Engines / APU Flashcards
(88, 90) Meaning of “ENG SYNC ON” OAP message:
• Illuminates when LANDING GEAR handle is in the DOWN position and ENG SYNC selector is in N1 (88 and 90) or N2 (88 only) position.
(88) Indications that fuel heat is on:
• Blue L/R FUEL HEAT ON annunciator light(s) on OAP will illuminate. Fuel and oil temp. indications should also rise.
(88, 90) Explain what is indicated by the amber REVERSE UNLOCK light and the blue REVERSE THRUST light:
- L/R REVERSE UNLOCK Light (amber) - Illuminates when thrust reverser is unlocked.
- L/R REVERSE THRUST Light (blue) - Illuminates when thrust reverser is fully extended.
(88, 90) MD-90 engine warm up procedure during cold weather operations.
MD-90
• Min. oil temp before advancing throttle > idle is -10°C.
• Oil temp. must reach 50°C before takeoff.
NOTE (MD-90): Oil temp readout will momentarily flash when engine oil temperature < -10°C and throttle is moved above idle.
(88, 90) MD-88 engine warm up procedure during cold weather operations.
MD-88 - For 1st flight of the day w/ OAT ≤ -6°C (20°F):
• Start both engines to allow for full 5’ warm-up.
• Engine anti-ice on (regardless of environmental conditions).
• After warm-up is complete, advance both throttles to 1.2 EPR and check for normal EPR increase.
• If EPR indications are not approximately equal for both engines, allow engines to warm up for additional 2’
• Advance throttles again to check for normal EPR increase, and if still abnormal, contact MCC.
Note: Failure to comply with above procedure may result in erroneous EPR indications on takeoff roll.
If OAT ≤ -35°C (-30°F):
• Operate engine(s) at idle for 2’ before advancing throttle.
(88) Positions and function of fuel heat switch
- OFF - Removes power from fuel heat circuit following completion of fuel heat cycle.
- ON - (Momentary) Timer is energized for one minute. Respective fuel heat valve opens, supplying high stage bleed air to the air/fuel heat exchanger.
- Fuel heat is not installed on the MD-90.
(90) What automatically occurs with APU pneumatics when a L/R TAIL TEMP HIGH light illuminates?
• APU pneumatic duct depressurizes automatically on L/R TAIL TEMP HIGH light
(90) Describe the engine vibration display:
• Engine vibration displays show vibration level from 0 to 9.9 (normal range is approximately 0.0 to 4.0).
(88, 90) What conditions would lead to MANUAL ABORTED START (assumes a manual start on the MD-90) for both MD-88/90?
- No N2 rotation
- No oil pressure prior to 20% N2
- Rapid EGT rise toward limit.
(88, 90) What conditions would lead to MANUAL ABORTED START for MD-88?
- No N2 rotation
- No oil pressure prior to 20% N2
- Rapid EGT rise toward limit.
MD-88 only
• No N1 rotation prior to 20 % N2
• No fuel flow indication or EGT rise within 20 seconds after placing fuel lever ON
• Hung start (N2 fails to increase above 42%).
• Fuel flow digits are flashing combined with one or more of the abnormal engine indications listed above.
(88, 90) What conditions would lead to MANUAL ABORTED START (assumes a manual start on the MD-90) for MD-90?
- No N2 rotation
- No oil pressure prior to 20% N2
- Rapid EGT rise toward limit.
MD-90 only
• No N1 rotation prior to 33% N2
• No EGT rise w/in 20 sec. after fuel flow
• Engine vibrations above 4.0
(All) Recall the required engine warm up period prior to T/O power application:
• Start second engine in sufficient time (5’ minimum if possible if engine has been shut down more than 2 hrs) to achieve 2’ at idle prior to takeoff.
(All) Recall max APU start and operating altitude:
MD-88 / 90
- Max altitude for electric start: FL 370
- Max altitude for windmill start: FL 300
- Max operating altitude is FL 370
MD-90
• Max altitude for electric start: FL 350 (All APU starts are electric)
(90) Understand what conditions will cause an AUTO ABORT during automatic start on the MD-90:
- Normal mode performs AUTO ABORT for hot start, hung start, locked N1 rotor, ignition failure, electronic control lost, engine stall and EGT failure.
- AUTO-ABORT feature inhibited ≥ 50% N2
NOTE: No AUTO ABORT is available for low oil press or high vibration.
All) Recall the required engine cool down time prior to engine shutdown:
• Engines require 3’ cool down prior to shutdown.