- Registered owner
- Hyannis Air Service Inc
- Location
- Hyannis, MA
- Owner type
- Corporation
- Serial number
- 402C0303
- Year built
- 1980
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- May 30, 1980
- Certificate issued
- January 29, 1999
- Expires
- April 30, 2029
- Mode S code
- AA635C
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 · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
NTSB ERA12IA550Incident · No injuriesIncident investigationFinal reportNantucket, MACompany maintenance personnel’s failure to comply with the airplane manufacturer’s service instructions by not removing the cracked drag brace from service nor inspecting the repaired drag brace at the appropriate interval, which resulted in the failure of…NTSB ERA09IA267Incident · No injuriesIncident investigationFinal reportNantucket, MAInstallation of an improper bearing in the landing gear actuator.
FAA incident reports · 3
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20120831026359ILanding: Rollout · Nantucket, MAPilot reported extended landing gear on approach to Nantucket runway 24. Performed landing checklist and verified three green landing gear down lock lights illuminated. Landed on the mains and lowered the nose which continued to lower until the fuselage nose…Incident 20110319003709ILanding: Touchdown · San Juan, PRA daily report received from the FAA southern region operations center indicating that on March 19, 2011, at 12:55 eastern standard time (EST), hyannis air service (dba. Cape air) flight KAP130 declared an emergency due to left main landing gear would not…Incident 20090427005789ILanding · Nantucket, MA(-23) Aircraft experienced a faulty gear indication during final. The left main landing gear indicator did not turn green indicating the gear was down and locked. The pilot followed emergency procedures and cycled the gear to no avail. He attempted to blow…
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR HYIA20211015001Rudder Pedal · bindingTHE PILOT REPORTED THE RUDDER PEDALS JAMMED IN FLIGHT. MAINTENANCE HAS INSPECTED ALL PULLEYS, BELLCRANKS, TORQUE TUBES AND INTERCONNECT SPRINGS WITH NO DEFECTS NOTED. TROUBLESHOOTING IS ONGOING AND THE SUBMISSION WILL BE UPDATED.SDR HYIA20161010172Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA03192016001Reflector · meltedTHIS ACFT WAS MODIFIED TO INCORPORATE STC SA04160AT ON 12 16 2015. THIS STC REMOVES OEM GRIMES STYLE RETRACTABLE LANDING LIGHT ASSEMBLIES INSTALLED AT LT & RT WINGTIPS & PROVIDES FOR INSTALLATION OF FLUSH MOUNTED HID LIGHTS WITHIN THE LE OF LT & RT WINGTIPS. SDR HYIA20160318001Coil · defectivePILOT REPORTED ELECTRIC ODOR & SMOKE IN COCKPIT. FOUND IGNITION UNIT & COIL PACK BURNED, SMOKED DURING TEST. REPLACED UNIT, OPERATIONS OK.SDR HYIA20130416001Spar · damagedDURING A SCHEDULED MX EVENT, DAMAGE WAS NOTED TO THE AFT CARRY THROUGH SPAR. MULTIPLE DAMAGE POINTS WERE DISCOVERED ON THE SPAR FLOOR SUPPORT FLANGE. OPENSDR HYIA20120904002Drag Brace · failedON LANDING ROLLOUT, ACFT SUSTAINED DAMAGE FROM A NOSE GEAR DRAG BRACE STRUCTURAL FAILURE. NOSE GEAR DRAG BRACE REPLACED, DRAG BRACE HAD BEEN INSPECTED 130 HOURS PRIOR TO FAILURE, UTILIZING A DIE PENETRANT INSPECTION. DIE PENETRANT INSPECTION FAILED TO DETECSDR HYIA20140415056Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, OEM 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURESDR HYIA769EALFTMAINLine · defectiveCREW REPORTED, ON FINAL APPROACH, LANDING GEAR DOWNLOCK LIGHTS FAILED TO ILLUMINATE. WITH GEAR SELECTED DOWN, BOTH HYD FLOW WARNING LIGHTS CAME ON STEADY. CREW ELECTED TO RETURN TO ORIGINAL DEPARTURE FIELD. EMERGENCY DECLARED, PERFORMED EMERGENCY GEAR EXTENSSDR HYIA20140415029Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OSDR HYIA769EA709Master Switch · unserviceableCREW REPORTED AVIONICS MASTER SWITCH INOPERATIVE, WILL NOT SHUTOFF. MX REMOVED AND REPLACED AVIONICS MASTER SWITCH.SDR HYIA769EAUplock Actuator · damagedON APPROACH, CREW REPORTED NO LEFT MAIN GEAR DOWN LOCK INDICATION. PERFORMED GEAR WILL NOT EXTEND HYDRAULICALLY PROCEDURE, STILL NO DOWN LOCK INDICATION. TOWER FLYBY INDICATED GEAR SEEMED TO BE DOWN. ON LANDING LEFT MAIN GEAR COLLAPSED. GEAR SWING INDICATESDR HYI2001F00007Drag Brace · crackedREGULAR SCHEDULED INSPECTION FOUND NOSE GEAR DRAG BRACE CRACKED AT ACTUATOR ATTACH LUG. MECHANIC REMOVED AND REPLACED DRAG BRACE.(K)SDR 97ZZZX1839Line · crackedFOUND PRESSURE LINE 5100111-71 CRACKED IN A BEND. CRACK ALLOWED ALL HYDRAULIC FLUID TO PUMP OVERBOARD. THE FAILURE POINT OF THE LINE IS AFT OF THE ENGINE FIREWALL WITH NO DIRECT ACCESS FOR INSPECTION. THE FAULT WAS FOUND WHEN THE LINE WAS REMOVED FOR TROUBL
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