# N385US: 1985 Boeing 737-3B7, 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 737-3B7](https://openairdocs.org/model/boeing-737-3b7) (registry code 138447F)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Serial number: 22958
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 31, 1985
- Certificate issued: November 14, 2005
- Last registry action: November 14, 2005
- Mode S code: A46FB0
- Owner when cancelled: [Jet Partners LLC](https://openairdocs.org/faa-owner/JET%20PARTNERS%20LLC)
- Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)
- Owner type: Corporation
- Owner's area on the map: 40.7657° N, 73.9851° W: Placed by OpenAirDocs at the center of ZIP code 10019, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N385US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=385US
- Page: https://openairdocs.org/deregistered/N385US-2006-09-06

From the FAA registry file of October 28, 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 737-3B7: https://openairdocs.org/model/boeing-737-3b7.md

## Service difficulty reports (50)

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

- [SDR PIDR2006023](https://openairdocs.org/sdr/PIDR2006023), Jan 5, 2006: FLOORBEAM. CORRODED. BS 986.5 FLOORBEAM CORRODED AT A PREVIOUS REPAIR FROM RBL14 TO RBL18. REPLACED UPPER T CAP OF FLOORBEAM IAW EA NR 53-264.
- [SDR USAA200507001](https://openairdocs.org/sdr/USAA200507001), Jul 9, 2005: SKIN. CRACKED. CRACK AT BS 767 BETWEEN STRINGERS 21 RT AND 22 RT ON FUSELAGE SKIN. REMOVED DAMAGED FUSELAGE SKIN AND INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 229, DETAIL 
- [SDR USAA041075](https://openairdocs.org/sdr/USAA041075), Dec 12, 2004: SKIN. CRACKED. PIT - A-CHECK - SKIN, 2 INCH CRACK, STA 760, STR 19R, INSTALLED DOUBLER IAW SRM.
- [SDR SB04159](https://openairdocs.org/sdr/SB04159), Nov 27, 2004: ODOR. DETECTED. PHL - FLT1227, EN ROUTE FROM BTV TO PHL, CREW REPORTED A STRONG OIL SMELL IN CABIN. CREW WAS ABLE TO ISOLATE SOURCE TO LEFT PACK/LEFT ENGINE. FLIGHT LANDED AT P
- [SDR USAA040829](https://openairdocs.org/sdr/USAA040829), Oct 19, 2004: SKIN. DELAMINATED. PIT - C4, IB AFT FLAP SKIN, 3 INCHES BY 2.5 INCH AREA, DELAMINATION, IB AFT FLAP OB T/E LEFT WING. REMOVED SKIN AND CORE, INSTALLED REPAIR AND DOUBLER IAW TYP R
- [SDR USAA040837](https://openairdocs.org/sdr/USAA040837), Oct 19, 2004: SKIN. DELAMINATED. PIT - C4, IB AFT FLAP SKIN, 3 INCHES X 2.5 INCHES AREA, DELAMINATION. IB AFT FLAP OB T/E LT WING. REMOVED DELAMINATION, INSTALLED REPAIR CORE, SKIN AND DOUBLER 
- [SDR USAA040750](https://openairdocs.org/sdr/USAA040750), Oct 15, 2004: SKIN. CRACKED. PIT, C3; SKIN, .2500 INCH CRACK, BETWEEN STR 13/16R AND FRA 947.5. 11 INCH W X 9.5 INCH H FILLER, ALONG WITH 10 INCH W X 13.5 H DOUBLER IAW SRM 53-60-01, FIG 20
- [SDR USAA040748](https://openairdocs.org/sdr/USAA040748), Oct 7, 2004: BULKHEAD. CRACKED. PIT, C1; SKIN WITH .5 INCH LONG CRACK AT AFT PRESSURE BULKHEAD AT BL0 AND 10 INCHES ABOVE CENTER. INSTALLED DOUBLER IAW SRM 53-80-08.
- [SDR USAA040749](https://openairdocs.org/sdr/USAA040749), Oct 6, 2004: SKIN. CRACKED. PIT, C3; SKIN, (3 EA) CRACKS; 1 INCH, 2.7 INCHES AND 1 INCH, AFT OF 727E-747, S18R. INSTALLED REPAIRS IAW SRM 53-00-01, FIG 228.
- [SDR SB04137](https://openairdocs.org/sdr/SB04137), Oct 2, 2004: PROXIMITY SENSOR. FAULTY. EWR - FLT 2164 - ON DESCENT INTO LGA FROM DCA, CREW RECEIVED A NR 4 LEADING EDGE KRUGER FLAP AMBER LIGHT ALONG WITH A LEADING EDGE TRANSIT AMBER LIGHT DURING SL
- [SDR USAA040506](https://openairdocs.org/sdr/USAA040506), Aug 24, 2004: BEAM. CRACKED. PIT - FOUND VERTICAL BEAM CRACKED, VERT CHORD 5.7 LEFT WL 184 STATION 178 FPBH. REMOVED DEFECTIVE PARTS, INSTALLED REPAIR ANGLE PER EO 5300V155. (M)
- [SDR USAASB04077](https://openairdocs.org/sdr/USAASB04077), Jun 25, 2004: UPLOCK SENSOR. MALFUNCTIONED. AFTER TAKEOFF FROM GSO, CREW RECEIVED A RIGHT MLG RED UNSAFE LIGHT AFTER GEAR RETRACTION. CREW LOWERED GEAR PER QUICK REF HANDBOOK PROCEDURES AND RECEIVED A NOR
- [SDR USA2004F00050](https://openairdocs.org/sdr/USA2004F00050), May 17, 2004: FLAP. MALFUNCTIONED. ON APPROACH, CREW RECEIVED A LEADING EDGE FLAPS TRANSIT LIGHT ASSOCIATED WITH A YELLOW TRANSIT LIGHT ON THE NR 3 LEADING EDGE SLAT. CAPTAIN REPORTED THE FLAPS W
- [SDR USAASB04012](https://openairdocs.org/sdr/USAASB04012), Jan 26, 2004: CONTROLLER. MALFUNCTIONED. PIT - FLT 385 - EN ROUTE FROM PHL-MSY, AT FL250, THE CABIN ALTITUDE BEGAN TO CLIMB MODERATELY. FLIGHT DESCENED TO 10,000 FEET WHERE CABIN WAS REGAINED. FLIGHT T
- [SDR USAA030318](https://openairdocs.org/sdr/USAA030318), Dec 11, 2003: SKIN. CRACKED. PIT - FOUND SKIN WRINKLE CRACK 2.5 INCHES LONG, STATION 747 STRINGER 22R. INSTALLED REPAIR DOUBLERS PER SRM 53-00-01 PG 205, FIG 202. (M)
- [SDR USAASB03206](https://openairdocs.org/sdr/USAASB03206), Nov 23, 2003: ENGINE. FAILED. CLIMBING THROUGH 16,000 FT OUT OF BOS, EN ROUTE TO DCA, THE NR 1 ENGINE EXPERIENCED A LOUD BANG. THE AIRCRAFT STARTED TRACKING TO THE LT. CREW DETERMINED NO THR
- [SDR USAASB03031](https://openairdocs.org/sdr/USAASB03031), Feb 28, 2003: LIGHT. FAILED. ATL - MAINTENANCE REPORTED THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACD THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT/SOCKET ASSEMBLY.
- [SDR USAA020477](https://openairdocs.org/sdr/USAA020477), Dec 27, 2002: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 3 INCHES LONG, RIGHT SIDE STATION 867 STRINGER 24 RIGHT. CUT OUT DAMAGE, INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01 FIG 202. (M)
- [SDR USAASB02125](https://openairdocs.org/sdr/USAASB02125), Jun 26, 2002: WIRE. PINCHED. RDU - MAINTENANCE FOUND THE SIDEWALL EMERGENCY EXIT LIGHTS AT THE FORWARD FLIGHT ATTENDANT POSITION AND FORWARD GALLEY POSITION INOPERATIVE. ALSO, FOUND THE AIS
- [SDR USAA011376](https://openairdocs.org/sdr/USAA011376), Nov 19, 2001: SKIN. CRACKED. PIT - FOUND SKIN CRACKED .5 INCH HOLE, LEFT UPPER WING T/E JUST OUTBOARD OF AILERON. REPLACED PANEL PER SRM 57-51-01 AND EA 72942. (M)
- [SDR USAA011375](https://openairdocs.org/sdr/USAA011375), Nov 19, 2001: WEB. CRACKED. PIT - FOUND DOOR REINFORCING WEB CRACKED 1 INCH, STATION 921, 1 INCH BELOW S11R IN DOOR REINFORCING WEB. REPAIR DOUBLER INSTALLED PER SRM 51-70-13 AND EA 72800.
- [SDR USAA011373](https://openairdocs.org/sdr/USAA011373), Nov 19, 2001: SKIN. CRACKED. PIT - FOUND SKIN CRACKED .045 INCH DEEP, 3 INCHES LONG BY 2 INCHES WIDE, STATION 420 43 INCHES FORWARD OF CARGO BETWEEN 22R AND 23R. DOUBLER INSTALLED PER SRM 5
- [SDR USAA011363](https://openairdocs.org/sdr/USAA011363), Nov 12, 2001: SKIN. DELAMINATED. PIT - FOUND RIGHT ELEVATOR HAS DELAMINATION TOP SKIN PEELING 2 SPOTS 7.5 INCHES LONG BY 1 INCH WIDE, INBOARD EDGE 84 INCHES OUTBOARD FROM INBOARD 7.5 INCHES LON
- [SDR USAA011377](https://openairdocs.org/sdr/USAA011377), Nov 5, 2001: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 1.5 INCH, STATION 952 STRINGER 11L. INSTALLED DOUBLER PER EA 72801. (M)
- [SDR USAA011374](https://openairdocs.org/sdr/USAA011374), Oct 26, 2001: FRAME. CRACKED. PIT - FOUND FRAME CRACKED 2 INCHES, AT STATION 847 BETWEEN STRINGER 8L-9L. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M)
- [SDR USAASB01246](https://openairdocs.org/sdr/USAASB01246), Sep 2, 2001: BATTERY PACK. INOPERATIVE. LGA- MAINTENANCE FOUND THE AISLE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT POWER SUPPLY (P/N 11-0049) AND BATTERY PACK ALONG WITH T
- [SDR USAA011146](https://openairdocs.org/sdr/USAA011146), Aug 23, 2001: PRESSURE PANEL. CRACKED. CLT - FOUND WEB CRACKED 1.5 INCH, MAIN W/W PRESSURE DECK AT 664 RBL 40. INSTALLED DOUBLER PER TR 53-60-04. (M)
- [SDR USAA011129](https://openairdocs.org/sdr/USAA011129), Aug 21, 2001: WEB. CRACKED. CLT - FOUND ON WALKAROUND, WEB CRACKED .5 INCH AND .125 INCH, WHEEL WELL CEILING AT LBL 30 BS 685. INSTALLED DOUBLER PER TR 53-60-04. (M)
- [SDR USAASB01124](https://openairdocs.org/sdr/USAASB01124), May 1, 2001: UPLOCK SENSOR. FAULTY. IAH - FLT 1620 - AFTER TAKEOFF FROM IAH, WHEN THE LANDING GEAR WAS RAISED, CREW RECEIVED TWO GREEN LIGHTS AND A LEFT MLG RED LIGHT. AN UNUSUAL RUMBLE WAS ALSO N
- [SDR USAASB00363](https://openairdocs.org/sdr/USAASB00363), Dec 30, 2000: CIRCUIT BREAKER. FAULTY. CLT - FLT 1775 - EN ROUTE FROM PHL-ORD - THE LEFT FORWARD WINDOW HEAT OVERHEAT LIGHT ILLUMINATED. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES BUT LIGH
- [SDR USAASB00194](https://openairdocs.org/sdr/USAASB00194), Jul 21, 2000: DOWNLOCK SENSOR. FAULTY. CLT - FLT 250 - ON PREPARATION FOR LANDING AT CLT FROM PNS, THE RIGHT MLG GREEN LIGHT FLICKERED. WHEN GEAR WAS EXTENDED, THE RED UNSAFE LIGHT ILLUMINATED AND NO
- [SDR USAA000780](https://openairdocs.org/sdr/USAA000780), Jun 2, 2000: STRAP. CRACKED. TPA - FOUND STRIP CRACKED .25 INCH, MAIN ENTRY DOOR, INNER STRUCTURE UPPER HINGE WEB. REPLACED STRAP PER SRM 51-10-2. (M)
- [SDR USAASB00109](https://openairdocs.org/sdr/USAASB00109), Apr 9, 2000: VALVE. FAILED. CLT - FLT 1930 - EN ROUTE FROM PHL TO PBI, CREW NOTIFIED DISPATCH VIA ACARS THATY THEY WERE LOSING CABIN PRESSURE ALTITUDE AND UNABLE TO CONTROL THE PRESSURE LO
- [SDR USAA990864](https://openairdocs.org/sdr/USAA990864), Aug 8, 1999: STIFFENER. CRACKED. PIT - DURING CX3 CONV CHECK, FOUND .5 INCH CRACK IN STIFFENER AT STATION 344 INTERCOSTAL. REPLACED ANGLES PER EA 52604. (M)
- [SDR USAA990863](https://openairdocs.org/sdr/USAA990863), Aug 8, 1999: SKIN. CRACKED. PIT - DURING CX3 CONV CHECK, FOUND CRACK APPROX .500 INCH IN AFT CARGO DOOR, FLAPPER DOOR CUT OUT (A/C SKIN) UPPER AFT CORNER. REPAIRED PER TYPICAL REPAIR 52-10
- [SDR USAA990862](https://openairdocs.org/sdr/USAA990862), Aug 8, 1999: FLOORBEAM. CRACKED. PIT - DURING CX 3 CONV CHECK, FOUND CRACK APPROX .500 INCH FLOORBEAM AT FS 344 AT LBL 11. REPAIRED PER SRM 53-10-51 AND EA 52604. (M)
- [SDR USAASB99198](https://openairdocs.org/sdr/USAASB99198), Jul 28, 1999: CHARGER. FAILED. EWR - PILOT REPORTED THAT THE FORWARD ENTRY DOOR EMERGENCY LIGHT WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. 
- [SDR USAASB99163](https://openairdocs.org/sdr/USAASB99163), Jul 5, 1999: YAW DAMPER. FAILED. SDF - FLT 1548 - ON TAKEOFF ROLL FROM SDF, AT APPROX 125 KNOTS, AIRCRAFT EXPERIENCED A BRIEF UNCOMMANDED YAW TO THE RIGHT WITH NO FEEDBACK THROUGH RUDDER PEDALS
- [SDR USAASB99156](https://openairdocs.org/sdr/USAASB99156), Jun 28, 1999: BATTERY PACK. DISCHARGED. LGA - FLT 528 - PILOT REPORTED PRIOR TO DEPARTURE, THE FORWARD ENTRY AND FORWARD SERVICE DOOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REP
- [SDR 99ZZZX2961](https://openairdocs.org/sdr/99ZZZX2961), Jun 28, 1999: CHARGER. INOPERABLE. LGA - FLT 528 - PILOT REPORTED PRIOR TO DEPARTURE, THE FORWARD ENTRY AND FORWARD SERVICE DOOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REP
- [SDR USAA970293](https://openairdocs.org/sdr/USAA970293), Oct 10, 1997: SKIN. CRACKED. CLT - DURING EDDY CURRENT Q-3 CHECK INSPECTION, FOUND 2 CRACKS EACH LESS THAN 2 INCHES LONG NR 2 PYLON AT PANEL 5824R CUT OUT AT PYLON SKIN DOUBLER. INSTALLED D
- [SDR USAA970292](https://openairdocs.org/sdr/USAA970292), Oct 10, 1997: FLOOR BEAM. CORROSION. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION ON STA FLOOR BEAM COVERING APPROXIMATELY 124 INCHES BY 2 INCHES LONG AT 328 FLOOR BEAM FROM LBL 36 TO 
- [SDR USAA970291](https://openairdocs.org/sdr/USAA970291), Oct 10, 1997: BULKHEAD. CORROSION. CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AT ALL SCREW HOLES .50 INCH BY .50 INCH AT STA 294 ENTIRE LENGTH UPPER CHORD SECTION 41, BULKHEAD. C
- [SDR 97ZZZX4561](https://openairdocs.org/sdr/97ZZZX4561), Oct 10, 1997: SKIN. CRACKED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK FROM THE EDGE OF LIGHTENING HOLE ON INTERIOR OF FORWARD CARGO DOOR SKIN IN THE CENTER OF THE DO
- [SDR USAASB97237](https://openairdocs.org/sdr/USAASB97237), Aug 23, 1997: BATTERY PACK. DISCHARGED. CLT - SEVERAL CABIN EMERGENCY LIGHTS EXTINGUISHED PREMATURELY WHEN TESTED ON AN OVERNIGHT CHECK. REPLACED BATTERY ASSEMBLIES AT CHARGERS (M1136) AND (M1197) FOR
- [SDR USAASB97093](https://openairdocs.org/sdr/USAASB97093), Mar 29, 1997: AIR DISTRIBUTION. ODOR. CLT - FL 2314 - AT FL 280, A SMOKE/BURNING ODOR WAS NOTED IN THE MID CABIN. THE ODOR WOULD COME AND GO. CREW COULD NOT ISOLATE ODOR WITH ALTERNATE PACKS OR GALL
- [SDR USAASB97040](https://openairdocs.org/sdr/USAASB97040), Feb 5, 1997: BATTERY PACK. DISCHARGED. ROC - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS WOULD ONLY REMAIN ILLUMINATED FOR APPROXIMATELY 45 SECONDS, FOLLOWING OPERATIONAL CHECK, AT THE FOLLOWING LOCA
- [SDR USAASB95028](https://openairdocs.org/sdr/USAASB95028), Dec 17, 1995: PRESSURIZATION. MALFUNCTIONED. FLT 2301 - SYR - ON TAKEOFF, AUTO PRESSURIZATION FAILED. STANDBY WOULD NOT PRESSURIZE THE AIRCRAFT. LEVELED OFF AT 8000 FEET AND RETURNED TO SYR. (M)
- [SDR USAA950971](https://openairdocs.org/sdr/USAA950971), Aug 23, 1995: STRINGER. CORRODED. CLT - DURING DROP-IN CHECK INSPECTION, VISUALLY FOUND A 5 INCH BY 2 INCH CORRODED AREA LOCATED AT S-25RT FROM STATION 352 TO STATION 357. DROP IN AIRCRAFT. CORR
- [SDR USAA950603](https://openairdocs.org/sdr/USAA950603), Jun 8, 1995: ACTUATOR. FAILED. PIT - FLT 1662 - AFTER DEPARTURE, CREW WAS UNABLE TO TRIM STABLIZER WITH THE YOKE SWITCHS. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANC

## 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 19901126057699I](https://openairdocs.org/incident/19901126057699I), Nov 26, 1990: Boeing 7373B7 (N385US), Wichita, KS. Passenger became ill en route. Diverted to Wichita to provide medical attention for the passenger.

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