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28 Cards in this Set
- Front
- Back
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OXYGEN SYSTEM |
1. Passenger manual drop-out - Push off 2. O2 system - Systems ready 3. EROS O2 system - Check a. Dilutor Levers each mask - 100% b. N-100% regulator control - 100% position EMERGENCY "PRESS TO TEST" button (red) - Press and release, O2 heard Note: 1850 psi at 15º is fully charged bottle Read O2 from gauge Read OAT (with battery on) Determine % usable (fig P-1) Compute O2 duration in minutes (table P-1) Cylinder volume - 77 CU FT
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FUEL PUMPS/CROSSFEED OPERATION |
1. FIRE PULL handles - Pull 2. STANDBY PUMPS - On 3. BATT switch - ON (L & R FUEL PRESS and MASTER WARNING annunciators illuminated) 4. FIRE PULL handles - IN (L & R FUEL PRESS and MASTER WARNING annunciators extinguished) 5. STANDBY PUMPS - OFF (L & R FUEL PRESS and MASTER WARNING annunciators illuminated) 6. CROSSFEED FLOW - LEFT & RIGHT (FUEL CROSSFEED and MASTER WARNING annunciator illuminated, L & R FUEL PRESS annunciators extinguished) 7. CROSSFEED FLOW - OFF (L & R FUEL PRESS and MASTER WARNING annunciators illuminated) 8. AUX TRANSFER switches - AUTO
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ENGINE FIRE PROTECTION SYSTEM |
1. FIRE PROTECTION TEST switch - Rotate CCW to check all 3 DETR positions - check illumination of a. MASTER WARNING b. #1 FIRE PULL c. #2 FIRE PULL 2. Rotate switch CCW to EXTGH #1, check illumination of: a. SQUIB OK (green) on PUSH TO EXTINGUISH switch. b. #1 EXTGH DISCH light on caution/advisory panel 3. Rotate switch CCW to EXTCH #2, check illumination of : a. SQUIB OK (green) on PUSH TO EXTINGUISH switch. b. #2 EXTGH DISCH light on caution/advisory panel |
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CABIN / CARGO DOORS |
1. Cabin Door - Check closed and latched as follows: a. Safety arm and diaphragm plunger - Check b. Index marks on rotary cam locks (6) - Check 2. Cargo Door- Check closed and latched as follows: a. Upper handle - Check closed and latched b. Index marks on rotary cam locks (4) - Check aligned with indicator windows c. Lower pin latch handle - Check closed and latched. d. Carrier rod - Check orange indicator aligned with orange stripe on carrier rod. |
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OVERHEAD PANEL |
1. MASTER PANEL LIGHTS - As required 2. Lighting rheostats - As required 3. WINDSHIELD WIPERS - OFF |
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PEDESTAL CONTROLS - SET |
1. POWER levers - IDLE 2. PROP levers - HIGH 3. COND levers - FUEL CUTOFF 4. FLAPS - As required |
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LOWER CONSOLE SWITCHES - SET |
1. Avionics - As required 2. RUDDER BOOST switch - On |
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PILOTS/COPILOTS INST PANEL - SET |
1. Pilots - Compass control slaved 2. Copilots - Compass control slaved
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FIRST ENGINE START (BATT) |
1. START switch - On 2. PROP turning 3. FUEL PRESS light out 4. IGN ON light 5. 12% 6. Stable 7. 5 seconds 8. COND lever low idle 9. IGN within 10 seconds 10. N1 50% 11. TGT decreasing 12. START swith - OFF |
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SECOND ENGINE START (BATT) |
1. START switch - On 2. PROP turning 3. FUEL PRESS light out 4. IGN ON light 5. 12% 6. GEN reset and ON (first engine) 6. Stable 7. 5 seconds 8. COND lever low idle 9. IGN within 10 seconds 10. N1 50% 11. TGT decreasing 12. START swith - OFF |
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ABORT START |
1. CONDITION lever - FUEL CUTOFF 2. IGN & ENG START switch - STARTER ONLY 3. TGT - Monitor for drop in temp 4. IGN & ENG START switch - OFF |
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ENGINE CLEARING |
1. CONDITION lever - FUEL CUTOFF 2. IGN & ENG START swith - OFF (1 min minimum) 3. IGN & ENG START switch - STARTER ONLY (15 sec minimum, 40 sec maximum) 4. IGN & ENG START switch - OFF |
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AC/DC POWER - CHECK |
AC frequency 394 -406 Hz AC voltage 104 - 124 Vac (press)
DC load - Parallel within 10% 75% Max low idle 85% Max high idle 85% Max ground operations DC voltage 28.0 - 28.5 Vdc (press)
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AUTOPILOT SYSTEM CHECK |
1. Electric elevator trim - Check a. Elevator trim - ON b. P/CP trim switches - Check c. P/CP check individual element for no movement of trim and check proper operation of both elements d. Check P switches override CP and moves in direction commanded e. Check P/CP trim disconnects while activating trim f. Elevator trim switch - OFF and ON 2. Engage the AP and YD. Press RED AP/YD disconnect, ensure AP/YD disengage |
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WX RADAR TEST |
1. Select Terrain Awareness Display - Both HSIs 2. Select WXR TERRAIN DISPLAY ON/OFF switches on both P/CP sides to WX 3. WX Control knob - Rotate (until MFD's indicate WX TEST and pattern is visible |
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BRAKE DEICE - CHECK |
1. BLEED AIR VALVES - OPEN 2. BRAKE DEICE - ON, annunciator illuminated 3. Observe the following indicators a. Increase in TGT b. Decrease in torque c. Brake Deice Advisory light d. Decrease in PNEU, pressure within limits 4. BRAKE DEICE - OFF, annunciator extinguished |
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TCAS CHECK |
1. Select ALT and TA/RA, set TVI range to 5NM, momentarily actuate the test selection on the TCAS/ATC control panel 2. Code readout displays 8888 for 1 sec, and the ATC FAIL lamp illuminates for 1 sec then extinguish. 3. The TA/RA/VSI indicators should present a target display 4. After completion of self-test, TCAS SYSTEM TEST OK audio heard |
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EGPWS CHECK |
1. TERRAIN INHIBIT switch not engaged 2. EGPWS PUSH TO TEST switch - Press a. Amber GPWS inop annunciation lower left of EADIs remains on during test b. TERR INOP lamp in glareshield remains on during test c. TERR TEST displayed on EHSIs during test d. MASTER CAUTION lamps flash on/off e. Amber GPWS annunciation displayed in center of EADIs f. GLIDESLOPE aural message g. Amber GPWS annunciatoin displayed in center of EADIs extinguishes h. Red PULL UP annunciation displayed in center of EADIs i. PULL UP aural message j. 9-color terrain test pattern displayed k. TERRAIN, TERRAIN, PULL UP aural message l. Red PULL UP annunciation displayed in center of EADIs exteinguishes m. Amber GPWS annunciation displayed in center of EADIs n. Amber GPWS annunciation displayed in center of EADIs extinguishes o. 9-color terrain test pattern extinguishes p. Amber GPWS inoperative annunciation in lower left of EADOs extinguishes q. TERR INOP lamp in glareshield extinguishes r. TERR TEST displayed on HSI changes to TERR |
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IFF Transponder (APX-119) Check and set |
1. XPDR switch - 2 2 TA/RA - Set 3. Mode 4 switches - Out 4. MODE 3/A - Test position/Release a. Check TVI's for four traffic sybols, GREEN arc +300' - 0', RED arc 0' - -6000' and +6000 - +2000, TEST in white letters with white box bottom center, TCAS in black letters on yellow background in top left, TCAS OFF in white letters with white outline box top right. b. TCAS System test OK. |
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ALTIMETER - SET AND CHECK |
1. Set to field elevation - KPOB is 218' 2. Local altimeter within 70' of field elevation |
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FLIGHT INSTRUMENTS - CHECK |
1. Airspeed Indicator 2. Attitude indication level 3. No warning flags on EADI 4. VSI 0 5. Turns left and right |
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AUTOFEATHER/AUTO IGNITION CHECK |
Note: Turn AC OFF 1. AUTO IGNITION - ARM 2. CONDITION levers - LOW IDLE 3. POWER levers - 22% 5. POWER levers retard individually a. 16-21% Opposite AUTOFEATHER light out, IGN ON illuminated b. 9-14% both AUTOFEATHER lights out (prop begins to feather) c. POWER levers 22% 6. Repeat with other engine 7. POWER levers - IDLE 8. AUTOFEATHER - ARM 9. AUTO IGNITION - OFF |
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OVERSPEED GOVERNORS AND RUDDER BOOST |
1. RUDDER BOOST switch - ON 2. PROP levers - HIGH RPM 3. #1 PROP GOV switch - TEST (hold) 4. L POWER lever 1830 - 1910 RPM (stabilized) 5. PROP GOV switch - Release (RPM increases) 6. Cont until rudder boost movement is noted 7. POWER lever - IDLE 8. Repeat for other engine with #2 switch 9. CONDITION levers - HIGH IDLE Note: AC ON |
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PRIMARY GOVERNORS CHECK |
1. POWER levers - 1800 RPM 2. PROP levers - FEATHER detent 3. PROPS - 1600 to 1640 4. PROP levers - HIGH RPM 5. PROPS - 1800 6. POWER levers - IDLE |
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ICE VANES CHECK |
1. ICE VANES - EXTEND 2. TQ drop, TGT inc, Advisory light on 3. Bypass doors extended (max time 15 sec) 4. ICE VANES - RETRACT 5. TQ/TGT return, advisory light out 5. Bypass doors retracted (max time 15 sec) |
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ICE PROTECTION - CHECK |
1. PROP Deice - Auto (90 sec) Amps 14-18 (start clock) 2. PROP Deice - Manual select inner/outer (rise on DC loadmeter) 3. WSHLD ANTI-ICE - Check Normal/High (rise on DC loadmeter) 4. DEICE CYCLE switch - SINGLE Pneumatic pressure decreases, returns to green arc (12-20 psi) Fluctuation at 6 sec (wing boot inflation) Fluctuation at 4 sec (stabilizer boot inflation) Check for boot deflation 5. DEICE CYCLE switch - MANUAL Pneumatic pressure deceases, returns to green arc Boots inflate until switch is released 6. PROP DEICE switch - OFF |
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VACUUM AND PNEUMATIC SYSTEM |
1. LEFT BLEED AIR VALVE - OFF a. Pneumatic/Suction press normal b. L BL AIR OFF light on c. Both BL AIR FAIL lights remain off 2. RIGHT BLEED AIR VALVE - OFF a. Pneumatic/Suction reads 0 b. Both BL AIR OFF/FAIL lights on 3. LEFT BLEED AIR VALVE - ON a. Pneumatic/Suction press normal b. Both BL AIR FAIL lights off c. L BL AIR OFF light off 4. RIGHT BLEED AIR VALVE - ON |
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PRESSURIZATION CHECK |
1. BLEED AIR VALVES - Both ON 2. CABIN ALTITUDE - Set 500' below PA 3. CABIN PRESS switch - TEST 4. Cabin climb/descent gauge shows descent 5. CABIN PRESS switch - Release 6. Cabin shows climb then 0 climb 7. Set PA +500' |
