# Service difficulty reports: N371FE, cancelled Jan 29, 2024

A list on [N371FE, cancelled Jan 29, 2024](https://openairdocs.org/deregistered/N371FE-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 · 76 reports

- [SDR FDEA201503201032](https://openairdocs.org/sdr/FDEA201503201032.md): Door · stuck · Mar 20, 2015 · N371FE · Doug MD1010F · Passenger/Crew Doors
  > R1 DOOR WILL NOT OPEN. RELEASED FOR SERVICE IAW MEL 52-10-03 CATEGORY C. TROUBLESHOOTING REQUIRED FOR REPAIR.
- [SDR FDEA201503060699](https://openairdocs.org/sdr/FDEA201503060699.md): Mechanism · lack of lube · Mar 6, 2015 · N371FE · Doug MD1010F · Passenger/Crew Doors
  > RECEIVED A CABIN DOOR FWD RT, DURING FLIGHT HANDLE IS NOT UP, FLUSH LIKE ON LT SIDE BUT WON'T GO UP ANYMORE. WHILE TROUBLESHOOTING WRI 52-10-6839 FOUND R1 DOOR UNABLE TO OPEN OR CLOSE ELECTRICALLY ALL CIRCUIT BREAKERS ARE CLOSED. LUBRICATED RT DOOR ARMING
- [SDR FDEA201408292353](https://openairdocs.org/sdr/FDEA201408292353.md): Light · wrong part · Aug 29, 2014 · N371FE · Doug MD1010F · Emergency Equipment
  > EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INDICATING SYS IS INOPERATIVE. RELEASED FOR SERVICE IAW MEL. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY. T/S AND FOUND L1 SLIDE REMOTE
- [SDR FDEA201403200538](https://openairdocs.org/sdr/FDEA201403200538.md): Wire Harness · damaged · Mar 20, 2014 · N371FE · Doug MD1010F · Engine Indicating System Wiring
  > RTO AT 110KTS FOR, ENG 3 EXCEEDANCE, LVL 1 ALERT. NR 3 EGT SHOWED YELLOW, 1011, FOR EXCEEDANCE, ESTIMATE EXCEEDANCE WAS MOMENTARY. PULLED UP VIA NR 3 ENG EXCEEDANCES. THE ACARS EXCEEDENCE SHOWS IT WAS AN EGT INDICATION PROBLEM. R & R NR 3 ENG TOP LT EGT TH
- [SDR FDEA201403020430](https://openairdocs.org/sdr/FDEA201403020430.md): Push-Pull Cable · malfunctioned · Mar 2, 2014 · N371FE · Doug MD1010F · Power Lever
  > ON TOP OF DESCENT NR 2 THROTTLE FROZE AT 92% N1 FROM FL 370 TO 10,000 FT NO MOVEMENT, SHUTDOWN ENG. CREW REPORTED THAT AFTER ARRIVAL AT GATE & SHUTDOWN NR 2 THROTTLE OPERATED NORMALLY. R & R NR 2 ENG THROTTLE PUSH PULL CABLE. RIG & OPERATIONS CHECKED OK IAW
- [SDR FDEA201311052693](https://openairdocs.org/sdr/FDEA201311052693.md): Doubler · cracked · Nov 5, 2013 · N371FE · Doug MD1010F · Fuselage Main, Bulkhead
  > CENTER WHEEL WELL DOUBLER HAS AN APPROXIMATLEY 5 INCH VERTICAL CRACK AT BS 1381. REMOVED AND REPLACED DOUBLER IAW SRM 51-31-01, RIGGED GOOD IAW AMM 27-60-00-05.
- [SDR FDEA201304241003](https://openairdocs.org/sdr/FDEA201304241003.md): Doubler · cracked · Apr 24, 2013 · N371FE · Doug MD1010F · Fuselage Main, Structure
  > WHEN REMOVING EXISTING REPAIR DOUBLER, FOUND ADDITIONAL CRACK IN AEA0161-11 DOUBLER. BS 1391 APPROX 4" DOWN FROM TOP. REPAIRED IAW EA 8-5310-157389, PART 1.
- [SDR FDEA201304241000](https://openairdocs.org/sdr/FDEA201304241000.md): Bulkhead · cracked · Apr 24, 2013 · N371FE · Doug MD1010F · Fuselage Main, Bulkhead
  > LEFT BULKHEAD CRACKED 16 INCHES AFT OF FWD BULKHEAD AND 4 INCHES DOWN FROM UPPER BULKHEAD. CRACK END MARKED USING HFEC. REPAIRED IAW EA 8-5310-157389, PART 1.
- [SDR FDEA201208293198](https://openairdocs.org/sdr/FDEA201208293198.md): Proximity Sensor · out of adjust · Aug 29, 2012 · N371FE · Doug MD1010F · Landing Gear Position and Warning
  > ON GEAR RETRACTION RECEIVED A RED LT MAIN GEAR LIGHT ON THE PRIMARY AND SECONDARY INDICATORS. PERFORMED QHR PROCEDURES AND HAD SAME INDICATIONS. DUMPED FUEL TO MAX LANDING WT AND RETURNED TO DEPARTURE. R & R LT MLG CRANK SENSOR SUPPORT FOR THE UP AND LA
- [SDR FDEA201206012043](https://openairdocs.org/sdr/FDEA201206012043.md): Fire Warning · illuminated · Jun 1, 2012 · N371FE · Doug MD1010F · Fire Detection
  > A LEVEL 3 CARGO FIRE LOWER FWD ILLUMINATED. PUSHED FLASHING DISCHARGE SWITCH, LANDED & ROLLED OUT TO FULL STOP. FIRE DEPTARTMENT REPORTED SLIGHT HEAT SIGNATURE ON LOWER FORWARD BELLY. ALL CHECKLIST COMPLETED.
- [SDR FDEA201111134891](https://openairdocs.org/sdr/FDEA201111134891.md): Door Frame · corroded · Nov 13, 2011 · N371FE · Doug MD1010F · Fuselage Main, Structure
  > AFT CARGO DOOR LWR FWD FRAME CORRODED. REMOVED CORROSION FROM AFT CARGO DOOR LWR FWD INTERIOR JAMB REF SRM53-50-00, VOL 1 FIG 15 AND ER 11-04534. REPAIRED IAW REF EA3 8-5310-153320 AND SR10530057 AND EA 8-5350-156806.
- [SDR FDEA201111034740](https://openairdocs.org/sdr/FDEA201111034740.md): Fitting · cracked · Nov 3, 2011 · N371FE · Doug MD1010F · Cargo/Baggage Doors
  > MAIN CARGO DOOR NR6 LATCH SPOOL LOWER FITTING CRACKED FROM INBD FWD SPOOL MOUNT BOLT HOLE. R & R SPOOL FITTING NR 6 REF SRM 51-33-01, VOL II.
- [SDR FDEA201107212886](https://openairdocs.org/sdr/FDEA201107212886.md): Pitot Line · damaged · Jul 21, 2011 · N371FE · Doug MD1010F · Pitot/Static System
  > ON TAKEOFF AIRSPEED STAGNATED THEN BECAME ERRATIC. COMPLIED WITH QRH. RETURNED TO KIND. R & R 3EA PITOT TUBES IAW MM 34-11-02-2. OPS CHECK REQ'D. PERFORMED A LOW RANGE LEAK TEST ON PITOT AND STATIC SYS. ALL TESTS NORMAL. NO LEAKS IN SYS OR LEAK DOWN. AL
- [SDR FDEA201107212885](https://openairdocs.org/sdr/FDEA201107212885.md): Pitot Line · damaged · Jul 21, 2011 · N371FE · Doug MD1010F · Pitot/Static System
  > ON TAKEOFF, AIRSPEED STAGNATED THEN BECAME ERRATIC. COMPLIED WITH QRH. RETURNED TO FIELD. R & R 3 PITOT TUBES IAW MM 34-11-02-2. PERFORMED A LOW RANGE LEAK TEST ON PITOT AND STATIC SYS. ALL TESTS NORMAL. NO LEAKS IN SYS OR LEAK DOWN. ALL PITOT LINES
- [SDR FDEA201003100734](https://openairdocs.org/sdr/FDEA201003100734.md): Relief Valve · failed · Mar 10, 2010 · N371FE · Doug MD1010F · Fuel Indicating System
  > FUEL SYS AUTO, ON LONG APP WITH MEL 28-22-01-04A. ALL PUMPS WERE ON THAT WERE NOT DEFFERRED. FUEL QTY TANK NR 2 STARTED A SLOW INCREASE AS FUEL QTY TANK NR1 DROPPED FASTER THAN IT SHOULD ON 8 ML FINAL, GOT WARNING OF TANK IMBALANCE AND POSSIBLE FUEL LEAK. O
- [SDR FDEA200712115024](https://openairdocs.org/sdr/FDEA200712115024.md): Frame · cracked · Dec 11, 2007 · N371FE · Doug MD1010F · Fuselage Main, Frame
  > MAIN CABIN FOUND 1 CRACK ON FRAME STA 1741, STR 14, RT. REPAIRED AREA IAW SRM 53-30-00 FIG 5 VOL I AND EA NR 8-5310-111521, 8-5330-111563.
- [SDR 07FDEA05024](https://openairdocs.org/sdr/07FDEA05024.md): Frame · cracked · Dec 11, 2007 · N371FE · Doug DC1010 · Fuselage Main, Frame
  > MAIN CABIN FOUND 1 CRACK ON FRAME STA 1741 STR 14 RT REPAIRED IAW SRM 53-30-00 FIG 5 VOL I AND EA NR 8-5380-111563.
- [SDR 07FDEA04984](https://openairdocs.org/sdr/07FDEA04984.md): Lug · cracked · Dec 3, 2007 · N371FE · Doug DC1010 · Wing, Attach Fittings
  > FOUND LOWER CHORD LUG CRACKED. REPAIRED AREA IAW SRM 57-20-00 FIG 27 SHT 2 VOL I.
- [SDR 07FDEA04983](https://openairdocs.org/sdr/07FDEA04983.md): Stringer · cracked · Dec 3, 2007 · N371FE · Doug DC1010 · Wing, Longeron/Stringer
  > FOUND LOWER CHORD LUGS CRACKED. REPAIRED AREA IAW SRM 57-20-00 FIG 27 SHT 2 VOL I.
- [SDR 07FDEA04965](https://openairdocs.org/sdr/07FDEA04965.md): Angle · cracked · Nov 29, 2007 · N371FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > LOWER FWD COMPT CRACK ON TEE ANGLE. REPAIRED TEE CAP IAW EA NR 8-5310-111463.
- [SDR 07FDEA04964](https://openairdocs.org/sdr/07FDEA04964.md): Lug · cracked · Nov 29, 2007 · N371FE · Doug DC1010 · Wing Miscellaneous Structure
  > FOUND LOWER CHORD LUG CRACKED. REPAIRED AREA IAW EA NR 8-5710-111524A.
- [SDR 07FDEA04963](https://openairdocs.org/sdr/07FDEA04963.md): Lug · cracked · Nov 29, 2007 · N371FE · Doug DC1010 · Wing Miscellaneous Structure
  > AT ACCESS 634 AT FOUND LOWER CHORD LUG CRACKED. REPAIRED AREA IAW EA NR 8-5710-111525A.
- [SDR 07FDEA04962](https://openairdocs.org/sdr/07FDEA04962.md): Skin · cracked · Nov 29, 2007 · N371FE · Doug DC1010 · Wing, Plate/Skin
  > RT WING DROOPED FOUND CRACK ON UPPER EXTERNAL SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 55 VOL I.
- [SDR FDEA200711204866](https://openairdocs.org/sdr/FDEA200711204866.md): Seat Track · cracked · Nov 20, 2007 · N371FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > DURING PERFORMING OK TO CLOSE FLOOR PANELS WITH J/C MD10-53210290-1J FOUND SEAT TRACK CRACK ON MAIN CABIN. REPAIRED AREA IAW SRM 53-70-00 FIG 1 VOL I.
- [SDR 07FDEA04868](https://openairdocs.org/sdr/07FDEA04868.md): Seat Track · cracked · Nov 20, 2007 · N371FE · Doug DC1010 · Fuselage, Seat/Cargo Attach Fittings
  > ENTRY WAY ZONE AFTER REMOVAL FLOOR PANEL WITH OAN J/C MD10-600C220-1JR FOUND CRACK ON SEAT TRACK LUG LT SIDE. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 SHT 1 AND 3 VOL I.
- [SDR 07FDEA04867](https://openairdocs.org/sdr/07FDEA04867.md): Channel · corroded · Nov 20, 2007 · N371FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > CTR CARGO COMPT SEVERE CORROSION WITH EXFOLIATION ON CHANNEL. REPAIRED CHANNEL IAW SRM 53-70-00 VOL I FIG 5 SHT 5.
- [SDR 07FDEA04866](https://openairdocs.org/sdr/07FDEA04866.md): Seat Track · cracked · Nov 20, 2007 · N371FE · Doug DC1010 · Fuselage, Seat/Cargo Attach Fittings
  > DURING PERFORMING OK TO CLOSE FLOOR PANELS WITH J/C MD10-53210290-1J FOUND SEAT TRACK CRACK ON MAIN CABIN.
- [SDR 07FDEA04862](https://openairdocs.org/sdr/07FDEA04862.md): Stringer · cracked · Nov 19, 2007 · N371FE · Doug DC1010 · Wing, Longeron/Stringer
  > AT ACCESS 534 AT FOUND CRACK, ACCOMPLISHED EA NR 8-5710-111526.
- [SDR 07FDEA04861](https://openairdocs.org/sdr/07FDEA04861.md): Skin · cracked · Nov 19, 2007 · N371FE · Doug DC1010 · Horizontal Stabilizer, Plate/Skin
  > DURING U/S INSP OF HORIZ STB, FOUND TWO PANEL WITH CRACK IN FLYABLE LIMITS. ACCOMPLISHED EA NR 8-5510-111533.
- [SDR 07FDEA04859](https://openairdocs.org/sdr/07FDEA04859.md): Skin · loose · Nov 19, 2007 · N371FE · Doug DC1010F · Trailing Edge Flaps
  > LT WING I/B FLAP UPPER SKIN EXISTING REPAIR. REPAIRED SKIN IAW SRM 57-10-00 FIG 86 VOL I.
- [SDR 07FDEA04858](https://openairdocs.org/sdr/07FDEA04858.md): Bulkhead · cracked · Nov 19, 2007 · N371FE · Doug DC1010 · Fuselage Main, Bulkhead
  > CLG WW CENTER CRACKS ON VERTICAL RT BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 10 VOL I.
- [SDR 07FDEA04853](https://openairdocs.org/sdr/07FDEA04853.md): Skin · cracked · Nov 19, 2007 · N371FE · Doug DC1010 · Wing, Plate/Skin
  > LT WING DROOPED FOUND CRACK AND DEEP WEAR ON EXT SKIN OUTBOARD SIDE DROOPED. REPAIRED SKIN IAW SRM 57-10-00 VOL I FIG 15 SHT 1.
- [SDR 07FDEA04851](https://openairdocs.org/sdr/07FDEA04851.md): Skin · worn · Nov 19, 2007 · N371FE · Doug DC1010 · Wing, Plate/Skin
  > RT WING DROOPED FOUND DEEP WEAR ON LWR EXTERNAL SKIN. REPAIRED SKIN IAW SRM 57-10-00 VOL I FIG 39.
- [SDR 07FDEA04753](https://openairdocs.org/sdr/07FDEA04753.md): Stringer · cracked · Nov 8, 2007 · N371FE · Doug DC1010 · Wing, Longeron/Stringer
  > FOUND 2" CRACK ON RT WING STRINGER NR 40 AT XORS 346. REPAIR PER SRM 57-20-00 VOL 1 FIG 36 CONF.
- [SDR FDEA200710244668](https://openairdocs.org/sdr/FDEA200710244668.md): Hinge · damaged · Oct 24, 2007 · N371FE · Doug DC1010 · Horizontal Stabilizer Structure
  > HINGE ASSY ITEM 360 BROKEN, REF IPC 55-22-02-01. REPLACE HINGE IAW STD REWORK DWG SR10-55-501.
- [SDR FDEA200710244665](https://openairdocs.org/sdr/FDEA200710244665.md): Seat Track · cracked · Oct 24, 2007 · N371FE · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > FOUND 1 CRACK 4 INCH ON SEAT TRACK AT STA 635 X= 67 CUT APPROX AT STA 666 AND 624 AND REPAIR IAW SRM 53-70-00 VOL 1 FIG 1 AND FIG 11.
- [SDR 07FDEA04669](https://openairdocs.org/sdr/07FDEA04669.md): Skin · damaged · Oct 24, 2007 · N371FE · Doug DC1010 · Wing, Plate/Skin
  > LT WING L/E SKIN LOWER SLAT TRACK CUT OUT NR 8 AT STA XOS 549 EXISTING REPAIR. REPLACED REPAIR PER SRM 57-10-00 VOL.1 FIG 68.
- [SDR 07FDEA04668](https://openairdocs.org/sdr/07FDEA04668.md): Hinge · damaged · Oct 24, 2007 · N371FE · Doug DC1010 · Horizontal Stabilizer Structure
  > HINGE ASSY ITEM 360 BROKEN (REF IPC 55-22-02-01). REPLACED LATCH IAW FEDEX STD REWORK DWG SR10-55-501.
- [SDR 07FDEA04667](https://openairdocs.org/sdr/07FDEA04667.md): Angle · corroded · Oct 24, 2007 · N371FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > CTR CARGO COMPT EXFOLIATION CORROSION ON CAP ANGLE AT STA 1541 L NR 52 REPAIR CAP IAW SRM 53-30-00 VOL 1 FIG 8 SHEET 1.
- [SDR 07FDEA04666](https://openairdocs.org/sdr/07FDEA04666.md): Angle · corroded · Oct 24, 2007 · N371FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > EXFOLIATION CORROSION ON CAP ANGLE AT STA 1561 L NR 52 REPAIR IAW SRM 53-30-00 VOL 1 FIG 8 SHEET 1.
- [SDR 07FDEA04665](https://openairdocs.org/sdr/07FDEA04665.md): Seat Track · cracked · Oct 24, 2007 · N371FE · Doug DC1010 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND 1 CRACK 4" ON SEAT TRACK AT STA 635 X= 67 CUT APPROX AT STA 666 AND 624 AND REPAIR IAW SRM 53-70-00 VOL 1 FIG 1 AND FIG 11.
- [SDR 07FDEA04664](https://openairdocs.org/sdr/07FDEA04664.md): Stringer · cracked · Oct 24, 2007 · N371FE · Doug DC1010 · Wing, Longeron/Stringer
  > RT WING L/E INTERNAL STRUCTURE FOUND 1 CRACK 0,75" LONG ON FIXED TEE AT XOS 906 REPAIR WING LOWER L/E STRINGER DOUBLER IAW SRM 57-10-00 FIG 49 VOL 1.
- [SDR 07FDEA04423](https://openairdocs.org/sdr/07FDEA04423.md): Angle · cracked · Oct 1, 2007 · N371FE · Doug DC1010 · Cargo/Baggage Doors
  > LOWER CTR CARGO DOOR CRACK ON FWD LWR CORNER. REPAIRED AREA IAW SRM 52-10-00 FIG 17 VOL I.
- [SDR 07FDEA04340](https://openairdocs.org/sdr/07FDEA04340.md): Rib · cracked · Sep 27, 2007 · N371FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.
- [SDR 07FDEA04339](https://openairdocs.org/sdr/07FDEA04339.md): Rib · cracked · Sep 27, 2007 · N371FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.
- [SDR 07FDEA04338](https://openairdocs.org/sdr/07FDEA04338.md): Rib · cracked · Sep 27, 2007 · N371FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.
- [SDR 07FDEA04337](https://openairdocs.org/sdr/07FDEA04337.md): Rib · cracked · Sep 27, 2007 · N371FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.
- [SDR 07FDEA03821](https://openairdocs.org/sdr/07FDEA03821.md): Membrane · corroded · Sep 17, 2007 · N371FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > COCKPIT INT AFTER REMOVAL FLOOR PANEL WITH OAN J/C MD10-0600C210-1JR FOUND SEVERE CORROSION ON 2 HORIZ MEMBRANE: FROM STA 303 TO STA 330 FROM X= 7.50 TO X=17 LT SIDE; FROM STA 303 TO STA 330 FROM X= 27 TO X= 60 LT SIDE. THE FIRST CASE REPLACED MEMBRANE IAW
- [SDR 07FDEA03820](https://openairdocs.org/sdr/07FDEA03820.md): Frame · cracked · Sep 17, 2007 · N371FE · Doug DC1010 · Fuselage Main, Frame
  > MAIN CABIN STRUCTURE HAS CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-30-00 FIG 5 VOL I.
- [SDR 07FDEA03816](https://openairdocs.org/sdr/07FDEA03816.md): Rib · cracked · Sep 17, 2007 · N371FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING L/E INT STRUCTURE FOUND CRACK ON RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.

Next page: https://openairdocs.org/deregistered/N371FE-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 = 'N371FE' AND deregistration_id = 'N371FE-2024-01-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N371FE-2024-01-29/reports

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