N662FE
Service difficulty reports · 229
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 = 'N662FE' 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 = 'N662FE' 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 FDEA202607100896Sensor · faultedGREEN SYSTEM OVERHEAT LIGHT FLASHING AND CHIME WARINING.SDR FDEA202605250637Actuator · stuckAIR RETURN IN RJAA DUE TO CABIN PRESSURE 1 & 2 FAULT. FORWARD OUTFLOW VALVE STUCK FULL OPEN. NO EMERGENCY OR PRIORITY DECLARED. R & R FWD OUTFLOW VALVE ACTUATOR PER AMM 21-31-12-04.SDR FDEA202604240530Frame · crackedINSPECTION OF FR40 LOWER JUNCTION FASTENER HOLE NR 3 RT SIDE FOUND CRACK SIGNAL. COMPLIED WITH EA:6-5710-T0387217 P1 TO REPAIR FR40 RH SIDE LOWER JUNCTION CRACKED FASTENER HOLE #3, MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 57107960 FOR WORK DETAILS.SDR FDEA202604230503Skin · delaminatedLEFT WING NR 5 SPOILER INBD MID HINGE ARM OTBD SURFACE DELAMINATED. SIZE: 60 MM - 23 MM - DEPTH: 1.0 MM. COMPLIED WITH EA:6-5750-T0387139 P1 TO REPAIR LH WING #5 SPOILER I/B MID HINGE ARM O/B SURFACE DELAMINATION, HIS IS CATEGORY A REPAIR. MAJOR REPAIR IAWSDR FDEA202604190507Rib · crackedLEFT CENTER FLAP RIB UPPER FLANGE FOUND ONE CRACK AT RIB 11 BETWEEN STGR 2.7 AND STGR 2.8. COMPLIED WITH EA:6-5750-T0344015 A P2 TO REPAIR LH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB11 BETWEEN STGR2.7 AND STGR2.8, EA TITLE: WINGS - FLIGHT SURFACES - CRSDR FDEA202604190506Rib · crackedLEFT CENTER FLAP RIB UPPER FLANGE FOUND ONE CRACK AT RIB 25 BETWEEN STGR 2.8 AND REAR SPAR. COMPLIED WITH EA:6-5750-T0344015 A P2 TO REPAIR LH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB25 BETWEEN STGR2.8 AND REAR SPAR, EA TITLE: WINGS - FLIGHT SURFACES - SDR FDEA202604190505Rib · crackedRIGHT CENTER FLAP RIB UPPER FLANGE FOUND ONE CRACK AT RIB 13 BETWEEN STGR 2.7 AND STGR 2.8. COMPLIED WITH EA:6-5750-T0344016 A P2 TO REPAIR RH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB13 BETWEEN STGR2.7 AND STGR2.8, EA TITLE: WINGS - FLIGHT SURFACES - CSDR FDEA202604190504Rib · crackedRIGHT CENTER FLAP RIB UPPER FLANGE FOUND ONE CRACK AT RIB 25 BETWEEN STGR 2.7 AND STGR 2.8. COMPLIED WITH EA:6-5750-T0344016 A P2 TO REPAIR RH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB25&RIB27 BETWEEN STGR2.7 AND STGR2.8, EA TITLE: WINGS - FLIGHT SURFACESSDR FDEA202602220253Safety Wire · misinstalledREMOVE AND REPLACE RT SLIDE. (AMM: 25-61-21-04) DURING INSPECTION FOR FEA 6-2560-F0386375 REV NO. A PS P1 FOUND EJECTOR BAG RELEASE HANDLE INCORRECTLY SAFETY WIRED AND BOTTLE EMPTY MAKING UNIT UNSERVICEABLE. REMOVED AND REPLACED RT SLIDE ASSY. OPS CHKD GSDR FDEA202510031877Warning Light · illuminatedDURING GEAR RETRACTION OUT OF ORD, GOT AMBER L/G DOORS NOT CLOSED ECAM. BOTH GEAR PANELS SHOWED NOSE GEAR DOOR AMBER DOOR LIGHT ON. COMPLETED ECAM AND QRH. WE FLEW TO IND AT 260 KIAS. AMBER DOOR LIGHT REMAINED ON ENTIRE FLIGHT UNTIL GEAR EXTENSION. JACKESDR FDEA202508081873Battery · no testCOURIER AREA EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE DURING TEST. R & R EXIT LIGHT BATTERY AND OPS CHECKS GOOD. OKAY FOR SERVICE.SDR FDEA202409241355Hydraulic System · lowDURING CRUISE AT FL330, GREEN HYD INDICATOR NEEDLE MOVING LOWER TOWARD YELLOW RANGE. INDICATION CONTINUED MOVING RAPIDLY FROM MIDDLE GREEN RANGE INTO YELLOW RANGE. HYD PRESSURE REMAINED NORMAL. END OF FLIGHT QTY INDICATION WAS SIGNIFICANTLY LESS THAN PREVISDR FDEA202407201037Jackscrew · corrodedSLAT SYS 1 2 FAULT. QRH PROCEDURE COMPLIED WITH. PERFORMED NO SLAT LANDING. HIGHEST BRAKE TEMP ON LANDING 260. AMM: 27-84-00-02 TSM: 27-80-02 AMM: 12-13-27-00 JRH: A300-600 CARRIED OUT THE BITE CHECK ON BOTH SFCC1 AND SFCC2, BOTH SFCCS INDICATED A SLSDR FDEA202310051713Aileron · unknownEXISTING DOUBLER REPAIR FOUND ON LH AILERON LOWER SKIN BETWEEN RIB 15~16, TRAILING EDGE-4",EVALUATE TO DETERMINE WHETHER IT IS MAJOR OR MINOR AND WHETHER ACCOMPLISHED PER APPROVED DATA COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OFSDR FDEA202309281759Floorbeam · corrodedMAIN DECK FLOOR CROSS BEAM FOUND CORROSION AT FR47 Y-330 TO Y-400 REPLACED THE CROSS BEAM WITH FASTENERS I.A.W A300-600F SRM 51-72-10-001, PAGE.2 & 51- 40-21-001, PARA.6-7, PAGE.7B~50SDR FDEA202309271783Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK FOUND CORROSION AT FR45 PLUS 3", Y450 INSTALLED NEW SECTION OF SEAT TRACK AND ACCOMPLISHED THE SPLICE REPAIR THIS IS CAT.A REPAIR I.A.W FEDEX EA NO:T6-5310-T0376506 P1, TITLE: FUSELAGE-MAINFRAME-MAIN CARGO SEAT TRACK SPLICE REPAISDR FDEA202309271724Angle · damagedCHECK FOUND ANGLE BROKEN NEAR 6030VT AT BAY UNDER AFT CGO COMPT. REPLACED THE BROKEN ANGLE WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE.2SDR FDEA202309261814Rib · corrodedLH WING T/E #5 SPOILER O/B JACK RIB SURROUNDING UPR BORE AREA CORROSION ACCOMPLISHED THE REINFORCING REPAIR, THIS IS CAT.B REPAIR I.A.W FEDEX EA NO:T6-5740- T0376432 P1, SEQ NO:1202, TITLE:WING-ATTACH FITTINGS-LH WING #5 SPOILER JACK RIB AT STA ABX184.625 BSDR FDEA202309261813Rib · corrodedLH WING T/E #3 SPOILER I/B JACK RIB SURROUNDING LWR BORE AREA CORROSION ACCOMPLISHED THE REINFORCING REPAIR, THIS IS CAT.B REPAIR I.A.W FEDEX EA NO:T6-5740- T0376377 P1, SEQ NO:1201, TITLE:WING-ATTACH FITTINGS-LH WING #3 SPOILER JACK RIB AT STA ABX31.675 BESDR FDEA202309261727Floor Support · corrodedMAIN DECK FLOOR FOUND SUPPORT CORROSION BETWEEN FR11 PLUS 10" AND FR11 PLUS 16",Y730 REPLACED THE DAMAGE SUPPORT WITH NEW I.A.W A300-600F SRM 51-72-10-001, PAGE 2SDR FDEA202309261723Profile · crackedMAIN DECK FLOOR STRUCTURE Z-PROFILE CRACK NEAR FR80/82, -Y1487. REPLACED THE NEW PROFILE-Z. I.A.W A300-600F SRM 51-72-10-001,P2SDR FDEA202309261722Spoiler · damagedLH WING #6 SPOILER RH SIDE HINGE ARM PARTIAL DISBONDED. REPAIRED THE HINGE ARM BY HOT BONDING REPAIR, THIS IS CAT.A REPAIR I.A.W A300-600F SRM 57-73-11-201, PARA 13, PAGE 218-221, FIG 208. MAJOR REPAIRSDR FDEA202309261721Support · damagedMAIN DECK FLOOR FOUND SUPPORT BROKEN NEAR FR37 PLUS 5" , STGR26L REPLACED THE NEW SUPPORT I.A.W A300-600F SRM 51-72-10-001, P.2SDR FDEA202309241790Bracket · crackedAFT CGO COMP'T FWD PRESSURE BULKHEAD SUPPORT BRACKET CRACK AT Y1959,FR54 POSITION. REPLACED DAMAGE PART WITH NEW ONE. I.A.W. A300-600F SRM 51-72-10-001, PAGE2.SDR FDEA202309241785Bracket · crackedAFT CARGO COMP'T FWD PRESSURE BULKHEAD SUPPORT BRACKET CRACK AT -Y1959, FR54 POSITION REPLACED THE CRACK BRACKET WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE.2SDR FDEA202309231786Web · crackedFWD CARGO COMPT WAS FOUND A WEB CRACK AT STGR44LH, FR20 POS REMOVED CRACK WEB AND INSTALLED NEW WEB I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, P.7B-P.23SDR FDEA202309221812Flange · gougedLH M/L/G DOOR CENTER HINGE FWD SUPPORT FLANGE FOUND GOUGE REPLACED WITH NEW FLANGE FITTING I.A.W A300-600F SRM 51-72-10-001, PAGE.2SDR FDEA202309221809Flange · gougedRH M/L/G DOOR CENTER HINGE AFT SUPPORT FLANGE FWD SURFACE FOUND GOUGE REPLACED WITH NEW FLANGE FITTING I.A.W A300-600F SRM 51-72-10-001, PAGE.2SDR FDEA202309221726Support Fitting · damagedRH M/W/W AFT WALL CENTER 1 EA HYD TUBE SUPPORT FITTING BROKEN. REPLACED BROKEN FITTING WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001 PAGE2SDR FDEA202309221725Shear Web · crackedMAIN DECK FLOOR STRUCTURE SHEAR WEB CRACK NEAR FR79 PLUS 5" ,-Y1620. REMOVED CRACK SHEAR WEB THEN INSTALLED NEW ONE WITH FASTENERS I.A.W A300-600F SRM 51-72-10-001,PAGE 2 AND 51-40-21-001,PAGE 24-50,PARA.7SDR FDEA202309221718Web · crackedMAIN DECK FLOOR STRUCTURE SHEAR WEB CRACK NEAR FR77 -Y1887 REPLACED THE WEB WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE.2SDR FDEA202309221689Shear Web · crackedMAIN DECK FLOOR STRUCTURE SHEAR WEB CRACK NEAR FR79 5" Y1620. REPLACED THE NEW SHEAR WEB. ONE.I.A.W A300-600F SRM 51-72-10-001,P2.SDR FDEA202309221687Elevator · damaged1EA WATER STRAPPED AREA (200MM X 70MM) WAS FOUND AT ER7 OF LH ELEVATOR TOP SKIN. REPAIRED THE DAMAGE AREA WITH CORE AND PLIES. THIS IS CAT A REPAIR I.A.W A300-600F SRM 55-21-12-201 PARA 5J, PAGE 268-270. FIG212(SHEET2). MAJOR REPAIRSDR FDEA202309211760Seat Track · corrodedMAIN DECK FLOOR FOUND SEAT TRACK CORROSION BETWEEN FR44 PLUS 3" AND FR44 PLUS 10", Y450 REPLACED THE NEW SEAT TRACK (P/N:A5383202020400) I.A.W A300-600F SRM 51-72-10-001, PAGE.2SDR FDEA202309201784Door · damagedBULK CARGO COMP'T DOOR EXTERNAL SURFACE GOT A PUNCH AT FR68 PLUS 2", BEAM5-0.4" POSITION ACCOMPLISHED THE DOUBLER REPAIR, THIS IS CAT.B REPAIR I.A.W A300-600F SRM 52-34-00-201, PARA.7, PAGE.217-223/224, FIG.203(SHEET-2) & SRI:52-34-00-201, IIR:52-34-00-2-0SDR FDEA202309201720Strap · bentREAR FUSELAGE INTERNAL STRUCTURE FOUND S-39R WEB PLATE DEFORM BETWEEN FR86 & FR87 AREA INSTALLED THE NEW STRAP WITH RIVETS I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21- 001, PARA6, PAGE.7B-23SDR FDEA202309191829Fitting · crackedTHE MDC DOOR ACTUATOR YOKE FWD SUPPORT FRAME WAS FOUND CRACK FABRICATED NEW SUPPORT FRAMES AND INSTALLED WITH FASTENERS,I.A.W FEDEX EA NO:T6- 5230-T0376261 P1,SEQ NO:1214,TITLE:DOORS-CARGO DOOR/HYD SYS-MAIN CARGO DOOR ACTUATOR BEARING FITTING REPLACEMENT (FSDR FDEA202306141031Check Valve · failedACRID FUMES & HAZE FROM A/C VENTS ON TAKEOFF. SECURED PACKS & BLEEDS & HAZE APPEARED TO CLEAR. LANDED NORMAL & SHUT DOWN ENGINES. TOWED TO GATE. INSTALLED APU PRESSURIZATION CHECK VALVE. PURGED & CLEANED ALL LINES & DUCTING AS NEEDED TO REMOVE RESIDUAL HYD SDR FDEA202301270169Connector · chafedMDIS 662 26-12 4356 27JAN23 RIC OPEN U RAMP CREW REPORTS SMOKE COMING FROM AFT BELLY AREA. MX CALLED OUT AND SHUT OFF A/C POWER, FIRE DEPT NOTIFED AS PRECAUTION. REF AWM 25-52-04, RETERMINATED WIRES 2454-5004, 2454-5006,2451-6604,2451-6605, 2SDR FDEA202111112830None · damagedRH FR47 HOLE 11 HAS THREAD DAMAGE INDICATIONS IN ALL LAYERS. REFER TO EO 6-5710- E0342809 FOR LOCATIONS COMPLIED WITH E.A. 6 - 5710 - T0353473 D P11 "WINGS - BASIC WING STRUCTURE - FR 47 RHS REPAIRED HOLES"SDR FDEA202111112829None · damagedRH FR47 HOLE 13 HAS THREAD DAMAGE INDICATIONS IN ALL LAYERS. REFER TO EO 6-5710- E0342809 FOR LOCATIONS COMPLIED WITH E.A. 6 - 5710 - T0353473 D P11 " WINGS - BASIC WING STRUCTURE - FR 47 RHS REPAIRED HOLES"SDR FDEA202111112828None · damagedRH FR47 HOLE 10 HAS THREAD DAMAGE INDICATIONS IN ALL LAYERS. REFER TO EO 6-5710- E0342809 FOR LOCATIONS COMPLIED WITH E.A. 6-5710-TO353473 D P11 "WINGS - BASIC WING STRUCTURE - FR47 RHS REPAIRED HOLESSDR FDEA202103250764Spar · crackedNDT INSPECTED - RH WING FR47 RH 11# HOLE FOUND CRACKED SINGNAL. REPAIRED THE CRACKED HOLE 11 OF RH WING FR47 REAR SPAR AND INTERNAL CORNER ANGLE PER EA 6-5710-T0353473 B P10 & SRM 51-40-44 & SRM 51-40-21. THIS IS A CAT B REPAIR. THE FURTHER INSPECTION REQSDR FDEA202103250763Fitting · crackedNDT INSP - RH WING FR47 171# HOLE FOUND CRACKED SINGNAL. REPAIRED THE CRACKED HOLE 171 OF RH WING FR47 AFT FITTING PER EA 6-5710-T0353473 B P10 & SRM 51-40-44 & SRM 51-40-21. THIS IS A CAT B REPAIR. THE FURTHER INSPECTION REQUIREMENT PER EA 6-5710-T0353473SDR FDEA202103140640Skin · delaminatedRH 5# SPOILER LOWER HINGE ARM AND TOP SKIN FOUND DELAMINATED. PERFORMED THE REPAIR ON RH 5# SPOILER LOWER HINGE ARM AND TOP SKIN PER FEDEX EA # 6-5750-T0360394 P1, TITLE : WING - FLIGHT SURFACE - RH 5# SPOILER CENTER HINGE ARMS LOWER AND OUTSIDE SURFACES SDR FDEA202011112813Adc · failedDURING DEPARTURE NAV ADC IAS DISCREPANCY ON CAPT'S SIDE MASTER WARNING FOR OVERSPEED DISCREPANCY. SELECTED "SYS" 2 ON ADC SWITCHING PANEL FOR F/O'S AIRSPEED INFO ON CAPT'S SIDE. MULTIPLE EXTRA ADC ISSUES ON ECAM REPORTED TO MAINTENANCE AFTER LANDING. REMOVESDR FDEA2019122643300Indicator · inoperativeDOOR R1 SLIDE WILL NOT INDICATE ARMED. ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR INOPERATIVE. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. . ARMED DOOR AFTER ARRIVAL, DOOR OPERATED AND ARMED PROPERLY IAW AMSDR FDEA201905171094Limiter · trippedPDIS 662 27-80 0819 17MAY19 MEM FACT U LOGPAGES:2913364 ON APPROACH INTO KMEM RECEIVED SLATS SYSTEM 1&2 FAULT. RECYCLED SLATS PER PHASE 1S, NO HELP. COMPLIED WITH ECAM AND QRH PROCEDURES. FLAPS WORKED NORMALLY. LANDED 0/40 SLATS WERE 0 UNEVENTFUL LASDR FDEA2019042290868Smoke Detector · failedAFTER TAKEOFF AT APPROX. 1500 AGL. GOT AN AVIONICS SMOKE LIGHT, IT STAYED ON UNTIL 50FT FROM THE GATE TAXIING IN WE ADHERED TO THE QRH & THE ECAM, NEVER HAD ANY SMOKE INDICATONS FIRE CHIEF CONFIRMED NO SMOKE. ALSO AFTER BLOCKIN, THE AVIONICS SMOKE LIGHTSDR FDEA2019042290866Smoke Detector · false activationAFTER TAKEOFF AT APPROX. 1500 AGL. GOT AN AVIONICS SMOKE LIGHT, IT STAYED ON UNTIL 50FT FROM THE GATE TAXIING IN ADHERED TO THE QRH & THE ECAM, NEVER HAD ANY SMOKE INDICATONS FIRE CHIEF CONFIRMED NO SMOKE. ALSO AFTER BLOCKIN, THE AVIONICS SMOKE LIGHT A
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