# N27610: 1994 Boeing 737-524, registration cancelled 2012-05-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 14, 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: 27323
- Year built: 1994
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 31, 1994
- Certificate issued: June 1, 1994
- Last registry action: April 10, 2012
- Mode S code: A2BF5A
- 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/N27610
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=27610
- Page: https://openairdocs.org/deregistered/N27610-2012-05-14

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 (43)

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

- [SDR CALA2012031900188](https://openairdocs.org/sdr/CALA2012031900188), Mar 10, 2012: SKIN. DENTED. REF L/P 7810838 FOR RECORD OF DAMAGES 6 X 1.6 X 0.090 DEEP ON FUSELAGE BETWEEN STATIONS 767 TO 787 BETWEEN STRINGERS 15R AND 16R. EC/RA 5330-03726 COVERS THREE 
- [SDR CALA2011120700794](https://openairdocs.org/sdr/CALA2011120700794), Dec 3, 2011: WIRE HARNESS. DEFECTIVE. APU FIRE INDICATION ON CLIMBOUT AT FL240. APU HANDLE WAS PULLED AND BOTTLE DISCHARGED. REPLACED HARNESS M/E 24-2611-3-0003 IAW WDM 26-11-31 RE N/R4479597. ALSO 
- [SDR CALA2011101400663](https://openairdocs.org/sdr/CALA2011101400663), Oct 14, 2011: UNKNOWN. ODOR. THEN GOT FULL FIRE WARNING LIGHT& BELLS RAN QRH DISCHARGED BOTTLES. FLT ATTENTANT CALLED UP, REPORTED SMELLED SMOKE, CALLED FOR FIREMEN AND WHEN THEY OPENED
- [SDR CALA2011021500093](https://openairdocs.org/sdr/CALA2011021500093), Feb 15, 2011: WARMER. ODOR. 1.5 HR INTO FLT, F/A'S REPORT THE BURNT WIRE SMELL IS BACK. DOES NOT APPEAR TO BE COMING FROM AIR VENT BUT IS PRESENT IN ACFT GALLEY. COFFEEMAKERS & OVENS W
- [SDR CALA2010061400278](https://openairdocs.org/sdr/CALA2010061400278), Jun 12, 2010: CONNECTOR. DEFECTIVE. CLIMBING OUT OF AT 18,000FT STARTED TO GET INTERMITTENT APU FIRE WARNING FOLLOWED IMMEDIATE ACTION ITEMS & QRH. DECLARED AN EMERGENCY & RETURNED TO CLE.
- [SDR CALA2010051000192](https://openairdocs.org/sdr/CALA2010051000192), May 9, 2010: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM AT STA 344 BETWEEN LBL 10 AND RBL 10 SEE WORK CARD MASTER PANEL CLOSE ZONE 107C SEQ 1007 FOR FLOOR PANELS INSTALLATION. REPAIRED CABIN FL
- [SDR CALA2010050400186](https://openairdocs.org/sdr/CALA2010050400186), May 3, 2010: SEAT TRACK. DAMAGED. RIGHT O/B SEAT TRACK 6 INCHES FWD OF STA 807 IS DAMAGED. CUT OUT DAMAGED SECTION OF SEAT TRACK AND SPLICED IN NEW SECTION OF TRACK REF SRM 53-00-52 REPAIR 4 OPT
- [SDR CALA2010050400184](https://openairdocs.org/sdr/CALA2010050400184), Apr 30, 2010: FRAME. CRACKED. FRAME STA 360 CRACKED BETWEEN STR 8L&9L AT A/C OUTLET EXTRUSION ATTACHMENT REPAIRED CABIN FRAME STA 360 L/T PER ECRA 5311-01488 AND GENERATED DIP PER PER EC
- [SDR CALA2010043000179](https://openairdocs.org/sdr/CALA2010043000179), Apr 29, 2010: BEAM. CORRODED. CORROSION AT L1 DOOR LWR SILL BEAM DOOR CHORD BETWEEN STA 300 AND 360. INSTALLED NEW CHORD AT L1 DOOR LWR SILL BEAM AREA REF SRM 51-40-02.
- [SDR CALA2010042900176](https://openairdocs.org/sdr/CALA2010042900176), Apr 29, 2010: FRAME. CRACKED. SUPPORT TASK - FRAME WEB OVAL HOLE CRACKED .5 INCH LONG AT STA BS 303.9 AND STRINGER S16L AREA. TRIMMED OUT CRACKED SECTION OF FRAME & SPLICED IN NEW SECTIO
- [SDR CALA2010042800175](https://openairdocs.org/sdr/CALA2010042800175), Apr 28, 2010: HINGE FITTING. CRACKED. L-1 DOOR JAMB, LOWER HINGE FITTING CRACKED ABOVE WL 236.68 AND JUST AFT OF STA 303.9. REMOVED AND REPLACED L-1 DOOR LOWER HINGE FITTING PER SRM 51-40-02.
- [SDR CALA2010050400183](https://openairdocs.org/sdr/CALA2010050400183), Apr 27, 2010: SKIN. CRACKED. CRACK FUSELAGE BETWEEN S-8L AND S-9L.
- [SDR CALA2010042700173](https://openairdocs.org/sdr/CALA2010042700173), Apr 26, 2010: FRAME. CRACKED. FRAME 907 CRACKED BETWEEN S-8L & S-9L AT A/C OUTLET EXTRUSION ATTACHMENT(MARKED). FRAME AT STA 907 STR 8L&9L REPAIRED PER EA5310-04498 OP2 DIP REQUIRED 
- [SDR CALA2010042700172](https://openairdocs.org/sdr/CALA2010042700172), Apr 26, 2010: FRAME. CRACKED. FRAME 867 CRACKED BETWEEN S-8L & S-9L AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). FRAME AT STA 867 STR 8L&9L REPAIRED PER EA5310-04498 OP2 DIP REQUIRED
- [SDR CALA2010042700171](https://openairdocs.org/sdr/CALA2010042700171), Apr 26, 2010: FRAME. CRACKED. SUPPORT TASK PAX CABIN FRAME AT STA 440 BETWEEN STR 8L AND 9L HAS CRACKED INDICATION WHEN PERFORMED HFEC PER EA 5310-04498 OP2. FRAME AT STA 440 STR 8L&9L R
- [SDR CALA2010042700170](https://openairdocs.org/sdr/CALA2010042700170), Apr 26, 2010: FRAME. CRACKED. FRAME 400 CRACKED BETWEEN S-8L & S-9L AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). FRAME AT STA 400 STR 8L&9L REPAIRED PER EA5310-04498 OP2 DIP REQUIRED
- [SDR CALA2010042700169](https://openairdocs.org/sdr/CALA2010042700169), Apr 26, 2010: FRAME. CRACKED. SUPPORT TASK PAX CABIN FRAME STA 440 BETWEEN SRT 8R AND 9R HAS CRACKED INDICATION WHEN PERFORMED HFEC INSPECTION PER EA 5310-04498 OP20. FRAME AT STA 440 STR 8L
- [SDR CALA2010042700168](https://openairdocs.org/sdr/CALA2010042700168), Apr 26, 2010: FRAME. CRACKED. FRAME 380 CRACKED BETWEEN S-8R & S-9R AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). FRAME AT STA 380 STR 8R&9R REPAIRED PER EA5310-04498 OP2 DIP REQUIRED
- [SDR CALA2010042600165](https://openairdocs.org/sdr/CALA2010042600165), Apr 25, 2010: FRAME. CRACKED. SUPPORT TASK PAX CABIN FRAME STA 727B BETWEEN STR 8R AND 9R HAS CRACKED INDICATION WHEN PERFORMED HFEC PER EA 5310-04498 OP 2. REMOVED DAMAGED AREA, FABRICATED 
- [SDR CALA2010042600163](https://openairdocs.org/sdr/CALA2010042600163), Apr 24, 2010: SILL. CORRODED. SUPPORT TASK B737-53-4-0010 L-1 DOOR LOWER SILL WEB IS CORRODED BETWEEN STA 312 & 344. REMOVED AND REPLACED L1 DOOR LOWER SILL WEB REF SRM 51-40-02.
- [SDR CALA2010042600162](https://openairdocs.org/sdr/CALA2010042600162), Apr 24, 2010: DOOR FRAME. CRACKED. SUPPORT TASK FWD CARGO DOOR CUTOUT, AFT FRAME CRACKED AT DOOR STOP ATTACHMENT HOLE AT S-22R REFERENCE EA 5310-0444E REV C. REMOVED AND REPLACED CRACKED FRAME PE
- [SDR CALA2010042600161](https://openairdocs.org/sdr/CALA2010042600161), Apr 23, 2010: FRAME. CRACKED. SUPPORT TASK PER EA 5310-04498 OP.2, FRAME CRACKED STA 727B BETWEEN S8L AND 9SL. REPAIRED FRAME STA 727B BETWEEN S-8L AND S9-L REF EA 5310-04498.
- [SDR CALA2010042600159](https://openairdocs.org/sdr/CALA2010042600159), Apr 23, 2010: FRAME. CRACKED. FRAME CRACKED BETWEEN S-8R & S9R AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). REPAIRED FRAME 787 BETWEEN S-8R AND S-9R REF EA 5310-014498.
- [SDR CALA2010042600158](https://openairdocs.org/sdr/CALA2010042600158), Apr 23, 2010: FRAME. CRACKED. FRAME 747 CRACKED BETWEEN S-8R AND S-9R AT OUTLET EXTRUSION ATTACHMENT (MARKED). REPAIRED FRAME STA 747R BETWEEN S-8R AND S-9R REF EA 5310-0449 8.
- [SDR CALA2010042600156](https://openairdocs.org/sdr/CALA2010042600156), Apr 23, 2010: FRAME. CRACKED. FRAME 907 CRACKED BETWEEN S-8R & S-9R AT A/C OUTLET T EXTRUSION ATTACHMENT (MARKED). PERFORMED REPAIR PER EA5310-04498,OP 02.
- [SDR CALA2010042600155](https://openairdocs.org/sdr/CALA2010042600155), Apr 23, 2010: FRAME. CRACKED. FRAME 867 CRACKED BETWEEN S-8R & S-9R AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). PERFORMED REPAIR PER EA 5310-04498, OP. O2.
- [SDR CALA2010042300154](https://openairdocs.org/sdr/CALA2010042300154), Apr 23, 2010: FRAME. CRACKED. FRAME 827 CRACKED BETWEEN S-8L & S9L AT A/C OUTLET EXTRUSION ATTACHMENT. REPAIRED FRAME 827 LT PER EC/RA 5311-01489.
- [SDR CALA2010042300153](https://openairdocs.org/sdr/CALA2010042300153), Apr 23, 2010: FRAME. CRACKED. FRAME 827 CRACKED BETWEEN S-8R &S-9R AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). REPAIRED CRACKED FRAME 827 RT PER EC/RA 5311-01489.
- [SDR CALA2010042200147](https://openairdocs.org/sdr/CALA2010042200147), Apr 21, 2010: FRAME. CRACKED. FRAME 400 CRACKED BETWEEN S-8R & S-9R AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). PERFORMED REPAIR PER EA5310-04498, OP.02.
- [SDR CALA2009031700143](https://openairdocs.org/sdr/CALA2009031700143), Mar 16, 2009: TRANSMITTER. FAILED. ON APPROACH WHILE SETTING THE FLAPS TO 30, GOT A SPLIT FLAPS 17 TO 24. ON G/A PLACED FLAPS TO 15 DEGREES AND FLAPS STAYED AT 17 AND 24, ON DOWNWIND FLAPS CAME U
- [SDR CALA0700309](https://openairdocs.org/sdr/CALA0700309), Jun 18, 2007: SILL. CORRODED. INSPECTION FOUND R-1 DOOR SILL LOWER CHORD CORRODED AT STA 277-360, RBL 113. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0500050](https://openairdocs.org/sdr/CALA0500050), Feb 22, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND AFT ENTRY FLOORBEAM CORRODED AT FASTENER HOLES, STA 986.5, LBL 54 TO RBL 54. REPAIRED IAW ECRA 5310-04461.
- [SDR CALA0400481](https://openairdocs.org/sdr/CALA0400481), May 8, 2004: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN CORRODED AFT OF FORWARD BAG BIN DOOR CUTOUT AT STA 452, S22R. A REPAIR WAS INSTALLED IAW ECRA 5330-03351.
- [SDR CALA0400479](https://openairdocs.org/sdr/CALA0400479), May 7, 2004: SKIN. DENTED. INSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE SKIN DENTED AT STA 105.26. THE DENTED AREA WAS CUT OUT AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW
- [SDR CALA0200567](https://openairdocs.org/sdr/CALA0200567), Nov 26, 2002: CARGO TRACK. CRACKED. INSPECTION FOUND A 7 INCH CRACK IN TIE DOWN RAIL AT STA 807, RBL 14. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 53-00-53, FIGURE 202.
- [SDR CALA0200566](https://openairdocs.org/sdr/CALA0200566), Nov 26, 2002: SKIN. CRACKED. INSPECTION FOUND A 1/8" CRACK IN SKIN OF CO-PILOT'S WINDSHIELD POST AT UPPER R/H CORNER. A DOUBLER WAS INSTALLED IAW SRM 53-10-01.
- [SDR CALA0200565](https://openairdocs.org/sdr/CALA0200565), Nov 25, 2002: WEB. CRACKED. INSPECTION FOUND A 2" CRACK IN WEB AT STA 344-360, BL 0. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0200562](https://openairdocs.org/sdr/CALA0200562), Nov 24, 2002: ANGLE. CRACKED. INSPECTION FOUND A 1" CRACK IN ANGLE AT STA 500-520, BL O. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0200561](https://openairdocs.org/sdr/CALA0200561), Nov 24, 2002: ANGLE. CRACKED. INSPECTION FOUND A 1" CRACK IN ANGLE AT STA 344-360, LBL 12. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0200560](https://openairdocs.org/sdr/CALA0200560), Nov 23, 2002: SKIN. DENTED. A DENT WAS DISCOVERED IN FUSELAGE SKIN AT STA 360 ABOUT 3" ABOVE CUSP LINE AND 22" AFT OF L-1 DOOR. INSTALLED DOUBLER IAW SRM 53-00-01.
- [SDR CALA0200357](https://openairdocs.org/sdr/CALA0200357), Jun 19, 2002: WIRE. OUT OF POSITION. THE WHITE EMERGENCY PATH LIGHT AT SEAT 18C WAS FOUND INOPERATIVE DUE TO A PULLED WIRE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-81.
- [SDR CALA0000742](https://openairdocs.org/sdr/CALA0000742), May 25, 2000: WINDOW. OUT OF ADJ. THE R-2 SLIDING COCKPIT WINDOW REQUIRED EXCESS FORCE TO LATCH AND UNLATCH. THE R-2 SLIDING WINDOW WAS ADJUSTED IAW MM 56-12-11, PAGE 501-511.
- [SDR CALA9701713](https://openairdocs.org/sdr/CALA9701713), Dec 9, 1997: BATTERY PACK. DISCHARGED. INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE AT RIGHT OVERWING AND AISLE RIGHT SIDE, ROW 7 AND 8. THE BATTERY PACK WAS REMOVED AND REPLACED.

## 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 19940717030939I](https://openairdocs.org/incident/19940717030939I), Jul 17, 1994: Boeing 737524 (N27610), No damage

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