N362FE, cancelled Mar 2, 2024
Service difficulty reports · 37
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 = 'N362FE' AND deregistration_id = 'N362FE-2024-03-02' 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201507152225Warning System · false activationNUMBER 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 FDEA201502060465Indicator · failedL1 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 FDEA201406231527Skin · crackedEVIDENCE 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 FDEA201406231528Support · crackedSUSPECT 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 51-31-0SDR FDEA201405301230Skin · crackedON 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 WSDR FDEA201403140509Spar Cap · crackedDURING 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 STANSDR FDEA201212284394Wire · damagedON 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,B115-27SDR FDEA201202260688Skin · corrodedCORROSION FOUND ON EXTERNAL FUSELAGE SKIN AT BS 1109 AT S46R. REPAIRED SKIN IAW SRM 53-20-00, FIG 6, REPAIR CLASSIFED AS MAJOR.SDR FDEA201202230673Cargo Track · wornMAIN 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 FDEA201202200627Skin · tornRIGHT 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 FDEA201202160595Skin · corrodedEXTERNAL 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 FDEA201202120563Seat Track · wornMAIN 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 FDEA201102090510Light · inoperativeL1 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 FDEA201102090514Antenna · malfunctionedCONSTANT 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 ANTENNASDR FDEA201004061088Web · crackedNR 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 FDEA201003230968Feeder Cable · damagedWIRE 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 SEPASDR FDEA200909173323Relay · malfunctionedREJECTED 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 FDEA200908213070Cylinder · shearedWHILE 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 FDEA200903060858Line · looseNR 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 FDEA200903040835Push-Pull Cable · damagedAT 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 NESDR FDEA200812115180Bearing · failedNR 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 07FDEA02482Skin · corrodedCORROSION POSSIBLE ON FUSELAGE SKIN CORROSION LIMITED TO LONGERON DAMAGE WHICH WAS REPAIRED PER 53-10-00 VOL 1 OF MD10-10.SDR 07FDEA01503Proximity Sensor · unknownON 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 COSDR 06FDEA03585Bracket · crackedRT 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 05FDEA01029Keelbeam · crackedAUXILIARY 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 51-31-01SDR 05FDEA01028Keelbeam · crackedAUXILIARY 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 51-31-01SDR 04FDEA03168Door · vibrates14000 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 8-3SDR 03FDEA01465Hinge Bracket · corrodedLT 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 03FDEA01466Hinge Bracket · corrodedRT 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 S00018SDR 03FDEA01455Arm · corrodedWINGS-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 03FDEA01456Bolt · inaccurateWINGS-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 03FDEA01457Web · crackedEXHAUST SYSTEM THRUST REVERSER SUPPORT WEB CRACK REPAIR. COMPLIED WITH E.A.8-7830-72281. EXHAUST SYSTEM THRUST REVERSER SUPPORT ASSY WEB CRACK REPAIR.SDR 03FDEA01458Support · crackedTHRUST REVERSER-SUPPORT ASSY TORQUE BOX WEB REPAIR. COMPLIED WITH E.A.8-7830-72283. EXHAUST-THRUST REVERSER-SUPPORT ASSY TORQUE BOX WEB REPAIR.SDR 03FDEA01459Case · gougedGOUGES 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 03FDEA01387Support · crackedCOMPLY 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 03FDEA01383Thrust Reverser · crackedCOMPLY WITH EA 8-7832-72265 EXHAUST-THRUST REV- FIXED BODY UPPER ANGLE CRACK REPAIR. EXHAUST-THRUST REV FIXED BODY UPPER ANGLE CRACK REPAIR.SDR 03FDEA01334Support Angle · crackedLEFT 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.
Back to N362FE, cancelled Mar 2, 2024