# Service difficulty reports: N524FE, cancelled Mar 2, 2024

A list on [N524FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N524FE-2024-03-02.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 4 · 157 reports

- [SDR FDEA201407231930](https://openairdocs.org/sdr/FDEA201407231930.md): Battery · faulty · Jul 23, 2014 · N524FE · Doug MD11F · Battery/Charger System
  > EMERGENCY POWER TEST FAIL & BATTERY VOLTS LOW. R & R MAIN ACFT BATTERIES IAW AMM 24-34-02-4-0.
- [SDR FDEA201406201502](https://openairdocs.org/sdr/FDEA201406201502.md): Handle · dirty · Jun 20, 2014 · N524FE · Doug MD11F · Landing Gear Selector
  > AFTER TAKEOFF LG RETRACTED NORMALLY BUT ALL 4 PRIMARY INDICATIONS & SYNOPTIC PAGE CONFIG REMAINED RED. CYCLED GEAR IAW QRH. DOWN GREEN & RETRACT RED. INSPECTED GEAR HANDLE & FOUND TO BE STICKING OUT WHEN PULLED & WOULD NOT SEAT ALL THE WAY BACK IN CAUSING U
- [SDR FDEA201406141449](https://openairdocs.org/sdr/FDEA201406141449.md): Skin · cracked · Jun 14, 2014 · N524FE · Doug MD11F · Wing, Plate/Skin
  > LT WING LE SKIN FOR ACCESS PANEL CUTOUT IS CRACKED. CONFIRMED CRACK BY HFEC INSPECTION IAW NDTSPM PT 6. CRACK TERMINATES AT FASTENER. REMOVED LT WING ACCESS PANEL & REMOVED ALL EVIDENCE OF CRACK SRM REPAIR 7 & VERIFIED ALL CRACK IS REMOVED BY HFEC INSPECTIO
- [SDR FDEA201406131423](https://openairdocs.org/sdr/FDEA201406131423.md): Slat Track · cracked · Jun 13, 2014 · N524FE · Doug MD11F · Leading Edge Devices
  > RT WING NR 14 SLAT TRACK CUT OUT AFT OTBD. CRACK IS LOCATED ON THE MATING FLANGE WHERE THE CLOSEOUT DOOR RESTS. VERIFIED CRACK USING HFEC IAW NDT SPM PART 6. CRACK TERMINATES AT FASTENER. CRACK IS APPROXIMATELY 1/2 INCHES. REPAIR INSTALLED IAW SRM.
- [SDR FDEA201406131422](https://openairdocs.org/sdr/FDEA201406131422.md): Skin · cracked · Jun 13, 2014 · N524FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING AFT OF NR 1 SLAT HFEC INSPECTED AND FOUND CRACKED. CUT OUT DAMAGE IAW SRM 57-40-01. COMPLIED WITH HFEC AROUND AREA IAW NDT SPM PART 6, NO CRACKS FOUND. FABRICATED REPAIR PARTS IAW EA 1-5710-T0308850 PT1. MAJOR REPAIR.
- [SDR FDEA201402180352](https://openairdocs.org/sdr/FDEA201402180352.md): Light · inoperative · Feb 18, 2014 · N524FE · Doug MD11F · Escape Slide
  > L1 DOOR SLIDE PUSH TO TEST LIGHT INOPERATIVE. R & R L1 SLIDE & CONTAINER ASSEMBLY IAW AMM 25-61-01-4.
- [SDR FDEA201401160115](https://openairdocs.org/sdr/FDEA201401160115.md): Connector · loose · Jan 16, 2014 · N524FE · Doug MD11F · Equipment/Furnishings Wiring
  > L1 DOOR EVACUATION SLIDE REMOTE PRESS TO TEST INDICATING SYS INOPERATIVE. FOUND CONNECTOR LOOSE, SECURED CONNECTOR IAW MM 25-61-04-5 PTT OK FOR SERVICE.
- [SDR FDEA201305251088](https://openairdocs.org/sdr/FDEA201305251088.md): Line · broken · May 25, 2013 · N524FE · Doug MD11F · Hydraulic System, Main
  > HYD 3 OFF ALERT AFTER GEAR DOWN & LOCKED, RECEIVED HYD 3 FAIL ALERT 58 DEG C MAX PUMP TEMP HYD QTY 2.0 AT BLOCK IN. LEAK APPEARES TO BE AT LT INBD AILERON AREA. FOUND LEAK AT LT INBD AILERON, NR 3 SYS PRESSURE LINE UNION-CHECK VALVE FOUND LOOSE(JUST SNUG) A
- [SDR FDEA201302140348](https://openairdocs.org/sdr/FDEA201302140348.md): Skin · misrepaired · Feb 14, 2013 · N524FE · Doug MD11F · Wing, Control Surfaces
  > LT WING INBD T/E FLAP INBD LOWER SEGMENT UPPER SURFACE AT FLAP STATION XIFH 219.55 MISREPAIRED. REPAIRED IAW EA 1-5750-163585. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201302140347](https://openairdocs.org/sdr/FDEA201302140347.md): Skin · misrepaired · Feb 14, 2013 · N524FE · Doug MD11F · Wing, Control Surfaces
  > RT WING INBD T/E FLAP INBD LOWER SEGMENT UPPER SURFACE AT FLAP STATION XIFH 225.140 MISREPAIRED. REPAIRED IAW EA 1-5750-163586. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201302140345](https://openairdocs.org/sdr/FDEA201302140345.md): Skin · misrepaired · Feb 14, 2013 · N524FE · Doug MD11F · Wing, Control Surfaces
  > RT WING INBD T/E FLAP INBD LOWER SEGMENT UPPER SURFACE AT FLAP STATION XIFH 147.300 MISREPAIRED. REPAIRED IAW EA 1-5750-163586. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201302140344](https://openairdocs.org/sdr/FDEA201302140344.md): Skin · misrepaired · Feb 14, 2013 · N524FE · Doug MD11F · Wing, Control Surfaces
  > RT WING INBD T/E FLAP INBD LOWER SEGMENT UPPER SURFACE AT FLAP STATION XIFH 165.300 MISREPAIRED. REPAIRED IAW EA 1-5750-163586. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201302120325](https://openairdocs.org/sdr/FDEA201302120325.md): Skin · misrepaired · Feb 12, 2013 · N524FE · Doug MD11F · Trailing Edge Flaps
  > RT WING INBD T/E FLAP INBD LOWER SEGMENT UPPER SURFACE MISREPAIRED. REPAIRED IAW EA 1-5750-163586. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.
- [SDR FDEA201302080303](https://openairdocs.org/sdr/FDEA201302080303.md): Skin · misrepaired · Feb 8, 2013 · N524FE · Doug MD11F · Trailing Edge Flaps
  > LT INBD T/E FLAP INBD LOWER SEGMENT UPPER SURFACE FOUND MISREPAIRED. REPAIRED IAW EA 1-5750-163585. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201302080302](https://openairdocs.org/sdr/FDEA201302080302.md): Panel · cracked · Feb 8, 2013 · N524FE · Doug MD11F · Vertical Stabilizer, Plate/Skin
  > LOWER VERTICAL STABILIZER, NR 2 ENGINE INTAKE DUCT, REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. REPAIRED IAW SRM 55-30-02 REPAIR 2 FIGURE 201 REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201302080301](https://openairdocs.org/sdr/FDEA201302080301.md): Web · cracked · Feb 8, 2013 · N524FE · Doug MD11F · Fuselage Miscellaneous Structure
  > AFT FUSELAGE BS 2015, X= -15 UPPER STABILIZER CUT-OUT PANEL LINE WEB FOUND CRACKED.
- [SDR FDEA201302080300](https://openairdocs.org/sdr/FDEA201302080300.md): Skin · misrepaired · Feb 8, 2013 · N524FE · Doug MD11F · Wing, Control Surfaces
  > RT WING INBD FLAP UPPER SKIN AT XIFH 140 MISREPAIRED. REPAIRED IAW SRM 57-00-01 FIGURE 201 REPAIR 2 REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201302050270](https://openairdocs.org/sdr/FDEA201302050270.md): Vane · chafed · Feb 5, 2013 · N524FE · Doug MD11F · Trailing Edge Flaps
  > RT WING OTBD T/E FLAP VANE, OTBD LOWER EDGE FOUND CHAFED. REPAIRED AS PER EA 1-5750-165191. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.
- [SDR FDEA201302050268](https://openairdocs.org/sdr/FDEA201302050268.md): Skin · misrepaired · Feb 5, 2013 · N524FE · Doug MD11F · Fuselage Main, Plate/Skin
  > FUSELAGE LOWER SKIN BS 1021, LONGERON 40 RT MISREPAIRED. REPAIRED PER SRM 53-00-01 FIGURE 201 REPAIR 1 REVISION 51. FUSELAGE LOWER SKIN STATION 1021 LONGERON 40 RIGHT CARRIED OUT REPAIR PER SRM 53-00-01 FIGURE 201, CLASS 1, REPAIR 1 & REVISION 51. EO 1-5100
- [SDR FDEA201302050267](https://openairdocs.org/sdr/FDEA201302050267.md): Skin · cracked · Feb 5, 2013 · N524FE · Doug MD11F · Leading Edge Devices
  > LEFT WING DROOP L/E SLAT UPPER SKIN FOUND CRACKED. REPAIRED IAW EA 1-5740-165189. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.
- [SDR FDEA201302020259](https://openairdocs.org/sdr/FDEA201302020259.md): Fillet · eroded · Feb 2, 2013 · N524FE · Doug MD11F · Leading Edge Devices
  > RT WING NR 1 SLAT PERFORMANCE FILLET EXTERIOR COMPOSITE ERODED. REPAIRED IAW EA 1-5740-163000. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.
- [SDR FDEA201302020258](https://openairdocs.org/sdr/FDEA201302020258.md): Fillet · eroded · Feb 2, 2013 · N524FE · Doug MD11F · Leading Edge Devices
  > LT WING NR 1 SLAT PERFORMANCE FILLET EXTERIOR COMPOSITE ERODED. REPAIRED IAW EA 1-5740-162999. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.
- [SDR FDEA201302020257](https://openairdocs.org/sdr/FDEA201302020257.md): Access Panel · cracked · Feb 2, 2013 · N524FE · Doug MD11F · Wing, Plate/Skin
  > 12 EA FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STA=700. REPAIRED AS PER SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 51. INITIAL REPEAT
- [SDR FDEA201302020256](https://openairdocs.org/sdr/FDEA201302020256.md): Access Panel · cracked · Feb 2, 2013 · N524FE · Doug MD11F · Wing, Plate/Skin
  > 11 EA FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS =690 AND STA=700. REPAIRED AS PER SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 51. INITIAL REPEAT INSP
- [SDR FDEA201301310232](https://openairdocs.org/sdr/FDEA201301310232.md): Frame · misrepaired · Jan 31, 2013 · N524FE · Doug MD11F · Fuselage Main, Frame
  > FRAME MISREPAIRED BS 535, LONGERON 24L. REPAIRED IAW SRM 53-20-07 FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.
- [SDR FDEA201301310231](https://openairdocs.org/sdr/FDEA201301310231.md): Frame · misrepaired · Jan 31, 2013 · N524FE · Doug MD11F · Fuselage Main, Frame
  > FRAME MISREPAIRED BS 535, LONGERON 18L, REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.
- [SDR FDEA201301290215](https://openairdocs.org/sdr/FDEA201301290215.md): Longeron Splice · cracked · Jan 29, 2013 · N524FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LOWER CENTER CARGO LONGERON SPLICE BETWEEN STATION 5-113 AND 1541, LONGERON 37 LT FOUND CRACKED. REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01 REVISION 51. SPLICE FABRICATED AS PER DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR
- [SDR FDEA201301290212](https://openairdocs.org/sdr/FDEA201301290212.md): Longeron Splice · cracked · Jan 29, 2013 · N524FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LOWER CENTER CARGO LONGERON SPLICE BETWEEN STATION 5-113 AND 1541, LONGERON 34 LT FOUND CRACKED. REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01 REVISION 51. SPLICE FABRICATED AS PER DWG A5A7112 REVISION D. REPAIR CLASSIFIED AS MAJOR PER GM
- [SDR FDEA201301290210](https://openairdocs.org/sdr/FDEA201301290210.md): Longeron Splice · cracked · Jan 29, 2013 · N524FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LOWER CENTER CARGO LONGERON SPLICE BETWEEN STATION 5-113 AND 1541, LONGERON 51 RT FOUND CRACKED. REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01 REVISION 51. SPLICE FABRICATED AS PER DOUGLAS DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED A
- [SDR FDEA201301290213](https://openairdocs.org/sdr/FDEA201301290213.md): Longeron Splice · cracked · Jan 29, 2013 · N524FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LOWER CENTER CARGO LONGERON SPLICE BETWEEN STATION 5-113 AND 1541, LONGERON 43 LT FOUND CRACKED. R & R WITH FABRICATED SPLICE IAW SRM 51-33-01, REV 51. SPLICE FABRICATED IAW DWG A5A7116, REV D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201301290211](https://openairdocs.org/sdr/FDEA201301290211.md): Longeron Splice · cracked · Jan 29, 2013 · N524FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LOWER CENTER CARGO LONGERON SPLICE BETWEEN STA 5-113 AND 1541, LONGERON 43 RT FOUND CRACKED. R & R WITH FABRICATED SPLICE IAW SRM 51-33-01, REV 51. SPLICE FABRICATED IAW DWG A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201301290209](https://openairdocs.org/sdr/FDEA201301290209.md): Longeron Splice · cracked · Jan 29, 2013 · N524FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LOWER CENTER CARGO LONGERON SPLICE BETWEEN STATION 5-113 AND 1541, LONGERON 52 FOUND CRACKED. R & R WITH FABRICATED SPLICE IAW SRM 51-33-01, REV 51. SPLICE FABRICATED IAW DWG A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201301280206](https://openairdocs.org/sdr/FDEA201301280206.md): Door Frame · cracked · Jan 28, 2013 · N524FE · Doug MD11F · Fuselage Main, Structure
  > LOWER CENTER CARGO DOOR UPPER FRAME AT DOOR ACTUATOR ARM AREA FOUND CRACKED. REPAIRED IAW EA 1-5310-163577 TITLE: FUSELAGE - MAINFRAME- CENTER CARGO DOOR UPPER JAMB BEAM - CRACK REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201301280205](https://openairdocs.org/sdr/FDEA201301280205.md): Trunnion · cracked · Jan 28, 2013 · N524FE · Doug MD11F · Fuselage, Landing Gear Attach Fittings
  > NOSE LANDING GEAR LT TRUNNION ATTACHMENT FITTING FOUND CRACKED. REPAIRED IAW SRM 53-10-14, FIG 202, REPAIR 2, REV 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.
- [SDR FDEA201301280204](https://openairdocs.org/sdr/FDEA201301280204.md): Skin · cracked · Jan 28, 2013 · N524FE · Doug MD11F · Leading Edge Devices
  > LEFT WING NR 8 SLAT INNER SKIN FOUND CRACKED BETWEEN NR 17 AND NR 18 SLAT TRACK AREA. REPAIRED IAW SRM 57-40-01 FIGURE 201 REPAIR 3 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.
- [SDR FDEA201301280203](https://openairdocs.org/sdr/FDEA201301280203.md): Cargo Track · damaged · Jan 28, 2013 · N524FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO TRACK AT BS 1125, "X" = 27.5 FOUND DAMAGED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.
- [SDR FDEA201301280202](https://openairdocs.org/sdr/FDEA201301280202.md): Seat Track · damaged · Jan 28, 2013 · N524FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO TRACK AT BS 1125, "X" = -8.5 FOUND DAMAGED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.
- [SDR FDEA201111134889](https://openairdocs.org/sdr/FDEA201111134889.md): Light · inoperative · Nov 13, 2011 · N524FE · Doug MD11F · Emergency Equipment
  > R1 DOOR DISARM LIGHT INOPERATIVE. REMOVED & REPLACED DOOR 1 R DOOR DISARMED LIGHT ASSY (L2-1117) IAW WDM 52-11-01. OP'S CHECKED NORMAL.
- [SDR FDEA201102220692](https://openairdocs.org/sdr/FDEA201102220692.md): Rib · cracked · Feb 22, 2011 · N524FE · Doug MD11F · Wing, Rib/Bulkhead
  > LT WING - CRUISE PERFORMANCE FILLET, ADJACENT TO T/E, OTBD RIB FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 57-40-71 FIG 201 REPAIR 1 REVISION 45. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.
- [SDR FDEA201102220691](https://openairdocs.org/sdr/FDEA201102220691.md): Rib · cracked · Feb 22, 2011 · N524FE · Doug MD11F · Leading Edge Devices
  > LT WING NR 1 SLAT, ADJACENT TO T/E, INBD RIB FOUND CRACKED. CRACKED RIB REMOVED AND REPLACED WITH A NEW RIB AS PER SRM 51-31-01 REVISION 45. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.
- [SDR FDEA201102200637](https://openairdocs.org/sdr/FDEA201102200637.md): Seat Track · corroded · Feb 20, 2011 · N524FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CABIN, LT STA 1359, "X" = 8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1331 TO STA 1371 X=8.5 AS PER SRM 53-00-52 FIG 201 REPAIR I REVISION 45. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.
- [SDR FDEA201102200638](https://openairdocs.org/sdr/FDEA201102200638.md): Beam · cracked · Feb 20, 2011 · N524FE · Doug MD11F · Fuselage Main, Structure
  > MAIN DECK CABIN, RT 3 DOOR NR 2 BEAM FWD STOP SUPPORT FOUND CRACKED. BEAM REMOVED AS PER SRM 51-31-01 REVISION 45. NEW BEAM FABRICATED AND INSTALLED AS PER EA 1-5210-143528. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.
- [SDR FDEA201102200636](https://openairdocs.org/sdr/FDEA201102200636.md): Vane · delaminated · Feb 20, 2011 · N524FE · Doug MD11F · Trailing Edge Flaps
  > RT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 69.0. ADJUSTMENT AND OPERATION TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 69.0.
- [SDR FDEA200905311860](https://openairdocs.org/sdr/FDEA200905311860.md): Seat Track · corroded · May 31, 2009 · N524FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO AT STA 5-70 TO STA 5-120 X= -8.5 SEAT TRACK FOUND CORRODED ON SEVERAL LOCATIONS. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-70-00 FIGURE 1 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 107.
- [SDR FDEA200905271802](https://openairdocs.org/sdr/FDEA200905271802.md): Rib · cracked · May 27, 2009 · N524FE · Doug MD11F · Wing, Rib/Bulkhead
  > RIGHT HAND WING LEADING EDGE LOWER ACCESS AT STATION XOS 1003 INBOARD RIB FOUND CRACKED. REMOVED IAW SRM 51-31-01. VOLUME II REVISION 40 AND REPLACED WITH A NEW RIB IAW SRM 51-33-01 VOLUME II REVISION 40. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 10
- [SDR 08FDEA03566](https://openairdocs.org/sdr/08FDEA03566.md): Cable · failed · Aug 23, 2008 · N524FE · Doug MD11F · Landing Gear Retraction/Extension System
  > ON TAKEOFF RT MAIN GEAR INDICATED UNSAFE AFTER RAISING HANDLE. ALSO, CONFIRMED ON SD. QRH HAD US CYCLE. SAME INDICATION, ON GEAR DOWN, ALL INDICATED SAFE. INSTALLED NEW TARGET RT MLG GEAR WELL DOOR 32-61-15-4. ADJ CLEARANCE BET PROX SENSOR AND THE TARGET
- [SDR 07FDEA05073](https://openairdocs.org/sdr/07FDEA05073.md): Channel · cracked · Dec 17, 2007 · N524FE · Doug MD11F · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT: STA 979 TO STA 1019 X = -35 CHANNEL FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5340-117084, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR 07FDEA05072](https://openairdocs.org/sdr/07FDEA05072.md): Channel · chafed · Dec 17, 2007 · N524FE · Doug MD11F · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT: STA 859 TO STA 899 X = -35 CHANNEL FOUND CHAFED. COMPLIED WITH FEDEX E.A. 1-5340-117085, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR 07FDEA05071](https://openairdocs.org/sdr/07FDEA05071.md): Channel · damaged · Dec 17, 2007 · N524FE · Doug MD11F · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT: STA 899 TO STA 919 X = -40 CHANNEL DOLLY ASSEMBLY RETRACTOR MOUNTING HOLE FOUND ELONGATED. COMPLIED WITH FEDEX E.A. 1-5340-117082, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR 07FDEA05070](https://openairdocs.org/sdr/07FDEA05070.md): Channel · damaged · Dec 17, 2007 · N524FE · Doug MD11F · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT: STA 615 X = -40 CHANNEL DOLLY ASSEMBLY END STOP MOUNTING ANCHOR NUT MOUNTING AREA FOUND DAMAGED. COMPLIED WITH FEDEX E.A.1-5340-117080. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Next page: https://openairdocs.org/deregistered/N524FE-2024-03-02/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 = 'N524FE' AND deregistration_id = 'N524FE-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N524FE-2024-03-02/reports

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