Crash of a Cessna 421C Golden Eagle III in Humberside: 1 killed

Date & Time: Mar 29, 2003 at 1229 LT
Registration:
G-SAIR
Flight Type:
Survivors:
Yes
Schedule:
Humberside - Humberside
MSN:
421C-0471
YOM:
1978
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2250
Captain / Total hours on type:
1850.00
Copilot / Total flying hours:
20000
Copilot / Total hours on type:
600
Circumstances:
About 50 minutes into the flight, the aircraft returned to Humberside circuit and was cleared by ATC for a touch-and-go landing on Runway 21. The landing was firm but otherwise uneventful and witnesses heard the power being applied as it accelerated for takeoff. Just before rotation two large "puffs of smoke" were seen to come from the vicinity of the mainwheels as both propellers struck the runway. The aircraft then lifted off and almost immediately began to yaw and roll to the left. The left bank reached an estimated maximum of 90° but reduced just before the left wing tip struck the ground. The aircraft then cartwheeled across the grass to the south of the runway and burst into flames. The owner in the left pilot's seat and the pilot in the right pilot's seat escaped from the wreckage, but the flight examiner, who was occupying a seat in the passenger cabin, was unable to vacate the aircraft and subsequently died of injuries sustained in the post impact fire. An engineering investigation found no fault with the aircraft that might have caused the accident. The investigation concluded that the most probable cause was an inadvertent retraction of the landing gear whilst the aircraft was still on the ground.
Probable cause:
An engineering investigation found no fault with the aircraft that might have caused the accident. The investigation concluded that the most probable cause was an inadvertent retraction of the landing gear whilst the aircraft was still on the ground. The confusion over individual roles would have been resolved if the examiner had given a pre-flight briefing in line with the guidance contained in the FAA Designated Examiners' Handbook, but both pilots have stated that this briefing did not take place. In any event, the FAA Handbook and FARs are unclear on who should be the commander of the flight although FAR 61.47 states the examiner is not normally to be the Pilot in Command except by prior agreement with the applicant or other person who would normally be acting as Pilot in Command. Nevertheless, it is clear that the instructor should have been briefed that he was fulfilling the safety pilot role and was responsible for "protect(ing) the overall safety of the flight to whatever extent is necessary". If the instructor had clearly understood this responsibility, he might have monitored the owner's actions more closely during the touch-and-go and might have intervened earlier. Notwithstanding the confusion, the instructor took control when he considered that the owner was not taking appropriate action to control the aircraft, although the actual moment that he took control is in dispute. Given the owner's belief that the instructor was the commander and that the instructor was in any case by far the more experienced pilot, it is not surprising that he relinquished control even though, unknowingly, he had a more complete understanding of the aircraft's predicament. The flight time from the propeller strikes to the next ground impact was only a few seconds. Once the aircraft became airborne with a significant amount of power applied and a badly damaged left propeller, the situation was well beyond any emergency for which either pilot might have trained. The options for action were very limited and would have required a full appreciation of the circumstances, plus extremely rapid analysis and reactions if those actions were to be successful.
Final Report:

Crash of a Canadair CL-215-6B11 off Port de Pollença: 2 killed

Date & Time: Mar 25, 2003
Type of aircraft:
Operator:
Registration:
UD.13-29
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
1124
YOM:
1990
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew was completing a training flight consisting of dropping survival equipment when the aircraft crashed in unknown circumstances in the sea off Port de Pollença. Two crew members were rescued while two others were killed.

Ground accident of a Fokker F27 Friendship 500 in Blenheim

Date & Time: Feb 27, 2003 at 1950 LT
Type of aircraft:
Operator:
Registration:
ZK-NAN
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Blenheim - Blenheim
MSN:
10365
YOM:
1968
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The Airwork F-27 was on a training flight, during which the crew carried out an exercise that simulated a gear problem. They extended the gear using the emergency system. However, after landing they did not select the main gear handle down and in addition did not install the gear locking pins. The crew were then distracted by other events and during this the co-pilot selected the emergency gear handle up to reset the system. The main gear then partially collapsed.

Ground accident of a Dornier DO228-201 in Karachi

Date & Time: Feb 19, 2003
Type of aircraft:
Operator:
Registration:
AP-BGF
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Karachi - Karachi
MSN:
8016
YOM:
1983
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful training flight at Karachi-Quaid-e-Azam Airport, the crew was taxiing to his parking place when control was lost. The aircraft rolled across the apron and eventually collided with a concrete wall. Both pilots escaped uninjured while the aircraft was damaged beyond repair.

Crash of a Britten-Norman BN-2A-21 Defender at Braasschaat AFB

Date & Time: Feb 14, 2003
Type of aircraft:
Operator:
Registration:
B-03
Flight Type:
Survivors:
Yes
Schedule:
Braasschaat - Braasschaat
MSN:
476
YOM:
1975
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a local training flight at Braasschaat AFB. For unknown reasons, the twin engine aircraft landed hard and bounced several times before coming to rest on the runway. Both pilots escaped with minor injuries and the aircraft was damaged beyond repair.

Crash of a Cessna 208B Super Cargomaster in San Angelo

Date & Time: Jan 24, 2003 at 1015 LT
Type of aircraft:
Operator:
Registration:
N944FE
Flight Type:
Survivors:
Yes
Schedule:
San Angelo - San Angelo
MSN:
208B-0044
YOM:
1987
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4356
Copilot / Total flying hours:
13884
Aircraft flight hours:
7503
Circumstances:
The airplane impacted a dirt field and a power line following a loss of control during a simulated engine failure while on a Part 135 proficiency check flight. Both pilots were seriously injured and could not recall any details of the flight after the simulated engine failure. Witnesses observed the airplane flying on a westerly heading at an altitude of 100 to 200 feet, and descending. They heard the sound of an engine “surging” and observed the airplane’s wings bank left and right. The airplane continued to descend and impacted the ground and power lines before becoming inverted. A pilot-rated witness reported that he observed about ¼ inch of clear and rime ice on the airplane’s protected surfaces (deice boots) and about ½ inch of ice on the airplane’s unprotected surfaces. An NTSB performance study of the accident flight based on radar data indicated that the airplane entered a descent rate of 1,300 feet per minute (fpm) about 1,100 feet above the ground. This rate of descent was associated with a decrease in airspeed from 130 knots to 92 knots over a span of 30 seconds. The airplane’s rate of descent leveled off at the 1,300 fpm rate for 45 seconds before increasing to a 2,000 fpm descent rate. The true airspeed fluctuated between a low of 88 knots to 102 knots during the last 45 seconds of flight. According to the aircraft manufacturer, the clean, wing flaps up stall speed was 78 knots. However, after a light rime encounter, the Pilot’s Operating Handbook (POH) instructed pilots to maintain additional airspeed (10 to 20 KIAS) on approach “to compensate for the increased pre-stall buffet associated with ice on the unprotected areas and the increased weight.” With flaps up, a minimum approach speed of 105 KIAS was recommended. The POH also stated that a significantly higher airspeed should be maintained if ½ inch of clear ice had accumulated on the wings.
Probable cause:
The flight crew's failure to cycle the deice boots prior to conducting a simulated forced landing and their failure to maintain adequate airspeed during the maneuver, which resulted in an inadvertent stall and subsequent loss of control. A contributing factor was the ice accumulation on the leading edges of the airfoils.
Final Report:

Crash of a Lockheed MC-130H Hercules in Caguas: 10 killed

Date & Time: Aug 7, 2002 at 2050 LT
Type of aircraft:
Operator:
Registration:
90-0161
Flight Type:
Survivors:
No
Site:
Schedule:
Roosevelt Roads - Roosevelt Roads
MSN:
5265
YOM:
1991
Country:
Crew on board:
10
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
10
Circumstances:
The crew departed Roosevelt Roads NAS on a local training flight. In the evening, while returning the to NAS, the crew encountered poor weather conditions with low clouds, limited visibility and rain falls. While descending at low height, the crew suffered a loss of situational awareness and failed to respond to obstacle warnings. The four engine aircraft collided with trees and crashed on the top of Mt Perucho. The aircraft disintegrated on impact and all 10 crew members were killed.
Probable cause:
By clear and convincing evidence, the cause of this mishap was an uncharacteristic loss of situational awareness by the entire mishap flight deck crew and the subsequent lack of an appropriate response to obstacle warnings. The Board President further found the following factors substantially contributed to the mishap: overall crew preparation, a misdirected focus on the weather, crew resource management dynamics, and crew judgment as it relates to existing directives.

Crash of a De Havilland DHC-5 Buffalo near Mugumo

Date & Time: Jul 25, 2002
Type of aircraft:
Operator:
Flight Phase:
Flight Type:
Survivors:
Yes
Location:
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was engaged in a training mission when the crew encountered engine problems. The aircraft crash landed near Mugumo and was damaged beyond repair. All seven occupants escaped uninjured.
Probable cause:
Engine failure for unknown reasons.

Crash of an Antonov AN-24RV in Yakutsk

Date & Time: Jul 13, 2002 at 1418 LT
Type of aircraft:
Operator:
Registration:
RA-46670
Flight Type:
Survivors:
Yes
Schedule:
Yakutsk - Yakutsk
MSN:
47309601
YOM:
1974
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The Antonov departed Yakutsk on a crew training flight. Two approach and landings were carried out using flap settings of 38 and 15 degrees. During the third approach the captain called for lowering of the landing gear. The flight engineer moved the landing gear handle from neutral into the "retract" position. He did not check for three greens so failed to notice his mistake. Then the captain requested the flaps to be selected at 10 degrees. The Antonov turned to finals, but the crew did not carry out the final approach checks and continued after having obtained landing clearance. Fourteen seconds before touchdown an air traffic controller informed the crew that they should go around because the landing gear was not down. The captain did not hear this because at that moment height and speed were called out by the flight engineer. Five seconds later the controller repeated his warning. One of the crew members heard the call and noticed three reds on the instrument panel. He informed that captain about this, but it was already too late. The captain added takeoff power, but within three seconds the tail struck the runway. The airplane skidded about 1000 metres before coming to rest.
Probable cause:
The accident was caused by the combination of the following factors:
- The erroneous actions of the flight engineer when trying to lower the landing gear,
- Failure of the flight crew to conduct the necessary (final approach) checks,
- The failure by the crew to check and respond to landing gear warning indications,
- The execution of a flight with an incomplete composition of crew, causing additional workload on the flight engineer during the approach (height and speed call outs),
- Late commands to go around by the air traffic controller,
- On the Yak-40 the landing gear handle moves to the opposite direction for retraction and lowering compared to the Antonov 24 (the flight mechanic had more, and recent, flight experience on the Yakovlev 40 jet),
- The large workload and fatigue of the crew during the recent six days before the incident.

Crash of a Boeing 767-281 in Shimoji-shima

Date & Time: Jun 26, 2002 at 1254 LT
Type of aircraft:
Operator:
Registration:
JA8254
Flight Type:
Survivors:
Yes
Schedule:
Shimoji-shima - Shimoji-shima
MSN:
23433
YOM:
1987
Flight number:
NH8254
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
10375
Captain / Total hours on type:
6654.00
Copilot / Total flying hours:
259
Copilot / Total hours on type:
5
Aircraft flight hours:
35347
Circumstances:
On June 26, 2002, a Boeing 767-200 of All Nippon Airways, registration JA8254, took off from Shimoji-Shima Airport at around 11:32 on a flight for takeoff and landing training. The flight plan of the aircraft submitted to the Shimoji-Shima Airport Office of the Japan Civil Aviation Bureau (CAB) was as follows: FLIGHT RULES: VFR, AERODROME of DEPARTURE: Shimoji-Shima Airport, TIME: 11:20, CRUISING SPEED: 250kt, LEVEL: VFR, ROUTE: Traffic Pattern, DESTINATION AERODROME: Shimoji-Shima Airport, FLIGHT PURPOSE: Training Flight, TOTAL EET: 1 hour 40 minutes, ENDURANCE: 6 hrs 32 minutes, PERSONS ON BOARD: 3. The three persons on board were in the cockpit at the time of the accident: A pilot undergoing training for promotion to First Officer (Trainee Pilot-A) occupying the left pilot’s seat, the Captain acting as instructor occupying the right pilot’s seat, and another pilot undergoing training for promotion to First Officer (Trainee Pilot-B) occupying the left observer’s seat. First, Trainee Pilot-B made seven landings on runway 17 from the left pilot’s seat, including two landings with one engine simulated inoperative, and a go-around with both engines operative. He then changed places with Trainee Pilot-A. At around that time, the wind direction changed from the south to the west, and the aerodrome control tower instructed a change to runway 35. Trainee Pilot-A then made two landings on runway 35 with both engines operative, and training then switched to landing with one engine simulated inoperative. The first landing was made with the left engine simulated inoperative. After that, during a landing with the right engine simulated inoperative, the touchdown was late and Trainee Pilot-A attempted to go-around with go-around thrust on the left engine only. A few seconds later the instructor increased power on the right engine to go-around thrust, but at that time even though the left engine thrust had started to increase the right engine was still at minimum idle thrust. As a result, a thrust imbalance occurred between the left and right engines while right rudder was
being applied, and the aircraft rolled and yawed to the right (East). Although Trainee Pilot-A and the instructor attempted to correct the attitude changes, the aircraft veered off the runway into a grass field on east side of the runway and came to a stop around 1,990m from the point it had first touched down. The accident occurred at runway 35 of Shimoji-Shima Airport at around 12:54.
Probable cause:
It is estimated that the accident was caused as follows:
The aircraft was being operated on a training flight at Shimoji-Shima Airport, and was making a one-engine-out touch-and-go landing with the right engine simulated inoperative. The touchdown was late and beyond the normal aim point, and on the direction of the instructor, the trainee pilot attempted to go around on only the left engine. However, the trainee mishandled the aircraft, and then, seeing the instructor advance the right engine’s thrust lever, he applied right rudder pedal mechanically. This coincided with an increase in the rotation speed of the left engine, and the aircraft’s attitude suddenly changed towards the right. Because the trainee pilot could not fully correct this and the instructor was late in taking over control, the aircraft veered off the east side of the runway into a grass area and was damaged. Moreover, it is estimated that the following causal factors contributed to the accident:
1) The instructor did not take over when he directed the trainee to go around, or at an earlier stage, because he thought to allow the trainee pilot to handle the aircraft as much as possible, and because he did not sufficiently recognize that a go-around with one-engine simulated inoperative is a difficult maneuver for an inexperienced pilot.
2) Regarding the instructor’s intent to allow the trainee pilot to handle the aircraft as much as possible, the company’s instructional guidelines contained statements meaning that a judgment to go around should be made by the trainee pilot, and that during simulated one-engine-out touch-and-go training landings, the go-around after landing should continue with one engine simulated inoperative.
3) Regarding the instructor’s insufficient recognition of the difficulty of a go-around with one engine simulated inoperative for an inexperienced pilot, the instructor had not been trained to deal with the situation encountered in the accident, and the company’s regulations and manuals did not describe considerations on the difficulty of executing a go-around with one-engine simulated inoperative for an inexperienced pilot or on the effects of the wind on such maneuvers.
4) Regarding the delay in the instructor taking over control of the aircraft, the instructor was not following with his hands on the control wheel and was not in a position to take over immediately if necessary, and when the instructor had changed from being a simulator instructor to a flight instructor, he had not received sufficient training on cautionary matters regarding training in actual aircraft.
Final Report: