# N16649: Boeing 737-524, registration cancelled 2011-11-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 30, 2011
- Exported to: Bermuda
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-524](https://openairdocs.org/model/boeing-737-524) (registry code 1384721)
- Engine: [GE CFM56 series](https://openairdocs.org/engine/ge-cfm56-series) (registry code 30016)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 28910
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 19, 1997
- Certificate issued: November 22, 2011
- Last registry action: November 22, 2011
- Mode S code: A10AFE
- 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/N16649
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16649
- Page: https://openairdocs.org/deregistered/N16649-2011-11-30

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 CALA2010062800307](https://openairdocs.org/sdr/CALA2010062800307), Jun 28, 2010: FRAME. CORRODED. FRAME STA 767 AT S27R TO S26R HAS CORROSION. INSTALLED REPAIR PARTS ON FRAME, REPAIR 4 REF-SRM 53-00-07.
- [SDR CALA2010062800306](https://openairdocs.org/sdr/CALA2010062800306), Jun 27, 2010: FRAME. CORRODED. FRAME STA 767 AT STR 27L TO STR 28L HAS CORROSION. REMOVED DAMAGED SECTION OF FRAME AND INSTALLED REPAIR REF SRM 53-00-07 FIG 201 REPAIR 4.
- [SDR CALA2010062800303](https://openairdocs.org/sdr/CALA2010062800303), Jun 25, 2010: HINGE FITTING. CRACKED. SUPPORT TASK CRACK INDICATION W/HFEC HOLE PROBE REF STEP 20.0 OF 5330-03736. REMOVED AND INSTALLED NEW HINGE FITTING PER SRM 51-40-01 AND 51-10-02 PARAGRAPH 8.
- [SDR CALA2010062500301](https://openairdocs.org/sdr/CALA2010062500301), Jun 24, 2010: SKIN. CRACKED. SUPPORT TASK-L-1 DOOR OPENING SURROUND STRUCTURE-UPPER HINGE CUTOUT INTERNAL CASTING (FITTING) IS CRACKED APPROX .6250 INCH IN LENGTH (MARKED). REMOVED AND REPL
- [SDR CALA2010062500300](https://openairdocs.org/sdr/CALA2010062500300), Jun 23, 2010: SKIN. CRACKED. L-1 DOOR INNER SKIN FASTENERS CRACKED (MARKED) TASK {B737-52-4-0048}. REMOVED AND REPLACED 91 MARKED INNER SKIN FASTENERS ON L-1 DOOR REF: SRM 51-40-02.
- [SDR CALA2010062200291](https://openairdocs.org/sdr/CALA2010062200291), Jun 21, 2010: WEB. CRACKED. WEB LOCATED AT BL 0 FROM STA 380-STA 400 IS CRACKED AT TOP, FWD FASTENER HOLE. INSTALLED NEW WEB AT BL 0 STA 380-400 REF SRM 51-40-02.
- [SDR CALA2010062200290](https://openairdocs.org/sdr/CALA2010062200290), Jun 21, 2010: INTERCOSTAL. CRACKED. MULT-06-3-0037 CABIN FLOOR INTERCOSTAL BETWEEN STA 380 AND STA 400 AT BL 0 IS CRACKED FASTENER HOLE. INSTALLED NEW CABIN FLOOR INTERCOSTAL BETWEEN STA 380-400 A
- [SDR CALA2009082400458](https://openairdocs.org/sdr/CALA2009082400458), Aug 16, 2009: MEGAPHONE. INOPERATIVE. AFT FLT ATTENDANT EMERGENCY MEGAPHONE SIREN WILL NOT TEST. REMOVED AND REPLACED THE AFT FLT ATTENDANT EMERGENCY MEGAPHONE. OPS CHECKS GOOD.
- [SDR CALA0800963](https://openairdocs.org/sdr/CALA0800963), Oct 10, 2008: FRAME. CRACKED. FUSELAGE STATION 360 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET INBOARD RIVET BETWEEN STRINGERS 8 AND 9. REPAIRED 360 FRAME AT STR 8-9 LE
- [SDR CALA0800960](https://openairdocs.org/sdr/CALA0800960), Oct 7, 2008: FRAME. CRACKED. FUSELAGE STATION 867 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. CUT OUT DAMAGE AT FUSELAGE STATION 867 BETWE
- [SDR CALA0800959](https://openairdocs.org/sdr/CALA0800959), Oct 7, 2008: FRAME. CRACKED. FUSELAGE STATION 827 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. CUT OUT DAMAGE AT FUSELAGE STATION 827 BETWE
- [SDR CALA0800958](https://openairdocs.org/sdr/CALA0800958), Oct 7, 2008: FRAME. CRACKED. FUSELAGE STATION 747 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. CUT OUT DAMAGE AT FUSELAGE STATION 747 BETWE
- [SDR CALA0800957](https://openairdocs.org/sdr/CALA0800957), Oct 7, 2008: FRAME. CRACKED. FUSELAGE STATION 787 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. CUT OUT DAMAGE AT FUSELAGE STATION 787 BETWE
- [SDR CALA0800956](https://openairdocs.org/sdr/CALA0800956), Oct 7, 2008: FRAME. CRACKED. FUSELAGE STATION 867 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 867 BETWE
- [SDR CALA0800955](https://openairdocs.org/sdr/CALA0800955), Oct 7, 2008: FRAME. CRACKED. FUSELAGE STATION 827 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 827 BETWE
- [SDR CALA0800954](https://openairdocs.org/sdr/CALA0800954), Oct 7, 2008: FRAME. CRACKED. FUSELAGE STATION 787 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 787 BETWE
- [SDR CALA0800953](https://openairdocs.org/sdr/CALA0800953), Oct 7, 2008: FRAME. CRACKED. FUSELAGE STATION 747 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 747 BETWE
- [SDR CALA0800952](https://openairdocs.org/sdr/CALA0800952), Oct 7, 2008: FRAME. CRACKED. FUSELAGE STATION 400 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 400 BETWE
- [SDR CALA0800949](https://openairdocs.org/sdr/CALA0800949), Oct 6, 2008: SKIN. DELAMINATED. RIGHT WING NUMBER 5 SLAT TRAILING EDGE OUTBOARD END DELAMINATED. REPAIRED DELAMINATION ON OUTBOARD END OF NUMBER 5 SLAT PER B737-500 SRM 51-70-10.
- [SDR CALA0800944](https://openairdocs.org/sdr/CALA0800944), Oct 6, 2008: WEB. DAMAGED. BODY STATION 787 AT STRINGER 25R FRAME CLOSE-OUT WEB DAMAGED. REMOVED DAMAGED WEB CLOSE-OUT AT BODY STATION 787 AT STR 25R IAW B737 SRM 51-40-02, FABRICATED NEW
- [SDR CALA2008100600944](https://openairdocs.org/sdr/CALA2008100600944), Oct 6, 2008: FRAME. DAMAGED. BODY STATION 787 AT STRINGER 25R FRAME CLOSE-OUT WEB DAMAGED. REMOVED DAMAGED WEB CLOSE-OUT AT BODY STATION 787 AT STR 25R IAW B737 SRM 51-40-02, FABRICATED NEW
- [SDR CALA0800939](https://openairdocs.org/sdr/CALA0800939), Oct 3, 2008: FRAME. CRACKED. FUSELAGE STATION 400 LEFT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGER'S 8L AND 9L. REPAIRED FRAME 400 LT PER EA 5310-04498 B
- [SDR CALA0800943](https://openairdocs.org/sdr/CALA0800943), Oct 2, 2008: ANGLE. CRACKED. AFT CARGO COMPARTMENT RIGHT FLOOR TO SIDEWALL TRANSITION ANGLE IS CRACKED AT STATION 747 AND STATION 727C. REMOVED DAMAGED SECTION OF AFT CARGO COMPARTMENT RIGH
- [SDR CALA0800938](https://openairdocs.org/sdr/CALA0800938), Oct 1, 2008: TORQUE BOX. CORRODED. L-2 DOOR TWO MOUNT HOLES ON TORQUE BOX CORRODED. REMOVED AND REPLACED L2 DOOR TORQUE BOX AS CORROSION WAS FOUND TO BE OUT OF LIMITS PER B737 CMM 52-6-03.
- [SDR CALA0800935](https://openairdocs.org/sdr/CALA0800935), Sep 29, 2008: INTERCOSTAL. CRACKED. FORWARD CARGO INTERCOSTAL DAMAGED BETWEEN STATIONS 380-400 AT S-22R. REPAIRED FORWARD CARGO INTERCOSTAL DAMAGED BETWEEN STATIONS 380-400 AT S-22R PER B737-500 S
- [SDR CALA0800925](https://openairdocs.org/sdr/CALA0800925), Sep 26, 2008: INTERCOSTAL. CRACKED. FWD WET AREA CROSS BRACE CRACKED AT FLOORBOARD ATTACH HOLES BETWEEN STA 340-360 LBL 46. REMOVED AND REPLACED INTERCOSTAL AT LBL 46 BS 328 TO BS 344 REF 737-500 
- [SDR CALA0800922](https://openairdocs.org/sdr/CALA0800922), Sep 25, 2008: INTERCOSTAL. CRACKED. FORWARD WET AREA CROSSBRACE CRACKED AT FLOORBOARD ATTACH HOLES BETWEEN STATION 360-380 LBL 12. ORIGINAL DAMAGE WAS TO INTERCOSTAL LOCATED AT LBL 12 BETWEEN BODY
- [SDR CALA0300694](https://openairdocs.org/sdr/CALA0300694), Dec 5, 2003: SKIN. GOUGED. APU ACCESS DOOR INNER SKIN GOUGED LT SIDE FORWARD OF AFT LATCH. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED DOUBLER PER SRM 5200-01.
- [SDR CALA0300685](https://openairdocs.org/sdr/CALA0300685), Dec 2, 2003: BUSHING. CORRODED. CORROSION ON FORWARD LOWER HORIZONTAL STAB CENTER SECTION LUG ON AFT CLEVIS ON AFT FACE AT BUSHING. REMOVED AND REPLACED BUSHING PER SOPM 20-50-03.
- [SDR CALA0300684](https://openairdocs.org/sdr/CALA0300684), Dec 2, 2003: BUSHING. CORRODED. FORWARD LEFT LOWER HORIZONTAL STAB CENTER SECTION FORWARD CLEVIS HAS PITTING CORROSION AT BUSHING ON FORWARD FACE. REPAIRED AND REPLACED OVERSIZE BUSHING PER SR
- [SDR CALA0300683](https://openairdocs.org/sdr/CALA0300683), Dec 2, 2003: BUSHING. CORRODED. FORWARD LEFT UPPER STAB CENTER SECTION FORWARD CLEVIS HAS PITTING CORROSION AT THE BUSHING ON FORWARD EDGE. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10
- [SDR CALA0300682](https://openairdocs.org/sdr/CALA0300682), Dec 2, 2003: BUSHING. CORRODED. CORROSION ON FORWARD UPPER HORIZONTAL STAB CENTER SECTION LUG AFT CLEVIS ON AFT FACE AT BUSHING. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10-10.
- [SDR CALA0300680](https://openairdocs.org/sdr/CALA0300680), Dec 1, 2003: ANGLE. CORRODED. INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 967-990. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0300377](https://openairdocs.org/sdr/CALA0300377), Jul 4, 2003: SKIN. DAMAGED. THE FUSELAGE SKIN WAS FOUND DAMAGED AFT OF BS 1088 BETWEEN STRINGER 18L AND 20L. THE TRIM OUT TO REMOVE DAMAGE MEASURED 1.3 X 1.15 INCH. THE AREA WAS REPAIRED I

## 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 19990308020769I](https://openairdocs.org/incident/19990308020769I), Mar 8, 1999: Boeing 737524 (N16649), Indianapolis, IN, Minor damage. On 3/7/99 a service truck ran into the left wing tip, rendering the aircraft in an unairworthy condition.

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