曝光台 注意防骗
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10° C/50° F or below and:
· Visible moisture (clouds, fog with visibility less than one mile, rain,
snow, sleet, ice crystals, and so on) is present, or
· Standing water, ice, slush or surface snow is present on the ramps,
taxiways, or runways which may be ingested by the engines or freeze
on engines or nacelles
Limitations
1. If the aircraft has been deiced:
The control column will be smoothly and slowly cycled from the full aft to the
full forward position a minimum of three times to minimize the residual fluids
in the balance bay during flight.
2. BC Per Airworthiness Directive 2002-08-20 / AMOC 120S-02-907:
“After ground deicing / anti-icing of the horizontal stabilizer using Type II or
Type IV fluids, airspeed must be limited to 270 KIAS until the flight crew has
been informed that applicable maintenance procedures have been
accomplished that would allow exceedance of 270 KIAS. Once the applicable
maintenance procedures have been accomplished, exceeding 270 KIAS is
permissible until the next application of Type II or Type IV deicing / anti-icing
fluids.”
Note:
· Aircraft is restricted to a maximum of 270 KIAS after using Type II or
Type IV fluid application. No MACH restriction.
· Flight Plan Release (amended if required) displays 270-knot restriction.
· Restriction remains in effect for all flights until elevator tab surfaces are
cleaned of Type II and Type IV fluids.
· It has been determined that Type I fluid does not affect the flight controls
of the aircraft. If only Type I fluid is used for deicing / anti-icing, the
speed restriction is not applicable.
Caution: Flight Crews will evaluate the need to land at the nearest suitable
airport if in-flight vibrations (ELEVATOR TAB LIMIT CYCLE
OSCILLATION) occur as a result of de-icing.
Sec. 1 Page 18
Rev. 11/15/02 #41 Continental
737
Flight Manual
3. Engine anti-ice:
Must be ON during all ground operations, including after landing, when
icing conditions exist or are anticipated.
Must be ON during all flight operations when icing conditions exist or are
anticipated, except during climb and cruise when the temperature is below
–40°C SAT.
Must be ON prior to and during descent in all icing conditions, including
temperatures below –40°C SAT.
Engine ignition must be selected to CONT prior to and during engine anti-ice
operation.
4. Wing anti-ice:
Must be ON during all ground operations between engine start and takeoff
when icing conditions exist or are anticipated.
Do not operate wing anti-ice on the ground when the OAT is above
10°C/50°F.
Do not use wing anti-ice as a substitute for ground de-icing/anti-icing.
Operating Parameters
1. Do not operate windshield wiper on a dry windshield.
2. Window heat must be ON 10 minutes before takeoff.
3. Pitot heat must be ON prior to takeoff.
4. During takeoff, to meet second segment climb requirements, wing heat
will not be used below 800 feet AGL.
Instrument And Navigation
Limitation
Altitude Display limits for RVSM Operations:
BCD
Standby altimeters do not meet altimeter accuracy requirements of RVSM
airspace.
The maximum allowable in-flight difference between Captain and First
Officer altitude displays for RVSM operations is 200 feet.
737
Flight Manual Continental
Sec. 1 Page 19
Rev. 11/15/02 #41
The maximum allowable on-the-ground display differences for RVSM
operations are:
Field Elevation
Max Difference
Between
Captain & F/O
Max Difference
Between Captain or
F/O & Field Elevation
Sea Level to 5,000 Feet 50 Feet 75 Feet
10,000 Feet 60 Feet 75 Feet
1. Takeoff with the Forward Looking Predictive Windshear Warning Alert
annunciated is not authorized.
Operating Parameters
1. Do not operate weather radar during fueling, near fuel spills, or near
personnel except in test mode.
2. Altimeter differences:
>>@
ALTITUDE ELEC/PNEU ELEC/ELEC
SEA LEVEL
5,000 FEET
10,000 FEET
20,000 FEET
30,000 FEET
40,000 FEET
50 FEET
80 FEET
120 FEET
220 FEET
280 FEET
425 FEET
50 FEET
50 FEET
60 FEET
80 FEET
120 FEET
160 FEET
BCD
ALTITUDE CDS/CDS CDS/STANDBY
SEA LEVEL
5,000 FEET
10,000 FEET
15,000 FEET
20,000 FEET
25,000 FEET
30,000 FEET
35,000 FEET
40,000 FEET
41,000 FEET
50 FEET
50 FEET
60 FEET
70 FEET
80 FEET
100 FEET
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737 FLIGHT MANUAL 737飞行手册1(14)
