# Service difficulty reports: N781FD

A list on [N781FD](https://openairdocs.org/aircraft/N781FD.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 2 · 67 reports

- [SDR FDEA202511172188](https://openairdocs.org/sdr/FDEA202511172188.md): Slide · low pressure · Nov 17, 2025 · N781FD · Boeing 757222 · Escape Slide
  > R1 DOOR SLIDE PRESSURE BELOW GREEN BAND. REMOVED AND REPLACED R-1 DOOR ESCAPE SLIDE ASSY. IAW AMM 25-66-01-4 OK FOR SERVICE.
- [SDR FDEA202502200254](https://openairdocs.org/sdr/FDEA202502200254.md): Warning Light · malfunctioned · Feb 20, 2025 · N781FD · Boeing 757222 · Emergency Equipment
  > DURING POST FLIGHT FOUND RIGHT ENTRY DOOR DISARMED AND OPENED SLIDE LIGHT REMAINS ILLUMINATED. OPERATED R1 DOOR SLIDE ARMING LEVER SEVERAL TIMES. R1 DOOR SLIDE LIGHT OPERATED NORMAL PER MM. A/C OK FOR SERVICE.
- [SDR FDEA202502150234](https://openairdocs.org/sdr/FDEA202502150234.md): Indication Sys · malfunctioned · Feb 15, 2025 · N781FD · Boeing 757222 · Passenger/Crew Doors
  > PER CREW RIGHT ENTRY DOOR DISARMED AND OPENED SLIDE LIGHT REMAINS ILLUMINATED. WORKED WRI IN CONJUCTION WITH TSI 52-10/6355 COMPLETING THE REQUIRED STEP ON TSI LUBE EMERGENCY MECHANISM OPS CHECK DOOR SEVERAL TIMES SLIDE LIGHT ARMED AND DISARMED AS DESCRIBED
- [SDR FDEA202502070193](https://openairdocs.org/sdr/FDEA202502070193.md): Girt Bar · fod · Feb 7, 2025 · N781FD · Boeing 757222 · Emergency Equipment
  > R-1 DOOR "SLIDE" LIGHT ABOVE R-1 DOOR STAYS ILLUMINATED WITH DOOR IN DISARM POSITION. FACT 08FEB25 03:10 ORD FOUND R1 DOOR GIRT BAR AND FLOOR FITTINGS WITH SOME DEBRIS, CLEANED PROX SENSOR AND FLOOR FITTING AND LUBRICATED ACCORDINGLY. REF. AMM 12-21-1
- [SDR FDEA202412271844](https://openairdocs.org/sdr/FDEA202412271844.md): Battery Pack · no test · Dec 27, 2024 · N781FD · Boeing 757222 · Emergency Lighting
  > THROUGHOUT MAINTANENCE PREFLIGHT ROUTINE FOR LAYOVER'S FOUND EMERGENCY LIGHTS FORWARD TEST SYS 1, INOP. REMOVED AND REPLACED BATTERY PACK ASSY, PERFORMED SYS OPS CHECK, ALL CHECKS NORMAL, ALL IAW B757-200 AMM CH 33-51-07-2.
- [SDR FDEA202412071779](https://openairdocs.org/sdr/FDEA202412071779.md): Wedge · damaged · Dec 7, 2024 · N781FD · Boeing 757222 · Trailing Edge Flaps
  > RH WING, MAIN FLAP TRAILING EDGE WEDGE AT THE OUTBD END OF THE EXTENSION HAS COMPOSITE DAMAGE AND DENT. REMOVED RH WING MAIN FLAP TRAILING EDGE WEDGE AT THE OUTBD IAW SRM 51-40-02. REPAIRED FLAP WEDGE IAW SRM 51-70-10-2R REPAIR 4. REINSTALLED RH WING MAIN
- [SDR FDEA202412031770](https://openairdocs.org/sdr/FDEA202412031770.md): Floor Panel · damaged · Dec 3, 2024 · N781FD · Boeing 757222 · Cargo Compartments
  > MAIN DECK CARGO COMPT FLOORBOARD PANEL 252MTF HAS SEVERAL INSERTS DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 252MTF ON VTMAE TRAVELER #T24/1787480 IAW DWG 11864182 REVISION D MAJOR REPAIR.
- [SDR FDEA202412031771](https://openairdocs.org/sdr/FDEA202412031771.md): Floor Panel · damaged · Dec 3, 2024 · N781FD · Boeing 757222 · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT FLOORBOARD PANELS 251MSF INSERTS TORN. FABRICATED ZONE 250 FLOORBOARD PANEL 251MSF ON VTMAE TRAVELER #T24/1787474 IAW DWG 11864182 REVISION D MAJOR REPAIR
- [SDR FDEA202412031769](https://openairdocs.org/sdr/FDEA202412031769.md): Floor Panel · damaged · Dec 3, 2024 · N781FD · Boeing 757222 · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT FLOORBOARD PANEL 241MDF DAMAGED. FABRICATED ZONE 240 FLOORBOARD PANEL 241MDF ON VTMAE TRAVELER #T24/1787472 IAW DWG 11863182 REVISION C MAJOR REPAIR
- [SDR FDEA202412031768](https://openairdocs.org/sdr/FDEA202412031768.md): Floor Panel · damaged · Dec 3, 2024 · N781FD · Boeing 757222 · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT FLOORBOARD PANEL 251MTF HAS SEVERAL INSERTS DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 251MTF ON VTMAE TRAVELER #T24/1787475 IAW DWG 1186182 REVISION D MAJOR REPAIR
- [SDR FDEA202412031767](https://openairdocs.org/sdr/FDEA202412031767.md): Shear Tie · corroded · Dec 3, 2024 · N781FD · Boeing 757222 · Fuselage Internal Mounting Structure
  > DOT 139/41 AFT CARGO COMP. FRAME CLIP AND SKIN WITH CORROSION STA 1460 STRG 29L-29R. REWORK ON FRAMECLIP (SHEAR TIE) AND SKIN @ STA 1460 BTWN STR 29L TO 29R: NO CORROSION WAS FOUND ON FRAME AND SKIN. FOUND 2 EA SHEAR-TIES CORROSION OUT OF LIMIT IAW SRM 53-
- [SDR FDEA202411271745](https://openairdocs.org/sdr/FDEA202411271745.md): Floor Panel · damaged · Nov 27, 2024 · N781FD · Boeing 757222 · Fuselage Floor Panel
  > FLOOR PANEL 222MAF HAS FIBER DAMAGED CRACKED AND PEELED DUE TO REMOVAL OF TAPE. FABRICATED ZONE 220 FLOOR PANEL 222MAF ON VTMAE TRAVELER # T24/1786765 IAW DWG 141N5370 REV. CY MAJOR REPAIR
- [SDR FDEA202411271749](https://openairdocs.org/sdr/FDEA202411271749.md): Floor Panel · damaged · Nov 27, 2024 · N781FD · Boeing 757222 · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT FLOORBOARD PANEL 252MFF DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 252MFF ON VTMAE TRAVELER # T24/1787479 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR
- [SDR FDEA202411271748](https://openairdocs.org/sdr/FDEA202411271748.md): Floor Panel · damaged · Nov 27, 2024 · N781FD · Boeing 757222 · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT FLOORBOARD PANEL 241MNF DAMAGED. FABRICATED ZONE 240 FLOORBOARD PANEL 241MNF ON VTMAE TRAVELER # T24/1787473 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR
- [SDR FDEA202411271747](https://openairdocs.org/sdr/FDEA202411271747.md): Floor Panel · damaged · Nov 27, 2024 · N781FD · Boeing 757222 · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT FLOORBOARD PANEL 232MFF BROKEN FABRICATED ZONE 230 FLOORBOARD PANEL 232MFF ON VTMAE TRAVELER #T24/1787469 IAW DWG 11862181 REV L MAJOR REPAIR
- [SDR FDEA202411271746](https://openairdocs.org/sdr/FDEA202411271746.md): Floor Panel · damaged · Nov 27, 2024 · N781FD · Boeing 757222 · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT FLOORBOARD PANEL 232MWF DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 232MWF ON VTMAE TRAVELER # T24/1787471 IAW DWG 11862182 REV. H, MAJOR REPAIR
- [SDR FDEA202305090860](https://openairdocs.org/sdr/FDEA202305090860.md): Skin · damaged · May 9, 2023 · N781FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > JUST AFT OF THE PRESSURE BULKHEAD, STA 1845 RBL 10 SKIN IS PUNCTURED. REPAIRED FUSELAGE SKIN AT STA 1845 RBL 10 JUST AFT OF PRESSURE BULKHEAD IAW EA F-5330- T0373981. THIS IS A MAJOR REPAIR
- [SDR FDEA202210072514](https://openairdocs.org/sdr/FDEA202210072514.md): Wedge · delaminated · Oct 7, 2022 · N781FD · Boeing 757222 · Leading Edge Devices
  > #6 SLAT REQUIRES REPLACEMENT DUE TO T/E WEDGE DELAMINATION FOUND ON FEDEX E.O F- 5750-E0336930-P6 REPAIRED #6 SLAT T/E WEDGE IAW FEDEX EA# F-5750-T0370813-P1 - WINGS - FLIGHT SURFACES - #6 SLAT, TRAILING EDGE WEDGE, ISS 193, DELAMINATION
- [SDR FDEA202210062499](https://openairdocs.org/sdr/FDEA202210062499.md): Angle · cracked · Oct 6, 2022 · N781FD · Boeing 757222 · Wing Miscellaneous Structure
  > **PARTS RACK ITEM** R/W FLAP FAIRIG 672HB HAS A BENT FORWARD R/H CLOSEOUT ANGLE REPAIRED R/W, I/B FLAP FAIRING 672HB FORWARD R/H CLOSEOUT ANGLE IAW FEDEX EA # F-5720-T0370931- P1, TITLED "WING - SECONDARY WING STRCT - RH INBD FLAO FAIRING, 672HB, INBD AND OUT
- [SDR FDEA202210042463](https://openairdocs.org/sdr/FDEA202210042463.md): Floor Support · corroded · Oct 4, 2022 · N781FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > MAIN CABIN, FLOOR SUPPORT AT STA 1640 TO 1660, LBL 55 HAS CORROSION AROUND NUT PLATES. BLENDED CORRODED AREAS IAW B757 SRM 51-10-02-0G. ORIGINAL MATERIAL THICKNESS OF.071" IAW B757 SRM 53-60-13-0I, FIG. 1, DETAIL VII. REMOVED.003" FOR REMAINING THICKNESS
- [SDR FDEA202210042461](https://openairdocs.org/sdr/FDEA202210042461.md): Fitting · none · Oct 4, 2022 · N781FD · Boeing 757 · Fuselage Main, Structure
  > ACCOMPLISH FEDEX E.A. F-5310-T0357573-P2 REQUIRED, REPLACEMENT OF THE L4 DOOR LOWER HINGE SUPPORT FITTING P/N 146N8762-13. REMOVED AND REPLACED THE L-4 DOOR LOWER HINGE SUPPORT FITTING IAW BAC DWG 146N8739, REV. K AND FEDEX E.A. F-5310-T0357573-P2, TITLE:
- [SDR FDEA202210012439](https://openairdocs.org/sdr/FDEA202210012439.md): Floor Panel · cracked · Oct 1, 2022 · N781FD · Boeing 757222 · Fuselage Floor Panel
  > MAIN CABIN, FLOOR PANEL 251MVF IS CRACKED AND HAS AREAS OF DISBOND ON LOWER SIDE REPAIRED FLOOR PANEL 251MVF IAW BAC D6-55191, REV. C, AND B757 SRM 53-00-50-2R, REPAIR 2, FIG. 201, SHEET 1 AND PARA. 4.A., AND VT MAE DWG 11864182, REV. A
- [SDR FDEA202209302420](https://openairdocs.org/sdr/FDEA202209302420.md): Shear Web · corroded · Sep 30, 2022 · N781FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > MAIN CABIN, AFT FLOOR, SHEAR WEB HAS SEVERAL, AREAS OF CORROSION, STA 1681 TO 1720, LBL 56 TO RBL 56 REPAIRED THE AFT MAIN CABIN SHEAR WEB (DECK PLATE), STA 1681 TO 1720, LBL 56 TO RBL 56, IAW FEDEX E.A. F-5310-T0370865-P1, RELEASE DATE: 29 SEPTEMBER, 2022
- [SDR FDEA202209302418](https://openairdocs.org/sdr/FDEA202209302418.md): None · none · Sep 30, 2022 · N781FD · Boeing 757200 · Standard Practices/Structures
  > FOUND EXISTING COMPOSITE REPAIR LOCATED ON R/WING OUTBOARD AFT FLAP, LOWER SURFACE. REPAIR INSTALLED ON REMOVABLE STRUCTURAL COMPONENT AND REQUIRES TRACKING OF COMPONENT, NOT EXISTING REPAIR. EXISTING COMPOSITE REPAIR LOCATED ON R/WING OUTBOARD AFT FLAP,
- [SDR FDEA202209292396](https://openairdocs.org/sdr/FDEA202209292396.md): Floor Panel · delaminated · Sep 29, 2022 · N781FD · Boeing 757222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 251MWF HAS AREA OF DISBON ON THE BOTTOM SIDE REPAIRED DISBOND ON MAIN CABIN FLOOR PANEL 251MWF IAW B757 SRM 53-00-50-1A REPAIR 2, BAC D6-55191 REV: C
- [SDR FDEA202209292395](https://openairdocs.org/sdr/FDEA202209292395.md): Floor Panel · delaminated · Sep 29, 2022 · N781FD · Boeing 757222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 252MVF HAS AREAS OF DISBOND ON BOTTOM SIDE REPAIRED DISBOND ON MAIN CABIN FLOOR PANEL 252MVF IAW B757 SRM 53-00-50-1A TABLE 2, BAC D6-55191 REV: C PARA 8.4.3, 8.4.6 FIG 14, 15, 2 TABLE 5
- [SDR FDEA202209292394](https://openairdocs.org/sdr/FDEA202209292394.md): Floor Panel · delaminated · Sep 29, 2022 · N781FD · Boeing 757222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 252MVF HAS DELAMINATION ON TOP SIDE REPAIRED DELAMINATION ON MAIN CABIN FLOOR PANEL 252MVF IAW B757 SRM 53-00-50-1A TABLE 2, BAC D6-55191 REV: C PARA 8.4.3, 8.4.6 FIG 14, 15, 2 TABLE 5
- [SDR FDEA202209292393](https://openairdocs.org/sdr/FDEA202209292393.md): Floor Panel · delaminated · Sep 29, 2022 · N781FD · Boeing 757222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 52MVF HAS AREAS OF DISBONDED ON THE BOTTOM SIDE REPAIRED DISBOND ON MAIN CABIN FLOOR PANEL 252MVF IAW B757 SRM 53-00-50-1A TABLE 2, BAC D6-55191 REV: C PARA 8.4.3, 8.4.6 FIG 14, 15, 2 TABLE 5
- [SDR FDEA202209262371](https://openairdocs.org/sdr/FDEA202209262371.md): Plate · cracked · Sep 26, 2022 · N781FD · Boeing 757222 · Wing, Plate/Skin
  > RIGHT WING T/E REAR SPAR LOWER CORD WIGGLE PLATE CRACK AT WSTA330 APPROX STREAMER ATTACHED CRACKED WIGGLE PLATE AT WS 330 RIGHT WING T/E REAR SPAR LOWER CHORD WAS REMOVED AS REQ IAW FEDEX B757 SRM 51-40-02-0G AND REPLACED WITH NEW WIGGLE PLATE P/N 113N16
- [SDR FDEA202203120485](https://openairdocs.org/sdr/FDEA202203120485.md): None · cracked · Mar 12, 2022 · N781FD · Boeing 757200 · Wing, Plate/Skin
  > DURING POST FLIGHT, FOUND THE LEFT OB TE FLAP SKIN CRACKED APPROX 3" THROUGH A RIVET. REF SRM 57-53-01-01 SHEET 8, LOWER AFT, MOST OB LOWER SKIN PAINTED FABRICATED DOUBLER ON LEFT OB TE FLAP REF. AMM 51-21-07.
- [SDR FDEA202010222603](https://openairdocs.org/sdr/FDEA202010222603.md): Skin · cracked · Oct 22, 2020 · N781FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > AIRCRAFT DAMAGED STA 1620 UNDER STR 17L DENT IS L=1.75" W=1". C/W EA NR F-5330-T0357572 P1 TITLE: FUSELAGE-PLATES AND SKIN-FUSELAGES SKIN REPAIR NEAR STA 1620 BETWEEN STRINGERS S-16L AND S-18L.
- [SDR FDEA202010102459](https://openairdocs.org/sdr/FDEA202010102459.md): Frame · cracked · Oct 10, 2020 · N781FD · Boeing 757222 · Fuselage Main, Frame
  > LT BS 1640 FRAME LEWER INBOARD HOLE HAS (2) INDICATIONS OF CRACKS AT 3 O`CLOCK AND 9 O`CLOCK POSITIONS. C/W FEDEX EA NR F-5310-T 0357202 P1 TITLE: FUSELAGE-MAINFRAME-STA 1640 SPLICE REPAIR BETWEEN STRINGER I-9 F AND S-20L.
- [SDR FDEA202010062423](https://openairdocs.org/sdr/FDEA202010062423.md): Strap · cracked · Oct 6, 2020 · N781FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > COURIER AREA STA 350 LBL 25 LOWER SUPPORT STRAP LOWER SURFACE IS CRACKED. REMOVED EXISTING STABILIZATION STRAP REPAIR BETWEEN STA 345 TO STA 377 LBL 25, IAW B757 SRM 51-40-02-OG. FABRICATED AND INSTALLED NEW STABILIZATION STRAP REPAIR AND FILLER SECTION, IAW
- [SDR FDEA202010062422](https://openairdocs.org/sdr/FDEA202010062422.md): Strap · cracked · Oct 6, 2020 · N781FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > UPON REMOVE LOWER STRAP (STABILIZATION) FOUND INTERCOSTAL PREVIOUS REPAIR CRACKED BETWEEN BS 350 TO BS 365.5 ON LBL 24.750. REMOVED INTERCOSTAL BETWEEN STA 350 TO STA 365.5 LBL 24.75, IAW B 757 SRM 51-40-02-OG. FABRICATED AND INSTALLED NEW INTERCOSTAL, IAW B
- [SDR FDEA202010052420](https://openairdocs.org/sdr/FDEA202010052420.md): Floorbeam · damaged · Oct 5, 2020 · N781FD · Boeing 757222 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR PANEL SUPPORT HAS PULLED RIVETS THRU UPPER SHIM AT BS 1055 LBL 24.75 TO 45.5. REMOVED AND FABRICATED, INSTALLED NEW FLOOR SUPPORT (PLATE) AT STA 1055 BETWEEN LBL 24.75-LBL 45.5, IAW B 757 SRM 51-40-02-OG, 51-40-05-OG AND BOEING DWG 144N5070 R
- [SDR FDEA202010052419](https://openairdocs.org/sdr/FDEA202010052419.md): Floorbeam · cracked · Oct 5, 2020 · N781FD · Boeing 757222 · Fuselage Main, Floor Beam
  > MAIN DECK STA 900 BETWEEN LBL 24.75-LBL 44.5 FLOOR SUPPORT CRACKED. REMOVED, FABRICATED, AND INSTALLED NEW FLOOR SUPPORT (PLATE) STA 900 BETWEEN LBL 24.75-LBL 44.5, IAW B 757 SRM 51-40-02-OG, 51-40-05-OG AND BOEING DWG 144N5070 REV W AND REV B.
- [SDR FDEA202010042414](https://openairdocs.org/sdr/FDEA202010042414.md): Crease Beam · corroded · Oct 4, 2020 · N781FD · Boeing 757222 · Fuselage Main, Structure
  > MAIN DECK BETWEEN STA 1020-1040 RT CREASE BEAM CORRODED. REMOVED CORROSION AT CREASE BEAM STA 1020-1040 RT SIDE, IAW B 757 SRM 51-10-02-OG, ORIGINAL MAT.070", MINIMUN REMAINING.022". MAT LOSS.048" FOUND TO BE OUT OF LIMITS, IAW B757 SRM 53-30-13-1A FIG
- [SDR FDEA202010012384](https://openairdocs.org/sdr/FDEA202010012384.md): Frame · cracked · Oct 1, 2020 · N781FD · Boeing 757222 · Fuselage Main, Structure
  > HFEC SURFACE INDICATION OF DEFECT(CRACK)NOTED AND MARKED IN RED SHARPIE ON FUSELAGE MAIN FRAME 1640RIGHT HAND SIDE INNER CHORD FWD RETURN FLANGE RADIUS INLINE WITH STRINGER 14R. INDICATION RUNS FROM EDGE OF FLANGE UNDER STRAP TO SINGLE FASTENER ATTACHED
- [SDR FDEA2019042650929](https://openairdocs.org/sdr/FDEA2019042650929.md): Unknown · vibration · Apr 25, 2019 · N781FD · Boeing 757222 · Elevator Control System
  > ON APPROACH AT 150 FT A STRANGE /MODERATE ELEVATOR RYTHMIC VIBRATION, ALMOST NOT CONTROTABLE ACCURED, LASTED ALL THE WAY TO LANDING FLAP 25 137 KTS WIND 190 AT 12 GUST 18. PERFORMED BITE ON BOTH SAM COMPUTERS, NO FAULTS FOUND, PERFORMED A BITE CHECKS ALL
- [SDR FDEA201903020527](https://openairdocs.org/sdr/FDEA201903020527.md): Fitting · obstructed · Mar 2, 2019 · N781FD · Boeing 757222 · Emergency Equipment
  > AFTER LANDING FO NOTED LEFT DOOR SLIDE ARM LIGHT FLASHING INTERMITTANTLY. REF AMM 25-66-00 CLEANED DEBRIS FROM GIRT BAR FLOOR FITTINGS. OPERATIONAL CHECKS GOOD.
- [SDR FDEA201809242668](https://openairdocs.org/sdr/FDEA201809242668.md): Door Frame · gouged · Sep 24, 2018 · N781FD · Boeing 757222 · Fuselage Main, Structure
  > LOWER FUSELAGE FWD ACCY COMPT ACCESS DOOR CUTOUT FWD FRAME, AND LATCH PLATE HAS GOUGES AT BS 231.25. EVALUATED DAMAGED AREA ON FRAME AT BS 231.25, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-2R AND EVALUATED LATCH PLATE AREA WITH NO DEFECT NOTED ONLY PAINT DAM
- [SDR FDEA2018091872560](https://openairdocs.org/sdr/FDEA2018091872560.md): Seat Track · cracked · Sep 17, 2018 · N781FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK CROWN BETWEEN STA 500-550 RBL 24.75 CRACKED. EVALUATED DAMAGE AREA ON SEAT TRACK FROM STA 484 AND STA 546 TO BE FOUND OUT OF LIMITS IAW SRM 53-00-52-1A DETAIL II & III FIG 101. CUT-OUT DAMAGED AREA SEAT TRACK STA 470 TO STA 570 RBL 24.75
- [SDR FDEA201809112440](https://openairdocs.org/sdr/FDEA201809112440.md): Collar · defective · Sep 11, 2018 · N781FD · Boeing 757222 · Passenger/Crew Doors
  > L1 DOOR HOLD OPEN LOCK INOP. DOOR CLOSES NORMAL. REPLACED L1 DOOR HOLD-OPEN LOCK COLLAR PER AMM 52-11-08-8.
- [SDR FDEA201612154470](https://openairdocs.org/sdr/FDEA201612154470.md): Warning Light · false activation · Dec 15, 2016 · N781FD · Boeing 757222 · Central Warning
  > DURING APPROACH, MOMENTARY LT WING SLIDE EICAS ALERT. OPS CHECKED DOOR IAW AMM 52-71-00-5. NO FAULTS NOTED
- [SDR FDEA201609093161](https://openairdocs.org/sdr/FDEA201609093161.md): Access Panel · damaged · Sep 9, 2016 · N781FD · Boeing 757222 · Wing, Plate/Skin
  > RIGHT WING, TANK DRY BAY ACCESS DOOR ASSY PANEL BROKEN, OTBD WS 258.5, PN 112N8003-2 COMPLIED WITH EA F-5720-T0326684, DATED SEPT 02,2016. FUEL SYSTEMS, CELLS, TANKS, VENTS, RT WING TANK ACCESS DOOR ASSY CAT-B, MAJOR REPAIR.
- [SDR FDEA201609093160](https://openairdocs.org/sdr/FDEA201609093160.md): Spar · corroded · Sep 9, 2016 · N781FD · Boeing 757222 · Wing Spar
  > RIGHT WING REAR SPAR AT IRSS 183, CORROSION ON AFT SPAR, FOUND ON REMOVAL OF BONDING JUMPER REPLACEMENT, THE LOWER BONDING POINT. ACCOMPLISHED ON EA F-5710-T0326498, DATED AUG 02,2016. WINGS BASIC WING STRUCTURE, RT REAR SPAR WEB CORROSION AT IRSS 183, REF: F
- [SDR FDEA201609063122](https://openairdocs.org/sdr/FDEA201609063122.md): Panel · delaminated · Sep 6, 2016 · N781FD · Boeing 757222 · Vertical Stabilizer Miscellaneous Structure
  > DELAMINATION ON VERTICAL STABILIZER, LEFT SIDE ADJACENT TO L/E PANEL 321CL. DELAMINATION ON VERTICAL STABILIZER PANEL, LT SIDE FOUND TO BE OUT OF LIMITS IAW SRM 55-30-01-1A, FIG 101, NOTE K AND SRM 51-70-10-2R. R & R PANEL 175N2001-3 WITH O/H PANEL 175N2001-
- [SDR FDEA201608232957](https://openairdocs.org/sdr/FDEA201608232957.md): Shear Tie · corroded · Aug 23, 2016 · N781FD · Boeing 757222 · Fuselage Internal Mounting Structure
  > AFT CARGO BS 1620, ONE SHEAR TIE CORRODED, STRINGER 29R. REMOVED THE CORROSION IAW SRM 51-10-02-0G, FOUND NO ALLOWABLE DAMAGE IN SRM. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02-0G, MAJOR REPAIR.
- [SDR FDEA201608192942](https://openairdocs.org/sdr/FDEA201608192942.md): Stringer · corroded · Aug 19, 2016 · N781FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > MCD BS 438, STG CORRODED AT 5L. REPAIRED STR 5L, STA 410-440, IAW-SRM-53-00-53-2R, SHEET 6, DETAIL I, FOUND TO BE OUT OF LIMITS IAW SRM-53-00-03-1A, FIG 101, SHEET 1, CAT-A, MAJOR REPAIR.
- [SDR FDEA201608192941](https://openairdocs.org/sdr/FDEA201608192941.md): Aileron · damaged · Aug 19, 2016 · N781FD · Boeing 757222 · Ailerons
  > LT AILERON UPPER COAT INBD SIDE CHIPPED COMPOSITE. LT AILERON REPAIRED AS REQUIRED IAW-SRM-51-70-04 PARA. 5G, FIG 9, AILERON REBALANCE ACCOMPLISHED ON NR N00658, FOR WEIGHT ADDED AT REPAIR, DAMAGE LOCATION, WING STA 670.266-673.266, PN:113N7100-64, SN:32942

Next page: https://openairdocs.org/aircraft/N781FD/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 = 'N781FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N781FD/reports

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