|
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