T-6 Annunciators (Caution)

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Author:
C17FLYR
ID:
43978
Filename:
T-6 Annunciators (Caution)
Updated:
2010-10-21 10:40:05
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Description:
AMBER (Caution) Annunciators
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  1. CKPT ALT cause
    cockpit pressure altitude above 19,000 feet
  2. CKPT ALT procedure
    • 1. OBOGS - MAX (as required)
    • 2. Descend below 25,000 feet MSL
    • 3. Bleed air inflow switch- HI
    • 4. Land as soon as practicalIF COCKPIT ALTITUDE EXCEEDED 25,000 FEET MSL
    • 5. Land as soon as possible
  3. DUCT TEMP cause
    Enviornmental duct or defog duct above 300 F
  4. DUCT TEMP procedure
    • 1. Cockpit temperature controller - Move toward MANUAL COLDIF CONDITIONS PERSIST
    • 2. Defog switch - OFFIF CONDITIONS PERSIST
    • 3. Bleed air inflow switch - OFF
    • 4. Descend - Below 25,000 feet MSL
  5. HYDRO FL LO cause
    HYD reservoir fluid level below 55 cubuic inches (1qt)
  6. HYDRO FL LO procedure
    • 1. Hydraulic pressure - Check
    • 2. Airspeed - 150 KIAS or below
    • 3. Landing gear handle - Down
    • 4. Flaps - Extend (As required)
    • 5. Land as soon as practical
  7. BUS TIE cause
    Bus tie switch open, or bus tie failure
  8. BUS TIE procedure
    • 1. Bus tie switch - NORMIF BUS TIE ANNUNCIATOR REMAINS ILLUMINATED
    • 2. Land as soon as practical
  9. FUEL BAL cause
    Fuel imbalance exceeds 30 lbs, or fuel probe fail
  10. FUEL BAL procedure
    • 1. Fuel gages - Verify imbalance and check for fuel leaks
    • 2. Fuel imbalance switch - MAN/RESET (M FUEL BAL annunciator illuminates)
    • 3. Manual fuel balance switch - To low tank
    • 4. Fuel gages - Monitor
    • 5. Manual fuel balance switch - OFF, when imbalance is corrected
    • 6. Fuel balance switch - AUTO, if desiredIf system is returned to autobalance, monitor for correct operation
  11. EHYD PX LO cause
    Emergency hydraulic pressure at or below 2400 psi
  12. EHYPD PX LO procedure
    • 1. Hydraulic pressure - Check
    • 2. Airspeed - 150 KIAS or below
    • 3. Landing gear handle - Down
    • 4. Flaps - Extend (As required)
    • 5. Land as soon as practical
  13. OBOGS TEMP cause
    OBOGS temperature above 200 F
  14. OBOGS TEMP procedure
    • 1. Green Ring - PULL (as Required)
    • 2. OBOGS - OFF (BOTH)
    • 3. Descend - Below cabin altitude of 10,000 feet
    • 4. Land as soon as practical
  15. TAD FAIL cause
    Rudder trim aid device failure
  16. TAD FAIL procedure
    • 1. AHRS/TAD circuit breaker (right console) - Pull and reset
    • 2. TAD switch - Engage after TAD FAIL annunciator extinguishes
  17. L FUEL LO cause
    R FUEL LO
    cause
    Left/Right wing tank below 110 lbs usable fuel
  18. PMU STATUS cause
    PMU has detected and accommodated a fault in-flight or WOW switch failure
  19. PMU STATUS procedure
    • ON GROUND:
    • 1. PMU switch - OFF, then NORMIf PMU STATUS annunciator remains illuminated, confirm source of fault prior to flight
    • INFLT:
    • 1. The PMU has detected a discrepancy in the weight on wheels switch. A reset is not possible.

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