Diamond Aircraft (formally Hoffmann) (Austria)

Status Subject

Detail

Reference information

Contact: UK Agent- Soaring Oxford 01636 525318 and Airborne Composites (Tim Dews) 01985 40981

LBA and Austro Control Airworthiness Directives Service Bulletins found on link below. http://support.diamond-air.at/hk36-tt.html

HOFFMAN H-36 Dimona & HK-36 & HK-36-R Super Dimona

M Aileron, elevator, wings M Wing M Fuel tank M Engine brackets M Fuel systems M Aerobatics & spins M Fuel tank
M Flight limitations & placarding M Tail/elevator unit M Shoulder harness fixings M Wing to fuselage joint M Wings
Fin skin separation Extension of service life M Exhaust system M Air brake system M Elevator root rib M Engine software M Aileron Controls M Propeller (Hoffmann) M Air Brake (H36 only)
Page 1 BGA Compendium 07/11

water accumulation Composite skin inspection capacity check inspect and modify vapour lock prohibited gel coat detached and restricts fuel flow, Optional - fit aluminium fuel tank changed (CAA letter 9/97/CtAw/119) front fixing inspection inspection additional bracing dimensional check main bolts at top rudder hinge inspect from 3 000 to 6 000 hours (Super Dimona) modify (Super Dimona) modify modification before 3000 hours or if damaged Check software version of engine TCU Inspection and modification of push rods Pitch change rods (L2400 or SS2100 engines) Inspection, inhibit then 5 year repeat

AD 82-236, TN 2 AD 82-237-2, TN 3/2 AD 83-156, TN 6 AD 83-157-2, TN 7/2 AD 84-205, TN 11 AD 85-34, TN 12
AC AD 60, AD 85-128-2, TN 13/1 AD 86-177-3 AC AD 53, AD 87-93, TN 15/2 AC AD 54, AD 87-94, TN 17 AC AD 52/2, AD 86-177-3, TN 19 AC AD 55, AD 88-108, TN 24
AC AD 65, SB 25/1 AD 74, SB 33 AD 74, SB 34 AD 85, SB 51 AD 99, SB 66/1 Iss2 AD 111, MSB 36-72 AD D-2005-370 AD 2011-0110, MSB 36-105/1

TNS
CAA CAA CAA CAA CAA CAA
08/85 12/86 06/87 06/87 08/87 08/88 08/90 02/92 12/93 12/93 08/96 06/00 04/02 10/05 3/2011