# N636AW: 1990 Airbus Industrie A320-231, registration cancelled 2009-11-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 3, 2009 - Status when cancelled: Triennial form not returned - Airframe: [Airbus Industrie A320-231](https://openairdocs.org/model/airbus-industrie-a320-231) (registry code 3930325) - Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999) - Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs) - Serial number: 098 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: May 8, 1990 - Certificate issued: September 28, 1990 - Last registry action: July 21, 2009 - Mode S code: A8541B - Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N636AW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=636AW - Page: https://openairdocs.org/deregistered/N636AW-2009-11-03 From the FAA registry file of November 3, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Airbus Industrie A320-231: https://openairdocs.org/model/airbus-industrie-a320-231.md ## Service difficulty reports (135, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA2009051191141](https://openairdocs.org/sdr/USAA2009051191141), May 9, 2009: BRACKET. LOOSE. FLT 632 - PHX - EEL - ROW 11D LOW LEVEL EMERGENCY LIGHTING DETACHED. MAINTENANCE RESECURED BRACKET AS REQUIRED. - [SDR USAA2009032390648](https://openairdocs.org/sdr/USAA2009032390648), Mar 21, 2009: SLIDE RAFT. MISINSTALLED. FLT 117 - PHX - EMERGENCY EGRESS SYSTEM - R-1 DOOR EMERGENCY SLIDE PACKED INCORRECTLY. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR SLIDE RAFT. - [SDR USAA2009032390647](https://openairdocs.org/sdr/USAA2009032390647), Mar 21, 2009: SLIDE RAFT. MISINSTALLED. FLT 117 - PHX - EMERGENCY EGRESS SYSTEM - R-2 DOOR EMERGENCY SLIDE PACKED INCORRECTLY. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR SLIDE RAFT. - [SDR USAA2009032390646](https://openairdocs.org/sdr/USAA2009032390646), Mar 21, 2009: CABLE. MISROUTED. FLT 117 - PHX - EMERGENCY EGRESS SYSTEM - L-2 DOOR SLIDE INSULATION CABLE ROUTED INCORRECTLY. MAINTENANCE REMOVED AND REPLACED L-2 DOOR SLIDE. - [SDR USAA920080991](https://openairdocs.org/sdr/USAA920080991), May 2, 2008: POWER SUPPLY. FAILED. FLT 610 - PHX - EEL - FWD LEFT EMERGENCY POWER SUPPLY UNIT FAILS TEST PER T/C A1C33302. MAINTENANCE REMOVED AND REPLACED THE FWD EPSU. OPERATIONAL CHECK WAS NOR - [SDR USAA920080753](https://openairdocs.org/sdr/USAA920080753), Apr 4, 2008: PTU. DEFECTIVE. FLT 625 - PHX-OAK - RTF - CREW REPORTED TOTAL LOSS OF YELLOW SYSTEM HYDRAULIC FLUID. DESELECTED PTU AND ENG NR 2 YELLOW PUMP PER ECAM, HOWEVER BOTH RAN WITHOUT - [SDR USAA920071106](https://openairdocs.org/sdr/USAA920071106), Nov 8, 2007: POWER SUPPLY. DEFECTIVE. FLT 170, JFK-PHX - EEL - FAA RAMP CHECK FOUND EMERGENCY LIGHT INOP ROWS 9 & 11. REMOVED AND REPLACED POWER SUPPLY UNIT AT RIGHT OVERWING, MFG P/N 3214-54, S/N 4 - [SDR USAA920070958](https://openairdocs.org/sdr/USAA920070958), Oct 8, 2007: SPAR. DELAMINATED. SAL - MAJOR REPAIR - C-5 CHECK - LEFT AILERON LEADING EDGE SPAR IS DELAMINATED, WS 13464 - WS 14057. REPAIRED LEFT AILERON LEADING EDGE SPAR, WS 13464 - WS 1405 - [SDR USAA920070878](https://openairdocs.org/sdr/USAA920070878), Sep 29, 2007: HINGE FITTING. WORN. SAL - MAJOR REPAIR - C-05 CHECK - NR 5989775, RIGHT ELEVATOR HINGE ARM FITTING NR 2 WORN, HORIZONTAL STABILIZLER STATION 227 / RIB 6. REPLACED RIGHT ELEVATOR HI - [SDR USAA920070907](https://openairdocs.org/sdr/USAA920070907), Sep 25, 2007: SPAR. CRACKED. MAJOR REPAIR - C-04 CHECK - NR 5989697, RIGHT PYLON OUTBOARD SPAR CRACKED, RIB 6. REPAIRED RIGHT PYLON OUTBOARD SPAR, RIB 6 IAW A320 SRM 54-52-12 FIGURE 203. - [SDR USAA920070959](https://openairdocs.org/sdr/USAA920070959), Sep 21, 2007: STOP. CORRODED. SAL - MAJOR REPAIR - C-05 CHECK - CORROSION ON THE L2 DOOR STOP ASSEMBLY, BEAM 3. REPLACED THE L2 DOOR STOP ASSEMBLY, BEAM 3 IAW A320 AMM 52-11-00. - [SDR USAA920070879](https://openairdocs.org/sdr/USAA920070879), Sep 21, 2007: SEAT TRACK. CORRODED. SAL - MAJOR REPAIR - C-05 CHECK - NR 5989136, CORROSION ON SEAT TRACK, BS 1430 - BS 1560, +Y1292. REPLACED SEAT TRACK, BS 1430 - BS 1560, +Y1292 IAW A320 SRM 51 - [SDR USAA920070858](https://openairdocs.org/sdr/USAA920070858), Sep 21, 2007: SEAT TRACK. CORRODED. SAL - MAJOR REPAIR - C-05 CHECK - NR 5989144, CORROSION ON CABIN SEAT TRACK, -Y765, BS 1650 / FR 41 - BS 1976 / FR 47. REPLACED CABIN SEAT TRACK, -Y765, BS 1650 - [SDR AWXA200700844](https://openairdocs.org/sdr/AWXA200700844), Jul 13, 2007: POWER SUPPLY. FAILED. LAS - EEL - LOG NR 7811308 - CREW REPORTED EMERGENCY EXIT SIGNS, LEFT OVERWING AND MID CABIN OVERHEAD ARE INOP. MX REPLACED THE POWER SUPPLY UNIT. OPERATIONAL C - [SDR AWXA200700103](https://openairdocs.org/sdr/AWXA200700103), Jan 16, 2007: POWER SUPPLY. FAILED. LAS - EEL - POWER SUPPLY ROW 23 A/C LEFT INOP. REMOVED AND REPLACED POWER SUPPLY ROW 23 A/C LEFT REF AMM 23-73-38. OPS CHECK NORMAL. - [SDR AWXA200601697](https://openairdocs.org/sdr/AWXA200601697), Sep 10, 2006: WIRE. BROKEN. PHX - EEL - DURING ROUTINE MAINTENANCE IT WAS DISCOVERED THAT THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17L WAS INOP (WIRES WERE PULLED OUT). MX - [SDR AWXA200601056](https://openairdocs.org/sdr/AWXA200601056), Jun 28, 2006: SHOCK ABSORBER. DEFECTIVE. PHX - AIR TURNBACK - FLT 675A - LOG 7335803 - CREW REPORTED THAT AFTER TAKEOFF, ON CLIMB OUT, DURING GEAR RETRACTION THEY RECEIVED ECAM CLASS 1 MESSAGE FOR LAND - [SDR AWXA200601007](https://openairdocs.org/sdr/AWXA200601007), Jun 19, 2006: WIRE. BROKEN. PHX - EEL - NR 4099472 - DURING OVERNIGHT MAINTENANCE DISCOVERED ROW 24L EMERGENCY EXIT LIGHT INOP. MAINTENANCE RE-TERMINATED BROKEN WIRE AT CONNECTION IAW ESPM - [SDR AWXA200601005](https://openairdocs.org/sdr/AWXA200601005), Jun 19, 2006: WIRE. BROKEN. PHX - EEL - NR 4080757 - DURING OVERNIGHT MAINTENANCE DISCOVERED ROW 26L EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE IAW ESPM. OPERATIONAL - [SDR AWXA200600491](https://openairdocs.org/sdr/AWXA200600491), Mar 21, 2006: SPLICE. DAMAGED. DFW - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED ROW 26 LEFT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED SPLICE ON EMERGENCY EXIT LIGHT AT ROW 26 - [SDR AWXA200600407](https://openairdocs.org/sdr/AWXA200600407), Mar 1, 2006: LIGHT. INOPERATIVE. LAS - EEL - DURING OVERNIGHT MAINTENANCE, DISCOVERED THE EMERGENCY LIGHT INOPERATIVE AT ROW 26 LEFT. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT ROW - [SDR AWXA200600363](https://openairdocs.org/sdr/AWXA200600363), Feb 18, 2006: STIFFENER. CRACKED. MCN - DURING C4 CHECK DISCOVERED LEFT A/C BAY FRAME 39 INBOARD VERTICAL STIFFENER CRACKED 1.3" IN LENGTH. MAINTENANCE REMOVED AND INSTALLED NEW STIFFENER AT FRA - [SDR AWXA200600364](https://openairdocs.org/sdr/AWXA200600364), Feb 8, 2006: ATTACH ANGLE. CRACKED. MCN - DURING C4 CHECK DISCOVERED LEFT A/C BAY FRAME 39 STR 35L INSIDE AND OUTSIDE ATTACH ANGLE ON WEB CRACK 2.6" IN LENGTH. REMOVED AND INSTALLED NEW ATTACH ANG - [SDR AWXA200600362](https://openairdocs.org/sdr/AWXA200600362), Feb 8, 2006: SHEAR PLATE. CRACKED. MCN - DURING C4 CHECK DISCOVERED LEFT AIR CONDITIONING SHEAR PLATE CRACKED, 1.1 INCHES IN LENGTH, AT FS 39 AND STR 35L. MAINTENANCE STOP DRILLED CRACK IN SHEAR - [SDR AWXA200600335](https://openairdocs.org/sdr/AWXA200600335), Feb 7, 2006: SILL. CORRODED. MCN - DURING C4 CHECK DISCOVERED LEVEL 2 CORROSION ON THE BULK CARGO DOOR SILL, FORWARD END, UPPER SCREW HOLE AT FS 60 AND STR 38R. CORROSION WAS FOUND TO BE OU - [SDR AWXA200600418](https://openairdocs.org/sdr/AWXA200600418), Feb 5, 2006: FLOOR PANEL. DELAMINATED. MCN - DURING C4 CHECK DISCOVERED THE AFT RT FLOOR PANEL DELAMINATED FROM FR 64 TO FR 66 AT WL Z-240 AND FROM BL Y-765 TO BL Y-1292. MAINTENANCE REMOVED DAMAGED - [SDR AWXA200600367](https://openairdocs.org/sdr/AWXA200600367), Feb 4, 2006: INTERCOSTAL. CORRODED. MCN - DURING C4 CHECK DISCOVERED LEVEL 2 CORROSION ON INTERCOSTAL (BRIDGE ASSY) AT FS 59 ABOVE STR 38R AFT CARGO COMPARTMENT. REMOVED AND INSTALLED NEW INTERCOS - [SDR AWXA200600381](https://openairdocs.org/sdr/AWXA200600381), Jan 29, 2006: FITTING. CORRODED. MCN - DURING C4 CHECK IT WAS DISCOVERED THAT THE R1 DOOR AFT GIRT BAR ANGLE FITTING BRACKET WAS CORRODED AT FS 20. CORROSION WAS EVALUATED AT LEVEL 2 AND THE DA - [SDR AWXA200600377](https://openairdocs.org/sdr/AWXA200600377), Jan 29, 2006: SEAT TRACK. CORRODED. MCN - DURING C4 CHECK LEVEL 2 EXFOLIATION CORROSION WAS FOUND ON RIGHT HAND OUTBOARD SEAT TRACK FROM FS 20 TO FS 24. ORIGINAL DAMAGE WAS OUT OF LIMITS. MAINTENA - [SDR AWXA200600375](https://openairdocs.org/sdr/AWXA200600375), Jan 29, 2006: SEAT TRACK. CORRODED. MCN - DURING C4 CHECK IT WAS DISCOVERED THAT THE RIGHT INBOARD SEAT TRACK AT FS 20-24 HAD LEVEL 2 EXFOLIATION CORROSION 19" IN LENGTH, 3" WIDE AND 0.015" DEEP. - [SDR AWXA200600361](https://openairdocs.org/sdr/AWXA200600361), Jan 29, 2006: ATTACH FITTING. CORRODED. MCN - DURING C4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION LOCATED ON THE R1 LOWER SILL OUTBOARD ATTACH FITTING FROM FS 17 TO FS 19 AND AT STR 23R. NO CORROSIO - [SDR AWXA200600295](https://openairdocs.org/sdr/AWXA200600295), Jan 29, 2006: SEAT TRACK. CORRODED. MCN - DURING C4 CHECK DISCOVERED LEVEL 2 CORROSION ON THE LT OUTBOARD SEAT TRACK BETWEEN FS 46 AND FS 47 AT Y1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW A - [SDR AWXA200600294](https://openairdocs.org/sdr/AWXA200600294), Jan 29, 2006: SEAT TRACK. CORRODED. MCN - DURING C4 CHECK DISCOVERED LEVEL 2 CORROSION ON THE RT OUTBOARD SEAT TRACK BETWEEN FS 43 AND FS 44 AND AT Y-1292. CORROSION WAS FOUND TO BE OUT OF LIMITS - [SDR AWXA200600293](https://openairdocs.org/sdr/AWXA200600293), Jan 29, 2006: SEAT TRACK. CORRODED. MCN - DURING C4 CHECK DISCOVERED LEVEL 2 CORROSION ON THE RT OUTBOARD SEAT TRACK BETWEEN FS 36 AND FS 41 AND AT Y-1292. CORROSION WAS FOUND TO BE OUT OF LIMITS - [SDR AWXA200600292](https://openairdocs.org/sdr/AWXA200600292), Jan 29, 2006: SEAT TRACK. CORRODED. MCN - MAJOR REPAIR - DURING C4 CHECK DISCOVERED LEVEL 2 CORROSION ON THE LT INBOARD SEAT TRACK BETWEEN FS 41 AND FS 47 AND AT Y765. CORROSION WAS FOUND TO BE OU - [SDR AWXA200600291](https://openairdocs.org/sdr/AWXA200600291), Jan 29, 2006: SEAT TRACK. CORRODED. MCN - DURING C4 CHECK DISCOVERED LEVEL 2 CORROSION ON THE LT AND RT INBOARD SEAT TRACK AT FS 40 AND FROM Y765 TO Y-765. CORROSION WAS FOUND TO BE OUT OF LIMITS - [SDR AWXA200600282](https://openairdocs.org/sdr/AWXA200600282), Jan 29, 2006: FLOORBEAM. CORRODED. MCN - DURING C4 CHECK DISCOVERED CORROSION ON Y254 BEAM, AT FS 16 AND FS 20+4". CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-11-14 FIG 104. MAI - [SDR AWXA200600276](https://openairdocs.org/sdr/AWXA200600276), Jan 29, 2006: FLOORBEAM. CORRODED. MCN - DURING C4 CHECK DISCOVERED CORROSION ON THE Y-1350 FLOORBEAM PLATE AT FS 16. NO CORROSION REMOVAL LIMITS AVAILABLE IN THE AIRBUS SRM. MAINTENANCE REMOVED - [SDR AWXA200600368](https://openairdocs.org/sdr/AWXA200600368), Jan 28, 2006: FLOOR PANEL. DELAMINATED. MCN - DURING C4 INSPECTION IT WAS DISCOVERED THAT GALLEY FLOOR PANEL NR 261 WAS DELAMINATED. THE FLOORPANEL NR 261DF WAS REPAIRED IAW AIRBUS A320 SRM 53-12-00 F - [SDR AWXA200600274](https://openairdocs.org/sdr/AWXA200600274), Jan 28, 2006: FLOOR PANEL. CRACKED. MCN - DURING C4 CHECK DISCOVERED CABIN FLOOR PANEL, 221DF, CRACKED 6 INCHES. MAINTENANCE REMOVED FLOOR PANEL 221DF, FABRICATED REPLACEMENT PANEL AND INSTALLED I - [SDR AWXA200600273](https://openairdocs.org/sdr/AWXA200600273), Jan 28, 2006: FLOOR PANEL. DELAMINATED. MCN - DURING C4 CHECK DISCOVERED CABIN FLOOR PANEL, 232DF, DELAMINATED. MAINTENANCE REMOVED FLOOR PANEL 232DF AND FABRICATED REPLACEMENT PANEL AND INSTALLED IAW - [SDR AWXA200600369](https://openairdocs.org/sdr/AWXA200600369), Jan 27, 2006: SEAL. CORRODED. DURING C4 CHECK LEVEL 2 GALVANIC CORROSION WAS DISCOVERED ON FWD CARGO BAY DOOR THRESHOLD LOWER STRAP SEAL BUTT AT FS 27 JUST ABOVE NR 5 LATCH ROLLER. CORROSION - [SDR AWXA200600304](https://openairdocs.org/sdr/AWXA200600304), Jan 27, 2006: BEAM. CORRODED. MCN - DURING C4 CHECK DISCOVERED CORROSION ON 2 FASTENER HOLES AT THE FWD END OF THE BULK CARGO DOOR CUTOUT, LOWER SILL BEAM AT FR60+6" AND STR 38R. CORROSION W - [SDR AWXA200600289](https://openairdocs.org/sdr/AWXA200600289), Jan 26, 2006: BOLT. CORRODED. MCN - LEVEL 2 CORROSION WAS FOUND ON THE RT WING, SPOILERS 1 THROUGH 5, INNER HINGE PIN BOLTS AT THE THREAD AND HEAD RADIUS. NO CORROSION LIMITS WERE AVAILABLE. - [SDR AWXA200600275](https://openairdocs.org/sdr/AWXA200600275), Jan 26, 2006: FLOOR PANEL. CORRODED. MCN - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON THE AFT SIDE OF FLOOR PANEL 262FF. NO CORROSION REMOVAL LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTE - [SDR AWXA200600366](https://openairdocs.org/sdr/AWXA200600366), Jan 25, 2006: PLATE. CORRODED. DURING C4 CHECK LEVEL 2 CORROSION WAS FOUND ON THE R2 FORWARD GIRT FITTING PLATE AT FS 66 TO FS 67. MAINTENANCE REMOVED AND INSTALLED NEW PLATE ON THE R2 FWD GI - [SDR AWXA200600365](https://openairdocs.org/sdr/AWXA200600365), Jan 25, 2006: SHEAR PLATE. CORRODED. MCN - DURING C4 CHECK LEVEL 1 CORROSION WAS DISCOVERED ON THE BOTTOM SURFACE OF THE LEFT HAND LATERAL SHEAR PLATE AT Y1295 AND FS 69-70. MAINTENANCE REMOVED AND - [SDR AWXA200600303](https://openairdocs.org/sdr/AWXA200600303), Jan 25, 2006: BEAM. CORRODED. MCN - DURING C4 CHECK DISCOVERED CORROSION ON 2 FASTENER HOLES AT THE AFT END OF THE BULK CARGO DOOR CUTOUT, LOWER SILL BEAM AT FS 62 AND STR 38R. CORROSION WAS - [SDR AWXA200600290](https://openairdocs.org/sdr/AWXA200600290), Jan 25, 2006: BOLT. CORRODED. MCN - LEVEL 2 CORROSION WAS FOUND ON THE LT WING, SPOILERS 3 THROUGH 5, INNER HINGE PIN BOLTS AT THE THREAD AND HEAD RADIUS. NO CORROSION LIMITS WERE AVAILABLE. - [SDR AWXA200600288](https://openairdocs.org/sdr/AWXA200600288), Jan 25, 2006: FLOORBEAM. CORRODED. MCN - DURING C4 CHECK DISCOVERED CORROSION ON Y765 BEAM AND FS 68. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-04 FIG 102. MAINTENANCE REMO All 135: https://openairdocs.org/deregistered/N636AW-2009-11-03/reports.md ## Other aircraft with N636AW - [Cancelled 2019-05-02](https://openairdocs.org/deregistered/N636AW-2019-05-02): DJI PHANTOM 3 PROFESSION, S/N P78DCF28031646. Registration expired, pending cancellation. Owner: [Hill And Wilkinson](https://openairdocs.org/faa-owner/HILL%20AND%20WILKINSON), [Richardson, TX](https://openairdocs.org/faa-place/TX/Richardson) --- 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.