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N83PB

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1980 Cessna 402C · Continental TSIO-520 series

Open in FAA registry

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Registered owners
Hyannis Air Service Inc DBACape Air
Location
Hyannis, MA
Owner type
Corporation
Serial number
402C0350
Year built
1980
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
November 13, 1980
Certificate issued
October 24, 2018
Expires
October 31, 2028
Mode S code
AB5748
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 N83PBMatched 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 19991107036499ILevel Off Touchdown · Christiansted, U.S. Virgin Islands(-23) Upon landing at stx the nose gear collapsed. Passengers and crew evacuated the aircraft safely with no injuries. It was found that the nose gear dragged brace failed.Nov 7, 1999 · Minor damage

Service difficulty reports · 24

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

SDR HYIA20220511002Rib · crackedWHILE PERFORMING OTHER MAINTENANCE, A CRACK WAS DISCOVERED IN THE LEFT CLOSE OUT RIB. THIS CRACK EXTENDS VERTICALLY THROUGH TWO FASTENERS HOLES IN THE FIRST ROW OF ATTACH HI-LOKS BETWEEN THE AFT TRUNNION SUPPORT AND THE CLOSE OUT RIB. THE CRACK EXTENDS BETWEMay 11, 2022 · N83PB · Cessna 402C · Fuselage Main, StructureSDR HYIA20220511001Spar Cap · corrodedWHILE PERFORMING OTHER MAINTENANCE, CORROSION WAS IDENTIFIED ON THE LEFT HAND AFT LOWER OUTBOARD SPAR CAP (P/N 5122041-23) AT WING STATION 222.0 TO 229.71. THE DEEPEST AREA OF CORROSION WAS MEASURED AT .033. THIS SPAR CAP WAS REPLACED WITH A FACTORY NEW PARMay 11, 2022 · N83PB · Cessna 402C · Fuselage Main, StructureSDR HYIA20190401001Trim Tab · delaminatedPILOT REPORTED "AILERON TRIM TAB EXPLODED IN FLIGHT" INITIAL INSPECTION FOUND THE AILERON TRIM TAB TOP SKIN TO BE DE-LAMINATED FROM THE FORWARD EDGE. MAINTENANCE INSPECTED AND FOUND THE DAMAGE LIMITED TO THE AILERON TRIM TAB, THE TAB WAS REPLACED WITH NO FURTHMar 29, 2019 · N83PB · Cessna 402C · Aileron Tab Control System
See all 24 reports

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