# Service difficulty reports: N363DH, cancelled Feb 29, 2012

A list on [N363DH, cancelled Feb 29, 2012](https://openairdocs.org/deregistered/N363DH-2012-02-29.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 4 · 164 reports

- [SDR DHLA200900030](https://openairdocs.org/sdr/DHLA200900030.md): Fan · failed · May 17, 2009 · N363DH · Airbus A300B42C · Landing Gear Brake System
  > ON 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 DHLA200700067](https://openairdocs.org/sdr/DHLA200700067.md): Light · inoperative · Nov 23, 2007 · N363DH · Airbus A300B4203 · Emergency Lighting
  > EMERGENCY EXIT LIGHT DISARM WARNING DOES NOT ILLUMINATE. REPLACED LIGHT BULBS ON DISARM CAPSULE PER MM 33-51-00. OPS TEST OK.
- [SDR DHL2007363500](https://openairdocs.org/sdr/DHL2007363500.md): Gusset · cracked · Sep 8, 2007 · N363DH · Airbus A300B4203 · Nacelle/Pylon Miscellaneous Structure
  > NR 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 DHL2007363001](https://openairdocs.org/sdr/DHL2007363001.md): Tripler · damaged · Jun 24, 2007 · N363DH · Airbus A300B4203 · Fuselage Main, Plate/Skin
  > DURING 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 53-13-00
- [SDR DHL2006363552](https://openairdocs.org/sdr/DHL2006363552.md): Skin · corroded · Nov 14, 2006 · N363DH · Airbus A300B4203 · Wing, Plate/Skin
  > BOTTOM 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 SHEET
- [SDR DHL2006363513](https://openairdocs.org/sdr/DHL2006363513.md): Seat Track · corroded · Oct 26, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN 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 DHL2006363533](https://openairdocs.org/sdr/DHL2006363533.md): Seat Track · corroded · Oct 26, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN 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 DHL2006363520](https://openairdocs.org/sdr/DHL2006363520.md): Seat Track · corroded · Oct 26, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN 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 DHL2006363512](https://openairdocs.org/sdr/DHL2006363512.md): Seat Track · corroded · Oct 26, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN 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 DHL2006363511](https://openairdocs.org/sdr/DHL2006363511.md): Seat Track · corroded · Oct 26, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN 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 DHL2006363510](https://openairdocs.org/sdr/DHL2006363510.md): Seat Track · corroded · Oct 26, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN 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 DHL2006363544](https://openairdocs.org/sdr/DHL2006363544.md): Seat Track · corroded · Oct 26, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN 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 DHL2006363509](https://openairdocs.org/sdr/DHL2006363509.md): Seat Track · gouged · Oct 26, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 DHL2006363500](https://openairdocs.org/sdr/DHL2006363500.md): Seat Track · corroded · Oct 26, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN 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 MATERIA
- [SDR DHL2006363549](https://openairdocs.org/sdr/DHL2006363549.md): Seat Track · corroded · Oct 25, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN 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 DHL2006363506](https://openairdocs.org/sdr/DHL2006363506.md): Seat Track · corroded · Oct 25, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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 DHL2006363505](https://openairdocs.org/sdr/DHL2006363505.md): Seat Track · corroded · Oct 25, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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 DHL2006363553](https://openairdocs.org/sdr/DHL2006363553.md): Stringer · corroded · Oct 24, 2006 · N363DH · Airbus A300B4203 · Fuselage Main, Longeron/Stringer
  > E/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 PRO
- [SDR DHL2006363508](https://openairdocs.org/sdr/DHL2006363508.md): Seat Track · corroded · Oct 24, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 DHL2006363507](https://openairdocs.org/sdr/DHL2006363507.md): Cargo Track · corroded · Oct 24, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 DHL2006363501](https://openairdocs.org/sdr/DHL2006363501.md): Skin · dented · Oct 24, 2006 · N363DH · Airbus A300B4203 · Fuselage Main, Plate/Skin
  > DENT 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 CRA
- [SDR DHL2006363551](https://openairdocs.org/sdr/DHL2006363551.md): Attach Fitting · worn · Oct 23, 2006 · N363DH · Airbus A300B4203 · Ailerons
  > L/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 RIB
- [SDR DHL2006363545](https://openairdocs.org/sdr/DHL2006363545.md): Seat Track · corroded · Oct 23, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 OUT
- [SDR DHL2006363547](https://openairdocs.org/sdr/DHL2006363547.md): Seat Track · corroded · Oct 23, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 DHL2006363503](https://openairdocs.org/sdr/DHL2006363503.md): Seat Track · corroded · Oct 21, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN 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 DHL2006363504](https://openairdocs.org/sdr/DHL2006363504.md): Seat Track · corroded · Oct 21, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN 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 REF
- [SDR DHL2006363548](https://openairdocs.org/sdr/DHL2006363548.md): Cargo Track · corroded · Oct 1, 2006 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 DHL2006363006](https://openairdocs.org/sdr/DHL2006363006.md): Computer · faulted · May 16, 2006 · N363DH · Airbus A300B4203 · Airspeed/Mach Indicator
  > CAPT'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 PERFO
- [SDR DHL2006363005](https://openairdocs.org/sdr/DHL2006363005.md): Indicator · malfunctioned · May 16, 2006 · N363DH · Airbus A300B4203 · Airspeed/Mach Indicator
  > CAPT'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 34-1
- [SDR DHL2006363004](https://openairdocs.org/sdr/DHL2006363004.md): Switch · malfunctioned · May 4, 2006 · N363DH · Airbus A300B4203 · Landing Gear Position and Warning
  > NOSE 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 DHL2006363003](https://openairdocs.org/sdr/DHL2006363003.md): Skin · torn · Apr 12, 2006 · N363DH · Airbus A300B4203 · Fuselage Main, Plate/Skin
  > FUSELAGE 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 SHE
- [SDR DHL2006363002](https://openairdocs.org/sdr/DHL2006363002.md): Skin · damaged · Apr 12, 2006 · N363DH · Airbus A300B4203 · Fuselage Main, Plate/Skin
  > AIRCRAFT 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, WO
- [SDR DHL2006363001](https://openairdocs.org/sdr/DHL2006363001.md): Power Supply · inoperative · Feb 20, 2006 · N363DH · Airbus A300B4203 · Emergency Lighting
  > LT EMERGENCY EXIT LIGHT AT L1 INOP. REMOVED & REPLACED LT EMERGENCY LIGHT POWER SUPPLY CK. GOOD IAW MM 3351-1.
- [SDR DHL2005363005](https://openairdocs.org/sdr/DHL2005363005.md): Gcu · failed · Jun 30, 2005 · N363DH · Airbus A300B4203 · AC Generation System
  > POWER 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 16.5
- [SDR DHL2005363004](https://openairdocs.org/sdr/DHL2005363004.md): Switch · malfunctioned · Jun 18, 2005 · N363DH · Airbus A300B4203 · Landing Gear Position and Warning
  > ON 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. REP
- [SDR DHL2005363003](https://openairdocs.org/sdr/DHL2005363003.md): Switch · sticking · Jun 17, 2005 · N363DH · Airbus A300B4203 · Landing Gear Position and Warning
  > NOSE 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 DHL2005363002](https://openairdocs.org/sdr/DHL2005363002.md): Engine · failed · Apr 27, 2005 · N363DH · Airbus A300B4203 · Powerplant System
  > AT 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 72-00-00
- [SDR DHL2004363014](https://openairdocs.org/sdr/DHL2004363014.md): Brake Assy · malfunctioned · Dec 18, 2004 · N363DH · Airbus A300B4203 · Landing Gear Brake System
  > BRAKES GRAB ON RT SIDE. PERFORMED OPERATIONAL CHECK OF NORMAL, ALT, AND ANTI-SKID SYSTEMS. NO DEFECTS NOTED IAW MM 32-42-00.
- [SDR DHL2004363013](https://openairdocs.org/sdr/DHL2004363013.md): Warning System · activated · Dec 5, 2004 · N363DH · Airbus A300B4203 · Central Warning
  > T/O REJECTED DUE TO CONTINUOUS CHIME. NOTED CAB PRESSURE LIGHT FLICKER. REPLACED SEQUENCE BOX. SYS TESTS OK PER 21-31-00.
- [SDR DHL2004363012](https://openairdocs.org/sdr/DHL2004363012.md): Warning System · malfunctioned · Dec 5, 2004 · N363DH · Airbus A300B4203 · Central Warning
  > RTO DUE TO CONTINUES CHIME. NO ANNUNCIATORS ILLUMINATED. REPLACE MWC PER MM 33-15-11. AURAL WARNING CHECKS OK PER MM 31-24-00.
- [SDR DHL200436311](https://openairdocs.org/sdr/DHL200436311.md): Brake · malfunctioned · Dec 5, 2004 · N363DH · Airbus A300B4203 · Landing Gear Brake System
  > ON 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 DHL200436310](https://openairdocs.org/sdr/DHL200436310.md): Indicator · inoperative · Dec 5, 2004 · N363DH · Airbus A300B4203 · Overheat Detection
  > APPROXIMATELY 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 DHL2004363009](https://openairdocs.org/sdr/DHL2004363009.md): B-Nut · loose · Nov 20, 2004 · N363DH · Airbus A300B4203 · Master Cylinder/Brake Valve
  > AFTER 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 32-43-6
- [SDR DHL2004363008](https://openairdocs.org/sdr/DHL2004363008.md): Pitot Line · separated · Nov 11, 2004 · N363DH · Airbus A300B4203 · Airspeed/Mach Indicator
  > DURING 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. PERFORMED
- [SDR DHL2004363534](https://openairdocs.org/sdr/DHL2004363534.md): Skin · dented · Oct 12, 2004 · N363DH · Airbus A300B4203 · Fuselage Main, Plate/Skin
  > DURING 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 DISCRE
- [SDR DHL2004363532](https://openairdocs.org/sdr/DHL2004363532.md): Skin · dented · Oct 12, 2004 · N363DH · Airbus A300B4203 · Fuselage Main, Plate/Skin
  > DURING "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. PE
- [SDR DHL2004363511](https://openairdocs.org/sdr/DHL2004363511.md): Seat Track · corroded · Oct 5, 2004 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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. INS
- [SDR DHL2004363509](https://openairdocs.org/sdr/DHL2004363509.md): Seat Track · corroded · Oct 5, 2004 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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 DHL2004363512](https://openairdocs.org/sdr/DHL2004363512.md): Seat Track · corroded · Oct 4, 2004 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > DURING "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 57
- [SDR DHL2004363530](https://openairdocs.org/sdr/DHL2004363530.md): Seat Track · corroded · Sep 30, 2004 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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

Next page: https://openairdocs.org/deregistered/N363DH-2012-02-29/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 = 'N363DH' AND deregistration_id = 'N363DH-2012-02-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N363DH-2012-02-29/reports

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