B737 AUTOMATIC FLIGHT

After lift-off, the A/T remains in THR HLD until: 400 feet Radio Altitude. 800 feet Radio Altitude. 400 feet Radio Altitude and 18 seconds after lift-off. 800 feet Radio Altitude and 18 seconds after lift-off.

Minimum speed reversion is not available when: The A/T is OFF and the AFDS is in ALT HOLD. The A/T is OFF and after G/S capture. AFDS is in V/S mode. Both A and B.

With the autopilot in CMD and V/S mode engaged, vertical speeds can be selected that command flight toward or away from the selected MCP altitude. True. False.

When control wheel pressure is released during CWS roll operation, the airplane will roll wings level when the bank angle is: 5 degrees or less. 6 degrees or less. 10 degrees or less. 15 degrees or less.

The Automatic Flight System (AFS) consists of: The autopilot flight director system (AFDS). The Control Display Unit (CDU). The autothrottle (A/T). Both A and C.

In normal operation, what provides the A/T system with N1 limit values?. The A/T computer. The AFDS. The FMC. The ADIRUs.

The autopilot cannot be engaged while force is applied to the control wheel: True. False.

Moving the STAB TRIM autopilot cutout switch to the CUTOUT position will disengage the autopilot. True. False.

Trimming the stabilizer with the electrical trim switch on the control wheel with the autopilot engaged, will disengage the autopilot: True. False.

Which mode must be armed before the second autopilot can be selected?. VNAV. VOR/LOC. APP. LNAV.

Which of the following occurs when a TO/GA switch is pressed below 2000 feet Radio Altitude during a single autopilot ILS approach?. The autopilot disengages. The A/T (if armed) engages in GA mode. The A/T (if armed) advances thrust levers to reduced go-around N1. All of the above.

What pitch mode is annunciated after takeoff when the autopilot is first engaged in CMD?. CWS P. MCP SPD. VNAV. V/S.

Is CWS an autopilot mode of operation?. Yes. No.

The airplane is in level flight with ALT HOLD engaged. Changing the MCP altitude by more than 100 feet from current altitude arms the V/S mode: True. False.

Level change used for automatic climbs and descents to a pre-selected altitude in the IAS/MACH display is on. The CDU. The MCP. The A/T Computer. D A and C.

With VNAV engaged, the AFDS pitch and A/T modes are commanded by the: MCP. FMC. FCC. GPWS.

If the pilot overrides the autopilot with control column force pitch input, which of the following occurs immediately?. The autopilot engages in LNAV. LNAV disengages. The autopilot changes to CWS P. LEVEL CHANGE annunciates on the FMA.

Which A/T modes permit manual thrust changes without A/T interference. GA and ARM. N1 and ARM. THR HLD and ARM. Only THR HLD.

Engaging LVL CHG or VNAV climb modes automatically engage the A/T in the N1 mode. True. False.

During a dual A/P ILS approach, at which height should the FLARE maneuver start. 300 ft RA. 200 ft RA. 150 ft RA. 50 ft RA.

VNAV is terminated by?. Selecting a different pitch mode. Capturing G/S. Reaching the end of a LNAV route. All of the above.

What is the minimum altitude for selecting CMD on the second autopilot during a dual channel A/P approach?. 2000 RA. 1500 RA. 800 RA. 500 RA.

The ALT HOLD mode of the AFDS is inhibited after the glide slope is captured during an ILS: True. False.

When performing an autopilot ILS approach, the glide slope can be captured from above or below: True. False.

Which statement is true of the autothrottle?. The A/T moves the thrust levers with a separate servo motor on each thrust lever. The A/T will automatically disengage approx. 2 sec after touch down. The A/T will reduce thrust toward idle at 27 feet RA. All of the above.

LNAV automatically disconnects when. The HDG SEL mode is engaged. Upon VOR or localizer capture. Reaching a route discontinuity. All of the above.