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N439PW

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2000 Raytheon C90A · Pratt & Whitney Canada PT6A-21

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Registered owner
N439pw LLC
Location
Destin, FL
Owner type
LLC
Serial number
LJ-1589
Year built
2000
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
April 13, 2020
Certificate issued
November 13, 2020
Expires
November 30, 2027
Mode S code
A545E7
Raytheon C90AAirframe model · 9 seats · 2 engines · 155 registeredTCDS 3A20Airframe · Raytheon C90ATCDS E4EAEngine · Pratt & Whitney Canada PT6A-21

From the FAA registry file of October 24, 2026.

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Airworthiness directives that may apply · 37

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

1980In forceSuperseded2026
See all 41 ADs

Information bulletins that may apply · 4

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 N439PWMatched 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 Raytheon C90A aircraft

FAA incident reports

No FAA accident or incident reports matched to N439PWMatched 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 Raytheon C90A aircraft

Service difficulty reports · 5

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

SDR E812005F00001Brace · corrodedDURING INITIAL 6 YEAR/8000 CYCLE INSPECTION OF MAIN GEAR ASSY, FOUND INTERNAL SURFACE OF UPPER BRACE PITTED AND CORRODED AT AREA IN CONTACT WITH UPPER MAIN GEAR STRUT. CORROSION APPEARS UNUSUAL FOR A CLEAN, NEWER, LOW-TIME AIRCRAFT THAT IS HANGARED IS A NON SNov 16, 2005 · N439PW · Beech C90A · Main Landing GearSDR 2005FA0001560Brace · corrodedDURING INITIAL 6-YEAR/8000 CYCLE INSPECTION OF MAIN GEAR ASSY FOUND INTERNAL SURFACE OF UPPER BRACE PITTED AND CORRODED AT AREA IN CONTACT WITH UPPER MAIN GEAR STRUT. CORROSION APPEARS UNUSUAL FOR A CLEAN, NEWER, LOW-TIME AIRCRAFT THAT IS HANGARED IN A NON SANov 16, 2005 · N439PW · Beech C90A · Main Landing GearSDR 2005FA0001559Bushing · seizedDURING COMPLIANCE WITH ELEVATOR TAB TO ACTUATOR PUSHROD INSPECTION FOR SAFETY NR 243, FOUND ELEVATOR TAB HORN BUSHING SEIZED. REPLACED TAB HORN BUSHING AND ACTUATOR PUSHROD TO HORN ATTACH BOLT BUSHING, VERIFIED TAB HORN TO ACTUATOR PUSHROD OPERATIONS NORMAL INov 16, 2005 · N439PW · Beech C90A · Elevator, Spar/RibSDR 2005FA0001558Bushing · seizedDURING COMPLIANCE WITH ELEVATOR TAB TO ACTUATOR PUSHROD INSP FOR SAFETY NR 243 FOUND ELEVATOR TAB HORN BUSHING SEIZED. REPLACED TAB HORN BUSHING AND ACTUATOR PUSHROD TO HORN ATTACH BOLT BUSHING VERIFIED TAB HORN TO ACTUATOR PUSHROD OPERATIONS NORMAL IAW SAFETNov 16, 2005 · N439PW · Beech C90A · Elevator, Tab StructureSDR 2003FA0001264Bracket · gougedDURING SCHEDULED PHASE INSPECTION NOTED OB SIDE OF RT RUDDER BOOST BRACKET AT FS 303 GOUGED DEEPLY THROUGH BY ADJACENT CABLE AT AFT END. LOCATION JUST IB OF AFT FUSELAGE ACCESS DOOR. APPEARS BRACKET HAD BEEN INSTALLED INCORRECTLY AT MFG OR HAD SOMEHOW BECOMENov 25, 2003 · N439PW · Beech C90A · Rudder Structure

STCs that may be installed · 278

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

See all 278 STCs