N651FE
Service difficulty reports · 421
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 = 'N651FE' 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 = 'N651FE' 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 FDEA202412101647Control Unit · failedDURING OPS CHECK OF 71WN FOUND THE AUTONOMOUS STANDBY UNIT FAILED OPS CHECK. REMOVED AND REPLACED AUTONOMOUS STANDBY UNIT. OPS CHECK GOOD.SDR FDEA202408151129Connector · damagedR1 CEILING EMERGENCY LIGHT INOP. AMM: 33-51-00-05 WDM: 33-51-04 CLEANED AND RECECURED PLUG CONNETION 5824VC AND PERFORMED EMERGENCY LIGHT OPS TEST REF ABOVE REF, EMERGENCY LIGHTING NOW OPS CHECK NORMAL. PLACARD REMOVED. IDENTIFIED ITEM AS AN SDR, NSDR FDEA202408151128Power Supply · failedWHEN A/C WAS BOARDED, L1 AND R1 EMERGENCY EXIT SIGNS WERE ILLUMINATED WITH BOTH COCKPIT EMERGENCY SWITCH AND COURIER EMERGENCY SWITCH IN THE OFF POSITION. R/I 06JUL24 11:13 BWI REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 3214-41 POS: ONLSDR FDEA202404300533Pitot Tube · blockedIN CRUISE AT FL340, .80M (279 IAS) ABOUT 40 MINUTES INTO THE FLIGHT, RECEIVED FO IAS DISCREPANCY ECAM. HIS STANDBY AIRSPEED INDICATOR REMAINED AT 279-280 BUT HIS PFD SPEED TAPE WENT TO 220 KTS AND VERY SLOWLY CREEPED BACK UP TO 279-280. TOOK ABOUT TWO MINSDR FDEA202404260534Indicator · malfunctionedAFTER TURBULENCE AND ICING ENCOUNTER, FL360 ADC 2 AIRSPEED INDICATION DROPPED TO 60KTS. FO STANDBY, CAPT STANDBY AND ADC 1 SHOWED CORRECT INDICATION. FOLLOWED QRH PROCEDURE. AMM: 34-10-00-05, AMM: 22-40-00-05 PERFORMED BITE CHECK ON #2 ADC, TEST OK, AIRSPESDR FDEA202404230535Adc · failedAT FL350, .78 MACH, ABOUT 1 HOUR INTO FLIGHT, FO SPEED TAPE BEGAN ROLLING BACK FOLLOWED BY IAS DISCREPANCY ECAM ALERT. FOLLOWED ECAM AND QRH SWITCHING TO SYS 1 ADC ON FO SIDE. SUSPECT ADC2 FAILURE. R & R NO.2 ADC, PERFORMED SATISFACTORY ADS2 BITE TEST. COMPSDR FDEA202403280390Seat Track · brokenSEAT TRACK LOBES BROKEN UNDER LOCK POSITION MG0828. NO FLOOR PANEL DAMAGE AND NO SEAT TRACK CRACKS. FABRICATED, LOCATED, AND MATCH-DRILLED NEW SEAT TRACK SECTION AND SPLICE FITTINGS IAW SRM FIG. 201. INSTALLED THE SEAT TRACK AND REPAIR IAW SRM 53-10-16.SDR FDEA202312220068Fitting · corrodedLH RIB 5, MLG FWD PINTLE AIRFRAME ATTACH FITTING HAS CORROSION ON AFT SPOT FACE. REPAIRED PER AIRBUS INSTRUCTIONS R57240425SDR FDEA202312220067Fitting · corrodedLH RIB 5, MLG FWD PINTLE AIRFRAME ATTACH FITTING HAS CORROSION ON FWD SPOT FACE. REPAIRED PER AIRBUS INSTRUCTIONS R57240425SDR FDEA202312200066Fitting · corrodedL/H MLG AFT PINTLE FWD LUG HAS SIGN OF CORROSION. REPAIRED PER AIRBUS INSTRUCTIONS R57240425SDR FDEA202303210563Skin · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB 11~13 T/E-9". COMPLIED WITH ATTACHMENT B OF EO: E 6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CSDR FDEA202303210562Skin · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB 11~13 T/E-9". COMPLIED WITH ATTACHMENT B OF EO: E 6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CSDR FDEA202303210561Skin · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP UPR SKIN BTW RIB 1C~5,STGR 2.1~2.2. COMPLIED WITH ATTACHMENT B OF EO: E 6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS SDR FDEA202303150622Skin · unknownEXISTING REPAIR ON RH WING #1 SLAT TAIL SECTION UPR SKIN, T/E-8.5" POSITION, BTW RIB 22~24, EVALUATE TO DETERMINE WHETHER IT IS ACCOMPLISHED BY APPROVED DATA DUE TO NO EXISTING DOCUMENTATION SUPPORTING THIS REPAIR, REMOVED THE EXISTING REPAIR AND PERFORMEDSDR FDEA202303150621Skin · unknownEXISTING REPAIR ON RH WING #1 SLAT TAIL SECTION UPR SKIN, T/E-11.5" POSITION, BTW RIB 8~9, EVALUATE TO DETERMINE WHETHER IT IS ACCOMPLISHED BY APPROVED DATA DUE TO NO EXISTING DOCUMENTATION SUPPORTING THIS REPAIR, REMOVED THE EXISTING REPAIR AND PERFORMED SDR FDEA202303090400Seat Track · wornFR54/FR54.2 RH NO.2 DUMMY SEAT TRACK GAP OVER 1.0MM. I.A.W A300-600 SRM 53-15-16 PARA 5A FIG.201 P201-P210 PERFORM REPAIR ACCOMPLISHED.SDR FDEA202303080646Spoiler · delaminatedLH WING #6 SPOILER L/E CTR SECTION DELAMINATED. REMOVED L6 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L6 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, PAGE.211-213, FIG.206. "MAJOR REPAIR"SDR FDEA202303080626Skin · delaminatedLH WING #6 SPOILER L/E CTR SECTION DELAMINATED REMOVED L6 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L6 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, PAGE.211-213, FIG.206. "MAJOR REPAIR"SDR FDEA202303070645Slat · unknownAGING AIRCRAFT ASSESSMENT : EXISTING FLUSH DOUBLER REPAIR FOUND ON RH WING #3 SLAT NOSE SKIN O/B END. DUE TO NO APPROVED DOCUMENTATION TO SUPPORT THE REPAIR, REMOVED ALL REPAIR PARTS AND PERFORMED NEW REPAIR TO THE AREA I.A.W. EA# T6-5750-T0373565 P1, TITLSDR FDEA202303070644Spoiler · delaminated1EA DELAMINATION WAS FOUND (2" X 1") AT LH SPOILER NO.5 UPPER SKIN. REMOVED L5 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L5 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, P.211~213, FIG.206. SDR FDEA202303070631Skin · noneEXISTING FLUSH DOUBLER REPAIR FOUND ON RH WING #3 SLAT NOSE SKIN O/B END. DUE TO NO APPROVED DOCUMENTATION TO SUPPORT THE REPAIR, REMOVED ALL REPAIR PARTS AND PERFORMED NEW REPAIR TO THE AREA I.A.W. EA# T6-5750-T0373565 P1, TITLE: WINGS- FLIGHT SURFACES-RSDR FDEA202303070625Skin · delaminated1EA DELAMINATION WAS FOUND (2" X 1") AT LH SPOILER NO.5 UPPER SKIN REMOVED L5 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L5 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, P.211~213, FIG.206. SDR FDEA202303070544Seat Track · unknownN00119 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 31~32, -Y1456 FOUND THE EXISTING SPLICE REPAIR UPPER FLANGE NOT COMPLIANCE WITH APPROVED DATA: A300-600F SRM 53-10-16-201, FIG.201, REMOVED HILOKS AND PERFORMED ROTOTSDR FDEA202303070493Seat Track · unknownN00125 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 69~70, 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 121SDR FDEA202303070492Seat Track · unknownN00124 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 67~68, -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 12SDR FDEA202303070491Seat Track · unknownN00123 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 67~68, -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 1SDR FDEA202303070490Seat Track · unknownN00122 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 65~69, Y0 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 FDEA202303070489Seat Track · unknownN00121 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 62~63, -Y953 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 12SDR FDEA202303070488Seat Track · unknownN00120 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 55~56, -Y953 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 12SDR FDEA202303030483Aileron · damagedLH WING AILERON UPPER SKIN DEFORMED AT RIB1 & REAR SPAR-17" ACCOMPLISHED THE DOUBLER REPAIR, THIS IS CAT.A REPAIR I.A.W A300-600F SRM 57-61-11-201, PARA.4D, PAGE.213-PAGE.216, FIG.204 MAJOR REPAIRSDR FDEA202303020596Skin · damagedEVALUATE PREVIOUS DENT AT LHS FUSELAGE LWR SKIN FR10 6", 8 O'CLOCK. ACCOMPLISHED THECAT B DOUBLER REPAIR IAW A300-600F SRM 53-12-12-201, CONFIG 2, PAR. 5A, PAGE 203-208, FIG.201 & SRI 53-12-12-201, IR 53-12-12-2-006-00, PARA. 3F, TABLE 207 "MAJOR REPAIR".SDR FDEA202204180988Control Module · unknownMDIS 651 26-10 5623 18APR22 IND OPEN U #1 ENGINE AGENT #2 SQUIB INOP SHGN 18APR22 15:25 IND U WHEN TESTING #1 ENG SQUIB, AGENT 2 SQUIB LIGHT IS NOT ILLUMINATING. SQUIB LIGHT ILLUMINATES W/ ANNUN LT TEST. PER A300-600 TSM 26-21-00, FIG 11SDR FDEA202203180745Light · inoperativeMDIS 651 33-50 5547 18MAR22 LRD FACT U LAVATORY AUXILIARY MIRROW EMERGENCY LIGHT OUT. FACT 18MAR22 14:45 LRD U RELAMPED LAV AUX MIRROW EMERGENCY, IAW AMM 33-51-21-04, OPS CKS NORMAL AT THIS TIME.SDR FDEA202203150527Power Supply · unknownSLIDE DID NOT DISPLAY ON ECAM WHEN ARMING RIGHT CABIN DOOR. RELEASED FOR SERVICE PER MEL : 52- XX-XX CATEGORY : C EXP: 25MAR22 - (R1) DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE." AUTONOMOUS STANDBSDR FDEA202109232384Controller · inoperativeAFTER T/O ON SLAT RETRACTION HAD KRUEGER FAULT. RAN APPROPRIATE CHECKLISTS AND RTB. PERFORMED BITE DISPLAY OF BOTH SFCC'S AND FOUND ALL OF THE FAULT BALLS FOR THE NR 1 UNIT LIGHT. THAT FAULT CODE CORRESPONDS WITH BAD SFCC REF AMM 27-80-00. IND INSPECTEDSDR FDEA202010032403Actuator · failedCREW REPORT: DURING MANUAL GEAR EXTENSION GOT LOUD NOISE AND EXCESSIVE VIBRATION ABOVE NORMAL LEVELS. WOULD NOT RECYCLE, REMOVED AND REPLACED NLG DOOR ACTUATOR LT SIDE. REMOVED AND REPLACED NOSE GEAR SEQUENCE VALVE. REMOVED AND REPLACED NON RETURN VALVE. SDR FDEA202008272047Pin · missingMISSING PASSENGER CREW DOOR 831 INFLATE RESERVOIR SAFETY PIN ESCAPE SLIDE RAFT AT FWD GALLEY AREA (1EA). REPLACED PASSENGER CREW DOOR 831 ESCAPE SLIDE RAFT IAW AMM 25-61-21-04 AT FWD GALLEY AREA.SDR FDEA202008171959Bolt · corrodedCORROSION BOLT ATTACHMENT SLAT TRACK 7 UPPER POSITION ON LH WING (1 EA) REPLACED BOLT ATTACHMENT SLAT TRACK 7 UPPER POSITION ON LH WING IAW AMM 27-80-14- 04.SDR FDEA2020081871927Bolt · corrodedONE CORRODED BOLT ATTACHMENT ON SLAT TRACK NR 7 LOWER POSITION OF THE LT WING. REPLACED THE BOLT IAW AMM 27-80-14-04.SDR FDEA2020009091896Floor Panel · crackedCRACK FLOOR PANEL 232VH. THIS NON ROUTINE CARD IS FOR PURPOSE RDR GENERATION IN PASSENGER CABIN (1 EA). MANUFACTURED FLOOR PANEL 232VH, AS PER DWG SRZ-25-005 REV. R AUG-22-2019. FLOOR PANEL MARKED WITH P/N FX B5327048401400 FDX AUG-11-2020, AS PER GMM 7-0-1SDR FDEA2020082851896Floor Panel · crackedCRACK FLOOR PANEL 232VH THIS NON ROUTINE CARD IS FOR PURPOSE RDR GENERATION IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 232VH AS PER DWG SRZ-25-005 REV.R AUG-22-2019 AND FLOOR PANEL MARKED WITH P/N: FX B5327048401400 FDX AUG-11-2020 AS PER GMM 7-0-1001,SDR FDEA2020082051941Floor Panel · delaminatedDELAMINATED FLOOR PANEL 242LK. REPAIRED THE FLOOR PANEL IAW DWG SRZ 25-005 REV. R.SDR FDEA2020081851896Floor Panel · crackedCRACK FLOOR PANEL 232VH THIS NON ROUTINE CARD IS FOR PURPOSE RDR GENERATION IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 232VH AS PER DWG SRZ-25-005 REV. R AUG-22-2019. THIS NON ROUTINE CARD IS FOR PURPOSE RDR, SDR GENERATION. THIS JOB IS DOCUMENTED SDR FDEA202008071957Floor Panel · delaminatedDELAMINATED FLOOR PANEL 231UG ON MAIN DECK AFT CARGO COMPARTMENT THIS TASK CARD IS GENERATED FOR RDR PURPOSE IN PASSENGER CABIN (1 EA) THE REPAIR IS DOCUMENTED ON NON ROUTINE CARD N00343,SDR FDEA202008071960Floor Panel · delaminatedDELAMINATED FLOOR PANEL 231ZG ON MAIN DECK AFT CARGO COMPARTMENT THIS TASK CARD IS GENERATED FOR RDR PURPOSE IN PASSENGER CABIN (1 EA) THE REPAIR IS DOCUMENTED ON NON ROUTINE CARD N00343, THIS SNRM, (N00653) IS GENERATED RDR PURPOSESDR FDEA202008071958Floor Panel · delaminatedDELAMINATED FLOOR PANEL 231NG ON MAIN DECK AFT CARGO COMPARTMENT THIS TASK CARD IS GENERATED FPR RDR PURPOSE IN PASSENGER CABIN (1 EA) THE REPAIR IS DOCUMENTED ON NON ROUTINE CARD N00543,SDR FDEA2020082071956Floor Panel · delaminatedDELAMINATED TOP LAYER FLOOR PANEL (MAIN DECK) 241EF IN PASSENGER CABIN (1 EA) REPAIRED FLOOR PANEL 241EF ON MAIN DECK ASPER A300 SRM 53-10-20 PAGEBLOCK 201 PARA B TOOL USED CALIPER PN 500-197-30 S/N A18135089 DUE DATE JUL-11-2021 SCALE PN CL5000 S/N AE-398SDR FDEA2020082641977Bolt · corrodedCORROSION BOLT ATTACHMENT SLAT TRACK 8 ECCENTRIC BOLT ON RT WING. REPLACED BOLT ATTACHMENT SLAT TRACK 8 ECCENTRIC BOLT ON RY WING IAW AMM 27-80-14-04.SDR FDEA2020082141961Bolt · corrodedCORROSION SLAT 2 SCREWJACK 4 BOLT ON LH WING REPLACED SLAT 2 SCREWJACK BOLT ON LH WING IAW AMM 27-84-22-04 STEP 2.D(5)(A)SDR FDEA2020082041955Bolt · corrodedCORROSION BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING REPLACED BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING IAW AMM 27- 80-12-04
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