# N10323: 1986 Boeing 737-3TO, registration cancelled 2011-04-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 28, 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: 23374
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 10, 1986
- Certificate issued: January 18, 2011
- Last registry action: January 18, 2011
- Mode S code: A01293
- 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/N10323
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=10323
- Page: https://openairdocs.org/deregistered/N10323-2011-04-28

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 (59, newest 50)

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

- [SDR CALA2009050700246](https://openairdocs.org/sdr/CALA2009050700246), May 7, 2009: DOWNLOCK SENSOR. FAILED. IN FLIGHT WITH THE LANDING GEAR UP, THE GREEN NOSE GEAR LIGHT WOULD FLASH INTERMITTENTLY. TROUBLESHOT PER M/M 32-61-00, FOUND NLG DOWN LOCK SENSOR RED TO YELLOW
- [SDR CALA2009021000091](https://openairdocs.org/sdr/CALA2009021000091), Feb 10, 2009: CHARGER. INOPERATIVE. DURING CHECK OF EMERGENCY LIGHTING, R1 DOOR EMERGENCY EXIT SIGN DID NOT ILLUMINATE. T/S PER WDM 33-51-31 PG 1. FOUND BATTERY CHARGER INOPERATIVE AT STATION 338R
- [SDR CALA0700294](https://openairdocs.org/sdr/CALA0700294), Jun 6, 2007: SKIN. CORRODED. INSPECTION FOUND SKIN AT TOP ATC ANTENNA MOUNTING SURFACE CORRODED, STA 420-440, S1L TO 2L. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201. A DIP WAS INITI
- [SDR CALA0700288](https://openairdocs.org/sdr/CALA0700288), Jun 3, 2007: KEELBEAM. CORRODED. INSPECTION FOUND RIGHT KEELBEAM CORRODED JUST INSIDE A/C BAY AT STA 537. THE KEELBEAM WAS REPAIRED IAW SRM 53-60-12.
- [SDR CALA0700278](https://openairdocs.org/sdr/CALA0700278), Jun 2, 2007: FRAME. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 887 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700287](https://openairdocs.org/sdr/CALA0700287), Jun 1, 2007: FRAME. CRACKED. INSPECTION FOUND A 5 INCH CRACK IN AFT CARGO DOOR CUTOUT FORWARD FRAME AT LOWER DOOR STOP AREA, STA 947.5, S16R-26R. THE FRAME WAS REPLACED IAW SRM 51-40-02 AND
- [SDR CALA0700286](https://openairdocs.org/sdr/CALA0700286), Jun 1, 2007: FRAME. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 480 BETWEEN STRINGER 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700285](https://openairdocs.org/sdr/CALA0700285), Jun 1, 2007: FRAME. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 847 BETWEEN STRINGER 8R AND 9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700284](https://openairdocs.org/sdr/CALA0700284), Jun 1, 2007: FRAME. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 867 BETWEEN STRINGER 8R AND 9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700283](https://openairdocs.org/sdr/CALA0700283), Jun 1, 2007: FRAME. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 827 BETWEEN STRINGER 8R AND 9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700282](https://openairdocs.org/sdr/CALA0700282), Jun 1, 2007: FRAME. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 887 BETWEEN STRINGER 8R AND 9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700281](https://openairdocs.org/sdr/CALA0700281), Jun 1, 2007: FRAME. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 807 BETWEEN STRINGER 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700280](https://openairdocs.org/sdr/CALA0700280), Jun 1, 2007: FRAME. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 747 BETWEEN STRINGER 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700279](https://openairdocs.org/sdr/CALA0700279), Jun 1, 2007: FRAME. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 827 BETWEEN STRINGER 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700277](https://openairdocs.org/sdr/CALA0700277), Jun 1, 2007: FRAME. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 867, S8L-9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700276](https://openairdocs.org/sdr/CALA0700276), Jun 1, 2007: SKIN. CORRODED. INSPECTION FOUND MOUNTING SKIN SURFACE FOR NR 2 COMM ANTENNA CORRODED AT STA 480-500B, S28L TO S28R. THE SKIN WAS REPAIRED IAW ECRA 5331-01316.
- [SDR CALA0700269](https://openairdocs.org/sdr/CALA0700269), May 27, 2007: FRAME. CORRODED. INSPECTION FOUND LOWER O/B CHORD CORRODED AT STA 227, RBL 0 TO LBL 3. REPAIRED IAW ECRA 5311-01324 ITEM 1-16, PAGE 1-3.
- [SDR CALA0700267](https://openairdocs.org/sdr/CALA0700267), May 26, 2007: DOOR FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN FORWARD CARGO DOOR CUTOUT AFT FRAME AT LOWER DOOR STOP FITTING, STA 480-500, S16R TO S28R. THE FRAME WAS REMOVED AND A NEW 
- [SDR CALA0700265](https://openairdocs.org/sdr/CALA0700265), May 25, 2007: SHEAR TIE. CORRODED. INSPECTION FOUND RIGHT NLG WW SHEAR TIE CORRODED AT STA 285. A REPAIR WAS INSTALLED IAW SRM 53-00-07.
- [SDR CALA0700262](https://openairdocs.org/sdr/CALA0700262), May 24, 2007: SHEAR TIE. CORRODED. INSPECTION FOUND RIGHT NLG WW CHORD SHEAR TIE CORRODED AT STA 275, S25R-S26R. A SHEAR TIE FILLER REPAIR WAS INSTALLED IAW SRM 53-00-07.
- [SDR CALA0700257](https://openairdocs.org/sdr/CALA0700257), May 22, 2007: FRAME. CORRODED. INSPECTION FOUND FRAME CORRODED AT STA 312, RBL 2, S27R-28R. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-00-07, FIGURE 201, REPAIR 1.
- [SDR CALA0700255](https://openairdocs.org/sdr/CALA0700255), May 22, 2007: FRAME. CORRODED. INSPECTION FOUND FRAME CORRODED AT STA 312, S28L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40-02 AND 53-00-07.
- [SDR CALA0700254](https://openairdocs.org/sdr/CALA0700254), May 21, 2007: STRINGER. CORRODED. INSPECTION FOUND STRINGER 28R CORRODED AT STA 325. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-20-01 AND 51-70-13.
- [SDR CALA0700253](https://openairdocs.org/sdr/CALA0700253), May 18, 2007: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LEFT MAIN FRAME AT STA 616, S17L, BELOW MAIN DECK FLOOR. THE FRAME WAS REPAIRED IAW ECRA 5311-01158.
- [SDR CALA0700248](https://openairdocs.org/sdr/CALA0700248), May 15, 2007: ANGLE. CORRODED. INSPECTION FOUND Z-ANGLE AT R-2 DOOR ENTRYWAY, STA 947.5-1000, S17R, CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700246](https://openairdocs.org/sdr/CALA0700246), May 15, 2007: ANGLE. CORRODED. INSPECTION FOUND Z-ANGLE AT L-2 DOOR, STA 907-1006, LBL 50 CORRODED. THE Z-ANGLE WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0700242](https://openairdocs.org/sdr/CALA0700242), May 13, 2007: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT FLOORBOARD MOUNT HOLES, STA 967, S17L TO S17R. REPAIRED FLOORBEAM IAW SRM 53-00-51, FIGURE 201, PAGE 201.
- [SDR CALA0700241](https://openairdocs.org/sdr/CALA0700241), May 13, 2007: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, RBL 43-54. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0700238](https://openairdocs.org/sdr/CALA0700238), May 9, 2007: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, RBL 32-34. A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51, FIGURE 201.
- [SDR CALA0700258](https://openairdocs.org/sdr/CALA0700258), May 8, 2007: SKIN. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AROUND L-2 DOOR LOWER HINGE CUTOUT. THE SKIN WAS REPAIRED IAW SRM 53-60-01.
- [SDR CALA0400436](https://openairdocs.org/sdr/CALA0400436), Apr 28, 2004: WIRE. SHORTED. EMERGENCY LIGHTS INOP AT SEAT ROWS 5-12. REPAIRED SHORTED WIRE UNDER SEAT ROW 5 PER STANDARD PRACTICES MANUAL.
- [SDR CALA0300283](https://openairdocs.org/sdr/CALA0300283), May 21, 2003: SKIN. CRACKED. INSPECTION FOUND THE AFT CARGO DOOR INNER SKIN CRACKED AT THE EDGE OF A LIGHTENING HOLE. THE DOOR SKIN WAS REPAIRED IAW ECRA 5232-01029.
- [SDR CALA0300263](https://openairdocs.org/sdr/CALA0300263), May 21, 2003: SKIN. CRACKED. INSPECTION FOUND A 1/2 INCH CRACK IN C-2 DOOR INNER SKIN AT ACCESS PANEL CUTOUT BELOW HANDLE. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5232-01029.
- [SDR CALA0300256](https://openairdocs.org/sdr/CALA0300256), May 19, 2003: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR INNER SKIN ABOVE HANDLE ON LIGHTENING HOLE. THE SKIN WAS REPAIRED IAW ECRA 5232-01015.
- [SDR CALA0300251](https://openairdocs.org/sdr/CALA0300251), May 15, 2003: CHANNEL. CORRODED. INSPECTION FOUND U-CHANNEL FOR DRAIN MAST CORRODED AT STA 986.5 BETWEEN S24L AND S25L. INSTALLED DRAIN MAST IAW MM 30-71-00, PAGE 501-503.
- [SDR CALA0300248](https://openairdocs.org/sdr/CALA0300248), May 14, 2003: STIFFENER. CORRODED. INSPECTION FOUND STIFFENER AFT OF STA 1016, BL 0 CORRODED ON BOTH RIGHT AND LEFT SIDES. LEFT AND RIGHT STIFFENERS AND SPLICES WERE INSTALLED IAW EA 5310-04045 A
- [SDR CALA0300247](https://openairdocs.org/sdr/CALA0300247), May 14, 2003: STRINGER. CORRODED. INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-01.
- [SDR CALA0300245](https://openairdocs.org/sdr/CALA0300245), May 12, 2003: ANGLE. CORRODED. INSPECTION FOUND L-2 DOOR ENTRYWAY Z-ANGLE CORRODED AT STA 943-987. A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-40-2.
- [SDR CALA0300241](https://openairdocs.org/sdr/CALA0300241), May 12, 2003: BULKHEAD. CORRODED. INSPECTION FOUND FORWARD FACE OF AFT PRESSURE BULKHEAD CORRODED JUST AFT OF FS 1016 AT LBL 6 TO RBL 6. REPAIRED APB IAW DRAWING 65C28106-1.
- [SDR CALA0300236](https://openairdocs.org/sdr/CALA0300236), May 9, 2003: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 992-1006, RBL 7. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0300160](https://openairdocs.org/sdr/CALA0300160), Mar 28, 2003: SKIN. DAMAGED. WHILE PERFORMING A PERMANENT REPAIR OF THE LT HORIZONTAL STABILIZER LE SKIN AT LE STA 69.93 IN IAH PER SRM 55-10-01, FIGURE 203, MAINTENANCE NOTED THE REQUIRED 
- [SDR CALA0100934](https://openairdocs.org/sdr/CALA0100934), Oct 5, 2001: SKIN. DENTED. INSPECTION FOUND L/H HORIZONTAL STABILIZER L/E SKIN DENTED AT STA 147.90. A REPAIR WAS INSTALLED IAW ECRA 5510-01602.
- [SDR CALA0100931](https://openairdocs.org/sdr/CALA0100931), Oct 4, 2001: SKIN. GOUGED. INSPECTION FOUND R/H RUDDER L/E SKIN GOUGED BELOW ACCESS PANEL 9559. REPAIRED IAW SRM 51-70-17 AND ECRA 5543-01017.
- [SDR CALA0100927](https://openairdocs.org/sdr/CALA0100927), Oct 3, 2001: SKIN. DENTED. INSPECTION FOUND THE L/H HORIZONTAL STABILIZER FIXED L/E SKIN DENTED AT SECOND RIB FROM I/B. A REPAIR WAS INSTALLED IAW SRM 55-10-01, PAGE 202.
- [SDR CALA0100924](https://openairdocs.org/sdr/CALA0100924), Oct 2, 2001: ANGLE. DENTED. INSPECTION FOUND APU DOOR ANGLE DENTED ON AFT EDGE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-13.
- [SDR CALA0100910](https://openairdocs.org/sdr/CALA0100910), Sep 30, 2001: WEB. CORRODED. INSPECTION FOUND WEB CORRODED AROUND FASTENERS AT LOWER SIDE OF C-2 DOOR UPPER THRESHOLD. A NEW WEB WAS INSTALLED IAW SRM 51-10-2.
- [SDR CALA0100907](https://openairdocs.org/sdr/CALA0100907), Sep 29, 2001: KEELBEAM. CORRODED. INSPECTION FOUND KEEL BEAM CORRODED ON LOWER SURFACE AT STA 705-727, LT SIDE. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5310-03740.
- [SDR CALA0100546](https://openairdocs.org/sdr/CALA0100546), Jun 15, 2001: BOLT. CRACKED. INSPECTION FOUND BOTH RT LANDING GEAR DOOR TO STABILIZER BEAM BOLTS PITTED AND ONE BOLT HAD A .25 INCH CRACK. NEW BOLTS, WASHERS, AND NUTS WERE INSTALLED IAW MM
- [SDR CALA0100545](https://openairdocs.org/sdr/CALA0100545), Jun 15, 2001: BOLT. CRACKED. INSPECTION FOUND BOTH LT LANDING GEAR DOOR TO STABILIZER BEAM BOLTS PITTED AND CRACKED. THE CRACKS WERE .25 INCH LONG. NEW BOLTS, WASHERS, AND NUTS WERE INSTALL
- [SDR CALA0100397](https://openairdocs.org/sdr/CALA0100397), Apr 18, 2001: WARN PANEL. FAULTY. THE CARGO FIRE LIGHT ILLUMINATED WHILE EN ROUTE FROM IAH TO YYZ. NO BELL SOUNDED. THE CARGO FIRE SYSTEM TESTED NORMALLY, BUT THE LIGHT REMAINED ON AFTER TEST. R

All 59: https://openairdocs.org/deregistered/N10323-2011-04-28/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 20080212847499I](https://openairdocs.org/incident/20080212847499I), Feb 12, 2008: Boeing 7373TO (N10323), Cleveland, OH, No damage. (-23) Aircraft was taxiing when braking and directional control was lost. Crew applied reverse thrust to bring aircraft to a stop. Use of reverse thrust caused…

## Other aircraft with N10323

- [Cancelled 1981-08-21](https://openairdocs.org/deregistered/N10323-1981-08-21): Mooney M20J, S/N 24-1117, built 1981. Exported to Canada. Owner: [Business Aviation Inc](https://openairdocs.org/faa-owner/BUSINESS%20AVIATION%20INC), [Sioux Falls, SD](https://openairdocs.org/faa-place/SD/Sioux%20Falls)
- [Cancelled 1933-08-08](https://openairdocs.org/deregistered/N10323-1933-08-08): Aeronca C-2, S/N A-89. Owner: [Fifer Edward](https://openairdocs.org/faa-owner/FIFER%20EDWARD), [Elkhart, IN](https://openairdocs.org/faa-place/IN/Elkhart)

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