SDR 510021172 | Embraer ERJ-170-100 Airfoil anti-ice/de-ice system—windshield shattered. LH windshield heat failed with accompanied by smoke and sparks. Shortly after No.1 windshield shattered. P/No: NP18730115.
SDR 510021366 | Piper PA31350 Main landing gear strut/axle/truck—torque link corroded. LH main landing gear upper torque link heavily corroded in area under the squat switch. P/No: 40257000. TSN: 13386 hours/444 months.
SDR 510021363 | Sikorsky S76C Main rotor blades—cap disbonded. Black main rotor blade tip cap trailing edge disbonded. Length of disband approximately 63.5mm (2.5in). P/No: 7615009043050.
SDR 510021354 | Alpha Aviation R2160 Control column section—joystick broken. Pilot’s control stick grip broken during aerobatics. P/No: CCG1457. TSN: 2960 hours.
SDR 510021351 | Gulfstream 500S Wing fuselage attach fittings—strap cracked. RH lower wing to fuselage attachment strap cracked. Found during inspection iaw AD/AC/93 Req1. P/No: 1700368. TSN: 25888 hours.
SDR 510021337 | Proppellerwerk HOV62R Propeller blade section—screw sheared. No. 1 propeller blade lag screw sheared. Sheared screw head jammed in feathering mechanism preventing blade from feathering. Evidence of corrosion at point of failure.
SDR 510021337 | Proppellerwerk HOV62R Propeller blade section—screw sheared. No. 1 propeller blade lag screw sheared. Sheared screw head jammed in feathering mechanism preventing blade from feathering. Evidence of corrosion at point of failure.
SDR 510021336 | Fokker F28 MK0100 Horizontal stabiliser plates/skin—screw corroded. Horizontal stabiliser leading edge attachment screws corroded. Steel screws P/No NAS517 were fitted instead of the correct titanium screws P/No NAS5030. Suspect screws had been fitted by a previous operator. P/No: NAS517.
SDR 510021328 | Cessna 172S Master cylinder/brake valve—shaft sheared. Shaft attaching brake master cylinder to brake/rudder pedal sheared. P/No: 98820125. TSN: 4424 hours/104 months.
SDR 510021322 | Airbus A330-202 Escape slide—aspirator damaged. Door 4R escape slide failed to fully inflate during workshop testing. Investigation found the lower tube aspirator extensively damaged. P/No: 5A326514. TSN: 43597 hours TSO: 11525 hours.
SDR 510021294 | Pacific Aerospace CT4A Landing gear steering system—lever failed. Nose wheel steering arm snapped. P/No: 07528481. TSN: 6984 hours.
SDR 510021290 | Cessna 208B Cabin compressor system—bearing collapsed. Air compressor drive bearing collapsed. Suspect caused by lack of grease in bearing. P/No: MRC206SZZC. TSN: 2806 hours.
SDR 510021280 | Lear Jet 35A Tyre—tyre unserviceable. RH main landing gear inboard tyre shredded. Suspect caused by under inflation. P/No: 178K235. TSN: 63 hours/40 cycles.
SDR 510021277 | Cessna 441 Hydraulic system main—hydraulic line cracked and leaking. Landing gear retraction system hydraulic line cracked and leaking. Loss of hydraulic fluid.
SDR 510021242 | Bell 412 Main rotor mast/swashplate—support cracked. Main rotor swashplate support assembly cracked. P/No: 412010453105. TSN: 2378 hours TSO: 985 hours.
SDR 510021239 | Lycoming O360A1H6 Engine starter—bearing seized. Starter motor rear housing worn through. Caused by seized bearing spinning in the housing. P/No: 149NLR. TSN: 2054 hours.
SDR 510021238 | Piper PA31350 Engine air intake system—door unserviceable. LH and RH alternate air intake door mechanism unserviceable with worn parts and suspect incorrect door springs. P/No: 5491602.
SDR 510021236 | Lycoming TIO540J2BD Engine collector/tailpipe/nozzle—exhaust pipe unserviceable. RH engine No. 6 cylinder cracked and holed in area of riser flange. Size of hole approximately 50.8mm by 50.8mm (2in by 2in). Found during inspection iaw PA31/2013-10-04.
SDR 510021215 | Piper PA31350 Engine oil distribution (airframe) system—hose fitting incorrect routed. Engine oil cooler hose incorrectly routed and resting against turbocharger waste gate. Hose damaged due to heat. P/No: 156F0038D0266. TSN: 675 hours/26 months.
SDR 510021214 | Piper PA31350 Engine cowl flaps—cowling cracked. RH engine cowl flap cracked at both control rod attachment points. Crack length approximately 50.8mm (2in). P/No: 41803000. TSN: 16504 hours.
SDR 510021202 | Embraer EMB-120 Rudder structure—rudder damaged. Rudder sustained major damage during towing accident when it was contacted by the RH wing tip of another aircraft being towed.
SDR 510021202 | Embraer EMB-120 Rudder structure—rudder damaged. Rudder sustained major damage during towing accident when it was contacted by the RH wing tip of another aircraft being towed.
SDR 510021192 | Cessna 152 Horizontal stabiliser spar/rib—spar cracked. RH horizontal stabiliser rear spar cracked in area adjacent to vertical fin attachment bracket. P/No: 043200156. TSN: 13694 hours.
SDR 510021178 | Airbus A330-303 Cargo station equipment section—insulation blanket burnt. Rear pressure bulkhead insulation blanket burnt around cut-out due to contact with bleed air duct. P/No: F2587160600200.
SDR 510021173 | MDH 369D Tail rotor head—PCL cracked. Tail rotor pitch change link (PCL) cracked at outer end. P/No: 369X2172313. TSO: 525 hours.