# N395US: 1986 Boeing 737-3B7, registration cancelled 2006-07-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 3, 2006
- Exported to: Indonesia
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-3B7](https://openairdocs.org/model/boeing-737-3b7) (registry code 138447F)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Serial number: 23317
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: April 23, 1986
- Certificate issued: June 12, 2006
- Last registry action: June 12, 2006
- Mode S code: A4972F
- Owner when cancelled: [Wells Fargo Bank Northwest Na](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N395US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=395US
- Page: https://openairdocs.org/deregistered/N395US-2006-07-03

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 737-3B7: https://openairdocs.org/model/boeing-737-3b7.md

## Service difficulty reports (58, newest 50)

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

- [SDR SB05145](https://openairdocs.org/sdr/SB05145), Nov 14, 2005: CHARGER. INOPERATIVE. PIT - MAINTENANCE REPORTED THE AFT CABIN EMERGENCY LIGHTS FROM SEAT ROWS 17 THROUGH 22 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY AND CHAR
- [SDR SB05141](https://openairdocs.org/sdr/SB05141), Oct 30, 2005: CHARGER. INOPERATIVE. CLT - MAINTENANCE REPORTED THE AFT CABIN SEAT/AISLE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY CHARGER AND BATTERY. OPERATIO
- [SDR SB05133](https://openairdocs.org/sdr/SB05133), Oct 16, 2005: BATTERY PACK. DISCHARGED. CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT POWER SOURCE BATTERY WAS WEAK IN THE FORWARD CABIN. MAINTENANCE REMOVED AND REPLACED THE FORWARD CABIN BATTE
- [SDR SB05132](https://openairdocs.org/sdr/SB05132), Oct 16, 2005: CONNECTOR. DAMAGED. CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS AT THE FORWARD ENTRY AND SERVICE DOORS AND SEAT ROWS 1 THROUGH 4 WERE INOPERATIVE. MAINTENANCE FOUND 2 PINS
- [SDR USAA051170](https://openairdocs.org/sdr/USAA051170), Oct 3, 2005: SKIN. CRACKED. FOUND FUSELAGE STATION 727, STRINGER 22L CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 DETAIL X DEFECT SIZE: 1.5".
- [SDR SB04173](https://openairdocs.org/sdr/SB04173), Dec 29, 2004: WIRE. BROKEN. PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT AISLE LIGHT AT ROW 19 INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER THE SEAT. OPERATIONAL CHECK GOOD.
- [SDR USAA040752](https://openairdocs.org/sdr/USAA040752), Oct 8, 2004: KEELBEAM. CORRODED. PIT, C1, KEELBEAM, 1 INCH X 20 INCH AREA, CORROSION; NO LEVEL OR TASK, BS520-540 AT STR 26L. REMOVED CORROSION, INSTALED NESTED REPAIR ON ONE SIDE ONLY IAW SRM 
- [SDR USAA040648](https://openairdocs.org/sdr/USAA040648), Sep 23, 2004: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1.5 INCH, STATION 870, .5 INCH BELOW STRINGER 23R. INSTALLED DOUBLER IAW SRM 53-00-01. (M)
- [SDR USAA040646](https://openairdocs.org/sdr/USAA040646), Sep 22, 2004: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1 INCH, STATION 945.5, .5 INCH ABOVE STRINGER 24R. INSTALLED DOUBLER IAW 53-00-01 FIG 229. (M)
- [SDR USAA030235](https://openairdocs.org/sdr/USAA030235), Nov 4, 2003: SKIN. CRACKED. FOUND SKIN 2.75 INCH CRACK BS 882-884, 3/4 ABOVE STRINGER 26R. CUT OUT DAMAGE, INSTALLED DOUBLER, TRIPLER AND FILLER PER SRM 53-00-01 FIG 229. (M)
- [SDR USAASB03056](https://openairdocs.org/sdr/USAASB03056), Apr 28, 2003: WIRE. LOOSE. PIT - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHTS, AT SEAT ROWS 17 THROUGH 22, INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE SPLICE IN SEAT ROW 20, LE
- [SDR USAASB03001](https://openairdocs.org/sdr/USAASB03001), Jan 2, 2003: WINDSHIELD. CRACKED. CLT - FLT 1641 - EN ROUTE FROM PHL-ATL, AT FL350, THE FIRST OFFICERS WINDSHIELD BEGAN ARCING, DELAMINATING AND CRACKING. CAPTAIN LOWERED CABIN PRESSURIZATION TO
- [SDR USAA020474](https://openairdocs.org/sdr/USAA020474), Dec 1, 2002: SKIN. CRACKED. SKIN, 2 INCH CRACK, 3 INCHES BELOW PREVIOUS PATCH AT WING EMERGENCY LIGHT. CUT OUT DAMAGE, INCORP ENTIRE AREA INTO ONE EXTERIOR DOUBLER/TRIPLER REPAIRED IAW EA.
- [SDR USAASB02204](https://openairdocs.org/sdr/USAASB02204), Nov 9, 2002: CONTROLLER. FAILED. CLT - FLT 1279 - ON CLIMB-OUT FROM CLT, EN ROUTE TO MKE, CREW REPORTED THE CABIN ALTITUDE WARNING HORN SOUNDED PASSING THROUGH FL030. FLIGHT RETURNED TO FIELD A
- [SDR USAA020402](https://openairdocs.org/sdr/USAA020402), Oct 25, 2002: SKIN. DELAMINATED. PIT - FOUND RUDDER WITH DELAMINATION, STATION 0.00 RT, 1.5 LEFT, 121.0 LEFT, 174.9 RT, 200.0 RT. REPAIRED WITH WET LAYUP USING SRM 51-70-17, 51-60-00 PER EA 751
- [SDR USAA020357](https://openairdocs.org/sdr/USAA020357), Aug 22, 2002: STIFFENER. CORRODED. TPA - FOUND CHANNEL STIFFENER CORRODED 6 INCHES, STATION 0 BULKHEAD 1016. CUT AND REMOVED DAMAGED PART, SPLICED IN NEW CHANNEL STIFFENER PER SB 737-53A1075 AND 
- [SDR USAA020214](https://openairdocs.org/sdr/USAA020214), Jun 2, 2002: SKIN. CRACKED. CLT - FOUND SKIN CRACKED STATION 727 AND 727A STRINGER 23L. REPAIRED, INSTALLED DOUBLER PER SRM 53-00-01. (M)
- [SDR USAA011176](https://openairdocs.org/sdr/USAA011176), Aug 14, 2001: STRINGER. CORRODED. TPA - FOUND STRINGER CORRODED 6 SQUARE INCH AREA, STRINGER 25L STATION 967 PLUS 10 INCHES. CORROSION LEVEL 2. SPLICED IN SECTION OF STRINGER PER SRM 53-00-03 PA
- [SDR USAASB01138](https://openairdocs.org/sdr/USAASB01138), May 16, 2001: CHARGER. FAILED. CLE - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN NR 2 AND NR 3 BULL NOSE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK GO
- [SDR USAA010100](https://openairdocs.org/sdr/USAA010100), Jan 30, 2001: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 3 INCHES, STATION 727D PLUS 3, STRINGER 23R. INSTALLED DOUBLER PER EA 69060. (M)
- [SDR USAASB00301](https://openairdocs.org/sdr/USAASB00301), Oct 25, 2000: CHARGER. FAILED. ALB - MAINTENANCE FOUND THE EMERGENCY LIGHT IN THE COCKPIT, RIGHT INTERIOR LIGHT OVER SERVICE DOOR AND PASSENGER DOOR EXTERIOR EVACUATION LIGHT INOPERATIVE. MAI
- [SDR USAASB00268](https://openairdocs.org/sdr/USAASB00268), Sep 21, 2000: ACTUATOR. DETACHED. BDL - FLT 1738 - WHEN FLAPS WERE EXTENDED FOR LANDING AT BDL, FROM PHL, THE AIRCRAFT ROLLED RIGHT. IT REQUIRED OPPOSING AILERON FORCE OF 2 TO 3 DEGREES LEFT AIL
- [SDR USAASB00202](https://openairdocs.org/sdr/USAASB00202), Jul 30, 2000: INDICATOR. FAILED. PHL - FLT 409 - EN ROUTE FROM GSO TO PHL, AT 24,000 FT, CAPTIAN NOTICED THE NR 1 ENGINE OIL TEMPERATURE WAS REDLINED THEN BEGAN BOUNCING AROUND. POWER WAS PULLE
- [SDR USAA000663](https://openairdocs.org/sdr/USAA000663), Apr 30, 2000: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 1.75 INCH, RIGHT SIDE STATION 727D TO STATION 727E AT STRINGER 24R. INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01 FIG 201. (M)
- [SDR USAASB99175](https://openairdocs.org/sdr/USAASB99175), Jul 18, 1999: UPLOCK SENSOR. FAILED. CLT - FLT 249 - DURING CLIMB-OUT FROM CLT, THE RIGHT MLG UNSAFE LIGH TILLUMINATED WITH THE GEAR UP. FLIGHT RETUREND TO FIELD AT CLT AND LANDED WITHOUT FURTHER I
- [SDR USAASB99077](https://openairdocs.org/sdr/USAASB99077), Mar 20, 1999: BATTERY CHARGER. FAILED. PHL - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 1 THROUGH 4 INOPERATIVE AND THE LAST 6 SEAT ROWS IN THE AFT CABIN INOPERATIVE. MAINTENANCE REPAIRED SH
- [SDR USAASB99053](https://openairdocs.org/sdr/USAASB99053), Feb 24, 1999: SNUBBER. MISINSTALLED. TPA - FLT1795 - CAPTAIN REPORTED THAT DURING CLIMB-OUT FROM PBI, AN UNCOMFORTABLY LOUD NOISE WAS COMING FROM THE FORWARD ENTRY DOOR AREA. PRESSURIZATION AS NORM
- [SDR USAA980548](https://openairdocs.org/sdr/USAA980548), Oct 26, 1998: FLOORBEAM. CORRODED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AROUND NUTPLATE STATION 328 LBL 36 RBL 66 FLOORBEAM UPPER SURFACE FORWARD E
- [SDR USAA980547](https://openairdocs.org/sdr/USAA980547), Oct 26, 1998: FLOORBEAM. CORRODED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AROUND NUTPLATE STATION 344 FLOORBEAM UPPER SURFACE FORWARD ENTRY T-CAP. CO
- [SDR USAA980542](https://openairdocs.org/sdr/USAA980542), Oct 26, 1998: STRINGER. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK STATION 616 STRINGER 3R STRINGER SHEAR TIE. REMOVED AND REPLACED STRINGER SHEAR TIE PER SRM 51-1
- [SDR USAA980541](https://openairdocs.org/sdr/USAA980541), Oct 26, 1998: STRINGER. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 639 STRINGER 3R STRINGER SHEAR TIE. REMOVED AND REPLACED STRINGER SHEAR TIE PER SRM 51-
- [SDR USAA980533](https://openairdocs.org/sdr/USAA980533), Oct 26, 1998: FRAME. DAMAGED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A HOLE AT APU BLEED AIR DUCT CHAFFING FRAME FROM LIGHTENING BS 1064. INSTALLED FRAME REPAIR PER EA 62609B. (M)
- [SDR USAA980532](https://openairdocs.org/sdr/USAA980532), Oct 26, 1998: FRAME. CORRODED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH CORROSION AREA STATION 500D BETWEEN STRINGER 26L AND STRINGER 27L ON FRAME, CORROSION TASK NR
- [SDR USAA980501](https://openairdocs.org/sdr/USAA980501), Oct 26, 1998: SEAT TRACK. GOUGED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH BY .25 INCH GOUGE STATION 646 LBL 25 ON SEAT TRACK. SPLICED IN NEW SEAT TRACK SECTION PER SRM 53-00-5
- [SDR USAA980500](https://openairdocs.org/sdr/USAA980500), Oct 26, 1998: SKIN. CORRODED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT STATION 727 PLUS 12 LBL 6.5 ON SKIN. CORROSION TASK NR C53-208-01. INSTALLED DOUBL
- [SDR USAA980499](https://openairdocs.org/sdr/USAA980499), Oct 26, 1998: CLIP. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK STATION 616 STRINGER 8 L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA980498](https://openairdocs.org/sdr/USAA980498), Oct 26, 1998: SKIN. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK FORWARD GALLEY DOOR UPPER HINGE AREA. INSTALLED DOUBLER PER EA 38966A SB 737-52-1096 REV 1. (M)
- [SDR USAA980472](https://openairdocs.org/sdr/USAA980472), Oct 26, 1998: FRAME. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1.25 INCH CRACK OUTER CHORD STATION 727 STRINGER 14L. INSTALLED REPAIR FILLER, DOUBLER AND STRINGER CLIP PER E
- [SDR USAA980471](https://openairdocs.org/sdr/USAA980471), Oct 26, 1998: FRAME. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT LWR TERMINUS OF DOOR SURROUND FRAME BS 300 STRINGER 17R WL 209. INSTALLED FRAME REQUIRE PER 
- [SDR USAASB98133](https://openairdocs.org/sdr/USAASB98133), Jun 1, 1998: LIGHT. FAILED. ALB - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 5, 6, 7, 9, AND 11. MAINTENANCE REPAIRED EMERGENCY LIGHT WIRING AT SEAT ROWS 7 AND 8, LEFT
- [SDR USAASB97228](https://openairdocs.org/sdr/USAASB97228), Aug 16, 1997: PROX SWITCH. DIRTY. CUN - FLT 1607 - WHILE LOWERING LANDING GEAR ON APPROACH INTO CUN, THE CREW RECEIVED A 3-GREEN LIGHT INDICATION, BUT, ALSO, THREE RED LIGHTS. THE GEAR WAS RECYC
- [SDR USAASB97043](https://openairdocs.org/sdr/USAASB97043), Feb 6, 1997: HOSE ASSY. FAILED. LGA - FL 785 - SHORTLY AFTER TAKEOFF, THE NR 1 ENGINE, HYD SYSTEM A, LOW PRESS LIGHT ILLUMINATED. CREW NOTICED HYD SYSTEM A QTY GAUGE ALSO STARTED TO GO DOWN. C
- [SDR USAA950447](https://openairdocs.org/sdr/USAA950447), Apr 27, 1995: SEAL. LEAKING. LAX - FLT 2139 - AIR LEAK FROM MAIN ENTRANCE DOOR AFTER TAKEOFF. FLIGHT RETURNED TO LAX WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT FO
- [SDR USAA950398](https://openairdocs.org/sdr/USAA950398), Mar 23, 1995: SKIN. CORRODED. INT - DURNG Q-4 CHECK VISUAL INSPECTION, FOUND 16 INCH BY 8 INCH AREA OF SPOTS CORROSION ON DOOR SILL WEB SKIN, BS 804 AT AFT CARGO DOOR SILL AREA. REPAIRED PER
- [SDR USAA950396](https://openairdocs.org/sdr/USAA950396), Mar 23, 1995: INTERCOSTAL. CORRODED. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCHES BY 12 INCHES CORRODED AREA ON INTERCOSTAL AT BS 947 TO BS 967 RBL 45 INCHES. REPAIRED PER SRM 51-10-2. 
- [SDR USAA950395](https://openairdocs.org/sdr/USAA950395), Mar 23, 1995: ANGLE. CORROSION. INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 2 INCHES BY 40 INCHES CORRODED AREA, AFT SERVICE DOOR. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, 
- [SDR USAA950394](https://openairdocs.org/sdr/USAA950394), Mar 23, 1995: INTERCOSTAL. CORRODED. INT - DURING Q-4 CHECK, VISUAL INSPECTION, FOUND 2 INCH BY 12 INCH CORRODED AREA ON INTERCOSTAL AT BS 957 RBL 18 INCHES TO RBL 45 INCHES. REPAIRED PER SRM 51-10
- [SDR USAA950392](https://openairdocs.org/sdr/USAA950392), Mar 9, 1995: T-CAP. CORRODED. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, ON T-CAP AT BS 986.5. REPAIRED PER TR 53-107-02, CORROSION LE
- [SDR USAA950400](https://openairdocs.org/sdr/USAA950400), Mar 8, 1995: INTERCOSTAL. CORRODED. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION INTERCOSTAL, BS 967 - BS 987 RBL 22 INCH. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-0. CORRO
- [SDR USAA950399](https://openairdocs.org/sdr/USAA950399), Mar 8, 1995: 'T' CAP. CORRODED. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION THE ENTIRE LENGTH OF BEAM 25 PERCENT TO 40 PERCENT LOSS, BS 1016 LEFT END TO RIGHT END. REPAIRED PER S

All 58: https://openairdocs.org/deregistered/N395US-2006-07-03/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 19921105048809I](https://openairdocs.org/incident/19921105048809I), Nov 5, 1992: Boeing 7373B7 (N395US), Covington/Cinci, KY. Flight attendant observed smoke exiting from lavatory. Exiting lavatory was female passenger. Police met flight.

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