# Service difficulty reports: N365FE, cancelled Jan 29, 2024

A list on [N365FE, cancelled Jan 29, 2024](https://openairdocs.org/deregistered/N365FE-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 6 · 267 reports

- [SDR FDEA201901130127](https://openairdocs.org/sdr/FDEA201901130127.md): Girt Bar · loose · Jan 13, 2019 · N365FE · Doug MD1010F · Emergency Equipment
  > GIRT BAR DOOR 1L HAS COME LOOSE RESECURED L-1 DOOR GIRT BAR. OK FOR SERVICE.
- [SDR FDEA201812163525](https://openairdocs.org/sdr/FDEA201812163525.md): Slide · failed · Dec 16, 2018 · N365FE · Doug MD1010F · Escape Slide
  > L1 DOOR SLIDE LIGHT FOUND ON DURING PREFLIGHT. RELEASED FOR SERVICE PER MEL 52-10-03. PERFORMED RESISTANCE CHECK PER MEL 25-61-01 OF DOOR SLIDE ELECTRICAL JACK. RESISTANCE READ APPROX.5 OHMS. R&R L1 DOOR SLIDE ASSY REF MM 25-61-01-2.
- [SDR FDEA201812153505](https://openairdocs.org/sdr/FDEA201812153505.md): Switch · malfunctioned · Dec 15, 2018 · N365FE · Doug MD1010F · Passenger/Crew Doors
  > ON PREFLIGHT L1 DOOR SLIDE CIRCUITRY LIGHT REMAINS ILLUMINATED. WHILE TRYING TO COMPLY WITH MEL 25-61-01 FOR THE "PRESS-TO-TEST" INDICATION, METHOD "A", THE TEST FAILED STEP 1A 4B, DISCONTINUED WITH MEL 25-61-01 PROCEDURES AND RETURNED L1 DOOR BACK TO ITS ORIG
- [SDR FDEA201802220478](https://openairdocs.org/sdr/FDEA201802220478.md): Cable · deformed · Feb 22, 2018 · N365FE · Doug MD1010F · Service Doors
  > R1 DOOR CLUTCH RELEASE CABLE HAS DEFORMATION AND KINKING AT FWD CABLE END. REMOVED AND REPLACED THE R1 DOOR CLUTCH RELEASE CABLE IAW AMM 52-11-12.
- [SDR FDEA201801080037](https://openairdocs.org/sdr/FDEA201801080037.md): Cable · broken · Jan 8, 2018 · N365FE · Doug MD1010F · Passenger/Crew Doors
  > L1 DOOR AFT CABLE IS BROKEN AND WRAPPED AROUND SPOOL. UNABLE TO OPEN OR CLOSE DOOR WITHOUT DAMAGING OTHER COMPONENTS. R & R THE CABLE IAW AMM 52-10-02-2.
- [SDR FDEA201701120139](https://openairdocs.org/sdr/FDEA201701120139.md): Bulkhead Web · cracked · Jan 12, 2017 · N365FE · Doug MD1010F · Fuselage Main, Bulkhead
  > BS 595 BULKHEAD WEB AT LONGERON 41L HAS A.800 IN CRACK AT THE UPPER FASTENERS HOLE COMMON TO THE TEE CAP. INSTALLED REPAIRED PER SRM 53-40-00
- [SDR FDEA201701030077](https://openairdocs.org/sdr/FDEA201701030077.md): Floor Support · corroded · Jan 3, 2017 · N365FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN DECK BS 1881, RBL 27 FLOOR SUPPORT IS CORRODED.. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG WSP0711.
- [SDR FDEA201612294573](https://openairdocs.org/sdr/FDEA201612294573.md): Panel · delaminated · Dec 29, 2016 · N365FE · Doug MD1010F · Nacelle/Pylon, Plate/Skin
  > #2 ENGINE INLET (PICKLE BARREL) PANEL AJC7068 IS DELAMINATED. REPAIRED IAW SRM 51-71-00 VOL 2.
- [SDR FDEA201612214518](https://openairdocs.org/sdr/FDEA201612214518.md): Skin · corroded · Dec 21, 2016 · N365FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > CAC BAY LWR SKIN, BETWEEN STA 1079 TO STA 1099 LONGERON 52 TO LONGERON 51R, HAS CORROSION AND SHEAR RIVET. REPAIRED PER DWG AGA3097 AND SRM 53-20-00.
- [SDR FDEA201612214513](https://openairdocs.org/sdr/FDEA201612214513.md): Fitting · cracked · Dec 21, 2016 · N365FE · Doug MD1010F · Fuselage Main, Structure
  > LEFT BS 1156 SUGAR SCOOP FITTING HAS THREE CRACKS ON HORIZONTAL LEG BETWEEN LONGERONS 38 AND 39L. REMOVED AND REPLACED FITTING IAW DWG. AYB 7000-1.
- [SDR FDEA201612214516](https://openairdocs.org/sdr/FDEA201612214516.md): Shear Tie · corroded · Dec 21, 2016 · N365FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > CAC BAY LOWER SKIN, BETWEEW BS 1079 TO 1099 LONGERON 51TO 52R HAS CORROSION AND SHEAR RIVET. REPLACED CORRODED SHEAR TIE IAW DWG. ADA 0112.
- [SDR FDEA201612214515](https://openairdocs.org/sdr/FDEA201612214515.md): Fitting · cracked · Dec 21, 2016 · N365FE · Doug MD1010F · Fuselage Main, Attach Fittings
  > CAC BAY LT CTR WING TO FUSELAGE HAIRPIN FITTING UPPER AFT FASTENER AREA HAS 0.500 CRACK. REPAIRED IAW SRM 53-30-00 FIG 7 VOL 1.
- [SDR FDEA201612154464](https://openairdocs.org/sdr/FDEA201612154464.md): Bulkhead · cracked · Dec 15, 2016 · N365FE · Doug MD1010F · Fuselage Main, Bulkhead
  > FWD CARGO COMP STA 595 AT LONGERON 36L PRESSURE BULKHEAD SUSPECT CRACK. REPAIRED PER SRM 53-40-00 FIG 4.
- [SDR FDEA201612154463](https://openairdocs.org/sdr/FDEA201612154463.md): Tee Fitting · cracked · Dec 15, 2016 · N365FE · Doug MD1010F · Fuselage Main, Attach Fittings
  > FWD CARGO BAY BS 595, LONGERON 36L CRACKED. REPAIRED PER EA. 8-5310-T0330353.
- [SDR FDEA201612154462](https://openairdocs.org/sdr/FDEA201612154462.md): Tee Fitting · cracked · Dec 15, 2016 · N365FE · Doug MD1010F · Fuselage Main, Bulkhead
  > FWD CARGO BAY PRESSURE BULKHEAD AT BS 595, LWR TEE CAP UPPER TANG CRACKED BETWEEN TWO FASTENERS AND PROPAGATING TO THE EDGE BETWEEN L39L AND L40L. REPAIRED IAW EA. 8-5310-T0330353.
- [SDR FDEA201612154459](https://openairdocs.org/sdr/FDEA201612154459.md): Cap · cracked · Dec 15, 2016 · N365FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > FWD CARGO, COMPARTMENT STA 595 LONGERON 39R SUSPECT CRACK. AFTER EVALUATION, FOUND TEE CAP CRACKED. REPAIRED TEE CAP PER EA 8-5310-T0330385
- [SDR FDEA201612114568](https://openairdocs.org/sdr/FDEA201612114568.md): Skin · cracked · Dec 11, 2016 · N365FE · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING NR 7 SLAT TRACK CUTOUT O/B CORNER CRACKED. REPAIRED IAW SRM 57-10-00, FIG.104 A, VOL. I
- [SDR FDEA201612054326](https://openairdocs.org/sdr/FDEA201612054326.md): Oxygen Mask · unserviceable · Dec 5, 2016 · N365FE · Doug MD1010F · Portable Oxygen System
  > COCKPIT PORTABLE OXYGEN MASK FOUND DRY-ROTTED. REMOVED AND REPLACED COCKPIT PORTABLE OXYGEN MASK IN REF TO AMM 35-30-01-4. ACFT OK FOR SERVICE.
- [SDR FDEA201607152451](https://openairdocs.org/sdr/FDEA201607152451.md): Door · cracked · Jul 15, 2016 · N365FE · Doug MD1010F · Landing Gear Doors
  > ON T/O, HAD UNSAFE, RED LIGHT, GEAR UP. LEFT MAIN CYCLED GEAR. GEAR DOWN, 3 GREEN, CYCLE D UP, UNSAFE LT MAIN, ACFT DIVERTED. REPLACED LT MLG DOOR.
- [SDR FDEA201604181255](https://openairdocs.org/sdr/FDEA201604181255.md): Crank Assy · defective · Apr 18, 2016 · N365FE · Doug MD1010F · Landing Gear Brake System
  > CAPTAIN DURING POST FLIGHT DEBRIEF REPORTED, RT BRAKE PEDAL EXCESSIVE TRAVEL & SLOW TO ACTUATE. R & R CAPTAINS RT BRAKE FEATHERING CRANK IAW EA 8-2720-TO324787.
- [SDR FDEA201511103550](https://openairdocs.org/sdr/FDEA201511103550.md): Contact · unsecure · Nov 10, 2015 · N365FE · Doug MD1010F · Emergency Equipment
  > FOUND LI DOOR SLIDE PRESS TEST LIGHT INOPERATIVE. RELEASED FOR SERVICE IAW MEL 25-61-01 CATEGORY C EXPIRATION 20 NOV 15. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY. L1 DOOR SLIDE PR
- [SDR FDEA201510173273](https://openairdocs.org/sdr/FDEA201510173273.md): Windshield · cracked · Oct 17, 2015 · N365FE · Doug MD1010F · Flight Compartment Windows
  > DURING DESCENT PASSING THROUGH 16000 FEET THE CAPTAINS WINDSHIELD STARTED CRACKING. NEITHER PILOT NOTICED ANY BIRD IMPACT OR OTHER EXTERIOR FORCE THAT COULD HAVE CAUSED IT. R & R CAPTAINS LT WINDSHIELD IAW MM 56-11-00-2. REINSTALLED WINDSHIELD WIPER ARM IAW
- [SDR FDEA201507102195](https://openairdocs.org/sdr/FDEA201507102195.md): Indicator · inoperative · Jul 10, 2015 · N365FE · Doug MD1010F · Emergency Equipment
  > R1 DOOR SLIDE REMOTE PRESSURE, PRESS TO TEST SWITCH INOPERATIVE. R & R RT REMOTE SLIDE PACK PRESS INDICATOR. OPERATIONS CHECKED NORMAL.
- [SDR FDEA201506231958](https://openairdocs.org/sdr/FDEA201506231958.md): Power Supply · defective · Jun 23, 2015 · N365FE · Doug MD1010F · Emergency Lighting
  > EMERGENCY LIGHT BATTERY 1 LO LVL 1 ALERT DURING EMER LIGHT TEST ON PREFLIGHT. REMOVED AND REPLACED EMERGENCY LIGHTS PWR SUPPLY PER AMM 33-51-01-4. OPS CHECKS GOOD PER AMM 31-51-01-5. OK FOR SERVICE.
- [SDR FDEA201506091729](https://openairdocs.org/sdr/FDEA201506091729.md): Warning Message · false activation · Jun 9, 2015 · N365FE · Doug MD1010F · Emergency Lighting
  > LEVEL 1 EMERGENCY LIGHT BATTERY 1 LOW, ILLUMINATED DURING PREFLIGHT. ARMED EMERGENCY LIGHTS AND THE MESSAGE DID NOT RETURN. EMERGENCY LIGHTS TESTED GOOD IAW AMM 33-51-00-5.
- [SDR FDEA201505031378](https://openairdocs.org/sdr/FDEA201505031378.md): Battery Pack · discharged · May 3, 2015 · N365FE · Doug MD1010F · Emergency Lighting
  > EMERGENCY LIGHT BATTERY 1 LOW, LEVEL 1 ALERT ON EAD DURING EMERGENCY LIGHT PREFLIGHT TEST.
- [SDR FDEA201503030638](https://openairdocs.org/sdr/FDEA201503030638.md): Light · inoperative · Mar 3, 2015 · N365FE · Doug MD1010F · Emergency Equipment
  > MAIN ENTRY DOOR SLIDE 1L DOES NOT TEST. RELEASED FOR SERVICE IAW MEL 25-61-01 CATEGORY C. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE IAW MEL 25-61-01. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY. R & R LIGHT BULBS. FOUND PUSH
- [SDR FDEA201501230374](https://openairdocs.org/sdr/FDEA201501230374.md): Door · out of adjust · Jan 23, 2015 · N365FE · Doug MD1010F · Passenger/Crew Doors
  > THE L1 DOOR WILL NOT CLOSE. WHEN ATTEMPTING TO CLOSE THE DOOR THE TOP OF THE DOOR POPS INWARD ABOUT 10 INCHES. COMPLETED ADJUSTMENT TEST OF L1 DOOR PER AMM 52-11-00-5.
- [SDR FDEA201412174135](https://openairdocs.org/sdr/FDEA201412174135.md): Support · out of position · Dec 17, 2014 · N365FE · Doug MD1010F · Main Landing Gear
  > DURING RAISING GEAR AFTER TAKEOFF, RT MAIN GEAR DID NOT INDICATE UP, RED LIGHT IN BOTH CONFIG PAGE & INDICATOR ABOVE GEAR HANDLE, DID NOT FEEL ADVERSE YAW OR NOISE THAT ONE MIGHT EXPECT WITH ONE GEAR DOWN. GEAR INDICATED DOWN WITH THREE GREEN FOR LANDING. R
- [SDR FDEA201412104101](https://openairdocs.org/sdr/FDEA201412104101.md): Spar · damaged · Dec 10, 2014 · N365FE · Doug MD1010F · Wing Spar
  > FOUND HOLE ON LT WING REAR LOWER SPAR TO BE DIFFERENT. COMPLY WITH EA 8-5710-T0313003 PT 1.
- [SDR FDEA201411173717](https://openairdocs.org/sdr/FDEA201411173717.md): Seat Track · damaged · Nov 17, 2014 · N365FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO COMPARTMENT STATION 1422, RBL8 SEAT TRACK IS DAMAGED.552 BEYOND LIMITS IAW SRM 53-70 VOL 1 PAGE 21. SEAT TRACK SECTION REPLACED IAW SRM 53-70-00 VOL 1.
- [SDR FDEA201411143700](https://openairdocs.org/sdr/FDEA201411143700.md): Panel · gouged · Nov 14, 2014 · N365FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING LOWER WING HINGE PANEL 551DB HAS GOUGE ON INNER SECTION FROM FLAP VANE CONTACT. REPAIRED HINGE PANEL 551DB AS REQUIRED IAW SRM 51-71-00 VOL II.
- [SDR FDEA201411143679](https://openairdocs.org/sdr/FDEA201411143679.md): Access Panel · delaminated · Nov 14, 2014 · N365FE · Doug MD1010F · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STAB TE ACCESS PANEL 334HB HAS DELAMINATION INNER OTBD SECTION OF PANEL. REPAIR PANEL 334HB IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-02 VOL II.
- [SDR FDEA201411123663](https://openairdocs.org/sdr/FDEA201411123663.md): Bulkhead Web · cracked · Nov 12, 2014 · N365FE · Doug MD1010F · Fuselage Main, Bulkhead
  > NOSE WW LT SIDEWALL SKIN HAS A FOUR INCH CRACK AT BS 485. REPAIRED IAW SRM 53-30-00 FIG 6
- [SDR FDEA201411123665](https://openairdocs.org/sdr/FDEA201411123665.md): Panel · delaminated · Nov 12, 2014 · N365FE · Doug MD1010F · Wing Miscellaneous Structure
  > RIGHT WING ROOT PANEL ARC0446-502 IS DELAMINATED. REPAIRED PANEL ARC0446-502 AS REQUIRED IAW SRM 51-71-00 VOL II.
- [SDR FDEA201411123655](https://openairdocs.org/sdr/FDEA201411123655.md): Panel · delaminated · Nov 12, 2014 · N365FE · Doug MD1010F · Wing, Plate/Skin
  > PANEL 541AB AT LT WING ROOT HAS SEPARATED LAYERS. REPAIRED IAW SRM 51-71-00 VOL II.
- [SDR FDEA201411113643](https://openairdocs.org/sdr/FDEA201411113643.md): Skin · damaged · Nov 11, 2014 · N365FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT INBD FLAP INBD LE HAS DAMAGE. REPAIRED IAW SRM 57-10-00 & DWG SG 10570001.
- [SDR FDEA201411083594](https://openairdocs.org/sdr/FDEA201411083594.md): Panel · delaminated · Nov 8, 2014 · N365FE · Doug MD1010F · Wing Miscellaneous Structure
  > PANEL ARC0446-503 AT LT WING ROOT HAS SEPARATED LAYERS. REPAIRED PANEL ARC0446-503 AS REQUIRED IAW SRM 51-71-00 VOL II.
- [SDR FDEA201411083580](https://openairdocs.org/sdr/FDEA201411083580.md): Bracket · cracked · Nov 8, 2014 · N365FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT OTBD FLAP, INBD HINGE FWD ATTACH POINT FITTING, Z BRACKET CRACKED ON INBD SIDE. R & R CRACKED BRACKET IAW SRM 51-31-01.
- [SDR FDEA201411043471](https://openairdocs.org/sdr/FDEA201411043471.md): Seat Track · damaged · Nov 4, 2014 · N365FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK STATION 750 LBL 47 SEAT TRACK DAMAGED. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 VOL I.
- [SDR FDEA201411043470](https://openairdocs.org/sdr/FDEA201411043470.md): Seat Track · damaged · Nov 4, 2014 · N365FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK STATION 1015 LBL 47 SEAT TRACK DAMAGED. SPLICED IN NEW SECTION OF SEAT TRACK IAW SRM 53-7--00 VOL 1.
- [SDR FDEA201410303426](https://openairdocs.org/sdr/FDEA201410303426.md): Doubler · cracked · Oct 30, 2014 · N365FE · Doug MD1010F · Fuselage Main, Bulkhead
  > CENTER LANDING GEAR WW BAY BS 1381, X=31.50 DOUBLER IS CRACKED. REMOVED AND REPLACED DOUBLER.
- [SDR FDEA201407172078](https://openairdocs.org/sdr/FDEA201407172078.md): Skin · cracked · Jul 17, 2014 · N365FE · Doug MD1010F · Wing, Plate/Skin
  > FOUND CRACKS ON RT WING FIXED LE UPPER SURFACE ANTI-ICE TELESCOPING DUCT CUT OUT. COMPLIED WITH EA 8-5720-T0309797 COMPLYING WITH SRM 57-40-01.
- [SDR FDEA201312213026](https://openairdocs.org/sdr/FDEA201312213026.md): Battery · inoperative · Dec 21, 2013 · N365FE · Doug MD1010F · Escape Slide
  > L1 DOOR EVACUATION SLIDE RAFT PRESS. INDICATOR LIGHT INOPERATIVE. REPLACED BATTERIES FOR L1 DOOR EVACUATION SLIDE RAFT PRESS TEST LIGHT, OPERATIONS CHECKED NORMAL. ACFT OK FOR SERVICE IAW MM 25-61-01-2.
- [SDR FDEA201304300889](https://openairdocs.org/sdr/FDEA201304300889.md): Lamp · inoperative · Apr 30, 2013 · N365FE · Doug MD1010F · Escape Slide
  > R1 DOOR SLIDE PRESSURE INDICATOR LIGHT INOPERATIVE. REPLACED LAMP IAW 26-61-03-2, OPS CHECKED GOOD.
- [SDR FDEA201303150580](https://openairdocs.org/sdr/FDEA201303150580.md): Doubler · cracked · Mar 15, 2013 · N365FE · Doug MD1010F · Fuselage Main, Bulkhead
  > CLG W/W COMPARTMENT LT SIDEWALL CUTOUT DOUBLER CRACKED. R & R CENTER LANDING GEAR W/W LT SIDEWALL CUTOUT DOUBLER PN AEA0526U1.
- [SDR FDEA201303150579](https://openairdocs.org/sdr/FDEA201303150579.md): Doubler · cracked · Mar 15, 2013 · N365FE · Doug MD1010F · Fuselage Main, Bulkhead
  > CLG W/W COMPARTMENT RT SIDEWALL CUTOUT DOUBLER CRACKED. REMOVED CRACKED DOUBLER, INSTALLED DOUBLER RT SIDE REF SRM 51-00-01, VOL 2 AND 51-33-01, VOL 2.
- [SDR FDEA201211154038](https://openairdocs.org/sdr/FDEA201211154038.md): Spar · cracked · Nov 15, 2012 · N365FE · Doug MD1010F · Horizontal Stabilizer, Spar/Rib
  > RT SIDE OF HORIZONTAL STAB REAR SPAR VERTICAL TANG HAS A CRACK EMANATING FROM FASTENER HOLE, UPPER ROW SECOND OTBD APPROX.375" LONG. (MKD) NEED TO COMPLY WITH WORK CARD STEP 8 B IN WORK CARD INSTRUCTIONS 55X1203ALI-P4 SEQ 140 STOP DRILLED CRACK WITH.250 HOLE
- [SDR FDEA201210263753](https://openairdocs.org/sdr/FDEA201210263753.md): Attach Angle · cracked · Oct 26, 2012 · N365FE · Doug MD1010F · Fuselage Main, Attach Fittings
  > NR 3 ACM COMPARTMENT STA 565-595 OTBD CEILING WEB TO SKIN ATTACHING ANGLE CRACKED, CRACK RUNS FWD TO AFT IN ANGLE RADIUS APPROX 30 INCHES LONG. INSTALLED CUSP REPAIR ANGLE IAW SRM 53-40-00 VOL I,FIG 28.
- [SDR FDEA201210183662](https://openairdocs.org/sdr/FDEA201210183662.md): Control Panel · burned · Oct 18, 2012 · N365FE · Doug MD1010F · Electrical Power System
  > ELECTRICAL ODOR, LIKE HOT EQUIPTMENT, NOTICABLE IN THE COCKPIT. STRONGER ON THE CAPTAIN'S SIDE AND THE STRONGEST ON GROUND. ODOR APPEARS TO BE COMING FROM THE ELECTICAL SYS CONTROL PANEL. R & R ELECTICAL SYS CONTROL PANEL IAW AMM.

Next page: https://openairdocs.org/deregistered/N365FE-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 = 'N365FE' AND deregistration_id = 'N365FE-2024-01-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N365FE-2024-01-29/reports

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