AS 202 Bravo

© Franz Wegmann

ADs applicable to Swiss registred aeronautical products.

Design holder:

ACC Columbia Jet Services GmbH
(formerly Gomolzig Aircraft Services GmbH, Gomolzig Flugzeug- und Maschinenbau GmbH, FFA Aircraft Bravo AG, FFA Flugzeugwerke Altenrhein AG, FFA Flug- und Fahrzeugwerke AG, Flugzeugwerke Altenrhein AG (FWA), Flug- und Fahrzeugwerke AG Altenrhein (FFA))

Pertaining to Model: AS 202 Bravo Series
TCDS: EASA.A.591
Last update: 22 February 2022

AD Reference	Superseded by	Subject	SB Ref.
EASA 2015-0023-E (PDF, 215 kB, 18.02.2015)		UPPER FORWARD FUSELAGE STRINGERS	GFM SB 2015-1 (PDF, 282 kB, 05.02.2015)
EASA 2009-0233 (PDF, 63 kB, 28.10.2009)		FUEL SUCTION TUBE	Shop Manual Parts Cat. 5-20-00 28-40-01
EASA 2009-0177 (PDF, 63 kB, 05.08.2009)	EASA 2009-0233	FUEL SUCTION TUBE	Shop Manual Parts Cat. 5-20-00 28-40-01
HB-1992-403 (PDF, 341 kB, 02.12.1992)		FUEL GRAVITY FEED HOSE	44 (PDF, 300 kB, 31.10.1992)
HB-1991-202 (PDF, 177 kB, 19.06.1991)		LANDING GEAR SPRING PINS	36B (PDF, 135 kB, 01.05.1991)
HB-1991-147 (PDF, 89 kB, 14.05.1991)		VERTICAL STABILIZER RIB	42 (PDF, 257 kB, 01.04.1991)
HB-1991-146 (PDF, 209 kB, 14.05.1991)		ELEVATOR DRIVE SHAFT	41A (PDF, 154 kB, 01.05.1991)
HB-1991-001 (PDF, 211 kB, 16.01.1991)	HB-1991-146	ELEVATOR DRIVE SHAFT	41
HB-1990-141 (PDF, 137 kB, 16.05.1990)		RUDDER PEDAL ASSEMBLIES	33B (PDF, 92 kB, 01.03.1990)
HB-1988-221 (PDF, 142 kB, 09.11.1988)	HB-1991-202	LANDING GEAR SPRING PINS	36
HB-1985-124 (PDF, 246 kB, 28.08.1985)	HB-1990-141	RUDDER PEDAL ASSEMBLIES	33A
HB-1983-077 (PDF, 216 kB, 01.06.1983)	HB-1985-124	RUDDER PEDAL ASSEMBLIES	33
TM-L Nr.: 80.590-202 (PDF, 1 MB, 31.12.1982)		AD Summary pre 1983 TM-L Nr.: 80.590-202

ADs pre 1983:

AS 202 Bravo Airworthiness Directives issued prior to 1983 are not published as individual issues. However you may download (1.29 MB) the AS 202 Bravo AD-Summary TM-L Nr.: 80.590-202 with all AS 202 Bravo ADs issued prior to 31 December 1982 in the above mentioned list.