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N261GB

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1985 Beech C90A · Pratt & Whitney Canada PT6A-60A

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Registered owner
Safford Aviation Service Inc
Location
Coolidge, AZ
Owner type
Corporation
Serial number
LJ-1119
Year built
1985
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
April 14, 1986
Certificate issued
November 2, 2015
Expires
November 30, 2028
Mode S code
A2834C
Beech C90AAirframe model · 9 seats · 2 engines · 125 registeredTCDS 3A20Airframe · Beech C90ATCDS E4EAEngine · Pratt & Whitney Canada PT6A-60A

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 34

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1987In forceSuperseded2026
See all 38 ADs

Information bulletins that may apply · 5

Advisory, not mandatory.

Historical bulletins · 2
SAIB CE-10-34R1Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and 89-25-08Issued Aug 20, 2013SAIB CE-10-34Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and AD 89-25-08Issued May 18, 2010

NTSB investigations

No NTSB investigations matched to N261GBMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Beech C90A aircraft

FAA incident reports

No FAA accident or incident reports matched to N261GBMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Beech C90A aircraft

Service difficulty reports · 2

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

SDR 2008FA0000763Solenoid Valve · stuckINVESTIGATED PILOT REPORT OF RUDDER BOOST CONSTANTLY KICKING TO LEFT. FOUND PN 717 LT SOLENOID VALVE STUCK IN OPEN POSITION. ALSO FOUND (3) PN AN9181D RUDDER BOOST CONTROL SYSTEM CROSS FITTING CRACKED AND WATER IN SYSTEM. PURGED WATER FROM SYSTEM AND REPLACOct 8, 2008 · N261GB · Beech C90 · Rudder Control SystemSDR 2006FA0000649Switch · out of limitsDURING SCHEDULED 12 MONTH TEST OF CABIN ALTITUDE WARNING SYSTEM FOUND BAROMETRIC SWITCH OPERATING OUT OF SPECIFIED MM. REPLACED PN 1013384028-3 SWITCH ASSY. CABIN ALTITUDE WARNING TESTS WITHIN SPECIFIED SERVICE LIMITS ON RETEST. SUGGEST A SB BE ISSUED TO REJun 22, 2006 · N261GB · Beech C90 · Cabin Pressure Control System

STCs that may be installed · 266

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 266 STCs