Registered owner
Murray Co
Location
Compton, CA
Owner type
Corporation
Serial number
340A0476
Year built
1978
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
March 17, 1978
Certificate issued
July 28, 2016
Expires
July 31, 2029
Mode S code
A840D9

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental TSIO-520 model are included below.

On this page

Airworthiness directives that may apply · 89

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

1969In forceSuperseded2026
ADs by the year they took effect: 91 ADs
19691
19701
19711
19722
19751
19761
19772
19783
19792
19806
19813
19822
19851
19872
19885
19892
19903
19911
19934
19941
19952
19962
19971
19985
19991
20002
20012
20042
20053
20072
20081
20092
20102
20112
20122
20142
20163
20201
20223
20236
20261
See all 100 ADs

Information bulletins that may apply · 19

Advisory, not mandatory.

See all 20 bulletins

NTSB investigations

No NTSB investigations matched to N6305XMatched 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 340A aircraft

FAA incident reports

No FAA accident or incident reports matched to N6305XMatched 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 340A 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 2025FA0000646Intake Duct · rupturedR/H ENGINE MP WILL NOT GO OVER 32 INCHES ABOVE 15,000. PRESSURE TESTED THE RH ENGINE INTAKE SYSTEM AND FOUND THE REAR INTAKE PIPE TORN.Sep 16, 2025 · N6305X · Cessna 340A · Engine Air Intake SystemSDR 2021FA0000032Bellcrank · crackedAFTER DISCOVERING FAILED RH MLG IDLER BELLCRANK, P/N 0841106-6, DECIDED TO PERFORM NDI INSPECTION OF LH MLG IDLER BELLCRANK P/N 0841106-5. MULTIPLE CRACK INITIATION POINTS WERE FOUND IN THE SAME AREA AS THE FAILED LINKFeb 4, 2021 · N6305X · Cessna 340A · Landing Gear Retraction/Extension SystemSDR 2021FA0000033Bellcrank · crackedR/H INNER GEAR DOOR BELLCRANK IDLER HAD BROKEN IN TWO PIECES. CUSTOMER BOUGHT A NEW PART WITH HIM TO INSTALL. BREAKAGE LOOKED CLEAN WITH NO CORROSION AT THE BREAKAGE SURFACE. IN CONVERSATION WITH CUSTOMER, WE HAD THE LEFT SIDE REMOVED AND CHECKED IT IN SAME ARFeb 3, 2021 · N6305X · Cessna 340A · Landing Gear Door Retract SectionSDR 2021FA0000025Bellcrank · brokenAFTER LANDING ON POSTFLIGHT WALK AROUND, DISCOVERED RT INBOARD GEAR DOOR OPEN. FOUND BELLCRANK ASSEMBLY IDLER RT, P/N 0841106-6 FAILED AT ARM THAT ATTACHES TO DOOR ACTUATOR CRANK ASSEMBLY.Jan 27, 2021 · N6305X · Cessna 340A · Landing Gear Door Retract SectionSDR ANCF2014FA0000376Resistor · burnedDURING ANNUAL INSPECTION, FOUND HEATER BLOWER LOW SPEED RESISTOR, BURNED. ATTACHED WIRE INSULATION WAS BURNED BACK ABOUT TWO INCHES . FOUND HEAT DAMAGE TO MOUNTING SURFACE. REPLACED RESISTOR AND WIRING.Jun 9, 2014 · N6305X · Cessna 340A · Electrical Power System Wiring

STCs that may be installed · 357

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

See all 357 STCs