OpenAirDocs.org

N242RA

Open the Markdown

Piper PA-42

Open in FAA registry

© OpenStreetMap
Registered owner
Johnston Properties LLC
Location
Garden City, KS
Owner type
LLC
Serial number
42-8001003
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
August 19, 1980
Certificate issued
March 6, 2019
Expires
March 31, 2029
Mode S code
A238E5
Piper PA-42Airframe model · 11 seats · 2 engines · 17 registeredTCDS A23SOAirframe · Piper PA-42

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 11

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

1990In forceSuperseded2026
Superseded and historical ADs · 1
AD 2009-13-06Nose baggage doorHistoricalEffective Jul 24, 2009 · Replaced by AD 2009-13-06 R1

Information bulletins that may apply · 2

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N242RAMatched 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-42 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 19980921038389IFcd/Prec Ldg From Cruise · Youngstown, OH(-5) Landing gear would not extend with normal system for landing. Pilot was able to extend main gear with emergency system but nose gear would not extend. The pilot landed with the nose gear retracted causing damage to the nose of the aircraft and one prop.…Sep 21, 1998 · Minor damage

Service difficulty reports · 1

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

SDR 97ZZZX2905Clamp · missingFUEL FLOW TRANSMITTER IS MOUNTED TO ENGINE WITH 2 STAINLESS LINES PN 3032010 AND PN 3026779 B1; AND, IF SUPPORT CLAMP PN 30006614 IS NOT INSTALLED, LINES WILL CRACK AT WELDS CREATING A HEAVY FUEL LEAKING ENGINE COMPARTMENT AND ONTO WING.Jun 8, 1997 · N242RA · Piper PA42 · Fuel Flow Sensor

STCs that may be installed · 107

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

See all 107 STCs