# N16339: 1987 Boeing 737-3TO, registration cancelled 2011-08-11 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 11, 2011 - Status when cancelled: Third renewal notice - 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: 23577 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 12, 1987 - Certificate issued: March 28, 2001 - Last registry action: October 21, 2008 - Mode S code: A0FFB6 - 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/N16339 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16339 - Page: https://openairdocs.org/deregistered/N16339-2011-08-11 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 (38) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0800088](https://openairdocs.org/sdr/CALA0800088), Feb 2, 2008: HEATER. SPARKS. L-1 WINDOW HEAT CAUSED SPARKING AND SMOKE IN THE COCKPIT TO COME FROM THE L-1 WINDOW CONNECTION. - [SDR CALA0700662](https://openairdocs.org/sdr/CALA0700662), Nov 8, 2007: CHARGER. INOPERATIVE. THE EMERGENCY EXIT LIGHTS FROM ROW 21-25 LEFT WERE FOUND INOPERATIVE. THE AFT BATTERY PACK AND CHARGER WERE REMOVED AND REPLACED IAW AMM 33-51-51 PG 201. - [SDR CALA0600310](https://openairdocs.org/sdr/CALA0600310), Aug 24, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, S19L, LBL 10-12. A REPAIR STRAP AND SHIM WERE INSTALLED IAW SRM 53-00-51. - [SDR CALA0600063](https://openairdocs.org/sdr/CALA0600063), Feb 15, 2006: ANGLE. CORRODED. INSPECTION FOUND BOTTOM ANGLE CORRODED BETWEEN STA 227.8 AND 259.5, S27R, RT NOSE WHEEL WELL. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND MM 51-40-0 - [SDR CALA0600047](https://openairdocs.org/sdr/CALA0600047), Feb 10, 2006: ANGLE. CORRODED. INSPECTION FOUND R-1 DOOR THRESHOLD Z-ANGLE CORRODED ON UPPER AND LOWER SURFACES AT STA 312-328, RBL 56-57. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-0 - [SDR CALA0600046](https://openairdocs.org/sdr/CALA0600046), Feb 9, 2006: STIFFENER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RT WHEEL WELL WING CENTER BOX VERTICAL STIFFENER, RBL 6.15, WL 170.4. THE CRACK WAS COMING FROM A FASTENER. REPAIRED IAW EA - [SDR CALA0600316](https://openairdocs.org/sdr/CALA0600316), Feb 6, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED ON FORWARD SIDE AT STA 1016, LBL 35.5. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 3. - [SDR CALA0500374](https://openairdocs.org/sdr/CALA0500374), Oct 9, 2005: WIRE HARNESS. BURNED. MAINTENANCE DISCOVERED THE W802 WIRE BUNDLE AT LT WING ROOT UNDER I/B FLAP FAIRING BURNT. THERE WAS EVIDENCE OF CHAFING AND ARCING. THE WIRING BUNDLE WAS REPAIR - [SDR CALA0400301](https://openairdocs.org/sdr/CALA0400301), Mar 31, 2004: CHANNEL. CORRODED. INSPECTION FOUND FORWARD CARGO COMPARTMENT BILGE ANTENNA SUPPORT CHANNEL CORRODED AT STA 500-500A, BL 0. THE SUPPORT CHANNEL WAS REMOVED AND REPLACED IAW SRM 51 - [SDR CALA0400300](https://openairdocs.org/sdr/CALA0400300), Mar 30, 2004: FLOOR SUPPORT. CRACKED. INSPECTION FOUND CABIN FLOOR SUPPORT CRACKED AT STA 540 JUST LEFT OF BL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0400173](https://openairdocs.org/sdr/CALA0400173), Feb 26, 2004: SPAR. CRACKED. INSPECTION FOUND THE RT WING REAR SPAR UPPER CHORD CRACKED AT RSS 288. THE SPAR CHORD WAS REPAIRED IAW ECRA 5711-01055. - [SDR CALA0400069](https://openairdocs.org/sdr/CALA0400069), Jan 30, 2004: WIRE. SHORTED. AFT SERVICE & AFT ENTRY DOOR LIGHTS ILLUMINATED AT ROTATION. FORWARD SERVICE LIGHTS CAME ON AFTER A COUPLE OF MIN. FLT ATTENDANT REPORTED STRONG TOXIC FUMES IN - [SDR CALA0300299](https://openairdocs.org/sdr/CALA0300299), Jun 9, 2003: SKIN. DENTED. A DENT WAS DISCOVERED IN THE LT HORIZONTAL STABILIZER SKIN 15 INCHES O/B OF FUSELAGE ON LEADING EDGE AT STA 60. THE DENTED AREA PREVIOUSLY HAD AN INTERIM REPAIR - [SDR CALA0300246](https://openairdocs.org/sdr/CALA0300246), May 12, 2003: PRESSURE PANEL. CRACKED. INSPECTION FOUND A CRACK IN RT PRESSURE DECK AT STA 665-675, RBL 35-45. THE PRESSURE DECK WAS REPAIRED IAW ECRA 5312-01021. - [SDR CALA0300244](https://openairdocs.org/sdr/CALA0300244), May 10, 2003: SKIN. DENTED. THE LT FUSELAGE SKIN HAD A DENT LOCATED BETWEEN STA 211.80 AND 219.80, WL 200, (S19L LAP SPLICE). THE AREA PREVIOUSLY HAD AN INTERIM REPAIR INSTALLED AND WAS PL - [SDR CALA0200132](https://openairdocs.org/sdr/CALA0200132), Mar 15, 2002: KEELBEAM. CORRODED. INSPECTION FOUND RT WHEEL WELL WASHERS FRETTING INTO KEEL BEAM FROM STA 663-727. REPAIRED IAW ECRA 5311-01115. - [SDR CALA0200119](https://openairdocs.org/sdr/CALA0200119), Mar 4, 2002: SKIN. DENTED. INSPECTION FOUND C-2 DOOR SKIN DENTED, CENTERLINE 8 INCHES AFT OF LEADING EDGE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203. - [SDR CALA0200121](https://openairdocs.org/sdr/CALA0200121), Mar 1, 2002: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 340, RBL 12 TO LBL 12. THE CORRODED AREA OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-51, F - [SDR CALA0200114](https://openairdocs.org/sdr/CALA0200114), Mar 1, 2002: CARGO TRACK. CORRODED. INSPECTION FOUND FORWARD CARGO RT TIE DOWN RAIL CORRODED AT BS 500B-500D. A NEW SECTION OF TIE DOWN RAIL WAS SPLICED IN IAW SRM 53-00-53. - [SDR CALA0200113](https://openairdocs.org/sdr/CALA0200113), Feb 28, 2002: KEELBEAM. DAMAGED. INSPECTION FOUND LT WHEEL WELL WASHERS FRETTING INTO KEEL BEAM FROM STA 700-727. A REPAIR WAS INSTALLED IAW ECRA 5310-03740. - [SDR CALA0200111](https://openairdocs.org/sdr/CALA0200111), Feb 28, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AT STA 270-294.5, RBL 35. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND DRAWING # 69-40352. - [SDR CALA0200110](https://openairdocs.org/sdr/CALA0200110), Feb 27, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 986.5-1006, LBL 10-20. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0200109](https://openairdocs.org/sdr/CALA0200109), Feb 27, 2002: ANGLE. CORRODED. INSPECTION FOUND Z-ANGLE CORRODED AT L-2 DOOR, STA 940-993. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0200106](https://openairdocs.org/sdr/CALA0200106), Feb 27, 2002: SUPPORT. CORRODED. INSPECTION FOUND RT LAV WALL SUPPORT CORRODED AT STA 993.5, RBL 13-44. THE WALL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02. - [SDR CALA0200105](https://openairdocs.org/sdr/CALA0200105), Feb 27, 2002: WEB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN UPPER CHORD ON WEB BETWEEN STA 500D AND 520, BL 0. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0200104](https://openairdocs.org/sdr/CALA0200104), Feb 27, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 986.5-993.5, RBL 13-44. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0200103](https://openairdocs.org/sdr/CALA0200103), Feb 27, 2002: INTERCOSTAL. CORRODED. INSPECTION FOUND L/H LAV O/B WEB INTERCOSTAL CORRODED AT STA 1006-1016. THE INTERCOSTAL WAS REPLACED IAW SRM 53-10-02. - [SDR CALA0200101](https://openairdocs.org/sdr/CALA0200101), Feb 26, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 951.5, RBL 8-16. A NEW FLOOR SUPPORT WAS INSTALLED IAW ECRA 5310-03585. - [SDR CALA0200100](https://openairdocs.org/sdr/CALA0200100), Feb 26, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 947.5-967, RBL 17.5. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02. - [SDR CALA0200098](https://openairdocs.org/sdr/CALA0200098), Feb 25, 2002: WEB. CRACKED. INSPECTION FOUND A 2" CRACK IN SHEAR WEB UPON REMOVAL OF UPPER ANGLE AT STA 380-400, BL 0. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0200097](https://openairdocs.org/sdr/CALA0200097), Feb 25, 2002: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN UPPER CHORD ON FLOOR SUPPORT AT STA 380-400, BL 0. THE UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0200089](https://openairdocs.org/sdr/CALA0200089), Feb 22, 2002: WEB. CRACKED. INSPECTION FOUND A 1/4" CRACK IN WEB AT STA 277, S14R. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0000551](https://openairdocs.org/sdr/CALA0000551), Apr 25, 2000: SKIN. CRACKED. NR 1 PYLON CRACK IN CUT-OUT FOR PANEL 5724 (1). REPAIRED PER EC/RA 5430-01204. - [SDR CALA0000511](https://openairdocs.org/sdr/CALA0000511), Apr 23, 2000: SKIN. CRACKED. CRACK ON O/B SIDE OF ACCESS PANEL CUTOUT FOR PANEL 5727L NR 1 (1 INCH). STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER EC/RA 5430-01230. - [SDR CALA9802092](https://openairdocs.org/sdr/CALA9802092), Nov 23, 1998: CARD. MALFUNCTIONED. THE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. THE LIGHT EXTINGUISHED DURING CHECKLIST PROCEDURES. WHEN THE LANDING GEAR HANDLE - [SDR CAL960401](https://openairdocs.org/sdr/CAL960401), Mar 12, 1996: GEAR DOOR. CRACKED. HOU - INSPECTION FOUND A CRACK IN RADIUS INBOARD/AFT FLANGE OF LT MLG INNER DOOR. THE CRACK LENGTH WAS NOT IDENTIFIED. THE DOOR WAS REPAIRED IAW ECRA 5280-01076 - [SDR CAL960400](https://openairdocs.org/sdr/CAL960400), Mar 12, 1996: GEAR DOOR. CRACKED. HOU - INSPECTION FOUND A CRACK IN RADIUS TOP/AFT END FLANGE OF LT MLG CENTER DOOR. THE CRACK LENGTH WAS NOT IDENTIFIED. THE DOOR WAS REPAIRED IAW ECRA 5280-0107 - [SDR CAL960399](https://openairdocs.org/sdr/CAL960399), Mar 12, 1996: SUPPORT. CRACKED. HOU - INSPECTION FOUND TWO 1 INCH CRACKS IN FLOOR SUPPORT AT STA 380 - STA 400. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-30-51. (X) ## 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 19930730036799I](https://openairdocs.org/incident/19930730036799I), Jul 30, 1993: Boeing 7373T0 (N16339), Nantucket, MA. Aircraft landed short of runway. Four threshold lights were broken. NR1 and NR2 main tires cut. --- 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.