FAA REGISTRY

N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N935CW is Assigned

N-Number Entered: 935cw Aircraft Description
Serial Number 4496213 Status Valid
Manufacturer Name PIPER Certificate Issue Date 09/30/2025
Model PA-44-180 Expiration Date 09/30/2032
Type Aircraft Fixed Wing Multi-Engine Type Engine Reciprocating
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 53174203
MFR Year 2005 Mode S Code (Base 16 / Hex) ACF883
Type Registration LLC Fractional Owner NO
Registered Owner
Name IN FLIGHT AIRCRAFT LLC
Street 1273 SPRINGWOOD CT
City HOWELL State MICHIGAN
County LIVINGSTON Zip Code 48843-7032
Country UNITED STATES
Airworthiness INFORMATION PROVIDED HERE SHOULD NOT BE USED TO DETERMINE THE AIRWORTHINESS OF AN AIRCRAFT.
Refer to 14 CFR Parts 39, 43, 91, and FAA Order 8130.2 for airworthiness regulations and guidance.
Type Certificate Data Sheet None Type Certificate Holder None
Engine Manufacturer LYCOMING Classification Standard
Engine Model O-360 SERIES Category Normal
A/W Date 10/23/2025 Exception Code No
The information contained in this record should be the most current Airworthiness information available in the historical aircraft record. However, this data alone does not provide the basis for a determination regarding the
airworthiness of an aircraft or the current aircraft configuration. For specific information, you may request a copy of the aircraft record at https://aircraft.faa.gov/e.gov/ND/
Other Owner Names
None
Temporary Certificates
Certificate Number T253842 Issue Date 09/30/2025 Expiration Date 10/30/2025
Fuel Modifications
Mod Code 28 Mod Date 20071218
TEMP FUEL SYSTEM INSTALLED A ND CHECKED AND FOUND TO OPERATE SATISFACTORILY. WEIGHT AND BALANCE COMPUTATION DATED AUGUST 2007. THIS TEMP LONG RANGE SYSTEM INSTALLATION WAS PERFORMED IAW REPORT KR-1390 AS REVISED DUPLICATION ALTERATION APPROVED ON FAA FORM 337 DATED JULY 30, 1990 FOR PIPER PA-44-180 SN 44-7995289 REGISTRATION N7174Q AND EXTENDED GROSS WEIGHT PERMIT INCLUDED AS PERFORMED AND FILED WITH THIS REPAIR STATION. OIL CONSUMPTION ESTABLISHED DURING PREVIOUS FLIGHTS AND OIL SUPPLY DETERMINED TO BE ADEQUATE FOR LENGTH OF FLIGHT. FERRY SYSTEM SHALL BE REMOVED UPON ARRIVAL AT DESTINATION BY A CERTIFIED MECHANIC OR REPAIR STATION AS REQUIRED BY THE FAA ADMINISTRATOR. LOG BOOK ENTRY MUST BE COMPLETED. AIRCRAFT ACTUAL GROSS WEIGHT 3800 LBS. ALLOWABLE MAX WEIGHT AUTHORIZED FOR FERRY PURPOSES 4180 LBS. ALSO NOTE IN AIRCRAFT LOG. ALSO NOTE FERRY FUEL PLACARD LOCATED IN AIRCRAFT IN FULL VIEW OF PILOT. AIRCRAFT IS WITHINTHE FORWARD AND AFT C.G. LIMITS. PILOT IS RESPONSIBLE FOR DETERMININGAIRCRAFT C.G. LIMITS ARE NOT EXCEEDED IN OVERWEIGHT CONDITION.

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