Piper PA-28-181
N244AA is a Piper PA-28-181, a fixed-wing airplane with one motor with a piston engine, built in 2024. It has 4 seats. It is registered to Ff22 LLC, an LLC in Scottsdale, Arizona. The registration is valid: it was issued on April 29, 2024 and expires on April 30, 2031. It holds a standard airworthiness certificate for normal; utility, dated April 2, 2024.
Where is it now Last seen today at 12:26 pm.
Last seen today at 12:26 pm. Checking whether it is in the air right now…
Aircraft broadcast their own position; volunteer receivers pool what they hear. Owners who have asked the FAA not to be displayed are not shown.
Flight history: where it flew in the last seven days · follow it on the live map
Aircraft
- Maker
- Piper
- Model
- PA-28-181 · all PA-28-181s and related versions
- Built of
- aluminiumThe airframe is aluminium: sheet metal over a riveted frame, the way most aircraft have been built since the 1940s. This is how the Piper PA-28 Cherokee, Warrior, Archer and Arrow family is built; the FAA does not record construction for each aircraft, and the type certificate data sheet is the authority for this one.
- Serial number
- 2881734
- Type
- Fixed-wing, single engineFAA type of aircraft code 4 (the FAA's broad category for the airframe). Every aircraft with this code · All codes
- Power
- Piston (reciprocating)FAA type of engine code 1 (what powers it, as the FAA classes engines). Every aircraft with this code · All codes, 1 motor · Lycoming IO-360-B4A · 180 hp
- Seats
- 4
- Year built
- 2024
- Cruising speed
- 105 mph
- Transponder code
- A23EDC (octal 50437334)
Registration
- Status
- Valid registrationFAA registration status code V (whether the registration certificate is in force). Every aircraft with this code · All codes
- Certificate issued
- April 29, 2024
- Expires
- April 30, 2031
- Last FAA action
- January 27, 2025
- Airworthiness
- StandardFAA airworthiness class code 1 (the kind of airworthiness certificate it flies under and what it is approved for). Every aircraft with this code · All codes · Normal; UtilityFAA certificate purpose code NU (the kind of airworthiness certificate it flies under and what it is approved for). All codes · April 2, 2024
- FAA region
- Western-PacificFAA region code 4 (the FAA regional office that handles the record). All codes
- FAA record id
- 01444064
Owner as the FAA publishes it
- Name
- Ff22 LLC
- Type
- LLCFAA type of owner code 7 (who holds the registration: a person, a company, a trust or a government body). Every aircraft with this code · All codes
- Address
- 8711 e Pinnacle Peak Rd Ste 304
Scottsdale, AZ 85255
Owners can ask the FAA to withhold their name and address from public files. When they do, those fields are blank here as well. How that works.
Documents on file 0
No bills of sale, loans or other documents are indexed against this tail number.
Earlier use of this number 1
Connections how N244AA links to the rest of the register
- Piper PA-28 Cherokee, Warrior, Archer and Arrow 18,635 registered
- Piper 44,844 aircraft on the register
- Built of aluminium · as the model family is built; the register does not record it per aircraft
- Lycoming IO-360-B4A 986 aircraft with this engine series · 180 hp
- Ff22 LLC 49 aircraft in the fleet
- Scottsdale, AZ 685 aircraft registered in this town
- Scottsdale Airport · SDL
- Arizona 8,422 aircraft registered
- FAA orders naming the Piper PA-28 Cherokee, Warrior, Archer and Arrow 90 airworthiness directives
- Failure reports filed on the Piper PA-28 Cherokee, Warrior, Archer and Arrow 3,269 reports since 1995
- Approved modifications for the Piper PA-28 Cherokee, Warrior, Archer and Arrow 697 supplemental type certificates
- FAA orders naming the Lycoming IO-360-B4A 32 airworthiness directives
- Failure reports on the Lycoming IO-360-B4A 65 reports since 1995
- Report filed on this aircraft: Stop Fitting, cracked · 2009-12-03
- Report filed on this aircraft: Wire, shorted · 2008-02-13
- Report filed on this aircraft: Blade, failed · 2006-12-08
- Where N244AA is now · Last seen today at 12:26 pm.
The whole map of how records connect · these connections as data: /graph/aircraft/N244AA.json.
Records check free · 2 to understand · 3 clear
The public federal record on N244AA, read the way a buyer, lender or insurer reads it: FAA registration, prior tail numbers keyed on the serial number, reuse of the tail number, recent registry filings, and the NTSB accident record under this and every earlier registration.
Valid registration to Ff22 LLC, an LLC, certificate issued April 29, 2024, expires April 30, 2031. No fractional interest recorded. [1]
Standard certificate for normal; utility, dated April 2, 2024, consistent with the 2024 manufacture year. [1]
No earlier tail number is recorded against serial 2881734 for this model in the deregistered file. [2]
N244AA was previously assigned to 1 other aircraft: Mcdonnell Douglas DC-9-82(MD-82) (serial 49256, cancelled June 14, 2010). Histories keyed to the tail number alone can mix aircraft up; this check keys on the serial number. [2]
No bills of sale, loans or releases have reached the registry in recent weeks. The index covers only recent filings; older liens are in the records file. [3]
2 NTSB records under N244AA: Accident on October 29, 1996 at Jamaica, NY: serious injuries, minor damage. Accident on September 12, 1989 at Chicago, IL: minor injuries, substantial damage. Details below. [4]
These live in the FAA aircraft records file (every document ever filed against the aircraft) and, for larger aircraft, the International Registry. Part of the full report.
AD compliance against the logbooks and flight-activity reconciliation are researched layers of the full report.
NTSB records 2
Aircraft on the NTSB record: Mcdonnell Douglas MD-80 · operated under 121
Failure of the nose landing gear upper lock link.
Full record in plain English · Docket and reports at the NTSB
Aircraft on the NTSB record: Mcdonnell Douglas MD-80 · operated under 121
A LOSS OF HYDRAULIC SYSTEM PRESSURE DUE TO THE OPERATOR'S FAILURE TO REPLACE A SYSTEM COMPONENT THAT HAD A KNOWN HISTORY OF FAILURES, AND THE PILOT'S IMPROPER USE POWERPLANT CONTROLS RESULTING IN A DEGRADATION OF RUDDER EFFECTIVENESS. A CONTRIBUTING FACTOR WAS THE FAILURE OF THE POWER TRANSFER UNIT SHUTOFF VALVE.
Full record in plain English · Docket and reports at the NTSB
- FAA Releasable Aircraft Database, master file, file of October 28, 2026. registry.faa.gov/
- FAA deregistered aircraft file (part of the same download), file of October 28, 2026. registry.faa.gov/
- FAA document index: registry documents received in recent weeks, file of October 28, 2026. registry.faa.gov/
- NTSB aviation accident database (CAROL), records through September 30, 2026. data.ntsb.gov/carol-main-public/basic-search
This automated check reads the public federal record. Nothing here is a legal opinion, an appraisal or a statement about the aircraft's condition; a CLEAR line is a statement about the searched record, not the aircraft.
Source: FAA Civil Aviation Registry, Releasable Aircraft Database, October 28, 2026. See this record on the FAA site · This record as data