Registered owner
Conquest 425jh LLC
Location
Bow, WA
Owner type
LLC
Serial number
425-0124
Year built
1981
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
September 7, 2000
Certificate issued
December 15, 2008
Expires
January 31, 2029
Mode S code
A50F02

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 16

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

1984In forceSuperseded2026
ADs by the year they took effect: 17 ADs
19842
19861
19941
19961
19971
19983
20012
20053
20182
20231
See all 17 ADs

Information bulletins that may apply · 8

Advisory, not mandatory.

Historical bulletins · 1

NTSB investigations

No NTSB investigations matched to N425JHMatched 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 Cessna 425 aircraft

FAA incident reports

No FAA accident or incident reports matched to N425JHMatched 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 Cessna 425 aircraft

Service difficulty reports · 6

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

SDR 2009FA0000193Line · cutPREVIOUSLY REPORTED TO MFG, DURING THE SUPPLEMENTAL INSP FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUPPLEMENTAL INSP NR 57-10-14 CARRY-THRU FWD SPAR CAP, FOUND MULTIPLE PNEUMATIC LINES SPLICED TOGETHER WITH STANDARD MIL-SPEC HOSE ON LT AND RT WINGS.Sep 2, 2008 · N425JH · Cessna 425 · Pneumatic Distribution SystemSDR 2009FA0000160Hinge · corrodedPREVIOUSLY REPORTED TO MFG DURING SUPPLEMENTAL INSPECTION FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUPPLEMENTAL INSP NR 52-10-01 CABIN DOOR RETENTION FOUND HARDWARE UNABLE TO REMOVE FROM UPPER CABIN DOOR DUE TO CORROSION. DRILLED OFF UPPER AND LOWSep 2, 2008 · N425JH · Cessna 425 · Passenger/Crew DoorsSDR 2009FA0000140Bellcrank · crackedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. NOSE GEAR STEERING BELLCRANK PN 5942001-1 FAILED NDT IAW SUPPLEMENTAL INSPECTION 32-50-00. REPLACED BELLCRANK WITH PN 594Sep 2, 2008 · N425JH · Cessna 425 · Landing Gear Steering SystemSDR 2009FA0000133Strut · crackedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. NOSE GEAR FORK FAILED NDT IAW SUPPLEMENTAL INSPECTION 32-20-02. REPLACED NOSE STRUT ASSEMBLY PN 5842000-230.Sep 2, 2008 · N425JH · Cessna 425 · Nose/Tail Landing Gear Strut/AxleSDR 2009FA0000122Torque Tube · corrodedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN THE SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. FOUND RUDDER TORQUE TUBE RUSTED DURING INSPECTION OF SUPPLEMENTAL INSPECTION 27-20-04. REPLACED TORQUE TUBE PN 583301Sep 2, 2008 · N425JH · Cessna 425 · Rudder Control SystemSDR 2009FA0000105Attach Fitting · corrodedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE LWR RT WING AFT ATTACH FITTING PN 5011024-2 FAILED NDT INSPECTION. REPLACED WING FITTING.Sep 2, 2008 · N425JH · Cessna 425 · Wing Miscellaneous Structure

STCs that may be installed · 161

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

See all 161 STCs