NORMAL PROCEDURES CHECKLIST
SA227‐ SERIES/FCOM/VTM
2A‐i
CHECKLIST INDEX PREFLIGHT.............................................................................................................................................. 2A‐3 A. COCKPIT (SAFETY CHECK)........................................................................................................... 2A‐3 B. LEFT WING................................................................................................................................... 2A‐3 C. TAIL SECTION………………………....................................................................................................... 2A‐3 D. RIGHT WING................................................................................................................................ 2A‐4 E. NOSE SECTION.............................................................................................................................. 2A‐4 BEFORE STARTING ENGINES.................................................................................................................. 2A‐5 CABIN............................................................................................................................................... 2A‐5 COCKPIT............................................................................................…………………………………….…….. 2A‐5 PILOT’S CONSOLE ............................................................................................................................ 2A‐5 INSTRUMENT PANEL........................................................................................................................ 2A‐5 COPILOT’S CONSOLE........................................................................................................................ 2A‐5 PEDESTAL......................................................................................................................................... 2A‐5 PREFLIGHT POWER ON CHECKS…………………………………………………………………………….………………………….. 2A‐7 BEFORE START……………………………………………………………………………………..…………………………………………… 2A‐8 AFTER START.......................................................................................................................................... 2A‐8 TAXI...................................................................................................................................................…… 2A‐9 TAKEOFF................................................................................................................................................. 2A‐9 CLIMB..................................................................................................................................................... 2A‐9 10,000 FEET……………………………………………………………………………………………………………………………….. 2A‐9 CRUISE........................................................................................................................................... 2A‐10 DESCENT………………………………………...................................................................................................... 2A‐10 BEFORE LANDING................................................................................................................................. 2A‐10 AFTER LANDING................................................................................................................................... 2A‐11 STOPPING ENGINES.............................................................................................................................. 2A‐11 SECURING……………………………………………………………………………………………………………………………………….. 2A‐11
FIGURES Figure 2A‐1 PREFLIGHT WALK‐AROUND INSPECTION……………………………………………………………………….. 2A‐1
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NORMAL PROCEDURES CHECKLIST
SA227‐ SERIES/FCOM/VTM
2A‐ii
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NORMAL PROCEDURES CHECKLIST
SA227‐ SERIES/FCOM/VTM
2A‐1
PREFLIGHT WALK-AROUND INSPECTION
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NORMAL PROCEDURES CHECKLIST
SA227‐ SERIES/FCOM/VTM
2A‐2
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NORMAL PROCEDURES CHECKLIST
SA227‐ SERIES/FCOM/VTM
2A‐3
PREFLIGHT A. COCKPIT (SAFETY CHECK) 1. LANDING GEAR HANDLE................................................................................. DOWN 2. LANDING GEAR HAND PUMP VALVE HANDLE….................... AFT/PIP PIN INSTALLED 3. GPU/BATTERY DISCONNECT SYSTEM….................................... CHECK/BATTERIES ON 4. LANDING GEAR POSITION INDICATOR.................. …… PRESS‐TO‐TEST/DIMMER SET 5. CONTROL LOCK...................................................................................... AS REQUIRED 6. CONTROL SURFACE TRIM............................................................................. NEUTRAL 7. PARKING BRAKE..................................................................................... AS REQUIRED 8. GPU/BATTERY SWITCHES....................................................................... AS REQUIRED
B. LEFT WING 1. FUEL SUMPS....................................................................................................... DRAIN 2. LOWER ANTENNAS................................................................................... CONDITION 3. LEADING EDGE RAM AIR SCOOP........................................................................ CLEAR 4. GEAR DOORS (FIRST FLIGHT OF DAY).......................................................... ……. OPEN 5. LANDING GEAR, BRAKES, TIRES, HUB CAPS, AND WHEELWELL................ CONDITION 6. GENERATOR CIRCUIT BREAKERs………………………………………………………………………..... IN 7. GEAR DOORS…................................................................................................ CLOSED 8. CHOCKS.......................................................................................................... REMOVE 9. COWLING AND DOORS..................................................................................... SECURE 10. FIRE EXTINGUISHER BOTTLE PRESSURE........................................................... CHECK 11. OIL COOLER INLET....................................................................... CLEAR/CONDITION 12. ENGINE INLET AND SENSORS...................................................... CLEAR/CONDITION 13. PROPELLER AND PROPELLER DEICE BOOTS................ FREE ROTATION/CONDITION 14. ENGINE OIL QUANTITY AND FILLER CAP............................................ CHECK/SECURE 15. HYDRAULIC RESERVOIR SIGHT GLASSES.......................................................... CHECK 16. WING ICE DETECTOR LIGHT….......................................................................... CHECK 17. FUEL SUMP....................................................................................................... DRAIN 18. WING DEICE BOOTS................................................................................ CONDITION 19. FUEL VENT....................................................................................................... CLEAR 20. LANDING AND RECOGNITION LIGHTS AND SHIELD…..................................... CHECK 21. NAVIGATION LIGHTS....................................................................................… CHECK 22. AILERON AND TAB………................................................................... …… CONDITION 23. WING FUEL CAP........................................…………………………………………………. SECURE 24. FLAPS............................................................................................... ……. CONDITION 25. EXHAUST……….................................................................................................. CLEAR
C. TAIL SECTION 1. CARGO DOOR.................................................................................................. SECURE 2. STATIC SOURCES................................................................................................ CLEAR 3. DEICE BOOTS…........................................................................................ CONDITION 4. STABILIZER SETTING................... CHECK IN AGREEMENT WITH COCKPIT INDICATOR 5. CONTROL SURFACES AND RUDDER TAB................................................... CONDITION 6. NAVIGATION LIGHTS........................................................................................ CHECK 7. UPPER ANTENNAS............................................................................. ……. CONDITION 8. OXYGEN BOTTLE THERMAL RELIEF DISC........................................... ….. CONDITION
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NORMAL PROCEDURES CHECKLIST
SA227‐ SERIES/FCOM/VTM PREFLIGHT (continued)
2A‐4
D. RIGHT WING 1. FLAPS................................................................................................. CONDITION 2. EXHAUST.................................................................................................... CLEAR 3. WING FUEL CAP....................................................................................... SECURE 4. AILERON AND TAB….......................................................................... CONDITION 5. NAVIGATION LIGHTS................................................................................. CHECK 6. LANDING AND RECOGNITION LIGHTS AND SHIELD................................... CHECK 7. FUEL VENT.................................................................................................. CLEAR 8. WING DEICE BOOTS…........................................................................ CONDITION 9. WING ICE DETECTOR LIGHT....................................................................... CHECK 10. FUEL SUMP.............................................................................................. DRAIN 11. CHOCKS…….......................................................................................... REMOVE 12. FIRE EXTINGUISHER BOTTLE PRESSURE................................................... CHECK 13. OIL COOLER INLET................................................................ CLEAR/CONDITION 14. ENGINE INLET AND SENSORS…..………………………………………. CLEAR/CONDITION 15. PROPELLER AND PROPELLER DEICE BOOTS………. FREE ROTATION/CONDITION 16. ENGINE OIL QUANTITY AND FILLER CAP…................................. CHECK/SECURE 17. COWLING AND DOORS.......................................................................... SECURE 18. GEAR DOORS (FIRST FLIGHT OF DAY)........................................................ OPEN 19. LANDING GEAR, BRAKES, TIRES, HUB CAPS, AND WHEELWELL...... CONDITION 20. GENERATOR CIRCUIT BREAKERS…………………………………………………................. IN 21. GEAR DOORS......................................................................................... CLOSED 22. LEADING EDGE RAM AIR SCOOP.............................................................. CLEAR 23. FUEL SUMPS............................................................................................. DRAIN E. NOSE SECTION 1. OUTSIDE AIR TEMPERATURE SENSOR........................................................ CLEAR 2. STATIC SOURCES........................................................................................ CLEAR 3. CAWI TANK SIGHT GAUGE....................................................... CHECK QUANTITY 4. CAWI TANK FILLER CAP............................................................................ SECURE 5. BAGGAGE DOORS............................................….…………………………………. SECURE 6. SAS VANE…................................................................................................ CHECK 7. PITOT COVERS…..................................................................................... REMOVE 8. WINDSHIELD WIPERS...........................................................…………… CONDITION 9. NOSE GEAR, TIRES, WHEELWELL, AND GEAR DOORS....................... CONDITION
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NORMAL PROCEDURES CHECKLIST
SA227‐ SERIES/FCOM/VTM
2A‐5
BEFORE STARTING ENGINES 1. EXTERIOR PREFLIGHT INSPECTION.................................................. COMPLETED 2. WEIGHT AND CENTER OF GRAVITY.......................... COMPUTED WITHIN LIMITS 3. PERFORMANCE DATA..................................................................... DETERMINED CABIN 1. ENTRANCE LIGHTS............................................................................. AS DESIRED 2. CABIN DOOR.............................. LOCKED (VISUALLY CHECK LATCH INDICATORS) 3. CARGO AND BAGGAGE............................................................................ SECURE 4. EMERGENCY EXITS................................................................................... SECURE COCKPIT 1. BATTERY SWITCH/GPU................................................................... AS REQUIRED 2. INTERIOR LIGHTS.....................................................………………………. AS DESIRED 3. LANDING GEAR HANDLE............................................................................ DOWN *4. NO SMOKING – FASTEN BELTS SWITCH.......................................................... ON PILOT’S CONSOLE 1. LEFT ESSENTIAL BUS TIE SWITCH.................................................................... ON 2. BUS TRANSFER SWITCHES..................................................................... LEFT BUS 3. ALL CIRCUIT BREAKERS..................................................................................... IN 4. CABIN PRESSURE SELECTOR LEVER………..................................................... AUTO 5. CABIN PRESSURE MANUAL CONTROL KNOB..................................... CLOCKWISE 6. AUTO/CONT IGNITION SWITCHES.............................................................. AUTO 7. STARTER TEST SWITCH........................................................................ CENTERED 8. SPEED SWITCH SELECT SWITCHES.............................................................. AUTO 9. START MODE SWITCH.................................................................... AS REQUIRED 10. NOSE WHEEL STEERING SWITCH................................................................. OFF 11. BATTERY VOLTAGES................................................................................. CHECK 12. SRL – Δ P/P POWER SWITCHES............................................................ NORMAL 13. TEMP LIMITER TEST SWITCH............................................................. CENTERED 14. LIGHT CONTROL KNOBS............................................................... AS REQUIRED 15. UNFEATHER TEST SWITCH................................................................. CENTERED INSTRUMENT PANEL 1. STATIC SELECTOR…................................................................................ NORMAL *2. COCKPIT CONDITIONED AIR CONTROLS (PILOT AND COPILOT)…... AS REQUIRED 3. CABIN ALTITUDE AND RATE INDICATORS AND CONTROLS............ CHECKED/SET 4. ALL ROCKER SWITCHES (EXCEPT BATTERY SWITCHES).................................. OFF 5. PITCH TRIM................... COMPARE WITH POSITION NOTED DURING PREFLIGHT 6. FUEL COUNTER........................................................................................ ZEROED 7. FUEL QUANTITY..................................................................... CHECK IMBALANCE 8. CROSSFLOW SWITCH............................................................................... CLOSED *9. TEMPERATURE CONTROLS........................................................................... OFF *10. CABIN PRESSURE DUMP SWITCH........................................................ NORMAL
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NORMAL PROCEDURES CHECKLIST
SA227‐ SERIES/FCOM/VTM
2A‐6
BEFORE STARTING ENGINES (continued) *11. BLEED AIR SWITCHES...................................................................................
OFF *12. FRESH AIR FAN SWITCH............................................................................... OFF *13. WINDSHIELD DEFOG SWITCH (IF INSTALLED).............................................. OFF *14. OXYGEN PRESSURE.................................................................................. CHECK *15. PASSENGER OXYGEN TOGGLE CONTROL..................................................... OFF COPILOT’S CONSOLE 1. CARGO DOOR AUXILIARY WARNING LIGHT............................. TEST/CHECK OUT 2. LIGHT CONTROL KNOBS................................................................. AS REQUIRED 3. ALL CIRCUIT BREAKERS….................................................................................. IN 4. NONESSENTIAL BUS TIE SWITCH……............................................................... ON 5. RIGHT ESSENTIAL BUS TIE SWITCH…............................................................... ON PEDESTAL 1. LIGHT CONTROL KNOBS…............................................................... AS REQUIRED 2. AILERON TRIM….................................................................................... NEUTRAL 3. RUDDER TRIM…..................................................................................... NEUTRAL 4. PARKING BRAKE................................................................………….. AS REQUIRED 5. AUXILIARY TRIM SWITCH…......................................…………………………………… OFF 6. SAS CLUTCH OR SAS SERVO SWITCH….......................................…………………. OFF 7. FUEL AND HYDRAULIC SHUTOFF SWITCHES…...........................………………. OPEN 8. FUEL BOOST SWITCHES…......................................................……………………… OFF 9. ENGINE STOP AND FEATHER CONTROLS…....................................................... IN 10. TRIM SELECT SWITCH…............................................................................. PILOT 11. OUT‐OF‐TRIM WARNING (FIRST FLIGHT OF DAY)…................................. CHECK A. STABILIZER TRIM….......................................... NOT IN GREEN TAKEOFF BAND B. POWER LEVERS…................................................... ADVANCE TO 50% TRAVEL C. OUT‐OF‐TRIM WARNING HORN.............................……..…………………… STEADY D. STABILIZER TRIM…........................................... SET IN GREEN TAKEOFF BAND E. OUT‐OF‐TRIM WARNING HORN…..................................................... SILENCED 12. FLAPS CONTROL….......................................................................................... UP 13. WATER INJECTION SWITCH.......................................................................... OFF 14. CONTROL LOCK….............................................. OFF/CONTROLS CHECKED FREE 15. SPEED LEVERS….......................................................... LOW RPM/FRICTION SET 16. POWER LEVERS. …......................................... CHECK / SET AT FLIGHT IDLE GATE
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NORMAL PROCEDURES CHECKLIST
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FO FIRST FLIGHT OF THE DAY SYSTEMS CHECKS 1. Batteries & GPU Volts ………...........…………................. 2. SAS Stall Test…………….…………….............................. 3. Intake Heat Test…………………………………………….. 4. Fuel Qty Indicator Test……………………………………… 5. Crossflow Switch …..……………….................................. 6. Out-Of-Trim Warning Horn …………………..…………….. 7. Stabilizer Trim System………………………….…..……... 8. Boost Pumps……….………....…………………………….. 9. Fuel & Hydraulic Switches……………………………...…. 10. AWI Quantity & Pumps.……………….............................. 11. Inverters…………………………………….……………….. 12. Gear Position Lights Test & Dimmer………..……………. 13. Fire Extinguisher Test …………….....………..…………… 14. Annunciator Panel & Warning lights………………………. 15. Oxygen System..………………………………………..(L & R) 16. Cargo Door Secondary Warning (if installed)……….…… 17. Exterior/Interior Lights ……………………………..……..…
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CA CHECKED CHECKED CHECKED CHECKED CHECKED CHECKED CHECKED CHECKED CHECKED CHECKED CHECKED CHECKED CHECKED CHECKED CHECKED CHECKED CHECKED
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NORMAL PROCEDURES CHECKLIST
SA227‐ SERIES/FCOM/VTM
2A‐8
1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 1. 2. 3. 4. 5. 6. 7. 8. 9.
FO BEFORE START CA Airplane & Crew Documents……..………………….….…(B) ON BOARD Takeoff Power, Weight & Speeds…..………………….(FO) COMPUTED Seatbelts & Shoulder Straps……………………..………………..(L & R) SET Parking Brake………………………………………………………………………. SET GPU(if available).…….………………….……..……................... CHECKED Batteries …………….…………………………………………………………….... ON Generators………………………..……………………………………………….. OFF Beacon…………………………...…………………..……..……………………… ON Power & Speed Levers………...…………………….... FLIGHT IDLE/LOW Start Mode……….……....…..……….........………………….. AS REQUIRED Annunciator Panel…………………….................................. CHECKED Fuel Qty. & Counter ……….………………………………… __Lbs & RESET Inverter…………………………………………………………………………….... ON 1 Boost Pumps…………………………………….. CHECKED/AS DESIRED 1 SAS Clutch…………………………………….……………………….…(FO) OFF 1 Avionics………………………………..….……………...………………(FO) OFF 1 Pressurization………………..…………………………………….…(SIDE) SET 1 Bleed Air & Dump Switches…………….…………(FO) OFF/NORMAL EGT……………………………………………………………….……. BELOW 200˚C Fuel Cap, Propeller & Intake…..(L & R) SET/UNFEATHERED/CLEAR FO AFTER START CA Engine Instruments & Annunciator Panel…….…….……… CHECKED Suction, De‐Ice & Hydraulic Pressures…..…..………..(FO) CHECKED Nose Wheel Steering ………..…………………..……………………. ARMED GPU……………………………………………….……………….. DISCONNECTED Current Limiter…………………………………………………………… CHECKED Boost Pumps………………………………..…..………………………..…(FO) ON SAS Clutch………………………………………..……………………………(FO) ON Bleed Air……………………………………….….…………..…..………….(FO) ON Start Locks………………………………….……..……………………. REMOVED
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NORMAL PROCEDURES CHECKLIST
SA227‐ SERIES/FCOM/VTM
2A‐9
FO
TAXI
CA
1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15.
Parking Brake……………………………………….……………….. REMOVED 1 Brakes (Both)…………………………………….……………(L & R) CHECKED * Ice Protection & Ignition………………............................ CHECKED 1 Nose Wheel Steering………………..……………… CHECKED/ARMED 1 SAS Cruise Test……………………………………….……..... CHECKED/ON Flaps.....................................................................(BOTH) SET 1/4 Controls…………..........................................................(BOTH) FREE Stabilizer, Rudder & Aileron Trim……........(FO) SET FOR TAKEOFF Flight & NAV Instruments.............................(L & R) SET/CHECKED CAWI System (If Wet Takeoff)………………………………(FO) CHECKED Fuel Qty & Crossflow Valve…………............... BALANCED/CLOSED Radar, Transponder & TCAS……………………(FO) STBY/SQUAWK__ Takeoff Power, Weight & Speeds………(CONFIRMED) CONFIRMED Briefing…………………………………………….……………... ACOMPLISHED 1 NTS…………………...................................................... CHECKED PM TAKEOFF PF
1. 2. 3. 4. 5. 6.
Lights…………………………………………………………………..…………(C) ON Radar, Transponder & TCAS……………. ………………………….(FO) ON Bleed Air…………..….................................................... ….…(C) OFF Steering…………………………….……………………………………..……(C) OFF Ice Protection & Ignition…..................................(C) AS REQUIRED Speed Levers…………………………………….. ……………..……………. HIGH PM CLIMB PM
1. 2. 3. 4. 5. 6.
1. 2. 3.
1. 2.
Landing Gear……………………………..………................................... UP Flaps……………………………..……………..……………………….……………. UP CAWI………................................................................. …………. OFF Bleed Air…………........................................................................ ON Ice Protection & Ignition…..................................(C) AS REQUIRED Taxi & landing lights…………………………………………..……………(C) OFF PM 10,000 FEET (MSL) PF Cabin Pressure………………………………………………(ON SIDE)CHECKED Annunciator Panel……………..………………..……………………. CHECKED Ammeters…………………………………………………………….…(C) CHECKED PM CRUISE PF Cruise Power………………………………………………..…………………….. SET Pressurization…………….………………………….…(ON SIDE) AS DESIRED
* When icing conditions are anticipated during flight.
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NORMAL PROCEDURES CHECKLIST
SA227‐ SERIES/FCOM/VTM
2A‐10
1. 2. 3. 4. 5. 6. 7. 8. 1. 2. 3. 4. 5. 6. 7.
PM DESCENT PM Seatbelts & Shoulder Straps…………………….…………..…(L & R) SET Altimeters.................................................................. (L & R) SET Pressurization………................................ …………..…(ON SIDE) SET Fuel Quantity & Balance......... ………………..…..(C) __LBS CHECKED Crossflow Valve............................................................. CLOSED Ice Protection & Ignition………………….………………(C) AS REQUIRED Landing Weight & Speeds……………………….………(BOTH) CONFIRM Briefing……………………………………………………………. ACOMPLISHED PM BEFORE LANDING PM Landing Gear & Hydraulic Pressure…..…(BOTH) DOWN/CHECKED Speed Levers...........................................................................HIGH Flaps…...................................................................... AS REQUIRED Ignition Mode…..................................................(C) AS REQUIRED Steering……………………………………………………………………….…(C) OFF Lights…………………………………………………………….…(C) AS REQUIRED Final Approach Speed……………………………..………..…….. CONFIRM APPROACH SPEED (KIAS) WEIGHT 1,000 (POUNDS)
1/4 1/2 FULL
10 108 103 99
10.5 110 105 101
11 112 107 103
11.5 113 108 105
12 115 110 106
12.5 116 111 108
13 118 113 109
13.5 120 114 111
16,000 MTOW AIRCRAFT
14 121 116 112
14.5 123 118 114
15 125 119 115
15.5 127 121 117
Partial flaps landing and normal landing Figure 4G‐5
Revision: Original Aug 1,2013
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NORMAL PROCEDURES CHECKLIST
SA227‐ SERIES/FCOM/VTM
2A‐11
1. 2. 3. 4. 5. 6. 1. 2. 3. 4. 5. 6. 7. 8. 9. 1. 2. 3. 4.
FO AFTER LANDING FO Radar, Transponder & TCAS………………………… …….…………… STBY Flaps…………………………………………………………………….…………….. UP Stabilizer Aileron & Rudder Trim………………………..…….. NEUTRAL Steering…………………………………………………………………….(C) ARMED Ice Protection & Ignition ……………………………………..(C) OFF/AUTO Lights………………………….......................................(C) AS REQUIRED FO STOPPING ENGINES FO Parking Brake…………………………………………………..……………..(C) SET Bleed Air Switches……………………………………….…..…….. ………… OFF Avionics……………………………………………………………………………… OFF Temperature Controller……………………………..……………………….. OFF Inverter...……………………………………………………….….…………….… OFF SAS Clutch…………………………………………………………………….….. OFF Boost Pumps…………..………………………….. ………………….………… OFF Steering …………….………….….…………….…………………….…..…(C) OFF Generators…………………………………………………………….………(C) OFF FO SECURING CA Parking Brakes……………….…………………………..……… AS REQUIRED Control Lock……………………………………………………………………….. SET External & Internal Light Switches………..……... OFF/AS REQUIRED Battery Switches……………………………………………..…………………. OFF
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NORMAL PROCEDURES CHECKLIST
SA227‐ SERIES/FCOM/VTM
2A‐12
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Revision: Original Aug 1,2013
GO/FCOM/SA227‐SERIES/VTM