ATA 27. FLIGHT CONTROLS (LVL 3)
Nbsp; Content checked IAW course syllabus by responsible examiner: _________________ _____________________ Name Signature/ Stamp Course reference: A320F(CFM56) B1.1 + B2 Training session: 4 ATA Chapters: VAR.1 51-57/29/29A/27/27A/25/25A Exam: X Re-Exam: Candidate`s name: Signature:
ATA 51. Airframe structure (LVL 3)
Which of the fuselage skin panels are made of titanium alloys? 51-010
a. The skin panels which installed just above and below the emergency escape hatches.
b. The skin panels which installed just above the cargo compartments doors.
c. The skin panels which installed just above the cockpit windshields
ATA 52. Doors (LVL 3)
The When the Emergency Control Handle is in the ARMED position, what part of the emergency escape slide release mechanism does fasten the slide? 52-003
a) The girt bar fittings
b) The cam disk
c) The girt bar
The Cargo Doors FWD and AFT... 52-004
a. cannot be opened manually.
b. are hydraulically operated
c. can be opened/closed from inside and outside.
ATA 53. Fuselage (LVL 3)
The keel beam is... 53-016
a. a stainless steel beam.
b. an aluminum alloy box structure.
c. a composite structure
ATA 54. Nacelles/Pylons (LVL 3)
The pylon box is ... 54-014
a.a forward fairing (secondary structure).
b. a primary structure.
c. a aft fairing (secondary structure).
ATA 55. Stabilizers (LVL 3)
Is there any difference between the vertical stabilizer on the A-318 and on other A-320 family aircraft? 55-011
a. Yes, the vertical stabilizer on the A-318 is higher than other ones on A-320 family aircraft.
b. Yes, the vertical stabilizer on the A-318 is shorter than other ones on A-320 family aircraft.
c. No, there are no differences.
ATA 56. Window s (LVL 3)
For what reason the little whole is drilled in the inner pane of the door windows?
56-003
a) For window heating.
b) For window antifogging system.
c) For equalizing the pressure between the panes.
ATA 57. Wing s (LVL 3)
The access for maintenance to the center wing box is ... 57-010
a. done through two triangular openings in the rear spar.
b. access panels between Rib 1 and Rib 3 clamped on the wing skin.
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c. possible only through the outer wing box.
ATA 27A. Flight control surfaces (LVL 3)
How many spoilers used on the airplane as the speed brakes? 27A-027
a. 6
b. 8
c. 10
ATA 29. HYDRAULIC POWER SYSTEMS (LVL 3)
Where is the ground service panel for the Green system located? 29-002
a. Aft of the main landing gear bay on the LH side
b. Aft of the main landing gear bay on the RH side
c. Fwd of the main landing gear bay on the RH side
Which hydraulic system is not powered from engine
a) Yellow and Blue
b) Blue
c) Yellow
When the blue electric pump will run, if one engine is running? 29-003
a.In case of the ELECtric (ELEC) PUMP P/B set to AUTO.
b.In case of the ELECtric (ELEC) PUMP P/B set to OFF.
c.In case BLUE PUMP OverRiDe (OVRD) P/B is set to ON
Which hydraulic systems have engine driven pumps? 29-016
a. Green and yellow.
b. Blue and yellow.
c. Green and blue.
Which of the following requirements must be performed to refill the Yellow hydraulic system reservoir? 29-026
a. The Reservoir Filling Selector on the Green service panel is turned to YELLOW position and hand pump on the Yellow service panel is operated.
b. The Reservoir Filling Selector on the Green service panel is turned to YELLOW position and hand pump on the Green service panel is operated.
c. The Reservoir Filling Selector in the Yellow hydraulic system bay is turned to YELLOW position and hand pump on the Yellow service panel is operated.
The hydraulic hand pump used for the cargo door operation is installed on the... 29-027
a. Green system service panel.
b. Yellow system service panel.
c. Blue system service panel.
When is the PTU operation inhibited?
a. When the aircraft is on the ground.
b. When the cargo door is electro-hydraulically operated only.
c. On the ground when the cargo doors are operated or at one engine start.
ATA 29A. HYDRAULIC POWER SYSTEMS MONITORING and INDICATING (LVL 3)
17.The hydraulic temperature transmitters monitor the hydraulic fluid temperature in the … 29A-003
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a. related hydraulic system pressure line.
b. related hydraulic system return line.
c. related hydraulic system case drain line.
18.Each of three hydraulic systems has a pressure transducer which gives data… 29A-008
a. on the ECAM for pressure indication and sends information to
ELevator Aileron Computers (ELACs) 1 and 2.
b. on the related pressure gage located in the Main Landing Gear wheel well.
c. on the Flight Management and Guidance Computer (FMGC) 1 and 2 for good flight control.
ATA 27. FLIGHT CONTROLS (LVL 3)
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