N653FE
Service difficulty reports · 221
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 = 'N653FE' 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 = 'N653FE' 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 FDEA202402210193Skin · delaminatedRH ELEVATOR TOP SKIN BROKEN AT ER2 - ER5 INSTALLED THE REPAIR FLIES ON RH ELEVATOR TOP SKIN AT ER2 - ER5 PER A300-600F SRM55--21- 12-201 PARA.5.H & SRM51-77-12-201. MINOR REPAIR IAW FEDEX GMM 6-2-100 ENTERED BY ERROR. THIS REPAIR IS JUST A COSMETIC REPAIR PESDR FDEA202402180183Seat Track · wornMAIN DECK SEAT TRACK Y-2462 WORN AT FR63 REPAIRED THE WORN SEAT TRACK IN MAIN DECK Y-2462 AT FR63 PER A300-600F SRM53-10-16-201 PARA.4.THIS IS ACT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.SDR FDEA202402180182Floorbeam · crackedMDCC FLOOR CROSSBEAM FR30 CRACKED BETWEEN Y1456 - Y1959 COMPLIED WITH EA 6-5310 -T REPAIRED THE MDCC FLOOR CROSSBEAM FR30 CRACKED. REPAIR WITH MINOR DEVIATIONS. THIS REPAIR IS CAT. A REPAIR , MAJOR REPAIR IAW FEDEX GMM6-2-100.SDR FDEA202402180181Web · crackedMAIN DECK FLOOR STRUCTURE WEB CRACKED AT FR47 Y-953 - Y-1456 REPAIRED THE CRACKED WEB IN MAIN DECK FLOOR STRUCTURE AT FR47 Y-953 - Y-1456 PER A300-600F SRM53-15-15-201 FIG.201.THIS IS CAT B REPAIR.MAJOR REPAIR IAW FEDEX GMM6-2-100.SDR FDEA202402180180Web · crackedMAIN DECK FLOOR STRUCTURE WEB CRACKED AT FR47 Y-953 - Y-1456 REPAIRED THE CRACKED WEB IN MAIN DECK FLOOR STRUCTURE AT FR47 Y-953 - Y-1456 PER A300-600F SRM53-15-15-201 FIG.201.THIS IS CAT B REPAIR.MAJOR REPAIR IAW FEDEX GMM6-2-100.SDR FDEA202402180179Web · crackedMAIN DECK FLOOR STRUCTURE WEB CRACKED AT FR47 Y-450 - Y0 REPAIRED THE CRACKED WEB IN MAIN DECK FLOOR STRUCTURE AT FR47 Y-450 - Y0 PER A300- 600F SRM53-15-15-201 FIG.201.THIS IS CAT B REPAIR.MAJOR REPAIR IAW FEDEX GMM6-2-100.SDR FDEA202402180178Web · crackedMAIN DECK FLOOR STRUCTURE WEB CRACKED AT FR47 Y450 - Y0 REPAIRED THE CRACKED WEB IN MAIN DECK FLOOR STRUCTURE AT FR47 Y450 - Y0 PER A300- 600F SRM53-15-15-201 FIG.201.THIS IS CAT B REPAIR.MAJOR REPAIR IAW FEDEX GMM6-2-100.SDR FDEA202402170175Skin · crackedLH WNG CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB11 BETWEEN STGR2.7 AND REAR SPAR COMPLIED WITH EA 6-5750-T0378165 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB11 BETWEEN STGR2.7 AND REAR SPAR. TITLE: WING - FLIGHT SURFACESSDR FDEA202402170174Skin · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB13 AND RIB15 BETWEEN STGR2.6 AND REAR SPAR COMPLIED WITH EA 6-5750-T0378165 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB13 AND RIB15 BETWEEN STGR2.6 AND REAR SPAR. TITLE: WSDR FDEA202402170173Skin · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB18 AND RIB19 BETWEEN STGR2.7 AND REAR SPAR COMPLIED WITH EA 6-5750-T0378165 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB18 AND RIB19 BETWEEN STGR2.7 AND REAR SPAR. TITLE: WSDR FDEA202402170172Skin · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB25 AND RIB26 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0378165 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB25 AND RIB26 BETWEEN STGR2.8 AND REAR SPAR. TITLE: SDR FDEA202402170171Skin · crackedRH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB18 BETWEEN STGR2.8 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0378134 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB18 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING - FLIGHT SURFASDR FDEA202402170170Skin · crackedRH WING CENTER FLAP RIB UPPER FLANGE FOUND 6EA CRACKED AT RIB25,RIB26,RIB27 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0378134 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB25,26,27 BETWEEN STGR2.7 AND REAR SPAR. TITLE: WSDR FDEA202402170169Rib · crackedRT WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACKED AT RIB21 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA 6-5750-T0378134 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB21 BETWEEN STGR2.7 AND STGR2.8. TITLE: WING - FLIGHT SURFACES -SDR FDEA202402170168Rib · crackedRT WING CENTER FLAP RIB UPPER FLANGE FOUND CRACKED AT RIB13 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA 6-5750-T0378134 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB13 BETWEEN STGR2.7 AND STGR2.8. TITLE: WING - FLIGHT SURFACES - RH SDR FDEA202402130154Floorbeam · crackedMDCC FLOOR CROSSBEAM FR59 CRACKED BETWEEN Y-953 ~ Y-1456 REPAIRED THE CRACK IN THE MDCC FLOOR CROSSBEAM FR59 BETWEEN Y-953 ~ Y-1456 PER A300-600F SRM51-40-21 & SRM53-10-15-201 PARA.14. THE REPAIR IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.SDR FDEA202401130074Control Unit · failedON INITIAL CLIMB OUT RECEIVED TRIM TANK AFT TRANSFER NOT AVAILABLE CAUTION. PASSING 8000 MSL, LEFT ECAM SHOWED AMBER XXX IN GW, CG, AND T. FUEL. RIGHT ECAM SHOWED AMBER XXX IN LEFT INNER AND LEFT OUTER FUEL TANKS, AS WELL AS TOTAL FUEL, GW, AND CG. THE OVSDR FDEA202401020007Coalescer Bag · failedDURING DESCENT WHEN THROTTLES REDUCED TO IDLE, STRONG BURST OF SMOKE SMELL AND SLIGHT HAZE IN THE COCKPIT. IMMEDIATELY CLEARED AND DID NOT REOCCUR. REMOVED AND REPLACED BOTH COALESCER BAGS IAW A300 AMM 21-51-16-03. ITEM CLOSED. GROUND RUN CARRIED OUT ASSDR FDEA202312140107Transmitter · faultedON LANDING ROLLOUT BRAKING WAS NOT AVAILABLE ON THE RIGHT SIDE FROM EITHER SEAT WITH THE BRAKES IN NORM/ON. SWITCHED BRAKES TO ALTN /ON AND BRAKING WAS RESTORED. PUMPED BRAKES IN NORMAL POSITION ON BOTH CAPT AND FO SIDE. NOTICED BRAKES WERE SLOW AND SPOSDR FDEA202310231880Bulb · failedMDIS 653 33-50 6974 23OCT23 GSO FACT U ON 'A' CHECK, EMERG TEST BUTTON ON PANEL 25WL NOT ILLUMINATED. T/S PE ABOVE AMM, FOUND RED FAILURE LIGHT ON POWER SUPPULY UNIT 29WL. INSTALLED NEW BATTERY PER ABOVE AMM, NO RED OR GREEN LIGHT ON POWER USDR FDEA202210282684Valve · faultedON DEPARTURE WHEN RAISING THE GEAR WE GOT A LANDING GEAR RETRACTION FAULT. WE COMPLIED WITH THE QRH AND RETURN TO SDF FOR LANDING. MAX SPEED 255 KIAS / 0.65 M. DO NOT USE FMS PROFILE MODE. REMOVED AND REPLACED LANDING GEAR ELECTROVALVE 3GA IAW AMM 32-SDR FDEA202209132318Overheat Loop · failedDURING CLIMBOUT, GOT AN ECAM MESSAGE GREEN RSVR OVHT . COMPLETED THE ECAM AND QRH, OVHT LIGHT INTERMITTENT. CONTINUED FLIGHT. DURING DESCENT, OVHT LIGHT EXTINGUISHED, DECIDED TO RESTORE SYS USING EDP. DECLARED AN EMERGENCY & LANDED WITHOUT ISSUES. IAW MMSDR FDEA202205131201Control Unit · failedAT FL 310, THE AUTOPILOT AND AUTO THROTTLES KICKED OFF. LOST FMAS AND FCP FOR THE REMAINDER OF THE FLIGHT. THE FD WERE NOT WORKING EITHER. REMOVED AND REPLACED FLIGHT CONTROL UNIT (303CA) USING MM 22-15-12-04, PERFORMED AFS/LAND AND LIGHT DISPLAY ALL CHECSDR FDEA202112033045Switch · unknownR1 DOOR CLOSES AND GREEN LOCKED INDICATORS SHOW IT CLOSED BUT SLIDES DOESN'T APPEAR ON ECAM MEL 03DEC21 RELEASED FOR SERVICE PER MEL : 52-XX-XX CAT : C EXP: 13DEC21 MEL 52-XX-XX ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSDR FDEA202112033044Switch · unknownR1 DOOR CLOSES AND GREEN LOCKED INDICATORS SHOW IT CLOSED BUT SLIDES DOESN'T APPEAR ON ECAM MEL 03DEC21 RELEASED FOR SERVICE PER MEL : 52-XX-XX CAT : C EXP: 13DEC21 MEL 52-XX-XX ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSDR FDEA202108272108Skin · damagedSCRATCHES WERE FOUND AT FR57 10", S41L 0.2" AND FR57 13" TO FR57 18", S43L. ACCOMPLISHED EXTERNAL SKIN DOUBLER REPAIR I.A.W. A300-600F SRM 53-10-12-201 P.265~268 FIG207 SM4.THIS IS CAT B REPAIR I.A.W. A300-600F SRI 53-10-12-201 AND IIR 53-10-12- 2-001-00.SDR FDEA202107272005Doubler · gougedDURING PFM WORKCARD:E6-5100-7-5000 D7 PT1, FOUND GOUGE ON THE EXISTING REPAIR DOUBLER SURFACE AND SKIN CUTOUT EDGE AREA AT FR20A BETWEEN S-38R TO S-41R. GENERTAING FROM EO:E6-5100-7-5000 D7 PT1 & WO/NRC:00080535/N00132, ACCOMPLISHED THE WORK I.A.W. E.A:T6-SDR FDEA202107261934Frame · damaged1EA DAMAGE HOLE WAS FOUND AT FR47, S-24R, SPLICE FITTING, HOLE H AREA I.A.W. EO: 6-5310-7-50170 PART 6 FUSELAGE MAINFRAME - INSPECTION HOLE IN FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STR 24 & 26 LH/RH, AIRBUS SB A300-53-6123( SEQ NO: 001066) PERFORM ASDR FDEA202107261857Skin · delaminated1EA WATER TRAPPED AREA (50MMX50MM) WAS FOUND AT RH RUDDER T/E SCREW NEAR NO.37 FASTENER. ACCOMPLISHED THE WATER TRAPPED AREA CAT. B REPAIR I.A.W. A300-600F SRM 55-41-12-201, PARA. 22, FIG. 220, P. 286-294 AND SRI 55-71-12-201, IIR 55-41-12-2-005-00, 3E.SDR FDEA202107251898Floor Panel · damagedTHE #131NG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.SDR FDEA202107251897Floor Panel · damagedTHE #131LG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.SDR FDEA202107251896Floor Panel · damagedTHE #131SG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.SDR FDEA202107251895Floor Panel · damagedTHE #131RG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.SDR FDEA202107251894Floor Panel · damagedTHE #132QG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.SDR FDEA202107251893Floor Panel · damagedAFT CARGO COMPT FLOOR PANEL #151QF WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.SDR FDEA202107251892Floor Panel · damagedMAIN DECK COMPT FLOOR PANEL #251UH WAS FOUND EDGE DAMAGED.SDR FDEA202107251891Floor Panel · damagedMAIN DECK COMPT FLOOR PANEL #241PH WAS FOUND INSERT DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.SDR FDEA202107251890Floor Panel · damagedMAIN DECK COMPT FLOOR PANEL #241RJ WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.SDR FDEA202107181844Rudder · delaminated1EA WATER TRAPPED AREA (90MMX100MM) WAS FOUND AT RH RUDDER HOISTING POINT 2. ACCOMPLISHED THE WATER TRAPPED AREA CAT. B REPAIR I.A.W. A300-600F SRM 55-41-12-201, PARA. 25, FIG. 225A, P. 343-362 AND SRI 55-41-12-201, IIR 55-41-12-2-008-00, 3H.SDR FDEA202105131213Servo Valve · malfunctionedNR 2 BRAKE DID NOT RELEASE AFTER LANDING ROLLOUT. #2 TEMP REACHED MAX OF 370 DEGREES. PER MOCC THE #2 (13GG) SERVOVALVE IS REQUIRED TO BE CHANGED. REMOVED THE #2 (13GG) SERVOVALVE IAW AMM 32-42-48-04. INSTALLED THE #2 (13GG) SERVO VALVE DOWN TO AMM 32-42-SDR FDEA201912043171Indicator · failedR1 DOOR WILL NOT ARM. . RELEASED FOR SERVICE PER MEL : 52-XX-XX CATEGORY : C EXPIRATION : MM-DD-YY "MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR ( R1) _____ DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPASDR FDEA2019093082370Tachometer · malfunctionedNR 5 BRAKE INDICATED ON DURING TAXI DRIFTED LEFT. THEN OFF, ATTEMPTED T/O AND HAD SAME INDICATION @80 KTS. CONDUCTED RTO AND RETURNED TO RAMP. TSI 2779 COMPLETED AND PROBLEM CORRECTED IN ASSOCIATED TSI ACTION IAW AMM 32-42-57-00, MAIN TACHOMETER REPLACESDR FDEA201902286505Bracket · chafedMCD FR24 CHAFFED BETWEEN S-12R AND S-13R REMOVED AND REPLACED 1EA BRACKET AND 1EA SPLICE AT FR24 RH SIDE ON MCD IAW SRM 51-40-21 MAJOR REPAIRSDR FDEA201902250502Floor Panel · delaminatedPANEL 162DF WAS FOUND DELAMINATED AFTER REMOVAL FOR FOM FABRICATED NEW PANEL 162DF IAW SRZ-25-005 AND TRAVELER T19/1395153 MAJOR REPAIRSDR FDEA201902250501Floor Panel · damagedFLOOR PANEL 162CF WAS FOUND DAMAGED AFTER REMOVAL FOR FOM 162CF FABRICATED NEW PANEL IAW SRZ-25-005 AND TRAVELER T19/1395152 MAJOR REPAIRSDR FDEA201902210475Seat Track · damagedMAIN CARGO DECK FR63 RT OUTBD Y-2462 SEAT TRACK LOBE MISSING. REPAIRED SEAT TRACK IAW SRM 53-10-16 FIG 201. MAJOR REPAIR.SDR FDEA201902210474Seat Track · crackedMAIN SEAT TRACK LBL 1456 WORN AND GOUGED FR57.1 TO FR60. UPON FURTHER INVESTIGATION SEAT TRACK FOUND TO BE CRACKED. REPAIRED SEAT TRACK IAW SRM 53-10-16 FIG 201. MAJOR REPAIR.SDR FDEA201902210469Adapter · damagedMCD ADAPTER FR 57.3 LT HAS DAMAGED LOBE FABRICATED NEW ADAPTER ON T19/1396201. REMOVED AND REPLACED MDCC ADAPTER AT FR57.3 LT IAW SRM 51-40-21, Y1456 TO Y1959 CLASSIFIED AS A CAT"A" MAJOR REPAIR.SDR FDEA201902170440Closeout Panel · damagedFOUND PANEL PULLED LOSE AND CRACKED ON LT ENGINE, I/B THRUST REVERSER AT APPROX THE 6 O'CLOCK POSITION. REMOVED DAMAGED PANEL ON NR 1 ENG THRUST REVERSER AT 6 O'CLOCK POS REF SRM 51-40-20. PART REPLACEMENT WAS ACCOMPLISHED ON EA 6-530-TO343829 PART 2 WRI 543SDR FDEA201902160434Seat Track · corrodedMAIN DECK BETWEEN FR69 AND FR72 Y-953 SEAT TRACK HAS CORROSION BLEND OUT AREA ON SEAT TRACK AT BETWEEN FR69 TO FR72 Y-953 FOUND OUT OF LIMITS IAW SRM 53-10-16 FIG 102. REMOVED AND REPLACED SEAT TRACK BETWEEN FR69 TO FR72 Y- 953 IAW SRM 53-40-21 MAJOR REPAIR.
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