# Service difficulty reports: N913FD

A list on [N913FD](https://openairdocs.org/aircraft/N913FD.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 4 · 184 reports

- [SDR FDEA202504020553](https://openairdocs.org/sdr/FDEA202504020553.md): Floor Support · misaligned · Apr 2, 2025 · N913FD · Boeing 75728A · Fuselage Main, Floor Beam
  > STA. 580 TO 600 LBL 45.5 BLOW OUT PANEL STRUCTURE IS MISSALIGNED. ACCOMPLISHED WITH EA# F5330-T0382716 P1, TITLE "FUSELAGE-FLOOR BEAMS REPAIR OF MISALIGNED FASTENER HOLES ON BLOWOUT PANEL STRUCTURE AT 580 AND 600 LBL 45.5" MAJOR REPAIR.
- [SDR FDEA202504020552](https://openairdocs.org/sdr/FDEA202504020552.md): Frame · damaged · Apr 2, 2025 · N913FD · Boeing 75728A · Fuselage Main, Frame
  > CABIN R/H FRAME HAS A FASTENER SHEARED AND THE HOLE IS ELONGATED AT STA 1640, BETWEEN STR 8R-9R DOT# 3521. ACCOMPLISHED REPAIR ON EA# F-5310-T0382395 P1 "FUSELAGE -MAINFRAME-STA1640, S-8R AND S-9R, FASTENER HEAD BROKE OFF AND MISSING, HOLE FOUND TO HAVE BE
- [SDR FDEA202503290537](https://openairdocs.org/sdr/FDEA202503290537.md): Skin · not reported · Mar 29, 2025 · N913FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING GVI OF STRINER S-14L LAP SPLICE ON EO F-5330-E0344603 P1 STEP 3.A A SKIN REPAIR DOUBLER WAS FOUND INSTALLED AT STA. 1600-STA 1620 STRINGER S-12L TO S-14L ACCOMPLISHED WITH REPAIR ON EA F-5330-T0382552 P1 FUSELAGE-PLATES & SKINS-STA1600
- [SDR FDEA202503280530](https://openairdocs.org/sdr/FDEA202503280530.md): Skin · corroded · Mar 28, 2025 · N913FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > (DOT 38-24) RH LOWER FUSELAGE SKIN CORRODED STA 1788 APPROX 4" AREA, 3" ABOVE THE APU RH DOOR CUTOUT. COMPLIED WITH REPAIR ON EA F-5330-T0382463 P1 FUSELAGE-PLATES & SKINS-SKIN REPAIRS AT STA 1885 RHS AND STRINGER S-17R FOR CORROSION MAJOR REPAIR
- [SDR FDEA202503240484](https://openairdocs.org/sdr/FDEA202503240484.md): Seat Track · corroded · Mar 24, 2025 · N913FD · Boeing 75728A · Fuselage, Seat/Cargo Attach Fittings
  > MCD SEAT TRACK RBL 47.5 I/B FLANGE HAS CORROSION AT STA. 1460 AND 1520 REMOVED AND REPLACED DAMAGE SEAT TRACK FROM BS 1420 TO BS 1520 AT RBL 47.5 ON MATERIAL P/N BAC1520-792 BATCH # 0004362542 AND REPAIR SPLICE P/N; BAC1509-100449 BATCH # 0004189129 IAW SR
- [SDR FDEA202503220474](https://openairdocs.org/sdr/FDEA202503220474.md): Seat Track · corroded · Mar 22, 2025 · N913FD · Boeing 75728A · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 58.22 HAS CORROSION AT STA 1108, 1140, 1170, AND 1180- DOT 45-048 REMOVED AND REPLACED SEAT TRACK AT MAIN DECK, FROM STA 900 TO STA 1180 IAW SRM 51-40- 02 & 53-00-52-2R, PART MARKED IAW GMM 07-0-1001 MAJOR REPAIR
- [SDR FDEA202503200464](https://openairdocs.org/sdr/FDEA202503200464.md): Strap · corroded · Mar 20, 2025 · N913FD · Boeing 75728A · Fuselage Miscellaneous Structure
  > DOT 80-021 AFT CARGO COMPARTMENT F/S 1380-1460 CEILING AREA RH SIDE FLOOR BEAM STABILIZATION STRAP CORRODED. REMOVED AND REPLACED STABILIZATION STRAP AFT CARGO COMPARTMENT STA 1380-1540 IAW SRM 53-00-51-2R AND IAW SRM 51-40-02. FABRICATED STABILIZATION STR
- [SDR FDEA202503150428](https://openairdocs.org/sdr/FDEA202503150428.md): Floor Panel · delaminated · Mar 15, 2025 · N913FD · Boeing 75728A · Fuselage Floor Panel
  > (DOT 38-31) MDC FLOOR PANEL 252MTF DELAMINATED BS1620-1640 RBL58.22 FABRICATED FLOOR PANEL 252 MTF ZONE 250 ON VTMAE TRAVELER #T25/1804424 IAW MAE DWG PL11864182 MAJOR REPAIR
- [SDR FDEA202503150427](https://openairdocs.org/sdr/FDEA202503150427.md): Floor Panel · damaged · Mar 15, 2025 · N913FD · Boeing 75728A · Fuselage Floor Panel
  > FLOOR PANEL 232 MJF DAMAGED FABRICATED FLOOR PANEL 232 MJF ZONE 230 ON VTMAE TRAVELER #T25/1802791 IAW MAE DWG 11862181 REV. L MAJOR REPAIR
- [SDR FDEA202503150426](https://openairdocs.org/sdr/FDEA202503150426.md): Floor Panel · damaged · Mar 15, 2025 · N913FD · Boeing 75728A · Fuselage Floor Panel
  > FLOOR PANEL 252 MSF DAMAGED FABRICATED FLOOR PANEL 252 MSF ZONE 250 ON VTMAE TRAVELER #T25/1802794 IAW MAE DWG PL 11864182 MAJOR REPAIR
- [SDR FDEA202503140416](https://openairdocs.org/sdr/FDEA202503140416.md): Floor Panel · damaged · Mar 14, 2025 · N913FD · Boeing 75728A · Fuselage Floor Panel
  > FLOORBOARD 242MHF AT STA 1019 RBL 64.2 HAS INSERT PULLED OUT WITH SCREW STILL IN THE FLOOR STRUCTURE- DOT 45-045 FABRICATED FLOOR PANEL 242MHF ZONE 240 ON VTMAE TRAVELER #T25/1802598 IAW MAE DWG #PL11863182 REV A, MAJOR REPAIR, FASTENER REMOVED IAW SRM 51-
- [SDR FDEA202503140415](https://openairdocs.org/sdr/FDEA202503140415.md): Floor Panel · damaged · Mar 14, 2025 · N913FD · Boeing 75728A · Fuselage Floor Panel
  > FLOORBOARD PANEL 242MAF HAS INSERT PULLED OUT AND FASTENER STILL IN FLOOR STRUCTURE- DOT 45-048 FABRICATED FLOOR PANEL 242MAF ZONE 240 ON VTMAE TRAVELER #T25/1802793 IAW MAE DWG PL11863182 MAJOR REPAIR, FASTENER REMOVED IAW SRM 51-40-02-OG.
- [SDR FDEA202503140414](https://openairdocs.org/sdr/FDEA202503140414.md): Floor Panel · damaged · Mar 14, 2025 · N913FD · Boeing 75728A · Fuselage Floor Panel
  > FLOOR PANEL 222 BF DAMAGED FABRICATED FLOOR PANEL 222BF ZONE 220 ON VTMAE TRAVLER #T25/1802961 IAW BOEING DWG PL141N5361 REV. BC, MAJOR REPAIR
- [SDR FDEA202503140413](https://openairdocs.org/sdr/FDEA202503140413.md): Floor Panel · damaged · Mar 14, 2025 · N913FD · Boeing 75728A · Fuselage Floor Panel
  > FLOORBOARD PANEL 241MPF HAS PULLED INSERT- DOT 45-052 FABRICATED FLOOR PANEL 241MPF ZONE 240 ON VTMAE TRAVELER #T25/1802792 IAW MAE DWG PL11863182, MAJOR REPAIR.
- [SDR FDEA202412131800](https://openairdocs.org/sdr/FDEA202412131800.md): Warning Message · false activation · Dec 13, 2024 · N913FD · Boeing 75728A · Trailing Edge Flap Control System
  > ON FINAL (RWY 27 KMEM) 170 KIAS 1200AGL, FLAPS 20 TO 25, GEAR DOWN GOT TE FLAP DISAGREE EICAS. EXECUTED GO AROUND, RAN QRH, LANDED WITHOUT INCIDENT EMERGENCY DECLARED. PERFORMED PER 757 STEPS IN FIM 27-51 FAULT TREE 808. NO FAULTS FOUND AT THIS MOMENT. NO
- [SDR FDEA202304170800](https://openairdocs.org/sdr/FDEA202304170800.md): Floorbeam · cracked · Apr 17, 2023 · N913FD · Boeing 757200 · Fuselage Structure (General)
  > FOUND CRACK ON FLOOR BEAM AT STA 580 AT LBL 45 ON UPPER FLANGE LOWER AREA WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A# F-5310-T0374058-FLOOR BEAM AT STA 580 AND LBL 45- CRACKED-REPAIR PER DRAWING SR 57-53-004-TRACKING MAJOR REPAIR
- [SDR FDEA202304160703](https://openairdocs.org/sdr/FDEA202304160703.md): Flap · damaged · Apr 16, 2023 · N913FD · Boeing 757200 · Wing Structure
  > R/H WING INBD FLAP INNER SIDE NEAR MIDDLE SUPPORT HAS A SMALL HOLE "1/4 PERFORMED WET LAYUP REPAIR FOR MENTIONED AREA OF MAIN FLAP PER SRM 51-70-06,PARAGRAPH 5.B. REF. SRM 57-53-01-2R,FIG.201, DETAIL I,TABLE III.REP. DIM.: 5.5" X 5.5". REP. LOC.: 4" FROM T
- [SDR FDEA202211302865](https://openairdocs.org/sdr/FDEA202211302865.md): Bulb · inoperative · Nov 30, 2022 · N913FD · Boeing 75728A · Emergency Lighting
  > L1 DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. BULB REPLACED IAW AMM 33-51-06-2-1, REV 130.9, X1.
- [SDR FDEA202211152785](https://openairdocs.org/sdr/FDEA202211152785.md): Bearing · misaligned · Nov 15, 2022 · N913FD · Boeing 75728A · Cargo/Baggage Doors
  > AFTER LOADING, UNABLE TO LOCK MAIN CARGO DOOR, ONLY THE FWD CAM IS LOCKED, AFT CAM WOULD NOT MOVE. AMM: 52-32-00-5 DURING INSPECTION OF THE HOOK PIN, FOUND MISALIGNEMENT BETWEEN BOTH BEARING HOUSINGS, CAUSING POINT OF CONTACT AT WRONG LOCATION AND BLOCKING TH
- [SDR FDEA202206291618](https://openairdocs.org/sdr/FDEA202206291618.md): Lamp · inoperative · Jun 29, 2022 · N913FD · Boeing 757200 · Cargo Compartment Lighting
  > FOUND ARM/DISARM LIGHT SWITCH BULB INOP. RELAMPED ARM/DISARM LIGHT SWITCH FROM P82 PANEL AS PER AMM 33-30-00-0. OPN CHECK GOOD. OK FOR FURTHER SERVICE.
- [SDR FDEA202203230764](https://openairdocs.org/sdr/FDEA202203230764.md): Flap · dented · Mar 23, 2022 · N913FD · Boeing 757200 · Trailing Edge Flaps
  > L/H WING OUTBD AFT FLAP FOUND SMALL DENT ON LOWER SURFACE CLOSE TO OUTBD END WITH ON DELAMINATION SIGHN PERFORMED WET LAYER REPAIR FOR MENTIONED AREA PER SRM 51-70-03, PAR. 5L REF. SRM 57-53-01-2R-1 REPAIR 1 FIG. 201 DETAIL 4, TABLE 2. REP. DIM.: 4" REP
- [SDR FDEA202203210912](https://openairdocs.org/sdr/FDEA202203210912.md): Seat Track · corroded · Mar 21, 2022 · N913FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON SEAT TRACK UPPER FLANGE AT STA 880-860 AT RBL 45 WORK ACCOMPLISHED PER FEDEX E.A # F-5310-T0367599 CRACKED SEAT TRACK BTWN STA 860-880 LBL/RBL 45.50, ALTERNATE MATERIAL REQUEST FOR SRM REPAIR. MAJOR REPAIR.
- [SDR FDEA202203210911](https://openairdocs.org/sdr/FDEA202203210911.md): Seat Track · none · Mar 21, 2022 · N913FD · Boeing 757 · Fuselage Structure (General)
  > FOUND MISSING PIECES OF UPPER FLANGE OF SEAT TRACK BETWEEN STA 880-860 AT LBL 45 WORK ACCOMPLISHED PER FEDEX E.A #F-5310-T0367599 CRACKED SEAT TRACK BTWN ST A860-880 LBL/RBL 45.50, ALTERNATE MATERIAL REQUEST FOR SRM REPAIR. MAJOR REPAIR
- [SDR FDEA202202240930](https://openairdocs.org/sdr/FDEA202202240930.md): Floorbeam · corroded · Feb 24, 2022 · N913FD · Boeing 75728A · Fuselage Structure (General)
  > FOUND CORROSION ON FLOOR BEAM UPPER T-CHORD AT STA 880 BETWEEN RBL 45-68 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A #F-5310-T0367576 B, FLOOR BEAM ASSY, STA 879, UPPER CHORD, BL 45-68, CORROSION, REPAIR MAJOR REPAIR.
- [SDR FDEA202202240929](https://openairdocs.org/sdr/FDEA202202240929.md): Floorbeam · corroded · Feb 24, 2022 · N913FD · Boeing 75728A · Standard Practices/Structures
  > CORROSION WERE FOUND ON FLOOR BEAM UPPER T-CHORD LOCATED STA 880 LBL 45-60 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0367576 B, FLOOR BEAM ASSY, STA 879, UPPER CHORD, BL 45-68 CORROSION, REPAIR. MAJOR REPAIR
- [SDR FDEA202202240834](https://openairdocs.org/sdr/FDEA202202240834.md): Floorbeam · corroded · Feb 24, 2022 · N913FD · Boeing 757200 · Fuselage Main, Floor Beam
  > CORRODED FLOOR BEAM UPPER T-CHORD LOCATED STA 1200 LBL 35-LBL 50 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0367712: FLOOR BEAM AT STA 1200 BTWN LBL24.75-45.5, UPPER CHORD CORROSION, PERMANENT REPAIR MAJOR REPAIR
- [SDR FDEA202202240779](https://openairdocs.org/sdr/FDEA202202240779.md): Skin · none · Feb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/Structures
  > UNDOCUMENTED COMPOSITE REPAIR WERE FOUND ON SKIN EMPENNAGE STA 1981.9-1941 11 O'CLOCK POSITION PERFORMED TAP TEST INSP. PER SRM 51-10-06 AND EVALUATED I.A.W CASCADE AEROSPACE WORK CARD 07765 NR0408 AND NR0407 AND NO DAMAGE OR DEVIATIONS NOTED. FOR RECORD
- [SDR FDEA202202240778](https://openairdocs.org/sdr/FDEA202202240778.md): Skin · unknown · Feb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/Structures
  > UNDOCUMENTED COMPOSITE REPAIR WERE FOUND ON SKIN EMPENNSGE STA 1918.9-1941 12 O'CLOCK POSITION PERFORMED TAP TEST INSP PER SRM 51-10-06 AND EVALUATED I.A.W CASCADE AEROSPACE WORK CARD 07765 NR0408 AND NR0407 AND NO DAMAGE OR DEVIATION NOTED. FOR RECORD PU
- [SDR FDEA202202240767](https://openairdocs.org/sdr/FDEA202202240767.md): Skin · delaminated · Feb 24, 2022 · N913FD · Boeing 757200 · Wing Structure
  > FOUND CRACK AND DELAMINATION ON R/H WING LEADING EDGE SKIN UNDER SLAT #6 PERFORMED HOT BOND REPAIR FOR MENTIONED PANEL PER SRM 51-70-08, REF SRM 57-41-01- 2R, FIG.201 DETAIL I, TABLE II, REP. DIM.: 14"X27". REP. LOCATION: ISS 205.5 AND FROM FWD TO AFT ED
- [SDR FDEA202202240766](https://openairdocs.org/sdr/FDEA202202240766.md): Flap · none · Feb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/Structures
  > UNDOCUMENTED COMPOSITE REPAIR ON L/H WING OUTER AFT FLAP LOWER SURFACE 11" FROM AFT EDGE 105" FROM OUTBD EDGE PERFORMED WET LAYUP REPAIR FOR MENTIONED AREA PER SRM 51-70-17, REF SRM 57-53-01- 2R-1 REPAIR 1, FIG.201 DETAIL IV TABLE II REP.DIM: 4". REP. LOC
- [SDR FDEA202202240763](https://openairdocs.org/sdr/FDEA202202240763.md): Skin · unknown · Feb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/Structures
  > UNDOCUMENTED COMPOSITE REPAIR WERE FOUND ON STA 1963.8-1992.8 STR 6 O'CLOCK POSITION PERFORMED HOT BOND REPAIR PER SRM 51-70-10-2R, REF. SRM 53-80-01-2R, DETAIL 1. REP. DIM:5.5" REF. LOCATION: 6.5" FROM FWD EDGE OF PANEL AT 6 O'CLOCK. MAJOR REPAIR
- [SDR FDEA202202240741](https://openairdocs.org/sdr/FDEA202202240741.md): Seat Track · corroded · Feb 24, 2022 · N913FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPE CORROSION WERE FOUND ON SEAT TRACK LOCATED STA 1180-1420 LBL 58 WORK ACCOMPLISHED PER FEDEX E.A # F-5300-T0367321. SEAT TRACK BTWN STA 1180-1420, LBL 58.22, CORROSION, PERMANENT REPAIR. MAJOR REPAIR
- [SDR FDEA202202240740](https://openairdocs.org/sdr/FDEA202202240740.md): Seat Track · cracked · Feb 24, 2022 · N913FD · Boeing 75728A · Standard Practices/Structures
  > CRACK ON SEAT TRACK LOCATED STA1580-1600 RBL 45 WORK ACCOMPLISHED PER FEDEX E.A # F-5300-T0367320: SEAT TRACK AT STA 1580-1600 RBL 58.22, CRACK, PERMANENT REPAIR MAJOR REPAIR
- [SDR FDEA202202240708](https://openairdocs.org/sdr/FDEA202202240708.md): Channel · unknown · Feb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/Structures
  > UNDOCUMENTED REPAIR WERE FOUND ON 2 CHANNEL LOCATED STA 1380-1400 RBL 11 PERFORMED NEW SRM REPAIR PER SRM 53-60-52-2R, AND PER SRM 51-70-12 TYPICAL EXTRUDED REPAIR, THIS REPAIR IS A CAT. A REPAIR AND NO SUPPLIMENTAL INSP. ARE REQUIRED. MAJOR REPAIR
- [SDR FDEA202202240707](https://openairdocs.org/sdr/FDEA202202240707.md): Seat Track · corroded · Feb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/Structures
  > CORROSION ON SEAT TRACK LOCATED STA 1540 LBL 45.5 PERFORMED SEAT TRACK REPAIR USING NEW SEAT TRACK SECTION, 2 EA ANGLES, AND STRAP PER SRM 53-00-52, FIG 201, REPAIR 1. THIS REPAIR IS A CATEGORY "A" REPAIR AND NO SUPPLEMENTARY INSP. ARE REQUIRED
- [SDR FDEA202202240642](https://openairdocs.org/sdr/FDEA202202240642.md): Channel · unknown · Feb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/Structures
  > UNDOCUMENTED SPLICE REPAIR WERE FOUND ON Z-CHANNEL OF FWD CARGO FLOOR STRUCTURE LOCATED STA 560-580 RBL 29 PERFORMED DVI PER SRM 51-10-08 AND EVALUATED I.A.W SRM 51-70-12 AND NO DAMAGE OR DEVIATIONS NOTED THIS IS A MAJOR REPAIR
- [SDR FDEA202202240641](https://openairdocs.org/sdr/FDEA202202240641.md): Channel · corroded · Feb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/Structures
  > UNDOCUMENTED SPLICE REPAIR WERE FOUND ON Z-CHANNEL OF FWD CARGO FLOOR STRUCTURE LOCATED STA 560-580 LBL 8 PERFORMED DVI PER SRM 51-10-08 AND EVALUATED I.A.W SRM 51-70-12 AND NO DAMAGE OR DEVIATION NOTED. THIS IS A MAJOR REPAIR
- [SDR FDEA202202240640](https://openairdocs.org/sdr/FDEA202202240640.md): Seat Track · corroded · Feb 24, 2022 · N913FD · Boeing 757200 · Fuselage Structure (General)
  > FOUND CORROSION ON SEAT TRACK UPPER CROWN AT STA 345-377 LBL 7 DAMAGED PART REMOVED AN NEW FABRICATED SEAT TRACK PER FEDEX EA # F-5310-T0367282 SUPERNUMERARY SEAT TRACK MATERIAL SUBSTITUTION, AND VENTURA PRODUCTION DWG INSTALLED PER SRM 51-40-02
- [SDR FDEA202202240639](https://openairdocs.org/sdr/FDEA202202240639.md): None · none · Feb 24, 2022 · N913FD · Boeing 757200 · Standard Practices/Structures
  > MULTIPLE CORROSION ON SEAT TRACK BETWEEN STA 1280-1320 RBL 45 PERFORMED SEAT TRAK REPLACEMENT USING A NEW FABRICATED SEAT TRACK PER SRM 53- 00-52, FIG 201 REPAIR 1. AND FEDEX GMM 7-0-1001. THIS REPAIR IS A CATEGORY "A" REPAIR AND NO SUPPLEMENTARY INSP. AR
- [SDR FDEA202202240611](https://openairdocs.org/sdr/FDEA202202240611.md): Floorbeam · corroded · Feb 24, 2022 · N913FD · Boeing 757200 · Fuselage Main, Floor Beam
  > CORROSION ON EXISTING REPAIR UPPER T-CHORD LOCATED STA 1540 LBL 10 PERFORMED REPAIR TO ONE FLANGE OF THE FLOOR BEAM UPPER CHORD PER SRM 53-00-51-2R, FIG.201, REPAIR 5. THIS REPAIR IS A CAT. A REPAIR AND NO SUPPLEMENTAL INSPECTIONS ARE THIS IS MAJOR REPAI
- [SDR FDEA202202220742](https://openairdocs.org/sdr/FDEA202202220742.md): Beam · elongated · Feb 22, 2022 · N913FD · Boeing 75728A · Fuselage Floor Panel
  > FLOOR BEAM UPPER T CHORD STA 1681 FOUND WITH ELONGATED HOLE AT LBL 4 AND 2EA UNUSED HOLES AT RBL 12 PERFORMED AFT DECK AND FLOOR BEAM REPAIRS PER SRM 53-60-51-2R REPAIR 2, AND REPAIR 3, FIG 201. THE REPAIRS ARE CAT. A REPAIRS, AND NO SUPPLIMENTAL INSPECTI
- [SDR FDEA202202220610](https://openairdocs.org/sdr/FDEA202202220610.md): Skin · unknown · Feb 22, 2022 · N913FD · Boeing 757200 · Passenger/Crew Doors
  > FOUND UNDOCUMENTED DOUBLER REPAIR AT DOOR 4R INNER SKIN ADJACENT TO STR 10R PERFORMED DVI PER SRM 51-10-08 AND EVALUATED I.A.W EA F-5210-T0367359 AND NO DAMAGE OR DEVIATIONS NOTED THIS IS A MAJOR REPAIR
- [SDR FDEA202202220609](https://openairdocs.org/sdr/FDEA202202220609.md): Floorbeam · unknown · Feb 22, 2022 · N913FD · Boeing 757200 · Passenger/Crew Doors
  > FOUND UNDOCUMENTED UPPER T CHORD REPAIR AT STA 345 LBL 52-RBL52 PERFORMED DVI PER SRM 51-10-08 AND EVALUATED I.A.W SRM 53-00-51 AND MONARCH W/O 770838 NR AND NO DAMAGES OR DEVIATIONS FOUND FOR RECORDS PURPOSES ONLY
- [SDR FDEA202202170381](https://openairdocs.org/sdr/FDEA202202170381.md): Floor Panel · worn · Feb 17, 2022 · N913FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > FLOOR PANEL P/N 11861182-16 AT STA 300 R/H FOUND WORN FABRICATED PANEL IAW FEDEX SRZ-25-005, REF ENGINEERING DISPOCITION OF RFTA NO:02858-0204 P/N:N00236-T01-221MBF, B/N:20308927
- [SDR FDEA202202170380](https://openairdocs.org/sdr/FDEA202202170380.md): Floor Panel · worn · Feb 17, 2022 · N913FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > FLOOR PANEL P.N 11861182-15 AT STA 440 FOUND WORN FABRICATED THE PANEL IAW FEDEX SRZ-25-005, REF ENGINEERING DISPOSITION OF RFTA NO:02858-0204. P/N:N00236-T02-221MAF, B/N:20308931
- [SDR FDEA202202170379](https://openairdocs.org/sdr/FDEA202202170379.md): Floor Panel · worn · Feb 17, 2022 · N913FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > FLOOR PANEL P/N 141N5361-213 AT STA 440 FOUND WORN FABRICATED THE PANEL IAW FEDEX SRZ-25-005, REF ENGINEERING DISPOSITION OF RFTA NO:02858-0204 P/N:N00236-T03-221AF, B/N:20308935
- [SDR FDEA202201300913](https://openairdocs.org/sdr/FDEA202201300913.md): Skin · gouged · Jan 30, 2022 · N913FD · Boeing 757200 · Trailing Edge Flaps
  > EVALUATE EXISTING REPAIR AT L/H WING O/B MAIN FLAP L/E PER EO F-5100-7-5001 PERFORMED DVI PER SRM 51-10-08 AND GOUGE FOUND ON EXISTING REPAIR. NEW REPAIR PERFORMED I.A.W EA F-5750-T0367457. L/H WING O/B MAIN FLAP GOUGE ON EXISTING REPAIR ON L/E SKIN REPA
- [SDR FDEA202110312703](https://openairdocs.org/sdr/FDEA202110312703.md): Warning Message · false activation · Oct 31, 2021 · N913FD · Boeing 75728A · Rudder Tab Control System
  > ON FINAL AT 160-170 KNOTS, GOT RUDDER RATIO EICAS. HYDRAULIC PRESSURE WAS NORMAL. COMPLIED WITH QRH, AND DIVERTED DUE TO WIND LIMITATIONS. TROUBLELSHOOTING CARRIED OUT ON BOTH RRCM 'S FOUND MODULE FAULT BALL S SHOWING ON BOTH RRCM'S ACCOMPLISHED FIM 27-
- [SDR FDEA202107231845](https://openairdocs.org/sdr/FDEA202107231845.md): Girt Bar · dirty · Jul 23, 2021 · N913FD · Boeing 75728A · Emergency Equipment
  > FORWARD ENTRY DOOR WILL NOT ARM. DOOR 1RH GIRT BAR MECHANISM INSPECTION PERFORMED I.A.W. AMM 52-11-25-5. FLOOR FITTINGS INSPECTED AND CLEANED. GIRT BAR RIPOSITIONED IN CORRECT POSITION AND GIRT BAR LEVER CHECKED FOR PROPER OPERATION SEVERAL TIME, SATISFACT
- [SDR FDEA202104230996](https://openairdocs.org/sdr/FDEA202104230996.md): Sensor · dirty · Apr 23, 2021 · N913FD · Boeing 75728A · Emergency Equipment
  > RH DOOR SLIDE LIGHT INOP. DOOR 1R GIRT BAR PROXY SENSOR CLEANED. OPS TEST ACC AMM 25-66-11-2 REV 127.9 (SUBTASK 25-66-11-822-045 046) SATIS. DOOR 1R GIRT BAR PROXY SENSOR CLEANED. OPS TEST ACC AMM 25-66-11-2 REV 127.9 (SUBTASK 25-66-11-822-045 046) SAT

Next page: https://openairdocs.org/aircraft/N913FD/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 = 'N913FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N913FD/reports

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