曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
DC Voltage ........................................................................................ 1-26
DC Amperes...................................................................................... 1-26
Oxygen Pressure...................................................................................... 1-27
Hydraulic Pressure.................................................................................. 1-27
Emergency Air ......................................................................................... 1-27
TFM 2006-02 Page 1 of 1
FAA
APPROVED DATE
for MARGARET KLINE, MANAGER
AIRCRAFT CERTIFICATION OFFICE
FEDERAL AVIATION ADMINISTRATION
WICHITA, KANSAS
TEMPORARY FLIGHT MANUAL CHANGE
Publication Affected: Model 31A FAA Approved AFM (FM-121)
Description of Change: Revises wording of Icing approval.
Filing Instructions: Insert this Temporary Flight Manual Change in the
Limitations Section of the affected AFM adjacent
to page 1-1 and retain until further notice.
Replace existing Icing approval with the following:
• Icing
When icing or frost conditions exist, this airplane must be inspected
and operated in accordance with the Cold Weather Operation
procedures of Section II. These procedures include the
requirement to assure that all critical surfaces of the airplane
(wing, vertical and horizontal stabilizers, flight control surfaces,
spoilers and flaps) are free of frost, ice and snow for takeoff. Conducting
only a visual inspection may not detect very small levels
of contamination; therefore, a tactile (hand on surface) check of
the wing leading edge and adjacent wing upper surface is required
when the ambient temperature is less than 10°C (50°F).
Learjet 31A AFM Limitations
FM-121 1-1
FAA Approved 7-25-91
Change 28
GENERAL
CERTIFICATION STATUS
This airplane is certified in accordance with FAR 25.
TYPE OF OPERATION
This airplane is approved for:
• VFR (Visual)
• IFR (Instrument)
• Day
• Night
• Icing
Icing conditions exist when outside air temperature (OAT) on
the ground and for takeoff is 10°C (50°F) or below, or the static
air temperature (SAT) in flight is 10°C (50°F) to -40°C (-40°F), and
visible moisture in any form is present (such as clouds, fog with
visibility of one mile or less, rain, snow, sleet, or ice crystals).
Icing conditions also exist when the OAT on the ground and for
takeoff is 10°C (50°F) or below when operating on ramps, taxiways,
or runways where surface snow, ice, standing water, or
slush may be ingested by the engines, or freeze on engines, nacelles,
or engine sensor probes.
When icing or frost conditions exist, this airplane must be inspected
and operated in accordance with the Cold Weather Operation
procedures of Section II. These procedures include the
requirement to assure that all critical surfaces of the airplane
(wing, vertical and horizontal stabilizers, flight control surfaces,
spoilers and flaps) are free of frost, ice and snow for takeoff. Conducting
only a visual inspection may not detect very small levels
of contamination; therefore, a tactile (hand on surface) check of
the wing leading edge and adjacent wing upper surface is required
when the ambient temperature is less than 10°C (50°F).
This airplane is not approved for ditching under FAR 25.801.
PERFORMANCE CONFIGURATION
The airplane configuration must be as presented under Standard Performance
Conditions in Section V.
MINIMUM FLIGHT CREW
The minimum flight crew shall consist of pilot and copilot.
Change 28
Limitations Learjet 31A AFM
1-2 FM-121
FAA Approved 7-25-91
Change 17
WEIGHT AND C.G. LIMITS
MAXIMUM RAMP WEIGHT
• Standard .................................................................... 15,750 Pounds
7,144 kg
• Optional .................................................................... 16,750 Pounds
7,598 kg
• Optional .................................................................... 17,200 Pounds
7,802 kg
MAXIMUM CERTIFIED TAKEOFF WEIGHT
• Standard .................................................................... 15,500 Pounds
7,031 kg
• Optional .................................................................... 16,500 Pounds
7,484 kg
• Optional .................................................................... 17,000 Pounds
7,711 lkg
Refer to Takeoff Weight Limit placard installed on
the airplane instrument panel.
MAXIMUM ZERO FUEL WEIGHT ......................................... 13,500 Pounds
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
庞巴迪挑战者手册9(88)
