# Service difficulty reports: N941FD

A list on [N941FD](https://openairdocs.org/aircraft/N941FD.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 · 150 reports

- [SDR FDEA202205051122](https://openairdocs.org/sdr/FDEA202205051122.md): Gcu · faulted · May 5, 2022 · N941FD · Boeing 757225 · AC Generator-Alternator
  > AFTER SETTING THRUST FOR TAKEOFF, GOT L GEN OFF EICAS. REJECTED TAKEOFF. SWAPPED APU GCU TO LEFT POSITION TO RETURN PREVIOUSLY SWAPPED PARTS BACK TO THEIR ORIGINAL POSITIONS. THEN SWAPPED LEFT GCU WITH RIGHT GCU IAW MM 24-22-02-4. RECONNECTED LEFT IDG AND V
- [SDR FDEA202203210623](https://openairdocs.org/sdr/FDEA202203210623.md): Oil System · leaking · Mar 21, 2022 · N941FD · Boeing 757225 · APU Oil System
  > DURING FLIGHT OPERATING WITH MEL 24.00.01. APU SHUTDOWN INFLT. FL 350. RAN QRH & DECLARED AN EMERGENCY. DIVERTED. OPENED APU COWLINGS TO INVESTIGATE SOURCE OF OIL LEAK. SIGHT GLASS SHOWS NO OIL INDICATION SAME IN COCKPIT INDICATION. MASTER CHIP DETECTOR SHOW
- [SDR FDEA202201050008](https://openairdocs.org/sdr/FDEA202201050008.md): None · worn · Jan 5, 2022 · N941FD · Boeing 757200 · Wing, Control Surfaces
  > LEFT WING I/B FWD FLAP L/E AREA LOWER SKIN WORN. ACCOMPLISHED PERMANENT REPAIR TO L/W I/B FWD FLAP L/E BY BONDING AN ALUMINUM DOUBLER IAW FED EX EA# F-5750-TO366153-P1 WING-FLIGHT SURFACEES-LH INBD FORE FLAP, LOWER OOUBD LEADING EDGE SKIN, MF STA 235, DOUB
- [SDR FDEA202112313159](https://openairdocs.org/sdr/FDEA202112313159.md): None · none · Dec 31, 2021 · N941FD · Boeing 757200 · Nacelle/Pylon Structure
  > #2 PYLON UNDER PANEL #443HL CORROSION ON INNER SURFACE LOWER CORNER AROUND FASTENER ACCOMPLISHED FEDEX EA# F-5450-T0366121 P1, NACELLES / PYLON - WING PYLON/STRUT - #2 PYLON, INB SIDE, SKIN, INNER SURFACE PP STA 144, CORROSION
- [SDR FDEA202112293157](https://openairdocs.org/sdr/FDEA202112293157.md): Strap · cracked · Dec 29, 2021 · N941FD · Boeing 757200 · Engine Exhaust System
  > #2 ENG I/B T/R FWD STRAP CRACKED REMOVED AND REPLACED STRAP PER B757 AMM 78-31-20-8
- [SDR FDEA202112293155](https://openairdocs.org/sdr/FDEA202112293155.md): None · cracked · Dec 29, 2021 · N941FD · Boeing 757200 · Wing, Control Surfaces
  > #8 SLAT I/B TRACK I/B SIDE COVE PANEL CRACKED REMOVED AND REPLACED COVE PANEL PER BAC DWG #114N4004 REV F
- [SDR FDEA202112273152](https://openairdocs.org/sdr/FDEA202112273152.md): None · cracked · Dec 27, 2021 · N941FD · Boeing 757200 · Nacelle/Pylon Structure
  > #2 PYLON UNDER ACCESS PANEL 611KT FWD OUTBOARD END U-CHANNEL CRACKED. REMOVED AND REPLACED U-CHANNEL ON #2 PYLON UNDER ACCESS PANEL 611KT IAW BAC DWG 313N5004 REV D
- [SDR FDEA202112243138](https://openairdocs.org/sdr/FDEA202112243138.md): None · none · Dec 24, 2021 · N941FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN, STA 460 STR28R, HAS 2EA DEEP GOUGES ACCOMPLISHED FEDEX EA# F-5330-T0365972-P1: FUSELAGE - PLATES AND SKIN - STA 456, S- 27R - S-28R, GOUGES, DOUBLER REPAIR.
- [SDR FDEA202112243137](https://openairdocs.org/sdr/FDEA202112243137.md): None · worn · Dec 24, 2021 · N941FD · Boeing 757200 · Engine Thrust Reverser
  > #1 ENGINE OTBD T/R UPPER AFT INNER THERMAL SHIELD METAL PLATE IS WORN THRU. ENGINE EXHAUST - TR STRUCTURE/SLEEVE - #1 LH TR INNER DUCT REAR INNER PANDOWN WELD REPAIR PER FEDEX EA F-7833-T0366003
- [SDR FDEA202112223119](https://openairdocs.org/sdr/FDEA202112223119.md): Bracket · loose · Dec 22, 2021 · N941FD · Boeing 757200 · Trailing Edge Flap Control System
  > L/W I/B FLAP O/B TRACK UNDER FAIRING SUPPORT BRACKET IS LOOSE REMOVED AND REINSTALLED L-WING FLAP UPPER PANEL IAW BAC DWG 113N2003 REV A AND B757 SRM 51-40-04 - T# E110392G. ACCOMPLISHED INBOARD MAIN FLAP FASTENER HOLE REPAIR AT THE AFT FAIRING SUPPORT F
- [SDR FDEA202112223120](https://openairdocs.org/sdr/FDEA202112223120.md): Strap · cracked · Dec 22, 2021 · N941FD · Boeing 757200 · Engine Exhaust System
  > #2 ENG I/B T/R FWD CROSSBRACE SUPPORT BRACKET IS CRACKED REMOVED AND REPLACED BRACKET PER B757 AMM 78-30-20-8
- [SDR FDEA202112213114](https://openairdocs.org/sdr/FDEA202112213114.md): Skin · corroded · Dec 21, 2021 · N941FD · Boeing 757200 · Nacelle/Pylon Structure
  > @2 PYLON LANDING FOR ACCESS PANEL #443GL HAS CORROSION FWD LOWER CORNER NACELLES/PYLONS - SKIN/PLATES/PANELS - #2 PYLON INBD SKIN PANEL, PP STA 114, INNER SURFACE, CORROSION REPAIR PER FEDEX EA F-5430-T0366016
- [SDR FDEA202112213113](https://openairdocs.org/sdr/FDEA202112213113.md): None · none · Dec 21, 2021 · N941FD · Boeing 757200 · Engine (Turbine/Turboprop)
  > NO.2 ENGINE INBD COWL EXTERIOR SURFACE HAS A DENT REPAIRED NO 2 ENGINE COWL ENG INBD EXTERIOR SURFACE IAW B757 SRM 54-20-01-1A, SRM 54-20-01-2R,
- [SDR FDEA202112213112](https://openairdocs.org/sdr/FDEA202112213112.md): None · cracked · Dec 21, 2021 · N941FD · Boeing 757200 · Powerplant System
  > #1 ENGINE EXHAUST DUCT LOWER FORWARD EDGE HAS A CRACKED BRACKET REMOVED AND REPLACED BRACKET PER RR EM 78-11-04-300-008-801
- [SDR FDEA202112203107](https://openairdocs.org/sdr/FDEA202112203107.md): Panel · delaminated · Dec 20, 2021 · N941FD · Boeing 757200 · Aerodynamic Fairings
  > WING TO BODY PANEL 195EL IS DELAMINATED ON THE EDGE REPAIRED PER B757 SRM 53-00-70-2R-1 AND 53-60-70-2R
- [SDR FDEA202112203106](https://openairdocs.org/sdr/FDEA202112203106.md): Bracket · cracked · Dec 20, 2021 · N941FD · Boeing 757200 · Powerplant System
  > #2 ENGINE AFT DRAIN LINE BRACKET CRACKED LOWER AFT HOT SECTION REMOVED AND REPLACED BRACKET PER RR EM 78-11-04-300-010
- [SDR FDEA202112083048](https://openairdocs.org/sdr/FDEA202112083048.md): Frame · cracked · Dec 8, 2021 · N941FD · Boeing 757200 · Fuselage Main, Structure
  > STA 1640 FRAME, RHS, HAS CRACK INDICATION @ LOWER, INBD HOLE @ S14R ACCOMPLISHED FEDEX EA# F-5310-T0365884: FUSELAGE - MAINFRAME - FRAME, STA 1640, S14R CRACK INDICATION *THIS EA DEVIATES FROM EO F-5310-E0344602
- [SDR FDEA202112083046](https://openairdocs.org/sdr/FDEA202112083046.md): Frame · damaged · Dec 8, 2021 · N941FD · Boeing 757200 · Fuselage Main, Structure
  > REPLACEMENT OF THE CAT C REPAIR INSTALLED ON FRAME BOTTOM ASSEMBLY AT STATION 1640, S26R - S27R REQUIRED ACCOMPLISHED PERMANENT REPAIR IAW FEDEX EA F--5310-T0352854-P2 (A), RELEASED JAN 03, 2022, TITLED "FUSELAGE - MAINFRAME - FRAME, STA 1640, S-26R - S-2
- [SDR FDEA202105121209](https://openairdocs.org/sdr/FDEA202105121209.md): Circuit Card · malfunctioned · May 12, 2021 · N941FD · Boeing 757225 · Central Warning
  > AURAL WARNING SOUNDED CONTINUOUSLY INFLIGHT NO LAND 3. PERFORMED MCDP TEST 30/40 WITH NO FAULTS FOUND. LAST FLIGHT FAULT WAS "RUD SRVO/FCC C" DIAGNOSTIC CODE 131361. REMOVED AND REPLACED LEFT AND RIGHT SIREN/OWL CARD MODULE (M999 & M619) IAW 757 AMM 31-51
- [SDR FDEA202012243204](https://openairdocs.org/sdr/FDEA202012243204.md): Throttle · faulted · Dec 24, 2020 · N941FD · Boeing 757 · Power Lever
  > RIGHT THRUST LEVER FROZEN AT 12 O'CLOCK POSITION. RT ENGINE SHUT DOWN IN FLIGHT. DISCONNECTED THROTTLE CABLE OF RH ENGINE BETWEEN UPPER GEARBOX AND INTERMEDIATE GEARBOX AT ARROWHEAD DISCONNECT. THROTTLE FREE IN COCKPIT. DISCONNECTED LOWER GEARBOX FROM FFG.
- [SDR FDEA2020052621035](https://openairdocs.org/sdr/FDEA2020052621035.md): Slide · deployed · May 22, 2020 · N941FD · Boeing 757225 · Escape Slide
  > LT FWD ENT DOOR SLIDE DEPLOY IN MEM. REMOVED AND REPLACED L1 PASSENGER DOOR ESCAPE SLIDE IAW AMM 25-66-01-4. OPS CHK GOOD. REMOVED FROM MEL. A/C OK FOR SERVICE.
- [SDR FDEA202003200595](https://openairdocs.org/sdr/FDEA202003200595.md): Frame · gouged · Mar 20, 2020 · N941FD · Boeing 757225 · Fuselage Main, Frame
  > FUSELAGE STATION 1640 STRINGER 26 RIGHT, FRAME HAS A GOUGE AND SUPPORT ANGLE HAS AN ELONGATED HOLE. ACCOMPLISHED EA # F-5310-T0352854 P1 FUSELAGE - MAINFRAME - FRAME, STA 1640, S26R-S27R, GOUGE, ANGLE REPAIR
- [SDR FDEA2020031970590](https://openairdocs.org/sdr/FDEA2020031970590.md): Floorbeam · damaged · Mar 17, 2020 · N941FD · Boeing 757225 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR BEAM LWR SURFACE IS DAMAGED AT STA 1560 APPROX LBL 53 (STREAMER ATTACHED) ALL WORK ACOMPLISHED IAW FEDEX EA# F-5321-T0352761 P1, FUSELAGE- CARGO COMP FLOORS- STA 1560 1560 LBL 53 FLOOR BEAM LWR FWD FLANGE
- [SDR FDEA202003170583](https://openairdocs.org/sdr/FDEA202003170583.md): Skin · gouged · Mar 17, 2020 · N941FD · Boeing 757225 · Fuselage Main, Plate/Skin
  > FUSELAGE EXT SKIN STA 1280 TO 1400 AND FROM S26L TO S26R HAS SEVERAL PREVIOUS BLENDS REPAIRED AREA PER EA# F-5310-T0352664-P1
- [SDR FDEA202003170580](https://openairdocs.org/sdr/FDEA202003170580.md): Frame · bent · Mar 17, 2020 · N941FD · Boeing 757225 · Fuselage Main, Frame
  > AFT CARGO PIT LH STA 1580 FRAME BENT ALL WORK ACOMPLISHED IAW FED EX EA# F-5310-T0352536-P1
- [SDR FDEA202003160575](https://openairdocs.org/sdr/FDEA202003160575.md): Frame · bent · Mar 16, 2020 · N941FD · Boeing 757225 · Fuselage Main, Frame
  > AFT CARGO LT BS 1600 FRAME BENT. ALL WORK ACOMPLISHED IAW EA F-5310-T0352546-P1.
- [SDR FDEA2020031760575](https://openairdocs.org/sdr/FDEA2020031760575.md): Frame · bent · Mar 16, 2020 · N941FD · Boeing 757225 · Fuselage Main, Frame
  > AFT CARGOPIT LH STA 1600 FRAME BENT ALL WORK ACOMPLISHED IAW FEDEX EA# F-5310-T0352546-P1
- [SDR FDEA2020031760574](https://openairdocs.org/sdr/FDEA2020031760574.md): Skin · gouged · Mar 16, 2020 · N941FD · Boeing 757224 · Fuselage Main, Plate/Skin
  > FUSELAGE EXT SKIN STA 1400 TO 1440 AND FROM S30 TO S26L HAS SEVERAL PREVIOUS BLENDS AREA REPAIRED PER EA # F-5310-T0352664 P1
- [SDR FDEA2020031760573](https://openairdocs.org/sdr/FDEA2020031760573.md): Skin · dented · Mar 16, 2020 · N941FD · Boeing 757225 · Fuselage Main, Plate/Skin
  > FUSELAGE EXT SKIN STA 1400 TO 1440 AND FROM S27R TO S29R HAS 4EA DENTS. REPAIRED AREA PER EA# F-5310-T0352664-P1
- [SDR FDEA2020031760572](https://openairdocs.org/sdr/FDEA2020031760572.md): Shear Tie · broken · Mar 16, 2020 · N941FD · Boeing 757225 · Fuselage Internal Mounting Structure
  > BROKEN SHEAR TIE AT STA 1600 BETWEEN STR 27L AND 28L REMOVED BROKEN SHEAR TIE IAW B757-200 SRM 51-40-02. FABRICATED NEW SHEAR TIE IAW FED EA F-5310-T0352992-P1 AND BOEING DWG 146N1021 REV A. INSTALLED NEW SHEAR TIE IAW SRM 51-40-02 AND DWG 146N1021 REV A.
- [SDR FDEA2020031760569](https://openairdocs.org/sdr/FDEA2020031760569.md): Doubler · gouged · Mar 16, 2020 · N941FD · Boeing 757225 · Fuselage Main, Plate/Skin
  > FUSELAGE EXT BETWEEN STA 1540 AND STA 1560 AND BETWEEN S20L AND S22L PREVIOUS REPAIR HAS SEVERAL TOOLING MARKS REMOVED REPAIR AND REPAIRED AREA IAW FEDEX EA # F-5330-T0352692-P1
- [SDR FDEA2020031750568](https://openairdocs.org/sdr/FDEA2020031750568.md): Intercostal · damaged · Mar 15, 2020 · N941FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > AFT PIT LBL 16.21 WL 160.0 INTERCOSTAL HAS MULTIPLE ELONGATED AND DOUBLE DRILLED HOLES REMOVED AND REPLACED INTERCOSTAL IAW BOEING DWG 146N5443 REV J AND DWG 146N5451 REV C
- [SDR FDEA2020031750567](https://openairdocs.org/sdr/FDEA2020031750567.md): Intercostal · damaged · Mar 15, 2020 · N941FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > AFT PIT RBL 16.21 WL 160.0 INTERCOSTAL HAS MULTIPLE ELONGATED AND DOUBLE DRILLED HOLES REMOVED AND REPLACED INTERCOSTAL IAW BOEING DWG 146N5443 REV J AND DWG 146N5451 REV C
- [SDR FDEA202003130560](https://openairdocs.org/sdr/FDEA202003130560.md): Support Angle · corroded · Mar 13, 2020 · N941FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT DECK PLATE VIEWED FROM BELOW STA 1715 RBL 12 SUPPORT ANGLE CORRODED REMOVED AND REPLACED CORRODED ANGLE IAW BOEING DWG 146N5221 REV B
- [SDR FDEA202003120558](https://openairdocs.org/sdr/FDEA202003120558.md): Seat Track · corroded · Mar 12, 2020 · N941FD · Boeing 757225 · Fuselage, Seat/Cargo Attach Fittings
  > SURFACE CORROSION AT BODY STATION 118 (UNDERNEATH MAIN CARGO DECK FLOORBOARD) FLOOR SUPPORT BEAM, SECOND BEAM FROM LEFT, AROUND AND BELOW SEAT TRACK, AROUND HYLOCKS ON SEAT TRACK STANDOFF BRACKET, AND AROUND AND ON STANDOFF FOR SEAT TRACK. DOT AND STREAM
- [SDR FDEA202003120554](https://openairdocs.org/sdr/FDEA202003120554.md): Shear Web · corroded · Mar 12, 2020 · N941FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT, STRUCTURAL SHEAR WEB IS CORRODED AT APPROX STA 1691 APPROX LBL10 REPAIRED IAW B757-200 SRM 53-60-51-2R REPAIR 2
- [SDR FDEA202003120553](https://openairdocs.org/sdr/FDEA202003120553.md): Shear Web · corroded · Mar 12, 2020 · N941FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT SHEAR WEB (DECK PLATE) IS CORRODED AT APPROX STA 1686 APPROX LBL10 ALL WORK ACCOMPLISHED ON N/R N00342 IAW B757-200 SRM 53-60-51-2R REPAIR 2
- [SDR FDEA2020031210544](https://openairdocs.org/sdr/FDEA2020031210544.md): Shear Web · corroded · Mar 11, 2020 · N941FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STRUCTURE SHEAR WEB (DECK PLATE) IS PITTED AT APPROX STA 1683 APPROX LBL 12.5 REPAIR ACCOMPLISHED ON N/R N00342 IAW B757-200 SRM 53-60-51-2R REPAIR 2
- [SDR FDEA2020031210543](https://openairdocs.org/sdr/FDEA2020031210543.md): Shear Web · corroded · Mar 11, 2020 · N941FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STRUCTURE SHEAR WEB (DECK PLATE) IS CORRODED AT APPROX STA 1701 APPROX LBL7 REPAIR ACCOMPLISHED ON N/R N00342 IAW B757-200 SRM 53-60-51-2R REPAIR 2
- [SDR FDEA2020031210542](https://openairdocs.org/sdr/FDEA2020031210542.md): Shear Web · corroded · Mar 11, 2020 · N941FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STRUCTURE SHEAR WEB (DECK PLATE) IS PITTED AT APPROX STA 1706 APPROX LBL7 ALL WORK ACCOMPLISHED ON NR N00342 IAW B757-2 SRM 53-60-51-2R REPAIR 2
- [SDR FDEA2020031210540](https://openairdocs.org/sdr/FDEA2020031210540.md): Nut Plate · corroded · Mar 11, 2020 · N941FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STRUCTURE AT STA 1681 APPROX RBL 23 FLOOR BOARD NUT PLATE STRIP IS CORRODED FABRICATED NUTPLATE STRIP IAW BOEING DWG 146N5693 REV C AND INSTALLED ON N/R N00334
- [SDR FDEA2020031210539](https://openairdocs.org/sdr/FDEA2020031210539.md): Nut Plate · corroded · Mar 11, 2020 · N941FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STRUCTURE AT STA 1681 APPROX RBL 32 FLOOR BOARD NUT PLATE STRIP IS CORRODED FABRICATED NUTPLATE STRIP IAW BOEING DWG 146N5693 REV C AND INSTALLED ON N/R N00334
- [SDR FDEA2020031210538](https://openairdocs.org/sdr/FDEA2020031210538.md): Shear Web · corroded · Mar 11, 2020 · N941FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STRUCTURE AT STA 1681 APPROX RBL 22 SHEAR WEB IS CORRODED REPAIR ACCOMPLISHED ON N/R N00334 IAW B757-200 SRM 53-60-51-2R REPAIR 2
- [SDR FDEA2020031210537](https://openairdocs.org/sdr/FDEA2020031210537.md): Shear Web · damaged · Mar 11, 2020 · N941FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STRUCTURE SHEAR WEB (DECK PLATE) IS CORRODED AT APPROX 1683 RBL 31 ACCOMPLISHED FEDEX EA # F-5321-T0352653, FUSELAGE - CARGO COMP FLOORS - FLOOR SUPPORT, STA 1681 - 1701, RBL 20 AND 23, EDGE DAMAGE, BLEND REPAIR. ACCOMPLISHED DOU
- [SDR FDEA2020031210536](https://openairdocs.org/sdr/FDEA2020031210536.md): Nut Plate · corroded · Mar 11, 2020 · N941FD · Boeing 757225 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STRUCTURE AT STA 1681 APPROX RBL 40 FLOOR BOARD NUTPLATE STRIP IS CORRODED ACCOMPLISHED FEDEX EA # F-5321-T0352606 FUSELAGE- CARGO COMP FLOORS - STA 1681, RBL 40, DOUBLE DRILLED HOLE, FREEZE PLUG REPAIR. ACCOMPLISHED DOUBLER REPAIR
- [SDR FDEA202003090506](https://openairdocs.org/sdr/FDEA202003090506.md): Door Frame · cracked · Mar 9, 2020 · N941FD · Boeing 757225 · Passenger/Crew Doors
  > R-2 DOOR SKIN UPPER HINGE CUT OUT IS CRACKED. REPAIR OF FWD FRAME OF NUMBER 2 RIGHT SIDE PASSENGER DOOR COMPLIED WITH IAW B757-200 SRM 52-10- 02 02-2R REPAIR 1. HFEC INSPECTION REQUIRED AT 50,000 TOTAL DOOR FLIGHT CYCLES OR 5,800 FLIGHT CYCLES AFTER REPAIR
- [SDR FDEA2020030970500](https://openairdocs.org/sdr/FDEA2020030970500.md): Seat Track · corroded · Mar 7, 2020 · N941FD · Boeing 757225 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK CORRODED ABS1071- BS 1075, BL LBL 24 REPAIRED SEAT TRACK IAW B757-2 SRM 53-00-52-2R REPAIR #4
- [SDR FDEA202003050495](https://openairdocs.org/sdr/FDEA202003050495.md): Slat · delaminated · Mar 5, 2020 · N941FD · Boeing 757225 · Leading Edge Devices
  > #3 SLAT REQUIRES REPLACEMENT REMOVED AND REPLACED AND PERFORMED OPS TEST ON #3 SLAT IAW B757 AMM 27-81-02-4 OPS CHECK GOOD
- [SDR FDEA2020030540485](https://openairdocs.org/sdr/FDEA2020030540485.md): Seat Track · gouged · Mar 4, 2020 · N941FD · Boeing 757225 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN RH SIDE SEAT TRACK IS GOUGED BS 619, RBL 00 REPAIRED SEAT TRACK IAW FEDEX EA# F-5320-T0352523-P1 FUSELAGE AUXILIARY STRUCTURE - CABIN SEAT TYRACK STA 619 BL 0 GOUGE SPLICE REPAIR
- [SDR FDEA2020030530481](https://openairdocs.org/sdr/FDEA2020030530481.md): Rub Strip · cracked · Mar 3, 2020 · N941FD · Boeing 757225 · Trailing Edge Flaps
  > RIGHT WING INBD FLAP SUPPORT BRACKET HAS CRACKED RUB STRIP AT AFT TRUNNION FAIRING REMOVED ABD REPLACED RUB STRIP AT R/W I/B FLAP SUPPORT AT AFT TRUNNION FAIRING IAW BAC DWG 113N1831 REV-SRM 51-40-02

Next page: https://openairdocs.org/aircraft/N941FD/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 = 'N941FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N941FD/reports

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