N371AA
Service difficulty reports not matched to an aircraft · 80
They name N371AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N371AA' AND registry_match IS NULL 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 = 'N371AA' AND registry_match IS NULL 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 MK1Y20170602001Frame · crackedFOUND A .236 INCH CRACK ON THE FRAME INNER TRANSITION RADIUS, BS 883.5, RBL 89.SDR MK1Y20170604005Frame · crackedCRACK AT BS 883.5, LBL 89 FRAME.SDR MK1Y20170604004Frame · crackedCRACK AT BS 859.5, RBL 89 RT FRAME.SDR MK1Y20170604003Skin · crackedCRACK FOUND ON THE LT WING SKIN AT AFT PITCH LOAD FITTING, REPAIRED IAW DRAWING 112T7001.SDR MK1Y20170604001Frame · crackedDURING PERFORMANCE OF AD 2012-22-17, FOUND A CRACK, 0.236 INCHES IN LENGTH AT THE FRAME IN THE TRANSITION RADIUS BS 903.5, RBL 89.SDR AALA20150821013Window · openABORTED TAKEOFF BETWEEN 70 & 75 KNOTS FOR COCKPIT SLIDING WINDOW OPENED ON TAKEOFF ROLL. NO DEFECTS NOTED WITH THE WINDOW, OPERATES NORMALLY. PERFORMED HIGH ENERGY STOP INSPECTION WITH NO DEFECTS NOTED.SDR AALA20150223005O-Ring · tornEMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. AT TOP OF DESCENT RECEIVED, C HYD QTY EICAS MSG. QTY CONTINUED TO DECREASE TO .15 DURING FINAL APPROACH. PRESS NEVER INDICATED LOW. FOUND LEAK AT CTR HYD SYS CASE DRAIN DIFFERENTIAL PRESS INDICASDR AALA20150119004Computer · failedAIR INTERRUPT, RETURNED & EMER NOT DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB BOTH FLIGHT MANAGEMENT COMPUTERS FAILED. R & R LT FLIGHT MANAGEMENT COMPUTER IAW AMM 34-61-00. SYS CHECKED NORMAL.SDR AALA20150101006Pseu · faultyLEADING EDGE SLAT ASSYM MSG ON CLIMB OUT. FLAP NEEDLES FLUCTUATED BETWEEN 0 & 1. ON ARRIVAL AT JFK, BITE OF PSEU SHOWS CARD FAULT 10 & LE SLAT TARGET FAULT 297. R & R PSEU IAW AMM 32-09-04 & ALTERNATE OTBD SLAT EXT RELAY K221 IAW AMM 27-81-00-735-277.SDR AALA20141209010Warning System · false activationEMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. LE SLAT ASYMMETRY MSG ILLUMINATED AFTER TAKEOFF. LANDED 20 DEGREE FLAPS USING FLAP HANDLE. ACCOMPLISHED FIM 27-81-00. CYCLED SLATS ELECTRICALLY & HYDRAULICALLY MULTIPLE TIMES. SYS CHECKED NORMASDR AALA20140910001Light · inoperativeLEFT NR 2 DOOR EXTERNAL EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 2 DOOR EXTERNAL EMER LIGHT. OPERATIONS CHECKED NORMAL.SDR AALA20140531005Skin · damagedFUSELAGE SKIN AT STATION 1460 & STRINGER 28 RT DAMAGED. ACCOMPLISHED REPAIR IAW EA B767-53-035130.SDR AALA20140530015Structure · crackedCRACKS FOUND IN OUTER CORD AT RT STATION 1725.5. ACCOMPLISHED REPAIR IAW SRM 53-80-01 REPAIR 5, FIGURE 201 DETAIL 3 & EA B767-53-035085.SDR AALA20140524006Frame · crackedNUMBER 2 PYLON FRAME CHORD AT STATION 285.450 OTBD SIDE CRACKED AT BOTTOM. REPLACED CHORD IAW SRM 51-10-02 & DWG 311T2400.SDR AALA20140524005Frame · crackedRIGHT PYLON FRAME CHORD AT STATION 285.450 INBD SIDE CRACKED AT BOTTOM. REPLACED CHORD IAW B767-300 SRM 51-10-02 & DWG 311T2400.SDR AALA20140524004Stiffener · crackedRIGHT PYLON STIFFENER CRACKED 2 INCHES AFT OF INBD FRAME CHORD AT STATION 285.450. R & R STIFFENER IAW SRM 51-10-02-0G, 51-40-02-0G & DWG 311T2400.SDR AALA20140516009Socket · dirtyEXTERIOR EMERGENCY LIGHT AFT OF LT NR 4 DOOR INOPERATIVE. CLEANED LIGHT SOCKET & REPLACED LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.SDR AALA20140401002Skin · damagedFUSELAGE SKIN DAMAGED FROM BS 1390 - 1480 BETWEEN STRINGERS 27 & 28 RT. INSTALLED EXTERNAL REPAIR IAW EA B767-53-034141.SDR AALA20140131006Light · defectiveOVERWING LIGHT WAS DIM. REPLACED LAMP FOR OVERWING LIGHT. OPERATIONS CHECKED NORMAL.SDR AALA20140131005Light · inoperativeLT NR 4 EXIT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 4 EXIT EXTERIOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.SDR AALA20131123008Controller · inoperativeGIG CREW REPORTED DUAL BLEED FAULTS & RT HIGH PRESSURE SHUTOFF VLV EICAS MESSAGE WITH WARNING LIGHT & LT PRESSURE RELIEF VLV MESSAGE DISPLAYED. EMERGENCY DECLARED FLIGHT RETURNED GIG LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED HIGH PRESSDR AALA20130604010Charger · failedCREW REPORTED MULTIPLE ELECTRICAL FAULTS AND MAIN BATTERY CHARGER MESSAGE. EMERGENCY DECLARED FLIGHT RETURNED LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED MAIN BATTERY CHARGER AMD RELAY K102. SYS GROUND CHECK NORMAL OPERATION.SDR AALA20130223002Wire Harness · faultyJFK - INFLIGHT ORD-LHR. CREW REPORTED RIGHT ENGINE HP BLEED AIR *HPSOV* LIGHT ILLUMINATED DURING FLIGHT. FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE WIRE HARNESS. SYSTEM GROUND CHECK NORMAL OPERATION.SDR AALA20121116004Structure · corrodedCORROSION FOUND ON TOP OF HORIZONTAL STABILIZER BOX. REPAIRED CORROSION ON STABILIZER BOX PER EA B767-55-026959.SDR AALA20121116003Skin · corrodedHORIZONTAL STABILIZER CENTER BOX UPPER SKIN FROM STRINGER 1 TO REAR SPAR, RIGHT BUTTLINE 2.75. INSTALLED DOUBLER PER EA B767-55-027021.SDR AALA20121116002Skin · corrodedHORIZONTAL STABILIZER CENTER BOX UPPER SKIN FROM STRINGERS 3 TO 2, LEFT BUTTLINE 1.75. INSTALLED DOUBLER PER EA B767-55-027021.SDR AALA20121116001Structure · crackedRIGHT STATION 1809.5 OUTER CHORD CRACK. ACCOMPLISHED SPLICE REPAIR PER ECO C1945DN.SDR AALA20121116013Angle · crackedRIGHT PYLON CLOSE OUT ANGLE CRACKED. REPLACED ANGLE PER SRM 51-00-05-1.SDR AALA20121106005Slat · debondedNUMBER 5 LEADING SLAT STARTING TO DISBOND. ACCOMPLISHED BONDED REPAIR PER SRM 57-43-02-01.SDR AALA20121106004Skin · delaminatedRIGHT WING OUTBOARD FLAP LOWER SKIN SURFACE DELAMINATED. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-07.SDR AALA20120403009Lamp · burned outL2 DOOR EMERGENCY EXIT LIGHT. REPLACED LAMP FOR L2 EMERGENCY EXIT LIGHT. OPS CHECKED NORMAL.SDR AALA20120403008Lamp · burned outRIGHT NUMBER 2 DOOR EMERGENCY EXIT LIGHT UPPER INTERIOR LOWER SECTION INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EMERGENCY EXIT LIGHT. OPS CHECKED NORMAL.SDR AALA20120403007Lamp · burned outRIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT AFT OVERWING EMERGENCY LIGHT. OPS CHECKED NORMAL.SDR AALA20120403006Lamp · burned outOVERHEAD EMERGENCY LIGHT AT SEAT 43C INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT AT SEAT 43C. OPS CHECKED NORMAL.SDR AALA20120403005Lamp · burned outOVERHEAD EMERGENCY LIGHT AT SEAT 34B INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT AT SEAT 34B. OPS CHECKED NORMAL.SDR AALA20120403004Lamp · burned outSEAT 37H OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 37H OVERHEAD LIGHT. OPS CHECKED NORMAL.SDR AALA20120403003Lamp · burned outMID GALLEY OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR MID GALLEY OVERHEAD EMERGENCY LIGHT. OPS CHECKED NORMAL.SDR AALA20120403002Lamp · burned outFORWARD GALLEY OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR FORWARD GALLEY OVERHEAD EMERGENCY LIGHT. OPS CHECK NORMAL.SDR AALA20120209MIA01Lens · looseEMERGENCY EXIT LIGHT LENS COVER AT RIGHT NUMBER 4 DOOR LOOSE. SECURED LENS COVER FOR RIGHT NUMBER 4 DOOR. OPS CHECK NORMAL.SDR AALA20120125TUL05Light · inoperativeRIGHT EXTERIOR EMERGENCY LIGHT NEAR AFT CARGO DOOR INOPERATIVE. REPLACED LAMP FOR RIGHT EXTERIOR EMERGENCY LIGHT NEAR AFT CARGO DOOR. OPS CHECK NORMAL.SDR AALA20120125SFO02Light · inoperativeLEFT AFT EXTERIOR EMERGENCY LIGHT NEAR LEFT NUMBER 2 DOOR INOPERATIVE. REPLACED LAMP FOR LEFT AFT EXTERIOR EMERGENCY NEAR LEFT NUMBER 2 DOOR. OPS CHECK NORMAL.SDR AALA20110402DFW01Brake · overheatedDFW - CREW REPORTED TAIL STRIKE ON TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. BRAKES OVERHEATED UPON LANDING CAUSING ALL MAIN LANDING GEAR TIRES TO DEFLATE. AIRCRAFT REMOVED FROM SERVICE. REPLACED ALL MAIN LANDING GEAR TIRES ASDR AALA20110302LHR01Smoke Detector · faultyUPON LANDING RIGHT AFT LAVATORY SMOKE DETECTOR WENT OFF. NO GREEN LIGHT ON. CHECKED LAVATORY FOR SMOKE AND FIRE NONE NOTED. REPLACED SMOKE DETECTOR. OPS CHECK NORMAL.SDR AALA20110228LHR03Transformer · failedLHR - INFLIGHT CDG-JFK. CREW REPORTED RIGHT AC BUSS OFF LIGHT WITH CORRESPONDING ELECTRICAL BUS FAILURE. EMERGENCY DECLARED FLIGHT DIVERTED LHR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CURRENT TRANSFORMER T113. SYSTEM GROUND CHECK NSDR AALA20100224TUL12Frame · crackedFRAME AT STATION 522 IN THE FORWARD CARGO BETWEEN STRINGER 30 LEFT AND 31 LEFT WERE FOUND DAMAGED. THE SUBJECT DAMAGE IS LIMITED TO THE FRAME INNER CHORD BETWEEN STRINGER 30 LEFT AND 31 LEFT APPROXIMATELY 6 INCHES IN LENGTH. REPAIRED UNDER ENGINEERING AUTHORSDR AALA20100224TUL10Structure · crackedFOUND CRACK INDICATION AT STATION 1809.5 RIGHT FORWARD CHORD FASTENER HOLE. THE HOLE WAS OVERSIZED TO 0.2782 INCH IN ORDER TO REMOVE ANY CRACK INDICATIONS. BOEING REQUIRED AN INSURANCE CUT OF AT LEAST 0.030 INCH. THE INSURANCE CUT RESULTED IN A FINAL HOLE SSDR AALA20100118AFW03Frame · crackedFRAME AT STATION 500 IN THE FORWARD CARGO BETWEEN STRINGER 30 LEFT AND 31 LEFT WERE FOUND DAMAGED. THE SUBJECT DAMAGE IS LIMITED TO THE FRAME INNER CHORD BETWEEN STRINGER 30 LEFT AND 31 LEFT APPROXIMATELY 6 INCHES IN LENGTH. REPAIRED UNDER ENGINEERING AUTHORSDR AALA20100118AFW02Torque Box · crackedFOUND SEVERAL CRACKS AROUND THE LEFT PYLON STRUT TORQUE BOX FORWARD UPPER WEB POWER FEEDER CABLE CUTOUT. REPAIRED UNDER ENGINEERING AUTHORIZATION B767-54-008424 NR 1267610.SDR AALA20100118AFW01Structure · crackedFOUND CRACK INDICATION AT STATION 1809.5 LEFT FORWARD CHORD FASTENER HOLE. THE HOLE WAS OVERSIZED TO 0.2636 INCH IN ORDER TO REMOVE ANY CRACK INDICATIONS. BOEING REQUIRED AN INSURANCE CUT OF AT LEAST 0.030 INCH. THE INSURANCE CUT RESULTED IN A FINAL HOLE SISDR AALA20100224TUL08Skin · damagedONE UPPER SKIN PANEL 666JT FASTENER HOLE ON THE RIGHT OUTBOARD LEADING EDGE FLAP WAS DAMAGED DURING MAINTENANCE. REPAIRED UNDER EA COMP-57-008495.
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