Cessna 402A N99AT

Summary

On 9 March 2004 at about 18:25 local time, a Cessna 402A registered N99AT, operated by King Airlines, Inc., was involved in an accident near Peach Springs, Arizona, United States. 10 people were on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

9 March 2004 at 18:25

Classification

Accident

Location

Peach Springs, Arizona, United States

Nearest airport

Grand Canyon West (1G4)

Coordinates

35.9950, -113.8000

Aircraft

Cessna 402A

Registration

N99AT

Category

Airplane

Engines

2

Operator

King Airlines, Inc.

Operating rule

Part 135: Air Taxi & Commuter

Phase of flight

Not recorded

Route

Henderson → Peach Springs

Aircraft damage

Substantial

Weather

VMC

Light

Day

NTSB number

LAX04LA149

Nobody was injured.

the pilot's inadequate flare and touchdown that imparted high side loadings on the right main landing gear, which resulted in an overload failure of the landing gear bellcrank and the collapse of that gear.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The right main landing gear collapsed during the landing roll. The pilot placed the landing gear in the down position on downwind and noted three green lights, which indicated that the gear was down and locked. He noted a left crosswind, and landed on the left main landing gear first and then the right main landing gear. When the right main landing gear touched the ground, it folded up, and the airplane departed the runway. The airplane went over a berm, which sheared off the left main landing gear and the nose landing gear. The passengers safely deplaned. A pilot in another company airplane about 1 mile behind and 1,000 feet above the accident airplane observed the landing. He indicated that the approach and landing appeared normal. According to the Federal Aviation Administration inspector who inspected the accident scene, the airplane touched down near the threshold. There were two propeller strikes on the runway about 15 inches apart about 40 feet past the touchdown point. About 200 feet farther down the runway, there were multiple propeller strikes. The area between the first set of propeller strikes and the second set was clear of any marks. The inspector observed skid marks that began at the second set of propeller strikes and continued down the runway where the airplane departed the runway. The airplane had flown 2 hours since a routine maintenance inspection that included many components of the landing gear system. No discrepancies were noted on the failed components of the right main landing gear. Post accident inspection by the operator's maintenance personnel found that the pivot bolt in the right main landing gear bellcrank assembly (part number NAS 464P4-26) had sheared in two places, and the clevis ears at both ends of the bell crank were fractured. They said that this lead to other parts shifting and breaking, which lead to the right main landing gear collapsing. Metallurgical examination of the bell crank, the clevis ears, and the bolt determined that all of the materials examined were within specification. None of the fractures showed any evidence of pre-existing damage or fatigue cracking. The bolt fractured in shear overstress on a plane flush with the edge of the bellcrank. The damage to the pivot bolt appeared to be most consistent with an event where the gear was heavily loaded outward, away from its normal retracted position. Detailed analysis of the loadings on the failed components and the lack of damage on the surrounding structures and landing gear parts revealed no obvious scenario that would have led to the bellcrank being the first component loaded sufficiently to cause the damage observed and/or initiate the collapse of the landing gear. It is most likely that the damage to the bellcrank was a result of the collapse of the gear, rather than a cause.

Quoted verbatim from the NTSB record.