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N54KA

Open the Markdown

1978 Piper PA-32-300 · Lycoming IO-540 series

Open in FAA registry

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Registered owner
Point To Point Air LLC
Location
Arlington, WA
Owner type
LLC
Serial number
32-7840197
Year built
1978
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
October 3, 1978
Certificate issued
November 3, 2018
Expires
November 30, 2028
Mode S code
A6D675
Piper PA-32-300Airframe model · 6 seats · 1 engine · 992 registeredTCDS A3SOAirframe · Piper PA-32-300TCDS 1E4Engine · Lycoming IO-540 series

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming IO-540 model are included below.

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Airworthiness directives that may apply · 92

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

1963In forceSuperseded2026
See all 108 ADs

Information bulletins that may apply · 30

Advisory, not mandatory.

See all 33 bulletins

NTSB investigations

No NTSB investigations matched to N54KAMatched 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 Piper PA-32-300 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 20020407025789ILevel Off Touchdown · Juneau, AK(-23) Left outboard flap hinge bolt separated while landing, allowing flap structure to bend up 90' at second hinge point. Aircraft landed safely.[privacy data omitted]Apr 7, 2002 · Minor damage

Service difficulty reports · 3

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

SDR LAB2004F00002Ahrs · malfunctionedAHRS (ALTITUDE HEADING REF SYSTEM) INSTALLED IAW EFIS-SV SYSTEM UNDER STC NR SA02203AK FAILED TO REPORT HEADING INDICATION.Sep 21, 2004 · N54KA · Piper PA32300 · Integrated Flight SystemSDR 2003F00388Diaphragm · tornAIRCRAFT EXPERIENCED ERRATIC FUEL FLOW AND SURGING ON CLIMB-OUT. AIRCRAFT RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. UPON TROUBLESHOOTING BY MAINT DEPT THE UPPER DIAPHRAGM ON ENG DRIVEN PUMP WAS FOUND TORN. THIS WAS EVIDENTLY ALLOWING AIR INTO THE FUEJun 23, 2003 · N54KA · Piper PA32300 · Engine Fuel PumpSDR LAB2002F00001Tube · crackedRUDDER TRIM ADJ. TUBE, FOUND CRACKED ON PHASE INSPECTION OF AIRCRAFT.Jun 2, 2002 · N54KA · Piper PA32300 · Rudder Tab Control System

STCs that may be installed · 388

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

See all 388 STCs