# Service difficulty reports: N334AW, cancelled Jul 16, 2012

A list on [N334AW, cancelled Jul 16, 2012](https://openairdocs.org/deregistered/N334AW-2012-07-16.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 7 · 311 reports

- [SDR USAA2012012400002](https://openairdocs.org/sdr/USAA2012012400002.md): Sign · damaged · Jan 21, 2012 · N334AW · Boeing 7373Y0 · Emergency Lighting
  > C21 CHECK - AFT CLOSET LOWER EXIT SIGN DAMAGED. REPLACED AFT CLOSET LOWER EXIT SIGN AS NEEDED.
- [SDR USAA2012013000005](https://openairdocs.org/sdr/USAA2012013000005.md): Skin · cracked · Jan 10, 2012 · N334AW · Boeing 7373Y0 · Fuselage Main, Plate/Skin
  > C21 CHECK - 1.7 INCH CRACK IN FUSELAGE SKIN AT BS 874, S25R. REPAIRED FUSELAGE SKIN AT BS 874, S25R IAW B737 SRM 53-00-01-2R-31 FIG 201.
- [SDR USAA2012013000007](https://openairdocs.org/sdr/USAA2012013000007.md): Door Frame · cracked · Jan 6, 2012 · N334AW · Boeing 7373Y0 · Passenger/Crew Doors
  > C21 CHECK -.250 INCH LONG CRACK IN L1 DOOR AFT DOOR FRAME AT NR 6 STOP FITTING AT BS 344, WL 255. REPAIRED L1 DOOR AFT DOOR FRAME AT NR 6 STOP FITTING AT BS 344, WL 255 IAW EA 130781.
- [SDR USAA2012011800014](https://openairdocs.org/sdr/USAA2012011800014.md): Stringer · cracked · Jan 3, 2012 · N334AW · Boeing 7373Y0 · Fuselage Main, Longeron/Stringer
  > C21 CHECK - CRACK ON STRINGER AT BS 440, S28R. REPAIRED STRINGER AT BS 440, S28R IAW B737-300 SRM 53-00-03-2R-1 FIG 201.
- [SDR USAA2012010900020](https://openairdocs.org/sdr/USAA2012010900020.md): Support · corroded · Dec 30, 2011 · N334AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > C21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON WEB SUPPORT BETWEEN BS 1001 TO BS 1005, WL 208, BETWEEN LBL 41 TO LBL 42. REPLACED WEB SUPPORT BETWEEN BS 1001 TO BS 1005, WL 208, BETWEEN LBL 41 TO LBL 42 IAW B737-300 SRM 51-40-02-0G FIGURE 11 AND 16.
- [SDR USAA2012012500003](https://openairdocs.org/sdr/USAA2012012500003.md): Angle · corroded · Dec 20, 2011 · N334AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > C21 CHECK - CORROSION ON SPLICE ANGLE AT BS 317, WL 208, LBL 54. REPLACED SPLICE ANGLE AT BS 317, WL 208, LBL 54 IAW B737 SRM 51-40-02-0G FIG 12.
- [SDR USAA2011122700010](https://openairdocs.org/sdr/USAA2011122700010.md): Lens · crazed · Dec 20, 2011 · N334AW · Boeing 7373Y0 · Emergency Lighting
  > EXTERNAL FUSELAGE RT OVER WING EMERGENCY EXIT LIGHT LENS COVER IS CRAZED AFT OF EXIT DOOR. REMOVED AND REPLACED RT OVERWING EMERGENCY EXIT LIGHT LENS COVER EXTERNAL FUSELAGE AFT EXIT DOOR IAW B737 AMM.
- [SDR USAA2012012300006](https://openairdocs.org/sdr/USAA2012012300006.md): Strap · cracked · Dec 18, 2011 · N334AW · Boeing 7373Y0 · Cargo/Baggage Doors
  > C21 CHECK - CRACKS ON FORWARD CARGO DOOR LOWER SEAL STRAP BETWEEN BS 478.5 TO BS 484.5, WL 150, S26R. REPLACED FORWARD CARGO DOOR LOWER SEAL STRAP BETWEEN BS 478.5 TO BS 484.5, WL 150, S26R IAW B737-300 SRM 51-40-05-0G.
- [SDR USAA2012013000008](https://openairdocs.org/sdr/USAA2012013000008.md): Frame · cracked · Dec 12, 2011 · N334AW · Boeing 7373Y0 · Fuselage Main, Frame
  > C21 CHECK - 2 CRACKS IN FUSELAGE FRAME AT BS 440, S22R. REPLACED FUSELAGE FRAME AT BS 440, S22R IAW B737-300 SRM 51.40.02.0G FIG 8, 12.
- [SDR USAA2012012500006](https://openairdocs.org/sdr/USAA2012012500006.md): Floorbeam · corroded · Dec 10, 2011 · N334AW · Boeing 7373Y0 · Fuselage Main, Floor Beam
  > C21 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM BETWEEN BS 996 TO BS 1006, WL 208, RBL 36. REPLACED FLOORBEAM BETWEEN BS 996 TO BS 1006, WL 208, RBL 36 IAW B737 SRM 51-40-02-0G FIG 3 & 8.
- [SDR USAA2012012500005](https://openairdocs.org/sdr/USAA2012012500005.md): Floor Support · corroded · Dec 10, 2011 · N334AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > C21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT BS 994, WL 208 BETWEEN LBL 14 TO LBL 44. REPLACED FLOOR SUPPORT AT BS 994, WL 208 BETWEEN LBL14 TO LBL 44 IAW B737 SRM 51-40-02-0G FIG 3 & 8.
- [SDR USAA2012012500004](https://openairdocs.org/sdr/USAA2012012500004.md): Shear Web · corroded · Dec 10, 2011 · N334AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > C21 CHECK - LEVEL 2 FILIFORM CORROSION ON SHEAR WEB BETWEEN BS 996 TO BS 1016, WL 208 & BETWEEN RBL 37 TO RBL 45. REPLACED SHEAR WEB BETWEEN BS 996 TO BS 1016, WL 208 & BETWEEN RBL 37 TO RBL 45 IAW B737 SRM 51-40-02-0G FIG 3 & 8.
- [SDR USAA2012012300007](https://openairdocs.org/sdr/USAA2012012300007.md): Shear Web · corroded · Dec 10, 2011 · N334AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > C21 CHECK - LEVEL 2 FILIFORM CORROSION ON SHEAR WEB BETWEEN BS 986 TO BS 1016, WL 208, BETWEEN LBL 41 TO LBL 42. REPLACED SHEAR WEB BETWEEN BS 986 TO BS 1016, WL 208, BETWEEN LBL 41 TO LBL 42 IAW B737-300 SRM 51-40-02-0G FIGURE 3 & 8.
- [SDR USAA2012011700011](https://openairdocs.org/sdr/USAA2012011700011.md): Channel · corroded · Dec 10, 2011 · N334AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > C21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON HAT CHANNEL AT BS 996, WL 208 BETWEEN RBL 13 TO RBL 44. REPLACED HAT CHANNEL AT BS 996, WL 208 BETWEEN RBL 13 TO RBL 44 IAW B737 SRM 51-40-02-0G FIG 12.
- [SDR USAA2012011000011](https://openairdocs.org/sdr/USAA2012011000011.md): Floorbeam · corroded · Dec 10, 2011 · N334AW · Boeing 7373Y0 · Fuselage Main, Floor Beam
  > C21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN BS 1006 TO BS 1016, WL 208 & BETWEEN RBL 4 TO RBL 11. REPLACED FLOORBEAM BETWEEN BS 1006 TO BS 1016, WL 208 & BETWEEN RBL 4 TO RBL 11 IAW B737 SRM 51-40-02-0G FIG 12.
- [SDR USAA2012011000010](https://openairdocs.org/sdr/USAA2012011000010.md): Floorbeam · corroded · Dec 10, 2011 · N334AW · Boeing 7373Y0 · Fuselage Main, Floor Beam
  > C21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN BS 996 TO BS 1006, WL 208 & BETWEEN RBL 9 TO RBL 17. REPLACED FLOORBEAM BETWEEN BS 996 TO BS 1006, WL 208 & BETWEEN RBL 9 TO RBL 17 IAW B737 SRM 51-40-02-0G FIG 12.
- [SDR USAA2012010900022](https://openairdocs.org/sdr/USAA2012010900022.md): Strap · corroded · Dec 10, 2011 · N334AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > C21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON WEB UPPER STRAP AT BS 1027, WL 208, LBL 3. REPLACED WEB UPPER STRAP AT BS 1027, WL 208, LBL 3 IAW B737-300 SRM 51-40-02-0G FIGURE 9 AND 10.
- [SDR USAA2012010900019](https://openairdocs.org/sdr/USAA2012010900019.md): Floor Support · corroded · Dec 10, 2011 · N334AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > C21 CHECK - FILIFORM CORROSION ON FLOOR SUPPORT BETWEEN BS 1006 TO BS 1016, WL 208, LBL 38. REPLACED FLOOR SUPPORT BETWEEN BS 1006 TO BS 1016, WL 208, LBL 38 IAW B737-300 SRM 51-40-02-0G FIGURE 12.
- [SDR USAA2011122800024](https://openairdocs.org/sdr/USAA2011122800024.md): Floorbeam · corroded · Dec 10, 2011 · N334AW · Boeing 7373Y0 · Fuselage Main, Floor Beam
  > C21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT AFT LAV FLOORBEAM BETWEEN BS 1006 TO BS 1016 & BETWEEN LBL 6 TO LBL 11. REPLACED LEFT AFT LAV FLOORBEAM BETWEEN BS 1006 TO BS 1016 & BETWEEN LBL 6 TO LBL 11 IAW B737 SRM 51-10-02-0G, 53-60-51-1A-1 & 51-40-02-0
- [SDR USAA2011122800023](https://openairdocs.org/sdr/USAA2011122800023.md): Floor Support · corroded · Dec 10, 2011 · N334AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > C21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT AFT LAV FLOOR SUPPORT BEAM BETWEEN BS 986 TO BS 1016, LBL 12. REPLACED LEFT AFT LAV FLOOR SUPPORT BEAM BETWEEN BS 986 TO BS 1016, LBL 12 IAW B737 SRM 51-40-02-0G FIG 2.
- [SDR USAA2012013000010](https://openairdocs.org/sdr/USAA2012013000010.md): Attach Angle · corroded · Dec 8, 2011 · N334AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > C21 CHECK - CORROSION ON DOOR THRESHOLD ATTACH ANGLE BETWEEN BS 312 TO BS 344, WL 208, LBL 53. REPLACED DOOR THRESHOLD ATTACH ANGLE BETWEEN BS 312 TO BS 344, WL 208, LBL 53 IAW B737-300 SRM 51-40-02-0G FIG 8 & 12.
- [SDR USAA2012013000009](https://openairdocs.org/sdr/USAA2012013000009.md): Skin · corroded · Dec 8, 2011 · N334AW · Boeing 7373Y0 · Fuselage Main, Plate/Skin
  > C21 CHECK - CORROSION ON LOWER MARKER BEACON ANTENNA PANEL AT BS 585, BL 0. REPAIRED LOWER MARKER BEACON ANTENNA PANEL AT BS 585, BL 0 IAW B737-300 SRM 51-40-02-0G FIG 3 & 8.
- [SDR USAA2012013000006](https://openairdocs.org/sdr/USAA2012013000006.md): Door Frame · cracked · Dec 8, 2011 · N334AW · Boeing 7373Y0 · Service Doors
  > C21 CHECK - 250 INCH LONG CRACK IN R1 DOOR FRAME AT NR 4 STOP (30.5" FROM BOTTOM OF DOOR) AT BS 328, WL 238.5. REPAIRED R1 DOOR FRAME AT NR 4 STOP (30.5" FROM BOTTOM OF DOOR) AT BS 328, WL 238.5 IAW EA 130764.
- [SDR USAA2012010900021](https://openairdocs.org/sdr/USAA2012010900021.md): Attach Angle · cracked · Dec 8, 2011 · N334AW · Boeing 7373Y0 · Fuselage Miscellaneous Structure
  > C21 CHECK - CRACKS ON ATTACH ANGLE BETWEEN BS 500D TO BS 520, BL 0. REPLACED ATTACH ANGLE BETWEEN BS 500D TO BS 520, BL 0 IAW B737-300 SRM 51-40-02-0G FIGURE 2.
- [SDR USAA2012012000008](https://openairdocs.org/sdr/USAA2012012000008.md): Wedge · debonded · Nov 30, 2011 · N334AW · Boeing 7373Y0 · Leading Edge Devices
  > C21 CHECK - RIGHT WING NR 4 SLAT TRAILING EDGE WEDGE DISBONDED BETWEEN SS116 TO SS124, 6 INCHES INBOARD OF OUTBOARD END 2.5 INCHES FROM TRAILING EDGE. REPAIRED NR 4 SLAT IAW B737-300 SRM 51-70-10-2R-4, REPAIR 4 FIGURE 202.
- [SDR USAA2011090600019](https://openairdocs.org/sdr/USAA2011090600019.md): Skin · cracked · Sep 4, 2011 · N334AW · Boeing 7373Y0 · Fuselage Main, Plate/Skin
  > RON CHECK - CRACK ON RIGHT SIDE OF FUSELAGE SKIN ABOVE WINDOW NR 13 FROM FRONT ABOVE S10R SKIN 16 INCHES FORWARD OF BS 540. REPAIRED FUSELAGE SKIN AT BS 540, S10R IAW B737 SRM 53-00-01 REPAIR 31.
- [SDR USAA2011081000009](https://openairdocs.org/sdr/USAA2011081000009.md): Skin · debonded · Aug 9, 2011 · N334AW · Boeing 7373Y0 · Trailing Edge Flaps
  > WIRE HOLE INSP - DISBONDING ON LEFT OUTBOARD FLAP TRAILING EDGE AT LOWER INBOARD CORNER UPPER SURFACE AT WBL 203. REPLACED LEFT OUTBOARD FLAP IAW JOB CARD R3M27034.
- [SDR USAA2011081000008](https://openairdocs.org/sdr/USAA2011081000008.md): Frame · cracked · Aug 9, 2011 · N334AW · Boeing 7373Y0 · Fuselage Main, Frame
  > WIRE HOLE INSP - CRACK IN FUSELAGE FRAME AT BS 500C, S21L. REPAIRED FUSELAGE FRAME AT BS 500C, S21L IAW B737 SRM 53-00-07 REPAIR 13.
- [SDR USAA2011081000007](https://openairdocs.org/sdr/USAA2011081000007.md): Frame · cracked · Aug 9, 2011 · N334AW · Boeing 7373Y0 · Fuselage Main, Frame
  > WIRE HOLE INSP - CRACK IN FUSELAGE FRAME AT BS500B, S20R. REPAIRED FUSELAGE FRAME AT BS 500B, S20R IAW B737 SRM 53-00-07 REPAIR 13.
- [SDR USAA2011042291610](https://openairdocs.org/sdr/USAA2011042291610.md): Skin · cracked · Apr 20, 2011 · N334AW · Boeing 7373Y0 · Fuselage Main, Plate/Skin
  > PHX - WALKAROUND - CRACK IN FUSELAGE SKIN APPROX 3 INCHES FORWARD OF AFT CARGO DOOR LOWER FWD CORNER AT BS 747, S25R. REPAIRED FUSELAGE SKIN AT BS 747, S25R IAW B737 SRM 53-00-01.
- [SDR USAA20110301SB035](https://openairdocs.org/sdr/USAA20110301SB035.md): Acm · malfunctioned · Feb 25, 2011 · N334AW · Boeing 7373Y0 · Cabin Cooling System
  > PHX - A STRONG ODOR OF OLD SOCKS WAS COMING FROM THE AIR CONDITIONING SYSTEM, ESPECIALLY AT LOW ENGINE POWER SETTINGS. SUSPECT FILTERS NEED CHANGED. MAINTENANCE COMPLIED WITH TROUBLESHOOTING CARD 03L00021001. REMOVED AND REPLACED RIGHT AIR CYCLE MACHINE ALO
- [SDR USAA20101202SB198](https://openairdocs.org/sdr/USAA20101202SB198.md): Fuse · blown · Nov 28, 2010 · N334AW · Boeing 7373Y0 · Emergency Lighting
  > DFW - WHILE REPLACING DISLODGED BULKHEAD EMERGENCY EXIT LIGHT AT EXIT ROW 15, RIGHT SIDE, MAINTENANCE FOUND NO POWER TO THE LIGHT ASSEMBLY. MAINTENANCE REMOVED AND REPLACED THE FUSE IN EMERGENCY EXIT LIGHT POWER SUPPLY BASE. OPERATIONAL CHECK GOOD.
- [SDR USAA2010112692669](https://openairdocs.org/sdr/USAA2010112692669.md): Lamp · defective · Nov 24, 2010 · N334AW · Boeing 7373Y0 · Passenger Compartment Lighting
  > FLT 668 - PHX - ON FINAL APPROACH THE AFT RIGHT LAVATORY SMOKE DETECTOR SOUNDED. FLIGHT ATTENDANT CHECKED LAVATORY COULD FIND NO FIRE BUT SMELLED A BURNED ELECTRICAL ODOR. ODOR WAS NOTICED AT AFT LEFT ATTENDANT WORK LIGHT. NO DEFECTS FOUND, NEW LAMPS INSTAL
- [SDR USAA20101124SB195](https://openairdocs.org/sdr/USAA20101124SB195.md): Wire · shorted · Nov 23, 2010 · N334AW · Boeing 7373Y0 · Light System Wiring
  > PHX - APPROXIMATELY 10 MILES FROM AIRPORT WHILE ON FINAL APPROACH, THE SMOKE ALARM FOR THE AFT RIGHT LAVATORY WENT OFF AND WAS HEARD IN COCKPIT BY FLIGHT CREW. FLIGHT ATTENDANT CHECKED LAVATORY. NO FIRE BUT COULD SMELL SMOKE. CREW DECLARED AN EMERGENCY WITH
- [SDR USAA20101001SB152](https://openairdocs.org/sdr/USAA20101001SB152.md): Torque Tube · worn · Sep 27, 2010 · N334AW · Boeing 7373Y0 · Elevator Control System
  > PHX - DURING CRUISE, EN ROUTE FROM SNA TO PHX, AIRCRAFT EXPERIENCED FLIGHT CONTROL ISSUES. CREW REPORTED A STRONG RYTHMIC VIBRATION, FELT POSSIBLY IN THE TAIL, AS AIRSPEED INCREASED ABOVE 250 KNOTS. AIRCRAFT APPROACHED MODERATE BUFFET AT 300 KNOTS AND DECREA
- [SDR USAA2010092292072](https://openairdocs.org/sdr/USAA2010092292072.md): Drag Angle · cracked · Sep 22, 2010 · N334AW · Boeing 7373Y0 · Vertical Stabilizer Miscellaneous Structure
  > MIA - C20 - MAJOR REPAIR - CRACK ON LEFT AFT VERTICAL STABILIZER ATTACH FITTING DRAG ANGLE AT BS 1016, VERT FIN STA 0. REPAIRED LEFT AFT VERTICAL STABILIZER ATTACH FITTING DRAG ANGLE AT BS 1016, VERT FIN STA 0 IAW TYPICAL REPAIR 53-80-30.
- [SDR USAA2010092292071](https://openairdocs.org/sdr/USAA2010092292071.md): Skin · cracked · Sep 22, 2010 · N334AW · Boeing 7373Y0 · Trailing Edge Flaps
  > MAJOR REPAIR - CRACK ON LT WING OTBD MID FLAP L/E SKIN BETWEEN WBL204.4 TO WBL219.4. REPAIRED LT WING OTBD MID FLAP L/E SKIN BETWEEN WBL204.4 TO WBL219.4 IAW SRM 57-53-01 REPAIR NR 8.
- [SDR USAA2010091491989](https://openairdocs.org/sdr/USAA2010091491989.md): Floorbeam · corroded · Sep 8, 2010 · N334AW · Boeing 7373Y0 · Fuselage Main, Floor Beam
  > MIA - C20 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT BS 328 BETWEEN RBL 26 TO RBL 36. REPAIRED FLOORBEAM AT BS 328 BETWEEN RBL 26 TO RBL 36 IAW B737 SRM 53-10-51, 53-30-51 & 53-00-51.
- [SDR USAA2010092292073](https://openairdocs.org/sdr/USAA2010092292073.md): Hinge Pin · corroded · Aug 22, 2010 · N334AW · Boeing 7373Y0 · Horizontal Stabilizer Structure
  > MIA - C20 - MAJOR REPAIR - CORROSION ON RIGHT HORIZONTAL STABILIZER OUTER HINGE PIN AT BS 1146.508, HORIZ STAB STA 67.54. REPLACED RIGHT HORIZONTAL STABILIZER OUTER HINGE PIN AT BS 1146.508, HORIZ STAB STA 67.54 IAW JOB CARD I6C55040.
- [SDR USAA2010072391481](https://openairdocs.org/sdr/USAA2010072391481.md): Skin · delaminated · Jul 24, 2010 · N334AW · Boeing 7373Y0 · Leading Edge Devices
  > PHX - B4 - MAJOR REPAIR - DELAMINATION ON LEFT WING NR 2 SLAT WEDGE UPPER SURFACE BETWEEN SLAT STA 167 TO 207. REPLACED LEFT WING NR 2 SLAT IAW B737 AMM 27-81-21-4.
- [SDR USAA2010071491416](https://openairdocs.org/sdr/USAA2010071491416.md): Lanyard · faulty · Jul 13, 2010 · N334AW · Boeing 7373Y0 · Escape Slide
  > PHX - RON - EES - R-2 DOOR SLIDE DID NOT FULLY DEPLOY DURING SLIDE SAMPLE DEPLOYMENT. BREAKAWAY LANYARD DID NOT BREAK RESULTING IN ONLY PARTIAL DEPLOYMENT. REPLACED R-2 DOOR SLIDE IAW JOB CARD 03T10025002.
- [SDR USAA20100714SB115](https://openairdocs.org/sdr/USAA20100714SB115.md): Lanyard · defective · Jul 13, 2010 · N334AW · Boeing 7373Y0 · Escape Slide
  > PHX - DURING R2 DOOR ESCAPE SLIDE OPERATIONAL CHECK, THE ESCAPE SLIDE DID NOT FULLY DEPLOY. THE BREAKAWAY LANYARD DID NOT BREAK, RESULTING IN ONLY HALF DEPLOYMENT. MAINTENANCE REMOVED AND REPLACED THE R2 DOOR ESCAPE SLIDE.
- [SDR USAA2009113093259](https://openairdocs.org/sdr/USAA2009113093259.md): Flap · debonded · Nov 27, 2009 · N334AW · Boeing 7373Y0 · Trailing Edge Flaps
  > PHX - B02 - MAJOR REPAIR - LEFT WING OUTBOARD FORE FLAP LEADING EDGE DISBOND ON AFT FACE AT FLAP MID SPAN. REMOVED LEFT OUTBOARD FORE FLAP ASSEMBLY IAW JOB CARD R3M22022.
- [SDR USAA20090807SB131](https://openairdocs.org/sdr/USAA20090807SB131.md): Uplock Actuator · faulty · Aug 5, 2009 · N334AW · Boeing 7373Y0 · Landing Gear Actuator
  > ONT - ON CLIMBOUT FROM ONT, EN ROUTE TO PHX PASSING 10,000 FEET, CREW REPORTED THE RIGHT MAIN LANDING GEAR RED LIGHT ILLUMINATED. WHEN GEAR HANDLE WAS RAISED TO UP POSITION, THE RED LIGHT REMAINED ILLUMINATED. WHEN GEAR HANDLE WAS RETURNED TO OFF POSITION, T
- [SDR USAA2009080391987](https://openairdocs.org/sdr/USAA2009080391987.md): Spoiler Panel · delaminated · Jul 31, 2009 · N334AW · Boeing 7373Y0 · Spoilers
  > PHX - RON - MAJOR REPAIR - LEFT WING NR 1 FLIGHT SPOILER HAS A 5 INCH AREA OF DISBOND. NR 1 SPOILER BOARD REPLACED IAW B737 MM 27-62-91.
- [SDR USAA20090622SB103](https://openairdocs.org/sdr/USAA20090622SB103.md): Circuit Card · faulty · Jun 20, 2009 · N334AW · Boeing 7373Y0 · Landing Gear Position and Warning
  > AFTER LIFTOFF FROM PHX, WHEN LANDING GEAR HANDLE WAS PLACED TO OFF POSITION, CREW RECEIVED BOTH THE RED AND GREEN RIGHT MAIN LANDING GEAR LIGHTS. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD AT PHX. A NORMAL GEAR INDICATION WAS NOTED WHEN GEAR
- [SDR USAA2009060891431](https://openairdocs.org/sdr/USAA2009060891431.md): Skin · corroded · Jun 7, 2009 · N334AW · Boeing 7373Y0 · Fuselage Main, Plate/Skin
  > SAL - MAJOR REPAIR - C19 CHECK - CORROSION ON FUSELAGE SKIN INTERNAL SURFACE AT BS 727 TO BS 727A, S27L. REPAIRED FUSELAGE SKIN INTERNAL SURFACE AT BS 727 TO BS 727A, S27L IAW US AIRWAYS EA 132457.
- [SDR USAA2009060891432](https://openairdocs.org/sdr/USAA2009060891432.md): Skin · cracked · Jun 6, 2009 · N334AW · Boeing 7373Y0 · Fuselage Main, Plate/Skin
  > SAL - MAJOR REPAIR - C19 CHECK - FUSELAGE SKIN CRACKED AT BS 303.9, S10L AT THE L1 DOOR UPPER HINGE CUTOUT. REPAIRED FUSELAGE SKIN AT BS 303.9, S10L AT THE L1 DOOR UPPER HINGE CUTOUT IAW US AIRWAYS EA 132435.
- [SDR USAA2009060891435](https://openairdocs.org/sdr/USAA2009060891435.md): Keelbeam · corroded · Jun 5, 2009 · N334AW · Boeing 7373Y0 · Fuselage Main, Keel
  > SAL - MAJOR REPAIR - C19 CHECK - CORROSION ON KEEL BEAM AT BS 727 - BS 727A, S27L. REPAIRED KEEL BEAM AT BS 727 - BS 727A, S27L IAW US AIRWAYS EA 132457.
- [SDR USAA2009060891434](https://openairdocs.org/sdr/USAA2009060891434.md): Frame · cracked · Jun 5, 2009 · N334AW · Boeing 7373Y0 · Fuselage Main, Frame
  > SAL - MAJOR REPAIR - C19 CHECK - CRACKED FRAME AT BS 303.9, S16L. REPAIRED FRAME AT BS 303.9, S16L IAW US AIRWAYS TASK CARD M1C53001.

Next page: https://openairdocs.org/deregistered/N334AW-2012-07-16/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 = 'N334AW' AND deregistration_id = 'N334AW-2012-07-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N334AW-2012-07-16/reports

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