N687FE
Service difficulty reports · 126
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 = 'N687FE' 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 = 'N687FE' 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 FDEA202602260281Slide · faultedWHILE ACCOMPLISHING F.E.A. 6-2560-F0386375 FOUND RIVETS PULLED THROUGH AND METAL STRIP PULLED AWAY FROM SLIDE HOUSING. AMM: 25-61-21-04 FEA: 6-25-0-F0386375 REMOVED AND REPLACED L1 DUAL ESCAPE SLIDE - SAFETY PIN PULLED - ARMED AND DISARMED INDICATIONSSDR FDEA202602180231Battery · inoperativeEMERGENCY LIGHTS DOOR TEST INOP AMM: 33-51-14-04 REMOVED/INSTALLED EMERGENCY POWER SUPPLY UNIT PER AMM REF. ABOVE, OPS CHECK GOOD. A/C OK FOR SERVICE.SDR FDEA202508201511None · noneEXISTING REPAIR FOUND ON RH WING NEW #5 SPOILER CENTER HINGE ARM COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING SDR FDEA202508201510None · noneEXISTING REPAIR FOUND ON LH WING NEW #5 SPOILER OF TRAILING EDGE COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTINSDR FDEA202508181508None · no discrepancyEXISTING REPAIR FOUND ON LH WING NEW #5 SPOILER CENTER HINGE ARM COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING SDR FDEA202508111406Profile · crackedMAIN DECK FLOOR STRUCTURE WAS FOUND PROFILE-Z CRACK AT FR80/82, Y1448. REPLACED THE CRACK PROFILE-Z WITH NEW PART.LOCATE AT MAIN DECK FLOOR FR80/82 Y1448.I.A.W A300-600F SRM 51-72-10-001 PAGE 2 AND 51-40-21-001 PARA 6 PAGE 7B~PAGE 23.REPAIR CLASSIFIED AS SDR FDEA202508071530Seat Track · wornMAIN DECK FLOOR STRUCTURE WAS FOUND SEAT TRACK CROWN WORN AT FR28 PLUS 13"~FR28 PLUS 14", Y450. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK AT FR26~30,Y450 I.A.W A300-600F SRM 53-10-16-201 PARA.4 FIG201, PAGE203~208. THIS REPAIRSDR FDEA202508071529Seat Track · wornMAIN DECK FLOOR STRUCTURE WAS FOUND SEAT TRACK CROWN WORN AT FR28 PLUS 14", -Y953 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK AT FR26~32,- Y953 I.A.W A300-600F SRM 53-10-16-201 PARA.4 FIG201, PAGE203~208. THIS REPAIR IS CLASSIFIED SDR FDEA202508051405Profile · crackedMAIN DECK FLOOR STRUCTURE WAS FOUND PROFILE-Z CRACK AT FR80/82,-Y1448. REPLACED THE CRACK PROFILE-Z WITH NEW PART.LOCATE AT MAIN DECK FLOOR FR80/82 - Y1448.I.A.W A300-600F SRM 51-72-10-001 PAGE 2 AND 51-40-21-001 PARA 6 PAGE 7B~PAGE 23.REPAIR CLASSIFIED ASSDR FDEA202508041520Skin · contaminated1EA WATER TRAPPED AREA(80MM*100MM) WERE FOUND AT L/H ELEVATOR TOP SKIN PANEL T/E NO.22 FASTENER. *COUNTING FASTENER FROM I/B TO O/B* ACCOMPLISHED THE COMPOSITE REPAIR AT L/H ELEVATOR TOP SKIN PANEL T/E NO.22 FASTENER POSITION. I.A.W A300-600F SRM 55-21-12-SDR FDEA202508041519Skin · contaminated1EA WATER TRAPPED AREA(110MM*100MM) WERE FOUND AT L/H ELEVATOR TOP SKIN PANEL T/E NO.30 FASTENER. *COUNTING FASTENER FROM I/B TO O/B* ACCOMPLISHED THE COMPOSITE REPAIR AT L/H ELEVATOR TOP SKIN PANEL T/E NO.30 FASTENER POSITION. I.A.W A300-600F SRM 55-21-12SDR FDEA202508041518Skin · contaminated1EA WATER TRAPPED AREA(95MM*70MM) WERE FOUND AT L/H ELEVATOR TOP SKIN PANEL T/E NO.20 FASTENER. *COUNTING FASTENER FROM I/B TO O/B* ACCOMPLISHED THE COMPOSITE REPAIR AT L/H ELEVATOR TOP SKIN PANEL T/E NO.20 FASTENER POSITION. I.A.W A300-600F SRM 55-21-12-2SDR FDEA202508041517Skin · contaminated1EA WATER TRAPPED AREA(70MM*70MM) WERE FOUND AT L/H ELEVATOR TOP SKIN PANEL T/E NO.5 FASTENER. *COUNTING FASTENER FROM I/B TO O/B* ACCOMPLISHED THE COMPOSITE REPAIR AT L/H ELEVATOR TOP SKIN PANEL T/E NO.5 FASTENER POSITION. I.A.W A300-600F SRM 55-21-12-201SDR FDEA202508041385Seat Track · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING REPAIR ANGLE FOUND ON MDCC SEAT TRACK BTW FR60~61,-Y450 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.7SDR FDEA202508041384Doubler · no discrepancyEXISTING DOUBLER REPAIR FOUND ON RH O/B FLAP UPR SKIN BTW RIB3~4,S-1.2 ~ FRONT SPAR COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPSDR FDEA202508041375Seat Track · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON MDCC SEAT TRACK BTW FR31~34,-Y450 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.SDR FDEA202508031488Floor Support · crackedFOUND SUPPORT CRACK AT MDCC FLOOR STRUCTURE FR37~FR38,-Y2465 POS. REPLACED CRACK SUPPORT WITH NEW ONE. AT MDCC FLOOR STRUCTURE FR37~FR38, -Y2465 POS. I.A.W A300-600F SRM 51-72-10-001, PAGE2 AND 51-40-21-001 PARA6 PAGE 7B-23. THIS REPAIR CLASSIFIED AS MINORSDR FDEA202508031487Floor Support · crackedFOUND SUPPORT CRACK AT MDCC FLOOR STRUCTURE FR38.1~FR38.2,-Y2465 POS. REPLACED CRACK SUPPORT WITH NEW ONE. AT MDCC FLOOR STRUCTURE FR38.1~FR38.2, - Y2465 POS. I.A.W A300-600F SRM 51-72-10-001, PAGE2 AND 51-40-21-001 PARA6 PAGE 7B-23. THIS REPAIR CLASSIFIED SDR FDEA202508031486Floor Support · crackedFOUND SUPPORT CRACK AT MDCC FLOOR STRUCTURE FR38.1~FR38.2, Y2465 POS. REPLACED CRACK SUPPORT WITH NEW ONE. AT MDCC FLOOR STRUCTURE FR38.1~FR38.2, Y2465 POS. I.A.W A300-600F SRM 51-72-10-001, PAGE2 AND 51-40-21-001 PARA6 PAGE 7B-23. THIS REPAIR CLASSIFIED SDR FDEA202508031485Floor Support · crackedFOUND SUPPORT CRACK AT MDCC FLOOR STRUCTURE FR38~FR38.1, Y2465 POS REPLACED CRACK SUPPORT WITH NEW ONE. AT MDCC FLOOR STRUCTURE FR38~FR38.1, Y2465 POS. I.A.W A300-600F SRM 51-72-10-001, PAGE2 AND 51-40-21-001 PARA6 PAGE 7B-23. THIS REPAIR CLASSIFIED AS MISDR FDEA202508021537Skin · dentedLH WING #1 SLAT O/B AFT SURFACE TOP AREA GOT A DENT ABOVE FOLDING NOSE. PERFORMED CUT OUT DAMAGED BOTTOM SKIN. AND INSTALLED 2EA REPAIR PARTS WITH ADHESIVE FOR CURE AT LH WING #1 SLAT O/B AFT SURFACE TOP AREA ABOVE FOLDING NOSE POSITION. I.A.W FEDEX EA NO:SDR FDEA202507311605Fitting · damagedREPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23 PER EO NO:E6- 5230-E0378588 B P5 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR23, LONGN1~LONGN3. I.A.W FEDEX EO NO:E6-5230-E0378588 B P5, SEQ NO:1101, TITLE:DOOSDR FDEA202507301551Flap · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON LH INBD FLAP LWR SKIN BTW RIB12A~14A, T/E-21" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF DOUBLER REPAIR WITHOUT REPAIR RECORD AND DETERMINED IT NOT CONFORMITY ANY FAASDR FDEA202507301386Doubler · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING FLUSH DOUBLER REPAIR FOUND ON LH WING #1 SLAT NOSE SKIN BTW RIB 9~10 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTSSDR FDEA202507301372Skin · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER16-12", T/E-22" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTSDR FDEA202507291604Fitting · crackedTHE MDCD BEARING FITTING AT FR24 WAS FOUND CRACK ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR24, LONGN 1 ~ LONGN 3. I.A.W FEDEX EO NO:E6-5230-E0378588B P5, SEQ NO:1101, TITLE:DOORS - CARGO DOOR /HYD SYS -DETAILED VISUAL INSPSDR FDEA202409051246Steering Sys · malfunctionedLOW SPEED RTO AT APPROX 60 KNOS ON RW 31 AT YWG. FO REPORTED DIFFICULTY W/DIRECTIONAL CONTROL. FULL LEFT RUDR ALL THE WAY TO THE STOPS WAS NEEDED TO MAINTAIN CENTERLINE. AFTER THE REJECT THE WHEELS ON THE LEFT TRUCK HEATED TO OVER 300 DEGREES, WHILE THE TSDR FDEA202408281180Support Fitting · corrodedSMIS 687 57-10 6415 01JUL24 17:18 MEM FACT WS-C 00088832 MOD TYPE F MOD NO. 6-5710-F0377949 REV NO. PS P1 WINGS - MAIN LANDING GEAR SUPPORT WING RIB 5 - INSPECTION OF FWD PINTLE BUSHES COMPLY WITH FEA 6-5710-F0377949 REV NO. POS. P1 WINGS SDR FDEA202408271178Support Rib · corrodedRH FWD LUG RIB 5 CORROSION FOUND IN BORE . REMOVED CORROSION FROM R/H MLG RIB 5 FWD LUG PER, E.A.6-5710-T0380346 PT 1SDR FDEA202404300532Pitot Tube · cloggedIN CRUISE, BOTH CAPT AND FO STANDBY AIRSPEED INDICATORS WERE INACCURATE. STANDBY INDICATORS SEEMED TO INDICATE APPROXIMATELY HALF OF ACTUAL IAS AT ALL ALTITUDES. AT FL340, .787M, 280 IAS, CAPTAIN STANDBY AIRSPEED SHOWED 129 AND FOS SHOWED 130. AT 25K SDR FDEA202307081187Actuator · failedPDIS 687 52-30 5349 08JUL23 MEM OPEN U UPON ARRIVAL IN MEMPHIS. BLOCKED AT GATE.GROUND CREW ADVISED MAIN CARGO DOOR LOCKS WERE OPEN ALONG WITH MAIN HANDLE.NO INDICATIONS IN COCKPIT ECAM DOOR PAGE .UPON VISUAL INSPECTION FOUND LATCHES AND DOORSDR FDEA202304140643Seat Track · damagedHUB REPORTED BROKEN LOCK AT POSITION (3D) DURING LOAD, ID OF LOCK IS (J754) ITEM PLACED ON MEL 25-50-02-01-J WRI2550-5158. THIS ACTION TO OIL SEAT TRACK DAMAGE FOR REPAIR AT LATER DATE. REPAIRED THE DAMAGED SEAT TRACK AT FR28-FR30 -Y953 PER A300-600F SRM53SDR FDEA202108011915Valve · failedMDIS 687 36-10 3306 31JUL21 MEM OPEN U FWD GROUND PNUMATIC SUPPLY PORT CHECK VALVE LEAKS AFTER ENGINE AIRSTART COMPLETED. SHGN 31JUL21 23:40 MEM U INSPECTED FWD GROUND PNUMATIC AIR SUPPLY CHECK VALVE. FOUND SPRING THAT NORMALLY CLOSES THE CSDR FDEA202010302723Compressor · stalledAFTER DEPARTURE PASSING 10,000 RECEIVED ENG #2 MODE FAULT FOLLOWED ECAM AND REDUCED POWER AND RESELECT N1 MODE. FAULT CLEARED AFTER 10 SECOND HAD SEVERE BANK AND YAW ON RIGHT SIDE.SUSPECT COMPRESSOR STALL. ACCOMPLISHED BORESCOPE AND ENGINE STALL INSPECTISDR FDEA202010142485Skin · gougedRT NR 1 SLAT OUTBOARD INNER SURFACE GOUGED (3 LOCATION) RT NR 1 SLAT OUTBOARD INNER SURFACE GOUGED. COMPLIED WITH EA: 6-5750-T0357343 P1. THIS IS CAT A REPAIR. MAJOR REPAIR, IAW GMM 6-2-100.SDR FDEA202010142487Beam · crackedNDT INSP LT CENTER WING JOINT AT FR 40 MID HOLE FOUND CRACKED SIGNAL. REAMED THE HOLE THROUGH ALL LAYERS STEP BY STEP 0.4OMM EACH TIME NOT EXCEED R2 DIMENSION, PER A300-600F SRM51-40-44. PERFORMED ROTO-TEST INSPECTION AND NO CRACK FOUND, PER A300-600F NTM51-SDR FDEA202010132470Skin · delaminatedRT WING NR 5 SPOILER INBOARD HINGE ARM OUTBOARD SURFACE DELAMINATED. 20MM X 25MM DEPTH: 1.10MM. OUTBOARD HINGE ARM LOWER SURFACE DELAMINATED. 15MM X 20MM DEPTH: 1.97MM. RT WING NR 5 SPOILER INBOARD HINGE ARM DELAMINATED. COMPLIED WITH EA: 6-5750-T0357149SDR FDEA202010132469Skin · delaminatedRT WING NR 4 SPOILER INBOARD HINGE ARM OUTBOARD SURFACE DELAMINATED, 20MMX30MM DEPTH: 1.20MM. OUTBOARD HINGE ARM LOWER SURFACE DELAMINATED, 15MM X 55MM DEPTH: 1.93MM. OUTBOARD HINGE ARM OUTBOARD SURFACE DELAMINTED, 20MM X 25MM DEPTH: 1.20MM. RT WING NR 4 SPSDR FDEA202010132468Skin · delaminatedLT WING NR 5 SPOILER INBOARD HINGE ARM OUTBOARD SURFACE DELAMINATED, 30MM X 35MM DEPTH: 1.35MM. OUTBOARD HINGE ARM LOWER SURFACE DELAMINATED, 20MM X 55MM DEPTH: 1.95MM. OUTBOARD HINGE ARM OUTBOARD SURFACE DELAMINATED, 20MM X 40MM DEPTH: 1.30MM. LT WING NR 5SDR FDEA202010132467Skin · delaminatedLT WING NR 3 SPOILER INBOARD HINGE ARM OUTBD SURFACE DELAMINATED. 63MM X 23MM DEPTH: 1.50MM LT WING NR 3 SPOILER INBOARD HINGE ARM OUTBOARD SURFACE DELAMINATED. COMPLIED WITH EA: 6-5750-T0357145. THIS IS CAT A REPAIR. MAJOR REPAIR, IAW GMM 6-2-100.SDR FDEA202010132466Skin · delaminatedLT WING NR 4 SPOILER INBOARD HINGE ARM OUTBOARD SURFACE DELAMINATED, 20MM X 15MM DEPTH: 1.30MM. INBOARD HINGE ARM LOWER SURFACE DELAMINATED, 15MM X 20MM DEPTH: 1.90MM. OUTBOARD HINGE ARM OUTBD SURFACE DELAMINATED, 30MM X 20MM DEPTH: 1.27MM. LT WING NR 4 SPOSDR FDEA202007311736Handle · unsecurePASSING 180 CLIMBING, HEARD THUMP AND AIRCRAFT LURCHED. CONTROLS AND CONTROLABILITY FELT NORMAL. FOUND MAIN CARGO DOOR LATCH HANDLE DEPLOYED APPROX.3 INCHES UPON BLOCK IN. OPERATED DOOR SEVERAL TIMES AND OPERATION WAS NORMAL. WHILE UNLATCHING DOOR AT CSDR FDEA202007301729Handle · unsecurePASSING 180, HEARD A THUMP & ACFT LURCHED, CONTROLS & CONTROLABILITY NORMAL. FOUND MAIN CARGO DOOR LATCH HANDLE DEPLOYED APPROX 3 INCHES. OPERATED DOOR SEVERAL TIMES & OPERATION WAS NORMAL. WHILE UNLATCHING DOOR AT CONTROL PANEL, THERE WAS A 2 SEC DELASDR FDEA2020061631252Smoke Detector · failedAFTER TAKE OFF, RECEIVED AN AVIONICS SMOKE ECAM. COMPLIED WIH QRH PROCEDURES AND RETURNED TO DEPARTURE. R & R THE SMOKE DETECTOR 13WA IAW MM 26-15-12-04, TESTED GOOD IAW MM 26-15-00-05. OK FOR SERVICE.SDR FDEA2019081521853Relay · failedSHUTDOWN THE NR 1 ENGINE WHILE TAXING IN. AFTER THE HYDRAULIC PRESSURE FELL TO ZERO, THE NOSEWHEEL STEERING LOST HYD PRESSURE AND SLOWLY ROTATED TILLER TO FULL LEFT DEFLECTION. WAS UNABLE TO TURN THE TILLER. RESTARTED THE NR 1 ENGINE, ALL CONTROL OF NWS SDR FDEA201810263022Switch · inoperativeDURING PUSHBACK, AND DURING SECOND ENGINE START, RECEIVED A YELLOW SERVO CONTROL JAMB. REMOVE AND REPLACED RIGHT ELEVATOR YELLOW SYSTEM SERVO CONTROL CONTROL JAMB DETECTION SWITCH IAW MM 27-34-12-04, OPS TESTED GOOD IAW MM 27-34-12-04, OK FOR SERVICE.SDR FDEA201809142526Switch · inoperativeON CLIMB OUT GOT MAIN CARGO DOOR NOT LOCKED. COMPLETED QRH AND RTB CYYC. RELEASED FOR SERVICE. MAIN CARGO DOOR CLOSED & LOCKED INDICATION ON ECAM DOOR PAGE INOP. REMOVED AND REPLACED WARNING SWITCH 49WS IAW AMM 52-71-00-04-02 AND PERFORMED ADJUSTMENT/TEST IAWSDR FDEA201804130987Frame · crackedUNDER FLOOR PANEL 242YH AT -Y225, FRAME 47 WEB IS CRACKED. REMOVED AND REPLACED DAMAGED WEB IAW SRM 51-40-21. WEB FABRICATED ON T18/1334842 IAW SRM 53-15-15 CLASSIFIED AS A CAT "A" MAJOR REPAIR.SDR FDEA201804130986Floor Panel · brokenMDCC 231GG FLOOR PANEL BROKEN FABRICATED NEW PANEL 231GG ON T18/1334619 IAW DWG SRZ 25-005 REV M. CLASSIFIED AS A CAT "A" MAJOR REPAIR.SDR FDEA201804130985Floor Panel · damagedMDCC 232GG FLOOR PANEL BROKEN FABRICATED NEW PANEL 232GG ON T18/1334801 IAW DWG SRZ 25-005 REV M. CLASSIFIED AS A CAT "A" MAJOR REPAIR.
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