Jodel DR.100 Series Airworthiness Directives and Service Bulletins |
Aircraft Part |
LTA (German) |
Orig. Doc. of issuing Authority |
Corresp. SB |
Title |
Remarks |
Interval |
Airframe |
LTA 2001-078 |
DGAC CN 2001-035(A) (24 Jan 2001) |
Avions Robin SB No. 169 (03 Jul 2000) |
The lid installed on the hydraulic fluid container possibly does not meet the certification specifications, which could lead to loss of brake fluid and subsequent failure of the brake system. |
|
In Germany: Within 10 flying hours after the LTA becomes effective on 08 Mar 2001. |
Airframe |
LTA 2000-224/3 |
DGAC CN 1969-019(A) R1 (24 Jan 2001) DGAC CN 2000-173(A) R1 (24 Jan 2001) |
Avions Robin SB No. 156 R1 (06 Oct 2000) |
Possible installation of incorrect mounting bolts for the elevator control cables at the control column |
Replaces LTA 2000-224/2 and LTA 1969/045 |
In Germany: Within 50 hours after the LTA becomes effective on 22 Mar 2001. |
Airframe |
LTA 2000-224/2 |
DGAC CN 2000-173(A) (19 Apr 2000) |
Avions Robin SB No. 156 (29 Mar 2000) |
Possible installation of incorrect mounting bolts for the elevator control cables at the control column |
Replaces LTA 2000-224 to correct errors contained in the original german issue. |
In Germany: Within 50 hours after the first issue of this LTA (LTA 2000/224) became effective on 27 Jul 2000. |
Airframe |
LTA 2000-224 |
DGAC CN 2000-173(A) (19 Apr 2000) |
Avions Robin SB No. 156 (19 Mar 2000, PDF 83 kB) |
Possible installation of incorrect mounting bolts for the elevator control cables at the control column |
|
In Germany: Within 50 hours after the LTA becomes effective on 27 July 2000. |
Engine |
LTA 99-174/2 |
|
|
Continental Crankshaft Cracks due to manufacturing defect |
n/a for O-200 series engines |
|
Engine |
LTA 99-174 |
|
|
Continental Crankshaft Cracks due to manufacturing defect |
n/a for O-200 series engines |
|
Engine |
LTA 99-150/2 |
DGAC CN 199-470(A) (1 Dec 1999) |
Avions Robin SB No. 161 Rev. 1 (3 Sep 1999) |
Paint flakes in the engine/carburetor air intake |
supersedes LTA 99-150 |
|
Engine |
LTA 99-150 |
DGAC CN 199-053(A)R1 (10 Mar 1999) |
Avions Robin SB No. 161 (26 Jan 1999) |
Paint flakes in the engine/carburetor air intake |
superseded by LTA 99-150/2 |
|
Engine |
LTA 98-393 |
|
|
Continental & Lycoming Crankshafts overhauled by 'Nelsen Balancing Service' |
|
|
Engine |
LTA 96-283/2 |
|
|
Oil Filter Adapter |
|
|
Engine |
LTA 96-283 |
|
|
Oil Filter Adapter |
|
At every oil filter change. |
Engine |
LTA 96-233/2 |
|
|
Ignition Timing |
|
|
Engine |
LTA 95-165/2 |
|
|
Cracks in the rocker arm bearing area |
|
During the next and all following cylinder and engine overhauls. |
Engine |
LTA 94-202/2 |
|
|
Carburetor Air Intake Housing |
|
|
Engine |
LTA 93-235 |
|
|
Carburetor Air Intake Housing |
|
|
Electrical |
LTA 93-149 |
|
|
Ignition Switch/Diode |
|
|
Engine |
LTA 93-132 |
|
|
Connecting Rod |
|
|
Engine |
LTA 93-123 |
|
|
Cylinder/Valve |
|
|
Carburetor |
LTA 91-107/2 |
|
MSA-2 |
Marvel-Schebler Venturi |
|
|
Carburetor |
LTA 91-106/4 |
|
MSA-1 |
Marvel-Schebler Float |
|
|
Airframe |
LTA 89-109 |
|
|
Safety Harness |
|
|
Engine |
LTA 89-148/2 |
|
|
Fuel Pump |
|
|
Engine |
LTA 79-6/2 |
|
|
Ignition Timing |
superseded by LTA 96-233/2 |
100 hrs |
Engine |
LTA 77-161/2 |
|
|
Fuel Lines |
|
|
Engine |
LTA 76-221 |
|
|
Continental O-200 Cylinder |
|
100 hrs |
Engine |
LTA 75-229/3 |
|
|
Cylinder Leak Test |
|
100 hrs |
Airframe |
LTA 66-83 |
|
|
Seat Tube Frame |
|
50 hrs |
Airframe |
LTA 66-62 |
|
Avions Robin SB No. 8 Rev. 1 ?? |
Elevator |
|
|
Airframe |
LTA 66-34 |
|
|
Aileron Pulleys |
|
50 hrs |
Airframe |
LTA 63-93 |
|
|
Aileron Cables |
|
50 hrs |