N715AA
Service difficulty reports not matched to an aircraft · 116
They name N715AA, 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 = 'N715AA' 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 = 'N715AA' 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 C8GA20120208003Gyro · inaccurateDURING CRUISE, BOTH CAPTAIN'S AND FIRST OFFICER'S ADI SHOWED A 10 DEGREE LT TURN. AN EMERGENCY WAS DECLARED AND THE ACFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED. R & R THE NR 1 AND NR 2 GYRO, PERFORM OPERATION CHECKS WITH NO DEFECTS. SDR C8GA2011000027Warning Horn · false activationDURING TAKEOFF ROLL AT APPROX 60 KNOTS THE TAKEOFF WARNING HORN SOUNDED. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE BLOCKS WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED AND OPS CHECK OF THE TAKEOFF WARNING SYS WAS CONDUCTED NOTING NO DEFECTSDR C8GA2011000020Actuator · stickingAFTER TAKEOFF AND DURING CLIMB, THE NR 8 L/E SLAT IN TRANSIT LIGHT STAYED ON DURING FLAP RETRACTION AND ACFT ROLLED TO THE LT. THE ACFT RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED, R & R THE NR 8 L/E ACTUATOR AND PERSDR C8GA2011000018Relief Valve · leakingWHILE EN-ROUTE, THE CREW NOTED THAT THE B-SYSTEM HYD QUANTITY WAS DECREASING AND THE LOW LIGHT ILLUMINATED. ACFT DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED, NOTING THAT THE UPPER RUDDER LOAD LIMIT RELIEF VALUE WASSDR C8GA2011000015Carriage · brokenDURING CLIMB OPERATION, THE OTBD FLAPS FROZE AT 3 DEGREES ON CLIMBOUT, 9 UNITS OF AILERON TRIM WAS REQUIRED FOR LEVEL FLIGHT. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED NOTING THAT BOTH RT OTBD FORE FLAP SESDR C8GA2011000008Flap System · lack of lubeDURING DEPARTURE, ON FLAP RETRACTION THE OTBD FLAPS WOULD NOT RETRACT ABOVE 4 DEGREES. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED, FLAP SYS WAS LUBRICATED AND OPS CHECK PERFORMED WITH NO DEFECTS NOTED. ACFT WSDR C8GA2011000006Power Supply · inoperativeDURING TAKEOFF ROLL OUT, ALL 3 ENGINE FUEL FLOW INDICATIONS FLUXUATED BY + / - 5000 LBS. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO BLOCKS WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED NOTING FUEL FLOW POWER SUPPLY AT FAULT. R & R THE FUEL FLOW POWSDR C8GA2011000004Engine · damagedON TAKEOFF DEPARTING, WHILE CLIMBING THROUGH 1000' A LOUD BANG EMERGED FROM THE NR1 ENGINE. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED NOTING THAT NR 1 ENGINE REQUIRES REPLACEMESDR C8GA2010000072Floorbeam · corrodedDURING HEAVY MX INSP, IT WAS NOTED THAT THE FLOORBEAM FLANGE AT STA 1110 LBL 64. REMOVED CORROSION AND FABRICATED REPAIR ANGLES FROM 7075 T6, .090" DIM 13.5" X 4", 10.5" X 4" AND 4" X 1" FILLER INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SSDR C8GA2010000071Fitting · corrodedDURING HEAVY MX INSP, IT WAS NOTED THAT THE NLG RT TRUNNION FITTING HAVE CORROSION. REMOVED CORROSION AND REWORKED AREA. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000070Fitting · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE NOSE LANDING GEAR LT TRUNNION FITTINGS HAVE CORROSION. REMOVED CORROSION AND REWORKED AREA. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000069Fitting · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE LT MLG FWD TRUNNION FITTING HAS CORROSION. REMOVED CORROSION AND REWORKED AREA AND INSTALLED 2EA LOWER BUSHINGS AND 2EA UPPER BUSHINGS. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000068Fitting · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE RT MLG FWD TRUNION FITTING HAS CORROSION. REMOVED CORROSION AND REWORKED AREA AND INSTALLED 2 EA LOWER BUSHINGS. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000067Shear Tie · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE AFT CARGO STA 1148, BL 0 SHEAR-TIE IS CORRODED. REMOVED SHEAR-TIE AND FABRICATED NEW FROM 2024 T3 .050". INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000066Floorbeam · corrodedDURING HEAVY MX IT WAS NOTED THAT THE MAIN CARGO FLOORBEAM IS CORRODED AT STA 1110 LBL 35. CORROSION WAS REMOVED, FABRICATED DOUBLER FROM 7075 T6 .090", FILLER FROM 7075 T6 .125. INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000065Floorbeam · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE AFT CARGO FLOORBEAM STAT 1010, LBL 10 IS CORRODED. CUT OUT DAMAGE, FABRICATED REPAIR PARTS FROM 7075 T6 .063" DIM 18" X 3", STRAP FROM 7075 T6 .100" DIM. 18" X 2" FILLER FROM BAC1505-100797 DIM. 7.25" X 2.25" AND INSTSDR C8GA2010000064Floorbeam · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE AFT CARGO FLOORBEAM STA 1030, RBL 20 IS CORRODED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000063Bulkhead · crackedDURING HEAVY MX, WHILE PERFORMING INSPECTIONS, IT WAS NOTED THAT THE RT INBD WHEEL WELL FWD BULKHEAD SKIN IS CRACKED AT APU OUTLET DUCT CUT-OUT LOWER. FABRICATED DOUBLER'S FROM 15-5PH .050". INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVSDR C8GA2010000062Duct · corrodedDURING HEAVY MX, WHILE PERFORMING INSP, IT WAS NOTED THAT THE NR2 ENGINE "S" DUCT AT STATION 1203 6 O'CLOCK POSITION HAS CORROSION. REMOVED CORROSION AND FABRICATED REPAIR PARTS SPLICE STRAP FROM 301 1/2 HD , FABRICATED REPAIR DOUBLER FROM 7075 T6 .080". INSTASDR C8GA2010000061Skin · corrodedDURING HEAVY MX, WHILE PERFORMING INSPECTIONS, IT WAS NOTED THAT THE LT MLG WW INBD CTR CEILING AREA BL 0, STA 930 ABOVE APU SCREEN HAS CORROSION. REMOVED CORROSION AND FABRICATED DOUBLER FROM 2024 T3 .080" DIM 22" X 13". INSTALLED REPAIR, NO OTHER DEFECTS NOTSDR C8GA2010000060Web · dentedDURING HEAVY MX WHILE PERFORMING INSPECTIONS IT WAS NOTED THAT THE FWD CARGO DOOR FRAME AFT SIDE OF CUT-OUT AT BS 620 BETWEEN RBL 25-30 STRINGER 25R. REMOVED DAMAGE AND FABRICATED WEB REPAIR FROM 2024 T3 .040 DIM. 16.5" X 5". INSTALLED REPAIR, NO OTHER DEFECTSSDR C8GA2010000059Web · dentedDURING HEAVY MX PERFORMING INSPECTIONS IT WAS NOTED THAT THE FWD CARGO COMPARTMENT RT SIDE OF CARGO DOOR FRAME CUT-OUT AT BS 560 BETWEEN STR 23R & 25R. REMOVED DAMAGE AND FABRICATED WEB REPAIR FROM 7075 T6 .050 DIM. 15.5" X 5". INSTALLED REPAIR, NO OTHER DEFESDR ABXR201005260002Strap · crackedDURING A HEAVY MX EVENT THE LT WHEEL WELL STA 930 DECK STRAP WAS DISCOVERED CRACKED AND CORRODED JUST ABOVE THE HYD LINK CLUSTER. FABRICATED PRESSURE DECK STRAP FROM 2024-T3 .090 PO404503638 IAW SRM 53-1-02, FIG 5, SHEET 14, ITEM 164. ITEM WAS RETURNED TO SERVSDR C8GA20090298Actuator · malfunctionedDURING CLIMB OPERATION THE NR 7 L/E SLAT FAILED TO RETRACT. CREW PERFORMED REQUIRED CHECKLISTS AND RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED, THE NR 7 SLAT ACTUATOR WAS DETERMINED TO BE AT FAULT. REMOVED AND REPLSDR C8GA20090297Beam · corrodedWHILE PERFORMING AN "A" MX CHECK, CORROSION WAS NOTED ON THE RT HORIZ STAB T/E UPPER BEAM APPROX 24" FROM HORIZ TIP. CORROSION WAS EVALUATED AND REMOVED, INSTALLED PERMANENT REPAIR 2024 T3 .063" DIM 3" X 12". NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TOSDR C8GA20090067Wire · brokenFLT 1740 FROM BNA TO CLT, DURING APPROACH THE NOSE LANDING GEAR FAILED TO INDICATE DOWN AND LOCKED. THE RED LIGHT WAS ILLUMINATED AND THE GREEN LIGHT WAS OUT. THE CREW PERFORMED APPROPRIATE CHECK LIST AND LANDED WITHOUT INCIDENT IN CLT. POST FIGHT INSPECTIOSDR C8GA20090066Wire · chafedFLT 715 FROM MEM TO BNA, DURING SHORT APPROACH THE NOSE LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. THE RED LIGHT WAS ILLUMINATED AND THE GREEN LIGHT WAS OUT. THE CREW PERFORMED APPROPRIATE CHECK LIST AND LANDED WITHOUT INCIDENT IN BNA. POST FIGHT INSPECSDR C8GA20090065Accessory Unit · defectiveFLT 716 FROM BNA TO MEM, WHILE ON APPROACH INTO MEM THE NOSE GEAR FAILED TO INDICATE DOWN AND LOCKED. THE GREEN NOSE GEAR LIGHT WAS OUT, AND THE RED LIGHT WAS ILLUMINATED. AN ABORTED APPROACH WAS ACCOMPLISHED, CHECKLIST FOLLOWED AND AIRCRAFT LANDED IN MEM WISDR C8GA20080103Stiffener · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE WING CENTER SECTION LOWER FORWARD STIFFENER ON FORWARD CHORD AT BS 740 LBL-45 CORRODED. CORROSION TO BE OUT OF LIMITS, REMOVED STIFFENER, FABRICATED NEW FROM 7075 T6 DIM 15 INCH AND INSTALSDR C8GA20080102Structure · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE NR 3 SLAT OTBD STOP CUTOUT CORNER CRACKED. STOP DRILLED CRACK, PERFORMED HFEC WITH NO DEFECTS. FABRICATED DOUBLER FROM 2024 T3 .063 INCH DIM 9 INCH BY 9 INCH. INSTALLED REPAIR IAW SRM 57SDR C8GA20080101Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 686.50. REPAIRED LT WING TANK FUEL VENT LINE AT WBL 686.50 IAW COTNEY ED NR EDAG52-1. FABRICATED DOUBLER FROM 2024 0.040 INCH DIM 1.625 INCH SDR C8GA20080099Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 601.50. REPAIRED LT WING TANK FUEL VENT LINE AT WBL 601.50 IAW COTNEY ED NR EDAG52-1. FABRICATED DOUBLER FROM 2024 0.040 INCH DIM 1.625 INCH SDR C8GA20080100Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 656.50. REPAIRED L/WING TANK FUEL VENT LINE AT WBL 656.50 IAW COTNEY ED NR EDAG52-1. FABRICATED DOUBLER FROM 2024 0.040 INCH DIM 1.625 INCH BSDR C8GA20080098Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 601.50. REPAIRED LT WING TANK FUEL VENT LINE AT WBL 601.50 IAW COTNEY ED NR EDAG52-1. FABRICATED DOUBLER FROM 2024 0.040 INCH DIM 1.625 INCH SDR C8GA20080097Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 519. REPAIRED LT WING TANK FUEL VENT LINE AT WBL 519 IAW COTNEY ED NR EDAG52-1. FABRICATED DOUBLER FROM 2024 0.040 INCH DIM 1.625 INCH BY 4.2SDR C8GA20080096Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT TOP CLAMP WBL 442. REPAIRED LT WING TANK FUEL VENT LINE AT WBL 442 IAW COTNEY ED NR EDAG52-1. FABRICATED DOUBLER FROM 2024 0.040 INCH DIM 1.625 INCH BYSDR C8GA20080095Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 383.50. REPAIRED LT TANK FUEL VENT LINE AT WBL 383.50 IAW COTNEY ED NR EDAG52-1. FABRICATED DOUBLER FROM 2024 0.040 INCH DIM 1.625 INCH BY 4.SDR C8GA20080094Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT TOP OF CLAMP WBL 348.00. REPAIRED LT WING TANK FUEL VENT LINE AT WBL 348 IAW ED NR EDAG52-1. LEAK CHECK GOOD. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RESDR C8GA20080093Fitting · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE AFT I BEAM SUPPORT SHACKLE FITTING HAS EXFOLIATING CORROSION AT BS 307-0. REMOVED FITTINGS AND FABRICATED 2 NEW FITTINGS. INSTALLED NEW FITTINGS IAW DWG NR 69-45947-1-1 AND 51-30-1. NO OSDR C8GA20080092Skin · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING L/E WS 530 AT HOOK CUTOUT AFT REPAIR HAS CRACK. REMOVED PREVIOUS REPAIR, FABRICATED NEW PLATE FROM AISI 301 1/2 HARD .020 INCH DIM 8 INCH BY 6 INCH. INSTALLED REPAIR IAW SRM 57-30SDR C8GA20080091Intercostal · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE INTERCOSTAL WEB AT BS 490-510 STR 28R HAS CORROSION. REMOVED INTERCOSTAL AND FABRICATED ANGLE FROM 7075 T6 DIM 18.5". INSTALLED INTERCOSTAL AND FABRICATED ANGLE IAW B727 SRM 53-10-2, 51-3SDR C8GA20080087Skin · dentedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS 2 EA DENTS WERE NOTED AT BS 575-583 BETWEEN STR. 26R-27R. CUT OUT 2 EA DAMAGED AREAS, FABRICATED DOUBLER, AND SHIMS. PERFORMED HFEC INSPECTION NO DEFECTS NOTED. INSTALLED REPAIR IAW DWG AG52-53-101. NO OTHER SDR C8GA20080085Intercostal · brokenWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE INTERCOSTAL SKIN ATTACH FLANGE WAS BROKEN AT BS 950A - 950B STR 28L. REMOVED BROKEN INTERCOSTAL AND FABRICATED NEW. INSTALLED FABRICATED INTERCOSTAL IAW SRM 53-10-2 AND 51-20-1. NO OTHESDR C8GA20080086Skin · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT FUSELAGE SKIN IS CORRODED BELOW STR 28R AT BS 490-510.CORROSION OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED DOUBLER, FABRICATED 2 FILLERS. INSTALLED REPAIR IAW SRM 53-30-3. NO OTHER DEFECTS NSDR C8GA20080070Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT STRINGER 29L STA 950C - 1000 IS CORRODED. REMOVED AND REPLACED STRINGER 29L P/N 65-56441-7. INSTALLED STRINGER IAW SB 727-53-0179. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA20080067Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STRINGER 29R WAS CORRODED UNDER BS 950E FRAME EXTENDING TO BS 1000. CORROSION AT STR. 29R WAS OUT OF LIMITS. CUT OUT DAMAGED STR 29R AT BS 950 TO 1006. INSTALLED NEW STRINGER P/N 65-56441-8. WORK PERFORMED IASDR C8GA20080064Stringer · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT STR. 27R LOCATED AT BS. 1010-1030 HAD EXFOLIATED CORROSION. REMOVED CORROSION, CORROSION AFTER CLEAN UP FOUND TO BE BEYOND LIMITS. FABRICATED DOUBLER. INSTALLED REPAIR AT BS 950E-1010 PER EA ESDR C8GA20080084Structure · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE LOWER CHORD RUNNING ALONG STR 27R BY THE C2 DOOR IS CORRODED AND CRACKED AT BOTH ENDS, STA 950E-1010. CUT OUT DAMAGED AREA, PERFORMED HFEC INSPECTION AND FABRICATED REPAIR ANGLE FROM 7075SDR C8GA20080083AIntercostal · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS SURFACE CORROSION WAS NOTED ON INTERCOSTAL BS 695 STR 27R. DAMAGED INTERCOSTAL WAS REMOVED, A NEW INTERCOSTAL WAS FABRICATED. INSTALLED REPAIR IAW SRM 53-10-2 AND 51-10-3. NO OTHER DEFECTS NOTED. AIRCRAFT WSDR C8GA20080083Frame · corrodedWHILE IN HEAVY PERFORMING INSPECTIONS IT WAS NOTED THAT THE FRAME WAS DENTED AT BS 1110 JUST ABOVE STR 26R CUT OUT DAMAGED FRAME AND FABRICATED NEW FRAME FROM 7075-O .063 INCH 23 INCH BY 4.5 INCH. HEAT TREATED FRAME TO T6. INSTALLED REPAIR IAW SRM 53-10-2 AN
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