N312AA
Service difficulty reports · 139
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 = 'N312AA' AND registry_match = 'registration' 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 = 'N312AA' AND registry_match = 'registration' 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 ABXA20211123123None · noneSPOILERS DISCRETE AND EICAS MESSAGE CAME ON DURING PUSHBACK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPERATIONAL TEST IAW B767 AMM 27-61-00. OPS CHECK GOOD.AIRCRAFT RETURNED TO SERVICESDR 2021F00370Stringer · crackedDURING C CHECK IT WAS FOUND THAT MAIN CABIN, UPPER ANGLE OF STRINGER 9L CRACKED AFT OF FRAME STA676. REMOVED STR 9L SECTION AND REPAIR PARTS AS REQ IAW B767-200 SRM 53-00-03 REPAIR 1 FIG 201, VERIFIED MAT ID FOR STR SECTION BAC1498.205, RC0699402 IAW B767-200 SDR ABXA20211116114Gearbox · out of adjustRIGHT AILERON DID NOT DROOP WITH FLAPS SET TO 15. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND R/H DROOP ANGLE GEAR BOX OUT OF ADJUSTMENT. ADJUSTED ITEM PER AMM 27-51-40, THEN CONDUCTED IN BOARD AILERON DROOP TEST PER AMM 27-11-00. DROSDR ABXA2021118108Pin · wornWHILE IN C-CHECK IT WAS DISCOVERED THAT MAIN CARGO DOOR LATCH CAM PINS WERE WORN BEYOND LIMITS. PINS #2,7,11 AND 12 WERE REPLACED IAW B767-200 MMS 52-32-11SDR ABXA2021105116Stringer · crackedDURING C CHECK AT AMES TAMPAIT WAS FOUND THAT MAIN CABIN, UPPER ANGLE OF STRINGER 9L CRACKED AFT OF FRAME STA676. REMOVED STR 9L SECTION AND REPAIR PARTS AS REQ IAW B767-200 SRM 53-00-03 REPAIR 1 FIG 201, VERIFIED MAT ID FOR STR SECTION BAC1498.205, RC0699402SDR ABXA20210913091Warning Message · false activationRT. ENG FUEL VALVE EICAS MSG APPEARS DURING ENGINE START. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPS CHECK OF FUEL CONDITION MOTOR IAW B767 AMM 76-11-00 OPS CHECK NORMAL A/C REMAINS ETOPS 180. AICRAFT RETURNED TO SERVICE.SDR ABXA202108097072Lock · out of adjustMAIN CARGO WARNING DURING PUSHBACK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. ADJUSTED MCD LOCK BAR IAW B767 AMM 52-32-00, OPS CHECK GOOD. DOOR VERIFIED LOCKED RII FORM ACCOMPLISHED. AIRCRAFT RELEASED FOR FLIGHT.SDR ABXA20200803188Pneumatic System · bindingLT ENG BLEED VALVE OFF LIGHT WITH ASSOCIATED LEFT ENGINE BLEED AND LEFT PACK OFF LIGHT. AIRCRAFT BACK TO GATE. AIRCRAFT GROUNDED. VERIFIED PRSOV WON'T OPEN, REMOVED AND REPLACED LT ENG PRSOV. OPERATIONS CHECKED GOOD, IAW B767 MM 36-11-18. REMAIN ETOPS 180SDR ABXA202008073160Warning Message · illuminatedL FWD WINDOW EICAS MESSAGE ON CLIMB OUT.CONTINUED TO DESTINATION. AIRCRAFT WAS GROUNDEDSDR ABXA202008053157Warning Message · illuminatedL FWD WINDOW EICAS ON CLIMB OUT. AIRCRAFT WAS GROUNDED.SDR ABXA20200710122Speaker · abnormalLOUD SQUEAL COMING FROM CAPTAIN`S. SPEAKER, UNABLE TO CONTROL. AIRCRAFT WAS GROUNDED.SDR ABXA2019112202173Escape Reel · dislodgedTWO EMERGENCY DESCENT DEVICES WERE DISLODGED FROM THEIR STORAGE CONTAINER LOCATED IN THE SUPERNUMERARY COMPARTMENT CEILING. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE TWO DESCENT DEVICES WERE REPLACED WITH SERVICEABLE DESCENT DEVICES. THE CAUSE FSDR ABXA2019102517161Escape Reel · detachedONE DESCENT DEVICE WAS FOUND DISLODGED FROM ITS STORAGE CONTAINER LOCATED IN THE SUPERNUMERARY COMPARTMENT CEILING. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE DESCENT DEVICE WAS REPLACED WITH SERVICEABLE DESCENT DEVICE. THE CAUSE FOR THE DESCENT SDR ABXA201910316172Stringer · crackedCRACK IN OUTBOARD SURFACE OF STRINGER 25L AT FUSELAGE STATION 676+6. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201910316171Stringer · crackedCRACK IN OUTBOARD SURFACE OF STRINGER 24L AT FUSELAGE STATION 676+7.75. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201910316170Stringer · crackedCRACK IN OUTBOARD SURFACE OF STRINGER 23L AT FUSELAGE STATION 676. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201910316169Skin · crackedCRACK IN RIGHT ENGINE OUTBOARD CORE COWL LOWER LONGERON AT SECOND FROM AFT LATCH. THE CORE COWL WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA201910316168Stringer Splice · corrodedCORROSION ON THE SPLICE FITTING AT FUSELAGE STATION 786, STRINGER 39L. THE SPLICE FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA201910316167Structure · gougedGOUGE IN THE RIGHT PYLON AFT FAIRING CHORD BELOW THE LATCH PIN. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201910316166Keelbeam · corrodedCORROSION ON THE KEEL BEAM FLANGE UPPER SURFACE AT FUSELAGE STATION 820. THE KEEL BEAM WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201910316165Attach Angle · corrodedCORROSION ON THE ATTACH ANGLE AT FUSELAGE STATION 786, RIGHT BUTT LINE 4, KEEL BEAM AREA. THE ATTACH ANGLE WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA20180322044Intercostal · damagedEVIDENCE OF BURN DAMAGE ON AN INTERCOSTAL ASSEMBLY AND TWO OF THE THREE APU GENERATOR FEEDER WIRES FROM CONTACT WITH THE INTERCOSTAL AT BS 1021, RBL 35.SDR ABXA20171002123Fitting · crackedCRACK IN PRESSURE DECK FITTING (PYLON FITTING) AT FUSELAGE STATION 1062. THE FITTING WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20171002122Stringer · crackedCRACK IN AFT LOWER SIDE OF STRINGER 13L AT SPLICE. THE STRINGER WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR ABXA20171002121Structure · corrodedCORROSION AROUND NUTPLATES AND STIFFENERS ON THE CHORD AT THE LEFT WING REAR SPAR TO TRAILING EDGE UPPER PANEL. THE CHORD WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20171002120Attach Angle · corrodedCORROSION ON THE ATTACH ANGLE FOR PANEL 196BR IN THE RIGHT WHEEL WELL. THE ANGLE WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20171002119Frame · crackedDURING ULTRASONIC INSPECTION REQUIRED BY AD 2012-22-17, A CRACK WAS FOUND IN THE INNER CHORD OF THE RIGHT SIDE FRAME BELOW FLOOR LEVEL OF THE UPPER CARGO COMPARTMENT. THE CHORD WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR ABXA20171002118Keelbeam · corrodedCORROSION ON UPPER SURFACE OF LOWER INBOARD HORIZONTAL FLANGE OF THE LEFT KEEL BEAM AT BS 1007 - 1014. THE KEEL BEAM WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR ABXA20170830098Carabiner · missingTHREE EMERGENCY DESCENT SAFETY HARNESS CARABINERS WERE MISSING FROM THEIR STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), THREE NEW SAFETY HARNESS CARABINERS WERE INSTALLED INTO THE STOWAGE POUCH. THE CAUSE OF THE MISSING CARABINERS IS USDR ABXA20170308013Escape Rope · defectiveTWO DESCENT DEVICES WERE FOUND NOT PROPERLY STOWED. THE AIRPLANE WAS REMOVED FROM SERVICE. THE DESCENT DEVICES WERE REPLACED WITH SERVICEABLE DESCENT DEVICES. THE CAUSE FOR THE DESCENT DEVICES BECOMING UNSTOWED IS UNKNOWN.SDR ABXA20161029152Escape Rope · unwanted deployAFTER NORMAL LANDING, THE CREW FOUND TWO INERTIAL REEL HANDLES DANGLING TO THE FLOOR OF THE SUPERNUMERARY COMPARTMENT. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) UNTIL ONE OF THE DESCENT DEVICES WAS REWOUND, RESEALED, AND RESTOWED. THE OTHER INERTIAL RESDR ABXA20161011148Support · corrodedNUMBER ONE FLAP SUPPORT GOUGED AND SIGNS OF CORROSION. REPAIRED IAW REA B657-62231-MR AND JC 57500006-001. AIRCRAFT WAS GROUNDED.SDR ABXA20160917145Escape Reel · unwanted deployTWO DESCENT DEVICES WERE FOUND NOT PROPERLY STOWED. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) UNTIL THE DESCENT DEVICES WERE REPLACED WITH SERVICEABLE DESCENT DEVICES. THE CAUSE FOR THE DESCENT DEVICE BECOMING UNSTOWED IS UNKNOWN.SDR ABXA20150930159Structure · corrodedLEFT WING ACCESS PANEL 552AB HAS CORROSION ON AFT INBD FLANGE UPPER SIDE. GAINED ACCESS & REMOVED LOWER TE CHORD AT WS 157 - 228. INSTALLED NEW CHORD PN 654T0391-35 & REINSTALLED PANELS IAW DWG 113T1400 & SRM CH51-40-02-PAR 7. CORRODED, PART NAME CHORD, PN SDR ABXA20150924157Stringer · corrodedCORROSION WHERE STRINGER 35L MEETS FUSELAGE SKIN AT FS 412, FOUND CORROSION ON STRINGER 35L, STATION 412, OUT OF LIMITS. FABRICATED STRINGER IAW SRM 53-00-03 FIG 201 REPAIR 2. CORRODED, PN 144T3001, PART NAME STRINGER, SN NSN, FS & BS LOCATION 412, STRINGER SDR ABXA20150923158Skin · crackedFORWARD LOWER CORNER OF R1 DOOR HAS AN EXTERNAL HFEC CRACK INDICATION, APPROX 3/8" LONG. INSTALLED REPAIR TO FWD LOWER CORNER OF R1 DOOR CUT OUT IAW SRM 53-10-01. PN 141T3330, PART NAME SKIN, CRACKED 3/8", EXACT FS LOCATION ON ACFT 287. ACFT WAS GROUNDED.SDR ABXA201509010155Floorbeam · corrodedAFT LOWER CARGO FLOORBEAM, UPPER CHORD STATION 1153 WAS CORRODED BEYOND LIMITS & WAS REPLACED IAW DWG 146T1204. PN 146T1204-7, SN NSN, PART NAME UPPER CHORD, CORRODED LEVEL 2, EXACT FS & BS LOCATION ON ACFT STATION 1153, EXACT STRINGER & WS LOCATION ON ACFT LSDR ABXA20150908152Attach Fitting · corrodedREAR SPAR TO WING TE PANEL ATTACH BEAM, LOWER CHORD CORRODED ABOVE WIRE BUNDLE RACE WAY AT WS 250, INBD & OTBD SIDES AS SEEN IN RT WW. FOUND ATTACH BEAM CORRODED BEYOND LIMITS. REPAIRED ATTACH BEAM IAW SRM 51-70-12 FIG 1 DETAIL III. CORRODED L2, PN 113T1621SDR ABXA20150828156Support Angle · corrodedAFT LOWER CARGO ON UNDER SIDE, CORRODED STATION 1219, LBL 24 - 34. R & R SUPPORT ANGLE 451T2409-2 IAW DWG 451T2402. CORRODED LEVEL 2, PN 451T2409-2, PART NAME SUPPORT ANGLE, SN N/A, FS & BS LOCATION STATION 1219, STRINGER & WS LOCATION LBL 24 TO LBL 34. ACFSDR ABXA20150828153Attach Fitting · corrodedREAR SPAR TO TE, UPPER PANEL ATTACH BEAM, UPPER CHORD CORRODED AROUND NUTPLATES AT WS 290 AS SEEN IN RT WW. FOUND ATTACH BEAM TO BE CORRODED OUT OF LIMITS IAW SRM 51-10-00. R & R ATTACH BEAM IAW SRM 51-40-2 & 51-40-5. CORRODED LEVEL 2, PN 113T1622-125, PARTSDR ABXA20150816151Skin · crackedAPU DOOR 316AL EXTERIOR SKIN, LOWER EDGE BENT IN SEVERAL PLACES. FWD CORNER HAD 2 CRACKS .2 INCHES DEEP, OUT OF LIMITS IAW SRM 52-40-01 FIG 101 DETAIL III. ROUTED OUT 2 CRACKS AT EDGE OF PANEL WITHIN LIMITS IAW SRM 52-40-01 FIG 101 DETAIL III. STOP DRILLED SDR IXXA201311050068Structure · damagedLOWER SURFACE OF LT WING FUEL TANK HAS HOLE DAMAGED IN THE CENTER AT WING STA 128. REPAIRED DAMAGE IAW ATI 57-767-4910 & DWG 57-13075-2, HOLE DIA .3750". ACFT WAS GROUNDED.SDR IXXA2013110500067Mount · corrodedRT ENGINE AFT MOUNT IS BLEEDING RUST FROM THE BEARING AND THE POCKETS IN MULTIPLE AREAS. R & R AFT ENGINE MOUNT IAW AMM 71-21-01, ACFT WAS GROUNDED.SDR IXXA201311050070Stiffener · crackedLEFT PYLON OTBD HORIZONTAL STIFFENER IS CRACKED. R & R OTBD STIFFENER IAW SRM 51-40-02. ACFT WAS GROUNDED.SDR IXXA201311050069Vertical Support · crackedNOSE WHEEL WELL AFT BULKHEAD AT STA. 287, LT SIDE ANGLE 10" FROM TOP CRACKED. REPAIRED LEFT AFT VERTICAL NOSE WELL WHELL CORD IAW SRM 51-70-12, ACFT WAS GROUNDED.SDR IXXA20120212003SValve · damagedON POST FLIGHT INSPECTION, FOUND HOLE IN LOWER LT WING SURFACE (LT CENTER FUEL TANK). UPON INSP, INSIDE LT CENTER FUEL TANK, DAMAGE WAS FOUND TO THE FUEL TANK VENT VALVE AND ON THE L5 STRINGER. TEMPORARY REPAIR ACCOMPLISHED TO LOWER LT WING SURFACE IAW DWG 57-SDR IXXA20121222037OEscape Reel · damagedDURING DAILY CHECK, EMERGENCY DESCENT DEVICE CABLE FOUND EXTENDED. R & R EMERGENCY DESCENT DEVICE IAW AMM 25-61-03. DEVICE INSPECTION DUE DATE IS 09/15/2016.SDR IXXA20120910024OFuel Cell · leakingDURING TAKEOFF ROLL, WITH AIR CONDITIONING PACKS TURNED OFF, THERE WAS A STRONG JET FUEL ODOR IN FLIGHT DECK. ODOR DISSIPATED WHEN PACKS WERE SWITCHED ON. FOUND CENTER FUEL TANK RIB "O" CENTER MEMBER AND LT MAIN TANK RIB 4 AFT SKIN JOINT LEAKING. ALL WORK PESDR IXXA20120730018SSkin · damagedON POST FLIGHT WALK AROUND FOUND EVIDENCE OF A TAIL STRIKE. SKIN DAMAGE WAS FOUND TO THE APU DOORS AND AFT FROM BS 1898.4 TO 1923. FRAME DAMAGE WAS FOUND FROM BS 1898.45 TO 1923.5.SDR IXXA20120523012OSeal · brokenDURING A-CHECK FOUND POSITION NR 1 EMERGENCY DESCENT DEVICE SEAL BROKEN. R & R EMERGENCY DESCENT DEVICE IAW AMM 25-61-00.
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