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External Power......................................................................................1-11
Generator Limits...................................................................................1-11
Oxygen System .................................................................................... 1-12
Rudder Boost........................................................................................ 1-12
Spoilers/Autospoilers/Spoilerons ................................................... 1-12
Starter .................................................................................................... 1-12
Thrust Reversers ................................................................................. 1-13
Tires ....................................................................................................... 1-13
Yaw Damper......................................................................................... 1-13
Powerplant Limits.................................................................................. 1-14
Engine Type.......................................................................................... 1-14
Engine Computer ................................................................................ 1-14
Engine Operating Limits (Figure 1-4)............................................... 1-15
Engine Transient Speed Limits.......................................................... 1-16
N1 Limits (Figure 1-5)...................................................................... 1-16
N2 Limits (Figure 1-5)...................................................................... 1-16
Engine Temperature Limits (ITT)...................................................... 1-17
Starting (Figure 1-6)......................................................................... 1-17
Except Starting (Figure 1-7) ............................................................ 1-18
Fuel Limits............................................................................................... 1-19
Fuel Load/Balance .............................................................................. 1-19
Approved Fuels ................................................................................... 1-19
Fuel Additives...................................................................................... 1-19
Anti-Icing Additive ......................................................................... 1-19
Biocide Additive .............................................................................. 1-20
Fueling .................................................................................................. 1-20
Hydraulic Fluid Limits ......................................................................... 1-20
Approved Hydraulic Fluids ............................................................. 1-20
Auxiliary Power Unit (APU) Limits ................................................... 1-21
APU Starter Limits ............................................................................. 1-21
APU Generator Limits ....................................................................... 1-21
Approved Fuels ................................................................................... 1-21
Approved Oils ..................................................................................... 1-21
TFM 2005-14 Page 1 of 1
FAA
APPROVED DATE
for MARGARET KLINE, MANAGER
AIRCRAFT CERTIFICATION OFFICE
FEDERAL AVIATION ADMINISTRATION
WICHITA, KANSAS
TEMPORARY FLIGHT MANUAL CHANGE
Publications Affected: Learjet 40 AFM — FM-132
Learjet 40 AFM — FM-132 (Metric)
Learjet 40 AFM — EASA AFM — FM-132 (EASA)
Learjet 40 Brazilian AFM — FM-132 (CTA)
Learjet 40 Canadian AFM — FM-132 (TCA)
Learjet 45 AFM — FM-126
Learjet 45 AFM — FM-126 (Metric)
Learjet 45 AFM — EASA AFM — FM-126 (EASA)
Learjet 45 Brazilian AFM — FM-126 (CTA)
Learjet 45 Canadian AFM — FM-126 (TCA)
Learjet 60 AFM — FM-123
Description of Change: Adds additional limitation to Icing under the heading
TYPE OF OPERATION.
Filing Instructions: Insert this Temporary Flight Manual Change in the
affected AFMs adjacent to page 1-1 and retain
until further notice.
Add the following paragraph under Icing in TYPE OF OPERATION:
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
　
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