# N334AW: 1987 Boeing 737-3Y0, registration cancelled 2012-07-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 16, 2012
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-3Y0](https://openairdocs.org/model/boeing-737-3y0) (registry code 138447W)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Serial number: 23748
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 14, 1995
- Certificate issued: December 30, 1998
- Last registry action: October 17, 2008
- Mode S code: A3A4C0
- Owner when cancelled: [Acg Acquisition Xx LLC](https://openairdocs.org/faa-owner/ACG%20ACQUISITION%20XX%20LLC)
- Location: [Newport Beach, CA](https://openairdocs.org/faa-place/CA/Newport%20Beach)
- Owner type: Corporation
- Owner's area on the map: 33.6346° N, 117.8749° W: Placed by OpenAirDocs at the center of ZIP code 92660, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N334AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=334AW
- Page: https://openairdocs.org/deregistered/N334AW-2012-07-16

From the FAA registry file of November 12, 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 Boeing 737-3Y0: https://openairdocs.org/model/boeing-737-3y0.md

## Service difficulty reports (311, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR USAA2012012400002](https://openairdocs.org/sdr/USAA2012012400002), Jan 21, 2012: SIGN. DAMAGED. C21 CHECK - AFT CLOSET LOWER EXIT SIGN DAMAGED. REPLACED AFT CLOSET LOWER EXIT SIGN AS NEEDED.
- [SDR USAA2012013000005](https://openairdocs.org/sdr/USAA2012013000005), Jan 10, 2012: SKIN. CRACKED. 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), Jan 6, 2012: DOOR FRAME. CRACKED. 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 34
- [SDR USAA2012011800014](https://openairdocs.org/sdr/USAA2012011800014), Jan 3, 2012: STRINGER. CRACKED. 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), Dec 30, 2011: SUPPORT. CORRODED. 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 B
- [SDR USAA2012012500003](https://openairdocs.org/sdr/USAA2012012500003), Dec 20, 2011: ANGLE. CORRODED. 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), Dec 20, 2011: LENS. CRAZED. 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 EXTE
- [SDR USAA2012012300006](https://openairdocs.org/sdr/USAA2012012300006), Dec 18, 2011: STRAP. CRACKED. 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 47
- [SDR USAA2012013000008](https://openairdocs.org/sdr/USAA2012013000008), Dec 12, 2011: FRAME. CRACKED. 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), Dec 10, 2011: FLOORBEAM. CORRODED. 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 
- [SDR USAA2012012500005](https://openairdocs.org/sdr/USAA2012012500005), Dec 10, 2011: FLOOR SUPPORT. CORRODED. 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
- [SDR USAA2012012500004](https://openairdocs.org/sdr/USAA2012012500004), Dec 10, 2011: SHEAR WEB. CORRODED. 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, 
- [SDR USAA2012012300007](https://openairdocs.org/sdr/USAA2012012300007), Dec 10, 2011: SHEAR WEB. CORRODED. 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, W
- [SDR USAA2012011700011](https://openairdocs.org/sdr/USAA2012011700011), Dec 10, 2011: CHANNEL. CORRODED. 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 RB
- [SDR USAA2012011000011](https://openairdocs.org/sdr/USAA2012011000011), Dec 10, 2011: FLOORBEAM. CORRODED. 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 10
- [SDR USAA2012011000010](https://openairdocs.org/sdr/USAA2012011000010), Dec 10, 2011: FLOORBEAM. CORRODED. 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
- [SDR USAA2012010900022](https://openairdocs.org/sdr/USAA2012010900022), Dec 10, 2011: STRAP. CORRODED. 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 51-4
- [SDR USAA2012010900019](https://openairdocs.org/sdr/USAA2012010900019), Dec 10, 2011: FLOOR SUPPORT. CORRODED. 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 IA
- [SDR USAA2011122800024](https://openairdocs.org/sdr/USAA2011122800024), Dec 10, 2011: FLOORBEAM. CORRODED. 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 BETWEE
- [SDR USAA2011122800023](https://openairdocs.org/sdr/USAA2011122800023), Dec 10, 2011: FLOOR SUPPORT. CORRODED. 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
- [SDR USAA2012013000010](https://openairdocs.org/sdr/USAA2012013000010), Dec 8, 2011: ATTACH ANGLE. CORRODED. 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
- [SDR USAA2012013000009](https://openairdocs.org/sdr/USAA2012013000009), Dec 8, 2011: SKIN. CORRODED. 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
- [SDR USAA2012013000006](https://openairdocs.org/sdr/USAA2012013000006), Dec 8, 2011: DOOR FRAME. CRACKED. 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 B
- [SDR USAA2012010900021](https://openairdocs.org/sdr/USAA2012010900021), Dec 8, 2011: ATTACH ANGLE. CRACKED. 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), Nov 30, 2011: WEDGE. DEBONDED. 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 
- [SDR USAA2011090600019](https://openairdocs.org/sdr/USAA2011090600019), Sep 4, 2011: SKIN. CRACKED. 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, S1
- [SDR USAA2011081000009](https://openairdocs.org/sdr/USAA2011081000009), Aug 9, 2011: SKIN. DEBONDED. 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 R3M27
- [SDR USAA2011081000008](https://openairdocs.org/sdr/USAA2011081000008), Aug 9, 2011: FRAME. CRACKED. 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), Aug 9, 2011: FRAME. CRACKED. 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), Apr 20, 2011: SKIN. CRACKED. 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
- [SDR USAA20110301SB035](https://openairdocs.org/sdr/USAA20110301SB035), Feb 25, 2011: ACM. MALFUNCTIONED. 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
- [SDR USAA20101202SB198](https://openairdocs.org/sdr/USAA20101202SB198), Nov 28, 2010: FUSE. BLOWN. DFW - WHILE REPLACING DISLODGED BULKHEAD EMERGENCY EXIT LIGHT AT EXIT ROW 15, RIGHT SIDE, MAINTENANCE FOUND NO POWER TO THE LIGHT ASSEMBLY. MAINTENANCE REMOVED 
- [SDR USAA2010112692669](https://openairdocs.org/sdr/USAA2010112692669), Nov 24, 2010: LAMP. DEFECTIVE. 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 ELECT
- [SDR USAA20101124SB195](https://openairdocs.org/sdr/USAA20101124SB195), Nov 23, 2010: WIRE. SHORTED. 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. 
- [SDR USAA20101001SB152](https://openairdocs.org/sdr/USAA20101001SB152), Sep 27, 2010: TORQUE TUBE. WORN. 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, 
- [SDR USAA2010092292072](https://openairdocs.org/sdr/USAA2010092292072), Sep 22, 2010: DRAG ANGLE. CRACKED. 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 ATT
- [SDR USAA2010092292071](https://openairdocs.org/sdr/USAA2010092292071), Sep 22, 2010: SKIN. CRACKED. 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 SR
- [SDR USAA2010091491989](https://openairdocs.org/sdr/USAA2010091491989), Sep 8, 2010: FLOORBEAM. CORRODED. 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 53-10-5
- [SDR USAA2010092292073](https://openairdocs.org/sdr/USAA2010092292073), Aug 22, 2010: HINGE PIN. CORRODED. 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 O
- [SDR USAA2010072391481](https://openairdocs.org/sdr/USAA2010072391481), Jul 24, 2010: SKIN. DELAMINATED. 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 27-81-2
- [SDR USAA2010071491416](https://openairdocs.org/sdr/USAA2010071491416), Jul 13, 2010: LANYARD. FAULTY. 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. REPL
- [SDR USAA20100714SB115](https://openairdocs.org/sdr/USAA20100714SB115), Jul 13, 2010: LANYARD. DEFECTIVE. 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 DEPLOYME
- [SDR USAA2009113093259](https://openairdocs.org/sdr/USAA2009113093259), Nov 27, 2009: FLAP. DEBONDED. 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
- [SDR USAA20090807SB131](https://openairdocs.org/sdr/USAA20090807SB131), Aug 5, 2009: UPLOCK ACTUATOR. FAULTY. 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
- [SDR USAA2009080391987](https://openairdocs.org/sdr/USAA2009080391987), Jul 31, 2009: SPOILER PANEL. DELAMINATED. 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), Jun 20, 2009: CIRCUIT CARD. FAULTY. 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 W
- [SDR USAA2009060891431](https://openairdocs.org/sdr/USAA2009060891431), Jun 7, 2009: SKIN. CORRODED. 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
- [SDR USAA2009060891432](https://openairdocs.org/sdr/USAA2009060891432), Jun 6, 2009: SKIN. CRACKED. 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 D
- [SDR USAA2009060891435](https://openairdocs.org/sdr/USAA2009060891435), Jun 5, 2009: KEELBEAM. CORRODED. 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), Jun 5, 2009: FRAME. CRACKED. 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.

All 311: https://openairdocs.org/deregistered/N334AW-2012-07-16/reports.md

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