# Service difficulty reports: N951FD

A list on [N951FD](https://openairdocs.org/aircraft/N951FD.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 · 84 reports

- [SDR FDEA202403090268](https://openairdocs.org/sdr/FDEA202403090268.md): Warning System · false activation · Mar 9, 2024 · N951FD · Boeing 757236 · Central Warning
  > DURING TAKEOFF ROLL AT APPROXIMATELY 80 KTS GOT OVERSPEED CLACKER ALONG WITH AIRSPEED, ALTITUDE AND VERTICAL SPEED FLAGS ON CAPT PFD. ALSO HAD GRND PROX EICAS AND GND PROX STATUS MESSAGES. TERR OVRD FAIL LIGHT ALSO ILLUMINATED FACT 09MAR24 14:43 CHS U
- [SDR FDEA202310041707](https://openairdocs.org/sdr/FDEA202310041707.md): Strap · corroded · Oct 4, 2023 · N951FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > STAB COMPT FWD O/B CORNER OF APU INLET STRAP HAS CORROSION. DOT 10/012. COMPLIED WITH EA # F-5330-T0376272 A P1 FUSELAGE - PLATES OF SKINS - APU DOOR SURROUND STRUCTURE FABRICATION OF SUPPORT ANGLES ALTERNATIVE SURFACE FINISH. MAJOR REPAIR.
- [SDR FDEA202310041702](https://openairdocs.org/sdr/FDEA202310041702.md): Strap · corroded · Oct 4, 2023 · N951FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > STAB COMPT FWD O/B CORNER OF APU INLET STRAP HAS CORROSION. DOT 10/012. COMPLIED WITH EA # F-5330-T0376272 A P1 FUSELAGE - PLATES OF SKINS - APU DOOR SURROUND STRUCTURE FABRICATION OF SUPPORT ANGLES ALTERNATIVE SURFACE FINISH. MAJOR REPAIR.
- [SDR FDEA202309281666](https://openairdocs.org/sdr/FDEA202309281666.md): Strap · corroded · Sep 28, 2023 · N951FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > STAB COMPT FWD O/B CORNER OF APU INLET STRAP HAS CORROSION. COMPLIED WITH EA F-5330-T0376272 A P1.
- [SDR FDEA202309261655](https://openairdocs.org/sdr/FDEA202309261655.md): Filler · gouged · Sep 26, 2023 · N951FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > LH AFT FUSE STA 1801 BTW STR 16L-17L HAS GOUGE ON FUSE SKIN. DOT 10/008. EVALUATED AREA,FOUND FILLER TO BE GOUGED ONLY. REMOVED AND REPLACED FILLER ONLY IAW SRM 53-80-70-2R REPAIR 2, FIG 201 AND TABLE 201 DETAIL I ON LH AFT FUSELAGE STA 1801 BETWEEN STR
- [SDR FDEA202212202959](https://openairdocs.org/sdr/FDEA202212202959.md): Girt Bar · obstructed · Dec 20, 2022 · N951FD · Boeing 757236 · Emergency Equipment
  > L1 DOOR SLIDE RAFT UNABLE TO BE ARMED. FOUND ATTACH SURVIVAL KIT STRAP D RING UNDER GIRT BAR (NO DAMAGE), REINSTALLED SURVIVAL KIT STRAP D RING IAW AMM FIG 405. L1 DOOR SLIDE ARMS AND DISARMS NORMAL IAW AMM 25-66-01-4.
- [SDR FDEA202110312702](https://openairdocs.org/sdr/FDEA202110312702.md): None · cracked · Oct 31, 2021 · N951FD · Boeing 757200 · Engine Thrust Reverser
  > #2 ENG I/B T/R EXTERNAL SURFACE FWD LOWER CORNER IS CRACKED. REPAIRED CRACK IN FIBERGLASS LAYERS OF #2 ENGINE I/B T/R EXTERNAL SURFACE FWD LOWER END ACTORATOR ACCESS PANEL IAW RR RB211 535-E4-37110 EM 78-31-300-084 PARA 17.
- [SDR FDEA202110312701](https://openairdocs.org/sdr/FDEA202110312701.md): None · delaminated · Oct 31, 2021 · N951FD · Boeing 757200 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE FAN CASE ATTRITION LINER AT 6 O,CLOCK POSITION HAS APPROX 2.5" BY 2" HOLE/HONEYCOMB MISSING. REMOVED AND INSTALLED NEW ATTRITION LINER IAW RB211 EM 72-34-14-300-007 AND REMOVED AND INSTALLED NEW ICE BREAKER PANELS IAW RB211 EM 72-34-14-300-014
- [SDR FDEA202110312699](https://openairdocs.org/sdr/FDEA202110312699.md): None · cracked · Oct 31, 2021 · N951FD · Boeing 757200 · Wing Main, Frame Structure
  > #9 SLAT INTERNAL COVE PANEL IS CRACKED @ OSS 574 REMOVED & REPLACED COVE PANEL IAW BAC DWG 114N4003, REV G & BAC DWG 114N4076 REV C
- [SDR FDEA202110312698](https://openairdocs.org/sdr/FDEA202110312698.md): None · cracked · Oct 31, 2021 · N951FD · Boeing 757200 · Wing Main, Frame Structure
  > #9 SLAT, INTERNAL COVE PANEL IS CRACKED @ OSS 604 REMOVED & REPLACE COVE PANEL ASSY IAW BAC DWG 114N4003 REV G & BAC DWG 114N4076 REV C
- [SDR FDEA202110302683](https://openairdocs.org/sdr/FDEA202110302683.md): None · none · Oct 30, 2021 · N951FD · Boeing 757200 · Trailing Edge Flap Control System
  > RH WING INB FWD FLAP LEADING EDGE WORN APPROX 73" OUTB OF THE INB EDGE REPAIRED RH WING INB FLAP LEADING EDGE NOSE SKIN DOUBLER IAW B757-200 SRM 57-53-01- 2R REPAIR 3
- [SDR FDEA202110262624](https://openairdocs.org/sdr/FDEA202110262624.md): None · delaminated · Oct 26, 2021 · N951FD · Boeing 757200 · Trailing Edge Flap Control System
  > RH I/B FWD FLAP UPPER SURFACE IS DELAMINATED APPROX 38" I/B OF THE O/B EDGE REPAIRED RH WING I/B FWD FLAP UPPER SKIN DELAM IAW B757 SRM: 57-53-01-2R FIG. 201 SHEET 2 AND 51-70-10-0G. MAJOR REPAIR.
- [SDR FDEA202110262623](https://openairdocs.org/sdr/FDEA202110262623.md): None · delaminated · Oct 26, 2021 · N951FD · Boeing 757200 · Trailing Edge Flap Control System
  > RH WING I/B FLAP UPPER SURFACE IS DELAMINATED APPROX 47" I/B OF O/B EDGE REPAIRED R/H WING I/B FWD FLAP UPPER SURFACE DELAM IAW B757 SRM: 57-53-01-2R FIG. 201 SHEET 2 AND 51-70-10-0G. MAJOR REPAIR
- [SDR FDEA202110212586](https://openairdocs.org/sdr/FDEA202110212586.md): Floor Panel · none · Oct 21, 2021 · N951FD · Boeing 757200 · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 242MAF, UPPER SURFACE IS DENTEDON FWD, INBD SIDE REPAIRED FLOOR PANEL IAW B757 SRM 53-00-50-2R, FIG 201, REPAIR 1
- [SDR FDEA202110212585](https://openairdocs.org/sdr/FDEA202110212585.md): Floor Panel · none · Oct 21, 2021 · N951FD · Boeing 757200 · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 242MBF, UPPER SURFACE IS DENTED IN 2EA LOCATIONS REPAIRED FLOOR PANEL IAW B757 SRM 53-00-50-2R, FIG 201, REPAIR 1
- [SDR FDEA202110212584](https://openairdocs.org/sdr/FDEA202110212584.md): Floor Panel · damaged · Oct 21, 2021 · N951FD · Boeing 757200 · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 241MAF, UPPER SURFACE IS PUNCTURED ON FWD, INBD SIDE REPAIRED FLOOR PANEL IAW B757 SRM 53-00-50-2R, FIG 201 REPAIR 1
- [SDR FDEA202110212583](https://openairdocs.org/sdr/FDEA202110212583.md): Floor Panel · none · Oct 21, 2021 · N951FD · Boeing 757200 · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 241MGF, UPPER SURFACE IS DENTED IN 2EA PLACES REPAIRED 2EA DENTS IAW B757 SRM 53-00-50-2R, FIG 201, RPEAIR 1
- [SDR FDEA202110212582](https://openairdocs.org/sdr/FDEA202110212582.md): Skin Panel · none · Oct 21, 2021 · N951FD · Boeing 757200 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER UPPER SKIN INBOARD OF LOGO LIGHT IS DENTED REPAIRED HORIZONTAL STABILIZER UPPER SKIN PANEL IAW B757 SRM 51-70-10-2R REPAIR 3 AND 4.
- [SDR FDEA202110192575](https://openairdocs.org/sdr/FDEA202110192575.md): Frame · cracked · Oct 19, 2021 · N951FD · Boeing 757200 · Fuselage Main, Structure
  > CRACK INDICATION NOTED AT THE LOWER, OUTBD HOLE AT STATION 1640 FRAME WEB, COMMON TO STRINGER 14L AS FOUND WHILE ACCOMPLISHING EO F-5310-E0344602 REPAIRED HOLE IAW FEDEX EA F-5310-T0364795
- [SDR FDEA202110132523](https://openairdocs.org/sdr/FDEA202110132523.md): None · cracked · Oct 13, 2021 · N951FD · Boeing 757200 · Fuselage Main, Structure
  > STATION 580 FLOORBEAM HAS A CRACK IN AFT UPPER FLANGE RADIUS @ APPROXIMATE LBL 40 REPAIRED FLOOR BEAM IAW FEDEX DRAWING SR57-53-004 & EA # F-5310-T0364849-P1
- [SDR FDEA2020010640017](https://openairdocs.org/sdr/FDEA2020010640017.md): Control Unit · failed · Jan 4, 2020 · N951FD · Boeing 757236 · Brake Anti-Skid Section
  > FOUND DURING WRI# 05-50/6574. ANTISKID/AUTOBRAKE CONTROL UNIT HAS MSG "BOX 1-5" THAT WILL NOT CLEAR. DURING TRANSDUCER SPINUP TEST, TRANSDUCER #1 SPINUP DOES NOT RESULT IN RELEASE OF BRAKE #5. REMOVED AND REPLACED ANTISKID/AUTOBRAKE CONTROL
- [SDR FDEA2019102422729](https://openairdocs.org/sdr/FDEA2019102422729.md): Skin · gouged · Oct 22, 2019 · N951FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > L\H SIDE OF EMPENNAGE HAS 2 EACH SMALL GOUGES AT STABILIZER LOWER SLIDING SEAL AREA BETWEEN B.S. 1800 AND B.S. 1810 BLENDED GOUGES ON L\H SIDE OF EMPENNAGE STA 1800 TO 1810 IAW B757 SRM 51-10-02. AFTER FURTHER EVAL FOUND STA 1810 TO BE OUT OF LIMITS IAW B7
- [SDR FDEA2019101762674](https://openairdocs.org/sdr/FDEA2019101762674.md): Skin · corroded · Oct 16, 2019 · N951FD · Boeing 757236 · Horizontal Stabilizer, Plate/Skin
  > LEFT SIDE HORIZONTAL STABILIZER EXTERIOR UPPER SKIN ALONG FRONT SPAR LOOSE AND FLAKING PAINT WITH BARE METAL AS MARKED. COMPLIED WITH EA # F-5510-T0350222 P1 TITLE: STABILIZERS - HORIZON STABILIZER - LH HORIZONTAL STABILIZER FWD TORQUE BOX UPPER SKIN B
- [SDR FDEA2019101762673](https://openairdocs.org/sdr/FDEA2019101762673.md): Skin · corroded · Oct 16, 2019 · N951FD · Boeing 757236 · Horizontal Stabilizer, Plate/Skin
  > RIGHT SIDE HORIZONTAL STABILIZER EXTERIOR UPPER SKIN ALONG FRONT SPAR LOOSE AND AND FLAKING PAINT WITH BARE METAL AS MARKED. COMPLIED WITH EA # F-5510-T0350281 P1. TITLE: STABILIZES-HORIZON STABILIZER-RH HORIZONTAL STABILIZER FWD TORQUE BOX UPPER SKIN BLEN
- [SDR FDEA2019041190776](https://openairdocs.org/sdr/FDEA2019041190776.md): Indicator · failed · Apr 9, 2019 · N951FD · Boeing 757236 · Trailing Flap Position Indicating System
  > WHEN EXTENDING FLAPS FROM 15 DEGREES TO 20 DURING APPROACH, TRAILING EDGE LIGHT ILLUMINATED, AND THE TE FLAP DISAGREE EICAS MESSAGE APPEARED. DELARED EMERGENCY, COMPLIED WITH THE QRH AND LANDED. ARFF RESPONSED TO THE EMERGENCY. TROUBLESHOT IN REF TO FIM
- [SDR FDEA201901030009](https://openairdocs.org/sdr/FDEA201901030009.md): Adc · failed · Jan 3, 2019 · N951FD · Boeing 757236 · Air Data Computer
  > AT 4000FT IN THE TURN TO JOIN 36L LOC THE CAPTAINS AIRSPEED BECAME UNRELIABLE. TEMP WAS 13 DEGREES C WITH ENG TAI OFF. AN EMERGENCY WAS DECLARED. ATC PROVIDED VECTORS TO ALLOW US TIME TO RUN THE AIRSPEED UNRELIABLE CHECKLIST. THE CHECKLIST WAS FOLLOWED AND D
- [SDR FDEA201711013128](https://openairdocs.org/sdr/FDEA201711013128.md): Guide · out of adjust · Nov 1, 2017 · N951FD · Boeing 757236 · Passenger/Crew Doors
  > UNABLE TO CLOSE THE L1 DOOR. DOOR PROGRAMMING INCORRECT. TIGHT AT FRONT, GAP AT TOP AFT CORNER. REMOVED THE L1 DOOR SLIDE COVER IAW AMM 52-11-00-5. ADJUSTED THE L1 DOOR GUIDE ARM AND HANDLE MECHANISM IAW AMM 52-11-04-2, AND 52-11-13-2. OPS CHECKED GOOD
- [SDR FDEA201701200236](https://openairdocs.org/sdr/FDEA201701200236.md): Cover · broken · Jan 20, 2017 · N951FD · Boeing 757236 · Escape Slide
  > R1 DOOR SLIDE COVER BOTTOM EDGE BROKEN POTTED NEW INSERTS IN R1 DOOR SLIDE COVER IAW AMM 25-00-00-8. REMOVED SAFTEY PIN AND INSTALLED R1 DOOR SLIDE COVER IAW AMM 52-11-02-4. OK FOR SERVICE
- [SDR FDEA201701200231](https://openairdocs.org/sdr/FDEA201701200231.md): Cover · broken · Jan 20, 2017 · N951FD · Boeing 757236 · Escape Slide
  > R1 DOOR SLIDE COVER BOTTOM EDGE BROKEN. POTTED NEW INSERTS IN R1 DOOR SLIDE COVER IAW AMM 25-00-00-8. REMOVED SAFTEY PIN AND INSTALLED R1 DOOR SLIDE COVER IAW AMM 52-11-02-4. OK FOR SERVICE.
- [SDR FDEA201510053084](https://openairdocs.org/sdr/FDEA201510053084.md): Skin · delaminated · Oct 5, 2015 · N951FD · Boeing 757236 · Trailing Edge Flaps
  > RIGHT WING INBD FLAP UPPER SURFACE IS DELAMINATION AT WS 258. REPAIRED RT WING, INBD FLAP UPPER SURFACE WS 258 BY HOT BONDING REPAIR PLYS IAW SRM 57-53-01-2R REPAIR 1 FIG 201 & SRM 51-70-07 PARA 4 G & EA F-5750-TO320630.
- [SDR FDEA201310282630](https://openairdocs.org/sdr/FDEA201310282630.md): Web · corroded · Oct 28, 2013 · N951FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > FLOOR WEB CORRODED UPPER SURFACE LBL 12 BS 420-440. REMOVED CORROSION FROM WEB, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 5.4.3.
- [SDR FDEA201310272628](https://openairdocs.org/sdr/FDEA201310272628.md): Seat Track · corroded · Oct 27, 2013 · N951FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SPLICE CORRODED, LBL 24, BS 420-440. REMOVED DAMAGED SEAT TRACK SPLICE. FABRICATED AND INSTALLED IAW DRAWINGS 3505,3475 REV G, AND 3458 REV K.
- [SDR FDEA201302060289](https://openairdocs.org/sdr/FDEA201302060289.md): Girt Bar · obstructed · Feb 6, 2013 · N951FD · Boeing 757236 · Emergency Equipment
  > LEFT FWD ENTRY DOOR DIFFICULT TO GET DOOR TO ARM PROPERLY, IN ARM POSITION, BUT TAKE REPEATED ATTEMPTS TO GET SLIDE ARMED LIGHT TO ILLUMINATE. CLEANED DEBRIS FROM LT FWD ENTRY DOOR, OPERATED SLIDE ARM SYSTEM IAW MM REF 25-66-00-5. ACFT OK TO CONTINUE.
- [SDR FDEA201208173056](https://openairdocs.org/sdr/FDEA201208173056.md): Seal · dirty · Aug 17, 2012 · N951FD · Boeing 757236 · Flight Compartment Windows
  > DURING DESCENT OUT OF 35000, PSID APPROX 8.0-7.8, A LOUD SQUEAL FROM F/O'S WINDOW. ONCE PSID GOT LOWER THAN 7.8 SQUEAL WENT AWAY. CLEAN WINDOW SEAL IAW MM 56-11-53-4 AND RETORQUED. FASTENERS ON FO'S SLIDING WINDOW IAW MM 56-11-02-4. PRESSURIZED ACFT
- [SDR FDEA201206082143](https://openairdocs.org/sdr/FDEA201206082143.md): Wire · damaged · Jun 8, 2012 · N951FD · Boeing 757236 · Hydraulic Power System Wiring
  > DURING CLIMB OUT, AT FL 330 RT HYD PRESSURE DROPPED TO ZERO, EICAS RT HYD SYS PRESSURE ILLUMINATED RT RF ON STATUS PAGE. PRESSURE RETURNED TO NORMAL AND EICAS WARNING EXTINGUISHED. FOUND THAT WHEN WIRE W4220-1001-22 AT ABOUT 3" FROM D42134P IS MOVED, THE RT H
- [SDR FDEA201112165324](https://openairdocs.org/sdr/FDEA201112165324.md): Girt Bar · malfunctioned · Dec 16, 2011 · N951FD · Boeing 757236 · Emergency Equipment
  > DOOR SLIDE DOES NOT ENGAGE WHEN ARMED. SLIDER FOUND NOT ATTACED TO GIRT BAR. REINSTALLED SLIDER AND GIRT BAR ASSY ONTO L1 DOOR AND PERFORMED ADJUSTMENT TESTS IAW MM 52-11-25-5. WITH DOOR CLOSED, GIRT BAR SLIDERS ENGAGE FLOOR FITTINGS AND SLIDE ARMS PROPERL
- [SDR FDEA201112155312](https://openairdocs.org/sdr/FDEA201112155312.md): Slide · malfunctioned · Dec 15, 2011 · N951FD · Boeing 757236 · Escape Slide
  > L1 DOOR SLIDE ARMED LIGHT DOES NOT ILLUMINATE. RELEASED FOR SERVICE IAW MEL 52-11-01-A.
- [SDR FDEA201112155284](https://openairdocs.org/sdr/FDEA201112155284.md): Lamp · inoperative · Dec 15, 2011 · N951FD · Boeing 757236 · Escape Slide
  > L1 ENTRY DOOR SLIDE LIGHT IS BURNED OUT. RELAMPED L1 ENTRY DOOR SLIDE LIGHT IAW MM 33-13-00-2, CHECKED GOOD AT THIS TIME.
- [SDR FDEA201111164932](https://openairdocs.org/sdr/FDEA201111164932.md): Skin · damaged · Nov 16, 2011 · N951FD · Boeing 757236 · Trailing Edge Flaps
  > LT WING OTBD T/E FLAP OTBD L/E CHAFING MARK FOUND. DAMAGED SKIN PANEL REPAIRED IAW EA F-5730-152588. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201111144905](https://openairdocs.org/sdr/FDEA201111144905.md): Tie Down · corroded · Nov 14, 2011 · N951FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > AFT LWR CARGO BAY TIE DOWN FITTING LT HAS CORROSION AT STA 1300. REPAIR CARRIED OUT IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201111144919](https://openairdocs.org/sdr/FDEA201111144919.md): Skin · dented · Nov 14, 2011 · N951FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN WITH EXISTING DENT AT BS 1701, BETWEEN STR 14L TO STR 15L. DENT REPAIR CARRIED OUT IAW EA F-5330-152589. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201111144909](https://openairdocs.org/sdr/FDEA201111144909.md): Tie Down · corroded · Nov 14, 2011 · N951FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > AFT LWR CARGO COMP TIE DOWN FITTING LT HAS CORROSION AT STA 1620. CORROSION REPAIR ON CARGO TIE DOWN FITTING CARRIED OUT IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201111144907](https://openairdocs.org/sdr/FDEA201111144907.md): Tie Down · corroded · Nov 14, 2011 · N951FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > AFT LWR CARGO COMP RT TIE DOWN FITTING HAS CORROSION AT STA 1220. REPAIR CARRIED OUT ON RT CARGO TIE DOWN FITTING IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201111144906](https://openairdocs.org/sdr/FDEA201111144906.md): Tie Down · corroded · Nov 14, 2011 · N951FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > AFT LWR CARGO COMP RT TIE DOWN FITTING HAS CORROSION AT STA 1240. REPAIR CARRIED OUT ON RT CARGO TIE DOWN FITTING IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201111144904](https://openairdocs.org/sdr/FDEA201111144904.md): Tie Down · corroded · Nov 14, 2011 · N951FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > AFT LWR CARGO BAY TIE DOWN FITTING LT HAS CORROSION AT STA 1460. REPAIR CARRIED OUT ON LT CARGO TIE DOWN FITTING AT STA 1460 IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201111144903](https://openairdocs.org/sdr/FDEA201111144903.md): Tie Down · corroded · Nov 14, 2011 · N951FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > AFT LWR CARGO BAY TIE DOWN FITTING LT HAS CORROSION AT STA 1240. REPAIR CARRIED OUT ON LT TIE DOWN FITTING AT STA 1240 IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201111144902](https://openairdocs.org/sdr/FDEA201111144902.md): Tie Down · corroded · Nov 14, 2011 · N951FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > AFT LWR CARGO BAY RT TIE DOWN FITTING HAS CORROSION AT STA 1280 CORROSION. REPAIR CARRIED OUT ON RT TIE DOWN FITTING AT STA 1280 IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201111144901](https://openairdocs.org/sdr/FDEA201111144901.md): Tie Down · corroded · Nov 14, 2011 · N951FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > AFT LWR CARGO BAY RT TIE DOWN FITTING HAS CORROSION AT STA 1600. REPAIR CARRIED OUT ON RT TIE DOWN FITTING AT STA 1600 IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201111144900](https://openairdocs.org/sdr/FDEA201111144900.md): Tie Down · corroded · Nov 14, 2011 · N951FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > AFT LWR CARGO BAY TIE DOWN FITTING LT HAS CORROSION AT STA 1220. REPAIR CARRIED OUT ON AFT CARGO COMPARTMENT LT TIE DOWN FITTING AT STA 1220 IAW EA F-5340-152586. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201111144899](https://openairdocs.org/sdr/FDEA201111144899.md): Tie Down · corroded · Nov 14, 2011 · N951FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > FWD LWR CARGO BAY RT TIE DOWN FITTING HAS CORROSION AT STA 540. CORROSION REPAIR CARRIED OUT ON RT TIE DOWN FITTING AT STA 540 IAW EA F-5340-152585. REPAIR IS CLASSIFIED AS MAJOR.

Next page: https://openairdocs.org/aircraft/N951FD/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 = 'N951FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N951FD/reports

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