AD No.: issued | SB No.: issued | Subject: | Eligibility |
---|---|---|---|
G304CZ17 - 01 b) 27.11.2000 | Type change Glasflügel 304 CZ to Glasflügel 304 CZ-17 . | Optional for 304 CZ. | |
G304CZ17 - 02 a) 20.12.2000 | Flight manual change . | All 304 CZ-17 | |
G304CZ - 02 a) 20.12.2000 | Flight manual change . | All 304 CZ | |
G304CZ - 03 b) 11.06.2001 | Installation of Rögger Hook canopy mechanism. | For all 304 CZ, 304 CZ-17, 304 C exported to the USA , other optional | |
G304CZ - 04 a) Change 1 21.10.2002 | Change of the weights and moments of the controls rudders | All 304 CZ | |
G304CZ17 - 04 a) Change 1 21.10.2002 | Change of the weights and moments of the controls rudders | All 304 CZ-17 | |
CAA-AD-040/2003 | G304CZ - 05 a) G304CZ17 – 05 a) 26.03.2003 | Airbrake handle check. | All 304 CZ, 304 CZ-17, 304 C S.No.: from 1 up to 60-17 |
EASA AD: 2012-0073 | G304CZ - 06 a)_R01 G304C - 06 a)_R01 G304CZ17 - 06 a)_R01 23.04.2012 | Inspection of elevator control rod. | All 304 CZ, 304 CZ-17, 304 C |
G304MS - 07 b) 26.09.2016 | Optional installation of steerable tail wheel. | Optional for 304 MS. | |
EASA EAD:2017-0167-E | G304MS - 08 a) 15.12.2017 | FES system modification | Mandatory for 304eS up sn 77-MS (including). |
G304MS - 09 b) 15.12.2017 | Optional Maintenance manual supplement issued. | Optional for 304 eS. | |
EASA EAD: 2018-0207-E | G304CZ - 10 a) G304C - 10 a) G304CZ17 - 10 a) 28.08.2018 | Deflector-angles at the C.G. release. Usage of connection ring pair meeting standard LN 65091 | All 304 CZ, 304 CZ-17, 304 C equipped with SH 72 release hook |