Registered owner
Hyannis Air Service Inc
Location
Hyannis, MA
Owner type
Corporation
Serial number
402C0109
Year built
1979
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
October 6, 1999
Certificate issued
September 14, 2000
Expires
April 30, 2028
Mode S code
A4B20A

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.

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Airworthiness directives that may apply · 79

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: 85 ADs
19691
19701
19711
19722
19751
19762
19771
19792
19804
19812
19821
19841
19851
19872
19884
19892
19903
19911
19921
19933
19952
19961
19971
19985
19992
20003
20041
20055
20072
20081
20092
20102
20112
20123
20141
20151
20163
20171
20182
20201
20222
20236
See all 95 ADs

Information bulletins that may apply · 24

Advisory, not mandatory.

See all 25 bulletins

NTSB investigations

No NTSB investigations matched to N401TJMatched 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 402C aircraft

FAA incident reports

No FAA accident or incident reports matched to N401TJMatched 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 402C aircraft

Service difficulty reports · 15

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

SDR HYIA20201030001Fitting · crackedDURING MAINTENANCE A CRACK WAS IDENTIFIED ON THE INBOARD LEG OF THE LEFT HAND OUTBOARD NACELLE FITTING, (P/N: 5292029-23). THIS CRACK MEASURES APPROXIMATELY .170 INCHES LONG AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEOct 30, 2020 · N401TJ · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20200904002Control Cable · brokenTHE PILOT REPORTED THAT THE RIGHT PROPELLER RAN AWAY IN FLIGHT, BUT DID NOT OVERSPEED. MAINTENANCE INSPECTED AND FOUND THAT THE PROPELLER CONTROL CABLE HAD BROKEN. REMOVED AND REPLACED RT PROPELLER CONTROL CABLE ASSEMBLY. NO FURTHER DEFECTS NOTED.Sep 2, 2020 · N401TJ · Cessna 402C · Propeller Controlling SystemSDR HYIA20161205001Exhaust Valve · failedPILOT REPORTED "LEFT ENGINE RUNNING ROUGH AND WON'T IDLE BELOW 500 RPM". UPON INSPECTION MAINTENANCE FOUND THE NR 5 CYLINDER WAS READING ZERO COMPRESSION DUE TO AN EXHAUST VALVE CRACKED IN HALF. MAINTENANCE REPLACED THE CYLINDER AND PISTON ASSEMBLY WITH NO FURDec 1, 2016 · N401TJ · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161102001Torque Tube · brokenPILOT REPORTED THE BRAKES FAILED PRIOR TO DEPARTURE. DURING INSPECTION, MAINTENANCE FOUND THE BRAKE PEDAL TORQUE TUBE CRACKED & BROKEN, REMOVED AND REPLACED TORQUE TUBE ASSEMBLY. NO FURTHER DEFECTS WERE NOTED.Oct 27, 2016 · N401TJ · Cessna 402C · Landing Gear Brake SystemSDR HYIA20160902112Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Aug 29, 2016 · N401TJ · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20150827001Door · openPILOT REPORTED CREW DOOR IN FLIGHT UNLATCHED & CAME OPEN. INSPECTED THE DOOR LATCH MECHANISM WITH NO DEFECTS NOTED. DAMAGE NOTED AT FWD HINGE & REPAIRED AS NECESSARY. CREW WAS UNABLE TO VERIFY IF THE DOOR WARNING LIGHT HAD ILLUMINATED DURING FLIGHT.Aug 24, 2015 · N401TJ · Cessna 402C · Passenger/Crew DoorsSDR HYIA20150206001Wire Harness · chafedPILOT REPORTED SEEING SMOKE FROM RT ENG ON SHUT DOWN. FURTHER INVESTIGATION FOUND CHAFED WIRE HARNESS IN RT ENG BAY. ACFT IS CURRENTLY IN MX REPAIRING & REPLACING AFFECTED WIRING.Feb 1, 2015 · N401TJ · Cessna 402C · Powerplant System WiringSDR HYIA20140529116Control Cable · frayedDURING A PRE-FLIGHT INSPECTION THE PILOT REPORTED CAPTAINS CONTROL YOKE HAS A SPONGY FEEL WHEN PULLED AFT. MAINTENANCE INSPECTED & FOUND THE RT ELEVATOR CABLE, PN 5200008-31CR, FRAYED AT FS 112.07, ALONG WITH DAMAGE TO THE AILERON CABLE GUARD PIN PN NAS427K22.May 23, 2014 · N401TJ · Cessna 402C · Elevator Control SystemSDR HYIA20140415033Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OMar 11, 2011 · N401TJ · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415010Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 27, 2011 · N401TJ · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA401TJ REV 1Gyro · unreliableIFR CONDITION, CREW REPORTED HORIZONTAL SITUATION INDICATOR UNRELIABLE IN SLAVE AND UN-SLAVED MODE. CREW ELECTED TO RETURN, LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED KG-102 REMOTE GYRO. SYSTEM CHECKED OK. RELEASED BACK TO SERVICE.May 12, 2009 · N401TJ · Cessna 402C · Directional Gyro and Indicating SystemSDR HYIA401TJAGyro · unreliableIFR CONDITIONS, CREW REPORTED HORIZONTAL SITUATION INDICATOR UNRELABLE IN SLAVE AND UN-SLAVE MODE. CREW ELECTED TO RETURN, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT.May 12, 2009 · N401TJ · Cessna 402C · Directional Gyro and Indicating SystemSDR HYIA401TJRelay · burnedSMOKE COMING OUT OFF THE COCKPIT. MAINTENANCE INSPECTED FOUND RIGHT ENGINE'S STARTER RELAY HAD FAILED. MAINTENANCE REMOVED AND REPLACED RELAY RETURNED AIRCRAFT TO SERVICE.Dec 25, 2008 · N401TJ · Cessna 402C · Engine Starting System WiringSDR 1350527N401TCircuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH.Aug 19, 2006 · N401TJ · Cessna 402C · Electrical Power SystemSDR 20010205CW004Fitting · corrodedAFT SPAR REAR TOP WING ATTACH FITTING CORRODED. INSTALLED NEW FITTING.Jan 5, 2001 · N401TJ · Cessna 402C · Wing, Attach Fittings

STCs that may be installed · 321

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

See all 321 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N401TJ before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.