N130FE

Service difficulty reports · 32

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 = 'N130FE' 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 FDEA202603060324Skin · dentedDENT ON LOWER SURFACE OF LT OTBD FLAP, LOCATED AT 39.5" FROM INBOARD EDGE AND 2.5" FROM AFT EDGE. LT OTBD FLAP LOWER SURFACE WAS REPAIRED IAW SRM 57-53-01-2R, REPAIR 1, FIG 201, SHEET 6, & SRM 51-70-17-0G, PAR 4A, FIG 10, SHEET 1, REV 94.Mar 6, 2026 · N130FE · Boeing 7673S2F · Trailing Edge FlapsSDR FDEA202603010302Wedge · wornWEAR IN WEDGE TRAILING EDGE LOWER SURFACE AT 33.75 INCHES OF INBD END ON SLAT NR 4, LT WING. WEAR IN WEDGE T/E LOWER SURFACE AT 33.75 INCHES OF INBD EDGE WAS REPAIRED IAW SRM 51-70-10-2R, REP 4, FIG 202, REV 94 & SRM 57-43-02-2R, FIG 201, REP 1, SHEET 1, REV Mar 1, 2026 · N130FE · Boeing 7673S2F · Leading Edge DevicesSDR FDEA202603010301Wedge · wornWEAR IN WEDGE TRAILING EDGE LOWER SURFACE AT 30" OF INBD END ON SLAT NR 5, LT WING. LT WING, SLAT NR 5 TRAILING EDGE WEDGE LOWER SURFACE AT 30" OF INBD END EDGE WAS REPAIRED IAW SRM 51-70-10-2R, REP 4, FIG 202, SHEET B, REV 94 AND SRM 57-43-02-2R, FIG 201, REMar 1, 2026 · N130FE · Boeing 7673S2F · Leading Edge DevicesSDR FDEA202602240277Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231NFF MDC FLOOR PANEL 231NFF MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 93.Feb 24, 2026 · N130FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202602240276Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231QFF MDC FLOOR PANEL 231QFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 93.Feb 24, 2026 · N130FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202602240275Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 251QFF MDC FLOOR PANEL 251QFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 93.Feb 24, 2026 · N130FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202602230270Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 241LFF MDC FLOOR PANEL 241LFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 93 AUG 15/2025Feb 23, 2026 · N130FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202602230269Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 251DFF MDC FLOOR PANEL 251DFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 93 AUG 15/2025Feb 23, 2026 · N130FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202506271070Bulb · inoperativeUPON SELECTING GEAR DOWN HAD NO GREEN LIGHT FOR NOSE GEAR. RAN QRH & DETERMINED IT WAS BULB & REPLACED BULBS. NORMAL GEAR EXTENSION THEREAFTER. NORMAL INDICATIONS. CHECKED NOSE GEAR GREEN LIGHTS FOR PROPER INSTALLATION AS PER AMM 33-13-00-2. FOUND SATISJun 27, 2025 · N130FE · Boeing 7673S2F · Landing Gear Position and WarningSDR FDEA202406170810Bulb · failedON APPROACH, AT GEAR EXTENSION, THE RT MLG DID NOT INDICATE SAFE (NO GREEN LIGHTS). THERE WAS NO EICAS OR GEAR DISAGREE LIGHT. BULBS TESTED GOOD. AFTER RETRACTING MLG ON GO AROUND & EXTENDING IT FOR SUBSEQUENT APPROACH, MLG EXTENDED NORMALLY. IAW CREW REPORT,Jun 17, 2024 · N130FE · Boeing 7673S2F · Landing Gear Position and WarningSDR FDEA202403080263Support Angle · cracked[UPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, LBL 78, "I" BEAM REINFORCE "L" ANGLE ON OUTBOARD SIDE OF "I" BEAM IS CRACKED., 2024-03-08] REMOVED AND REPLACED ANGLE P/Mar 8, 2024 · N130FE · Boeing 7673S2F · Fuselage Miscellaneous StructureSDR FDEA202403050249Angle · crackedMAIN CARGO DECK, AT STA. 1582 LBL 78, HAS ANGLE BRACKET (P/N 146T5651-5) CRACKED REMOVED AND REPLACE ANGLE BRACKET P/N 146T5651-5 PER BOEING DWG 146T5651 AND SRM 51-40-02-0GMar 5, 2024 · N130FE · Boeing 7673S2F · Fuselage Main, StructureSDR FDEA202402260266Support Beam · crackedUPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, RBL 78, "I" BEAM REINFORCE "L" ANGLE ON OUTBOARD SIDE OF "I" BEAM IS CRACKED. REMOVED AND REPLACED ANGLE BRACKET REF 767 DFeb 26, 2024 · N130FE · Boeing 7673S2F · Fuselage Miscellaneous StructureSDR FDEA202402260265Support Beam · crackedUPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, LBL 78, "I" BEAM REINFORCE "L" ANGLE ON OUTBOARD SIDE OF "I" BEAM IS CRACKED. REMOVED AND REPLACED ANGLE P/N 146T5651-7 PERFeb 26, 2024 · N130FE · Boeing 7673S2F · Fuselage Miscellaneous StructureSDR FDEA202402260243Support Angle · crackedUPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, RBL 78, "I" BEAM REINFORCE "L" ANGLE ON OUTBOARD SIDE OF "I" BEAM IS CRACKED. 0000191391 : LINTON, LOREN E - 04-MAR-2024 03Feb 26, 2024 · N130FE · Boeing 7673S2F · Fuselage Miscellaneous StructureSDR FDEA202402250258Bracket · crackedLH WING L/E BRACKET CRACKED, VIEWED INSIDE LIGHTNING HOLE AT APPROX WING STATION 510 (BETWEEN #5 SLAT OUTBD SIDE AND #5 SLAT OUTBD AUX TRACK). MARKED WITH ORANGE DOT MK1. BRACKET P/N 114T2800-165. REPAIRED PER EA H-5720-T0378377 BFeb 25, 2024 · N130FE · Boeing 7673S2F · Wing, Attach FittingsSDR FDEA202402250257Bracket · crackedRH WING L/E BRACKET CRACKED, VIEWED INSIDE LIGHTNING HOLE AT APPROX WING STATION 510 (BETWEEN #8 SLAT OUTBD SIDE AND #8 SLAT OUTBD AUX TRACK). MARKED WITH ORANGE DOT MK2. BRACKET P/N 114T2800-165. 0000730634 : NGUYEN,QUYNH Q - 07-MAR-2024 19:17 REMOVED AND Feb 25, 2024 · N130FE · Boeing 7673S2F · Wing, Attach FittingsSDR FDEA202402250241Shear Tie · cracked#2 PYLON AFT TORQUE BOX BULKHEAD INBOARD SHEAR TIE CRACKED. REMOVE AND REPLACED SHEAR TIE (313T3310-1155) USING 767 SRM REFERENCE 51-40-02-0G AND IPC 54-51-53-13C ALONG WITH BOEING DRW 313T3310-1155 & 313T3310 SH 91.Feb 25, 2024 · N130FE · Boeing 7673S2F · Nacelle/Pylon, Main FrameSDR FDEA202402220267Support Beam · crackedUPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, RBL 78, "I" BEAM REINFORCE "L" ANGLES ON BOTH SIDES ARE CRACKED. REMOVED AND REPLACED "L" ANGLES AT RBL 78 BETWEEN STA 1564Feb 22, 2024 · N130FE · Boeing 7673S2F · Fuselage Miscellaneous StructureSDR FDEA202402220264Support Angle · crackedUPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, RBL 78, "I" BEAM REINFORCE "L" ANGLES ON BOTH SIDES ARE CRACKED. 0000239190 : BASTIN, WILLIAM D - 08-MAR-2024 20:33 REMOVEFeb 22, 2024 · N130FE · Boeing 7673S2F · Fuselage Miscellaneous StructureSDR FDEA202308111397Former · failedNOSE FORMER ANGLE AT OSS 499.6 ON THE LEFT WING FIXED LEADING EDGE IS CRACKED. REMOVED THE BROKEN NOSE FORMER ANGLE AT OSS 499.6 ON THE LEFT WING FIXED LEADING EDGE. INSTALLED A 114T251U13 ANGLE. FEDEX DRAWING B67-57-002.Aug 11, 2023 · N130FE · Boeing 767300 · Wing Main, Frame StructureSDR FDEA202011132839Skin · gougedNR 2 ENGINE INBOARD CORE COWL INNER SIDE NR 2 FRAME FROM FWD END IS GOUGED. REPAIRED NR 2 ENGINE INBOARD CORE COWL NR 2 FRAME, IAW B767 SRM 54-45-01-2R REPAIR 3.Nov 13, 2020 · N130FE · Boeing 7673S2F · Nacelle/Pylon, Plate/SkinSDR FDEA202011112827Beam · damagedNR 2 PYLON INBOARD LATCH BEAM MISSING NUTPLATE. REMOVED NR 2 PYLON INBOARD LATCH BEAM, IAW B767 SRM 54-52-71-2R. REPAIRED LATCH BEAM, IAW B767-SRM 54-52-71-2R. REINSTALLED NR 2 PYLON INBOARD LATCH BEAM, IAW B767 SRM 54-52-71-2R.Nov 11, 2020 · N130FE · Boeing 7673S2F · Nacelle/Pylon, Main FrameSDR FDEA202011052783Bracket · crackedRIGHT WING NR 7 SLAT DRIVESHAFT LOOP BRACKET CRACKED, STREAMER ATTACHED. REMOVED AND REPLACED LOOP BRACKET, PER B767 SRM 51-40-02 AND BOEING DWG 114T1240 REV E.Nov 5, 2020 · N130FE · Boeing 7673S2F · Wing Miscellaneous StructureSDR FDEA202011052782Bracket · crackedLEFT WING LES 284 SLAT DRIVESHAFT LOOP BRACKET CRACKED, STREAMER ATTACHED. REMOVED AND REPLACED LOOP BRACKET, PER B767 SRM 51-40-02 AND BOEING DWG 114T1240 REV E.Nov 5, 2020 · N130FE · Boeing 7673S2F · Wing Miscellaneous StructureSDR FDEA202007291700Flap System · malfunctionedON APPROACH, SELECTED FLAPS 1 TO FLAPS 5. RECEIVED TE FLAP ASYMMETRY EICAS MSG & TRAILING EDGE LIGHT. COMPLETED THE QRH, TE FLAP ASYMMETRY CHECK LIST & USED ALTERNATE FLAPS, SETTING 20 DEGREES FOR LANDING. 'EMERGENCY DECLARED. ALL SWITCHES BACK TO NORMAL. Jul 29, 2020 · N130FE · Boeing 767300 · Trailing Edge Flap Control SystemSDR FDEA2020080329699Warning Message · false activationON APPROACH, AT 7000 FT, 210KTS, SELECTED FLAPS 1 TO FLAPS 5. RECEIVED TE FLAP ASYMMETRY EICAS MESSAGE AND TRAILING EDGE LIGHT. COMPLETED THE QRH TRAILING EDGE FLAP ASYMMETRY CHECK LIST AND USED ALTERNATE FLAPS, SETTING 20 DEGREES FOR LANDING. EMERGENCY Jul 29, 2020 · N130FE · Boeing 7673S2F · Trailing Edge Flap Control SystemSDR FDEA2020073091699Flap System · malfunctionedDURING APPROACH, SELECTED FLAPS 1 TO FLAPS 5. RECEIVED TE FLAP ASYMMETRY EICAS MESSAGE AND TRAILING EDGE LIGHT. COMPLETED THE QRH, T/E FLAP ASYMMETRY CHECK LIST AND USED ALTERNATE FLAPS, SETTING 20 DEGREES FOR LANDING. EMERGENCY DECLARED. CREW STATED TE FLJul 29, 2020 · N130FE · Boeing 7673S2F · Trailing Edge Flap Control SystemSDR FDEA2020060111104Motor · failedLEVEL AT FL340 GOT A CABIN ALT WARNING. CABIN ALTITUDE WAS JUST ABOVE 10,00 FT. STARTED AN EMERGENCY DESCENT. WHILE IN DESCENT GOT CABIN ALT AUTO 1 INOPERATIVE MESSAGE. SWITCH TO AUTO 2 CONTROLLER AND CABIN ALTITUDE RETURNED TO NORMAL. BITE NR 1 CPC FOUNDMay 31, 2020 · N130FE · Boeing 7673S2F · Cabin Pressure Control SystemSDR FDEA2020042730778Warning System · false activationTE FLAP DISAGREE LANDING MOVING FROM 1 TO 5 OPERATED FLAPS IN ALTN, NO FAULTS NO DISAGREE. OPERATED FLAPS NORAMLLY WITH ALL CENTER PUMPS ON (WITH ACMP ON) NO FAULTS NO DISAGREE. CHECKED FLAP POS. MODULES FOR FAULTS NO FAULTS IAW AMM 27-58-01. PERFORMED BITApr 23, 2020 · N130FE · Boeing 7673S2F · Trailing Flap Position Indicating SystemSDR FDEA201901120103Eva System · inoperativeWHILE C\W EA H-2560-E0324416 FOUND PILOTS(L\H) EVAS LIGHTS INOP\UNSEEABLE. REMOVED AND REPLACED CAPT EVAS, OPS CHECK GOOD. NOMENCLATURE - EMERGENCY VISION ASSURANCE SYSTEM ,Jan 12, 2019 · N130FE · Boeing 7673S2F · Emergency EquipmentSDR FDEA201901110093Light · inoperativePDIS 130 33-50 2856 11JAN19 BWI FACT U LOGPAGES:3045527 EMERG LIGHTS DISARM LIGHT ON OVERHEAD PANEL INOP. MEL 11JAN19 13:09 BWI U RELEASED FOR SERVICE PER MEL : 33-51-02 CATEGORY : B EXPIRATION : 14JAN19 "MEL 33-51-02: EXTERIOR EMERGENCY LIGHTS - INOP. FLIGHTJan 11, 2019 · N130FE · Boeing 7673S2F · Flight Compartment Lighting
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