N365FE, cancelled Jan 29, 2024

Service difficulty reports · 267

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201901130127Girt Bar · looseGIRT BAR DOOR 1L HAS COME LOOSE RESECURED L-1 DOOR GIRT BAR. OK FOR SERVICE.Jan 13, 2019 · N365FE · Doug MD1010F · Emergency EquipmentSDR FDEA201812163525Slide · failedL1 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.Dec 16, 2018 · N365FE · Doug MD1010F · Escape SlideSDR FDEA201812153505Switch · malfunctionedON 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 ORIGDec 15, 2018 · N365FE · Doug MD1010F · Passenger/Crew DoorsSDR FDEA201802220478Cable · deformedR1 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.Feb 22, 2018 · N365FE · Doug MD1010F · Service DoorsSDR FDEA201801080037Cable · brokenL1 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.Jan 8, 2018 · N365FE · Doug MD1010F · Passenger/Crew DoorsSDR FDEA201701120139Bulkhead Web · crackedBS 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 53-40-00Jan 12, 2017 · N365FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201701030077Floor Support · corrodedMAIN DECK BS 1881, RBL 27 FLOOR SUPPORT IS CORRODED.. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG WSP0711.Jan 3, 2017 · N365FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201612294573Panel · delaminated#2 ENGINE INLET (PICKLE BARREL) PANEL AJC7068 IS DELAMINATED. REPAIRED IAW SRM 51-71-00 VOL 2.Dec 29, 2016 · N365FE · Doug MD1010F · Nacelle/Pylon, Plate/SkinSDR FDEA201612214518Skin · corrodedCAC 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.Dec 21, 2016 · N365FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201612214513Fitting · crackedLEFT 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.Dec 21, 2016 · N365FE · Doug MD1010F · Fuselage Main, StructureSDR FDEA201612214516Shear Tie · corrodedCAC BAY LOWER SKIN, BETWEEW BS 1079 TO 1099 LONGERON 51TO 52R HAS CORROSION AND SHEAR RIVET. REPLACED CORRODED SHEAR TIE IAW DWG. ADA 0112.Dec 21, 2016 · N365FE · Doug MD1010F · Fuselage Internal Mounting StructureSDR FDEA201612214515Fitting · crackedCAC 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.Dec 21, 2016 · N365FE · Doug MD1010F · Fuselage Main, Attach FittingsSDR FDEA201612154464Bulkhead · crackedFWD CARGO COMP STA 595 AT LONGERON 36L PRESSURE BULKHEAD SUSPECT CRACK. REPAIRED PER SRM 53-40-00 FIG 4.Dec 15, 2016 · N365FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201612154463Tee Fitting · crackedFWD CARGO BAY BS 595, LONGERON 36L CRACKED. REPAIRED PER EA. 8-5310-T0330353.Dec 15, 2016 · N365FE · Doug MD1010F · Fuselage Main, Attach FittingsSDR FDEA201612154462Tee Fitting · crackedFWD 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.Dec 15, 2016 · N365FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201612154459Cap · crackedFWD CARGO, COMPARTMENT STA 595 LONGERON 39R SUSPECT CRACK. AFTER EVALUATION , FOUND TEE CAP CRACKED. REPAIRED TEE CAP PER EA 8-5310-T0330385Dec 15, 2016 · N365FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201612114568Skin · crackedRIGHT WING NR 7 SLAT TRACK CUTOUT O/B CORNER CRACKED. REPAIRED IAW SRM 57-10-00, FIG.104 A , VOL. IDec 11, 2016 · N365FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201612054326Oxygen Mask · unserviceableCOCKPIT 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.Dec 5, 2016 · N365FE · Doug MD1010F · Portable Oxygen SystemSDR FDEA201607152451Door · crackedON 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.Jul 15, 2016 · N365FE · Doug MD1010F · Landing Gear DoorsSDR FDEA201604181255Crank Assy · defectiveCAPTAIN 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.Apr 18, 2016 · N365FE · Doug MD1010F · Landing Gear Brake SystemSDR FDEA201511103550Contact · unsecureFOUND 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 PRNov 10, 2015 · N365FE · Doug MD1010F · Emergency EquipmentSDR FDEA201510173273Windshield · crackedDURING 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 IAWOct 17, 2015 · N365FE · Doug MD1010F · Flight Compartment WindowsSDR FDEA201507102195Indicator · inoperativeR1 DOOR SLIDE REMOTE PRESSURE, PRESS TO TEST SWITCH INOPERATIVE. R & R RT REMOTE SLIDE PACK PRESS INDICATOR. OPERATIONS CHECKED NORMAL.Jul 10, 2015 · N365FE · Doug MD1010F · Emergency EquipmentSDR FDEA201506231958Power Supply · defectiveEMERGENCY 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.Jun 23, 2015 · N365FE · Doug MD1010F · Emergency LightingSDR FDEA201506091729Warning Message · false activationLEVEL 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.Jun 9, 2015 · N365FE · Doug MD1010F · Emergency LightingSDR FDEA201505031378Battery Pack · dischargedEMERGENCY LIGHT BATTERY 1 LOW, LEVEL 1 ALERT ON EAD DURING EMERGENCY LIGHT PREFLIGHT TEST.May 3, 2015 · N365FE · Doug MD1010F · Emergency LightingSDR FDEA201503030638Light · inoperativeMAIN 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 Mar 3, 2015 · N365FE · Doug MD1010F · Emergency EquipmentSDR FDEA201501230374Door · out of adjustTHE 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.Jan 23, 2015 · N365FE · Doug MD1010F · Passenger/Crew DoorsSDR FDEA201412174135Support · out of positionDURING 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. RDec 17, 2014 · N365FE · Doug MD1010F · Main Landing GearSDR FDEA201412104101Spar · damagedFOUND HOLE ON LT WING REAR LOWER SPAR TO BE DIFFERENT. COMPLY WITH EA 8-5710-T0313003 PT 1.Dec 10, 2014 · N365FE · Doug MD1010F · Wing SparSDR FDEA201411173717Seat Track · damagedUPPER 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.Nov 17, 2014 · N365FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201411143700Panel · gougedLEFT 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.Nov 14, 2014 · N365FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201411143679Access Panel · delaminatedLEFT 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.Nov 14, 2014 · N365FE · Doug MD1010F · Horizontal Stabilizer, Plate/SkinSDR FDEA201411123663Bulkhead Web · crackedNOSE WW LT SIDEWALL SKIN HAS A FOUR INCH CRACK AT BS 485. REPAIRED IAW SRM 53-30-00 FIG 6Nov 12, 2014 · N365FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201411123665Panel · delaminatedRIGHT WING ROOT PANEL ARC0446-502 IS DELAMINATED. REPAIRED PANEL ARC0446-502 AS REQUIRED IAW SRM 51-71-00 VOL II.Nov 12, 2014 · N365FE · Doug MD1010F · Wing Miscellaneous StructureSDR FDEA201411123655Panel · delaminatedPANEL 541AB AT LT WING ROOT HAS SEPARATED LAYERS. REPAIRED IAW SRM 51-71-00 VOL II.Nov 12, 2014 · N365FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201411113643Skin · damagedRIGHT INBD FLAP INBD LE HAS DAMAGE. REPAIRED IAW SRM 57-10-00 & DWG SG 10570001.Nov 11, 2014 · N365FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201411083594Panel · delaminatedPANEL ARC0446-503 AT LT WING ROOT HAS SEPARATED LAYERS. REPAIRED PANEL ARC0446-503 AS REQUIRED IAW SRM 51-71-00 VOL II.Nov 8, 2014 · N365FE · Doug MD1010F · Wing Miscellaneous StructureSDR FDEA201411083580Bracket · crackedLEFT OTBD FLAP, INBD HINGE FWD ATTACH POINT FITTING, Z BRACKET CRACKED ON INBD SIDE. R & R CRACKED BRACKET IAW SRM 51-31-01.Nov 8, 2014 · N365FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201411043471Seat Track · damagedMAIN DECK STATION 750 LBL 47 SEAT TRACK DAMAGED. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 VOL I.Nov 4, 2014 · N365FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201411043470Seat Track · damagedMAIN DECK STATION 1015 LBL 47 SEAT TRACK DAMAGED. SPLICED IN NEW SECTION OF SEAT TRACK IAW SRM 53-7--00 VOL 1.Nov 4, 2014 · N365FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201410303426Doubler · crackedCENTER LANDING GEAR WW BAY BS 1381, X=31.50 DOUBLER IS CRACKED. REMOVED AND REPLACED DOUBLER.Oct 30, 2014 · N365FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201407172078Skin · crackedFOUND 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.Jul 17, 2014 · N365FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201312213026Battery · inoperativeL1 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.Dec 21, 2013 · N365FE · Doug MD1010F · Escape SlideSDR FDEA201304300889Lamp · inoperativeR1 DOOR SLIDE PRESSURE INDICATOR LIGHT INOPERATIVE. REPLACED LAMP IAW 26-61-03-2, OPS CHECKED GOOD.Apr 30, 2013 · N365FE · Doug MD1010F · Escape SlideSDR FDEA201303150580Doubler · crackedCLG W/W COMPARTMENT LT SIDEWALL CUTOUT DOUBLER CRACKED. R & R CENTER LANDING GEAR W/W LT SIDEWALL CUTOUT DOUBLER PN AEA0526U1.Mar 15, 2013 · N365FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201303150579Doubler · crackedCLG 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.Mar 15, 2013 · N365FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201211154038Spar · crackedRT 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 HOLENov 15, 2012 · N365FE · Doug MD1010F · Horizontal Stabilizer, Spar/RibSDR FDEA201210263753Attach Angle · crackedNR 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.Oct 26, 2012 · N365FE · Doug MD1010F · Fuselage Main, Attach FittingsSDR FDEA201210183662Control Panel · burnedELECTRICAL 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.Oct 18, 2012 · N365FE · Doug MD1010F · Electrical Power System
Back to N365FE, cancelled Jan 29, 2024