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Details

53 EP Indications
emergency procedure indications
21
Aviation
Professional
07/19/2014

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Cards

Term
SINGLE- OR DUAL-ENGINE FAILURE
Definition
All parameters decreasing and Nf -Nr split
Term
COMPRESSOR STALL
Definition
AFF ENG: T5 increase — All other parameters decrease

NORM ENGINE: All parameters increase except for steady Nf/Nr.

(As long as the affected engine is producing any usable torque, Nf will remain matched with the normal Nf/Nr. If torque drops to zero, Nf will likely split off and decay.)
Term
ENGINE POWER LOSS (FLAME OUT)
Definition
SYMPTOM: All engine parameters decreasing.

(if producing some torque- Nf/Nr will remain matched
Term
ENGINE OVERSPEED
Definition
SYMPTOM-All parameters increasing, fuel flow may jump to 1,700 pounds or more.
Term
POWER TRAIN FAILURE
Definition
SYMPTOM: (FAIL BETWEEN Nf AND NGB)
a.Sudden decrease to zero on Nf and torque indicators.
b. Ng and T5 increasing until overspeed system actuation, then T5 decreasing and Ng decreasing to flight idle.
c. Grinding/howling noise may be heard.

FAIL OF TRANS -a. Ng, T5 — Decrease.
b.Nf — May increase to overspeed cut in (110% ±2%), then decrease with Ng stabilizing at flight idle speed.
c.Torque — Decrease to zero.
Term
Engine Postshutdown Fire
Definition
Indications would be a rise in T5 above 320 _C after shutdown and/or excessive smoke from the engine exhaust outlet.
Term
Hydraulic Fire in Main Rotor Pylon
Definition
indicated by white smoke and/or flames in the vicinity of the main transmission and/or by illumination of a number of unassociated caution lights.
Term
Utility Hydraulic System Failure
Definition
(1) The UTIL HYD PRESS gauge on the instrument panel, redlined at 2,600 psi minimum or 3,300 maximum;
(2) the UTILITY PRESS caution light that goes on when hydraulic pressure drops below 1,500 psi;
(3) the UTILITY OIL HOT caution light that goes on when the hydraulic fluid temperature rises to 107 _C; and
(4) the UTILITY QTY T/R caution light that goes on when reservoir quantity drops to an unsatisfactory level.
Term
Flight Control Hydraulic System Failure
Definition
1) 1ST and 2ND STAGE HYD PRESS gauges on the instrument panel redlined at 2,600 psi minimum or 3,300 psi maximum,
(2) the 1 STG PRESS M/R T/R and 2 STG PRESS M/R caution lights that go on when pressure drops below 2,000 psi,
(3) the 1 STG QTY M/R T/R and 2 STG QTY M/R caution lights that go on when reservoir fluid quantity drops to an unsatisfactory low level, and
(4) the 2 STG OIL HOT caution light that goes on when the second stage hydraulic fluid temperature rises to 107 _C.
Term
Primary Tandem Servo Malfunction
Definition
1 STG M/R SERVO BYPASS or 2 STG M/R SERVO BYPASS caution lights that go on when a servo has malfunctioned in such a manner to cause it to bypass hydraulic pressure or it has lost system pressure.
Term
Tail Rotor Tandem Servo Malfunction
Definition
1 STG T/R SERVO BYPASS and 2 STG T/R SERVO BYPASS caution lights that go on when the servo has malfunctioned in such a manner to cause it to bypass hydraulic pressure or it has lost system pressure.
Term
Main Gearbox Failure
Definition
abnormal noise/ may also be indicated by an unusual yaw kick accompanied by fluctuations in the torquemeters.
Term
Main Gearbox Chip Locator Light
Definition
When the CHIP DETECTED caution light is accompanied by the MAIN GB chip locator light on the chip locator panel, progressive failure of the main gearbox may be occurring.
Term
Main Gearbox Oil System Failure
Definition
f the MGB OIL PRESS and the MGB AUX lube pump caution lights both illuminate and the MGB oil pressure drops rapidly or decreases below minimum, the main gearbox has lost all means of lubrication
Term
Free Wheeling Unit Failure
Definition
Nf to exceeds Nr
Term
Nose Gearbox Failure
Definition
1. abnormal noise or change in noise frequency.
2.A malfunction that would cause a binding or restriction within the gearbox will cause a high engine torque reading to be observed.
3.A malfunction that would cause a no-load condition on the engine should produce a tendency for the engine to overspeed
Term
Nose Gearbox Chip Locator Light
Definition
CHIP DETECTED caution light is accompanied by either of the nose gearbox chip locator lights,
Term
Nose Gearbox Oil System Failure
Definition
indicated by the nose gearbox oil temperature gauge and oil temperature and pressure caution lights.
Term
Intermediate or Tail Gearbox Failure and Chip Light
Definition
chip light and the TGB/IGB OIL PRESS caution lights
Term
ENGINE CHIP LOCATOR LIGHT
Definition
An engine chip locator light accompanied by unusual vibrations and/or low oil pressure/high oil temperature, or an engine chip locator light returning after resetting circuit breaker
Term
AGB Fail
Definition
Indicated by abnormal noise and loss or malfunction of AGB systems (1&3 Gens/ Engine start pump/ AGB oil pump/2nd stage hyd pump/ Utility Hyd pump)
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