# N70352: 1987 Boeing 737-3TO, registration cancelled 2009-11-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 24, 2009 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 737-3TO](https://openairdocs.org/model/boeing-737-3to) (registry code 138447G) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 23590 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 12, 1987 - Certificate issued: October 8, 1998 - Last registry action: November 18, 2008 - Mode S code: A962D5 - 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/N70352 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=70352 - Page: https://openairdocs.org/deregistered/N70352-2009-11-24 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 737-3TO: https://openairdocs.org/model/boeing-737-3to.md ## Service difficulty reports (56, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0700325](https://openairdocs.org/sdr/CALA0700325), Jun 26, 2007: STRINGER. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN TAIL COMPARTMENT STRINGER 21R BETWEEN STA 1040 AND 1064. A REPAIR ANGLE AND SHIM WERE INSTALLED IAW SRM 53-00-00. - [SDR CALA0700322](https://openairdocs.org/sdr/CALA0700322), Jun 26, 2007: SKIN. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN THE FUSELAGE SKIN AT AFT EDGE INSTRUMENT COOLING AIR DUCT OUTLET, STA 380, LBL 4, S28L TO S28R. THE CRACK WAS STOP DRILLED - [SDR CALA0700320](https://openairdocs.org/sdr/CALA0700320), Jun 25, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN FORWARD CARGO DOOR CUTOUT FORWARD FRAME AT LOWER STOP PAD, STA 440, S16R TO S27R. THE FRAME WAS REMOVED AND REPLACED IAW SR - [SDR CALA0700318](https://openairdocs.org/sdr/CALA0700318), Jun 24, 2007: SKIN. CRACKED. INSPECTION FOUND A 2.2 INCH CRACK IN THE FUSELAGE SKIN AT THE AFT LOWER CORNER OF THE R-1 DOOR. REPAIRED IAW SRM 53-10-01, REPAIR 2. - [SDR CALA0700317](https://openairdocs.org/sdr/CALA0700317), Jun 24, 2007: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FORWARD CARGO DOOR CUTOUT AFT FRAME AT LOWER PAD FITTING, STA 480-500, S16R TO S27R. A NEW FRAME WAS INSTALLED IAW SRM 51-40 - [SDR CALA0700315](https://openairdocs.org/sdr/CALA0700315), Jun 20, 2007: FLOORBEAM. CORRODED. INSPECTION FOUND AFT ENTRY FLOORBEAM UPPER CHORD CORRODED IN NUMEROUS AREAS THE ENTIRE LENGTH, STA 986.5, LBL 40 TO RBL 40. THE FLOORBEAM WAS REPAIRED IAW ECRA - [SDR CALA0700312](https://openairdocs.org/sdr/CALA0700312), Jun 19, 2007: FLOORBEAM. CORRODED. INSPECTION FOUND MAIN CABIN FLOORBEAM HAD CORROSION EXTENDING UNDER FLOOR MOUNT AT STA 946, LBL 13. THE UPPER FLANGE I-BEAM WAS REMOVED AND REPLACED FROM RBL 35 - [SDR CALA0700305](https://openairdocs.org/sdr/CALA0700305), Jun 14, 2007: FLOORBEAM. CORRODED. INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AT STA 967, RBL 28. THE FLOORBEAM WAS REPAIRED IAW SRM 53-30-51, REPAIR 2. - [SDR CALA0600418](https://openairdocs.org/sdr/CALA0600418), May 3, 2006: SPAR. CRACKED. LEFT REAR SPAR CRACKED 3 INCHES AT STA 297. REPAIRED IAW ECRA 5510-01835. - [SDR CALA0500377](https://openairdocs.org/sdr/CALA0500377), Oct 25, 2005: KEELBEAM. CORRODED. INSPECTION FOUND RT LOWER CHORD OF KEELBEAM CORRODED AT STA 540, RT A/C BAY COMPARTMENT. THE CORROSION WAS REMOVED IAW ECRA 5310-04491. - [SDR CALA0500314](https://openairdocs.org/sdr/CALA0500314), Sep 12, 2005: SKIN. CRACKED. MAINTENANCE FOUND A 2 INCH CRACK IN RT FUSELAGE SKIN AT STA 727D AND S23R. A REPAIR WAS INSTALLED IAW ECRA 5330-03482. A DIP WAS ISSUED TO REINSPECT THE AREA WI - [SDR CALA0400679](https://openairdocs.org/sdr/CALA0400679), Oct 15, 2004: SKIN. CRACKED. A WALKAROUND INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STA 727D TO STA 727E, S22L TO S24L. THE SKIN WAS REPAIRED IAW ECRA 5330-03376. - [SDR CALA0400586](https://openairdocs.org/sdr/CALA0400586), Jul 24, 2004: DRIVE SHAFT. SHEARED. THE NR 2 ENGINE STOPPED RUNNING AT TOP OF CLIMB AT FL 270 AFTER DEPARTING DFW BOUND FOR IAH. THE ENGINE FAILURE CHECKLIST WAS PERFORMED. A RESTART WAS NOT ATTEM - [SDR CALA0400564](https://openairdocs.org/sdr/CALA0400564), Jul 3, 2004: BATTERY PACK. INOPERATIVE. INSPECTION FOUND THE EMERGENCY LIGHTS INOPERATIVE NEAR L-1 DOOR. THE OVERHEAD BATTERY PACK IN FORWARD GALLEY WAS REMOVED AND REPLACED. - [SDR CALA0400289](https://openairdocs.org/sdr/CALA0400289), Mar 28, 2004: MEGAPHONE. INOPERATIVE. THE MEGAPHONE IN FIRST CLASS CABIN WAS FOUND INOPERATIVE. THE MEGAPHONE WAS REPLACED. - [SDR CALA0300327](https://openairdocs.org/sdr/CALA0300327), Jun 21, 2003: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN INTERIOR SKIN OF FORWARD CARGO DOOR LOCATED OVER HANDLE AREA. A DOUBLER WAS INSTALLED IAW ECRA 5232-01031. - [SDR CALA0300325](https://openairdocs.org/sdr/CALA0300325), Jun 17, 2003: ANGLE. CORRODED. INSPECTION FOUND SUPPORT ANGLE CORRODED AT STA 1016, BL 0. THE ANGLE WAS REPLACED IAW SRM 51-10-02 AND ECRA 5311-01152. - [SDR CALA0300316](https://openairdocs.org/sdr/CALA0300316), Jun 16, 2003: SKIN. GOUGED. INSPECTION FOUND A GOUGE IN CENTER OF AFT BAGGAGE BIN DOOR EXTERIOR SKIN ABOUT 12 INCHES ABOVE HANDLE. THE SKIN WAS REPAIRED IAW SRM 52-00-01, PAGE 203. - [SDR CALA0300314](https://openairdocs.org/sdr/CALA0300314), Jun 14, 2003: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN NR 4 SLAT ACTUATOR CUTOUT ON RT FIXED LEADING EDGE SKIN AT WBL 325. A DOUBLER WAS INSTALLED IAW SRM 57-41-01. - [SDR CALA0300307](https://openairdocs.org/sdr/CALA0300307), Jun 11, 2003: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN NR 6 SLAT PANEL SKIN AT LOWER RIVET LOCATED JUST O/B OF I/B AUX TRACK, RIGHT SLAT STA 300. A REPAIR WAS INSTALLED IAW SRM 57- - [SDR CALA0300302](https://openairdocs.org/sdr/CALA0300302), Jun 10, 2003: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LT WINDSHIELD POST SKIN. THE CRACK WAS ROUTED OUT AND DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-10-01, FIGURE 210. - [SDR CALA0300301](https://openairdocs.org/sdr/CALA0300301), Jun 9, 2003: FITTING. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN HORIZONTAL STABILIZER CENTER SECTION UPPER CROSS BEAM FITTING AT STA 1121, LBL 10. THE FITTING WAS REMOVED AND REPLACED IAW B - [SDR CALA0300300](https://openairdocs.org/sdr/CALA0300300), Jun 9, 2003: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED FROM STA 787 TO 850 AT STRINGER 25R. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-02. - [SDR CALA0300298](https://openairdocs.org/sdr/CALA0300298), Jun 8, 2003: FITTING. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN HORIZONTAL STABILIZER CENTER SECTION UPPER CROSS BEAM FITTING AT STA 1121, RBL 10. THE FITTING WAS REMOVED AND REPLACED IAW S - [SDR CALA0300296](https://openairdocs.org/sdr/CALA0300296), Jun 7, 2003: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN NR 5 SLAT PANEL AT I/B AUX TRACK. REPAIRED SLAT SKIN IAW SRM 57-43-01, FIGURE 206, SHEETS 1-4. - [SDR CALA0300295](https://openairdocs.org/sdr/CALA0300295), Jun 7, 2003: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN EXTERIOR FUSELAGE SKIN AT R-2 DOOR UPPER HINGE ARM CUTOUT. THE SKIN WAS REPAIRED IAW SRM 53-60-01. - [SDR CALA0300294](https://openairdocs.org/sdr/CALA0300294), Jun 7, 2003: CARGO TRACK. CORRODED. INSPECTION FOUND RIGHT CARGO TRACK CORRODED AT STA 944. THE CORRODED SECTION OF TRACK WAS REMOVED AND A NEW TRACK AND SPLICE WERE INSTALLED IAW SRM 53-00-53. - [SDR CALA0300293](https://openairdocs.org/sdr/CALA0300293), Jun 7, 2003: INTERCOSTAL. CRACKED. INSPECTION FOUND A 2 INCH CRACK AT SCREW HOLE OF INTERCOSTAL AT BS 500D-520, MAIN CABIN FLOOR CENTERLINE. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10 - [SDR CALA0300304](https://openairdocs.org/sdr/CALA0300304), Jun 6, 2003: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN VERTICAL ANGLE ON BOTTOM END AT BS 616, LBL 65 OF MAIN CABIN, TOP OF WING CENTER SECTION. THE ANGLE FORMS I/B SECTION OF BS 6 - [SDR CALA0300292](https://openairdocs.org/sdr/CALA0300292), Jun 6, 2003: FITTING. CORRODED. INSPECTION FOUND LEFT O/B SUPPORT FITTING CORRODED BETWEEN STA 1006 AND 1016, LBL 36. THE SUPPORT FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0300290](https://openairdocs.org/sdr/CALA0300290), Jun 6, 2003: FITTING. CORRODED. INSPECTION FOUND FITTING O/B OF STRINGER 18R AT STA 1016 CORRODED. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0300285](https://openairdocs.org/sdr/CALA0300285), Jun 6, 2003: ANGLE. CORRODED. INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 940-992. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 53-60-15. - [SDR CALA0300284](https://openairdocs.org/sdr/CALA0300284), Jun 5, 2003: STIFFENER. CORRODED. INSPECTION FOUND STIFFENERS ON FORWARD SIDE OF AFT PRESSURE BULKHEAD CORRODED AT STA 1016 BETWEEN S28L AND S28R. THE STIFFENERS WERE REPAIRED IAW BOEING DRAWING - [SDR CALA0300330](https://openairdocs.org/sdr/CALA0300330), Jun 2, 2003: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN THE INNER CHORD OF THE LT FRAME AT STA 616. REPAIRED IAW ECRA 5311-01150. - [SDR CALA0300281](https://openairdocs.org/sdr/CALA0300281), Jun 2, 2003: STRINGER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN STRINGER 16L AT BS 500C + 4, JUST FORWARD OF LEFT ICE LIGHT HOUSING. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, FIGURE 201. - [SDR CALA0300277](https://openairdocs.org/sdr/CALA0300277), Jun 1, 2003: FLOOR SUPPORT. CORRODED. INSPECTION FOUND LEFT O/B FLOOR SUPPORT CORRODED BETWEEN STA 1006-1016, LBL 36. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0200482](https://openairdocs.org/sdr/CALA0200482), Oct 2, 2002: SKIN. CRACKED. A WALKAROUND INSPECTION FOUND A 3" CRACK IN L/H FUSELAGE SKIN AT STA 727C, STRINGER 25L AND 26L. THE CRACKED AREA OF SKIN WAS REMOVED AND A DOUBLER WAS INSTALLE - [SDR CALA0100954](https://openairdocs.org/sdr/CALA0100954), Oct 16, 2001: FLANGE. CORRODED. AFT CARGO COMPARTMENT UNDER LAV FLOOR BEAMS AT STATION 986.5 NUT CLIPS CORRODED ON UPPER BEAM. REMOVED DAMAGED UPPER BEAM AND CLIPS. INSTALLED REPAIR DOUBLER PE - [SDR CALA0100953](https://openairdocs.org/sdr/CALA0100953), Oct 16, 2001: FLANGE. CORRODED. AFT CARGO COMPARTMENT UNDER RIGHT LAV FLOOR BEAM STATION 986.5 HAS CORROSION ON THE OUTBOARD. REMOVED CORRODED PREVIOUS REPAIR AND INSTALLED NEW UPPER FLANGE DO - [SDR CALA0100952](https://openairdocs.org/sdr/CALA0100952), Oct 16, 2001: FLANGE. CORRODED. AFT CARGO COMPARTMENT UNDER LEFT LAV FLOOR BEAM STATION STATION 986.5 CORRODED. REMOVED CORRODED REPAIR AND REINSTALLED NEW UPPER FLANGE DOUBLER PER SRM 5310-03 - [SDR CALA0100951](https://openairdocs.org/sdr/CALA0100951), Oct 15, 2001: CARGO TRACK. CRACKED. FORWARD BAG BIN CRACKED (10 INCHES) ON RIGHT TIE DOWN RAIL FROM STATION 480 - 500. INSTALLED NUT PLATES ON UPPER FLANGE OF TIE DOWN RAIL PER SRM 51-10-2. - [SDR CALA0100948](https://openairdocs.org/sdr/CALA0100948), Oct 15, 2001: FLOOR SUPPORT. CRACKED. FBB 3 INCH CRACK ON FLOOR SUPPORT STRUCTURE BETWEEN STA 500 AND 500A AND ABOUT 2 INCHES TO RT SIDE FROM CENTER LINE MARKED. REMOVED AND REPLACED SUPPORT PER SRM - [SDR CALA0100941](https://openairdocs.org/sdr/CALA0100941), Oct 11, 2001: WEB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN CABIN FLOOR WEB ON FORWARD SIDE OF FLOORBEAM AT BS 328. AN INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0100940](https://openairdocs.org/sdr/CALA0100940), Oct 11, 2001: WEB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN CABIN FLOOR WEB ON AFT SIDE OF FLOORBEAM AT BS 328. AN INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0100827](https://openairdocs.org/sdr/CALA0100827), Sep 3, 2001: CONTROL CABLE. OUT OF RIG. THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM DTW. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND THE RT MLG T - [SDR CALA0100012](https://openairdocs.org/sdr/CALA0100012), Jan 11, 2001: SOCKET. INOPERATIVE. INSPECTION FOUND THE AFT EXTERIOR OVERWING EXIT EMERGENCY LIGHT INOPERATIVE AT STA 773. THE SOCKET ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. - [SDR CALA0001946](https://openairdocs.org/sdr/CALA0001946), Dec 15, 2000: STRUT. FLAT. THE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM IAH. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT I - [SDR CALA0000002](https://openairdocs.org/sdr/CALA0000002), Jan 6, 2000: FIRE DETECTOR. MALFUNCTIONED. THE APU FIRE WARNING LIGHT ILLUMINATED WHILETHE APU WAS NOT RUNNING, AFTER TAKEOFF FROM JAX. THE FIRE BOTTLE WAS DISCHARGED, BUT THE LIGHT DID NOT EXTINGUISH. T - [SDR CALA9901541](https://openairdocs.org/sdr/CALA9901541), Nov 29, 1999: FAN. FAILED. A BURNING ODOR ENTERED THE COCKPIT AND CABIN ON CLIMBOUT FROM ABQ. THE AIRCRAFT WAS RETURNED TO ABQ WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AVIO - [SDR CALA9900871](https://openairdocs.org/sdr/CALA9900871), Jul 27, 1999: SKIN. CRACKED. INSPECTION FOUND A 1 CRACK IN NR 1 ENGINE PYLON SKIN AT PANEL CUTOUT 5727L (NAC STA 213). THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-0 All 56: https://openairdocs.org/deregistered/N70352-2009-11-24/reports.md ## Other aircraft with N70352 - [Cancelled 2017-02-13](https://openairdocs.org/deregistered/N70352-2017-02-13): Piper PA-28-181, S/N 2843829, built 2016. Exported to Indonesia. Owner: [Globe Aero LLC](https://openairdocs.org/faa-owner/GLOBE%20AERO%20LLC), [Lakeland, FL](https://openairdocs.org/faa-place/FL/Lakeland) - [Cancelled 1970-06-05](https://openairdocs.org/deregistered/N70352-1970-06-05): Piper J3C-65, S/N 17337. Owner: [Kenneth D Burden Sr](https://openairdocs.org/faa-owner/KENNETH%20D%20BURDEN%20SR), [Waynesfield, OH](https://openairdocs.org/faa-place/OH/Waynesfield) --- 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.