# N305AW: 1988 Boeing 737-3G7, registration cancelled 2012-01-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 12, 2012
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 737-3G7](https://openairdocs.org/model/boeing-737-3g7) (registry code 138447J)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Serial number: 24012
- Year built: 1988
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 11, 1988
- Certificate issued: September 14, 2000
- Last registry action: November 13, 2008
- Mode S code: A331FA
- Owner when cancelled: [Bank Of New York Mellon Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20NEW%20YORK%20MELLON%20TRUSTEE)
- Location: [Los Angeles, CA](https://openairdocs.org/faa-place/CA/Los%20Angeles)
- Owner type: Corporation
- Owner's area on the map: 34.0531° N, 118.2645° W: Placed by OpenAirDocs at the center of ZIP code 90017, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N305AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=305AW
- Page: https://openairdocs.org/deregistered/N305AW-2012-01-12

From the FAA registry file of October 29, 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 737-3G7: https://openairdocs.org/model/boeing-737-3g7.md

## Service difficulty reports (254, newest 50)

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

- [SDR USAA2011072800018](https://openairdocs.org/sdr/USAA2011072800018), Jul 16, 2011: SLIDE. UNSERVICEABLE. C21 CHECK - L-1 DOOR ESCAPE SLIDE GIRT BAR NOT ATTACHED TO GIRT. REPLACED L-1 DOOR ESCAPE SLIDE PACK ASSEMBLY IAW B737 AMM 25-61-35-002-005.
- [SDR USAA2011072800015](https://openairdocs.org/sdr/USAA2011072800015), Jul 12, 2011: CLOSEOUT PANEL. WORN. C21 CHECK - NR 1 PYLON MID FAIRING CLOSE OUT PANEL IS WORN AT FORWARD END UNDER INBOARD AND OUTBOARD ANGLE BRACKETS AT NAC STA 282.67. REPAIRED NR 1 PYLON MID F
- [SDR USAA2011072000021](https://openairdocs.org/sdr/USAA2011072000021), Jul 11, 2011: SHEAR WEB. BROKEN. C21 CHECK - RIGHT SIDE SHEAR WEB HAS ATTACH HOLES BROKEN OUT AT BS 1017 & BS 1024, BL 0. REPLACED SHEAR WEB IAW B737 SRM 51-40-02 FIG 3, 8, 9, 10 & 12.
- [SDR USAA2011072000019](https://openairdocs.org/sdr/USAA2011072000019), Jul 11, 2011: STRAP. CRACKED. C21 CHECK - CRACKS IN CABIN FLOORBEAM STABILIZER STRAP AT BS 328, LBL 4. REPAIRED CABIN FLOORBEAM STABILIZER STRAP AT BS 328, LBL 4 IAW B737 SRM 53-10-51 FIG 20
- [SDR USAA2011072000018](https://openairdocs.org/sdr/USAA2011072000018), Jul 11, 2011: STRAP. CRACKED. C21 CHECK - CRACK IN FLOORBEAM STABILIZING STRAP AT BS 314.5, LBL 17. REPAIRED FLOORBEAM STABILIZING STRAP AT BS 314.5, LBL 17 IAW B737 SRM 53-10-51 FIG 201 REP
- [SDR USAA2011072600009](https://openairdocs.org/sdr/USAA2011072600009), Jul 8, 2011: SHEAR WEB. CORRODED. C21 CHECK - LEVEL 2 FILIFORM CORROSION ON SHEAR WEB AT BS 1016 BETWEEN BL 0 TO LBL 39. REPLACED SHEAR WEB AT BS 1016 BETWEEN BL 0 TO LBL 39 IAW B737 SRM 51-40-0
- [SDR USAA2011072600008](https://openairdocs.org/sdr/USAA2011072600008), Jul 8, 2011: STRUCTURE. CORRODED. C21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON INNER CHORD BETWEEN BS 947 TO BS 998, LBL 42. REPLACED INNER CHORD BETWEEN BS 947 TO BS 998, LBL 42 IAW B737 SRM 51
- [SDR USAA2011072000001](https://openairdocs.org/sdr/USAA2011072000001), Jul 8, 2011: ATTACH ANGLE. CRACKED. C21 CHECK - CRACKS ON CABIN FLOOR STRUCTURE WEB UPPER ATTACH ANGLE BETWEEN BS 927 TO BS 947.5, BL 0. REPLACED CABIN FLOOR STRUCTURE WEB UPPER ATTACH ANGLE IAW B
- [SDR USAA2011072800017](https://openairdocs.org/sdr/USAA2011072800017), Jul 7, 2011: PRESSURE DECK. CRACKED. C21 CHECK - CRACK IN LEFT MAIN WHEEL WELL PRESSURE DECK AT BS 665, LBL 40. REPAIRED LEFT MAIN WHEEL WELL PRESSURE DECK IAW EA 130643.
- [SDR USAA2011072000020](https://openairdocs.org/sdr/USAA2011072000020), Jul 7, 2011: DOOR FRAME. CRACKED. C21 CHECK - CRACK IN R1 DOOR UPPER FORWARD REVEAL STUB FRAME AT BS 297, S8R. REPLACED R1 DOOR UPPER FORWARD REVEAL STUB FRAME IAW B737 SRM 51-40-02 FIG 3, 8 & 1
- [SDR USAA2011072000017](https://openairdocs.org/sdr/USAA2011072000017), Jul 7, 2011: SKIN. CRACKED. C21 CHECK - CRACK ON BOTTOM OF NR 6 SLAT SKIN BETWEEN SS254.4 TO SS255.0. REPAIRED NR 6 SLAT SKIN BETWEEN SS254.4 TO SS255.0 IAW B737 SRM 57-43-01 FIG 201.
- [SDR USAA2011050991797](https://openairdocs.org/sdr/USAA2011050991797), May 6, 2011: SKIN. CRACKED. PHX - DAILY - CRACK IN FUSELAGE SKIN AT 2.5 INCHES FORWARD OF AFT CARGO DOOR AT BS 747, S18R. REPAIRED FUSELAGE SKIN AT 2.5 INCHES FORWARD OF AFT CARGO DOOR AT 
- [SDR USAA20100617SB104](https://openairdocs.org/sdr/USAA20100617SB104), Jun 16, 2010: UPLOCK SENSOR. FAULTY. PHX - ON CLIMBOUT FROM PHX, CREW REPORTED THE RIGHT MAIN LANDING GEAR RED LIGHT FLASHED OFF AND ON INTERMITTENTLY AFTER GEAR RETRACTION. AN EMERGENCY WAS DECLAR
- [SDR USAA2010050390883](https://openairdocs.org/sdr/USAA2010050390883), Apr 30, 2010: FLAP. DELAMINATED. MCN - C20 - MAJOR REPAIR - DELAMINATION ON RIGHT OUTBOARD FORE FLAP 40 INCHES FROM INBOARD END. REPLACED RIGHT OUTBOARD FORE FLAP IAW JOB CARDS O3R27002 & C3R27
- [SDR USAA2010042990868](https://openairdocs.org/sdr/USAA2010042990868), Apr 6, 2010: FRAME. CRACKED. MCN - C20 - MAJOR REPAIR - CRACK IN FRAME WEB AT BS 303.9, S16L FORWARD OF L-1 DOOR. REPAIRED FRAME WEB AT BS 303.9, S16L FORWARD OF L-1 DOOR IAW JOB CARD M1L53
- [SDR USAA2010043090873](https://openairdocs.org/sdr/USAA2010043090873), Apr 3, 2010: SEAT TRACK. CORRODED. MCN - C20 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT BS 328, RBL 25. REPLACED SEAT TRACK AT BS 328, RBL 25 IAW B737 SRM 53-00-52.
- [SDR USAA2010042190808](https://openairdocs.org/sdr/USAA2010042190808), Apr 3, 2010: CHANNEL. CRACKED. MCN - C20 - MAJOR REPAIR - CRACK IN CHANNEL AT BS 329, LBL 47. REPLACED CHANNEL AT BS 329, LBL 47 IAW B737 SRM 51-40-02.
- [SDR USAA2010041990805](https://openairdocs.org/sdr/USAA2010041990805), Apr 3, 2010: STIFFENER. CRACKED. MCN - C20 - MAJOR REPAIR - CRACKS ON VERTICAL STIFFENER ON AFT SIDE OF FLOORBEAM AT BS 329, LBL 47. REPLACED VERTICAL STIFFENER ON AFT SIDE OF FLOORBEAM AT BS 3
- [SDR USAA2010043090871](https://openairdocs.org/sdr/USAA2010043090871), Apr 1, 2010: SKIN PANEL. CRACKED. MCN - C20 - MAJOR REPAIR - CRACK ON FUSELAGE SKIN AT MAIN ENTRY DOOR UPPER / LOWER HINGE CUTOUTS AT BS 312 BETWEEN S9L TO S15L. REPAIRED FUSELAGE SKIN AT MAIN E
- [SDR USAA2010042990866](https://openairdocs.org/sdr/USAA2010042990866), Mar 31, 2010: DOOR FRAME. CRACKED. MCN - C20 - MAJOR REPAIR - 2 CRACKS IN L-1 DOOR AFT FRAME AT BS 344 BETWEEN S9L TO S10L. REPAIRED L-1 DOOR AFT FRAME AT BS 344 BETWEEN S9L TO S10L IAW EA 130394
- [SDR USAA2010042990865](https://openairdocs.org/sdr/USAA2010042990865), Mar 31, 2010: FRAME. CRACKED. MCN - C20 - MAJOR REPAIR - CRACK IN FUSELAGE FRAME AT BS 360, S13R. REPAIRED FUSELAGE FRAME AT BS 360, S13R IAW TYPICAL REPAIR 53-10-21B.
- [SDR USAA2010042690838](https://openairdocs.org/sdr/USAA2010042690838), Mar 31, 2010: SKIN. CRACKED. MCN - C20 - MAJOR REPAIR - CRACK ON RIGHT HORIZONTAL STABILIZER LOWER SKIN AT SS125. REPAIRED RIGHT HORIZONTAL STABILIZER LOWER SKIN AT SS125 IAW TYPICAL REPAIR
- [SDR USAA2010042690839](https://openairdocs.org/sdr/USAA2010042690839), Mar 30, 2010: STRINGER. CORRODED. MCN - C20 - MAJOR REPAIR - CORROSION ON STRINGER 27R AT BS 946. REPAIRED STRINGER 27R AT BS 946 IAW B737 SRM 53-00-03.
- [SDR USAA2010021290350](https://openairdocs.org/sdr/USAA2010021290350), Feb 9, 2010: SLAT. DEBONDED. PHX - B4 - MAJOR REPAIR - NR 4 SLAT DISBONDED AT INBOARD CORNER BETWEEN SLAT STA 12 TO SLAT STA 16. REPAIRED NR 4 SLAT AT INBOARD CORNER BETWEEN SLAT STA 12 TO 
- [SDR USAA2010021290349](https://openairdocs.org/sdr/USAA2010021290349), Feb 9, 2010: WEDGE. DEBONDED. PHX - B4 - MAJOR REPAIR - NR 3 SLAT DISBONDED ON THE TRAILING EDGE WEDGE END CAP AFT CORNER BETWEEN SLAT STA 115 TO SLAT STA 124.4. REPAIRED NR 3 SLAT SKIN IAW 
- [SDR USAA2010021290348](https://openairdocs.org/sdr/USAA2010021290348), Feb 9, 2010: SKIN. CRACKED. PHX - B4 - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT FORWARD LEFT CORNER OF GROUND AIR CONDITIONING SERVICE DOOR CUTOUT AT BS 530, S28L. REPAIRED FUSELAGE SKIN A
- [SDR USAA2009101992800](https://openairdocs.org/sdr/USAA2009101992800), Oct 18, 2009: FLAP. DEBONDED. PHX - DAILY - MAJOR REPAIR - RIGHT WING AFT OUTBOARD TRAILING EDGE FLAP DISBONDED ON INBOARD CORNER. REPLACED RIGHT OUTBOARD TRAILING EDGE FLAP IAW CARD R3M2703
- [SDR USAA20090828SB143](https://openairdocs.org/sdr/USAA20090828SB143), Aug 27, 2009: WARNING SYSTEM. MALFUNCTIONED. PHX - DURING APPROACH, AS FLAPS WERE SELECTED FROM FLAPS 1 TO 5, CREW RECEIVED A LEADING EDGE FLAPS TRANSIT LIGHT ALONG WITH THE NR 2 SLAT. CREW EXECUTED A MISS
- [SDR USAA20090622SB104](https://openairdocs.org/sdr/USAA20090622SB104), Jun 21, 2009: WIRE. BROKEN. PHX - MAINTENANCE REPORTED THE EMERGENCY EXIT SIGN AT MID CABIN CEILING WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE ON THE EMERGENCY EXIT SIGN. DISCOVERED 
- [SDR USAA20090601SB092](https://openairdocs.org/sdr/USAA20090601SB092), Jun 1, 2009: WIRE. BROKEN. DFW MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEATS 10 AND 11, LEFT-HAND SIDE, ARE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE IN ASSOCIATION WITH SWPM 2
- [SDR USAA20090512SB078](https://openairdocs.org/sdr/USAA20090512SB078), May 11, 2009: POWER SUPPLY. FAULTY. PHX - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS FLASH ON AND OFF INTERMITTENTLY. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT POWER SUPPLY IN ASSOCI
- [SDR USAA20090402SB046](https://openairdocs.org/sdr/USAA20090402SB046), Feb 11, 2009: TRANSFORMER. FAULTY. ON SHORT FINAL INTO PDX, FULLY CONFIGURED, TR1 CIRCUIT BREAKER POPPED. AS A PRECAUTION, CAPTAIN REQUESTED TO HAVE THE EMERGENCY EQUIPMENT STANDING BY. AIRCRAFT 
- [SDR 2009F00032](https://openairdocs.org/sdr/2009F00032), Jan 23, 2009: SNUBBER. MISINSTALLED. ON CLIMB OUT , L1 EMERGENCY EXIT DOOR SEAL LEAKING, NOISE LEVEL UNACCEPTABLE, PRESSURIZATION OK. ACFT 13,000 LBS OVERWEIGHT FOR LANDING, DECLARED AN EMERGENCY U
- [SDR USAA2009012190109](https://openairdocs.org/sdr/USAA2009012190109), Jan 6, 2009: FITTING. CORRODED. SAL - C19 - MAJOR REPAIR - CORROSION ON UPPER, LOWER, & MIDDLE CLEVIS JOINT OF LEFT HORIZONTAL STABILIZER AT ELEVATOR HINGE LINE 113.25. REPAIRED UPPER, LOWER, 
- [SDR USAA2009010890051](https://openairdocs.org/sdr/USAA2009010890051), Jan 5, 2009: WEB. CORRODED. SAL - C19 - MAJOR REPAIR - NR 6143586 - GALVANIC CORROSION ON WEB BETWEEN BS 1016 TO BS1030, LBL17. REPAIRED WEB BETWEEN BS 1016 TO BS1030, LBL17 IAW B737 SRM 5
- [SDR USAA2009010890052](https://openairdocs.org/sdr/USAA2009010890052), Jan 4, 2009: BATTERY. DISCHARGED. SAL - C19 - EMERGENCY LIGHT - NR 6142265 - LOW BATTERY IN FLASHLIGHT ON FORWARD CABIN ATTENDANTS SEAT. REPLACED BATTERY IN FLASHLIGHT ON FORWARD CABIN ATTENDANT
- [SDR USAA2009012190110](https://openairdocs.org/sdr/USAA2009012190110), Dec 29, 2008: BULKHEAD. CRACKED. SAL - C19 - MAJOR REPAIR - CRACK AT BS 178 BULKHEAD ON WEB SURFACE OF VERTICAL BEAM, RBL 5.7, BETWEEN WL 180 & WL 190. REPAIRED BS 178 BULKHEAD ON WEB SURFACE O
- [SDR USAA2009012190106](https://openairdocs.org/sdr/USAA2009012190106), Dec 29, 2008: SKIN. DELAMINATED. SAL - C19 - MAJOR REPAIR - DELAMINATION ON UPPER SKIN OF RIGHT OUTBOARD AFT FLAP WBL 350 TO WBL 368. REPAIRED UPPER SKIN OF RIGHT OUTBOARD AFT FLAP WBL 350 TO W
- [SDR USAA2009012390132](https://openairdocs.org/sdr/USAA2009012390132), Dec 27, 2008: CHANNEL. CORRODED. SAL - C19 - MAJOR REPAIR - CORROSION ON CHANNEL BETWEEN BS 787 TO BS 947, LBL 12.5. REPAIRED CHANNEL BETWEEN BS 787 TO BS 947, LBL 12.5 IAW B737 SRM 53-00-53.
- [SDR USAA2009012190113](https://openairdocs.org/sdr/USAA2009012190113), Dec 27, 2008: FRAME. CRACKED. SAL - C19 - MAJOR REPAIR - CRACK ON FRAME AT BS 380 BETWEEN S8R & S9R. REPAIRED FRAME AT BS 380 BETWEEN S8R & S9R IAW US AIRWAYS TASK CARD M1C53002.
- [SDR USAA2009011690083](https://openairdocs.org/sdr/USAA2009011690083), Dec 27, 2008: FRAME. CRACKED. SAL - C19 - MAJOR REPAIR - CRACK ON FRAME AT BS 500C, BETWEEN S8L TO S9L. REPAIRED FRAME AT BS 500C, BETWEEN S8L TO S9L IAW AMERICA WEST AIRLINES TASK CARD M1C5
- [SDR USAA2009011590078](https://openairdocs.org/sdr/USAA2009011590078), Dec 27, 2008: FRAME. CRACKED. SAL - C19 - MAJOR REPAIR - NR 6192125 - FRAME CRACKED AT BS480, BETWEEN S-8L & S9L. REPAIRED FRAME AT BS480, BETWEEN S-8L & S9L IAW AMERICA WEST AIRLINES TASK C
- [SDR USAA2009012190107](https://openairdocs.org/sdr/USAA2009012190107), Dec 26, 2008: WEB. CORRODED. SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON UPPER WEB AT S26R BETWEEN BS 847 TO BS 867. REPAIRED UPPER WEB AT S26R BETWEEN BS 847 TO BS 867 IAW B737 SRM 51
- [SDR USAA2009012190117](https://openairdocs.org/sdr/USAA2009012190117), Dec 26, 2008: FLOORBEAM. CORRODED. SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT BS 967, BETWEEN LBL 18 TO LBL 44. REPAIRED FLOORBEAM AT BS 967, BETWEEN LBL 18 TO LBL 44 IAW B737 
- [SDR USAA2009012190114](https://openairdocs.org/sdr/USAA2009012190114), Dec 26, 2008: SUPPORT. CORRODED. SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON INTERCOSTAL SUPPORT BETWEEN BS 947 TO BS 967, LBL 18. REPAIRED INTERCOSTAL SUPPORT BETWEEN BS 947 TO BS 967, LB
- [SDR USAA2009012190112](https://openairdocs.org/sdr/USAA2009012190112), Dec 26, 2008: COVER. CORRODED. SAL - C19 - MAJOR REPAIR - CORROSION ON COVER SHEET BETWEEN BS 767 TO BS 787, S26R. REPLACED COVER SHEET BETWEEN BS 767 TO BS 787, S26R IAW B737 SRM 51-40-02.
- [SDR USAA2009011390068](https://openairdocs.org/sdr/USAA2009011390068), Dec 26, 2008: SEAT TRACK. CORRODED. SAL - C19 - MAJOR REPAIR - NR 6142261 - GALVANIC CORROSION ON SEAT TRACK AT BS919, RBL45. REPAIRED SEAT TRACK AT BS919, RBL45 IAW B737 SRM 53-00-52.
- [SDR USAA2009012390131](https://openairdocs.org/sdr/USAA2009012390131), Dec 24, 2008: WEB. CRACKED. SAL - C19 - MAJOR REPAIR - CRACK ON WEB AT BS 987.5, RBL 40. REPAIRED WEB AT BS 987.5, RBL 40 IAW B737 SRM 51-10-02-0G.
- [SDR USAA2009012190116](https://openairdocs.org/sdr/USAA2009012190116), Dec 24, 2008: SUPPORT. CORRODED. SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON STRAP ANGLE SUPPORT AT BS 1006, RBL 41. REPAIRED STRAP ANGLE SUPPORT AT BS 1006, RBL 41 IAW B737 SRM 51-40-02 &
- [SDR USAA2009012190115](https://openairdocs.org/sdr/USAA2009012190115), Dec 24, 2008: FLOORBEAM. CORRODED. SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM UPPER FLANGE AT BS 986.5, BL 0 TO RBL 54. REPAIRED FLOORBEAM UPPER FLANGE AT BS 986.5, BL 0 TO RBL 54

All 254: https://openairdocs.org/deregistered/N305AW-2012-01-12/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19950315008709I](https://openairdocs.org/incident/19950315008709I), Mar 15, 1995: Boeing 7373G7 (N305AW), Omaha, NE. Narrative: on Wednesday, March 15, 1995, N305AW, a Boeing 737-3G7, operated by america west airlines, inc., flight 510, a normally scheduled part 121 flight…

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