Dash 1 Section 5

Question 1

What do red markings on the instruments indicate?

Answer 1

Limit above or below which continued operation is likely to cause damage or shorten operating life.

Question 2

What do green and white markings indicate on the instrumentation?

Answer 2

Safe and normal operation

Question 3

What do amber markings indicate on the instrumentation?

Answer 3

Range at which special attention should be given to the operation covered by the instrument.

Question 4

Do not connect external power…?

Answer 4

If the battery reads below 22.0 V.

Question 5

Connect external power if…?

Answer 5

The battery reads between 22.0 and 23.5 V.

Question 6

D.C. Voltage goes amber and red when what limits are exceeded respectively?

Answer 6

Amber: 29.6-32.2 V; below 22.0 V
Red: 32.3 V and above

Question 7

IDLE torque is normally at what?

Answer 7

1-10% (ground)

Question 8

Ground ops with 106-110 deg C oil temperature is permissible when?

Answer 8

When at and below 20% torque.

Question 9

What are the generator limitations?

Answer 9

+50 to -2 Amps

Question 10

The propeller overspeed limit is what? Don’t think governor limits.

Answer 10

110% Np

Question 11

VMo is what up to what altitude?

Answer 11

316 KIAS up to 18,769’ MSL

Question 12

What are the turbulent air penetration airspeed limits?

Answer 12

195 KIAS maximum, 180 KIAS recommended.

Question 13

What is the operating maneuvering speed (Vo)?

Answer 13

Speed at which full or abrupt control movements in one axis can result in structural damage to the aircraft. It’s 227 KIAS but full rudder deflection above 150 KIAS will exceed the rudder control system limits.

Question 14

Due to gage tolerances the aircraft may be at zero G with gage readings from what to what?

Answer 14

+0.25 G to -0.25 G

Question 15

Allowable aft CG limit for aircraft at all weights is what?

Answer 15

26% MAC

Question 16

What is the maximum ramp weight?

Answer 16

6550 lbs

Question 17

What is the maximum takeoff weight?

Answer 17

6500 lbs

Question 18

What is the maximum landing weight?

Answer 18

6500 lbs.

Question 19

What is the maximum zero fuel weight?

Answer 19

5500 lbs.

Question 20

What is the maximum total weight of bags and pubs on the glareshield?

Answer 20

8.5 lbs

Question 21

Maximum rate of descent at touchdown is what when main tires are serviced to 185+/-5 lbs? 225+/-5 lbs?

Answer 21

600 fpm (3.7 G's)
780 fpm (5.1 G's)

Question 22

Aerobatics after an icing encounter are prohibited and maneuvers are limited to what?

Answer 22

30 deg bank angle, 0-2 G’s

Question 23

During landing phase final approach speed must be increased by how much?

Answer 23

10 knots.

Question 24

Engine operation using only the engine-driven high pressure fuel pump is limited to what?

Answer 24

10 hours.

Question 25

Ground operation during ambient temperatures exceeding 43 deg C is permitted for up to what?

Answer 25

Up to 15 minutes for the purpose of taxiing the aircraft to park.

Question 26

When the aircraft is stored in temp of 35 deg C or more what limitations apply?

Answer 26

Storage time: Greater than 15 min
Canopy: closed
Sunshields: not installed, canopy open 1 hr before engine start
Sunshields: installed, canopy open 15 min before engine start
Storage time: no limit
Canopy: on prop strut
Sunshields: not installed, canopy open 15 min before engine start
Sunshields: installed, no requirement
If canopy fully open, no requirement for flight

Question 27

Ejection seat pilot weight limits are what with equipment and flight gear?

Answer 27

121-271 lbs or 131.8-265.4 lbs

Question 28

Ejection seat nude body weight limits are what?

Answer 28

103-245 lbs. Increased spinal injury risk for less than 103 lbs; increased injury risk during landing for more than 245 lbs and 0/0 capability degraded or lost.