Engine malfunctions and situations which may require precautionary approach

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UJPT, E2-C2, ADV, & IUT EMFP-03

Engine and Hydraulic Emergency Procedures

PROGRESS CHECK

Question 4 -- 1.8.1.5.4.2

What are the before-landing emergency procedures for

HYD 1 pump failure?

ANSWER:

1. Landing gear - EMERGENCY EXTEND

2. Emergency flap switch - DOWN

3. Anti-skid switch - OFF

4. Brakes - DO NOT TEST

5. Make short-field arrested landing, if available

Question 5 -- 1.8.1.5.9.2

At what HYD 2 pressure will the RAT extend?

ANSWER:

1,500 psi

III. Engine malfunctions and situations which may require

Sg 3, fr 2

precautionary approach 1.8.1.1.4.2, 1.8.1.1.7.2

Lesson Organization

EGT/RPM malfunctions (in flight)

Sg 3, fr 3, 4

RPM Malfunction

Indications

Sg 3, fr 5, 6

MSTR ALERT light flashes and warning tone

EGT Malfunction

sounds

EGT/RPM warning light illuminates

EGT gauge indicates out of limit condition

N2 RPM gauge exceeds 104%

NOTE: The EGT/RPM light will illuminate in-

flight if either of the following occur: transient/

acceleration to 112.4 + 1% N1 rpm - EGT

exceeds 650 + 8o C.

(9-98) Original

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