20180426004139A

Accident · Substantial damage

FAA accident report · Cessna 402B · New Braintree, MA · April 26, 2018

Date
April 26, 2018 · 17:15 local
Place
New Braintree, MA
Airport
Tanner-Hiller
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N87266
NTSB investigation
NTSBERA18LA136
Reported as
Cessna 402B
People aboard
4
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
337 total225 in this make and model3 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

On April 26, 2018 at approximately 5:15 p.m. (eastern time), aircraft N87266 was involved in an accident at Tanner-Hiller Airport (8B5) located in New Braintree, MA. privacy data omitted Pilot privacy data omitted was acting as pilot in command (PIC). The aircraft took-off with four on board but only landed with three on board due to a planned parachute jump. The aircraft attempted to land on runway 6 but ended-up going off the FAR end of the runway onto a dirt road until it impacted a tree. Distance from edge of runway asphalt to the aircraft?s final resting point was about 300 feet. After it impacted several trees, the aircraft came to a stop and a fire started on the left wing, number 1 engine, and parts of the aircraft that had separated on impact. All on-board were able to escape the aircraft with no assistance and had no injuries.

The inspector in charge (iic) immediately started photographing the scene when he arrived at the scene. There were two segmented skid marks directly after the runway end line that were created from the right main tire. There were two fairly straight main tire indications once the aircraft was in the dirt. It appeared that the brakes were working appropriately. The PIC confirmed proper brake operation. The main tire marks started to drift left until the left wing impacted the first tree. Iic verified flight control function for all channels except the rudder. The rudder had tree branches stuck inside the hinge area. Flap selector was set full down at 45DEGREES and was only verifiable on right wing due to left wing damage.

The iic was able to find all major part of the aircraft. Substantial damage was determined due to the following issues: left wing separated about 2 1/2 feet outboard of number 1 engine causing significant structural damage and fire damage, structural damage to right lower side of the empennage, structural damage to horizontal stabilizer on the leading edge and elevator attachment point. We are unable to see the extent of damage to the underside of the aircraft due to the current resting position of the aircraft after the left main landing gear separation.

According to both the PIC and the jumper, the jumper jumped out early due to miscommunication. This and the wind gusts caused the jumper to be off course of the target landing area. The PIC believed that the wind data in the weather reports were incorrect. The weather data showed that the aircraft would have landed with a quartering tail wind. The PIC stated in part that he made two go-arounds due to the ?air being bumpy? And he "did not like it". On the PIC?s third attempt, he stated ?he had a tailwind and the aircraft would not settle.? Upon touchdown, privacy data omitted applied the brakes but due to the position of the aircraft, it departed the runway. The PIC stated the brakes were fully functional. The aircraft hit the first tree between the left tip tank and the number one engine. The aircraft hit several other trees and sustained substantial damage. The aircraft and some pieces caught fire. The PIC and all passengers remaining onboard evacuated the aircraft on their own with no injuries.

As the FAA filed it

ON APRIL 26, 2018 AT APPROXIMATELY 5:15 P.M. (EASTERN TIME), AIRCRAFT N87266 WAS INVOLVED IN AN ACCIDENT AT TANNER-HILLER AIRPORT (8B5) LOCATED IN NEW BRAINTREE, MA. ^PRIVACY DATA OMITTED^ PILOT ^PRIVACY DATA OMITTED^ WAS ACTING AS PILOT IN COMMAND (PIC). THE AIRCRAFT TOOK-OFF WITH FOUR ON BOARD BUT ONLY LANDED WITH THREE ON BOARD DUE TO A PLANNED PARACHUTE JUMP. THE AIRCRAFT ATTEMPTED TO LAND ON RUNWAY 6 BUT ENDED-UP GOING OFF THE FAR END OF THE RUNWAY ONTO A DIRT ROAD UNTIL IT IMPACTED A TREE. DISTANCE FROM EDGE OF RUNWAY ASPHALT TO THE AIRCRAFT?S FINAL RESTING POINT WAS ABOUT 300 FEET. AFTER IT IMPACTED SEVERAL TREES, THE AIRCRAFT CAME TO A STOP AND A FIRE STARTED ON THE LEFT WING, NUMBER 1 ENGINE, AND PARTS OF THE AIRCRAFT THAT HAD SEPARATED ON IMPACT. ALL ON-BOARD WERE ABLE TO ESCAPE THE AIRCRAFT WITH NO ASSISTANCE AND HAD NO INJURIES.

THE INSPECTOR IN CHARGE (IIC) IMMEDIATELY STARTED PHOTOGRAPHING THE SCENE WHEN HE ARRIVED AT THE SCENE. THERE WERE TWO SEGMENTED SKID MARKS DIRECTLY AFTER THE RUNWAY END LINE THAT WERE CREATED FROM THE RIGHT MAIN TIRE. THERE WERE TWO FAIRLY STRAIGHT MAIN TIRE INDICATIONS ONCE THE AIRCRAFT WAS IN THE DIRT. IT APPEARED THAT THE BRAKES WERE WORKING APPROPRIATELY. THE PIC CONFIRMED PROPER BRAKE OPERATION. THE MAIN TIRE MARKS STARTED TO DRIFT LEFT UNTIL THE LEFT WING IMPACTED THE FIRST TREE. IIC VERIFIED FLIGHT CONTROL FUNCTION FOR ALL CHANNELS EXCEPT THE RUDDER. THE RUDDER HAD TREE BRANCHES STUCK INSIDE THE HINGE AREA. FLAP SELECTOR WAS SET FULL DOWN AT 45DEGREES AND WAS ONLY VERIFIABLE ON RIGHT WING DUE TO LEFT WING DAMAGE.

THE IIC WAS ABLE TO FIND ALL MAJOR PART OF THE AIRCRAFT. SUBSTANTIAL DAMAGE WAS DETERMINED DUE TO THE FOLLOWING ISSUES: LEFT WING SEPARATED ABOUT 2 1/2 FEET OUTBOARD OF NUMBER 1 ENGINE CAUSING SIGNIFICANT STRUCTURAL DAMAGE AND FIRE DAMAGE, STRUCTURAL DAMAGE TO RIGHT LOWER SIDE OF THE EMPENNAGE, STRUCTURAL DAMAGE TO HORIZONTAL STABILIZER ON THE LEADING EDGE AND ELEVATOR ATTACHMENT POINT. WE ARE UNABLE TO SEE THE EXTENT OF DAMAGE TO THE UNDERSIDE OF THE AIRCRAFT DUE TO THE CURRENT RESTING POSITION OF THE AIRCRAFT AFTER THE LEFT MAIN LANDING GEAR SEPARATION.

ACCORDING TO BOTH THE PIC AND THE JUMPER, THE JUMPER JUMPED OUT EARLY DUE TO MISCOMMUNICATION. THIS AND THE WIND GUSTS CAUSED THE JUMPER TO BE OFF COURSE OF THE TARGET LANDING AREA. THE PIC BELIEVED THAT THE WIND DATA IN THE WEATHER REPORTS WERE INCORRECT. THE WEATHER DATA SHOWED THAT THE AIRCRAFT WOULD HAVE LANDED WITH A QUARTERING TAIL WIND. THE PIC STATED IN PART THAT HE MADE TWO GO-AROUNDS DUE TO THE ?AIR BEING BUMPY? AND HE "DID NOT LIKE IT". ON THE PIC?S THIRD ATTEMPT, HE STATED ?HE HAD A TAILWIND AND THE AIRCRAFT WOULD NOT SETTLE.? UPON TOUCHDOWN, ^PRIVACY DATA OMITTED^ APPLIED THE BRAKES BUT DUE TO THE POSITION OF THE AIRCRAFT, IT DEPARTED THE RUNWAY. THE PIC STATED THE BRAKES WERE FULLY FUNCTIONAL. THE AIRCRAFT HIT THE FIRST TREE BETWEEN THE LEFT TIP TANK AND THE NUMBER ONE ENGINE. THE AIRCRAFT HIT SEVERAL OTHER TREES AND SUSTAINED SUBSTANTIAL DAMAGE. THE AIRCRAFT AND SOME PIECES CAUGHT FIRE. THE PIC AND ALL PASSENGERS REMAINING ONBOARD EVACUATED THE AIRCRAFT ON THEIR OWN WITH NO INJURIES.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N87266 · 1

Matched to the same aircraft by N-number and date.