# N371US: 1984 Boeing 737-3B7, registration cancelled 2006-03-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 28, 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: 22950
- Year built: 1984
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 30, 1985
- Certificate issued: April 25, 2002
- Last registry action: May 19, 2005
- Mode S code: A43955
- 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/N371US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=371US
- Page: https://openairdocs.org/deregistered/N371US-2006-03-28

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 (86, newest 50)

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

- [SDR SB05065](https://openairdocs.org/sdr/SB05065), May 28, 2005: POWER SUPPLY. INOPERATIVE. CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHT BATTERY PACK AT LOCATION M1135 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPERATIONAL CHECK 
- [SDR USAASB04040](https://openairdocs.org/sdr/USAASB04040), Mar 30, 2004: BATTERY PACK. INOPERATIVE. PIT - MAINTENANCE REPORTED THE MID CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLCED THE BATTERY PACK. OPS CHECK GOOD. (M)
- [SDR USAASB03214](https://openairdocs.org/sdr/USAASB03214), Dec 13, 2003: POWER SUPPLY. INOPERATIVE. MAINTENANCE REPORTED THE LT OVERWING HATCH EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK, P/N 2013-1A. OPS CHE
- [SDR USAASB03207](https://openairdocs.org/sdr/USAASB03207), Nov 24, 2003: CHARGER. INOPERATIVE. MAINTENANCE REPORTED THE LT OVERWING EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY PACK, P/N 2013-1A. OPS CH
- [SDR USAA030026](https://openairdocs.org/sdr/USAA030026), Mar 9, 2003: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 2 INCH, BS 727E AND S24R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)
- [SDR USA2002F00072](https://openairdocs.org/sdr/USA2002F00072), Jul 30, 2002: MODULE. FAULTY. ON DESCENT, THE FIRE WARNING ANNUNCIATOR ON THE GLARESHIELD ILLUMINATED. CREW COULD NOT CANCEL THE LIGHT. NO OTHER INDICATIONS OF FIRE WAS NOTED. FIRE DETECTION
- [SDR USAA020211](https://openairdocs.org/sdr/USAA020211), Jun 1, 2002: FRAME. CORRODED. TPA - FOUND FRAME CORRODED 3 INCH BY 1.5 INCH AREA, STATION 251.6 RIGHT SIDE NOSE W/W AREA. CORROSION LEVEL 2, TASK NR C53-100-01. FABRICATED NEW PARTS PER SRM,
- [SDR USAASB02044](https://openairdocs.org/sdr/USAASB02044), Mar 7, 2002: LIGHT. INOPERATIVE. PHL - MAINTENANCE REPORTED THE FLOOR LEVEL EMERGENCY LIGHT AT SEAT ROW 5 ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT ROW 5 ABC.
- [SDR USAASB01333](https://openairdocs.org/sdr/USAASB01333), Dec 2, 2001: BATTERY PACK. DISCHARGED. PIT - MAINTENANCE FOUND THE MID CABIN, CENTER OVERHEAD EMERGENCY EXIT LIGHT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)
- [SDR USAA010894](https://openairdocs.org/sdr/USAA010894), Jul 20, 2001: SKIN PANEL. BUCKLED. CLT - FOUND SKIN PANEL BUCKLED APPROXIMATELY 3 SQUARE INCHES, KEEL BEAM STATION 663 TO 685. REMOVED AND REPLACED KEEL BEAM LOWER PANEL PER SRM 51-10-02. (M)
- [SDR USAA010895](https://openairdocs.org/sdr/USAA010895), Jul 20, 2001: FITTING. CORRODED. CLT - FOUND FITTING CORRODED 3 INCHES BY 2 INCH AREA, BS 727, STRINGER 27R, AFT CARGO COMPARTMENT. CORROSION LEVEL 2 TASK NR C53-202-01. FABRICATED AND INSTALLE
- [SDR USAA010905](https://openairdocs.org/sdr/USAA010905), Jul 20, 2001: ATTACH FITTING. CORRODED. CLT - FOUND UPPER ATTACH LUGS APPROX .5 INCH TOTAL AREA, CORRODED, LEFT HORIZONTAL STABILIZER CENTER SECTION, FRONT SPAR. REAMED CLEVIS TO REMOVE CORROSION, MAC
- [SDR USAA010904](https://openairdocs.org/sdr/USAA010904), Jul 20, 2001: ATTACH FITTING. CORRODED. CLT - FOUND LUG ATTACH FITTING CORRODED APPROX 5 INCH AREA, LEFT HORIZONTAL STABILIZER CENTER SECTION, REAR SPAR FORWARD LUG, FORWARD FACE. LUG SPOT FACED TO DE
- [SDR USAA010903](https://openairdocs.org/sdr/USAA010903), Jul 20, 2001: ATTACH FITTING. CORRODED. CLT - FOUND ATTACH LUG FITTING CORRODED .75 INCH TOTAL SURFACE AREA, LEFT HORIZONTAL STABILIZER CENTER SECTION, FRONT LOWER FORWARD LUG. CORROSION REMOVED, FABR
- [SDR USAA010902](https://openairdocs.org/sdr/USAA010902), Jul 20, 2001: SHEAR TIE. CORRODED. CLT - FOUND FRAME SHEAR TIE CORRODED .5 INCH BY .5 INCH, BS 947.5, BETWEEN S27L AND S26L. CORROSION LEVEL 1, TASK NR C53-208-01. REMOVED AND REPLACED SHEAR TIE 
- [SDR USAA010901](https://openairdocs.org/sdr/USAA010901), Jul 20, 2001: SHEAR TIE. CORRODED. CLT - FOUND FRAME SHEAR TIE CORRODED 14 INCH AREA, BS 727A, LBL 7 AND RBL 7. CORROSION LEVEL 1 TASK NR C53-202-01. REMOVED AND REPLACED SHEAR TIE PER SRM 51-10-
- [SDR USAA010900](https://openairdocs.org/sdr/USAA010900), Jul 20, 2001: KEELBEAM. CORRODED. CLT - FOUND KEEL BEAM CHORD CORRODED 6 INCHES BY 2 INCHES, BS 500C PLUS 9 TO 500D, RBL 7. DAMAGE REMOVED, INSTALLED REPAIR ANGLES PER SRM 53-30-12 FIG 202, EA 6
- [SDR USAA010899](https://openairdocs.org/sdr/USAA010899), Jul 20, 2001: KEELBEAM. CORRODED. CLT - FOUND KEEL BEAM STRINGER CORRODED 3 INCHES BY 4 INCH AREA, BS 727D TO E, LEFT KEEL BEAM. CORROSION LEVEL 2, TASK NR C53-202-01. REMOVED KEEL BEAM, REMOVED
- [SDR USAA010898](https://openairdocs.org/sdr/USAA010898), Jul 20, 2001: FRAME. CORRODED. CLT - FOUND FRAME CORRODED 14 INCH AREA, BS 727B, LEFT AND RIGHT KEEL BEAMS, LOWER FLANGE. REMOVED DAMAGE, INSTALLED NEW FRAME SECTION PER SRM 51-40-02 AND 51-4
- [SDR USAA010987](https://openairdocs.org/sdr/USAA010987), Jul 20, 2001: KEELBEAM. CORRODED. CLT - FOUND LOWER CHORD OUTBOARD FLANGE CORRODED 1 INCHES BY 22 INCH, BS 673-695 RIGHT, BS 693-727 KEEL BEAMS. CORROSION LEVEL 2 TASK C53-100-01. REMOVED DAMAGE
- [SDR USAA010896](https://openairdocs.org/sdr/USAA010896), Jul 20, 2001: KEELBEAM. CORRODED. CLT - FOUND KEEL BEAM CORRODED 5 SQUARE INCHES, BS 767, RIGHT KEEL BEAM SPLICE. CORROSION LEVEL 2 TASK NR C53-202-01. REMOVED KEEL BEAM, REMOVED CORROSION, REIN
- [SDR USAA010893](https://openairdocs.org/sdr/USAA010893), Jul 19, 2001: FRAME. CORRODED. CLT - FOUND Z-CHORD CORRODED 4 INCHES BY 1 INCH AREA, BS 270, RBL 6. DAMAGED REMOVED, INSTALLED Z-CHORD REPAIR KIT PER TR 53-20-08. (M)
- [SDR USAA010892](https://openairdocs.org/sdr/USAA010892), Jul 19, 2001: FRAME. CORRODED. CLT - FOUND FRAME CHORD CORRODED 1 INCHES BY 3 INCHES, BS 500D, RBL 7, FORWARD CARGO FLOOR. CORRODED LEVEL 1 TASK NR C53-208-01. DAMAGE REMOVED, INSTALLED REPAI
- [SDR USAA010891](https://openairdocs.org/sdr/USAA010891), Jul 19, 2001: CHANNEL. CORRODED. CLT - FOUND CHANNEL CORRODED 5 SQUARE INCH AREA CORRODED, AFT CARGO DOOR, LOWER WILL STRUCTURE. REMOVED AND REPLACED CHANNEL PER SRM 51-10-01 AND 51-10-02. (M)
- [SDR USAA010890](https://openairdocs.org/sdr/USAA010890), Jul 19, 2001: ANGLE. CORRODED. CLT - FOUND Z-ANGLE CORRODED 4 INCHES BY 40 INCHES AFT ENTRY DOOR SILL. CORROSION LEVEL 1, TASK C53-202-01. REMOVED AND REPLACED Z-ANGLE PER SRM 51-40-02. (M)
- [SDR USAA010889](https://openairdocs.org/sdr/USAA010889), Jul 19, 2001: FRAME. CORRODED. CLT - FOUND FRAME CORRODED 10 INCHES BY 1 INCH AREA, BS 807 LBL 5 TO RBL 5, AFT CARGO. REMOVED DAMAGE, INSTALLED REPAIR DOUBLER PER SRM 53-00-07 AND 51-40-02. (
- [SDR USAA010888](https://openairdocs.org/sdr/USAA010888), Jul 19, 2001: SHEAR TIE. CORRODED. CLT - FOUND SHEAR TIE CORRODED 1 INCH BY 5 INCH AREA, BS 807, BETWEEN RBL 15 TO 20, AT BELLY SKIN LEVEL. FABRICATED AND REPLACED SHEAR TIE PER SRM 51-10-01 AND 
- [SDR USAA010887](https://openairdocs.org/sdr/USAA010887), Jul 19, 2001: STRINGER. CORRODED. CLT - FOUND STRINGER CORRODED 14 INCHES BY 2.5 INCHES, BS 907 TO 927, S25L, BELOW AFT CARGO FLOOR. REMOVED AND REPLACED STRINGER PER SRM 51-40-02. (M)
- [SDR USAA010886](https://openairdocs.org/sdr/USAA010886), Jul 19, 2001: STRINGER. CORRODED. CLT - FOUND STRINGER CORRODED 6 INCHES BY 1 INCH AREA, BS 1006 TO 1016, STRINGER 26R. REMOVED DAMAGE, SPLICED IN NEW STRINGER SECTION PER SRM 51-40-04 AND BAC D
- [SDR USAA010885](https://openairdocs.org/sdr/USAA010885), Jul 19, 2001: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 4 INCHES BY 2 INCH AREA, BS 1006, LBL 8 TO LBL 12. REPLACED UPPER T-CAP PER EA 69770 AND TR 53-10-05A. (M)
- [SDR USAA010883](https://openairdocs.org/sdr/USAA010883), Jul 19, 2001: FRAME. CORRODED. CLT - FOUND FRAME CORRODED 6 SQUARE INCH AREA, BS 1006, STRINGER 23R TO FLOOR LEVEL. CORROSION LEVEL 1 TASK NR C53-107-02. REMOVED DAMAGE, INSTALLED REPLACEMENT
- [SDR USAA010881](https://openairdocs.org/sdr/USAA010881), Jul 19, 2001: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH AREA, BS 1016 LBL 6 TO LBL 34. CORROSION LEVEL 1, TASK NR C53-202-01. REMOVED AND REPLACED T-CAP PER TYPICAL REP
- [SDR USAA010874](https://openairdocs.org/sdr/USAA010874), Jul 18, 2001: FRAME. DENTED. CLT - FOUND FRAME UPPER FLANGE DENTED, 1 INCH LONG, BS 747 RBL 24 AFT CARGO FLOOR. DAMAGE REMOVED, INSTALLED DOUBLER PER TYPICAL REPAIR 53-60-07. (M)
- [SDR USAA010875](https://openairdocs.org/sdr/USAA010875), Jul 18, 2001: BULKHEAD. GOUGED. CLT - FOUND BULKHEAD WEB GOUGED .016 INCH DEEP BY .150 INCH LONG, BS 178 WL 176 LBL 5.5. TRIMMED OUT DAMAGE, INSTALLED REPAIR DOUBLER PER EO 5300V153 AND EA 697
- [SDR USAA010878](https://openairdocs.org/sdr/USAA010878), Jul 18, 2001: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 18 INCH AREA, BS 986.5, BL 0 TO RBL 18. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED AND REPLACED T-CAP PER TYPICAL REPAIR 53-1
- [SDR USAA010877](https://openairdocs.org/sdr/USAA010877), Jul 18, 2001: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED, ENTIRE LENGTH OF FLOORBEAM, BS 294.5 STRINGER 17L TO 17R. CORROSION LEVEL 1, TASK NR C53-107-02. DAMAGE REMOVED, INSTALLED DOUBL
- [SDR USAA010876](https://openairdocs.org/sdr/USAA010876), Jul 18, 2001: ANGLE. CORRODED. CLT - FOUND CREASEBEAM ANGLE CORRODED 40 INCHES, BS 947.5 AFT SERVICE DOOR FRAME. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED AND REPLACED Z-ANGLE AND WEB PE
- [SDR USAA010809](https://openairdocs.org/sdr/USAA010809), Jul 16, 2001: FRAME. CRACKED. CLT - FOUND SIDE CHORD CRACKED TWO PLACES, 1.75 INCHES ON LEFT SIDE, 1 INCH ON RIGHT SIDE, BS 178, WL 207, LEFT AND RIGHT SIDE. DAMAGE REMOVED, SPLICED IN NEW R
- [SDR USAA010812](https://openairdocs.org/sdr/USAA010812), Jul 16, 2001: PRESSURE PANEL. CRACKED. CLT - FOUND FLOORWEB CRACKED TWO PLACES .5 INCH, BS 178 WL 207, LEFT AND RIGHT SIDE. REMOVED AND REPLACED FLOORWEB PER EO 5300V157 AND SRM 51-10-2. (M)
- [SDR USAA010814](https://openairdocs.org/sdr/USAA010814), Jul 16, 2001: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, BS 807, BETWEEN STRINGER 8 AND 9R. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14. (M)
- [SDR USAA010824](https://openairdocs.org/sdr/USAA010824), Jul 16, 2001: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED TWO PLACES .25 INCH, BS 663, STRINGER 10R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA010826](https://openairdocs.org/sdr/USAA010826), Jul 16, 2001: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, BS 887 BETWEEN STRINGER 8 AND 9L. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M)
- [SDR USAA010828](https://openairdocs.org/sdr/USAA010828), Jul 16, 2001: FRAME. CRACKED. CLT - FOUND FRAME CRACKED APPROXIMATELY .25 INCH, BS 847, BETWEEN STRINGER 8 AND 9L. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M)
- [SDR USAA010829](https://openairdocs.org/sdr/USAA010829), Jul 16, 2001: FRAME. CRACKED. CLT - FOUND FRAME CRACKED APPROX .25 INCH, BS 847, BETWEEN STRINGER 8 AND 9R. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M)
- [SDR USAA010830](https://openairdocs.org/sdr/USAA010830), Jul 16, 2001: SKIN. CRACKED. CLT - FOUND FUSELAGE SKIN CRACKED .25 INCH, BS 727C, STRINER 24L. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER SRM 53-00-01, FIG 225. (M)
- [SDR USAA010831](https://openairdocs.org/sdr/USAA010831), Jul 16, 2001: FRAME. CRACKED. CLT - FOUND FRAME CRACKED 1 INCH, BS 616, RIGHT CREASE BEAM, INNER CHORD ANGLE. DAMAGE REMOVED, INSTALLED REPAIR ANGLE AND FILLER PER TYPICAL REPAIR 53-62-01. (
- [SDR USAA010832](https://openairdocs.org/sdr/USAA010832), Jul 16, 2001: DOOR FRAME. CRACKED. CLT - FOUND DOOR FRAME CRACKED TWO PLACES 1 INCH EACH, BS 294.5, RBL 55, STRINGER 17R. INSTALLED REPAIR DOUBLER PER SRM 51-70-11. (M)
- [SDR USAA010833](https://openairdocs.org/sdr/USAA010833), Jul 16, 2001: ANGLE. CRACKED. CLT - FOUND SUPPORT ANGLE CRACKED 5 INCHES, BS 290 TO 294.5, RBL 55, INBOARD CREASE BEAM ANGLE. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-01-02. (M)
- [SDR USAA010834](https://openairdocs.org/sdr/USAA010834), Jul 16, 2001: FRAME. CRACKED. CLT - FOUND FRAME CRACKED 3 INCHES, BS 954, BETWEEN STRINGER 9 AND 10R, INNER RADIUS. DAMAGE REMOVED, INSTALLED NEW PARTS PER SRM 51-40-03, 51-40-02 AND BAC DRA
- [SDR USAA010835](https://openairdocs.org/sdr/USAA010835), Jul 16, 2001: SKIN. CRACKED. CLT - FOUND FUSELAGE SKIN CRACKED .8 INCH, BETWEEN BS 727D AND E, BL 0. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER SRM 51-10-2, 51-20-01, 51-40-00 AND 53-00-0

All 86: https://openairdocs.org/deregistered/N371US-2006-03-28/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 19900206005389I](https://openairdocs.org/incident/19900206005389I), Feb 6, 1990: Boeing 7373B7 (N371US), Indianapolis, IN. Unable to extend right gear. Emergency procedures corrected problem. Landed safely. Lubricated gear.

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