N129FE
Service difficulty reports · 55
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 = 'N129FE' 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 = 'N129FE' 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 FDEA202512012216Power Supply · failedEMERGENCY LIGHTS INOP ON WALK AROUND. IAW AMM 33-51-07-2 REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY IAW 33-51-07-2-0, CHECKED GOOD FOR SECURITY AND OPS IAW AMM 33-51-07-2.SDR FDEA202509051632Skin · dentedA DENT ON EXTERNAL SKIN OF VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR AT FSS 28 AND B. STA 1643 APROX (LH SIDE). VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR AT FSS 28 AND B. STA 1643 APROX (LH SIDE) WAS REPAIRED IAW B767 SRM 55-30-01-2R FIG 201 SDR FDEA202509041619Floor Panel · crackedFLOOR PANEL HAS A SMALL GOUGE IN TOP OF FLOOR PANEL FLOOR PANEL 222CFF LOCATED AT STATION 347.00 WAS REPAIRED IAW SRM 53-00-50-2R PAR 4B, FIG 201, SHEET 2, REV. 92, APR 15, 2025SDR FDEA202509041618Floor Panel · crackedBROKEN PANEL 241ZFF, UPPER CARGO COMPT FLOOR PANEL 241ZFF UPPER CARGO COMPARTMENT WAS REPAIRED I.A.W. B767 SRM 53-00-50-2R PARAGRAPH 4G (2) REV 92 APR 15, 2025SDR FDEA202509041617Floor Panel · crackedBROKEN FLOOR PANEL 241MFF, UPPER CARGO COMPT FLOOR PANEL 241MFF UPPER CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PARAGRAPH 4G (2) REV 92 APR 15, 2025.SDR FDEA202509021611Floor Panel · damagedBROKEN PANEL 241LFF, UPPER CARGO COMPT. FLOOR PANEL 241LFF, UPPER CARGO COMPT. WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 92 APR. 15, 2025.SDR FDEA202509011598Floor Panel · delaminatedDISBONDED CORNER AT FLOOR PANEL 242SFF, MDCC. FLOOR PANEL 242SFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B FIG. 201 DETAIL I REV. 92 APR. 15, 2025.SDR FDEA202509011597Floor Panel · damagedBROKEN COMPOSITE LAYER AT FWD CORNER OF FLOOR PANEL 242UFF, 2" X 2.5" APROX. FLOOR PANEL 242UFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B FIG. 201 DETAIL I REV. 92 APR. 15, 2025.SDR FDEA202509011596Floor Panel · delaminatedDISBONDED CORNER AT FLOOR PANEL 242UFF, MDCC. FLOOR PANEL 242UFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B FIG. 201 DETAIL I REV. 92 APR. 15, 2025.SDR FDEA202509011595Floor Panel · damagedBROKEN UPPER COMPOSITE LAYERS. FLOOR PANEL 241QFF. UPPER COMPOSITE LAYERS OF FLOOR PANEL 241QFF WERE REPAIRED IAW B767 SRM 53-00-50- 2R PAR. 4.B FIG. 201 SHEET 2 REV. 92 APR. 15, 2025.SDR FDEA202509011593Floor Panel · dentedSEVERAL DENTS ON FLOOR PANEL 212CFF OF CONTROL CABIN. FLOOR PANEL 212CFF OF CONTROL CABIN WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 92 APR 15, 2025SDR FDEA202509011591Floor Panel · delaminatedDISBONDED CORNER AT FLOOR PANEL 242JFF, MDCC. FLOOR PANEL 242JFF, MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4.B FIG. 201 SHEET 2 REV. 92 APR 15, 2025SDR FDEA202509011588Floor Panel · damagedSEVERAL PUNCTURES ON FLOOR PANEL 242UFF LOWER SURFACE, MDCC. FLOOR PANEL 242UFF LOWER SURFACE AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B FIG 201 SHEET 2 REV. 92 APR 15, 2025SDR FDEA202509011587Floor Panel · dentedSEVERAL DENTS AT EDGES OF LOWER SURFACE OF FLOOR PANEL 241YFA. EDGES OF LOWER SURFACE OF FLOOR PANEL 241YFA WERE REPAIRED IAW B767 SRM 53-00-50- 2R PAR. 4.B FIG. 201 SHEET 2 REV. 92 APR. 15, 2025.SDR FDEA202508291578Skin · dentedDENT INNER PART OF INBOARD FLAP WING RH INBOARD FLAP, INNER PART, WING RH WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1, FIG. 201, SHEET 1-6, TABLE I REV.92 APR 15/2025SDR FDEA202508291577Floor Panel · damagedEXPOSED FIBERS ON FLOOR PANEL 242KFF, MDCC. EXPOSED FIBERS ON FLOOR PANEL 242KFF WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. 92 APR 15,2025SDR FDEA202508291576Floor Panel · crackedSEVERAL PUNCTURES AT FLOOR PANEL 241AGF SEVERAL PUNCTURES AT FLOOR PANEL 241AGF WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV.92 APR 15,2025SDR FDEA202508291575Floor Panel · brokenBROKEN PANEL 241PFF, UPPER CARGO COMPT BROKEN PANEL 241PFF, UPPER CARGO COMPT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 REV. 92 APR 15,2025SDR FDEA202508291574Floor Panel · dentedDENT ON FLOOR PANEL 242VFF UPPER SURFACE MDCC DENT ON FLOOR PANEL 242VFF UPPER SURFACE, MDCC WAS REPAIRED IAW B767 SRM 53-00-50- 2R PAR 4-B FIG 201 SHEET 2 REV.92 APR 15,2025SDR FDEA202508291573Floor Panel · dentedSEVERAL DENTS ON FLOOR PANEL 222CFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT FLOOR PANEL 222CFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4B FIG 201 SHEET 2 REV92 APR 15,2025SDR FDEA202508291572Floor Panel · dentedSEVERAL DENTS ON FLOOR PANEL 221 CFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT FLOOR PANEL 221CFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV.92 APR15,2025SDR FDEA202508291571Floor Panel · dentedSEVERAL DENTS ON FLOOR PANEL 221 CFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT FLOOR PANEL 221CFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV.92 APR15,2025SDR FDEA202508291570Floor Panel · dentedSEVERAL DENTS ON FLOOR PANEL 221DFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT FLOOR PANEL 221DFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4 B FIG 201 SHEET 2 REV. 92 APR 15,2025SDR FDEA202508291569Floor Panel · dentedSEVERAL DENTS ON FLOOR PANEL 222AFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT FLOOR PANEL 222AFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4.B FIG. 201 SHEET 2 REV 92 APR 15,2025SDR FDEA202508291568Floor Panel · dentedSEVERAL DENTS ON FLOOR PANEL 222BFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT FLOOR PANEL 222BFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4.B FIG. 201 SHEET 2 REV 92 APR 15,2025SDR FDEA202508281560Skin · dentedDENT ON LOWER SURFACE OF OUTBOARD FLAP, AT 70" FROM OUTBOARD EDGE AND 8" FROM TRAILING EDGE, LH WING. LOWER SURFACE OF OUTBOARD FLAP, AT 70" FROM OUTBOARD EDGE AND 8" FROM TRAILING EDGE, LH WING WAS REPAIRED IAW B767 SRM 53-53-01-2R REPAIR 1, FIG. 201, SHESDR FDEA202310201780Flap · dentedR/H WING INBD FLAP TRAILING EDGE LOWER SURFACE DENTS REMOVED , REPAIRED AND REINSTALLED R/H WING INBD FLAP IAW FEDEX EA# : H-5750-T0376594SDR FDEA202310171771Angle · crackedAREA AFT OF THE BULK CARGO COMPARTMENT R/H SIDE MAIN CABIN FLOOR SUPPORT STRUCTURE HAS 2EA SPLICE ANGLES CRACKED BETWEEN STA 1562 & 1582, RBL 70 REMOVED AND REPLACED 2EA MAIN DECK CANTILEVER SUPPORT ANGLES (146T5651-6 & 146T5651-8) IAW BAC DWG 146T5650 REVSDR FDEA202310171770Angle · crackedAREA AFT OF THE BULK CARGO COMPARTMENT L/H SIDE MAIN CABIN FLOOR SUPPORT STRUCTURE HAS 2EA SPLICE ANGLES CRACKED BETWEEN STA 1562 & 1582, LBL 70 REMOVED AND REPLACED 2EA MAIN DECK CANTILEVER SUPPORT ANGLES (146T5651-5 & 146T5651-7) IAW BAC DWG 146T5650 REVSDR FDEA202310161768Frame · cracked#1 PYLON: NACELLE STA 329, MID-SPAR FRAME IS CRACKED AT THE INBOARD, UPPER CORNER REPAIRED #1 PYLON, NAC STA 329 FRAME IAW FEDEX EA # H-5450-T0376579-P1, RELEASED OCT 10, 2023, TITLED "NACELLES/PYLON - WING PYLON/STRUT - #1 PYLON NAC STA 329 FAIRING FRAME,SDR FDEA202310061748Skin · crackedRH ELEVATOR CTR PCA CUTOUT HAS A SMALL CRACK AND DELAMINATION REPAIRED RH ELEVATOR CENTER PCA CUTOUT CRACK AND DELAMINATION IAW FED EX EA H- 5520-T0376560-P1-STABLIZERS-ELEVATORS-RH OUTBD ELEVATOR, LOWER SKIN, ELEV STA 175 EDGE TRIM REPAIR, B767 SRM 55-20-0SDR FDEA202010172546Bracket · crackedNR 1 PYLON OUTBOARD FWD END OF PANEL 437BL BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON THE NR 1 PYLON FWD END OF PANEL 437BL, PER B DWG 313T3310.SDR FDEA202010172545Bracket · crackedHYDRAULIC DRAIN TUBE BRACKET IS CRACKED ON NR 1 OUTBOARD PYLON. REMOVED AND REPLACED DRAIN TUBE BRACKET, PER B767 SRM 51-40-02 AND BOEING DWG 313T2380 REV E.SDR FDEA202010172543Former · crackedLEFT WING LEADING EDGE, NR 5 SLAT OUTBOARD ACTUATOR ROD APPROXIMATELY LES 489 HAS CRACKED FORMER. REMOVED AND REPLPACED FORMER AT NR 5 SLAT OUTBOARD ACTUATOR ROD CUTOUT P/N 114T2511-13, PER B DWG 114T2511 REV D EA H-5720-T0357392-P1. TITLE: WINGS-SECONDARY WSDR FDEA202010172542Angle · crackedLEFT WING LEADING EDGE, NR 5 SLAT OUTBOARD ACTUATOR ROD APPROXIMATELY LES 489 HAS CRACKED ANGLE. REMOVED AND REPLACED ANGLE AT APPROXIMATELY LES 489, PER EA H-5720-T0357358-P1. TITLE: WING-SECONDARY WING STRCT-LT WING, OSS 499, LEADING EDGE RIB ANGLE, ALTERNSDR FDEA202010172541Angle · crackedRIGHT WING NR 8 SLAT, INBOARD GUIDE ARM, FORMER CRACKED. REMOVED AND REPLACED FORMER AT NR 8 SLAT INBOARD GUIDE ARM CUTOUT, PER B DWG 114T2241, EA4-5720-T0357420-P1. TITLED: WINGS-SECONDARY WING STRCT-RT WING, LEADING EDGE, ANGLE, OSS 441, ALT FASTENERS.SDR FDEA202010172540Skin · chafedLEFT WING, INBOARD FLAP, LOWER SURFACE, ABOVE NR 6 TIRE, PREVIOUS REPAIR GOUGED, CIRCLED. REMOVED DAMAGED ROCKSHIELD. REPAIRED IAW EA H-2750-T0357370, B767 SRM 51-70-17-0G. RESTORED FINISH, IAW B767 AMM 51-24-02 B767 SRM 51-70-17-0G PARA 3H/EA H-2750-T03573SDR FDEA202010152522Latch · chafedNR 2 ENGINE T/R HINGE LATCH PANEL FWD EDGE GOUGED AND HAS BARE METAL. REPAIRED NR 2 FWD LATCH PANEL, IAW STEA CMM 78-32-09 REPAIR 5.SDR FDEA202010152521Latch · chafedNR 1 INBOARD FWD T/R LATCH PANEL, FWD LIP WORN AND CHAFED 2 PLACES. REPAIRED NR 1 FWD LATCH PANEL, IAW STEA CMM 78-32-09 REPAIR 5.SDR FDEA202010152520Former · crackedRIGHT WING, NR 8 SLAT, OUTBOARD ROTARY ACTUATOR ARM CUTOUT, FORMER IS CRACKED. REMOVED AND REPLACED NOSE FORMER, IAW BOEING DWG 114T2161 REV E AND FEDEX EA H-5720-T0357395 P1. TITLED: WINGS-SECONDARY WING STRCT-RT WING, LEADING EDGE, ANGLE, OSS 499, ALTERNATSDR FDEA202010152519Skin · gougedNR 2 ENGINE CORE COWLING LT LOWER SURFACE IS GOUGED. ACCOMPLISHED REPAIR OF NR 2 ENGINE CORE COWLING LT, IAW ROHR SRM 54-40-00 REPAIR 2.SDR FDEA202010132479Angle · crackedLEFT WING FUEL PANEL 521QB HINGE ANGLE CRACKED IN CENTER AREA. REPAIRED LEADING EDGE AT FUEL PANEL 521QB HINGE, IAW B767 SRM 57-41-13-2R REPAIR 3.SDR FDEA202010132478Skin · gougedRIGHT HORIZONTAL STABILIZER FIXED LOWER SKIN GOUGED. REPAIRED DAMAGE, IAW B767 SRM 55-10-01-2R FIG 201 AND SRM 51-70-10-2R REPAIR 4 FIG 201.SDR FDEA202010122465Bracket · crackedLT WING INBOARD LEADING EDGE AREA TORQUE TUBE GUIDE BRACKET IS CRACKED AT THE LOWER AFT FASTENER HOLE. REMOVED AND REPLACED TORQUE TUBE GUIDE BRACKET, IAW B767 SRM 51-40-02 AND BOEING DWG 114T1240 REV E.SDR FDEA202010122464Seal · crackedLEFT WING APPROXIMATELY LES 506, STRAP IS CRACKEDAT FASTENER HOLE. REMOVED AND REPLACED LT WING APPROXIMATELY LES 506 STRAP, IAW BAC DWG 114T2800.SDR FDEA202010102458Angle · crackedNR 1 PYLON AFT OUTBOARD ANGLE CLIP CRACKED. REMOVED AND REPLACED ANGLE CLIP, PER B767 SRM 51-40-02 AND BOEING DWG 313T3380 REV N.SDR FDEA202010102457Angle · crackedNR 2 ENG PYLON AFT A-FRAME IN BOARD CLIP CRACKED. REMOVED AND REPLACED CLIP, IAW B767 SRM 51-40-02 AND BOEING DWG 313T3380 REV N.SDR FDEA2020072301436Warning Message · false activationAT LEVEL 360 MAIN CARGO DOOR EICAS MESSAGE , NO VIBRATION, NO PRESSURIZATION ISSUES. MESSAGE EXTINGUISHED DESCENDING THRU 16000FT. OPENED DOOR PANEL EXPOSING S891 SENSOR OBSERVED A CLOSED DOOR, GAP OF 0.050 ANDLCR METER 6.7MH WITH LIMITS. VISUALLY INSPECTESDR FDEA2020070631436Warning System · false activationLEVEL 360 MAIN CARGO DOOE EICAS MESSAGE, NO VIBRATION, NO PRESSURIZATION ISSUES. MESSAGE EXTINGUISHED DESCENDING THRU 16000.SDR FDEA2018122193545Switch · brokenPDIS 129 33-40 2768 19DEC18 IND OPEN U LOGPAGES:3055686 AN ACRID ODOR WAS SENSED THREE TIMES. WE BELIEVE THE ODOR COICIDES WITH TURNING ON THE RUNWAY TURNOFF LIGHTS. FACT 20DEC18 12:23 IND
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