# N352US: 1987 Boeing 737-301, registration cancelled 2006-09-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 6, 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: 23555
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 14, 1987
- Certificate issued: April 21, 2006
- Last registry action: April 21, 2006
- Mode S code: A3EE0E
- 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/N352US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=352US
- Page: https://openairdocs.org/deregistered/N352US-2006-09-06

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 (78, newest 50)

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

- [SDR SB05131](https://openairdocs.org/sdr/SB05131), Oct 13, 2005: POWER SUPPLY. INOPERATIVE. MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 12 THROUGH 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL
- [SDR SB05123](https://openairdocs.org/sdr/SB05123), Sep 26, 2005: BATTERY PACK. DISCHARGED. PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT ABOVE THE L2 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK PER MM 33-51-51. OPERATIONA
- [SDR SB05112](https://openairdocs.org/sdr/SB05112), Sep 9, 2005: OUTFLOW VALVE. LEAKING. AIRCRAFT WOULD NOT MAINTAIN CABIN PRESSURIZATION. AT FL030, CABIN ALTITUDE CLIMBED 1,200 FEET PER MINUTE WITH OUTFLOW VALVE FULLY CLOSED. CREW DESCENDED BELOW F
- [SDR USAA040844](https://openairdocs.org/sdr/USAA040844), Nov 12, 2004: SKIN. CRACKED. FWD SERVICE DOOR SKIN, .1875 INCH CRACK, UPPER HINGE CUTOUT, LWR RADIUS TO DRAIN HOLE. INSTALLED DOUBLER IAW TYP REP 52-10-13.
- [SDR USAA041040](https://openairdocs.org/sdr/USAA041040), Nov 11, 2004: SKIN. GOUGED. PIT - Q4 - LOWER SKIN SURFACE, SINGLE LAYER COMPOSITE DAMAGE .75 INCH GOUGE, RT ELEVATOR AT 84.5 AND 4 - 5 INCH IN FROM FWD SPAR. PREPARED DAMAGED AREA, APPLIED
- [SDR USAA041039](https://openairdocs.org/sdr/USAA041039), Nov 11, 2004: SKIN. GOUGED. PIT - Q4 -LOWER SKIN SURFACE, SINGLER LAYER COMPOSITE DAMAGE .50 INCH GOUGE. RT ELEVATOR AT STA 62 AND 15 INCHES FROM FWD SPAR. PREPARED DAMAGED AREA, APPLIED W
- [SDR USAA041038](https://openairdocs.org/sdr/USAA041038), Nov 11, 2004: SKIN. GOUGED. PIT - Q4 - LOWER SKIN SURFACE, SINGLE LAYER COMPOSITE DAMAGE .50 INCH GOUGE, RT ELEVATOR AT STA 71 AND 10 INCHES FROM FWD SPAR. PREPARED DAMAGED AREA, APPLIED W
- [SDR USAA041037](https://openairdocs.org/sdr/USAA041037), Nov 11, 2004: SKIN. DAMAGED. PIT - Q4 - LOWER SKIN SURFACE, SINGLE LAYER COMPOSITE, 2 GOUGES 1.25 INCHES, COMPOSITE DAMAGE, 2 GOUGES, RT ELEVATOR AT STA 70 AND 8 TO 9 INCHES FROM FWD SPAR. 
- [SDR USAA041036](https://openairdocs.org/sdr/USAA041036), Nov 11, 2004: SKIN. DAMAGED. PIT - Q4 - LOWER SKIN SURFACE, COMPOSITE DAMAGE, .3750 INCH GOUGE, COMPOSITE DAMAGE - SINGLE LAYER, RT ELEVATOR AT STA 64 + 7 INCH FROM FWD SPAR. REPAIRED DAMAG
- [SDR USAA041035](https://openairdocs.org/sdr/USAA041035), Nov 11, 2004: SKIN. DAMAGED. PIT - Q4 - LOWER SKIN, COMPOSIT DAMAGE .3750 INCH GOUGING. COMPOSITE DAMAGE - SINGLE LAYER RT ELEVATOR AT STA 68 + 6 INCHES FROM FWD SPAR LOWER SKIN. PREPARED D
- [SDR USAA041034](https://openairdocs.org/sdr/USAA041034), Nov 11, 2004: SKIN. DELAMINATED. PIT - Q4 - LOWER SKIN SURFACE, 2 INCH SQ DELAMINATION, RT LELVATOR 41 INCH FROM IB END AND 13 INCH AFT OF L/E. REMOVED DAMAGED SKIN AND CORE, INSTALLED SER COR,
- [SDR USAA040973](https://openairdocs.org/sdr/USAA040973), Nov 11, 2004: FITTING. CRACKED. PIT- Q4 - MLG SUPPORT BEAM AFT FITTING, .0625 INCH CRACK (2) HOLES ON MLG SUPPORT AFT BEAM FITTING, 12 O`CLOCK AND 9 O`CLOCK. REPLACED LT MGL SUPPORT BEAM AFT F
- [SDR USAA040972](https://openairdocs.org/sdr/USAA040972), Nov 11, 2004: SPAR. CRACKED. PIT - Q4 - LT SPAR UPPER CHORD, .0625 INCH CRACK; NR 2 HOLE VERTICAL LEG OF LT SPAR UPPER CHORD AT MLG SUPPORT. INSTALLED FATIGUE ENHANCEMENT PLATE IAW EA 79286
- [SDR USAA040971](https://openairdocs.org/sdr/USAA040971), Nov 11, 2004: DOUBLER. CRACKED. PIT - Q4 - DOUBLER, .25 INCH LONG CRACKS (2 EA), RT WING FUEL PANEL REBATE PANEL NR 8817R. INSTALLED EXT DOUBLER .125 THICK IAW EA 79453.
- [SDR USAA040875](https://openairdocs.org/sdr/USAA040875), Nov 11, 2004: FLANGE. CRACKED. FUEL PLATE FLANGE, (2 EA) .189 INCH IN LENGTH, CRACK (2) FUEL PANEL NR 881, 17R, 6 O`CLOCK AND 12 O`CLOCK POSITIONS. STOP DRILLED CRACKS, TRIMMED SKIN PANEL, IN
- [SDR USAA040874](https://openairdocs.org/sdr/USAA040874), Nov 3, 2004: STIFFENER. CRACKED. STIFFENER, .1250 INCH CRACK, LBL 5.7 IB AND OB SIDE 8 INCH IN FROM BOTTOM. STRAPS, ANGLES AND FILLERS INSTALLED ON BOTH SIDES OF VERT CORD IAW EO 5300V155 AND E
- [SDR USAA040856](https://openairdocs.org/sdr/USAA040856), Oct 30, 2004: FRAME. CRACKED. PIT - Q4 - FRAME, .2500 INCH CRACK. CRACK EMANATING FROM FASTENER, FRAME STA 867 AND STR 9L. INSTALLED DOUBLERS IAW TYP REP 53-10-20A.
- [SDR USAA040855](https://openairdocs.org/sdr/USAA040855), Oct 30, 2004: FRAME. CRACKED. PIT - Q4 - FRAME, .1250 INCH CRACK, STA 787 AND STR 9L. INSTALLED DOUBLERS IAE TYP REP 53-10-20A.
- [SDR USAA040854](https://openairdocs.org/sdr/USAA040854), Oct 30, 2004: FRAME. CRACKED. FRAME, .3750 INCH CRACK, STA 540 BETWEEN RT IB SEAT TRACK, RBL 24.75 AND CRT FLOOR SUPPORT BEAM BL 0. DEFECTIVE PART, REPLACED WITH IDENT PN IAW MFG DWG 65-4681
- [SDR USAA040857](https://openairdocs.org/sdr/USAA040857), Oct 30, 2004: FRAME. CRACKED. PIT - Q4, FRAME, .1250 INCH CRACK, EMANATING FROM FASTENER, FRAME STA 847, STR 9L. INSTALLED DOUBLERS IAW TYPE REP 53-10-20A.
- [SDR USAA040862](https://openairdocs.org/sdr/USAA040862), Oct 28, 2004: ANGLE. WORN. ANGLE, 4, DEEP WEAR MARKS, VERT SUPPORT Z, VERT OB LEG AT AFT LEG GEAR WELL CUTOUT CORNER. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG 65-48690.
- [SDR USAA040864](https://openairdocs.org/sdr/USAA040864), Oct 25, 2004: SKATE ANGLE. CHAFED. SKATE ANGLE, 11 INCHES LONG, EXCESSIVELY DEEP CHAFE MARK, 1104 TO 1121, STR 2 L.
- [SDR USAA040845](https://openairdocs.org/sdr/USAA040845), Oct 22, 2004: FRAME. CRACKED. FRAME, .5 INCH CRACK, STR 9 LT AT FRAME, STA 767. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES IAW TR 53-10-20A.
- [SDR USAA040863](https://openairdocs.org/sdr/USAA040863), Oct 22, 2004: SKIN. GOUGED. Q4, SKIN, 16 INCHES W BY 22 INCHES L, GOUGES, STA 887 BETWEEN S35R AND S27R. REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 53-00-01.
- [SDR USAA040853](https://openairdocs.org/sdr/USAA040853), Oct 21, 2004: FRAME. CRACKED. FRAME .2500 INCH LONG CRACK BS 360 ON FRAME BETWEEN S8L AND S9L. INSTALLED REPAIR ANGLES IAE TYP REP 53-10-20A.
- [SDR USAA040851](https://openairdocs.org/sdr/USAA040851), Oct 21, 2004: FRAME. CRACKED. FRAME, .1250 INCH CRACK, CRACKED AROUND RIVET AT FRAME AT STA 827, STR 9L. REMOVED CRACK AND INSTALLED REPAIR ANGLES IAW TR 53-10-20A.
- [SDR USAA040850](https://openairdocs.org/sdr/USAA040850), Oct 21, 2004: STRINGER. CRACKED. STRINGER, .5 INCH LONG CRACK, STR 7L AT BS 1010. INSTALLED REPAIR ANGLE IAW 53-00-03.
- [SDR USAA040849](https://openairdocs.org/sdr/USAA040849), Oct 21, 2004: FRAME. CRACKED. FRAME .2500 INCH CRACK, FRAME STA 787 AND STR 9R, CRACK EMANATING FROM FASTENER. INSTALLED REPAIR DOUBLER IAW TR 53-10-20A.
- [SDR USAA040861](https://openairdocs.org/sdr/USAA040861), Oct 21, 2004: ATTACH BRACKET. DAMAGED. PIT - Q4, ATTACH BRACKET, MIGRATING AND MISSING BUSHINGS. RT MLG SUPPORT BEAM, SPOILER ACT ATTACH BRACKET. REPLACED SPOILER ACTUATOR ATTACH BRACKET IAW MFG DWG 
- [SDR USAA040860](https://openairdocs.org/sdr/USAA040860), Oct 21, 2004: FITTING. WORN. PIT - Q4, STAB BEAM FITTING, WORN BUSHING. STAB BEAM LUG, RT MLG SUPPORT BEAM. REPLACED STAB BEAM FITTING IAW AMM 57-15-00-434.
- [SDR USAA040859](https://openairdocs.org/sdr/USAA040859), Oct 21, 2004: HANGER ASSY. WORN. PIT - Q4, WALKING BEAM HANGAR, WORN BUSHINGS. RT MAIN LANDING SUPPORT BEAM. REPLACED WALKING BEAM HANGAR IAW AMM 57-15-00-434.
- [SDR USAA040952](https://openairdocs.org/sdr/USAA040952), Oct 20, 2004: STRINGER. CRACKED. PIT - Q4 - STRINGER, .1250 INCH CRACKS, CRACKS IN STRING AROUND FASTENERS, STA 907, STR 4R. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG 65-45772.
- [SDR USAA040872](https://openairdocs.org/sdr/USAA040872), Oct 20, 2004: SKATE ANGLE. CHAFED. PIT - Q4 - SKATE ANGLE, 10 INCHES, CHAFED, 1006 TO 1016 BETWEEN STR 2L AND 3L. FABRICATED NEW ANGLE IAW MFG ENG DWG 65-548423.
- [SDR USAA040873](https://openairdocs.org/sdr/USAA040873), Oct 20, 2004: SKATE ANGLE. CHAFED. SKATE ANGLE, 10 INCHES OF CHAFING, 1006 TO 1016 BETWEEN STR 2R AND 3R. FABRICATED NEW ANGLE FROM ENG DWG 65548424.
- [SDR USAA040876](https://openairdocs.org/sdr/USAA040876), Oct 20, 2004: STRINGER. CRACKED. PIT - Q4, STRINGER, .1250 INCH CRACK, STA 907, STR4L, AROUND FASTENERS. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG 65-52988.
- [SDR USAA040848](https://openairdocs.org/sdr/USAA040848), Oct 19, 2004: FRAME. CRACKED. FRAME, .5 INCH CRACK, FRAME STA907,STR9L, CRACK EMANATING FROM FASTENER. CUTOUT CRACKED AREA AND INSTALLED REPAIR ANGLES IAW T.R. 53-10-20A.
- [SDR USAA040882](https://openairdocs.org/sdr/USAA040882), Oct 19, 2004: FITTING. CORRODED. PIT - Q4, FITTING, 1 INCH BY .5 INCH AREA, CORROSION; NO LEVEL OR TASK. RT WING AFT SPAR OB BUSHING BORE FTG WALKING BEAM HANGAR LUG AT STA 202. REMOVED AND REP
- [SDR USAA040858](https://openairdocs.org/sdr/USAA040858), Oct 19, 2004: BRACKET. CRACKED. BRACKET, 1 INCH CRACK, LT WING SPAR (AFT) STA 218, MFG NEW BRACKET IAW J020-37-20.
- [SDR USAA040847](https://openairdocs.org/sdr/USAA040847), Oct 18, 2004: INTERCOSTAL. CRACKED. INTERCOSTAL, .5 INCH CRACK, STA 947.5, LBL43. REPLACED INTERCOSTAL IAW SRM 51-70-11.
- [SDR USAA040883](https://openairdocs.org/sdr/USAA040883), Oct 18, 2004: STRINGER. CORRODED. STRINGER, 6 INCHES FULL WIDTH AND SIDES, CORROSION; LEVEL 1; TASK NR C53-208-01, STR 27 R JUST FWD OF FRAME, STA 1006. CUT STR REPAIR SECTION TO FIT AND INSTALL
- [SDR USAA040880](https://openairdocs.org/sdr/USAA040880), Oct 18, 2004: FITTING. CORRODED. PIT - Q4, LAV FLOOR ANCHOR FITTING, 2 AREAS, 1 INCH BY 2 INCHES, CORRODED; LEVEL 1; TASK NR C53-107-02, LT AFT LAV STA 986.5. REMOVED AND REPLACED FITTING (2 EA
- [SDR USAA040881](https://openairdocs.org/sdr/USAA040881), Oct 18, 2004: ANCHOR FITTING. CORRODED. PIT - Q4, LAV FLOOR ANCHOR FITTING, 2 INCHES BY 2 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, RT LAV FLOOR STA 1016.
- [SDR USAA040877](https://openairdocs.org/sdr/USAA040877), Oct 16, 2004: FLOORBEAM. CRACKED. PIT - Q4, BEAM, ABOUT .5 INCH, CRACKED, FLOOR SUPPORT BEAM, STA 540 AND LT OB SEAT TRACK. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG 65-46819-4.
- [SDR USAA040741](https://openairdocs.org/sdr/USAA040741), Oct 15, 2004: DOOR FRAME. CRACKED. PIT, Q4, EDGE FRAME SERVICE DOOR, .5 INCH CRACK, EDGE FRAME CRACKED, FWD SERVICE DOOR AFT EDGE FRAME, MID STOP AREA. INSTALLED DOUBLER IAW TYPE REP 52-10-11.
- [SDR USAA040852](https://openairdocs.org/sdr/USAA040852), Oct 14, 2004: DOOR FRAME. CRACKED. PIT - Q4 - DOOR EDGE FRAME, .5 INCH CRACK, FWD SERVICE DOOR AFT END FRAME AT MIDSTOP FITTING. ROUTED OUT CRACK, INSTALLED DOUBLER IAW TYP REP 52-10-11.
- [SDR USAA040878](https://openairdocs.org/sdr/USAA040878), Oct 14, 2004: ATTACH BRACKET. CRACKED. ATTACH BRACKET, .5 INCH LONG CRACK, S10L, STA 360. MANUFACTURED ATTACH BRACKET IAW SRM 51-40-03.
- [SDR USAA040884](https://openairdocs.org/sdr/USAA040884), Oct 12, 2004: FLOORBEAM. CORRODED. FLOORBEAM, 2 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, LBL 30.5 BETWEEN STA 947.5 AND 967. REMOVED AND REPLACED DEFECTIVE PART WITH IDENT PART IAW SRM 
- [SDR USAA040885](https://openairdocs.org/sdr/USAA040885), Oct 12, 2004: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT, 4 INCHES BY 1 INCH, CORROSION; LEVEL 1; TASK NR C53-107-02, RBL 17.61, STA 986.5 TO 967. REMOVED AND REPLACED DEFECTIVE PART WITH IDENT PART IAW 
- [SDR USAA040886](https://openairdocs.org/sdr/USAA040886), Oct 12, 2004: SUPPORT. CORRODED. SUPPORT, 5 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, LBL 25 BETWEEN STA 947.5 AND 967.
- [SDR USAA040846](https://openairdocs.org/sdr/USAA040846), Oct 11, 2004: FRAME. CRACKED. FRAME, 1.7500 INCH CRACK, BS 787, STR 9L. REPAIRED IAW TYP REP 53-10-20A.

All 78: https://openairdocs.org/deregistered/N352US-2006-09-06/reports.md

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