Block 14 Project 7-P32b
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AVIATION INSTITUTE OF MAINTENANCE
INDUCTION AND EXHAUST SYSTEMS – Block 14
PROJECT 7-P32b
Name: _________________________
Date: _______________
ITEM:
Troubleshoot and repair engine thrust reverser systems, and related
components.
STUDENT PERFORMANCE GOALS
OBJECTIVE:
Understanding of Basic Thrust Reverser Systems
AM.III.L.R2
Operation of turbine engine reversing systems.
AM.III.L.S6
Locate procedures for testing and troubleshooting a turbine thrust
reverser system.
PROCEDURE:
1
.
The student will answer a series of multiple-choice questions and
answers.
The student will select the best answer for each question
and reference where the answer was located.
2.
The student should utilize the following books to complete this project:
FAA-H-8083-32.
3.
Present your completed work to your instructor for evaluation.
SCORING:
ACCURATE ANSWERS
= 50 Points = 5 Each
ACCURATE REFERENCES
= 50 Points = 5 Each
1.
The most successful thrust reversers can be divided into two categories, they are:
a.
Solid Blockage and Porous Blockage.
b.
Convergent Blockage and Divergent Blockage.
c.
Mechanical Blockage and Aerodynamic Blockage.
Reference: _________________
2.
Thrust reverser operation is typically controlled by:
a.
The flight attendant when the plane is too early.
b.
The engine throttle position.
c.
Placing the gearshift in the “R” detent.
Reference: _________________
3.
Some of the most popular “HOT STREAM” thrust reverser systems are:
a.
Clamshell and Bucket Type.
b.
“J” Channel and Pail Type.
c.
Seashell and Cascade Type.
Reference: _________________
Induction & Exhaust Project 7-P32b
03/27/2023
Page 1 of 2
4.
Mechanical blockage is accomplished by placing a removable obstruction in the:
a.
Air ingestion path.
b.
Exhaust gas stream.
c.
Around the brake system.
Reference: _________________
5.
Operating thrust reversers at low ground speeds can sometimes cause:
(1) Sand or other foreign object ingestion.
(2) Hot gas re-ingestion.
(3) Compressor stalls.
a.
1 and 2 are correct.
b.
2 and 3 are correct.
c.
1, 2 and 3 are correct.
Reference: _________________
6.
Most cascade type reverser systems are:
a.
Electrically operated.
b.
Pneumatically operated.
c.
Mechanically operated.
Reference: _________________
7.
What is utilized to prevent inflight activation on some aircraft of the thrust reverser
system?
a.
A key to activate / de-activate the system.
b.
It’s bolted closed by maintenance personnel.
c.
With a landing gear safety switch.
Reference: _________________
8.
To satisfy minimum braking requirements after landing, a reverser should be able to
provide in reverse:
a.
At least 100% of the full forward thrust of which the engine is capable.
b.
At least 75% of the full forward thrust of which the engine is capable.
c.
At least 50% of the full forward thrust of which the engine is capable.
Reference: _________________
9.
Thrust attenuators are utilized on some small corporate aircraft.
They provide:
a.
100% braking ability when activated.
b.
Reduced thrust at idle.
c.
Reduced noise levels for passengers.
Reference: _________________
10.Most thrust reversers in use at this time are combined with:
a.
Noise intensifiers.
b.
Critical airspeed information systems.
c.
Engine exhaust silencers.
Reference: _________________
Induction & Exhaust Project 7-P32b
03/27/2023
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