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 FDEA201807301854Bracket · corrodedCORROSION ON MAIN CARGO BAY THRUST BRACKET, BETWEEN FRAMES 26 AND 27, -Y1959 TO -Y2462. REMOVED & REPLACED THRUST BRACKET IAW SRM 51-40-21 AND 51-42-11 AND DWG 53781941, ISSUE D.SDR FDEA2018073091847Seat Track · corrodedCORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 26 AND FR28 AT Y1959. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-10-16 FIGURE 201.SDR FDEA2018073091846Seat Track · corrodedCORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 26 AND FR28 AT Y1959. REMOVED AND REPLACED SEAT TRACK SECTION PER SRM 53-10-16 AND DWG A53781970 ISSUE D.SDR FDEA2018073091845Seat Track · corrodedCORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 26.5 AND FR27.5 AT Y1456. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-10-16 FIGURE 201.SDR FDEA2018073091844Seat Track · corrodedCORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 26 AND FR28 AT Y1456. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-10-16 FIGURE 201.SDR FDEA2018073091843Seat Track · corrodedCORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 26 AND FR28 AT Y953. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-10-16 FIGURE 201.SDR FDEA2018073091842Seat Track · corrodedCORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 26 AND FR28 AT Y450. REMOVED & REPLACED SEAT TRACK PER SRM 53-10-16 AND DWG A53781970 ISSUE D.SDR FDEA2018073091841Seat Track · corrodedCORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK, FRAME 26 Y2462. REMOVED AND REPLACED SEAT TRACK SECTION IAW EA 6-5310-T0341529.SDR FDEA2018073081834Floor Panel · damagedMAIN CARGO COMPARMENT FLOOR PANEL 231GG HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.SDR FDEA2018073081832Floor Panel · damagedMAIN CARGO COMPARMENT FLOOR PANEL 231PG HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.SDR FDEA2018073081829Floor Panel · damagedMAIN CARGO COMPARMENT FLOOR PANEL 231CF HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.SDR FDEA2018073081828Floor Panel · damagedMAIN CARGO COMPARMENT FLOOR PANEL 231KG HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.SDR FDEA2018073081826Floor Panel · damagedMAIN CARGO COMPARMENT FLOOR PANEL 231NG HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.SDR FDEA2018073081825Floor Panel · damagedMAIN CARGO COMPARMENT FLOOR PANEL 231EH HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.SDR FDEA2018073081824Floor Panel · damagedMAIN CARGO COMPARMENT FLOOR PANEL 231DH HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.SDR FDEA2018073081823Floor Panel · delaminatedMAIN CARGO COMPARMENT FLOOR PANEL 231EF HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.SDR FDEA201802060315Relay · failedPASSING 30K FEET CLIMBING TO FL 340, A NR 1 ENGINE FIRE INDICATION, ENGINE INDICATIONS WERE NORMAL. FOLLOWED ECAMS AND SECURED THE NR 1 ENGINE. FIRE INDICATION REMAINED AFTER AGENT FIRED. FIRED THE NR 2 AGENT AND THE FIRE INDICATION DEACTIVED. RETURNED TSDR FDEA201801160098Control Module · malfunctionedAPPROACHING THE TOP OF DESCENT, RECEIVED SEVERAL 1 - 2 SECONDS NR 1 ENGINE FIRE ECAM INDICATIONS. ONLY THE LOOP A WAS ILLUNMINATED. TROUBLESHOT AND FOUND THE NR 1 ENGINE FIRE CONTROL MODULE HAS NOT YET BEEN REPLACED, R & R THE NR 1 FIRE CONTROL MODULE IAW SDR FDEA201801030005Duct · looseVERY SHORTLY AFTER LEVEL OFF, AT FL330, THE NR 1 ENGINE FIRE WARNING DISPLAYED. BEFORE INITIATING PROCEDURES, THE WARNING DISAPPEARED WITHIN A SHORT PERIOD, LESS THAN 10 SECONDS, THE WARNING DISPLAYED AGAIN AND REMAINED ILLUMINATED. COMPLIED WITH THE PROSDR FDEA201712273453Detection Sys · false activationNR 1 ENGINE FIRE INDICATION. SHUTDOWN THE ENGINE, PULLED FIRE HANDLE, DISCHARGED THE FIRE AGENT 1. FIRE INDICATION WENT AWAY AFTER AGENT DISCHARGED. FOIL WRAPPED TWO COUPLING DUCTS FOR LTP DUCT THAT HAD FOIL BLOWN OUT. RAN THE NR 1 ENGINE IAW JRH, TESTED NRSDR FDEA201712183409Rib · crackedR/H WING CENTER FLAP RIB 26 CRACKED FWD OF REAR SPAR. REMOVED THE DAMAGED FLANGE OF THE RIB IAW SRM 57-50-00, REPAIRED IAW SRM 57-50-00, FIG. 201 WITH A REPAIR ANGLE. CLASSIFIED AS CAT A AND MAJOR REPAIR.SDR FDEA201712183408Rib · crackedRIGHT WING, CENTER FLAP INTERNAL RIB 27 CRACKED AT 6 FASTENERS FWD OF REAR SPAR. REMOVED THE DAMAGED FLANGE OF THE RIB IAW SRM 57-50-00, REPAIRED IAW SRM 57-50-00 WITH REPAIR ANGLE, CLASSIFIED AS CAT A AND MAJOR REPAIR.SDR FDEA201712163403None · noneNEED TO ACCOMPLISH SKIN REPAIR ON L/H CENTER FLAP BETWEEN RIB #26 AND #27 FOR ACCESS TO RIB REPAIR. REPAIRED PER SRM 57-50-00, FIG 205, DOUBLER INSTALLED ON L/H CENTER FLAP BETWEEN RIBS 26 AND RIB 27, BETWEEN THE REAR SPAR AND STRINGER 2.3 BOTTOM SKIN IAW SDR FDEA201712163402None · noneNEED TO ACCOMPLISH SKIN REPAIR ON L/H CENTER FLAP ADJACENT TO RIB #12 FOR ACCESS TO RIB REPAIR. REPAIR PER SRM 57-50-00, FIG 205, DOUBLER INSTALLED ON L/H CENTER FLAP BETWEEN RIBS 11 AND 12 AND BETWEEN THE REAR SPAR AND STRINGER 2.1, BOTTOM SKIN IAW SRM 51SDR FDEA201712163401None · noneNEED TO ACCOMPLISH SKIN REPAIR ON R/H CENTER FLAP ADJACENT TO RIB #19 FOR ACCESS TO RIB REPAIR. REMOVED FASTENERS FOR REPAIR DOUBLER ON RIGHT WING CENTER FLAP RIB #19, FABRICATED REPAIR DOUBLER IAW SRM 57-50-00, INSTALLED REPAIR DOUBLER IAW SRM 51-40- 21,SDR FDEA201712163400Rib · crackedLEFT WING, CENTER FLAP INTERNAL RIB # 26 CRACKED 6 FASTENERS FWD OF REAR SPAR. REPAIRED RIB #26 WITH 3 EA. FLANGES IAW A300 SRM 57-50-00, FIG. 201. CLASSIFED AS CAT "A" AND MAJOR REPAIR.SDR FDEA201712163399Rib · crackedLEFT WING, CENTER FLAP INTERNAL RIB #12 CRACKED 6 FASTENERS FWD OF REAR SPAR. REMOVED DAMAGE ON L/H WING CENTER FLAP RIB #12 IAW SRM 57-50-00, FIG. 201, FABRICATED REPAIR ANGLE IAW SRM 57-50-00, FIG 20, INSTALLED REPAIR ANGLE IAW SRM 51-40-21, CLASSIFED ASSDR FDEA201712163398None · noneNEED TO ACCOMPLISH SKIN REPAIR ON R/H CENTER FLAP ADJACENT TO RIB #25 FOR ACCESS TO RIB REPAIR. REMOVED FASTENERS FOR REPAIR DOUBLER ON CENTER FLAP AT RIB #25 R/H, FABRICATED DOUBLER REPAIR IAW A300-600 SRM 57-50-00 PAGE 217, LOCATED AND DRILLED DOUBLER IASDR FDEA201712143390Rib · crackedLEFT WING, CENTER FLAP INTERNAL RIB NR 27 CRACKED FWD OF REAR SPAR. REPAIRED THE RIB IAW SRM 57-50-00, FIG 201 AND 202, CLASSIFIED AS A CAT "A' AND MAJOR REPAIR.SDR FDEA201712143386Coupling · bentMAIN DECK RH SIDE AT FRAME 22 STR8 AND STR9 FRAME AND SPLICE HAS BENT. REMOVED DAMAGE COUPLING IAW A300-600 SRM 51-40-21, FABRICATED NEW COUPLING P/ FX- A53770903210 ON VTMAE TRAVELER T17/1312426 IAW SRM 53-13-13, INSTALLATION COUPLING IAW A300 SRM 51-40-44SDR FDEA201712143391Angle · crackedRIGHT WING, CENTER FLAP INTERNAL RIB #19 CRACKED 6 FASTENERS FWD OF REAR SPAR. REMOVED CRACKED RIB #19 IAW SRM 57-50-00 FIG 201, REPAIR CRACKED RIB #19 RIGHT WING CENTER FLAP IAW SR 57-50-00 FIG 201 WITH REPAIR ANGLE. CLASSIFIED AS "A" AND MAJOR REPAIR.SDR FDEA201712143389Rib · crackedRIGHT WING CENTER FLAP INTERNAL RIB #25 CRACKED 6 FASTENERS FWD OF REAR SPAR. REMOVED CRACKED RIB #25 IAW SRM 57-50-00, REPAIRED CRACK RIB #25 ON R/H WING CENTER WING FLAP IAW SRM 57-50-00 WITH REPAIR ANGLE, REPAIR CLASSIFIED AS CAT "A" AND MAJOR REPAIR.SDR FDEA201712143387Coupling · bentMAIN DECK RH SIDE AT FRAME 23 BETWEEN STR 8 AND STR9 FRAME SPLICE HAS BENT. REMOVED DAMAGE COUPLING IAW A300 SRM 51-40-21, FABRICATED NEW COUPLING P/N FX- A53770903210 ON VT MAE TRAVELER T17/132376 IAW SRM 53-13-13, INSTALLATION NEW COUPLING IAW SRM A300 SRSDR FDEA201712123371Floor Panel · brokenMDCC 241LK FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL 241LK ON VTMAE TRAVELER #17/1311725 IAW SRZ 25-005, CLASSIFED AS CAT. 'A' AND MAJOR REPAIR.SDR FDEA201712123361Floor Panel · brokenMDCC 252BF FLOOR PANEL BROKEN FABRICATED FLOOR PANEL 252BF ON VTMAE TRAVELER #17/1311729 IAW SRZ 25-005, CLSSIFED AS CAT. "A" AND MAJOR REPAIR.SDR FDEA201708272376Hydraulic Line · leakingON CLIMBOUT FROM KMEM NOTICED YELLOW HYD SYSTEM FLUID DECREASING. WITHIN A COUPLE MINUTES THE ECAM ALERTED US TO LOW PRESSURE. WE FOLLWED ECAM PROCEDURES AND QRH PROCEDURES. THERE WAS A LITTLE FLUID LEFT UPON SHUTTING DOWN THE YELLOW PUMP. RTB UNEVENTFUSDR FDEA201704111130Engine · failedFLYING FROM SJC TO IND AT LEVEL OFF THE OIL BUGS WERE SET AT 16QTS ON EACH GAGE TO MATCH THE CORRECT OIL QUANTITY READING. APPROXIMATELY 15-20 MINS LATER, NR 1 ENG OIL QUANTITY DECREASED TO 13 QTS, THEN 5-10MIN LATER WENT TO 12.5 QTS. FO WENT TO THE CABIN ARESDR FDEA201604151232Limiter · leakingBOTH FLAP SYS 1 & 2 FAILED ON APPROACH. INTERROGATED SFCC 1 & 2. BOTH SHOWED JAM. RESET & DID BITE CHECK, BOTH PASSED. CHECKED LT & RT FLAP TORQUE LIMITERS. LT FLAP TORQUE LIMITER WAS POPPED IAW MM 27-51-00-05. WILL OPS CHECK FLAPS WHEN DONE UNLOADING. SDR FDEA201604081168Battery · dischargedR1 DOOR SLIDE WOULD NOT ARM. RELEASED FOR SERVICE IAW MEL 52-30-04 CATEGORY C EXPIRATION 16 APR1 16. ECAM SLIDE INDICATION SYS FOR R1 DOOR INOPERATIVE. DOOR ESCAPE SLIDE ARMING SYS IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. TROUBLE SHOT IAW SDR FDEA201508232693Indication Sys · faultyON CLIMB OUT PASSING FL 230 GOT ECAM FUEL ADVISORY, LT INNER WAS READING 16.5 & RT INNER READING APPROX 10.5, WITHIN 2 MINUTES WENT DOWN TO MATCH RT INNER, THEN WENT 4.0 BELOW RT INNER. RELEASED FOR SERVICE IAW MEL 28-42-01-05 CATEGORY C, EXPIRATION 02 SEPT 1SDR FDEA201506292123Thrust Reverser · damagedNUMBER 1 OTBD THRUST REVERSER AFT HINGE LUG DAMAGED EXHAUST SYS. THRUST REVERSER BLEND REPAIR OF HINGE BEAM REPAIRED IAW EA 6-7830-T0318435. THIS REPAIR IS CLASSIFIED AS A CATEGORY B MAJOR REPAIR.SDR FDEA201506262093Window Frame · gougedRIGHT SLIDING WINDOW PANEL FWD FRAME HAS CHAFED MARKS. ACCOMPLISHED FINAL EA 6-5610-T0318208 PT 1. RT SLIDING WINDOW FWD FRAME GOUGED.SDR FDEA201506262092Window Frame · gougedLEFT SLIDING WINDOW PANEL FWD FRAME CHAFED. ACCOMPLISHED FINAL EA 6-5610-T0318226 P 1 LT SLIDING WINDOW FWD FRAME GOUGED.SDR FDEA201506262091Floor Panel · damaged152 RF HAS 1 TORN OUT FASTENER HOLE & CRACKED ON BACKSIDE CORNER. FABRICATED NEW PANEL 15 2RF ON T15 1145409.SDR FDEA201506242019Floor Support · crackedBULK PIT FRAME 65 TO 66 AT -Y1949 FLOOR SUPPORT IS CRACKED FWD END. R & R FLOOR SUPPORT IAW SRM 51-40-21. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.SDR FDEA201506242016Rib · chafedLEFT WING AFT OF REAR SPAR HYD SUCTION LINE CLAMP BLOCK ATTACHMENT BOLT CHAFING ON RIB 7A. CUT OUT EDGE COMPLIED WITH EA 6-5710-T0318026 ON LT RIB 7A OTBD EDGE DUE TO MATERIAL REMOVED FROM RIB EXCEEDED SRM LIMITS IAW SRM 57-20-19. THIS REPAIR IS CLASSIFIED ASDR FDEA201506242015Floorbeam · corrodedBULK CARGO FLOOR LEVEL AT FRAME 66, LT SIDE FLOORBEAM HAS CORROSION. R & R FRAME 66 FLOORBEAM BULK CARGO FLOOR IAW SRM 51-40-21 DUE TO CORROSION OUT OF LIMITS IAW SRM 51-74-10 & SRM 51-10-10. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.SDR FDEA201506242013Floor Panel · damagedBULK CARGO FLOOR PANEL 161 CF HAS DENTS, PUNCTURED & CORROSIONS AT THE BACK. FABRICATED FLOOR PANEL 161 CF ON T15 1145406 IAW DWG SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.SDR FDEA201506242012Floor Panel · damagedFORWARD CARGO COMPARTMENT, FLOOR PANEL 132 SG HAS SEVERAL DENTS, CRACKS, DAMAGED EDGES, HONEY COMB & MISSING SEALANT. FABRICATED FLOOR PANEL 132 SG ON T15 1145781 IAW DWG SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.SDR FDEA201506242011Floor Panel · damagedFORWARD CARGO COMPARTMENT FLOOR PANEL 131 KG HAS SEVERAL DENTS & DAMAGED INSERTS. FABRICATED FLOOR PANEL 131 KG ON T15 1146564 PER DWG SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
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