FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N712AL and the event date: up to this one’s cancellation.
Incident 19900820045959IPrw On Run Landing (Rotorcraft · Gulf Of Mexico, TXNR2 engine spooled down and fuel pressure light on. Landed safely. Loose fuel line fitting at pump.Incident 19880830055769IFcd/Prec Ldg From Cruise · Freeport, TXFire warning for NR2 engine actuated. Landed on a barge next to drilling platform. No fire.
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 20001215SH040Link · failedFLOATS WERE INADVERTENTLY INFLATED. LINK DID NOT SEPARATE AT SHEAR POINT. (X)SDR 20001206SH004Explosive Link · dischargedAIRCRAFT FLOATS WERE INADVERTENTLY DISCHARGED. MALFUNCTION WAS DISCOVERED DURING REMOVAL OF RT MAIN GEAR DOOR. EXPLOSIVE CHARGE DISCHARGED WHEN FLOATS TRIPPED, BUT LINK DID NOT SEPARATE. (X)SDR 20001206SH001Blade · debondedDISCOVERED DURING POST-FLIGHT INSPECTION (VIBRATION WAS FELT DURING FLIGHT). EXTENSIVE UPPER SURFACE SKIN DISBOND. (X)SDR 20000502SH014Blade · debondedDURING 500-HOUR INSPECTION, FOUND TIP PLATE COMPLETELY DEBONDED. (X)SDR 99ZZZX47Blade · debondedDISCOVERED DURING 500-HOUR INPSECTION, TIP RIB STRAP DEBONDED, (RECURRING PROBLEM). TIP RIB STRAPS REPLACED BY C.T.I. 04-04-97, TT: 6,245.1 HOURS. 05-19-97, TT: 6,340.1 HOURS, AND 12-23-97, TT: 7,207.8 HOURS.SDR 98ZZZX3093Blade · debondedDISCOVERED DURING 500-HOUR INSPECTION, TIP RIB STRAP DEBONDED (RECURRING PROBLEM WITH THIS BLADE). TIP RIB STRAPS REPLACED BY C.T.J. 4-4-97 TT 6,245.1 HOURS - 5-19-97 TT 6,340-1 HOURS - 12-23-98 TT 7,207.8 HOURS.SDR 99ZZZX208Gearbox · making metalUPON INSPECTION OF GEARBOX PARTS DURING DISASSEMBLY, FOUND CUT O-RING UNDER SCREEN NR 6840136 IN OIL DELIVERY TUBE OIL PASSAGE. THIS COULD HAVE CAUSED RESTRICTED OIL FLOW TO OIL DELIVERY TAKE WHICH LUBES 2-1/2 BEARING AREA. SUBMITTER STATED LACK OF OIL IN 2SDR 98ZZZX241Detector · malfunctionDURING CRUISE FLIGHT, NR 2 FIRE LIGHT ILLUMINATED. RETURNED TO BASE. NO FIRE-FLAME. DETECTOR MALFUNCTION.SDR 97ZZZX259Blade · crackedDISCOVERED DURING 500 HOUR INSPECTION, FOUND BLADE SKIN CRACKED ALONG FORWARD EDGE OF TRIM TAB.SDR 97ZZZX258Blade · debondedDURING 500 HOUR INSPECTION FOUND BLADE TIP RIB DEBONDED.SDR 95ZZZX4420N1 Cable · brokenAFTER COMPLETION OF THE ENGINE WASH, ATTEMPTED TO START NR 1 ENGINE FOR A DRYING RUN. THE ENGINE WOULD NOT LIGHT-OFF AND THE THROTTLE LEVER WAS STUCK IN THE FLIGHT POSITION. NR 1 THROTTLE CABLE WAS INSPECTED AND FOUND BROKEN APPROXIMATELY 3.50 INCHES FROM THSDR 95ZZZX2817Hose · leakingDURING CRUISE FLIGHT, NR 2 HYDRAULIC SYSTEM STARTED A SLIGHT DROP BELOW RED LINE (3000 PSI) TO 2350-2500 PSI. LANDING GEAR ACTUATED TO DOWN POSITION. LANDING GEAR INDICATED SAFE. UPON INSPECTION, NOSE LANDING GEAR UP HYD FLEX HOSE WAS FOUND LEAKING. FLEX HOSDR 95ZZZX2818Rod · wornSHOP REPAIR OF DAMPER ASSY DUE TO LEAKING OIL. HEAVY WEAR TO ROD INNER SEAL SURFACE. ROD WORN BEYOND REPAIR LIMIT.SDR 95ZZZX2093Blade · crackedDISCOVERED WHEN COMPLYING WITH AD 84-10-2, 500-HOUR INSPECTION. FOUND CRACK IN SPAR AT ROOT END LOWER SIDE ON BLADE EXTENDING FROM FORWARD OUTBOARD BUSHING HOLE TO LEADING EDGE APPROXIMATELY 1.5 INCHES LONG.SDR 95ZZZX2092Blade · crackedDEFECT DISCOVERED DURING C.A.M.P. 500-HOUR BLADE INSPECTION, FOUND CRACK IN SPAR AND LOWER SKIN AT TIP END EXTENDING INBOARD FROM APPROXIMATELY STA 249.88 TO STA 247.65. CAUSE UNKNOWN.
Other aircraft with N712AL · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N712AL is registered now to the first aircraft listed.