# N355US: 1987 Boeing 737-301, registration cancelled 2006-08-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 9, 2006
- Exported to: Mexico
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-301](https://openairdocs.org/model/boeing-737-301) (registry code 138447R)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 23558
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 30, 1987
- Certificate issued: April 21, 2006
- Last registry action: April 21, 2006
- Mode S code: A3F933
- Owner when cancelled: [Afs Investments 73 LLC](https://openairdocs.org/faa-owner/AFS%20INVESTMENTS%2073%20LLC)
- Location: [Stamford, CT](https://openairdocs.org/faa-place/CT/Stamford)
- Owner type: Corporation
- Owner's area on the map: 41.0534° N, 73.5387° W: Placed by OpenAirDocs: center of Stamford, CT, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N355US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=355US
- Page: https://openairdocs.org/deregistered/N355US-2006-08-09

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 737-301: https://openairdocs.org/model/boeing-737-301.md

## Service difficulty reports (53, newest 50)

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

- [SDR SB05176](https://openairdocs.org/sdr/SB05176), Dec 25, 2005: CHARGER. FAULTY. TPA - THE SEAT MOUNTED EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE AFT LEFT BATTERY CHARGER ASSEMBLY. EMERGENCY LIGHTS CHECK OK.
- [SDR SB05147](https://openairdocs.org/sdr/SB05147), Nov 16, 2005: FUSE. BLOWN. MAINTENANCE REPORTED THE AFT LEFT EXTERIOR EMERGENCY LIGHT AND THE SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 22 AND 23 INOPERATIVE. MAINTENANCE RELAMPED THE EXTERIO
- [SDR USAA040340](https://openairdocs.org/sdr/USAA040340), Jul 8, 2004: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .125 INCH, STATION 480, S8L-S9L. INSTALLED REPAIR ANGLES PER TYPICAL REPAIR 53-10-20A. (M)
- [SDR USAA040288](https://openairdocs.org/sdr/USAA040288), Jun 11, 2004: BEAM. CRACKED. PIT - FOUND BEAM CRACKED 2 INCHES, 3 INCHES FROM LOWER END OF VERT STAB LT T/E BEAM. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-30-13 FIG 1. (M)
- [SDR USAA040287](https://openairdocs.org/sdr/USAA040287), Jun 10, 2004: FLOORBEAM. CORRODED. PIT - FOUND BEAM CORRODED THREE 1 INCH DIAMETER AREAS, BS 947 LBL 30 TO LBL 46. REMOVED CORROSION, TREATED AND PRIMED, PERFORMED TYP REPAIR 53-15-01B, SRM 51-10
- [SDR USAA040348](https://openairdocs.org/sdr/USAA040348), Mar 27, 2004: STRINGER. CORRODED. FOUND STRINGER CORRODED TWO AREAS, 1 INCH BY 6 INCHES AND 1 INCH BY 4 INCHES, FS 1016-1022 FORWARD SIDE OF AFT PRESSURE BULKHEAD. REPLACED STIFFENERS AND INSTAL
- [SDR USAASB04024](https://openairdocs.org/sdr/USAASB04024), Mar 2, 2004: ARM. FRACTURED. CLT - FLT 240 - UPON GEAR RETRACTION, CREW HEARD A LOUD THUMP. THE LEFT MAIN GEAR INDICATED RED. CREW DECLARED AN EMERGENCY. THE FLIGHT RETURNED TO CLT AND LAND
- [SDR USA2004F00019](https://openairdocs.org/sdr/USA2004F00019), Mar 2, 2004: ARM. CRACKED. UPON GEAR RETRACTION, CREW HEARD A LOUD THRUMP. THE LEFT MAIN GEAR INDICATED RED. CREW DECLARED AN EMERGENCY. THE FLIGHT RETURNED AND LANDED WITHOUT FURTHER INC
- [SDR USAA040049](https://openairdocs.org/sdr/USAA040049), Feb 12, 2004: SKIN. CRACKED. FOUND SKIN CRACKED 2 INCHES, 727D AND S23R. INSTALLED DOUBLER PER SRM 53-00-01. (M)
- [SDR USAASB03211](https://openairdocs.org/sdr/USAASB03211), Dec 5, 2003: SERVO. FAILED. DURING FLIGHT, EN ROUTE, THE STABILIZER OUT OF TRIM LIGHT ILLUMINATED. THE AUTOPILOT WOULD NOT TRIM. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTE
- [SDR USAA030029](https://openairdocs.org/sdr/USAA030029), Mar 21, 2003: SUPPORT FITTING. WORN. PIT - FOUND TERMINAL SUPPORT FITTING HAS TWO WORN BOLTS, VERTICAL STABILIZER AFT TERMINAL SUPPORT FITTING BOLT HOLES. REWORKED WORN HOLES PER EA 94263A, THIS IS
- [SDR USAA020390](https://openairdocs.org/sdr/USAA020390), Oct 4, 2002: STIFFENER. CRACKED. IT - FOUND STIFFENER ANGLE CRACKED 1 INCH LONG, VERTICAL STIFFENER MLG W/W FORWARD BULKHEAD CENTER LINE STATION 663. FABRICATED AND INSTALLED 2 REPAIR STRAPS AN
- [SDR USAASB01224](https://openairdocs.org/sdr/USAASB01224), Aug 7, 2001: OUTFLOW VALVE. FAILED. PIT - FLT 1146 - EN ROUTE FROM PHL TO CMH, AT FL350, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW NOTICED CABIN ALTITUDE AT 11,000 FEET. CREW WAS UNABLE TO CON
- [SDR USAA010022](https://openairdocs.org/sdr/USAA010022), Jan 15, 2001: SKIN. CRACKED. CLT - FOUND SKIN CRACKED, STATION 200, LBL 5. INSTALLED EXTERIOR DOUBLER PER EA 68798. (M)
- [SDR USAA002204](https://openairdocs.org/sdr/USAA002204), Dec 27, 2000: BULKHEAD. CRACKED. CLT - FOUND WEB CRACKED 1 INCH, STATION 178, WL 198, LBL 4. INSTALLED DOUBLER PER EA 68679. (M)
- [SDR USAA002197](https://openairdocs.org/sdr/USAA002197), Dec 26, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCH, STATION 727B STRINGER 14R. INSTALLED ANGLE PER SRM 53-00-07. (M)
- [SDR USAA002198](https://openairdocs.org/sdr/USAA002198), Dec 26, 2000: FRAME. CRACKED. CLT - FOUND CHORD CRACKED 1.5 INCH, BS 178, WL 207, RBL 29. REMOVED SECTION AND INSTALLED NEW SECTION PER EA 68680 AND EO 5300V157. (M)
- [SDR USAA002199](https://openairdocs.org/sdr/USAA002199), Dec 26, 2000: INTERCOSTAL. CRACKED. CLT - FOUND INTERCOSTAL CRACKED 1 INCH BY 1 INCH, BS 178, WL 195, LBL 24. INSTALLED NEW INTERCOSTAL PER SRM 51-10-02. (M)
- [SDR USAA002200](https://openairdocs.org/sdr/USAA002200), Dec 26, 2000: INTERCOSTAL. CRACKED. CLT - FOUND INTERCOSTAL CRACKED .750 INCH BY 1 INCH, BS 178, WL 195, RBL 24. INSTALLED NEW INTERCOSTAL PER SRM 51-10-02 AND EO5300V157. (M)
- [SDR USAA002194](https://openairdocs.org/sdr/USAA002194), Dec 22, 2000: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM CRACKED 1 INCH BY 1 INCH, STATION 344, LBL 9. CORROSION LEVEL 1. REMOVED T-CAP AND FABRICATED NEW T-CAP AND SPLICE PER SRM 53-10-51 AND 53
- [SDR USAA002184](https://openairdocs.org/sdr/USAA002184), Dec 21, 2000: DOUBLER. CRACKED. CLT - FOUND ANTENNA DOUBLER CRACKED .5 INCH, STATION 727D-727E, BL 0. INSTALLED NEW DOUBLER PER SRM 51-10-02. (M)
- [SDR USAA002175](https://openairdocs.org/sdr/USAA002175), Dec 20, 2000: FLOORBEAM. CORRODED. CLT - FOUND T-CAP CORRODED 1 INCH, STATION 328 FLOORBEAM AT RBL 14, 21, 35. CORROSION LEVEL 1 C53-107-01. INSTALLED NEW T-CAP AND FABRICATED SPLICE ANGLES PER S
- [SDR USAA002176](https://openairdocs.org/sdr/USAA002176), Dec 20, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED 1 INCH, STATION 344, STRINGER 10R. FABRICATED NEW CLIP PER SRM 53-10-15 AND SRM 51-10-2. (M)
- [SDR USAA002177](https://openairdocs.org/sdr/USAA002177), Dec 20, 2000: SHEAR TIE. CRACKED. CLT - FOUND TIE ANGLE CRACKED .333 INCH, FRAME 360 BETWEEN STRINGER 14R AND STRINGER 15R. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-07 FIG 207. (M)
- [SDR USAA002178](https://openairdocs.org/sdr/USAA002178), Dec 20, 2000: INTERCOSTAL. CRACKED. CLT - FOUND INTERCOSTAL CRACKED .25 INCH, INTERCOSTAL AT FS 294.5, STRINGER 7L. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER PER SRM 51-70-11. (M)
- [SDR USAA002163](https://openairdocs.org/sdr/USAA002163), Dec 18, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED .5 INCH, STATION 312 BL 0. CORROSION LEVEL 2 C53-107-02. REPLACED T-CAP PER SRM 53-00-51. (M)
- [SDR USAA002160](https://openairdocs.org/sdr/USAA002160), Dec 18, 2000: ATTACH ANGLE. CRACKED. CLT - FOUND ATTACH ANGLE CRACKED .5 INCH, FORWARD OF FS 303.9 ABOVE STRINGER 10L. INSTALLED NEW ATTACH ANGLE PER SRM 51-10-02. (M)
- [SDR USAA002161](https://openairdocs.org/sdr/USAA002161), Dec 18, 2000: ATTACH ANGLE. CRACKED. CLT - FOUND FRAME ATTACH ANGLE CRACKED .25 INCH, FRAME ATTACH ANGLE AT FS 348.2 STRINGER 11L. FABRICATED NEW ATTACH ANGLE PER SRM 51-10-2. (M)
- [SDR USAA002162](https://openairdocs.org/sdr/USAA002162), Dec 18, 2000: SHEAR TIE. CRACKED. CLT - FOUND FRAME SHEAR TIE CRACKED .5 INCH, STATION 967, BETWEEN STRINGER 6L AND 7L. REMOVED AND INSTALLED DOUBLER PER EA 68751. (M)
- [SDR USAA002158](https://openairdocs.org/sdr/USAA002158), Dec 15, 2000: FLOORBEAM. CORRODED. CLT - FOUND SPLICE ANGLE T-CAP CORRODED, STATION 344, RBL 9, LBL 37. REPLACED T-CAP PER SRM 53-10-51. (M)
- [SDR USAA002156](https://openairdocs.org/sdr/USAA002156), Dec 15, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, FRAME STATION 887 STRINGER 9R. REPAIRED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA002157](https://openairdocs.org/sdr/USAA002157), Dec 15, 2000: ANGLE. CRACKED. CLT - FOUND CORNER ANGLE CRACKED .75 INCH, DOOR CUTOUT LOWER AFT CORNER ANGLE. INSTALLED NEW CORNER ANGLE. (M)
- [SDR USAA002148](https://openairdocs.org/sdr/USAA002148), Dec 14, 2000: STRINGER CLIP. CRACKED. CLT - FOUND STRINGER CLIP CRACKED 1 INCH, STATION 807, STRINGER 4L. REPLACED CLIP PER SRM 51-10-02. (M)
- [SDR USAA002149](https://openairdocs.org/sdr/USAA002149), Dec 14, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, FS 847, STRINGER 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA002150](https://openairdocs.org/sdr/USAA002150), Dec 14, 2000: FRAME. CRACKED. CLT - FOUND FUSELAGE FRAME CRACKED .5 INCH, STATION 827 ABOVE STRINGER 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA002151](https://openairdocs.org/sdr/USAA002151), Dec 14, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, FRAME 400 ABOVE STRINGER 9R. REPAIRED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA002152](https://openairdocs.org/sdr/USAA002152), Dec 14, 2000: STRINGER CLIP. CRACKED. CLT - FOUND STRINGER CLIP CRACKED .5 INCH, STATION 639, STRINGER 2L CLIP. REPLACED PART PER SRM 51-10-2 AND 51-40-2. (M)
- [SDR USAA002092](https://openairdocs.org/sdr/USAA002092), Dec 11, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .50 INCH, STATION 616 STRINGER 2R. INSTALLED TIE CLIP PER SRM 51-10-02 AND SRM 51-40-03. (M)
- [SDR USAA002093](https://openairdocs.org/sdr/USAA002093), Dec 11, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .125 INCH, STATION 727E, STRINGER 7R. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA002077](https://openairdocs.org/sdr/USAA002077), Dec 7, 2000: WEB. CRACKED. CLT - FOUND WEB PLATE CRACKED 2 INCHES, STATION 639 STRINGER 17R. REPAIRED PER SRM 51-10-2. (M)
- [SDR USAA002078](https://openairdocs.org/sdr/USAA002078), Dec 7, 2000: CREASE BEAM. CRACKED. CLT - FOUND CREASE BEAM CRACKED 1 INCH, BS 639 BETWEEN STATION 619-639 STRINGER 17L REPAIRED PER SRM 51-10-2. (M)
- [SDR USAASB00055](https://openairdocs.org/sdr/USAASB00055), Feb 28, 2000: ACTUATOR. FAILED. PHL - FLT 1063 - EN ROUTE FROM RIC TO BOS, THE STABILIZER ELECTRIC TRIM HAD FAILED. FLIGHT DIVERTED TO PHL AND LANDED WITHOUT FURTEHR INCDIENT. NO EMEGENCY WAS 
- [SDR USAASB00039](https://openairdocs.org/sdr/USAASB00039), Feb 12, 2000: BATTERY PACK. DISCHARGED. CLT - MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHTING INOPERATIVE AT ROW 12 ABC THROUGH ROW 16 ABC AND AT ROW 21 AND 22 ABC. ALSO, FOUND THE RIGHT AFT SERVI
- [SDR USAASB00014](https://openairdocs.org/sdr/USAASB00014), Jan 21, 2000: CONTROLLER. FAILED. PIT - FLT 723 - ON CLIMB-OUT FROM PIT, THE AUTO FAIL PRESSURIZATION LIGHT ILLUMINATED. CREW ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES BUT WAS UNABLE TO PRESSUR
- [SDR USAASB99301](https://openairdocs.org/sdr/USAASB99301), Dec 23, 1999: UNKNOWN. ODOR. MCO - FLT 2152 - 20 MINUTES AFTER T/O FROM RSW, UNIDENTIFIED FUMES WERE RECOGNIZED IN THE AFT GALLEY. CREW TURNED OFF GALLEY POWER SWITCH AND PULLED ALL CIRCUIT
- [SDR USAASB99293](https://openairdocs.org/sdr/USAASB99293), Dec 14, 1999: ENGINE. VIBRATION. CLT - FLT 8052 - ON CLIMB-OUT FROM CLT, THE NR1 ENGINE VIBRATION MONITOR INDICATED 2 UNITS ACCELERATING THROUGH 210 KNOTS. FLIGHT RETURNED TO FIELD AT CLT AND L
- [SDR USAASB99261](https://openairdocs.org/sdr/USAASB99261), Oct 29, 1999: COFFEEMAKER. MALFUNCTIONED. IAD - FLT 488 - EN ROUTE FROM PIT-BWI, F/A REPORTED SMELL OF BURNING WIRES AND FUMES IN THE AFT CABIN. NO VISIBLE SMOKE WAS NOTED. AN EMERGENCY WAS DECLARED AND
- [SDR USAASB98095](https://openairdocs.org/sdr/USAASB98095), Apr 15, 1998: INDICATOR. FAILED. RDU - FL 1494 - ON APPROACH TO RDU, CREW EXTENDED FLAPS FROM 25 TO 30 DEGREES AND RECEIVED A FLAP ASSYMETRY. CREW PLACED FLAPS BACK TO 25 DEGREES, ADVISED THE T
- [SDR USAASB97064](https://openairdocs.org/sdr/USAASB97064), Mar 2, 1997: WIRE. LOOSE. BWI - MAINTENANCE REPORTED THE LEFT AFT EXTERIOR EMERGENCY ESCAPE LIGHT WAS INOP. MAINTENANCE INSTALLED NEW WIRE FROM M1197 BATTERY PACK D3122 PIN 9 TO L732 ESC
- [SDR USAASB97062](https://openairdocs.org/sdr/USAASB97062), Feb 28, 1997: WIRE. BROKEN. BDL - AFT GALLEY OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. REPLACED WIRE BETWEEN POWER SUPPLY AND LIGHT ASSEMBLY CONNECTORS D3122 AND D3170. (M)

All 53: https://openairdocs.org/deregistered/N355US-2006-08-09/reports.md

## FAA accident and incident reports (3)

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 20020323009979I](https://openairdocs.org/incident/20020323009979I), Mar 23, 2002: Boeing 737301 (N355US), Kansas City, MO. (-23) On March 23, 2002 us airways flight 386 a B737 aborted takeoff due to an APU caution light. Aircraft returned to the terminal. Log entry indicated at…
- [Incident 19900311013479I](https://openairdocs.org/incident/19900311013479I), Mar 11, 1990: Boeing 737301 (N355US), Baltimore, MD. Electrical failure due to relay failure. On landing air cycle machine overheated and smoked. Evacuated aircraft.
- [Incident 19900310003649I](https://openairdocs.org/incident/19900310003649I), Mar 10, 1990: Boeing 737301 (N355US), Baltimore, MD. Partial electrical failure en route. Relay failure. On landing air cycle machine overheated and smoked. Evacuted.

## Other aircraft with N355US

- [Registered now](https://openairdocs.org/aircraft/N355US): Costruzioni Aeronautiche Tecna P2006T, S/N 355/US, built 2022
- [Cancelled 1971-03-04](https://openairdocs.org/deregistered/N355US-1971-03-04): Boeing 707-351B, S/N 18710. Exported to China. Owner: [Northwest Airlines Inc](https://openairdocs.org/faa-owner/NORTHWEST%20AIRLINES%20INC), [St Paul, MN](https://openairdocs.org/faa-place/MN/St%20Paul)

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