Operation Limits; Maneuver Limits; Temperature Limits; Flight Load Factor Limits - Daher-Socata TBM 900 Pilot's Information Manual

PILOT'S OPERATING HANDBOOK

2.6 - OPERATION LIMITS

MANEUVER LIMITS

This airplane is certified in the normal category.
The normal category is applicable to airplanes intended for non-aerobatic operations.
Non-aerobatic operations include any maneuvers incidental to normal flying, stalls (except whip stalls), lazy eights,
chandelles, and steep turns in which the angle of bank is no more than 60°.
Aerobatic maneuvers, including spins, are not approved.

TEMPERATURE LIMITS

Minimum temperature at start and takeoff : - 40°C (- 40°F)
Maximum temperature at start and takeoff :
ISA + 37°C (+ 67°F) from 0 to 8000 ft pressure altitude
Maximum temperature in flight :
ISA + 37°C (+ 67°F) from 0 to 8000 ft pressure altitude
ISA + 30°C (+ 54°F) above 8000 ft pressure altitude

FLIGHT LOAD FACTOR LIMITS

Flaps up
Weight below 6579 lbs (2984 kg) :
≤ n ≤ + 3.8 g
- 1.5
Weight above 6579 lbs (2984 kg) :
≤ n ≤ + 3.5 g
- 1.5
Flaps down
≤ n ≤ + 2.0 g
- 0

GENERATOR LIMITS

Generator load has to be below 200 amps when the airplane is on the ground.
Edition 0 -- October 31, 2013
Rev. 1
INTENTIONAL NEGATIVE LOAD FACTORS PROHIBITED
CAUTION
SECTION 2
LIMITATIONS
EASA Approved
Page 2.6.1