# N383US: 1984 Boeing 737-3B7, registration cancelled 2006-07-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 25, 2006
- 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: 22956
- Year built: 1984
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Experimental, research and development, market survey, showing compliance
- Airworthiness date: October 24, 1984
- Certificate issued: April 25, 2002
- Last registry action: May 18, 2005
- Mode S code: A46842
- Owner when cancelled: [J P Morgan Trust Co Na Trustee](https://openairdocs.org/faa-owner/J%20P%20MORGAN%20TRUST%20CO%20NA%20TRUSTEE)
- Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)
- Owner type: Corporation
- Owner's area on the map: 40.6898° N, 74.0174° W: Placed by OpenAirDocs at the center of ZIP code 10004, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N383US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=383US
- Page: https://openairdocs.org/deregistered/N383US-2006-07-25

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 (151, newest 50)

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

- [SDR SB05119](https://openairdocs.org/sdr/SB05119), Sep 23, 2005: ADC. FAILED. CLT FLT448 ON TAKEOFF ROLL, WITH FIRST OFFICER FLYING, THE FIRST OFFICER LOST AIRSPEED INDICATOR, ALTIMETER AND VERTICAL SPEED. AFTER TRANSFER OF CONTROLS TO CA
- [SDR USAA050464](https://openairdocs.org/sdr/USAA050464), Apr 2, 2005: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 1.5 INCH LONG, BS 747 BETWEEN 19L AND 20L. INSTALLED DOUBLER SKIN REPAIR PER EA 83173, SRM 53-00-01. (M)
- [SDR SB05036](https://openairdocs.org/sdr/SB05036), Mar 3, 2005: PRESSURE SWITCH. FAULTY. BWI - FLT141 - EN ROUTE FROM DCA TO IND, AT FL270, WITH THE APU POWERING THE NR 2 GENERATOR BUS, THE APU LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY AN APU A
- [SDR SB05027](https://openairdocs.org/sdr/SB05027), Feb 18, 2005: BATTERY PACK. DISCHARGED. PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS ABOVE THE AFT LEFT SERVICE DOOR AND THE AFT RIGHT SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACE
- [SDR SB04169](https://openairdocs.org/sdr/SB04169), Dec 21, 2004: LOGIC CARD. DIRTY. ALB - FLT1231 - ON APPROACH TO ALB FROM CLT, THE RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED. CREW PERFORMED MANUAL GEAR EXTEN
- [SDR USAA040866](https://openairdocs.org/sdr/USAA040866), Nov 11, 2004: SKIN. CRACKED. SKIN, 1.75 INCHES CRACKED AT STA 927 AND 947.5 AT STR 25R. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01.
- [SDR USAA040786](https://openairdocs.org/sdr/USAA040786), Oct 29, 2004: FLOOR SUPPORT. CORRODED. PIT - Q5, FLOOR SUPPORT, .1250 INCH BY .1250 INCH AREA, CORROSION; LEVEL 1; TASK NRC53-107-02, FASTENER HOLE AT STA 947 RBL 20. CUT OUT DAMAGED AREA, FABRICATED
- [SDR USAA040798](https://openairdocs.org/sdr/USAA040798), Oct 29, 2004: CHANNEL. CRACKED. PIT, Q5, CHANNEL, 6 INCH LONG CRACK, NR 2 PYLON LOWER CHANNEL NAC STA 363. REMOVED AND REPLACED CHANNEL IAW SRM 51-10-02.
- [SDR USAA040782](https://openairdocs.org/sdr/USAA040782), Oct 23, 2004: SKIN PANEL. DAMAGED. PIT, Q5, SKIN PANEL, REMOVED AND REPLACED SKIN PANEL AT BS 980 FROM S20R-S25R. REMOVED AND REPLACED SKIN PANEL DUE TO TEMPORARY REPAIRS; REPAIR TOO CLOSE TO LAP
- [SDR USAA040793](https://openairdocs.org/sdr/USAA040793), Oct 23, 2004: THRESHOLD. CORRODED. PIT,Q5, THRESHOLD, 2 INCH X 4 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-202-01 AFT CARGO DOOR THRESHOLD S25R. INSTALLED THRESHOLD IAW DWG 65-47957. AFT CARGO D
- [SDR USAA040795](https://openairdocs.org/sdr/USAA040795), Oct 23, 2004: FRAME. CORRODED. PIT, Q5, FRAME .2500 INCH X .2500 INCH- 6 EA AREAS, CORROSION; LEVEL 1; TASK NR C53-208-01 AROUND FASTENER HOLES - STA 847 FRAME BETWEEN S26R, ES25R. SPLICED IN
- [SDR USAA040794](https://openairdocs.org/sdr/USAA040794), Oct 19, 2004: INTERCOSTAL. CORRODED. PIT, Q5, INTERCOSTAL, .5000 INCH AND .2500 INCH, 2 BRACKETS, CORROSION; NO LEVEL OR TASK. E11 DOOR FRAME AT SWITCH NR 3196 INSIDE OF FRAME, BL0, STA 203.8. FABR
- [SDR USAA040827](https://openairdocs.org/sdr/USAA040827), Oct 18, 2004: PRESSURE BLKHD. DAMAGED. PIT - Q5, AFT PRESSURE BULKHEAD, NUMEROUS TENSION BOLTS LOOSE, STA 1016 AFT PRESSURE BULKHEAD. REPLACED TENSION BOLTS IAW EA 79074 AND SB 737-53-1229.
- [SDR USAA040828](https://openairdocs.org/sdr/USAA040828), Oct 13, 2004: TEE FITTING. DEFECTIVE. STRINGER T FITTING, NO EDGE DISTANCE. NO EDGE DISTANCE FOR FASTENERS, FWD SIDE AFT PRESSURE BULKHEAD AT S10L. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DW
- [SDR USAA040825](https://openairdocs.org/sdr/USAA040825), Oct 8, 2004: FRAME. CRACKED. PIT - Q5, FRAME, CRACKED, (2EA) 2 INCHES AND 2.2500 INCH, 727D BETWEEN S-27L AND S-27R AT 1 RBBL AND LBBL. REPAIRED DOUBLER IAW SRM 51-70-11.
- [SDR USAA040826](https://openairdocs.org/sdr/USAA040826), Oct 2, 2004: ATTACH FITTING. CHAFED. PIT - Q5, FITTINGS, .1250, .5, .5, .5 INCH AREAS, HEAVY CHAFING (4 AREAS), ALL 4 AFT LUGS OF VERT STAB ATTACH FITTINGS.
- [SDR USAA040785](https://openairdocs.org/sdr/USAA040785), Oct 2, 2004: SEAT TRACK. CORRODED. PIT - Q5, SEAT TRACK, 2 INCH BY 4 INCH CORRODED AREA, LEVEL 1 TASK NR C53-107-02, AFT END OF RT OB SEAT TRACK, STA 947. MANUFACTURED FILLERS AND SPLICED IN A NE
- [SDR USAA040789](https://openairdocs.org/sdr/USAA040789), Oct 2, 2004: FLOORBEAM. CORRODED. PIT - Q5, FLOORBEAM TEE CAP, .1250 INCH BY .1250 INCH (6 AREAS), CORROSION; LEVEL 1; TASK NR C53-107-02, TOPS OF FLOORBEAMS IN AROUND SCREW HOLES STA 1016-986.5
- [SDR USAA040790](https://openairdocs.org/sdr/USAA040790), Oct 2, 2004: CHANNEL. CORRODED. PIT,Q5, Z-CHANNEL, 4 INCH X 1 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-01, FWD SERVICE DOOR Z-CHANNEL. REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR USAA040799](https://openairdocs.org/sdr/USAA040799), Oct 2, 2004: FLOORBEAM. CRACKED. PIT, Q5, FLOORBEAM, 3 INCH CRACK (BROKEN) .400 INCH CRACK, STA 540 LBL 1 AND LBL 19 SUPPORT). REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 53-21-00.
- [SDR USAA040800](https://openairdocs.org/sdr/USAA040800), Oct 2, 2004: BRACKET. CRACKED. PIT, Q5, BRACKET, 1 INCH X .2500 INCH CRACK, (L) BRACKET, STA 350 RBL 20. FABRICATED NEW BRACKET IAW DWG 69-74588.
- [SDR USAA040801](https://openairdocs.org/sdr/USAA040801), Oct 2, 2004: FLOOR SUPPORT. CRACKED. PIT, Q5, FLOOR SUPPORT WITH .2500 INCH X .3750 INCH CRACKS, END OF FLOOR SUPPORT, STA 540 LT AND RT OF BL-0. REMOVED AND REPLACED IAW SRM 53-21-00.
- [SDR USAA040784](https://openairdocs.org/sdr/USAA040784), Oct 1, 2004: SKIN. CRACKED. PIT - Q5, NR 1 SLAT, .2500 INCH CRACK, NR 1 SLAT L/E LOWER SURFACE AFT ROW OF RIVETS. DOUBLER INSTALLED IAW 57-43-01.
- [SDR USAA040791](https://openairdocs.org/sdr/USAA040791), Sep 30, 2004: FLOOR SUPPORT. CORRODED. PIT, Q5, ANGLE/TRACK, 2 INCH CORROSION, LEVEL 1; TASK NR C53-202-01 AFT CARGO CORE, FLOOR TIE DOWN TRACK, STA 859 LBL 17.20. SPLICED REPAIR SECTION INTO FLOOR T
- [SDR USAA040821](https://openairdocs.org/sdr/USAA040821), Sep 30, 2004: CHANNEL. CRACKED. PIT, Q5, CHANNEL WITH A 4 INCH LONG CRACK IN LOWER CHANNEL AT NR 2 NAC, STA 345. REMOVED AND REPLACED CHANNEL IAW SRM 51-10-02.
- [SDR USAA040788](https://openairdocs.org/sdr/USAA040788), Sep 25, 2004: KEELBEAM. CORRODED. PIT Q5, KEEL BEAM, 2 INCHES X 40 INCHES AREA CORROSION; LEVEL 1 TASK NR C53-208-01, L KEEL BEAM STA 500D-540. REMOVED AND REPLACED, SPLICED IN NEW SECTION IAW T
- [SDR USAA040802](https://openairdocs.org/sdr/USAA040802), Sep 21, 2004: SKIN. CRACKED. PIT, Q5, SKIN, 6 INCH CRACK, RT PYLON LOWER PAN FROM NAC 319 AFT TO END. REMOVED AND REPLACED SKIN AND INSTALLED DOUBLER IAW SRM 51-70-13.
- [SDR USAA040781](https://openairdocs.org/sdr/USAA040781), Sep 16, 2004: INTERCOSTAL. DAMAGED. PIT, Q5, INTERCOSTAL, HOLE DAMAGE. LIGHTENING HOLE DAMAGE, STA 294.5 + 312 LBL 10 INCH INTERCOSTAL FLOORBEAM LIGHTENING HOLE DAMAGE. FABRICATED WEB AND INSTALLE
- [SDR USAA040792](https://openairdocs.org/sdr/USAA040792), Sep 14, 2004: ANGLE. CORRODED. PIT, Q5, KEEP REPAIR ANGLE, 20 INCH AREA, CORROSION; LEVEL 1; TASK NR C 53-208-01 R KEEL STA 520-540. INSTALLED NEW REPAIR ANGLE/ DOUBLER IAW SRM 51-70-11.
- [SDR USAA040805](https://openairdocs.org/sdr/USAA040805), Sep 13, 2004: DOOR FRAME. CRACKED. PIT, Q5, WEB FRAME, 3 INCH CRACK AT FWD ENTRY DOOR LOWER WEB FRAME FORWARD CORNER. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 52-10-02 FIG 1, SRM 51-70
- [SDR USAA040787](https://openairdocs.org/sdr/USAA040787), Sep 12, 2004: FLOOR SUPPORT. CORRODED. PIT, Q5, FLOOR SUPPORT, 4 INCH X 3 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02 FLOOR SUPPORT, STA 986.5 RT BL0. DEFECTIVE PART REPLACED WITH IDENT PART IA
- [SDR USAA040797](https://openairdocs.org/sdr/USAA040797), Sep 12, 2004: ANGLE. CORRODED. PIT, Q5, Z-ANGLE, 4 INCHES LONG, CORROSION; LEVEL 1 TASK NR C53-107-01 AFT ENT DOOR Z-ANGLE. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG.
- [SDR USAA040824](https://openairdocs.org/sdr/USAA040824), Sep 11, 2004: KEELBEAM. CRACKED. PIT - Q5, KEEL REPAIR ANGLE, .2500 INCH CRACK, FASTENER HOLE, STA 520 ON KEELBEAM REPAIR ANGLE RT. REPAIR ANGLES/DOUBLER INSTALLED IAW SRM 51-70-11.
- [SDR USAA040803](https://openairdocs.org/sdr/USAA040803), Sep 10, 2004: SKIN. DELAMINATED. PIT, Q5, TOP SKIN AND CORE BOND, 3.5 INCH AREA. DELAMINATION, NR 4 SLAT OB END TOP SURFACE. REMOVED DAMAGE, INSTALLED NEW CORE SECTION AND DOUBLER IAW SRM 51-70
- [SDR USAA040804](https://openairdocs.org/sdr/USAA040804), Sep 10, 2004: SKIN. DELAMINATED. PIT, Q5, TOP SKIN - CORE BOND 1 INCH AREA, DELAMINATION, LT WING NR 1 SPOILER AT AFT OB CORNER - TOP SURFACE. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER
- [SDR USAA040808](https://openairdocs.org/sdr/USAA040808), Sep 10, 2004: SKIN. DELAMINATED. PIT, O5, TOP SKIN- CORE BOND, 2 INCH AREA. NR 4 SLAT IB END TOP SURFACE. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW CORE AND DOUBLER IAW SRM 51-70-10.
- [SDR USAA040807](https://openairdocs.org/sdr/USAA040807), Sep 9, 2004: SPAR. CRACKED. PIT, Q5, ANGLE SUPPORT .7500 INCH CRACK, VERT STAB SPAR ANGLE FOR RIB 163.90 FRONT LT SIDE. INSTALLED DOUBLER AND SHIM IAW EA 79100.
- [SDR USAA040806](https://openairdocs.org/sdr/USAA040806), Sep 8, 2004: SKIN. DEBONDED. PIT, Q5, TOP SKIN - CORE BOND, 3 INCH X 3 INCH AREA, DEBONDED. LT IB AFT FLAP, UPPER OB T/E. REMOVED DAMAGE, INSTALLED CORE, DOUBLER IAW TR 57-53-01A, EA 79082,
- [SDR USAA040796](https://openairdocs.org/sdr/USAA040796), Sep 5, 2004: FLOOR SUPPORT. CORRODED. PIT, Q5, FLOOR SUPPORT 1 INCH 10 INCH AREA. CORROSION; LEVEL 1; TASK NR C53-107-02 LOCATED AT STA 986.5 TO 1016, RBL 3.54 TO RBL 18.25. DEFECTIVE PART REPLACED 
- [SDR USAA040809](https://openairdocs.org/sdr/USAA040809), Sep 3, 2004: SKIN. DELAMINATED. PIT, Q5, TOP SKIN - CORE BOND, 2 INCH AREA AT NR 5 SLAT T/E; 1 AT IB END AND 1 AT OB END. REMOVED DELAMINATED AREA, INSTALLED NEW TOP SKIN IAW SRM 51-70-10.
- [SDR USAA040815](https://openairdocs.org/sdr/USAA040815), Sep 1, 2004: CLIP. CRACKED. PIT, Q5, CLIP 1 INCH CRACK, STR 19 AND STA 986 BULKHEAD. INSTALLED CLIP IAW SRM 5-40-02.
- [SDR USAA040820](https://openairdocs.org/sdr/USAA040820), Sep 1, 2004: CREASE BEAM. CRACKED. PIT, Q5, CREASE BEAM WEB 1 INCH CRACK. LT CREASE BEAM BS 616-639. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02.
- [SDR USAA050822](https://openairdocs.org/sdr/USAA050822), Sep 1, 2004: SKIN. WORN. MID FLAP L/E, 24 INCHES WORN. IB 24 INCHES ON THE LT OB MID FLAP L/E AT IB END. INSTALLED DOUBLER IAW SRM 57-53-01, FIG 208.
- [SDR USAA040783](https://openairdocs.org/sdr/USAA040783), Aug 29, 2004: STRINGER CLIP. CRACKED. PIT - Q5, TIE- .1250 INCH CRACK, RIVET, STR TO FRAME CLIP, STA 663.75-S10R. REMOVED AND REPLACED STRINGER CLIP (TIE) IAW 53-00-03.
- [SDR USAA040812](https://openairdocs.org/sdr/USAA040812), Aug 29, 2004: CLIP. CRACKED. PIT, Q5, CLIP EST. .125 INCH STA 500D S 8L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40.
- [SDR USAA040813](https://openairdocs.org/sdr/USAA040813), Aug 29, 2004: CLIP. CRACKED. PIT, Q5, CLIP EST. .125 INCH CRACK, STA 500B S 10L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40.
- [SDR USAA040814](https://openairdocs.org/sdr/USAA040814), Aug 29, 2004: CLIP. CRACKED. PIT, Q5, CLIP EST. .125 INCH CRACK, STA 440S 10L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40.
- [SDR USAA040823](https://openairdocs.org/sdr/USAA040823), Aug 29, 2004: CLIP. CRACKED. CLIP, EST. .125 INCH CRACK, STA 500D SGL. REMOVED AND REPLACED CLIP IAW SRM 51-10-02, 51-40.
- [SDR USAA040810](https://openairdocs.org/sdr/USAA040810), Aug 28, 2004: STRINGER CLIP. CRACKED. PIT, Q5, STRINGER CLIPS, .5000 INCH AND .1250 INCH CRACKS, STA 578, STR S9R. CLIP REPLACED IAW SRM 51-40-02.
- [SDR USAA040819](https://openairdocs.org/sdr/USAA040819), Aug 28, 2004: SKIN. CRACKED. PIT, Q5, SKIN WITH 1.2500 INCH CRACKS (3 EA). NR 1 SLAT, LOWER SURFACE AT ROW IB END 4TH RIVET. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.

All 151: https://openairdocs.org/deregistered/N383US-2006-07-25/reports.md

## Other aircraft with N383US

- [Registered now](https://openairdocs.org/aircraft/N383US): Aviat A-1C-200, S/N 3091, built 2010

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