# Service difficulty reports: N323AW, cancelled Jun 23, 2006

A list on [N323AW, cancelled Jun 23, 2006](https://openairdocs.org/deregistered/N323AW-2006-06-23.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 · 153 reports

- [SDR AWXA200600229](https://openairdocs.org/sdr/AWXA200600229.md): Battery · inoperative · Jan 31, 2006 · N323AW · Boeing 7373Y0 · Emergency Equipment
  > MCN - EEL - DURING C16 CHECK DISCOVERED 2 EMERGENCY FLASHLIGHTS ON THE FORWARD WALL OF AFT LT LAV INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH FLASHLIGHT BATTERIES ON THE FORWARD WALL OF THE AFT LT LAV. OPERATIONAL CHECKS WERE GOOD.
- [SDR AWXA200600195](https://openairdocs.org/sdr/AWXA200600195.md): Support Fitting · cracked · Jan 18, 2006 · N323AW · Boeing 7373Y0 · Fuselage, Landing Gear Attach Fittings
  > MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED RT MLG SUPPORT BEAM OUTBOARD AFT SUPPORT FITTING CRACKED 2.75 INCHES IN LENGTH. MAINTENANCE REMOVED AND REPLACED THE RT MLG SUPPORT BEAM, OUTBOARD AFT SUPPORT FITTING IAW AMERICA WEST AIRLINES ENGINEERING REPAI
- [SDR AWXA200600085](https://openairdocs.org/sdr/AWXA200600085.md): Stringer Clip · cracked · Dec 30, 2005 · N323AW · Boeing 7373Y0 · Fuselage Main, Attach Fittings
  > MCN - DURING C16 CHECK DISCOVERED STRINGER TIE CRACKED,.50 INCHES, AT STR 10L. AND BS 1006. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE AT STR 10L AND BS 1006 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12.
- [SDR AWXA200600084](https://openairdocs.org/sdr/AWXA200600084.md): Stringer Clip · cracked · Dec 30, 2005 · N323AW · Boeing 7373Y0 · Fuselage Main, Attach Fittings
  > MCN - DURING C16 CHECK DISCOVERED STRINGER TIE CRACKED,.75 INCHES, AT STR 5L. AND BS 1006. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE AT STR 5L AND BS 1006 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12.
- [SDR AWXA200600015](https://openairdocs.org/sdr/AWXA200600015.md): Regulator · stuck · Dec 28, 2005 · N323AW · Boeing 7373Y0 · Crew Oxygen System
  > EMERGENCY EQUIPMENT, DURING C 16 CHECK DISCOVERED CAPTAIN'S OXYGEN MASK DEMAND REGULATOR STUCK IN EMERGENCY POSITION. MAINTENANCE REMOVED AND REPLACED THE O2 MASK IAW TASK CARD R1B35001. OPERATIONAL CHECKS WERE GOOD. VENDOR TEAR DOWN DOES NOT CONFIRM FAULT.
- [SDR AWXA200600087](https://openairdocs.org/sdr/AWXA200600087.md): Angle · cracked · Dec 21, 2005 · N323AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > MCN - DURING C16 CHECK DISCOVERED REINFORCEMENT ANGLE CRACKED AT BS 294.5, WL 208 AND FROM BL 40R TO BL 55R. MAINTENANCE REMOVED AND INSTALLED FABRICATED REINFORCEMENT ANGLE IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 12, 13, 14 AND BOEING DWG 65-45808.
- [SDR AWXA200600197](https://openairdocs.org/sdr/AWXA200600197.md): Floorbeam · corroded · Dec 18, 2005 · N323AW · Boeing 7373Y0 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED LEVEL TWO CORROSION ON FLOORBEAM LOCATED AT BS 294.5, WL 207 AND BL 44R. RE-WORK WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-05-1A FIG 101. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM IAW B
- [SDR AWXA200600108](https://openairdocs.org/sdr/AWXA200600108.md): Structure · corroded · Dec 18, 2005 · N323AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > MCN - DURING C19 CHECK DISCOVERED CORROSION ON RT CHORD FROM BS 288 TO BS 292, WL 208 AND BL 52R. REMOVED CORROSION AND RE-WORK WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-15-1A1 FIG 101. MAINTENANCE REMOVED THE RT CHORD FROM BS 288 TO BS 292,
- [SDR AWXA200600083](https://openairdocs.org/sdr/AWXA200600083.md): Stringer Clip · cracked · Dec 16, 2005 · N323AW · Boeing 7373Y0 · Fuselage Main, Attach Fittings
  > MCN - DURING C16 CHECK DISCOVERED STRINGER CLIP CRACKED,.25 INCHES, AT STR 8L AND BS 1006. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP AT STR 8L AND BS 1006 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12.
- [SDR AWXA200600082](https://openairdocs.org/sdr/AWXA200600082.md): Stringer Clip · cracked · Dec 16, 2005 · N323AW · Boeing 7373Y0 · Fuselage Main, Attach Fittings
  > MCN - DURING C16 CHECK DISCOVERED STRINGER TIE CRACKED,.25 INCHES, AT STR 7L. AND BS 1006. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE AT STR 7L AND BS 1006 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12.
- [SDR AWXA200600092](https://openairdocs.org/sdr/AWXA200600092.md): Skin · debonded · Dec 15, 2005 · N323AW · Boeing 7373Y0 · Trailing Edge Flaps
  > MCN - DURING C16 CHECK DISCOVERED LT OUTBOARD AFT FLAP DISBONDED 3" FROM THE INBOARD EDGE FROM WS 230.68L TO WS 232.68L. MAINTENANCE REMOVED DISBONDED SKIN IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R
- [SDR AWXA200600081](https://openairdocs.org/sdr/AWXA200600081.md): Stringer · damaged · Dec 14, 2005 · N323AW · Boeing 7373Y0 · Fuselage Main, Longeron/Stringer
  > MCN - DURING C16 CHECK DISCOVERED STRINGER 9R, BS 907 TO BS 947, HAS 1/4" HOLE IN IT. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER AT STRINGER 9R, BS 907 TO BS 947, IAW BOEING 737-300 SRM 51-40-02-0G FIG 12.
- [SDR AWXA200600196](https://openairdocs.org/sdr/AWXA200600196.md): Wire Harness · damaged · Dec 13, 2005 · N323AW · Boeing 7373Y0 · Light System Wiring
  > MCN - EEL - DURING C16 CHECK DISCOVERED EMERGENCY ESCAPE PATH LIGHT HARNESS DAMAGED FROM BS 360 TO BS947, WL 208 AND BL 26L. MAINTENANCE REPAIRED SPLICES AND CONNECTORS ON THE EMERGENCY ESCAPE PATH LIGHT HARNESS IAW BOEING SWPM 20-13-12. REMOVED AND REPLACED
- [SDR AWXA200600095](https://openairdocs.org/sdr/AWXA200600095.md): Skin · cracked · Dec 9, 2005 · N323AW · Boeing 7373Y0 · Fuselage Main, Plate/Skin
  > MCN - DURING C16 CHECK DISCOVERED, THE R1 DOOR LOWER HINGE CUTOUT, LOWER RADIUS, CRACKED,.25 INCHES AT BS 294 AND STRINGER 13R. MAINTENANCE CUTOUT DAMAGED AREA AT THE R1 DOOR HINGE CUTOUT RADIUS IAW AMERICA WEST AIRLINES ENGINEERING NR 03-5240-05349-RC1. FA
- [SDR AWXA200600094](https://openairdocs.org/sdr/AWXA200600094.md): Frame · cracked · Dec 9, 2005 · N323AW · Boeing 7373Y0 · Fuselage Main, Frame
  > MCN - DURING C16 CHECK DISCOVERED THE L2 DOOR FRAME CRACKED,.125 INCHES, AT BS 957 JUST BELOW STR 8L. MAINTENANCE REMOVED CRACKED L2 DOOR FRAME FROM BS 957, STRINGER 8L AND INSTALLED A NEW FRAME AT THE L2 DOOR, BS 957 JUST BELOW STR 8L IAW BOEING 737-300 SRM
- [SDR AWXA200600080](https://openairdocs.org/sdr/AWXA200600080.md): Channel · cracked · Dec 9, 2005 · N323AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > MCN - DURING C16 CHECK DISCOVERED CHANNEL CRACKED, 1.1 INCHES, AT BS 907 AND STR 4R. MAINTENANCE REMOVED AND INSTALLED NEW CHANNEL AT BS 907 AND STR 4R IAW BOEING 737-300 SRM 51-40-02-0G FIG 8 AND 12.
- [SDR AWXA200600079](https://openairdocs.org/sdr/AWXA200600079.md): Channel · cracked · Dec 9, 2005 · N323AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > MCN - DURING C16 CHECK DISCOVERED CHANNEL CRACKED, 1.2 INCHES, AT BS 907 AND STR 4L. MAINTENANCE REMOVED AND INSTALLED NEW CHANNEL AT BS 907 AND STR 4L IAW BOEING 737-300 SRM 51-40-02-0G FIG 8 AND 12.
- [SDR AWXA200600097](https://openairdocs.org/sdr/AWXA200600097.md): Skin · cracked · Dec 7, 2005 · N323AW · Boeing 7373Y0 · Leading Edge Devices
  > MCN - DURING C16 CHECK DISCOVERED 5 CRACKS,.80 INCHES EACH, ON THE BOTTOM OF THE NR 6 SLAT SKIN, FROM SS 320R TO SS 325R. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FAB`D FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-4
- [SDR AWXA200600096](https://openairdocs.org/sdr/AWXA200600096.md): Skin · cracked · Dec 7, 2005 · N323AW · Boeing 7373Y0 · Leading Edge Devices
  > MCN - DURING C16 CHECK DISCOVERED 4 CRACKS,.500 INCHES EACH, ON THE BOTTOM OF THE NR 4 SLAT SKIN, FROM SS 57R TO SS 61R. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM
- [SDR AWXA200600089](https://openairdocs.org/sdr/AWXA200600089.md): Support · corroded · Dec 7, 2005 · N323AW · Boeing 7373Y0 · Fuselage, Landing Gear Attach Fittings
  > MCN - DURING C16 CHECK DISCOVERED CORROSION AROUND 4 FASTENER HOLES ON LOWER SURFACE OF THE RT MLG AFT SUPPORT BEAM. MAINTENANCE REMOVED CORROSION ON LOWER SURFACE OF THE RT MLG AFT SUPPORT BEAM IAW BOEING 737-300 SRM 51-10-02-0G. MATERIAL LOSS WAS BEYOND DE
- [SDR AWXA200600093](https://openairdocs.org/sdr/AWXA200600093.md): Skin · debonded · Dec 6, 2005 · N323AW · Boeing 7373Y0 · Spoilers
  > MCN - DURING C16 CHECK DISCOVERED TWO SPOTS OF DISBOND ON THE NR 6 SPOILER, LOWER SURFACE, FROM WBL 228.53R TO WBL 330.53R. MAINTENANCE REMOVED DISBONDED SKIN AND CORE IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 203. FABRICATED REPLACEMENT CORE AND DOUBLER IAW B
- [SDR AWXA200600086](https://openairdocs.org/sdr/AWXA200600086.md): Shear Tie · corroded · Dec 6, 2005 · N323AW · Boeing 7373Y0 · Fuselage Internal Mounting Structure
  > MCN - DURING C16 CHECK DISCOVERED CORROSION ON INTERCOSTAL SHEAR TIE BETWEEN STATIONS 727A AND 727B AT BL 17L IN THE AFT PIT. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-04-1A1. REMOVED AND INSTALLED NEW FABRICATED SHEAR TIE
- [SDR AWXA200600078](https://openairdocs.org/sdr/AWXA200600078.md): Channel · cracked · Dec 6, 2005 · N323AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > MCN - DURING C16 CHECK DISCOVERED CHANNEL CRACKED,.75 INCHES, AT BS 540, WL 206 AND BL 1L. MAINTENANCE REMOVED AND INSTALLED NEW CHANNEL ASSY AT BS 540, WL 206 AND BL 1L IAW BOEING 737-300 SRM 51-40-02-0G FIG 12.
- [SDR AWXA200600077](https://openairdocs.org/sdr/AWXA200600077.md): Channel · cracked · Dec 6, 2005 · N323AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > MCN - DURING C16 CHECK DISCOVERED CHANNEL CRACKED,.7 INCHES, AT BS 540, WL 206 AND BL 1R. MAINTENANCE REMOVED AND INSTALLED NEW CHANNEL ASSY AT BS 540, WL 206 AND BL 1R IAW BOEING 737-300 SRM 51-40-02-0G FIG 12.
- [SDR AWXA200600099](https://openairdocs.org/sdr/AWXA200600099.md): Skin · cracked · Dec 5, 2005 · N323AW · Boeing 7373Y0 · Leading Edge Devices
  > MCN - DURING C16 CHECK DISCOVERED 1 CRACK,.375 INCHES, ON THE BOTTOM OF THE NR 3 SLAT SKIN, AT SS 92L. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 2
- [SDR AWXA200600098](https://openairdocs.org/sdr/AWXA200600098.md): Skin · cracked · Dec 5, 2005 · N323AW · Boeing 7373Y0 · Leading Edge Devices
  > MCN - DURING C16 CHECK DISCOVERED 2 CRACKS ON THE BOTTOM OF THE NR 3 SLAT SKIN, FROM SS 67L TO SS 69L. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 20
- [SDR AWXA200600090](https://openairdocs.org/sdr/AWXA200600090.md): Skin · delaminated · Dec 5, 2005 · N323AW · Boeing 7373Y0 · Trailing Edge Flaps
  > MCN - DURING C16 CHECK DISCOVERED LT OUTBOARD AFT FLAP DELAMINATED AT THE INBOARD TRAILING EDGE FROM WS 230.68L TO WS 234.68L. MAINTENANCE REMOVED DISBONDED SKIN AND CORE IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPLACEMENT CORE AND DOUBLER IAW BOEING
- [SDR AWXA200600088](https://openairdocs.org/sdr/AWXA200600088.md): Intercostal · cracked · Dec 4, 2005 · N323AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > MCN - DURING C16 CHECK DISCOVERED INTERCOSTAL CRACKED, 1.5 INCHES, AT BS 347 ABOVE THE E-2 SHELF, BL 11.1 AND WL 207. MAINTENANCE REMOVED AND INSTALLED FABRICATED INTERCOSTAL FROM BS 344 TO BS 360, BL 11.10L AND WL 207 IAW AMERICA WEST AIRLINES ENGINEERING RE
- [SDR AWXA200600091](https://openairdocs.org/sdr/AWXA200600091.md): Skin · delaminated · Dec 3, 2005 · N323AW · Boeing 7373Y0 · Trailing Edge Flaps
  > MCN - DURING C16 CHECK DISCOVERED RT OUTBOARD AFT FLAP DELAMINATED AT THE INBOARD TRAILING EDGE FROM WBL 289R TO WBL 309R. MAINTENANCE REMOVED DISBONDED SKIN AND CORE IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPLACEMENT CORE AND DOUBLER IAW BOEING 737
- [SDR AWXA200501130](https://openairdocs.org/sdr/AWXA200501130.md): Wire Harness · inoperative · Sep 28, 2005 · N323AW · Boeing 7373Y0 · Light System Wiring
  > PHX - EEL - DURING 8 DAY CHECK, DISCOVERED ROW 16, EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY WIRE HARNESS AT ROW 16. OPERATIONAL TESTS WERE GOOD.
- [SDR AWXA200500990](https://openairdocs.org/sdr/AWXA200500990.md): Wire · inoperative · Aug 22, 2005 · N323AW · Boeing 7373Y0 · Light System Wiring
  > PHX - EEL - DURING 8 DAY CHECK, DISCOVERED EMERGENCY ESCAPE PATH LIGHTING FOR SEAT 11 TO 15 ON THE LT SIDE INOPERATIVE. MAINTENANCE REPAIRED A WIRE AT SEAT 15 IAW BOEING 737-300 WDM TR 33-042AW. OPERATIONAL CHECKS WERE GOOD.
- [SDR AWXA200500913](https://openairdocs.org/sdr/AWXA200500913.md): Wire Harness · damaged · Aug 7, 2005 · N323AW · Boeing 7373Y0 · Light System Wiring
  > DEN - EEL - DURING 4 DAY CHECK DISCOVERED ROW 22L, SEAT MOUNTED, EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHTING SEAT HARNESS AT ROW 22L. OPERATIONAL CHECKS GOOD.
- [SDR AWXA200500850](https://openairdocs.org/sdr/AWXA200500850.md): Wire · failed · Jul 25, 2005 · N323AW · Boeing 7374Y0 · Windshield/Door Rain/Ice Removal
  > PHX - SMOKE - FLT 0075 - PILOT REPORTED ON GROUND THAT THE A1 CB POPPING AND WONT RESET. MAINTENANCE REMOVED AND REPLACED THE PITOT STATIC WINDOW HEAT MODULE ON P5. ALSO, SEVERAL WIRES WERE BURNED IN THAT VICINITY. REMOVED AND REPLACED WIRES ON WINDOW HEAT
- [SDR AWXA200500768](https://openairdocs.org/sdr/AWXA200500768.md): Girt Bar · loose · Jun 29, 2005 · N323AW · Boeing 7373Y0 · Escape Slide
  > DURING GROUND HANDLING CREW REPORTED DOOR L1 SLIDE/GIRT BAR LOOSE. MAINTENANCE REPACKED L1 DOOR SLIDE GIRT BAR AND SLIDE IAW AMERICA WEST AIRLINES TASKCARD R1C25001.
- [SDR AWXA200500737](https://openairdocs.org/sdr/AWXA200500737.md): Wire · broken · Jun 22, 2005 · N323AW · Boeing 737300 · Light System Wiring
  > FOUND EMERGENCY EXIT LIGHTS AT ROWS 11 THROUGH ROW 15 ESCAPE PATH LIGHTING INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE. SEATS OPERATIONAL CHECKS GOOD.
- [SDR AWXA200500562](https://openairdocs.org/sdr/AWXA200500562.md): Csd · failed · May 13, 2005 · N323AW · Boeing 7373Y0 · Alternator-Generator Drive
  > EN ROUTE NR 1 CONSTANT SPEED DRIVE (CSD) LOW OIL PRESSURE LIGHT ILLUMINATED & NR 1 GENERATOR DROPPED OFF LINE, APU ALREADY ON MEL, DIVERTED INTO RNO FOR REPAIR. MX R & R NR 1 CSD / GENERATOR IAW T/C R5M24007, AND CSD OIL COOLER AND IN-LINE FILTER IAW T/C R5M2
- [SDR AWXA200500537](https://openairdocs.org/sdr/AWXA200500537.md): Indicator · faulty · May 4, 2005 · N323AW · Boeing 7373Y0 · Trailing Flap Position Indicating System
  > ON APPROACH, T/E FLAPS WOULD NOT EXTEND PAST 8 DEGREES, L/E FLAP INTRANSIT LIGHT REMAINED ILLUMINATED. MX R & R THE T/E FLAP POSITION INDICATOR IAW 27-58-41. DURING OPS CHECK A LOUD POPPING SOUND OBSERVED COMING FROM NR 3 SLAT AREA. MX FOUND THE NR 3 SLAT O
- [SDR AWXA200500304](https://openairdocs.org/sdr/AWXA200500304.md): Module · faulty · Mar 3, 2005 · N323AW · Boeing 7373Y0 · Hydraulic System, Main
  > AFTER DEPARTURE AT APPROXIMATELY 1,000 FT A-SYSTEM HYDRAULICS AND FEEL DIFFERENTIAL LIGHT ILLUMINATED, TURNED BACK TO PHX, FLIGHT CONTROLS FELT STIFF BUT FUNCTIONAL. MAINTENANCE FOUND A-SYSTEM FLIGHT CONTROL MODULAR PACKAGE FAULTING, REPLACED MODULAR PACKAGE
- [SDR AWXA200500101](https://openairdocs.org/sdr/AWXA200500101.md): Wire Harness · broken · Jan 31, 2005 · N323AW · Boeing 7373Y0 · Light System Wiring
  > PHX - EEL - DURING 4-DAY CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LEFT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED WIRE HARNESS TO EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200401317](https://openairdocs.org/sdr/AWXA200401317.md): Attach Angle · corroded · Nov 12, 2004 · N323AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-15 CHECK A.5 INCH CRACK WAS FOUND IN UPPER ATTACH ANGLE OF FLOOR INTERCOSTAL BETWEEN BS 380 AND BS 400, BL 0. MAINTENANCE REMOVED CORRODED UPPER ATTACH ANGLE ON FLOOR INTERCOSTAL FROM BS 380 TO BS 400, BL 0; FABRICATED A NEW REP
- [SDR AWXA200401352](https://openairdocs.org/sdr/AWXA200401352.md): Doubler · cracked · Nov 11, 2004 · N323AW · Boeing 7373Y0 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-15 CHECK A 3/8 INCH CRACK WAS FOUND IN TCAS EXTERNAL DOUBLER SKIN LOCATED BETWEEN BS 380 AND BS 390, STR 1 RT AND STR 2 RT. MAINTENANCE STOP DRILLED CRACK AND PERFORMED AN HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED. FABRICATE
- [SDR AWXA200401348](https://openairdocs.org/sdr/AWXA200401348.md): Panel · cracked · Nov 4, 2004 · N323AW · Boeing 7373Y0 · Spoilers
  > MCN - FLIGHT CONTROL - DURING C-15 CHECK A.50 CRACK WAS FOUND ON NR 4 SPOILER CENTER OUTBOARD HINGE. MAINTENANCE REMOVED AND REPLACED NR 4 SPOILER PANEL ASSEMBLY IAW AMM 27-62-12.
- [SDR AWXA200401284](https://openairdocs.org/sdr/AWXA200401284.md): Slide · frayed · Nov 4, 2004 · N323AW · Boeing 7373Y0 · Escape Slide
  > MCN - EES - DURING C-15 CHECK THE R-2 DOOR EMERGENCY ESCAPE SLIDE WEBBING WAS FOUND FRAYED. MAINTENANCE REPLACED THE R-2 DOOR EMERGENCY ESCAPE SLIDE WEBBING IAW B737-300 SRM 51-40-02 FIG 3-4, & 6-8.
- [SDR AWXA200401351](https://openairdocs.org/sdr/AWXA200401351.md): Shear Tie · corroded · Nov 3, 2004 · N323AW · Boeing 7373Y0 · Fuselage Main, Structure
  > MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR TIE AND BEAR STRAP IN AFT BILGE AREA BS 967, BL "0". MAINTENANCE REMOVED SHEAR TIE AND AFTER CLEANING OFF CORROSION FOUND NO MATERIAL LOSS. TRIMMED OUT CORRODED AREA OF BEAR STRA
- [SDR AWXA200401347](https://openairdocs.org/sdr/AWXA200401347.md): Angle · corroded · Nov 3, 2004 · N323AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > DURING C-15 CHECK, CORROSION WAS FOUND ON ATTACH ANGLE AT BOTTOM OF L-2 CREASE BEAM INNER CHORD BETWEEN BS 969 AND BS 979, LBL 49. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED ATTACH ANGLE BS 969 - 979, LBL 4
- [SDR AWXA200401244](https://openairdocs.org/sdr/AWXA200401244.md): Skin · debonded · Nov 3, 2004 · N323AW · Boeing 7373Y0 · Leading Edge Devices
  > DURING C-15 CHECK, AN AREA OF DISBOND WAS FOUND ON LT WING NR 3 SLAT INBOARD TRAILING EDGE TIP BETWEEN SLAT STA 12.25 AND 15.25 LT. MAINTENANCE REMOVED DISBONED NR 3 SLAT SKIN; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10,
- [SDR AWXA200401303](https://openairdocs.org/sdr/AWXA200401303.md): Skin · cracked · Nov 2, 2004 · N323AW · Boeing 7373Y0 · Leading Edge Devices
  > MCN - MAJOR REPAIR - DURING C-15 CHECK 3 EACH.125 INCH CRACKS WERE FOUND IN NR 6 SLAT LOWER SKIN AT AFT ROW RIVET HOLES INBOARD OF ACTUATOR ATTACH FITTINGS SLAT STA 291 RT THRU SLAT STA 294 RT. MAINTENANCE CUT OUT DAMAGE IN NR 6 SLAT LOWER SKIN FROM SS 291 R
- [SDR AWXA200401245](https://openairdocs.org/sdr/AWXA200401245.md): Tab · debonded · Nov 2, 2004 · N323AW · Boeing 737300 · Aileron Tabs
  > DURING C-15 CHECK AN AREA OF DISBOND WAS FOUND ON RT AILERON TAB AT OUTBOARD AFT CORNER BETWEEN WBL 479.75 AND WBL 480 RT. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-06, FIG 13.
- [SDR AWXA200401290](https://openairdocs.org/sdr/AWXA200401290.md): Door Frame · cracked · Nov 1, 2004 · N323AW · Boeing 7373Y0 · Passenger/Crew Doors
  > MCN - MAJOR REPAIR - DURING C-15 CHECK A.125 INCH CRACK WAS FOUND IN AFT EDGE OF R-1 DOOR AT 4TH DOOR STOP FROM BOTTOM BS 312, STR 12 RT. MAINTENANCE TRIMMED OUT CRACK IN AFT EDGE OF R-1 DOOR AT 4TH DOOR STOP FROM BOTTOM BS 312, STR 12 RT. PERFORMED HFEC IN
- [SDR AWXA200401289](https://openairdocs.org/sdr/AWXA200401289.md): Door Frame · cracked · Nov 1, 2004 · N323AW · Boeing 7373Y0 · Passenger/Crew Doors
  > MCN - MAJOR REPAIR - DURING C-15 CHECK A.125 INCH CRACK WAS FOUND IN AFT EDGE OF R-1 DOOR AT 3RD DOOR STOP FROM BOTTOM BS 312, STR 13 RT. MAINTENANCE STOP DRILLED CRACK IN AFT EDGE OF R-1 DOOR AT 3RD DOOR STOP FROM BOTTOM BS 312, STR 13 RT. PERFORMED HFEC I

Next page: https://openairdocs.org/deregistered/N323AW-2006-06-23/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 = 'N323AW' AND deregistration_id = 'N323AW-2006-06-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N323AW-2006-06-23/reports

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