AD's and SB's download for information only

NEW: Lycoming EASA AD 2005-0023 and SB388C and Hartzell AD971802R1 and SB217R2

LTA-Nr.:

Modell Titel: Gültig: SB/TM
2002-240 all Fuelsystem/Flight Control System 26.07.2002 1141-0000
1996-271 all Inspection of rivets on horizontal tail bearing-fitting fuselage side 10.10.1996 1140-0000
1988-109/2 all Flight control system - Wing flap position selector 24.01.1989 1123-0000/1
1979-249 all Calibration of VDO Tachometer 16.10.1979 KL/L/1067
1969-011/2 diff s/n Elevator Outboard Hinge - Inspection / Exchange of Bearings 08.12.1975 27-28c
1975-233 all Fuel and oil hoses - Damaged hoses; Inspection and exchange 06.10.1975 1059-0000
1969-012 Q and H Fuselage - Cracks on flange of frame 5 of fuselage-wing attachment 04.02.1969 27-33
1968-126 Q Fuel-Tank - Exchange of "Curtis-Valve" 29.11.1968 27-31
1965-085  diff s/n Fuel and oil hoses - Inspection for reduction 29.09.1965 27-29
1965-008 A4,Q5,Q6 Steel wire armoured hoses for fuel, oil and loadpressure - Inspection for cracks, swelling, soaking and similar defects 15.02.1965 27-27
1964-024 all Frame - Cracks of the web plate of frame No. 3 in the area of the rudder shift lever attachment 09.04.1964 27-24
1964-011 all Flaps - In 35° or 45° position flaps may retract when actuation lever is unintentionally touched slightly 21.02.1964 27-18
1963-079 all Elevator 22.09.1963 27-1, 27-13
1961-027 Q1-Q4,H2 Flaps 22.06.1961 27-11

Further AD's concerning engine and propeller

Lycoming GO480

  • 98/416 FAA 98-18-12: Lear Romec Fuelpump

Propeller Hatzell HC-82-V20/HC-A2-V20

  • SB 61-217 Propeller Inspection
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