Temporary Changes Learjet 35A/36A with FC-200
TFM-2 FM-102
6-23-2008
Change 14
84-02
3-15-84
1-3
Maximum zero wing and tip fuel weight
replaces maximum wing bending weight.
Removed by
Chg 5.
85-02
3-8-85
IV Revised FUEL CMPTR light procedure.
Removed by
Chg 6.
85-10
1-3-86
2-2
Engine oil and hydraulic accumulator pre-
flight checks.
Removed by
Chg 6.
85-16
11-8-85
3-5
Current limiter failure procedure associ-
ated with AMK 85-1.
Removed by
Chg 8.
87-05
3-2-87
4-17
Clarify operation of emergency gear
extension valve.
Removed by
Chg 7.
87-06
3-2-87
4-19
Clarify operation of emergency gear
extension valve.
Removed by
Chg 7.
87-15
7-16-87
II
Bleed hydraulic pressure to zero before
setting battery switches off.
Superseded
by TFM 88-17.
88-07
2-13-89
4-29 Pitot-static system malfunction procedure.
Removed by
Chg 7.
88-17
1-17-89
II
Bleed hydraulic pressure to zero before
setting battery switches off.
Removed by
Chg 9.
89-17
11-16-89
4-16
Fuel imbalance during fuel transfer proce-
dure.
Removed by
Chg 9.
92-02
9-10-92
2-16 Clarify the oil pressure annunciator.
Removed by
Chg 10.
93-15
12-3-93
2-35 Cold weather operations.
Removed by
Chg 10.
94-15
1-9-95
1-14
Maximum operating altitude — 41,000 FT.
(When cabin outflow or safety valve has
been replaced between 1-1-89 and 1-9-95)
Active, until
SB 35/36-21-19
is accomplished.
94-23
3-6-95
5-8 Revised noise level compliance statement.
Removed by
Chg 10.
96-08
5-30-96
2-49 Standby fuel pump annunciators.
Removed by
Chg 10.
96-09
5-30-96
4-17
Procedure for standby fuel pump failing
to shut off.
Removed by
Chg 10.
96
-10
7-12-96
1-14
Adds paved runway restriction to limita-
tions section.
Removed by
Chg 10.
99-02
7-16-99
1-18B Revises the list of approved oils.
Superseded by
TFM 99-24.
99-03
4-16-99
1-20
Revises fuel anti-icing additive
limitations.
Removed by
Chg 12.
99-24
11-30-99
1-18B Revises the list of approved oils.
Superseded by
TFM 99-26.
99-26
12-21-99
1-18B Revises the list of approved oils.
Removed by
Chg 12.
Continued
TFM #
Dated
Section
or Page Description Status
Temporary Changes Learjet 35A/36A with FC-200
TFM-2 FM-102
6-23-2008
Change 14
84-02
3-15-84
1-3
Maximum zero wing and tip fuel weight
replaces maximum wing bending weight.
Removed by
Chg 5.
85-02
3-8-85
IV Revised FUEL CMPTR light procedure.
Removed by
Chg 6.
85-10
1-3-86
2-2
Engine oil and hydraulic accumulator pre-
flight checks.
Removed by
Chg 6.
85-16
11-8-85
3-5
Current limiter failure procedure associ-
ated with AMK 85-1.
Removed by
Chg 8.
87-05
3-2-87
4-17
Clarify operation of emergency gear
extension valve.
Removed by
Chg 7.
87-06
3-2-87
4-19
Clarify operation of emergency gear
extension valve.
Removed by
Chg 7.
87-15
7-16-87
II
Bleed hydraulic pressure to zero before
setting battery switches off.
Superseded
by TFM 88-17.
88-07
2-13-89
4-29 Pitot-static system malfunction procedure.
Removed by
Chg 7.
88-17
1-17-89
II
Bleed hydraulic pressure to zero before
setting battery switches off.
Removed by
Chg 9.
89-17
11-16-89
4-16
Fuel imbalance during fuel transfer proce-
dure.
Removed by
Chg 9.
92-02
9-10-92
2-16 Clarify the oil pressure annunciator.
Removed by
Chg 10.
93-15
12-3-93
2-35 Cold weather operations.
Removed by
Chg 10.
94-15
1-9-95
1-14
Maximum operating altitude — 41,000 FT.
(When cabin outflow or safety valve has
been replaced between 1-1-89 and 1-9-95)
Active, until
SB 35/36-21-19
is accomplished.
94-23
3-6-95
5-8 Revised noise level compliance statement.
Removed by
Chg 10.
96-08
5-30-96
2-49 Standby fuel pump annunciators.
Removed by
Chg 10.
96-09
5-30-96
4-17
Procedure for standby fuel pump failing
to shut off.
Removed by
Chg 10.
96
-10
7-12-96
1-14
Adds paved runway restriction to limita-
tions section.
Removed by
Chg 10.
99-02
7-16-99
1-18B Revises the list of approved oils.
Superseded by
TFM 99-24.
99-03
4-16-99
1-20
Revises fuel anti-icing additive
limitations.
Removed by
Chg 12.
99-24
11-30-99
1-18B Revises the list of approved oils.
Superseded by
TFM 99-26.
99-26
12-21-99
1-18B Revises the list of approved oils.
Removed by
Chg 12.
Continued
TFM #
Dated
Section
or Page Description Status
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