- Registered owner
- Hyannis Air Service Inc
- Location
- Hyannis, MA
- Owner type
- Corporation
- Serial number
- 402C1006
- Year built
- 1985
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- March 20, 1999
- Certificate issued
- December 28, 2010
- Expires
- December 31, 2029
- Mode S code
- A631BA
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 · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports
No FAA accident or incident reports matched to N499CAMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna 402C aircraft
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR HYIA20230707001Fitting · crackedWHILE PERFORMING LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02R3 TO SATISFY AD2017-10-09, A CRACK WAS VISUALLY IDENTIFIED ON THE INBOARD VERTICAL LEG OF THE LEFT HAND OUTBOARD NACELLE FITTING. THIS CRACK MEASURES APPROXIMATELY .138 INSDR HYIA20230525001Fitting · crackedDURING SCHEDULED NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS NOTED ON THE RIGHT HAND INBOARD NACELLE FITTING P/N: 5292029-30. THE CRACK MEASURES .125 INCHES LONG AND IS CONSISTENT WITH OTHERS FOUND USING THE LIGHTED BORESCOPE INSPECTION TECHNIQUE (TEXSDR HYIA20210407003Ignition Unit · brokenTHE PILOT REPORTED A BURNING SMELL DURING CRUISE. MAINTENANCE INSPECTED AND FOUND THE SMELL TO BE COMING FROM THE HEATER IGNITION UNIT. THE COMPONENT WAS REMOVED AND REPLACED WITH NO FURTHER DEFECTS NOTED.SDR HYIA20161229001Manifold · low pressurePILOT REPORTED THAT DURING FLIGHT, MANIFOLD PRESSURE DROPPED EIGHT INCHES FROM 29-21. LANDED WITH NO INCIDENT. OPEN.SDR HYIA20160825093Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160825092Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160812067Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGESDR HYIA20160812066Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGESDR HYIA20160205001Cotter Pin · brokenPILOT REPORTED LT BRAKE FAILED. RUDDER PEDAL APPEARS DISCONNECTED FROM CYLINDER. INSPECTED & FOUND THE CONNECTING CLEVIS PIN HAD FALLEN OUT DUE TO BROKEN COTTER PIN. MX THEN RE-CONNECTED LT RUDDER PEDAL TO BRAKE CYLINDER IAW MM CH 20-10-01.SDR 8PCR20150414001Sleeve · looseNUMBER 5 EXHAUST LIFTER BORE ALUMINUM SLEEVE IN THE CRANKCASE WAS FOUND TO BE LOOSE & MISSING MATERIAL. THIS CRANKCASE HAD THE LIFTER BORES SLEEVED DURING CRANKCASE OVERHAUL & REPAIR. THE LOOSE LIFTER BORE SLEEVE MOVED OUT OF ITS BORE & CAME IN CONTACT WITH SDR HYIA20150316001Bearing · failedBURNING SMELL WHEN HEATER TURNED ON, AS WELL AS A GRINDING SOUND WHEN HEATER FAN TURNED ON. REPLACED THE HEATER FAN BLOWER MOTOR BEARINGS, AS WELL AS SECURED OIL LINE ON RT ENG WASTE GATE TO PRESS CONTROLLER.SDR HYIA20141014001Fitting · wornEMERGENCY EXIT OPENED IN FLIGHT, DIVERTED. INSPECTED EMER EXIT DOOR. FOUND LATCH CLIP WORN. R & R AS PRECAUTIONARY MEASURE. R & R PLASTIC COVER, OPERATIONS CHECKED GOOD.SDR HYIA20140414045Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20121220001Relay · shortedPILOT REPORTED THAT SHORTLY AFTER TAKEOFF THE ACFT HAD A COMPLETE ELECTRICAL FAILURE. THE PILOT ELECTED TO RETURN TO THE DEPARTURE AIRPORT AND LANDED THE ACFT SAFELY. WHEN INSPECTED BY MX A BATTERY RELAY WAS FOUND SHORTED TO GROUND. THE BATTERY RELAY WAS RE
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
Earlier aircraft with this N-number · 1
This aircraft carried N499CA before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.