# N156AW: 1987 Boeing 737-3G7, registration cancelled 2012-02-15 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 15, 2012 - Status when cancelled: Sale reported - 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: 23778 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 15, 1987 - Last registry action: February 15, 2012 - Mode S code: A0E08E - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Individual - Owner's area on the map: 25.8050° N, 80.3151° W: Placed by OpenAirDocs at the center of ZIP code 33122, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N156AW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=156AW - Page: https://openairdocs.org/deregistered/N156AW-2012-02-15 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 (327, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA2011093000002](https://openairdocs.org/sdr/USAA2011093000002), Sep 29, 2011: LENS. MISSING. MAINTENANCE REPORTED ROW 23 EMERGENCY EXIT LIGHT LENS CAP MISSING. MAINTENANCE INSTALLED NEW LENS CAP AT ROW 23 EMERGENCY EXIT LIGHT. OPS CHECK GOOD. - [SDR USAA2011092200002](https://openairdocs.org/sdr/USAA2011092200002), Sep 21, 2011: LENS. DIRTY. MAINTENANCE REPORTED THE LT SIDE, AFT OF WING TO BODY FAIRING, EMERGENCY LIGHT LENS IS DIRTY. MAINTENANCE CLEANED LT SIDE AFT EMERGENCY LIGHT LENS. - [SDR USAA2011081600001](https://openairdocs.org/sdr/USAA2011081600001), Aug 16, 2011: CONNECTOR. DAMAGED. MAINTENANCE REPORTED SEAT ROW 4ABC EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE RE-TERMINATED CONNECTOR AT SEAT 4C IAW SWPM 20-64-17. OPERATIONAL CHECK GOOD - [SDR USAA2011081200014](https://openairdocs.org/sdr/USAA2011081200014), Aug 11, 2011: FRAME. CRACKED. WEEKLY CHECK - CRACK IN FUSELAGE FRAME AT BS 520 BETWEEN S20L TO S21L. REPAIRED FUSELAGE FRAME AT BS 520 BETWEEN S20L TO S21L IAW B737 SRM 53-00-07 REPAIR 13. - [SDR USAA2011081200013](https://openairdocs.org/sdr/USAA2011081200013), Aug 11, 2011: FRAME. CRACKED. WEEKLY CHECK - CRACK IN FUSELAGE FRAME AT BS 500D BETWEEN S20L TO S21L. REPAIRED FUSELAGE FRAME AT BS 500D BETWEEN S20L TO S21L IAW B737 SRM 53-00-07 REPAIR 13. - [SDR USAA2011081200012](https://openairdocs.org/sdr/USAA2011081200012), Aug 11, 2011: FRAME. CRACKED. WEEKLY CHECK - CRACK IN FUSELAGE FRAME AT BS 500B BETWEEN S20L TO S21L. REPAIRED FUSELAGE FRAME AT BS 500B BETWEEN S20L TO S21L IAW B737 SRM 53-00-07 REPAIR 13. - [SDR USAA2011081200011](https://openairdocs.org/sdr/USAA2011081200011), Aug 11, 2011: FRAME. CRACKED. WEEKLY CHECK - CRACK IN FUSELAGE FRAME AT BS 500D BETWEEN S20R TO S21R. REPAIRED FUSELAGE FRAME AT BS 500D BETWEEN S20R TO S21R IAW B737 SRM 53-00-07 REPAIR 13. - [SDR USAA2011081200010](https://openairdocs.org/sdr/USAA2011081200010), Aug 11, 2011: FRAME. CRACKED. WEEKLY CHECK - CRACK IN FUSELAGE FRAME AT BS 500C BETWEEN S20R TO S21R. REPAIRED FUSELAGE FRAME AT BS 500C BETWEEN S20R TO S21R IAW B737 SRM 53-00-07 REPAIR 13. - [SDR USAA2011081200009](https://openairdocs.org/sdr/USAA2011081200009), Aug 11, 2011: FRAME. CRACKED. WEEKLY CHECK - CRACK IN FUSELAGE FRAME AT BS 500B BETWEEN S20R TO S21R. REPAIRED FUSELAGE FRAME AT BS 500B BETWEEN S20R TO S21R IAW B737 SRM 53-00-07 REPAIR 13. - [SDR USAA2011080800006](https://openairdocs.org/sdr/USAA2011080800006), Aug 5, 2011: LENS. MISSING. CREW REPORTED THE EMERGENCY EXIT AISLE LIGHT AT SEAT 11C IS MISSING LENS COVER THAT SAYS EXIT. MAINTENANCE REPLACED LENS COVER FOR EMERGENCY EXIT AISLE LIGHT AT - [SDR USAA2011071900002](https://openairdocs.org/sdr/USAA2011071900002), Jul 18, 2011: SKIN PANEL. CRACKED. OVERNIGHT CHECK - CRACK FOUND ON KEEL BEAM PANEL LOCATED AFT & TO THE LEFT OF RT PACK EXHAUST LOUVERS AT BS 550, RBL 6. REPAIRED KEEL BEAM PANEL AT BS 550, RBL - [SDR USAA2011070100003](https://openairdocs.org/sdr/USAA2011070100003), Jun 30, 2011: BATTERY. WEAK. MCN - C23 - 2 EA AFT EMERGENCY FLASHLIGHT BATTERIES WEAK. REMOVED AND REPLACED 2EA AFT EMERGENCY FLASHLIGHT BATTERIES AS REQUIRED. - [SDR USAA2011070700005](https://openairdocs.org/sdr/USAA2011070700005), Jun 28, 2011: SKIN. CRACKED. C23 CHECK - CRACK ON NR 1 PYLON SKIN AND PANEL DOUBLER CRACKED PAST STOP DRILL AT PANEL 5727L. REPAIRED NR 1 PYLON SKIN AND PANEL DOUBLER CRACKED PAST STOP DRIL - [SDR USAA2011070500014](https://openairdocs.org/sdr/USAA2011070500014), Jun 15, 2011: SKIN. CRACKED. MCN - C23 CHECK - CRACK ON LOWER AFT CORNER OF L2 DOOR OUTER SKIN UPPER HINGE CUTOUT AT BS 966, WL 266. REPAIRED LOWER AFT CORNER OF L2 DOOR OUTER SKIN UPPER HI - [SDR USAA2011070100025](https://openairdocs.org/sdr/USAA2011070100025), Jun 15, 2011: STRAP. CRACKED. MCN - C23 CHECK - CRACK ON FLOORBEAM STABILIZING STRAP AT BS 344, BL 0. REPAIRED FLOORBEAM STABILIZING STRAP AT BS 344, BL 0 IAW B737 SRM 53-10-51 FIG 201. - [SDR USAA2011070500012](https://openairdocs.org/sdr/USAA2011070500012), Jun 14, 2011: DOOR FRAME. CRACKED. MCN - C23 CHECK - CRACK ON R1 DOOR AFT FRAME AT BS 329, BETWEEN WL 237 TO WL 275. REPAIRED R1 DOOR AFT FRAME AT BS 329, BETWEEN WL 237 TO WL 275 IAW EA 130620. - [SDR USAA2011051891887](https://openairdocs.org/sdr/USAA2011051891887), May 15, 2011: SKIN. CRACKED. PHX - RON - CRACK ON FUSELAGE SKIN AT BS 727E, S21L. REPAIRED FUSELAGE SKIN AT BS 727E, S21L IAW B737 SRM 53-00-01 REPAIR 31. - [SDR USAA20110516SB077](https://openairdocs.org/sdr/USAA20110516SB077), May 15, 2011: LIGHT. INOPERATIVE. PHX - MAINTENANCE REPORTED THE EMERGENCY LIGHT ON SEAT ROW 18 INOPERATIVE. RELAMP WAS NO HELP. MAINTENANCE REMOVED AND REPLACED THE AISLE LIGHT ASSEMBLY AT SEAT - [SDR USAA2011051291836](https://openairdocs.org/sdr/USAA2011051291836), May 10, 2011: WEDGE. DELAMINATED. PHX - B4 - DELAMINATION ON LEFT WING NR 2 SLAT TRAILING EDGE WEDGE AT THE INBOARD END. REPLACED LEFT WING NR 2 SLAT IAW B737 AMM 27-81-21-4 & 27-81-00. - [SDR USAA20110504SB071](https://openairdocs.org/sdr/USAA20110504SB071), May 1, 2011: GEARBOX. FAILED. LAS - DURING CRUISE, AT FL330, CREW REPORTED THE RIGHT ENGINE HAD FLAMED OUT AND THAT THEY RECIEVED A LOW FUEL FLOW INDICATION. CREW WAS UNABLE TO RESTART THE E - [SDR USAA20101217SB202](https://openairdocs.org/sdr/USAA20101217SB202), Dec 16, 2010: TERMINAL. INOPERATIVE. PHX - THE CABIN AISLE EMERGENCY LIGHT WAS INOPERATIVE AT 4L. REPLACED THE EMERGENCY LIGHT TERMINAL. OPERATIONALLY CHECKS GOOD. - [SDR USAA2010121793110](https://openairdocs.org/sdr/USAA2010121793110), Dec 16, 2010: SKIN. CRACKED. PHX - OVERNIGHT - MAJOR REPAIR - CRACK ON FUSEALAGE SKIN 2 INCHES ABOVE S25L AT BS 727. REPAIRED FUSELAGE SKIN 2 INCHES ABOVE S25L AT BS 727 IAW B737 SRM 53-00- - [SDR USAA2010121793109](https://openairdocs.org/sdr/USAA2010121793109), Dec 16, 2010: PANEL. CRACKED. PHX - OVERNIGHT - MAJOR REPAIR - CRACK ON KEEL BEAM PANEL AT BS 727, BETWEEN S30L TO S30R. REPAIRED KEEL BEAM PANEL AT BS 727, BETWEEN S30L TO S30R IAW B737 SRM - [SDR USAA20100629SB106](https://openairdocs.org/sdr/USAA20100629SB106), Jun 25, 2010: WIRE. BROKEN. PHX - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEATS 9 AND 22 INOPERATIVE. MAINTENANCE REPAIRED SPLICE AT SEAT 9 AND RELAMPED LIGHT AT SEAT 22. OPERATIONAL - [SDR USAA2010061491112](https://openairdocs.org/sdr/USAA2010061491112), Jun 13, 2010: SKIN. CRACKED. PHX - B1 - MAJOR REPAIR - FUSELAGE SKIN CRACK AT STA 787. STR 20R. REPAIRED FUSELAGE SKIN AT STA 787 STR 20R IAW B737 SRM 53-00-01 REPAIR 31. - [SDR USAA20100614SB101](https://openairdocs.org/sdr/USAA20100614SB101), Jun 13, 2010: WIRE. BROKEN. PHX - MAINTENANCE REPORTED THE EMERGENCY LIGHT WIRE AT SEAT ROW 11 LEFT, WAS BROKEN. MAINTENANCE REPAIRED BROKEN WIRE ON EMERGENCY LIGHT AT SEAT ROW 11, LEFT PE - [SDR USAA20100602SB095](https://openairdocs.org/sdr/USAA20100602SB095), Jun 1, 2010: CONNECTOR. LOOSE. PHX - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT ROW 18, LEFT SIDE, INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR LOOSE. RECONNECTED LOOSE CONNECTOR. OPERA - [SDR USAA20100518SB077](https://openairdocs.org/sdr/USAA20100518SB077), May 15, 2010: WIRE. BROKEN. PHX - MAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHT AT SEAT 9C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT SEAT 9C PER CHAPTER 20. - [SDR USAA20100504SB064](https://openairdocs.org/sdr/USAA20100504SB064), Apr 30, 2010: WIRE. BROKEN. PHX - PILOT REPORTED THE EMERGENCY EXIT LIGHTS AT 9C AND 19C WERE INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT SEAT 9C AND RELAMPED LIGHT AT 19C. ALL LIGHTS - [SDR USAA20100412BB050](https://openairdocs.org/sdr/USAA20100412BB050), Apr 9, 2010: TARGET. DEFECTIVE. PVR FLT 349 EN-ROUTE PHX TO PVR. ON APPROACH, WITH FLAPS 1 SELECTED, THE NR 6 LEADING EDGE DEVICE DID NOT EXTEND. THE OVERHEAD PANEL AND FORWARD FLAP TRANSIT AM - [SDR USAA2010040590716](https://openairdocs.org/sdr/USAA2010040590716), Mar 30, 2010: SUPPORT. CRACKED. SAL - C22 - MAJOR REPAIR - CRACK ON SUPPORT ZEE SECTION AT BS 492.4 TO BS 500A, S26R. REPLACED SUPPORT ZEE SECTION AT BS 492.4 TO BS 500A, S26R IAW B737 SRM 51- - [SDR USAA2010032690647](https://openairdocs.org/sdr/USAA2010032690647), Mar 25, 2010: STRINGER CLIP. CRACKED. SAL - MAJOR REPAIR - C22 CHECK - CRACKED STRINGER TIE CLIP AT BS 500D, S26R. REPLACED STRINGER TIE CLIP AT BS 500D, S26R IAW B737 SRM 51-10-02. - [SDR USAA2010032690646](https://openairdocs.org/sdr/USAA2010032690646), Mar 25, 2010: STRINGER CLIP. CRACKED. SAL - MAJOR REPAIR - C22 CHECK - CRACKED STRINGER TIE CLIP AT BS 500C, S27L. REPLACED STRINGER TIE CLIP AT BS 500C, S27L IAW B737 SRM 51-10-02. - [SDR USAA2010032690645](https://openairdocs.org/sdr/USAA2010032690645), Mar 25, 2010: STRINGER CLIP. CRACKED. SAL - MAJOR REPAIR - C22 CHECK - CRACKED STRINGER TIE CLIP AT BS 500D, S27L. REPLACED STRINGER TIE CLIP AT BS 500D, S27L IAW B737 SRM 51-10-02. - [SDR USAA2010032590639](https://openairdocs.org/sdr/USAA2010032590639), Mar 24, 2010: SILL. CORRODED. SAL - MAJOR REPAIR - C22 CHECK - LEVEL 2 GALVANIC CORROSION ON THE L1 DOOR CUTOUT LOWER SILL CHORD AT BS 312 - BS 337, S17L. REPLACED THE L1 DOOR CUTOUT LOWER S - [SDR USAA2010032490637](https://openairdocs.org/sdr/USAA2010032490637), Mar 23, 2010: STRINGER CLIP. CRACKED. SAL - MAJOR REPAIR - C22 CHECK - CRACKED STRINGER TIE CLIP AT BS 380, S20L. REPLACED STRINGER TIE CLIP AT BS 380 S20L IAW 737 SRM 51-10-02. - [SDR USAA2010032990679](https://openairdocs.org/sdr/USAA2010032990679), Mar 17, 2010: STRINGER SPLICE. CORRODED. SAL - C22 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON STRINGER SPLICE AT BS 364, S26L. REPLACED STRINGER SPLICE AT BS 364, S26L IAW B737 SRM 51-10-02 & BOEIN - [SDR USAA2010040790726](https://openairdocs.org/sdr/USAA2010040790726), Mar 16, 2010: BULKHEAD. CORRODED. SAL - C22 - MAJOR REPAIR - CORROSION ON FUSELAGE BULKHEAD LOWER CHORD AT BS 227.8 BETWEEN BL 0 TO RBL 8. REPAIRED FUSELAGE BULKHEAD LOWER CHORD AT BS 227.8 BETW - [SDR USAA2010040590719](https://openairdocs.org/sdr/USAA2010040590719), Mar 15, 2010: FITTING. CRACKED. SAL - C22 - MAJOR REPAIR - CRACK ON CENTER CONNECTION FITTING OF FORWARD ENTRY DOOR LOWER GATE AT BS 328, WL 209.8. REPAIRED CENTER CONNECTION FITTING OF FORWAR - [SDR USAA2010032990674](https://openairdocs.org/sdr/USAA2010032990674), Mar 14, 2010: WEB. CRACKED. SAL - C22 - MAJOR REPAIR - CRACK ON SUPPORT WEB BETWEEN BS 294.5 TO BS 328 + 1 INCH, S17R AT FORWARD SERVICE DOOR. REPLACED SUPPORT WEB BETWEEN BS 294.5 TO BS 3 - [SDR USAA2010032390633](https://openairdocs.org/sdr/USAA2010032390633), Mar 13, 2010: TIE CLIP. CRACKED. SAL - C22 - MAJOR REPAIR - CRACKED STRINGER TIE CLIP AT BS 727D, S5R. REPLACED STRINGER TIE CLIP AT BS 727D, S5R IAW B737 SRM 51-10-02 & BOEING DRAWING 65C25229 - [SDR USAA2010032390632](https://openairdocs.org/sdr/USAA2010032390632), Mar 13, 2010: TIE CLIP. CRACKED. SAL - C22 - MAJOR REPAIR - CRACKED STRINGER TIE CLIP AT BS 727C, S7L. REPLACED STRINGER TIE CLIP AT BS 727C, S7L IAW B737 SRM 51-10-02 & BOEING DRAWING 65C25228 - [SDR USAA2010040890742](https://openairdocs.org/sdr/USAA2010040890742), Mar 12, 2010: HINGE PIN. CORRODED. SAL - C22 - MAJOR REPAIR - CORROSION ON LEFT HORIZONTAL STABILIZER OUTER HINGE PIN AT BS 1154, WL 274. REPLACED LEFT HORIZONTAL STABILIZER OUTER HINGE PIN AT BS - [SDR USAA2010040890741](https://openairdocs.org/sdr/USAA2010040890741), Mar 12, 2010: HINGE PIN. CORRODED. SAL - C22 - MAJOR REPAIR - CORROSION ON LEFT HORIZONTAL STABILIZER INNER HINGE PIN AT BS 1154, WL 274. REPLACED LEFT HORIZONTAL STABILIZER INNER HINGE PIN AT BS - [SDR USAA2010040890740](https://openairdocs.org/sdr/USAA2010040890740), Mar 12, 2010: HINGE PIN. CORRODED. SAL - C22 - MAJOR REPAIR - CORROSION ON RIGHT HORIZONTAL STABILIZER OUTER HINGE PIN AT BS 1154, WL 274. REPLACED RIGHT HORIZONTAL STABILIZER OUTER HINGE PIN AT - [SDR USAA2010040890739](https://openairdocs.org/sdr/USAA2010040890739), Mar 12, 2010: HINGE PIN. CORRODED. SAL - C22 - MAJOR REPAIR - CORROSION ON RIGHT HORIZONTAL STABILIZER INNER HINGE PIN AT BS 1154, WL 274. REPLACED RIGHT HORIZONTAL STABILIZER INNER HINGE PIN AT - [SDR USAA2010040890737](https://openairdocs.org/sdr/USAA2010040890737), Mar 12, 2010: SKIN. CORRODED. SAL - C22 - MAJOR REPAIR - CORROSION ON INTERNAL SKIN AT BS 518.5 BETWEEN S28L TO S28R. REPAIRED INTERNAL SKIN AT BS 518.5 BETWEEN S28L TO S28R IAW EA 132933. - [SDR USAA2010040790730](https://openairdocs.org/sdr/USAA2010040790730), Mar 12, 2010: SKIN. DELAMINATED. SAL - C22 - MAJOR REPAIR - DELAMINATION ON RIGHT WING NR 5 GROUND SPOILER UPPER SURFACE. REPLACED RIGHT WING NR 5 GROUND SPOILER IAW B737 AMM 27-62-12-4. - [SDR USAA2010040590717](https://openairdocs.org/sdr/USAA2010040590717), Mar 12, 2010: SUPPORT ANGLE. CORRODED. SAL - C22 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT ANGLE INNER CHORD BETWEEN BS 294.5 TO BS 316, S17R. REPLACED SUPPORT ANGLE BETWEEN BS 294.5 TO - [SDR USAA2010032990678](https://openairdocs.org/sdr/USAA2010032990678), Mar 12, 2010: FRAME. CORRODED. SAL - C22 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FUSELAGE FRAME AT BS 967 BETWEEN S27L TO S27R. REPLACED FUSELAGE FRAME AT BS 967 BETWEEN S27L TO S27R I All 327: https://openairdocs.org/deregistered/N156AW-2012-02-15/reports.md ## Other aircraft with N156AW - [Registered now](https://openairdocs.org/aircraft/N156AW): Dassault-Breguet FALCON 50, S/N 184, built 1987 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.