# Service difficulty reports: N364FE, cancelled Feb 25, 2004

A list on [N364FE, cancelled Feb 25, 2004](https://openairdocs.org/deregistered/N364FE-2004-02-25.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR 03FDEA02175](https://openairdocs.org/sdr/03FDEA02175.md): Pressure Switch · failed · Dec 8, 2003 · N364FE · Doug DC1010 · Pneumatic System
  > RECEIVED NR 1 MANIFOLD FAIL ALERT AT FL350. COULD NOT MAINTAIN CABIN PRESSURE. RAN RED TABS AND DIVERTED TO DEN. FOUND LEFT WING PRESSURE SWITCH FAULT BALL NO LEAKS NOTED. PERFORMED DECAY CHECK PER MD-10 MM 36-00-01-5 DECAY CHECK WITHIN LIMITS. REMOVED AN
- [SDR 03FDEA00822](https://openairdocs.org/sdr/03FDEA00822.md): Bulkhead · cracked · May 28, 2003 · N364FE · Doug DC1010 · Fuselage Main, Bulkhead
  > COMPLY WITH E.A.8-5310-70387. FUSELAGE-MAINFRAME-REPAIR OF STA 1987 BULKHEAD P/N AJC7066-1. CLOSING ACTION ON 05-27-03 ON N/R C00019. COMPLIED WITH E.A.8-5310-70387.
- [SDR 03FDEA00800](https://openairdocs.org/sdr/03FDEA00800.md): Rib · cracked · May 24, 2003 · N364FE · Doug DC1010 · Nacelle/Pylon, Main Frame
  > NR 855 NR 3 ENGINE RTCORE COWL FWD RIB CRACKED AT UPPER L/E RADIUS. CLOSING ACTION ON 05/24/03. REMOVED FASTENERS FOR ACCESS IAW SRM 51-31-01. WELLED CRACK ON MAE TRAVELER T2/336399 IAW SRM 54-31-01. REINSTALLED FASTNERS IAW SRM 51-35-01, PAINTED TEFLO
- [SDR 03FDEA00801](https://openairdocs.org/sdr/03FDEA00801.md): Control Valve · failed · May 24, 2003 · N364FE · Doug DC1010 · Engine Thrust Reverser
  > N 860 #2 O/B T/R FAILS TO AUTO-RESTOW CHECK. CLOSING ACTION ON 05/24/03. REMOVED AND REPLACED DIRECTI0NAL CONTROL VALVE IAW M/M 78-31-11-2, LEAK TO BE ACCOMPLISHED ON W/C 78X3501CMR.
- [SDR 03FDEA00802](https://openairdocs.org/sdr/03FDEA00802.md): Skin · cracked · May 24, 2003 · N364FE · Doug DC1010 · Leading Edge Devices
  > NR S 17 COMPLY WITH E.A.8-5710-70392.WINGS-RT-FIXED LEADING EDGE BEADED DOUBLER REPAIR ACB 1242. CLOSING ACTION ON 05/23/03. COMPLIED WITH E.A.8-5710-70392.
- [SDR 03FDEA00803](https://openairdocs.org/sdr/03FDEA00803.md): Clip · damaged · May 24, 2003 · N364FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE PENTHOUSE CANTED FRAME AT Y=2029.88. HAS REPAIRS, SHOULD BE REPLACED PER E.O.8-5310-7-5000.PT 1. CLOSING ACTION ON 02/22/03. REMOVED AND REPLACED CLIP IAW E.O.8-5310-7-5000.PT1 AND SRM 51-31/01.
- [SDR 03FDEA00804](https://openairdocs.org/sdr/03FDEA00804.md): Rub Strip · cracked · May 24, 2003 · N364FE · Doug DC1010 · Cargo/Baggage Doors
  > LT PATIO DOOR UPPER STAINLESS STRIP CRACKED AND CRUSHED. CLOSING ACTION ON 05/24/03. REMOVED CLOSEOUT STRIP IAW SRM 51-31-01.FAB NEW RUB STRIP ON TRAVLER T2/33374, LOCATED AND DRILLED NEW PART IAW SRM 51-31-01.INSTALLED RUB STRIP IAW SRM 51-31-01
- [SDR 03FDEA00781](https://openairdocs.org/sdr/03FDEA00781.md): Hinge · corroded · May 20, 2003 · N364FE · Doug MD1010F · Wing Main, Frame Structure
  > S 16 COMPLY WITH E.A.8-5740-70384. WINGS INBD FLAP OUTBD HINGE SUPPORT FITTING TO WING ATTACH HOLES REWORK. CLOSING ACTION ON 05/19/03. COMPLIED WITH E.A.8-5740-70384.
- [SDR 03FDEA00760](https://openairdocs.org/sdr/03FDEA00760.md): Hinge · corroded · May 19, 2003 · N364FE · Doug MD1010F · Trailing Edge Flaps
  > S 14 C/W E.A.8-5740-70390. WINGS-RT INBD FLAP HINGE ASSY CORROSION REWORK. CLOSING ACTION ON 05/17/03. COMPLIED WITH E.A.8-5740-70390.WINGS R/H INBD FLAP HINGE ASSY CORROSION REWORK.
- [SDR 03FDEA00726](https://openairdocs.org/sdr/03FDEA00726.md): Door Frame · cracked · May 12, 2003 · N364FE · Doug DC1010 · Fuselage Main, Structure
  > NR 200 RT PATIO DOOR NR 10 FRAME CRACKED AS MARKED. STOPPED DRILL CRACK IAW MD-10 SRM 53-30-00. FAB ANGLE REPAIR IAW MAE TRAVLER T2/333232. LOCATED AND DRILLED ANGLE IAW MD-10 SRM 53-30-00, INSTALLED ANGLE REPAIR IAW SRM 51-31-01, 51-33-01.
- [SDR 03FDEA0163](https://openairdocs.org/sdr/03FDEA0163.md): Proximity Switch · inoperative · Feb 21, 2003 · N364FE · Doug DC1010F · Landing Gear Position and Warning
  > WHEN GEARS WERE LOWERED, ALL 3 GEAR INDICATED UNSAFE ON MAIN GEAR INDICATORS AND CONFIGURATION PAGE. NO ABNORMAL YAW OR NOISE. RECYCLED GEAR AND GOT 3 GOOD DOWN INDICATIONS. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONICS UNIT IN REF TO MD1 0-10 M/M 31-71
- [SDR 02FDEA00210](https://openairdocs.org/sdr/02FDEA00210.md): Detector · inoperative · Mar 19, 2002 · N364FE · Doug DC1010F · Pneumatic Indicating System
  > ON CLIMBOUT NR 2 MANIFOLD FAIL ILLUM'D. NR 2 MANIFOLD FAIL DET LOOP INOP, DO NOT PRESS PNEU SYS NR 2 EXCEPT FOR ENG START.
- [SDR 01FDEA00954](https://openairdocs.org/sdr/01FDEA00954.md): Skin · cracked · Nov 1, 2001 · N364FE · Doug DC1010F · Trailing Edge Flaps
  > LEFT HAND INBOARD FLAP OUTER SKIN HAS.5 INCH CRACK. REMOVED AND REPLACED SKIN PER SRM 57-00-01.
- [SDR 01FDEA00953](https://openairdocs.org/sdr/01FDEA00953.md): Vane · gouged · Nov 1, 2001 · N364FE · Doug DC1010F · Trailing Edge Flaps
  > LEFT HAND OUTBOARD FLAP VANE HAS GOUGE. REMOVED AND REPLACED FLAP PER SRM 51-71-00.
- [SDR 01FDEA00887](https://openairdocs.org/sdr/01FDEA00887.md): Attach Angle · cracked · Oct 11, 2001 · N364FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > IN CTR CARGO AT BS 1521 BILGE AREA BETWEEN LONGERONS R44 & R46 CRACK IN BULKHEAD ATTACH ANGLE. REMOVED AND REPLACED TEE CHORD PER SRM & AEA0453-1 & SRM 51-39-01.
- [SDR 01FDEA00884](https://openairdocs.org/sdr/01FDEA00884.md): Splice · cracked · Oct 11, 2001 · N364FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > CTR CARGO BILGE AREA LEFT LONGERON 46 BETWEEN BS 1744 & 1761 LONGERON SPLICE CRACKED. REMOVED AND REPLACED SPLICE PER SRM 51-21-01, 51-35-01.
- [SDR 01FDEA00885](https://openairdocs.org/sdr/01FDEA00885.md): Splice · cracked · Oct 11, 2001 · N364FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > CTR CARGO BILGE AREA L47 BETWEEN BS 1741 & 1761 LONGERON SPLICE CRACKED. REMOVED AND REPLACED SPLICE PER SRM 51-23-01, 51-00-00.
- [SDR 01FDEA00886](https://openairdocs.org/sdr/01FDEA00886.md): Splice · cracked · Oct 11, 2001 · N364FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > IN CTR CARGO BILGE AREA BETWEEN BS 1701 & 1721 CRACK ON LONGERON SPLICE 51L. REMOVED AND REPLACED LONGERON SPLICE PER SRM 51-23-01 & 51-00-00.
- [SDR 01FDEA00871](https://openairdocs.org/sdr/01FDEA00871.md): Aileron · corroded · Oct 8, 2001 · N364FE · Doug DC1010F · Ailerons
  > SIX SEPARATE AREAS ON RT OUTBOARD AILERON LWR CORRODED. REMOVED AND REPLACED AILERON PER IAW AMM 27-10-02-4.
- [SDR 2000ZZZX652](https://openairdocs.org/sdr/2000ZZZX652.md): Web · cracked · Feb 11, 2000 · N364FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE, 3.0 INCH CRACK WAS FOUND ON RIGHT/CENTER WHEELWELL WEB. CRACK AFFECTED UPPER SPLICE WEB, P/N AEA0161-1, RT SIDE, AND AEA0501-1. (X)
- [SDR 99FDEA00304](https://openairdocs.org/sdr/99FDEA00304.md): Bolt · corroded · Mar 10, 1999 · N364FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > N2764, DURING A/C P-F CONV AT AERONAVALI, A SUSPECTED BOLT FAILURE WAS FOUND AT STA Y=275 FOR ATTACH P/N ABA7003-2, ABA7023-1, NBA6044-15 AND ABA7171. REPAIR WAS ACCOMPLISHED IAW EA NR 8-5311-44057 AND IT WAS APPROVED PER FEDEX 8110-3 DATED 29 APR 99. THE AP
- [SDR 99FDEA00305](https://openairdocs.org/sdr/99FDEA00305.md): Spar · cracked · Oct 21, 1998 · N364FE · Doug DC1010 · Horizontal Stabilizer, Spar/Rib
  > N2420 - DURING A/C PF CONVERSION AT AERONAVALI AND ACCOMPLISHMENT OF DAC SB 55-17, R3, AD 88-03-08, A CRACK WAS FOUND ON THE HORIZONTAL STAB. REPAIR ATTEMPS TO REMOVE CRACK DAMAGE BY LOCAL BLENDING AND PERF HFEC TO QUAN DAMAGE. B/P EQUIVALENT BOLT IS REINSTA
- [SDR 99FDEA00307](https://openairdocs.org/sdr/99FDEA00307.md): Web · cracked · Sep 4, 1998 · N364FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > N0527 - DURING AC P-F CONV AT AERONAVALI, A CRACK 0.87 IN LONG WAS FOUND ON WEB OF UPPER TORQUE BOX PLANE AT Y=2017 AND RBL = 20. SRM 53-00-01, FIG 4 SHEET 2 WEB REPAIR COULD NOT BE ACCOMPLISHED. REPAIR TO STOP DRILL CRACK AND VERIFY CONTAINMENT. THEN INST
- [SDR 99FDEA00306](https://openairdocs.org/sdr/99FDEA00306.md): Doubler · corroded · Aug 18, 1998 · N364FE · Doug DC1010 · Wing Miscellaneous Structure
  > N0235 - DURING A/C P-F CONV AT AERONAVALI, CORROSION WAS FOUND ON LT UPPER WING AND MLG DOUBLER, TYPICAL PER DC10 SRM 57-00-01, FIG 8. THE AMOUNT OF DAMAGE FOUND ON PN ARB0866-1 IS NOT COVERED BY SRM. REPAIR REMOVES ALL CORROSION BY CUTTING OUT DAMAGE AND TH

## 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 = 'N364FE' AND deregistration_id = 'N364FE-2004-02-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N364FE-2004-02-25/reports

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