# N17614: 1994 Boeing 737-524, registration cancelled 2012-10-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 9, 2012
- Exported to: Indonesia
- 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: 27327
- Year built: 1994
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 29, 1994
- Certificate issued: September 14, 2012
- Last registry action: September 14, 2012
- Mode S code: A1320F
- 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/N17614
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17614
- Page: https://openairdocs.org/deregistered/N17614-2012-10-09

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 (53, newest 50)

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

- [SDR CALA2012041100253](https://openairdocs.org/sdr/CALA2012041100253), Apr 11, 2012: SENSOR. OUT OF RIG. AFTER TAKEOFF, GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. AIR RETURN PER QRH, SUSPECT FAILURE OF AIR/GROUND SENSING LOGIC. EXPERIENCED DEGRADED SYSTEMS INDI
- [SDR CALA2011120700796](https://openairdocs.org/sdr/CALA2011120700796), Dec 5, 2011: WIRE HARNESS. SHORTED. F/O SIDE WINDOW SHORTHED OUT DURING T/O. FOUND SHORTHED WIRE BUNDLE (COILED HARNESS) ON F/O SIDE AT WINDOW BASE. REMOVED AND REPLACED COILED HARNESS FOR WINDOW 
- [SDR CALA2010061400276](https://openairdocs.org/sdr/CALA2010061400276), Jun 11, 2010: SKIN. CRACKED. SUPPORT TASK, FWD ENTRY DOOR CUTOUT AREA, HOLE CRACK INDICATION AT STA 302.9 THIRD FASTENER BELOW WL 236.68 (REF EA 5330-03736 CIRCLE NOTE 3 FIG 5 LAST LWR HOLE
- [SDR CALA2010061400275](https://openairdocs.org/sdr/CALA2010061400275), Jun 10, 2010: WEB. WORN. RIGHT WING AT APPROX RSS 500 HAS A WORN AREA ON I/B SIDE OF WEB ABOUT 3 INCHES AFT OF AILERON CABLE GROMMET. INSTALLED DOUBLERS REPAIR REF ECRA 5720-02138 PART 
- [SDR CALA2010061400274](https://openairdocs.org/sdr/CALA2010061400274), Jun 10, 2010: FRAME. CORRODED. FRAME STA 380 AT S28R HAS CORROSION. REPAIRED PER ECRA 5311-01495 PART 1 REF NR LP 9717663 FOR DIP.
- [SDR CALA2010061400273](https://openairdocs.org/sdr/CALA2010061400273), Jun 10, 2010: FLOOR SUPPORT. CORRODED. SUPPORT TASK - STA 270 CORROSION AROUND SEVERAL FASTENER HOLES ON FLOOR SUPPORT STRUCTURE AT NLG DOWN LOCK VIEWER APPROXIMATELY BETWEEN LBL 6 TO LBL 9. REPAIRED
- [SDR CALA2010061400272](https://openairdocs.org/sdr/CALA2010061400272), Jun 10, 2010: SKIN. CRACKED. SUPPORT TASK FORWARD ENTRY DOOR UPPER HINGE CUTOUT, CRACK INDICATION AT LOWER, MOST FORWARD HOLE OF LWR FITTING LEG. FIG 4 CIRCLE NOTE 7 OF EA 5330-03736 REV B,
- [SDR CALA2010061400271](https://openairdocs.org/sdr/CALA2010061400271), Jun 10, 2010: SKIN. CRACKED. L2 DOOR INNER SKIN IS CRACKED AT UPPER SECTION AT CENTER LIGHTENING HOLE. FABRICATED AND INSTALLED REPAIR DOUBLER PER ECRA 5210-02156.
- [SDR CALA2010061400270](https://openairdocs.org/sdr/CALA2010061400270), Jun 10, 2010: FLOORBEAM. CORRODED. ABB ALL FLOORBEAMS UNDER STRAP BETWEEN STA 767 &AMP; 787 CORRODED. REPAIRED PER ECRA 5320-01990. COMPLETED AND ATTACHED FORM 44.00 08.
- [SDR CALA2010061000266](https://openairdocs.org/sdr/CALA2010061000266), Jun 9, 2010: SKIN. DENTED. DENT ON BOTTOM OF FWD FUSELAGE AT STATION 197 AND A FEW INCHES RIGHT OF CENTER LINE REF ECRA 5331-01463. INSP DENT PER ECRA PART 1 STEP 1-5. NO DEF C/W ECRA 533
- [SDR CALA2010061000269](https://openairdocs.org/sdr/CALA2010061000269), Jun 9, 2010: ATTACH FITTING. CRACKED. SUPPORT TASK, L-1 DOOR FUSELAGE OPENING AFT SIDE STR 15 INTERCOSTAL FWD ATTACH CLIP STA 348.2 CRACKED IN RADIUS I/B SIDE. REMOVED AND REPLACED ATTACH CLIP STA 3
- [SDR CALA2010061000268](https://openairdocs.org/sdr/CALA2010061000268), Jun 9, 2010: STRINGER SPLICE. CRACKED. SUPPORT TASK, CRACK IN STR SPLICE CHANNEL AT STR 14L JUST FWD OF FRAME STA 360. REMOVED AND REPLACED STR SPLICE CHANNEL AT STR 14L STA 360 REF ECRA 5311-01496.
- [SDR CALA2010061000267](https://openairdocs.org/sdr/CALA2010061000267), Jun 9, 2010: SUPPORT ANGLE. CRACKED. L-1 DOOR SURROUND STRUCTURE HAS CRACK ON STR 11 SUPPORT AT STA 360. REMOVED AND REPLACED SUPPORT ANGLE AT STR 11L STA 360 REF ECRA 5311-01496.
- [SDR CALA2010060800257](https://openairdocs.org/sdr/CALA2010060800257), Jun 7, 2010: FITTING. CORRODED. ABB SKIN CLIP CORRODED STA 727C BETWEEN STR-26 RT. &AMP; 27 RT. REMOVED DAMAGED SHEAR TIE AND INSTALLED REPAIR REF SRM 53-00-07 FIG 201 REPAIR 4.
- [SDR CALA2010060800252](https://openairdocs.org/sdr/CALA2010060800252), Jun 5, 2010: FLAP TRACK. CORRODED. RT WING NR 8 FLAP TRACK AFT ATTACH POINT EMITTING RUST. REMOVED NR 8 FLAP TRACK. INSTALLED NEW SERVICEABLE FLAP TRACK REF M/M 27-51-49-404-006.
- [SDR CALA2010060800251](https://openairdocs.org/sdr/CALA2010060800251), Jun 5, 2010: FLAP TRACK. CORRODED. EVIDENCE OF RUST BETWEEN NR 7 FLAP TRACK AND LWR SURFACE OF REAR SPAR REMOVED NR 7 FLAP TRACK ASSY. ROTABLE PARTS CHANGE WAS INDICATED - 24-5753-9-9001 TRACK, F
- [SDR CALA2010060800250](https://openairdocs.org/sdr/CALA2010060800250), Jun 5, 2010: FITTING. CORRODED. ABB STA 747 BETWEEN STR 26 RT.&AMP; 27 RT SKIN CLIP CORRODED. REMOVED SHEAR TIE AND INSTALLED REPAIR REF SRM 53-00-07 FIG 20 1.
- [SDR CALA2010060100241](https://openairdocs.org/sdr/CALA2010060100241), Jun 1, 2010: SEAT TRACK. CORRODED. LT OTBD SEAT TRACK HAS CORROSION FROM STA 787 TO STA 887. REPAIRED LT OTBD SEAT TRACK BETWEEN STA 787-807, REF SRM 53-00-52, REPAIR 4, PAGE 201, SHEET 1-4, AND 
- [SDR CALA2010060100235](https://openairdocs.org/sdr/CALA2010060100235), May 28, 2010: TRANSITION PANEL. CORRODED. ABB LT TRANSITION PANEL CORRODED FROM 727C TO 947.5. REMOVED AND INSTALLED FABRICATED TRANSITION PANEL FROM STA 727- STA 947.5 IN REF TO SRM 53-60-53 AND SRM 53
- [SDR CALA2010060100234](https://openairdocs.org/sdr/CALA2010060100234), May 28, 2010: ANGLE. CORRODED. L1 DOOR LT ANGLE, STA 349 JUST AFT OF DRAIN AND ON UNDER SIDE HAS CORROSION. R & R LT ANGLE REF SRM 51-40-02.
- [SDR CALA2010052700227](https://openairdocs.org/sdr/CALA2010052700227), May 28, 2010: SEAT TRACK. CORRODED. RIGHT O/B SEAT TRACK HAS CORROSION STA 695 FOUND OUT OF LIMITS. CUT &AMP; REMOVED SEAT TRACK, FABRICATED NEW TRACK, APPLIED PROTECTIVE COATING, PRIMED &AMP; INS
- [SDR CALA2010052700229](https://openairdocs.org/sdr/CALA2010052700229), May 27, 2010: STOP FITTING. CRACKED. R-1 DOOR LOWER AFT STOP FITTING, INTERIOR LEG CRACKED THROUGH HI-LOK HOLE (MARKED). VERIFIED WITH HFEC P/N OF FITTING 65-51647-501. REMOVED CRACKED FRAME REINFO
- [SDR CALA2010052700228](https://openairdocs.org/sdr/CALA2010052700228), May 26, 2010: FITTING. CORRODED. NR 3 MID FLAP O/B TORQUE TUBE HOUSING HAS CORROSION. REMOVED AND INSTALLED NEW FITTING PER SRM 51-40-02 PARAGRAPH 7 AND 51-20-02 PARAGRAPH 8.
- [SDR CALA2010052700222](https://openairdocs.org/sdr/CALA2010052700222), May 23, 2010: FRAME. CRACKED. MAIN FRAME CRACKED AT STA 616 BELOW STR 17 RT. INSTALLED REPAIR PER ECRA 5311-01158.
- [SDR CALA2010051700205](https://openairdocs.org/sdr/CALA2010051700205), May 17, 2010: FRAME. CRACKED. PAX CABIN HAS CRACKED FRAME STA 380 BETWEEN STR 8R AND 9R. REPAIRED FRAME PER EA 5310-04498.
- [SDR CALA2010051700210](https://openairdocs.org/sdr/CALA2010051700210), May 17, 2010: FRAME. CRACKED. LEFT FRAME CRACKED STA 482 BETWEEN STR 8&AMP;9. REPAIRED LT FRAME AT STR 482 BETWEEN STR 8&AMP;9 REF EA5310-04498 OP2.
- [SDR CALA2010051700209](https://openairdocs.org/sdr/CALA2010051700209), May 17, 2010: FRAME. CRACKED. SUPPORT TASK LT FUSELAGE FRAME CRACKED BETWEEN STR 8&AMP;9 STA 400. INSTALLED REPAIR ANGLES A&AMP;B PER EA 5310-04498.
- [SDR CALA2010051700208](https://openairdocs.org/sdr/CALA2010051700208), May 17, 2010: FRAME. CRACKED. PAX CABIN HAS CRACKED FRAME STA 867 BETWEEN STA 8R AND 9R. REPAIRED CRACKED FRAME AT STA 867 BETWEEN STR 8R AND 9R REF EA 5310-04498 OP 2.
- [SDR CALA2010051700207](https://openairdocs.org/sdr/CALA2010051700207), May 17, 2010: FRAME. CRACKED. PAX CABIN HAS CRACKED FRAME STA 787 BETWEEN STR 8R AND 9R. INSTALLED REPAIR ANGLES REF EA5310-04498.
- [SDR CALA2010051700206](https://openairdocs.org/sdr/CALA2010051700206), May 17, 2010: FRAME. CRACKED. PAX CABIN HAS CRACKED FRAME STA 440 BETWEEN STR 8R AND 9R. INSTALLED REPAIR ANGLES, REF EA5310-04498.
- [SDR CALA2010051700204](https://openairdocs.org/sdr/CALA2010051700204), May 17, 2010: FRAME. CRACKED. RIGHT FRAME CRACKED STA 842 BETWEEN STR 8-9 FRAME WAS CRACKED DURING PSU RAIL BLOCK REMOVAL. REPAIRED RT FRAME AT STA 482 BETWEEN STR8-9 REF EA 5310-04498 OP2.
- [SDR CALA2010051700203](https://openairdocs.org/sdr/CALA2010051700203), May 17, 2010: FRAME. CRACKED. LEFT FRAME STA 440 BETWEEN STR 8 &AMP;9 CRACKED. REPAIRED FRAME STA 440 LT BETWEEN STR 8&AMP;9 LT PER EA 5310-04498 OP2.
- [SDR CALA2009122100748](https://openairdocs.org/sdr/CALA2009122100748), Dec 21, 2009: BATTERY. DISCHARGED. AFT RT EMERGENCY FLASHLIGHT INDICATOR DOES NOT FLASH. REMOVED AND REPLACED AFT RT EMERGENCY FLASHLIGHT BATTERY. OPS CHECK GOOD.
- [SDR CALA2009102300644](https://openairdocs.org/sdr/CALA2009102300644), Oct 23, 2009: CIRCUIT BREAKER. TRIPPED. AT FLIGHT IDLE ONLY THE NOSE GEAR RED LIGHT IS ILLUMINATED NOT THE MAIN GEARS. FOUND AIR/GND RELAY C/B OUT (PG-3, ROW 17C) AS DIRECTED BY MAINTENANCE, RESET C/B
- [SDR CALA2009082600500](https://openairdocs.org/sdr/CALA2009082600500), Aug 26, 2009: CABLE. FRAYED. L2 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR LATCH CABLE HAS BROKEN STRANDS (FCD 2561-01189). REMOVED AND REPLACED L2 EMERGENCY ESCAPE SLIDE CABLE IAW 737AMM 25-61-3
- [SDR CALA2009080600439](https://openairdocs.org/sdr/CALA2009080600439), Aug 6, 2009: CABLE ASSY. FRAYED. L2 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR LATCH CABLE HAS BROKEN STRANDS (FCD 2561-01189). REMOVED AND REPLACED L2 EMERGENCY ESCAPE SLIDE CABLE IAW 737 AMM 25-61-
- [SDR CALA2009080600438](https://openairdocs.org/sdr/CALA2009080600438), Aug 6, 2009: CABLE ASSY. FRAYED. R2 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR LATCH CABLE HAS BROKEN STRANDS (FCD 2561-01189). REMOVED AND REPLACED R2 DOOR EMERGENCY ESCAPE SLIDE CABLE IAW 737 AMM 2
- [SDR CALA2009080300404](https://openairdocs.org/sdr/CALA2009080300404), Jul 31, 2009: UPLOCK ACTUATOR. MALFUNCTIONED. RIGHT MAIN GEAR UNSAFE AFTER TAKEOFF, AIRCRAFT DESCENDED TO LOWER ALT, AS THROTTLES ADVANCED RIGHT MAIN GEAR FREE FELL DOWN. EXECUTED UNSAFE GEAR INDICATION CHE
- [SDR CALA0700084](https://openairdocs.org/sdr/CALA0700084), Feb 23, 2007: CHARGER. INOPERATIVE. THE EMERGENCY EXIT LIGHTS AT SEATS 20-25 WERE FOUND INOPERATIVE. THE CHARGER AND BATTERY PACK WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD.
- [SDR CALA0600080](https://openairdocs.org/sdr/CALA0600080), Mar 4, 2006: POWER SUPPLY. INOPERATIVE. INSPECTION FOUND THE EMERGENCY ESCAPE AISLE PATH LIGHTING INOPERATIVE AT ROWS 15-21. THE BATTERY PACK AND POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-51-51.
- [SDR CALA0500432](https://openairdocs.org/sdr/CALA0500432), Dec 9, 2005: WIRE. SHORTED. INSPECTION FOUND THE EMERGENCY EXIT LIGHTS OUT ON SEAT ROWS 7-14ABC. MAINTENANCE FOUND A POWER WIRE SHORTED TO SEAT TRACK AT SEAT 7ABC. THE WIRE WAS REPAIRED IA
- [SDR CALA0500130](https://openairdocs.org/sdr/CALA0500130), Apr 26, 2005: FLOORBEAM. CORRODED. FLOORBEAM CORRODED AT STA 986.5, LBL 43. INSTALLED DOUBLER PER ECRA 5321-01210.
- [SDR CALA0500129](https://openairdocs.org/sdr/CALA0500129), Apr 26, 2005: FLOORBEAM. CORRODED. FLOORBEAM CORRODED AT STA 986.5, RBL43. INSTALLED DOUBLER PER ECRA 5321-01209.
- [SDR CALA0500072](https://openairdocs.org/sdr/CALA0500072), Mar 8, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED AT FASTENER HOLE OF FORWARD FLANGE OF UPPER CHORD, STA 986, LBL 43. A REPAIR WAS INSTALLED IAW ECRA 5321-01210.
- [SDR CALA0500071](https://openairdocs.org/sdr/CALA0500071), Mar 7, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM FORWARD FLANGE OF UPPER CHORD FASTENER HOLE CORRODED AT STA 986, RBL 43 TO RBL 44. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-012
- [SDR CALA0500060](https://openairdocs.org/sdr/CALA0500060), Feb 27, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED AT AFT FLANGE OF UPPER CHORD, STA 986, LBL 14 TO LBL 18. THE CORRODED AREA WAS CUT OUT AND ANGLES WERE INSTALLED IAW S
- [SDR CALA0300332](https://openairdocs.org/sdr/CALA0300332), Jun 23, 2003: CIRCUIT BREAKER. FAILED. A HEAVY ELECTRICAL ODOR WAS NOTICED IN THE CABIN WHILE EN ROUTE TO DCA. THE ODOR WAS ACCOMPANIED BY FAILURE OF CABIN LIGHTS, OVEN, AND AUTOPILOT AND THE NR 1 EN
- [SDR CALA9900769](https://openairdocs.org/sdr/CALA9900769), Jul 5, 1999: MEGAPHONE. INOPERATIVE. THE AFT MEGAPHONE WAS FOUND INOPERATIVE. THE MEGAPHONE WAS REPLACED.
- [SDR CALA9900696](https://openairdocs.org/sdr/CALA9900696), Jun 15, 1999: LIGHT. INOPERATIVE. INSPECTION FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT L-2 DOOR. THE EXIT LIGHT ASSEMBLY WAS REPLACED IAW MM 33-51-11.
- [SDR CALA9802181](https://openairdocs.org/sdr/CALA9802181), Dec 17, 1998: CIRCUIT BREAKER. TRIPPED. THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. THE GEAR HANDLE WOULD NOT RAISE BEYOND THE OFF POSITION. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LA

All 53: https://openairdocs.org/deregistered/N17614-2012-10-09/reports.md

## 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 19980429025209I](https://openairdocs.org/incident/19980429025209I), Apr 29, 1998: Boeing 737524 (N17614), Cleveland, OH. Flight crew declared emergency due to smoke and fumes coming from the aft galley. Aircraft landed without incident. Maintenance found a "oven mit" in the aft…

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