# Service difficulty reports: N126FE A list on [N126FE](https://openairdocs.org/aircraft/N126FE.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR FDEA202507241313](https://openairdocs.org/sdr/FDEA202507241313.md): Floor Panel · cracked · Jul 24, 2025 · N126FE · Boeing 7673S2F · Fuselage Floor Panel > CRACK ON FLOOR PANEL 251EFF AT MDC SEC 46 FLOOR PANEL 251EFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15/2025 - [SDR FDEA202507231305](https://openairdocs.org/sdr/FDEA202507231305.md): Floor Panel · cracked · Jul 23, 2025 · N126FE · Boeing 7673S2F · Fuselage Floor Panel > CRACK ON PREVIOUS REPAIR OF FLOOR PANEL 251CFF AT MDC SEC 46 FLOOR PANEL 251CFF MDC SEC 46 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15/2025 - [SDR FDEA202507231303](https://openairdocs.org/sdr/FDEA202507231303.md): Floor Panel · cracked · Jul 23, 2025 · N126FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURE ON FLOOR PANEL 251DFF AT MDC SEC 46. FLOOR PANEL 251DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15/2025 - [SDR FDEA202507231301](https://openairdocs.org/sdr/FDEA202507231301.md): Floor Panel · cracked · Jul 23, 2025 · N126FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURE ON FLOOR PANEL 232DFF AT MDC SECTION 43 FLOOR PANEL 232DFF MDC SECTION 43 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15/2025 - [SDR FDEA202507231300](https://openairdocs.org/sdr/FDEA202507231300.md): Floor Panel · cracked · Jul 23, 2025 · N126FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURE ON FLOOR PANEL 251KFF AT MDC SEC 46. FLOOR PANEL 251KFF MDC SEC 46 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15/2025 - [SDR FDEA202507231299](https://openairdocs.org/sdr/FDEA202507231299.md): Floor Panel · cracked · Jul 23, 2025 · N126FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURE ON FLOOR PANEL 251PFF AT MDC SEC 46. FLOOR PANEL 251PFF MDC SEC 46 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15/2025 - [SDR FDEA202507221292](https://openairdocs.org/sdr/FDEA202507221292.md): Floor Panel · cracked · Jul 22, 2025 · N126FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURES ON ACCESS PANEL 221EFF SECTION 41 OF MDC FLOOR PANEL 221EFF MDC SECTION 41 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 92 APR 15/2025 - [SDR FDEA202507211285](https://openairdocs.org/sdr/FDEA202507211285.md): Floor Panel · cracked · Jul 21, 2025 · N126FE · Boeing 7673S2F · Fuselage Floor Panel > CRACK ON FLOOR PANEL 241DFF AT MDC SEC 45 FLOOR PANEL 241DFF MDC SEC 45 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15, 2025. - [SDR FDEA202507211284](https://openairdocs.org/sdr/FDEA202507211284.md): Floor Panel · cracked · Jul 21, 2025 · N126FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURE ON FLOOR PANEL 241KFF AT MDC SEC 45 FLOOR PANEL 241KFF MDC SEC 45 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15, 2025 - [SDR FDEA202507211283](https://openairdocs.org/sdr/FDEA202507211283.md): Floor Panel · cracked · Jul 21, 2025 · N126FE · Boeing 7673S2F · Fuselage Floor Panel > DENT WITH CRACK ON FLOOR PANEL 252DFF AT MDC SEC 46 FLOOR PANEL 252DFF MDC SEC 46 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15, 2025 - [SDR FDEA202507211282](https://openairdocs.org/sdr/FDEA202507211282.md): Floor Panel · cracked · Jul 21, 2025 · N126FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURE ON FLOOR PANEL 241ZFF AT MDC SEC 45 FLOOR PANEL 241ZFF MDC SEC 45 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15, 2025 - [SDR FDEA202507171230](https://openairdocs.org/sdr/FDEA202507171230.md): Skin · dented · Jul 17, 2025 · N126FE · Boeing 7673S2F · Trailing Edge Flaps > ONE DENT IN SURFACE INNERSIDE LOWER SKIN INSIDE CORNER OF INBOARD AFT FLAP OF INBOARD FLAP RIGHT WING. RT WING, INBD T/E FLAP LOWER SURFACE, DENT WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 201 (SHEET 4) DETAIL III AND SRM 51-70-03-0G PAR 5L FIGURE 16 REV 9 - [SDR FDEA202505120751](https://openairdocs.org/sdr/FDEA202505120751.md): Pitot Head · obstructed · May 12, 2025 · N126FE · Boeing 7673S2F · Pitot/Static System > DURING CLIMB AT ABOUT 20K, JUST AFTER PASSING THRU SOME CLOUDS, RECEIVED ALT DISAGREE ADVISORY EICAS. CONSULTED QRH AND DETERMINED FO ALTIMETER WAS THE ISSUE AT APPROX 300 HIGHER THAN CA. SWITCHED FO FLIGHT INSTRUMENTS TO ALTN AIR DATA AND EICAS MESSAGE E - [SDR FDEA202408051083](https://openairdocs.org/sdr/FDEA202408051083.md): Floorboard · delaminated · Aug 5, 2024 · N126FE · Boeing 7673S2F · Fuselage Floor Panel > NR #7 READ "FLOORBOARD DAMAGED BETWEEN STATIONS 1100-1197". INSPECTED NOT ACCEPTED. MAIN DECK FLOORBOARD REPAIR MISCLASSIFIED AS MINOR REPAIR. RII BUYBACK FOR MAJOR REPAIR MISSED ON SHIFT REF GMM 6-1-800. FABRICATED NEW FLOORBOARD (251AFF) (MPN: 146T5869-8 - [SDR FDEA202408051082](https://openairdocs.org/sdr/FDEA202408051082.md): Seat Track · damaged · Aug 5, 2024 · N126FE · Boeing 7673S2F · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK LOBE DAMAGED AT APPROXIMATELY STA.500 RBL 11. REMOVED AND INSTALLED SEAT TRACK, REPAIR ANGLES (2EACH) AND REPAIR STRAP (1EACH) PER FDX E.A. H-5310-T0380146 AND SRM 53-00-52-2R REPAIR 9. - [SDR FDEA202403210330](https://openairdocs.org/sdr/FDEA202403210330.md): Outlet · inoperative · Mar 21, 2024 · N126FE · Boeing 7673S2F · AC Power Distribution System > EFB POWER OUTLET ON THE FO SIDE WAS NOT PROVIDING 110V AC POWER. WHEN THE F/O PLUGGED INTO THE 110V AC POWER OUTLET WE SMELLED ELECTRICAL SMOKE, SO HE UNPLUGGED HIS IPAD AND THE SMELL DISSIPATED. CONNECTED EFB TO POWER OUTLET COULD NOT SMELL ANY ELECTRICAL - [SDR FDEA202311231887](https://openairdocs.org/sdr/FDEA202311231887.md): Orifice · failed · Nov 23, 2023 · N126FE · Boeing 767300 · Doors > THE DOOR TO THE CRM IS EXTREMELY HARD TO OPEN - THE CRM IS HOLDING TOO MUCH PRESSURE. DID NOTICE THE EYEBALL VENT DOES NOT EMIT MUCH AIR - SUSPECT MAYBE THE CRM IS NOT VENTING CORRECTLY. WE ARE PUSHING THE BLACK RELIEF BUTTON AND CAN HEAR IT RELIEVING PRE - [SDR FDEA202307271320](https://openairdocs.org/sdr/FDEA202307271320.md): Slat · gouged · Jul 27, 2023 · N126FE · Boeing 767300 · Leading Edge Slat Control System > RW #8 SLAT LOWER T/E SURFACE AFT OF I/B AUX TRACK GUIDE ARM IS GOUGED REPAIRED RW #8 SLAT LOWER T/E SURFACE AFT OF I/B AUX TRACK GUIDE ARM IAW B767 SRM 57- 43-02-2R AND 51-70-10-2R - [SDR FDEA202307271319](https://openairdocs.org/sdr/FDEA202307271319.md): Aileron · damaged · Jul 27, 2023 · N126FE · Boeing 767300 · Ailerons > LEFT WING I/B AILERON I/B L/E ATTACH FAIRING HAS EXPOSED COMPOSITE MATERIAL COMPLETED PERMANENT REPAIR TO L/H WING AILERON I/B L/E ATTACH FAIRING IAW B767 SRM 51-70-05-0G AND 57-60-01. - [SDR FDEA202307271318](https://openairdocs.org/sdr/FDEA202307271318.md): Bracket · cracked · Jul 27, 2023 · N126FE · Boeing 767300 · Wing Miscellaneous Structure > LW INBD L/E AT LES 289 SLAT TORQUE TUBE GUIDE BRACKET IS CRACKED IN SEVERAL PLACES REMOVED AND REPLACED GUIDE BRACKET IAW BOEING DRAWING 114T1240, SHEET 6, REV - - [SDR FDEA202307251291](https://openairdocs.org/sdr/FDEA202307251291.md): Beam · cracked · Jul 25, 2023 · N126FE · Boeing 767300 · Nacelle/Pylon, Main Frame > #2 PYLON, O/B WING DOOR ATTACH ANGLE IS CRACKED REPARED #2 PYLON, OUTBOARD LATCHBEAM IAW EA# H-5450-T0375415-P1, RELEASED AUG 01, 2023, - [SDR FDEA202307241331](https://openairdocs.org/sdr/FDEA202307241331.md): Unknown · unknown · Jul 24, 2023 · N126FE · Boeing 767300 · Rudder Structure > RUDDER TIP HAS WEAR ON UPPER LEADING EDGE. PERFORMED PERMANENT REPAIR OF RUDDER TIP UPPER LEADING EDGE IAW FDX B767-300 SRM 55-40-30-2R, FDX B767-300 SRM 55-40-30-2R, FDX B767 SRM 51-70-17-0G, AND FDX B767 SRM 51-70-14-0G. NO FURTHER ACTION REQUIRED. - [SDR FDEA202307201255](https://openairdocs.org/sdr/FDEA202307201255.md): Bracket · cracked · Jul 20, 2023 · N126FE · Boeing 767300 · Wing Miscellaneous Structure > R/H WING I/B FIXED L/E SLAT TORQUES TUBE GUIDE BRACKET CRACKED AT THE FASTENER HOLES APPROX LES 285. REMOVED AND REPLACED TORQUE TUBE GUIDE BRACKET IAW BAC DWG 114T1240, SHEET 6, REV -. - [SDR FDEA202302210329](https://openairdocs.org/sdr/FDEA202302210329.md): Control Lever · failed · Feb 21, 2023 · N126FE · Boeing 767300 · Landing Gear Retraction/Extension System > WHEN LANDING GEAR LEVER PLACE TO OFF DURING AFTER TAKE OFF CHECK FROM MMMY THE RIGHT MAIN AND NOSE GEAR EXTENDED WITH GREEN LIGHTS ON. LEFT MAIN STAYED UP. DOORS AND GEAR ANNUNCIATORS AND GEAR DISAGREE EICAS WERE ON. ALL GEAR RETRACTED AND DOORS CLOSED WH - [SDR FDEA202210292694](https://openairdocs.org/sdr/FDEA202210292694.md): Idg · faulted · Oct 29, 2022 · N126FE · Boeing 7673S2F · AC Generator-Alternator > BEGINNING T/O ROLL ON RWY 18L AT MEM, RECEIVED R GEN DRIVE EICAS T/O REJECTED AT 7 KTS GROUND SPEED. EXITED RUNWAY. RAN QRH, DIRECTED RIGHT GEN DRIVE DISCONNECT, APU STARTED, REJECTED LANDING CHECKLIST ACCOMPLISHED AND AFTER LANDING CHECKLIST. RETURNED T - [SDR FDEA202209252369](https://openairdocs.org/sdr/FDEA202209252369.md): Former · cracked · Sep 25, 2022 · N126FE · Boeing 7673S2F · Wing Main, Frame Structure > CRACK ON NOSE FORMER OSS 441.596 L/H SIDE. REPLACED L/H LEADING EDGE FORMER AT STA OSS441 IAW E.A. H-5720-T0370796 PART1 - [SDR FDEA202209252368](https://openairdocs.org/sdr/FDEA202209252368.md): Former · cracked · Sep 25, 2022 · N126FE · Boeing 7673S2F · Wing Main, Frame Structure > R/H LEADING EDGE FORMER CRACKED AT OSS 441 REPLACED R/H LEADING EDGE FORMER AT STA OSS-441 IAW E.A. H-5720-T0370795 PART1 - [SDR FDEA202204120941](https://openairdocs.org/sdr/FDEA202204120941.md): Former · cracked · Apr 12, 2022 · N126FE · Boeing 7673S2F · Wing Miscellaneous Structure > R/H WING L/E AT STA OSS-441 HAS LOOSE RIVETS AND A CRACKED FORMER P/N 114T2170-6 0000452710: ROSNER, DANIEL D - 13-APR-2022 02:58 COMPLIED WITH E.A WORK CARD TH-5720-T0367964 P1. SEQ NO 000150 - [SDR FDEA202204120940](https://openairdocs.org/sdr/FDEA202204120940.md): Former · cracked · Apr 12, 2022 · N126FE · Boeing 7673S2F · Wing Miscellaneous Structure > L/H WING L/E AT STA OSS565 HAS LOOSE RIVETS AND A CRACKED FORMER P/N 114T2512-13 0000355851: MITROVICH, DAVID T - 13-APR-2022 02:39 C/W EA T H-5720-T0367965 P1, SEQ:151, W/O:82517, WRI:5720-6343. - [SDR FDEA202204120938](https://openairdocs.org/sdr/FDEA202204120938.md): Former · cracked · Apr 12, 2022 · N126FE · Boeing 7673S2F · Wing Miscellaneous Structure > L/H WING L/E AT STA OSS441 HAS LOOSE RIVETS AND A CRACKED FORMER P/N 114T2170-5 0000553921: DAVIES, ANDREW M - 13-APR-2022 00:38 REPLACED LOOSE FASTENERS AND REPLACED CRACKED FORMER PER E.A,#:H-5720-T0367963 P1 - [SDR FDEA202204120937](https://openairdocs.org/sdr/FDEA202204120937.md): Rivet · loose · Apr 12, 2022 · N126FE · Boeing 7673S2F · Wing Miscellaneous Structure > R/H WING L/E AT STA OSS-565 HAS LOOSE RIVETS 0000301922: VERNON, JAMES L - 12-APR-2022 22:36 REPLACED FASTENERS REF E.A. TH-5729-T0367962, PAGE 3 OF 3, W/O 82517, SEQ.# 148 AND WRI 57- 20/6340 - [SDR FDEA202204120936](https://openairdocs.org/sdr/FDEA202204120936.md): Rivet · loose · Apr 12, 2022 · N126FE · Boeing 7673S2F · Wing Miscellaneous Structure > R/H WING L/E AT STA OSS-499 HAS LOOSE RIVETS 0000301922: VERNON, JAMES L - 12-APR-2022 22:33 REPLACED FASTENERS REF E.A. TH-5720-T0367962 P2, PAGE 3 OF 3, SEQ. # 148, W/O 82517, WRI 57- 20/6340 - [SDR FDEA202204120935](https://openairdocs.org/sdr/FDEA202204120935.md): Rivet · loose · Apr 12, 2022 · N126FE · Boeing 7673S2F · Wing Main, Frame Structure > L/H WING L/E AT STA OSS499 HAS LOOSE RIVETS. REPLACED LOOSE RIVETS WITH SCREWS. REF. E.A. H-5720-T0367962 P1. - [SDR FDEA202204120934](https://openairdocs.org/sdr/FDEA202204120934.md): Rivet · loose · Apr 12, 2022 · N126FE · Boeing 7673S2F · Wing Miscellaneous Structure > R/H WING L/E AT STA OSS-437 HAS LOOSE RIVETS 0000301922: VERNON, JAMES L - 12-APR-2022 22:27 REPLACED FASTENERS REF E.A. TH-5720-T0367962 P2, PAGE 3 OF 3, SEQ. #148, W/O 82517 AND WRI 57- 20/6340 - [SDR FDEA202202210933](https://openairdocs.org/sdr/FDEA202202210933.md): Rivet · loose · Feb 21, 2022 · N126FE · Boeing 7673S2F · Fuselage Structure (General) > LOOSE RIVETS INSTALLED SCREWS - [SDR FDEA202012143155](https://openairdocs.org/sdr/FDEA202012143155.md): Switch · out of tolerance · Dec 14, 2020 · N126FE · Boeing 7673S2F · Door Warning System > AT FL380 EICAS MAIN CARGO DOOR ILLUMINATED FOLLOWED QRH PROCEDURES & LANDED. LIGHT EXTINGUISHED PASSING 16,000 IN DECENT. NO CABIN DEPRESSURIZATION OR NOISE FROM CARGO DOOR. ON BOARDING ACFT FOUND BOTH DOOR LATCHED AND DOOR LOCKED INDICATIONS SHOWING GR - [SDR FDEA2020072311601](https://openairdocs.org/sdr/FDEA2020072311601.md): Skin · dented · Jul 21, 2020 · N126FE · Boeing 7673S2F · Trailing Edge Flaps > LEFT WING INBOARD FLAP DENTED OUTBOARD END. REPAIRED THE LT WING INBD FLAP IAW EA H-5750-T0355223-P1. - [SDR FDEA2020072301592](https://openairdocs.org/sdr/FDEA2020072301592.md): Floorboard · delaminated · Jul 20, 2020 · N126FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CABIN FLOORBOARD 241TFF WAS DELAMINATED ON BOTTOM FLOOR PANEL SKIN. FABRICATED NEW FLOORBOARD IAW SRZ 25-005 - [SDR FDEA2020072301591](https://openairdocs.org/sdr/FDEA2020072301591.md): Floorboard · delaminated · Jul 20, 2020 · N126FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 242QFF HAS DELAM ON BOTTOM FLOOR SKIN. FAB'D NEW FLOORBOARD 242QFF IAW FED EX SRZ-25-005 - [SDR FDEA2020072301589](https://openairdocs.org/sdr/FDEA2020072301589.md): Floor Panel · delaminated · Jul 20, 2020 · N126FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 242UFF HAD BROKEN INSERTS. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005, REV R. - [SDR FDEA202004230774](https://openairdocs.org/sdr/FDEA202004230774.md): Switch · out of adjust · Apr 23, 2020 · N126FE · Boeing 7673S2F · Door Warning System > ON CLIMBOUT APPROACHING LEVEL OFF ALTITUDE (PASSING FL 330) EICAS MAIN CARGO DOOR DISPLAYED. PRESSURIZATION WAS NORMAL, DIFFERENTIAL PRESSURE WAS SHOWING APPROX. 8.3 PSID WHEN EICAS DISPLAYED. COMPLIED WITH QRH & DESCENDED TO 10,000'. MAIN CARGO EICAS NO - [SDR FDEA201904100780](https://openairdocs.org/sdr/FDEA201904100780.md): Tire · failed · Apr 10, 2019 · N126FE · Boeing 7673S2F · Tire > PDIS 126 32-41 3425 09APR19 MEM SUSPECT NOSE TIRE FAILURE DURING TAXI OUT AT NORMAL TAXI SPEED ON STRAIGHT AWAY. FACT 09APR19 19:13 MEM AMM: 32-45-02-4 - FOUND BOTH NOSE TIRES ROLLED OFF WHEELS - REMOVED BOTH NOSE WHEEL ASSY. - INSPED AX - [SDR FDEA201811243366](https://openairdocs.org/sdr/FDEA201811243366.md): Latch · out of position · Nov 24, 2018 · N126FE · Boeing 7673S2F · Emergency Equipment > CAPT'S SIDE ESCAPE ROPE COVER WILL NOT STAY LATCHED CLOSED. REPOSITIONED LATCH 10C80-2 ON PANEL ASSY TO ENSURE ESCAPE ROPE COVER DOOR WILL LATCH CLOSED. REF DRAWING B67-25-014 AND EA H-2560-T0343723. - [SDR FDEA201810032774](https://openairdocs.org/sdr/FDEA201810032774.md): Bushing · worn · Oct 3, 2018 · N126FE · Boeing 7673S2F · Nacelle/Pylon Miscellaneous Structure > NR 2 ENGINE INBOARD AFT FAIRING STRUT SKIRT BEAM AFT HINGE BUSHING AND LUG WORN. INSTALLED REPAIR BUSHINGS AT WORN HINGE LOCATION ON NR 2 ENGINE INBD AFT FAIRING PANEL 447 BL PER SRM 54-52-70-2R. - [SDR FDEA2018091082422](https://openairdocs.org/sdr/FDEA2018091082422.md): Adapter · leaking · Sep 8, 2018 · N126FE · Boeing 7673S2F · AC Generator-Alternator > RIGHT GEN DRIVE EICAS CAME ON RESULTED IN A REJECTED TAKE OFF AT 40 KTS. INSPECTED THE RIGHT IDG AND OIL SYSTEM, NO LEAKAGE WAS FOUND. DRAINED AND SERVICED THE RIGHT IDG PER AMM 12-13-03-3. REMOVED & REPLACED THE IDG SCAVENGE FILTER PER AMM 24-11-02-2, NO DEBR - [SDR FDEA201711203282](https://openairdocs.org/sdr/FDEA201711203282.md): Unknown · odor · Nov 20, 2017 · N126FE · Boeing 7673S2F · Air Distribution System > BURNED RUBBER ODOR IN THE COCKPIT DURING TAXI. ODOR WENT AWAY AND CAME BACK ON POWER RUN UP FOR TAKEOFF. RAN BOTH ENGINES UP TO HIGH POWER AND APU IAW JRH. RAN WITH PACKS ON/OFF, ENGINE ANTI-ICE ON/OFF, CARGO HEAT ON/OFF. UNABLE TO DUPLICATE AT ANY POWE - [SDR FDEA201704171226](https://openairdocs.org/sdr/FDEA201704171226.md): Unknown · odor · Apr 17, 2017 · N126FE · Boeing 7673S2F · Air Distribution System > DURING DESCENT, WITH THROTTLES AT IDLE PASSING 16,000', CREW NOTICED FAINT ODOR OF BURNING TIRES. NO VISIBLE SMOKE OBSERVED BY CREW DURING FLIGHT. ODOR LESSENED UNTIL ON FINAL APPROACH AND THEN GREW SLIGHTLY STRONGER. NO OTHER UNUSUAL INDICATIONS OBSERVED. NO - [SDR FDEA201601200212](https://openairdocs.org/sdr/FDEA201601200212.md): Valve · disconnected · Jan 20, 2016 · N126FE · Boeing 7673S2F · Cabin Cooling System > AT APPROX 4000' WE HEARD AN ABNORMAL NOISE FOLLOWED BY A RUMBLE OF AIRFLOW FROM LOWER EQUIP COMPARTMENT. RECEIVED A FWD EQUIPMENT VALVE, EICAS. RAN ALL QRH PROLS. AND RECEIVED A, CABIN PRESSURE, EICAS & FOLLOWED QRH PROLS. DIVERTED. FOUND FWD EQUIP COOLIN - [SDR FDEA201601190205](https://openairdocs.org/sdr/FDEA201601190205.md): Connector · disconnected · Jan 19, 2016 · N126FE · Boeing 7673S2F · Air Conditioning System Wiring > AT APPROX 4000' WE HEARD AN ABNORMAL NOISE FOLLOWED BY A RUMBLE OF AIRFLOW FROM LOWER EQUIP COMPARTMENT. WE THEN GOT A, FWD EQPT VAL, EICAS. RAN ALL QRH PROLS. THEN GOT A CABIN PRESS EICAS & FOLLOWED QRH PROLS. MADE DECISION TO DIVERT. FOUND FWD EQUIP COO ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N126FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N126FE/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.