# N58606: 1994 Boeing 737-524, registration cancelled 2013-01-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 2, 2013
- 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: 27319
- Year built: 1994
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 21, 1994
- Certificate issued: December 21, 2012
- Last registry action: December 21, 2012
- Mode S code: A78EA9
- 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/N58606
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=58606
- Page: https://openairdocs.org/deregistered/N58606-2013-01-02

From the FAA registry file of October 31, 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 (38)

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

- [SDR CALA2012101800681](https://openairdocs.org/sdr/CALA2012101800681), Oct 18, 2012: PCU. LEAKING. DURING CRUSE ENG 1 A HYD PUMP LOW PRESS LIGHT ILLUMINATED. FOLLOWED BY GRADUAL DEPLETION OF SYS A HYD. FLUID LEVEL, FOLLOWED B Y ELECT HYD A PUMP, PUMP LOW PRES
- [SDR CALA2012010600013](https://openairdocs.org/sdr/CALA2012010600013), Jan 6, 2012: WARNING SYSTEM. FALSE ACTIVATION. DURING CLIMBOUT, AFTER LANDING GEAR LEVER TO NEUTRAL LEFT GEAR MAIN INDICATED GREEN AND RED, RIGHT GEAR INDICATED GREEN. REFERENCE T/S 32-61-00-101, C/W MAIN GE
- [SDR CALA2011032900214](https://openairdocs.org/sdr/CALA2011032900214), Dec 4, 2010: FRAME. CRACKED. BS 303.9 FRAME CRACKED AT STR 16L FORWARD SIDE AROUND OVAL HOLE. INSTALLED REPAIR PER ECRA 5311-01515. GENERATED DIP TO REINSPECT BEFORE THE ACCUMULATION OF 660
- [SDR CALA2010120100600](https://openairdocs.org/sdr/CALA2010120100600), Dec 1, 2010: SKIN. CRACKED. CRACK INDICATION FOUND AT FWD ENTRY DOOR UPPER HINGE CUTOUT AFT FASTENER HOLE 4TH FROM TOP, REF EA 5330-03736 REV B, STEP 14, INSTALLED REPAIR IAW ECRA 5330-040
- [SDR CALA2010120100599](https://openairdocs.org/sdr/CALA2010120100599), Dec 1, 2010: SKIN. WORN. SUPPORT TASK - RT OTBD MIDFLAP, INBD L/E WORN. MARKED, TRIMMED OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER IAW E CRA 5752-01496.
- [SDR CALA2010120100597](https://openairdocs.org/sdr/CALA2010120100597), Nov 29, 2010: BELTFRAME. CRACKED. SUPPORT TASK BELTFRAME STA 706 HAS CRACK INDICATION BETWEEN STRINGERS S8R AND S9R AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT (RIVET BUCKED TAIL) ARE
- [SDR CALA2011031500140](https://openairdocs.org/sdr/CALA2011031500140), Nov 24, 2010: SUPPORT FITTING. CORRODED. SUPPORT TASK LT WING NR 2 FLAP TRACK MOUNT HOLES SPOT FACE HAS SURFACE CORROSION UPPER SIDE. REMOVED AND REPLACED FLAP TRACK SUPPORT FITTING REF BOEING DWG 65C8
- [SDR CALA2010112400596](https://openairdocs.org/sdr/CALA2010112400596), Nov 24, 2010: SKIN. DENTED. SUPPORT TASK: WHEN PERFORMED DMG LOG 9593545 INSP ON A/B/B DOOR FOUND DENT AT 15 INCHES FROM TOP AND 14 INCHES FROM FWD EDGE OUT OF LIMITS PER SRM 52-00-01. A=1
- [SDR CALA2010112200595](https://openairdocs.org/sdr/CALA2010112200595), Nov 22, 2010: HINGE FITTING. CRACKED. L-1 DOOR LOWER HINGE FITTING CRACK INDICATION. INSTALLED NEW LOWER HINGE FITTING SRM 51-40-02, AFTER DISCOVERY LOWER HINGE FITTING WAS CRACKED.
- [SDR CALA2010112200594](https://openairdocs.org/sdr/CALA2010112200594), Nov 22, 2010: HINGE FITTING. CRACKED. L-1 DOOR UPPER HINGE FITTING CRACK INDICATION. INSTALLED NEW UPPER HINGE FITTING / SRM 51-40-02, AFTER DISCOVERY UPPER HINGE FITTING WAS CRACKED.
- [SDR CALA2010112200591](https://openairdocs.org/sdr/CALA2010112200591), Nov 19, 2010: SHEAR TIE. CRACKED. SHEAR TIE CRACKED STA 967 AT S4L CABIN CTN 53-304-108. REMOVED AND REPLACED SHEAR TIE REF SRM 51-40-02 AND BOEING DWG 65-46563.
- [SDR CALA2010111900589](https://openairdocs.org/sdr/CALA2010111900589), Nov 19, 2010: ATTACH FITTING. CRACKED. SUPPORT TASK - BS 360L STR 11L, CRACK ON ATTACH CLIP. REMOVED CLIP, INSPECTED HOLES IN AREA AND INSTALLED NEW CLIP PER ECRA 5311-01513.
- [SDR CALA2010111900588](https://openairdocs.org/sdr/CALA2010111900588), Nov 19, 2010: BELTFRAME. CRACKED. SUPPORT TASK - BELFRAME STA 827 HAS CRACK AT FASTENER HOLE BETWEEN STRINGERS S8L AND S9L AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. REPAIRED F
- [SDR CALA2010111900587](https://openairdocs.org/sdr/CALA2010111900587), Nov 19, 2010: SKIN. CRACKED. SUPPORT TASK - RIVET HOLE STA 420 BETWEEN S-17 AND S-17 SHOWS CRACK INDICATION ON HFEC HOLE PROBE INSP REF NDT PT 6 51-00-00 FIG 16. REMOVED RIVET, REPAIRED SKI
- [SDR CALA2011031500139](https://openairdocs.org/sdr/CALA2011031500139), Nov 17, 2010: FLAP TRACK. CORRODED. RT WING NR 7 FLAP TRACK AFT ATTACH POINT EMITTING RUST. CORRECTED 11/10/2010 HOU 66274 INSTALLED NEW SERVICEABLE NR 7 FLAP TRACK; REF AMM 27-51-49-404-006. ROTA
- [SDR CALA2010111500541](https://openairdocs.org/sdr/CALA2010111500541), Nov 15, 2010: FRAME. CRACKED. MAIN FRAME CRACKED AT STA 616 JUST BELOW FLOOR DECK LT SIDE. COMPLETED REPAIR OF STA 616 FRAME REF EC/RA 5311-01158.
- [SDR CALA2010111500540](https://openairdocs.org/sdr/CALA2010111500540), Nov 15, 2010: FRAME. CRACKED. MAIN FRAME CRACKED STA 616 RT JUST BELOW MAIN DECK FLOOR. COMPLETED REPAIR FRAME STA 616R REF EC/RA 5311-01158.
- [SDR CALA2010111000534](https://openairdocs.org/sdr/CALA2010111000534), Nov 10, 2010: BELTFRAME. CRACKED. SUPPORT TASK - BELTFRAME STA. 747 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8L AND S9L AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. INSTAL
- [SDR CALA2010110900533](https://openairdocs.org/sdr/CALA2010110900533), Nov 9, 2010: BELTFRAME. CRACKED. SUPPORT TASK - BELTFRAME STA 360, CRACKED AT FASTENERS HOLE BETWEEN STR 8L & 9L AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. INSTALLED REPAI
- [SDR CALA2010110900532](https://openairdocs.org/sdr/CALA2010110900532), Nov 8, 2010: BELTFRAME. CRACKED. SUPPORT TASK - BELTFRAME AT STA 727B HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8L AND S9L AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. REP
- [SDR CALA2010110900531](https://openairdocs.org/sdr/CALA2010110900531), Nov 8, 2010: BELTFRAME. CRACKED. SUPPORT TASK - BELTFRAME STA 867 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8L AND S9L AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. REPAIRE
- [SDR CALA2010110800528](https://openairdocs.org/sdr/CALA2010110800528), Nov 8, 2010: BELTFRAME. CRACKED. SUPPORT TASK - BELTFRAME STA 440 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8L AND S9L AT THE A/C OUTLET SUPPORT BRACKET ATTACHMENT AREA (ALL WORK ACCOMPLI
- [SDR CALA2010110800527](https://openairdocs.org/sdr/CALA2010110800527), Nov 8, 2010: BELTFRAME. CRACKED. SUPPORT TASK - BELTFRAME STA 400 CRACKED AT FASTENER HOLE BETWEEN STR 8L & 9L AT A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. INSTALLED REPAIR ANGL
- [SDR CALA2010110800526](https://openairdocs.org/sdr/CALA2010110800526), Nov 8, 2010: BELTFRAME. CRACKED. SUPPORT TASK. BELTFRAME STA 400 CRACK INDICATION BETWEEN STR 8R AND 9R AT A/C OULET EXTRUSION SUPPORT BRACKET ATTACHMENT (RIVET BUCKED TAIL) AREA PER MID-FREQ E
- [SDR CALA2010110800525](https://openairdocs.org/sdr/CALA2010110800525), Nov 7, 2010: BELTFRAME. CRACKED. SUPPORT TASK BELTFRAME STA 380 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8R AND S9R AT THE A/C OUTLET SUPPORT BRACKET DAMAGED AREA REMOVED FROM FRAME AT S
- [SDR CALA2010110800524](https://openairdocs.org/sdr/CALA2010110800524), Nov 7, 2010: BELTFRAME. CRACKED. SUPPORT TASK BELTFRAME STA 867 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8R AND S9R AT A/C OUTLET EXTRUSION BRACKET DAMAGED AREA REMOVED FROM FRAME AT STA
- [SDR CALA2010110800523](https://openairdocs.org/sdr/CALA2010110800523), Nov 7, 2010: BELTFRAME. CRACKED. SUPPORT TASK BELTFRAME STA440 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8R AND S9R AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET DAMAGED AREA REMOVED FROM F
- [SDR CALA2010110800522](https://openairdocs.org/sdr/CALA2010110800522), Nov 6, 2010: INTERCOSTAL. CRACKED. FWD ENTRY BETWEEN STA 344 - 360 BL-0 INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL, ALL HOLES DRILLED AS NEEDED REF SRM 51-40-02 & 51-40-05.
- [SDR CALA0700252](https://openairdocs.org/sdr/CALA0700252), May 16, 2007: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR CUTOUT FORWARD FRAME AT LOWER STOP PAD, STA 400, S17R TO S28R. A NEW FRAME WAS INSTALLED IAW SRM 51-10-02 
- [SDR CALA0500453](https://openairdocs.org/sdr/CALA0500453), Dec 25, 2005: SLIDE. LOW. THE L-2 DOOR SLIDE WAS FOUND WITH LOW PRESSURE. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-35.
- [SDR CALA0300528](https://openairdocs.org/sdr/CALA0300528), Sep 13, 2003: FIRE DETECTOR. INOPERATIVE. THE APU FIRE DETECTION LIGHT ILLUMINATED WHILE ENROUTE FROM PHL TO IAH. THE APU FIRE BOTTLE WAS DISCHARGED, BUT THE WARNING LIGHT REMAINED ILLUMINATED. THE AIRC
- [SDR CALA0000583](https://openairdocs.org/sdr/CALA0000583), Apr 28, 2000: ENGINE. LEAKING. ON TAKE-OFF AND LANDING WITH THROTTLES ADVANCED COCKPIT AND CABIN HAS STRONG UNPLEASANT ODOR. REMOVED AND REPLACED ENGINE DUE TO OIL LEAK PER MM 71-00-00.
- [SDR CALA0000437](https://openairdocs.org/sdr/CALA0000437), Apr 7, 2000: ACCESS DOOR. WORN. INSPECTION FOUND LEFT WING TANK NR 1 FUEL BOOST PUMP ACCESS PANEL UNSECURABLE DUE TO WORN SPOTS ON LOWER WING SKIN AT WBL 146. REPAIRED AREA IAW ECRA 5720-01793
- [SDR CALA0000436](https://openairdocs.org/sdr/CALA0000436), Apr 7, 2000: SKIN. DENTED. INSPECTION FOUND SKIN LAP DENTED AT STA 967, STRINGER 26L. REPAIRED IAW ECRA 5360-01039.
- [SDR CALA0000364](https://openairdocs.org/sdr/CALA0000364), Mar 28, 2000: ANGLE. CORRODED. INSPECTION FOUND CABIN FLOOR R-1 DOOR THRESHOLD Z-ANGLE ATTACH CHORD CORRODED AT STA 294 - 298. THE ATTACH CHORD STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0000152](https://openairdocs.org/sdr/CALA0000152), Feb 13, 2000: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 295,S23L. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5330-02924.
- [SDR CAL950483](https://openairdocs.org/sdr/CAL950483), Jun 14, 1995: SENSOR TARGET. OUT OF ADJUST. EWR - FLT 1535 - THE NLG RED LIGHT REMAINED ILLUMINATED WHEN GEAR WAS EXTENDED FOR LANIDNG AT IAH. THE GEAR WAS CYCLED WITH NO CHANGE. EMERGENCY PROCEDURES WERE
- [SDR CAL950466](https://openairdocs.org/sdr/CAL950466), Jun 7, 1995: EGT INDICATOR. INOPERATIVE. FLT NR 1646 - DFW - THE NR 1 ENGINE OVERHEATED ACCOMPANIED BY ILLUMINATION OF RED LIGHT WHILE AT CRUISE. THE THROTTLE WAS REDUCED TO IDLE AND THE ENGINE SHUTDOW

## 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 20031025032879I](https://openairdocs.org/incident/20031025032879I), Oct 25, 2003: Boeing 737524 (N58606), Eagle Lake, TX. (-23) Time - 1430Z wx cond - IMC capt/s narrative-during descent thru 16000 ft encountered moderate turbulence. Forward galley f/a fell with ankle injury. Flt…

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