- Registered owners
- Hyannis Air Service Inc DBACape Air
- Location
- Hyannis, MA
- Owner type
- Corporation
- Serial number
- 402C0435
- Year built
- 1980
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- January 28, 1981
- Certificate issued
- February 17, 1994
- Expires
- December 31, 2029
- Mode S code
- A8FCFF
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 N67886Matched 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 · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20260708010119IClimb · San Juan, PR08 July 2026, [privacy data omitted] (C402), declared an emergency on climb out after departing San Juan (sju), due to the crew door opening and striking the radio antenna. The aircraft returned to San Juan and landed without incident. No injuries were noted.…Incident 19950619018959ITo Init Climb(1st Pwr Reduct) · Hyannis, MADeparted hya to reposition to ack. Door light came on. Tried close crew door. Door departed. Returned. Cut his arm.
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR HYIA20210525001Master Cylinder · faultedTHE PILOT A LOSS OF PRESSURE ON THE RIGHT BRAKE DURING PARKING. MAINTENANCE INSPECTED AND FOUND THE RIGHT MASTER CYLINDER TO BE AT FAULT. REPLACED THE MASTER CYLINDER HOSE, AND RESEALED THE MASTER CYLINDER. PERFORMED BLAKE BLEEDING PROCEDURES WITH NO FURTHER SDR HYIA20170705003Attach Bracket · crackedWHILE PREFORMING MAINTENANCE, A CRACK WAS DISCOVERED IN THE RT MAIN ACTUATOR ATTACH BRACKET.SDR HYIA20150804002Fluid · lowLEFT FOOT BRAKE, NO PRESS ON LT SIDE, NO BRAKING ACTION LT SIDE. INSPECTED LT BRAKE LININGS, CHECKED FOR LEAKS, NO DEFECTS NOTED. SERVICED MASTER CYLINDER WITH FLUID. OPERATIONS CHECKED GOOD.SDR HYIA01242015001Beam · crackedDURING SCHEDULED INSPECTION EVENT, THE RT NACELLE INBD ENG BEAM WAS FOUND TO BE CRACKED AT UPPER FWD INBD RADIUS IN THE AREA CORRESPONDING TO FWD INBD ENG MOUNT. A SUPPLEMENT TO THIS SDR WILL BE SUBMITTED TO ILLUSTRATE DAMAGE POINT. CORRECTIVE ACTION WILL BESDR HYIA20140414054Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMESDR HYIA20121210001B-Nut · leakingTHE PILOT REPORTED A STEADY LOSS OF RT ENGINE OIL PRESSURE AFTER TAKEOFF. ENGINE SHUTDOWN AND FEATHERED BEFORE OIL PRESSURE REACHED THE RED LINE. DIVERTED BACK TO THE DEPARTURE. DURING MX INSPECTION, A LOOSE B-NUT WAS ALSO FOUND ON THE OIL PRESSURE LINE TSDR HYIA20140415062Drag 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 SDR HYIA67886LFTTQLNKBolt · missingCREW REPORTED, ON TOUCHDOWN, LT MAIN GEAR BRAKE APPEARED TO LOCK UP. DIRECTIONAL CONTROL PARTIALLY MAINTANED, BUT DID VEER OFF RUN WAY ON TO GRASS APRON. MX INSPECTED LT MAIN GEAR AND FOUND TORQUE LINK CTR PIVOT BOLT AND ASSOCIATED HARDWARE MISSING. R & R LT SDR HYIA67886RTMLGActuator · malfunctionedCREW REPORTED WITH GEAR RETRACTED, RT MAIN GEAR DOWNLOCK LIGHT ILLUMINATED. CREW EXTENDED GEAR USING EMERGENCY EXTENSION SYS. LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED RT MLG ACTUATOR. COMPLIED WITH GEAR SWINGS, CHECK NORMAL, ACFT RELEASED BACK TO SESDR HYIA67886AACircuit Breaker · unserviceableCREW REPORTERD AVIONICS MASTER SWITCH FAILED TO TURN OFF. WORKED OK AFTER SEVERAL ATTEMPTS. MAINTENANCE REMOVED AND REPLACED SWITCH AS A PRECAUTIONART MEASURE.SDR HYIA67886Circuit Breaker · inoperativePILOT DID NOT HAVE THREE DOWN AND LOCK GREEN LIGHTS. MX INSPECTED AIRCRAFT FOUND BAD C/B AND ONE BAD BULB ON INDICATOR. MX REPLACED C/B AND BULB. PERFORMED REQUIRED INSPECTIONS AND OPERATIONAL CHECKS AND RETURNED ACFT TO SERVICE.SDR 1350527N67786Master Switch · defectiveCREW REPORTED AVIONICS MASTER SWITCH ION. MX CHANGED CIRCUIT BREAKER SWITCH.SDR 97ZZZX4331Rod End · brokeRIGHT LANDING GEAR DOOR CONTROL ROD BROKE AT ROD END, DOOR WOULD HANG DOWN WITH GEAR UP. INSTALLED NEW CONTROL ROD AND RIGGED. NO FURTHER TROUBLE.
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