# Service difficulty reports: N794FD

A list on [N794FD](https://openairdocs.org/aircraft/N794FD.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 · 92 reports

- [SDR FDEA202609171355](https://openairdocs.org/sdr/FDEA202609171355.md): Pitot Tube · dirty · Sep 17, 2026 · N794FD · Boeing 757222 · Pitot/Static System
  > AT APPROXIMATELY 3,000 AIRCRAFT HIT A LARGE BIRD. NO UNUSUAL INDICATIONS ON ANY INSTRUMENTS. STRIKE HIT DIRECTLY IN FRONT OF RIGHT SIDE PITOT TUBES. DECLARED EMERGENCY AND RETURNED TO MEM. REMOVED AND REPLACED FO AUX PITOT PROBE. APPLIED SEALANT AROUND BOTH
- [SDR FDEA202608271241](https://openairdocs.org/sdr/FDEA202608271241.md): Lamp · inoperative · Aug 27, 2026 · N794FD · Boeing 757222 · Emergency Lighting
  > FOUND CENTER OVERHEAD EMERGENCY EXIT SIGN VERY DIM DURING MX PRE-FLIGHT. FOUND 22 OF THE 24 BULBS BURNT OUT. REMOVED AND REPLACED ALL 24 CENTER OVERHEAD EMERGENCY EXIT SIGN BULBS IAW AMM: 33-51-01-2. OPS CHKD GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202608201190](https://openairdocs.org/sdr/FDEA202608201190.md): Unknown · odor · Aug 20, 2026 · N794FD · Boeing 757222 · Air Distribution System
  > ODOR OF BURNING OCCURRED AFTER TAKEOFF. ODOR INTENSIFIED DURING CLIMB. EMERGENCY DECLARED. O2 MASKS DEPLOYED. QRH FOR FUMES EVENT C/W. COCKPIT SWITCHES LEFT IN QRH POSIT. EMER DECLARED. AMM 21-51-02-7, AMM 21-00-01-3, FIM 71-05, FAULT TREE 811. INSPECTED
- [SDR FDEA202603060323](https://openairdocs.org/sdr/FDEA202603060323.md): Skin · gouged · Mar 6, 2026 · N794FD · Boeing 757222 · Elevator, Plate/Skin
  > DURING AGING, FOUND REPAIR IN LH ELEVATOR FWD OF T/E 1" FROM I/B EDGE ORIGINALLY REPAIRED ON NR N00012 WO# 00080212 WITH DATA INCOMPLETE BLOCKS 16,17,20,21,21A OF ORIGINAL NR FILLED OUT INCORRECTLY REMOVED EXISTING REPAIR AT LH ELEVATOR UPPER SURFACE 24.7
- [SDR FDEA202603050316](https://openairdocs.org/sdr/FDEA202603050316.md): Skin · cracked · Mar 5, 2026 · N794FD · Boeing 757222 · Wing, Plate/Skin
  > L/WING O/B LEADING EDGE SLAT # 3 O/B INTERNAL MAIN TRACK SLAT HAS COVER SKIN PANEL POSSIBLE CRACK REMOVED AND REPLACED COVE SKIN PANEL LOC AT SLAT # 3 LH WING O/B LEADING EDGE MAIN TRACK AREA IAW BOEING DWG # 114N4077 REV - PL # 114N4077 REV D AND B757 SR
- [SDR FDEA202510212056](https://openairdocs.org/sdr/FDEA202510212056.md): Battery Pack · inoperative · Oct 21, 2025 · N794FD · Boeing 757222 · Emergency Lighting
  > ON PRE-DAPARTURE CHECK FOUND EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED R/H EMERGENCY LIGHT BATTERY ASSY IAW AMM 33-51-07-2. OPERATIONAL CHECK OK. A/C OK FOR SERVICE.
- [SDR FDEA202404300531](https://openairdocs.org/sdr/FDEA202404300531.md): Drag Fitting · cracked · Apr 30, 2024 · N794FD · Boeing 757222 · Nacelle/Pylon, Main Frame
  > C/W EA F-5730-T0378682 WING - PLATES AND SKIN - RHW PYLON DRAG FITTING TO SKIN HOLES REINSPECTION OF PREVIOUS REPAIRS AND APPROVAL. COMPLIED WITH AND COMPLETED ALL STEPS 1-15 OF EA TF-5730-T0378682 PT1 WINGS - PLATES AND SKIN - RHW PYLON DRAG FITTING TO SK
- [SDR FDEA202404300527](https://openairdocs.org/sdr/FDEA202404300527.md): Drag Fitting · cracked · Apr 30, 2024 · N794FD · Boeing 757222 · Nacelle/Pylon, Main Frame
  > CW EA F-5730-T0378768 WINGS - PLATES AND SKIN - LHW PYLON DRAG FITTING TO SKIN HOLES - REINSPECTION OF PREVIOUS REPAIRS AND APPROVAL. COMPLIED WITH AND COMPLETED ALL STEPS 1-13 OF EA TF-5730-T0378768 PT1. WINGS - PLATES AND SKIN - LHW PYLON DRAG FITTING TO
- [SDR FDEA202205031106](https://openairdocs.org/sdr/FDEA202205031106.md): None · damaged · May 3, 2022 · N794FD · Boeing 757200 · Emergency Exits
  > PDIS 794 52-20 6569 02MAY22 BFM OPEN U FLT TEST: R1 DOOR SLIDE LIGHT INOP. INFO 02MAY22 19:33 ** ATTACHED TO WORK ORDER 00082315 ** INFO 02MAY22 19:46 ** DETACHED FROM WORK ORDER 00082315 ** NOT IN PCSE INFO 02MAY22 19:47 ** ATTACHED TO WO
- [SDR FDEA202204180986](https://openairdocs.org/sdr/FDEA202204180986.md): Angle · cracked · Apr 18, 2022 · N794FD · Boeing 757200 · Fuselage Floor Panel
  > FWD CARGO COMPT STA. 580 LBL 45.5 MDC FLOOR BEAM HAS CRACK. PERFORMED A ANGLE REPAIR AT STA. 580 LBL 45 PER FEDEX DRAWING #SR57-53-004 AND E.A. F- 5310-T0367757A P1, FUSELAGE-MAINFRAME-FLOOR BEAM AT STA 580 AND LBL 45 CRACKED- REPAIR PER DRAWING SR57-53-004,
- [SDR FDEA202204150969](https://openairdocs.org/sdr/FDEA202204150969.md): Floorboard · damaged · Apr 15, 2022 · N794FD · Boeing 757 · Standard Practices/Structures
  > ZONE 220 FLOOR BOARD 221MBF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VT MAE TRAVELER T22/1610229 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR
- [SDR FDEA202204150968](https://openairdocs.org/sdr/FDEA202204150968.md): Floor Panel · damaged · Apr 15, 2022 · N794FD · Boeing 757 · Standard Practices/Structures
  > ZONE 220 FLOOR BOARD 222MAF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VT MAE TRAVELER T22/1610312 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR
- [SDR FDEA202204150966](https://openairdocs.org/sdr/FDEA202204150966.md): Floorboard · damaged · Apr 15, 2022 · N794FD · Boeing 757 · Standard Practices/Structures
  > ZONE 220 FLOOR BOARD 221AF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VT MAE TRAVELER T22/1610228 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR
- [SDR FDEA202204150965](https://openairdocs.org/sdr/FDEA202204150965.md): Floorboard · damaged · Apr 15, 2022 · N794FD · Boeing 757 · Standard Practices/Structures
  > ZONE 220 FLOOR BOARD 221MAF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MAF ON VT MAE TRAVELER T22/1610230 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR
- [SDR FDEA202204150964](https://openairdocs.org/sdr/FDEA202204150964.md): Floorboard · damaged · Apr 15, 2022 · N794FD · Boeing 757 · Ignition System
  > ZONE 220 FLOOR BOARD 222MCF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MCF ON VT MAE TRAVELER #T22/1610311 IAW DWG SRZ-25-005. MAJOR REPAIR
- [SDR FDEA202010302722](https://openairdocs.org/sdr/FDEA202010302722.md): Gust Lock · failed · Oct 30, 2020 · N794FD · Boeing 757222 · Service Doors
  > R1 ENTRY DOOR GUST LOCK COLLAR CRACKED/BROKEN. REPLACED BROKEN R1 DOOR HOLD-OPEN LOCK COLLAR WITH A NEW SPLIT COLLAR AND CATCH, REF B757 AMM 52-11-08-8. ALLIANCE AEROSPACE ENGINEERING KIT PN 10-N0244-8 CONTAINS 10-N6008-4 (LOT 22457 SN 12-0010) 10-N6009-1 (L
- [SDR FDEA202004300847](https://openairdocs.org/sdr/FDEA202004300847.md): Light · inoperative · Apr 30, 2020 · N794FD · Boeing 757222 · Emergency Lighting
  > EXTERIOR EXIT DOOR LIGHT OUTSIDE OF L1 DOOR NOT TESTING.
- [SDR FDEA202004300846](https://openairdocs.org/sdr/FDEA202004300846.md): Light · inoperative · Apr 30, 2020 · N794FD · Boeing 757222 · Emergency Lighting
  > DURING PRE-FLIGHT NOTED EMERGENCY EXIT LIGHT OVER L1 DOOR NOT TESTING. ALONG WITH THE EMERGENCY LIGHT JUST OUTSIDE OF L1 DOOR
- [SDR FDEA202003170582](https://openairdocs.org/sdr/FDEA202003170582.md): Stringer · corroded · Mar 17, 2020 · N794FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > POPPED RIVET HEAD EXTERIOR FUSELAGE STA 1460 STR 29L. REMOVED RIVETS AT STA 1460,STR 29L IAW B 757 SRM 51-40-02-OG,REMOVED AND REINSTALLED STRINGER SPLICE AT STA 1452 TO 1468 IAW B 757 SRM 51-40-02-OG.FOUND CORROSION ON STRINGER SECTION,29L 100% MAT. LOSS,
- [SDR FDEA2020031200520](https://openairdocs.org/sdr/FDEA2020031200520.md): Angle · corroded · Mar 10, 2020 · N794FD · Boeing 757222 · Cargo/Baggage Doors
  > AFTER REMOVING C1 DOOR LOWER CENTER DEPRESSOR,FOUND #3 ANGLE CORRODED,LOKING FWD TO AFT AT APPROX. STA 588.93 EVALUATED FWD CARGO DOOR LOWER #3 ANGLE 100% MATERIAL LOSS DUE TO CORR. OUT OF LIMITS IAW B 757,SRM 52-30-02-1A,DETAIL VI. REMOVED,FABRICATED AND
- [SDR FDEA2020031200519](https://openairdocs.org/sdr/FDEA2020031200519.md): Angle · corroded · Mar 10, 2020 · N794FD · Boeing 757222 · Cargo/Baggage Doors
  > AFTER REMOVING C1 DOOR LOWER CENTER DEPRESSOR,FOUND #4 ANGLE CORRODED,LOKING FWD TO AFT AT APPROX. STA 600. EVALUATED FWD CARGO DOOR LOWER #4 ANGLE,ORIF. MAT=.050",REM. MAT=.024",MAT LOSS=.026" FOUND TO BE OUT OF LIMITS IAW B 757 SRM 52-30-02-1A,DETAIL VI
- [SDR FDEA2020031200522](https://openairdocs.org/sdr/FDEA2020031200522.md): Angle · corroded · Mar 10, 2020 · N794FD · Boeing 757222 · Cargo/Baggage Doors
  > AFTER REMOVING C1 DOOR LOWER CENTER DEPRESSOR,FOUND #1 ANGLE CORRODED,LOKING FWD TO AFT AT APPROX. STA 572.53 EVALUATED FWD CARGO DOOR LOWER # 1 ANGLE 100% MATERIAL LOSS DUE TO COORR. OUT OF LIMITS IAW B 757 SRM 52-30-02-1A DET VI. REMOVED,FABRICATED AND I
- [SDR FDEA2020031200521](https://openairdocs.org/sdr/FDEA2020031200521.md): Angle · corroded · Mar 10, 2020 · N794FD · Boeing 757222 · Cargo/Baggage Doors
  > AFTER REMOVING C1 DOOR LOWER CENTER DEPRESSOR,FOUND #2 ANGLE CORRODED,LOKING FWD TO AFT AT APPROX. STA 580. EVALUATED FWD CARGO DOOR LOWER #2 ANGLE 100% MATERIAL LOSS DUE TO CORR. OUT OF LIMITS IAW B 757 SRM 52-30-02-1A DET.VI. REMOVED,FABRICATED AND INST
- [SDR FDEA2020031200518](https://openairdocs.org/sdr/FDEA2020031200518.md): Angle · corroded · Mar 10, 2020 · N794FD · Boeing 757222 · Cargo/Baggage Doors
  > AFTER REMOVING C1 DOOR LOWER CENTER DEPRESSOR,FOUND #5 ANGLE CORRODED,LOKING FWD TO AFT AT APPROX. STA 607.47 EVALUATED FWD CARGO LOWER #5 ANGLE 100% MATERIAL LOSS DUE TO CORR. OUT OF LIMITS IAW B 757 SRM 52-30-02-1A DET VI REMOVED,FABRICATED AND INSTALLED
- [SDR FDEA2020030650496](https://openairdocs.org/sdr/FDEA2020030650496.md): Skin · gouged · Mar 5, 2020 · N794FD · Boeing 757222 · Trailing Edge Flaps
  > R / WING OB FLAP L/E UPPER SKIN GOUGE. REMOVED GOUGE ON RT WING O/B FLAP L/E FOUND O/B BLENDOUT TO BE OUT LIMITS IAW B757 SRM 57-53-01-1A FIG 101 DET. VI AND SRM 51-10-02-OG,CUT OUT DAMAGE AREA AND INSTALLED REPAIR DOUBLERS,STRAPS AND REPAIR PLATE IAW B75
- [SDR FDEA201903060553](https://openairdocs.org/sdr/FDEA201903060553.md): Brake · lack of lube · Mar 6, 2019 · N794FD · Boeing 757222 · Trailing Edge Flap Control System
  > TE FLAPS DISAGEE WHEN SELECTING FLAPS 25. FLAPS DID NOT MOVE PAST 20. TROUBLESHOT PER FIM 27-51-01 FT 808 FIG 105. FOUND RIGHT INBOARD FLAP TRANSMISSION OVERLOAD INDICATOR TRIPPED. PERFORMED LUBRICATION OF THE FLAP TRANSMISSION TORQUE BRAKE AND BALLSCREW/G
- [SDR FDEA201807211808](https://openairdocs.org/sdr/FDEA201807211808.md): Tail Cone · damaged · Jul 21, 2018 · N794FD · Boeing 757222 · Aerodynamic Fairings
  > TAIL SECTION DAMAGE AROUND APU EXHAUST AREA ALONG WITH APU DR(S). APU DOOR DAMAGE WILL BE WORKED ON WRI 52-40/3817. REMOVED DAMAGED APU EXHAUST TAIL CONE REF AMM 49-81-01-2. NO DAMAGE FOUND TO APU EXHAUST DUCT REF AMM 49-81-01-2. FIVE MISS-ALIGNED HOLES NEED W
- [SDR FDEA201807211807](https://openairdocs.org/sdr/FDEA201807211807.md): Door · damaged · Jul 21, 2018 · N794FD · Boeing 757222 · Auxiliary Power Unit (APU) Doors
  > APU ACCESS DOORS DAMAGED. REMOVED DAMAGED LEFT AND RIGHT APU ACCESS DOORS REFERENCING THE AMM 52-48-05-4. INSTALLED SERVICEABLE RIGHT APU ACCESS DOOR REFERENCING AMM 52-48-05-4. OPERATIONAL CHECKS GOOD FOR FUNCTION AND SECURITY.
- [SDR FDEA201807211806](https://openairdocs.org/sdr/FDEA201807211806.md): Door · damaged · Jul 21, 2018 · N794FD · Boeing 757222 · Auxiliary Power Unit (APU) Doors
  > APU ACCESS DOORS DAMAGED. REMOVED DAMAGED LEFT AND RIGHT APU ACCESS DOORS REFERENCING AMM 52-48-05-4. INSTALLED A SERVICEABLE LEFT DOOR ASSY (315AL) REFERENCING AMM 52-48-05-4 AND ERS 18-03216. REMOVED PART HAS NO P/N OR S/N. WORKBENCH REMOVAL AND INSTALLATIO
- [SDR 201712243443](https://openairdocs.org/sdr/201712243443.md): Unknown · unknown · Dec 24, 2017 · N794FD · Boeing 757 · Fuselage Main, Plate/Skin
  > A/C WAS HIT BY GROUND VEHICLE DURING LOADING REPAIR CURRENTLY IN PROGRESS REQUIRING SHEET METAL FABRICATION AND ENGINEERING SUPPORT. SDR SUBMITTED TO DOCUMENT MAJOR REPAIR.
- [SDR FDEA201711073185](https://openairdocs.org/sdr/FDEA201711073185.md): Light · inoperative · Nov 7, 2017 · N794FD · Boeing 757222 · Emergency Lighting
  > R1 DOOR EMERGENCY SLIDE LIGHT INOP DURING TEST. RELAMPED AND OPS CHECK NORMAL REF MM 33-51-06-2-1. A/C OK FOR SERVICE.
- [SDR FDEA201708222294](https://openairdocs.org/sdr/FDEA201708222294.md): Transmission · failed · Aug 22, 2017 · N794FD · Boeing 757222 · Leading Edge Slat Actuator
  > ON APPROACH, RECEIVED A TE FLAPS DISAGREE EICAS AND LIGHT THROUGH FLAPS 15 TO 20 SETTING. COMPLIED WITH QRH AND FOUND THE RIGHT INBD FLAP INBD FLAP TRANSMISSION OVERLOAD INDICATOR TRIPPED. RESET OVERLOAD INDICATOR,. LUBRICATED THE FLAP BALLSCREW, GIMBLE
- [SDR FDEA201612294574](https://openairdocs.org/sdr/FDEA201612294574.md): Indicator · defective · Dec 29, 2016 · N794FD · Boeing 757222 · Trailing Flap Position Indicating System
  > DURING FLAP EXTENSION FROM 20 TO 30, L FLAP INDICATOR MOVED TO 30 WHILE R FLAP INDICATOR REMAINED AT 20. NO FLAP ASYM EICAS, NO ROLLING MOTION FELT (AUTOPILOT WAS OFF). REPOSITIONED FLAPS TO 20, COMPLIED WITH QRH, LANDED FLAPS 20. INSTALLED NEW INDICATOR AND
- [SDR FDEA201409142610](https://openairdocs.org/sdr/FDEA201409142610.md): Reservoir · low pressure · Sep 14, 2014 · N794FD · Boeing 757222 · Passenger/Crew Doors
  > R1 DOOR EMER POWER RESERVOIR PRESS LOW. REPLACED EMER POWER RESERVOIR FOR R1 DOOR. CHECK GOOD IAW MM.
- [SDR FDEA201407021603](https://openairdocs.org/sdr/FDEA201407021603.md): Light · inoperative · Jul 2, 2014 · N794FD · Boeing 757222 · Emergency Lighting
  > L1 DOOR SLIDE EMER LIGHT INOPERATIVE. RELAMPED L1 DOOR SLIDE LIGHT IAW MM 33-51-06-2-1. OPERATIONS CHECKED GOOD.
- [SDR FDEA201404230795](https://openairdocs.org/sdr/FDEA201404230795.md): Skin · scratched · Apr 23, 2014 · N794FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN REPAIR SCRATCHED BS 1480 - 1500 STRINGER 21L. REPAIRED IAW EA F-5330-T0305873 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201404230794](https://openairdocs.org/sdr/FDEA201404230794.md): Skin · gouged · Apr 23, 2014 · N794FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN REPAIR GOUGED AT BS 1500 - 1520 BETWEEN STRINGERS 21 - 22 LT. REPAIRED IAW EA F-5330-T0305873 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201404230793](https://openairdocs.org/sdr/FDEA201404230793.md): Skin · gouged · Apr 23, 2014 · N794FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN REPAIRGOUGED AT BS 1498 BETWEEN STRINGERS 22 - 23L. REPAIRED IAW EA F-5330- T0305873 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201404230792](https://openairdocs.org/sdr/FDEA201404230792.md): Skin · gouged · Apr 23, 2014 · N794FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE REPAIR GOUGED AT BS 1485 BETWEEN STRINGER 22 - 23L. REPAIRED IAW EA F-5330-T0305873 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201404230796](https://openairdocs.org/sdr/FDEA201404230796.md): Strap · corroded · Apr 23, 2014 · N794FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT CARGO DOOR CUT OUT NUTPLATE RETAINING STRAP HAS CORROSION. COMPLIED WITH EA F-5310-T0306966 PT 1, TITLE FUSELAGE, MAINFRAME, ACCOMPLISH EXISTING REPAIR AT LOWER NR 2 CARGO DOOR WAY LOWER MAIN SILL STATION 1391, 1400, 1406 & 1429. REP
- [SDR FDEA201404230788](https://openairdocs.org/sdr/FDEA201404230788.md): Floorbeam · corroded · Apr 23, 2014 · N794FD · Boeing 757222 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM BS 365 EXISTING REPAIR HAS CORROSION AT RBL 8 & 24. ACCOMPLISHED EA F-5310-T0307490 PART 1 TITLE FUSELAGE, MAINFRAME & FLOORBEAM REPAIR, STATION 365.25 LBL 10 - RBL 70. REFER TO SNRM N01804 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201404200790](https://openairdocs.org/sdr/FDEA201404200790.md): Skin · scratched · Apr 20, 2014 · N794FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE REPAIR SCRATCHED AT BS 1440 - 1460 STRINGER 23 - 24L. REPAIRED IAW EA F-5330-T0305827 PART 1. REPAIR CLASSIFIED MAJOR IAW 6-2-100.
- [SDR FDEA201404200789](https://openairdocs.org/sdr/FDEA201404200789.md): Skin · damaged · Apr 20, 2014 · N794FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXISTING REPAIR, THERE IS A DAMAGED RIVET WITH A BULGE AT BS 1455 AT STRINGER 18 - 20 LT. COMPLIED WITH EA F-5330-T0305872 PART 1, TITLE FUSELAGE, PLATES & SKINS & FUSELAGE SKIN LAP JOINT REPAIR STATION 1400 - STATION 1459 STRINGER 18L - STRINGER 23L
- [SDR FDEA201403230549](https://openairdocs.org/sdr/FDEA201403230549.md): Sill · corroded · Mar 23, 2014 · N794FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY DOOR LOWER SILL BS 1380 - 1440 CORRODED AROUND SCREW HOLES. CORROSION REMOVED IAW SRM 51-40-05 REV 111. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
- [SDR FDEA201403210540](https://openairdocs.org/sdr/FDEA201403210540.md): Floorbeam · corroded · Mar 21, 2014 · N794FD · Boeing 757222 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM BS 310 RT SIDE, CORRODED ON THE EXISTING REPAIR. REPAIRED IAW SRM 51-40-02 REV 111 & DWG 141N5810 SHT 13 REV B. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201403190527](https://openairdocs.org/sdr/FDEA201403190527.md): Seat Track · chafed · Mar 19, 2014 · N794FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > BS 1320 - 1350, LBL 24.75, SEAT TRACK CROWN & BOTTOM FOUND CHAFED. REPAIRED IAW SRM 53-00-52 FIG. 201 REPAIR 1 REV 111. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201403190526](https://openairdocs.org/sdr/FDEA201403190526.md): Seat Track · chafed · Mar 19, 2014 · N794FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > BS 1280 - 1320, SEAT TRACK CROWN & BOTTOM FOUND CHAFED. REPAIRED IAW SNRM N02161. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201403170516](https://openairdocs.org/sdr/FDEA201403170516.md): Seal Depressor · chafed · Mar 17, 2014 · N794FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > R4 DOOR CUTOUT UPPER INNER SURFACE SEAL DEPRESSOR CHAFED. SEAL DEPRESSOR REMOVED AND REPLACED WITH NEW DEPRESSOR FABRICATED AS PER DWG 146N6123 SHT.1 REV.- AND INSTALLED IAW DWG 146N3700 SHT.11 REV.B. REPAIR IS MAJOR.
- [SDR FDEA201403090468](https://openairdocs.org/sdr/FDEA201403090468.md): Floor Panel · corroded · Mar 9, 2014 · N794FD · Boeing 757222 · Fuselage Floor Panel
  > CABIN RT SIDE FLOOR PANEL CORRODED ON EXISTING REPAIR AT BS 1681 AT RBL 12 UPPER SIDE. REPAIRED IAW EA F-5310-T0306261 PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201403090467](https://openairdocs.org/sdr/FDEA201403090467.md): Floor Panel · gouged · Mar 9, 2014 · N794FD · Boeing 757222 · Fuselage Floor Panel
  > FLOOR PANEL GOUGED ON THE EXISTING REPAIR AT BS 1683 AT RBL 55 UPPER SIDE. REPAIRED IAW EA F-5310-T0306261 PART 1. REPAIR CLASSIFIED AS MAJOR.

Next page: https://openairdocs.org/aircraft/N794FD/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 = 'N794FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N794FD/reports

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