# Service difficulty reports: N918FD

A list on [N918FD](https://openairdocs.org/aircraft/N918FD.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 · 190 reports

- [SDR FDEA202508291579](https://openairdocs.org/sdr/FDEA202508291579.md): Frame · cracked · Aug 29, 2025 · N918FD · Boeing 75723A · Fuselage Main, Frame
  > CRACK INDICATIONS FOUND IN STA 1640 AT S-14R BOTTOM I/B OPEN HOLE APROX AT 8 O' CLOCK LOOKING AFT AND TWO CRACK INDICATIONS IN UPPER O/B OPEN HOLE APROX AT 6 & 7 O' CLOCK LOOKING AFT COMPLIED WITH EA # F-5310-T0384596 P1 TITLE: FUSELAGE -MAINFRAME -STA 16
- [SDR FDEA202508281562](https://openairdocs.org/sdr/FDEA202508281562.md): Skin · delaminated · Aug 28, 2025 · N918FD · Boeing 75723A · Wing, Plate/Skin
  > LH WING LEADING EDGE SKIN AREA CRACKED BETWEEN WS 150.5 AND 204.50 (#5 LEADING EDGE SLAT AREA) PERFORMED TAP TEST ON LH WING L/E DELAMINATION FOUND DIM L= 18.5" W=15" OUT OF LIMIT IAW B757 SRM 57-41-01-1A FIG 101 SHEET 2 TABLE I NOTE A AND IAW B757 SRM 5
- [SDR FDEA202501270142](https://openairdocs.org/sdr/FDEA202501270142.md): Lens · detached · Jan 27, 2025 · N918FD · Boeing 75723A · Emergency Lighting
  > L EXTERNAL EMERGENCY LIGHT COVER DETACHED. IAW AMM 33-51-06-2-1 EA TF-3350-T0313211 L EMERG LIGHT LENS REATTACHED IAW SPM AND AMM 33-51-06-2-1 TESTED OK.
- [SDR FDEA202501270141](https://openairdocs.org/sdr/FDEA202501270141.md): Lens · detached · Jan 27, 2025 · N918FD · Boeing 75728A · Emergency Lighting
  > EXTERNAL EMERGENCY LIGHT COVER DETACHED. IAW AMM 33-51-06-2-1 EA TF-3350-T0313211 L EMERG LIGHT LENS REATTACHED IAW SPM AND AMM 33-51-06-2-1 TESTED OK.
- [SDR FDEA202501270140](https://openairdocs.org/sdr/FDEA202501270140.md): Lens · detached · Jan 27, 2025 · N918FD · Boeing 75723A · Emergency Lighting
  > EXTERNAL LH EMER. LIGHT LENSE DETACHED. L EMERG LIGHT LENS REATTACHED IAW SPM AND AMM 33-51-06-2-1 TESTED OK ADD CLEARED
- [SDR FDEA202412021762](https://openairdocs.org/sdr/FDEA202412021762.md): Guard · damaged · Dec 2, 2024 · N918FD · Boeing 75723A · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ARE UNARMED WHEN EMERGENCY EXIT LIGHT SWITCH IS CLOSED. FOUND SWITCH GUARD SPRING LOAD OUTSIDE OF THE SWITCH, REPOSITIONED THE SPRING, PERFORMED EMERGENCY LIGHTS OPERATIONAL IAW AMM 33-51-00-5 TEST OK
- [SDR FDEA202408081109](https://openairdocs.org/sdr/FDEA202408081109.md): Skin · corroded · Aug 8, 2024 · N918FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > FOUND EXFOLIATION CORROSION ON EXTERIOR SKIN SURFACE ADJACENT TO L/H APY DOOR FWD HINGE POINT AREA COMPLIED WITH MAJOR REPAIR CLASSIFICATION. E.A. #-F-5330-T0380244 P1 FUSELAGE-PLATES AND SKIN- LH APU COMPARTMENT SKIN PANEL REPAIR BETWEEN STA. 1885.20 AND
- [SDR FDEA202407251057](https://openairdocs.org/sdr/FDEA202407251057.md): Relay · failed · Jul 25, 2024 · N918FD · Boeing 75723A · Landing Gear Steering System
  > NOSE L/G COMPONENTS INSPECTION REQUIRED TO CONFIRM NO DAMAGES. NOSE GEAR COMPONENTS VISUAL INSPECTION PERFORMED. NO OBVIOUS DAMAGES OBSERVED. ALSO NOSE GEAR STEERING OPERATIONAL TEST PERFORMED SATIS REF AMM 32-51-00-5-3.
- [SDR FDEA202407251056](https://openairdocs.org/sdr/FDEA202407251056.md): Relay · failed · Jul 25, 2024 · N918FD · Boeing 75723A · Fuel Controlling System
  > RUNWAY ENGINE START. INSTEAD OF STABILIZING AT IDLE, THE RPM AND THRUST INCREASED WITH NO THROTTLE INPUT AND THROTTLES AT IDLE AND CONTINUED TO INCREASE RAPIDLY UNTIL CREW CUTOFF FUEL. SLIGHTLY PUSHED THE TUG. EVERYONE IS OK. APPLIED AND IDLE CONTROL RELA
- [SDR FDEA202404300520](https://openairdocs.org/sdr/FDEA202404300520.md): Fan · failed · Apr 30, 2024 · N918FD · Boeing 75723A · Air Distribution Fan
  > OIL BURNING SMOKE BELOW 5000FEET WITH LOW POWER SETTING. R & R L/H RECIRCULATION FILTER AND FAN, REVERSED MEL 21-25-01-02 & MEL 21-58-07, RECONNECTED WIRE ON PLUG D40910J, PERFORMED LT RECIRCULATION FAN & EQUIPMENT COOLING TEST, ALL TESTS PASSED, LEAK CHEC
- [SDR FDEA202404230272](https://openairdocs.org/sdr/FDEA202404230272.md): Girt Bar · out of alignment · Apr 23, 2024 · N918FD · Boeing 75723A · Emergency Equipment
  > LIGHT ON LEFT CREW ENTRY DOOR INOP. FACT 23APR24 08:51 AMS AMM: 25-66-10-2 AMM: 25-66-11-2 RELAMP NO HELP. FOUND SLIDE VERY HARD TO ARM AND GIRTBAR FITTINGS NOT REACHING THE TARGETS. RE-INSTALLED GIRTBAR FLAP AS PER AMM 25-66-10-2 REV 133.9 VERIFED
- [SDR FDEA202310231791](https://openairdocs.org/sdr/FDEA202310231791.md): Web · misaligned · Oct 23, 2023 · N918FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > REMOVE FRAME REPAIR AT STA 1360 L/H AFT CARGO FRAME PER EA # F-5310-TO376446 REPAIR PREFORMED PER EA # F-5310-T0376446 P 1. EO TITLE: FUSELAGE - MAIN - FRAME - EXISTING REPAIR FOUND FRAME 1360 AT S-26L DURING EO F- 5310 - E0347443 - REPAIR REPLACED.
- [SDR FDEA202310121757](https://openairdocs.org/sdr/FDEA202310121757.md): Floorboard · damaged · Oct 12, 2023 · N918FD · Boeing 757200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD PANEL 231 MAF IN ZONE 230 DAMAGED. FABRICATED MAIN CABIN FLOORBOARD 231 MAF ON VT MAE TRAVELER # T23/1709112 IAW DWG SRZ-25-005 REV R MAJOR REPAIR
- [SDR FDEA202310121756](https://openairdocs.org/sdr/FDEA202310121756.md): Floorboard · damaged · Oct 12, 2023 · N918FD · Boeing 757200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 231 MEF IN ZONE 230 DAMAGED. FABRICATED MAIN CABIN FLOORBOARD PANEL 231MEF ON VT MAE TRAVELER # T23/1709132 IAW DWG SRZ-25-005 REV R MAJOR REPAIR
- [SDR FDEA202310121751](https://openairdocs.org/sdr/FDEA202310121751.md): Floor Panel · damaged · Oct 12, 2023 · N918FD · Boeing 757200 · Fuselage Floor Panel
  > ZONE 220 COURIER FLOORBOARD 221 MBF DAMAGED. FABRICATED ZONE 220 FLOORBOARD 221 MBF ON VT MAE TRAVELER # T23/1707219 IAW DWG SRZ-25-005 REV R MAJOR REPAIR.
- [SDR FDEA202310121750](https://openairdocs.org/sdr/FDEA202310121750.md): Floor Panel · damaged · Oct 12, 2023 · N918FD · Boeing 757200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD PANEL 231MFF IN ZONE 230 DAMAGED FABRICATED MAIN CABIN FLOORBOARD PANEL 231MFF ON VT MAE TRAVELER # T23/1709136 IAW DWG SRZ-25-005 REV R MAJOR REPAIR.
- [SDR FDEA202310121749](https://openairdocs.org/sdr/FDEA202310121749.md): Floor Panel · damaged · Oct 12, 2023 · N918FD · Boeing 757200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD PANEL 231MBF IN ZONE 230 DAMAGED. FABRICATED MAIN CABIN FLOORBOARD PANEL 231MBF ON VT MAE TRAVELER # T23/1709121 IAW DWG SRZ-25-005 REV R MAJOR REPAIR.
- [SDR FDEA202310111746](https://openairdocs.org/sdr/FDEA202310111746.md): Seat Track · corroded · Oct 11, 2023 · N918FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO FLOOR SEAT TRACK FLANGE HAS SEVERAL CORROSION LOC BET STA 1180 AND 122 RBL 45. SEAT TRACK WAS REMOVED, FABRICATED AND INSTALLED ON MAIN DECK CARGO FLOOR BETWEEN STA 1180 TO STA 1280 AND RBL 45, IAW SRM 51-40-02. MAJOR REPAIR
- [SDR FDEA202310111745](https://openairdocs.org/sdr/FDEA202310111745.md): Seat Track · corroded · Oct 11, 2023 · N918FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > MDC SAET TRACK BETWEEN BS 1420 AND 1540 AT LBL 45.50 HAS LIGHT SURFACE CORROSION SEAT TRACK WAS REPAIRED BETWEEN STA 1480 TO 1540 AND LBL 45.50 IAW B757 SRM 53-00-52-2 R REPAIR 3 OPTION 2 REPAIR CATEGORY "A" MAJOR REPAIR.
- [SDR FDEA202310111744](https://openairdocs.org/sdr/FDEA202310111744.md): Floorboard · damaged · Oct 11, 2023 · N918FD · Boeing 757200 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD PANEL 252 MTF DAMAGED FABRICATED MAIN CABIN FLOORBOARD PANEL 252 MTF ON VT MAE TRAVELER # T23/1709138 IAW DWG SRZ-25-005 REV R MAJOR REPAIR.
- [SDR FDEA202307171230](https://openairdocs.org/sdr/FDEA202307171230.md): Rudder · damaged · Jul 17, 2023 · N918FD · Boeing 757200 · Rudder Structure
  > THE WINGTIP OF A MANEUVERING AIRCRAFT STRUCK THE RIGHT HAND SIDE LOWER SECTION OF THE RUDDER STRUCTURE, PENETRATING THE RUDDER SKIN SURFACE AND HONEYCOMB CORE. DETAILED ASSESSMENT UNDERWAY. RUDDER ASSY R & R IAW AMM 27-21-21-4.
- [SDR FDEA202212243010](https://openairdocs.org/sdr/FDEA202212243010.md): Seal · damaged · Dec 24, 2022 · N918FD · Boeing 75723A · Passenger/Crew Doors
  > AT CRUISE FL370, NOTICED LOUD NOISE COMING FROM FORWARD AIRCRAFT LEFT, SUSPECTED LEAKY DOOR SEAL. CABIN ALTITUDE DISPLAYED 9100 WITH A SLIGHT CLIMB AND OUTFLOW VALVE POSITION FULLY CLOSED. CABIN ALTITUDE CONTINUED TO CLIMB TO 9500. MOVED SELECTOR FROM AUT
- [SDR FDEA202212082890](https://openairdocs.org/sdr/FDEA202212082890.md): Battery · failed · Dec 8, 2022 · N918FD · Boeing 75723A · DC Generating System
  > FOUND APU BATTERY OVERHEATED AND FUMES ON IT DURING APU BITE TEST ON ECU. BATTERY INMEDIATELY DISCONNECTED AND FIRE BRIGADE ADVISED. INSTALLED NEW APU BATTERY IAW AMM 24-31-03-4-0, ALL TEST PASSED PER SAME AMM, STARTED APU TWICE PER JRH ALL PARAMETER
- [SDR FDEA202211152784](https://openairdocs.org/sdr/FDEA202211152784.md): Screw · loose · Nov 15, 2022 · N918FD · Boeing 75723A · Electrical Power System Wiring
  > ON APPROACH TO 26L WITH THE LT AUTOPILOT ENGAGED, RECEIVED MULTIPLE FAILURES, INCLUDING EICAS MESSAGES & INDICATIONS: AUTOPILOT FAIL, BLEED ISLN VAL, LT YAW DAMPER, RUDDER RATIO. AMBER REV, LT EPR, DUAL AMBER DCU ON CAPT PFD & ND STBY ATTITUDE (EFI) FAILED
- [SDR FDEA202209292386](https://openairdocs.org/sdr/FDEA202209292386.md): Light · loose · Sep 29, 2022 · N918FD · Boeing 75723A · Emergency Lighting
  > DURING PREFLIGHT UNARMED LIGHT CAME OUT OF EMERGENCY LIGHTS MODULE ON OVERHEAD PANEL FOUND KORRY LIGHT ASSY BROKEN. R&R KORRY ASSY IAW AMM 33-13-00-2 AND SWPM 20-84-18. OPS CHECK SATIS. A/C OK TO CONTINUE.
- [SDR FDEA202203030408](https://openairdocs.org/sdr/FDEA202203030408.md): None · failed · Mar 3, 2022 · N918FD · Boeing 757200 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ARMING SWITCH WIRE BROKEN. DOES NOT ARM LIGHTS WHEN TOGGLE SWITCH CLOSED. FOUND THE SPRING OF THE SAFE GUARD SWITCH BROKEN. OIL 03MAR22 14:35 MXP U NO RESTRICTION REF: EA F-3350-T0367281 EMERGENCY LIGHTS GUARD SWITCH S1 ON PANEL M
- [SDR FDEA202202260378](https://openairdocs.org/sdr/FDEA202202260378.md): None · none · Feb 26, 2022 · N918FD · Boeing 757200 · Emergency Lighting
  > MDIS 918 33-50 3520 26FEB22 LGG FACT U DURING SERVICE CHECK FOUND L1 SLIDE LIGHT INOP. RELAMPED L1 SLIDE LIGHT IAW AMM 33-51-06-2-1, LIGHT OPERATIONAL.
- [SDR FDEA202111222974](https://openairdocs.org/sdr/FDEA202111222974.md): Skin · damaged · Nov 22, 2021 · N918FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > FUSELAGE BELLY SKIN AT BS 1460 TO 1480 BETWEEN STRINGER 29L AND 29R THERE IS A DOUBLER AND A TRIPLER INSTALLED UNDER THE VHF ANTENAN. REPAIR REQUIRES EVALUATION TO DETERMINE IF IT WAS ACCOMPLISHED IN ACCORDANCE WITH APPROVED DATA A DVI WAS PERFORMED PE
- [SDR FDEA202111222972](https://openairdocs.org/sdr/FDEA202111222972.md): None · damaged · Nov 22, 2021 · N918FD · Boeing 757200 · Standard Practices/Structures
  > FOUND 20 4EA HOLES DRILLED AND UNUSED ON AFT PLATE BETWEEN STA 1681-1700 ON BL 0 THE DAMAGED SECTION OF THE AFT DECK PLATE WAS TRIMMED OUT PER SRM 51-10-02, THE AFT THECK PLATE WAS REPAIRED I.A.W EA # F-5310-T0365378 P1. THIS IS A MAJOR CATAGORY A REPAIR
- [SDR FDEA202111222970](https://openairdocs.org/sdr/FDEA202111222970.md): None · corroded · Nov 22, 2021 · N918FD · Boeing 757200 · Standard Practices/Structures
  > FOUND CORROSION ON UPPER CHORD OF FLOOR BEAM AT STA 1681 LBL 40 TO RBL 40 UNDER SHEAR WEB THE FLOOR BEAM UPPER CHORD FWD FLANGE WAS REPAIRED WITH 2 ANGLES, 1 FILLER AND 1 STRAP P/N N918FD-NRC-N00352-01/-02/-03/-04 PER SRM 53-60-51, REPAIR 3, FIG. 201, DE
- [SDR FDEA202111182976](https://openairdocs.org/sdr/FDEA202111182976.md): Skin · damaged · Nov 18, 2021 · N918FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > EMPENNAGE, TAIL CONE UPPER SURFACE LEFT HAND SIDE, CIRCULAR DUBLER REPAIR ON EXTERNAL SKIN FORWARD OF THE APU EXHAUST OUTLET AT BS 1980, REPAIR REQUIRES EVALUATION TO DETERMINE IF IT WAS ACCOMPLISHED IN ACCORDANCE WITH APPROVED DATA PERFORMED DVI PER S
- [SDR FDEA202111182975](https://openairdocs.org/sdr/FDEA202111182975.md): Skin · damaged · Nov 18, 2021 · N918FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > APU COMPARTMENT R/H SIDE, CIRCULAR DOUBLER REPAIR ON INNER SKIN AT BS 1925 AND INCHES FROM THE PANEL LOWER EDGE REPAIR REQUIRES EVALUATION TO DETERMINE IF IT WAS ACCOMPLISHED IN ACCORDANCE WITH APPROVED DATA PERFORMED DVI PER SRM 51-10-08. REPAIR EVALUA
- [SDR FDEA202111182973](https://openairdocs.org/sdr/FDEA202111182973.md): None · unknown · Nov 18, 2021 · N918FD · Boeing 757200 · Standard Practices/Structures
  > FORWARD LOWER CARGO FLOOR,RIGHT HAND SIDE Z CHANNEL HAS A REPAIR SPLICE AT BS 710. REPAIR REQUIRES EVALUATION TO DETERMINE IF IT WAS ACCOMPLISHED IN ACCORDANCE WITH APPROVED DATA A DVI WAS PERFORMED PER SRM 51-10-08 AND THIS EXISTING REPAIR WAS FOUND IN
- [SDR FDEA202110252971](https://openairdocs.org/sdr/FDEA202110252971.md): Floorbeam · corroded · Oct 25, 2021 · N918FD · Boeing 75723A · Fuselage Main, Floor Beam
  > FOUND CORROSION ON STA 1640 ON UPPER CHORD OF FLOOR BEAM BETWEEN LBL 45 TO RBL 45 THE CORREDED UPPER CHORD WAS REMOVED AND DISCARDED A NEW REPAIR UPPER CHORD P/N FX-F-5310-T036209-01 WAS INSTALLED PER EA # F-5310-T036209 P1 USING FASTENERS PER SRM 51-40-
- [SDR FDEA202110242977](https://openairdocs.org/sdr/FDEA202110242977.md): Wedge · damaged · Oct 24, 2021 · N918FD · Boeing 75723A · Flight Control System
  > DURING C-DUCT REMOVEL R/H INBD L/H SLAT DAMAGED PERFORMED REPAIR PER EA F-5750-T0365723A REP DIM. 5.2" X 7" REP. LOC. ISS 137 AT T/E. PERFORMED HOT BOND REPAIR PER SRM 51-70-10, REF SRM 57-43-02-2R, FIG 201 DETAIL II, NOTE D, TABLE 201
- [SDR FDEA2020082091946](https://openairdocs.org/sdr/FDEA2020082091946.md): Mechanism · lack of lube · Aug 19, 2020 · N918FD · Boeing 75723A · Passenger/Crew Doors
  > DURING WALKAROUND FOUND DOOR L1 NOT ABLE TO OPERATE FROM THE OUTSIDE HANDLE. ABLE TO OPEN THE L1 DOOR BUT EXTERIOR HANDLE BUTTERFLY STICKY AND HARD TO MOVE. TRIED TO CLEAN AND LUBRICATE FROM EXTERIOR BUT NO HELP, AS PER AMM 52-11-13-2 NEED TO CHECK FOR LU
- [SDR FDEA2020051530931](https://openairdocs.org/sdr/FDEA2020051530931.md): Light · inoperative · May 13, 2020 · N918FD · Boeing 75723A · Door Warning System
  > L/H FOWARD ENTRY DOOR "SLIDE" LIGHT FOUND TO BE INOP AS DOOR WAS CLOSED RE-LAMPED L/H FWD DOOR ARM/SLIDE IAW STANDARD PRACTICES ELECTRICAL. TEST OK
- [SDR FDEA2020041760752](https://openairdocs.org/sdr/FDEA2020041760752.md): Collar · worn · Apr 16, 2020 · N918FD · Boeing 75723A · Passenger/Crew Doors
  > L1 DOOR INOP GUST LOCK INOP. SPARES KIT CONTAINS 10-N6008-1 TWO PIECE COLLAR ASSEMBLY TOGETHER WITH 10-N6009-1 CATCH ASSEMBLY. 10-N0244-7 IS INTERCHANGEABLE WITH 654N0244-7. IDENTIFIED PARTS COLLAR ASSY MPN: 10-N0244-7 CPN: 5214377 QTY: 1. REMOVED AND REPLAC
- [SDR FDEA202002210363](https://openairdocs.org/sdr/FDEA202002210363.md): Gust Lock · cracked · Feb 21, 2020 · N918FD · Boeing 75723A · Passenger/Crew Doors
  > LEFT CREW ENTRY GUST LOCK HAS SMALL PIECE CRACKED OFF. REMOVED AND REPLACED COLLAR AND CATCH ASSY AS PER AMM 52-11-08-8. OPS CHECK OK. MEL CLOSED PLACARDS REMOVED. A/C OK FOR SERVICE.
- [SDR FDEA2019100322398](https://openairdocs.org/sdr/FDEA2019100322398.md): Door Frame · cracked · Oct 2, 2019 · N918FD · Boeing 75723A · Fuselage Main, Structure
  > MDCC L2 DOOR FRAME CRACKED AT THE UPPER HINGE CUTOUT. REPAIRED THE DOOR FRAME BS 680 - 700 IAW SRM 52-10-02-2R, REPAIR 1 & EA F-5210-T0321335 A P2. CLASSIFIED AS A MAJOR IAW GMM 6-2-100.
- [SDR FDEA2019100322397](https://openairdocs.org/sdr/FDEA2019100322397.md): Door Frame · cracked · Oct 2, 2019 · N918FD · Boeing 75723A · Fuselage Main, Structure
  > MDCC RT NR 2 DOOR FRAME CRACKED AT THE UPPER HINGE CUTOUT. REPAIRED THE DOOR FRAME BS 680 - 700 IAW SRM 52-10-02-2R, REPAIR 1. CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA2019082872032](https://openairdocs.org/sdr/FDEA2019082872032.md): Valve · failed · Aug 27, 2019 · N918FD · Boeing 75723A · Pneumatic Distribution System
  > ABORTED TAKEOFF AT 70 KTS DUE TO RT ENG BLEED OFF EICAS.EICAS WENT AWAY WITH THROTTLES AT IDLE.ON TAXIBACK SAME EICAS WHENEVER THROTTLES PUSHED UP. REMOVED AND REPLACED RH ENGINE BLEED PRSOV PER MM 36-11-09-2-1, OPS CHECK OK
- [SDR FDEA2018092542667](https://openairdocs.org/sdr/FDEA2018092542667.md): Floorboard · dented · Sep 24, 2018 · N918FD · Boeing 75723A · Fuselage Floor Panel
  > FLOORBOARD DENTED AT B/S 830 LBL 50 CARRIED OUT EVALUATION OF FLOORBOARD DENTED ON UPPER DECK BS830 LBL 50 AS PER SRM 53-00-50-1A REV 125. DAMAGE WAS FOUND TO BE OUT OF LIMITS AND REQUIRES REPAIR. CARRIED OUT REPAIR TO FLOORBOARD IAW SRM 53-00-50-2R REV
- [SDR FDEA2018092512663](https://openairdocs.org/sdr/FDEA2018092512663.md): Door Frame · damaged · Sep 21, 2018 · N918FD · Boeing 75723A · Fuselage Main, Structure
  > GOUGE DAMAGE FOUND ON B-STA 231-25 BL O FRAME FROM CONTACT WITH MEC ACCESS DOOR LATCH PIN REPAIRED IAW SRM 53-00-07-2R REPAIR 7. THIS IS A MAJOR REPAIR.
- [SDR FDEA2018091432521](https://openairdocs.org/sdr/FDEA2018091432521.md): Hydraulic Line · leaking · Sep 13, 2018 · N918FD · Boeing 75723A · Hydraulic System, Main
  > ON SHORT FINAL, L HYD QTY WENT TO ZERO. AS WE WERE FULLY CONFIGURED, WE OPTED TO LAND AND STOP ON THE RUNWAY. PTU KICKED IN ABOUT 150 AGL. WE CAME TO A STOP RAN THE QRH AND SHUT OFF BOTH LT ENG AND LT ELEC HYD PUMPS, PER QRH PROC. TOTAL RUN TIME OF LT HYD PUM
- [SDR FDEA201805091199](https://openairdocs.org/sdr/FDEA201805091199.md): Computer · malfunctioned · May 9, 2018 · N918FD · Boeing 75723A · Autopilot Computer
  > MCP WENT BLANK EXCEPT FOR IAS, HDG AND ALT. WHEN GS WAS SELECTED FLIGHT DIRECTORS SUDDENLY COMMANDED A CLIMBING LEFT TURN, WHICH WAS TOTALLY INCONSISTENT. WE TURNED OFF FD AND RIGHT AUTOPILOT IN UNSUCCESSFUL ATTEMPT TO RESET SYSTEM. PERFORMED T/S PER FIM 22-02
- [SDR FDEA201710032840](https://openairdocs.org/sdr/FDEA201710032840.md): Structure · corroded · Oct 3, 2017 · N918FD · Boeing 75723A · Nacelle/Pylon Miscellaneous Structure
  > LT PYLON CORROSION ON ACCESS PANEL 433GR CUTOUT AREA CARRIED OUT REPAIR TO CORROSION ON LT PYLON AROUND ACCESS PANEL 433GR CUTOUT IAW SRM 54-50-01-1A ALLOWABLE DAMAGE 1, FIG 101, DETAIL III AND EA F-5450-T0335537.
- [SDR FDEA201710032839](https://openairdocs.org/sdr/FDEA201710032839.md): Floorbeam · corroded · Oct 3, 2017 · N918FD · Boeing 75723A · Fuselage Main, Floor Beam
  > EVIDENCE OF CORROSION FOUND RBL 2.90 FLOORBEAM LOCATED AFT CARGO COMPARTMENT BETWEEN STA 1330 AND STA 1440. CARRIED OUT REPAIR TO FLOORBEAM AT STA 1330 RBL 2.90 IAW SRM 53-00-53 REPAIR 1 FIG 201 REV 121. REPLACED CORRODED FLOORBEAM STRINGER BETWEEN STA 1343 AN
- [SDR FDEA201709252843](https://openairdocs.org/sdr/FDEA201709252843.md): Web · cracked · Sep 25, 2017 · N918FD · Boeing 75723A · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR WEB AT BS 580, LBL 47. CARRIED OUT REPAIR TO CRACKED FLOOR WEB AT STA 580 LBL 47 IAW EA F-5330-T0335604.
- [SDR FDEA201709232680](https://openairdocs.org/sdr/FDEA201709232680.md): Floor Support · corroded · Sep 23, 2017 · N918FD · Boeing 75723A · Fuselage Miscellaneous Structure
  > EVIDENCE OF CORROSION FOUND AT RBL 10.45, FLOOR SUPPORT LOCATED IN THE AFT CARGO BAY BETWEEN BS 1330 AND 1440. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 1, REV 121.

Next page: https://openairdocs.org/aircraft/N918FD/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 = 'N918FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N918FD/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.