# Service difficulty reports: N366FE, cancelled Jan 29, 2024

A list on [N366FE, cancelled Jan 29, 2024](https://openairdocs.org/deregistered/N366FE-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 · 67 reports

- [SDR FDEA201506051699](https://openairdocs.org/sdr/FDEA201506051699.md): Door · cracked · Jun 5, 2015 · N366FE · Doug MD1010F · Cargo/Baggage Doors
  > UPON ARRIVAL FOUND FWD LOWER CORNER OF FWD LOWER CARGO DOOR DAMAGED. FWD CARGO DOOR CORNER DAMAGED, OK FOR SERVICE IAW EA 8-5230-T0317891. COMPLIED WITH PART 1 OF EA 8-5230-T0317891. INSTALLED REPAIR PARTS & PAINTED IAW SRM 52-10-00. COMPLIED WITH EA 8-523
- [SDR FDEA201505241627](https://openairdocs.org/sdr/FDEA201505241627.md): Panel · missing · May 24, 2015 · N366FE · Doug MD1010F · Nacelle/Pylon, Plate/Skin
  > ON WALK AROUND NOTICED FWD INBD PANEL MISSING ON NR 1 PYLON LE. REPLACED PANEL WITH SERVICEABLE PANEL.
- [SDR FDEA201504081169](https://openairdocs.org/sdr/FDEA201504081169.md): Connector · not seated · Apr 8, 2015 · N366FE · Doug MD1010F · Electrical Power System Wiring
  > EMER PWR TEST FAIL, LEVEL ONE ALERT ON PREFLIGHT. RESET 3 FUEL LEVERS & PERFORMED SYS TEST ALSO RESEATED BATTERY CHARGER CONNECTORS ON CHARGER. PREFORMED SYSTEM TEST IAW AMM 24-34-02. ALL TESTED NORMAL. OK FOR SERVICE.
- [SDR FDEA201503271102](https://openairdocs.org/sdr/FDEA201503271102.md): Unknown · failed · Mar 27, 2015 · N366FE · Doug MD1010F · DC Generating System
  > ON PREFLIGHT EMER POWER TEST FAILED. CALLED MX.
- [SDR FDEA201407261981](https://openairdocs.org/sdr/FDEA201407261981.md): Power Supply · failed · Jul 26, 2014 · N366FE · Doug MD1010F · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST, RECEIVED LEVEL 1 ALERT; EMERGENCY LIGHT BATTERY ONE LOW. R & R EMERGENCY LIGHTS POWER SUPPLY. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA201406011246](https://openairdocs.org/sdr/FDEA201406011246.md): Skin · cracked · Jun 1, 2014 · N366FE · Doug MD1010F · Wing, Plate/Skin
  > APPEARS TO BE A CRACK IN RADIUS ON LT INBD FUELING PNL. PERFORMED HFEC INSP ON NEW CUT OUT IAW NTM PT 6, NO CRACK INDICATION FOUND. FABRICATED REPAIR DOUBLER & FILLERS FROM PREVIOUSLY VERIFIED MATERIAL IAW SRM 57-10-00. MX REQUEST OK TO INSTALL REPAIR PARTS
- [SDR FDEA201310152511](https://openairdocs.org/sdr/FDEA201310152511.md): Spar · cracked · Oct 15, 2013 · N366FE · Doug MD1010F · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STABILIZER REAR SPAR UPPER ANGLE VERTICAL TANG HAS TWO CRACKS AT THE UPPER ROW OF FASTENERS COMING OUT FROM UNDER WASHER, SECOND AND THIRD FASTENER HOLES. CRACKS ARE BEYOND BLEND LIMITS. REAMED HOLES TO REMOVE CRACK INDICATIONS. PLUGGED AND R
- [SDR FDEA201310042412](https://openairdocs.org/sdr/FDEA201310042412.md): Support Fitting · cracked · Oct 4, 2013 · N366FE · Doug MD1010F · Fuselage Main, Structure
  > MCD LOWER FRAME 6 SUPPORT FITTING IS CRACKED AT "C" HOLE. VERIFIED WITH HFEC AND BORESCOPE. R & R NR 6 SUPPORT FITTING MCD SPOOL REF SRM 51-31-01, VOL II.
- [SDR FDEA201309252311](https://openairdocs.org/sdr/FDEA201309252311.md): Sill · corroded · Sep 25, 2013 · N366FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO COMPARTMENT DOOR SILL LOWER WEB AT BS 1835, JUST AFT OF AFT LATCH SPOOL FITTING, DOOR SILL WEB IS CORRODED. REMOVED CORROSION IAW SRM 53-50-00. REPAIRED IAW EA 8-5316-T03085A.
- [SDR FDEA201302040262](https://openairdocs.org/sdr/FDEA201302040262.md): Switch · failed · Feb 4, 2013 · N366FE · Doug MD1010F · Escape Slide
  > R1 EVACUATION SLIDE PRESSURE PRESS TO TEST INDICATING INOPERATIVE. R & R R1 DOOR ESCAPE SLIDE PRESSURE PRESS-TO-TEST SWITCH IAW MM 25-61-03-2, OPS CHECKED GOOD, ACFT OK FOR SERVICE.
- [SDR FDEA201211284193](https://openairdocs.org/sdr/FDEA201211284193.md): Bulkhead Web · cracked · Nov 28, 2012 · N366FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RIGHT BULKHEAD CRACKED 25 INCHES FWD OF BS 1521 AND 19 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED BULKHEAD IAW SRM 53-00 -01, FIG 10.
- [SDR FDEA201109163910](https://openairdocs.org/sdr/FDEA201109163910.md): Skin · dented · Sep 16, 2011 · N366FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT INBD FLAP UPPER SURFACE, DENTED 86" FROM INBD AND 6.5" FROM T/E. FOUND OUT OF LIMITS IAW SRM 51-80-01, PG 1, PARA 2. REPAIRED SKIN IAW SRM 57-00-01, FIG 4. (MAJOR)
- [SDR FDEA201109163909](https://openairdocs.org/sdr/FDEA201109163909.md): Skin · corroded · Sep 16, 2011 · N366FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT WING TE FLAP UPPER SKIN CORRODED OUT OF LIMITS. REPAIRED SKIN IAW SRM 57-10-00, FIG 86.
- [SDR FDEA201109133864](https://openairdocs.org/sdr/FDEA201109133864.md): Cable · out of limits · Sep 13, 2011 · N366FE · Doug MD1010F · Passenger/Crew Doors
  > R1 DOOR SEQUENCE CABLE FOR AIR BOTTLE IS BINDING FOUND CABLE ADJUSTMENT OUT OF LIMITS. CABLE MOVEMENT GOOD. ADJUSTED AIR BOTTLE CABLE IAW MM 52-11-00-5. OPS CHECKED GOOD IAW MM 52-11-00-5 STEP 3G.
- [SDR FDEA201109133866](https://openairdocs.org/sdr/FDEA201109133866.md): Motor · binding · Sep 13, 2011 · N366FE · Doug MD1010F · Passenger/Crew Doors
  > R1 DOOR SEQUENCE CABLE FOR DECLUTCH IS BINDING. REMOVED AND REPLACED AC MOTOR AND ADJUSTED DECLUTCH CABLE IAW MM 52-11-01-2 AND 52-11-00-5. OPS CHECKED GOOD IAW MM 52-11-00-5 STEP 3G.
- [SDR FDEA201109133865](https://openairdocs.org/sdr/FDEA201109133865.md): Cable · binding · Sep 13, 2011 · N366FE · Doug MD1010F · Passenger/Crew Doors
  > R1 DOOR SEQUENCE CABLE FOR UPLOCK IS BINDING REMOVED AND REPLACED UPLOCK/CLOSE CABLE IAW AMM 52-11-12-2. ADJUSTED IAW AMM 52-11-00-5. OPS CHECKED GOOD.
- [SDR FDEA201109093809](https://openairdocs.org/sdr/FDEA201109093809.md): Roller · gouged · Sep 9, 2011 · N366FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT INBOARD FLAP WELL LOWER FORWARD ROLLER FITTING ASSY GOUGED. R & R LEFT INBOARD LOWER DUAL BRACKET ASSY IAW SRM 51-31-01.
- [SDR FDEA201109083769](https://openairdocs.org/sdr/FDEA201109083769.md): Seat Track · worn · Sep 8, 2011 · N366FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, FS 1251 LBL 75, HAS WORN LOBE. CHECKED DAMAGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG. 5. R & R SEAT TRACK IAW SRM 53-70-00 FIG 1 SH 2.
- [SDR FDEA201109083767](https://openairdocs.org/sdr/FDEA201109083767.md): Seat Track · worn · Sep 8, 2011 · N366FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FS 1320 RBL 28 HAS WORN LOBE. FOUND OUT OF LIMITS IAW SRM 53-70-00 FIG 5. CUT OUT DAMAGED PART REPAIRED IAW SRM 53-70-00 FIG 1 AND SRM 51-31-01. MAJOR REPAIR.
- [SDR FDEA201106032103](https://openairdocs.org/sdr/FDEA201106032103.md): Battery · failed · Jun 3, 2011 · N366FE · Doug MD1010F · Emergency Lighting
  > DURING PREFLIGHT FOUND EMERGENCY LIGHT TEST SHOWS "EMER LT BATT 1 FAIL". R & R EMERGENCY LIGHTING BATTERY IAW AMM 33-51-01-4, OK FOR SERVICE.
- [SDR FDEA201106032102](https://openairdocs.org/sdr/FDEA201106032102.md): Lens · damaged · Jun 3, 2011 · N366FE · Doug MD1010F · Emergency Lighting
  > DURING PREFLIGHT CHECK FOUND L1 DOOR EMERGENCY LIGHT LENS DAMAGED ON FLOOR. RELEASED FOR SERVICE IAW MEL: 33-50-02. REPLACED L1 DOOR EMERGENCY LIGHT LENS COVER IAW SMP.
- [SDR FDEA201106032101](https://openairdocs.org/sdr/FDEA201106032101.md): Lens · damaged · Jun 3, 2011 · N366FE · Doug MD1010F · Emergency Lighting
  > DURING PREFLIGHT CHECK FOUND L1 DOOR EMERGENCY LIGHT LENS DAMAGED ON FLOOR. RELEASED FOR SERVICE IAW MEL: 33-50-02.
- [SDR FDEA201103070903](https://openairdocs.org/sdr/FDEA201103070903.md): Switch · failed · Mar 7, 2011 · N366FE · Doug MD1010F · Extinguishing System
  > FOUND NR 2 ENGINE FIRE AGENT 1 LOW LIGHT ILLUMINATED WHILE PREFORMING ENGINE RUN CHECK LIST FOR REQUAL. TROUBLESHOT PROBLEM TO A BAD AGENT 1 LOW SWITCH, L2-216, AT THE APU GROUND CONTROL PANEL. R & R L2-216 AND L2-217 NR 1 AND NR 2 AGENT LOW LIGHTS AT REMOT
- [SDR FDEA201102150566](https://openairdocs.org/sdr/FDEA201102150566.md): Engine · vibration · Feb 15, 2011 · N366FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > SHUTDOWN ENG NR 1 INFLIGHT FOR UNUSUAL VIBRATIONS. VIBES START AT 91 PERCENT - AND VERY NOTICABLE ABOVE 94 PERCENT - LIGHT TO MEDIUM "SHUDDER" RAPTED VIBRATION. REMOVED NR 1 ENGINE SPINNER ASSY & FIRST STAGE FAN ROTOR BLADES IAW MM 72-21-00-4. LUBED IAW AMM
- [SDR FDEA201010314199](https://openairdocs.org/sdr/FDEA201010314199.md): Battery · inoperative · Oct 31, 2010 · N366FE · Doug MD1010F · Emergency Lighting
  > DURING THE EMERGENCY LIGHT TEST RECEIVED EMERG BAT 1 LOW ALERT. R & R NR1 EMERGENCY LIGHT BATTERY REF33-51-01-4-0. OPS CHECKED GOOD ACFT OK TO CONTINUE.
- [SDR FDEA201001190178](https://openairdocs.org/sdr/FDEA201001190178.md): Handle · malfunctioned · Jan 19, 2010 · N366FE · Doug MD1010F · Landing Gear Selector
  > ON FIRST LANDING ATTEMPT, GOT 3 RED ON PANEL AND CONFIG PAGE (TRIED PUSHING DOWN ON HANDLE, NO HELP). RAN CHECKLIST AND PUT GEAR HANDLE DOWN THE SECOND TIME WITH FORCE, GOT 3 DOWN GREEN ON ALL INDICATIONS. HANDLE ASSY INSTALLATION REPLACED. ADJUSTED LANDI
- [SDR FDEA200909273392](https://openairdocs.org/sdr/FDEA200909273392.md): Engine · malfunctioned · Sep 27, 2009 · N366FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > ABORT TAKEOFF, 75 KNOTS, ENG 3 EXCEEDANCE ON N2 PEAK 101,.2 RED: 101.0 FOR 2.3 SECONDS NO RESTRICTION, REF: AMM 72-00-00-6, NR 3 ENGINE N2 EXCEEDANCE 101.2 WILL REQUIRE CORE COMPRESSOR AND HPT BORESCOPE WITH IN 10 CYCLES INSPECTED EXHAUST NOZZLES FOR PARTI
- [SDR FDEA200902100498](https://openairdocs.org/sdr/FDEA200902100498.md): Skin · corroded · Feb 10, 2009 · N366FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE DISHED RIVET AT LONG 48L STA 1761. REPAIRED AREA REF SRM 53-20-00.
- [SDR FDEA200902100497](https://openairdocs.org/sdr/FDEA200902100497.md): Skin · corroded · Feb 10, 2009 · N366FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE DISHED RIVET AT LONG. 46L STA 1741. REPAIRED AREA REF SRM 53-20-00.
- [SDR FDEA200902100496](https://openairdocs.org/sdr/FDEA200902100496.md): Skin · corroded · Feb 10, 2009 · N366FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE DISHED RIVET AT LONG 441 STATION 1682. REPAIRED FUSELAGE SKIN IAW DC 10 SRM 53-20-00 FIG 6.
- [SDR FDEA200901150209](https://openairdocs.org/sdr/FDEA200901150209.md): Link · damaged · Jan 15, 2009 · N366FE · Doug MD1010F · Main Landing Gear
  > RIGHT MAIN GEAR INDICATED UNSAFE ON DEPARTURE COMPLIED WITH QRH AND DIVERTED TO LAX. FOUND RT CRANK ASSY UPPER BOLT NUT MISSING. LINK ASSY FOUND DAMAGED REMOVED AND REPLACED LINK ASSEMBLY AND PERFORMED OPS CHECK IN REF TO MM 32-61-15-4. CHECKS GOOD OK TO CO
- [SDR FDEA200809093782](https://openairdocs.org/sdr/FDEA200809093782.md): Pump · leaking · Sep 9, 2008 · N366FE · Doug MD1010F · Hydraulic Pump (Electric/Engine), Main
  > 35 MINUTES INTO FLT, ENG NR 2 OIL QTY DROPPED TO ZERO, TEMP 7 PRESSURE NORMAL. PRESSURE FLUCTUATED CONSTANTLY DECREASING TO APPROX (15 PSI) FLUCTUATING /- 5 PSI WHEN ENGINE WAS SHUT DOWN IN ACCORDANCE W/QRH. WINDMILLING PRESSURE GREATER THAN 2 PSI. REPLAC
- [SDR 08FDEA03782](https://openairdocs.org/sdr/08FDEA03782.md): Oil System · low · Sep 9, 2008 · N366FE · Doug MD1010F · Turbine Engine Oil System
  > 35 MINUTES INTO FLT ENG NR 2 OIL QTY DROPPED TO ZERO. TEMP 7 PRESSURE NORMAL. PRESSURE FLUCTUATED CONSTANTLY DECREASING TO APPROX (15 PSI) FLUCTUATING /- 5 PSI WHEN ENGINE WAS SHUT DOWN IN ACCORDANCE W/QRH. WINDMILLING PRESSURE GREATER THAN 2 PSI.
- [SDR 08FDEA02167](https://openairdocs.org/sdr/08FDEA02167.md): None · none · Jun 5, 2008 · N366FE · Doug MD1010F · Standard Practices/Structures
  > REJECTED TAKEOFF FOR WINDSHEAR AURAL ALERT 80 KTS,34 DEG C,386K FACT 05 JUN08 21:47 AFW U CHECKED PER AMM 05-56-00 AND 05-57-00, ACFT OK FOR SERVICE CHECKED PER AMM 05-56-00 AND 05-57-00, ACFT OK FOR SERVICE.
- [SDR 07FDEA04880](https://openairdocs.org/sdr/07FDEA04880.md): Frame · misrepaired · Nov 20, 2007 · N366FE · Doug DC1010 · Fuselage Main, Frame
  > DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON FRAME CAP AT STA 840 BETWEEN LONG NR 50R AND 50L WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA. REPAIR HAS BEEN REPLACED WITH A NEW ONE IAW SRM 53-30-00, FIG 5, VOL I.
- [SDR 07FDEA04879](https://openairdocs.org/sdr/07FDEA04879.md): Skin · misrepaired · Nov 20, 2007 · N366FE · Doug DC1010 · Wing, Plate/Skin
  > DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON LT DROOPED L/E SKIN WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA REPAIR HAS BEEN REPLACED WITH A NEW ONE IAW SRM 57-10-00, FIG 55, VOL I.
- [SDR 07FDEA04878](https://openairdocs.org/sdr/07FDEA04878.md): Doubler · damaged · Nov 20, 2007 · N366FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON EXTERNAL SKIN AT FWD CARGO DOOR AFT JAMB WAS FOUND DAMAGED. REPAIR AS BEEN REPLACED WITH A NEW ONE IAW SRM 53-50-00 FIG 9.
- [SDR 07FDEA04877](https://openairdocs.org/sdr/07FDEA04877.md): Frame · misrepaired · Nov 20, 2007 · N366FE · Doug DC1010 · Fuselage Main, Frame
  > DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON FRAME CAP AT STA 879 BETWEEN LONG NR 47R AND 47L WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA. REPAIR HAS BEEN REPLACED WITH A NEW IAW SRM 53-30-00, FIG 5, VOL I.
- [SDR 07FDEA04876](https://openairdocs.org/sdr/07FDEA04876.md): Frame · misrepaired · Nov 20, 2007 · N366FE · Doug DC1010 · Fuselage Main, Frame
  > DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON FRAME CAP AT STA 824 BETWEEN LONG NR 50R AND 50L WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA. REPAIR HAS BEEN REPLACED WITH A NEW ONE IAW SRM 53-30-00, FIG 5, VOL I.
- [SDR 07FDEA04875](https://openairdocs.org/sdr/07FDEA04875.md): Frame · misrepaired · Nov 20, 2007 · N366FE · Doug DC1010 · Fuselage Main, Frame
  > DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON FRAME CAP AT STA 859 BETWEEN LONG NR 50R AND 50L WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA REPAIR HAS BEEN REPLACED WITH A NEW ONE IAW SRM 53-30-00, FIG 5, VOL I.
- [SDR 07FDEA04860](https://openairdocs.org/sdr/07FDEA04860.md): Fitting · cracked · Nov 19, 2007 · N366FE · Doug DC1010 · Fuselage Structure (General)
  > DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), VANE AIR CONDITION LT SIDE BAY JAMB STRUCTURE FRAME TO STA 528 DEFORMED CORROSION AND CRACK LONG 2" ON SUPPORT FITTING. REPLACED FRAME ACA3347-3 AND FITTING ACA3799-501 FOR SRM 51-35-01 VOL II.
- [SDR 07FDEA04857](https://openairdocs.org/sdr/07FDEA04857.md): Frame · damaged · Nov 19, 2007 · N366FE · Doug DC1010 · Fuselage Main, Frame
  > DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), AVIONIC COMPT AT STA 449 RT AND X= -10 FRAME WITH HOLE OVALIZED PERFORMED REPAIR FOR SRM 53-30-00 FIG 4 VOL I.
- [SDR 07FDEA04855](https://openairdocs.org/sdr/07FDEA04855.md): Skin Panel · cracked · Nov 19, 2007 · N366FE · Doug DC1010 · Wing, Plate/Skin
  > DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), LT WING T/E ON UPPER SKIN OUTBOARD FLAP XOF 620 FOUND DENT 1" BY 1" AND A TEE ANGLE WITH CRACK 1 INCH LONG REPLACED PANEL ARC 1959U27 FOR SRM 51-35-01 VOL II.
- [SDR 07FDEA04852](https://openairdocs.org/sdr/07FDEA04852.md): Fitting · corroded · Nov 19, 2007 · N366FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING THE HOLES OF THE BOLTS WITH CORROSION. PERFORMED CORROSION REWORK REAMED HOLES, PERFORMED INSPECT HFEC AND INSTALLED BUSHINGS FOR SRM 53-50-00 FIG 17.
- [SDR 07FDEA04849](https://openairdocs.org/sdr/07FDEA04849.md): Fitting · cracked · Nov 19, 2007 · N366FE · Doug DC1010 · Fuselage Main, Keel
  > DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), CTR SECTION BOX WHEEL WELL AREA STA 1370 LT SIDE XCW 31.500 KEEL FITTING APB7078-1 WITH CRACK 5" LONG REPLACED KEEL FITTING FOR SRM 51-33-01 AND SRM 51-32-01.
- [SDR 07FDEA04846](https://openairdocs.org/sdr/07FDEA04846.md): Door Frame · deformed · Nov 19, 2007 · N366FE · Doug DC1010 · Fuselage Main, Structure
  > DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), VANE AIR CONDITION COMPT LT SIDE BAY JAMB STRUCTURE FRAME AT STA 486 DEFORMED REPAIRED FOR SRM 53-30-00 FIG 5 VOL I.
- [SDR 07FDEA04845](https://openairdocs.org/sdr/07FDEA04845.md): Frame · cracked · Nov 19, 2007 · N366FE · Doug DC1010 · Nacelle/Pylon, Frame/Spar/Rib
  > DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK) PYLON NR 3 FOUND INTERNAL SIDE FRAME BROKEN AND DEFORMED. REPLACED STRAP P/N AVB7123-3, ANGLE P/N AUB7123-5, ZEE P/N AUB7123-7, CLIP P/N AUB7124-2 FOR SRM 51-33-01 VOL II.
- [SDR 07FDEA04844](https://openairdocs.org/sdr/07FDEA04844.md): Stringer · cracked · Nov 19, 2007 · N366FE · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), VANE AIR CONDITION LT SIDE FROM STA 561 TO STA 587 STRINGER 48 WITH CRACK AND SEVERAL CORROSION REPAIRED WITH REFERENCE SRM 53-10-00 FIG 6 VOL I.
- [SDR 07FDEA04843](https://openairdocs.org/sdr/07FDEA04843.md): Channel · corroded · Nov 19, 2007 · N366FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK) FOUND IN LOWER FWD CARGO LIGHT CORROSION ON CHANNEL FROM STA 759 TO STA 879 X= 59. REMOVED CORROSION FOR SRM 51-21-01 VOL 2. PERFORMED CHECK LIMIT THICKNESS IS OUT LIMITS. REPLACED CHANNEL FOR S
- [SDR 07FDEA04671](https://openairdocs.org/sdr/07FDEA04671.md): Stiffener · cracked · Oct 24, 2007 · N366FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > VANE AIR CONDITION COMPARTIMENT LT PACK N°2 INTERNAL SIDE STA 475 TEE P/N NCA6048-105 WITH CRACK 4 INCH. REPAIRED STIFFENER FOR SRM 53-40-00 FIG 10 VOL I.

Next page: https://openairdocs.org/deregistered/N366FE-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 = 'N366FE' AND deregistration_id = 'N366FE-2024-01-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N366FE-2024-01-29/reports

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