T-34C Turbo Mentor — Beechcraft T-34C Turbo Mentor
Fleet & certification
- Built
- 2
- Active
- 1
- Origin
- US
Per-variant specifications
| Variant | Engine | MTOW | Range | Cruise | Pax |
|---|---|---|---|---|---|
T34T T34T | — | 1,900 kg | 700 nm | 246 kt | 2 |
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Beechcraft T-34C Turbo Mentor manuals & documents
9 documents for the Beechcraft T-34C Turbo Mentor — Emergency Procedures · Pilot's Operating Handbook · Checklist · Flight Manual · Specifications · Other Documents. PDFs served from cdn.sprinkle.com.
This document provides critical limitations and operational parameters for the Beechcraft T-34C Turbo Mentor. It is intended for pilots and maintenance personnel to ensure safe and effective operation of the aircraft. The manual covers various aspects including engine performance, airspeed limitations, weight limitations, and other operational limits necessary for flight planning and execution. Pilots will find essential data regarding engine temperatures, torque, fuel flow, and G limits, which are crucial for maintaining the aircraft within its operational envelope.
- Normal operating ITT range: 400-695°C
- Max takeoff weight: 4,400 lbs
- Max clean airspeed: 280 KIAS up to 20,000 feet
- Oil system capacity: 4.4 gallons
- G limits: +4.5/-1.0 G's up to 280 KIAS
Emergency Procedures
Pilot's Operating Handbook
Flight Manual
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