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N232US

Cancelled 2003

Deregistered aircraft · 1980 Boeing 737-201 · Pratt & Whitney JT8D-9 series

Open in FAA registry

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Cancelled: April 11, 2003
Exported to: Mexico
Status when cancelled: Valid registration
Serial number: 22018
Year built: 1980
Type: Fixed wing multi engine
Engine: Turbo-jet
Airworthiness: Standard, transport
Airworthiness date: December 7, 2000
Certificate issued: July 16, 2002
Last registry action: January 10, 2003
Mode S code: A211C1
Owner when cancelled: Alameda Corp Trustee
Location: San Antonio, TX
Owner type: Corporation

Airframe modelBoeing 737-201TCDS A16WE · ADs, bulletins and aircraft registered now Engine modelPratt & Whitney JT8D-9 seriesTCDS E2EA · Turbo-jet

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.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N232US and the event date: up to this one’s cancellation.

Incident 19910314012179IFcd/Prec Ldg From Cruise · Indianapolis, INExperienced a cracked outer windshield. Reduced pressurization and diverted to Indianapolis.Mar 14, 1991 · Minor damage

Service difficulty reports · 35

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

SDR USAA010642Skin · crackedTPA - FOUND SKIN CRACKED BETWEEN STATION 727A AND 727B BELOW 13L. INSTALLED DUOBELR PER SRM USING BLIND FASTENERS PER SRM 53-30-3 FIG 1 AND MPP 308-25. (M)Jun 11, 2001 · N232US · Boeing 737201 · Fuselage Structure (General)SDR USAA010643Skin · crackedTPA - FOUND SKIN CRACKED 2.5 INCH AND 2.75 INCH, STATION 873 AND 885 ABOVER 19R. INSTALLED DOUBLER .063 INCH CLAD 2024TB USING BLIND FASTENERS PER SRM 53-30-3 FIG 1. (M)Jun 11, 2001 · N232US · Boeing 737201 · Fuselage Main, Plate/Skin SDR USAA010679Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, BETWEEN BS 727A AND 727B, BELOW S13L. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER USING BLIND FASTENERS PER SRM 53-30-3 FIG 1. (M)Jun 10, 2001 · N232US · Boeing 737201 · Fuselage Structure (General)

See all 35 reports