Installation of handle covers on the overwing exits must be verified prior to departure whenever passengers are carried. T/F?
True
Verify thet an operational check of the flight deck door access system has been accomplished according to approved procedures once each flight day. T/F?
True
Maximum demonstrated T/O and landing crosswind?
33 knots
36 knots (YK007,YL352,YL353)
On revenue flights, the escape slide retention bar (girt bar) must be installed during taxi, takeoff and landing. T/F?
True
Do not operate HF radios during refueling operations. T/F?
True
Does STBY altimeter meet RVSM standards?
No
Max allowable in-flight difference between Captain and FO altitude displays for RVSM operations?
200 ft
Max allowable altitude display difference (for RVSM operations) between Captain and FO on the ground?
SL to 5,000ft elevation - 50 ft
5,001 to 10,000 ft elevation - 60 ft
Max allowable altitude display difference between Captain or FO and Field Elevation on the ground?
75 ft
Max taxi weight?
62,224 kgs
63,225 kgs
70,306 kgs
77,110 kgs
79,227 kgs
79,242 kgs
85,366 kgs
Max T/O weight?
61,998 kgs
62,998 kgs
70,080 kgs
76,883 kgs
79,000 kgs
79,015 kgs
85,139 kgs
Max landing weight?
58,059 kgs
66,088 kgs
66,360 kgs
71,350 kgs
Max zero fuel weight?
54,657 kgs
62,459 kgs
62,731 kgs
67,721 kgs
Max cabin differential pressure?
9.1 psi
With engine bleed air switches on, do not operate the air conditioning packs in ...... for T/O, approach or landing.
HIGH
(The fire protection non-normal checklist overrides this limitation)
Engine TAI must be on when icing conditions exist or anticipated, except during climb and cruise below .......*C SAT.
-40*C
Use of aileron trim with the autopilot engaged is prohibited. True/False?
True
Do not engage autopilot for T/O below ...... ft AGL.
400 ft AGL
For single channel operation during approach, the autopilot shall not remain engaged below ..... ft AGL.
50 ft AGL (FAA)
50 ft below MDA unless it is coupled to an ILS G/S & Localizer or in the go-around mode.
140 ft AGL (JAA)
158 ft AGL (JAA)
140 ft AGL (JAA)
Do not use HDG SEL or CWS north of ........ latitude or south of ......... latitude.
89 degrees 30 minutes
89 degrees 30 minutes
Maximum allowable wind speeds for autoland operations:
FAA
Headwind 25 kts
Crosswind 20 kts
Tailwind 15 kts
JAA
Crosswind 20/25 kts
Tailwind 10/12/15 kts
Max and min G/S angles for autoland?
3.25 degrees
2.5 degrees
Autoland capability may only be used with flaps ..... or ..... and both engines .......... .
30, 40, operative
For airplanes operating under JAA Rules: Autoland capability may only be used with flaps 30 with the one engine operative and only for DH at or above 50 feet.
Do not use IAN FAC or G/P guidance under either of the following conditions:
- The flight crew has entered an AT or AT/BELOW altitude constraint for a FAF, or for waypoints between a FAF and a runway
- Any altitude constraint specified by the approach procedure for a FAF, or waypoints between a FAF and a runway, has been modified by the flight crew, after the aircraft has passed the IAF. T/F?
True
Do not use VHF-3 for ATC communications with ACARS operational. T/F?
True
Flights predicated on the use of following frequencies (MHz) are prohibited.
29.490 and 29.489
Flights predicated on the use of the following HF frequencies are prohibited:
- 11.133Mhz
- 22.434Mhz
- 22.683Mhz
- 22.766Mhz
T/F?
True
The ACARS is limited to the transmission and receipt of messages that will not create an unsafe condition if the message is improperly received, such as the following conditions:
• the message or parts of the message are delayed or not received,
• the message is delivered to the wrong recipient, or
• the message content may be frequently corrupted.
However, Pre-Departure Clearance, Digital Automatic Terminal Information Service, Oceanic Clearances, Weight and Balance and Takeoff Data messages can be transmitted and received over ACARS if they are verified per approved operational procedures. T/F?
True
Use the VHF radio connected to the ..... of fuselage antenna for primary ATC communications on the ground.
top
The use of Flight Deck Auxiliary Power outlets in the flight deck requires operational regulatory approval. T/F?
True
Engine ignition must be on for:
T/O
Landing
Operation in heavy rain
Anti-ice operation
Intentional selection of reverse thrust in flight is ........... .
prohibited
Inflight - APU bleed + electrical load: max altitude?
10,000 ft
Ground only - APU bleed + electrical load: max altitude?
15,000 ft
APU bleed max altitude?
17,000 ft
APU electrical load max altitude?
41,000 ft
APU bleed valve must be closed when:
Gnd air connected and isolation valve open
Eng#1 bleed valve open
Isolation and eng#2 bleed valves open
APU bleed valve may be open during engine start, but avoid engine power above idle.
No cargo may be carried in the cargo compartment if the corresponding cargo fire protection equipment is not operational. T/F?
True
Max flap extension altitude?
20,000 ft
Holding in icing conditions with flaps extended is prohibited. T/F?
True
Do not deploy S/B in flight at radio altitudes less than ..... ft.
1,000 ft AGL
In flight, do not extend S/B lever beyond ........... .
FLIGHT DETENT
Avoid rapid and large alternating control inputs, as they may result in structural failure at any speed, including below VA. T/F?
True
Airplanes operating under JAA rules: Flaps 15 normal landings are prohibited. A Flaps 15 landing may be performed when required by a non-normal procedure. T/F?
True
Alternate flap duty cycle for flap position:
Release-reengage: ......seconds pause
0-15-0 cycle: .......minutes off
15 seconds
5 minutes
ADIRU alignment must not be attempted at latitudes greater than ......... degrees ....... minutes.
78 degrees 15 minutes
QFE operations are prohibited if the option for QFE altitude reference selection is not installed in the Flight Management System (FMS). T/F?
True
The use of Look-Ahead terrain alerting and terrain display functions with the altimeters referenced to QFE is prohibited. T/F?
True
The use of VNAV or LNAV with the altimeters referenced to QFE is prohibited. T/F?
True
Do not use terrain display for navigation. T/F?
True
Do not use look-ahead terrain alerting and terrain display functions within 15 nm of T/O, approach or landing at an airport not contained in the GPWS terrain database. T/F?
True
Do not operate weather radar in hangar or ..... ft of any personnel or fuel spill. (Does not apply with weather test mode)
50 ft
Note:The hangar and personnel restrictions do not apply to the weather radar test mode.
Do not use RAAS callouts or alerts for navigation. T/F?
True
Do not use RAAS callouts or alerts as a substitute for NOTAM or ATIS information. T/F?
True
Maximum tank fuel temperature?
49*C
Minimum tank fuel temperature prior to takeoff and inflight?
3*C above the freezing point of the fuel being used or -43*C, whichever is higher
Note:The use of Fuel System Icing Inhibitor additives does not change the minimum fuel tank temperature limit.
Intentional running of a center tank fuel pump (low pressure light illuminated) is prohibited. T/F?
True
Engaging the auxiliary fuel maintenance (MAINT) sw in flight is prohibited. T/F?
True
The center tank should be used until all aux fuel has been transferred. T/F?
True
Lateral imbalance between main tanks 1 and 2 must be scheduled to be ...... .
Zero
Random fuel imbalance must not exceed ....... kgs for taxi, T/O, flight or landing.
453 kgs
Main tanks 1 and 2 must be full if center tank contains more than ........ kgs.
453 kgs
The center and main fuel tanks must be scheduled to be full if the aux fuel sys is to be loaded or contains fuel. T/F?
True
Operation with assumed temperature reduced takeoff thrust is not permitted with ......... inoperative.
Anti-skid
Airplanes operating under JAA Rules: Towing operations without the use of a tow bar is restricted to tow vehicles that are designed and operated to preclude damage to the airplane steering system or which provide a reliable and unmistakable warning when damage to the steering system may have occurred. T/F?
True
Do not apply brakes until after touchdown. T/F?
True
Author
skartas
ID
7009
Card Set
B737NG THY LIMITATIONS by SKY.txt
Description
B737NG THY LIMITATIONS by SKY (Based on FCOM 737-700/-800/-900ER Rev 8)