N298FE
Service difficulty reports · 50
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 = 'N298FE' 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 = 'N298FE' 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 FDEA202607110902Support Beam · crackedCRACK ON UPPER PANEL SUPPORT BEAM, WS 1054 INNER ACCESS PANEL 561QB, LH WING UPPER PANEL SUPPORT BEAM, WS1054 INNER ACCESS PANEL 561QB, LH WING WAS REPLACED AND FASTENERS, SHIM S AND CHORDS WERE INSTALLED I.A.W. E.O. #: H-5720-E0353920 C (P5) RELEASE DATE: SDR FDEA202607100885Floor Panel · puncturedTWO PUNCTURES ON FLOOR PANEL 231QFF AT MDCC FLOOR PANEL 231QFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV.94 DEC 15/ 2025SDR FDEA202607090876Floor Panel · puncturedFIVE PUNCTURES ON FLOOR PANEL 231AFF AT MDCC. THE FLOOR PANEL 231AFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2, PAR 4.B, FIG 201, SHEET 2, REV 94. DEC 15/2025.SDR FDEA202607090874Floor Panel · puncturedTHREE PUNCTURES ON FLOOR PANEL 232NFF AT MDCC FLOOR PANEL 232 NFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R, PAR. 4-B, FIG. 201, SHEET 2, REV 94 DEC 15/2025SDR FDEA202607090873Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231LFF AT MDCC FLOOR PANEL 231 LFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202607090872Floor Panel · dentedDENT WITH DELAMINATION ON FLOOR PANEL 242CFF AT MDCC FLOOR PANEL 242CFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201, SHEET 2, REV 94, DEC 15/2025.SDR FDEA202607090871Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231KFF AT MDCC FLOOR PANEL 231KFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV. 94 DEC 15/2025SDR FDEA202607090870Floor Panel · dentedDENT WITH DELAMINATION ON FLOOR PANEL 231LFF AT MDCC FLOOR PANEL 231LFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4-B FIG 201 SHEET 2 REV. 94 DEC 15/2025SDR FDEA202607070861Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231EFF AT MDCC FLOOR PANEL 231 EFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4-B FIG.201 SHEET 2 REV.94 DEC 15/2025SDR FDEA202607070860Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231CFF AT MDCC FLOOR PANEL 231CFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202607070859Floor Panel · damagedTWO PUNCTURES ON FLOOR PANEL 231DFF AT MDCC FLOOR PANEL 231DFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4-B FIG 201 SHEET 2 REV.94 DEC 15/2025SDR FDEA202607070858Floor Panel · dentedDENT WITH DELAMINATION ON FLOOR PANEL 251KFF AT MDCC FLOOR PANEL 251KFF AT MDCC WAS REPAIRED IAW B767 53-00-50-2R PAR. 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202607070856Floor Panel · damaged2 PUNCTURE ON FLOOR PANEL 251KFF AT MDCC FLOOR PANEL 251KFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. 94 DEC 15/2025SDR FDEA202607070855Floor Panel · dentedTHREE DENTS WITH DELAMINATION ON FLOOR PANEL 241AFF AT MDCC, THE FLOOR PANEL 241AFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4-B FIG. 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202607070853Floor Panel · damagedPUNTURE ON FLOOR PANEL 241KFF AT MDCC FLOOR PANEL 241KFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 94 DEC 15/2025SDR FDEA202607070850Floor Panel · damagedTWO PUNCTURES ON FLOOR PANEL 251PFF AT MDCC FLOOR PANEL 251PFF AT MDCC. REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2, REV. 94 DEC 15/2025SDR FDEA202607070849Floor Panel · damagedPUNCTURED FLOOR PANEL 232HFF AT MDCC FLOOR PANEL 232HFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV. 94 DEC 15/2025SDR FDEA202607060843Floor Panel · cracked2 PUNCTURES ON FLOOR PANEL 231 RFF AT MDCC. FLOOR PANEL 231 RFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201 SHEET 2 REV. 94 DEC 15/2025.SDR FDEA202607060842Floor Panel · crackedPUNCTURE ON FLOOR PANEL 241WFF AT MDCC. FLOOR PANEL 241 WFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV. 94 DEC 15/2025.SDR FDEA202607060841Floor Panel · crackedPUNCTURE ON FLOOR PANEL, 242SFF AT MDCC. FLOOR PANEL 242 SFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. 94 DEC 15/2025.SDR FDEA202607030839Skin · puncturedPUNCTURE AT AFT FLAP LOWER SURFACE BTW 32" FROM INBOARD EDGE AND 2.5" FROM LOWER EDGE. LH WING PUNCTURE AT AFT FLAP LOWER SURFACE BTW 32" FROM INBOARD EDGE AND 2.5" FROM LOWER EDGE LH WING. WAS REPAIRED IAW B767 SRM 51-70-03-0G FIG 15 SHEET 1 AND SRM 57-53SDR FDEA202607030838Floor Panel · dentedDENT WITH DELAMINATION ON FLOOR PANEL 251FFF AT MDCC FLOOR PANEL 251FFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202607030837Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 252DFF AT MDCC FLOOR PANEL 252DFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202607030836Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 251EFF AT MDCC FLOOR PANEL 251EFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202607030835Floor Panel · cracked4 PUNCTURES ON FLOOR PANEL 251VFF AT MDCC FLOOR PANEL 251VFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC15/2025SDR FDEA202607030834Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 252MFF AT MDCC FLOOR PANEL 252MFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202607030833Floor Panel · crackedTHREE DENTS WITH DELAMINATION ON FLOOR PANEL 252HFF AT MDCC FLOOR PANEL 252HFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025.SDR FDEA202607030832Floor Panel · crackedPUNCTURE ON FLOOR PANEL 251LFF AT MDCC FLOOR PANEL 251LFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202407141000Floor Support · crackedSTA. 266, APROX RT BL 20 FLOOR SUPPORT "V" BRACKET CRACKED. REMOVED AND REPLACED SUPPORT V BRACKET 141T5602-8 REF BOEING DRAWING 141T5601 REV C & B767 SRM 51-40-03-0G. THIS IS A MINOR REPAIRSDR FDEA202209242364Switch · failedEMERGENCY EXIT UNARMED PUSH BUTTON LIGHT FELL APART DURNG RELAMPING ON PREFLIGHT. REPLACED ANNUNCIATOR I/A W M/M 33-16-02-2 OPS CHECKS GOOD REF M/M 33-51-08-4SDR FDEA202204030857None · noneLH WING LE AT STA OSS441 RIVETS LOOSE AND FORMER CRACKED P/N 114T2170-5. INSTALLED NEW FORMER REF: E.A. H-5720-T0367810. SEQ:146. W/O:82588.SDR FDEA202204030856None · noneL/H WING L/E #5 SLAT GOUGED STA 499. 0000452710 : ROSNER, DANIEL D - 05-APR-2022 02:00 SEQ 152.. TH-5750-T0367838 P1 N/R 23 L/H WING L/E #5 SLAT GOUGED STA 499. REMOVED DAMAGE MATERIAL AND BONDED IN NEW REPAIRS SEALED AND PAINTED. REF B-767 SRM 57-43-02-2SDR FDEA202204030855None · noneL/H WING L/E #5 SLAT GOUGED STA 441. 0000452710 : ROSNER, DANIEL D - 05-APR-2022 02:02 SEQ 151.. TH-5750-T0367837 P1 N/R 22 L/H WING L/E #5 SLAT GOUGED STA 441. REMOVED DAMAGE MATERIAL AND BONDED IN NEW REPAIRS, SEALED AND PAINTED. REF B-767 SRM 57-43-02-SDR FDEA202106301624Controller · malfunctionedCABIN ALTITUDE EICAS WARNING CLIMBING THROUGH 10,000 FEET OUT OF KGSO. LEVELED THE AIRCRAFT AT 10,000, RAN QRH, CONSULTED GOC AND GSO MAINTENANCE. TRIED BOTH AUTO 1 AND AUTO 2. THEN MOVED THE CONTROLLER TO MAN. WERE STILL UNABLE TO CONTROL THE PRESSURIZATSDR FDEA2020091412173Cabin Pressure · malfunctionedPDIS 298 21-30 4361 1SEP20 MEM. NO PRESSURIZATION ON TAKEOFF MODE SELECTORS 1 OR 2 WOULD NOT WORK, USED MANUAL MODE REMAINDER OF FLIGHT, STAYED 20,000 AND BELOW. FACT 11SEP20 21:14 MEM, REF AMM 21-31-00-5 AND FIM 21-31 FAULT TREE 803. PERFORMED BITE TEST ONSDR FDEA2020090982145Skin · chafedRT WING NR 8 SLAT T/E LOWER SURFACE CHAFED AT INBOARD AUX TRACK. REPAIRED RT WING NR 8 SLAT T/E LOWER SURFACE, IAW B767 SRM 57-43-02-2R REPAIR 1, 51-70-10-2R FIG. 202.SDR FDEA2020090962136Skin · dentedLT WING INBOARD AFT FLAP LOWER SURFACE IS DENTED 10.5 INCHES AFT OF THE LEADING EDGE AND 31.5 INCHES FROM INBOARD SIDE. REPAIRED LT WING INBOARD AFT FLAP LOWER SURFACE IAW B767-300 SRM 57-53-01-0I, SRM 57-53-01-1A, SRM 57-53-01-2R, SRM 51-70-03 PARA 5 FIG 5 ASDR FDEA2020090962135Skin · dentedLT WING INBOARD AFT FLAP LOWER SURFACE IS DENTED AT TRAILING EDGE AND 64 INCHES FROM INBOARD SIDE. REPAIRED LT WING INBOARD AFT FLAP LOWER SURFACE, IAW B767-300 SRM: 57-53-01-1A, SRM 57-53-01-2R REPAIR 1, SRM 51-70-10-2R REPAIR 4. MAJOR REPAIR.SDR FDEA202009032088Skin · chafedLEFT WING #5 SLAT WING STATION OSS 441 IS CHAFFED ON LOWER SURFACE DUE TO WORKING RIVETS REPAIRED LEFT WING #5 SLAT IAW B767 SRM 57-43-02-2R AND 51-70-10-2R REPAIR 4.SDR FDEA202009032087Skin · chafedLEFT WING #5 SLAT AT WING STATION OSS 499 IS CHAFFED ON LOWER SURFACE DUE TO WORKING RIVETS REPAIRED LEFT WING #5 SLAT IAW B767 SRM 57-43-02-2R AND 51-70-10-2R REPAIR 4SDR FDEA2020021080290Stick Shaker · inoperative"WARN ELEX" ON STATUS PAGE DURING PREFLIGHT TROUBLESHOOTING PER B767 FIM 27-32 FT803, WITH IRU'S ALIGNED THE WARN ELEX MSG CLEARS BUT PER BLK 2 WHEN THE LEFT STALL WARNING SWITCH IS TOGGLED THERE IS NO STICK SHACKER AND "WARN ELEX" APPEARS ON THE STATUSSDR FDEA201905261163Unknown · malfunctionedSPOILER DID NOT DEPLOY AT TOUCHDOWN AUTOMATICALLY. HAD TO MANUALLY DEPLOY. FACT 28MAY19 01:56 TPA PERFORMED AUTO SPEEDBRAKE OPERATIONAL TEST AND ALL FUNCTIONS PASSED. ALSO INTERROATED BOTH YSM'S (LEFT AND RIGHT) NO FAULTS OR HISTORY NOTED. PER FIM 27-62 00-SDR FDEA2019022870507Controller · failedPDIS 298 21-30 2907 26FEB19 LAX FACT U LOGPAGES:3042464 ON CLIMBOUT RECEIVED " CABIN ALTITUDE " WARNING LEVELED OFF ALERT WENT AWAY , AIRCRAFT PRESSURIZED TO BELOW SEA LEVEL AND BEYOND MAX DIFFERENTIAL PRESSURE . AIR TURN BACK FACT 26FEB1SDR FDEA201812273612Proximity Sensor · failedAT CRUISE, FL 380 GOT MAIN CARGO DOOR MESSAGE. RAN QRH, SET LANDING ALT TO 9500'. THE AIRPLANE HELD PRESSURE ALL THROUGH DESCENT. DESCENDING THROUGH FL 185, LIGHT WENT OUT BUT IT CAME BACK ON AT 9100'. IMMEDIATLY UPON TOUCHDOWN THE LIGHT WENT OUT BUT THE ACARSSDR FDEA2018120653439Sensor · failedPDIS 298 21-30 2688 05DEC18 MEM OPEN U LOGPAGES:2932480 AT FL 340, CABIN PRESSURE ALTITUDE WARNING. WENT ON CREW DONNED O2 MASK. DID RED TAB CABIN ALTITUDE LOSS - DESCENDED TO 10,000 FT AS AUTO CONTROLLER IN AUTO 1 AND 2 WOULD NOT RESPOND ANDSDR FDEA2018082322150Skin · dentedRIGHT INBD FLAP TOP SURFACE WAS DENTED APPROX 39 INCHES FROM INBD EDGE, AND 6 INCHES FROM AFT EDGE. ACCOMPLISHED A REPAIR ON THE RTFLAP TOP SURFACE IAW SRM 57-53-01-01, AND SRM 51-70-10, REPAIR 2.SDR FDEA201709292797Control Valve · failedALTERNATE SLAT INBD POWER CIRCUIT BREAKER FOUND TRIPPED, DURING FLIGHT DECK INSPECTION. REPLACED CONTROL VALVE MODULE ASSY IAW AMM 27-81-12-4 3.SDR FDEA201709132534Smoke Detector · false activationDURING PUSH BACK, AND ENGINE START, THE LAVATOPRY SMOKE DETECTOR STARTED GOING OFF. THE LED SHOWED RED AS ALARM SOUNDED. ALARM STOPPED AFTER ABOUT THREE MINUTES & LED LIGHT WAS GREEN. NO EVIDENCE OF SMOKE BUT LAVATORY HAD A FOUL ODOR. REMOVED AND REPLACED SDR FDEA201704211300Connector · defectiveON DEPARTURE CLIMBING THROUGH APPROXIMATE 2000 FT EICAS MESSAGE "FWD CARGO DOOR" DECLARED EMERGENCY. ACCOMPLISH QRH. RETURNED TO KEWR LANDED UNEVENTFULLY. REPLACED D6266J ON CARGO DOOR AND REPLACED D6266P REF WDM 52-71-13 PG 1 SHEET 2, REMOVED PSEU REF AMM 32SDR FDEA201607072308Light · brokenDURING APPROCH, FLT TO IND THE RIGHT MAIN GEAR INDICATOR LIGHT FAILED TO ILLUMINATE GREEN WHEN THE GEAR WAS EXTENDED. QRH PROCEDURES WERE FOLLOWED, ALTERNATE GEAR EXTEND PROCEDURES WERE USED. THE RIGHT LIGHT ASSEMBLY BROKE WHILE TRYING TO GET IT TO SUCCESFUL
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