# N158AW: 1987 Boeing 737-3G7, registration cancelled 2011-06-15

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 15, 2011
- 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: 23780
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 23, 1987
- Certificate issued: August 25, 1999
- Last registry action: July 21, 2009
- Mode S code: A0E7FC
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N158AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=158AW
- Page: https://openairdocs.org/deregistered/N158AW-2011-06-15

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 (315, newest 50)

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

- [SDR USAA2010090791929](https://openairdocs.org/sdr/USAA2010090791929), Sep 8, 2010: SKIN. CRACKED. PHX - OVERNIGHT - MAJOR REPAIR - CRACK ON FUSELAGE SKIN AT BS 827, S20L. REPAIRED FUSELAGE SKIN AT BS 827, S20L IAW B737 SRM 53-00-01 REPAIR 31.
- [SDR USAA20100907SB143](https://openairdocs.org/sdr/USAA20100907SB143), Sep 6, 2010: POWER SUPPLY. INOPERATIVE. PHX - THE EMERGENCY LIGHTS AT SEAT ROW 1, 2, 3, 4 & 20 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY FOR ROWS 1, 2, 3, AND 4,
- [SDR USAA20100720SB122](https://openairdocs.org/sdr/USAA20100720SB122), Jul 19, 2010: LIGHT. INOPERATIVE. PHX - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT ROW 2B AFT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT AT SEAT ROW 2B AFT. OPERATIO
- [SDR USAA20100719SB121](https://openairdocs.org/sdr/USAA20100719SB121), Jul 17, 2010: LIGHT. BROKEN. PHX - PILOT REPORTED THAT SEAT 13C EMERGENCY EXIT LIGHT ASSEMBLY WAS BROKEN/INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 
- [SDR USAA2010051090936](https://openairdocs.org/sdr/USAA2010051090936), May 8, 2010: SKIN. CRACKED. PHX - LAP INSPECTION - MAJOR REPAIR - 4643118 - AFT FUSELAGE AT BS727C, S25R HAS 3 INCH CRACK AT LAP SEAM VERIFIED BY HFEC INSPECTION. ENDS OF CRACK MARKED. REP
- [SDR USAA2010020490280](https://openairdocs.org/sdr/USAA2010020490280), Feb 4, 2010: FLAP. CRACKED. SAL - MAJOR REPAIR - C22 CHECK - RIGHT WING KRUEGER FLAP CRACKED AT LES 189.5- LES 199.5. REPAIRED RIGHT WING KRUEGER FLAP AT LES 189.5- LES 199 IAW EA 132847.
- [SDR USAA2010020490278](https://openairdocs.org/sdr/USAA2010020490278), Feb 3, 2010: GATE. CRACKED. SAL - MAJOR REPAIR - C22 CHECK - FORWARD ENTRY DOOR LOWER GATE CENTER BRACKET CONNECTION CRACKED. REPAIRED FORWARD ENTRY DOOR LOWER GATE CENTER BRACKET CONNECTI
- [SDR USAA2010020490274](https://openairdocs.org/sdr/USAA2010020490274), Feb 3, 2010: SKIN. CORRODED. SAL - MAJOR REPAIR - C22 CHECK - LEVEL 2 GALVANIC CORROSION ON FUSELAGE SKIN AT BS 907, S26L - S27L. REPAIRED FUSELAGE SKIN AT BS 907, S26L - S27L IAW B737 SRM 
- [SDR USAA2010020490273](https://openairdocs.org/sdr/USAA2010020490273), Feb 3, 2010: SKIN. CRACKED. SAL - MAJOR REPAIR - C22 CHECK - CRACKED PYLON SKIN AT ACCESS PANEL 5727L CUTOUT, NAC 177.50. REPAIRED PYLON SKIN AT ACCESS PANEL 5727L CUTOUT, NAC 177.50 IAW T
- [SDR USAA2010020590287](https://openairdocs.org/sdr/USAA2010020590287), Jan 29, 2010: CROSSBEAM. CRACKED. SAL - MAJOR REPAIR - C22 CHECK - CRACKED CROSS BEAM WEB ON THE FORWARD CARGO DOOR AT BS 422, S26R. REPAIRED CROSS BEAM WEB ON THE FORWARD CARGO DOOR AT BS 422, 
- [SDR USAA2010020590285](https://openairdocs.org/sdr/USAA2010020590285), Jan 26, 2010: STRINGER. CRACKED. SAL - MAJOR REPAIR - C22 CHECK - CRACKED STRINGER AT BS 294.5 - BS 303.90, S10L. REPAIRED STRINGER AT BS 294.5 - BS 303.90, S10L IAW B737 SRM 51-70-11.
- [SDR USAA2010020590289](https://openairdocs.org/sdr/USAA2010020590289), Jan 18, 2010: DOOR FRAME. CRACKED. SAL - MAJOR REPAIR - C22 CHECK - CRACKED FRAME ON THE FORWARD CARGO DOOR AT BS 469.90, S26R. REPAIRED FRAME ON THE FORWARD CARGO DOOR AT BS 469.90, S26R IAW EA 
- [SDR USAA2010020590292](https://openairdocs.org/sdr/USAA2010020590292), Jan 13, 2010: PAN. CRACKED. SAL - MAJOR REPAIR - C22 CHECK - CRACK ON LEFT WING FORWARD SPAR SEAL PAN ASSEMBLY AT WBL 190. REPLACED LEFT WING FORWARD SPAR SEAL PAN ASSEMBLY AT WBL 190 IAW 
- [SDR USAA2010020290263](https://openairdocs.org/sdr/USAA2010020290263), Jan 13, 2010: WEB. CORRODED. SAL - C22 - MAJOR REPAIR - CORROSION ON LOWER WEB BETWEEN BS 294 TO BS 344, RBL 54. REPLACED LOWER WEB BETWEEN BS 294 TO BS 344, RBL 54 IAW B737 SRM 51-10-02 & 
- [SDR USAA2010020490279](https://openairdocs.org/sdr/USAA2010020490279), Jan 12, 2010: STRAP. CORRODED. SAL - MAJOR REPAIR - C22 - GALVANIC CORROSION ON STRAP AT BS 277 - BS 294.5, RBL 54. REPLACED STRAP AT BS 277 - BS 294.5, RBL 54 IAW SRM 51-10-02.
- [SDR USAA2010020190251](https://openairdocs.org/sdr/USAA2010020190251), Jan 10, 2010: COLLAR. WORN. SAL - C22 - MAJOR REPAIR - NOSE LANDING GEAR FAILED TORSION FREE PLAY INSPECTION. REPLACED NOSE LANDING GEAR STEERING COLLAR ASSEMBLY IAW B737 AMM 32-51-61 PARG
- [SDR USAA2010020190249](https://openairdocs.org/sdr/USAA2010020190249), Jan 9, 2010: TEE FITTING. CORRODED. SAL - C22 - MAJOR REPAIR - CORROSION ON TEE AT BS 303.5, LBL 44. REPLACED TEE AT BS 303.5, LBL 44 IAW B737 SRM 51-10-02 & BOEING DRAWING 65-45834.
- [SDR USAA2010020190250](https://openairdocs.org/sdr/USAA2010020190250), Jan 8, 2010: TAB. DELAMINATED. SAL - C22 - MAJOR REPAIR - DELAMINATION ON LEFT ELEVATOR TAB BETWEEN ELEV STA 32.075 TO ELEV STA 124.047. REPAIRED LEFT ELEVATOR TAB BETWEEN ELEV STA 32.075 TO 
- [SDR USAA2010012990233](https://openairdocs.org/sdr/USAA2010012990233), Jan 8, 2010: TAB. DELAMINATED. SAL - C22 - MAJOR REPAIR - DELAMINATION ON RIGHT ELEVATOR TAB HINGE CUTOUT UPPER SURFACE BETWEEN ELEV STA 32.075 TO 124.040. REPAIRED RIGHT ELEVATOR TAB HINGE C
- [SDR USAA2010020290265](https://openairdocs.org/sdr/USAA2010020290265), Jan 7, 2010: STRUCTURE. CORRODED. SAL - C22 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON INNER CHORD AT BS 294.5, RBL 54. REPLACED CHORD AT BS 294.5, RBL 54 IAW B737 SRM 51-10-02.
- [SDR USAA2010020290264](https://openairdocs.org/sdr/USAA2010020290264), Jan 7, 2010: FLOORBEAM. CORRODED. SAL - C22 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM CHORD UPPER FACE AT BS 294.5, RBL 34. REPAIRED FLOORBEAM CHORD UPPER FACE AT BS 294.5, RBL 34
- [SDR USAA2010020190248](https://openairdocs.org/sdr/USAA2010020190248), Jan 7, 2010: FLAP. DELAMINATED. SAL - C22 - MAJOR REPAIR - DELAMINATION ON RIGHT INBOARD FORE FLAP BETWEEN WBL 176 TO 182, 284.96 TO 96.96 & WBL 117. REPAIRED RIGHT INBOARD FORE FLAP BETWEEN W
- [SDR USAA2010020590291](https://openairdocs.org/sdr/USAA2010020590291), Jan 6, 2010: SKIN. CRACKED. SAL - MAJOR REPAIR - C22 CHECK - CRACKED EXTERIOR FUSELAGE SKIN AT THE L1 DOOR UPPER AND LOWER HINGE CUTOUTS, BS 303.9 AND S12L - S14L. REPAIRED EXTERIOR FUSELA
- [SDR USAA2010020590290](https://openairdocs.org/sdr/USAA2010020590290), Jan 6, 2010: BULKHEAD. CRACKED. SAL - MAJOR REPAIR - C22 CHECK - CRACKED BULKHEAD SKIN WEB AT BS 178, WL 184. REPAIRED BULKHEAD SKIN WEB AT BS 178, WL 184 IAW EA 132693.
- [SDR USAA2010020590288](https://openairdocs.org/sdr/USAA2010020590288), Jan 6, 2010: DOOR FRAME. CRACKED. SAL - MAJOR REPAIR - C22 CHECK - CRACKED FRAME ON THE FORWARD CARGO DOOR AT BS 422, S26R. REPAIRED FRAME ON THE FORWARD CARGO DOOR AT BS 422, S26R IAW EA 132691
- [SDR USAA2010012590182](https://openairdocs.org/sdr/USAA2010012590182), Jan 6, 2010: TIE CLIP. CRACKED. SAL - C22 - MAJOR REPAIR - CRACK ON STRINGER TIE AT BS 500C, S26R. REPLACED STRINGER TIE AT BS 500C, S26R IAW B737 SRM 51-10-02.
- [SDR USAA2010012090148](https://openairdocs.org/sdr/USAA2010012090148), Jan 6, 2010: STRINGER CLIP. CRACKED. SAL - C22 - MAJOR REPAIR - NR 6227488 - CRACK ON STRINGER TIE AT BS 500D, S26R. REPLACED STRINGER TIE AT BS 500D, S26R IAW B737 SRM 51-40-02 AND BOEING DRAWING 
- [SDR USAA2010011990127](https://openairdocs.org/sdr/USAA2010011990127), Jan 6, 2010: STRINGER CLIP. CRACKED. MAJOR REPAIR - CRACK ON STRINGER CLIP AT BS 500B, S26R. REPLACED STRINGER CLIP AT BS 500B, S26R IAW SRM 51-40-02 AND DRAWING NR 69-35350-7.
- [SDR USAA2010011990126](https://openairdocs.org/sdr/USAA2010011990126), Jan 6, 2010: STRINGER CLIP. CRACKED. MAJOR REPAIR - CRACK ON STRINGER CLIP AT BS 500C, S26L. REPLACED STRINGER CLIP AT BS 500C, S26L IAW SRM 51-40-02 AND DRAWING NR 69-35352-1.
- [SDR USAA2010020490277](https://openairdocs.org/sdr/USAA2010020490277), Jan 5, 2010: FLAP. DELAMINATED. SAL - MAJOR REPAIR - C22 CHECK - RIGHT WING OUTBOARD AFT FLAP TRAILING EDGE IS DELAMINATED. REPAIRED RIGHT WING OUTBOARD AFT FLAP TRAILING EDGE IAW B737 SRM 51-
- [SDR USAA20090925SB152](https://openairdocs.org/sdr/USAA20090925SB152), Sep 24, 2009: LIGHT. INOPERATIVE. PHX - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 3 (FORWARD BULB) AND 20 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SEAT MOUNTED
- [SDR USAA2009081092059](https://openairdocs.org/sdr/USAA2009081092059), Aug 9, 2009: SKIN. CRACKED. PHX - OVERNIGHT - MAJOR REPAIR - FUSELAGE SKIN CRACKED ABOVE LAP SEAM AT STRINGER 20L BETWEEN BS 794 TO BS 798. REPAIRED FUSELAGE SKIN ABOVE LAP SEAM AT STRINGE
- [SDR USAA2009042891002](https://openairdocs.org/sdr/USAA2009042891002), Apr 26, 2009: FLAP. SEPARATED. PHX - RON - MAJOR REPAIR - SEPARATION ON RIGHT WING OUTBOARD AFT FLAP TRAILING EDGE APPROX 6 INCHES FROM OUTBOARD END. REPAIRED RIGHT WING OUTBOARD AFT FLAP TRA
- [SDR USAA2009042891001](https://openairdocs.org/sdr/USAA2009042891001), Apr 26, 2009: SPINDLE. CRACKED. PHX - RON - MAJOR REPAIR - RIGHT WING OUTBOARD FLAP SPINDLE UT INSPECTION INDICATES THAT THE SPINDLE IS CRACKED PER STEP 2 OF US AIRWAYS TASK CARD I3C57018. REP
- [SDR USAA20090427SB069](https://openairdocs.org/sdr/USAA20090427SB069), Apr 26, 2009: LIGHT. INOPERATIVE. PHX - MAINTENANCE REPORTED THE EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT AFT OF THE L2 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT HOUSING, INCLUDI
- [SDR USAA20090409SB053](https://openairdocs.org/sdr/USAA20090409SB053), Apr 8, 2009: SLIDING WINDOW. CRACKED. EN ROUTE FROM PHX TO ELP, DURING CRUISE, THE FIRST OFFICER'S SLIDING WINDOW ARCED AND CRACKED. FLIGHT RETURNED TO FIELD AT PHX AND LANDED WITHOUT FURTHER INCIDE
- [SDR USAA2009040290784](https://openairdocs.org/sdr/USAA2009040290784), Mar 29, 2009: SKIN. CRACKED. PHX - RON - MAJOR REPAIR - CRACK IN FUSELAGE SKIN BETWEEN BS 500C TO 500C + 10 INCHES, ABOVE S15R. REPAIRED FUSELAGE SKIN BETWEEN BS 500C TO 500C + 10 INCHES, A
- [SDR USAA20090318SB037](https://openairdocs.org/sdr/USAA20090318SB037), Mar 17, 2009: LIGHT. INOPERATIVE. PHX - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 2, LEFT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.
- [SDR USAA920082070](https://openairdocs.org/sdr/USAA920082070), Oct 20, 2008: INTERCOSTAL. CORRODED. SAL C21 MAJOR REPAIR NR 6136496 CORROSION ON INTERCOSTAL BETWEEN BS967 TO BS986.5, WL208.1, RBL17.5 IN PASSENGER CABIN. REPAIRED INTERCOSTAL BETWEEN BS967 TO BS
- [SDR USAA2008120292175](https://openairdocs.org/sdr/USAA2008120292175), Oct 18, 2008: WEB. CORRODED. SAL - C21 - MAJOR REPAIR - CORROSION ON WEB BETWEEN BS 847 TO BS 867, RBL 21. REPAIRED WEB BETWEEN BS 847 TO BS 867, RBL 21 IAW SRM 51-10-02.
- [SDR USAA2008111492059](https://openairdocs.org/sdr/USAA2008111492059), Oct 14, 2008: WEB. CRACKED. SAL - MAJOR REPAIR - C21 CHECK - NR# 6136447, CRACKED WEB AT BS 303.9, S16L. REPLACED WEB AT BS 303.9, S16L I/A/W US AIRWAYS TASK CARD M1C53001.
- [SDR USAA920081975](https://openairdocs.org/sdr/USAA920081975), Oct 14, 2008: FLOORBEAM. CORRODED. SAL C21 MAJOR REPAIR NR 6136443 CORROSION ON FLOORBEAM UPPER CHORD AT BS967, WL208, LBL18. REPAIRED FLOORBEAM UPPER CHORD AT BS967, WL208, LBL18 IAW B737 SRM 53
- [SDR USAA2008120292176](https://openairdocs.org/sdr/USAA2008120292176), Oct 10, 2008: INTERCOSTAL. CORRODED. SAL - C21 - MAJOR REPAIR - CORROSION ON INTERCOSTAL BETWEEN BS 967 TO BS 986.5, WL 208.1, LBL 17.5. REPAIRED INTERCOSTAL BETWEEN BS 967 TO BS 986.5, WL 208.1, L
- [SDR USAA920082069](https://openairdocs.org/sdr/USAA920082069), Oct 10, 2008: FLOORBEAM. CORRODED. SAL C21 MAJOR REPAIR NR 6139584 INTERGRANULAR CORROSION ON FLOOR BEAM UPPER CHORD AT BS986.5, WL208.1, BETWEEN LBL44 TO RBL44 IN PASSENGER CABIN. REPAIRED FLOOR
- [SDR USAA920082014](https://openairdocs.org/sdr/USAA920082014), Oct 10, 2008: WEB. CORRODED. SAL C21 MAJOR REPAIR NR 6139589 CORROSION ON WEB BETWEEN BS986.5 TO BS1006, WL208.1, RBL43. REPLACED WEB BETWEEN BS986.5 TO BS1006, WL208.1, RBL43 IAW BOEING DR
- [SDR USAA920082013](https://openairdocs.org/sdr/USAA920082013), Oct 10, 2008: WEB. CORRODED. SAL C21 MAJOR REPAIR NR 6139595 CORROSION ON WEB BETWEEN BS1016 TO BS1032, WL208.1, BLO TO LBL34. REPLACED WEB BETWEEN BS1016 TO BS1032, WL208.1, BLO TO LBL34 I
- [SDR USAA920082004](https://openairdocs.org/sdr/USAA920082004), Oct 10, 2008: SEAT TRACK. CORRODED. SAL C21 MAJOR REPAIR NR 6139601 CORROSION ON SEAT TRACK UPPER AND LOWER FLANGE BETWEEN BS907 TO BS947.5, WL208.1, LBL45.50. REPAIRED SEAT TRACK UPPER AND LOWER 
- [SDR USAA920082001](https://openairdocs.org/sdr/USAA920082001), Oct 10, 2008: SEAT TRACK. CORRODED. SAL C21 MAJOR REPAIR NR 6139600 CORROSION ON SEAT TRACK BETWEEN BS887 TO BS947.5, WL208, LBL 24.75. REPAIRED SEAT TRACK BETWEEN BS887 TO BS947.5, WL208, LBL 24.
- [SDR USAA920081990](https://openairdocs.org/sdr/USAA920081990), Oct 10, 2008: WEB. CORRODED. SAL MAJOR REPAIR C21 CHECK NR 6139596 CORROSION ON SHEAR WEB AT BS 1016 - BS 1032, BL 0 - RBL 34, WL 208.1. REPLACED SHEAR WEB AT BS 1016 - BS 1032, BL 0 - RBL 
- [SDR USAA920081976](https://openairdocs.org/sdr/USAA920081976), Oct 10, 2008: FLOORBEAM. CORRODED. SAL C21 MAJOR REPAIR NR 6139586 CORROSION ON FLOORBEAM UPPER CHORD AT BS967, WL208, LBL 18 TO RBL 18. REPAIRED FLOORBEAM UPPER CHORD AT BS967, WL208, LBL 18 TP 

All 315: https://openairdocs.org/deregistered/N158AW-2011-06-15/reports.md

## FAA accident and incident reports (3)

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 20011225038369I](https://openairdocs.org/incident/20011225038369I), Dec 25, 2001: Boeing 7373G7 (N158AW), Omaha, NE. (-23) America west flight 513 inbound to Omaha declared an emergency due to a flap problem. Aircraft landed without incident. Contract maintenance changed the…
- [Incident 19910318013639I](https://openairdocs.org/incident/19910318013639I), Mar 18, 1991: Boeing 7373G7 (N158AW), Las Vegas, NV, Minor damage. Recap separted from tire assembly on takeoff. Landed at destination safely with emergency equipment standing by.
- [Incident 19890918051889I](https://openairdocs.org/incident/19890918051889I), Sep 18, 1989: Boeing 7373G7 (N158AW), Las Vegas, NV, Minor damage. Had hydraulic system pressure problem. Found engine driven pump case drain filter housing assembly installed wrong.

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