|
61-26-01
WEB |
1/16/62 |
Deteriorated flexible
oil pickup hoses located within the engine oil tank will allow air
to be drawn into the engine oil supply line. This can cause
serious engine and propeller overspeeds due to improper propeller
governing or engine damage from inadequate lubrication. Applies to
T-34A (A45) only. |
|
62-24-01
WEB |
11/26/62 |
Horizontal stabilizer
inspection. (Superseded by AD 2007-06-01 R1 dated 4/16/07. See
below.) |
|
72-22-01
WEB |
10/25/72 |
To decrease the
possibility of gear-up landings caused by seizure of the uplock
rollers |
|
75-24-11
WEB |
11/28/75 |
Rudder-aileron bungee
interconnect cable assembly and the bellcrank assembly |
|
89-05-02
WEB |
3/24/89 |
Elevator control
fittings |
|
91-17-01
WEB |
11/25/91 |
Elevator trim tab
actuators |
|
99-05-13 R1 WD
WEB |
7/5/00 |
Withdrawal of AD
99-05-13. |
|
2001-13-18
PDF |
8/16/01 |
Supersedes AD
99-12-02. This AD requires repetitive inspections of the wing spar
assembly for cracks with replacement of any wing spar assembly
found cracked. This AD also includes a reporting requirement of
the results of the initial inspection and maintains the flight and
operating restrictions required by AD 99-12-02 until
accomplishment of the initial inspection. |
|
2001-13-18 R1
WEB
PDF |
3/15/04 |
Revision to AD
2001-13-18 to eliminate the AMOCs to AD 2001-13-18. |
|
2001-23-10
WEB |
12/13/01 |
The affected flap
flex shaft assemblies and flap actuator assembly could be
installed through spare replacement on all models of the T-34. |
|
2004-25-51
WEB PDF |
12/10/04 |
Emergency AD
grounding T-34s following Texas Air Aces crash on December 7,
2004. |
|
2004-25-51FR
WEB
PDF |
12/20/04 |
This AD becomes
effective on December 21, 2004, to all affected persons who did
not receive emergency AD 2004-25-51, issued December 10, 2004.
Emergency AD 2004-25-51 grounded all T-34s. |
|
Proposed AD
on McCauley Props |
11/16/05 |
Proposed AD for
McCauley C406 and C409 propellers that many T-34s (and Bonanzas
and Navion's) have. The document this link takes you to is a
NPRM -- Notice of Proposed Rulemaking. |
|
NPRM re Tail AD |
7/31/06 |
NPRM (Notice of
Proposed rule Making) to change the method of inspecting the
spar in the horizontal stab from dye penetrant to surface eddy
current. Official title: FAA–2006–25105; Directorate Identifier
2006–CE–33–AD. |
|
2007-06-01 R1
WEB
PDF |
4/16/07 |
Supersedes AD 62-24-01 (near the top
of this list). Retains the actions required in AD 62-24-01 and
changes the required inspection method from dye penetrant to
surface eddy current. |
|
2007-08-04
WEB
PDF |
5/17/07 |
A new AD regarding the McCauley
propellers. It only effects airplanes with the C406 or C409
props. |
|
2007-08-08
WEB
PDF |
5/25/07 |
Supersedes AD62-22-01 and pertains
to the up-lock rollers. This AD refers to Beech Service
Instructions No. 0448-211 Rev 1. Click
here
for PDF version of that service instruction. |
