# Service difficulty reports: N636AW, cancelled Nov 3, 2009

A list on [N636AW, cancelled Nov 3, 2009](https://openairdocs.org/deregistered/N636AW-2009-11-03.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 3 · 135 reports

- [SDR USAA2009051191141](https://openairdocs.org/sdr/USAA2009051191141.md): Bracket · loose · May 9, 2009 · N636AW · Airbus A320231 · Emergency Lighting
  > FLT 632 - PHX - EEL - ROW 11D LOW LEVEL EMERGENCY LIGHTING DETACHED. MAINTENANCE RESECURED BRACKET AS REQUIRED.
- [SDR USAA2009032390648](https://openairdocs.org/sdr/USAA2009032390648.md): Slide Raft · misinstalled · Mar 21, 2009 · N636AW · Airbus A320231 · Escape Slide
  > 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.md): Slide Raft · misinstalled · Mar 21, 2009 · N636AW · Airbus A320231 · Escape Slide
  > 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.md): Cable · misrouted · Mar 21, 2009 · N636AW · Airbus A320231 · Escape Slide
  > 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.md): Power Supply · failed · May 2, 2008 · N636AW · Airbus A320231 · Emergency Lighting
  > 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 NORMAL.
- [SDR USAA920080753](https://openairdocs.org/sdr/USAA920080753.md): Ptu · defective · Apr 4, 2008 · N636AW · Airbus A320231 · Hydraulic System, Main
  > 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 FLUID FOR SHORT PERIOD. ELECTRIC YELLOW PUMP WAS NOT ACTIVATED. CREW DECLARED AN EMERGENCY AND RE
- [SDR USAA920071106](https://openairdocs.org/sdr/USAA920071106.md): Power Supply · defective · Nov 8, 2007 · N636AW · Airbus A320231 · Emergency Lighting
  > 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 449, OPS CHECK GOOD.
- [SDR USAA920070958](https://openairdocs.org/sdr/USAA920070958.md): Spar · delaminated · Oct 8, 2007 · N636AW · Airbus A320231 · Ailerons
  > 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 14057 IAW USAIRWAYS EA 120326A.
- [SDR USAA920070878](https://openairdocs.org/sdr/USAA920070878.md): Hinge Fitting · worn · Sep 29, 2007 · N636AW · Airbus A320231 · Elevator Tab, Attach Fittings
  > 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 HINGE ARM FITTING NR 2, HORIZONTAL STABILIZLER STATION 227 / RIB 6 IAW A320 SRM 51-72-11.
- [SDR USAA920070907](https://openairdocs.org/sdr/USAA920070907.md): Spar · cracked · Sep 25, 2007 · N636AW · Airbus A320231 · Nacelle/Pylon, Frame/Spar/Rib
  > 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.md): Stop · corroded · Sep 21, 2007 · N636AW · Airbus A320231 · Passenger/Crew Doors
  > 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.md): Seat Track · corroded · Sep 21, 2007 · N636AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > 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 51-72-11.
- [SDR USAA920070858](https://openairdocs.org/sdr/USAA920070858.md): Seat Track · corroded · Sep 21, 2007 · N636AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > 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 / FR 41 - BS 1976 / FR 47 IAW A320 SRM 51-72-11.
- [SDR AWXA200700844](https://openairdocs.org/sdr/AWXA200700844.md): Power Supply · failed · Jul 13, 2007 · N636AW · Airbus A320231 · Emergency Lighting
  > 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 CHECK WAS GOOD.
- [SDR AWXA200700103](https://openairdocs.org/sdr/AWXA200700103.md): Power Supply · failed · Jan 16, 2007 · N636AW · Airbus A320231 · Emergency Lighting
  > 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.md): Wire · broken · Sep 10, 2006 · N636AW · Airbus A320231 · Light System Wiring
  > 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 REPAIRED THE WIRING AT ROW 17, LEFT EMERGENCY ESCAPE PATH LIGHTS IAW ASM 33-51-00/04. OPS CHECK WA
- [SDR AWXA200601056](https://openairdocs.org/sdr/AWXA200601056.md): Shock Absorber · defective · Jun 28, 2006 · N636AW · Airbus A320231 · Nose/Tail Landing Gear Strut/Axle
  > 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 LANDING GEAR SHOCK ABSORBER FAULT. AFTER A FEW MINUTES THE CREW REPORTED THE MESSAGE CLEARED. THE CR
- [SDR AWXA200601007](https://openairdocs.org/sdr/AWXA200601007.md): Wire · broken · Jun 19, 2006 · N636AW · Airbus A320231 · Light System Wiring
  > PHX - EEL - NR 4099472 - DURING OVERNIGHT MAINTENANCE DISCOVERED ROW 24L EMERGENCY EXIT LIGHT INOP. MAINTENANCE RE-TERMINATED BROKEN WIRE AT CONNECTION IAW ESPM. OPERATIONAL CHECKS GOOD.
- [SDR AWXA200601005](https://openairdocs.org/sdr/AWXA200601005.md): Wire · broken · Jun 19, 2006 · N636AW · Airbus A320231 · Emergency Lighting
  > PHX - EEL - NR 4080757 - DURING OVERNIGHT MAINTENANCE DISCOVERED ROW 26L EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE IAW ESPM. OPERATIONAL CHECKS WERE GOOD.
- [SDR AWXA200600491](https://openairdocs.org/sdr/AWXA200600491.md): Splice · damaged · Mar 21, 2006 · N636AW · Airbus A320231 · Light System Wiring
  > DFW - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED ROW 26 LEFT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED SPLICE ON EMERGENCY EXIT LIGHT AT ROW 26 LEFT, OPERATIONAL CHECKS WERE GOOD.
- [SDR AWXA200600407](https://openairdocs.org/sdr/AWXA200600407.md): Light · inoperative · Mar 1, 2006 · N636AW · Airbus A320231 · Emergency Lighting
  > LAS - EEL - DURING OVERNIGHT MAINTENANCE, DISCOVERED THE EMERGENCY LIGHT INOPERATIVE AT ROW 26 LEFT. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT ROW 26 LEFT. OPERATIONAL CHECKS WERE GOOD.
- [SDR AWXA200600363](https://openairdocs.org/sdr/AWXA200600363.md): Stiffener · cracked · Feb 18, 2006 · N636AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > 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 FRAME 39 AND STR 35L IAW AIRBUS A320 SRM51-42-11 PGS 22 AND 23 AND SRM 51-72-11 PGS 1 AND 2.
- [SDR AWXA200600364](https://openairdocs.org/sdr/AWXA200600364.md): Attach Angle · cracked · Feb 8, 2006 · N636AW · Airbus A320231 · Fuselage Main, Attach Fittings
  > 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 ANGLES IN LT A/C BAY FS 39 STR35L IAW AIRBUS A320 SRM 51-72-11 PG 2 AND AIRBUS A320 SRM 51-42-11 PGS 2
- [SDR AWXA200600362](https://openairdocs.org/sdr/AWXA200600362.md): Shear Plate · cracked · Feb 8, 2006 · N636AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > 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 PLATE ON WEB AT LT AC BAY FR39 IAW AIRBUS 320 SRM 53-35-11 FIG 222. FABRICATED REPAIR DOUBLER IAW
- [SDR AWXA200600335](https://openairdocs.org/sdr/AWXA200600335.md): Sill · corroded · Feb 7, 2006 · N636AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > 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 OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-49 FIG 101. MAINTENANCE REMOVED DAMAGED AREA ON SILL BEAM IAW
- [SDR AWXA200600418](https://openairdocs.org/sdr/AWXA200600418.md): Floor Panel · delaminated · Feb 5, 2006 · N636AW · Airbus A320231 · Fuselage Floor Panel
  > 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 AREA AND BONDED REPAIR PATCH W/FILLER TO THE AFT RT FLOOR PANEL FROM FR 64 TO FR 66 AT WL Z-240 AND
- [SDR AWXA200600367](https://openairdocs.org/sdr/AWXA200600367.md): Intercostal · corroded · Feb 4, 2006 · N636AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > 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 INTERCOSTAL (BRIDGE ASSY) AT FS 59 ABOVE STR 38R AFT CARGO COMPARTMENT IAW AIRBUS A320 SRM 51-72-11 AND 51
- [SDR AWXA200600381](https://openairdocs.org/sdr/AWXA200600381.md): Fitting · corroded · Jan 29, 2006 · N636AW · Airbus A320231 · Escape Slide
  > 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 DAMAGE WAS 4.2" IN LENGTH, 0.007" WIDE AND 0.120" DEEP. MAINTENANCE REMOVED THE DAMAGED ANGLE FITTIN
- [SDR AWXA200600377](https://openairdocs.org/sdr/AWXA200600377.md): Seat Track · corroded · Jan 29, 2006 · N636AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > 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. MAINTENANCE REMOVED THE DAMAGED SEAT TRACK, FABRICATED 4 REPAIR ANGLES. INSTALLED NEW SEAT TRACK EXTRUSIO
- [SDR AWXA200600375](https://openairdocs.org/sdr/AWXA200600375.md): Seat Track · corroded · Jan 29, 2006 · N636AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > 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. ORIGINAL DAMAGE WAS OUT OF LIMITS PER A320 SRM 53-00-15 FIG 10. MAINTENANCE FABBED 4 NEW REPAIR AN
- [SDR AWXA200600361](https://openairdocs.org/sdr/AWXA200600361.md): Attach Fitting · corroded · Jan 29, 2006 · N636AW · Airbus A320231 · Fuselage Main, Attach Fittings
  > 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 CORROSION LIMITS AVAILABLE IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED NEW FITTING ON THE R1 LOWE
- [SDR AWXA200600295](https://openairdocs.org/sdr/AWXA200600295.md): Seat Track · corroded · Jan 29, 2006 · N636AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > 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 AIRBUS 320 SRM 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK ON THE LT OUTBOAR
- [SDR AWXA200600294](https://openairdocs.org/sdr/AWXA200600294.md): Seat Track · corroded · Jan 29, 2006 · N636AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > 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 IAW AIRBUS 320 SRM 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK ON THE RT OU
- [SDR AWXA200600293](https://openairdocs.org/sdr/AWXA200600293.md): Seat Track · corroded · Jan 29, 2006 · N636AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > 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 IAW AIRBUS 320 SRM 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK ON THE RT OU
- [SDR AWXA200600292](https://openairdocs.org/sdr/AWXA200600292.md): Seat Track · corroded · Jan 29, 2006 · N636AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > 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 OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK
- [SDR AWXA200600291](https://openairdocs.org/sdr/AWXA200600291.md): Seat Track · corroded · Jan 29, 2006 · N636AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > 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 IAW AIRBUS 320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK ON THE LT AN
- [SDR AWXA200600282](https://openairdocs.org/sdr/AWXA200600282.md): Floorbeam · corroded · Jan 29, 2006 · N636AW · Airbus A320231 · Fuselage Main, Floor Beam
  > 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. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM AT Y254 FROM FS 12 TO FS 24 IAW AIRBUS 320 SRM 51-47-
- [SDR AWXA200600276](https://openairdocs.org/sdr/AWXA200600276.md): Floorbeam · corroded · Jan 29, 2006 · N636AW · Airbus A320231 · Fuselage Main, Floor Beam
  > 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 AND INSTALLED NEW FLOOR BEAM PLATE AT Y-1350 AND FR16 IAW AIRBUS 320 SRM 51-42-11 FIG 8.
- [SDR AWXA200600368](https://openairdocs.org/sdr/AWXA200600368.md): Floor Panel · delaminated · Jan 28, 2006 · N636AW · Airbus A320231 · Fuselage Floor Panel
  > 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 FIG 204.
- [SDR AWXA200600274](https://openairdocs.org/sdr/AWXA200600274.md): Floor Panel · cracked · Jan 28, 2006 · N636AW · Airbus A320231 · Fuselage Floor Panel
  > MCN - DURING C4 CHECK DISCOVERED CABIN FLOOR PANEL, 221DF, CRACKED 6 INCHES. MAINTENANCE REMOVED FLOOR PANEL 221DF, FABRICATED REPLACEMENT PANEL AND INSTALLED IAW AIRBUS DWG D53610334.
- [SDR AWXA200600273](https://openairdocs.org/sdr/AWXA200600273.md): Floor Panel · delaminated · Jan 28, 2006 · N636AW · Airbus A320231 · Fuselage Floor Panel
  > MCN - DURING C4 CHECK DISCOVERED CABIN FLOOR PANEL, 232DF, DELAMINATED. MAINTENANCE REMOVED FLOOR PANEL 232DF AND FABRICATED REPLACEMENT PANEL AND INSTALLED IAW AIRBUS DWG D53610331.
- [SDR AWXA200600369](https://openairdocs.org/sdr/AWXA200600369.md): Seal · corroded · Jan 27, 2006 · N636AW · Airbus A320231 · Cargo/Baggage Doors
  > 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 WAS 4.5" IN LENGTH AND 1" WIDE. MAINTENANCE REMOVED AND INSTALLED NEW STRAP SEAL BUTT AT FS 27 JU
- [SDR AWXA200600304](https://openairdocs.org/sdr/AWXA200600304.md): Beam · corroded · Jan 27, 2006 · N636AW · Airbus A320231 · Fuselage Main, Structure
  > 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 WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-49 FIG 203. MAINTENANCE REMOVED DAMAGE FROM
- [SDR AWXA200600289](https://openairdocs.org/sdr/AWXA200600289.md): Bolt · corroded · Jan 26, 2006 · N636AW · Airbus A320231 · Spoilers
  > 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. ALL SPOILER, INNER HINGE, PIN BOLTS WERE REMOVED AND REPLACED ON SPOILERS 1 THROUGH 5 IAW AIRBUS
- [SDR AWXA200600275](https://openairdocs.org/sdr/AWXA200600275.md): Floor Panel · corroded · Jan 26, 2006 · N636AW · Airbus A320231 · Fuselage Floor Panel
  > 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. MAINTENANCE REMOVED FLOOR PANEL 262FF AND INSTALLED NEW FLOOR PANEL.
- [SDR AWXA200600366](https://openairdocs.org/sdr/AWXA200600366.md): Plate · corroded · Jan 25, 2006 · N636AW · Airbus A320231 · Escape Slide
  > 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 GIRT FITTING AT FS 66 TO FS 67 IAW AIRBUS A320 AMM 52-11-31. CORROSION HAS BEEN RE-LEVELED TO A LEVE
- [SDR AWXA200600365](https://openairdocs.org/sdr/AWXA200600365.md): Shear Plate · corroded · Jan 25, 2006 · N636AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > 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 INSTALLED NEW LATERAL SHEAR PLATE AT Y1295 AND FS 69-70 IAW AIRBUS A320 SRM 51-42-11 PGS 22-23 FIG
- [SDR AWXA200600303](https://openairdocs.org/sdr/AWXA200600303.md): Beam · corroded · Jan 25, 2006 · N636AW · Airbus A320231 · Fuselage Main, Structure
  > 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 FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-49 FIG 203. MAINTENANCE REMOVED DAMAGE FROM TH
- [SDR AWXA200600290](https://openairdocs.org/sdr/AWXA200600290.md): Bolt · corroded · Jan 25, 2006 · N636AW · Airbus A320231 · Spoilers
  > 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. ALL SPOILER, INNER HINGE, PIN BOLTS WERE REMOVED AND REPLACED ON THE LT WING, SPOILERS 3 THROUGH
- [SDR AWXA200600288](https://openairdocs.org/sdr/AWXA200600288.md): Floorbeam · corroded · Jan 25, 2006 · N636AW · Airbus A320231 · Fuselage Main, Floor Beam
  > 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 REMOVED AND INSTALLED NEW FLOORBEAM AT Y765 AND FS 68 IAW AIRBUS 320 SRM 51-72-11.

Next page: https://openairdocs.org/deregistered/N636AW-2009-11-03/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 = 'N636AW' AND deregistration_id = 'N636AW-2009-11-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N636AW-2009-11-03/reports

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