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Jodel DR.100 Series Airworthiness Directives and Service Bulletins

French Airworthiness Directives (from their Civil Aiviation Administration DGAC) and the Service Bulletins by Avions Robin do not seem to be available on the web at the moment (7 March 2000).

28 Nov 2001: Since sometime during fall 2001, Robin has a new website: www.robinaviation.com. So far there is only a list of the available service bulletins available, but perhaps this will extended in future ...

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

Lutz Gebhardt

Created: Tue Mar 7 19:07:56 CET 2000
Last modified: Thu Nov 29 12:58:35 CET 2001