Cpt 1-4

Front 1

With flaps extended, a fair amount of stall
warning will exist. The stall is preceded by a mild
buffet approximately _______ knots above the stall,
increasing to strong buffeting at the stall.

Back 1

5 to 10

Front 2

With flaps retracted, the initial buffet occurs at
approximately _______ knots above the stall.

Back 2

10 to 15

Front 3

There is approximately a ______ knot difference in the stalling airspeed depending upon
whether the flaps are extended or retracted. The use of airbrakes has a negligible effect on the stalling
speed but full airbrakes will cause the initial buffet to occur at an airspeed approximately _______ knots higher than if no airbrakes are used.

Back 3

20 to 35; 2 to 4

Front 4

In case a spin is entered accidentally,
apply full opposite ________ immediately followed by
forward ____________ to reduce angle of attack with neutral __________. Apply nose-down _______ and close the _________ if they are extended. Reduce throttles to idle. Extend the gear. To augment the rudder, apply _______ asymmetrically to develop
thrust against the spin. As spin rotation stops, set all throttles in idle and neutralize rudder.

Back 4

rudder; control column; lateral control; trim; airbrakes; throttles

Front 5

Recovery procedures from any stalled condition are standard:

Back 5

stick forward, add thrust, maintain heading with rudder, level wings, recover to level flight with adequate airspeed.

Front 6

More specifically, an unusual
position for this aircraft may be considered as any
attitude or speed which results in inadvertent operation
outside the following limitations:

Back 6

1. An unintentional bank angle greater than 45°.

2. A nose-high attitude greater than that requiredfor a maximum steady climb angle at aircraft gross weights with which the pilot has had flight experience.

3. A nose down attitude greater than that required for the established descent procedures under conditions with which the pilot has had experience.

4. Maximum placard speed or structural load factor limitations for the particular aircraft configuration.

5. Minimum recommended speed.

Front 7

The time required to exceed
placard speeds from cruise Mach number at 30,000 feet at various dive angles is as follows: In a 13° dive, the flutter placard can be exceeded in less than __
seconds. In a 25° dive, the structural placard and the flutter boundary can be exceeded in less than __ seconds. At 45° or more, all placards are exceeded in
less than __ seconds if recovery procedures are not initiated immediately.

Back 7

20; 20; 10

Front 8

Recovery from a nose-high attitude immediately after takeoff can best be accomplished with... full forward control column, retracting
airbrakes if extended, continuous application
of nose-down trim, and maintaining
takeoff thrust and a wings-level attitude.

Back 8

full forward control column, retracting airbrakes if extended, continuous application of ose-down trim, and maintaining
takeoff thrust and a wings-level attitude.

Front 9

The following conditions are the most prevalent causes for unusual positions in the aircraft:

Back 9

1. Pilot disorientation or vertigo
2. Turbulence or weapons effects
3. Improper use or malfunction of airbrakes
4. Improper use or malfunction of stabilizer trim
5. Split flap operation
6. Unscheduled autopilot inputs.

Front 10

When operating without Airspeed indicator: ____% of the aircraft gross weight (clean aircraft) will equal a
safe initial fuel flow setting,

Back 10

5.5

Front 11

It is recommended that engine shutdown and air starting be practiced at altitudes between __________ feet, one engine at a time.

Back 11

10,000 and 40,000

Front 12

Except on engine(s) shutdown for __________, windmilling above ___%rpm, have fuel available to the firewall fuel shutoff valve, push the engine fire shutoff switch in, and advance the throttle to IDLE for ___ minutes out of every hour to prevent overheating the fuel control unit

Back 12

fire or fuel leak; 25; 3

Front 13

If engine is not restarted and windmilling above ___% RPM, have fuelrouted to the engine and advance the throttle to IDLE for ___ minutes out of
every hour to prevent overheating the fuel control unit.

Back 13

25; 3

Front 14

Starts made at an rpm below ___% are termed “airstarts.”

Back 14

65

Front 15

To obtain a relight, retard the
throttle to _____ and place the starter switch to _____. Do not place the starter switch to START at engine rpm below ___% without following the complete procedure because engine fire or damage can result from accumulation of fuel in the engine.

Back 15

IDLE; START; 65

Front 16

Open throttle to IDLE until stable fuel flow (________ PPH) is established. This normally requires
___ seconds, but may require repeat attempts depending on the amount of air in the system. This T.O. allows continuous windmilling with throttle at idle for up to __ minutes for cooling of the fuel control unit. With stable fuel flow, retard throttle to CLOSED for __ seconds to purge the fuel control unit of air and the engine of fuel.

Back 16

550 to 1200; 30; 3; 30

Front 17

When above _____ feet and operating on any fuel other than ____________, set the FUEL ENRICHMENT VALVE switch to ON.

Back 17

15,000; JP-4 or AVGAS

Front 18

IDLE position may not control fuel flow sufficiently to prevent an overtemperature condition between light-up and idle rpm. The ________
should be monitored closely and regulated by manipulation of the throttle as necessary until the desired power setting is restored.

Back 18

EGT and fuel flow

Front 19

during flight, if the system (ignition system) has not been energized,
ignition may be used continuously for a period of __ minutes or in excess of this period during emergencies. The system should not be energized longer than
necessary, but with __ minutes or more of continuous operation, the ignition system will be turned off
for a cooling period of at least __ minutes.

Back 19

10

Front 20

The NORM light at the pilot’s station indicates selection of ____ pitch/roll data for the pilot’s ADI and for the pitch and roll bars on the
pilots EVS monitor. The NORM light at the copilot’s station indicates selection of ______ pitch/roll data for the copilot’s ADI and EVS monitor.

Back 20

AHRS; MD-1

Front 21

The bleed selector switch should be returned to NORMAL LH INBD
position before descending below _________ feet. Excessive duct temperatures may result if this operation is not accomplished.

Back 21

25,000

Front 22

Do not depressurize until all crewmembers are on oxygen and the aircraft is _________ feet or below.

Back 22

42,000

Front 23

When fighting a fire with the fire extinguisher, remember when using the HALON 1211, the fumes from the decomposed products are _____. A noxious, irritating atmosphere will be present with its use when the agent is used on the open fire source and burning material. The supply of extinguisher agent is depleted in approximately ________ seconds of continuous use. Because of the HALON’s effectiveness, short bursts of _____ seconds should be used to fight small localized fires.

Back 23

toxic; 12 to 15; 2 to 3

Front 24

When using a portable oxygen bottle during firefighting, the regulator setting will be ___ or higher, commensurate with aircraft altitude. This setting should be used where there is the possibility of heavy concentrations of fumes. The supply in the portable oxygen bottle will last a minimum of __ minutes depending on...

Back 24

30M; 4; regulator setting, cabin altitude, and physical activity.

Front 25

In the event of fire in forward wheel well area, the jettisoning of an escape hatch will cause smoke and flames to be drawn into the crew compartment. In the event of fire in crew compartment, the jettisoning of an escape hatch
will rapidly intensify and spread the smoke and flames throughout the
crew compartment. Therefore, the jettisoning of an upward escape hatch
prior to the egress of all lower deck members and extra crewmembers could seriously hamper their escape. In this event, the revised order of bailout would be:

Back 25

N, EXTRA CREWMEMBERS, RN, G, EW, CP, and P.

Front 26

When the aircraft is below _____ feet above the terrain or if aircraft control is lost above ______ feet AGL, crewmembers occupying
ejection seats should eject immediately upon receiving the bailout command by either
interphone or abandon signal.

Back 26

2000; 15,000

Front 27

Eject immediately if control is lost below _______ feet AGL

Back 27

15,000

Front 28

Ejection should be accomplished while
the aircraft is in a positive climb and while the airspeed is above ____ knots IAS.

Back 28

120

Front 29

Under level flight conditions, eject at least ______ feet above the terrain whenever possible.

Back 29

2000

Front 30

Under spin or dive conditions, eject at least _______ feet above the terrain whenever possible.

Back 30

15,000

Front 31

Do not delay ejection to below _____ feet above the terrain in futile attempts to start engines or for any other reason that may commit you to an unsafe ejection or a dangerous
landing. Accident statistics emphatically show a progressive decrease in successful ejections as altitude decreases below
______ feet above the terrain.

Back 31

2000; 2000

Front 32

• If parachute automatic opening device has obviously failed,...

• Manually pull ripcord T-handle to open automatic parachute for all ejections below ______ feet.

Back 32

pull ripcord T-handle manually to open the parachute;

14,000

Front 33

Maximum airspeeds for manual bailout from the navigator’s escape hatch are ___ knots IAS for gear down and ___ knots IAS for gear up. Bailout from the escape hatch at higher airspeeds could result in fatal injuries.

Back 33

250; 275

Front 34

Bailout should be conducted in the following order: ____________ for controlled bailout

Back 34

N, IN, DI, 10th, IP, G, EW, RN, CP, P

Front 35

The minimum safe altitude for non-ejection bailout is ____ feet above the terrain.

Back 35

500