# N562AU: 1987 Boeing 737-301, registration cancelled 2006-05-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 17, 2006
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-301](https://openairdocs.org/model/boeing-737-301) (registry code 138447R)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 23550
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 8, 1987
- Certificate issued: December 15, 2003
- Last registry action: December 15, 2004
- Mode S code: A72E6B
- Owner when cancelled: [Aeroturbine Inc](https://openairdocs.org/faa-owner/AEROTURBINE%20INC)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Corporation
- 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/N562AU
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=562AU
- Page: https://openairdocs.org/deregistered/N562AU-2006-05-17

From the FAA registry file of November 5, 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 737-301: https://openairdocs.org/model/boeing-737-301.md

## Service difficulty reports (65, newest 50)

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

- [SDR USAASB02067](https://openairdocs.org/sdr/USAASB02067), Mar 29, 2002: COALESCER BAG. CONTAMINATED. CLT - FLT 897 - AFTER TAKEOFF FROM EWR, EN ROUTE TO CLT, A FOUL ODOR WAS REPORTED COMING FROM THE AIR CONDITION PACKS. ODOR DISSIPATED WITHIN 10-15 MINUTES. FLI
- [SDR USAASB01309](https://openairdocs.org/sdr/USAASB01309), Nov 6, 2001: ODOR. DETECTED. CLT - FLT 2135 - AFTER TAKEOFF FROM CLT, EN ROUTE TO MCO, THE FLIGHT ATTENDANTS AND PASSENGERS REPORTED A STRONG SMELL OF BURNING PLASTIC. FLIGHT ATTENDANT REPO
- [SDR USAASB00181](https://openairdocs.org/sdr/USAASB00181), Jun 29, 2000: STRUCTURE. CRACKED. PIT - FLT 9234 - EN ROUTE FROM ROC-CMH, CAPTAIN REPORTED AN AIRFRAME VIBRATION WHICH WAS FELT IN THE AFT GALLEY/LAVATORY AREA. VIBRATION WAS OF HIGH FREQUENCY A
- [SDR USAA000607](https://openairdocs.org/sdr/USAA000607), Apr 26, 2000: PAN. CORRODED. CLT - FOUND FLOOR PAN CORRODED 4 INCHES BY 5 INCHES, STATION 1029, LBL 27 FLOOR PAN. FABRICATED NEW STRAP PER EA 67046. (M)
- [SDR USAA000608](https://openairdocs.org/sdr/USAA000608), Apr 26, 2000: STRAP. CORRODED. CLT - FOUND STRAP CORRODED 3 INCHES BY 6 INCHES, STATION 1016-1006, LBL 27 STRAP. REPAIRED FABRICATED STRAP PER EA 67046. (M)
- [SDR USAA000609](https://openairdocs.org/sdr/USAA000609), Apr 26, 2000: STRAP. CORRODED. CLT - FOUND STRAP CORRODED 6 INCHES BY 3 INCHES, STATION 1006-1016, BL 0, WL 208 STRAP. FABRICATED NEW H STRAP PER EA 67046. (M)
- [SDR USAA000599](https://openairdocs.org/sdr/USAA000599), Apr 25, 2000: KEELBEAM. CORRODED. CLT - FOUND KEELBEAM CORRODED 1 INCH BY 11 INCHES, STATION 500C PLUS 17 TO 500D PLUS 8 STRINGER 28R. INSTALLED DOUBLER PER EA66939. (M)
- [SDR USAA000598](https://openairdocs.org/sdr/USAA000598), Apr 24, 2000: FITTING. CRACKED. CLT - FOUND FITTING CRACKED .375 INCH, LT MLG BEAM OUTBOARD ATTACH FITTING AT UPPER BOLT ON L/B. REPAIRED PER TR 57-40-13. (M)
- [SDR USAA000582](https://openairdocs.org/sdr/USAA000582), Apr 18, 2000: KEELBEAM. CORRODED. CLT - FOUND KEELBEAM CORRODED 2 INCHES BY 6 INCHES, RIGHT KEEL BEAM STATION 500C PLUS 17 TO 500D PLUS 8 STRINGER 28. INSTALLED SPLICE ANGLES PER EA 66939. (M)
- [SDR USAA000575](https://openairdocs.org/sdr/USAA000575), Apr 17, 2000: STRAP. CRACKED. CLT - FOUND SKIN AND BEARSTRAP CRACKED 2 INCHES, LOWER AFT CORNER OF FORWARD SERVICE DOOR CUTOUT. REPAIRED PER SRM 53-10-01. (M)
- [SDR USAA000576](https://openairdocs.org/sdr/USAA000576), Apr 17, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, BS 480, STRINGER 9L. REPAIRED DOUBLER INSTALLED PER SRM 53-00-07 AND SRM 51-30-01. (M)
- [SDR USAA000577](https://openairdocs.org/sdr/USAA000577), Apr 17, 2000: SKIN. CORRODED. CLT - FOUND FUSELAGE SKIN CORRODED, .75 INCH BY .75 INCH, BS 500C PLUS 10, LBL 18. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)
- [SDR USAA000561](https://openairdocs.org/sdr/USAA000561), Apr 14, 2000: FLOORBEAM. CORRODED. FOUND FLOORBEAM CORRODED .500 INCH, STATION 360 RBL 52 - RBL 72. INSTALLED T-CAP PER SRM 53-00-51 AND 51-70-11. CORROSION LEVEL 2 NR C53-107-01. (M)
- [SDR USAA000562](https://openairdocs.org/sdr/USAA000562), Apr 14, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 3 INCHES BY 1 INCH, STATION 328, RBL 51 TOP SURFACE. INSTALLED T-CAP PER SRM 53-10-51. CORROSION LEVEL 2 NR C53-107-01. (M)
- [SDR USAA000554](https://openairdocs.org/sdr/USAA000554), Apr 13, 2000: FRAME. CRACKED. CLT - FRAME CRACKED .75 INCH CRACK, FS 907 JUST LEFT OF STRINGER 1 FRAME. INSTALLED FILLER AND DOUBLER PER EA 66974. (M)
- [SDR USAA000555](https://openairdocs.org/sdr/USAA000555), Apr 13, 2000: BEAM. CORRODED. CLT - FOUND BEAM CORRODED .5 INCH, STATION 1016, LBL 6 AND LBL 10 SCREW HOLES. REPAIRED PER TR 53-20-10 AND EA 66954. (M)
- [SDR USAA000538](https://openairdocs.org/sdr/USAA000538), Apr 10, 2000: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM WEB CRACKED 4 PLACES .25 INCH, BS 328, RBL 44, WL 202.5 RIVET HOLES. REMOVED DAMAGED PER EA 66993. (M)
- [SDR USAA000539](https://openairdocs.org/sdr/USAA000539), Apr 10, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727B, STRINGER 4L. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA000540](https://openairdocs.org/sdr/USAA000540), Apr 10, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727B, STRINGER 5L. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA000541](https://openairdocs.org/sdr/USAA000541), Apr 10, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .500 INCH, BS 887, STRINGER 9L. REMOVED CRACK, INSTALLED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA000542](https://openairdocs.org/sdr/USAA000542), Apr 10, 2000: ANGLE. CRACKED. CLT - FOUND ANGLE CRACKED .5 INCH, BS 639, LBL 45, WL 203 VERT ATTACH ANGLE. REMOVED AND REPLACED ANGLE PER SRM 51-30-02 AND DWG 65-46540. (M)
- [SDR USAA000543](https://openairdocs.org/sdr/USAA000543), Apr 10, 2000: ANGLE. CORRODED. CLT - FOUND ANGLE CORRODED 1 INCH BY 15 INCHES, AFT ENT Z-CHANNEL ANGLE. REMOVED AND REPLACED Z-ANGLE PER SRM 51-40-02. (M)
- [SDR USAA000537](https://openairdocs.org/sdr/USAA000537), Apr 7, 2000: FRAME. CORRODED. CLT - FOUND FRAME CORRODED 2 INCHES, STATION 500D, LBL 18 SKIN. INSTALLED DOUBLER, T-ANGLE AND SHIM PER SRM 53-00-07. (M)
- [SDR USAA000531](https://openairdocs.org/sdr/USAA000531), Apr 7, 2000: BULKHEAD. CRACKED. CLT - FOUND WEB CRACKED .5 INCH, STATION 178, BULKHEAD WEB RBL 4.75, WL 201. INSTALLED DOUBLER PER SRM 53-10-08. (M)
- [SDR USAA000532](https://openairdocs.org/sdr/USAA000532), Apr 7, 2000: BULKHEAD. CRACKED. CLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB LBL 4.75, WL 201. INSTALLED DOUBLER. (M)
- [SDR USAA000533](https://openairdocs.org/sdr/USAA000533), Apr 7, 2000: BULKHEAD. CRACKED. CLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB LBL 4.75, WL 198. INSTALLED DOUBLER PER SRM 53-10-08. (M)
- [SDR USAA000534](https://openairdocs.org/sdr/USAA000534), Apr 7, 2000: BULKHEAD. CRACKED. CLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB RBL 4.75, WL 198. INSTALLED DOUBLER PER SRM 53-10-08. (M)
- [SDR USAA000535](https://openairdocs.org/sdr/USAA000535), Apr 7, 2000: STIFFENER. CRACKED. CLT - FOUND VERTICAL STIFFENER CRACKED 1 INCH, STATION 178 BULKHEAD VERTICAL STIFFENER LBL 6, WL 184. INSTALLED DOUBLER AND ANGLES PER SRM 53-10-08. (M)
- [SDR USAA000536](https://openairdocs.org/sdr/USAA000536), Apr 7, 2000: BULKHEAD. CRACKED. CLT - FOUND WEB CRACKED .25 INCH LONG, STATION 178 BULKHEAD WEB RBL 1, WL 206. INSTALLED DOUBLER PER SRM 53-10-08. (M)
- [SDR USAA000528](https://openairdocs.org/sdr/USAA000528), Apr 5, 2000: WEB. CRACKED. CLT - FOUND WEB CRACKED .25 INCH, BS 710-717, BBL 0, WL 203. INSTALLED DOUBLER PER SRM 51-70-13. (M)
- [SDR USAA000520](https://openairdocs.org/sdr/USAA000520), Apr 4, 2000: SKIN. CRACKED. CLT - FOUND DOOR SKIN CRACKED 5 INCHES BY 5 INCHES, FORWARD SERVICE DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 52-00-01 FIG 203. (M)
- [SDR USAA000523](https://openairdocs.org/sdr/USAA000523), Apr 4, 2000: CHANNEL. CORRODED. CLT - FOUND Z-CHANNEL CORRODED, AFT SERVICE DOOR. REPLACED WITH NEW Z-CHANNEL PER SRM 51-4-02. (M)
- [SDR USAA000524](https://openairdocs.org/sdr/USAA000524), Apr 4, 2000: ANGLE. CORRODED. CLT - FOUND DOOR Z-ANGLE CORRODED 6 FT BY 3 INCHES, STATION 947-1006, LBL 60, AFT ENTRY DOOR Z-ANGLE. INSTALLED NEW Z-ANGLE PER SRM 51-40-02. (M)
- [SDR USAA000522](https://openairdocs.org/sdr/USAA000522), Apr 4, 2000: STRINGER. CRACKED. CLT - FOUND STRINGER CRACKED .5 INCH, STRINGER 18 SHELF AT AFT END INBOARD RIVET IN WEB. REPLACED PER SRM 51-10-02. (M)
- [SDR USAA000521](https://openairdocs.org/sdr/USAA000521), Apr 4, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .75 INCHES LONG, BOTTOM END OF STATION 616 INBOARD CHORD ANGLE RIGHT SIDE. FABRICATED ANGLE AND FILLER PER TR 53-62-01. (M)
- [SDR USAA000508](https://openairdocs.org/sdr/USAA000508), Mar 30, 2000: STRINGER CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727A, STRINGER 2R TIE CLIP AFT SIDE. REPLACED TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA000509](https://openairdocs.org/sdr/USAA000509), Mar 30, 2000: STRINGER CLIP. CRACKED. CLT - FOUND STRINGER TIE CLIP WITH TWO CRACKS .5 INCH LONG, STATION 639, STRINGER 4R FUSELAGE FRAME. REPLACED TIE CLIP PER SRM 51-10-02 AND 51-40-02. (M)
- [SDR USAA000510](https://openairdocs.org/sdr/USAA000510), Mar 30, 2000: DOOR FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, FORWARD SERVICE DOOR FRAME LOWER FORWARD CORNER. INSTALLED DOUBLER AND FILLER PER SRM 51-10-11. (M)
- [SDR USAA000512](https://openairdocs.org/sdr/USAA000512), Mar 30, 2000: BULKHEAD. CRACKED. CLT - FOUND .5 INCH CRACK IN BULKHEAD, STATION 178, WEB LBL .75, WL 188. INSTALLED DOUBLER REPAIR PER SRM 53-10-08. (M)
- [SDR USAA000507](https://openairdocs.org/sdr/USAA000507), Mar 30, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .250 INCH, STATION 827, STRINGER 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA000506](https://openairdocs.org/sdr/USAA000506), Mar 30, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 986, RBL 14 UPPER CHORD FLOORBEAM. REPLACED NEW T-CAP PER TR 53-10-05A. (M)
- [SDR USAA000490](https://openairdocs.org/sdr/USAA000490), Mar 29, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 344 AT BL 0, LBL 22. CORROSION LEVEL 1. INSTALLED FLOORBEAM TOP CAP PER SRM 51-70-12. (M)
- [SDR USAA000491](https://openairdocs.org/sdr/USAA000491), Mar 29, 2000: BEAM. CORRODED. CLT - FOUND BEAM CORRODED .5 INCH BY .5 INCH, BS 1006, LBL 10 BEAM SCREW HOLES. REPAIRED DOUBLER PER SRM 53-00-51. (M)
- [SDR USAA000492](https://openairdocs.org/sdr/USAA000492), Mar 29, 2000: SEAT TRACK. CORRODED. CLT - FOUND SEAT TRACK CORRODED 2 INCHES BY 2 INCHES, STATION 344, LBL 25. INSTALLED NEW SEAT TRACK PER SRM 53-00-52. (M)
- [SDR USAA000464](https://openairdocs.org/sdr/USAA000464), Mar 27, 2000: STRINGER CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727B, STRINGER 16. REMOVED AND REPLACED WITH NEW TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA000465](https://openairdocs.org/sdr/USAA000465), Mar 27, 2000: BEAM. CORRODED. CLT - FOUND BEAM CORRODED .5 INCH, STATION 967, LBL 5 UPPER CHORD SCREW HOLE BEAM. INSTALLED T-CAP PER SRM 53-00-51. CORROSION LEVEL 1. (M)
- [SDR USAA000469](https://openairdocs.org/sdr/USAA000469), Mar 27, 2000: FRAME. CRACKED. CLT - FOUND CHORD CRACKED .5 INCH, BS 616, WL 202 RIGHT SIDE INNER FRAME CHORD AT LOWER FAST. REPAIRED DOUBLER PER TR 53-62-01. (M)
- [SDR USAA000453](https://openairdocs.org/sdr/USAA000453), Mar 24, 2000: ANGLE. CRACKED. CLT - FOUND CHORD ANGLE CRACKED .350 INCH, BS 291.5 BETWEEN STRINGER 10R AND 11R. REPAIRED PER SRM 51-40-02. (M)
- [SDR USAA000454](https://openairdocs.org/sdr/USAA000454), Mar 24, 2000: STRINGER CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .250 INCH, BS 663 STRINGER 10L. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA000455](https://openairdocs.org/sdr/USAA000455), Mar 24, 2000: STRINGER CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .500 INCH, BS 887, STRINGER 1. REPAIRED PER SRM 51-40-02 AND 51-10-00. (M)

All 65: https://openairdocs.org/deregistered/N562AU-2006-05-17/reports.md

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