Daher-Socata TBM 900 Pilot's Information Manual page 120

PILOT'S OPERATING HANDBOOK
NOTE : This procedure has to be followed in case of any doubt about the gear extension.
Maintain IAS ≤ 150 KIAS
1 - Landing gear control
2 - "LDG GEAR" circuit breaker
3 - Floor hatch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4 - By-pass selector
THE ENTIRE EXTENSION OF THE LANDING GEAR MAY TAKE UP TO 110 CYCLES. IT IS
MANDATORY TO HAVE A CLEAR HARDENING OF THE MANUAL CONTROL AT THE END
5 - Hand pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Press the CAS MASTER WARNING push-button to reset the
If "GEAR UNSAFE" red warning light is not illuminated and 3 green lights are illuminated :
Continue flight if necessary at a speed BELOW 178 KIAS, exit and/or remain outside icing conditions.
Land.
DO NOT ENTER ICING CONDITIONS (THIS COULD ADVERSELY INCREASE DRAG AND
WEIGHT DUE TO ICE ACCUMULATION, AND LOCK WHEELS AND STRUTS).
INDICATED CRUISE AIRSPEED WILL BE REDUCED COMPARED TO A CLEAN
THIS SHOULD BE TAKEN INTO ACCOUNT WHEN CALCULATING THE AIRPLANE
Edition 0 -- October 31, 2013
Rev. 1
EMERGENCY GEAR EXTENSION (1/2)
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OF THE MANEUVER
CLIMB PERFORMANCE WILL BE DEGRADED BY 50 %.
AIRPLANE, BECAUSE OF THE DRAG.
EMERGENCY PROCEDURES
CAUTION
ACTUATE with maximum amplitude
"GEAR UNSAFE"
CAUTION
RANGE.
SECTION 3
EASA Approved
DN
PULL
OPEN
FULLY PULL / LOCKED
CAS message.
Page 3.5.3