- Registered owner
- H2 Link Co
- Location
- Chino, CA
- Owner type
- Corporation
- Serial number
- 4496230
- Year built
- 2006
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- October 5, 2006
- Certificate issued
- August 20, 2022
- Expires
- August 31, 2029
- Mode S code
- A68A12
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 41
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1979 | 4 |
|---|---|
| 1980 | 3 |
| 1981 | 3 |
| 1982 | 1 |
| 1991 | 1 |
| 1992 | 1 |
| 1994 | 2 |
| 1996 | 2 |
| 1997 | 2 |
| 1998 | 1 |
| 2000 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 4 |
| 2006 | 5 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 2 |
| 2012 | 2 |
| 2013 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2022 | 1 |
| 2024 | 2 |
| 2026 | 1 |
Airframe · Piper PA-44-180
AD 2024-10-04Wing, Attach FittingsAD 2022-03-15Fuel Quantity IndicatorAD 2015-26-08Rudder Control SystemInformation bulletins that may apply · 16
Advisory, not mandatory.
See all 18 bulletins
NTSB investigations
No NTSB investigations matched to N520MSMatched 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-44-180 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.
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2015FA0000349Distributor Gear · looseAFTER LANDING AT THE DESTINATION AIRPORT, THE FLIGHT CREW REPORTED INTERMITTENT ENGINE VIBRATION IN CRUISE FLIGHT. A MAINTENANCE CREW WAS SENT TO INVESTIGATE BUT COULD NOT DUPLICATE THE ISSUE. ACFT WAS BROUGHT BACK TO HOME BASE WITH SOME INTERMITTENT ROUGHNESSDR 2010FA0000848Strip · migratedACFT REPORTED AS LT ENGINE WOULDN’T SLOW TO IDLE. DISCONNECTED THROTTLE CONTROL AND DETERMINED PROBLEM WITHIN THE CARB. THE CARB WAS REMOVED AND A VISUAL INSPECTED NOTED A FELT STRIP WEDGED IN BETWEEN THROTTLE PLATE AND CARB HSG. THE STRIP WAS REMOVED AND T
STCs that may be installed · 223
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 223 STCs