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
Do not use the ADF as the sole source for navigation or as a navigation
fix. NDB approaches are not approved.
AIR DATA SYSTEM
Air data systems (ADC 1 and 2) must be selected normal (NORM) for
takeoff.
To assure proper air data system operation, the ADC Check of the Before
Starting Engines procedure must be accomplished in accordance
with Section II, this manual.
Reduced Vertical Separation Minimums (RVSM) — This aircraft has
been shown to meet the airworthiness requirements for operation in
Reduced Vertical Separation Minimum (RVSM) airspace between
29,000 and 41,000 feet inclusive. This does not constitute an operational
approval.
ATTITUDE HEADING REFERENCE SYSTEM (AHRS)
Attitude heading reference systems (AHRS 1 and AHRS 2) must be selected
normal (NORM) for takeoff.
AUTOPILOT/FLIGHT DIRECTOR
Autopilot must be off for takeoff and landing.
Do not intentionally overpower the autopilot.
Autopilot Minimum Use Height:
Climb, En Route or Descent....................................................500 feet AGL
Approach...................................................................................200 feet AGL
Autopilot & Flight director are approved for Category I approaches.
TFM 2003-04 Page 1 of 1
TEMPORARY FLIGHT MANUAL CHANGE
Publication Affected: Learjet Model 45 AFM (FM-126)
Description of Change: Adds operational limitations for precision
approaches.
Filing Instructions: Insert this temporary change in the affected
AFM adjacent to page 1-10, and retain until
further notice.
Erroneous glide slope indications have occurred during ILS
approaches. The anomaly only occurs approaching the outer marker.
The glide slope stabilizes as the signal strengthens just inside the outer
marker.
Add the following limitations to the PRIMUS 1000 INTEGRATED
AVIONICS SYSTEM:
Precision approaches are allowed while adhering to the following:
1. When crossing the Outer Marker on glide slope, the altitude
must be verified with the value on the published procedure.
2. For aircraft with two operating glide slope receivers, the aircraft
may be flown to the published minimums for the approach
using normal procedures if both receivers are tuned to the
approach and both crew members are monitoring the approach
using independent data and displays.
3. For aircraft with single operating glide slope receiver, the
approach may be flown using normal procedures no lower than
Localizer Only Minimum Descent Altitude (MDA).
for RONALD K. RATHGEBER, MANAGER
AIRCRAFT CERTIFICATION OFFICE
FEDERAL AVIATION ADMINISTRATION
WICHITA, KANSAS
Limitations
FM-126 1-11
FAA Approved 5-19-2004
SYSTEM LIMITS (Cont)
PRESSURIZATION
Delta P ..........................................................................+9.9 psid to -0.5 psid
Do not land with the cabin pressurized.
ENVIRONMENTAL CONTROL SYSTEM
HI FLOW must be off with takeoff power selected, or for landing, antiice
operations, and flight above 30,000 ft.
PRIMUS 1000 INTEGRATED AVIONICS SYSTEM
The appropriate Honeywell PRIMUS 1000 Integrated Avionics System for
the Learjet Model 45/40 Pilot’s Manual must be immediately available to
the flight crew. The following table lists the approved manuals:
ENGINE SYNCHRONIZER
ENG SYNC must be OFF for takeoff, landing, and single-engine
operation.
EXTERNAL POWER
The maximum amperage from an external power source must be limited
to 1500 amps.
GENERATOR LIMITS
Generator output is limited as follows:
Ground or Flight Operations
• Continuous — 300 amps.
If more electrical load is applied than can be supplied
by the generators, the current will be drawn
from the aircraft batteries and will not be shown on
the DC amps display. If this occurs, DC voltage will
be reduced.
• Transient — Higher transient loads for cross-starts and battery
charging are authorized.
EFFECTIVITY APPROVED MANUAL
Aircraft 45-002 thru 45-235
Pub. No. A28-1146-106-02 (dated October
2000 or appropriate later revision)
Aircraft 45-236 & subsequent
and prior aircraft modified by
SB 45-22-5
Pub. No. A28-1146-165-XX (dated
March 2003 or appropriate later revision)
NOTE
Limitations
1-12 FM-126
FAA Approved 5-19-2004
SYSTEM LIMITS (Cont)
OXYGEN SYSTEM
The following aircraft certification requirements are in addition to the
requirements of applicable operating rules. The most restrictive requirements
(certification or operating) must be observed.
Hats and “ear-muff” type headsets must be removed
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
Bombardier_Learjet-Limitations(6)
