N182FE

Service difficulty reports · 34

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 = 'N182FE' 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.

SDR FDEA202604220492Slat System · faultedLEADING EDGE SLAT DISAGREE CAUTION MESSAGE APPEARED WHEN FLAPS WERE SELECTED FROM ZERO TO ONE. WE DECLARED AN EMERGENCY OUT OF AN ABUNDANCE OF CAUTION. RAN THE QRH FOR THE PROCEDURE. THE SLATS WERE RESTORED IN THE ALTERNATE MODE. LANDING UNEVENTFUL AT Apr 22, 2026 · N182FE · Boeing 7673S2F · Leading Edge Slat Control SystemSDR FDEA202510292110Strap · crackedDETACHED STRAP, WING RH REAR SPAR SLAT 9 REAR SPAR SLAT 9 RH WING WAS REPAIRED IAW B767 SRM 57-43-02-2R REPAIR 1 FIG 201 SHEET 2 DETAIL III NOTES B AND D AND B767 SRM 51-70-10-2R REPAIR 4 FIG 201 REV 93 APR 15 2025Oct 29, 2025 · N182FE · Boeing 7673S2F · Leading Edge DevicesSDR FDEA202510292109Skin · wornWEAR ON PREVIOUS REWORK OF OUTBOARD SLAT NO 5 TRAILING EDGE WEDGE AT OSS 420.71 APPROX LOWER SURFACE. LEFT WING LH WING OUTBOARD SLAT NO 5 T/E WEDGE LOWER SURFACE AT OSS 420.71 APPROX. WAS REPAIRED IAW B767 SRM 57-43-02-2R REPAIR 1 FIG 201 DETAIL III NOTEOct 29, 2025 · N182FE · Boeing 7673S2F · Leading Edge DevicesSDR FDEA202510292108Skin · puncturedPUNCTURE ON UPPER SURFACE AT 6 INCH INBD SIDE OF THE OUTBD AILERON RH WING RH WING OUTBD AILERON UPPER SURFACE AT 6 INCH OF INBD SIDE WAS REPAIRED IAW B767 SRM 57-60-02-2R REP 1 FIG 201 SHEET 2 AND B767 SRM 51-70-17-0G PAR 4B FIG 24 SHEET 1 REV 93 AUG 15/2Oct 29, 2025 · N182FE · Boeing 7673S2F · AileronsSDR FDEA202510292107Wedge · wornWEAR SKIN OF TRAILING EDGE WEDGE ON OUTBOARD SLAT NO 4 AT OSS 649.24 AND OSS 639.73 LOWER SURFACE, LEFT WING. SLAT SKIN OF T/E AT OUTBD SLAT NO 4 AT OSS 649.24 LWR SURFACE LH WING WAS REPAIRED IAW SRM B767 57-43-02-2R REPAIR 1 FIG 201 (SHEET2) DETAIL III NOct 29, 2025 · N182FE · Boeing 7673S2F · Leading Edge DevicesSDR FDEA202510212061Skin · dentedDENT RH WING, LOWER SURFACE OF OUTBOARD FLAP, 36.5" OUTBOARD EDGE AND 19" TRAILING EDGE DENT RH WING, LOWER SURFACE OF OUTBOARD FLAP, 36.5'' OUTBOARD EDGE AND 19'' TRAILING EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R AND SRM 57-70-10-2R REPAIR 4 FIG 201 SHOct 21, 2025 · N182FE · Boeing 7673S2F · Trailing Edge FlapsSDR FDEA202510212060Floor Panel · crackedPUNCTURE ON FLOOR PANEL 242LFA MDC. FLOOR PANEL 242LFA MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15, 2025Oct 21, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202510212059Floor Panel · dentedSEVERAL DENTS AND DISBOND AT FWD EDGE OF FLOOR PANEL 241WFF FLOOR PANEL 241WFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15, 2025Oct 21, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202510212058Floor Panel · crackedCRACK AND PUNCTURES ON SKIN OF FLOOR PANEL 242SFF MAIN CARGO COMPARTMENT. FLOOR PANEL 242SFF, MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15, 2025Oct 21, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202510172048Floor Panel · brokenBROKEN MAIN DECK PANEL 241ZFF. THE FLOOR PANEL 241ZFF WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, SHEET 2, REV 92.Oct 17, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202510172046Floor Panel · crackedBROKEN MAIN DECK FLOOR PANEL 241JFF. THE FLOOR PANEL 241JFF WAS REPAIRED IAW SRM 53-00-50-2R, PARA 4-B, FIG 201, SHEET 2. REV 92.Oct 17, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202510172045Floor Panel · brokenBROKEN MAIN DECK FLOOR PANEL 241DFF. THE FLOOR PANEL 241DFF WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, SHEET 2, REV 92.Oct 17, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202510172044Floor Panel · damagedMAIN CARGO BAY FLOOR PANEL 242EFF CRACKED AND PUNCTURED. REPAIRED IAW SRM 53-00-50-2R, PARA 4-B, FIG 201, SHEET 2, REV 92.Oct 17, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202510172041Floor Panel · crackedCRACK ON SKIN OF FLOOR PANEL 242TFA, MAIN CARGO COMPARTMENT FLOOR PANEL 242TFA, MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15,2025Oct 17, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202510172040Floor Panel · crackedBROKEN MAIN DECK PANEL 241AGF MAIN DECK PANEL 241AGF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR15,2025Oct 17, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202510172039Floor Panel · crackedBROKEN AT AFT EDGE OF FLOOR PANEL 241YFA FLOOR PANEL 241YFA WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15,2025Oct 17, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202510142004Floor Panel · puncturedPUNCTURE (2) ON FLOOR PANEL 252HFF. MDC FLOOR PANEL 252HFF MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 92 APR 15,2025Oct 14, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202510142003Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 251EFF. MDC FLOOR PANEL 251EFF. MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 92 APR 15,2025Oct 14, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202510142002Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231DFF. SEC 43 OF MDC FLOOR PANEL 231DFF SEC 43 OF MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4 B FIG 201, SHEET 2 REV 92 APR 15,2025Oct 14, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202510142001Floor Panel · crackedPUNCTURE ON FLOOR PANEL 241ZFF. MDC FLOOR PANEL 241ZFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15,2025Oct 14, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202510142000Floor Panel · crackedPUNCTURE ON FLOOR PANEL 231LFF. SEC 43 OF MDC FLOOR PANEL 231LFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15 2025Oct 14, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202510141999Floor Panel · crackedPUNCTURE ON FLOOR PANEL 232MFF. SEC 43 OF MDC FLOOR PANEL 232MFF SEC 43 OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15,2025Oct 14, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202510141998Floor Panel · crackedPUNCTURE ON FLOOR PANEL 231RFF. SEC 43 OF MDC FLOOR PANEL 231RFF SEC 43 OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15 2025Oct 14, 2025 · N182FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202306271123Former · crackedR/W L/E FORMER CRACKED STA OSS 499 0000237172 : LAFFOND, MARK P - 27-JUN-2023 19:21 REMOVED AND INSTALLED NEW FORMER A R/H L/E OSS 499. REF SR 67-57-002 REV F. (MPN: B67-57-002-12)Jun 27, 2023 · N182FE · Boeing 767300 · Wing Miscellaneous StructureSDR FDEA202306271122Former · crackedR/W L/E FORMER CRACKED STA OSS 437 CORRECTION, STA OSS 565 INSTEAD OF STA OSS 437 0000358872 : FERGUSON, STEVE M - 27-JUN-2023 19:18 REMOVED AND INSTALLED NEW FORMER ON RIGHT WING FIXED LEADING EDGE AT OSS 565 REF SR67-57-002 REV F (MPN: B67-57-002-06)Jun 27, 2023 · N182FE · Boeing 767300 · Wing Miscellaneous StructureSDR FDEA202306271121Former · crackedR/W L/E FORMER CRACKED STA OSS 441 0000245521 : EDWARDS, WILLIAM B - 27-JUN-2023 19:14 REMOVED AND REPLACED PANEL 621ANB FOR FORMER ACCESS REF B767 AMM 57-41-57-4. REMOVED AND REPLACED R/W L/E FORMER AT STA 441, REF FEDEX DRAWING SR67-57-002, SHEET 3. (MPN:Jun 27, 2023 · N182FE · Boeing 767300 · Wing Miscellaneous StructureSDR FDEA202208282095Former · crackedRIGHT WING HAS CRACKED FORMER UNDER #8 SLAT NEAR FLE OSS 441. MWT. REPLACED DAMAGED FORMER ON R/W L/E STA OSS-441.596, REF W/O 83954, SEQ 161 FOR E.A. TH-5720-T0370335 P1 FOR DETAILS.Aug 28, 2022 · N182FE · Boeing 7673S2F · Wing Main, Frame StructureSDR FDEA202111022762Slat · wornSLAT #8 WITH WEAR BEHIND WEDGE AREA NEAR TO OSS 441. SLAT #8 ON WEDGE AREA NEAR TO OSS 441 WAS REPAIRED I.A.W. SRM 57-43-02-2R FIG. 101 PAGE 1-2 SHEET 1-2 AND SRM 51-70-10-2R REPAIR 4 PAGE 9,10,82,149,162 FIG. 202 SHEET 8 REV. 81 AUG 15/2021Nov 2, 2021 · N182FE · Boeing 767300 · Wing, Control SurfacesSDR FDEA202111022761Slat · crackedLH WING SLAT NO. 5 WS 433.1 TRAILING EDGE WEDGE WITH NICK. LH WING SLAT #5 T.E. WEDGE AT POSITION OSS 427.5 - 439.5 UPPER AND LOWER SKIN WERE REPAIRED I.A.W. SRM 57-43-02-2R PAG. 1-2 FIG.201 REP. 1 AND SRM 51-70-10-2R PAG. 149, 159, 162,163 FIG. 202 REV. Nov 2, 2021 · N182FE · Boeing 767300 · Wing, Control SurfacesSDR FDEA202111022759Slat · crackedLH WING SLAT 5, OSS 488.8 TRAILING EDGE WITH CRACK. LH WING SLAT #5 T.E. WEDGE AT POSITION OSS 485.3-490.3 UPPER AND LOWER SKIN WERE REPAIRED I.A.W. SRM 57-43-02-2R REP. 1 PAG. 1,2 FIG. 201 AND SRM 51-70-10-2R REP. 4 PAG. 149, 159, 162, 163 FIG. 202 REV.8Nov 2, 2021 · N182FE · Boeing 767300 · Wing, Control SurfacesSDR FDEA202008181921Escape Rope · deployedON-LOAD CREW FOUND L1 DOOR EMERGENCY ESCAPE ROPE DEPLOYED. SECURED THE DEPLOYED L1 DOOR ESCAPE ROPE IAW AMM 25-61-04-2-1. ACFT OK FOR SERVICE AT THIS TIME. ACFT OK FOR SERVICE AT THIS TIME.Aug 18, 2020 · N182FE · Boeing 7673S2F · Emergency EquipmentSDR FDEA202006171259Flap System · malfunctionedPDIS 182 27-80 0467 16JUN20 MEM OPEN U. DURING LANDING CONFIGURATION GOT LEADING EDGE SLAT DISAGREE. RAN QRH AND LANDED FLAPS 20 VREF 30. SUSPECT FLAP HANDLE WAS NOT IN FLAP 25 DETENT TO CAUSE INITIAL LEADING EDGE DISAGREE WARNING. WORKED PERFORMED IN CONJJun 17, 2020 · N182FE · Boeing 7673S2F · Leading Edge Slat Control SystemSDR FDEA2020061971259Warning Message · illuminatedDURING LANDING CONFIGURATION, RECEIVED A LE SLAT DISAGREE. RAN QRH AND LANDED FLAPS 20 . SUSPECT FLAP HANDLE WAS NOT IN FLAP 25 DETENT TO CAUSE INITIAL LE DISAGREE WARNING.Jun 17, 2020 · N182FE · Boeing 7673S2F · Leading Edge Slat Control SystemSDR FDEA2020012190167Unknown · noiseAIR TURN BACK. DURING CLIMB ( 14000-16000) A LOUD BANGING SOUND STARTED. WE WERE AT ( 280-290 KTS). SLOWED SOUND STOPPED. AROUND 250 KTS FO'S WINDSHIELD WIPER WAS VIBRATING OPERATED WINDSHIELD WIPERS IAW AMM 30-42-00-5. WINDSHIELD WIPERS OPERATED NORMAJan 19, 2020 · N182FE · Boeing 7673S2F · Standard Practices/Structures
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