- Registered owner
- Airswiss Inc
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 402C0311
- Year built
- 1980
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- November 3, 2001
- Certificate issued
- August 11, 2020
- Expires
- August 31, 2027
- Mode S code
- AA7D14
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental TSIO-520 model are included below.
On this page
Airworthiness directives that may apply · 79
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1969 | 1 |
|---|---|
| 1970 | 1 |
| 1971 | 1 |
| 1972 | 2 |
| 1975 | 1 |
| 1976 | 2 |
| 1977 | 1 |
| 1979 | 2 |
| 1980 | 4 |
| 1981 | 2 |
| 1982 | 1 |
| 1984 | 1 |
| 1985 | 1 |
| 1987 | 2 |
| 1988 | 4 |
| 1989 | 2 |
| 1990 | 3 |
| 1991 | 1 |
| 1992 | 1 |
| 1993 | 3 |
| 1995 | 2 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 5 |
| 1999 | 2 |
| 2000 | 3 |
| 2004 | 1 |
| 2005 | 5 |
| 2007 | 2 |
| 2008 | 1 |
| 2009 | 2 |
| 2010 | 2 |
| 2011 | 2 |
| 2012 | 3 |
| 2014 | 1 |
| 2015 | 1 |
| 2016 | 3 |
| 2017 | 1 |
| 2018 | 2 |
| 2020 | 1 |
| 2022 | 2 |
| 2023 | 6 |
See all 95 ADs
Information bulletins that may apply · 24
Advisory, not mandatory.
See all 25 bulletins
NTSB investigations
No NTSB investigations matched to N775RCMatched 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 Cessna 402C 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 N3B2005F00000Connecting Rod · looseIT APPEARS FOR SURE THAT NUT ON CONNECTING ROD CAP, LOOSEN. BOLT HEAD SHEARED OFF. ENGINE STOPPED RUNNING SOOP AFTERWARD. (BOLT NR 629340) (K)SDR 2003FA0000967Control Cable · brokenLEFT RUDDER CABLE HAD CHAFED THROUGH ON THE FLEXIBLE BRAKE MASTER CYLINDER LINE. ROUTING OF THE BRAKE LINE OVER THE RUDDER CABLE PULLEY CAUSED THE CABLE TO FAIL BEFORE THE BRAKE FLEX LINE FAILED. ACCESS TO EFFECTED AREA IMPOSSIBLE DUE TO LACK OF WORKING AREA
STCs that may be installed · 321
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 402C
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller