Cessna 402

Operator:

Registration:

G-EYES

Flight Phase:

Flight Type:

Calibration

Survivors:

Site:

Schedule:

Coventry - Coventry

MSN:

402-0008

YOM:

1979

Location:

Country:

Region:

Crew on board:

Crew fatalities:

Pax on board:

Pax fatalities:

Other fatalities:

Total fatalities:

Captain / Total flying hours:

1627

Captain / Total hours on type:

125.00

Copilot / Total flying hours:

2281

Copilot / Total hours on type:

339

Circumstances:

Cessna 402C aircraft G-EYES was engaged in flight calibration training and was making an ILS approach to Runway 23 at Coventry Airport when it was involved in a mid-air collision with a Rand KR-2 aircraft, G-BOLZ, operating in the visual circuit. The collision occurred in Class G (uncontrolled) airspace. The four occupants of G-EYES and the single occupant of G-BOLZ received fatal injuries.

Probable cause:

The investigation identified the following primary causal factor:
The two aircraft collided because their respective pilots either did not see the other aircraft, or did not see it in time to take effective avoiding action.
The investigation identified the following contributory factors:
1. The likelihood that the crew of G-EYES would see G-BOLZ in time to carry out effective avoiding action was reduced by the small size of G-BOLZ, its position relative to G-EYES and the high rate of closure between the aircraft.
2. Insufficient or inaccurate information was provided to the pilots, which did not assist them in fulfilling their duty to take all possible measures to avoid collisions with other aircraft.
3. The Aerodrome Controller’s sequencing plan, which was based on an incomplete understanding of the nature of G-EYES’ flight, was unlikely to have been successful. By the time the risk of a collision was identified, it was too late to devise an effective method of resolving the situation.
4. There were no effective measures in place to give G-EYES priority over traffic in the visual circuit

Final Report:

Crash of a Cessna 402B in Ocean Ridge

Date & Time: Jul 22, 2008 at 1350 LT

Type of aircraft:

Operator:

Jean P. Bayardelle

Registration:

N3990C

Flight Phase:

Flight Type:

Survivors:

Site:

Schedule:

Lantana - Pompano Beach

MSN:

402B-0857

YOM:

1975

Location:

Ocean Ridge

Florida

Country:

United States of America

Region:

North America

Crew on board:

Crew fatalities:

Pax on board:

Pax fatalities:

Other fatalities:

Total fatalities:

Captain / Total flying hours:

1565

Aircraft flight hours:

7222

Circumstances:

The commercial pilot, who was also the former owner of the twin-engine airplane, stated that the purpose of the flight was to reposition the airplane to an airport approximately 22 miles south of the departure airport. Just prior to the flight, he purchased 10 gallons of fuel for each of the two main tanks. The pilot reported that about 5 minutes after takeoff, at an altitude of approximately 1,000 feet, he experienced a "loss of engine power." However, his three separate accounts of the event were inconsistent with respect to which engine had a problem, or the specific nature of the problem. The pilot reported that the airplane started to lose altitude "rapidly," and that he attempted to "wag the wings" in order to "get all the fuel to be useable." The airplane struck a building and terrain approximately 8 miles south of the departure airport. The pilot sustained serious injuries, but there was no fire. Damage to the left engine and propeller was consistent with the engine running at impact, and precluded an attempt to run the left engine in a test cell. Damage to the right engine and propeller was consistent with low or no power at impact. The right engine was subsequently successfully run in a test cell. No evidence of any pre-accident anomalies that could have contributed to the accident was noted with the airframe, engines, or propellers. The fuel selector valve placards did not accurately depict the fuel system configuration. The fuel quantity and its distribution in the tanks, either at the beginning of the flight or at the time of the accident, could not be determined.

Probable cause:

A partial loss of engine power due to fuel starvation. Contributing to the accident was the pilot’s decision to add only a limited amount of fuel prior to the flight, and the fuel selector valve placards' inaccurate depiction of the airplane fuel tank configuration.

Final Report:

EC-EHP

Read more about EC-EHP

Crash of a Cessna 402C in Freeport

Date & Time: Apr 21, 2006 at 0023 LT

Type of aircraft:

Operator:

Cambridge Air Services

Registration:

C6-KEV

Flight Phase:

Charter/Taxi (Non Scheduled Revenue Flight)

Flight Type:

Survivors:

Site:

Schedule:

Fort Lauderdale – Freeport

MSN:

402C-0051

YOM:

1979

Location:

Country:

Region:

Crew on board:

Crew fatalities:

Pax on board:

Pax fatalities:

Other fatalities:

Total fatalities:

Captain / Total flying hours:

3033

Circumstances:

At approximately 0423UTC on April 21, 2006 the pilot reported that approximately 20 miles out of Freeport, both hydraulic pressure lights illuminated on the annunciator panel. He extended the gear and noticed only the right gear safe light illuminated. The pilot obtained the assistance of a passenger, who retrieved the aircraft pilot operating handbook and read the appropriate procedures as the pilot followed the instructions for emergency gear extension. The pilot stated that he landed the aircraft on the right main gear, hoping this action would release the left main and nose gear. After realizing that this manoeuvre was not successful, he decided to initiate a go-around. Before he could get the aircraft airborne the left propeller made contact with the ground. The aircraft touched down approximately 9,000 feet from the threshold of runway 06; which has a total length of 11,000 feet. The aircraft travelled approximately 1,500 feet on its right main wheel before it veered off the left shoulder of the runway, struck several trees and finally came to rest pointing in a northwesterly direction. The approximate final position was measured to be 180 feet from the side of the runway. The aircraft left wing burst into flames. The left wing and left side of the fuselage was substantially damaged by fire. The four occupants escaped with only minor injuries.

Probable cause:

The investigation determines that the probable causes of this accident to be the following;
• Substandard maintenance that was performed. (Due to the improper flange on the hydraulic line, the hydraulic line came loose from its housing and depleted the fluid from the hydraulic
reservoir).
• Failure of the back up emergency blow down bottle system. It has been determined from inspection that the cable that connects the emergency blow down bottle system in the nose well of the aircraft to the T-handle in the cockpit, exhibited excessive play. Therefore even though the cable was pulled all the way to its fullest extent, it did not allow movement of the pin that would have provided activation of the system. Annual inspection report completed in December 2005 revealed that the portion of the Annual Inspection that required inspection of the emergency blow down bottle was not signed off by the mechanic as having been accomplished. However, the aircraft was returned to service with this discrepancy outstanding.
• Pilot’s lack of qualification and unfamiliarity with this aircraft, its systems and emergency procedures. ( Evidence of falsification of qualification and time requirement exists in pilot’s logbook).
• Pilot’s poor decision making and impaired judgement. (Possibility of impaired judgement due to pilot fatigue).
• Pilot’s failure in assessing the severity of his situation.
• Pilot’s failure to notify ATC of his problem. (Problem was discovered 20 miles prior to the accident).
• Pilot’s failure to properly assess the conditions for landing and maintain vigilant situational awareness while manoeuvring the aircraft after landing. (From post accident inspection, it was noted that the flaps were not extended for the landing. Had it been extended the aircraft glide path as well as the distance required for roll out after landing may have been greatly decreased).
• Pilot’s failure to take immediate action once he realized his predicament. (Pilot stated that after the propeller made contact with the ground, he decided to apply power and go around, but it was too late. Failure to act also can be attributed to possible pilot fatigue as (pilot was out all day shopping and then decided to leave at such a late hour) well as pilot’s unfamiliarity with aircraft systems and performance capabilities).
• Pilot’s failure to request Emergency Service Assistance. Had this service been requested in a timely manner, preparations could have been made to prevent the fire from spreading to the degree in which it did.

Final Report:

Crash of a Cessna 402B in Walker's Cay

Date & Time: Mar 31, 2004 at 1235 LT

Type of aircraft:

Operator:

Registration:

N269JH

Flight Phase:

Flight Type:

Cargo

Survivors:

Site:

Schedule:

Fort Lauderdale – Walker’s Cay

MSN:

402B-1213

YOM:

1976

Location:

Country:

Region:

Crew on board:

Crew fatalities:

Pax on board:

Pax fatalities:

Other fatalities:

Total fatalities:

Circumstances:

On March 31, 2004, about 1235 eastern standard time, a Cessna 402B, N269JH, registered to and operated by Tropic Air Charters, Inc., experienced collapse of all landing gears at the Walker's Cay Airport, Walker's Cay, Bahamas. Visual meteorological conditions prevailed at the time and a visual flight rules flight plan was filed for the 14 CFR Part 135 on-demand, non-scheduled, international, cargo flight from the Fort Lauderdale Executive Airport, Fort Lauderdale, Florida, to the Walker's Cay Airport, Walker's Cay, Bahamas. The airplane was substantially damaged and the commercial-rated pilot, the sole occupant, was not injured. The flight originated about 45 minutes earlier from the Fort Lauderdale Executive Airport. The pilot stated that after landing, the right wing tipped down in what appeared to be a flat tire. He attempted to maintain control of the airplane using the rudder and was successful until the airplane rolled approximately 1,000 feet. The airplane then veered to the right and collided with a tree. The left wing and fuselage were damaged.

Crash of a Cessna 402C in Nantucket: 1 killed

Date & Time: Sep 23, 2003 at 0523 LT

Type of aircraft:

Operator:

Registration:

N405BK

Flight Phase:

Flight Type:

Cargo

Survivors:

Site:

Schedule:

Hyannis – Nantucket

MSN:

402C-0459

YOM:

1981

Flight number:

IS400

Location:

Nantucket

Massachusetts

Country:

United States of America

Region:

North America

Crew on board:

Crew fatalities:

Pax on board:

Pax fatalities:

Other fatalities:

Total fatalities:

Captain / Total flying hours:

14000

Captain / Total hours on type:

4000.00

Aircraft flight hours:

9795

Circumstances:

The pilot was conducting an instrument landing system approach during night instrument meteorological conditions. The airplane was observed to descend toward the runway threshold to an altitude consistent with the approach decision height. A witness reported that he heard the airplane overhead, and assumed that the pilot had performed a missed approach. He described the engine noise as "cruise power" and did not hear any unusual sounds. Shortly thereafter, he received a call from airport operations stating that an airplane had crashed. The airplane impacted the ground about 1/4 mile to the left of the runway centerline, about 3,500 feet beyond the approach end of the runway. Examination of the airplane did not reveal any pre-impact mechanical malfunctions. A weather observation taken around the time of the accident, included a visibility 1/2 statue mile in fog, and an indefinite ceiling at 100 feet. The witness described the weather at the time of the accident as thick fog, and "pitch black."

Probable cause:

The pilot's failure to maintain aircraft control during a missed approach. Factors in this accident were fog and the night light conditions.

Final Report:

Crash of a Cessna 402B near Tecalitlán: 8 killed

Date & Time: Sep 13, 2003 at 1830 LT

Type of aircraft:

Operator:

Registration:

XB-FTA

Flight Phase:

Flight

Flight Type:

Private

Survivors:

Site:

Mountains

Schedule:

Toluca – Colima

MSN:

402B-1049

YOM:

1976

Location:

Country:

Region:

Crew on board:

Crew fatalities:

Pax on board:

Pax fatalities:

Other fatalities:

Total fatalities:

Circumstances:

While cruising under VFR mode at an altitude of 8,400 feet in poor weather conditions, the twin engine aircraft struck the slope of a mountain located near Tecalitlán. The aircraft was totally destroyed and all eight occupants were killed. At the time of the accident, weather conditions were poor over State of Jalisco due to a tropical storm with heavy rain falls and strong winds.

Probable cause:

Controlled flight into terrain after the pilot decided to continue under VFR mode in IMC conditions.

Crash of a Cessna 402 in Guadalajara

Date & Time: Sep 13, 2003

Type of aircraft:

Operator:

Registration:

XA-TVX

Flight Phase:

Takeoff (climb)

Flight Type:

Private

Survivors:

Site:

Guadalajara-Miguel Hidalgo y Costilla

Schedule:

Guadalajara – Zihuatanejo

Location:

Jalisco

Country:

Mexico

Region:

Central America

Crew on board:

Crew fatalities:

Pax on board:

Pax fatalities:

Other fatalities:

Total fatalities:

Circumstances:

Shortly after takeoff, the twin engine lost height and crashed in a cornfield. All seven occupants were injured and the aircraft was damaged beyond repair.

Crash of a Cessna 402C off Treasure Cay: 2 killed

Date & Time: Jul 13, 2003 at 1530 LT

Type of aircraft:

Operator:

Registration:

N314AB

Flight Phase:

Flight Type:

Scheduled Revenue Flight

Survivors: