# N14613: 1994 Boeing 737-524, registration cancelled 2012-08-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 13, 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: 27326
- Year built: 1994
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 19, 1994
- Certificate issued: July 26, 1994
- Last registry action: April 6, 2012
- Mode S code: A0BB91
- 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/N14613
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14613
- Page: https://openairdocs.org/deregistered/N14613-2012-08-13

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 (32)

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

- [SDR CALA2011112100755](https://openairdocs.org/sdr/CALA2011112100755), Nov 19, 2011: OVEN. DIRTY. AIR RETURN FOR UNDETERMINED OVEN SMOKE (OVER WEIGHT 117,800LBS LANDING). SMOKE FORM FILLED. DEBRIEFED F/A & FOUND AFT OVEN AT FAULT. OPS OVEN IN AFT GALLEY & FO
- [SDR CALA2011100400646](https://openairdocs.org/sdr/CALA2011100400646), Oct 4, 2011: WARNING SYSTEM. MALFUNCTIONED. DURING TO, GEAR HANDLE PLACED IN OFF POSITION - RT GEAR GREEN AND RED LIGHT ILLUMINATED. CHECKLIST ACCOMPLISHED, GEAR HANDLE DOWN - ALL GEAR INDICATED DOWN AND 
- [SDR CALA2010122200632](https://openairdocs.org/sdr/CALA2010122200632), Dec 22, 2010: BATTERY. DISCHARGED. SUPPORT TASK - EMERGENCY LIGHTS INOP AT 2R LOWER EXIT SIGN. REPLACED BATTERY IAW B737 MM 33-51-51, OP CHECKS GOOD.
- [SDR CALA2010122200631](https://openairdocs.org/sdr/CALA2010122200631), Dec 22, 2010: BATTERY. DISCHARGED. SUPPORT TASK - EMERGENCY LIGHTS INOP AISLE SIDE 28C, 29C, 30C, 31C. REPLACED BATTERY IAW B737MM 33-51-51 OP CHECK GOOD.
- [SDR CALA2010122200630](https://openairdocs.org/sdr/CALA2010122200630), Dec 22, 2010: BATTERY. DISCHARGED. SUPPORT TASK - EMERGENCY LIGHTS INOP AT OVERHEAD BINS 28DEF AND 31DEF. REPLACED BATTERY IAW B737 MM 33-51-51 AND OP CHECK GOOD.
- [SDR CALA2010122000625](https://openairdocs.org/sdr/CALA2010122000625), Dec 20, 2010: CHANNEL. CORRODED. STA 787, S24-25L CORRODED, REMOVED CORROSION, ORIGINAL THICKNESS .050 MAT REMAINING .033. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101. REMOVED CHANNEL I
- [SDR CALA2011040100249](https://openairdocs.org/sdr/CALA2011040100249), Dec 13, 2010: FRAME. CRACKED. SUPPORT TASK - FRAME AT STATION 400 RIGHT HAS CRACK INDICATION BETWEEN STRINGER 8 &9 AT A/C SUPPORT BRACKET ATTACHMENT HOLE. REPAIRED IAW CAL EA 5310-04498.
- [SDR CALA2011040100248](https://openairdocs.org/sdr/CALA2011040100248), Dec 13, 2010: FRAME. CRACKED. FRAME AT STATION 360 LEFT HAS CRACK INDICATION BETWEEN STRINGER 8 TO 9 AT A/C SUPPORT (SUPPORT TASK). CUT OUT FRAME DAMAGE NO CRACK FOUND REPAIR ANGLE B FABBED 
- [SDR CALA2011040100247](https://openairdocs.org/sdr/CALA2011040100247), Dec 13, 2010: FRAME. CRACKED. SUPPORT TASK - FRAME AT STATION 867 RIGHT HAS CRACK INDICATION BETWEEN STRINGER 8 &9 AT A/C SUPPORT BRACKET ATTACHMENT HOLES. REPAIRED IAW CAL EA5310-04498.
- [SDR CALA2011040100246](https://openairdocs.org/sdr/CALA2011040100246), Dec 13, 2010: FRAME. CRACKED. SUPPORT TASK - FRAME AT STATION 440 RIGHT HAS CRACK INDICATION BETWEEN STRINGER 8 &9 AT A/C SUPPORT BRACKET ATTACHMENT HOLES. REPAIRED IAW CAL EA 5310-04498
- [SDR CALA2011040100245](https://openairdocs.org/sdr/CALA2011040100245), Dec 13, 2010: FRAME. CRACKED. SUPPORT TASK - FRAME AT STATION 380 RIGHT HAS CRACK INDICATION BETWEEN STRINGER 8 &9 AT A/C SUPPORT BRACKET ATTACHMENT HOLES REPAIRED IAW CAL EA 5310-04498.
- [SDR CALA2011031700153](https://openairdocs.org/sdr/CALA2011031700153), Dec 13, 2010: FRAME. CRACKED. FRAME AT STATION 907 LEFT HAS CRACK INDICATION BETWEEN STRINGER 8&9 AT SUPPORT BRACKET ATTACHMENT HOLES. ACCOMPLISHED FRAME REPAIR AT STA 907 LEFT IAW CAL E
- [SDR CALA2011031700154](https://openairdocs.org/sdr/CALA2011031700154), Dec 13, 2010: FRAME. CRACKED. FRAME 747 RIGHT HAS CRACK INDICATION BETWEEN STRINGER 8&9 AT A/C SUPPORT BRACKET ATTACHMENT HOLES. ACCOMPLISHED FRAME REPAIR AT STA 747 RIGHT IAW CAL EA 531
- [SDR CALA2011031700152](https://openairdocs.org/sdr/CALA2011031700152), Dec 13, 2010: FRAME. CRACKED. FRAME AT STATION 867 LEFT HAS CRACK INDICATION BETWEEN STRINGER 8&9 AT A/C SUPPORT BRACKET ATTACHMENT HOLE. REMOVED BRACKET, PERFORMED HFEC, REMOVED DAMAGED
- [SDR CALA2011031700151](https://openairdocs.org/sdr/CALA2011031700151), Dec 13, 2010: FRAME. CRACKED. FRAME 482 LEFT HAS A CRACK INDICATION BETWEEN STRINGER 8&9 AT A/C SUPPORT BRACKET ATTACHMENT HOLES. ACCOMPLISHED FRAME REPAIR AT STATION 482 IAW CAL EA 5310
- [SDR CALA2011031700150](https://openairdocs.org/sdr/CALA2011031700150), Dec 13, 2010: FRAME. CRACKED. FRAME AT STATION 440 LEFT HAS CRACK INDICATION BETWEEN STRINGER 8&9 AT A/C SUPPORT BRACKET ATTACHMENT HOLES (SUPPORT TASK) - ACCOMPLISHED FRAME REPAIR IAW C
- [SDR CALA2011031700149](https://openairdocs.org/sdr/CALA2011031700149), Dec 13, 2010: FRAME. CRACKED. FRAME AT STATION 907 RIGHT HAS CRACK INDICATION BETWEEN STRINGER 8&9 AT A/C SUPPORT BRACKET ATTACHMENT HOLES. REPAIRED IAW CAL EA 5310-04498.
- [SDR CALA2010121300614](https://openairdocs.org/sdr/CALA2010121300614), Dec 13, 2010: FRAME. CRACKED. SUPPORT TASK - FRAME AT STATION 827 LEFT HAS CRACK INDICATION B ETWEEN STRINGER 8&9 AT A/C SUPPORT BRACKET ATTACHMENT HOLES REMOVED SUPPORT BRACKET IAW EA 5
- [SDR CALA2010120100598](https://openairdocs.org/sdr/CALA2010120100598), Nov 30, 2010: THRESHOLD. CORRODED. R2 DOOR THRESHOLD INNER CHORD CORRODED AT BS 967 RBL 50 REMOVED R-2 DOOR THRESHOLD CHORD. RECEIVED NEW CHORD P/N 65-4585 50103 PO 697353.1. LOCATED AND DRILLED 
- [SDR CALA2009072000378](https://openairdocs.org/sdr/CALA2009072000378), Jul 18, 2009: CABLE ASSY. FRAYED. R-2 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR LATCH CABLE HAS BROKEN STANDS. REPLACED R-2 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR LATCH CABLE PER AMM 25-61-35.
- [SDR CALA2009063000335](https://openairdocs.org/sdr/CALA2009063000335), Jun 26, 2009: WIRE HARNESS. CHAFED. WIRE BUNDLE CHAFED JUST O/B OF LT CTR BOOST PUMP. REMOVED AND REPLACED LT WING TANK TO EXTERNAL PRESSURE HULL IFQT WIRE (SAFE SIDE) HARNESS PER AMM 28-41-45, CH
- [SDR CALA2009063000334](https://openairdocs.org/sdr/CALA2009063000334), Jun 26, 2009: WIRE. CHAFED. WIRE BUNDLE W0186 HAS 3EA CHAFED WIRES O/B OF RT FWD BOOST PUMP. FOUND WIRES 053, 030 & AMP; 036 OF BUNDLE W0186 CHAFED BUT NOT COMPLETELY THROUGH INSULATION. R
- [SDR CALA2009040900187](https://openairdocs.org/sdr/CALA2009040900187), Apr 9, 2009: OVEN. DIRTY. AFTER TAXI IN AT IAH FLIGHT ATTENDANTS STATED, SMELLED A BURNING RUBBER ODOR IN THE AFT GALLEY, LIKE AN OVERHEATING WIRE IN A HAIR DRYER. REPLACED OVEN AND RECI
- [SDR CALA0700342](https://openairdocs.org/sdr/CALA0700342), Jul 8, 2007: KEELBEAM. CORRODED. INSPECTION FOUND CENTER KEEL BEAM AT RIGHT SIDE OF MLG WHEEL WELL BEAM EDGE CORRODED AT THE LOWER SURFACE AROUND FASTENER HOLES, STA 700-727, RBL 7. THE KEEL BE
- [SDR CALA0700332](https://openairdocs.org/sdr/CALA0700332), Jun 30, 2007: FRAME. CRACKED. INSPECTION FOUND A 1.75 INCH CRACK AT LOWER FASTENER ON FUSELAGE STUB FRAME FORWARD SIDE, STA 616, S16L. THE CRACKED AREA OF FRAME INNER CHORD WAS REMOVED AND A
- [SDR CALA0500005](https://openairdocs.org/sdr/CALA0500005), Jan 9, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT SCREW HOLE ON FORWARD FLANGE AT STA 986.5, RBL 43 TO RBL 44. THE CORROSION WAS REMOVED AND A REPAIR STRAP WAS INSTALLED I
- [SDR CALA0500004](https://openairdocs.org/sdr/CALA0500004), Jan 9, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT SCREW HOLE ON FORWARD FLANGE AT STA 986.5, RBL 29. THE CORROSION WAS REMOVED AND A STRAP REPAIR WAS INSTALLED IAW SRM 53-
- [SDR CALA0300018](https://openairdocs.org/sdr/CALA0300018), Jan 22, 2003: INTERCOSTAL. CRACKED. INSPECTION FOUND CENTER FLOOR INTERCOSTAL AT CENTERLINE OF AIRCRAFT CRACKED IN TWO PLACES AT STA 344-360. THE CRACKS WERE 1" IN LENGTH. THE INTERCOSTAL WAS REMO
- [SDR CALA0200063](https://openairdocs.org/sdr/CALA0200063), Feb 6, 2002: ACM. LEAKING. SMOKE AND FUMES ENTERED THE CABIN AFTER TAKEOFF FROM IAH. SOME ALARMS IN THE CABIN ACTIVATED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT.
- [SDR CALA0101015](https://openairdocs.org/sdr/CALA0101015), Nov 29, 2001: FAN. FAILED. CREW REPORTED SMOKE IN CABIN AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING BY MAINTENANCE FOUND THA
- [SDR CALA9900085](https://openairdocs.org/sdr/CALA9900085), Jan 27, 1999: COOLING FAN. SHORTED. A BURNING ODOR WAS SMELLED IN THE CABIN DURING CLIMBOUT OF EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AVIONIC
- [SDR CALA9700508](https://openairdocs.org/sdr/CALA9700508), Apr 8, 1997: COUPLER. INOPERATIVE. THE ACFT EXPERIENCED 5 UNCONTROLLED YAWS (2 LEFT, 2 RIGHT, THEN 1 LEFT) DURING CLIMBOUT. THE YAW DAMPER WAS TURNED OFF AND THE PROBLEM CEASED. THE FLIGHT CONTIN

## 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 19970408009119I](https://openairdocs.org/incident/19970408009119I), Apr 8, 1997: Boeing 737524 (N14613), Cleveland, OH. Narrative: aircraft was at top of climb and experienced five (5) uncontrolled rudder kicks (yaw) (2) left (2) right and then (1) left. Autopilot kicked off by…

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