N518AU, cancelled Oct 10, 2008
Service difficulty reports · 88
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N518AU' AND deregistration_id = 'N518AU-2008-10-10' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N518AU' AND deregistration_id = 'N518AU-2008-10-10' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR USAA920081294Skin · crackedCLT RON MAJOR REPAIR LOG 4390633- FUSELAGE SKIN CRACKED AT BS 727E, S-24R. REPAIRED FUSELAGE SKIN AT BS727E, S-24R IAW B737 SRM 53-00-01 AND US AIRWAYS TYPICAL REPAIR 53-33. (B)SDR USAA920070820Stringer · corrodedCLT - MAJOR REPAIR - C-5 CHECK, LEVEL 2 CORROSION ON STRINGER, BS 1006 - BS 1016, RBL 8. REPAIRED STRINGER, BS 1006 - BS 1016, RBL 8 IAW B737-300 SRM 51-10-02.SDR USAA920070821Floorbeam · corrodedCLT - MAJOR REPAIR - C-5 CHECK, LEVEL 2 CORROSION ON FLOORBEAM, BS 986, LBL 10. REPAIRED FLOORBEAM, BS 986, LBL 10 IAW USAIRWAYS TYPICAL REPAIR 53-10-05B.SDR USAA920070819Fitting · crackedCLT - MAJOR REPAIR - C-5 CHECK, LEFT HAND HORIZONTAL STABILIZER CENTER SECTION THRUST BEAM CORNER FITTING CRACKED, STABILIZER STATION 83.05. REPLACED LEFT HAND HORIZONTAL STABILIZER CENTER SECTION THRUST BEAM CORNER FITTING, STABILIZER STATION 83.05 IAW B737-SDR USAA920070887Skin · crackedCLT - MAJOR REPAIR - C-5 CHECK, FORWARD SERVICE DOOR EXTERIOR SKIN CRACKED AT UPPER HINGE CUTOUT. REPAIRED FORWARD SERVICE DOOR EXTERIOR SKIN AT UPPER HINGE CUTOUT IAW USAIRWAYS TYPICAL REPAIR 52-10-13.SDR USAA070497Frame · crackedFOUND BS 847 RBL 36. REPAIRED PER SRM 51-40-02, DEFECT SIZE: 1/16".SDR SB07045Wire · brokenPIT - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHT AT SEAT 7ABC BROKEN/INOPERATIVE. MAINTENANCE REPAIRED WIRES ON SEAT MOUNTED EMERGENCY LIGHT AT SEAT 7ABC. OPERATIONAL CHECK GOOD.SDR USAA200704005Skin · crackedCRACK FOUND AT STA 727D + 18" AND S24L. INSTALLED DOUBLER PER SRM 53-00-01 AND TR 53-60-03A.SDR USAA061216Door Frame · crackedFWD CARGO DOOR FWD FRAME AT LOWER DOOR STOP BS 440 S23R CRACK. INSTALLED DOUBLER AND FILLERS IAW EA 98153, DEFECT SIZE: .25 INCH.SDR SB06084Battery Pack · dischargedDCA - MAINTENANCE REPORTED THE FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.SDR SB06066Windshield · crackedPIT FLT288 DURING CRUISE, EN ROUTE FROM CLT TO YYZ, THE OUTER PANE OF THE CAPTAIN'S L1 WINDSHIELD SHATTERED. CREW DECLARED AN EMERGENCY AND DIVERTED TO PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S WINDSHIELD PESDR SB06020Cable · misroutedDURING FAA RAMP INSPECTION, FAA FOUND THE R2 DOOR ESCAPE SLIDE DEPLOY CABLE ROUTED INCORRECTLY. MAINTENANCE REROUTED THE R2 DOOR ESCAPE SLIDE CABLE (LATCH ASSEMBLY) PER MM 25-61-35. REINSTALLED R2 DOOR ESCAPE SLIDE PER MM 25-61-35-402-003.SDR USAA051389Stiffener · crackedAFT END OF LT PACK BAY AT I/B AFT CORNER CRACKED. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-10-02 BOEING DWG 65-45402. DEFECT SIZE: 1 INCH CRACK.SDR USAA050060Skin · delaminatedPIT - FOUND LOWER SKIN CORE BOND DELAMINATED 6 INCH BY 6 INCH AREA, BOTTOM SIDE 14 INCHES FROM INBOARD END. REMOVED DAMAGE, INSTALLED INTERNAL DOUBLERS AND FILLRS PER SRM 51-70-10. (M)SDR USAA050024Floorbeam · corrodedPIT - FOUND CHORD AND ANGLE CORRODED AT SCREW HOLES, STATION 344 RBBL -13 TO LBBL -24. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED T-CAP, FABRICATED NEW CHORD AND ANGLE SPLICES, INSTALLED PER SRM 53-10-51. (M)SDR USAA050061Skin · delaminatedPIT - FOUND LOWER SKIN CORE BOND DELAMINATED 6 INCH BY 4.5 INCH AREA, 34 INCHES FROM F/B EDGE. REMOVED DAMAGE, INSTALLED FILLERS, DOUBLERS PER SRM 51-70-10. (M)SDR USAA041101Strap · corrodedPIT - Q5 - STRAP, WEB, SKIN, 3 INCH X 4 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 492.5 BTW, 26R, 27R SKIN SECTION. REMOVED CORROSION, INSTALLED FILLER, STRAPS AND DOUBLER IAW EA. (K)SDR USAA041100Support · crackedPIT - Q05 - SUPPORT, .075 INCH CRACK, AFT CARGO DOOR UPLOCK SUPPORT. REMOVED AND REPLACED SUPPORT IAW SRM.SDR USAA041067Frame · corrodedPIT- Q5- FRAME, 1.5 INCH, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 500D, STR 28L FRAME. MANUFACTURED ANGLE IAW MFG DWG 65C22910. (K)SDR USAA041066Mount · corrodedPIT-Q5-LAV MOUNTS, 2 INCHES X 2 INCHES (2 EA) CORROSION; LEVEL 1; TASK NR C53-107-02, STA 913, LBL 21 AND LBL 34. DEFECTIVE PART REPLACED WITH IDENT PART NR. (K)SDR USAA041065Mount · corrodedPIT-Q5-LAV MOUNTS (2), 2 INCHES X 2 INCHES (2 EA), CORROSION; LEVEL 1; TASK NR C53-107-02, STA 994, RBL 21 AND RBL 34. DEFECTIVE PART REPLACED WITH IDENT PART NR. (K)SDR USAA041071Skin · chafedPIT - Q5 - SKIN, 9 INCHES X .5 INCH X .0075 INCH DEEP, CHAFED, RT OF S1 AT STA 867 TO 887. DOUBLER AND TRIPLER REPAIR SCHEME IAW SRM. (K)SDR USAA041069Intercostal · crackedPIT- Q5- INTERCOSTAL, 2 INCH CRACK, IN RADIUS- FLOOR INTERCOSTAL, STA 380, BBL 0. REPLACED SUPPORT ANGLE IAW SRM. (K)SDR USAA041068Skin · corrodedPIT - Q5- SKIN, 1.25 INCH, CORROSION, LEVEL 1; TASK NR C53-208-01, STA 500C + 19 INCH IB OF STR 28L. REMOVED CORROSION IAW SRM. (K)SDR USAA041072Frame · corrodedPIT - Q5 - FRAME, 3 INCH X 3 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 492.5 BETWEEN STR 27R AND 28R FRAME. INSTALLED DOUBLERS IAW SRM. (K)SDR USAA041070Frame · corrodedPIT - Q5 - FRAME, 1.5 INCH X 1 INCH AREA, CORROSION; LEVEL 1; TASK C53-107-02, FRAME AT STA 993.5, RBL 46. REMOVED CORROSION, PRIMED AND PAINTED ISW SRM. (K)SDR USAA041074Floorbeam · corrodedPIT - Q5 - BEAM, 10 INCH L X 1 INCH WIDE, CORROSION; LEVEL 1; TASK NR C53-107-01, FLOORBEAM SCREW HOLES, STA 312, LBBL 13 TO RBBL13. 22 INCH REPAIR ANGLE WITH 10 INCH X 1 INCH W FILLER IAW SRM. (K)SDR USAA041073Skin · delaminatedPIT - Q5 - SKIN, 4 INCH X 4 INCH AREA, DELAMINATION, AT IB AFT FLAP BOTTOM. REMOVED BOTTOM SKIN, CORE, INSTALLED BOTTOM REPAIR DOUBLER IAW SRM. (K)SDR USAA040981Stringer · crackedPIT - Q5 - STRINGER, .25 INCH LONG CRACK AT STA 887 S-9L. INSTALLED (2) REPAIR ANGLES IAW TR 53-10-20A, 51-30-02, 51-40-09, 51-30-01.SDR USAA040979Skin · crackedPIT - Q5 - NR 3 SLAT, 6 INCH X 6 INCH AREA, CRACKED AND DISBONDED AT IB LOWER T/E. REMOVED SKIN AND CORE, REPLACED CORE AND REPAIR PLYS IAW SRM 51-70-10 AND EA 70537.SDR USAA040978Skin · bulgedPIT - Q5 - NR 3 SLAT, 1 INCH X 2 INCH BUBBLE IN SKIN, T/E AT SKIN JOINT 12 INCHES FROM IB END. REMOVED DAMAGE, INSTALLED FILLER AND REPAIR PLYS IAW SRM 51-70-10, EA 79537.SDR USAA040977Skin · crackedPIT - Q5 - NR 6 SLAT SKIN, .1250 TO 4 INCH CRACKS- NUMEROUS; LOWER SURFACE AFT ROW RIVETS - NUMEROUS AREAS ENTIRE LENGTH. REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.SDR USAA040980Stringer · crackedPIT - Q5 - STRINGER, .75 INCH CRACK, S-5A, BS 1138, INSTALLED DOUBLER IAW T/R 53-80-04 AND 53-00-01, FIG 221.SDR USAA040982Tie · crackedPIT - Q5 - STRINGER TIE, 1 INCH CRACK AT STA 827, S4L. DEFECTIVE PART REPLACED WITH IDENT PART.SDR USAA040983Structure · crackedPIT - Q5 - NR 4 SLAT, SEVERAL .1250 INCH TO .2500 INCH CRACKS, LWR SURFACE, AFT ROW RIVETS AREA OF ACTUATOR. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.SDR USAA040843Skin · crackedSKIN, .1250 INCH CRACKS, LOWER SURFACE AFT ROW OF RIVET, NR 5 SLAT IB TRACK AREA. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.SDR USAA040984Bulkhead · crackedPIT - Q5 - WEB, 1 INCH CRACK, AT BS179, WL233.5, RBBL5.7 (178 BULKHEAD) WEB. INSTALLED DOUBLER IAW SRM 53-10-08, FIG 209 DETAIL II.SDR USAA040631Skin · crackedCLT - FOUND SKIN CRACKED 2.25 INCH, .5 INCH ABOVE STRINGER 25R SKIN LAP AT STATION 764. INSTALLED DOUBLER/TRIPLER AND FILLER PER SRM 53-00-01 FIG 229. (M)SDR SB04124Light · unsecurePHL - PILOT REPORTED THE EMERGENCY EXIT LIGHTS ON SEAT 10A INOPERATIVE. MAINTENANCE SECURED THE EMERGENCY EXIT LIGHTS ON SEAT 10A. OPERATIONAL CHECK GOOD.SDR USA2004F00051Outflow Valve · failedENROUTE, CREW REPORTED CABIN ALTITUDE WARNING HORN SOUNDED AS THEY ENCOUNTERED A SLOW LOSS OF CABIN PRESSURIZATION. PRESSURE LOSS WAS NOT EXPLOSIVE BUT CREW COULD NOT CNTRL PRESS. FLIGHT DESCENDED TO 10,000 FT AND CONTINUED. NO OXYGEN MASKS WERE DEPLOYED. SDR USA2004F00046Controller · malfunctionedENROUTE, CREW REPORTED VIA ACARS THEY ENCOUNTERED A SLOW LOSS OF CABIN PRESSURIZATION. PRESSURE LOSS WAS NOT EXPLOSIVE BUT CREW COULD NOT CONTROL PRESSURIZATION. FLIGHT DESCENDED TO 10,000 FEET AND CONTINUED. NO OXYGEN MASKS WERE DEPLOYED. FLIGHT LANDED WISDR USAASB04048Fan Blade · erodedIAH - FLT 775 - EN ROUTE FROM PHL-IAH, AT FL310, THE CABIN ALTITUDE CLIMBED VERY SLOWLY TO 9,500 FEET. AT THIS TIME, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW ACCOMPLISHED AN IMMEDIATE DESCENT OT FL240. CABIN ALTITUDE BEGAN TO DESCEND AND STABILIZE AT 3SDR USAASB04018Door · out of rigEN ROUTE AT FL330, A/C LOST PRESS. CREW ACCOMPLISHED RAPID DESCENT OT 10,000 FT. OXY MASKS DEPLOYED DURING DESCENT. STANDBY & MANUAL PRESS MODES USED BUT NOT EFFECTIVE. OUTFLOW VALVE REPORTED TO BE FULLY CLOSED. A RUMBLING SOUND HEARD BENEATH THE FLOORBOASDR USA2004F00014Cabin Pressure · failedENROUTE, WHILE LEVEL AT FL330, THE AIRCRAFT LOST PRESSURIZATION. CREW ACCOMPLISHED A RAPID DESCENT TO 10,000 FT. OXYGEN MASKS DID DEPLOY DURING DESCENT. STANDBY AND MANUAL PRESSURIZATION MODES WERE USED BUT WERE NOT EFFECTIVE. OUTFLOW VALVE WAS REPORTED TOSDR USAASB03215Door Seal · failedDURING CRUISE, EN ROUTE FROM IND-CLT AT FL290, A LOUD BANG WAS HEARD FROM THE FORWARD GALLEY AREA, FOLLOWED BY THE CABIN ALTITUDE CLIMBING UNCONTROLABLLY. CREW REPORTED THE OUTFLOW VALVE WAS IN THE FULL CLOSED POSITION. THE OXYGEN MASKS DEPLOYED AND BOTH TE SDR USAASB03131Wire · brokenORD - MAINTENANCE REPORTED THE EMERGENCY LIGHT ASSEMBLY ON SEAT ROW 10, LEFT SIDE, WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT SEAT ROW 10, LEFT SIDE. OPERATIONAL CHECK GOOD. (M)SDR USAASB03118Fuse · blownMAINTENANCE REPORTED THE LEFT OVERWING HATCH EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND A BLOWN FUSE IN POWER SUPPLY M1134 AND A BAD PLUG ON THE EMERGENCY SIGN. REPLACED FUSE AND PLUG. OPS CHECK GOOD. (M)SDR USAASB03082Wire · faultyMAINTENANCE REPORTED THE EMERGENCY LIGHTING AT SEAT 12 ABC WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED WIRING ON SEAT 12ABC PER STANDARD WIRING PRACTICES MANUAL 20-10-13. OPERATIONAL CHECK GOOD. (M)SDR USAASB03081Control Panel · faultyCLT - FLT 1254 - MCI TO CLT, AT FL350, CAPTAIN REPORTED A PRESSURIZATION PROBLEM, AS CABIN ALTITUDE INCREASED. CABIN ALTITUDE EXCEEDED 14,000 FT, THE OXYGEN MASKS AUTO DEPLOYED. AN EMERGENCY DESCENT TO FL100 WAS ACCOMPLISHED. THE FLT CONTINUED ONTO CLT, AT SDR USAASB04004Seal · failedDURING CLIMB-OUT FROM PHL, EN ROUTE TO ORD AT FL270, CRWE HEARD A LOUD BANG AND A BURST OF AIR. NO MASTER CAUTION WARNING OR DOOR WARNING LIGHTS ILLUMINATED. THE AUTO PRESSURZATION SYSTEM HAD FAILED AND WAS PLACED IN STANDBY. IN STANDBY, THE CABIN ALTITUDE
Back to N518AU, cancelled Oct 10, 2008