Props and drops (Propeller and Fuel)
Comfort (ECS, OBOGS and Canopy)
Engine and Electrical System
SA (Communication, Navigation, Instrument and TAS)
Ancillardeez (Hydraulics, landing gear, and ancillaries)
100

Fuel PX is triggered when fuel pressure drops below how much psi in the motive supply line?

10 psi

100

Except for air conditioning, no ECS systems will function when this switch is OFF.

BLEED AIR INFLOW switch

100

An 80% charge on the main battery ensures how many minutes of useful power with the BUS TIE open?

30 minutes

100

The Harvard is equipped with this mode of transponder.

Mode S Transponder

100

EHYD PX LO will illuminate when the hydraulic pressure in the emergency accumulator drops below this amount of pressure?

2400 psi, ± 150 psi

200

The propeller is a constant speed, variable pitch, ________, feathering propeller.

non-reversing

200

Setting the PRESSURIZATION switch to RAM/DUMP is the only method for allowing ram air, or ambient air, into the cockpit above what altitude?

7,500 ft

200

Exhaust gas from the engine augments the thrust produced by the propeller by adding up to how much thrust?

70 pounds (lb) of thrust

200

The GPS can store up to 25 flight plans with up to how many waypoints in each flight plan?

30 waypoints

200

What button allows the landing gear handle to be raised on the ground.

Downlock Override button

300

With the PMU functioning, the mechanical overspeed governor in the PIU attempts to limit Np below ___?

106%

300

The amber DUCT TEMP annunciator illuminates if the system detects an air temperature above which temperture?

149°C or 300°F

300

A voltage sensor protects the aircraft from over-voltage. If the external voltage level exceeds ____, external power will be disconnected from the Electrical System.

29.2 VDC

300

Do this on the VHF Backup Control Unit to automatically select the VHF emergency frequency of 121.5 MHz

Press and hold the frequency transfer button for 7 seconds

300

Normal gear extension and retraction of the landing gear takes approximately how long to complete?

6 seconds

400

When the propeller de-ice system is activated, the de-ice boots will operate for __ seconds of operation. The elements in the de-ice boots are then de-energized for__ seconds.

90, 90

400

The red OBOGS FAIL annunciator illuminates on the Main Annunciator Panel approximately how long after the oxygen concentration falls below normal?

20 to 30 seconds

400

What is the normal operating range of the gas generator turbine?

60% - 104%

400

The AHRS has two modes. Slaved and Directional Gyro (DG). In DG mode, how is the compass reference selected?

manually by the pilot

400

Apart from manually retracting the speed brake with the speed brake switch, what are all the other possible methods to retract the speed brake ?

Moving the flap selector out of the UP position and moving the PCL to the MAX position.

500

If the middle fuel probe in a tank were to fail, the indicated fuel level in that tank would be approximately how much?

308 +/- 50 lb

500

Which ECS switch is powered by the hot battery bus?

RAM AIR FLOW Switch

500

Should IOAT and ITT indications be invalid during high temperature operations, what action should be taken?


the PMU should be reset.

500

In the Harvard, the sensitivity level of the TAS is determined by the position of the landing gear. When landing gear is extended, what is the condition for issuance of traffic advisory of Non-Altitude Reporting (NAR) Intruders?

Non-Altitude Reporting (NAR) Intruder is within 15 seconds or 0.20 NM range.

500

With a landing gear malfunction, there is a set of circuit breakers to check if the gear does not appear visually down and safe gear indications are not obtained. Which of these circuit breakers are only in the aft cockpit?

INST LT circuit breaker