# N16647: 1997 Boeing 737-524, registration cancelled 2012-05-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 23, 2012 - Exported to: Bermuda - Status when cancelled: Valid registration - Airframe: [Boeing 737-524](https://openairdocs.org/model/boeing-737-524) (registry code 1384721) - 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: 28908 - Year built: 1997 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 24, 1997 - Certificate issued: May 18, 2012 - Last registry action: May 18, 2012 - Mode S code: A10AFC - 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: 40.8659° N, 112.0391° W: Placed by OpenAirDocs at the center of ZIP code 84116, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N16647 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16647 - Page: https://openairdocs.org/deregistered/N16647-2012-05-23 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 737-524: https://openairdocs.org/model/boeing-737-524.md ## Service difficulty reports (34) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA2010040600123](https://openairdocs.org/sdr/CALA2010040600123), Apr 5, 2010: DOUBLER. DAMAGED. DOUBLER FOUND ON RADIO ALTIMETER ANTENNA CUTOUT AT STA 410 WHILE ACCOMPLISHING EA- CONTACT ENGINEERING TO OBTAIN AMOC DISPOSITION FOR DOUBLER. PERFORMED ALL STE - [SDR CALA2010040500115](https://openairdocs.org/sdr/CALA2010040500115), Apr 3, 2010: SKIN. CRACKED. SUPPORT TASK STA 303 L-1 DOOR LOWER HINGE CUTOUT FASTENER HOLE HAS CRACK INDICATION. BOTTOM FASTENER REMOVED PER EA 5330-03736. REPAIRED FUSELAGE SKIN AT L-1 DO - [SDR CALA2010040500114](https://openairdocs.org/sdr/CALA2010040500114), Apr 2, 2010: SKIN. DENTED. SUPPORT TASK DENT AT RT FUSELAGE AT 822.5 15 INCHES BELOW LOWER EDGE OF CARGO DOOR CUTOUT. PREVIOUSLY BLENDED OUT OF LIMITS. NDT SHOWS .050 MATERIAL REMAINS AT - [SDR CALA0800750](https://openairdocs.org/sdr/CALA0800750), Jul 25, 2008: SKIN. DELAMINATED. NR 5 SLAT TRAILING EDGE WARPED AT OUTBOARD END AT PREVIOUS REPAIR. REPAIRED AT OUTBOARD END AT PREVIOUS REPAIR AND UPPER SURFACE REFINISHED PER SRM 51-70-10 AND - [SDR CALA0800749](https://openairdocs.org/sdr/CALA0800749), Jul 25, 2008: FRAME. CRACKED. LEFT SIDE STATION 360 FRAME CRACKED BETWEEN S-8 AND S-9 LT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REPAIRED CRACKED FRAME AT BODY STATION 360 BETWEEN S-8 A - [SDR CALA0800748](https://openairdocs.org/sdr/CALA0800748), Jul 25, 2008: ANGLE. CORRODED. AFT CARGO BAY RIGHT SIDE TRANSLATION ANGLE HAS CORROSION FROM STATION 727B TO 787. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION OF TRANSITION AN - [SDR CALA0800747](https://openairdocs.org/sdr/CALA0800747), Jul 25, 2008: STIFFENER. DEFORMED. STIFFENER STATION 1138 DEFORMED. REMOVED OUT OF LIMITS STIFFENER AT STATION 1138, FABRICATED AND INSTALLED NEW STIFFENER AND SPLICE AT STATION 1138 PER DWG 65-5 - [SDR CALA0800746](https://openairdocs.org/sdr/CALA0800746), Jul 25, 2008: SILL. CORRODED. FWD CARGO LOWER SILL PLATE HAS CORROSION ON TOP AND BOTTOM SIDES. INSTALLED NEW SILL PLATE IN FWD CARGO IAW B737 SRM51-40-02. - [SDR CALA0800745](https://openairdocs.org/sdr/CALA0800745), Jul 25, 2008: FRAME. CORRODED. CORROSION ON L2 DOOR SUPPORT STRUCTURE JUST AFT OF LOWER AFT CORNER. FOUND CORROSION TO BE BEYOND LIMITS PER SRM 51-10-02. FABRICATED AND REPLACED FRAME SECTION - [SDR CALA0800744](https://openairdocs.org/sdr/CALA0800744), Jul 25, 2008: SKIN. DELAMINATED. LEFT OUTBOARD AFT FLAP HAS A DELAMINATED AREA ON LOWER INBOARD SURFACE. REMOVED LEFT OUTBOARD AFT FLAP PER MM 27-51-39, REPAIRED PER SRM 51-70-10, REINSTALLED L - [SDR CALA0800742](https://openairdocs.org/sdr/CALA0800742), Jul 24, 2008: ANGLE. CORRODED. AFT CABIN L2 DOOR Z-ANGLE HAS CORROSION. CORROSION ON L2 DOOR Z-ANGLE FOUND TO BE BEYOND LIMITATIONS PER SRM 53-60-15 FIGURE 1, REMOVED AND REPLACED Z-ANGLE PRE - [SDR CALA0800738](https://openairdocs.org/sdr/CALA0800738), Jul 21, 2008: FRAME. CRACKED. LEFT SIDE STATION 867 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. CUT OUT DAMAGED AREA AND REPAIRED FRAME AT STATION 867 L - [SDR CALA0800737](https://openairdocs.org/sdr/CALA0800737), Jul 21, 2008: INTERCOSTAL. CORRODED. CORROSION FOUND ON STRAP BETWEEN STATION 967 AND 947 LBL 47. REMOVED CORROSION FOUND TO BE BEYOND LIMITS OF SRM 53-60-15. REMOVED AND REPLACED INTERCOSTAL LBL 4 - [SDR CALA0800728](https://openairdocs.org/sdr/CALA0800728), Jul 18, 2008: FRAME. CRACKED. LEFT SIDE STATION 907 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) A/C BRACKET INBOARD HOLE. REMOVED A/C BRACKET, CUT OUT DAMAGED AREA & REPAIRED - [SDR CALA0800727](https://openairdocs.org/sdr/CALA0800727), Jul 18, 2008: FRAME. CRACKED. LEFT SIDE STATION 827 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED A/C RAIL BRACKET, CUT OUT DAMAGED AREA AND REPAI - [SDR CALA0800722](https://openairdocs.org/sdr/CALA0800722), Jul 16, 2008: STRINGER CLIP. CRACKED. RIGHT SIDE STA 380 STRINGER 8 CLIP CRACKED. REMOVED DAMAGED STRINGER CLIP AT STA 380 RT S-8 RECEIVED NEW FROM STOCK LOCATED, DRILLED AND INSTALLED IAW SRM 51-40 - [SDR CALA0800721](https://openairdocs.org/sdr/CALA0800721), Jul 16, 2008: FRAME. CRACKED. RIGHT SIDE STA 380 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED A/C RAIL BRACKET CUTOUT DAMAGED AREA AND REPAIRED F - [SDR CALA0800720](https://openairdocs.org/sdr/CALA0800720), Jul 16, 2008: ANGLE. CORRODED. AFT CABIN R2 DOOR Z-ANGLE HAS CORROSION. REMOVED R2 DOOR Z-ANGLE IAW B737 SRM 51-40-02, INSTALLED NEW R2 DOOR Z-ANGLE IAW B737 SRM 51-40-02. - [SDR CALA0800719](https://openairdocs.org/sdr/CALA0800719), Jul 16, 2008: FRAME. CRACKED. LEFT SIDE STA 747 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET. REMOVED A/C RAIL BRACKET CUTOUT DAMAGED AREA AND REPAIRED FRAME AT STA 74 - [SDR CALA0800718](https://openairdocs.org/sdr/CALA0800718), Jul 16, 2008: SILL. CORRODED. R2 DOOR SILL WEB HAS CORROSION ON UPPER AND LOWER SURFACES. REMOVED R-2 DOOR SILL WEB IAW B737 SRM 51-40-02 MATL ID FOR NEW SIL WEB 7075 T6 .063 IAW B737 SRM 53 - [SDR CALA0800716](https://openairdocs.org/sdr/CALA0800716), Jul 16, 2008: FRAME. CRACKED. LEFT SIDE STA 787 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED A/C RAIL BRACKET CUT OUT DAMAGED AREA AND REPAIRED F - [SDR CALA0800715](https://openairdocs.org/sdr/CALA0800715), Jul 16, 2008: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED AT STA 344 TO 360 BL 11L. REMOVED CRACKED INTERCOSTAL AT STA 344 TO 360 BL 11L AND INSTALLED NEW INTERCOSTAL IAW B737 SRM 51-40-02. - [SDR CALA0800710](https://openairdocs.org/sdr/CALA0800710), Jul 16, 2008: FRAME. CRACKED. RIGHT SIDE STATION 747 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES - [SDR CALA0800709](https://openairdocs.org/sdr/CALA0800709), Jul 16, 2008: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED AT STATION 312 TO 328 BL 45L. REMOVED AND REPLACED INTERCOSTAL IAW B737 SRM 51-40-02. - [SDR CALA0800708](https://openairdocs.org/sdr/CALA0800708), Jul 16, 2008: FRAME. CRACKED. LEFT SIDE STATION 440 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES A - [SDR CALA0800707](https://openairdocs.org/sdr/CALA0800707), Jul 16, 2008: FRAME. CRACKED. RIGHT SIDE STATION 787 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED AIR CONDITIONING (A/C) RAIL BRACKET IAW EA5310- - [SDR CALA0800706](https://openairdocs.org/sdr/CALA0800706), Jul 16, 2008: FRAME. CRACKED. LEFT SIDE STATION 482 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES A - [SDR CALA0800705](https://openairdocs.org/sdr/CALA0800705), Jul 16, 2008: FRAME. CRACKED. LEFT SIDE STATION 400 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES A - [SDR CALA0800717](https://openairdocs.org/sdr/CALA0800717), Jul 15, 2008: FRAME. CRACKED. RIGHT SIDE STA 400 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REPAIRED FRAME AT STA 400 S-8 AND S-9 PER EA 5310-04498. - [SDR CALA0800713](https://openairdocs.org/sdr/CALA0800713), Jul 15, 2008: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED AT STA 328 TO 344 BL 45L. REMOVED CRACKED INTERCOSTAL AT STA 328 TO 344 BL 45L AND INSTALLED NEW INTERCOSTAL IAW B737 SRM 51-40-02. - [SDR CALA0800712](https://openairdocs.org/sdr/CALA0800712), Jul 15, 2008: FRAME. CRACKED. RIGHT SIDE STA 440 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REPAIRED CRACKED FRAME AT STA 440 BETWEEN S-8 AND S-9 PER E - [SDR CALA0300569](https://openairdocs.org/sdr/CALA0300569), Sep 30, 2003: ANGLE. CORRODED. INSPECTION FOUND UPPER SURFACE OF R-2 DOOR Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0300565](https://openairdocs.org/sdr/CALA0300565), Sep 27, 2003: SKIN. DENTED. INSPECTION FOUND LOWER SURFACE OF LT HORIZONTAL STABILIZER SKIN DENTED APPROXIMATELY 8 INCHES FORWARD OF AFT SPAR AND 102 INCHES O/B OF FUSELAGE. A REPAIR WAS I - [SDR CALA0200334](https://openairdocs.org/sdr/CALA0200334), Jun 9, 2002: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 907 BETWEEN S22R AND S23R. REPAIRED IAW SRM 53-00-01, FIGURE 224. ## 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 20000616033779I](https://openairdocs.org/incident/20000616033779I), Jun 16, 2000: Boeing 737524 (N16647), Charlotte, NC. (-23)In a telephone interview conducted by this inspector, [privacy data omitted] stated that he initiated a climb from his assigned altitude of FL280 in… --- 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.