# Service difficulty reports: N985FD

A list on [N985FD](https://openairdocs.org/aircraft/N985FD.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 · 83 reports

- [SDR FDEA202603110335](https://openairdocs.org/sdr/FDEA202603110335.md): Lamp · inoperative · Mar 11, 2026 · N985FD · Boeing 757230 · Emergency Lighting
  > R1 DOOR EXTERIOR SLIDE LIGHT INOP DURING LIGHT TEST RELAMPED IAW ABOVE REF, OPS CHECK GOOD.
- [SDR FDEA202508121410](https://openairdocs.org/sdr/FDEA202508121410.md): Elec Connector · shorted · Aug 12, 2025 · N985FD · Boeing 757230 · Fire Protection System Wiring
  > ON DEPARTURE, PASSING FL190, SPARKS CAME OUT OF OVERHEAD CIRCUIT BREAKER PANEL. THERE WAS NO SMOKE OR FUMES. LOST LT PFD & MFD, LT FMC, LT GPS. DECLARED AN EMERGENCY & RETURNED TO OUR DEPARTURE. AFTER CREW DEBRIEF FOUND 4 C/B'S POPPED. P6-3 CAPT PRIM IN
- [SDR FDEA202506040837](https://openairdocs.org/sdr/FDEA202506040837.md): Lamp · inoperative · Jun 4, 2025 · N985FD · Boeing 757230 · Emergency Lighting
  > R1 DOOR EXTERIOR SLIDE LIGHT DOES NOT ILLUMINATE DURING TEST AMM: 33-51-06-2-1 RELAMPED R1 DOOR SLIDE LIGHT (MPN 767) IAW ABOVE REF, OPS CHECK GOOD.
- [SDR FDEA202505080738](https://openairdocs.org/sdr/FDEA202505080738.md): Bearing · failed · May 8, 2025 · N985FD · Boeing 757230 · Passenger/Crew Doors
  > L1 DOOR WOULD NOT CLOSE. REMOVED AND REPLACED L1 DOOR INSIDE HANDLE CAM ASSEMBLY, LATCH ROLLER CRANK BEARING AND COCKING ROLLER CRANK BEARING IN REF. AMM 52-11-13-2 AND EAF-5210-T0383355. ADJUSTED L1 DOOR GUIDE ARM IN REF AMM 52-11-04-2. CLEARANCES AND OPS CH
- [SDR FDEA202505050717](https://openairdocs.org/sdr/FDEA202505050717.md): Girt Bar · lack of lube · May 5, 2025 · N985FD · Boeing 757230 · Emergency Equipment
  > R1 DOOR "SLIDE" ARMED LIGHT WILL NOT ILLIMUNATE. RELAMPED NO HELP. ARM LEVER DOES NOT APPEAR TO MOVE FULL TRAVEL WHEN ARMING AND PRESUME DOOR IS NOT ARMED. COMPLIED WITH INSPECTION/TEST GIRT BAR HANDLING IN REF TO AMM 52-11-25-5. COMPLIED WITH LUBE OF G
- [SDR FDEA202504150593](https://openairdocs.org/sdr/FDEA202504150593.md): Skin · unknown · Apr 15, 2025 · N985FD · Boeing 757230 · Trailing Edge Flaps
  > DURING AGING INSP. FOUND EXISTING REPAIR ON O/B LOWER FLAP 102" TO THE O/B EDGE, LH O/B AFT FLAP. COMPLIED WITH - EA # F - 5750-T0383010 P1 TITLE: WINGS - FLIGHT SURFACES - LH WING OTBD. AFT FLAP LOWER SKIN REPAIR, RSC TRACKING. THIS IS MAJOR REPAIR
- [SDR FDEA202504150592](https://openairdocs.org/sdr/FDEA202504150592.md): Skin · unknown · Apr 15, 2025 · N985FD · Boeing 757230 · Trailing Edge Flaps
  > DURING AGING INSP. FOUND EXISTING REPAIR ON O/B LOWER FLAP 14.5" TO THE I/B EDGE, LH O/B AFT FLAP. COMPLIED WITH EA # F-5750-T0383010 P1. THIS IS MAJOR REPAIR.
- [SDR FDEA202309221638](https://openairdocs.org/sdr/FDEA202309221638.md): Battery Pack · failed · Sep 22, 2023 · N985FD · Boeing 757200 · Emergency Lighting
  > ON PDC FOUND L1 DOOR INTERIOR EMERGENCY LIGHT INOP. RELEASED FOR SERVICE PER MEL: 33-51-01-01. REPLACED BATTERY PACK. NO DEFECTS NOTED. CHECKS SATIFACTORY.
- [SDR FDEA202110192572](https://openairdocs.org/sdr/FDEA202110192572.md): Frame · cracked · Oct 19, 2021 · N985FD · Boeing 757200 · Fuselage Main, Structure
  > FUSELAGE FRAME 1EA FASTENER HOLE CRACKED AT STA1640 S14R REPAIRED THE CRACKED FASTENER HOLE AT FUSELAGE FRAME STA1640 S14R PER EA: F- 5310-T0364454 P1 & SRM 51-40-02. EA TITLE: FUSELAGE - MAINFRAME - STA 1640 FRAME SPLICE REPAIR TO CRACK AT RH STRINGER S-14
- [SDR FDEA202102110326](https://openairdocs.org/sdr/FDEA202102110326.md): Valve · failed · Feb 11, 2021 · N985FD · Boeing 757230 · Engine (Turbine/Turboprop)
  > AFTER T/O AT ABOUT 6000' L/H ENGINE EPR STARTED TO FLUCTUATE ABOUT.05 UP AND DOWN. OIL PRESSURE ALSO FLUCTUATED /- 25 PSI. WE TURNED OFF TAI AND THE ENGINE SEEMED FINE.LESS THEN A MINUTE LATER THE SAME PROBLEM CAME BACK. PULLING THE POWER BACK ON DESCEN
- [SDR FDEA202004270807](https://openairdocs.org/sdr/FDEA202004270807.md): Rudder · failed · Apr 27, 2020 · N985FD · Boeing 757230 · Rudder Control System
  > SMIS 985 55-40 5529 23APR20 MEM OPEN U MOD TYPE T MOD NO. F-5540-T0353729 REV NO. PS P1 STABILIZERS - RUDDER - MAINTENANCE PROGRAM INSPECTION COMPLY WITH E..A. F-5540-T0353729 REV NO. POS. P1 DUE TO FAILED RUDDER INSPECTION R&R'ING RUDDER
- [SDR FDEA2019112653092](https://openairdocs.org/sdr/FDEA2019112653092.md): Skin · dented · Nov 25, 2019 · N985FD · Boeing 757230 · Leading Edge Devices
  > LARGE DENT SHOWING AT NR 8 SLAT WEDGE UPPER SKIN. ACCOMPLISHED REPAIR ON NR 8 SLAT T/E WEDGE UPPER SKIN IAW SRM 57-43-02-2R AND IAW SRM 51-70-10-2R REP 4 AND IAW EA T F-5750-T0351070 P1. WING - FLIGHT SURFACES - NR 8 SLAT TRAILING EDGE WEDGE UPPER SURFACE R
- [SDR FDEA201911223045](https://openairdocs.org/sdr/FDEA201911223045.md): Shear Web · corroded · Nov 22, 2019 · N985FD · Boeing 757230 · Fuselage Miscellaneous Structure
  > MAIN CABIN BETWEEN STA 1681-1720, BL0-LBL50 WEB CORRODED. REMOVED CORR ON SHEAR WEB STA 1681-1720 BL0 - LBL50 IAW SRM 51-10-02 ALL AREAS IN LIMITS EXCEPT STA 1701 LBL5 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101. AT STA 1701 LBL5 FABRICATED AND INS
- [SDR FDEA201911223044](https://openairdocs.org/sdr/FDEA201911223044.md): Doubler · cracked · Nov 22, 2019 · N985FD · Boeing 757230 · Passenger/Crew Doors
  > MAIN CARGO COMPT. L-4 DOOR INTERNAL STRUCTURE, FWD. AND NEAR TO LOWER CORNER GUSSET HAS 1EA. DEEP GOUGE. REMOVED GUSSET (DOUBLER) L-4 DOOR INTERNAL STRUCTURE LWR CORNER IAW B757 SRM 51-40-02. FABRICATED AND INSTALLED NEW GUSSET (DOUBLER) IAW BOEING DWG 14
- [SDR FDEA2019112213026](https://openairdocs.org/sdr/FDEA2019112213026.md): Web · corroded · Nov 21, 2019 · N985FD · Boeing 757230 · Fuselage Miscellaneous Structure
  > MAIN CABIN BETWEEN STA 1700-1720, BL0-RBL50 WEB CORRORED. REMOVED CORR ON SHEAR WEB 1700-1720 BL0 -RBL50 IAW B757 SRM 51-10-02. ALL AREA'S IN LIMIITS EXCEPT STA 1705 RBL6 IAW B757 SRM 53-00-51-1A FIG 101. FABRICATED AND INSTALLED DOUBLER AT STA 1705 RBL6
- [SDR FDEA201905111025](https://openairdocs.org/sdr/FDEA201905111025.md): Arming Lever · unsecure · May 11, 2019 · N985FD · Boeing 757230 · Passenger/Crew Doors
  > DURING SERVICE CHECK FOUND L1 DOOR ESCAPE SLIDE ARMED HANDLE ON FLOOR. REATTACHED THE L-1 DOOR ESCAPE SLIDE ARMING HANDLE REF MM 52-11-02-4-0. A/C OK FOR SERVICE.
- [SDR FDEA201901170161](https://openairdocs.org/sdr/FDEA201901170161.md): Unknown · malfunctioned · Jan 17, 2019 · N985FD · Boeing 757230 · Door Warning System
  > R FWD ENT DOOR SLIDE LIGHT FAILED TO ILLUMINATE CYCLED R1 DOOR ARM LEVER SEVERAL TIMES WITH NO FAULTS NOTED SLIDE LIGHT CHECKS GOOD, GIRT BAR ENGAGES FREELY AND WITHOUT OBSTRUCTION REF MM 25-66-00-0.
- [SDR FDEA201712193414](https://openairdocs.org/sdr/FDEA201712193414.md): Skin · corroded · Dec 19, 2017 · N985FD · Boeing 757230 · Wing, Plate/Skin
  > FUEL LEAK AT THE RT WING OVERWING FUELING CAP. EVALUTED THE AREA OF THE RT WING UPPER SURFACE AT FUELING PORT CUTOUT. FOUND CORROSION DAMAGE TO BE OUT OF LIMITS, MAX MATERIAL LOSS.351, CUT-OUT THE DAMAGE IAW SRM 57-25-01-1A AD3, & SRM 57-20-01-2R, REPAIR
- [SDR FDEA201712083348](https://openairdocs.org/sdr/FDEA201712083348.md): Stringer · corroded · Dec 8, 2017 · N985FD · Boeing 757230 · Fuselage Main, Longeron/Stringer
  > E & E COMPT. CORROSION ON STRINGER S21R BETWEEN STA. 460 TO 480. COMPLIED WITH EA F-5310-T0337218 P1.
- [SDR FDEA201712083347](https://openairdocs.org/sdr/FDEA201712083347.md): Stringer · corroded · Dec 8, 2017 · N985FD · Boeing 757230 · Fuselage Main, Longeron/Stringer
  > E & E COMPT. CORROSION ON STRINGERS S20R BETWEEN STA. 460 AND 480. COMPLIED WITH EA F-5310-T0337221 P1.
- [SDR FDEA201709252733](https://openairdocs.org/sdr/FDEA201709252733.md): Cowling · delaminated · Sep 25, 2017 · N985FD · Boeing 757230 · Engine Cowling System
  > NR 2 ENGINE RIGHT FAN COWL INNER LOWER FWD SURFACE IS DAMAGED. DAMAGE IS FROM CONTINUED OIL CONTAMINATION FROM EITHER SERVICING OR OIL LEAK AT IDG SERVICE DOOR ON INNER SKIN FORWARD LOWER CORNER OF FAN COWL. HOT BOND COMPOSITE REPAIR REF SRM 51-70-04.
- [SDR FDEA201511193716](https://openairdocs.org/sdr/FDEA201511193716.md): Shear Plate · corroded · Nov 19, 2015 · N985FD · Boeing 737230 · Fuselage Miscellaneous Structure
  > MAIN CABIN SHEAR PLATE HAS CORROSION, BETWEEN LBL 58 & 63, BS 377 - 440. ACCOMPLISHED IAW EA F-5310-T0321725 P1.
- [SDR FDEA201511143607](https://openairdocs.org/sdr/FDEA201511143607.md): Door Frame · gouged · Nov 14, 2015 · N985FD · Boeing 757230 · Fuselage Main, Structure
  > FORWARD E & E BAY DOOR CUT OUT STATION 231.25 IS DENTED & GOUGED. REPAIRED FWD E & E BAY DOOR CUT OUT, STATION 231.25 IAW EA F-5310-T0321509 P 1. FUSELAGE MAIN FRAME FWD E & E COMPARTMENT BS 231.25, BL0, FRAME DENT REPAIR.
- [SDR FDEA201501040018](https://openairdocs.org/sdr/FDEA201501040018.md): Proximity Sensor · dirty · Jan 4, 2015 · N985FD · Boeing 757230 · Emergency Equipment
  > ON PREFLIGHT FOUND THAT R1 SLIDE ARMED ANNUNCIATOR LIGHT IS INOPERATIVE. INSPECTED IAW AMM 25-66-11-2-0. CLEANED & REMOVED EXCESS GREASE & DEBRIS FROM BOTH GIRT BAR PROX SENSORS. ARM LIGHT OPERATIONS CHECKED GOOD.
- [SDR FDEA201412310001](https://openairdocs.org/sdr/FDEA201412310001.md): Roller · defective · Dec 31, 2014 · N985FD · Boeing 757230 · Passenger/Crew Doors
  > RIGHT FWD ENT DOOR EICAS APPEARED ON LANDING ROLLOUT. FOUND R1 DOOR PARTIALLY OPEN, UNABLE TO CLOSE THE DOOR WITHOUT PUSHING ON THE UPPER AFT CORNER. THE UPPER AFT LATCH ROLLER IS HITTING LATCH FITTING GOUGED. FOUND FWD UPPER CAM ROLLER BAD. R & R ROLLER &
- [SDR FDEA201405151029](https://openairdocs.org/sdr/FDEA201405151029.md): Girt Bar · lack of lube · May 15, 2014 · N985FD · Boeing 757230 · Emergency Equipment
  > R1 DOOR ARM LIGHT INOPERATIVE. CLEARED AT BLOCKING 1 HOUR ON GROUND LIGHT FAILED AGAIN. CHECKED GIRT BAR FLOOR FITTING ADJUSTMENT, CLEANED AND LUBED SLIDERS IAW AMM 52-11-25-5. DOOR SLIDE ARMS OK, NO DEFECTS NOTED. SLIDE AND GIRT BAR CHECKED GOOD IAW AMM 2
- [SDR FDEA201404110716](https://openairdocs.org/sdr/FDEA201404110716.md): Lanyard · out of position · Apr 11, 2014 · N985FD · Boeing 757230 · Emergency Equipment
  > RIGHT ENTRY DOOR VERY DIFFICULT TO ARM, IT FEELS LIKE THE MECHANISM IS LOOSE. FOUND RT ENTRY DOOR ESCAPE SLIDE LANYARD INTERFERING WITH GIRT BAR MECHANISM. STOWED LANYARD & GIRT BAR ARMING MECHANISM TO NORMAL IAW AMM 52-11-25-5.
- [SDR FDEA201311042681](https://openairdocs.org/sdr/FDEA201311042681.md): Elbow · loose · Nov 4, 2013 · N985FD · Boeing 757230 · Hydraulic System, Main
  > LEFT PYLON HIGH PRESSURE LINE ELBOW LOOSE. COMPLIED WITH EA F-2910-T0301760. MAJOR REPAIR.
- [SDR FDEA201311042680](https://openairdocs.org/sdr/FDEA201311042680.md): Spacer · wrong part · Nov 4, 2013 · N985FD · Boeing 757230 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 ENGINE STRUT FWD HYD LINE AT FEED THROUGH UNION HAS WRONG SPACER INSTALLED AT PYLON SKIN OTBD SIDE. COMPLIED WITH EA F-2910-T0301761. MAJOR REPAIR.
- [SDR FDEA201309122198](https://openairdocs.org/sdr/FDEA201309122198.md): Stringer · cracked · Sep 12, 2013 · N985FD · Boeing 757230 · Fuselage Main, Longeron/Stringer
  > STRINGER 2R, BS 440 IS DAMAGED, STRINGER REPAIRED IAW 49799180001 AND EA757-5311-16-F4303, REV.
- [SDR FDEA201309052134](https://openairdocs.org/sdr/FDEA201309052134.md): Frame · corroded · Sep 5, 2013 · N985FD · Boeing 757230 · Fuselage Main, Frame
  > AFTER REMOVING THE FLOORBEAM AT BS 1681, CORROSION WAS FOUND ON FRAME AT RBL 02, WL 208.10, BS 1681, RT SIDE
- [SDR FDEA201308201976](https://openairdocs.org/sdr/FDEA201308201976.md): Seat Track · corroded · Aug 20, 2013 · N985FD · Boeing 757230 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER LOBE SEAT TRACK HAS CORROSION BS 440, RBL 45. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. R & R SEAT TRACK IAW SRM 51-40-02 AND DWG 143N5091. CAT "A" MAJOR REPAIR.
- [SDR FDEA201308171921](https://openairdocs.org/sdr/FDEA201308171921.md): Skin · dented · Aug 17, 2013 · N985FD · Boeing 757230 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE AT BS 1520 BETWEEN S23-24R DENTED. FOUND DENT TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. REPAIRED SKIN IAW SRM 53-00-01, FIG 201, REPAIR 16. CAT "B" MAJOR REPAIR.
- [SDR FDEA201308151903](https://openairdocs.org/sdr/FDEA201308151903.md): Crease Beam · corroded · Aug 15, 2013 · N985FD · Boeing 757230 · Fuselage Main, Structure
  > L2 DOOR INBD CREASE BEAM CHORD CORRODED. REMOVED CORROSION IAW-SRM-51-10-02, ORIG. MAT.080 100 PERCENT MAT LOSS, OUT OF LIMITS IAW-SRM-53-30-15 DETAIL VI FIG 101, PROCURED NEW BEAM PN 143N8328U53, BATCH 0002482082, LOCATED AND DRILLED IAW SRM-51-40-02 AND DW
- [SDR FDEA201308141886](https://openairdocs.org/sdr/FDEA201308141886.md): Skin · misrepaired · Aug 14, 2013 · N985FD · Boeing 757230 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BETWEEN BS 440-460, STR 16R MISREPAIRED. REPAIRED IAW-SRM-53-00-01 FIG 201, REPAIR 16, CAT "B" MAJOR.
- [SDR FDEA201308141885](https://openairdocs.org/sdr/FDEA201308141885.md): Skin · misrepaired · Aug 14, 2013 · N985FD · Boeing 757230 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BETWEEN BS 440 - 460, S18-19R MISREPAIRED. REPAIRED IAW-53-00-01, FIG 201 REPAIR 16. CAT "B" MAJOR REPAIR.
- [SDR FDEA201308121834](https://openairdocs.org/sdr/FDEA201308121834.md): Crease Beam · corroded · Aug 12, 2013 · N985FD · Boeing 757230 · Fuselage Main, Structure
  > BS 756 TO 780 LT INBD CREASE BEAM IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53 -30-13, FIG 101, DETAIL VIII. R & R CREASE BEAM BS 760 -900 IAW SRM 51-40-02 AND 143N5522-27. MAJOR REPAIR.
- [SDR FDEA201308061798](https://openairdocs.org/sdr/FDEA201308061798.md): Floorbeam · damaged · Aug 6, 2013 · N985FD · Boeing 757230 · Fuselage Main, Floor Beam
  > FLOORBEAM UPPER TE AT BS 310.5 HAS AREAS WITH GOUGES, NICKS AND SCRATCHES. REMOVED NICKS, GOUGES, AND SCRATCHES IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. R & R TEE RBL 68 - LBL 68 IAW SRM 51-40-02 AND DWG 141N5810, CA
- [SDR FDEA201308021749](https://openairdocs.org/sdr/FDEA201308021749.md): Seat Track · gouged · Aug 2, 2013 · N985FD · Boeing 757230 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK BS 440 TO 645 RBL 24.75 GOUGED AND SCRATCHED. REMOVED GOUGES AND SCATCHES IAW-SRM-53-00-52 AT STA 440-645, RBL 24.75 SEAT TRACK, ORIG MAT.070 AFTER REWORK.045,.025 MAT. LOSS, FOUND TO BE OUT OF LIMITS IAW-SRM-53-00-52 PG.102. R & R
- [SDR FDEA201308021753](https://openairdocs.org/sdr/FDEA201308021753.md): Seat Track · damaged · Aug 2, 2013 · N985FD · Boeing 757230 · Fuselage, Seat/Cargo Attach Fittings
  > AFTER REMOVING SEAT TRACK AT STA 1080-1180, LBL 45. A DAMAGED ELONGATED HOLE. FOUND OUT OF LIMITS IAW DWG 144N5024 AND SRM 51-40-02. R & R SEAT TRACK IAW-SRM-51-40-02 AND DWG 144N5024. WORK ACCOMPLISHED IS A CAT "A" MAJOR REPAIR.
- [SDR FDEA201308011743](https://openairdocs.org/sdr/FDEA201308011743.md): Seat Track · gouged · Aug 1, 2013 · N985FD · Boeing 757230 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK FROM FS 1540 TO 1600 RBL 24.75 IS GOUGED AND SCRATCHED. BLENDED AREA IAW SRM-53-00-52 FIG 101, FOUND TO BE OUT OF LIMITS IAW SRM-53-00-52, FIG 101. REMOVED SEAT TRACK IAW-SRM-51-40-02, PRECURED NEW SEAT TRACK IAW-DWG 146N5135, LOCATED A
- [SDR FDEA201308011742](https://openairdocs.org/sdr/FDEA201308011742.md): Seat Track · gouged · Aug 1, 2013 · N985FD · Boeing 757230 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK FROM FS 1540 TO 1600 RBL 45.50 RBL 45.50 IS GOUGED AND SCRATCHED. BLENDED AREA IAW SRM-53-00-52, FIG 101, DETAIL I, FOUND TO BE OUT OF LIMITS, PRECURED NEW SEAT TRACK IAW-DWG 146N5135, TREATED AND PRIMED IAW-SRM-51-20-01 LOCATED AND DRIL
- [SDR FDEA201307301702](https://openairdocs.org/sdr/FDEA201307301702.md): Frame · corroded · Jul 30, 2013 · N985FD · Boeing 757230 · Fuselage Main, Frame
  > FOUND DURING REMOVAL OF WATER SERVICE PAN ASSY. FRAME AT BS 1661 S27-28L CORRODED ON FWD WEB. REMOVED CORROSION IAW-SRM-51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, PG 103, FIG 101 DET. II, R & R FRAME IAW SRM 51-40-02 AND DWG146N1024, CAT "A" MA
- [SDR FDEA201307291694](https://openairdocs.org/sdr/FDEA201307291694.md): Frame · dented · Jul 29, 2013 · N985FD · Boeing 757230 · Fuselage Main, Frame
  > BS 820 FWD CARGO BAY FRAME DENTED BETWEEN S24-25R. FOUND FRAME OUT OF LIMITS, IAW SRM-53-00-07 FIG 101 SHEET 1, NO DENTS ALLOWED ON FLANGES. R & R FRAME IAW SRM-51-40-02 AND DWG 143N1024, CAT "A" MAJOR REPAIR.
- [SDR FDEA201307251664](https://openairdocs.org/sdr/FDEA201307251664.md): Stringer · corroded · Jul 25, 2013 · N985FD · Boeing 757230 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 28R, BS 1520, FOUND EXFOLIATED OUT OF LIMITS IAW-SRM-53-00-03 FIG 101 DETAIL PG 102. REMOVED DAMAGED SECTION OF STRINGER IAW-SRM-53-00-03 FIG 201, SHEET 1 REPAIR 2. INSTALLED REPAIR STRINGER AND FILLER IAW SRM-53-00-03 FIG 201, SHEET
- [SDR FDEA201307241656](https://openairdocs.org/sdr/FDEA201307241656.md): Crease Beam · corroded · Jul 24, 2013 · N985FD · Boeing 757230 · Fuselage Main, Structure
  > R2 DOOR AREA, INBD CREASE BEAM CORRODED. REMOVED CORROSION IAW SRM-51-10-02, CHECKED LIMITS IAW-SRM-53-30-15, DET VI FIG 101 FOUND TO BE OUT OF LIMITS. R & R INBD CREASE BEAM IAW SRM 51-40-02 AND DWG 143N8328. CAT "A" MAJOR REPAIR.
- [SDR FDEA201307221636](https://openairdocs.org/sdr/FDEA201307221636.md): Floorbeam · corroded · Jul 22, 2013 · N985FD · Boeing 757230 · Fuselage Main, Floor Beam
  > FWD CARGO BAY BS 740 RBL 72 TO LBL72, FLOORBEAM IS CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL VI. R & R FLOORBEAM IAW SRM 51-40-02 AND DWG 143N5016. CLASSIFIED AS A CATEGORY `A` MAJOR REPAIR.
- [SDR FDEA201307161576](https://openairdocs.org/sdr/FDEA201307161576.md): Crease Beam · misrepaired · Jul 16, 2013 · N985FD · Boeing 757230 · Fuselage Main, Structure
  > CREASE BEAM BS 1620 MISREPAIRED. R & R CREASE BEAM BS 1370-1630 WITH A NEW ONE IAW-SRM-51-40-02 AND DWG 146N5590, CAT "A" MAJOR REPAIR.
- [SDR FDEA201307131554](https://openairdocs.org/sdr/FDEA201307131554.md): Bulkhead · gouged · Jul 13, 2013 · N985FD · Boeing 757230 · Nacelle/Pylon, Bulkhead/Firewall
  > LT PYLON, NAC STA 101 BULKHEAD, LT WEB GOUGED.
- [SDR FDEA201307131553](https://openairdocs.org/sdr/FDEA201307131553.md): Firewall · chafed · Jul 13, 2013 · N985FD · Boeing 757230 · Nacelle/Pylon, Bulkhead/Firewall
  > NR 2 ENGINE STRUT, INBD FIREWALL AFT SIDE CHAFED.

Next page: https://openairdocs.org/aircraft/N985FD/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 = 'N985FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N985FD/reports

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