T-44 CPT 4

=GROUND EMERGENCIES=

ABNORMAL START
(for HOT START & NO LIGHT OFF)

If ITT likely to exceed 925C or no rise in ITT within 10 sec after condition levers LOW IDLE: Caution: Starter time limited to 40 sec ON, 60 sec OFF, 40 sec ON, 60 sec OFF, 40 sec ON, 30 minutes OFF.
 * 1. Condition Lever – FUEL CUTOFF (ITT < 790C)
 * 2. Starter – OFF

Note: If start attempt discontinued and another start attempted, allow 60 sec delay to drain fuel and cool starter, then motor up starter for 15 sec minimum. Allow eng to completely stop before attempting another start.

EMERGENCY ENGINE SHUTDOWN ON DECK
(for FIRE, FIRE WARN LIGHT, CHIP LIGHT)


 * 1. Condition Levers – FUEL CUTOFF
 * 2. Firewall Valves – CLOSED
 * 3. Boost Pumps – OFF
 * 4. Fire Extinguisher – AS REQUIRED
 * 5. Gang Bar – OFF
 * 6. Evacuate aircraft

LOSS OF BRAKES

 * 1. Maintain direction control with rudder, nosewheel steering, or differential power.
 * 2. Prop reverse or beta range to decelerate
 * 3. Maneuver to open area and stop
 * 4. DON’T TAXI!
 * 5. Check shuttle brake valve (pull back on top of pedals)

HOT BRAKES

 * 1. STOP using reverse thrust and minimal braking
 * 2. Request assistance
 * 3. Cool brakes using propwash

BRAKE FIRE

 * 1. Stop aircraft using reverse thrust and beta range
 * 2. Request firefighting assistance
 * 3. EMERGENCY ENGINE SHUTDOWN ON DECK CHECKLIST:
 * [1] Condition Levers – IDLE
 * [2] Firewall Valves – CLOSED
 * [3] Boost Pumps – OFF
 * [4] Fire Extinguisher – AS REQUIRED
 * [5] Gang Bar – OFF
 * [6] Evacuate aircraft

=TAKEOFF EMERGENCIES=

ABORT & ENG FAILURE DURING TAKEOFF

 * 1. Announce -- “ABORT” (Initiate < 91KIAS)
 * 2. Power Levers – IDLE
 * 3. Reverse – AS REQUIRED (then beta range)
 * 4. Brakes – AS REQUIRED (smooth, even, don’t lock)

Prior to departing prepared surface:

(verbally recite remaining items) As soon as practicable: Warning: If direction control problems occur while reversing, advance both power levers to FLIGHT IDLE. Maintain directional control with rudder, nosewheel steering, and by pumping brakes.
 * 5. Condition Levers – FUEL CUTOFF
 * 6. Firewall valves – CLOSED
 * 7. Boost Pumps – OFF
 * 8. Fire Extinguishers – AS REQUIRED
 * 9. Gang bar – OFF
 * 10. Evacuate aircraft

Warning: Accelerate-stop distances increased 900 ft with condition levers HIGH IDLE and no reverse utilized.

ENGINE FAILURE AFTER TAKEOFF
(and DYNAMIC ENGINE CUT)

If sufficient runway to stop on ground, ABORT!

If insufficient runway to abort takeoff:

(POWER UP, RUDDER UP, CLEAN UP) If fire or fuel leak, continue checklist. If not, proceed to dead engine checklist.
 * 1. Power – AS REQUIRED
 * 2. Gear – UP
 * 3. Airspeed – (102 (obstacles) or 110)
 * 4. EMERGENCY SHUTDOWN CHECKLIST
 * [1] Power Lever – IDLE
 * [2] Propeller – FEATHER
 * [3] Condition Lever – FUEL CUTOFF
 * [3a] for dynamic engine cut:
 * (1) hold checklist after first 3 items
 * (2) Props – 1900RPM
 * (3) Power – max allowable (2nd redline)
 * (4) continue checklist
 * [4] Firewall valve – CLOSED
 * [5] Fire Extinguisher – AS REQUIRED
 * [6] Bleed Air – CLOSED
 * [7] Dead Engine Checklist – AS REQUIRED

Note: address first 2 items of dead engine checklist, transfer comm to CP and have him declare an emergency.

Note: Dynamic Engine Cut complete when trimmed at 110KIAS (min 102KIAS), on takeoff heading, and Emergency Shutdown Checklist complete.

=INFLIGHT EMERGENCIES=

Note:
 * 1. Rudder trim sufficient above 100KIAS. Below 100KIAS, supplement full rudder trim with constant rudder pressure.
 * 2. SSE waveoff with full flaps, result in loss of 200 feet before positive rate of climb established.
 * 3. Impending engine failure or flameout preceded by:
 * [1] unstable engine operation
 * [2] fluctuating turbine RPM
 * [3] torque and ITT temp changes
 * [4] illumination of fuel warning lights
 * [5] drop in oil pressure
 * [6] loss of thrust
 * 4. DON’T attempt an airstart if:
 * [MOVEOFF]
 * Mechanical malfunction
 * Overheating
 * Vibration
 * Explosion
 * O N1
 * Fire
 * Fuel Fumes

EMERGENCY SHUTDOWN CHECKLIST
(POWER UP, RUDDER UP, CLEAN UP) If fire or fuel leak, continue checklist. If not, proceed to dead engine checklist.
 * [1] Power Lever – IDLE
 * [2] Propeller – FEATHER
 * [3] Condition Lever – FUEL CUTOFF
 * [4] Firewall valve – CLOSED
 * [5] Fire Extinguisher – AS REQUIRED
 * [6] Bleed Air – CLOSED
 * [7] Dead Engine Checklist – AS REQUIRED

=ELECTRICAL SYSTEM FAILURES=

GENERATOR FAILURE
Note: Normal generator voltage in reset position indicates failure of generator control box, not the generator.
 * 1. Generator – OFF, RESET, ON

If the generator will NOT RESET:
 * 2. Generator – OFF
 * 3. Operating Generator – Load < 1.0
 * 4. Land as soon as practicable

DUAL GENERATOR FAILURE
Note: Loss of electric power will depressurize the cabin. If cabin altitude exceeds 10,000 ft, supplemental O2 for all occupants should be considered Note: (1) pilot turn and slip, UHF, landing gear annunc lights still powered (2) With total loss of power, following items work: [1] CP turn and slip [2] P & CP VSI [3] altimeters [4] airspeed [5] wet compass [6] N1 & N2 tachs [7] ITT [8] clocks (3) If attitude gyro & NAVAIDS required for flight, pull all C.B.s stated above except No. 1 avionic CB and leave No. 1 inverter and battery switches ON. (4) Anticipate a no-flap landing and manual gear extension.
 * 1. Cabin temp mode, electric heater, anti-ice/deice, lights – OFF
 * 2. Emergency call
 * 3. Gang bar – OFF (unless in IMC)
 * 4. Boost pumps – OFF
 * 5. Both invertors – OFF (unless IMC)
 * 6. Pull the following circuit breakers:
 * a. LT & RT feeder bus circuit breaker for NO. 2 subpanel bus
 * b. LT & RT fuel panel bus
 * c. No.1 avionics (unless IMC)
 * d. No.1 RMI, radar, CP FDI, No. 2 FD
 * e. LH fuel flow, LH oil temp
 * f. PR bleed air control, prop sync, annunc power, flap motor, & flap indicator
 * 7. Switch CP speaker/phone switch to speaker
 * 8. Battery – ON

EXCESSIVE LOADMETER INDICATIONS (> 1.0)
If charge rate > 30 amps: If loadmeter still > 1.0: Note: Loadmeter splits > 0.1 indicate abnormal generator paralleling. With air conditioner or electric heater activated, an excessive loadmeter indication for LEFT generator may indicate a current limiter failure.
 * 1. Battery/ammeter – NOTE
 * 2. Battery – OFF
 * 3. Nonessential loads – OFF

INVERTER FAILURE
Indicated by illum of failed INVERTER OUT annunc light. Note: After total AC power failure, only following work: [1] fuel flow [2] oil press [3] oil temp [4] P & CP turn & bank [5] VSI [6] airspeed [7] altimeters [8] N1 [9] ITT [10] prop RPM [11] clocks [12] NCS-31A [13] AOA indexers [14] RADALT [15] wet compass
 * 1. Failed inverter – OFF
 * 2. Check AC bus switchover
 * 3. Land as soon as practicable

Note: After dual-inverter failure, only following work: [1] DME [2] radar [3] VOR (audio only) [4] ADF-LF (audio only) [5] transponder (mode C) [6] marker beacons [7] VHF & UHF available

INSTRUMENT INVERTER FAILURE
Illum of INST INV annunc light. Indicates loss of both 26VAC stepdown transformers. Torquemeter readings erroneous (AC lies)

CIRCUIT BREAKER TRIPPED

 * 1. Nonessential CBs – DON’T reset in flight
 * 2. Essential CBs – only reset ONCE in flight

Note: Subpanel feeder CBs tripped indicates a short. DON’T RESET!

=LANDING EMERGENCIES=

FLAP SYSTEM FAILURE

 * 1. No provisions for emergency flap operations.
 * 2. If flaps inop, land with existing flap configuration.
 * 3. If split flaps, return flaps to previously selected position.
 * 4. Wing flap motor CB can by pulled to prevent inadvertent flap movement.

NO FLAP LANDING
FULL FLAP LANDING
 * 1. Same airspeeds and altitudes as approach flap landing up to 90 degree position.
 * 2. Cross threshold at 105KIAS
 * 3. Avoid abrupt pitch-up correction, especially > 105KIAS
 * 4. Aircraft will tend to balloon and then sink rapidly as approaching stall
 * 1. Don’t select flaps until after 90 position but before rolling onto final at 105KIAS.
 * 2. Additional power required for increase drag.
 * 3. Cross threshold at 95KIAS
 * 4. Beware of porpoising and/or flat landings

LANDING WITH GEAR UNSAFE UP INDICATION
If one or more landing gear fail to retract or don’t indicate safe up position: Note: Before landing, visually check gear down by another aircraft or tower fly-by.
 * 1. Gear handle – DOWN
 * 2. Gear position – CHECK
 * 3. If a safe down condition obtained and visually confirmed, LAND as soon as practicable.
 * 4. If SAFE gear down and locked indication NOT obtained or visual check indicates UNSAFE, proceed to Landing Gear Unsafe Down Indications.

LANDING GEAR UNSAFE DOWN INDICATIONS
If one or more landing gear fail to extend or fail to indicate a safe condition:

Note: If during any of following steps the problem is isolated and visual check indicates safe gear down, LAND as soon as practicable. Note: Windshield hear, prop deice, and eng lip boot heat have lock out mechanisms that override electric heater. Ensure these systems are secure before checking left main landing gear. Note: Attempt manual extension only if electrical malfunction. Caution: Don’t taxi with unsafe gear indication!
 * 1. Landing gear relay CB, landing gear indicator CB, landing gear motor CB – CHECK
 * 2. Cockpit gear position indicators – CHECK
 * a. Press-to-test bulbs
 * b. If unsafe green (for down) light accompanied by red light in gear handle, momentarily retard power levers well below 79 (+/-2)% N1. If no wheels up lights or horn detected, all 3 gears most probably in safe position.
 * c. AOA indexer lights – check if illum. Absence of indexers indicate premature landing gear motor cutoff (electrical problem).  If all gear indicate unsafe, consider manual extension.
 * d. For RT main unsafe – Prop Sync – ON. If prop sync light illum, right main NOT LOCKED.
 * e. For nosgear unsafe – Landing/Taxi Lights – ON. Note gen load.  If gen load increases, nosegear NOT LOCKED.
 * f. For left main unsafe – select manual heat and position electric heat switch to NORMAL. Note load.  Then hold electric heat switch in GRD MAX.  If significant gen load increase, left main NOT LOCKED.
 * 5. Gear position (visual) – CHECK
 * 6. If visual check indicates gear down, LAND as soon as practicable.
 * 7. If visual check confirms gear not down and locked, determine if malfunction electrical or mechanical. If electrical, raise gear handle, attempt manual extension, and obtain visual check prior to landing.
 * 8. Landing gear handle – SELECT UP
 * 9. Gear position (visual) – CHECK
 * 10. If visual check confirms gear retracted, gear up landing recommended. If gear are NOT retracted, refer to landing with gear up or unsafe.  Consult home squadron by direct radio comm or by ATC/FSS relay.

LANDING GEAR EMERGENCY EXTENSION
Note: If mechanical malfunction, don’t attempt manual gear extension! Gear can only be lowered manually if electrical gear malfunction. Gear can’t be raised mechanically. Gear is easier to manually actuate at lower airspeeds.

Note: Prop reverse not ready light WON’T illum with landing gear relay CB pulled. Landing gear motor switches may not activate; therefore, AOA indicator light may not be available.

To emergency extend gear:
 * 1. Airspeed – 120KIAS RECOMMENDED (155KIAS max)
 * 2. Autopilot – AS REQUIRED
 * 3. Landing gear relay ‘LDG GEAR’ CB – PULL
 * 4. Landing Gear Handle – DOWN
 * 5. Clutch Disengage lever – LIFT & TURN CLOCKWISE
 * 6. Manual Extension Handle – PUMP until 3 green gear indicator lights illum (approx 50 strokes to fully extend)

Note: Reduce handle stroke length when nosegear indicates safe. DON’T pump handle after 3 gear down lights illum. DON’T stow handle, move gear controls, switches, or CBs until on ground and malfunction found.

LANDING WITH ONE MAIN GEAR UP OR UNSAFE
Mechanical failure in drive mechanism. Land on runway or hard surface. Touch down well to same side of runway as extended gear. Roll on the down and locked gear, holding opposite wing up and nose straight as long as possible. As wing tip strikes ground, apply opposite brake to maintain straight path. Remove field arresting cables. If night emergency egress, pre-position threshold, spar, and aft compartment lighting ON.

Before touchdown: After touchdown:
 * 1. Crew and passengers – EMERGENCY BRIEF
 * 2. Seat belts and harnesses – SECURE (passengers assume braced position)
 * 3. Landing checklist – COMPLETE
 * 4. Power levers – IDLE
 * 5. Condition Levers – FUEL CUTOFF
 * 6. Use ailerons and rudder to maintain directional control and keep wings level as long as possible
 * 7. Brakes – AS REQUIRED
 * 8. Firewall Valves – CLOSED
 * 9. Boost Pumps – OFF
 * 10 . Fire extinguisher -- AS REQUIRED
 * 11. Gang Bar – OFF
 * 12. Evacuate aircraft

LANDING WITH MAIN GEAR DOWN, NOSE GEAR UP OR UNSAFE
If all attempts to lock nosegear fail, retract main gear, complete gear-up landing procedure, and execute gear-up landing. If main gear can’t be retracted, make a normal approach with power setting using minimum wing flap to hold nose up as much as possible after touchdown. DON’T USE BRAKES! Remove field arresting cables. If night emergency egress, pre-position threshold, spar, and aft compartment lighting ON.

Before touchdown: After touchdown:
 * 1. Crew and passengers – EMERGENCY BRIEF
 * 2. Seat belts and harnesses – SECURE (passengers assume braced position)
 * 3. Landing checklist – COMPLETE
 * 4. Power levers – IDLE
 * 5. Condition Levers – FUEL CUTOFF
 * 6. Firewall Valves – CLOSED
 * 7. Boost Pumps – OFF
 * 8 . Fire extinguisher -- AS REQUIRED
 * 9. Gang Bar – OFF
 * 10. Evacuate aircraft

GEAR UP LANDING
Main landing gear wheels protrude slightly from wheelwell in gear-up position and will roll on landing. Keep wings level. Land with approach flaps on a hard surface runway (paved preferred). Touch down at 85KIAS. If night emergency egress, pre-position threshold, spar, and aft compartment lighting ON.

Before touchdown:
 * 1. Crew and passengers – EMERGENCY BRIEF
 * 2. Seat belts and harnesses – SECURE (passengers assume braced position)
 * 3. Clutch disengage handle – LIFT & TURN COUNTERCLOCKWISE
 * 4. Manual extension handle – STOWED
 * 5. Landing gear relay ‘LDG GR’ – PULLED
 * 6. Flaps – APPROACH

Note: Tendancy to overshoot due to decreased drag. If conditions permit, gang bar – OFF prior to touchdown.

Immediately prior to touchdown:
 * 7. Condition levers – FUEL CUTOFF

After touchdown:
 * 8. Power levers – IDLE
 * 9. Condition levers – FUEL CUTOFF (only if power utilized to point of touchdown)
 * 10. Brakes – AS REQUIRED (directional control maintained using brakes and rudder)
 * 11. Firewall Valves – CLOSED
 * 12. Boost Pumps – OFF
 * 13. Fire extinguisher -- AS REQUIRED
 * 14 Gang Bar – OFF
 * 15. Evacuate aircraft