N363DH, cancelled Feb 29, 2012
Service difficulty reports · 164
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 = 'N363DH' AND deregistration_id = 'N363DH-2012-02-29' 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.
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 = 'N363DH' AND deregistration_id = 'N363DH-2012-02-29' 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 DHLA200900030Fan · failedON LAST TAKEOFF 3RD HOT BRAKES ILLUM AT 80KTS REJECTED TAKEOFF PERF APPROP CHECKLISTS TAXI IN. REPLACED NR 3 BRAKE IAW MM 32-42-27, OPS CK NORMAL.SDR DHLA200700067Light · inoperativeEMERGENCY EXIT LIGHT DISARM WARNING DOES NOT ILLUMINATE. REPLACED LIGHT BULBS ON DISARM CAPSULE PER MM 33-51-00. OPS TEST OK.SDR DHL2007363500Gusset · crackedNR 2 ENG PYLON AT COWL HINGE FITTING O/B SIDE HAS A CRACK APPROX 3/4" ABOVE T BRACKET AT RIB 4. REMOVED AN REPLACED GUSSET HINGE FITTING AN T BRACKET AT NR 2 ENG PYLON O/B SIDE RIB 4 IAW A300 SRM 51-30-30 AN A300 SB A300-54-068.SDR DHL2007363001Tripler · damagedDURING A WEEKEND CHECK AT AVBOURNE HEAVY MX, THE FOLLOWING DISCREPANCIES WERE NOTED; TRIPLER DAMAGED ON PREVIOUS REPAIR AT FWD SIDE OF FWD CARGO DOOR CUT-OUT, FROM STR 39R AT FRAME 20A. REMOVED AND REPLACED FWD CARGO DOOR CUT OUT TRIPLER IAW A300 SRM 53-13-00SDR DHL2006363552Skin · corrodedBOTTOM OF L/W SKIN HAS CORROSION AT DRAIN HOLE FWD OF NR 6 FLAP TRACK. CORROSION BLEND OUT TO A MAJOR REPAIR AT L/W BOTTOM SKIN SLAT TRACK NR 9 DRAIN HOLE FWD OF NR 6 FLAP TRACK ASSEMBLY, FOUND TO BE OUT OF LIMITS AS PER ATTACHED AIRBUS REPAIR APPROVAL SHEETSDR DHL2006363513Seat Track · corrodedCABIN FLOOR STRUCTURE FRAME 60 AND 61 AT BL 0 SEAT TRACK FLANGE HAS SURFACE CORROSION. INSTALLED ANGLE REPAIR AT CABIN SEAT TRACK FLANGE REF A300SRM 53-10-70 FIG 721A. TREATED AND PRIMED AND APPLY TOP COAT AS REQUIRED REF A300 SRM 51-40-12.SDR DHL2006363533Seat Track · corrodedCABIN FLOOR STRUCTURE FRAME 60 AND 61 AT BL 0 SEAT TRACK FLANGE HAS SURFACE CORROSION. INSTALLED ANGLE REPAIR AT CABIN SEAT TRACK FLANGE REF A300SRM 53-10-70 FIG 721A. TREATED AND PRIMED AND APPLY TOP COAT AS REQUIRED REF A300 SRM 51-40-12.SDR DHL2006363520Seat Track · corrodedCABIN FLOOR STRUCTURE FRAME 60 AND 61 AT BL 0 SEAT TRACK FLANGE HAS SURFACE CORROSION. INSTALLED ANGLE REPAIR AT CABIN SEAT TRACK FLANGE REF A300SRM 53-10-70 FIG 721A. TREATED AND PRIMED AND APPLY TOP COAT AS REQUIRED REF A300 SRM 51-40-12.SDR DHL2006363512Seat Track · corrodedCABIN FLOOR STRUCTURE FRAME 60 AND 61 AT BL 0 SEAT TRACK FLANGE HAS SURFACE CORROSION. INSTALLED ANGLE REPAIR AT CABIN SEAT TRACK FLANGE REF A300SRM 53-10-70 FIG 721A. TREATED AND PRIMED AND APPLY TOP COAT AS REQUIRED REF A300 SRM 51-40-12.SDR DHL2006363511Seat Track · corrodedCABIN FLOOR STRUCTURE FRAME 60 AND 61 AT BL 0 SEAT TRACK FLANGE HAS SURFACE CORROSION. INSTALLED ANGLE REPAIR AT CABIN SEAT TRACK FLANGE REF A300SRM 53-10-70 FIG 721A. TREATED AND PRIMED AND APPLY TOP COAT AS REQUIRED REF A300 SRM 51-40-12.SDR DHL2006363510Seat Track · corrodedCABIN FLOOR STRUCTURE FRAME 60 AND 61 AT BL 0 SEAT TRACK FLANGE HAS SURFACE CORROSION. INSTALLED ANGLE REPAIR AT CABIN SEAT TRACK FLANGE REF A300SRM 53-10-70 FIG 721A. TREATED AND PRIMED AND APPLY TOP COAT AS REQUIRED REF A300 SRM 51-40-12.SDR DHL2006363544Seat Track · corrodedCABIN FLOOR STRUCTURE FRAME 60 AND 61 AT BL 0 SEAT TRACK FLANGE HAS SURFACE CORROSION. INSTALLED ANGLE REPAIR AT CABIN SEAT TRACK FLANGE REF A300SRM 53-10-70 FIG 721A. TREATED AND PRIMED AND APPLY TOP COAT AS REQUIRED REF A300 SRM 51-40-12.SDR DHL2006363509Seat Track · gougedMAIN CARGO DECK SEAT TRACK IS GOUGED AT FS 48 AND LBL 58. INSTALLED NEW SECTION OF SEAT TRACK AT MAIN CARGO FROM FS 44.5 TO 48.5 IAW A300SRM 53-10-10 AND 51-30-30. MATERIAL USED TMS 60-22457 7075-T6511.SDR DHL2006363500Seat Track · corrodedCABIN FLOOR STRUCTURE AT FRAME 62 THRU 69 AT BL18L SEAT TRACK FLANGE SURFACE CORROSION. REMOVED LIGHT SURFACE CORROSION AT FS 62 TP FS 69 AT BL18L SEAT TRACK FLANGE SURFACE IAW A300 SRM 51-40-11. MATERIAL LOSS 0.003 REMAINING MATERIAL 0.0075 ORIGINAL MATERIASDR DHL2006363549Seat Track · corrodedCABIN FLOOR SEAT TRACK FLANGE AT BL 18 HAS CORROSION BETWEEN FRAME 30 AND FRAME 33. REMOVED AND REPLACED SEAT TRACK AND SPLICED IAW A300 SRM 53-10-10 PAGE 817, 818, 819 FIG 725 AT FS 30 TO FS 33 BL18L.SDR DHL2006363506Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE FS 48 TO 51, LBL18. REMOVED AND REPLACED SECTION OF SEAT TRACK AT FRAME 48 TO 51 IAW A300 SRM 51-10-40. FASTENERS INSTALLED IAW A300 SRM 51-30-30.SDR DHL2006363505Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE BETWEEN FS 50-52 LBL37. REMOVED SECTION OF SEAT TRACK AND REPLACED FROM FR50-52 LT IAW A300SRM 53-10-10 USED TMS 60-22457 7075-T6511.SDR DHL2006363553Stringer · corrodedE/E COMPT FLOOR AREA BETWEEN FS 17 AND FS 18 AND BETWEEN STR 52L AND STR 54L FLOOR SKIN AND FRAME ANGLE AND STRINGER HAS CORROSION. COMPLIED WITH FSI REPAIR DISPOSITION MSN085/01. FOUND TO BE WITHIN LIMITS, REFER TO ATTACHED 8110-3 DATED NOV 17,2006 (FAA PROSDR DHL2006363508Seat Track · corrodedMAIN CARGO COMPARTMENT FLOOR SUPPORT FS 20.5 LBL 80 SURFACE CORROSION. FABRICATED NEW SEAT TRACK AS REQUIRED FROM TMS 60-24257 7075T6,REF A300 SRM 51-10-40, TREATED AND PRIMED IAW A300 SRM 51-40-12. INSTALLED SEAT TRACK AT FS 20-22 LBL 80 IAW A300 SRM 53-10-SDR DHL2006363507Cargo Track · corrodedMAIN CARGO COMPARTMENT FLOOR SUPPORT FS 20.5 LBL 80 SURFACE CORROSION. FABRICATED NEW SEAT TRACK AS REQUIRED FROM TMS 60-24257 7075T6, REF A300 SRM 51-10-40, TREATED AND PRIMED IAW A300 SRM 51-40-12. INSTALLED SEAT TRACK AT FS 20-22 LBL 80 IAW A300 SRM 53-10SDR DHL2006363501Skin · dentedDENT IN FUSELAGE SKIN AT FS 13 STRINGER 31R APPROX. AVBORNE MAINTENANCE CAUSED DAMAGE. REWORKED DENT IN FUSELAGE SKIN AT FS 13 STRINGER 31R FOUND TO BE WITHIN LIMITS IAW A300 SRM 53-12-00, ALODINED AND PRIMED IAW A300 SRM 51-40-12. ACCOMPLISHED HFOC, NO CRASDR DHL2006363551Attach Fitting · wornL/W ALL SPEED AILERON FITTINGS FOR ALL ACTUATORS THE 3RD FROM I/B HAS THE SLIDING PLATE AND FITTING WITH A WORN OUT GROOVE AT O/B SIDE, MADE BY A ACTUATOR GUIDE PLATE SEE N/R 091621. PERFORMED MAJOR REPAIR OF L/W ALL SPEED AILERON INTERMEDIATE RIB BETWEEN RIBSDR DHL2006363545Seat Track · corrodedMAIN CABIN FLOOR STRUCTURE UPPER FLANGE HAS CORROSION BETWEEN FS 12A AND 13A LBL18". REMOVED CORROSION AT MAIN CABIN FLOOR STRUCTURE UPPER FLANGE BETWEEN FS 12A AND 13A LBL18 IAW A300 SRM 51-40-11 MAT LOSS .018 MAT REMAINING .062 ORIGINAL MAT .080. FOUND OUTSDR DHL2006363547Seat Track · corrodedMAIN CABIN FLOOR STRUCTURE UPPER FLANGE HAS CORROSION BETWEEN FS 12A & 13A LBL18". REMOVED CORROSION AT MAIN CABIN FLOOR STRUCTURE UPPER FLANGE BETWEEN FS 12A & 13A LBL18 IAW A300 SRM 51-40-11 MAT LOSS .018 MAT REMAINING .062 ORIGINAL MAT .080. FOUND OUT OF SDR DHL2006363503Seat Track · corrodedCABIN FLOOR BETWEEN FRAME 15C AND 14C SEAT TRACK SUPPORT FLANGE AND SEAT TRACK FLANGE HAS CORROSION AT BL28R. REMOVED AND REPLACED CABIN FLOOR SEAT TRACK FROM FS 12A TO FS 15C LBL38 REF A300 SRM 51-10-40 AND TREATED AND PRIME AND APPLY TOP COAT AS NEEDED REF SDR DHL2006363504Seat Track · corrodedCABIN FLOOR BETWEEN FRAME 15C AND 14C SEAT TRACK SUPPORT FLANGE AND SEAT TRACK FLANGE HAS CORROSION AT BL28R. REMOVED AND REPLACED CABIN FLOOR SEAT TRACK FROM FS 12A TO FS 15C LBL 38 REF A300 SRM 51-10-40 AND TREATED AND PRIME AND APPLY TOP COAT AS NEEDED REFSDR DHL2006363548Cargo Track · corrodedMAIN CARGO COMPARTMENT FLOOR SUPPORT FS 20-22 LBL 60 AND LBL 80 SURFACE CORROSION UNDER CLIP NUT. REPLACED SECTION OF TRACK AS REQUIRED FROM TMS 60-24257 7075T6, REF A300 SRM 51-10-40, TREATED AND PRIMED AND PAINTED IAW A300 SRM. INSTALLED SEAT TRACK AT FS SDR DHL2006363006Computer · faultedCAPT'S AIR SPEED INDICATOR SHOWED -0- DURING T/O ROLL, ABORTED T/O AT 85 KIAS, WEIGHT 310,000 LBS, OAT 23' PA-37 FT, MAX BRAKE TEMP 250 DEGREES CELSIUS. REMOVED AND REPLACED ADC NR 1 IAW MM 34-11-20, LEAK TEST PERFORMED IAW 34-11-10, HI-LEVEL PITOT TEST PERFOSDR DHL2006363005Indicator · malfunctionedCAPT'S AIR SPEED INDICATION SHOWED -0- DURING T/O ROLL ABORTED T/O AT 90KIAS WEIGHT:31300 LBS, AOT 24'C PA 0 FT MAX OBSERVED BRAKE TEMP 400 DEGREES CELSIUS. REMOVED AND REPLACED NR 1 AIR SPEED IND IAW MM 34-12-22. PITOT STATIC LEAK TEST PERFORMED IAW MM 34-1SDR DHL2006363004Switch · malfunctionedNOSE GEAR DOOR (ORANGE) IN TRANSIT LIGHT DID NOT COME ON WHEN EXTENDING GEAR (PILOTS PANEL) S/O PANEL OK. REPLACED RT NOSE GEAR DOOR SWITCH 38GB, NOSE GEAR DOOR INDICATION NORMAL IAW AMM 32-61-00, REF A-300 AWM 32-61-15, P/N 141FLO1D3.SDR DHL2006363003Skin · tornFUSELAGE SKIN AT AFT EDGE OF AFT CARGO COMPARTMENT DOOR CUTOUT IS TORN AND GOUGED 1.5 INCHES. DAMAGE IS AT FRAME 63A NEAR STRINGER 38. REPAIRED FUSELAGE SKIN AT AFT EDGE OF AFT CARGO COMPARTMENT DOOR AT FRAME 63A NEAR STRINGER 38 IAW SRM 53-17-00 FIG 720 SHESDR DHL2006363002Skin · damagedAIRCRAFT DAMAGE ON AFT FUSELAGE BETWEEN FRAMES 65 AND 66 JUST BELOW STRINGER 36. REPAIRED FUSELAGE BETWEEN FRAMES 65 AND 66 AT STRINGER 36 IAW SRM 53-10-10 FIG 749. EDDY CURRENT INSPECTION IAW AIRBUS NDT MANUAL PART I 51-30-00. NO CRACK INDICATION FOUND, WOSDR DHL2006363001Power Supply · inoperativeLT EMERGENCY EXIT LIGHT AT L1 INOP. REMOVED & REPLACED LT EMERGENCY LIGHT POWER SUPPLY CK. GOOD IAW MM 3351-1.SDR DHL2005363005Gcu · failedPOWER INTERUPTION B4 GEN 1 RESULTING IN RTO. DEFERRED NR 1 GEN IAW MEL 24-11-01 CONTROL NR 21499 ID NR 8742. PERFORMED AC GEN ADJ/TEST IAW MM 24-11-00 SYS OPS OK FOR SERVICE THIS CLEARS DMI NR 21499 REPLACED NR 1 GCU IAW MM 24-21-00. RAN ENG. IAW JRH 16.5SDR DHL2005363004Switch · malfunctionedON SHORT FINAL AFTER LANDING, GEAR EXTENSION, NOSE GEAR UNSAFE LIGHT (RED) ILLUMINATED ON PILOTS FRONT PANEL. ELECTED TO GO AROUND AND ACCOMPLISHED ABNORMAL PROCEDURE. RETURNED TO LANDING. NO COMPLICATIONS. SECOND OFFICERS GEAR LIGHTS OPERATE NORMALLY. REPSDR DHL2005363003Switch · stickingNOSE GEAR INDICATED UNSAFE ON FWD PANEL DURING CVG APPROACH. THREE GREEN AND SAFE ON S/O PANEL. COMPLETED ABNORMAL PROCEDURE. FOUND 40GB SWITCH PLUNGER STICKING. LUBED PLUNGER GEAR INDICATION CKS GOOD IAW MM 32-61-00.SDR DHL2005363002Engine · failedAT VR ENGINE NR 2 FAILED. COMPLETED APPROPRIATE ABNORMAL PROCEDURES. DUMP 18,800 LBS OF FUEL. EGT TEMP EXCEEDED 7 SECONDS AT 940. PERFORM BOROSCOPE INSPECTION ON NR 2 ENG FOR EGT OVERTEMP AND COMPRESSOR STALL ON TAKEOFF. PERFORMED BORO INSP PER MM 72-00-00SDR DHL2004363014Brake Assy · malfunctionedBRAKES GRAB ON RT SIDE. PERFORMED OPERATIONAL CHECK OF NORMAL, ALT, AND ANTI-SKID SYSTEMS. NO DEFECTS NOTED IAW MM 32-42-00.SDR DHL2004363013Warning System · activatedT/O REJECTED DUE TO CONTINUOUS CHIME. NOTED CAB PRESSURE LIGHT FLICKER. REPLACED SEQUENCE BOX . SYS TESTS OK PER 21-31-00.SDR DHL2004363012Warning System · malfunctionedRTO DUE TO CONTINUES CHIME. NO ANNUNCIATORS ILLUMINATED. REPLACE MWC PER MM 33-15-11. AURAL WARNING CHECKS OK PER MM 31-24-00.SDR DHL200436311Brake · malfunctionedON REJECT, AUTO BRAKES DIDN'T ENGAGE UNTIL BRAKES APPLIED WITH PEDALS. ALSO, DID NOT DISENGAGE WITH PEDAL PRESSURE. DEFERRED AUTO BRAKES AS PER MEL 32-42-07. CAT "C". TRANSFERED TO DMI LOG. CONTROL NR 18696 EMP 8662.SDR DHL200436310Indicator · inoperativeAPPROXIMATELY 15 MINUTES AFTER TAKEOFF AT FLIGHT LEVEL 290, THE BRAKE TEMP ON WHEEL NR 8 INDICATED 700 DEGREES AND BRAKES HOT ILLUMINATED ON MASTER WARNING PANEL. ABNORMAL PROCEDURE COMPLETED ON LANDING APR BRAKE. T/S, SUSPECT F/E NR 8 BRAKE TEMP INDICATION SDR DHL2004363009B-Nut · looseAFTER LANDING AND WHILE APPLYING BRAKES, AIRCRAFT PULLS NOTICABLY TO THE RIGHT. ALSO, RIGHT BRAKE PEDAL FEELS "SOFT". FOUND LOOSE B-NUT ON MASTER CYLINDER LOCATED UNDER F/O'S FLOOR PANEL. RESECURED B-NUT, LEAK CHECKS OK. NO FURTHER DEFECTS NOTED IAW 32-43-6SDR DHL2004363008Pitot Line · separatedDURING TAKEOFF ROLL, THERE WAS NO AIRSPEED INDICATED ON THE CAPTAIN'S AIRSPEED INDICATOR WHILE THE FIRST OFFICER'S CORRECTLY INDICATED 90KTS. TAKEOFF WAS ABORTED (293,000LBS, 90KTS, 8DEGC, NO THRUST REVERSER USED. FOUND PITOT LINE OFF OF NR 1 ADC. PERFORMEDSDR DHL2004363534Skin · dentedDURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3912, AFT. FUSELAGE SKIN HAS DENT AT FR 77 AND STR 22R. BLENDED OUT AREA, FOUND DENT BEYOND LIMITS IAW SRM 53-10-10. CUT OUT DAMAGE AREA SRM 53-10-10. PERFORMED HFEC OF CUT-OUT AREA NTM PT 1 51-31-05. NO DISCRESDR DHL2004363532Skin · dentedDURING "C" CHECK AT AVBORNE HEAVY MAINTENACE IN MIAMI, FL DISCREPANCY AS FOLLOWS, N/R 3911, AFT FUSELAGE SKIN HAS DENT AT FS 65 AND STR 31R. BLENDED OUT AREA FOUND DENT BEYOND OF LIMITS IAW A-300 SRM 53-10-10. CUT-OUT DAMAGED AREA IAW A-300 SRM 53-10-10. PESDR DHL2004363511Seat Track · corrodedDURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3899 LBL 36 BETWEEN FRAME 15 AND FRAME 19 SEAT TRACK CORRODED. REMOVED CORROSION FROM AREA FRAME 15 TO FRAME 19 LBL 36 FOUND OUT OF LIMITS SRM 53-10-00. REMOVED SEAT TRACK FOR REPAIR IAW SRM 51-30-30/51-10-40. INSSDR DHL2004363509Seat Track · corrodedDURING C-CHECK, DISCREPANCY AS FOLLOWS, NR 3898, RBL 36 BETWEEN FRAME AND FRAME 19 SEAT TRACK CORRODED. REMOVED CORROSION FROM AREA/FRAME IS TO FRAME 19 RBL 36 FOUND OUT OF LIMITS SRM 53-10-00. REMOVED SEAT TRACK FROM FR 15 TO FR. 19 AT RBL 36 IAW SRM 51-30-SDR DHL2004363512Seat Track · corrodedDURING "C" CHECK IN MIAMI, FL AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3900 MAIN CABIN SEAT TRACK FLANGE OUT OF LIMITS BETWEEN FRAME 27 TO FRAME 33, LBL 57. REMOVED CORROSION FROM AREA MAIN CABIN SEAT TRACK BETWEEN FRAME 27 AND FRAME 33 LBL 57SDR DHL2004363530Seat Track · corrodedDURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3887, FR.18-FR. 26.5 RBL 98 SEAT TRACKS MAIN CABIN CORRODED BEYOND LIMITS IAW SRM 51-40-11. REMOVED SEAT TRACKS FROM FR 18 TO FR 26.5 AT RBL 98 IAW SRM 51-30-30. REPLACED SEAT TRACK IAW SRM 51-10-40. INSTALLED NEW
Back to N363DH, cancelled Feb 29, 2012