# Service difficulty reports: N566FE, cancelled Jan 29, 2024

A list on [N566FE, cancelled Jan 29, 2024](https://openairdocs.org/deregistered/N566FE-2024-01-29.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 · 90 reports

- [SDR FDEA2018102653006](https://openairdocs.org/sdr/FDEA2018102653006.md): Engine · fire · Oct 25, 2018 · N566FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > MDIS 566 78-10 5297 24OCT18 MEM OPEN U ENG 2 TAIL PIPE FIRE DURING START. INSTRUCTED FLT CREW TO USE ENG FIRE PROCEDURES. BOTH BOTTLES DISCHARGED. PER FLT CREW DEBRIEF NO FIRE IND IN COCKPIT, NO EGT LIMIT EXCEDED FIRE DEPT CALLED. FIRE DEPT DISCHARGED FOAM INT
- [SDR FDEA201803290801](https://openairdocs.org/sdr/FDEA201803290801.md): Web · cracked · Mar 29, 2018 · N566FE · Doug MD1010F · Wing Miscellaneous Structure
  > NR 1 FUEL TANK WEB AFT BOOST PUMP OPENING HAS A CRACK BY THE OPENING. REPAIRED IAW EA 8-5710-T0339351, REV A, P1 AND SRM 57-10-00, FIG. 52.
- [SDR FDEA201803280800](https://openairdocs.org/sdr/FDEA201803280800.md): Web · cracked · Mar 28, 2018 · N566FE · Doug MD1010F · Wing Miscellaneous Structure
  > LEFT WING NR 1 FUEL TANK, INBD FUEL TRANSFER PUMP WEB CRACKED ON INBD SIDE OF OPENING.
- [SDR FDEA201803270792](https://openairdocs.org/sdr/FDEA201803270792.md): Pulley Bracket · gouged · Mar 27, 2018 · N566FE · Doug MD1010F · Leading Edge Devices
  > LEFT WING SLAT CABLE RUBBING INTO PULLEY BRACKET JUST OUTBOARD OF THE DRIVE ASSEMBLY BEHIND THE NR 3 & 4 SLAT SPLIT. OCCURRED DUE TO THE CABLE NOT RIDING INSIDE OF PULLEY TRACK. THE PULLEY GUIDE PIN WAS FOUND DANGLING UNSECURE AT THE BRACKET. REPLACED NEW A
- [SDR FDEA201706081595](https://openairdocs.org/sdr/FDEA201706081595.md): Uplock Sensor · out of adjust · Jun 8, 2017 · N566FE · Doug MD1010F · Landing Gear Position and Warning
  > DURING INTIAL ACCELERATION AND CLIMB AFTER TAKEOFF, RECEIVED INTERMITTENT LEFT MAIN GEAR UNLOCKED INDICATIONS, RED LIGHT BY GEAR HANDLE AND EAD CONFIGURATION PAGE. BEGAN AT 300 KIAS AND WOULD COME ON FOR APPROXIMATELY 2 SECONDS THEN OUT. SLOW TO 260/M. 70 A
- [SDR FDEA201701210235](https://openairdocs.org/sdr/FDEA201701210235.md): Indicator · failed · Jan 21, 2017 · N566FE · Doug MD1010F · Escape Slide
  > R1 DOOR SLIDE WILL NOT TEST. REMOVED AND REPLACED SLIDE PRESSURE INDICATOR ASSEMBLY IAW 25-63-03-2 AND PERFORMED OPS CHECKED IAW 25-61-03-5. OPS CHECK IS NORMAL.
- [SDR FDEA201701080079](https://openairdocs.org/sdr/FDEA201701080079.md): Solenoid · malfunctioned · Jan 8, 2017 · N566FE · Doug MD1010F · Passenger/Crew Doors
  > L1 DOOR INTERIOR ELECTRIC SWITCH IS INTERMITTANT. REPLACED L1 DOOR SOLENOID S2-730 PER AMM 52-11-13. PERFORMED NUMEROUS NORMAL OPERARATIONS WITH NO DISCREPANCIES. OK FOR SERVICE.
- [SDR FDEA201612034318](https://openairdocs.org/sdr/FDEA201612034318.md): Support Frame · cracked · Dec 3, 2016 · N566FE · Doug MD1010F · Nacelle/Pylon, Main Frame
  > NR 3 ENGINE PYLON, SUPPORT FRAME IS CRACKED. REPAIRED IAW EA 8-5410-T0330096 AND SRM 54-00-01 FIG 12 VOL 1.
- [SDR FDEA201611304297](https://openairdocs.org/sdr/FDEA201611304297.md): Shear Tie · corroded · Nov 30, 2016 · N566FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > AFT CARGO SHEAR TIE CORRODED STA 1781 RBL, REMOVED AND REPLACED SKIN ATTACH LEG IN REF TO SRM 53-30-00 FIG 9 PAGE 34 VOL1.
- [SDR FDEA201611284260](https://openairdocs.org/sdr/FDEA201611284260.md): Bolt · sheared · Nov 28, 2016 · N566FE · Doug MD1010F · Ailerons
  > RIGHT INBD AILERON, CENTER ATTACH FITTING BOLT HEAD SHEARED. REMOVED AND REPLACED CENTER ATTACH FITTING BOLT AS REQUIRED IAW AMM 57-44-01-2 AND AILERON OPS CHECKED GOOD IAW AMM 27-10-00-5.
- [SDR FDEA201611224185](https://openairdocs.org/sdr/FDEA201611224185.md): Floor Support · damaged · Nov 22, 2016 · N566FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > CENTER CARGO COMPARTMENT RT OF CENTER ROLLER TRAY FWD END FLOOR BOARD MOUNT HOLES ARE DOUBLE DRILLED CUT OUT DAMAGE SECTION OF FLOOR CHANNEL AND REPAIR IAW SRM 53-70-00 VOL 1, FIG 7, SHEET 3
- [SDR FDEA201611214142](https://openairdocs.org/sdr/FDEA201611214142.md): Attach Fitting · cracked · Nov 21, 2016 · N566FE · Doug MD1010F · Wing, Attach Fittings
  > LT WING ATTACH TEE FRONT SPAR TO FRAME HAS 2 IN CRACK IN RADIUS STA 1159 X=118 REF SRM 57-20-00 FIG 5. VERIFIED WITH NDT AND MARKED END OF CRACK. REPAIRED ATTACH TEE FRONT SPAR TO FRAME REF SRM 57-20-00 FIG 5 PAGE 19 VOL.1.
- [SDR FDEA201611214141](https://openairdocs.org/sdr/FDEA201611214141.md): Attach Fitting · cracked · Nov 21, 2016 · N566FE · Doug MD1010F · Wing, Attach Fittings
  > LT WING ATTACH TEE FRONT SPAR TO FRAME HAS 2 IN CRACK IN RADIUS STA 1159 X=118. REF SRM 57-20-00 FIG 5. VERIFIED WITH NDT AND MARKED END OF CRACK. REPAIRED TEE FRONT SPA TO FRAME REF SRM 57-20-00 FIG 5 PAGE 19 VOL 1.
- [SDR FDEA201611164042](https://openairdocs.org/sdr/FDEA201611164042.md): Skin · dented · Nov 16, 2016 · N566FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT WING TE FLAP LOWER SKIN AT APPROX XIFH 253 HAD TWO DENTS. REPAIRED IAW SRM 57-10-00 FIG 85, SHT 1, VOL 1.
- [SDR FDEA201611164041](https://openairdocs.org/sdr/FDEA201611164041.md): Skin · dented · Nov 16, 2016 · N566FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT INBD FLAP LOWER SURFACE DENTED. REPAIRED IAW SRM 57-10-00. FIG 85, SHT 1, VOL 1
- [SDR FDEA201611164037](https://openairdocs.org/sdr/FDEA201611164037.md): Skin · cracked · Nov 16, 2016 · N566FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT OTBD FLAP UPPER INBD SKIN IS CRACKED. REPAIRED IAW SRM 57-00-01, FIG 4, SHT 2, VOL 1.
- [SDR FDEA201611164036](https://openairdocs.org/sdr/FDEA201611164036.md): Skin · cracked · Nov 16, 2016 · N566FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT OTBD FLAP UPPER L/E SKIN CRACKED. REPAIRED IAW SRM 57-00-01, FIG 4, SHT 2, VOL 1.
- [SDR FDEA201611164035](https://openairdocs.org/sdr/FDEA201611164035.md): Skin · cracked · Nov 16, 2016 · N566FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT OTBD FLAP UPPER T/E SKIN FOUND CRACKED. REPAIRED IAW SRM 57-00-01 FIG 4 SHT 2 VOL 1.
- [SDR FDEA201611164033](https://openairdocs.org/sdr/FDEA201611164033.md): Skin · damaged · Nov 16, 2016 · N566FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > LOWER FWD CARGO DOOR CUT OUT IS DAMAGED AT THE LOWER AFT CORNER. REPAIRED IAW SRM 53-50-00 FIG.26 SHEET 3 VOL1.
- [SDR FDEA201611154025](https://openairdocs.org/sdr/FDEA201611154025.md): Shear Tie · cracked · Nov 15, 2016 · N566FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > MAIN CABIN SHEAR TIE HAS A CRACK AT BS 1661 JUST BELOW STRINGER 18L. REMOVED AND REPLACED THE DAMAGED SECTION OF THE SHEAR TIE IAW SRM 53-30-00 FIG. 10 AND DWG AFA0005.
- [SDR FDEA201611134009](https://openairdocs.org/sdr/FDEA201611134009.md): Skin · cracked · Nov 13, 2016 · N566FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING FIXED LEADING EDGE UPPER INTERIOR SKIN CRACKED. REPAIRED IAW SRM 57-10-00 FIG 71 PAGE 222 VOL1.
- [SDR FDEA201611134008](https://openairdocs.org/sdr/FDEA201611134008.md): Skin · cracked · Nov 13, 2016 · N566FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING FIXED LEADING EDGE INT UPPER SKIN CRACKED. SEVERAL CRACKS BEYOND PREVIOUS STOP DRILLS. REPAIRED IAW SRM 57-10-00 FIG.71 PAGE 222 VOL 1.
- [SDR FDEA201611113978](https://openairdocs.org/sdr/FDEA201611113978.md): Structure · cracked · Nov 11, 2016 · N566FE · Doug MD1010F · Passenger/Crew Doors
  > L1 DOOR UPPER AFT CORNER HAS DAMAGE. REPAIRED THE L1 DOOR IAW SRM 52-10-00 FIG 12A VOL 1.
- [SDR FDEA201611103946](https://openairdocs.org/sdr/FDEA201611103946.md): Skin · corroded · Nov 10, 2016 · N566FE · Doug MD1010F · Wing, Plate/Skin
  > RT WING UPPER SKIN AT STRINGER 13, XORS 264, SHOWS CORROSION. REMOVED CORROSION IAW EA 8-5730-T0329998.
- [SDR FDEA201611103943](https://openairdocs.org/sdr/FDEA201611103943.md): Skin · corroded · Nov 10, 2016 · N566FE · Doug MD1010F · Wing, Plate/Skin
  > RT WING UPPER SURFACE, AT STRINGER 16, XORS 264, 2 FASTENERS SHOW CORROSION. CORROSION REMOVED IAW EA 8-5730-T032-9998.
- [SDR FDEA201611103942](https://openairdocs.org/sdr/FDEA201611103942.md): Skin · corroded · Nov 10, 2016 · N566FE · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING UPPER SURFACE, STRINGER 17, XORS 264, PREVIOUS REPAIR HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 57-10-00 FIG 59 VOL 1.
- [SDR FDEA201611093941](https://openairdocs.org/sdr/FDEA201611093941.md): Skin · corroded · Nov 9, 2016 · N566FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE AT BS 1119, RBL 52 SHOWS EVIDENCE OF CORROSION. CUT OUT CORROSION AND REPAIRED IAW SRM 53-20-00 FIG. 6 SHEET 9 PAGE 78 VOL. 1.
- [SDR FDEA201611053851](https://openairdocs.org/sdr/FDEA201611053851.md): Skin · delaminated · Nov 5, 2016 · N566FE · Doug MD1010F · Spoilers
  > LEFT NR 5 SPOILER UPPERR SKIN IS DELAMINATED. REPAIRED IAW SRM 51- 21-02 VOL.II.
- [SDR FDEA201611053836](https://openairdocs.org/sdr/FDEA201611053836.md): Seat Track · worn · Nov 5, 2016 · N566FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK NEAR BS 1460 LBL 27.50 SHOWS WEAR. REMOVED AND REPLACED THE SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1, AND SRM 53-42-01 FIG 4, PAGE 11 VOL 3.
- [SDR FDEA201611043825](https://openairdocs.org/sdr/FDEA201611043825.md): Skin · delaminated · Nov 4, 2016 · N566FE · Doug MD1010F · Spoilers
  > LEFT NR 3 SPOILER UPPER SKIN WAS DELAMINATED. REPAIRED THE SKIN SRM 57-00-01 VOL.I, FIG.4, PG.11.
- [SDR FDEA201611023797](https://openairdocs.org/sdr/FDEA201611023797.md): Tee Fitting · cracked · Nov 2, 2016 · N566FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > FWD CARGO, BS 595, LONGERON 39L FOUND CRACKED. REMOVED AND REPLACED SECTION OF TEE FITTING BETWEEN LONGERONS 36 AND 40L IAW DWG SR10530064 AND EA 8-5310-T0329315.
- [SDR FDEA201611013783](https://openairdocs.org/sdr/FDEA201611013783.md): Tee Fitting · cracked · Nov 1, 2016 · N566FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > FWD CARGO RT BS 595 TEE LONGERON 39R FOUND CRACKED. REMOVED AND REPLACED THE TEE IAW DWG SR10530064 AND EA 8-5310-T0329368.
- [SDR FDEA201611013782](https://openairdocs.org/sdr/FDEA201611013782.md): Seat Track · corroded · Nov 1, 2016 · N566FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > [MAIN DECK SEAT TRACK BS 1388 RBL 47.50 WORN. REMOVE AND REPLACED THE SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1.
- [SDR FDEA201610123547](https://openairdocs.org/sdr/FDEA201610123547.md): Actuator · failed · Oct 12, 2016 · N566FE · Doug MD1010F · Passenger/Crew Doors
  > L1 DOOR WILL NOT OPEN ELECTRICALLY. REMOVED AND REPLACED L1 PASSENGER DOOR ELECTRIC ACTUATOR. OPS CHECKED GOOD IAW AMM 52-11-01-2.
- [SDR FDEA201609033121](https://openairdocs.org/sdr/FDEA201609033121.md): Skin · cracked · Sep 3, 2016 · N566FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > FOUND SMALL CRACK AT THE UPPER LT CORNER IN THE FUSELAGE JUST ABOVE THE NR 3 PACK BAY DOOR. INSTALLED REPAIR IN REF TO EA 8-5330-T0328078.
- [SDR FDEA201606152002](https://openairdocs.org/sdr/FDEA201606152002.md): Unknown · odor · Jun 15, 2016 · N566FE · Doug MD1010F · Air Distribution System
  > FUME EVENT ON DESCENT PASSING FLIGHT LEVEL 200 WITH ALL PACKS AND BLEEDS ON. ODOR OF MUSTY DIRTY SOCKS. RAN APU. OPERATED PACKS 1, 2, 3 SEPARATELY, THEN OPERATED PACKS TOGETHER ON HOT AND COLD SETTING. TT OF RUNNING PACKS WAS 1 HR. OPEN ALL PACKS BAYS TRY
- [SDR FDEA201511053490](https://openairdocs.org/sdr/FDEA201511053490.md): Coalescer Bag · dirty · Nov 5, 2015 · N566FE · Doug MD1010F · Humidity Control System
  > FUMES WHILE DIVERTING, INSPECTION ACCOMPLISHED ON ARRIVAL, CHEM-SPILL ISOLATED TO AAD CONTAINER AT POSITION 2L. NO SEEPAGE TO ACFT NOTED. CONTAINER QUARANTINED FOR EVALUATION. PERFORMED LIQUID CHEM & SPILLAGE MX PRACTICE. R & R ALL THREE PACK COALESCE BAGS
- [SDR FDEA201502190552](https://openairdocs.org/sdr/FDEA201502190552.md): Fire Warning · activated · Feb 19, 2015 · N566FE · Doug MD1010F · Fire Detection
  > DURING PREFLIGHT, RECEIVED A FWD CARGO FIRE ALERT & DISCHARGED BOTTLE. R & R NR 1 CARGO FIRE BOTTLE.
- [SDR FDEA201411123664](https://openairdocs.org/sdr/FDEA201411123664.md): Bracket · cracked · Nov 12, 2014 · N566FE · Doug MD1010F · Wing, Attach Fittings
  > LT WING TE BRACKET FOR FLIGHT CONTROL PULLEYS AFT OF PYLON IS CRACKED. REMOVED BRACKET & INSTALLED NEW BRACKET IAW SRM 51-31-01, PN ARB0107-5, MAJOR REPAIR.
- [SDR FDEA201411113644](https://openairdocs.org/sdr/FDEA201411113644.md): Skin · gouged · Nov 11, 2014 · N566FE · Doug MD1010F · Ailerons
  > LEFT INBD AILERON LOWER SKIN LE GOUGED. REMOVED OLD LE SKIN PANEL, RECEIVED NEW FABRICATED SKIN PANEL T14 1100803, LOCATED, DRILLED, INSTALLED & TREATED, PRIMED & TOP COATED IAW SRM 51-31-01 & 51-21-01. COMPLIED WITH EA 8-5750-TO313143 REV NO POS P1 WINGS FL
- [SDR FDEA201411083593](https://openairdocs.org/sdr/FDEA201411083593.md): Floorbeam · corroded · Nov 8, 2014 · N566FE · Doug MD1010F · Fuselage Main, Floor Beam
  > AFT CARGO FLOORBEAM UPPER CHORD AT STATION 1902 STRINGER 43R HAS HEAVY CORROSION ON LOWER SURFACE. REMOVED DAMAGE, ORIGINAL MATERIAL.063, MATERIAL REMOVED.050 & REMAINING MATERIAL.013 IAW SRM 53-00-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 1B. I
- [SDR FDEA201411083592](https://openairdocs.org/sdr/FDEA201411083592.md): Panel · cracked · Nov 8, 2014 · N566FE · Doug MD1010F · Nacelle/Pylon, Plate/Skin
  > RIGHT PYLON PANEL 457BT CRACKED AS MARKED. PANEL RACK WELDED ON T14 1102142 IAW EA 8-5480-T0312625 REV NO PS P 1. NACELLES & PYLON FILLETS FAIRINGS RT PYLON PANEL 457BT CRACKED. MINOR REPAIR.
- [SDR FDEA201411073569](https://openairdocs.org/sdr/FDEA201411073569.md): Attach Bracket · cracked · Nov 7, 2014 · N566FE · Doug MD1010F · Turbine Engine Reduction Gear
  > NUMBER 3 ENG FAN ACCESSORY INBD SIDE HYD PUMP HOSE LINE ATTACHED BRACKET CRACKED. REMOVED & INSTALLED ATTACHED BRACKET IAW SRM 51-31-01. WELDED ON T14 1103378 IAW EA 8-7210-T0312736 REV NO PS P1 TITLE ENG REDUCTION GEAR & SHAFT NR 3 ENG HYD PUMP. IN REPAIR.
- [SDR FDEA201411043497](https://openairdocs.org/sdr/FDEA201411043497.md): Frame Splice · corroded · Nov 4, 2014 · N566FE · Doug MD1010F · Fuselage Main, Frame
  > CENTER CARGO COMPARTMENT BILGE AT STATION 1781 BETWEEN LONGERON 48L - 49L LOWER FRAME SPLICE HAS CORROSION. R & R SPLICE STRAP, FABRICATED ON T14 1101840 IAW SRM 51-31-01 & REPAIRED LOWER FRAME CHANNEL STATION 1781 IAW SRM 53-30-00 FIG 5 & INSTALLED IAW SRM 5
- [SDR FDEA201411023453](https://openairdocs.org/sdr/FDEA201411023453.md): Floorbeam · corroded · Nov 2, 2014 · N566FE · Doug MD1010F · Fuselage Main, Floor Beam
  > AFT CARGO FLOORBEAM UPPER CHORD AT STATION 1902, STRINGER 43R HAS HEAVY CORROSION ON LOWER SURFACE. INSTALLED FILLER & ANGLE REPAIR AT AFT CARGO FLOORBEAM 43R IAW SRM 53-00-01 PAGE 29 FIG 28 & SRM 51-31-01. FLOORBEAM IS OUT OF LIMITS IAW SRM 53-00-01 FIG 1B
- [SDR FDEA201411023452](https://openairdocs.org/sdr/FDEA201411023452.md): Seat Track · mechanic error · Nov 2, 2014 · N566FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > AFT PIT LT SEAT TRACK HAS DOUBLE DRILLED HOLE BETWEEN STATION 1821 & 1801. REMOVED DAMAGE OF DOUBLE DRILLED HOLES IAW SRM 51-21-04. FABRICATED FILLER & STRAP IAW SRM 53-70-00 FIG 1B ITEM 2. INSTALLED FASTENERS TO FILLER & DOUBLER IAW SRM 51-31-01. MAJOR RE
- [SDR FDEA201411013447](https://openairdocs.org/sdr/FDEA201411013447.md): Floorbeam · corroded · Nov 1, 2014 · N566FE · Doug MD1010F · Fuselage Main, Floor Beam
  > LOWER FWD CARGO COMPARTMENT STATION 979 BL 0 FLOOR SUPPORT HAS CORROSION. REPAIRED FLOOR SUPPORT AT STATION 979 LBL 9.5 - RBL 8.5 IAW SRM 53-60-01 FIG 3. MAJOR REPAIR.
- [SDR FDEA201411013446](https://openairdocs.org/sdr/FDEA201411013446.md): Roller Tray · corroded · Nov 1, 2014 · N566FE · Doug MD1010F · Cargo Compartments
  > CENTER CARGO COMPARTMENT BETWEEN STATION 1641 - 1661, RT SIDE ROLLER TRAY SEVERAL AREAS HAVE CORROSION & DEFORMED, RBL 54. REPAIRED CTR CARGO COMPARTMENT ROLLER TRAY BETWEEN 1621 - 1661, RBL 54 IAW SRM 53-70-00 FIG 7. MAJOR REPAIR.
- [SDR FDEA201410313440](https://openairdocs.org/sdr/FDEA201410313440.md): Support Channel · cracked · Oct 31, 2014 · N566FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT PIT COMPARTMENT FWD BULKHEAD LT SEAT TRACK FWD ATTACH CHANNEL HAS CRACK ON BOTH ENDS. R & R FLOOR SUPPORT IAW SRM 51-31-01. FABRICATED FLOOR SUPPORT UNDER T14 1100289 FROM STATION 1786 LBL 20 - LBL 40.
- [SDR FDEA201410313439](https://openairdocs.org/sdr/FDEA201410313439.md): Rib · cracked · Oct 31, 2014 · N566FE · Doug MD1010F · Wing, Rib/Bulkhead
  > RIGHT WING FIXED LE UPPER CHAMBER LOWER SKIN, RIB SUPPORT ABOVE PULLEY HAS A CRACK. R & R SPLICE PLATE, FORMER ON RT WING FIXED LE. FABRICATED FROM 7075-T6.071 INCHES BATCH NR 2689862 IAW SRM 51-31-01 & DWG NRB1249-12. MAJOR REPAIR.

Next page: https://openairdocs.org/deregistered/N566FE-2024-01-29/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 = 'N566FE' AND deregistration_id = 'N566FE-2024-01-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N566FE-2024-01-29/reports

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