# N14320: 1986 Boeing 737-3TO, registration cancelled 2011-06-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 3, 2011 - Exported to: Thailand - Status when cancelled: Valid registration - 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: 23371 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 30, 1986 - Certificate issued: March 29, 2011 - Last registry action: March 29, 2011 - Mode S code: A0B08C - Owner when cancelled: [As&L LLC](https://openairdocs.org/faa-owner/AS%26L%20LLC) - Location: [Los Angeles, CA](https://openairdocs.org/faa-place/CA/Los%20Angeles) - Owner type: Corporation - Owner's area on the map: 34.0353° N, 118.4265° W: Placed by OpenAirDocs at the center of ZIP code 90064, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N14320 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14320 - Page: https://openairdocs.org/deregistered/N14320-2011-06-03 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 (85, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0801011](https://openairdocs.org/sdr/CALA0801011), Oct 25, 2008: CABLE. FRAYED. ESCAPE SLIDE LATCH CABLE HAS BROKEN STRANDS ON (L-2) AFT ENTRY DOOR. INSTALLED NEW CABLE REF AMM 25-61-35. - [SDR CALA0801010](https://openairdocs.org/sdr/CALA0801010), Oct 25, 2008: CABLE. FRAYED. ESCAPE SLIDE LATCH CABLE HAS BROKEN STANDS ON (R-2) AFT SERVICE DOOR. INSTALLED NEW CABLE REF AMM 25-61-35. - [SDR CALA0700688](https://openairdocs.org/sdr/CALA0700688), Nov 13, 2007: SKIN. CORRODED. INSPECTION FOUND CORROSION ON BONDED DOUBLER AT STA 986.5 BELOW S27L. THE AREA WAS REPAIRED IAW ECRA 5311-01372. - [SDR CALA0700686](https://openairdocs.org/sdr/CALA0700686), Nov 12, 2007: ANGLE. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN ATTACHMENT ANGLE ON STRINGER 16L BETWEEN STA 348.2 AND 351.2. THE ATTACHMENT ANGLE WAS REPLACED IAW ECRA 5311-01375. - [SDR CALA0700684](https://openairdocs.org/sdr/CALA0700684), Nov 12, 2007: ANGLE. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN UPPER ANGLE AT S16L BETWEEN STA 348.2 AND 351.2. THE ANGLE WAS REPLACED IAW ECRA 5311-01375. - [SDR CALA0700685](https://openairdocs.org/sdr/CALA0700685), Nov 12, 2007: INTERCOSTAL. CRACKED. INSPECTION FOUND A 5 INCH CRACK AND MISSING FASTENER HEAD IN INTERCOSTAL WEB ON STRINGER 16L AT STA 348.2. THE INTERCOSTAL WEB WAS REPLACED IAW ECRA 5311-01375. - [SDR CALA0700683](https://openairdocs.org/sdr/CALA0700683), Nov 12, 2007: STRINGER CLIP. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN ATTACHMENT CLIP (BROKEN FASTENER HEADS TOO) ON STRINGER 15L AT STA 348.2. THE ATTACHMENT CLIP WAS REPLACED IAW ECRA 5311-013 - [SDR CALA0700682](https://openairdocs.org/sdr/CALA0700682), Nov 12, 2007: SKIN. CORRODED. INSPECTION FOUND SKIN CORRODED AT RIVET ROW, STA 967 BETWEEN STRINGERS 27R AND 27L. A REPAIR WAS INSTALLED IAW ECRA 5311-01377. - [SDR CALA0700676](https://openairdocs.org/sdr/CALA0700676), Nov 12, 2007: FRAME. CORRODED. INSPECTION FOUND FRAME AND SUPPORTS CORRODED AT STA 227.8, LBL 5.7 TO RBL 5.7, S28L. THE AREA WAS REPAIRED IAW ECRA 5311-01373. - [SDR CALA0700675](https://openairdocs.org/sdr/CALA0700675), Nov 12, 2007: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN NR 2 PYLON ACCESS PANEL 5824 CUTOUT ON UPPER FORWARD CORNER, NAC STA 258. THE CRACK WAS STOP DRILLED AND A PERMANENT REPAIR - [SDR CALA0700674](https://openairdocs.org/sdr/CALA0700674), Nov 11, 2007: FRAME. CORRODED. INSPECTION FOUND FRAME AND SUPPORT CORRODED AT STA 203.8, S28L TO S28R, RBL 5.7 TO LBL 5.7. THE FRAME CHORD AND SUPPORT WERE REMOVED AND REPLACED IAW SRM 51-40- - [SDR CALA0700673](https://openairdocs.org/sdr/CALA0700673), Nov 11, 2007: DOOR FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR FRAME AT FORWARD LOWER SEGMENT AT PULLEY BOLT HOLE. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0700672](https://openairdocs.org/sdr/CALA0700672), Nov 11, 2007: DOOR FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR UPPER FRAME AT SPLICE POINT. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0700671](https://openairdocs.org/sdr/CALA0700671), Nov 11, 2007: KEELBEAM. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN KEEL BEAM IN RIGHT A/C BAY AT STA 540. THE KEEL BEAM SECTION WAS REMOVED AND REPLACED IAW SRM 53-60-12, FIGURE 201, PAGE 201 - [SDR CALA0700667](https://openairdocs.org/sdr/CALA0700667), Nov 9, 2007: STRUCTURE. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LT HORIZONTAL STABILIZER UPPER O/B CHORD AT STAB STA 101.90. THE CRACKED AREA OF CHORD WAS REMOVED AND A REPAIR WAS INSTALLE - [SDR CALA0700650](https://openairdocs.org/sdr/CALA0700650), Nov 5, 2007: STRINGER. CORRODED. INSPECTION FOUND STRINGER 25L CORRODED AT STA 360. A REPAIR STRINGER SPLICE WAS INSTALLED IAW SRM 53-00-03, FIGURE 201. - [SDR CALA0700649](https://openairdocs.org/sdr/CALA0700649), Nov 5, 2007: INTERCOSTAL. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL ANGLE AT STA 290 BELOW S10R FORWARD OF R-1 DOOR. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51- - [SDR CALA0700648](https://openairdocs.org/sdr/CALA0700648), Nov 2, 2007: STRINGER. CORRODED. INSPECTION FOUND HEAVY CORROSION ON STRINGER 27L AT STA 986.5. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03. - [SDR CALA0700647](https://openairdocs.org/sdr/CALA0700647), Nov 2, 2007: FRAME. CORRODED. INSPECTION FOUND FRAME CORRODED AT STA 500D BETWEEN STRINGERS 26L AND 27L. THE FRAME WAS REPAIRED IAW SRM 53-00-07. - [SDR CALA0700646](https://openairdocs.org/sdr/CALA0700646), Nov 2, 2007: FRAME. CORRODED. INSPECTION FOUND FRAME CORRODED AT STA 500D, ABOVE S26L. THE FRAME WAS REPAIRED IAW SRM 53-00-07. - [SDR CALA0700645](https://openairdocs.org/sdr/CALA0700645), Nov 2, 2007: ATTACH FITTING. CORRODED. INSPECTION FOUND AFT CARGO COMPARTMENT STRINGER 26R ATTACH CLIP CORRODED AT STA 747. A NEW CLIP WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0700643](https://openairdocs.org/sdr/CALA0700643), Nov 2, 2007: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR CUTOUT AFT FRAME AT LOWER DOOR STOP FITTING, STA 847 BETWEEN STRINGER 23R AND 24R. THE CRACKED FRAME WAS REMO - [SDR CALA0700651](https://openairdocs.org/sdr/CALA0700651), Nov 1, 2007: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT STA 280, S14R FORWARD OF R-1 DOOR. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0700642](https://openairdocs.org/sdr/CALA0700642), Nov 1, 2007: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN CORRODED JUST FORWARD OF STA 500D ABOVE S27R. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201. - [SDR CALA0700631](https://openairdocs.org/sdr/CALA0700631), Nov 1, 2007: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN MAIN FRAME AT STA 616 JUST BELOW CABIN FLOOR, S17L. THE FRAME WAS REPAIRED IAW ECRA 5311-01158. - [SDR CALA0700629](https://openairdocs.org/sdr/CALA0700629), Oct 31, 2007: STRINGER SPLICE. CORRODED. INSPECTION FOUND STRINGER SPLICE 27L CORRODED AT STA 360. THE CHANNEL SPLICE WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND AMM 51-31-00. - [SDR CALA0700627](https://openairdocs.org/sdr/CALA0700627), Oct 29, 2007: MOUNT. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN NR 2 VHF ANTENNA MOUNTING BRACKET AT FORWARD CARGO BIN BETWEEN S28L AND S28R. THE MOUNTING BRACKET WAS REMOVED AND REPLACED I - [SDR CALA0700626](https://openairdocs.org/sdr/CALA0700626), Oct 29, 2007: STRINGER. CORRODED. INSPECTION FOUND STRINGER 25R CORRODED AT STA 340-360. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03, REPAIR 1, FIGURE 201, DETAIL VII. - [SDR CALA0700628](https://openairdocs.org/sdr/CALA0700628), Oct 29, 2007: RELEASE MECH. INOPERATIVE. THE FIRST OFFICER'S SLIDING WINDOW (R2) FAILED OPERATIONAL TEST FROM OUTSIDE THE CONTROL CABIN (WINDOW DID NOT UNLOCK AND OPEN WHEN THE EXTERNAL RELEASE HANDLE - [SDR CALA0700625](https://openairdocs.org/sdr/CALA0700625), Oct 27, 2007: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 767, S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04669. - [SDR CALA0700624](https://openairdocs.org/sdr/CALA0700624), Oct 27, 2007: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 867, S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04669. - [SDR CALA0700623](https://openairdocs.org/sdr/CALA0700623), Oct 27, 2007: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 480 BETWEEN S8L AND S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04669. - [SDR CALA0700622](https://openairdocs.org/sdr/CALA0700622), Oct 27, 2007: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 480 BETWEEN S8R AND S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04669. - [SDR CALA0700621](https://openairdocs.org/sdr/CALA0700621), Oct 26, 2007: FLOORBEAM. CORRODED. INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AT STA 328, RBL 11. THE FLOORBEAM SECTION WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0700608](https://openairdocs.org/sdr/CALA0700608), Oct 24, 2007: STRINGER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN STRINGER 16L JUST AFT OF STA 500C FORWARD OF WING SCANNING LIGHT HOUSING. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, PAGE 2 - [SDR CALA0700600](https://openairdocs.org/sdr/CALA0700600), Oct 21, 2007: ANGLE. CORRODED. INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 907-1016, LBL 45. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0700597](https://openairdocs.org/sdr/CALA0700597), Oct 21, 2007: FLOORBEAM. CORRODED. INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED ON UPPER AND LOWER SURFACES AT STA 360, BL 0. REPAIRED IAW SRM 53-30-51. - [SDR CALA0600226](https://openairdocs.org/sdr/CALA0600226), Jun 29, 2006: PIN. WORN. THE R-1 DOOR COULD BE CLOSED WITHOUT RELEASING THE HOLD OPEN CAM PLATE PIN. MAINTENANCE FOUND THE PIN WORN. THE DOOR RELEASE LEVER WAS REPLACED IAW MM 52-41-00. - [SDR CALA0600094](https://openairdocs.org/sdr/CALA0600094), Mar 22, 2006: FRAME. CORRODED. INSPECTION FOUND FRAME CORRODED IN AFT BAGGAGE BIN AT FLOOR SUPPORT WEB FUSELAGE ATTACH AREA, STA 927 BETWEEN S26L AND S26R. A SHEAR TIE WAS INSTALLED IAW SRM 5 - [SDR CALA0600093](https://openairdocs.org/sdr/CALA0600093), Mar 22, 2006: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN NR 1 PYLON SKIN AT UPPER FORWARD O/B PANEL, NAC STA 224. A DOUBLER WAS INSTALLED IAW ECRA 5430-01230. - [SDR CALA0500375](https://openairdocs.org/sdr/CALA0500375), Sep 22, 2005: SLIDE. TWISTED. R-1 DOOR EVACUATION SLIDE FAILED TO DEPLOY PROPERLY DURING DEPLOYMENT TEST. SLIDE INFLATED EARLY CAUSING SLIDE TO INFLATE BETWEEN DOOR & DOOR OPENING NOT ALLOWI - [SDR CALA0300675](https://openairdocs.org/sdr/CALA0300675), Nov 22, 2003: KEELBEAM. CORRODED. INSPECTION FOUND UPPER SURFACE OF O/B FLANGE OF LEFT KEELBEAM CORRODED AT STA 720. A REPAIR WAS INSTALLED IAW ECRA 5311-01177. - [SDR CALA0300657](https://openairdocs.org/sdr/CALA0300657), Nov 20, 2003: WEB. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN WEB AT NR 1 PYLON STRUT. REPAIRED IAW ECRA 5421-01002. - [SDR CALA0300656](https://openairdocs.org/sdr/CALA0300656), Nov 20, 2003: STRAP. CRACKED. INSPECTION FOUND A 6 INCH CRACK IN O/B STRAP ON NR 1 PYLON AT STA 363.5. INSTALLED SPLICE STRAPS IAW ECRA 5421-01002. - [SDR CALA0300655](https://openairdocs.org/sdr/CALA0300655), Nov 20, 2003: STRAP. CRACKED. INSPECTION FOUND A 6 INCH CRACK IN I/B STRAP ON NR 1 PYLON AT STA 363.5. REPAIRED IAW ECRA 5421-01002. - [SDR CALA0300648](https://openairdocs.org/sdr/CALA0300648), Nov 14, 2003: FITTING. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN NR 1 PYLON FORWARD FITTING AT LOWER I/B CORNER. THE NR 1 PYLON FORWARD FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND - [SDR CALA0300647](https://openairdocs.org/sdr/CALA0300647), Nov 14, 2003: STRAP. BROKEN. INSPECTION FOUND STRAP BROKEN ON BOTTOM OF BEAMS AT STA 312-328, RBL 42. THE STRAP WAS REPAIRED IAW SRM 53-10-51. - [SDR CALA0300643](https://openairdocs.org/sdr/CALA0300643), Nov 14, 2003: CHANNEL. CORRODED. INSPECTION FOUND HAT CHANNEL FOR ANTENNA CORRODED AT STA 727D +12, S27L. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0300642](https://openairdocs.org/sdr/CALA0300642), Nov 14, 2003: SKIN. GOUGED. INSPECTION FOUND FUSELAGE SKIN GOUGED AT STA 727D + 8, LBL 2. THE GOUGED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202. - [SDR CALA0300641](https://openairdocs.org/sdr/CALA0300641), Nov 13, 2003: SKIN. GOUGED. INSPECTION FOUND LOWER FUSELAGE SKIN GOUGED AT STA 314, S27L. A DOUBLER WAS INSTALLED IAW SRM 53-00-01. All 85: https://openairdocs.org/deregistered/N14320-2011-06-03/reports.md ## 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 19860718050989I](https://openairdocs.org/incident/19860718050989I), Jul 18, 1986: Boeing 737300 (N14320), Denver, CO. Control problem en route. Found flight attendant inadvertantly actuated rudder trim to full left position. ## Other aircraft with N14320 - [Registered now](https://openairdocs.org/aircraft/N14320): DJI AGRAS T30, S/N 3U5BJ5E001008B - [Cancelled 1970-09-02](https://openairdocs.org/deregistered/N14320-1970-09-02): Fairchild 24 C8C, S/N 2611. Owner: [Johnson Rudolph H](https://openairdocs.org/faa-owner/JOHNSON%20RUDOLPH%20H), [Cloquet, MN](https://openairdocs.org/faa-place/MN/Cloquet) --- 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.