg (26,600 lb) Max. takeoff weight: From water: 17,100 kg (37,700 lb) From land: 19,730 kg (43,500 lb) Powerplant: 2 × Pratt & Whitney R-2800-83AM 18-cylinder radial engines, 2,100 hp (1,566 kW) each Performance Cruise speed: 291 km/h (157 knots, 181 mph) (max recommended power) Stall speed: 123 km/h (66 knots, 76 mph) Range: 2,260 km (1,220 nm, 1,405 mi) Service ceiling: 14,600 ft (4,450 m) 130

215

131

Beech 1900D

Dassault Falcon 10MER

132

Learjet 35A

Cessna Citation V

133

Boeing 747-8HTF

Airbus A330-243F

134

135

Aircraft Seen at NTM 16

All data supplied by Daniel Ferro Based in Zaragoza ; Ala 15 – McDonnell Douglas EF-18A(M) Hornet ; 15-01/C.15-14 , 15-02/C.15-15 15-10/C.15-23 , 15-11/C.15-24 15-17/C.15-30 , 15-18/C.15-31 15-25/C.15-38 , 15-26/C.15-39 15-30/C.15-43 , 15-31/C.15-47 +1 ( in hangar )

, , , , ,

15-03/C.15-16 15-12/C.15-25 15-22/C.15-35 15-27/C.15-40 15-33/C.15-67

, , , , ,

15-09/C.15-22 15-13/C.15-26 15-24/C.15-37 15-28/C.15-41 15-34/C.15-64

Ala 15 - McDonnell Douglas EF-18B(M) Hornet ; 15-70/CE.15-01 , 15-72/CE.15-03 , 15-74/CE.15-5 , 15-75/CE.15-06 15-76/CE.15-07 Ala 31 – Lockheed C-130H Hercules ; 31-03/T.10-03 , 31-05/T.10-08 , 31-06/T.10-09 , 31-01/TL.10-01 , +1 ( in hangar ) Ala 31 – Lockheed KC-130H Hercules ; 31-52/TK.10-07 , 31-53/TK.10-11 , 31-54/TK.10-12 Visitors ; SPAIN - CASA C-295M - 35-41/T.21-13 - Ala 35 SPAIN – CASA C-212-100 Aviocar - 72-01/T.12B-13 721 Esc SPAIN – CASA C-212-100 Aviocar - 72-11/T.12B-65 721 Esc SPAIN – CASA C-212 +1 ( arrived 21st ) SPAIN – CASA C-212-200 54-11/T.12D-74 CLAEX – INTA (Instituto Nacional de Tecnica Aerospacial) SPAIN – Cessna C560 Citation V - 403-11/TR.20-01 - 403 Esc SPAIN – Canadair CL-215T - 431-17/UD.13-17 - 431 Esc HUNGARY / NATO – Boeing C-17A Globemaster III - 03 – NATO SAC PAPA/HAW (19th) BELGIUM – Lockheed C-130H Hercules - CH-03 - 20 Smd/15 Wg FRANCE – Socata TBM-700A - 104/XJ FRANCE – Dassault Falcon 10MER – 101 - 57 S FRANCE – Dassault Falcon 10MER – 185 – 57 S SWITZERLAND - Raytheon 1900D - T-729 GERMANY – Panavia Tornado ECR - 46+24 - Tlg 51 GERMANY – Panavia Tornado ECR – 46+55 – Tlg 51 ITALY – Eurofighter EF-2000 Typhoon S - 36-21/MM7292 - 36 St ITALY – Eurofighter EF-2000 Typhoon S – 36-12/MM7341 – 36 St ITALY – Eurofighter EF-2000 Typhoon S – 36-10 – 36 St ITALY – Eurofighter EF-2000 Typhoon S – 36-02 – 36 St ITALY – Eurofighter EF-2000 Typhoon S – 36-25 – 36 St ITALY – Eurofighter EF-2000 Typhoon S – 36-34 – 36 St PORTUGAL – General Dynamics F-16AM Fighting Falcon – 15133 PORTUGAL – General Dynamics F-16AM Fighting Falcon - 15141 BELGIUM – General Dynamics (SABCA) F-16AM Fighting Falcon - FA-123

136

Patrulla Aspa - Eurocopter EC-120B Colibri ; 78-20/HE.25-1 , 78-22/HE.25-3 , 78-23/HE.25-4 , 78-27/HE.25-8 78-29/HE.25-10 , 78-34/HE.25-15 Patrulla Águila - CASA C-101EB Aviojets ; 79-06/E.25-06 , 79-08/E.25-08 , 79-12/E.25-12 , 79-13/E.25-13 79-14/E.25-14 , 79-19/E.25-19 , 79-28/E.25-28 , 79-29/E.25-87 79-39/E.25-38

NTM participants ; GERMANY Tlg 74 EF-2000 Typhoon S ; 30+11 , 30+12 , 30+22 , 30+29 , 30+30 , 30+40 , 30+25 , Tlg 74 EF2000 Typhoon T ; 30+35 , 30+42 TURKEY 192 Filo - General Dynamics (TUSAS) F-16CG Night Falcon ; 89-0024 , 192 Filo – General Dynamics (TUSAS) F-16DG Night Falcon ; 91-0022 , 192 Filo – General Dynamics (TUSAS) F-16CJ Fighting Falcon ; 92-0014 , 93-0003 BELGIUM 31Smd – General Dynamics (SABCA) F-16AM Fighting Falcon ; FA-56 , FA-77 , FA-84 , FA-95 , FA-102 , FA-114 , FA-118 , FA116 31Smd – General Dynamics (SABCA) F-16BM Fighting Falcon ; FB-20 NORWAY 338 Skv - General Dynamics (Fokker) F-16AM Fighting Falcon ; 286 , 295 , 663 , 664 , 674 338 Skv – General Dynamics (Fokker) F-16BM Fighting Falcon ; 692

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CZECH REPUBLIC 211 Tl. - Saab JAS-39C Gripen ; 9236 , 9237 , 9245 211T1. – Saab JAS-39D Gripen ; 9819 221 LtBVr - Mil Mi 35 ; 3366 , 3370 221 LtBVr – Mil Mi 17 ; 0839 RAF 230 Sqn – Aerospatiale (Westland) SA330E Puma HC.2 ; XW214 FRANCE 11 F – Dassault Rafale M ; 9 , 10 , 19 , 38 , 43 , 44 , 45 3 Rhc – Aerospatiale Sa-342M Gazelle ; GAL/3862 , GBY/4145 4 F – Grumman E-2C Hawkeye ; 2 , 3 ECE 01.030 - Dassault Mirage 2000D ; 627/30-JO , 642/30-IE , 675/3-JI , 683/3-IV HUNGARY Mh.59 – Saab Jas-39C Gripen ; 34 , 35 , 37 , 40 , 41 GFD – AERIAL TARGET GFD – Gates Learjet 35A ; D-CARL POLAND 6 Elt. – Lockheed Martin F-16CJ Fighting Falcon ; 4052 , 4055 , 4059 , 4060 6 Elt. – Lockheed Martin F-16DJ Fighting Falcon ; 4082 , 4084

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SWITZERLAND Flst 11 – Mcdonnell Douglas F/A-18C Hornet ; J-5004 , J-5006 , J-5009 , J-5011 , J-5013 ITALY 21 Gruppo – Agusta AB-212ICO ; 9-60/MM81160 , 9-61/MM81161 GREECE 335 Mira – Lockheed Martin F-16CJ Fighting Falcon ; 005 , 013 , 019 335 Mira – Lockheed Martin F-16DJ Fighting Falcon ; 028 NATO NAEWF – Boeing E-3A Sentry ; LX-N90451 , LX-N90455 SPAIN Ala 14 – Eurofighter EF-2000 Typhoon S ; 14-06/C.16-39 , 14-09/C.16-44 , 14-12/C.16-48 , 14-13/C.16-49 14-14/C.16-50 , C.16-56 NETHERLANDS 313 Sqn – General Dynamics (Fokker) F-16AM Fighting Falcon ; ( left early on the 20th ) J-136 , J-616

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