# Service difficulty reports: N974FD

A list on [N974FD](https://openairdocs.org/aircraft/N974FD.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 · 111 reports

- [SDR FDEA202306281120](https://openairdocs.org/sdr/FDEA202306281120.md): Hose · damaged · Jun 28, 2023 · N974FD · Boeing 757200 · Hydraulic System, Main
  > LEFT HYD SYS PRESS FOLLOWED BY L HYD QTY WHEN LANDING GEAR WAS EXTENDED ON FINAL. EXECUTED GO AROUND TO RUN QRH AND CAME BACK AND LANDED UNEVENTFUL. EMERGENCY DECLARED. UPON INSPECTION FOUND NLG STEARING PRESSURE SIDE FLEX LINE, IPC 32-34-51-15 ITEM 317,
- [SDR FDEA202306171048](https://openairdocs.org/sdr/FDEA202306171048.md): Unknown · unknown · Jun 17, 2023 · N974FD · Boeing 757200 · Flight Control System
  > DURING FLAP EXTENSION ON APPROACH, TRAILING EDGE FLAP DISAGREE EICAS MESSAGE WHEN FLAPS SELECTED FROM UP TO 1. COMPLIED WITH QRH, F20 LANDING, AND EMERGENCY WAS DECLARED. FLAP ISLN VAL STATUS MESSAGE DISPLAYED. FACT 17JUN23 12:44 CPR U FIM: 27-51 FAUL
- [SDR FDEA202304120630](https://openairdocs.org/sdr/FDEA202304120630.md): Unknown · unknown · Apr 12, 2023 · N974FD · Boeing 757200 · Trailing Edge Flap Control System
  > PDIS 974 27-50 9266 12APR23 MEM FACT U ON APPROACH AT FLAP EXTENSION TO FLAPS 1, RECEIVED A TE FLAP DISAGREE. DISCONTINUED APPROACH. COMPLIED WITH THE QRH, DECLARED AN EMERGENCY CHOSE 36C INSTEAD OF 36L. THE ALTERNATE SLAT/FLAP SYSTEM WORKE
- [SDR FDEA202211302859](https://openairdocs.org/sdr/FDEA202211302859.md): Unknown · odor · Nov 30, 2022 · N974FD · Boeing 7572Y0 · Air Distribution System
  > EXTREMELY STRONG ELECTRICALLY BURNING ODOR IN COCKPIT, DURING CLIMB AROUND 25,000 FT. ON ENTRY NO ODOR PRESENT.. CHECKED FOR CBS TRIPPED IN COCKPIT, ALL CLOSED. INSPECTED E & E BAY, OPENED ACCESS PANELS, FOUND NO EVIDENCE OF ODOR. FOUND LT LOGO LIGHT CB T
- [SDR FDEA202206161435](https://openairdocs.org/sdr/FDEA202206161435.md): Handle · unsecure · Jun 16, 2022 · N974FD · Boeing 757200 · Flight Compartment Windows
  > COPILOT S WINDOW HANDLE ROTATES OPEN DURING FLIGHT. THE FRONT LATCH STAYS LATCHED, BUT THE HANDLE ROTATES OPEN (HAS TO BE HELD SECURE) AND THE ALIGNMENT ARROWS AT THE AFT END OF THE WINDOW SPLIT APART FROM EACH OTHER. INSPECTED LOCKING MECHANISM OF THE
- [SDR FDEA202203120512](https://openairdocs.org/sdr/FDEA202203120512.md): None · none · Mar 12, 2022 · N974FD · Boeing 757200 · Passenger/Crew Doors
  > RAMP REPORTED L1 DOOR UNABLE TO BE OPEN FROM OUTSIDE. WHEN IT IS CLOSED WITH OUTSIDE HANDLE, INSIDE HANDLE DO NOT FOLLOW TO COMPLETE CLOSED POSITION. THE INSIDE HANDLE IS WORKING FINE, CLOSING AND OPENING DOOR WITHOUT PROBLEMS. REMOVED HANDLE MECHANISM I
- [SDR FDEA202110092503](https://openairdocs.org/sdr/FDEA202110092503.md): Flap System · faulted · Oct 9, 2021 · N974FD · Boeing 7572Y0 · Trailing Edge Flap Control System
  > TE FLAP DISAGREE ON APPROACH. RAN QRH. DECLARED EMERGENCY. LANDED. REPEAT WRITE UP. INTERROGATED FSEU, #1 SHOWS FAULT 305: FLAP ISOL VLV. T/S CONTINUE DURING INSPECTION, FOUND LACK OF LUBRICATION ON L/H AND R/H INBOARD DRIVE OF BOTH INNER FLAP WITH OVERLOAD I
- [SDR FDEA202110092501](https://openairdocs.org/sdr/FDEA202110092501.md): Unknown · faulted · Oct 9, 2021 · N974FD · Boeing 7572Y0 · Trailing Edge Flap Control System
  > TE FLAPS EICAS WHEN SELECTING FLAPS 1 FOR APPROACH. DUE TO QRH AND CHECKLIST DEMANDS, OPTED TO DISCONTINUE APPROACH. COORDINATED A HOLDING PATTERN AND RAN THE QRH AND ASSOCIATED CHECKLISTS. WERE ABLE TO COMPLETE ALTERNATE FLAPS TO 20 AND LAND NORMALLY.
- [SDR FDEA202102180399](https://openairdocs.org/sdr/FDEA202102180399.md): Battery Pack · inoperative · Feb 18, 2021 · N974FD · Boeing 7572Y0 · Emergency Lighting
  > MDIS 974 33-50 7299 18FEB21 MUC OPEN U SEE ALSO 33-50 WRI 7298: EMRGENCY LIGHTS IN CABIN MID AND RIGHT AND RIGHT EXTERIOR DOES NOT ILLUMINATE IN ALL POSITIONS. TROUBLESHOOTING PERFORMED, FOUND NO ILLUMINATION ON
- [SDR FDEA202102180398](https://openairdocs.org/sdr/FDEA202102180398.md): Battery Pack · misinstalled · Feb 18, 2021 · N974FD · Boeing 7572Y0 · Emergency Lighting
  > MDIS 974 33-50 7298 18FEB21 MUC OPEN U AFTER AIRCRAFT POWER OFF FOUND EMERGENCY LIGHT IN COCKPIT LEFT SIDE ABOVE DOOR AND LEFT EXTERIOR LIGHT ILLUMINATED. WITH AC POWER ON LIGHTS GO OFF. CHECKED AND MOVED EMERG. LIGHT SWITCH IN COCKPIT SEVER
- [SDR FDEA2020031210534](https://openairdocs.org/sdr/FDEA2020031210534.md): Collar · broken · Mar 11, 2020 · N974FD · Boeing 7572Y0 · Passenger/Crew Doors
  > L1 DOOR HOLD OPEN LOCK COLLAR BROKEN. REMOVED PANEL 221AL TO GET ACCESS TO COLLAR AS PER MM 52-11-08-4. INSTALLED COLLAR AND CATCH ASSY AS PER AMM 52-11-08-8. OPS CHECK OK. STILL NEED TO INSTALL THE 221AL PANEL WHICH STILL IN LEAD OFFICE. INSTALLED PANEL
- [SDR FDEA201912063197](https://openairdocs.org/sdr/FDEA201912063197.md): Power Supply · inoperative · Dec 6, 2019 · N974FD · Boeing 7572Y0 · Emergency Lighting
  > LT PASSENGER DOOR EXTERNAL EMERGENCY LIGHT L25 INOP. POWER SUPPLY M731 REPLACED.
- [SDR FDEA201909102200](https://openairdocs.org/sdr/FDEA201909102200.md): Shutoff Valve · inoperative · Sep 10, 2019 · N974FD · Boeing 7572Y0 · Pneumatic Distribution System
  > PDIS 974 36-10 5902 10SEP19 CDG OPEN U LOGPAGES:3010680 REJECTED TAKEOFF FOR " L ENG BLEED OFF " AFTER ENGINE REDUCED IDLE EICAS MESSAGE REMOVED. GOT EICAS MESSAGE ON SECOND TAKEOFF AND AFTER AIRBORNE RAN QRH AND SELECTED LEFT ENGINE BLEED AIR
- [SDR FDEA2019083092040](https://openairdocs.org/sdr/FDEA2019083092040.md): Skin · delaminated · Aug 29, 2019 · N974FD · Boeing 7572Y0 · Trailing Edge Flaps
  > RH I/B FLAP, LOWER SURFACE REPAIR 52" FORM O/B EDGE AND 13" FORM T/E. REPAIR FOUND TO BE UNSERVICABLE PLEASE PERFORM REPAIR IAW SRM 57-53-01-0I IDENT 1, SRM 57-53-01- 2R REPAIR 1, AND SRM 51-70-10-2R. RH I/B MAIN TRAILING EDGE FLAP REPLACED IAW AMM 27-51-02
- [SDR FDEA2019082191948](https://openairdocs.org/sdr/FDEA2019082191948.md): Panel · corroded · Aug 19, 2019 · N974FD · Boeing 7572Y0 · Engine Thrust Reverser
  > NR 2 ENG I/B C-DUCT UPPER BIFURICATION PANEL DAMAGE UPPER BIFURICATION UPPER TRACK BEAM SUPPORT PANEL EVALUATED AND FOUND TO BE CORROSION. CORROSION OUT OF LIMITS AS PER EM 78-31-28-300-085 REPLACED THE THRUST REVERSER ASSY IAW W/O:00074899 WRI:78305814 AND
- [SDR FDEA2019082191940](https://openairdocs.org/sdr/FDEA2019082191940.md): Skin · damaged · Aug 19, 2019 · N974FD · Boeing 7572Y0 · Fuselage Main, Plate/Skin
  > UPON EVALUATION OF AGING AIRCRAFT INSPECTION OF EXISTING DOUBLER AND TRIPLER REPAIR @ BSTA 620-624, STR21R - STR24R DAMAGED FASTENER HOLE FOUND ON INTERNAL SKIN WORK INSTRUCTIONS CARRIED OUT IAW FEDEX E.A.#F-5330-T0348760 TITLE: AD 2006-11-11 - FUSELAGE -
- [SDR FDEA2019082181930](https://openairdocs.org/sdr/FDEA2019082181930.md): Nozzle · cracked · Aug 18, 2019 · N974FD · Boeing 7572Y0 · Engine Collector/Tailpipe/Nozzle
  > NR 1 ENGINE CNA HAS CRACKS AT THE 3 O'CLOCK AND 9 O'CLOCK POSITIONS. CRACKS REMOVED IAW EM 78-11-04 AND CRACKS REPAIR IAW E.A. F-7810-T0348465.
- [SDR FDEA2019082181931](https://openairdocs.org/sdr/FDEA2019082181931.md): Panel · cracked · Aug 18, 2019 · N974FD · Boeing 7572Y0 · Leading Edge Devices
  > SLAT #6 IN/B T/E SKIRT (FLEX PANEL) IS CRACKED. REPAIRED CRACK IAW SRM 51-70-17 GENERAL & E.A. F-5750-T0348677
- [SDR FDEA2019081541877](https://openairdocs.org/sdr/FDEA2019081541877.md): Skin · dented · Aug 14, 2019 · N974FD · Boeing 7572Y0 · Fuselage Main, Plate/Skin
  > DENT OUTSIDE PERMITTED LIMITS IAW SRM 53-00-01 ALLOWABLE DAMAGE FIG101 DETAIL III @ B/S 580-597 STR 25L REAPIRED DENT IAW FEDEX EA# F-5300-T0348400 (P1) AND SRM 51-00-01 REPAIR 28 FIG 1
- [SDR FDEA2019081531854](https://openairdocs.org/sdr/FDEA2019081531854.md): Stringer Clip · cracked · Aug 13, 2019 · N974FD · Boeing 7572Y0 · Fuselage Main, Attach Fittings
  > STRINGER CLIP ' B/S 1500 STR2 WAS FOUND DAMAGED AND CRACKED. REPLACED STRINGER CLIP IAW SRM 51-40-02
- [SDR FDEA201908121843](https://openairdocs.org/sdr/FDEA201908121843.md): Seat Track · corroded · Aug 12, 2019 · N974FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK B/S 364 RBL 47-51 CORRODED BEYOND PERMITTED LIMITS. REPAIRED IAW FEDEX EA F-5310-T0348507(P1).
- [SDR FDEA201908071844](https://openairdocs.org/sdr/FDEA201908071844.md): Floor Support · none · Aug 7, 2019 · N974FD · Boeing 7572Y0 · Standard Practices/Structures
  > EXISTING REPAIR FOUND ON FLOOR SUPPORT STRUCTURE BS 570 APPROX. LBL 10. REPAIR REQUIRES EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA EVALUATION CARRIED OUT OF EXISTING REPAIR ON FLOOR SUPPORT STRUCTURE AT BS
- [SDR FDEA2019080211788](https://openairdocs.org/sdr/FDEA2019080211788.md): Strap · cracked · Aug 1, 2019 · N974FD · Boeing 7572Y0 · Fuselage Miscellaneous Structure
  > STRAP CRACKED FWD GALLEY FLOOR BS 367,LBL 24 FABRICATED NEW STRAP AND REPLACED OLD PART IAW EA F-5310-T034848 PART 1, SRM 53-00-5-2R, REPAIR 13, AND GMM. 7-0-1001.
- [SDR FDEA2019080211787](https://openairdocs.org/sdr/FDEA2019080211787.md): Floor Panel · delaminated · Aug 1, 2019 · N974FD · Boeing 7572Y0 · Fuselage Floor Panel
  > FLOOR PANEL DAMAGED @ DOORWAY #1R OUTSIDE PERMITTED LIMITS IAW SRM53-00-50-1A REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R
- [SDR FDEA2019080211786](https://openairdocs.org/sdr/FDEA2019080211786.md): Floor Panel · delaminated · Aug 1, 2019 · N974FD · Boeing 7572Y0 · Fuselage Floor Panel
  > FLOORBOARD @ 1L DOORWAY DAMAGED OUTSIDE PERMITTED LIMITS IAW SRM 53-00-50-1A. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R
- [SDR FDEA201907281732](https://openairdocs.org/sdr/FDEA201907281732.md): Seat Track · corroded · Jul 28, 2019 · N974FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK HAS EVIDENCE OF CORROSION @ B/S-344-356 AND 367-374. REMOVED SEAT TRACK SECTION IAW SRM 51-40-02. REMOVED CORROSION FROM SEAT TRACK SECTION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A FIG101 DETAIL 1. MATERIAL REMOVED 0.060" MAX ALLOWABLE 0
- [SDR FDEA201907081504](https://openairdocs.org/sdr/FDEA201907081504.md): Warning System · false activation · Jul 8, 2019 · N974FD · Boeing 7572Y0 · Trailing Flap Position Indicating System
  > PDIS 974 27-50 5786 08JUL19 TLV OPEN U LOGPAGES:3010096 TE FLAP ASYM INDICATED WHEN FLAPS SELECTED TO "1". FOLLOWED QRH PROCEDURES TO LANDING. TOUCHDOWN SPEED WAS APPROX 170 KIAS. FIM 27-51 TREE 805 PERFOMED NO FINDINGS, FLAPS SYS OPER TEST PERFOR
- [SDR FDEA201902030253](https://openairdocs.org/sdr/FDEA201902030253.md): Bulb · inoperative · Feb 3, 2019 · N974FD · Boeing 7572Y0 · Emergency Lighting
  > EMERGENCY SLIDE LIGHT L1 NO LIGHT FACT 03FEB19 11:23 CPH EMERGENCY SLIDE LIGHT L1 BULP REPLACED AMM 33-51-06-2-1 REV 123.4
- [SDR FDEA201707242026](https://openairdocs.org/sdr/FDEA201707242026.md): Skin · delaminated · Jul 24, 2017 · N974FD · Boeing 7572Y0 · Trailing Edge Flaps
  > COMPOSITE DISBOND TOP OF LEFT OUTBOARD AFT FLAP. REPAIRED AREA AT TOP OF LEFT OTBD AFT FLAP IAW SRM 57-53-01-2R, FIG 201, TABLE II, AND SRM 51-70-04, PAR 5.A.1. TAP TESTED AREA IAW 51-10-06 WITH NO DEFECTS NOTED. PRIMED AND TOPCOATED AREA IAW SRM 51-20-01 A
- [SDR FDEA201704181229](https://openairdocs.org/sdr/FDEA201704181229.md): Battery Pack · discharged · Apr 18, 2017 · N974FD · Boeing 7572Y0 · Emergency Lighting
  > FOUND ON PREDEPARTURE CHECK, 2 EA EMERGENCY EXIT SIGNS AND RT EXTERIOR LIGHT NOT TESTING. REMOVED AND REPLACED M730 POWER SUPPLY BATTERY PACK PER AMM 33-51-07-2, OPS CHECKS NORMAL.
- [SDR FDEA201704101135](https://openairdocs.org/sdr/FDEA201704101135.md): Pin · missing · Apr 10, 2017 · N974FD · Boeing 7572Y0 · Escape Slide
  > R1 DOOR SLIDE SAFTEY PIN MISSING. REPLACED MISSING SAFETY PIN AT R1 DOOR ESCAPE SLIDE POUCH IAW MM 52-11-02-4.
- [SDR FDEA201704101134](https://openairdocs.org/sdr/FDEA201704101134.md): Pin · missing · Apr 10, 2017 · N974FD · Boeing 7572Y0 · Emergency Equipment
  > L1 DOOR SLIDE SAFTEY PIN MISSING. REPLACED MISSING SAFETY PIN AT L1 DOOR ESCAPE SLIDE POUCH REF: 757 M.M. 52-11-02-4
- [SDR FDEA201608313087](https://openairdocs.org/sdr/FDEA201608313087.md): Skin · damaged · Aug 31, 2016 · N974FD · Boeing 7572Y0 · Rudder, Plate/Skin
  > RUDDER HAS HAIL DAMAGE. ACCOMPLISHED 3 EA REPAIRS ON RUDDER LT SIDE IAW SRM 55-40-01-2R, 51-70-04-0G AND EA F05540-T0328008, P1 TRACKING REPAIRS.
- [SDR FDEA201608303070](https://openairdocs.org/sdr/FDEA201608303070.md): Skin · dented · Aug 30, 2016 · N974FD · Boeing 7572Y0 · Cargo/Baggage Doors
  > DENTS IN MAIN CARGO DOOR SKIN. EVALUATED AND MEASURED DENTS, 224, MAIN CARGO DOOR SKIN, HFEC AND DVI INPSECTIONS CW, NO ADDITIONAL DEFECTS NOTED. DENTS, 195, FOUND TO BE WITHIN LIMITS IAW EA F-5230-TO327693 PT 1 AND DENTS, 43-55, 103-120, 29 TOTAL. REPAIRED
- [SDR FDEA201601210274](https://openairdocs.org/sdr/FDEA201601210274.md): Proximity Sensor · failed · Jan 21, 2016 · N974FD · Boeing 7572Y0 · Escape Slide
  > SLIDE LIGHT IN DOOR R1 FAILS TO ILLUMINATE WITH DOOR ARMED. R1 ESCAPE SLIDE ARMED INDICATOR LIGHTS INOPERATIVE. REMOVED AND REPLACED R1 DOOR AFT SLIDE PROXIMITY SENSOR IAW AMM 25-66-11-2. OPS CHECKED GOOD.
- [SDR FDEA201507252390](https://openairdocs.org/sdr/FDEA201507252390.md): Deck Plate · corroded · Jul 25, 2015 · N974FD · Boeing 7572Y0 · Fuselage Miscellaneous Structure
  > BS 415, LBL 54 DECK PLATE HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. FABRICATED DOUBLER REPAIR & INSTALLATION IAW SRM 757-200 RIGID CARGO BARRIER SECTION 5 4 3.
- [SDR FDEA201505311668](https://openairdocs.org/sdr/FDEA201505311668.md): Lanyard · out of position · May 31, 2015 · N974FD · Boeing 7572Y0 · Emergency Equipment
  > RIGHT SIDE ENTRY DOOR WOULD NOT ARM. FOUND GIRT BAR ARMING LANYARD WRAPPED AROUND GIRT BAR. R1 DOOR SLIDES INOPERATIVE OR MISSING. NO JUMP SEATERS OR ACM'S ARE TO OCCUPY COURIER AREA IN FLIGHT. INSPECTED THE SLIDE UPON ARRIVAL, SLIDE WAS REMOVED AT PREVIO
- [SDR FDEA201501150184](https://openairdocs.org/sdr/FDEA201501150184.md): Girt Bar · obstructed · Jan 15, 2015 · N974FD · Boeing 7572Y0 · Emergency Equipment
  > UPON LANDING, DOOR ARM LIGHT DOOR 1R WAS NOT ILLUMINATED. RELAMPED, NO HELP. FOUND SOME DEBRIS AT GIRT BAR AFT HOOK. REMOVED DEBRIS, LIGHT NOW OPERATES WHEN DOOR IS ARMED.
- [SDR FDEA201501060025](https://openairdocs.org/sdr/FDEA201501060025.md): Girt Bar · out of position · Jan 6, 2015 · N974FD · Boeing 7572Y0 · Emergency Equipment
  > ON BLOCK OUT R2 DOOR WOULD NOT ARM & ARM LIGHT WOULD NOT LIGHT. FOUND ESCAPE SLIDE GIRT BAR FELL OUT OF PLACE & WAS ABLE TO PLACE BACK IN PLACE. TESTED IAW MM 52-11-25-5 & NOW ARMS GOOD & IS GOOD FOR SERVICE.
- [SDR FDEA201408142176](https://openairdocs.org/sdr/FDEA201408142176.md): Lanyard · out of position · Aug 14, 2014 · N974FD · Boeing 7572Y0 · Emergency Equipment
  > RIGHT FWD ENTRY DOOR WILL NOT ARM DOOR SLIDES INOPERATIVE. NO JUMPSEATERS OR ACM'S ARE TO OCCUPY COURIER AREA IN FLIGHT. FOUND CORD OF SLIDE TANGLED IN BAR. NO TIME OR RII TO REMOVE & FIX. FOUND STATIC LANYARD LINE CLIP LAYING BETWEEN GIRT BAR CAM & FLOO
- [SDR FDEA201312102952](https://openairdocs.org/sdr/FDEA201312102952.md): Slide Raft · deployed · Dec 10, 2013 · N974FD · Boeing 7572Y0 · Escape Slide
  > L1 MAIN CABIN EXIT SLIDE DEPLOYED. RELEASED FOR SERVICE IAW MEL 52-11-01-A CATEGORY B EXPIRATION 10DEC13 MEL 52-11-01-A L1 DOOR SLIDE MISSING IDENTIFY INOPERATIVE OR MISSING. ADDED MPN D30654-122 CPN 2520951 QTY 1 SLIDE UPDT 07DEC13 19:01 GJT R AWAITING
- [SDR FDEA201308161926](https://openairdocs.org/sdr/FDEA201308161926.md): Lamp · burned out · Aug 16, 2013 · N974FD · Boeing 7572Y0 · Emergency Lighting
  > EMERGENCY LIGHTS R1 DOOR EXTERIOR SLIDE INOPERATIVE. REPLACED LAMPS, OPS NORMAL, IAW AMM 33-51-06-2-1. OK FOR SERVICE.
- [SDR FDEA201307221620](https://openairdocs.org/sdr/FDEA201307221620.md): Floorbeam · corroded · Jul 22, 2013 · N974FD · Boeing 7572Y0 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM BS 1640 RBL 24 CORRODED. R & R WITH FLOORBEAM FABRICATED IAW DWG 146N5136, SHT 1 REV - AND INSTALLED IAW DWG 146N5089, SHT 6, REV. MAJOR REPAIR.
- [SDR FDEA201307221613](https://openairdocs.org/sdr/FDEA201307221613.md): Tee Fitting · cracked · Jul 22, 2013 · N974FD · Boeing 7572Y0 · Fuselage Miscellaneous Structure
  > LOWER FUSELAGE BS 900 - 1037, LBL 60 WING TO BODY FAIRING SUPPORT TEE CRACKED AT AFT INBD CORNER. REPAIRED IAW EA F-5310-167523 PART 1.
- [SDR FDEA201307191587](https://openairdocs.org/sdr/FDEA201307191587.md): Panel · corroded · Jul 19, 2013 · N974FD · Boeing 7572Y0 · Trailing Edge Flaps
  > RIGHT WING INBD T/E MAIN FLAP UPPER PANEL FOUND CORRODED AT MAIN FLAP STA 92.5, FRONT SPAR UPPER AREA. REPAIRED IAW EA F-5750-167524, PART 1. REPAIR IS MAJOR.
- [SDR FDEA201307191586](https://openairdocs.org/sdr/FDEA201307191586.md): Panel · corroded · Jul 19, 2013 · N974FD · Boeing 7572Y0 · Trailing Edge Flaps
  > RT WING INBD T/E MAIN FLAP UPPER PANEL FOUND CORRODED AT MAIN FLAP STA 81.0 FRONT SPAR UPPER AREA. REPAIRED IAW EA F-5750-167524, PART 1. MAJOR REPAIR.
- [SDR FDEA201307071489](https://openairdocs.org/sdr/FDEA201307071489.md): Web · corroded · Jul 7, 2013 · N974FD · Boeing 7572Y0 · Service Doors
  > R4 DOOR INTERNAL DOOR HANDLE MECHANISM CUTOUT FWD INTERCOSTAL FWD SIDE FOUND CORRODED. REMOVED AND REPLACED, FABRICATED AND INSTALLED IAW DWG 146N6100 SHT.3, REV.H. REPAIR IS MAJOR.
- [SDR FDEA201307071487](https://openairdocs.org/sdr/FDEA201307071487.md): Web · corroded · Jul 7, 2013 · N974FD · Boeing 7572Y0 · Service Doors
  > R4 DOOR INTERNAL DOOR-MOUNTED WINDOW CUTOUT FWD WEB FWD SIDE HAD MINOR CORROSION. REMOVED AND REPLACED FABRICATED AND INSTALLED IAW DWG 146N6100 SHT.3, REV.H. REPAIR IS MAJOR.
- [SDR FDEA201307011434](https://openairdocs.org/sdr/FDEA201307011434.md): Crease Beam · corroded · Jul 1, 2013 · N974FD · Boeing 7572Y0 · Fuselage Main, Structure
  > BS 1000 -1010 RT CREASE BEAM INBD ANGLE FOUND CORRODED AROUND FASTENER HOLES. REPAIRED.
- [SDR FDEA201307011433](https://openairdocs.org/sdr/FDEA201307011433.md): Crease Beam · corroded · Jul 1, 2013 · N974FD · Boeing 7572Y0 · Fuselage Main, Structure
  > BS 960-980 RT CREASE BEAM INBD ANGLE FOUND CORRODED AROUND THREE FASTENERS HOLES. REPAIRED IAW REPAIR DWG LOR5L53017 SHT 3, REV A. REPAIR IS MAJOR.

Next page: https://openairdocs.org/aircraft/N974FD/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 = 'N974FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N974FD/reports

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