AEROPRAKT
A-22L2 / A-22LS
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Vibrations of the main landing gear legs of A-22LS and A-22L2 airplanes:: IB A-22LS-01
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Modernization of the main landing gear legs for A-22LS and A-22L2 airplanes: IB A-22LS-02
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Inspection and reinforcement of the tail boom of A-22LS and A-22L2 airplanes: IB A-22LS-03
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Ammendment of AMM: IB A-22LS-04
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Installation of protecting cover: IB A-22LS-05
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Modernization of parking brake valve: IB A-22LS-06
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Ammendment of AMM: IB A-22LS-08
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Ammendment of AMM: IB A-22LS-09
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Inspection of the nose landing gear leg: IB A-22L2-01
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Inspection of cardan rings and ammendment of AMM: IB A-22LS-10
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Ammendment of POH Glider towing supplement: IB A-22LS-07
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Ammendment of AMM: IB A-22LS-11
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Ammendment to POH: SB A-22LS-12
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Inspection and replacement of the threaded rod-end: SB A22LS-13
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Ammendment of AMM – inspection of elevator pushrod: SB A-22LS-14
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Ammendment of AMM – 50-hour work: SB A-22LS-15
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Inspection of rudder cables: SB A-22LS-16
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Replacement of rudder cables and fairleads: SB A-22-17
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AMM amendment – windscreen glass inspection: SB A-22LS-18
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Replacement of the nose wheel fork hinge bracket: SB A-22-LS-19
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Harness system check: SB A-22LS-20
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Change of rescue system rocket attachment: SB A-22LS-21
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Change of water pump screw-clamp torque: SB A-22LS-22
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Change of rescue system rocket attachment for Germany, Denmark, Poland and Lithuania: SB A-22LS-23
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Increase of MTOW to 525 kg: SB A22L2-02
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Amendment to POH: SB A-22LS-24
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Holes in the flaperon hinge axles: N A-22LS-25
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Upgrade of A-22LS fleet in Germany: SB A-22LS-26
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Limitation of ethanol content in fuel: SB A-22LS-27
A-32 / A-32L
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Temporary limitation of VNE: SA A32-01
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Modification of AMHT: SB A32-02
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Replacement of door latches: SA A32-03
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Reinforcement of roof at frame No.3: SB A32-04
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Reinforcement of frame No.10: SB A32-05
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AMM amendment – windscreen glass inspection: SB A32-06
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Replacement of the nose wheel fork hinge bracket: SB A32-07
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Upgrade of A32 fleet in Germany: SB A32-10
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Relocation of iS fuel pump: SB A32-11
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Amendment to POH: SB A32-12
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Amendment to AMM: SB A32-13
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ASI marking change: SB A32-16
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Holes in the flaperon hinge axles: N A32-17
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Installation the rear mounts’ screens: SB A32-14
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Replacement of the oil system hoses: SB A32-15
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AMM change 50-hour work: SB A32-18
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Trim tab deflection in POH: SB A32-19
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Limitation of ethanol content in fuel: SB A32-20
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VNE increase: SB A32-21
BRM AERO
BRISTELL CLASSIC/RG
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ELEVATOR CONTROL STUCK: ALL-SA-3-0-5-0001-2017
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AOI revision: ALL-SA-0-0-0-0001-2020
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Kavlico pressure sensors: ALL-SA-0-0-0-0005-2020
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Seat attachment: ALL-SA-0-0-0-ALL-0002-2021
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Automatic Trim/GDU™ 4XX Reset: 22112 Rev. A
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ROTAX 912 IS Engine Attachment: ALL-SA-5-0-0-ALL-0001-2024
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Control surfaces deflection: ALL-SB-0-0-0-DE-0002-2024
K F A
EXPLORER / SAFARI
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Tailpost insert: SB001
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Short axle tube: SB002
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Wrong Aileron mixer: SB003
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Wrong jury struts: SB004
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Lift-strut bolt lenght: SB005
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Old flaperon chord length: SB006
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Correct bungee tension: SB007
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Fuel-Cap Vent: SB008
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Carb overflow pipe: SB009
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Nose Landing Gear: SB010
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Control torque tube crack: SB011
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Axle shear: SB012
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Nose gear V-Brace: SB013
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Axle bolt lenght: SB014
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Stabilizer tabs broken: SB015
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582 engine mount isolator rubbers: SB016
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Rudder cable ferrule crimp: SB017
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Tailwheel block lube: SB018
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Control rod-end failure: SB019
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Fibre glass seat support: SB020
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Welded axle backing plate: SB021
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Throttle control bellcrank: SB022
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Nose-wheel axle bolts: SB023
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Rudder return springs: SB024
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Axle inspection and upgrade: SB025