# Service difficulty reports: N369FE

A list on [N369FE](https://openairdocs.org/aircraft/N369FE.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 · 63 reports

- [SDR FDEA201609093158](https://openairdocs.org/sdr/FDEA201609093158.md): Channel · corroded · Sep 9, 2016 · N369FE · Doug MD1010F · Fuselage Main, Frame
  > FORWARD CARGO COMPARTMENT FRAME DOUBLER AT STA 979 AT LONG 52, 51R AND 51L. FRAME MOUNT DOUBLER CHANNEL POSSIBLE CORROSION. FABRICATED AND INSTALLED J-CHANNEL IAW SRM 53-30-00, FIG 5, SHEET 2.
- [SDR FDEA200911194048](https://openairdocs.org/sdr/FDEA200911194048.md): Fire Bottle · low · Nov 19, 2009 · N369FE · Doug MD1010F · Fire Bottle, Fixed
  > ENG FIRE AGNT LO ALERT AND ENG 2 AGT 1 LOW LIGHT DURING CRUISE FOUND NR 2 ENG 1 FIRE BOTTLE LOW PRESS SWITCH BAD, REPLACED NR 2 ENG NR1 FIRE BOTTLE, LIGHT EXT. CHECKS OK
- [SDR FDEA200910203620](https://openairdocs.org/sdr/FDEA200910203620.md): Valve · activated · Oct 20, 2009 · N369FE · Doug MD1010F · Pneumatic Indicating System
  > "AIR SYS 1 OFF" ANNUNCIATED. AFTER ABOUT A MINUTE GOT "AIR MANF 1 FAIL" LEVEL 3 ALERT. COMPLIED WITH QRH. DIVERTED, DURING DECENT, AIR MANF 1 FAIL ALERT CAME ON SEVERAL TIMES. INTERIGATED MCDU FOUND NO FAULTS IN AIU, VIA, OR PSC1, PERFORMED RTS ON PSC1 A
- [SDR FDEA200902100502](https://openairdocs.org/sdr/FDEA200902100502.md): Relief Valve · failed · Feb 10, 2009 · N369FE · Doug MD1010F · Pressure Regulator/Outflow Valve
  > AT FL 310 RECEIVED LEVEL 3 "CABIN ALTITUDE" ALERT WITH NO OTHER NOISE OR INDICATIONS. ENG A/I WAS ON. FOLLOWED QRH AND COULD NOT (WITH 3 PACKS) MAINTAIN INDICATED CABIN ALTITUDE TO BELOW 10,000 FT. CABIN ALTITUDE INDICATED CLIMB WITH DDP AT APPROX 9.1. CO
- [SDR FDEA200801070057](https://openairdocs.org/sdr/FDEA200801070057.md): Skin · cracked · Jan 7, 2008 · N369FE · Doug MD1010F · Elevator, Plate/Skin
  > FROM J/C SP10270016-7000-10J OTBD ELEVATOR LT T/E TIP WITH CRACK DUE ACCIDENTAL CONTACT AGAINST CRADLE. REPAIRED AREA IAW SRM 55-10-00 FIG 7 VOL I AND SRM 55-20-00 FIG 4 VOL I.
- [SDR 08FDEA00057](https://openairdocs.org/sdr/08FDEA00057.md): Skin · cracked · Jan 7, 2008 · N369FE · Doug DC1010F · Elevator, Plate/Skin
  > OUTBD ELEVATOR LT T/E TIP WITH CRACK DUE ACCIDENTAL CONTACT AGAINST CRADLE.
- [SDR 07FDEA05046](https://openairdocs.org/sdr/07FDEA05046.md): None · none · Dec 13, 2007 · N369FE · Doug MD1010F · Standard Practices/Structures
  > MAIN CABIN L4 PASSENGER DOOR UPPER INTERNAL JAMB EXISTING DOUBLER. ACCOMPLISHED EA NR 8-5310-115295A.
- [SDR 07FDEA04985](https://openairdocs.org/sdr/07FDEA04985.md): Longeron · corroded · Dec 3, 2007 · N369FE · Doug DC1010F · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPT BILGE AREA FOUND CORROSION WITH EXFOLIATION ON LONGERON, REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 5.
- [SDR 07FDEA04982](https://openairdocs.org/sdr/07FDEA04982.md): Longeron · corroded · Dec 3, 2007 · N369FE · Doug DC1010F · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPT BILGE AREA FOUND SEVERE CORROSION ON LONGERON. REPAIRED AREA IAW SRM 53-30-00 FIG 10 VOL I.
- [SDR 07FDEA04981](https://openairdocs.org/sdr/07FDEA04981.md): Longeron · corroded · Dec 3, 2007 · N369FE · Doug DC1010F · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPT SUMP AREA FOUND CORROSION WITH EXFOLIATION, SEE NRC N00315, N00316, N00294, N00253. REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 5 SHEET 1.
- [SDR 07FDEA04977](https://openairdocs.org/sdr/07FDEA04977.md): Beam · cracked · Dec 3, 2007 · N369FE · Doug DC1010F · Fuselage Main, Structure
  > FWD CARGO COMPT BILGE AREA FOUND CRACK ON BEAM. REPAIRED BEAM IAW SRM 53-60-01 VOL I FIG 3.
- [SDR 07FDEA04902](https://openairdocs.org/sdr/07FDEA04902.md): Frame · cracked · Nov 23, 2007 · N369FE · Doug DC1010F · Fuselage Main, Frame
  > INT CAC CRACK ON FRAME. PERFORMED FRAME REPAIR IAW SRM 53-30-00 VOL I FIG 7.
- [SDR 07FDEA04901](https://openairdocs.org/sdr/07FDEA04901.md): Intercostal · damaged · Nov 23, 2007 · N369FE · Doug DC1010F · Wing Miscellaneous Structure
  > LT WING L/E INTERNAL STRUCTURE ON HORIZONTAL INTERCOSTAL EXISTING ANGLE REPAIR. REPLACED INTERCOSTAL IAW DWG ARB2408 AND ARB1333.
- [SDR 07FDEA04900](https://openairdocs.org/sdr/07FDEA04900.md): Longeron · cracked · Nov 22, 2007 · N369FE · Doug DC1010F · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPT BILGE AREA FOUND CRACK ON LONGERON, SEE NRC N00293, N00294, N00295, N00297. REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 1-2.
- [SDR 07FDEA04856](https://openairdocs.org/sdr/07FDEA04856.md): Skin Panel · cracked · Nov 19, 2007 · N369FE · Doug DC1010F · Horizontal Stabilizer, Plate/Skin
  > DURING STB INSP FOUND PANEL P/N 7206-1 AND P/N 7207-1 OF CONSTANT SECTION SKIN PANEL PLANKS, SEE ATTACHED SHEET FOR BEST DETAIL. CRACK IS IN FLYABLE LIMITS. ACCOMPLISHED EA NR 8-5510-99384.
- [SDR 07FDEA04716](https://openairdocs.org/sdr/07FDEA04716.md): Door Frame · cracked · Nov 2, 2007 · N369FE · Doug DC1030F · Fuselage Main, Structure
  > MAIN CABIN R1 DOOR FWD JAMB DURING PERFORM OAN J/C SP10240272-7001-2J FOUND CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-00-01 VOL I FIG 8.
- [SDR FDEA200710174625](https://openairdocs.org/sdr/FDEA200710174625.md): Sill · corroded · Oct 17, 2007 · N369FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT FOUND CORROSION WITH EXFOLIATION ON FITTING SILL DOOR INSIDE JAMB FWD. REPAIRED AREA IAW SRM 53-50-00 FIG 1 VOL I.
- [SDR 07FDEA04628](https://openairdocs.org/sdr/07FDEA04628.md): Longeron · cracked · Oct 17, 2007 · N369FE · Doug DC1010F · Fuselage Main, Longeron/Stringer
  > CTR CARGO COMPT CRACK ON LONGERON. REPAIRED LONGERON IAW SRM 53-10-00 FIG 1-2 VOL I.
- [SDR 07FDEA04627](https://openairdocs.org/sdr/07FDEA04627.md): Longeron · cracked · Oct 17, 2007 · N369FE · Doug DC1010F · Fuselage Main, Longeron/Stringer
  > CTR CARGO COMPT CRACK ON LONGERON. REPAIRED LONGERON IAW SRM 53-10-00 FIG 1-2 VOL I.
- [SDR 07FDEA04625](https://openairdocs.org/sdr/07FDEA04625.md): Sill · corroded · Oct 17, 2007 · N369FE · Doug DC1010F · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT FOUND CORROSION WITH EXFOLIATION ON FITTING SILL DOOR INSIDE JAMB FWD.
- [SDR 07FDEA04550](https://openairdocs.org/sdr/07FDEA04550.md): Seat Track · corroded · Oct 10, 2007 · N369FE · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > ENTRY WAY, DURING REMOVAL FLOOR PANELS WITH OAN J/C MD10-0600C220-1JR FOUND SEVERE EXFOLIATION CORROSION INTERNAL SEAT TRACK. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL I.
- [SDR 07FDEA04417](https://openairdocs.org/sdr/07FDEA04417.md): Doubler · damaged · Oct 1, 2007 · N369FE · Doug DC1010F · Leading Edge Devices
  > RT WING NR 1 SLAT EXTERNAL SKIN EXISTING DOUBLER. REPAIRED AREA IAW SRM 57-10-00 FIG 84 VOL I.
- [SDR 07FDEA04169](https://openairdocs.org/sdr/07FDEA04169.md): Skin · corroded · Sep 21, 2007 · N369FE · Doug DC1010F · Wing, Plate/Skin
  > LT WING INBD AILERON CORROSION BOTTOM UPPER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 86 VOL I.
- [SDR 07FDEA04167](https://openairdocs.org/sdr/07FDEA04167.md): Web · corroded · Sep 21, 2007 · N369FE · Doug DC1010F · Fuselage Miscellaneous Structure
  > PERFORMED INSPECTION AFTER REMOVAL FLOOR PANEL IN COCKPIT WITH OAN J/C SP10530208-2JR, FOUND SEVERE CORROSION WITH EXFOLIATION ON MEMBRANE AND CRACK 2" LONG. REPAIRED WEB IAW SRM 53-00-01 VOL I FIG 10.
- [SDR 07FDEA04165](https://openairdocs.org/sdr/07FDEA04165.md): Floor Panel · cracked · Sep 21, 2007 · N369FE · Doug DC1010F · Fuselage Floor Panel
  > PERFORMED INSPECTION AFTER REMOVAL FLOOR PANEL IN COCKPIT WITH OAN JC SP10530208-2JR, FOUND CRACK ON MEMBRANE. REPAIRED WEB IAW SRM 53-00-01 VOL I FIG 10.
- [SDR 07FDEA04008](https://openairdocs.org/sdr/07FDEA04008.md): Web · corroded · Sep 19, 2007 · N369FE · Doug DC1010F · Fuselage Miscellaneous Structure
  > PERFORMED INSPECTION AFTER REMOVAL FLOOR PANEL IN COCKPIT WITH OAN J/C SP10530208-2JR, FOUND MODERATE CORROSION AND CRACK 2" LONG ON MEMBRANE. REPLACED WEB SECTION IAW SRM 53-00-01 VOL I FIG 10.
- [SDR 07FDEA03818](https://openairdocs.org/sdr/07FDEA03818.md): Structure · cracked · Sep 17, 2007 · N369FE · Doug DC1010F · Fuselage Main, Structure
  > FWD CARGO COMPT BILGE AREA HAS CRACK ON CAP TEE OF BULKHEAD. REPAIRED AREA IAW EA 8-5310-99388.
- [SDR 07FDEA03590](https://openairdocs.org/sdr/07FDEA03590.md): Skin · cracked · Sep 12, 2007 · N369FE · Doug DC1010F · Nacelle/Pylon, Plate/Skin
  > PYLON NR 1 EXT SKIN FOUND CRACK ON SKIN UPPER SIDE RT. 10-25-07 REPAIRED PYLON SKIN IAW SRM 51-00-01 VOL I FIG 100 & SRM 54-00-01 VOL I FIG 2B.
- [SDR 07FDEA03369](https://openairdocs.org/sdr/07FDEA03369.md): Floor Panel · corroded · Sep 5, 2007 · N369FE · Doug DC1010F · Fuselage Floor Panel
  > PERFORMED INSPECTION AFTER REMOVAL FLOOR PANEL IN COCKPIT WITH OAN J/C SP10530208-2JR, FOUND SEVERE CORROSION WITH EXFOLIATION (OUT OF LIMIT) ON MEMBRANE AND CRACK. REPLACED WEB SECTION IAW SRM 53-00-01 FIG 10 VOL I.
- [SDR 07FDEA03336](https://openairdocs.org/sdr/07FDEA03336.md): Rib · cracked · Sep 4, 2007 · N369FE · Doug DC1010F · Wing, Rib/Bulkhead
  > RT WING TIP CRACKS, 1.5" LONG ON EXTERNAL SKIN XW 928, YW 799. CONTINUED CRACK ON INT OLD REPAIR ON FRAME XW 928, YW 799. REPAIRED AREA IAW SRM 57-00-01 FIG 10 VOL I.
- [SDR 07FDEA03335](https://openairdocs.org/sdr/07FDEA03335.md): Bulkhead · cracked · Sep 4, 2007 · N369FE · Doug DC1010F · Fuselage Main, Bulkhead
  > NLG W/W FOUND CRACK ON LT VERTICAL BULKHEAD. REPAIRED WEB IAW SRM 53-40-00 FIG 34 VOL I.
- [SDR 07FDEA03319](https://openairdocs.org/sdr/07FDEA03319.md): Skin · damaged · Sep 3, 2007 · N369FE · Doug DC1010F · Fuselage Main, Plate/Skin
  > R1 PASSENGERS DOOR DEFORMATION OLD REPAIR ON UPPER FWD CORNER EXTERNAL SKIN. REPAIRED AREA IAW SRM 52-10-00 FIG 12A VOL I.
- [SDR 07FDEA03318](https://openairdocs.org/sdr/07FDEA03318.md): Pan · cracked · Sep 3, 2007 · N369FE · Doug DC1010F · Fuselage Miscellaneous Structure
  > LOWER CENTER CARGO DOOR CRACK LONG.250" AND DEFORMATION ON LWR FORWARD CORNER. 11-07-07 REPAIRED AREA IAW SRM 52-10-00 FIG 17 VOL I.
- [SDR 07FDEA03217](https://openairdocs.org/sdr/07FDEA03217.md): Longeron · corroded · Aug 29, 2007 · N369FE · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPT BILGE AREA FOUND SEVERE CORROSION ON LONGERON. REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 1& 2.
- [SDR 07FDEA03216](https://openairdocs.org/sdr/07FDEA03216.md): Bulkhead · cracked · Aug 29, 2007 · N369FE · Doug DC1010F · Fuselage Main, Bulkhead
  > RT W/W CRACK 0.5" LONG ON VERTICAL BULKHEAD. REPAIRED BULKHEAD IAW SRM 53-00-01 VOL I FIG 10.
- [SDR 07FDEA03215](https://openairdocs.org/sdr/07FDEA03215.md): Bulkhead · cracked · Aug 29, 2007 · N369FE · Doug DC1010F · Fuselage Main, Bulkhead
  > CTR W/W SPACE CRACK ON VERTICAL BULKHEAD. PERFORMED REPAIR IAW SRM 53-00-01 VOL I FIG 4.
- [SDR 07FDEA03146](https://openairdocs.org/sdr/07FDEA03146.md): Intercostal · cracked · Aug 27, 2007 · N369FE · Doug DC1010F · Wing Miscellaneous Structure
  > LT WING L/E CRACK ON INTERNAL INTERCOSTAL. REPAIRED INTERCOSTAL IAW SRM 57-00-01 VOL I FIG 10.
- [SDR 07FDEA03145](https://openairdocs.org/sdr/07FDEA03145.md): Intercostal · cracked · Aug 27, 2007 · N369FE · Doug DC1010F · Wing Miscellaneous Structure
  > LT WING L/E INTERNAL CRACK LONG 0.50" ON INTERCOSTAL. 10-10-07 REPAIRED INTERCOSTAL IAW SRM 57-00-01 VOL I FIG 10.
- [SDR 07FDEA03143](https://openairdocs.org/sdr/07FDEA03143.md): Rib · cracked · Aug 27, 2007 · N369FE · Doug DC1010F · Wing, Rib/Bulkhead
  > LT WING INTERNAL L/E ON UPPER RIB FOUND CRACK 0.70" LONG. REPAIRED RIB IAW SRM 57-20-00 FIG 1 VOL I.
- [SDR 07FDEA03088](https://openairdocs.org/sdr/07FDEA03088.md): Bulkhead · cracked · Aug 24, 2007 · N369FE · Doug DC1010 · Fuselage Main, Bulkhead
  > CTR W/W SPACE: CRACKS ON VERTICAL BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 10 SHT 4 VOL I.
- [SDR 07FDEA03086](https://openairdocs.org/sdr/07FDEA03086.md): Skin · corroded · Aug 24, 2007 · N369FE · Doug DC1010F · Wing, Plate/Skin
  > LT WING OUTBOARD FLAP CORROSION UNDER UPPER SKIN. 10-11-07 REPAIRED AREA IAW SRM 57-10-00 VOL I FIG 85.
- [SDR FDEA200708223046](https://openairdocs.org/sdr/FDEA200708223046.md): Skin · cracked · Aug 22, 2007 · N369FE · Doug MD1010F · Wing, Plate/Skin
  > LT WING L/E CRACK ON EXTERNAL LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 VOL I.
- [SDR FDEA200708223034](https://openairdocs.org/sdr/FDEA200708223034.md): Skin · cracked · Aug 22, 2007 · N369FE · Doug MD1010F · Wing, Plate/Skin
  > L/E RT WING CRACK ON EXTERNAL SKIN L/E. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.
- [SDR 07FDEA03049](https://openairdocs.org/sdr/07FDEA03049.md): Skin · dented · Aug 22, 2007 · N369FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > EXT SURFACE RT SIDE FOUND DENT 2" BY 1" DEEP 0.062" ON SKIN. 09-19-07 REPAIRED SKIN IAW SRM 53-20-00 FIG 13 SHT 3-5 VOL I.
- [SDR 07FDEA03048](https://openairdocs.org/sdr/07FDEA03048.md): Skin · dented · Aug 22, 2007 · N369FE · Doug DC1010F · Fuselage Main, Plate/Skin
  > EXT FUSELAGE RT SIDE FOUND DENT.45" BY.25" DEEP 0.027" ON SKIN. 09-19-07 REPAIRED SKIN IAW SRM 53-20-00 FIG 13 SHT 3-5 VOL I.
- [SDR 07FDEA03047](https://openairdocs.org/sdr/07FDEA03047.md): Skin · cracked · Aug 22, 2007 · N369FE · Doug DC1010F · Wing, Plate/Skin
  > LT WING LWR SURFACE FOUND CRACK ON SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.
- [SDR 07FDEA03046](https://openairdocs.org/sdr/07FDEA03046.md): Skin · cracked · Aug 22, 2007 · N369FE · Doug DC1010F · Wing, Plate/Skin
  > LT WING L/E CRACK ON EXTERNAL LOWER SKIN.
- [SDR 07FDEA03034](https://openairdocs.org/sdr/07FDEA03034.md): Skin · cracked · Aug 22, 2007 · N369FE · Doug DC1010 · Wing, Plate/Skin
  > L/E RT WING CRACK ON EXTERNAL SKIN L/E.
- [SDR 07FDEA03033](https://openairdocs.org/sdr/07FDEA03033.md): Scoop · cracked · Aug 22, 2007 · N369FE · Doug DC1010 · Fuselage Main, Structure
  > INT CAC CRACK ON SUGAR SCOOP. REPAIR AREA IAW SRM 53-40-00 VOL I FIG 8.
- [SDR 06FDEA00043](https://openairdocs.org/sdr/06FDEA00043.md): Sensor · malfunctioned · Jan 5, 2006 · N369FE · Doug DC1010 · Stall Warning System
  > PDIS: ON ROTATION FOR TAKEOFF BOTH STICK SHAKERS ACTIVATED AND REMAINED ON WITH NORMAL AIRCRAFT INDICATIONS, NORMAL FEEL, AIRSPEED INDICATORS ALL THE SAME & NORMAL. FLAPS RETRACTED NORMALLY. SLATS LEFT EXTENDED. CAPTAIN AND F/O STICK SHAKER CB'S PULLED. RE

Next page: https://openairdocs.org/aircraft/N369FE/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 = 'N369FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N369FE/reports

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