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N810BW

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1980 Cessna 402C · Continental TSIO-520 series

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Registered owner
Hyannis Air Service Inc
Location
Hyannis, MA
Owner type
Corporation
Serial number
402C0279
Year built
1980
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
April 1, 1980
Certificate issued
July 25, 2011
Expires
July 31, 2027
Mode S code
AB098A
Cessna 402CAirframe model · 10 seats · 2 engines · 115 registeredTCDS A7CEAirframe · Cessna 402CTCDS E8CEEngine · Continental TSIO-520 series

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
See all 95 ADs

Information bulletins that may apply · 24

Advisory, not mandatory.

See all 25 bulletins

NTSB investigations

No NTSB investigations matched to N810BWMatched 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 · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Incident 20080305831689IOther Ground Ops · Nantucket, MA(-23) While parking the aircraft, N810BW, at the Nantucket airport gate, after engine shut-down, the pilot stated that he experienced a wind gust and the aircraft immediately and abruptly nosed-up and came down hard resting on the tail. The tail stinger was…Mar 5, 2008 · Minor damage

Service difficulty reports · 10

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

SDR HYIA20260811001Beam · crackedDURING SCHEDULED INSPECTION A CRACK WAS VISUALLY IDENTIFIED ON THE LEFT HAND CROSSOVER BEAM (OEM: 5654104-11) FORWARD FACE. THIS CRACK MEASURES APPROXIMATELY 1.375 INCHES LONG AND IS CONSISTENT WITH OTHER CRACKS VISUALLY IDENTIFIED ON THESE BEAMS IN THE PAST. Aug 4, 2026 · N810BW · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20231027002Display · failedPILOT REPORTED WEATHER RADAR WOULD NOT TURN ON AND HAD ELECTRIC BURNING SMELL IN FLIGHT. MAINTENANCE INSPECTED AND FOUND RADAR DISPLAY BURNED SMELL DURING INSPECTION. REMOVED AND REPLACED RADAR DISPLAY AND ANTENNA.Oct 27, 2023 · N810BW · Cessna 402C · Weather Radar SystemSDR HYIA20201005001Spar · crackedUPON REMOVAL OF LT WING TRAILING EDGE RIB ASSEMBLY PART NUMBER 5122053-35, A CRACK WAS IDENTIFIED AT AFT INBOARD WING SPAR ASSEMBLY. THE DAMAGE IS LOCATED AT LT WS 103.29 AND IS NOT VISIBLE WITH RIB ASSEMBLY INSTALLED. THE LT INBOARD SPAR ASSEMBLY PART NUMBEOct 1, 2020 · N810BW · Cessna 402C · Wing SparSDR HYIA20200911002Spar Cap · corrodedDURING MAINTENANCE CORROSION DAMAGE WAS IDENTIFIED ON BOTTOM FACE OF THE HORIZONTAL LEG OF THE LEFT HAND LOWER OUTBOARD SPAR CAP (P/N: 5122041-23). THIS DAMAGE IS LOCATED BETWEEN LWS 203.21 AND 212.46. AT IT'S DEEPEST THIS DAMAGE MEASURES .027 INCHES DEEP. Sep 11, 2020 · N810BW · Cessna 402C · Wing SparSDR HYIA20170828011Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED ON THE LT OUTBOARD FITTING. THE CRACK AS FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED .102 IN LENGTH.May 19, 2017 · N810BW · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20160511004Unknown · odorPILOT REPORTED BURNING SMELL FROM VENTS. INSPECTED CABIN DUCTS, CB CONSOLE, AVIONICS FAN, FOUND ALL IN GOOD CONDITION. AS PRECAUTIONARY MEASURE R & R CABIN FAN IAW MM CHAP 21-50-03.May 10, 2016 · N810BW · Cessna 402C · Air Distribution SystemSDR HYIA20150729004Relay · failedPILOT REPORTED LEFT ENGINE STARTER LIGHT ILLUMINATED. THE FLIGHT DIVERTED FROM ITS ORIGINAL DESTINATION. INSPECTED & FOUND LEFT STARTER RELAY INTERMITTENT. R & R LEFT STARTER RELAY, THE STARTER REMAINED INOPERATIVE. R & R THE LEFT ENGINE STARTER & OPERATIOJul 27, 2015 · N810BW · Cessna 402C · Engine Starting SystemSDR HYIA20150121001Unknown · odorINTERMITTENT SMELL OF ELEC OR PLASTIC CHEMICAL BURNING COMING FROM THE SWITCH BREAKER PANEL. INSPECTED PILOT SWITCH & BREAKER AREA. NO DEFECTS NOTED AT THIS TIME. R & R AVIONICS MASTER SWITCH IAW MM CHAPTER 39-40-00. OPERATIONS CHECKED GOOD.Jan 15, 2015 · N810BW · Cessna 402C · Air Distribution SystemSDR 2012FA0000701Fitting · corrodedDURING NEW ACFT CONFORMITY INSPECTION, IT WAS NOTED THAT THE LT UPPER FORWARD FUSELAGE FITTING WAS CORRODED. THE DETERMINED CORRECTIVE ACTION WAS TO REMOVE AND REPLACE WITH NEW PART. REPAIRS ARE ONGOING.Oct 17, 2012 · N810BW · Cessna 402C · Fuselage Miscellaneous StructureSDR HYIA20140414011Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, 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 BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & AApr 20, 2012 · N810BW · Cessna 402C · Landing Gear Retraction/Extension System

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