# Service difficulty reports: N362FE, cancelled Mar 2, 2024 A list on [N362FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N362FE-2024-03-02.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR FDEA201507152225](https://openairdocs.org/sdr/FDEA201507152225.md): Warning System · false activation · Jul 15, 2015 · N362FE · Doug MD1010F · Pneumatic Indicating System > NUMBER 1 AIR MANIFOLD FAIL ALERT AT CRZ FL 340 ENG & WING A/ION, PACKS 1 & 3 ON. DIVERTED & LANDED WITHOUT INCIDENT. PERFORMED NR 1 DECAY CHECK, PASSES 9 SEC, 7 SEC MIN IAW AMM 36-00-01-5. PERFORMED AIR SYS TEST, NO FAULTS NOTED. CHECKED AIU & NO RELATED - [SDR FDEA201502060465](https://openairdocs.org/sdr/FDEA201502060465.md): Indicator · failed · Feb 6, 2015 · N362FE · Doug MD1010F · Emergency Equipment > L1 SLIDE TEST LIGHT DOES NOT ILLUMINATE WHEN PUSHED TO TEST. R & R L1 DOOR REMOTE SLIDE PACK PRESSURE PRESS TO TEST INDICATOR. OPERATIONS TESTED NORMAL. - [SDR FDEA201406231527](https://openairdocs.org/sdr/FDEA201406231527.md): Skin · cracked · Jun 23, 2014 · N362FE · Doug MD1010F · Fuselage Main, Plate/Skin > EVIDENCE OF A CRACK IN THE NR 3 PACK BAY DOOR FRAME. NR 3 PACK DOOR FRAME/SKIN DAMAGE REPAIRED REF MD10/DC 10 SRM 53-50-00 FIG A SHEET 3. - [SDR FDEA201406231528](https://openairdocs.org/sdr/FDEA201406231528.md): Support · cracked · Jun 23, 2014 · N362FE · Doug MD1010F · Fuselage Miscellaneous Structure > SUSPECT CRACK ON UPPER AFT T CHORD OF DOOR CUT OUT STATION 535 ON INBD SIDE FROM RIVET HOLE TO EDGE. PERFORMED HFEC ON UPPER AFT T CHORD OF DOOR CUT OUT OF NR 3 PACK BAY DOOR FRAME IAW NTM PT6. CRACK VERIFIED. INSTALLED SUPPORT BRACKET REF MD 10 SRM 51-31-0 - [SDR FDEA201405301230](https://openairdocs.org/sdr/FDEA201405301230.md): Skin · cracked · May 30, 2014 · N362FE · Doug MD1010F · Wing, Plate/Skin > ON WALK AROUND FOUND POSSIBLE CRACK ON LT WING AT FWD INBD CORNER OF FUEL PNL. CONFIRMED CRACK AT FWD INBD CORNER OF FUEL PNL BY HFEC INSPECTION IAW NDTSPM PT 6. CRACK TERMINATES AT RIVET. STARTED REMOVING DOOR TO ASSIST SHEET METAL. FINISHED REMOVING LT W - [SDR FDEA201403140509](https://openairdocs.org/sdr/FDEA201403140509.md): Spar Cap · cracked · Mar 14, 2014 · N362FE · Doug MD1010F · Wing Spar > DURING C7, B9 CHECK AT LAX CRACK FOUND IN HOLE B & C IN REAR SPAR LOWER CAP AT XORS 345.75. ADDITIONAL INSPECTION FOUND UPPER SPAR CAP FLANGE TO HAVE A 2.8 INCH CRACK RUNNING BETWEEN HOLES A & C INCLUDING THE B HOLE. IN ADDITION A CRACK WAS FOUND IN THE STAN - [SDR FDEA201212284394](https://openairdocs.org/sdr/FDEA201212284394.md): Wire · damaged · Dec 28, 2012 · N362FE · Doug MD1010F · Air Conditioning System Wiring > ON POST FLIGHT CHECK FOUND NR 3 AVIONICS RACK COOLING BREAKER POPPED. RESET BREAKER AND IT POPPED AGAIN. REMOVED DAMAGED WIRING AND REPAIRED FOLLOWING WIRES. B115-280-14B,B115-12-14C,B115-281-14C,B115-283-14B, B115-284-14C,B115-282-14A,B115-42-12,B115-27 - [SDR FDEA201202260688](https://openairdocs.org/sdr/FDEA201202260688.md): Skin · corroded · Feb 26, 2012 · N362FE · Doug MD1010F · Fuselage Main, Plate/Skin > CORROSION FOUND ON EXTERNAL FUSELAGE SKIN AT BS 1109 AT S46R. REPAIRED SKIN IAW SRM 53-20-00, FIG 6, REPAIR CLASSIFED AS MAJOR. - [SDR FDEA201202230673](https://openairdocs.org/sdr/FDEA201202230673.md): Cargo Track · worn · Feb 23, 2012 · N362FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO TRACK AT BS 1387.5, LBL 72 HAS TWO WORN AND BROKEN SCALLOP LOBES, REPAIRED CARGO TRACK IAW SRM 53-70-00 FIG 1. - [SDR FDEA201202200627](https://openairdocs.org/sdr/FDEA201202200627.md): Skin · torn · Feb 20, 2012 · N362FE · Doug MD1010F · Trailing Edge Flaps > RIGHT OTBD T/E FLAP LOWER SKIN HAS OIL CANNING ABOUT 45" OTBD OF FLAP VANE CARTRIDGE CUT-OUT AND 25" FWD OF T/E. REPAIRED RT WING OTBD T/E FLAP LOWER SKIN IAW SRM 57-10-00, FIG 7, REPAIR CLASSIFIED AS MAJOR. - [SDR FDEA201202160595](https://openairdocs.org/sdr/FDEA201202160595.md): Skin · corroded · Feb 16, 2012 · N362FE · Doug MD1010F · Fuselage Main, Plate/Skin > EXTERNAL FUSELAGE SKIN BULGING AT BS 1621 BETWEEN S47-48R. REPAIRED EXTERNAL FUSELAGE SKIN IAW SRM 53-20-00, FIG 6, SHEET 5 AND 6, REPAIR CLASSIFIED AS MAJOR. - [SDR FDEA201202120563](https://openairdocs.org/sdr/FDEA201202120563.md): Seat Track · worn · Feb 12, 2012 · N362FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK SEAT TRACK AT BS 755 AT LBL 47.5 HAS CHIPPED LOBES. REMOVED AND REPLACED MAIN DECK SEAT TRACK BETWEEN BS 725 TO 765 AT LBL 47.5 IAW SRM 51-31-01 AND SRM 53-70-00, FIG. 1, REPAIR CLASSIFIED AS MAJOR. - [SDR FDEA201102090510](https://openairdocs.org/sdr/FDEA201102090510.md): Light · inoperative · Feb 9, 2011 · N362FE · Doug MD1010F · Equipment/Furnishings Wiring > L1 DOOR SLIDE PTT LIGHT INOP. WIRE THAT ATTACHES TO C BATTERY HOUSING BROKEN OFF. RELEASED FOR SERVICE IAW MEL: 25-61-01, PRESS VERIFIED IAW MEL 25-61-01. ACFT OK FOR SERVICE. - [SDR FDEA201102090514](https://openairdocs.org/sdr/FDEA201102090514.md): Antenna · malfunctioned · Feb 9, 2011 · N362FE · Doug MD1010F · Emergency Locator Beacon > CONSTANT ELT TONE ON 121.5 BOTH RADIOS. OVERHEAD COCKPIT ELT PANEL RESET NO HELP, RESET AT ELT NO HELP. TONE GOES AWAY THEN COMES BACK AFTER 5 TO 10 MINUTES. WITH ELT SWITCH IN OFF DETENT TONE STILL SOUNDS. WITH ELT SWITCH IN OFF AND ELT 6 INCH ANTENNA - [SDR FDEA201004061088](https://openairdocs.org/sdr/FDEA201004061088.md): Web · cracked · Apr 6, 2010 · N362FE · Doug MD1010F · Leading Edge Devices > NR 1 RT SLAT DAMAGED AT INBD WEB/RIB STRUCTURE R & R FITTING PN ARB701602 IAW DWG ARB 7016 VIEW CC AND SRM 51-31-01, VOL II. R & R WEB PN ARB7128-24 IAW SRM 51-33-01 VOL II AND DRWN ARB7128-24. - [SDR FDEA201003230968](https://openairdocs.org/sdr/FDEA201003230968.md): Feeder Cable · damaged · Mar 23, 2010 · N362FE · Doug MD1010F · Electrical Power System Wiring > WIRE NR C501-19-00A AT EXTERNAL POWER PLUG PIN "A" HAD OVERHEAT/ARCING DAMAGE AND POWER RECEPTACLE R5-1065 PIN "A" HOLE MELTED DUE TO OVERHEAT CONDITION. WIRE NR C501-23-00A AT LUG A2 OF EXTERNAL POWER BREAKER R2-218 HAD OVERHEAT DAMAGE AND WIRE STRANDS SEPA - [SDR FDEA200909173323](https://openairdocs.org/sdr/FDEA200909173323.md): Relay · malfunctioned · Sep 17, 2009 · N362FE · Doug MD1010F · Engine Thrust Reverser > REJECTED T/O DUE TO: LEVEL 1 ALERT: REV 1, PRESS FAIL T, DUPLICATED REV 1 PRESS FAULT ON 3 DIFFERENT TAXI/RUN-UP TESTS IAW JRH CHAPT 5 AND CHPT 4-8. REMOVED AND REPLACED NR 1 T/R ACTUATION SYS LOCK RELAY BOX IAW MM 78-33-10-6 AND CHECKED IAW MM 87-33-10-4. - [SDR FDEA200908213070](https://openairdocs.org/sdr/FDEA200908213070.md): Cylinder · sheared · Aug 21, 2009 · N362FE · Doug MD1010F · Leading Edge Slat Control System > WHILE CONFIGURING FOR LANDING, RECEIVED A LEVEL 2 SLAT DISAGREE ALERT. RAN QRH PROCEDURE WHICH REQUIRED A FLAPS 22/RETRACT LANDING. LANDED ILS 36C CAPTAINS LANDING. REMOVED AND REPLACED LT WING INBD AND OTBD SLAT CYLINDERS REF AMM 27-82-01-2. LEAK CK GOOD. - [SDR FDEA200903060858](https://openairdocs.org/sdr/FDEA200903060858.md): Line · loose · Mar 6, 2009 · N362FE · Doug MD1010F · Turbine Engine Oil System > NR 2 ENG OIL QTY DROPPED FROM 12 QTS TO 3 QTS IN 2HRS. TEMP/PRESS NORMAL. DECREASED TO 2 QTS AT IDLE WITH DECREASING PRESSURE. SHUTDOWN NR 2. NR 2 ENG AND FOUND LINE LOOSE FROM NR 2 ENG OIL SCAVENGE FILTER BOWL TO THE OIL STRAINER CLOGGING SWITCH. - [SDR FDEA200903040835](https://openairdocs.org/sdr/FDEA200903040835.md): Push-Pull Cable · damaged · Mar 4, 2009 · N362FE · Doug MD1010F · Power Lever > AT TOP OF DESCENT NR 2 ENG WOULD NOT RETARD BELOW 74 PERCENT N1. NR 2 THROTTLE WAS AT LEAST TWO KNOB WIDTHS ABOVE NR 1 AND NR 3 THROTTLES. SHUTDOWN NR 2 ENG ON APPROACH. UNEVENTFUL APPROACH AND LANDING. FINISHED REMOVING OLD PUSH-PULL CABLE AND INSTALLED NE - [SDR FDEA200812115180](https://openairdocs.org/sdr/FDEA200812115180.md): Bearing · failed · Dec 11, 2008 · N362FE · Doug MD1010F · Wheel/Ski/Float > NR 1 TIRE ASSY OUTSIDE BEARING FAILURE. REMOVED WHEEL AND BRAKE ASSY FROM NR 1 AXLE LT MLG TRUCK ASSEMBLY TAG NR 5023BO. REPLACED LEFT MAIN LANDING GEAR TRUCK BEAM AND AXLE ASSY PER M/M REF 32-12-01-2. AIRCRAFT OK FOR FURTHER SERVICE. - [SDR 07FDEA02482](https://openairdocs.org/sdr/07FDEA02482.md): Skin · corroded · Jul 13, 2007 · N362FE · Doug MD1010F · Fuselage Main, Plate/Skin > CORROSION POSSIBLE ON FUSELAGE SKIN CORROSION LIMITED TO LONGERON DAMAGE WHICH WAS REPAIRED PER 53-10-00 VOL 1 OF MD10-10. - [SDR 07FDEA01503](https://openairdocs.org/sdr/07FDEA01503.md): Proximity Sensor · unknown · Apr 13, 2007 · N362FE · Doug MD1010F · Door Warning System > ON DEPARTURE RECEIVED LVL 2 CARGO DOOR FWD "B" ALERT, RAN QRH AND ALERT DISAPPEARED, MEL 52-40-01-05: CARGO DOOR FWD "B" ALERT INOP. VERIFY DOOR IS CLOSED AND LOCKED PRIOR TO BLOCK-OUT. INSPECTED "B" DOOR WARNING SWITCH FOR FWD LWR CARGO DOOR WARNING FOR CO - [SDR 06FDEA03585](https://openairdocs.org/sdr/06FDEA03585.md): Bracket · cracked · Oct 4, 2006 · N362FE · Doug DC1010 · Wing, Attach Fittings > RT O/B SLAT DRIVE O/B BRACKET FWD FLANGE RADIUS IS CRACKED. SEQ CARD 735. REMOVED AND REPLACED RT O/B SLAT DRIVE MECHANISM. - [SDR 05FDEA01029](https://openairdocs.org/sdr/05FDEA01029.md): Keelbeam · cracked · Apr 16, 2005 · N362FE · Doug MD1010F · Fuselage Main, Keel > AUXILIARY POWER UNIT KEEL CAP ASSEMBLY HAS 9 INCH CRACK FROM FUSELAGE STATION 2019 TO STATION 2028 AT STRINGER 45 RIGHT. REPAIRED STRINGER IAW EA 8-5310-83868, FUSELAGE - AFT BODY KEEL CAP SPLICE AT STA 2040 - REPAIR, AND MD 10 SRM 51-31-01 VOL 2 AND 51-31-01 - [SDR 05FDEA01028](https://openairdocs.org/sdr/05FDEA01028.md): Keelbeam · cracked · Apr 16, 2005 · N362FE · Doug MD1010F · Fuselage Main, Keel > AUXILIARY POWER UNIT KEEL CAP ASSEMBLY HAS 9 INCH CRACK FROM FUSELAGE STATION 2019 TO STATION 2028 AT STRINGER 45 RIGHT. REPAIRED STRINGER IAW EA 8-5310-83868, FUSELAGE - AFT BODY KEEL CAP SPLICE AT STA 2040 - REPAIR, AND MD 10 SRM 51-31-01 VOL 2 AND 51-31-01 - [SDR 04FDEA03168](https://openairdocs.org/sdr/04FDEA03168.md): Door · vibrates · Nov 18, 2004 · N362FE · Doug MD1010F · Landing Gear Doors > 14000 FT HEAVY VIBRATION SLOWED AND LANDED WITH NO PROBLEM, EVEN WITH GEAR DOWN HAD VIBRATION. "DECLARED EMERGENCY" HAD FIRE TRUCKS STANDING BY. REMOVED AND REPLACED LT NOSE GEAR DOOR PER MM 32-23-01-2. ACCOMLISHED GEAR SWING AND DOOR FIT CHECK PER EA 8-3 - [SDR 03FDEA01465](https://openairdocs.org/sdr/03FDEA01465.md): Hinge Bracket · corroded · Sep 9, 2003 · N362FE · Doug MD1010F · Trailing Edge Flaps > LT OUTBOARD FLAP INBOARD HINGE BRACKET, CORROSION REPAIR (P/N ARC0502-11) LT O/B FLAP I/B HINGE BRACKET CORROSION REPAIR,P/N ARC,0502-11 CLOSED ON 09/09/2003 FEDEX N/R S00031. - [SDR 03FDEA01466](https://openairdocs.org/sdr/03FDEA01466.md): Hinge Bracket · corroded · Sep 9, 2003 · N362FE · Doug MD1010F · Trailing Edge Flaps > RT OUTBOARD FLAP- OB HINGE BRACKET CORROSION REPAIR (P/N ARC0503) COMPLIED WITH EA 8-5750-72274_WINGS RT O/B FLAP-O/B HINGE BRACKET CORROSION REPAIR P/N ARC, 0503 CLOSED ON 09/09/2003 FEDEX NR S00018 - [SDR 03FDEA01455](https://openairdocs.org/sdr/03FDEA01455.md): Arm · corroded · Sep 7, 2003 · N362FE · Doug MD1010F · Trailing Edge Flap Control System > WINGS-OUTBOARD FLAP REWORK OF CARRAGE SUPPORT ARM P/N ARC 2177. COMPLIED WITH E.A. 8-5740-72289. WINGS-OUTBD FLAPS REWORK OF CARRAGE SUPPORT ARM P/N ARC 2177. - [SDR 03FDEA01456](https://openairdocs.org/sdr/03FDEA01456.md): Bolt · inaccurate · Sep 7, 2003 · N362FE · Doug MD1010F · Trailing Edge Flap Control System > WINGS-RIBS AND BULKHEADS-LT OUTBOARD FLAP HINGE STUD BOLT SUBSTITUTION. COMPLIED WITH E.A.8-5710-72287. WINGS-RIBS AND BKHDS- FLAP HINGE STUD BOLT SUBSTITUTION. - [SDR 03FDEA01457](https://openairdocs.org/sdr/03FDEA01457.md): Web · cracked · Sep 7, 2003 · N362FE · Doug MD1010F · Engine Thrust Reverser > EXHAUST SYSTEM THRUST REVERSER SUPPORT WEB CRACK REPAIR. COMPLIED WITH E.A.8-7830-72281. EXHAUST SYSTEM THRUST REVERSER SUPPORT ASSY WEB CRACK REPAIR. - [SDR 03FDEA01458](https://openairdocs.org/sdr/03FDEA01458.md): Support · cracked · Sep 7, 2003 · N362FE · Doug MD1010F · Engine Thrust Reverser > THRUST REVERSER-SUPPORT ASSY TORQUE BOX WEB REPAIR. COMPLIED WITH E.A.8-7830-72283. EXHAUST-THRUST REVERSER-SUPPORT ASSY TORQUE BOX WEB REPAIR. - [SDR 03FDEA01459](https://openairdocs.org/sdr/03FDEA01459.md): Case · gouged · Sep 7, 2003 · N362FE · Doug MD1010F · Engine Cowling System > GOUGES IN EXTERIOR OF NR 2 FAN FRAME CASE. COMPLIED WITH E.A. 8-7220-72285 ENGINES-DISPOSITION OF GOUGES IN EXTERIOR OF NR 2 ENGINE FAN FRAME CASE. - [SDR 03FDEA01387](https://openairdocs.org/sdr/03FDEA01387.md): Support · cracked · Aug 26, 2003 · N362FE · Doug DC1010 · Turbine Engine Reduction Gear > COMPLY WITH E.A. 8-7210-72270- ENGINE-BASIC- FAN STATOR SUPPORT HALF, CRACK REPAIR. ENGINE-BASIC FAN STATOR SUPPORT HALF CRACK REPAIR. CLOSED ON 08/25/2003 FEDEX. - [SDR 03FDEA01383](https://openairdocs.org/sdr/03FDEA01383.md): Thrust Reverser · cracked · Aug 25, 2003 · N362FE · Doug DC1010 · Engine Thrust Reverser > COMPLY WITH EA 8-7832-72265 EXHAUST-THRUST REV- FIXED BODY UPPER ANGLE CRACK REPAIR. EXHAUST-THRUST REV FIXED BODY UPPER ANGLE CRACK REPAIR. - [SDR 03FDEA01334](https://openairdocs.org/sdr/03FDEA01334.md): Support Angle · cracked · Aug 18, 2003 · N362FE · Doug DC1010 · Trailing Edge Flaps > LEFT WING I/B FLAP FAIRING PANEL SUPPORT STRUCTURE ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-31-01 AT MAE ON N00420 WO 23696. ## 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 = 'N362FE' AND deregistration_id = 'N362FE-2024-03-02' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N362FE-2024-03-02/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.