N661FE
Service difficulty reports · 318
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 = 'N661FE' 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 = 'N661FE' 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 FDEA202609061267Frame · crackedINSPECTION OF FRAME 40 LT, LOWER WING JUNCTION, FOUND A CRACK SIGNAL AT FASTENER HOLE NR 1. COMPLIED WITH EA: 6-5710-T0388595 P1. REPAIRED FRAME 40 LT LOWER JUNCTION, CRACKED FASTENER HOLE NR 1. THIS IS CATEGORY B REPAIR. FOLLOW UP INSPECTION IAW EA 6-5710-SDR FDEA202609061266Seat Track · corrodedMAIN DECK SEAT TRACK AT Y1959 BETWEEN FR53 AND FR54 CORRODED. REPAIRED THE CORRODED MAIN DECK SEAT TRACK AT Y1959 BETWEEN FR53 AND FR54 PER SRM53-10-16-201 FIG.201 & EA: 6-5310-T0388627 P1. CATEGORY -A- MAJOR REPAIR IAW GMM6-2-100.SDR FDEA202609011253Seat Track · wornMAIN DECK SEAT TRACK AT Y1959 BETWEEN FR 62 AND FR 63 FOUND WORN. SEAT TRACK SECTION AT Y1959 BETWEEN FR62 AND FR63 PER A300-600F SRM51-40-21 & SRM53-10-16-201 FIG.201. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.SDR FDEA202608261228Attach Fitting · crackedFWD CARGO DOOR ACTUATOR ATTACH FITTING FOUND 2EA CRACKS BY HFEC INSPECTION. REPLACED THE CRACKED FWD CARGO DOOR ACTUATOR ATTACH FITTING WITH FABRICATED PART PER SRM51-40-21 & DWG: F52370695(ISSUE. J), A52370501(ISSUE. J) & A52370534(ISSUE. F). RSC TRACKING SDR FDEA202605040543Battery · no testEMERGENCY LIGHT TEST IN COURIER AREA WON'T TEST ON PREFLIGHT. MANUAL OPERATES OK. AMM 33-51-00-05 REMOVED AND REPLACED MAIN DECK EMERGENCY LIGHT BATTERY REF AMM 33-51-00-05. COURIER AREA EMERGENCY LIGHT TEST CKS GOOD.SDR FDEA202602150207Safety Wire · wrong partWHILE PERFORMING F.E.A. 6-2560-F0386375 A P1, FOUND EJECTOR BAG RELEASE CABLE WITH INCORRECT SAFETY WIRE. L1 DOOR SLIDE AMM: 25-61-20-05-01. REMOVED AND REPLACED COPPER WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE. OPS CHK GOOD. A/C OK FOR SERVICE.SDR FDEA202602150206Slide · damagedWHILE COMPLING WITH FEA 6-2560-F0386375 A PART 1, FOUND R1 DOOR SLIDE DAMAGED AND WILL RETURN TO STORES. R/I 15FEB26 01:46 MEM REASON CODE : FAILED OPS CK. & REPLACED WITH SERVICABLE UNIT REMOVED & REPLACED R1 DOOR SLIDE. BROKEN SLIDE REMOVED IS PSDR FDEA202512242287Valve · failedDURING APPROACH, LANDING GEAR WOULD NOT EXTEND AFTER MULTIPLE CYCLES AND SWITCHING SYSTEMS 1 & 2. HYDRAULICS GOOD. USED LANDING GEAR GRAVITY EXTENSION QRH PROCEDURE, GEAR EXTENDED. LANDED UNEVENTFULLY, TOWED IN FROM RUNWAY DUE TO NO NOSE WHEEL STEERING. SDR FDEA202508151454Monitor · expiredCO2 MONITOR (S/N AREJ-2218) CALIBRATION CYCLE EXPIRED. REMOVED AND REPLACED CO2 MONITOR WITH EXPIRED CALIBRATION CYCLE.SDR FDEA202504120591Power Supply · no testL1 AND R1 DOOR SLIDE TEST WARNING LIGHTS DO NOT ILLUMINATE DURING TEST. BUZZERS WORK NORMALLY. L1 AND R1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHTS - INOP. MEL: 52-73-01-01 REPLACED AUTONOMOUS STANDBY POWER SUPPLY UNIT PER A.M.M. 52-73-18- 04. SDR FDEA202407080963Csu · failedAFTER TAKEOFF ON GEAR RETRACTION THE CAPTAIN RED SPD LIM APPEARED ON PFD. THE NUMBER 2 FAC WAS DEFERRED PER MEL 22-26-34-01 AND THE OP NOTES ABOUT SPEED TREND ,VSS, VLS,VMAX,F,S SPEEDS ETC WERE ALSO INDICATED AND MISSING ON CAPT PFD. EMERGENCY DECLARED.SDR FDEA202407060950Jackscrew · failedON DEPARTURE 15/0 CONFIGURATION AFTER AT SAFE SPEED WE RETRACTED THE SLATS AND RECEIVED ECAM WARNING OF FLAPS SYS 1 AND 2 FAULT/ FLAPS STUCK. DID NOT CYCLE BECAUSE FLAPS WERE NOT USED AND BOTH FLAPS AND SLATS WERE AT 0. DECLARED AN EMERGENCY AND PROCEED SDR FDEA202406220835Controller · malfunctionedFLAPS STUCK AT 15 ON TAKEOFF. CYCLED NO CHANGE. NO OVERSPEED. AMM 27-51-18-04. T/S PER TSM 27-50-02. RESET TORQUE LIMITERS. OPS SLATS/FLAPS THROUGH ALL DETENTS. NO FAULTS OR ANOMALIES NOTED DURING OPS. TORQUE LIMITERS OPS NORMAL. CHECKED OIL LEVEL OF FLAPSDR FDEA202406010761Jackscrew · bindingFLAPS/SLATS STUCK 15/15 ON DEPARTURE. EMERGENCY DECLARED. QRH FOLLOWED. FLAPS OVERSPEED AT 15/15 TO APPROX 225 KTS. ***EMERGENCY DECLARED*** REF TSI 27-80/6666 FOR RH WING #1 SLAT SCREWJACK TORQUE INDICATOR FOUND TRIPPED. ALL SERVICING AND OTHER SDR FDEA202405060601Fitting · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIRS FOUND ON RHW RIBS OF T/E STRUCTURE AT WI.AX 21.9 NEAR AFT LUG COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQSDR FDEA202405060600Fitting · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIRS FOUND ON RHW RIBS OF T/E STRUCTURE AT WI.AX 13.9 NEAR AFT LUG COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQSDR FDEA202405060599Fitting · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIRS FOUND ON RHW RIBS OF T/E STRUCTURE AT RIB6A NEAR AFT LUG COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMSDR FDEA202405050577Skin · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON LHW CTR FLAP UPR SKIN BTW RIB12~13, T/E-13.8" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT WAS UNDOCUMENTED REPAIR, REMOVED EXISTING REPASDR FDEA202404260296None · noneEXISTING REPAIR FOUND ON M/D CROSSBEAM AT FR29, BTW Y1456 TO -Y1456 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 EXISTISDR FDEA202404210650Skin · crackedPFM EA#: 6-5750-T0378801 P1 FOUND NEW CRACK AT LH WING CTR FLAP RIB26 BTWN STGR 2.7-2.8 ACCOMPLISHED THE CAT.A FLANGE REPAIR AT RIB 26 UPPER FLANGE S-2.7~S-2.8, THE REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-T0378801 P1, SEQ NO:1119SDR FDEA202404160585Dummy Rail · wornFR54/FR54.2 LH NO.5 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.14MM REPLACED DAMAGED DUMMY SEAT TRACK WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001,P2 AND 51-40-21-001 PARA7 P24~P50, THE REPAIR CLASSIFIED AS MINOR PERSDR FDEA202404150670Fitting · crackedTHE MDC DOOR ACTUATOR AFT SUPPORT FRAME WAS FOUND CRACK ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR24 LONGN1~LONGN3 I.A.W FEDEX EA NO:T6-5230-T0378797 P1, SEQ NO:1121, TITLE:DOORS-CARGO DOOR /HYD SYS-MAIN CARGO ACTUATOR BEARISDR FDEA202404110576Rib · gougedR/H SPOILER 3 I/B JACK RIB LWR BORE EDGE DAMAGE. ACCOMPLISHED THE CAT.B HOLE REINFORCEMENT REPAIR AT RH WING NO.3 SPOILER JACK RIB AT ABX 31.675 LOWER HOLE. THE REPAIR CLASSIFIED AS MAJOR REF GMM 6-2-100. I.A.W FEDEX EA:T6-5740-T0378859 P1 SEQ NO:1106, TITSDR FDEA202404110575Rib · gougedR/H SPOILER 3 I/B JACK RIB UPR BORE EDGE DAMAGE. ACCOMPLISHED THE CAT.B HOLE REINFORCEMENT REPAIR AT RH WING NO.3 SPOILER JACK RIB AT ABX 31.675 UPPER HOLE. THE REPAIR CLASSIFIED AS MAJOR REF GMM 6-2-100. I.A.W FEDEX EA:T6-5740-T0378859 P1 SEQ NO:1106, TITSDR FDEA202404110574Rib · gougedR/H SPOILER 7 I/B JACK RIB UPR BORE EDGE DAMAGE ACCOMPLISHED THE CAT.B HOLE REINFORCEMENT REPAIR AT RH WING NO:7 SPOILER JACK RIB AT SP2X 31.675 UPPER HOLE. THE REPAIR CLASSIFIED AS MAJOR REF GMM 6-2-100. I.A.W FEDEX EA:T6-5740-T0378863 P1, SEQ NO:1109, TISDR FDEA202404110573Rib · corrodedLH WING NO.5 SPOILER I/B UPPER JACK RIB SCREW HOLE O/B EDGE CORRODED. ACCOMPLISHED THE CAT.B HOLE REINFORCEMENT REPAIR AT LH WING NO.5 SPOILER JACK RIB AT ABX 175.875 UPPER HOLE. THE REPAIR CLASSIFIED AS MAJOR REF GMM 6-2-100. I.A.W FEDEX EA:T6-5740-T03788SDR FDEA202404110572Rib · gougedLH WING NO.3 SPOILER UPR JACK RIB SCREW HOLE INNER SURFACE SCRATCH. ACCOMPLISHED THE CAT.B HOLE REINFORCEMENT REPAIR AT LH WING NO.3 SPOILER JACK RIB STA ABX 40.425 UPPER HOLE. THE REPAIR CLASSIFIED AS MAJOR REF GMM 6-2-100. I.A.W FEDEX EA:T6-5740-T037886SDR FDEA202404110571Rib · gougedLH WING NO.3 SPOILER LWR JACK RIB SCREW HOLE O/B EDGE DAMAGE. ACCOMPLISHED THE CAT.B HOLE REINFORCEMENT REPAIR AT LH WING NO.3 SPOILER JACK RIB AT ABX 40.425 LOWER HOLE. THE REPAIR CLASSIFIED AS MAJOR REF GMM 6-2-100. I.A.W FEDEX EA:T6-5740-T0378860 P1 SEQSDR FDEA202404110548Floor Support · corrodedMAIN DECK COMPT - COURIER AREA FOUND 1EA SUPPORT - FLOOR CORRODED LOCATION FROM FR11 TO FR14 , Y730 REPLACED THE DAMAGE SUPPORT WITH NEW PARTS, LOCATED IN FR11 TO FR14, Y730 I.A.W A300- 600F SRM 51-72-10-001,P2 REPAIR CLASSIFIED AS MINOR PER GMM6-2-100SDR FDEA202404110538Floor Support · corrodedMAIN DECK COMPT - COURIER AREA FOUND 1EA SUPPORT - FLOOR CORRODED LOCATION FROM FR11 TO FR15A , Y953 REPLACED THE 1EA SUPPORT WITH NEW AT MAIN DECK COMPT-COURIER AREA LOCATION FROM FR11 TO FR 15A , Y953 I.A.W A300-600F SRM 51-72-10-001, PAGE2 CLASSIFIED ASSDR FDEA202404100616Seat Track · gougedMAIN DECK COMPT FLOOR - SEAT TRACK CROWN AREA GOT GOUGED LOCATION AT FR62 PLUS 2",Y1959 CUT OUT DAMAGE SEAT TRACK,CUT OUT LENGTH=53 INCH AT FR62,Y1959. FABRICATE THE NEW SEAT TRACK AND REPAIR U-SECTION AND INSTALL ALL REPAIR PARTS WET WITH FASTENERS. I.A.SDR FDEA202404100539Seat Track · gougedMAIN DECK COMPT FLOOR - SEAT TRACK CROWN AREA GOT GOUGED LOCATION AT FR62 PLUS 2",Y1959 CUT OUT DAMAGE SEAT TRACK,CUT OUT LENGTH=53 INCH AT FR62,Y1959. FABRICATE THE NEW SEAT TRACK AND REPAIR U-SECTION AND INSTALL ALL REPAIR PARTS WET WITH FASTENERS. I.A.SDR FDEA202404100486Elevator · none00087566N00547 AIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON R/H ELEVATOR UPR SKIN AT ER10-8", T/E-23.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKSDR FDEA202404100468Elevator · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER16-16", T/E-10.9" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTSDR FDEA202404070540Support Bracket · crackedRH AIR CONDITION 144FR FAIRING LOWER SUPPORT BRACKET CRACK AT FR44,S-51R POSITION. REPLACED THE ANGLE BRACKET WITH NEW ONE IAW A300-600F SRM51-72-10-001 PAGE 2 THIS REPAIR CLASSIFIED AS MINOR PER GMM6-2-100 (AT FR44, S-51R FAIRING LOWER SUPPORT BRACKET)SDR FDEA202404070465None · none00087566N00415 AIRCRAFT REPAIR ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK BTW FR77 TO FR80/82, Y0 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUSDR FDEA202404060541Support Bracket · crackedLH AIRCONDITION 143FL FAIRING LOWER SUPPORT ANGLE BRACKET CRACK AT FR44,S-51L POSITION. REPLACED THE ANGLE BRACKET WITH NEW ONE IAW A300-600F SRM 51-72-10-001 PAGE 2 THIS REPAIR CLASSIFIED AS MINOR PER GMM6-2-100 (AT FR44, S-51L FAIRING LOWER SUPPORT BRASDR FDEA202404050649Skin · cracked2EA CRACKS (MAX:20MM) WERE FOUND AT LH WING CENTER FLAP RIB25 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGES REPAIR AT RIB25 UPPER FLANGE S-2.7~REAR SPAR AND EXTERNAL DOUBLERS REPAIR AT RIB26~25 S-2.2~REAR SPAR PLUS 10 INCHES, THE REPAIR CLSDR FDEA202404050648Skin · cracked1EA CRACK (75MM) WAS FOUND AT LH WING CENTER FLAP RIB20 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT RIB 20 BETWEEN UPPER SKIN S-2.8 TO REAR SPAR AND EXTERNAL DOUBLER REPAIR ENCLOSED BY LOWER SKIN RIB 19 TO RIB 20 AND S-2.1 TO REARSDR FDEA202404050646Skin · cracked1EA CRACK (25MM) WAS FOUND AT LH WING CENTER FLAP RIB13 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT RIB 13 UPPER FLANGE S-2.7~S-2.8, THE REPAIR CLASSIFIED AS CAT.A MAJOR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-T0378801 P1, SEQ SDR FDEA202404050638Skin · cracked3EA CRACKS (MAX70MM) WERE FOUND AT LH WING FLAP OF CENTER RIB12 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGES REPAIR AT RIB12 UPPER FLANGE S-2.7~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-T03788SDR FDEA202404050637Skin · cracked4EA CRACKS (MAX50MM) WERE FOUND AT LH WING CENTER FLAP RIB11 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT RIB 11 UPPER FLANGE S-2.7~REAR SPAR AND EXTERNAL DOUBLER REPAIR AT RIB11~RIB13 S-2.2~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.SDR FDEA202404050636Skin · cracked4EA CRACKS (MAX50MM) WERE FOUND AT LH WING CENTER FLAP RIB11 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT RIB 11 UPPER FLANGE S-2.7~REAR SPAR AND EXTERNAL DOUBLER REPAIR AT RIB11~RIB13 S-2.2~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.SDR FDEA202404050609Support Bracket · crackedLH LANDING GEAR DOOR OPEN ON GROUND PANEL INSIDE FWD SUPPORT BRACKET CRACK AT FR43, S-51L POSITION REPLACED THE DAMAGE SUPPORT WITH NEW AT FR43, S-51L I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.7, PAGE.24-50 REPAIR CLASSIFIED AS MINOR SDR FDEA202404050536Support · crackedAFT CGO COMP'T CEILING PANEL SUPPORT CRACK AT ENTRY AREA BTW FR60-FR61 POSITION. REPLACED THE HEADER WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21- 001, PARA6 PAGE7B~PAGE23, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 AND LOCATESDR FDEA202404020621Plate · crackedFWD CGO COMP'T UNDER FLOOR AREA LH SIDE PLATE CRACK AT S-43L~S-44L, FR21 POSITION. REPLACED THE SIDE PLATE WITH NEW PART AT FR21 AND S-43L~44L, I.A.W A300-600F SRM 51-72- 10-001, PAGE 2 & 51-40-21-001, PARA 6~7, PAGE 7B~50. REPAIR CLASSIFIED AS MINOR PER GMM SDR FDEA202404020546Seat Track · gougedMAIN DECK FLOOR - SEAT TRACK CROWN AREA GOT SOME GOUGES LOCATION FROM FR50 TO FR50 PLUS 3" AND Y0 ACCOMPLISHED THE MAIN DECK SEAT TRACK SPLICE REPAIR AT FR49~FR54 Y0, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FEDEX EA:T6-5310-T03788SDR FDEA202404020545Seat Track · gougedMAIN DECK FLOOR - SEAT TRACK CROWN AREA GOT SOME GOUGES LOCATION FROM FR50 TO FR50 PLUS 3" AND Y0 ACCOMPLISHED THE MAIN DECK SEAT TRACK SPLICE REPAIR AT FR49~FR54 Y0, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FEDEX EA:T6-5310-T03788SDR FDEA202404020544Skin · damaged1EA WATER TRAPPED AREA(70MM X 150MM) WAS FOUND AT R/H ELEVATOR UPPER SKIN PANEL T/E NO.9 SCREW AREA. ACCOMPLISHED THE CAT.A MAJOR COMPOSITE REPAIR AT RH ELEVATOR UPPER SKIN PANEL NO.9 T/E SCREW PER GMM 6-2-100 I.A.W A300-600F SRM 55-21-12-201, PARA 5J, PAGESDR FDEA202404020543Skin · damaged1EA WATER TRAPPED AREA(110MM X 250MM) WAS FOUND AT R/H ELEVATOR UPPER SKIN PANEL T/E NO.25 SCREW AREA. ACCOMPLISHED THE CAT.A MAJOR COMPOSITE REPAIR AT RH ELEVATOR UPPER SKIN PANEL NO.25 T/E SCREW PER GMM 6-2-100 I.A.W A300-600F SRM 55-21-12-201, PARA 5J,
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