N6813J
Registered owner: HYANNIS AIR SERVICE INC DBA, 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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
17 reports on file, 2001-10-08 – 2022-12-08.
Part: CIRCUIT BREAKER — FAILED (ANTI COLLISION) · airframe 37,096 hrs · 41,666 cycles
PILOT REPORTED SMOKE OBSERVED FROM SIDE PANEL. MAINTENANCE INSPECTED ANTI-COLLISION CIRCUIT BREAKER SWITCH AND WIRING, FOUND SWITCH INOP AND WIRE INSULATION BURNT ON LOAD SIDE OF SWITCH. REPAIRED DAMAGED ANTI-COLLISION LIGHT SWITCH WIRE IAW 402C WDM CHAPTER 20-10-01 AND REPLACED ANTI COLLISION CIRCUIT BREAKER SWITCH IAW MM 24-50-00.
Earlier reports · 2001–2019 · 16 reports
2019
Part: RIB — CRACKED (LT WING) · airframe 33,278 hrs · 37,610 cycles
DURING MAINTENANCE A CRACK WAS DISCOVERED ON THE LEFT HAND CLOSEOUT RIB LOCATED AT LEFT WING STATION 106.79. THIS CRACK STARTS AT A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT TRUNION SUPPORT AND EXTENDS FORWARD APPROXIMATELY .900 IN. THIS RIB WILL BE REPLACED USING NEW PARTS.
2018
Part: ENGINE — SHUTDOWN (RIGHT) · airframe 32,116 hrs
PILOT REPORTED THE RIGHT ENGINE SHUTDOWN IN FLIGHT. OPEN
2017
Part: TORQUE TUBE — FAILED (RUDDER) · airframe 32,002 hrs · 35,835 cycles
WHILE IN CRUISE, THE RT RUDDER PEDAL WENT TO THE FLOOR, FULL FORWARD. THE PILOT DID NOT HAVE ANY RUDDER AUTHORITY, BUT THE AIRCRAFT REMAINED IN STRAIGHT AND LEVEL FLIGHT. DIVERTED AND LANDED SAFELY WITH NO ISSUES. THE AIRCRAFT WAS UNABLE TO TAXI FROM THE RUNWAY. INSPECTION REVEALED THE RT RUDDER TORQUE TUBE HAD CRACKED AND FAILED AT THE WELD INTERSECTION OF RT PILOT RUDDER PEDAL. OPEN
Part: FITTING — CRACKED (LT NACELLE) · airframe 31,639 hrs · 35,387 cycles
WHILE PREPPING THE LOWER NACELLE SKIN FOR SID 57-10-16 NDT INSPECTION, TWO CRACKS WERE IDENTIFIED IN THE LT OUTBOARD NACELLE FITTING.
Part: CYLINDER — BROKEN (ENGINE) · airframe 31,510 hrs · 35,200 cycles
PILOT REPORTED SHUDDERING AND VIBRATION FROM LEFT ENGINE. UPON INSPECTION MAINTENANCE FOUND THE CYLINDER ROTOCOIL BROKEN. CYLINDER WAS REPLACED, ADDITIONAL DETAILS TO BE CONVEYED UPON TEARDOWN ANALYSIS.
2012
Part: DRAG BRACE — CRACKED (NLG) · airframe 25,446 hrs
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.
2011
Part: DRAG BRACE — CRACKED (NLG) · airframe 23,950 hrs
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.
Part: DRAG BRACE — CRACKED (NLG) · airframe 24,566 hrs
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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OUTLINED IN MEB941-11R1 & RETURNED TO SERVICE.
Part: DRAG BRACE — CRACKED (NLG) · airframe 24,325 hrs
AT 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 OUTLINED IN MEB941-11R1 & RETURNED TO SERVICE.
2010
Part: RESISTOR — BURNED (CABIN HEATER FAN) · airframe 23,775 hrs
CREW REPORTED, IN CRUISE, STRONG ELECTRIAL SMELL IN COCKPIT. CREW DIVERTED. MX INSPECTED ACFT, R & R OVERHEATED CABIN HEATER FAN HIGH - LOW RESISTOR. SYS CHECKS OK. ACFT RELEASED BACK TO SERVICE.
2007
Part: FITTING — LEAKING (HEATER) · airframe 15,558 hrs
PILOT NOTICED FUEL SMELL IN COCKPIT DURING HEATER START UP AND SHUT DOWN, WHEN BRINGING AIRCRAFT TO FLEET CENTER AT END OF NIGHT. MAINTENANCE FOUND PUMP OUTLET FITTING LEAKING. MAINTENANCE TIGHTENED FUEL PUMP OUTLET FITTING AND AS A PRECAUTIONARY MEASURE REMOVED AND REPLACED HEATER FUEL LINE. LEAK CHECKED AND OPERATIONALLY CHECKED GOOD.
2006
Part: CONNECTING ROD — DESTROYED (LEFT ENGINE)
PILOT REPORTED RPM/POWER LOSS, SHUT ENGINE AS A PRECAUTIONARY MEASURE, RETURNED TO DEPARTURE AIRPORT.
Part: CIRCUIT BREAKER — DEFECTIVE (AVIONICS)
AVIONICS CIRCUIT BREAKER FAILED IN THE ON POSITION.
Part: CIRCUIT BOARD — DEFECTIVE (AVIONICS)
CREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH.
2003
Part: LINER — DAMAGED (LT MLG BRAKE)
AFTER LANDING, ON ROLLOUT, AIRCRAFT STARTED VEERING TO THE LEFT. CREW WAS UNABLE TO STRAIGHTEN OR TURN RIGHT EVEN WITH DIFFERENTIAL POWER OR RT RUDDER. AIRCRAFT WAS SHUTDOWN ON RUNWAY. TOWED TO HANGER. MECHANIC UNABLE TO DUPLICATE CONDITION, REMOVED AND REPLACED LT WHEEL AND BOTH BRAKE ASSEMBLIES AS A PRECAUTIONARY MEASURE. TAXI CHECK, OK.
2001
Part: MASTER SWITCH — INOPERATIVE (AVIONICS)
CREW REPORTED AVIONICS MASTER SWITCH INOPERATIVE ON PREFLIGHT. MAINTENANCE REMOVED AND REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE. (PTRS-2001B5540)