SDR 510019538 | Robinson R22Beta Engine/transmission coupling drive belt frayed. Engine to transmission drive belts frayed. Sheave out of alignment. P/No: A1902. TSN: 9 hours.
SDR 510019512 | Eurocopter AS365N Main rotor gearbox oil jet leaking. Main rotor gearbox oil jet in area of LH engine input reduction housing leaking. See SDR 510018725 for similar defect. P/No: 365A32106601. TSO: 2136 hours/5439 cycles.
SDR 510019512 | Eurocopter AS365N Main rotor gearbox oil jet leaking. Main rotor gearbox oil jet in area of LH engine input reduction housing leaking. See SDR 510018725 for similar defect. P/No: 365A32106601. TSO: 2136 hours/5439 cycles.
SDR 510019483 | CASA C212200 Wing skin cracked. Lower wing centre section skin cracked in two places. Cracks approximately 6mm (0.23in) and 4mm (0.15in) long. Found during inspection iaw C-212-PV-02-SID. P/No: 21213104. TSN: 20045 hours/10215 cycles TSO: 20045 hours/10215 cycles.
SDR 510019437 | MDH 369 Engine/transmission coupling bearing unserviceable. Main transmission sprag clutch forward bearing had rivets missing in the roller ball cage. P/No: 369A5362.
SDR 510019436 | MDH 369F Tail rotor control system swashplate unserviceable. Tail rotor pitch control assembly swashplate splines damaged/missing. P/No: 369D2180111. TSO: 24 hours.
SDR 510019433 | Fokker F28 MK0100 Master cylinder/brake valve housing cracked. Brake housing cracked in two places from oil gallery and piston bore. Cracks approximately 12mm and 9mm (0.47in and 0.35in) long. Found using eddy current inspection. P/No: 50099043.
SDR 510019431 | Eurocopter AS365N Hydraulic system pipe corroded and leaking. Hydraulic brake pipe from brake control unit corroded and leaking. P/No: 365A75293000.
SDR 510019418 | Grob G115 Mixture control cable faulty manufacture. Mixture cable suspect faulty manufacture. Cable has a swaged threaded rod at the carburettor end and was mechanically damaged where the cable entered the rod. Two other cables in stock found to be in a similar condition. P/No: GS70000138.
SDR 510019414 | Bell 212 Engine mount section nut broken. Cracked/broken nut from engine tripod mount found in rear fuselage access panel, with two more nuts in similar condition. Suspect caused by hydrogen embrittlement. P/No: MS21042L4.
SDR 510019399 | Lycoming TIO541E1C4 Reciprocating engine cylinder section retainer broken. No. 5 cylinder exhaust valve spring retainer broken into several pieces. Three pieces found in rocker box. P/No: LW16475. TSO: 1163 hours.
SDR 510019399 | Lycoming TIO541E1C4 Reciprocating engine cylinder section retainer broken. No. 5 cylinder exhaust valve spring retainer broken into several pieces. Three pieces found in rocker box. P/No: LW16475. TSO: 1163 hours.
SDR 510019374 | Eurocopter EC225LP Main rotor gearbox shaft cracked. Main transmission splined input shaft cracked at base of spline. Found during NDT inspection. P/No: 332A32330522. TSN: /481 cycles.
SDR 510019374 | Eurocopter EC225LP Main rotor gearbox shaft cracked. Main transmission splined input shaft cracked at base of spline. Found during NDT inspection. P/No: 332A32330522. TSN: /481 cycles.
SDR 510019374 | Eurocopter EC225LP Main rotor gearbox shaft cracked. Main transmission splined input shaft cracked at base of spline. Found during NDT inspection. P/No: 332A32330522. TSN: /481 cycles.
SDR 510019360 | Boeing 777-3ZGER Tyre tread separation. No. 4 main wheel tyre tread separation. Tyre was new, not re-treaded. Suspect sidewall delamination caused by FOD. Investigation continuing. P/No: APR07700. TSN: 1390 hours/102 cycles.
SDR 510019326 | Airbus A330-202 Passenger compartment window damaged. Cabin window at seat 1AB crazed and chipped beyond limits. P/No: A5627000720400.
SDR 510019311 | Embraer ERJ-190-100 Nacelle/pylon attach fittings shear pin loose. LH and RH pylon shear pins P/No: 190-15181-003 loose and migrating. LH aft inboard nut P/No: NAS509-14C loose and held on by only one thread (lockwire still attached). Bushing P/No: 190-33686-001 migrating. Gap found between RH bushing and shear pin. Found during inspection iaw SB 190-54-0013. Several similar defects reported. P/No: 19015181003. TSN: 15976 hours/10805 cycles.
SDR 510019308 | Saab SF340B Pneumatic distribution system clamp incorrect part. Suspect incorrect part clamp fitted to bleed duct system. P/No: CA3S120C.
SDR 510019284 | Bombardier DHC8-402 Hydraulic hose leaking. Loss of hydraulic fluid from No. 2 hydraulic system caused loss of numerous aircraft systems. White smoke coming from No. 1 hydraulic system vent during disembarkation. Flexible hose between main landing gear yoke and nacelle was leaking. P/No: 46455-117.
SDR 510019280 | Boeing 737-838 Drag control system switch cracked. Speed brake lever take-off warning switch (S651) intermittent in operation due to cracked housing. P/No: V3L2228.
SDR 510019279 | Boeing 717-200 Drag control actuator – module unserviceable. Spoiler/speed brake module u/s due to cracked arm mechanism. P/No: 3F2201F.
SDR 510019258 | PWC PW535A Engine fuel pump failed. LH engine failed. Engine fuel filter contaminated. Fuel control unit (FCU) low- pressure fuel pump and driveshaft had failed, causing the contamination. Investigation continuing.
SDR 510019258 | PWC PW535A Engine fuel pump failed. LH engine failed. Engine fuel filter contaminated. Fuel control unit (FCU) low- pressure fuel pump and driveshaft had failed, causing the contamination. Investigation continuing.
SDR 510019244 | IAE V2533A5 Turbine engine turbine hub worn. First-stage high-pressure turbine hub worn beyond limits in fir tree. Found during inspection iaw FAA AD 2004-12-08 and AD/V2500/01. P/No: 2A5001. TSN: 17809 hours/8077 cycles.
SDR 510019224 | Continental IO550G Engine fuel injector line worn and damaged. No. 3 cylinder fuel injector line worn. Suspect due to contact with intake manifold clamp. Found during inspection iaw AD/Con/60 Amdt4. P/No: 646423. TSN: 1534 hours.
SDR 510019221 | Mooney M20R Landing gear selector switch distorted. Landing gear selector switch shaft bent by approximately 30 degrees. P/No: 8906K2875. TSN: 1534 hours.
SDR 510019191 | Bell 412 Crew station equipment system panel unserviceable. Smoke coming from upper circuit breaker panel. No fire observed. 5amp (lighting) CB had popped. P/No: BLPN6151.
SDR 510019172 | Cessna 402C Passenger/crew door spring broken. Top cabin door opened in flight. External door handle spring mechanism broken and fouling on shaft, opening the door when handle rotated to the stowed position. P/No: 51115204.
SDR 510019137 | Piper PA44180 Landing gear retract/extension system spring broken. Nose landing gear arm inner spring broken. Investigation found small imperfections in the area of breakage. Suspected they were present at time of manufacture. P/No: 487483. TSN: 1062 hours
SDR 510019129 | Piper PA32300 Wing spar corroded. Aft wing spar corroded. Found during inspection iaw AD/PA32/27. AD not due but carried out anyway due to increased frequency of corrosion problems. P/No: 6205400.
SDR 510019104 | Turbomeca Arriel 1E Turbine engine turbine section bearing failed. RH engine made unusual noises during start-up. Metal contamination of chip detectors and oil filter. Initial investigation of metal deposits found debris suspected to be from Module 4 roller bearing. Investigation continuing.