# Service difficulty reports: N917FD

A list on [N917FD](https://openairdocs.org/aircraft/N917FD.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 · 195 reports

- [SDR FDEA202608211211](https://openairdocs.org/sdr/FDEA202608211211.md): Power Supply · faulted · Aug 21, 2026 · N917FD · Boeing 75723A · Emergency Lighting
  > R1 EMERGENCY EXIT LIGHT FAILS OPS TEST. PREMATURE REMOVAL/INSTALLATION OFF MPN: 2012-1. REPLACED BATTERY, NO HELP. REMOVED AND REPLACED POWER SUPPLY/TRAY ASSY AND INSTALLED NEW BATTERY, OPS CHECKS NORMAL. OK TO CONTINUE. CHARGER/TRAY REMOVED P/N 201
- [SDR FDEA202607100886](https://openairdocs.org/sdr/FDEA202607100886.md): Lanyard · out of position · Jul 10, 2026 · N917FD · Boeing 75723A · Emergency Exits
  > DURING PREFIGHT FOUND R-1 DOOR WILL NOT ARM. DOOR IS LOCKED AND INDICATED. AMM: 25-66-01-4 FOUND R1 PASSENDER DOOR STATIC LINE CAUGHT IN PUSHROD. REROUTED CARBINER STATIC LINE NO DEFECTS NOTED. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA202604030397](https://openairdocs.org/sdr/FDEA202604030397.md): Skin · dented · Apr 3, 2026 · N917FD · Boeing 75723A · Trailing Edge Flaps
  > R/WING O/B T/E MAIN FLAP LOWER SURFACE HAS A DENT PANEL ASSY SKIN OUTER PLY THIS ITEM HAS BEEN ACCOMPLISHED ON EA F-5750-T0386919.
- [SDR FDEA202604020393](https://openairdocs.org/sdr/FDEA202604020393.md): Frame · cracked · Apr 2, 2026 · N917FD · Boeing 75723A · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT WC EF 530-E0329085 D P6 MAIN FRAME BODY STATION 1640 FUSELAGE FRAME INSPECTION FOUND MISSING INTERNAL STRAP IN FRAME AT BS 640 BETWEEN STR 13R TO STR 17R THIS ITEM HAS BEEN ACCOMPLISHED ON FEDEX EA # F-5310-T0353582 TITLE: "FUSELAGE-
- [SDR FDEA202602110171](https://openairdocs.org/sdr/FDEA202602110171.md): Flex Line · leaking · Feb 11, 2026 · N917FD · Boeing 75728A · Hydraulic System, Main
  > ON APPROACH EXTENDING MLG & FLAPS TO 20, LT HYD QTY EICAS & COMPLETE LOSS OF LT SYS HYD FLUID. MAINTAINED CONFIGURATION & COMPLETED LT HYD QTY QRH PROCEDURE PRIOR TO LANDING. EMERGENCY DECLARED AMM 12-12-01, AMM 29-11-17-4, FOUND FLEX LINE CONNECTED TO SWI
- [SDR FDEA202406230855](https://openairdocs.org/sdr/FDEA202406230855.md): Battery Pack · failed · Jun 23, 2024 · N917FD · Boeing 75723A · Emergency Lighting
  > DURING SVC FOUND THE L1 INSIDE AND OUT EMERGENCY LIGHTS WERE INOP. REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK AS REQUIRED IAW AMM 33-51-07-2. OPS CHECK GOOD.
- [SDR FDEA202403220346](https://openairdocs.org/sdr/FDEA202403220346.md): Hinge Fitting · cracked · Mar 22, 2024 · N917FD · Boeing 75723A · Fuselage, Door Hinge
  > DURING ROTO INSPECTION OF LH STA 1640 S-14L. A CRACK INDICATION WAS NOTED IN OUTBD UPPER HOLE AT 2 O'CLOCK (VIEW LOOKING AFT) REMOVED AND REPLACED WITH NEW HINGE FITTING #146N8762-17 AT STA 1640 LH IAW WITH EA F-5310-T0378328 PT1 FUSELAGE - MAINFRAME - ST
- [SDR FDEA202403210338](https://openairdocs.org/sdr/FDEA202403210338.md): Floorboard · damaged · Mar 21, 2024 · N917FD · Boeing 75723A · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD PANEL 232MJF DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 232MJF ON VT MAE TRAVELER T24/1738386 IAW DWG SRZ-25-005 REVISION "R" MAJOR REPAIR
- [SDR FDEA202403210332](https://openairdocs.org/sdr/FDEA202403210332.md): Floorboard · damaged · Mar 21, 2024 · N917FD · Boeing 75723A · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD PANEL 252MUF BROKEN. FABRICATED ZONE 250 FLOORBOARD PANEL 252MUF ON VT MAE TRAVELER T24/1738390 IAW DWG SRZ-25-005 REVISION "R" MAJOR REPAIR.
- [SDR FDEA202403210331](https://openairdocs.org/sdr/FDEA202403210331.md): Floorboard · damaged · Mar 21, 2024 · N917FD · Boeing 75723A · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD PANEL 251MUF DAMAGED. FABRICATED ZONE 250, 251MUF FLOORBOARD PANEL ON VT MAE TRAVELER T24/1738388 IAW DWG SRZ 25-005 REV "R" MAJOR REPAIR
- [SDR FDEA202403140289](https://openairdocs.org/sdr/FDEA202403140289.md): Floor Panel · damaged · Mar 14, 2024 · N917FD · Boeing 75723A · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD PANEL 231MEF DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 231MEF ON VT MAE TRAVELER # T24/1738374 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR.
- [SDR FDEA202403140288](https://openairdocs.org/sdr/FDEA202403140288.md): Floor Panel · damaged · Mar 14, 2024 · N917FD · Boeing 75723A · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD PANEL 231MFF DAMAGED FABRICATED ZONE 230 FLOORBOARD PANEL 231MFF ON VT MAE TRAVELER # T24/1738381 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR
- [SDR FDEA202403140287](https://openairdocs.org/sdr/FDEA202403140287.md): Floor Panel · damaged · Mar 14, 2024 · N917FD · Boeing 75723A · Fuselage Floor Panel
  > ZONE 220 COURRIER FLOORBOARD 221BF DAMAGED FABRICATED ZONE 220 FLOORBOARD 221BF ON VT MAE TRAVELER # T24/1738060 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIR
- [SDR FDEA202403140286](https://openairdocs.org/sdr/FDEA202403140286.md): Floor Panel · damaged · Mar 14, 2024 · N917FD · Boeing 75723A · Fuselage Floor Panel
  > ZONE 220 COURIER FLOORBOARD 221MBF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 221MBF ON VT MAE TRAVELER # T24/1738161 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR
- [SDR FDEA202403140285](https://openairdocs.org/sdr/FDEA202403140285.md): Floor Panel · damaged · Mar 14, 2024 · N917FD · Boeing 75723A · Fuselage Floor Panel
  > ZONE 220 COURIER FLOORBOARD 222MAF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 222MAF ON VT MAE TRAVELER # T24/1738162 IAW DRAWING SRZ-25-005 REVISION R MAJOR REPAIR
- [SDR FDEA202309231639](https://openairdocs.org/sdr/FDEA202309231639.md): Controller · failed · Sep 23, 2023 · N917FD · Boeing 75723A · Cabin Pressure Controller
  > LOST CABIN PRESSURE DESCENDING THROUGH APPROX FL 280. RECEIVED CABIN ALTITUDE WARNING MESSAGE. CABIN ALTITUDE SHOWED 10,000 & CLIMBING AT 500 FT/MIN. EMERGENCY DECLARED & DESCENDED RAPIDLY TO 10,000 FT, NORMAL RATE TO 5,000. WHILE LEVEL AT 5,000 FT, CABI
- [SDR FDEA202305090834](https://openairdocs.org/sdr/FDEA202305090834.md): Microphone · faulted · May 9, 2023 · N917FD · Boeing 75723A · HF Communications System
  > LEFT RADIO TRANSMITS INTERMITTENTLY. WHEN ATC IS ABLE TO HEAR THE TRANSMISSION THEY REPORT ONLY BEING ABLE TO HEAR 3 BY 5. A LOUD STATIC ACCOMPANIES EVERY TRANSMISSION. REF. FRM FIM 23-12 FT 802 FOR VHF COMMUNICATIONS TRANSCEIVER BITE PROCEDURE / L VHF
- [SDR FDEA202212263019](https://openairdocs.org/sdr/FDEA202212263019.md): Metering Valve · failed · Dec 26, 2022 · N917FD · Boeing 75723A · Landing Gear Brake System
  > RT HYD QTY EICAS MESSAGE IN FLIGHT, FOLLOWED BY RT HYD ENGINE PUMP EICAS MESSAGE, FOLLOWED BY RT HYD SYS PRESS MESSAGE. EMERGENCY DECLARED. CHECKED BOTH ANTI-SKID SHUTTLE IAW AMM: 29-11-24-4. REMOVED RT HYD RESERVOIR PRESSURE RELIEF VALVE IAW MM 29-11-24-4
- [SDR FDEA202209052207](https://openairdocs.org/sdr/FDEA202209052207.md): Socket · failed · Sep 5, 2022 · N917FD · Boeing 75723A · Emergency Equipment
  > AT BLOCK IN THE SLIDE ARM LIGHT ON DOOR L1 IS BURNT OUT. SERVICED L1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT WITH NEW BULB WITH NO HELP. TRIED WITH THE LENS & BULB HOLDER OF THE OTHER SIDE WITH NO HELP. CONFIRMED GOOD ADJUSTEMENT OF THE GIRT BAR & ITS ASSO
- [SDR FDEA202205181242](https://openairdocs.org/sdr/FDEA202205181242.md): Floor Panel · damaged · May 18, 2022 · N917FD · Boeing 757200 · Fuselage Floor Panel
  > FOUND DAMAGE ON FLOOR PANEL AT POS. 11RON STA 1300 RBL 55.00 SEE JOBCDID ON 53211717 PERFORMED PERMANENT REPAIR PER SRM 53-00-50-2R, PARAGRAPH 3.C,FIG/ 201. REV. 135.0. REPAIR MATERIAL P/N: BMS 8-301,CL. 2. B/N:0001285056. MAJOR REPAIR.
- [SDR FDEA202205031336](https://openairdocs.org/sdr/FDEA202205031336.md): Seat Track · corroded · May 3, 2022 · N917FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON SEAT TRACK RBL 24 BETWEEN STA 1520-1540 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52, FIG.201 REPAIR 1
- [SDR FDEA202204261333](https://openairdocs.org/sdr/FDEA202204261333.md): None · none · Apr 26, 2022 · N917FD · Boeing 757200 · Standard Practices/Structures
  > SUSPECTED REPAIR/SPLICE OUTER CREASE BEAM R/H STA 1400-1420 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.O # F-5310-T0368544, CREASE BEAM OUTBOARD CHORD, STA 1400-1420, S-17R, EXISTING UNAPPROVED REPAIR, PERMANENT REPAIR. MAJOR REPAIR
- [SDR FDEA202204261326](https://openairdocs.org/sdr/FDEA202204261326.md): None · none · Apr 26, 2022 · N917FD · Boeing 757200 · Standard Practices/Structures
  > UNDOCUMENTED EXISTING REPAIR ON L/H WING INBD FLAP OUTBD TRAILING EDGE LWR SKIN ADJACENT NO 5 SPOILER PERFORMED WORK STEPS PER EA 000710. MAJOR REPAIR.
- [SDR FDEA202204261325](https://openairdocs.org/sdr/FDEA202204261325.md): None · none · Apr 26, 2022 · N917FD · Boeing 757200 · Standard Practices/Structures
  > UNDOCUMENTED EXISTING REPAIR ON L/H WING INBD MAIN FLAP LWR SKIN APPROX WS 231.5 PERFORMED WORK STEPS PER EA 000711
- [SDR FDEA202204261302](https://openairdocs.org/sdr/FDEA202204261302.md): None · none · Apr 26, 2022 · N917FD · Boeing 757200 · Standard Practices/Structures
  > UNDOCUMENTED EXISTING REOAIR/SPLICE AT AFT CARGO STA 1540-1560 RBL 13 THIS REPAIR COMPLY WITH SRM 53-60-53-2R, NO DAMAGE OR DEVIATIONS NOTED, AND PERFORMED REPAIR ASSESSMENT PER E.O F-5100-7-5001. MAJOR REPAIR
- [SDR FDEA202204261301](https://openairdocs.org/sdr/FDEA202204261301.md): None · none · Apr 26, 2022 · N917FD · Boeing 757200 · Standard Practices/Structures
  > SUSPECTED REPAIR ON APU FIREWALL AT STA 1885.2 UPPER PART (APU SUPPORT STRUT L/H SIDE) THE REPAIR COMPLY WITH SRM 53-80-08-2R, NO DAMAGE OR DEVIATION NOTED, AND REPAIR EVALUATED PER EO F-5100-7-5001. MAJOR REPAIR
- [SDR FDEA202204261300](https://openairdocs.org/sdr/FDEA202204261300.md): None · none · Apr 26, 2022 · N917FD · Boeing 757200 · Standard Practices/Structures
  > UNDOCUMENTED EXISTING REPAIR ON APU FIRE WALL AT STA 1885.2 LWR PART THIS REPAIR COMPLY WITH SRM 53-80-08-2R, AND NO DAMAGE OR DEVIATIONS NOTED, AND REPAIR ASSESSMENT PERFORMED PER E.O F-5100-7-5001. MAJOR REPAIR
- [SDR FDEA202204261238](https://openairdocs.org/sdr/FDEA202204261238.md): Skin · dented · Apr 26, 2022 · N917FD · Boeing 757200 · Elevator, Plate/Skin
  > FOUND DENT ON ELEVATOR R/H SIDE LWR SKIN, SIZE: D=0.0130" L=0.839" W=0.691" PERFORMED REPAIR PER SRM 51-70-17,REF. SRM 55-20-01-2R,FIG. 201,TABLE I.REV. 135.0,17/1/22.REP. DIM.:5,5". REP LOC.:17"FROM AFT EDGE AND AT ELEV STA 74. MATERIAL P/N: EA9390,B/N:
- [SDR FDEA202204261233](https://openairdocs.org/sdr/FDEA202204261233.md): Skin · dented · Apr 26, 2022 · N917FD · Boeing 757200 · Horizontal Stabilizer Structure
  > FOUND DENT ON HORIZONTAL STABILAIZER R/H SIDE LWR SKIN, SIZE: D=0.0231" L=2.79" W=2.46" PERFORMED HOT BOND REPAIR PER SRM 51-70-10,REPAIR 4,REF. SRM 55-10-01-1A,FIG. 101,DETAIL I,TABLE I,NOTE I. REP. DIM.: 5.5".REP. LOC.:56" FROM I/B AND 3.5" FROM AUXI
- [SDR FDEA202204261232](https://openairdocs.org/sdr/FDEA202204261232.md): Skin · none · Apr 26, 2022 · N917FD · Boeing 757200 · Standard Practices/Structures
  > UNDOCUMENTED EXISTING REPAIR BETWEEN STA 1918.9-1941 LBL 7" DIMENSION 4.5"-5.0" PERFORMED DVI INSPECTION PER SRM 51-10-08 AND TAP TEST PER SRM 51-10-06, FOUND EXISTING REPAIR WITHIN GOOD CONDITION AND PERFORMED PER SRM 51-70-10-2R.REF. SRM 53-80-01-2R REV.
- [SDR FDEA202204261231](https://openairdocs.org/sdr/FDEA202204261231.md): Skin · none · Apr 26, 2022 · N917FD · Boeing 757200 · Fuselage Structure (General)
  > UNDOCUMENTED EXISTING REPAIR BETWEEN STA 1918.9-1941 LBL 16.5" DIMENSION 4.0"-4.3" PERFORMED DVI INSPECTION PER SRM 51-10-08 AND TAP TEST PER SRM 51-10-06, FOUND EXISTING REPAIR WITHIN GOOD CONDITION AND PERFORMED PER SRM 51-70-10-2R. REF. SRM 53-80-01-2R.
- [SDR FDEA202204261230](https://openairdocs.org/sdr/FDEA202204261230.md): Skin · none · Apr 26, 2022 · N917FD · Boeing 757200 · Standard Practices/Structures
  > UNDOCUMENTED EXISTING REPAIR BETWEEN STA 1918.9-1941 RBL 16.5" DIMENSION 4.3"-4.2" PERFORMED DVI INSPECTION PER SRM 51-10-08 AND TAP TEST PER SRM 51-10-06, FOUND EXISTING REPAIR WITHIN GOOD CONDITION AND PERFORMED PER SRM 51-70-10-2R, REF. SRM 53-80-01-2R.R
- [SDR FDEA202204251338](https://openairdocs.org/sdr/FDEA202204251338.md): Seat Track · corroded · Apr 25, 2022 · N917FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 560-580 FOUND CORROSION ON SEAT TRACK RBL 24.7 PERFORMED SEAT TRACK REAPAIR PER SRM 53-00-52 2R, FIG.201 REPAIR 1 MAJOR REPAIR
- [SDR FDEA202204251337](https://openairdocs.org/sdr/FDEA202204251337.md): Seat Track · corroded · Apr 25, 2022 · N917FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 1340-1380 FOUND SEVERAL CORROSION ON SEAT TRACK RBL 24.75 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52. FIG.201, REPAIR 1
- [SDR FDEA202204251335](https://openairdocs.org/sdr/FDEA202204251335.md): Seat Track · corroded · Apr 25, 2022 · N917FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN STA 660 FOUND CORROSION ON SEAT TRACK LBL 58.22 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52 2R, FIG.201 REPAIR 1 MAJOR REPAIR
- [SDR FDEA202204251334](https://openairdocs.org/sdr/FDEA202204251334.md): Seat Track · corroded · Apr 25, 2022 · N917FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 1320-1360 FOUND SEVERAL CORROSION ON SEAT TRACK RBL 45.5 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52.FIG.201 REPAIR 1
- [SDR FDEA202204251332](https://openairdocs.org/sdr/FDEA202204251332.md): Seat Track · damaged · Apr 25, 2022 · N917FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 560-580 FOUND ELONGATED HOLE BL 0 WORK ACCOMPLISHED PER FEDEX E.A # F-5310-T0368383, ELONGATED HOLE AT HORIZONTAL FLANGE OF SEAT TRACK AT BS 0 BETWEEN STA 560/580 FREEZE PLUG AND REPAIR STRAP INSTALLATION. MAJOR REPAIR
- [SDR FDEA202204251331](https://openairdocs.org/sdr/FDEA202204251331.md): Seat Track · gouged · Apr 25, 2022 · N917FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN STA 582 FOUND DEEP GOUGE/CHAP MARK AT SEAT TRACK LBL45 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0368307, STA 440-680, LBL 45.5, SEAT TRACK, CROWN, MATERIAL LOSS, PERMANENT REPAIR. MAJOR REPAIR
- [SDR FDEA202204251330](https://openairdocs.org/sdr/FDEA202204251330.md): None · none · Apr 25, 2022 · N917FD · Boeing 757200 · Standard Practices/Structures
  > CABIN STA 680 FOUND CORROSION ON BEAM EXISTING REPAIR LBL22-RBL12 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0368538, SECTION 43, FLOOR BEAM ASSY, STA 680, UPPER CHORD, LBL 25 TO RBL 12, CORROSION, REPAIR MAJOR REPAIR
- [SDR FDEA202204251329](https://openairdocs.org/sdr/FDEA202204251329.md): Floorbeam · corroded · Apr 25, 2022 · N917FD · Boeing 757200 · Fuselage Main, Floor Beam
  > CABIN BETWEEN STA 1200 FOUND CORROSION ON BEAM BETWEEN RBL 3-RBL 19 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0368550: SECTION 45, FLOOR BEAM ASSY, STA 1200, UPPER CHORD, RBL 3 TO RBL 19, CORROSION, REPAIR. MAJOR REPAIR
- [SDR FDEA202204251306](https://openairdocs.org/sdr/FDEA202204251306.md): Seat Track · damaged · Apr 25, 2022 · N917FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN BETWEEN STA 1200-1240 FOUND 2 PLACES WONGATED HOLES ON SEAT TRACK RBL 24.75 DAMAGED SEAT TRACK REMOVED AND NEW SEAT TRACK INSTALLED PER SRM 53-00-52-2R, REPAIR 3 AND SRM 51-40-02 MAJOR REPAIR
- [SDR FDEA202204251305](https://openairdocs.org/sdr/FDEA202204251305.md): Strap · corroded · Apr 25, 2022 · N917FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > CABIN STA 1420 FOUND CORROSION ON INTERCOSTAL STRAP RBL 24.75 AND RBL 45.5 PERFORMED FLOOR BEAM REPAIR STABILIZATION STRAP PER SRM 53-00-51-2R, FIG.201 REPAIR 13 MAJOR REPAIR
- [SDR FDEA202204201241](https://openairdocs.org/sdr/FDEA202204201241.md): Floor Panel · damaged · Apr 20, 2022 · N917FD · Boeing 757200 · Fuselage Floor Panel
  > FLOOR PANEL P.N 118662181-19 AT STA 680 NIR CARGO DOOR FOUND BROKEN PERFORMED WET LAYUP REPAIR FOR MENTIONED FLOOR PANEL PER SRM 53-00-50-2R, PARAGRAFH 3.D, FIG 201. REPAIR MATERIAL P/N: BMS8-301 CL-2. B/N: 0001285056. REV. 135.0. MAJOR REPAIR.
- [SDR FDEA202204191251](https://openairdocs.org/sdr/FDEA202204191251.md): Torque Ring · chafed · Apr 19, 2022 · N917FD · Boeing 757200 · Engine Exhaust System
  > ENG NO 2 OUTBORD C-DUCT ON THE UPPER FWO SIDE THERE IS A BROKEN PIECE FROM THER PANEL PERFORMED REPAIR PER SRM 51-71-03, REF. SRM 54-30-70-2R, FIG. 201,DETAIL I,TABLE I. REP. DIM.:3.5" X 2". REP. LOC.: UPPER EDGE OF TORQUE RING,R/H. REV. 135.0. REPAIR MATE
- [SDR FDEA202204191239](https://openairdocs.org/sdr/FDEA202204191239.md): Panel · cracked · Apr 19, 2022 · N917FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > PYLON NO 2 THERE IS A CRACK ON PANEL NO 444DR FEO SIDE PERFORMED HOT BOND REPAIR PER SRM 51-70-04,REF. SRM 54-50-70-2R,FIG. 201,DETAIL I,TABLE I.REP. DIM.: 2,5" X 2,5",REP. LOC.:FWD BOTTOM EDGE. REV.135.0. 17/1/22. MATERIAL: BMS8-139,B/N:92M0073723. MAJ
- [SDR FDEA202204191168](https://openairdocs.org/sdr/FDEA202204191168.md): Floor Panel · broken · Apr 19, 2022 · N917FD · Boeing 757200 · Fuselage Structure (General)
  > FLOOR PANEL FOUND BROKEN AT STA 1715.45 PN 11864182-42 PERFORMED WET LAYUP REPAIR FOR MENTIONED FLOOR PANEL PER SRM 53-00-50-2R, PARGRAPH 3.D, FIG.201 REPAIR MATERIAL P/N: BMS 8-301 CL 2. B/N D001285056. REV.135.0. MAJOR REPAIR
- [SDR FDEA202204181249](https://openairdocs.org/sdr/FDEA202204181249.md): Floor Panel · damaged · Apr 18, 2022 · N917FD · Boeing 757200 · Fuselage Floor Panel
  > FLOOR PANEL P.N 11861182-2 FOUND WORN REPLACED FLOOR PANEL PER FEDEX SRZ-25-005.REF ENGINEERING DISPOSITION OF RFTA NO: 02859-0207.P/N: N917FD-N00314-222MEF. B/N: 20354009. MAJOR REPAIR.
- [SDR FDEA202204181248](https://openairdocs.org/sdr/FDEA202204181248.md): Floor Panel · damaged · Apr 18, 2022 · N917FD · Boeing 757200 · Fuselage Floor Panel
  > FLOOR PANEL NO 221MBF FOUND WORN REPLACED FLOOR PANEL PER FEDEX SRZ-25-005. REF. ENGINEERING DISPOSITION OF RFTA NO:02859-0207. P/N: N917FD-N00309-221MBF. B/N: 20353938. MAJOR REPAIR.
- [SDR FDEA202204181247](https://openairdocs.org/sdr/FDEA202204181247.md): Floor Panel · damaged · Apr 18, 2022 · N917FD · Boeing 757200 · Fuselage Floor Panel
  > FLOOR PANEL NO 221AF FOUND WORN REPLACED FLOOR PANEL REP FEDEX SRZ-25-005. REF. ENGINEERING DISPOSITION OF RFTA NO:02859-0207. P/N: N917FD-N00310-221AF. B/N: 20353953. MAJOR REPAIR.
- [SDR FDEA202204181246](https://openairdocs.org/sdr/FDEA202204181246.md): Floor Panel · damaged · Apr 18, 2022 · N917FD · Boeing 757200 · Fuselage Floor Panel
  > FLOOR PANEL NO 222AF FOUND WORN REPLACED FLOOR PANEL PER FEDEX SRZ-25-005.REF. ENGINEERING DISPOSITION OF RFTA NO:02859-0207. P/N: N917FD-N00311-222AF. B/N: 20353964. MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N917FD/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 = 'N917FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N917FD/reports

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