# Service difficulty reports: N935FD

A list on [N935FD](https://openairdocs.org/aircraft/N935FD.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 6 · 298 reports

- [SDR FDEA202610131587](https://openairdocs.org/sdr/FDEA202610131587.md): Indication Sys · malfunctioned · Oct 13, 2026 · N935FD · Boeing 7572T7 · Hydraulic Indicating System
  > DURING CLIMB OUT, GOT RT HYD SYS PRESSURE EICAS & ASSOCIATED LIGHT ON OVERHEAD. LOWER EICAS STATUS PAGE SHOWED NORMAL PRESSURE & NORMAL QUANTITY. EMERGENCY DECLARED. IAW CHAPTER 6, AMM 26-18-00-5, AMM 29-11-00-5, AMM 28-22-00-5, AMM 75-32-01-2, AMM 73-2
- [SDR FDEA202610131564](https://openairdocs.org/sdr/FDEA202610131564.md): Wire · shorted · Oct 13, 2026 · N935FD · Boeing 7572T7 · Hydraulic Indicating System
  > DURING CLIMB OUT GOT R HYD SYS PRESS EICAS AND ASSOCIATED LIGHT ON OVERHEAD. LOWER EICAS STATUS PAGE SHOWED NORMAL PRESSURE AND NORMAL QUANTITY. EMERGENCY DECLARED. FOUND WIRE W5200-0073-20 SHORTED TO GROUND. REMOVED CONTACTS 2 & 3 OF C/P D3064 & SHORT T
- [SDR FDEA202609181374](https://openairdocs.org/sdr/FDEA202609181374.md): Eec · failed · Sep 18, 2026 · N935FD · Boeing 7572T7 · Fuel Controlling System
  > L EEC EICAS DURING TAKEOFF ROLL AND 4X IN FLIGHT ALL WITH ASSOCIATED AUTOTHROTTLES EICAS. NOTABLE YAW IN FLIGHT WHEN IT WOULD OCCUR. COMPLIED WITH QRH. FIM: 73-21 FAULT TREE 822 ON HIGH POWER RUN FOUND LH EEC WENT TO OFF AS THROTTLES WERE INCREASED. PER
- [SDR FDEA202607231013](https://openairdocs.org/sdr/FDEA202607231013.md): Beam · corroded · Jul 23, 2026 · N935FD · Boeing 7572T7 · Fuselage Main, Structure
  > NOSE WHEEL WELL STRUCTURE BS 310.5 LOWER AREA INTERNAL BEAM WITH CORROSION REMOVED VERTICAL BEAM OUT OF LIMITS AT NOSE WEEL STRUCTURE BS 310.5 LBL 20.05 LOWER AREA INTERNAL IAW B757 51-40-02-0G; TRIMED LOCATED, DRILLED AND INSTALLED NEW VERTICAL BEAM REPLA
- [SDR FDEA202607200955](https://openairdocs.org/sdr/FDEA202607200955.md): Strap · corroded · Jul 20, 2026 · N935FD · Boeing 7572T7 · Fuselage Miscellaneous Structure
  > APU INLET DUCT ATTACHMENTS AT THE AFT FRAME WITH CORROSION CORRSION OUT OF LIMITS AT APU INLET DUCT ATTACHMENTS ON THE AFT FRAME (MIDDLE STRAP) IAW B-757 SRM 53-80-15-1A WAS REPAIRED IAW B-757 SRM 53-80-15-2R REPAIR 1
- [SDR FDEA202607200954](https://openairdocs.org/sdr/FDEA202607200954.md): Crease Beam · corroded · Jul 20, 2026 · N935FD · Boeing 7572T7 · Fuselage Main, Structure
  > MCC CREASE BEAM SIDE LH BSTA 1620 TO BSTA 1370 IT HAS CORROSION SPOTS MCC L/H CREASE BEAM SECTION WITH CORROSION OUT OF LIMITS FROM STA 1430 TO 1530 LBL 64.40 IAW B-757 SRM 53-60-13-1A, WAS REPAIRED IAW B-757 SRM 53-00-13-2R REPAIR 1
- [SDR FDEA202607200953](https://openairdocs.org/sdr/FDEA202607200953.md): Crease Beam · corroded · Jul 20, 2026 · N935FD · Boeing 7572T7 · Fuselage Main, Structure
  > MCC SIDE LH BETWEEN BS 1080 TO BS 1100 CREASE BEAM WITH CORROSION MCC L/H CREASE BEAM SECTION WITH CORROSION OUT OF LIMITS FROM STA 1040 TO STA 1100 IAW B-757 SRM 53-40-13-1A WAS REPAIRED IAW B-757 SRM 53-40-13-1A, WAS REPAIRED IAW B-757 SRM 53-00-13-2R R
- [SDR FDEA202607150928](https://openairdocs.org/sdr/FDEA202607150928.md): Floorbeam · corroded · Jul 15, 2026 · N935FD · Boeing 7572T7 · Fuselage Main, Floor Beam
  > MCC BL 0 TO LBL 24.75 BS 1200 FLOOR BEAM WITH CORROSION AREA WITH CORROSION OUT OF LIMITS AT FLOOR BEAM BS 1200 LBL 8 TO LBL 14 WAS REPAIRED IAW B757 SRM 53-00-51-2R REPAIR 5
- [SDR FDEA202607100893](https://openairdocs.org/sdr/FDEA202607100893.md): Skin Panel · dented · Jul 10, 2026 · N935FD · Boeing 7572T7 · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE TAIL AREA BETWEEN B.S. 1918 TO B.S. 1941 TOP SECTION WITH 01 EA DENT. APPLIED PERMANENT REPAIR AT UPPER FUSELAGE TAIL AREA BS 1918 TO B.S. 1941 I.A.W B757 SRM 53-80-01-1A, TABLE I, NOTE 'C', FIG 101, SHEET 2 AND SRM 51-70-10-2R REP '4'
- [SDR FDEA202607100892](https://openairdocs.org/sdr/FDEA202607100892.md): Access Panel · cracked · Jul 10, 2026 · N935FD · Boeing 7572T7 · Wing, Plate/Skin
  > LH WING #3 SLAT LOWER SKIN ACCESS PANEL 523GB AREA WITH 02 EA CRACK. 2EA CRACK AT LH WING #3 SLAT LOWER COVE SKIN ACCESS PANEL 523GB AREA WERE REPAIRED IAW B-757 SRM 57-43-01-2R FIG 201 REPAIR 4
- [SDR FDEA202607100890](https://openairdocs.org/sdr/FDEA202607100890.md): Access Panel · cracked · Jul 10, 2026 · N935FD · Boeing 7572T7 · Wing, Plate/Skin
  > LH WING #3 SLAT LOWER SKIN ACCESS PANEL 523FB AREA WITH 01EA CRACK. CRACK AT LH WING #3 SLAT LOWER COVE SKIN ACCESS PANEL 523FB AREA WAS REPAIRED IAW B-757 SRM 57-43-01-2R FIG 201 REPAIR 4.
- [SDR FDEA202506060850](https://openairdocs.org/sdr/FDEA202506060850.md): Gust Lock · inoperative · Jun 6, 2025 · N935FD · Boeing 7572T7 · Passenger/Crew Doors
  > L1 DOOR GUST LOCK FOUND DAMAGED/BROKEN ON WALKAROUND. AMM: 52-11-08-8 INSTALLED NEW SPLIT COLLAR IRW AMM 52-11-08-8.
- [SDR FDEA202408171144](https://openairdocs.org/sdr/FDEA202408171144.md): Stringer · corroded · Aug 17, 2024 · N935FD · Boeing 7572T7 · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO LSTR 19-22 STA 760 FRAME HAS AREAS OF CORROSION AT SKIN ATTACHMENT POINTS AND STR EVALUATED CORROSION AT SKIN ATTACHMENT POINTS S-19L, 21L, AND 22L NO CORROSION NOTED. REPAIRED STRINGER WITH SPLICE, SHEAR TIE, AND FILLER BETWEEN S-19L TO 20L
- [SDR FDEA202403300423](https://openairdocs.org/sdr/FDEA202403300423.md): Battery Pack · inoperative · Mar 30, 2024 · N935FD · Boeing 7572T7 · Emergency Lighting
  > THROUGHOUT MAINTANENCE DAILY CHECK FOUND L1 EMER EXIT SIGN DOOR 1 LT, FLT DECK DOME EMER LT MODULE, SLIDE LT DR 1 EMER INOP. SHGN 30MAR24 05:49 BNA WDM: CH 33-51-12 PG 13.1 SHEET 1FX1 PERFORMED T/S PROCEDURES TO EMERGENCY LIGHTS FORWAR LEFT SIDE L1 D
- [SDR FDEA202403160300](https://openairdocs.org/sdr/FDEA202403160300.md): Girt Bar · out of alignment · Mar 16, 2024 · N935FD · Boeing 7572T7 · Emergency Equipment
  > L1 DOOR ESCAPE SLIDE BEGAN TO FALL OUT WHEN DOOR WAS OPENED FOR CREW STAIR MATING. DURING TROUBLESHOOTING FOUND LH DOOR AFT FLOOR FITTING MISALIGNED. RE-ALIGNED FITTING IAW AMM 25-66-10-2. REINSTALLED GIRT BAR ON LT DOOR AND OPS CHECKED PER THE ABOVE MANUAL
- [SDR FDEA202212062878](https://openairdocs.org/sdr/FDEA202212062878.md): Shutoff Valve · out of alignment · Dec 6, 2022 · N935FD · Boeing 757200 · Engine Thrust Reverser
  > ON TAKEOFF ROLL HAD ODOR IN COCKPIT. AFTER LIFTOFF GOT LEFT ENGINE OVERHEAT MESSAGE. THEN FOLLOWED BY FIRE BELL. RAN QRH AN LANDED. EMERGENCY DECLARED. R&R'D LH HIGH PRESSURE SHUT OFF VALVE. R&R BOTH LEFT ENGINE REVERSER MONTED VENTILATION BELLOWS. INSTA
- [SDR FDEA202208081928](https://openairdocs.org/sdr/FDEA202208081928.md): Skin · corroded · Aug 8, 2022 · N935FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > #2 PYLON INTERNAL SKIN THRU ACCESS PANEL 443HL IS CORRODED AT FWD LOWER SIDE. REPAIRED #2 PYLON I/B SKIN PER FEDEX EA F-5450-T0369607 TITLE: NACELLES/PYLON - WING PYLON/STRUT - NO 2 PYLON, INBD SIDE SKIN ASSY, PP STA 128 AND 144 CORROSION
- [SDR FDEA202208071908](https://openairdocs.org/sdr/FDEA202208071908.md): Frame · delaminated · Aug 7, 2022 · N935FD · Boeing 7572T7 · Elevator Structure
  > LEFT ELEVATOR O/B UPPER SURFACE CONDUCTIVE FRAME IS DELAMINATED. REMOVED & REPLACED -7 ADAPTER PLATE IAW DWG 183N2003 REV G, -5 SPLICE PLATE & CONDUCTIVE FRAME IAW SRM 51-40-02 & DWG 183N2003 REV G & AMM 55-29-00-8.
- [SDR FDEA202208061906](https://openairdocs.org/sdr/FDEA202208061906.md): Floor Panel · dented · Aug 6, 2022 · N935FD · Boeing 757200 · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL AT STA 1100-1200 BL0 TO LBL24.75 HAS DENT REMOVED, FABRICATED AND INSTALLED NEW PANEL IAW FEDEX REPAIR DWG SRZ-25-005 AND AMM 25-55-04-4
- [SDR FDEA202208061905](https://openairdocs.org/sdr/FDEA202208061905.md): Floor Panel · dented · Aug 6, 2022 · N935FD · Boeing 757200 · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL AT STA 1100-1200 BL0 TO RBL24.75 HAS DENT REMOVED, FABRICATED AND INSTALLED NEW PANEL IAW FEDEX REPAIR DWG SRZ-25-005 AND AMM 25-55-04-4
- [SDR FDEA202208061904](https://openairdocs.org/sdr/FDEA202208061904.md): Skin · worn · Aug 6, 2022 · N935FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > #1 PYLON PANEL 433LR LANDING CENTER AFT IS WORN FROM PANEL LATCH. REPAIRED WORN LATCH LANDING PER FEDEX EA F-5450-T0369581 TITLE: NACELLES/PYLONS - SKIN - NO. 1 PYLON INBD SKIN - WEAR AT DOOR 433LR LAND.
- [SDR FDEA202208051901](https://openairdocs.org/sdr/FDEA202208051901.md): Skin · corroded · Aug 5, 2022 · N935FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > #1 PYLON CORROSION ON INNER SKIN BETWEEN PANEL 433BL AND 433CL REPAIR DAMAGE PER FEDEX EA F-5450-T0369650 TITLE: NACELLES/PYLONS - WING PYLON - NO. 1 PYLON, OUTB PANEL, PP STA 136, SKIN ASSY, CORROSION.
- [SDR FDEA202208051900](https://openairdocs.org/sdr/FDEA202208051900.md): Skin · damaged · Aug 5, 2022 · N935FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > L. SIDE FUSELAGE SKIN AT STATION 213.5 HAS LIGHTENING STRIKE DAMAGE. REPAIR LIGHTENING STRIKE DAMAGE PER FEDEX EA F-5330-T0369622 TITLE: FUSELAGE - SKIN - LIGHTENING STRIKE AT STA 211, 213 AND 221 BELOW S-20L, DOUBLER REPAIR
- [SDR FDEA202208051899](https://openairdocs.org/sdr/FDEA202208051899.md): Skin · damaged · Aug 5, 2022 · N935FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > L. SIDE FUSELAGE SKIN AT STATION 221.5 HAS LIGHTENING STRIKE DAMAGE. REPAIR LIGHTENING STRIKE DAMAGE PER FEDEX EA F-5330-T0369622 TITLE: FUSELAGE - SKIN - LIGHTENING STRIKE AT STA 211, 213 AND 221 BELOW S-20L, DOUBLER REPAIR
- [SDR FDEA202208051898](https://openairdocs.org/sdr/FDEA202208051898.md): Skin · damaged · Aug 5, 2022 · N935FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > L. SIDE FUSELAGE SKIN @ BS 211, S21L HAS A LIGHTENING STRIKE DAMAGE. REPAIR LIGHTENING STRIKE DAMAGE PER FEDEX EA F-5330-T0369622 TITLE: FUSELAGE - SKIN - LIGHTENING STRIKE AT STA 211, 213 AND 221 BELOW S-20L, DOUBLER REPAIR.
- [SDR FDEA202208051897](https://openairdocs.org/sdr/FDEA202208051897.md): Web · corroded · Aug 5, 2022 · N935FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > AREA BELOW MAIN CABIN FLOOR SUPPORT STRUCTURE, WEB STA 1440 TO 1460 RBL 65, UPPER SURFACE IS CORRODED REMOVED AND REPLACED CORRODED WEB IAW BAC DWG 146N8521 REV H AND EA# F-5310- T0369700: FUSELAGE - MAINFRAME - FLOOR SUPPORT STRUCTURE - WEB - RBL 65, STA 1
- [SDR FDEA202208041883](https://openairdocs.org/sdr/FDEA202208041883.md): Web · corroded · Aug 4, 2022 · N935FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > AREA BELOW MAIN CABIN FLOOR,SUPPORT STRUCTURE, UPPER DOOR SILL WEB IS CORRODED ON THE UPPER SURFACE AT STA 1440, APPROX RBL 65 CUT-OUT CORRODED SECTION OF WEB AND REPAIRED IAW B757 53-60-15-2R AND B757 SRM 51-70-13-0G AND BAC DWG# 146N8516 REV L
- [SDR FDEA202208041873](https://openairdocs.org/sdr/FDEA202208041873.md): Beam · corroded · Aug 4, 2022 · N935FD · Boeing 757200 · Wing Miscellaneous Structure
  > L.WING I/B FIXED L/E NOSE BEAM IS CORRODED REPLACED NOSE BEAM ASSY. PER BAC DWG 114N1606 AND FEDEX EA F-5720-T0369810 TITLE WING - SECONDARY WING STRCT - LH WING, FIXED LEADING EDGE, ISS 106-168, NOSE BEAM, ALTERNATE NDT PROCESS AND ALTERNATE FINISH.
- [SDR FDEA202208031857](https://openairdocs.org/sdr/FDEA202208031857.md): Frame · delaminated · Aug 3, 2022 · N935FD · Boeing 757200 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT STA 1300 INBD OF STR 26R HAS EXISTING FRAME REPAIR, REF: OPS CARD 8508. REPAIRED AFT CARGO COMPARTMENT FRAME @ STA 1300 R/H PER EA F-5310-E0347443.
- [SDR FDEA202207281806](https://openairdocs.org/sdr/FDEA202207281806.md): Buttstrap · corroded · Jul 28, 2022 · N935FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE IS CORRODED IN THE BUTT SEAM AT STA 900 BETWEEN S12R AND S17R (4 PLACES EXPOSED) ACCOMPLISHED FEDEX EA# F-5330-T0369294 - FUSELAGE - PLATES AND SKINS - SKIN SPLICE STRAP, STA 900, S-12R - S-17R, CORROSION
- [SDR FDEA202207261801](https://openairdocs.org/sdr/FDEA202207261801.md): Floor Support · corroded · Jul 26, 2022 · N935FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > STATION 1715 MAIN CARGO FLOOR STRUCTURE RIGHT SIDE PAN HAS CORROSION UNDER NUT PLATE ON L-BRACKET REMOVED, FABRICATED AND REPLACED L-BRACKET IAW B757 SRM 51-40-02-0G IAW BOEING DWG 146N5300, APPLIED ALODINE AND PRIMER IAW B757 SRM 51-20-01-0G AND ACCOMP
- [SDR FDEA202207261800](https://openairdocs.org/sdr/FDEA202207261800.md): Floor Support · corroded · Jul 26, 2022 · N935FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > STATION 1710 MAIN CARGO FLOOR STRUCTURE LEFT SIDE PAN HAS CORROSION UNDER NUTPL;ATE ON L-BRACKET REMOVED, FABRICATED AND REPLACED L-BRACKET IAW B757 SRM 51-40-02-0G IAW BOEING DWG 146N5300, APPLIED ALODINE AND PRIMER IAW B757 SRM 51-20-01-0G AND ACCOMPLI
- [SDR FDEA202207261799](https://openairdocs.org/sdr/FDEA202207261799.md): Floor Support · corroded · Jul 26, 2022 · N935FD · Boeing 757200 · Fuselage Floor Panel
  > STATION 1710 MAIN CARGO FLOOR STRUCTURE CENTER OF PAN HAS CORROSION UNDER NUT PLATE ON L-BRACKET REMOVED, FABRICATED AND REPLACED L-BRACKET IAW B757 SRM 51-40-02-0G IAW BOEING DWG 146N5300, APPLIED ALODINE AND PRIMER IAW B757 SRM 51-20-01-0G AND ACCOMPLI
- [SDR FDEA202207251795](https://openairdocs.org/sdr/FDEA202207251795.md): None · unknown · Jul 25, 2022 · N935FD · Boeing 757 · Fuselage Main, Structure
  > EXISTING MAJOR REPAIR FOUND ON FLOOR BEAM, UPPER CHORD AT STA 345, 40 RBL TO 52 LBL. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA. EVALUATED EXISTING REPAIR LOCATED ON FLOOR BEAM UPPER CHORD AT STA 345, 40 RBL TO 52 L
- [SDR FDEA202207221790](https://openairdocs.org/sdr/FDEA202207221790.md): Intercostal · corroded · Jul 22, 2022 · N935FD · Boeing 7572T7 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT INTERCOSTAL @ STA 1520 LBL 2.90 HAS CORRODED CLIP. FABRICATED NEW ATTACHMENT ANGLE IAW BAC DWG 146N5450-7 REV A & INSTALLED IAW B757 SRM 51-40- 02.
- [SDR FDEA202207221789](https://openairdocs.org/sdr/FDEA202207221789.md): Intercostal · corroded · Jul 22, 2022 · N935FD · Boeing 7572T7 · Fuselage Floor Panel
  > INTERCOSTAL FROM STATION 1500 TO 1520 IN BILGE AREA HAS CORROSION IN 3 AREAS FABRICATED NEW INTERCOSTAL IAW BAC DWG 146N5451-11 REV C & INSTALLED IAW B757 SRM 51-40-02.
- [SDR FDEA202207211788](https://openairdocs.org/sdr/FDEA202207211788.md): Skin · delaminated · Jul 21, 2022 · N935FD · Boeing 7572T7 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER UPPER SKIN PANEL HAS DELAMINATED REPAIR DOUBLER REPAIRED BY REMOVING AND REPLACING REPAIR DOUBLER IAW B757 SRM 55-10-01-1A TABLE 1 AND 51-70-10- 2R FIG 201.
- [SDR FDEA202207191770](https://openairdocs.org/sdr/FDEA202207191770.md): Skin · corroded · Jul 19, 2022 · N935FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > #2 PYLON INTERNAL SKIN IS CORRODED ON THE O/B SIDE APPROX 9IN AFT OF ACCESS PANEL 443AR REPAIRED PER FEDEX EA # F-5450-T0369337 - TITLE: NACELLES/PYLON - WING PYLON/STRUT - #2 PYLON OUTBD SKIN DOUBLER CORROSION.
- [SDR FDEA202207191772](https://openairdocs.org/sdr/FDEA202207191772.md): Support Bracket · bent · Jul 19, 2022 · N935FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > RADOME BULKHEAD BRACKET BENT FOR HOLD OPEN RODS FABRICATED SUPPORT BRACKET IAW BAC DWG 141N7835-2 REV F & INSTALLED IAW B757 SRM 51-40-02
- [SDR FDEA202207191769](https://openairdocs.org/sdr/FDEA202207191769.md): Skin · corroded · Jul 19, 2022 · N935FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > #2 PYLON APPROX. 9IN AFT OF DOOR CUTOUT INTERNAL PYLON SIDE SKIN THRU ACCESS PANEL 443GL IS EXFOILATED REPAIRED PER FEDEX EA # F-5430-T0369607
- [SDR FDEA202207181763](https://openairdocs.org/sdr/FDEA202207181763.md): Web · corroded · Jul 18, 2022 · N935FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > AFT CABIN FLOOR SUPPORT AT L4 DOOR CORRODED AT FASTENER HOLE BS 1661 BL 54L ACCOMPLISHED FEDEX EA # F-5310-T0369397-P1: FUSELAGE, MAINFRAME - FLOOR WEB. STA 1661, LBL58, CORROSION
- [SDR FDEA202207181762](https://openairdocs.org/sdr/FDEA202207181762.md): Panel · cracked · Jul 18, 2022 · N935FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > #1 PYLON PANEL 433LR IS CRACKED IN CENTER AT LATCH. REPAIRED #1 PYLON PANEL 433LR BY REMOVING DAMAGED AREA AT LATCH AND BONDING FIBERGLASS PREPREG REPAIR IAW B757 SRM 51-70-08-0G AND BAC DWG 311N5049 REV AY
- [SDR FDEA202207151737](https://openairdocs.org/sdr/FDEA202207151737.md): Transition Panel · cracked · Jul 15, 2022 · N935FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > LBL 14 TRANSITION PANEL CRACKED AT STATION APPROXIMATELY 1530. REPAIRED TRANSITION PANEL @ STA 1530 IAW B757 SRM 51-70-13-OG SHEET 1 & 2, & B757 SRM 53-60- 53-2R FIG 201.
- [SDR FDEA202207151735](https://openairdocs.org/sdr/FDEA202207151735.md): Floor Panel · damaged · Jul 15, 2022 · N935FD · Boeing 757200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 251MVF IS DAMAGED REPAIRED MAIN CABIN FLOOR PANEL IAW B757 SRM 53-00-50-2R FIG. 201 REPAIR 1.
- [SDR FDEA202207141729](https://openairdocs.org/sdr/FDEA202207141729.md): Skin · gouged · Jul 14, 2022 · N935FD · Boeing 757200 · Ailerons
  > L/W AILERON LOWER SURFACE IS GOUGED 13 IN FROM I/B L/E REPAIRED PER B757 SRM 57-60-01-2R FIG 201 REPAIR # 2 SHEET 3
- [SDR FDEA202207111710](https://openairdocs.org/sdr/FDEA202207111710.md): Nut Plate · corroded · Jul 11, 2022 · N935FD · Boeing 757200 · Fuselage Main, Attach Fittings
  > AFT CABIN NUTPLATE STRAP IS CORRODED AT BS 1682 RBL 32 REMOVED, FABRICATED AND REPLACED NEW NUTPLATE STRAP IAW B757 DWG 146N5300 REV E - DWG 146N5393 REV C, B757-2 SRM 51-40-02-0G, APPLIED ALODINE AND PRIMER IAW B757-2 SRM 51-20-01-0G
- [SDR FDEA202207101705](https://openairdocs.org/sdr/FDEA202207101705.md): Skin · cracked · Jul 10, 2022 · N935FD · Boeing 757200 · Wing, Plate/Skin
  > LW INB LEADING EDGE SKIN BEHIND #5 SLAT AT INB MAIN TRACK CUTOUT IS CRACKED REPAIRED LEFT WING INBOARD LEADING EDGE SKIN BEHIND #5 SLAT AT INBOARD MAIN TRACK CUTOUT CRACK IAW B757-SRM-57-41-01-2R-1 FIG 201 SHEET 6.
- [SDR FDEA202107221842](https://openairdocs.org/sdr/FDEA202107221842.md): Slide · damaged · Jul 22, 2021 · N935FD · Boeing 7572T7 · Escape Slide
  > UPON ARRIVAL. DOOR OPEN ASSIST BOTTLE DEPLOYED LEFT SIDE. SLIDE LOCK DETACHED FROM GIRT BAR. SLIDE DID NOT DEPLOY. NOTE: F/O DID NOT DIS ARM SLIDE PRIOR TO UN-LATCH OF DOOR.DIS-ENGAGED GIRT BAR PRIOR TO DOOR BEING FULLY OPEND AND WHEN DOOR FULLY OPENED
- [SDR FDEA2020090312078](https://openairdocs.org/sdr/FDEA2020090312078.md): Switch · failed · Sep 1, 2020 · N935FD · Boeing 7572T7 · Drag Control System
  > REJECTED T/O FOR CONFIG SPOILERS EICAS WARNING. RAN QRH, TRIED TO T/O AGAIN, SAME ISSUE. RAN QRH AND RETURNED TO GATE. REMOVED SPEED BRAKE HANDLE POSITION SWITCH S493 IAW AMM 31-51-03-4, AND REPLACED TB190 XA1 AND YA1 IAW SWPM 20-90-11, AND RETERMINATED NUM
- [SDR FDEA202007161520](https://openairdocs.org/sdr/FDEA202007161520.md): Actuator · inoperative · Jul 16, 2020 · N935FD · Boeing 7572T7 · Landing Gear Actuator
  > GEAR DISAGREE EICAS MESSAGE W/AMBER GEAR CAUTION LIGHT ON TAKEOFF. NO LIGHT IN GEAR HANDLE AND 3 GREEN GEAR LIGHTS EXTINGUISHED. REMOVED NOSE GEAR LOCK ACTUATOR IAW AMM 32-34-02-4. INSTALLED NOSE GEAR LOCK ACTUATOR REF 32-34-02-4. LEAK CHECKED GOOD. PERFORME

Next page: https://openairdocs.org/aircraft/N935FD/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 = 'N935FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N935FD/reports

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