N810BW
Registered owner: HYANNIS AIR SERVICE INC, MA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| HYANNIS AIR SERVICE INC. (HYIA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
PILOT REPORTED WEATHER RADAR WOULD NOT TURN ON AND HAD ELECTRIC BURNING SMELL IN FLIGHT. MAINTENANCE INSPECTED AND FOUND RADAR DISPLAY BURNED SMELL DURING INSPECTION. REMOVED AND REPLACED RADAR DISPLAY AND ANTENNA.
UPON REMOVAL OF LT WING TRAILING EDGE RIB ASSEMBLY PART NUMBER 5122053-35, A CRACK WAS IDENTIFIED AT AFT INBOARD WING SPAR ASSEMBLY. THE DAMAGE IS LOCATED AT LT WS 103.29 AND IS NOT VISIBLE WITH RIB ASSEMBLY INSTALLED. THE LT INBOARD SPAR ASSEMBLY PART NUMBER 5122036-5 WEB IS CRACKED APPROXIMATELY 2.75 INCHES FROM BOTTOM EDGE AND BOTH LOWER SPAR CAP SPLICE ANGLES ARE FAILED. WE BELIEVE THE CRACKS STARTED ON THE SPAR CAP SPLICE MEMBERS (STARTED ON AFT SIDE SPLICE MEMBER) AND ONCE FAILED THE WEB BEGAN TO FAIL. AS AN IMMEDIATE RESULT OF THIS FINDING, THE OPERATOR DEVELOPED AND IMPLEMENTED A DETAILED VISUAL INSPECTION OF THIS AREA USING A VIDEO SCOPE. NO ADDITIONAL FINDINGS WERE FOUND AT ANY OF THE OPERATORS 76 AIRCRAFT. THE OPERATOR WILL CONTINUE THIS INSPECTION AT 60 HOUR INTERVALS WHILE THEY WORK TO DEVELOP A PRACTICAL NDT TECHNIQUE. THE OEM DESCRIBES THIS AREA AND NON-DESTRUCTIVE INSPECTION TECHNIQUE AS SID 57-10-19. THIS INSPECTION IS FOUND TO BE IMPRACTICAL AS THE AREA IS INACCESSIBLE WITHOUT COMPLEX DISASSEMBLY OF STRUCTURE. THE DAMAGED STRUCTURE WILL BE REPAIRED WITH OEM PARTS AND GUIDANCE.
DURING MAINTENANCE CORROSION DAMAGE WAS IDENTIFIED ON BOTTOM FACE OF THE HORIZONTAL LEG OF THE LEFT HAND LOWER OUTBOARD SPAR CAP (P/N: 5122041-23). THIS DAMAGE IS LOCATED BETWEEN LWS 203.21 AND 212.46. AT IT'S DEEPEST THIS DAMAGE MEASURES .027 INCHES DEEP. THIS MEASUREMENT EXCEEDS THE MAXIMUM ALLOWABLE REMOVAL LIMIT OUTLINED IN MEB95-11R1 SECTION 3. THIS CAP WILL BE REMOVED AND REPLACED USING NEW PARTS.
DURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED ON THE LT OUTBOARD FITTING. THE CRACK AS FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED .102 IN LENGTH.
PILOT REPORTED BURNING SMELL FROM VENTS. INSPECTED CABIN DUCTS, CB CONSOLE, AVIONICS FAN, FOUND ALL IN GOOD CONDITION. AS PRECAUTIONARY MEASURE R & R CABIN FAN IAW MM CHAP 21-50-03.
PILOT REPORTED LEFT ENGINE STARTER LIGHT ILLUMINATED. THE FLIGHT DIVERTED FROM ITS ORIGINAL DESTINATION. INSPECTED & FOUND LEFT STARTER RELAY INTERMITTENT. R & R LEFT STARTER RELAY, THE STARTER REMAINED INOPERATIVE. R & R THE LEFT ENGINE STARTER & OPERATIONALLY CHECKED WITH NO FURTHER DEFECTS NOTED. THE PILOT REPORTED HE NOTICED THE STARTER LIGHT ILLUMINATED DURING AN INSTRUMENT PANEL SCAN AT ABOUT 4000 FT. THIS LEADS US TO BELIEVE THE STARTER LIGHT SYSTEM WAS OPERATING NORMALLY.
INTERMITTENT SMELL OF ELEC OR PLASTIC CHEMICAL BURNING COMING FROM THE SWITCH BREAKER PANEL. INSPECTED PILOT SWITCH & BREAKER AREA. NO DEFECTS NOTED AT THIS TIME. R & R AVIONICS MASTER SWITCH IAW MM CHAPTER 39-40-00. OPERATIONS CHECKED GOOD.
DURING NEW ACFT CONFORMITY INSPECTION, IT WAS NOTED THAT THE LT UPPER FORWARD FUSELAGE FITTING WAS CORRODED. THE DETERMINED CORRECTIVE ACTION WAS TO REMOVE AND REPLACE WITH NEW PART. REPAIRS ARE ONGOING.
AT 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 REPLACEMENT DRAG BRACE HAS BEEN INSTALLED IN ACFT.