# N11641: 1997 Boeing 737-524, registration cancelled 2012-01-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 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: 28902 - Year built: 1997 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 29, 1997 - Certificate issued: October 28, 2011 - Last registry action: October 28, 2011 - Mode S code: A0457B - 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/N11641 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=11641 - Page: https://openairdocs.org/deregistered/N11641-2012-01-23 From the FAA registry file of October 28, 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 (33) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DU4R2011019](https://openairdocs.org/sdr/DU4R2011019), Nov 24, 2011: SKIN. DENTED. DENT/GOUGE AFT CARGO DOOR AT BS 820.5 AND 2.5" ABOVE STR 23R. - [SDR DU4R2011023](https://openairdocs.org/sdr/DU4R2011023), Nov 21, 2011: STIFFENER. CORRODED. DURING SCHEDULED INSPECTION, FOUND CORROSION ON AFT CABIN FLOOR WEB STIFFENER AT BS 992.9, RBL 33-45. - [SDR DU4R2011022](https://openairdocs.org/sdr/DU4R2011022), Nov 21, 2011: FLOORBEAM. CORRODED. DURING SCHEDULED INSPECTION, FOUND CORROSION ON AFT FUSELAGE FLOORBEAM AT BS 986, RBL 28 - 44. - [SDR DU4R2011021](https://openairdocs.org/sdr/DU4R2011021), Nov 20, 2011: FLOORBEAM. CORRODED. DURING SCHEDULED INSPECTION, FOUND CORROSION ON AFT CABIN FLOORBEAM AT BS 986, LBL 27 - 46. - [SDR DU4R20111119020](https://openairdocs.org/sdr/DU4R20111119020), Nov 19, 2011: FLOORBEAM. CORRODED. DURING SCHEDULED INSPECTION, FOUND CORROSION ON FLOORBEAM AT BS 344, RBL 12, LBL-11. - [SDR DU4R20111115018](https://openairdocs.org/sdr/DU4R20111115018), Nov 15, 2011: FLOORBEAM. CORRODED. DURING SCHEDULED INSPECTION, FOUND CORROSION ON FWD CABIN FLOORBEAM BS 312, RBL 12 TO LBL 56. - [SDR CALA2010082300397](https://openairdocs.org/sdr/CALA2010082300397), Aug 18, 2010: SHEAR TIE. CORRODED. SUPPORT TASK - CORROSION ON FRAME SKIN CLIP STA 787 LBL 5. HEAT TREAT FORMS INSTALLED FRAME REPAIR PER SRM 53-00-07 REPAIR 3. - [SDR CALA2010082300396](https://openairdocs.org/sdr/CALA2010082300396), Aug 17, 2010: INTERCOSTAL. CRACKED. SUPPORT TASK, INTERCOSTAL CRACKED BETWEEN STA 344 AND 360 BL 0. REMOVED AND REPLACED INTERCOSTAL REF SRM 51-40-02. - [SDR CALA2010081600394](https://openairdocs.org/sdr/CALA2010081600394), Aug 15, 2010: FITTING. CRACKED. SUPPORT TASK - REMOVE L-1 UPPER DOOR FITTING REMOVED AND REPLACED L-1 UPPER DOOR FITTING REF SRM 51-40-02. - [SDR CALA2009072700399](https://openairdocs.org/sdr/CALA2009072700399), Jul 25, 2009: WASHER. INCORRECT. L-2 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR LATCH CABLE HAS INCORRECT WASHERS INSTALLED IN THE ATTACHING HARDWARE. REPLACED L-2 DOOR LANYARD AND WASHERS PER MM 25- - [SDR CALA2009072700398](https://openairdocs.org/sdr/CALA2009072700398), Jul 24, 2009: CABLE ASSY. FRAYED. R-2 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR LATCH CABLE HAS BROKEN STRANS. REMOVED AND REPLACED BROKEN CABLE P/N 65C19901-15, NUT BACN10R1OL AND WASHERS NAS1149C11 - [SDR CALA0800301](https://openairdocs.org/sdr/CALA0800301), Mar 27, 2008: INTERCOSTAL. CRACKED. INTERCOSTAL FWD WET AREA BETWEEN FLOORBEAM 328 & 344 LBL 46 CRACKED AT CLIP NUT HOLE. REMOVED & REPLACED INTERCOSTAL BETWEEN STATIONS 328 & 344 LBL 46 IAW SRM 5 - [SDR CALA0800263](https://openairdocs.org/sdr/CALA0800263), Mar 27, 2008: FITTING. CRACKED. L1 ENTRY GIRT BAR ATTACH PTS (2) ARE CORRODED. L-1 GIRT BAR FITTING, STA 312, REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW B737 SRM 53-10-15. ALODINED, PRIME - [SDR CALA0800262](https://openairdocs.org/sdr/CALA0800262), Mar 25, 2008: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED STA 787 S-15R. REMOVED CRACKED TIE CLIP AT STA 787, STR 15R. LOCATED, DRILLED AND INSTALLED NEW STRINGER TIE CLIP P/N 69-35352-3 AT SA - [SDR CALA0800261](https://openairdocs.org/sdr/CALA0800261), Mar 18, 2008: ANGLE. CORRODED. Z-ANGEL AT L2 DOOR IS CORRODED IN SEVERAL AREAS. REMOVED CORRODED Z-ANGLE AND LOCATED AND DRILLED NEW Z-ANGLE AT L-2 DOOR PER B737 SRM 51-40-02. INSTALLED NEW Z - [SDR CALA0800311](https://openairdocs.org/sdr/CALA0800311), Mar 11, 2008: ATTACH FITTING. CRACKED. INTERCOSTAL ATTACH CLIP TO FRAME STA 348 AT STR 13 LT IS CRACKED (MARKED). REPAIRED PER PACE EA 641-53-001 CAL AND EC/RA5310-04742. - [SDR CALA0800310](https://openairdocs.org/sdr/CALA0800310), Mar 11, 2008: FRAME. DAMAGED. TWO RIVET HEADS SHEARED OFF ON AFT SIDE OF FRAME STA 348 AND THE AREA OF STR 12 LT (MARKED). REPLACED 2 RIVETS THAT WERE SHEARED OFF ON AFT SIDE OF FRAME AT STA - [SDR CALA0800309](https://openairdocs.org/sdr/CALA0800309), Mar 11, 2008: INTERCOSTAL. MISSING. INTERCOSTAL ATTACH POINT TO INBOARD FLANGE OF FRAME STA 348 AND STR 12 LT, MISSING FASTENERS 2 (MARKED). INSTALLED 2 FASTENERS AT INTERCOSTAL ATTACH POINT TO IN - [SDR CALA0800308](https://openairdocs.org/sdr/CALA0800308), Mar 11, 2008: INTERCOSTAL. MISSING. INTERCOSTAL ATTACH POINT TO INBOARD FLANGE OF FRAME STA 348 AND STR 13 LT, MISSING FASTENERS 2 (MARKED). INSTALLED 2 FASTENERS AT INTERCOSTAL ATTACH POINT TO IN - [SDR CALA0800307](https://openairdocs.org/sdr/CALA0800307), Mar 11, 2008: INTERCOSTAL. MISSING. INBOARD ATTACH BRACKET FOR STIFFENERS ON TOP AND BOTTOM OF INTERCOSTAL, BETWEEN FRAMES STA 348 & 360, AT STR 8 LT LOCATION, FASTENERS (4) MISSING (MARKED). INST - [SDR CALA0800306](https://openairdocs.org/sdr/CALA0800306), Mar 11, 2008: FASTENER. MISSING. INTERCOSTAL ATTACH POINT TO INBOARD FLANGE OF FRAME STA 348 AND STR 14 LT FASTENERS (2) MISSING (MARKED). INSTALLED 2 FASTENERS AT BS 348 STR 14 LT AT INTERCOST - [SDR CALA0800305](https://openairdocs.org/sdr/CALA0800305), Mar 11, 2008: ATTACH BRACKET. CRACKED. INTERCOSTAL ATTACH CLIP TO FRAME STA 348 AT STR 12 LT IS CRACKED. REPAIRED PER PACE EA 641-53-001CAL AND EC/RA 5310-04742. - [SDR CALA0800300](https://openairdocs.org/sdr/CALA0800300), Mar 8, 2008: INTERCOSTAL. CRACKED. INTERCOSTAL FWD WET AREA BETWEEN FLOORBEAM 312 AND 328 LBL 46 IS CRACKED AT CLIP NUT HOLE. REMOVED AND INSTALLED NEW INTERCOSTAL FWD WET AREA BETWEEN FLOORBEAM - [SDR CALA0700104](https://openairdocs.org/sdr/CALA0700104), Feb 26, 2007: BATTERY. DISCHARGED. EMERGENCY LIGHTS FOUND ON. REPLACED BATTERIES IAW 33-51-51. - [SDR CALA0500038](https://openairdocs.org/sdr/CALA0500038), Feb 2, 2005: CHARGER. INOPERATIVE. THE EMERGENCY LIGHTS ON SEAT ROWS 5-9 DID NOT ILLUMINATE DURING TEST. THE EMERGENCY EXIT LIGHT BATTERY CHARGER AT RT OVERWING EXIT WAS REMOVED AND REPLACED IAW - [SDR CALA0300388](https://openairdocs.org/sdr/CALA0300388), Jul 14, 2003: GATE. CORRODED. INSPECTION FOUND CORROSION AND GOUGES ON EXTERIOR OF L-1 DOOR LOWER GATE. THE LOWER GATE WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0300381](https://openairdocs.org/sdr/CALA0300381), Jul 12, 2003: BEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN C-1 DOOR T-BEAM. A REPAIR WAS INSTALLED IAW SRM 51-70-12. - [SDR CALA0300380](https://openairdocs.org/sdr/CALA0300380), Jul 12, 2003: SKIN. DENTED. INSPECTION FOUND AFT CARGO DOOR SKIN DENTED 39 INCHES FROM FORWARD EDGE AND 19 INCHES FROM TOP. REPAIRED IAW SRM 52-00-01. - [SDR CALA0300384](https://openairdocs.org/sdr/CALA0300384), Jul 11, 2003: SKIN. DENTED. INSPECTION FOUND THE AFT CARGO DOOR EXTERNAL SKIN DENTED 21 INCHES FROM FORWARD DOOR EDGE AND 40 INCHES FROM TOP EDGE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52 - [SDR CALA0300374](https://openairdocs.org/sdr/CALA0300374), Jul 9, 2003: ANGLE. CORRODED. INSPECTION FOUND R-2 DOOR THRESHOLD Z-ANGLE CORRODED AT AFT AREA OF DOOR CUTOUT. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA0300372](https://openairdocs.org/sdr/CALA0300372), Jul 9, 2003: INTERCOSTAL. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN INTERCOSTAL AT STA 344-360, RBL 3. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA9801335](https://openairdocs.org/sdr/CALA9801335), Jul 23, 1998: OUTFLOW VALVE. MALFUNCTIONED. THE AIRCRAFT PRESSURE COULD NOT BE CONTROLLED IN AUTO, ALTERNATE, OR MANUAL AFTER TAKEOFF FROM MEX. THE OXYGEN MASKS WERE DEPLOYED AND THE AIRCRAFT WAS RETURNED - [SDR CALA9701420](https://openairdocs.org/sdr/CALA9701420), Oct 6, 1997: GEARBOX. FAILED. THE NR 1 ENGINE FLAMED OUT WHILE ON DESCENT INTO OMA. ENGINE RESTART ATTEMPT WAS UNSUCCESSFUL. THE A/C LANDED WITHOUT INCIDENT. THE NR 1 ENGINE IS BEING REPLACE ## FAA accident and incident reports (2) 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 20000128000929I](https://openairdocs.org/incident/20000128000929I), Jan 28, 2000: Boeing 737524 (N11641), Newark, NJ. (-23) The aircraft landed on the centerline of runway 4R at Newark. Shortly after touchdown, the aircraft veered left, departed the runway and wound up… - [Incident 19971007043369I](https://openairdocs.org/incident/19971007043369I), Oct 7, 1997: Boeing 737524 (N11641), Omaha, NE. Narrative: crew reported #1 engine failed without warning during descent at 29,000 feet. The crew tried to restart the engine without success. Teardown… --- 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.