# N14324: 1986 Boeing 737-3TO, registration cancelled 2011-07-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 13, 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: 23375
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 17, 1986
- Certificate issued: February 17, 2011
- Last registry action: February 17, 2011
- Mode S code: A0B090
- 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/N14324
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14324
- Page: https://openairdocs.org/deregistered/N14324-2011-07-13

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 (115, newest 50)

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

- [SDR CALA2009100500585](https://openairdocs.org/sdr/CALA2009100500585), Oct 2, 2009: LOGIC CARD. MALFUNCTIONED. ON DESCENT WITH POWER AT IDLE, ONLY NOSE UNSAFE LIGHT ILLUMINATED. AFTER SELECTING GEAR DOWN NO INDICATION EITHER RED OR GREEN. RAN QHR CONSULTED WITH IAH MX. R
- [SDR CALA2009080400426](https://openairdocs.org/sdr/CALA2009080400426), Aug 4, 2009: LIGHT. INOPERATIVE. LEFT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REPLACED SOCKET ASSY, LAMP AND LENS ASSY. OPERATIONAL CHECKS GOOD.
- [SDR CALA2009012800064](https://openairdocs.org/sdr/CALA2009012800064), Jan 27, 2009: CHARGER. INOPERATIVE. FIRST CLASS EMERGENCY EXIT ROW AISLE LIGHTS INOPERATIVE. PERFORMED TROUBLESHOOTING PER MM 33-51-02, REPLACED FORWARD BATTERY PACK AND CHARGER, OPERATIONAL CHECK
- [SDR CALA0700513](https://openairdocs.org/sdr/CALA0700513), Sep 12, 2007: STRAP. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN STRAP ON RT SIDE OF FUSELAGE AT STA 1156, S13R BELOW HORIZONTAL STABILIZER. THE STRAP WAS REPAIRED IAW ECRA 5331-01344.
- [SDR CALA0700512](https://openairdocs.org/sdr/CALA0700512), Sep 12, 2007: SKIN. CRACKED. INSPECTION FOUND A 0.35 INCH CRACK AT LIGHTENING HOLE IN C-1 CARGO DOOR INTERIOR SKIN. A REPAIR WAS INSTALLED IAW ECRA 5232-01090.
- [SDR CALA0700507](https://openairdocs.org/sdr/CALA0700507), Sep 8, 2007: STRINGER. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16L AT STA 360. A STRINGER SPLICE WAS INSTALLED IAW ECRA 5311-01354.
- [SDR CALA0700506](https://openairdocs.org/sdr/CALA0700506), Sep 8, 2007: SHEAR TIE. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN SHEAR TIE AT STA 947 BELOW S25R. THE SHEAR TIE WAS REPAIRED IAW SRM 53-00-07.
- [SDR CALA0700504](https://openairdocs.org/sdr/CALA0700504), Sep 7, 2007: KEELBEAM. CORRODED. INSPECTION FOUND LEFT KEEL BEAM CORRODED JUST AFT OF STA 540 ON THE O/B FACE. THE CORRODED SECTION OF THE KEEL BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED 
- [SDR CALA0700503](https://openairdocs.org/sdr/CALA0700503), Sep 6, 2007: STRINGER. CORRODED. INSPECTION FOUND AFT CARGO STRINGER 26L CORRODED AT STA 727E + 11 INCHES. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A REPAIR WAS SPLICED IN IAW SRM 53-00
- [SDR CALA0700502](https://openairdocs.org/sdr/CALA0700502), Sep 6, 2007: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FRAME O/B OF LEFT KEEL BEAM AT STA 520, S27L TO S28L. THE CRACK WAS LOCATED AT THE SECOND FASTENER HOLE FROM THE BOTTOM.
- [SDR CALA0700487](https://openairdocs.org/sdr/CALA0700487), Sep 2, 2007: FRAME. CORRODED. INSPECTION FOUND FRAME CORRODED AT STA 807 BETWEEN S27L AND S27R, LBL 6 TO RBL 6. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 51-10-02.
- [SDR CALA0700485](https://openairdocs.org/sdr/CALA0700485), Sep 2, 2007: WEB. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN C-2 DOOR LOWER BEAM NR 5 WEB. THE CRACK WAS AT A FASTENER HOLE NEAR FORWARD STOP FITTING AND OUTER T-CHORD. THE WEB WAS REM
- [SDR CALA0700484](https://openairdocs.org/sdr/CALA0700484), Sep 2, 2007: STRUCTURE. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT FORWARD AND AFT CORNERS OF C-2 DOOR LOWER T-CHORD. THE T-CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700483](https://openairdocs.org/sdr/CALA0700483), Aug 31, 2007: FITTING. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FRAME TO STRINGER CLIP AT STA 847, S27L, LBL 3. A NEW CLIP WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0700482](https://openairdocs.org/sdr/CALA0700482), Aug 31, 2007: SHEAR TIE. CORRODED. INSPECTION FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT STA 767 BETWEEN STRINGER 26L AND 27L, LBL 5 TO LBL 15. THE SHEAR TIE WAS REPAIRED IAW SRM 53-00-07,
- [SDR CALA0700481](https://openairdocs.org/sdr/CALA0700481), Aug 31, 2007: SKIN. CRACKED. INSPECTION FOUND A 1/2 INCH CRACK IN C-2 DOOR OUTER SKIN AT DOOR HANDLE CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 52-00-01, REPAIR 2.
- [SDR CALA0700479](https://openairdocs.org/sdr/CALA0700479), Aug 30, 2007: FITTING. CORRODED. INSPECTION FOUND NR 2 ENGINE LT MIDSPAR ATTACH FITTING CORRODED. REPAIRED IAW ECRA 5410-01629.
- [SDR CALA0700478](https://openairdocs.org/sdr/CALA0700478), Aug 30, 2007: FITTING. CORRODED. INSPECTION FOUND NR 2 ENGINE RT MIDSPAR ATTACH FITTING CORRODED. REPAIRED IAW ECRA 5410-01629.
- [SDR CALA0700477](https://openairdocs.org/sdr/CALA0700477), Aug 30, 2007: SHEAR TIE. CORRODED. INSPECTION FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT STA 767 JUST I/B OF S27L, LBL 8. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 53-00-07.
- [SDR CALA0700476](https://openairdocs.org/sdr/CALA0700476), Aug 30, 2007: SKIN. CRACKED. INSPECTION FOUND A 1" CRACK IN SKIN JUST AFT OF STA 727E, S24L. A DOUBLER AND TRIPLER WERE INSTALLED IAW SRM 53-00-01, FIGURE 201, REPAIR 31.
- [SDR CALA0700474](https://openairdocs.org/sdr/CALA0700474), Aug 30, 2007: FRAME. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 500D ONE INCH ABOVE S13R. THE FRAME WAS REPAIRED IAW SRM 53-00-07.
- [SDR CALA0700473](https://openairdocs.org/sdr/CALA0700473), Aug 30, 2007: SKIN. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN C-1 CARGO DOOR SKIN AT HANDLE CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01.
- [SDR CALA0700472](https://openairdocs.org/sdr/CALA0700472), Aug 29, 2007: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK AROUND RIVET IN FRAME AT STA 887 ABOVE S9L STRINGER TIE. THE FRAME WAS REPAIRED IAW ECRA 5310-04650.
- [SDR CALA0700471](https://openairdocs.org/sdr/CALA0700471), Aug 29, 2007: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK AROUND RIVET IN FRAME AT STA 867 ABOVE S9L STRINGER TIE. THE FRAME WAS REPAIRED IAW ECRA 5310-04650.
- [SDR CALA0700470](https://openairdocs.org/sdr/CALA0700470), Aug 29, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 400 BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04650.
- [SDR CALA0700469](https://openairdocs.org/sdr/CALA0700469), Aug 29, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 380 BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04650.
- [SDR CALA0700468](https://openairdocs.org/sdr/CALA0700468), Aug 29, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK AROUND RIVET IN FRAME AT STA 827 ABOVE S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04650.
- [SDR CALA0700467](https://openairdocs.org/sdr/CALA0700467), Aug 29, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK AROUND RIVET IN FRAME AT STA 887 ABOVE S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04650.
- [SDR CALA0700466](https://openairdocs.org/sdr/CALA0700466), Aug 29, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK AROUND RIVET IN FRAME AT STA 827 ABOVE S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04650.
- [SDR CALA0700465](https://openairdocs.org/sdr/CALA0700465), Aug 29, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK AROUND RIVET IN FRAME AT STA 867 ABOVE S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04650.
- [SDR CALA0700464](https://openairdocs.org/sdr/CALA0700464), Aug 29, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK AROUND RIVET IN FRAME AT STA 807 ABOVE S9L. REPAIR PARTS WERE INSTALLED IAW ECRA 5310-04650.
- [SDR CALA0700463](https://openairdocs.org/sdr/CALA0700463), Aug 28, 2007: FRAME. CORRODED. INSPECTION FOUND FRAME CORRODED AT STA 947, S26R TO S27R. THE FRAME WAS REPAIRED IAW SRM 53-00-07.
- [SDR CALA0700461](https://openairdocs.org/sdr/CALA0700461), Aug 28, 2007: STRINGER. CORRODED. INSPECTION FOUND STRINGER 26R CORRODED AT STA 986.5. A STRINGER SPLICE WAS INSTALLED IAW SRM 53-00-03.
- [SDR CALA0700456](https://openairdocs.org/sdr/CALA0700456), Aug 25, 2007: PRESSURE PANEL. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN UPPER PRESSURE DECK IN MLG WHEEL WELL AT STA 664, RBL 38. REPAIRED IAW SRM 53-60-51, FIGURE 201.
- [SDR CALA0700455](https://openairdocs.org/sdr/CALA0700455), Aug 24, 2007: STRINGER. CORRODED. INSPECTION FOUND S27L CORRODED AT STA 957. THE STRINGER WAS REPAIRED IAW SRM 53-00-03.
- [SDR CALA0700454](https://openairdocs.org/sdr/CALA0700454), Aug 24, 2007: FITTING. CORRODED. INSPECTION FOUND SKIN CLIP CORRODED AT STA 986.5 BETWEEN S24R AND S25R. THE SKIN CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700453](https://openairdocs.org/sdr/CALA0700453), Aug 24, 2007: WEB. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN UPPER WEB FORWARD OF L-2 DOOR AT STA 947 AFT OF S11L. REPAIRED IAW SRM 51-10-02.
- [SDR CALA0700451](https://openairdocs.org/sdr/CALA0700451), Aug 22, 2007: STIFFENER. CORRODED. INSPECTION FOUND AFT PRESSURE BULKHEAD CHANNEL STIFFENER CORRODED ON LOWER END, BOTH SIDES, STA 1016 FRAME ASSEMBLY. THE CORRODED SECTION OF APB CHANNEL STIFFEN
- [SDR CALA0700450](https://openairdocs.org/sdr/CALA0700450), Aug 21, 2007: GUSSET. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF NOSE WHEEL WELL GUSSET AT AFT END OF NLG ACTUATOR SUPPORT FITTING, NWW STA 251, BL 0. THE GUSSET WAS REPLACED IAW 
- [SDR CALA0700449](https://openairdocs.org/sdr/CALA0700449), Aug 21, 2007: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN ANGLE AT STA 291 JUST BELOW S11R. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-00.
- [SDR CALA0700446](https://openairdocs.org/sdr/CALA0700446), Aug 20, 2007: FITTING. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN STRINGER TIE AT STA 727E, S3R. THE STRINGER TIE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0700444](https://openairdocs.org/sdr/CALA0700444), Aug 20, 2007: STRINGER. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16L AT STA 500C + 5. REPAIR PARTS WERE INSTALLED IAW SRM 53-00-03, FIGURE 201, REPAIR 1.
- [SDR CALA0600537](https://openairdocs.org/sdr/CALA0600537), Dec 9, 2006: OVEN. OVERHEATED. THE FORWARD GALLEY 103 OVEN WAS UNUSUALLY HOT AND HAD AN ELECTRICAL ODOR PRIOR TO STARTING IT. THE CIRCUIT BREAKER WAS PULLED. THE OVEN WAS REMOVED AND REPLACED
- [SDR CALA0600062](https://openairdocs.org/sdr/CALA0600062), Feb 14, 2006: FRAME. CORRODED. INSPECTION FOUND SURFACE CORROSION ON FRAME AT STA 794, S27R. A REPAIR WAS INSTALLED IAW SRM 53-00-07, FIGURE 201.
- [SDR CALA0600061](https://openairdocs.org/sdr/CALA0600061), Feb 13, 2006: CARGO TRACK. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN RT AFT CARGO TRACK BETWEEN STA 747-767, RBL 14. A NEW SECTION OF CARGO TRACK WAS SPLICED IN IAW SRM 53-00-53, FIGURE 201.
- [SDR CALA0600060](https://openairdocs.org/sdr/CALA0600060), Feb 13, 2006: CARGO TRACK. DAMAGED. INSPECTION FOUND THE LT CARGO TRACK CORRODED AT LOCK DOWN FITTING AND APPROXIMATELY TWO INCHES OF THE I/B FLANGE BROKEN OFF AT STA 789 LBL 17. A NEW SECTION OF 
- [SDR CALA0600059](https://openairdocs.org/sdr/CALA0600059), Feb 13, 2006: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT FORWARD UPPER CORNER OF NR 2 ENGINE PYLON O/B ACCESS PANEL. AN INTERIM REPAIR HAD BEEN INSTALLED PREVIOUSLY AND THE ITEM WAS
- [SDR CALA0600044](https://openairdocs.org/sdr/CALA0600044), Feb 9, 2006: STRUCTURE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN NR 2 PYLON I/B AFT HORSE COLLAR AT LOWER NUT PLATE. THE AFT HORSE COLLAR WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0600043](https://openairdocs.org/sdr/CALA0600043), Feb 9, 2006: SHEAR TIE. CORRODED. INSPECTION FOUND SKIN CLIP CORRODED AT STA 807, S28L. THE SKIN CLIP WAS REPLACED IAW SRM 51-10-02.
- [SDR CALA0500207](https://openairdocs.org/sdr/CALA0500207), Jul 1, 2005: LOCK ACTUATOR. MALFUNCTIONED. MLG EXTENDED INSTANTLY WHEN GEAR HANDLE WAS PLACED DOWN ON APPROACH. NLG EXTENDED AFTER MLG EXTENDED DOWN AND LOCKED. MAINTENANCE UNABLE TO DUPLICATE FAULT. NLG

All 115: https://openairdocs.org/deregistered/N14324-2011-07-13/reports.md

## FAA accident and incident reports (2)

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 19990102004469I](https://openairdocs.org/incident/19990102004469I), Jan 2, 1999: Boeing 7373T0 (N14324), Kansas City, MO. (-5) Aircraft N14324 flight #4992, was at cruise altitude in route from phx to ewr. #1 engine lost oil pressure and oil quantity. The crew shut down #1 engine…
- [Incident 19871225080979I](https://openairdocs.org/incident/19871225080979I), Dec 25, 1987: Boeing 7373TO (N14324), Portland, ME. Aircraft departed runway and became stuck in mud while taxiing to ramp.

## Other aircraft with N14324

- [Cancelled 1974-09-10](https://openairdocs.org/deregistered/N14324-1974-09-10): Piper PA-18-150, S/N 18-7409084. Exported to Brazil. Owner: [Aero Export International Inc](https://openairdocs.org/faa-owner/AERO%20EXPORT%20INTERNATIONAL%20INC), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale)
- [Cancelled 1950-02-20](https://openairdocs.org/deregistered/N14324-1950-02-20): Cunningham-Hall GA-36, S/N 211, built 1934. Owner: [Cunningham-Hall Aircraft Corp](https://openairdocs.org/faa-owner/CUNNINGHAM-HALL%20AIRCRAFT%20CORP), [Rochester, NY](https://openairdocs.org/faa-place/NY/Rochester)

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