N304FE
Service difficulty reports · 283
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 = 'N304FE' 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 = 'N304FE' 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 FDEA201008052841Floor Panel · damagedCENTER CARGO COMPARTMENT FLOOR PANEL 183 QF HAS A MISSING INSERT. FABRICATED NEW FLOOR PANEL 183 QF IAW DWG SRZ 25-005, REV "H".SDR FDEA201008052825Floorboard · mismanufacturedAFT CARGO FLOORBOARD 187DF DOES NOT CONFORM TO DWG SRZ 25-011. FABRICATED NEW FLOOR PANEL 187DF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".SDR FDEA201008052824Floorboard · mismanufacturedAFT CARGO FLOORBOARD 187CF DOES NOT CONFORM TO DWG SRZ 25-011. FABRICATED NEW FLOOR PANEL 187CF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".SDR FDEA201008052823Floorboard · mismanufacturedAFT CARGO FLOORBOARD 187BF DOES NOT CONFORM TO DWG SRZ 25-011. FABRICATED NEW FLOOR PANEL 187 BF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".SDR FDEA201008052822Floorboard · mismanufacturedAFT CARGO FLOORBOARD 187AF DOES NOT CONFORM TO DWG SRZ 25-011. FABRICATED NEW FLOOR PANEL 187 AF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".SDR FDEA201008042803Support · corrodedLEFT WING LEADING EDGE FIRE BOTTLE SUPPORT LANDING HAS FRETTING. BLENDED AND CHECKED LIMITS OF FRETTING ON LEFT WING L/E FIRE BOTTLE DOOR LANDING IAW SRM 57-00-01, FIG 1A, VOL I. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II AND PAINTED IAW SRM 51-21-01, VOL ISDR FDEA201006051831Sensor · inoperativeDURING CLIMBOUT AND ABOVE 300K RECIEVED RED UNLOCKED PRIMARY AND SECONDARY INDICATION FOR CTR GEAR. RAN QRH-CYCLED GEAR SUCCESFULLY AND ALL LIGHTS OUT SHOWING ALL GEAR UP AND LOCKED. NO RECURRENCE AND NEVER HAD PSEU FAULT OR PSEU FAIL ALERTS. ORIGINAL PLAN DASDR FDEA200907252751Controller · failedAFTER GEAR EXTENSION RECEIVED A ANTISKID L FAIL ALERT, WENT AROUND. PROCEDED WITH QRH PROCEDURE. USED RWY 36L AS PRECAUTION. LANDED NORMAL NO PROBLEMS WITH BRAKE OVERTEMP OR FAIL. DID A RTS ON ASCU IAW MM 32-45-01-5 PAR. 2, TEST FAILED, ASCU INTERNAL FAULSDR FDEA200811084795Engine · overtempAFTER 2 HOURS INTO FLT GOT EGT FLUCTUATING UP TO 1065 DEGREES CELSIUS TO VALUES AT OR BELOW NORMAL. RETARDED THROTTLE TO IDLE AND RAN CKLIST. EGT STILL FLUCTUATING WILDLY SO PERFORMED ENG SHUTDOWN. NO OTHER INDICATIONS OF SEVERE DAMAGE, BUT WITH EGT STILL SDR 08FDEA04795Engine · malfunctionedAT 2 00 INTO FLIGHT GOT EGT FLUCTUATING UP TO 1065 DEGREES CELSIUS TO VALUE S AT OR BELOW NORMAL. RETARDED THROTTLE TO IDLE AND RAN CHECKLIST EGT STILL FLUCTUATING WILDLY SO WE PERFORMED ENG SHUTDOWN. NO OTHER INDICATIONS OF SEVERE DAMAGE, BUT WITH EGT STILLSDR 08FDEA03596Seat Track · damagedMAIN CARGO DECK STA 1256-1276 RBL 48 SEAT TRACK IS DAMAGED REPLACED SEAT TRACK IAW SRM 51-70-00.SDR 08FDEA03595Seat Track · damagedMAIN CARGO DECK STA 1119-1159 RBL 48 SEAT TRACK IS DAMAGED. REPLACED SEAT TRACK IAW SRM 53-70-00.SDR 08FDEA03565Fitting · corrodedMCD HOLES NR 7 FITTING LWR JAMB SUPPORT 2 EA INBD HOLES HAVE CORROSION REMOVED AND REPLACED FITTING IAW SRM 53-50-00 PAGE 81 FIG 17. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR AND IS RII.SDR 08FDEA03564Fitting · corrodedMCD HOLES NR 5 FITTING LWR JAMB SUPPORT 2 EA AFT HOLES HAVE CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-50-00 PAGE 81 FIG 17. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR AND IS RII.SDR 08FDEA03563Fitting · corrodedMCD HOLES NR 3 FITTING LWR JAMB SUPPORT 1 AFT OUTBD HOLE HAVE CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-50-00 PAGE 81 FIG 17. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR AND IS RII.SDR 08FDEA03430Floorbeam · corrodedLWR FWD CARGO COMPT FLOOR SUPPORT FITTING ATTACHED ON FLOORBEAM UPPER FLANGE HAS CORROSION AROUND FASTENER HOLES AT STA 735, X4 - 25. FABRICATED NEW SUPPORT ON MAE TRAVELER T8/754216. REMOVED AND REPLACED SUPPORT IAW SRM 51-31-01. MAJOR REPAIR.SDR 08FDEA03429Floorbeam · corrodedLWR FWD CARGO COMPT FLOOR SUPPORT ANGLE ATTACHED ON FLOORBEAM UPPER FLANGE HAS CORROSION AROUND FASTENER HOLE AT STA 1059, X 41-55. FABRICATED NEW FLOOR SUPPORT ON MAE TRAVELER T8/754037. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-31-01. MAJOR REPAIR.SDR 08FDEA03428Floorbeam · corrodedLWR FWD CARGO COMPT FLOOR SUPPORT FITTING ATTACHED ON FLOORBEAM UPPER FLANGE HAS CORROSION AROUND FASTENER HOLES AT STA 791, X 4 - 25. FABRICATED NEW FLOOR SUPPORT ON MAE TRAVELER NR T8/754204. REMOVED AND REPLACED SUPPORT IAW SRM 51-31-01. MAJOR REPAIR.SDR 07FDEA05113Switch · failedPDIS: LEVEL AT FL330, 45 MINUTES INTO FLIGHT, GOT NR 3 MANF LIGHT, FOLLOWED BY A LEVEL 3 "MANIFOLD NR 3 FAIL" ALERT. COMPLIED WITH RED TABS AND LANDED AT NEAREST SUITABLE AIRFIELD (KLAS). MAN LIGHT EXTINGUISHED SOMEWHERE BETWEEN 8000' AND 5000' IN THE DESCENSDR 07FDEA02556Vent · malfunctionedPDIS: RCVD CABIN RATE ON DEPARTURE. A/C WOULD NOT PRESSURIZE. CHANGED CONTROLLER TO MANUAL NO CHANGE. OUTFLOW VALVE INDICATED CLOSED ENTIRE TIME ON SYNOPTIC PAGE AND ON PNL. ON SYNOPTIC "CLOSED" INDICATOR IN AMBER BUT VALVE INDICATOR WAS CLOSED. RETURNESDR 07FDEA02555Motor · failedPDIS: AFTER DEPARTURE, CLIMBING THROUGH 8000 FT RECEIVED "CABIN RATE" ALERT. LEVELED AT 10,000 FT THEN RECEIVED " CABIN ALTITUDE ALERT. REFER TO QRH PROCEDURE, NO CHANGE. A/C PRESSURIZED TO OUTSIDE PRESSURE AT 10,000 FT THROUGH LANDING. OUTFLOW VALVE SHOWESDR 07FDEA02078Fire Warning · illuminatedPDIS:304 EN ROUTE FROM KMEM TO TLC AT FL340, RECEIVED LEVEL 3 CRG FIRE LWR FWD. ACCOMPLISHED PHASE ONE AND REFERRED TO THE RED TABS. THE CKLIST DIRECTED US TO LAND AT THE NEAREST SUITABLE AIRPORT, LANDED KCRP. ACN RELEASED FOR SERVICE PER MEL/CDL: 26-22-01-SDR 07FDEA00859Rudder · damagedDURING AUTOPILOT TEST DAMAGED LOWER RUDDER AFT T/E. REPAIRED T/E SECTION IAW SRM 55-30-00 VOL 1 FIG 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I031562/N01562 AND IAW SRM 55-30-00 VOL 1 FIG 2.SDR 07FDEA00858Skin · dentedLWR FUSELAGE EXT ZONA FOUND DEEP DENT ON SKIN DIMENSION: 2" BY 1.25" DEEP 0.09" BTWN STA 1801 AND STA 1821 FROM LONG NR 42 TO LONG NR 43 RT SIDE. REMOVED EXTERNAL DOUBLER AND INTERNAL FINGER DOUBLERS IAW SRM 53-20-00 FIG 6 VOL 1. REPAIRED IAW SRM 53-20-00 FSDR 07FDEA00857Skin · corrodedFOUND LT WING L/E FOUND CORROSION WITH EXF ON SKIN FIXED PANEL AT STA XOS 910-930. REPAIRED SACRIFICIAL DOUBLER IAW SRM 57-10-00 FIG 19D SHT 1 VOL 1. TOUCHED UP IAW SRM 51-21-01 VOL 2 PAG 21-25 AND SRM 51-21-02 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVESDR 07FDEA00855Skin · crackedFOUND 3 CRACKS AND LOOSE RIVETS ON SKIN OF OUTBOARD FLAP LT WING LWR AND UPPER SURFACE BETWEEN STA XOF 533 & XOF 462. CUT OUT DAMAGED AREA IAW SRM 57-10-00 FIG 85 VOL 1. FOUND ON "C" 2 CRACKS 1" LONG AND .25" LONG. REMOVED TO GAIN ACCESS T/E PROFIL UP AND LSDR 07FDEA00593Skin · crackedLT HORIZ STAB OUTER SECTION UPPER AFT SKIN PANEL FOUND 1 CRACK 2, 5" LONG. REPAIRED CRACKED SKIN PANEL IAW SB 55-18 AND EA NR 8-5510-103679. WORKED IN CONJUNCTION WITH NRC N00898/I030898.SDR 07FDEA00592Spar Cap · crackedDURING HFEC INSP, ON LT HORIZONTAL STAB, AFT SPAR CAP, FOUND CRACK, ON UPPER SURFACE AND INNER SURFACE OF ONE BARREL NUT. RETAINER IS INSTALLED IN BARREL NUT HOLE. REMOVE FOR TOTAL CRACK LONGEST. REMOVED L/E CTR SECTION HORIZ STAB IAW MM 55-10-02. REMOVED SDR 07FDEA00558Fuel Tank · corrodedMAIN CABIN SEVERE CORROSION WITH EXFOLIATION ON LT CENTER TANK SKIN TUNNEL AREA, STA 1370 X= 101 (NEAR SLANT PANEL ). LT SLANT PANEL REMOVED, REMOVED BOLTS, ACCESSED AUX UPPER ANGLE REAR SPARE ANGLE. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. ALL REMOVSDR 07FDEA00557Door Frame · crackedFOUND MAIN CABIN CRACK 1" LONG ON WEB FWD JAMB DOOR NR 3 LT STA 1251 LONG NR 27. PERFORMED NDI CHECK FOR CRACKS POSITION. REMOVED JAMB DOOR COVER FOR ACCESS IAW MM 20-50-02. MAKE 2 STOP DRILL CRACK .250" DIA HOLE, INSTALLED REPAIR DOUBLER P/N I030889-3A IAWSDR 07FDEA00556Seat Track · crackedFOUND MAIN CABIN CRACK 12" LONG ON TRACK X=27 BTWN STA 1079 AND 1099. REMOVED FLOOR PANEL IAW MM 53-21-01-2. REMOVED SEAT TRACK SPLICE AT STA 1129 IAW SRM 51-33-01 VOL 2. CUT AND REPLACED SEAT TRACK SECTION AT STA 1069 IAW SRM 53-70-00 FIG 1 SHEET 1-2. REISDR 07FDEA00553Frame · crackedFWD CARGO COMPT FOUND 1 CRACK 0.25" LONG ON FRAME AT STA 615 BTWN LONG NR 39 AND LONG NR 40 LT FRAME FLANGE REPAIR CARRIED OUT IAW SRM 53-30-00 FIG 4A VOL 1 AND SRM 53-12-01 FIG 2 VOL 3 "SATIS" AREA REPROTECTED IAW SRM 51-21-01 VOL 2. FRAME REPAIRED IAW SRM 5SDR 07FDEA00109Seat Track · corrodedMAIN CABIN FROM STA 745 TO STA 949 X= -47 RT 6 EA EXISTING SEAT TRACK SPLICE. REMOVED SEAT TRACK SPLICE IAW SRM 51-30-00 VOL 2. REMOVED CORROSION (LIGHT) IAW SRM 51-21-01 PAGE 28 ORIGINAL THK IS .50" IAW SRM 53-70-00 FIG 1 SHEET 2 AND DWG S4932154, RESIDUAL SDR 07FDEA00107Skin · crackedFOR CUSTOMER REQUEST, HORIZONTAL STAB UPPER INTERIOR SKIN PANELS, FOUND CRACKED PANELS P/N7228-1, POSITION 6 AND 7 AND PANEL P/N7229-1 POSITION 2, SEE ATTACHING MAP FOR DETAIL. REMOVED AND REPLACED PANELS ALC7228-1 AND ALC7229-1 IAW SB55-16 GROUP 2 FOLLOWING SDR 07FDEA00106Skin · crackedDURING U/S INSP OF HORIZ STAB COSTANT AND OUTER SECTION SKIN PANEL, FOUND CRACKED PANEL: P/N7228-1, POSITION 6&7, P/N7229-1 POSITION 2 AND P/N7226-1 POSITION 18, SEE ATTACHED SHEET FOR DETAIL, POSITION 6, 7 AND 2 CRACKS ARE HANDLED BY NRC N00628. POSITION 18 SDR 07FDEA00105Skin · misrepairedLT WING L/E UPPER SIDE AT STA XIS240 EXISTING SKIN REPAIR. PERFORMED INSPECTION OF REPAIR AND NOT FOUND INCOMPLIANCE WITH CRITERIA REQ BY EO NR 8-5100-7-5001 BECAUSE FOUND WEAR ON SURFACE OF DOUBLER. REMOVED AND REPLACED REPAIR IAW SRM 57-10-00 FIG 15A SHTSDR 06FDEA04241Frame · wornCOCKPIT AREA FOUND DEEP WEAR ON FRAME AT STA 392 RT SIDE X=-39, AREA OF WORN AT FS 392 FRAME RT X=-39. BLENDED OUT AREA NDT NO CRACKS FOUND. FRAME REPAIRED IAW SRM 53-30-00 FIG 4 PAGE 13 VOL 1.SDR 06FDEA04180Door Frame · crackedMAIN CABIN, CRACK LONG 0.50" ON WEB AFT JAMB DOOR NR 3 LT STA 1305 LONG NR 27. REMOVED FLOOR COVER IAW MM 20-50-02. MAKE STOP DRILL CRACK DIAM .250". PERFORMED MFC INSP NOT FOUND ANOTHER CRACK, IAW NDI SPM 06. INSTALLED REPAIR DOUBLER IAW SRM 53-50-00 FIG SDR 06FDEA04075Skin · unknownRT WING L/E SKIN LOWER SIDE SLAT DRIVE MECHANISM ACCESS DOOR CUT OUT AT STA XORS 402 EXISTING SKIN REPAIR. REMOVED EXISTING REPAIR IAW SRM 57-10-00 VOL 1. INSTALLED REPAIR IAW SRM 57-10-00 FIG 68 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER NR N01203 ANDSDR 06FDEA04074Skin · misrepairedLT WING NR 2 SLAT ASSY INNER SKIN AT STA XIRS 225 EXISTING SKIN REPAIR. PERFORMED INSPECTION AND NOT FOUND REPAIR INCOMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 BECAUSE FOUND LOOSE CHERRY AND MISSING RIVETS ON STILL SEAL. REPLACED LOOSE BLIND FASTENSDR 06FDEA04073Skin · corrodedMAIN CABIN SEVERE CORROSION WITH EXFOLIATION ON LONG 17 RT FROM STA 1501 TO STA 1521. REMOVED FASTENERS IN CORRODED AREA IAW SRM 51-35-01 VOL 2. REMOVED CORROSION IAW SRM 53-00-01 FIG 1B VOL 1. ORIGINAL THK IS .105" IAW DWG AEA0220 (-1). RESIDUAL THK IS 0,SDR 06FDEA04072Skin · corrodedMAIN CABIN LIGHT CORROSION WITH EXFOLIATION ON LONG 17 RT BTWN STA 1159 AND STA 1179. REMOVED FASTENERS IN CORRODED AREA IAW SRM 51-35-01 VOL 2. REMOVED CORROSION IAW SRM 53-00-01 FIG 1B VOL 1. ORIGINAL THK IS .105" IAW DWG AEA0220(-509). RESIDUAL THK IS 0,SDR 05FDEA01001Line · leakingAFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT GO TO UP POSITION, ACCOMPLISHED QRH PROCEDURE. COULD NOT OVERRIDE. UPON RETURN TO GATE DISCOVERED THE RT MLG TRIM CYLINDER HYDRAULIC LINE HAS PIN HOLE. NO OTHER PROBLEMS NOTED FROM VISUAL INSPECTION. REPLACED SDR 05FDEA00256Access Panel · crackedLEFT HAND WING LEADING EDGE SKIN CRACKED AT STATION XORS 530, AROUND REFUELING STATION ACCESS PANEL INBOARD CORNER. COMPLIED WITH EA 8-5710-8352, WINGS- LEFT HAND LEADING EDGE TEE CRACK AT REFUELING DOOR CUTOUT- REPAIR.SDR 05FDEA00255Frame · corrodedFRAME AND INTERCOSTAL CORRODED AT STATION 1461 RIGHT WHEEL WELL INTERIOR AREA. COMPLIED WITH FEDEX EA 8-5310-83975, FUSELAGE- CORROSION DAMAGE TO LT STATION 1505, LONGERON 35 FRAME- REPAIR, AND FEDEX EA 8-5310-83974, AFT WHEEL WELL- PRESSURE BULKHEAD TEE FRAMSDR 05FDEA00254Hanger Assy · corrodedRIGHT WING LOWER AFT BEAM SUPPORT FITTING PN ARC0459-2 REQUIRES FABRICATION. FABRICATED FITTING ARC0459-2 IAW DAC DWG ARC0459-2 AND FEDEX EA 8-5732-83971, WINGS- RIGHT HAND WING, LOWER AFT BEAM, SUPPORT HANGER.SDR 05FDEA00252Spar · damagedLEFT HAND INBOARD FLAP WEDGE UPPER FORWARD ATTACH POINT AT OUTBOARD EDGE OF PANEL FIFTH (5) HOLE IS ELONGATED. FABRICATED AND INSTALLED BUSHING IAW FEDEX EA 8-5710-83968, WINGS- LEFT HAND INBOARD FLAP, INBOARD FLAP WEDGE OVERSIZE BOLT HOLE- REPAIR, AND DC10 SSDR 05FDEA00251Seal · leakingLAVATORY, WHEN A FLASHLIGHT IS PLACED IN TRASH CAN THE INNER AND OUTER TRASH RECEPTACLE DOORS AND TRASH CAN LEAKS LIGHT. SEALED LAVATORY TRASH RECEPTACLE IAW FEDEX EA 8-2540-83964, EQUIPMENT/FURNISHINGS - LAVATORY WASTE COMPARTMENT SEALS - REPAIR.SDR 05FDEA00250Skin · corrodedLEFT WING INBOARD FLAP, LOWER SKIN AT TRACK LOWER FILLET FAIRING TRAILING EDGE AREA, HAS SURFACE CORROSION, XIFH 126.650-XIFH 120.908. REMOVED FAIRING AND WEDGE, FABRICATED AND INSTALLED REPAIR IAW FEDEX EA8-5710-83969, WINGS - LEFT HAND INBOARD FLAP, LOWER SSDR 05FDEA00249Hinge · corrodedLEFT HAND OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE CORRODED. REMOVED CORROSION, FABRICATED OVERSIZED BUSHING, INSTALLED AND HONED TO FINAL INSIDE DIAMETER OF 0.8745-0.8755 INCHES, IAW DAC CMM 57-52-02 AND FEDEX EA 8-5710-83965, WINGS- LEFT HAND OUTBOAR
Back to N304FE