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General| Manufacturer | Daher-Socata |
|---|---|
| Service ceiling | 9, 144 m (30, 000 ft) |
| Model | TBM 700 |
| Type | Single-engine turboprop |
| Engine | Pratt & Whitney Canada PT6A-64 |
| Seating Capacity | 6-7 |
| Maximum speed | 600 km/h (370 mph, 320 knots) |
Table showing VMO, VA, VFE, VLO, VLE, and inertial separator operating speeds in KCAS and KIAS.
Engine operating limits for takeoff and continuous operations, including ITT, oil pressure, and fuel limitations.
Specifies maximum ramp, takeoff, landing, and zero fuel weights, and center of gravity limits.
Step-by-step procedure for rejecting takeoff for reasons other than engine failure.
Procedures for engine failure during takeoff (before rotation, after rotation) and during flight.
Details on air start envelope and procedures for starting with or without starter assist.
Procedures for engine fire on ground/in flight, cabin fire on ground, and smoke elimination.
Procedures for emergency descents in smooth or rough air, and glide distance considerations.
Procedures for forced landing, tire blowout, unlocked/defective landing gear, gear up landing, and ditching.
CAS messages related to fuel pressure, auxiliary boost pump, low fuel, and auto selection.
CAS messages for battery overheat, battery off, main generator, low voltage, and electrical distribution.
Procedures for cabin differential pressure, cabin altitude, cabin not depressurized, bleed off/temp, door, and vacuum low issues.
Procedures for discrepancies when landing gear goes up or down, and flaps asymmetry.
Detailed preflight inspection checklist for inside and outside the airplane, as well as before/after engine start and taxiing procedures.
Table of stall speeds in KIAS, KCAS, and MPH for different configurations and bank angles.
Tables providing torque settings for maximum climb, maximum cruise, and recommended cruise power based on OAT and flight level.
Takeoff distances for different weights, pressure altitudes, temperatures, and runway conditions.
Landing distances for different weights, pressure altitudes, temperatures, and runway conditions.
Methods for determining weight and balance using graphs, including airplane basic characteristics and foreseen loading.
Description of roll, roll trim, elevator, pitch trim, rudder, and rudder trim controls.
Details on the electro-hydraulically actuated, fully retractable tricycle landing gear system.
Description of the Pratt & Whitney Canada turboprop engine, its operation, controls, and accessories.
Overview of the fuel system components, fuel tanks, fuel unit, and tank manual selector.
Procedures for emergency oxygen system use, warnings, and passenger mask repacking instructions.
Emergency procedures for inconsistent display between SVS and primary flight instruments.
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