AOP MK 9

The Auster Air Observation Post (AOP) Mk 9 was developed and manufactured by Auster Aircraft. The AOP Mk 9 prototype first flew in March 1954 and entered service with the British Army in February 1955, with 182 units ultimately built. It succeeded the AOP Mk 6, featuring improvements that gave the Mk 9 better take-off and landing performance.

The design included an extended cabin, allowing it to function not only as an observation post but also for command and control, light transport, and liaison duties. It was powered by a Blackburn Cirrus Bombardier 702 4-Cyl Inverted Mk208 engine. Known for its capability in slow speed flight, the AOP Mk 9 was purposefully challenging for aircraft with higher stalling speeds and larger turning circles to target.

A range of access platforms and solutions are available to facilitate maintenance around this aircraft. These support access to critical sections such as the Nose Section (radome, avionics), Forward Fuselage (doors, cargo, lighting systems), Landing Gear (NLG and MLG), Middle Fuselage/Wing Box Area (fuel tanks, oil maintenance), Wing & Engine Pylon, AFT Fuselage, and the Tail Section (empennage, stabilisers). Products like the Reach Deck Platform, Modular Stepover Platforms, Super Trestle Scaffold, and Cantilever Platform provide access for detailed and methodical inspections across all aircraft zones.