UH-60 CH9

Card Set Information

Author:
Anonymous
ID:
44161
Filename:
UH-60 CH9
Updated:
2010-10-22 10:10:29
Tags:
UH Emergency procedures
Folders:

Description:
UH-60 Emergency procedures
Show Answers:

Home > Flashcards > Print Preview

The flashcards below were created by user Anonymous on FreezingBlue Flashcards. What would you like to do?


    • author "me"
    • tags "UH60"
    • description "-10 Chapter 9"
    • fileName "UH-60 CH9"
    • freezingBlueDBID -1.0
    • 9.10 Single Engine Failure
    • 1. Collective - Adjust to maintain % RPM R
  1. 2. External cargo/stores - Jettison (if required)
  2. If continued flight is NOT possible:
  3. 3. LAND AS SOON AS POSSIBLE
  4. If continued flight IS possible:
  5. 4. Establish single-engine airspeed
  6. 5. LAND AS SOON AS PRACTICABLE
  7. 9.13 Dual-Engine Failure
    AUTOROTATE
  8. 9.14 Decreasing % RPM R
    1. Collective - Adjust to control % RPM R

    • 2. PCL (low % TRQ/TGT Temp engine) - Lockout
    • Maintain % TRQ approx. 10% below other engine

    3. LAND AS SOON AS PRACTICABLE
  9. 9.15 Increasing % RPM R
    • 1. PCL (high % TRQ/TGT Temp engine) - Retard.
    • Maintain % TRQ approx.10% below other engine

    2. LAND AS SOON AS PRACTICABLE
  10. 9.18 Engine Compressor Stall
    1. Collective - Reduce

    if condition persists:

    2. PCL (affected engine) - Retard. (TGT should decrease)

    3. PCL (affected engine) - FLY

    If stall condition recurs:

    4. Est. Single English. airspeed

    5. EMER ENG SHUTDOWN (affected engine)

    6. Refer to single engine failure emergency procedure.
  11. 9.20 Engine High Speed Shaft Failure
    1. Collective - Adjust

    2. Est. Single ENG airspeed

    3. EMER ENG SHUTDOWN (affected engine)

    4. Refer to single engine failure emergency procedure.
  12. 9.21 Lightning Strike
    1. PCL - Adjust as Required to control % RPM.

    2. LAND AS SOON AS POSSIBLE
  13. 9.22.1 Loss of Tail Rotor Thrust in Cruise Flight
    1. Airspeed - Adjust to 80 KIAS or above

    2. AUTOROTATE - Maintain airspeed at or above 80 KIAS

    3. PCL's - OFF (during deceleration when intended pt. of landing is assured).
  14. 9.22.2 Loss of Tail Rotor Thrust or Tail Rotor Quadrant Caution Appears w/ Loss of Control at Low Airspeed/Hover (Right Rotation).
    1. Collective - Reduce

    2. PCL's - OFF (5-10 ft. Above touchdown).
  15. 9.22.3 Tail Rotor Quadrant Caution in Cruise Flight
    1. Collective - Adjust to determine controllability (Fixed Right or Left).

    2. Land As Soon As Practicable
  16. 9.22.4 Tail Rotor Quadrant Caution or Loss of Control at Low Airspeed/Hover (Left Rotation).
    1. PCL lever(s) - Retard to begin a partial power descent

    2. Collective - Adjust to preserve RPM R

    3. PCL's - OFF (5-10 ft above touchdown).

    4. Collective - Adjust for landing
  17. 9.22.5 Pedal Bind/Restriction or Drive w/ no accompanying caution
    1. Apply pedal force to oppose the drive

    2.- 8. Back Me Up w/ checklist
  18. 9.22.7 Main XMSN Oil Press Caution / XMSN Oil Press Low / XMSN Oil Temp High / XMSN Oil Temp Caution
    • 1. LAND AS SOON AS POSSIBLE
    • If time permits:
    • 2. Slow to 80 KIAS
    • 3. EMER APU START
    • 4. GENERATORS NO.1 & NO.2 switches - OFF
  19. 9.22.8 CHIP INPUT MDL LH or RH Caution Appears
    • 1. PCL (affected engine) - IDLE
    • 2. LAND AS SOON AS POSSIBLE
  20. 9.25.2 #1 and #2 FUEL FLTR BYPASS Cautions Appear
    LAND AS SOON AS POSSIBLE
  21. 9.25.4 #1 or #2 FUEL PRESS Caution Appears
    • 1. ENG FUEL SYS selector on affected engine - XFD
    • 2. FUEL BOOST PUMP CONTROL switches - NO.1 PUMP or NO. 2 PUMP - ON (As applicable)
    • 3. LAND AS SOON AS POSSIBLE
    • 4. EMER ENG SHUTDOWN after landing
  22. 9.25.5 #1 and #2 FUEL PRESS Cautions Appear
    • 1. LAND AS SOON AS POSSIBLE
    • 2. EMER ENG SHUTDOWN after landing
  23. 9.23.1 Engine/Fuselage Fire on Ground
    • 1. PCL's -OFF
    • 2. ENG EMER OFF handle - Pull if applicable
    • 3. FIRE EXTGH switch - MAIN/RESERVE as required
  24. 9.23.2 APU Compartment Fire
    • 1. APU fire T-handle - Pull
    • 2. FIRE EXTGH switch - MAIN/RESERVE as required
  25. 9.23.4 Engine Fire in Flight
    • 1. Establish single engine airspeed
    • 2. PCL (affected engine) - OFF
    • 3. ENG EMER OFF handle - Pull
    • 4. FIRE EXTGH switch - MAIN/RESERVE as required
    • 5. LAND AS SOON AS POSSIBLE
  26. 9.23.5 Electrical Fire in Flight
    • 1. BATT and GENERATORS switches - OFF
    • 2. LAND AS SOON AS POSSIBLE
  27. 9.25.2 #1 and#2 FUEL FLTR BYPASS Cautions Appear
    LAND AS SOON AS POSSIBLE
  28. 9.25.4 #1 or #2 FUEL PRESS Caution Appears
    • 1. ENG FUEL SYS selector on affected engine - XFD
    • 2. FUEL BOOST PUMP CONTROL switches - NO. 1 PUMP or NO.2 PUMP - ON (As applicable).
    • 3. LAND AS SOON AS POSSIBLE
    • 4. EMER ENG SHUTDOWN after landing
  29. 9.25.5 #1 and #2 FUEL PRESS Cautions Appear
    • 1. LAND AS SOON AS POSSIBLE
    • 2. EMER ENG SHUTDOWN after landing
  30. 9.26.1 #1 and #2 Generator Failure ( #1 and #2 CONV and AC ESS BUS OFF Cautions Appear)
    • 1. SAS 1 switch - Press off
    • 2. Airspeed - Adjust (80 KIAS or less)
    • 3. GENERATORS NO.1 and NO.2 switches - RESET; then ON
    • if cautions still appear:
    • 4. GENERATORS NO.1 and NO.2 switches - OFF
    • 5. EMER APU START
    • 6. SAS 1 switch - ON
    • 7. If MCU's are in use: BCA MCU control knobs (pilot, copilot, and crewmembers) - OFF
    • 8. LAND AS SOON AS PRACTICABLE
  31. 9.27.3 #1 and #2 HYD PUMP Cautions Appear
    LAND AS SOON AS POSSIBLE. Restrict control movement to moderate rates
  32. 9.27.4 #1 or #2 HYD PUMP Caution Appears and BACK-UP PUMP ON Advisory Does Not Appear
    • 1. Airspeed - Adjust to a comfortable airspeed
    • 2. BACKUP HYD PUMP switch - ON
    • If BACK-UP PUMP ON advisory still does not appear:
    • 3. FPS and BOOST switches - Off (for #2 HYD PUMP caution).
    • 4. LAND AS SOON AS POSSIBLE
  33. 9.27.5 #1 or #2 PRI SERVO PRESS Caution Appears
    • 1. SVO OFF switches - Check both are centered
    • 2. If the caution appears with the SVO OFF switch centered, move the SVO OFF switch to turn off the malfunctioning servo
    • 3. LAND AS SOON AS POSSIBLE
  34. 9.27.6 #1 RSVR LOW and #1 HYD PUMP Cautions Appear w/ BACK-UP PUMP ON Advisory Appearing
    • 1. LAND AS SOON AS PRACTICABLE
    • If the BACK-UP RSVR LOW caution also appears:
    • 2. SVO OFF switch - 1ST STG
    • 3. LAND AS SOON AS POSSIBLE
  35. 9.27.7 #2 RSVR LOW and #2 HYD PUMP Cautions Appear w/ BACK-UP PUMP ON Advisory Appearing
    • 1. POWER ON RESET switches - Simultaneously press then release
    • 2. LAND AS SOON AS PRACTICABLE
    • If BACK-UP RSVR LOW caution also appears:
    • 3. SVO OFF switch - 2ND STG
    • 4. LAND AS SOON AS POSSIBLE
  36. 9.27.9 Collective Boost Servo Hardover/Power Piston Failure
    • 1. BOOST switch - Off
    • 2. LAND AS SOON AS PRACTICABLE
  37. 9.28.1 Emergency Landing in Wooded Areas - Power Off
    • 1. AUTOROTATE. Decelerate helicopter to stop all forward speed at treetop level.
    • 2. Collective adjust to max. before main rotor contacts tree branches
  38. 9.28.3 Ditching - Power Off
    AUTOROTATE
  39. 9.29 FLIGHT CONTROL/MAIN-ROTOR SYSTEM MALFUNCTIONS
    • 1. LAND AS SOON AS POSSIBLE
    • 2. EMER ENG(S) SHUTDOWN after landing
  40. 9.30 STABILATOR MALFUNCTION - AUTO MODE FAILURE
    • 1. Cyclic mounted stabilator slew-up switch - Adjust if necessary to arrest or prevent nose down pitch rate
    • 2. AUTO CONTROL switch - Press ON once after establishing a comfortable airspeed.
    • If automatic control is not regained:
    • 3. MAN slew stabilator - Adjust to 0 for flight above 40 KIAS or full down when airspeed is below 40 KIAS
    • 4. LAND AS SOON AS PRACTICABLE
    • If manual control is not possible:
    • 5. STAB POS indicator - Check and fly at or below KIAS LIMITS shown on placard.
    • 6. LAND AS SOON AS PRACTICABLE
  41. 9.31 UNCOMMANDED NOSE DOWN PITCH ATTITUDE CHANGE
    • 1. Cyclic - Adjust as required
    • 2. Collective - Maintain or increase
    • 3. Cyclic mounted stabilator slew-up switch - Adjust as required to arrest nose down pitch rate
    • 4. MAN SLEW switch - Adjust to 0 at airspeeds above 40 KIAS and full down at airspeeds below 40 KIAS
    • 5. LAND AS SOON AS PRACTICABLE
  42. 9.31 UNCOMMANDED NOSE UP PITCH ATTITUDE CHANGE
    • 1. Cyclic - Adjust as required
    • 2. Collective - Reduce as required
    • 3. MAN SLEW switch - Adjust to 0 at airspeeds above 40 KIAS and full down at airspeeds below 40 KIAS
    • 4. LAND AS SOON AS PRACTICABLE
  43. 9.3d. EMER ENG SHUTDOWN
    • 1. PCL(s) - OFF
    • 2. ENG FUEL SYS selector(s) - OFF
    • 3. FUEL BOOST PUMP CONTROL switch(es) - OFF
    • If TGT is above 538C after shutdown:
    • 4. AIR SOURCE HEAT/START switch(es) - As required
    • 5. ENGINE IGNITION switch - OFF
    • 6. Starter button - Press to motor engine for 30 seconds or until TGT TEMP decreases below 538C
  44. 9.3f. EMER APU START
    • 1. FUEL PUMP switch - APU BOOST
    • 2. APU CONTROL switch - ON

What would you like to do?

Home > Flashcards > Print Preview