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Details airspeed limitations and their operational significance, including VMO, VA, VFE, VLO, VLE, and maximum inertial separator speeds.
Covers engine operating limits, oil specifications, and fuel limitations.
Details weight limits (ramp, takeoff, landing, zero fuel) and center of gravity limits.
Covers maneuver limits, temperature limits, autopilot limits, GPS navigation limits, and icing conditions.
Outlines the procedure for rejecting takeoff for any reason other than engine failure.
Details procedures for engine failures during takeoff and in flight, including oil pressure drops.
Provides procedures and envelope for air starting the engine, with or without starter assist.
Covers procedures for engine fires and cabin fires, both on ground and in flight.
Details procedures for emergency descents in various conditions, including glide distance.
Covers procedures for forced landings, tire blowouts, and landings with unlocked or failed landing gear.
Addresses CAS messages related to fuel pressure and fuel low indications.
Covers CAS messages related to battery overheat, battery off, main generator, and low voltage.
Addresses discrepancies with landing gear extension/retraction and flaps asymmetry.
Lists normal operation airspeeds for various configurations and conditions.
Provides detailed check-list procedures for preflight, engine start, taxiing, takeoff, climb, cruise, descent, landing, and shutdown.
Illustrates the useful cabin pressurization envelope based on cabin altitude and flight level.
Lists stall speeds for various configurations, bank angles, and aircraft weights.
Details engine operating parameters for maximum climb, maximum cruise, and recommended cruise power.
Provides takeoff distances for various weights, altitudes, and temperatures, including corrections.
Details climb speeds, time, consumption, and distance for various conditions.
Details landing distances for various weights, conditions, and runway surfaces, including corrections.
Provides a simple means for pilots to determine aircraft weight and balance.
Describes the electro-hydraulically actuated, fully retractable tricycle landing gear system.
Details the Pratt & Whitney PT6A-64 turboprop engine, including its operation and accessories.
Describes the fuel system components: tanks, fuel unit, selectors, boost pumps, and monitoring.
General| Brand | Daher-Socata |
|---|---|
| Model | TBM 700 B |
| Category | Tools |
| Language | English |
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