Registered owner
Wright Air Service Inc
Owner type
Corporation
Serial number
1438
Year built
1970
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
September 30, 1977
Certificate issued
January 30, 2020
Expires
January 31, 2030
Mode S code
A98764

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming GO-480 model are included below.

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Airworthiness directives that may apply · 20

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

1962In forceSuperseded2026
ADs by the year they took effect: 19 ADs
19621
19691
19701
19771
19791
19811
19821
19911
19921
19971
19981
20031
20041
20051
20061
20121
20222
20231
See all 21 ADs

Information bulletins that may apply · 5

Advisory, not mandatory.

NTSB investigations · 2

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

FAA incident reports · 3

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

Service difficulty reports · 5

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

SDR HYTA201606060001Relief Valve · backed outA DISCREPANCY WAS NOTED BY PILOT OF HIGH OIL PRESSURE, A MECHANIC WAS SOON DISPATCHED TO TURN THE OIL PRESSURE DOWN. HE TURNED DOWN THE OIL PRESSURE FROM THE OIL RELIEF VALVE AND REINSTALLED IAW ENGINE MFG DATA, WHEN COMPLETE HE PERFORMED AN OPS AND LEAK CHECJun 6, 2016 · N713C · Helio H295 · Reciprocating Engine Oil SystemSDR HYTA20150904001Structure · crackedCRACKS FOUND IN CARRY THRU ASSEMBLY AT LOW POINT OF MILLED CUT OUTS IN UPPER TUBE OF ASSEMBLY. THE MILLING PROCESS LEFT A SHARP EDGE CREATING A STRESS RISER. THIS WAS A FACTOR CONTRIBUTING TO CRACKS DEVELOPING. WE HAVE DRESSED OUR OTHER CARRY THRU ASSEMBLIEAug 27, 2015 · N713C · Helio H295 · Wing, Center BoxSDR HYTA2013043000012Cover Plate · crackedWHILE PERFORMING A 100 HOUR INSPECTION A .5 INCH CRACK WAS FOUND RADIATING FROM THE LIGHTENING HOLE IN .063" STEEL COVER/SPLICE PLATE, P/N 391-020-305-2 BOLTED TO FORWARD SIDE OF HORIZONTAL STABILATOR CENTER BOX/SPLICE STRUCTURE. THIS STRUCTURE ATTACHES THE LApr 30, 2013 · N713C · Helio H295 · Horizontal Stabilizer Miscellaneous StructureSDR HYTA2013043000010Web · crackedCRACKS FOUND IN .025 ALUMINUM WEB RIVETED TO FORWARD SIDE OF STABILATOR HORN ASSEMBLY P/N 250-020-401.Apr 30, 2013 · N713C · Helio H295 · Elevator Miscellaneous StructureSDR HYTA2013F00090Horn · crackedDURING A ROUTING 100HR/ANNUAL INSPECTION, CRACKS WERE FOUND IN SUPPORTING .025 WEB OF HORIZONTAL STABILATOR HORN ASSY AND ALSO A CRACK RADIATING FROM LIGHTNING HOLE OF .063 FORWARD COVER PLATE (PN 391-020-305-2) THAT IS PART OF THE BOLTED ASSEMBLIES SECURING TApr 22, 2013 · N713C · Helio H295 · Horizontal Stabilizer Structure

STCs that may be installed · 212

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

See all 212 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N713C before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.