# Service difficulty reports: N795FD

A list on [N795FD](https://openairdocs.org/aircraft/N795FD.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 3 · 134 reports

- [SDR FDEA202607220983](https://openairdocs.org/sdr/FDEA202607220983.md): Handle · no discrepancy · Jul 22, 2026 · N795FD · Boeing 757222 · Passenger/Crew Doors
  > DURING PREFLIGHT FOUND L1 DOOR OUTER DOOR HANDLES WILL NOT ENGAGE PROPERLY AND FREE SPIN.S. INNER DOOR HANDLES ENGAGE AND PROPERLY LOCK AND SECURE DOOR AND INDICATES CLOSED. RELEASED FOR SERVICE IAW MEL 52-11-01-A, CATEGORY B. FINISHED INSTALLATION OF
- [SDR FDEA202607110906](https://openairdocs.org/sdr/FDEA202607110906.md): Door · no discrepancy · Jul 11, 2026 · N795FD · Boeing 757222 · Passenger/Crew Doors
  > LEFT ENTRY DOOR WILL NOT CLOSE AND ARM. AMM 52-11-00-2 OPERATED L ENTRY DOOR FROM INSIDE AND OUTSIDE, DOOR ARMED AND DISARMED, A/C OK FOR SERVICE.
- [SDR FDEA202606120731](https://openairdocs.org/sdr/FDEA202606120731.md): Skin · cracked · Jun 12, 2026 · N795FD · Boeing 757222 · Elevator, Plate/Skin
  > LEFT HORIZONTAL STABILIZER, ELEVATOR TRAILING EDGE CRACKED BETWEEN ELEV STA 267.195 AND 244.501 UPPER AND LOWER T/E SKINS WITH CRACK AT LEFT HORIZONTAL STABILIZER ELEVATOR AREA BETWEEN ELEV STA 244.501-267.195 WERE REPAIRED IAW B757 SRM 55-20-01-2R AND SR
- [SDR FDEA202606120730](https://openairdocs.org/sdr/FDEA202606120730.md): Skin · cracked · Jun 12, 2026 · N795FD · Boeing 757222 · Wing, Plate/Skin
  > LEADING EDGE SLAT# 2 INTERNAL SKIN SHOWS A CRACK IN THE AREA OF THE INB MAIN TRACK PERFORMED REPAIR AT LEADING EDGE SLAT # 2 INTERNAL SKIN (COVE SKIN) OSS 737 IAW B757 SRM 57-43-01-2R REP 4 PARA 4
- [SDR FDEA202605050563](https://openairdocs.org/sdr/FDEA202605050563.md): Bulb · failed · May 5, 2026 · N795FD · Boeing 757222 · Emergency Lighting
  > FOUND L1 EXIT SIGN DIM DURING MX PRE-FLIGHT AMM: 33-51-01-2 REMOVED AND REPLACED 9 BAD BULBS AT THE L1 EMERGENCY EXIT SIGN (P/N OL3071BPEGPL). OPS CHECK GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202604250499](https://openairdocs.org/sdr/FDEA202604250499.md): Skin · delaminated · Apr 25, 2026 · N795FD · Boeing 757222 · Leading Edge Devices
  > LEFT WING NR 2 SLAT, UPPER SURFACE HAS SLAT SKIN PEELING UP. MARKED WITH TAPE. REPAIRED LT WING NR 2 SLAT TOP SKIN AT WS 688 IAW SRM 57-43-02-2R AND SRM 51-70-10-2R. THIS IS A MAJOR REPAIR, SEE JPF STEPS FOR OTHER WORK ACCOMPLISHED.
- [SDR FDEA202604250498](https://openairdocs.org/sdr/FDEA202604250498.md): Skin · delaminated · Apr 25, 2026 · N795FD · Boeing 757222 · Leading Edge Devices
  > LEFT WING NR 1 SLAT UPPER SURFACE HAS SLAT SKIN PEELING UP. REPAIRED LT WING NR 1 SLAT TOP SKIN AT WS 748.8 AND AT WS 737.5 (2 LOCATIONS) IAW SRM 57-43-02-2R, AND SRM 51-70-10-2R. THIS IS A MAJOR REPAIR, SEE JPF STEPS FOR OTHER WORK ACCOMPLISHED.
- [SDR FDEA202604240495](https://openairdocs.org/sdr/FDEA202604240495.md): Skin · dented · Apr 24, 2026 · N795FD · Boeing 757222 · Leading Edge Devices
  > NR 5 SLAT APPEARS TO HAVE A DENT REPAIRED LH WING #5 SLAT DENT DAMAGE AT WS.118 TOP SKIN SURFACE IN REF. TO 757 SRM:57- 43-02-2R AND 757 SRM 51-70-10-2R. THIS IS A MAJOR REPAIR, SEE JPF STEPS FOR OTHER WORK ACCOMPLISHED.
- [SDR FDEA202604120432](https://openairdocs.org/sdr/FDEA202604120432.md): Bearing · worn · Apr 12, 2026 · N795FD · Boeing 757222 · Passenger/Crew Doors
  > SUSPECT L1 DOOR OUT OF RIG. IT HAS BEEN MAKING CONTACT WITH THE LWR FWD AND THE UPPER AFT CAM ROLLERS ON DOOR FRAME. SEE PICS ATTACHED. REMOVED L1 PASSENGER DOOR GUIDE ARM AMM 52-11-04-2. R & R BEARINGS ITEM #25 IN BRACKET FOR L1 DOOR IAW CMM 52-17-09
- [SDR FDEA202604120431](https://openairdocs.org/sdr/FDEA202604120431.md): Bearing · worn · Apr 12, 2026 · N795FD · Boeing 757222 · Passenger/Crew Doors
  > L1 DOOR OUTER HANDLE MECHANISM FEELS WORN AND MAKING IT HARD TO OPERATE THE DOOR. PREVIOUS HISTORY. AMM 52-11-13-2 REMOVED L1 DOOR INTERIOR AND EXTERIOR HANDLES. REMOVED AND REPLACED BASKET CAM AND CAM FOLLOWER BEARING DUE TO WEAR. REINSTALLED INTERIOR
- [SDR FDEA202604100426](https://openairdocs.org/sdr/FDEA202604100426.md): Slide · damaged · Apr 10, 2026 · N795FD · Boeing 757222 · Escape Slide
  > ON WALK AROUND, FOUND L1 DOOR SLIDE PRESSURE GAUGE READING LOW. RELEASED FOR SERVICE PER MEL: 52-11-01-A CATEGORY: B. COMPLETED INSTALLATION OF L1 DOOR SLIDE AND PERFORMED OPS CHECK IAW M/M CHP 25-66-01-4.
- [SDR FDEA202512112238](https://openairdocs.org/sdr/FDEA202512112238.md): Slide · dislodged · Dec 11, 2025 · N795FD · Boeing 757222 · Escape Slide
  > STRAP HANGING OUT OF SLIDE PACK ON FWD LEFT ENTRY DOOR. STOWED STATIC LINE IAW AMM 25-66-01-4, & AMM 25-66-10-2. CHECKED OPERATION OF GIRT BAR ENGAGEMENT AND FOUND SATISFACTORY. OK FOR SERVICE.
- [SDR FDEA202506040834](https://openairdocs.org/sdr/FDEA202506040834.md): Power Supply · failed · Jun 4, 2025 · N795FD · Boeing 757222 · Emergency Lighting
  > EMERGENCY LIGHTS - FORWARD LEFT WILL NOT TEST. PERFORMED T/S PROCEDURES TO EMERGENCY LIGHTS FWR LEFT, FOUND POWER SUPPLY INOP, REMOVED AND REPLACE LEFT POWER SUPPLY "M731", SYS OPS CHECK NORMAL, ALL IAW FRMFIMFX1 33-51-00-815-802, AMM 33-51-07-2, WDM CH 3
- [SDR FDEA202505140752](https://openairdocs.org/sdr/FDEA202505140752.md): Stringer · corroded · May 14, 2025 · N795FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > S-29L WAS FOUND WITH SEVERE CORROSION DAMAGE NEAR STA 1460 (P/N 146N3110-184) REPAIRED IAW FDX EA# F-5310-T0383380 - FUSELAGE - MAINFRAME - STRINGER, STA 1430-1460, S- 29L, SPLICE
- [SDR FDEA202401060040](https://openairdocs.org/sdr/FDEA202401060040.md): Holder · inoperative · Jan 6, 2024 · N795FD · Boeing 757200 · Emergency Lighting
  > R1 EMERGENCY EXIT LIGHT, EMERGENCY EXIT LOCATION LIGHT AND SLIDE LIGHT INOP. REPLACED FORWARD BATTERY PACK IAW AMM 33-51-07-2, EMERGENCY LIGHTS AND SIGNS TEST GOOD. BATTERY PACK.
- [SDR FDEA202311101848](https://openairdocs.org/sdr/FDEA202311101848.md): Unknown · unknown · Nov 10, 2023 · N795FD · Boeing 757200 · Flight Compartment Equipment
  > PDIS 795 25-10 7278 10NOV23 OAK FACT U FO SHOULDER HARNESS NOT RETRACTING, STAYS PULLED OUT. AMM 25-11-04-4 PERFORMED ADJUSTMENT ON FO SHOULDER HARNESS AND OPS CHECK GOOD REF AMM 25-11-04-4
- [SDR FDEA202303300526](https://openairdocs.org/sdr/FDEA202303300526.md): Windshield · damaged · Mar 30, 2023 · N795FD · Boeing 757200 · Flight Compartment Windows
  > PDIS 795 56-10 6826 30MAR23 MEM OPEN U AT FL 390 AND 0.80M LEFT FRONT WINDOW SHATTERED. APPEARED TO BE SOME SORT OF STRIKE, MOST LIKELY A BIRD. REPLACED #1 WINDSHIELD
- [SDR FDEA202302210328](https://openairdocs.org/sdr/FDEA202302210328.md): None · none · Feb 21, 2023 · N795FD · Boeing 757200 · Standard Practices/Structures
  > PDIS 795 20-31 6768 21FEB23 MEM FACT U FO S SEATBELT BECAME DETACHED FROM SEAT WHEN FO TRIED TO BUCKLE BELT PRIOR TO PUSH BACK TIGHTEN BOLT UP.
- [SDR FDEA202207031683](https://openairdocs.org/sdr/FDEA202207031683.md): Drag Fitting · cracked · Jul 3, 2022 · N795FD · Boeing 757200 · Wing, Attach Fittings
  > #1 PYLON DRAG LINK FITTING HOLE #9 HAS REJECTABLE INDICATION AFTER REAMING TO 0.5930" DIAMETER. REMOVED AND REPLACED LH WING O/B DRAG FITTING IAW B757 SRM 57-20-01-2R REPAIR #8 AND E.A. F-5730-T0368664 P1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT DRAG
- [SDR FDEA202207031682](https://openairdocs.org/sdr/FDEA202207031682.md): Drag Fitting · cracked · Jul 3, 2022 · N795FD · Boeing 757200 · Wing, Attach Fittings
  > REMOVE RH WING INBD. DRAG FITTING TO COMPLY WITH E.A. #F-5730-T0368676 INSPECTION STEPS. C/W E.A.# F-5730-T0368676 P1 INSPECTION STEPS, WINGS-PLATES AND SKINS-RH WING, UPPER SKIN AT DRAG FITTING, CRACK AND CORROSION REPAIR-HOLE #2 AND SEVERAL OTHERS- DEVI
- [SDR FDEA202207031681](https://openairdocs.org/sdr/FDEA202207031681.md): Drag Fitting · cracked · Jul 3, 2022 · N795FD · Boeing 757200 · Wing, Attach Fittings
  > #2 PYLON SKIN, HOLE #2 HAS CRACK INDICATION AFTER REAMING TO 0.5930" REPAIRED #2 PYLON SKIN, HOLE #2 IAW B757 SRM 57-20-01-2R REPAIR #8 AND EA # F-5730- T0368676 P1 "WINGS-PLATES AND SKINS-RH WING, UPPER SKIN AT DRAG FITTING, CRACK AND CORROSION REPAIR-HOLE
- [SDR FDEA202207031680](https://openairdocs.org/sdr/FDEA202207031680.md): Drag Fitting · cracked · Jul 3, 2022 · N795FD · Boeing 757200 · Wing, Attach Fittings
  > RT WING I/B DRAG FITTING HOLE #3 HAS A REJECTABLE CRACK INDICATION. REMOVED AND REPLACED RH WING I/B DRAG FITTING IAW E.A. # F-5730-T0368676A PT1 AND DWG # 692N0001, SRM 57-20-01-2R (WINGS-PLATES AND SKINS-RH WING, UPPER SKIN AT DRAG FITTING, CRACK AND COR
- [SDR FDEA202206021357](https://openairdocs.org/sdr/FDEA202206021357.md): Seat Track · damaged · Jun 2, 2022 · N795FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > "DOT 143-036" FLIGHT DECK/COURIER AREA FLOOR STRUCTURE JUMP SEAT, L/H SEAT TRACK AT F/S 350 HAS DEEP DRILL START HOLE AND DEEP SCRATCHES FABRICATED SEAT TRACK IAW SRM 53-00-52-2R DETAIL I AND REMOVED AND REPLACED IAW SRM 53-00-52-2R, FIG. 201-OPTION 1 SHEE
- [SDR FDEA202205241289](https://openairdocs.org/sdr/FDEA202205241289.md): Floorboard · delaminated · May 24, 2022 · N795FD · Boeing 757200 · Fuselage Floor Panel
  > ZONE 220 FLOOR BOARD 221MBF IS DELAMINATED FABRICATED ZONE 220 FLOOR BOARD 221 MBF ON VTMAE TRAVELER T22/1617573 IAW DWG # SRZ-25-005 REVISION R, MAJOR REPAIR
- [SDR FDEA202205241287](https://openairdocs.org/sdr/FDEA202205241287.md): Floorboard · delaminated · May 24, 2022 · N795FD · Boeing 757200 · Fuselage Floor Panel
  > ZONE 220 FLOOR BOARD 222MAF IS DELAMINATED FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VTMAE TRAVELER T22/1617568 IAW DWG #SRZ-25-005 REVISION R, MAJOR REPAIR
- [SDR FDEA202011142854](https://openairdocs.org/sdr/FDEA202011142854.md): Lamp · inoperative · Nov 14, 2020 · N795FD · Boeing 757222 · Emergency Lighting
  > L-1 EXTERIOR EMERGENCY EXIT LIGHT INOPERABLE ON TEST. RELAMPED L 1 DOOR SLIDE LIGHT, PER B757-200 AMM 33-51-06-2-1. OPERATIONS CHECKS NORMAL.
- [SDR FDEA2020091422188](https://openairdocs.org/sdr/FDEA2020091422188.md): Light · inoperative · Sep 12, 2020 · N795FD · Boeing 757222 · Landing Gear Position and Warning
  > NO NOSE GEAR LIGHT AFTER GEAR WAS IN DOWN PISITION. R & R NOSE GEAR POSITION INDICATION MODULE, REF SMP'S AND IPC 33-14-70-03 & 32-61-51-01. MANUFACTURER KORRY P/N 674-1043-3205. OPS CHECK NORMAL. AC OK FOR SERVICE.
- [SDR FDEA2020061091169](https://openairdocs.org/sdr/FDEA2020061091169.md): Frame · cracked · Jun 9, 2020 · N795FD · Boeing 757222 · Fuselage Main, Frame
  > CRACK INDICATION FOUND: LT BS1640 AT S-14L AT LOWER I/B FASTENER HOLE AT INTERCOSTAL TEE CLIP. BETWEEN TEE CLIP & CHORD LAYER LOOKING AFT AT 8 O'CLOCK POSITION. (1ST & 2ND LAYER) ACCOMPLISHED EA F-5310-T0354398-P1 FUSELAGE - MAINFRAME - FRAME WEB, STA 1640 S14
- [SDR FDEA2020061091167](https://openairdocs.org/sdr/FDEA2020061091167.md): Latch · broken · Jun 9, 2020 · N795FD · Boeing 757222 · Escape Slide
  > R1 DOOR EVACUATION SLIDE LATCH ASSY BROKEN. REMOVED AND REPLACED R-1 DOOR EVACUATION SLIDE CATCH ASSY PER AMM 25-66-01-4 STEP 3.H1 (A).
- [SDR FDEA2020061091164](https://openairdocs.org/sdr/FDEA2020061091164.md): Pan · gouged · Jun 9, 2020 · N795FD · Boeing 757222 · Passenger/Crew Doors
  > L1 DOOR HAS GOUGE IN PAN AROUND HANDLE BASE. REMOVED AND REPLACED L-1 PASSENGER DOOR PER AMM 52-11-01-4.
- [SDR FDEA202005311094](https://openairdocs.org/sdr/FDEA202005311094.md): Strap · failed · May 31, 2020 · N795FD · Boeing 757200 · Fuselage Structure (General)
  > MAIN CABIN FLOOR BEAM AT STA 1681 HAS ONE NUTPLATE STRAP CORRODED AT APPROX. RBL 45 REMOVED CORRODED NUTPLATE STRAP IAW 757-200 SRM 51-40-02. FABRICATED AND INSTALLED NEW NUTPLATE STRAP IAW BAC DWG #146N5300 REV E.
- [SDR FDEA2020060111095](https://openairdocs.org/sdr/FDEA2020060111095.md): Fitting · cracked · May 31, 2020 · N795FD · Boeing 757222 · Nacelle/Pylon Miscellaneous Structure
  > RIGHT STRUT OB LOWER FWD END HAS A CRACKED CLIP. REMOVED AND REPLACED CLIP PART NR 313N3052-17 IAW DWG NR 313N3052 REV B AND SRM 51-40-02.
- [SDR FDEA2020060111094](https://openairdocs.org/sdr/FDEA2020060111094.md): Nut Plate · corroded · May 31, 2020 · N795FD · Boeing 757222 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM AT STATION 1681 HAS ONE NUTPLATE STRAP CORRODED AT APPROX RBL 45. REMOVED CORRODED NUTPLATE STRAP IAW SRM 51-40-02. FABRICATED AND INSTALLED NEW NUTPLATE STRAP IAW DWG NR 146N5300 REV E.
- [SDR FDEA2020043080809](https://openairdocs.org/sdr/FDEA2020043080809.md): Light · inoperative · Apr 28, 2020 · N795FD · Boeing 757222 · Emergency Lighting
  > L1 DOOR EXTERIOR EMERGENCY LIGHT INOP RELAMPED THE L1 DOOR EXTERIOR LIGHT IAW M/M33-51-06-2-1, AND OP'S TESTED NORMAL, THIS CLEARS MEL 33-51-02-02, A/C OK FOR SERVICE.
- [SDR FDEA201901130124](https://openairdocs.org/sdr/FDEA201901130124.md): Computer · failed · Jan 13, 2019 · N795FD · Boeing 757222 · Auto Throttle System
  > ON SELECTION OF THE THRUST TILE. AUTOTHROTTLES CAME UP NON SYMETRIC. REJECTED TAKE OFF IMMEDIATELY NO ENGINE ABNORMALITIES NOTED. REMOVED AND REPLACED TMC PER MM 22-31-01-4 AND OPS CHECK GOOD. ALSO PERFORMED SUCCESSFUL MCDP TESTS 30/40 AND RESET LLM TIMER REF
- [SDR FDEA201812073463](https://openairdocs.org/sdr/FDEA201812073463.md): Bulb · inoperative · Dec 7, 2018 · N795FD · Boeing 757222 · Emergency Lighting
  > R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P/N 767 IAW AMM 33-51-06-2. OPS CK NORMAL.
- [SDR FDEA201801130081](https://openairdocs.org/sdr/FDEA201801130081.md): Cable · iced · Jan 13, 2018 · N795FD · Boeing 757222 · Landing Gear Steering System
  > UPON LANDING NOTICED THAT TILLER WOULD NOT MOVE EITHER LEFT OR RIGHT. TILLER APPEARED TO BE LOCKED IN CENTER POSITION. STOPPED STRAIGHT AHEAD ON RUNWAY. FOUND ICE ON TRAILING EDGE OF BOTH NOSE GEAR DOORS, MATING SURFACE AS WELL AS ON STEERING CABLES. APPLIE
- [SDR FDEA201704081119](https://openairdocs.org/sdr/FDEA201704081119.md): Fitting · out of adjust · Apr 8, 2017 · N795FD · Boeing 757222 · Emergency Equipment
  > PORT SIDE MAIN ENTRY DOOR LIGHT WILL NOT COME ON WHEN DOOR ARMED. ADJUSTED THE GIRT BAR AND FLOOR FITTING IAW AMM 25-66-11-2. OPS CHECKED GOOD.
- [SDR FDEA201704081118](https://openairdocs.org/sdr/FDEA201704081118.md): Girt Bar · out of adjust · Apr 8, 2017 · N795FD · Boeing 757222 · Emergency Equipment
  > PORT SIDE MAIN ENTRY DOOR LIGHT WILL NOT COME ON WHEN DOOR ARMED. ADJUSTED GIRT BAR AND FLOOR FITTING IAW AMM 25-66-11-2. OPS CHECKED GOOD.
- [SDR FDEA201704051078](https://openairdocs.org/sdr/FDEA201704051078.md): Girt Bar · dirty · Apr 5, 2017 · N795FD · Boeing 757222 · Emergency Equipment
  > SLIDE LIGHT ABOVE LEFT DOOR WILL NOT ILLUMINATE WHEN ARMING THE DOOR. CLEANED AND LUBE GIRT BAR IAW AMM CH 12-21-18. PERFORMED OPERATIONAL CHECK IAW AMM CH 52-11-00. GRND OPS CKS GOOD, A/C RETURN TO SERVICE.
- [SDR FDEA201606292191](https://openairdocs.org/sdr/FDEA201606292191.md): Frame · dented · Jun 29, 2016 · N795FD · Boeing 757222 · Fuselage Main, Frame
  > LOWER FUSELAGE STA 231, BL0 FRAME HAS A DENT. TRIMMED OUT DAMAGED AREA ON FRAME BS 231.25 BL0. FABRICATED REPAIR ANGLE. INSTALLED REPAIR CW EA F-5310-T0326376 P1. THIS IS A MAJOR REPAIR. PERFORMED SATISFACTORY FUNCTIONAL OPS CHECK OF FWD ACCESS DOOR IAW
- [SDR FDEA201506111761](https://openairdocs.org/sdr/FDEA201506111761.md): Seal · contaminated · Jun 11, 2015 · N795FD · Boeing 757222 · Passenger/Crew Doors
  > R1 DOOR HAS VERY LOUD CONSTANT SQUEAL DURING FLIGHT. FOUND DEBRIS ON SEAL AND SILL, REMOVED THE DEBRIS IAW SMP.
- [SDR FDEA201501160204](https://openairdocs.org/sdr/FDEA201501160204.md): Girt Bar · loose · Jan 16, 2015 · N795FD · Boeing 757222 · Emergency Equipment
  > R1 DOOR REQUIRED MULTIPLE OPENINGS & CLOSINGS & SLIDE ARMING & DISARMING TO GET SLIDE ARM LIGHT TO COME ON. FOUND THE SCREWS LOOSE ON THE AFT GIRT BAR FITTING. TIGHTENED SCREWS AND IAW AMM 25-66-11-2,ARMING LIGHT AND PROXIMITY SWITCH OPERATES NORMAL.
- [SDR FDEA201407191857](https://openairdocs.org/sdr/FDEA201407191857.md): Shear Tie · chafed · Jul 19, 2014 · N795FD · Boeing 757222 · Fuselage Internal Mounting Structure
  > EXISTING REPAIR FINDING FWD CARGO EXISTING REPAIR AREA HAS CHAFE MARK ON THE SHEAR TIE AT STA 580 STR 27R - 28R. CHAFE MARK ON THE SHEAR TIE AT STA 580 STR 24R-28R REMOVED BY HANDCLEAN PER SRM 51-01-02 REV 111 AND TREATED PER SRM 51-20-01 REV 111. REPAIR CLA
- [SDR FDEA201407191856](https://openairdocs.org/sdr/FDEA201407191856.md): Angle · corroded · Jul 19, 2014 · N795FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > EXISTING REPAIR FINDING FWD CARGO EXISTING REPAIR AREA HAS CORROSION ON THE ANGLE AT STA 580 - 600 STR 26R - 27R. CORROSION ON INTERCOASTAL LOWER CHORD ANGLE REMOVED BY HANDCLEAN PER SRM 51-10-02 REV 111 AND TREATED PER SRM 51-20-01 REV 111. MATERIAL REMOVED
- [SDR FDEA201407181846](https://openairdocs.org/sdr/FDEA201407181846.md): Skin · scratched · Jul 18, 2014 · N795FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > EXISTING REPAIR FINDINGS FUSELAGE EXTERIOR SKIN HAS NUMEROUS SCRATCHES ON THE PERIMETER OF THE DOUBLER AT STATION 1560, STRINGER 6 LT AFTER DOUBLER REMOVED. SCRATCHES ON EXTERIOR SKIN REMOVED AND TREATED PER SRM 51-10-02 AND SRM 51-20-01 REV 111. REPAIR CL
- [SDR FDEA201407181848](https://openairdocs.org/sdr/FDEA201407181848.md): Skin · damaged · Jul 18, 2014 · N795FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > EA F-5330-T0308575 B SNRM 03640 PART 1 OF EA F-5330-T0308575 REV B TITLE FUSELAGE PLATES & SKINS AD 2006-11-11. GOUGE & DENT AT BS 1477 BETWEEN STRINGER 25L - 26L REPAIR COMPLIED. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201407181845](https://openairdocs.org/sdr/FDEA201407181845.md): Repair · damaged · Jul 18, 2014 · N795FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > EXISTING REPAIR FINDINGS FUSELAGE EXTERIOR EXISTING REPAIR EXTERIOR DOUBLER & TRIPLER HAVE NUMEROUS NICKS, SCRATCHES & TOOL MARKS AT STATION 1568 - 1613 STRINGER 18R - 24R. EXISTING REPAIR REMOVED & NEW REPAIR CARRIED OUT IAW PART 1 OF EA F-5330-T0308753 REV
- [SDR FDEA201407121751](https://openairdocs.org/sdr/FDEA201407121751.md): Skin · damaged · Jul 12, 2014 · N795FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN RT SIDE. AFTER DOUBLER REMOVAL & DEEP INSPECTION FOUND ELONGATED HOLES FROM BS 560 - 580 FROM STRINGER 26 TO 28. THERE ARE FIVE ELONGATED HOLES AS MARKED. ACCOMPLISH NEW REPAIR ON FUSELAGE SKIN BS 577. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201407121750](https://openairdocs.org/sdr/FDEA201407121750.md): Skin · damaged · Jul 12, 2014 · N795FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN. AFTER DOUBLER REMOVAL & DEEP INSPECTION FOUND ELONGATED HOLES FROM BS 560 - 580 FROM STRINGER 28 RT TO 28 LT. THERE ARE THREE ELONGATED HOLES AS MARKED. ACCOMPLISH NEW REPAIR ON FUSELAGE SKIN BS 577. REPAIR CLASSIFIED AS MAJOR.

Next page: https://openairdocs.org/aircraft/N795FD/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 = 'N795FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N795FD/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.