# Beechcraft T-34B Mentor — T-34Btest

> **NOT FOR FLIGHT** — source fidelity: unreviewed | operational review: none | completeness: full

## Beechcraft T-34B Mentor — T-34Btest

> **NOTE:** NAME  :                                            Date:
> **NOTE:** CFI:                                                     Grade:
- [ ] Engine model number is                HP               Max RPM
- [ ] Engine Oil Capacity is
- [ ] Minimum Fuel Octane is
- [ ] Maximum Takeoff Weight is
- [ ] Required Onboard Documents are
- [ ] Main Strut Extension is
- [ ] Maximum Mag. Drop is
- [ ] Best Rate of Climb Airspeed is
- [ ] VNE is
- [ ] Maximum Gear Extension Speed is?
- [ ] Clean Stall Speed is
- [ ] Maximum Gear Retraction Speed is
- [ ] Minimum Oil Pressure is
- [ ] Total Usable Fuel is
- [ ] Maximum Demonstrated Crosswind is
- [ ] Avoid Continuous Engine RPM Operation Between
- [ ] Engine Restart Procedures are
- [ ] Power off Emergency Glide Speed is
- [ ] Prop overspeed procedures are
- [ ] Spin Recovery Procedure is
- [ ] In the Emergency Landing Pattern downwind altitude is
- [ ] At best glide speed, windmilling engine, the T-34 will travel ______
   miles for each 1000 feet of altitude.
- [ ] The basic steps in an engine failure situation are (list 5):

1.

2.

3.

4.

5.
- [ ] The first step in an engine fire emergency is
- [ ] How is an alternator failure detected?
- [ ] What are alternator failure corrective steps
- [ ] Most probable causes for engine roughness are
- [ ] How do you prime the engine?
- [ ] Maximum starter cranking period is
- [ ] Recommend final approach airspeed with flaps full is
- [ ] The landing gear horn will operate if the throttle is reduced below
- [ ] What is the average rate of climb at sea level, 75 deg F, 2985 Lbs?
- [ ] What is the Takeoff Distance, 2985 lbs, 50 deg F, sea level?
- [ ] At max range power setting of 19”/1900 RPM, 5000 ft, max gross wt, what
   is CAS and fuel flow?  ________________  and                     .
- [ ] Determine if the aircraft is within weight and CG limits.

Given:

    Item    Weight     Arm  Moment
    BEW     2236.8     85.6 191470.6
    P/P       180.0      87.0
    Rear Pax       180.0    138.0
    Fuel (50 gal x 6)  300.0        80.0

    Oil     22.5  46.0

Aircraft          within weight and CG limits.
- [ ] Determine the takeoff distance over a 50’ obstacle and liftoff
airspeed.

Given:

    Air Temp:    50 deg F
    Pressure Alt:      sea level
    Weight: 2975 lbs
    Headwinds:   0 kts

Takeoff distance:

Liftoff airpseed:
- [ ] What is the specific range (nm/lb fuel) at 5000 ft, 2775 lbs., TAS
125?

Specific range:
- [ ] Determine landing distance and approach airspeed over a 50’ obstacle.

Given:

    Landing Wt.  2975 Lbs.
    Flaps:  100 % Dn.
    Pressure Alt:      Sea Level
    Headwinds:   Zero

Landing distance:

Approach airspeed:

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NOT FOR FLIGHT — source fidelity: unreviewed | operational review: none | completeness: full  
Source: Beechcraft/T-34B Mentor/T-34Btest.txt  
Rights: licensed  
Checklist hash: 21a2c41db469b915328fcfc83cca5945c9384cb313a8d0b30cca75db8a5d9e2e  
Verify against the aircraft's own approved documentation before use.