# Service difficulty reports: N923FD

A list on [N923FD](https://openairdocs.org/aircraft/N923FD.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 142 reports

- [SDR FDEA202610201625](https://openairdocs.org/sdr/FDEA202610201625.md): Stringer · abnormal · Oct 20, 2026 · N923FD · Boeing 757204 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY LOWER FRAME AT BS 1560, FOUND PREVIOUS REPAIR ON STR 26R.
- [SDR FDEA202610201624](https://openairdocs.org/sdr/FDEA202610201624.md): Structure · corroded · Oct 20, 2026 · N923FD · Boeing 757204 · Nacelle/Pylon, Main Frame
  > NR 2 ENGINE PYLON STRUT, OTBD LOWER STRUCTURE NAC S 146.675 FOUND CORRODED.
- [SDR FDEA202610191606](https://openairdocs.org/sdr/FDEA202610191606.md): Skin · corroded · Oct 19, 2026 · N923FD · Boeing 757204 · Nacelle/Pylon, Plate/Skin
  > NR 1ENGINE PYLON OUTB SIDE INTERNAL STRUCTURE SIDE SKIN CORRODED (PP STA 144.55 APROX.)
- [SDR FDEA202610151595](https://openairdocs.org/sdr/FDEA202610151595.md): Strut · corroded · Oct 15, 2026 · N923FD · Boeing 757204 · Nacelle/Pylon, Main Frame
  > ENG #2 PYLON STRUT INBD LOWER CHORD STA 144.425 CORROSION. THIS DISCREPANCY WAS ACCOMPLISHED ON EA # F-5430-T0389069 P1 TITLE: NACELLES / PYLONS-SKIN / PLATES / PANELS - CORROSION BLENDOUT #2 PYLON, LHS (INBD) SIDE SKIN DOUBLER INNER SURFACE, PP STA 153-16
- [SDR FDEA202610121558](https://openairdocs.org/sdr/FDEA202610121558.md): Frame · corroded · Oct 12, 2026 · N923FD · Boeing 757204 · Horizontal Stabilizer, Spar/Rib
  > RH ELEVATOR CONDUCTIVE FRAME MULTIPLE ZONES WITH CORROSION (UPPER AND LOWER) EVALUATED CONDUCTIVE FRAME RH ELEVATOR UPPER/LOWER HORIZONTAL STABILIZER AND REPLACED CONDUCTIVE SPLICE PLATE (02EA) AND SHIMS (02EA) UPPER/LOWER IAW B757 SRM 51-40-02-0G, SRM 55-
- [SDR FDEA202610121557](https://openairdocs.org/sdr/FDEA202610121557.md): Frame · corroded · Oct 12, 2026 · N923FD · Boeing 757204 · Elevator, Spar/Rib
  > LEFT ELEVATOR CONDUCTIVE FRAME MULTIPLE ZONES WITH CORROSION (UPPER AND LOWER) EVALUATED CONDUCTIVE FRAME LH ELEVATOR UPPER/LOWER HORIZONTAL STABILIZER AND REPLACED CONDUCTIVE SPLICE PLATE (02EA) AND SHIMS (02EA) UPPER/LOWER IAW B757 SRM 51-40-02-0G, SRM 5
- [SDR FDEA202610071490](https://openairdocs.org/sdr/FDEA202610071490.md): Seat Track · damaged · Oct 7, 2026 · N923FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BETWEEN BS 1080-1180, LBL 45.5. REMOVED AND REPLACED THE SEAT TRACK SECTION IAW SRM 51-40-02-OG, & DWG 144N5021, REV C.
- [SDR FDEA202610071489](https://openairdocs.org/sdr/FDEA202610071489.md): Seat Track · corroded · Oct 7, 2026 · N923FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BETWEEN STA 1140 TO STA 1160 RBL 45.50 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK SECTION ON MAIN CABIN FROM BS 1080 - 1180, RBL 45.5 IAW SRM 51-40-02-OG, & DWG 144N5021, REV C.
- [SDR FDEA202610071488](https://openairdocs.org/sdr/FDEA202610071488.md): Seat Track · corroded · Oct 7, 2026 · N923FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BETWEEN BS 1180 - 1200, RBL 45.50 WAS CORRODED. REMOVED AND REPLACED SEAT TRACK SECTION ON MAIN CABIN FROM BS 1180 - 1280, RBL 45.50 IAW SRM 51-40-02-OG, & DWG 146N5130 REV C.
- [SDR FDEA202605220627](https://openairdocs.org/sdr/FDEA202605220627.md): Girt Bar · out of adjust · May 22, 2026 · N923FD · Boeing 757204 · Emergency Equipment
  > LH ENTRY DOOR WILL NOT ARM. PERFORMED ADJUSTMENT OF L1 DOOR GIRT BAR. ARMED AND DISARMED L1 SLIDE MULTIPLE TIMES WITH GOOD INDICATION. DOOR ARMS AND DISARMS SMOOTHLY WITH NO BINDS. MEL CLEARED AND PLACARD REMOVED. A/C OK FOR SERVICE.
- [SDR FDEA202604040400](https://openairdocs.org/sdr/FDEA202604040400.md): Bottle · empty · Apr 4, 2026 · N923FD · Boeing 757204 · Passenger/Crew Doors
  > DURING MX PRE-FLIGHT, NOTICED THAT R1 DOOR EMERGENCY POWER RESEVOIR BOTTLE IS DEPLETED, READS 0 PSI. REMOVED AND REPLACED EMERGENCY POWER RESERVOIR FOR THE R1 DOOR W/REF TO B757 MM 52-11-30-4. ACFT OK TO CONTINUE.
- [SDR FDEA202603020305](https://openairdocs.org/sdr/FDEA202603020305.md): Battery Pack · inoperative · Mar 2, 2026 · N923FD · Boeing 757204 · Emergency Lighting
  > EMERGENCY LIGHTS AT DOOR L1 INOPERATIVE. REPLACED DOOR L1 EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51-07-2. OPS CHECKED GOOD.
- [SDR FDEA202602110174](https://openairdocs.org/sdr/FDEA202602110174.md): Bulb · dim · Feb 11, 2026 · N923FD · Boeing 757204 · Emergency Lighting
  > DURING MX PRE-FLIGHT FOUND R1 EMERGENCY EXIT SIGN DIM. REMOVED AND REPLACED 5 FAULTY BULBS AT THE R1 EMERGENCY EXIT SIGN IAW AMM 33-51-01-2. OPS CHECK GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA202602110173](https://openairdocs.org/sdr/FDEA202602110173.md): Bulb · inoperative · Feb 11, 2026 · N923FD · Boeing 757204 · Emergency Lighting
  > DURING PRE-FLIGHT CHECK, FOUND CENTER OVERHEAD EMERGENCY EXIT IDENTIFIER SIGN DIM. AMM 33-51-01-2 FOUND CENTER OVERHEAD EMERGENCY EXIT SIGN HAS 14 FAULTY BULBS. REMOVED AND REPLACED 14 FAULTY BULBS AS PER ABOVE REF. OPS CHECK GOOD.
- [SDR FDEA202602110172](https://openairdocs.org/sdr/FDEA202602110172.md): Bulb · inoperative · Feb 11, 2026 · N923FD · Boeing 757204 · Emergency Lighting
  > DURING PRE-FLIGHT FOUND L1 OVERHEAD EMERGENCY EXIT SIGN SLIGHTLY DIM. AMM 33-51-01-2 FOUND L1 OVERHEAD EMERGENCY EXIT SIGN HAS 5 FAULTY BULBS. REMOVED AND REPLACED 5 FAULTY BULBS AS PER ABOVE REF. OPS CHECKED GOOD.
- [SDR FDEA202508281564](https://openairdocs.org/sdr/FDEA202508281564.md): Outflow Valve · failed · Aug 28, 2025 · N923FD · Boeing 757204 · Pressure Regulator/Outflow Valve
  > DECLARED EMERGENCY DIVERTED TO IND. MECHS PERFORMED GVI OF PACK BAYS AND COMPONENTS. OUTFLOW VALVE CLEAR OF ANY DEBRIS, RAN LT PACK FOR LEAKS AND NO LEAKS DETECTED. WILL PROCEED WITH 757 AMM 21-51-00-5, PARG.10. SINGLE PACK PRESSURIZATION CONFIDENCE CHK
- [SDR FDEA202508271550](https://openairdocs.org/sdr/FDEA202508271550.md): Controller · inoperative · Aug 27, 2025 · N923FD · Boeing 757204 · Central Warning
  > AT FL350 RIGHT ENG BLEED EICAS FLICKERED THEN CABIN ALT HI DISCRETE LIGHT & EICAS ILLUM. CABIN RATE SHOWED A CLIMB OF 500-750 FT PER MIN & A CABIN ALT OF 12,000. DONNED O2 MASK. DESCENDED TO 10,000 FT. CABIN ALT INOP LIGHT ALSO ILLUM. DECLARED AN EMERGENCY.
- [SDR FDEA202410281596](https://openairdocs.org/sdr/FDEA202410281596.md): Skin · cracked · Oct 28, 2024 · N923FD · Boeing 757204 · Fuselage Main, Plate/Skin
  > FREIGHT ULD HIT AIRCRAFT AND CREATED A HOLE ON R/H OF A/C AFT OF AFT CARGO DOOR UPDT 25OCT24 08:28 EWR SRM 53-00-00-0G DAMAGE FOUND AROUND STATION 1608 (SECTION 46). DAMAGE DIMENSIONS ARE 10 FROM FWD TO AFT AND 9 FROM TOP TO BOTTOM WHILE BEING 2 1/
- [SDR FDEA202304140648](https://openairdocs.org/sdr/FDEA202304140648.md): Lamp · burned · Apr 14, 2023 · N923FD · Boeing 757200 · Emergency Lighting
  > DURING SERVICE CHECK, FOUND R1 DOOR AND FLIGHT DECK DOOR OVERHEAD EMERGENCY LIGHTS SIGN (QTY:2) INOPERATIVE. RELEASED FOR SERVICE PER MEL: 33-51-01-01 CATEGORY: D EXPIRATION: 12AUG23 "MEL 33-51-01-01: INTERIOR EMERGENCY LIGHTS - INOP."MEL: 33-51-01-01
- [SDR FDEA202301040198](https://openairdocs.org/sdr/FDEA202301040198.md): Seat Track · corroded · Jan 4, 2023 · N923FD · Boeing 757* · Fuselage Structure (General)
  > FOUND CRACK AND CORROSION ON SEAT TRACK BETWEEN STA 520 TO 560 AT LBL 45 ACCOMPLISHED REPAIR IAW FEDEX EA F-5310-T0372559 P1 TITLED: FUSELAGE- MAINFRAME-SEC 43, STA 520-560 AND LBL 45.5 SEAT TRACK UPPER FLANGE- CORROSION- REPAIR MAJOR REPAIR
- [SDR FDEA202301040191](https://openairdocs.org/sdr/FDEA202301040191.md): Seat Track · corroded · Jan 4, 2023 · N923FD · Boeing 757* · Fuselage Structure (General)
  > FOUND CORROSION ON SEAT TRACK BETWEEN STA 350 TO 365 RBL 14 REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02 AND INSTALLED NRE FX 3504-3 SEAT TRACK IAW SRM 51-40-02 MAJOR REPAIR
- [SDR FDEA202301040190](https://openairdocs.org/sdr/FDEA202301040190.md): Seat Track · corroded · Jan 4, 2023 · N923FD · Boeing 757* · Fuselage Structure (General)
  > FOUND CORROSION ON SEAT TRACK BETWEEN STA 350 TO 365 LBL 7 REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02 INSTALLED NEW FX3504-3 IAW SRM 51-40-02 MAJOR REPAIR
- [SDR FDEA202301040188](https://openairdocs.org/sdr/FDEA202301040188.md): Seat Track · corroded · Jan 4, 2023 · N923FD · Boeing 757* · Fuselage Structure (General)
  > FOUND CORROSION ON SEAT TRACK BETWEEN STA 840 TO 860 AT RBL 45 REMOVED SEAT TRACK IAW SRM 51-40-02 ACCOMPLISHED REPAIR IAW SRM 53-00-52-2R, FIG. 201, REPAIR 1 MAJOR REPAIR
- [SDR FDEA202301040187](https://openairdocs.org/sdr/FDEA202301040187.md): Not Entered · not entered · Jan 4, 2023 · N923FD · Boeing 757* · Fuselage Structure (General)
  > FOUND CORROSION ON INBD CREASE BEAM BETWEEN STA 860-880 LBL 64 REMOVED DAMAGED CREASE BEAM IAW SRM 51-40-02 ACCOMPLISHED REPAIR IAW FEDEX EA F-5310-T0372515 P1: FUSELAGE MAINFRAME: SEC 43, FLOOR STRUCTURE CREASE BEAM INNER CHORD, STA 860-880 LBL64. MAJO
- [SDR FDEA202301040184](https://openairdocs.org/sdr/FDEA202301040184.md): Seat Track · corroded · Jan 4, 2023 · N923FD · Boeing 757* · Fuselage Structure (General)
  > FOUND CORROSION ON SEAT TRACK BETWEEN STA 560 TO 600 AT RBL 45 REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02 PERFORMED SETA TRACK REPAIR IAW SRM 53-00-52 REPAIR 1 MAJOR REPAIR
- [SDR FDEA202301040182](https://openairdocs.org/sdr/FDEA202301040182.md): Crease Beam · corroded · Jan 4, 2023 · N923FD · Boeing 757* · Fuselage Structure (General)
  > FOUND CORROSION ON INBD CREASE BEAM BETWEEN STA 860 TO 880 AT RBL 64 ACCOMPLISHED REPAIR IAW FEDEX EA F-5310-T0372513 P1 FUSELAGE- MAINFRAME: SEC 43, FLOOR STRUCTURE, CREASE BEAM INNER CHORD, STA 860-880, RBL 64, PERMANENT REPAIR. MAJOR REPAIR
- [SDR FDEA202301010199](https://openairdocs.org/sdr/FDEA202301010199.md): Splice · corroded · Jan 1, 2023 · N923FD · Boeing 757* · Fuselage Structure (General)
  > FOUND CORROSION ON AFT CARGO INNER SKIN SPLICE STRAP AT STA 1400 ADJACENT TO STRG 27L ACCOMPLISHED REPAIR IAW FEDEX EA F-5310-T0372415 P1 TITLED: FUSELAGE-MAINFRAME- STA 1400 BUTT SPLICE STRAP CORROSION REPAIR BETWEEN S-27L AND S-30 MAJOR REPAIR
- [SDR FDEA202212290205](https://openairdocs.org/sdr/FDEA202212290205.md): Panel · cracked · Dec 29, 2022 · N923FD · Boeing 757200 · Wing Structure
  > R/H WING SLAT #7 HAS A CRACK AFT EDGE NEAR ANTI ICE DOOR PERFORMED REPAIR FOR CLOSURE PANEL OF SLAT#7 PER SRM 57-43-01, REPAIR 10,PARAGRAPH 4.D, OPTION A. REF. SRM 57-43-01-1A,FIG. 101, NOTE "N". REP. DIM AND LOC.: 17" X 2". 12" FROM I/B AT L/E. REV. 138.1
- [SDR FDEA202212290186](https://openairdocs.org/sdr/FDEA202212290186.md): Crease Beam · corroded · Dec 29, 2022 · N923FD · Boeing 757* · Fuselage Structure (General)
  > FOUND CORROSION ON INBD CREASE BEAM BETWEEN STA 1180 TO 1200 LBL 64 REMOVED AFFECTED PART IAW SRM 51-40-02 ACCOMPLISHED REPAIR IAW FEDEX EA F-5310-T0372399 P1 TITLED: FUSELAGE- MAINFRAME: SEC 46, FLOOR STRUCTURE, CREASE BEAM INNER CHORD, STA 1180-1200, LB
- [SDR FDEA202212290185](https://openairdocs.org/sdr/FDEA202212290185.md): Floorbeam · corroded · Dec 29, 2022 · N923FD · Boeing 757* · Fuselage Structure (General)
  > FOUND CORROSION ON MAIN DECK FLOOR BEAM AT STA 1681 BETWEEN RBL 24 TO RBL 33 ACCOMPLISHED REPAIR IAW FEDEX EA F-5310-T0372416 P1 TITLED: FUSELAGE- GENERAL- STA 1681 RBL 22-27 CORROSION FOUND ON UPPER AFT AND FWD FLANGE. MAJOR REPAIR
- [SDR FDEA202212290183](https://openairdocs.org/sdr/FDEA202212290183.md): Seat Track · corroded · Dec 29, 2022 · N923FD · Boeing 757* · Fuselage Structure (General)
  > FOUND CORROSION ON SEAT TRACK BETWEEN STA 1180 TO 1200 AT LBL 45 REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02 PART FAB. PER DWG 146N5130 AND FEDEX GMM 07-0-1001 SEE R/C W/O 20521483 INSTALLED SEAT TRACK IAW SRM 51-40-02 MAJOR REPAIR
- [SDR FDEA2023012380154](https://openairdocs.org/sdr/FDEA2023012380154.md): Floor Panel · worn · Dec 28, 2022 · N923FD · Boeing 757204 · Fuselage Floor Panel
  > DURING REMOVAL, FOUND FLOOR PANEL WORN. REPLACED THE FLOOR PANEL IAW DWG SRZ-25-005.
- [SDR FDEA2023012380153](https://openairdocs.org/sdr/FDEA2023012380153.md): Floor Panel · worn · Dec 28, 2022 · N923FD · Boeing 757204 · Fuselage Floor Panel
  > DURING REMOVAL FOUND FLOOR PANEL WORN. REPLACED THE FLOOR PANEL IAW DWG SRZ-25-005.
- [SDR FDEA202212280147](https://openairdocs.org/sdr/FDEA202212280147.md): Floor Panel · worn · Dec 28, 2022 · N923FD · Boeing 757200 · Fuselage Floor Panel
  > DURING REMOVEL FOUND FLOOR P.N 11861182-15 WORN REPLACED MENTIONED FLOOR PANEL PER DWG SRZ-25-005. P/N: FX11861182-15 222MAF. MAJOR
- [SDR FDEA202212280146](https://openairdocs.org/sdr/FDEA202212280146.md): Floor Panel · worn · Dec 28, 2022 · N923FD · Boeing 757200 · Fuselage Floor Panel
  > DURING REMOVEL FOUND FLOOR PANEL P.N 11861182-16 WORN REPLACED MENTIONED FLOOR PANEL PER DWG SRZ-25-005 P/N: FX11861182-16 221MBF. MAJOR.
- [SDR FDEA202212280145](https://openairdocs.org/sdr/FDEA202212280145.md): Floor Panel · worn · Dec 28, 2022 · N923FD · Boeing 757200 · Fuselage Floor Panel
  > DURING REMOVEL FOUND FLOOR PANEL P.N 141N5370-38 WORN REPLACED MENTIONED FLOOR PANEL PER DWG SRZ-25-005. P/N: FX141N5370-38. MAJOR.
- [SDR FDEA202212280144](https://openairdocs.org/sdr/FDEA202212280144.md): Floor Panel · worn · Dec 28, 2022 · N923FD · Boeing 757200 · Fuselage Floor Panel
  > DURING REMOVEL FOUND FLOOR PANEL P.N 11861182-14 WORN REPLACED MENTIONED FLOOR PANEL PER DWG SRZ-25-005. P/N: FX11861182-14 222MBF. MAJOR.
- [SDR FDEA202212280143](https://openairdocs.org/sdr/FDEA202212280143.md): Floor Panel · worn · Dec 28, 2022 · N923FD · Boeing 757200 · Fuselage Floor Panel
  > DURING REMOVEL FOUND FLOOR PANEL P.N 11861182-2 WORN REPLACED MENTIONED FLOOR PANEL PER DWG SRZ-25-005 P/N: FX11861182-2 222MDF. MAJOR.
- [SDR FDEA202205241290](https://openairdocs.org/sdr/FDEA202205241290.md): Servo · malfunctioned · May 24, 2022 · N923FD · Boeing 757200 · Autopilot System
  > PDIS 923 22-10 3694 24MAY22 BSL OPEN U WITH RIGHT AUTOPILOT ENGAGED THERE IS A CONSISTENT VIBRATION IN BOTH YOKES. THE LEFT AND CENTER AUTOPILOT DOES NOT HAVE THE VIBRATIONS. MEL 24MAY22 20:08 BSL U RELEASED FOR SERVICE PER MEL: 22-10
- [SDR FDEA202205161236](https://openairdocs.org/sdr/FDEA202205161236.md): Holder · damaged · May 16, 2022 · N923FD · Boeing 757200 · Emergency Lighting
  > MDIS 923 33-50 3670 16MAY22 HAJ FACT U RH EMERGENCY EXXIT LIGHTS DOES NOT ILLUMINATE R/I 16MAY22 19:09 HAJ U REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF MPN: 2013-1ASMI POS: 2 SRL: 3341
- [SDR FDEA202109302436](https://openairdocs.org/sdr/FDEA202109302436.md): Transmitter · faulted · Sep 30, 2021 · N923FD · Boeing 757204 · Trailing Flap Position Indicating System
  > TE FLAP ASYM ON EXTENSION BETWEEN 0 AND 1 DEGREES. FOLLOWED QRH PROCEDURE AND DECLARED EMERGENCY. UNEVENTFUL LANDING. FIM 27-51 FAULT TREE 809 FOLLOWED: - FSEU #1 READOUT AT FLAPS 20 POSN RH 274.13 LH 253.59 - LT FLAP POSITION TRANSMITTER REQUIRES REP
- [SDR FDEA202103160796](https://openairdocs.org/sdr/FDEA202103160796.md): Skin · dented · Mar 16, 2021 · N923FD · Boeing 757204 · Leading Edge Devices
  > FOUND A DENT ON SLAT #6 O/B TRAILING EDGE 10.5" FROM O/B TO 3.8" FROM TOP REPAIRED #6 SLAT UPPER T/E WEDGE 9.752 FROM OUTBOARD EDGE AND 4.5" FROM UPPER IAW IAW SRM 57-43-02-2R REPAIR 4 FIG 201 THIS IA A CAT A MAJOR REPAIR
- [SDR FDEA202103030546](https://openairdocs.org/sdr/FDEA202103030546.md): Flap Track · loose · Mar 3, 2021 · N923FD · Boeing 757204 · Trailing Edge Flaps
  > R/H O/B MAIN FLAP TRACKS #7 AND #8 ARE LOOSE AT AFT ATTACH POINTS REPLACED AFT ATTACH POINTS HARDWARE ON R/H O/B MAIN FLAP TRACKS #7 AND #8 IAW AMM 27-51-15
- [SDR FDEA202103030544](https://openairdocs.org/sdr/FDEA202103030544.md): Flap Track · loose · Mar 3, 2021 · N923FD · Boeing 757204 · Trailing Edge Flaps
  > L/H O/B MAIN FLAP TRACKS #1 AND #2 ARE LOOSE AT AFT ATTACH POINTS. REPLACED AFT ATTACH POINTS HARDWARE ON L/H O/B MAIN FLAP TRACKS #1 AND #2 IAW AMM 27-51-15
- [SDR FDEA202102190761](https://openairdocs.org/sdr/FDEA202102190761.md): Drag Fitting · corroded · Feb 19, 2021 · N923FD · Boeing 757204 · Wing, Attach Fittings
  > CORROSION FOUND DURING NOT INSPECTION ON L/H ENG #1 DRAG AND DIALONAL BRACE IN THE FOLLOWING HOLES 2,3,6,8,9,10,14,16 REMOVED CORROSION FROM HOLES #2,3,6,8,9,10,14,16, AND 16. CRACKS FOUND AT HOLES #3 AND #9. REPLACED INBOARD AND OUTBOARD DRAG BRACE FITTING I
- [SDR FDEA202102180762](https://openairdocs.org/sdr/FDEA202102180762.md): Drag Fitting · corroded · Feb 18, 2021 · N923FD · Boeing 757204 · Wing, Attach Fittings
  > CORROSION FOUND DURING NDT INSPECTION ON RH ENG #2 DRAG FITTING DIAGONAL BRACE HOLES #1, 2, 3, 5, 6, 8, 10, 11, 13, 14, 15, 16, 17, AND 18. REMOVED CORROSION FROM HOLES #1, 2, 3, 5, 6, 8, 10, 11, 13, 14, 15, 16, 17, AND 18. CRACKS FOUND AT HOLES #4 AND #9. REP
- [SDR FDEA202102160446](https://openairdocs.org/sdr/FDEA202102160446.md): Fill Port · corroded · Feb 16, 2021 · N923FD · Boeing 757204 · Fuel Storage
  > R/H OVERWING FILL PORT FAILED BONDING CHECK. HAVE EVIDENCE OF CORROSION EVALUATED R/H OVERWING FILL POART IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 3, FIG 102 AND FOUND FILL PORT TO BE OUTSIDE SRM LIMITS.LIMIT OF REMAINING THICKNESS 0.240" ACTUAL=0.210". REPAIRED
- [SDR FDEA202102160445](https://openairdocs.org/sdr/FDEA202102160445.md): Fill Port · corroded · Feb 16, 2021 · N923FD · Boeing 757204 · Fuel Storage
  > L/H OVERWING FILL PORT FAILED BONDING CHECK HAS EVIDENCE OF CORROSION EVALUATED L/H OVERWING FILL POART IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 3, FIG 102 AND FOUND FILL PORT TO BE OUTSIDE SRM LIMITS. LIMIT OF REMAINING THICKNESS 0.240" ACTUAL=0.220". REPAIRED
- [SDR FDEA202009142211](https://openairdocs.org/sdr/FDEA202009142211.md): Switch · out of adjust · Sep 14, 2020 · N923FD · Boeing 757204 · Door Warning System
  > PDIS 923 52-70 1907 14SEP20 CDG OPEN U. MN CARGO DR SYS ON STATUS PAGE AFTER BLK OUT FROM BSL INFO 14SEP20 18:20. MC1 R REF TECH TIP NR 18-0045 FACT 15SEP20 09:35 CDG, AS PER FIM 52-72-00-815-802 CLEANNING CONNECTORS D7174 OF S10518 AND D7170 OF V10129. PER
- [SDR FDEA202009032085](https://openairdocs.org/sdr/FDEA202009032085.md): Hose · leaking · Sep 3, 2020 · N923FD · Boeing 757204 · Hydraulic System, Main
  > PDIS 923, 32-51, 1866, 03SEP20, AMS, OPEN U. AT APPROX 500' ON LANDING, RECEIVED 'L HYD QTY' EICAS. OBSERVED QTY SLOWLY DECREASING. AFTER LANDING RECEIVED 'L HYD SYSTEM PRESSURE' EICAS, QTY=0.16 SHGN 03SEP20 09:25. AMS U DURING T/S FOUND FLEX HYDR. H

Next page: https://openairdocs.org/aircraft/N923FD/reports.md?page=2

## 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 = 'N923FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N923FD/reports

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