Crash of a BAe 125-3A in Waukegan

Date & Time: May 30, 1994 at 1842 LT
Type of aircraft:
Registration:
N900CD
Flight Type:
Survivors:
Yes
Schedule:
Wheeling - Waukegan
MSN:
25111
YOM:
1966
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
10000
Captain / Total hours on type:
950.00
Circumstances:
The corporate jet's sink rate increased during short final approach. The copilot applied elevator back pressure and nose up trim. The sink rate continued to increase. The captain observed the copilot's efforts and began applying back pressure on his control yoke. Through combined efforts of both pilots they were able to increase the pitch enough that the airplane touched down on the main gear first. However, the touchdown was hard. The on-scene investigation revealed that a trip manifest container was lodged between the copilot's control yoke column and seat frame. The pilots stated the container is required to be carried in the cockpit during lights. Both pilots said there is no designated space in the cockpit to retain the container.
Probable cause:
The pilot-in-command disregarding the location of the flight manifest container in the cockpit. Factor's associated with the accident were a jammed control column and inadequate procedures for the use and storage of the flight manifest container on the part of company management.
Final Report:

Crash of a Hawker-Siddeley HS.125-1A-522 on Mt Otay: 10 killed

Date & Time: Mar 16, 1991 at 0143 LT
Type of aircraft:
Registration:
N831LC
Flight Phase:
Survivors:
No
Site:
Schedule:
San Diego – Amarillo – Evansville
MSN:
25095
YOM:
1966
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
10
Captain / Total flying hours:
15000
Captain / Total hours on type:
150.00
Circumstances:
After flying personnel of entertainment group to Lindbergh Field, aircraft was positioned to nearby Brown Field, since late departure was planned after noise curfew was in effect at Lindbergh. Pilot talked with FSS specialist (splst) 3 times before takeoff. He reported he did not have instruction departure procedures from airport. Splst read departure procedures on phone. On last call to FSS, pilot said he planned to depart VFR toward northeast and obtain IFR clearance after airborne (this route was toward mountains.) During call, pilot expressed concern about remaining cleared of TCA and inquired about staying below 3,000 feet. Splst agreed with pilots concerns, but after accident, splst said he thought pilot was referring to 3,000 feet agl, rather than 3,000 feet msl. Pilot had filed to takeoff at midnight, but didn't get airborne until 0141 pst. Since flight was over 1.5 hours late, IFR flight plan had 'clocked out.' As controller was reentering flight plan in computer, aircraft hit rising terrain near top of mountain, about 8 miles northeast of airport at elevation of about 3,300 feet. No deficiencies were found with aircraft or its engines. Copilot had no type rating for this aircraft, tho he reportedly had made 3 takeoffs and landings in Hawker-Siddeley HS.125. All 10 occupants were killed, among them all members of the country music 'Reba McEntire Band'.
Passengers:
Chris Austin,
Kirk Cappello,
Joey Cigainero,
Paul Kaye Evans,
Jim Hammond,
Terry Jackson,
Anthony Saputo,
Michael Thomas.
Probable cause:
Improper planning/decision by the pilot, the pilot's failure to maintain proper altitude and clearance over mountainous terrain, and the copilot's failure to adequately monitor the progress of the flight. Factors related to the accident were: insufficient terrain information provided by the flight service specialist during the preflight briefing after the pilot inquired about a low altitude departure, darkness, mountainous terrain, both pilot's lack of familiarity with the geographical area, and the copilot's lack of familiarity with the aircraft.
Final Report:

Crash of a Hawker-Siddeley HS.125-3B in Columbia: 1 killed

Date & Time: Jan 30, 1990 at 2205 LT
Type of aircraft:
Operator:
Registration:
G-OBOB
Survivors:
Yes
Schedule:
Crossville - Olathe
MSN:
25069
YOM:
1966
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1525
Captain / Total hours on type:
400.00
Aircraft flight hours:
8720
Circumstances:
The aircraft was en route at 31,000 feet, when the low pressure fuel filter warning light illuminated. The pilot diverted toward Columbia, MO, but before reaching Columbia, both engines lost power. Subsequently, the aircraft crashed about 2 miles east of the airport. An investigation revealed the fuel was contaminated with water. The fuel filter deicing system was operational, but a post-accident examination revealed the deicing tank was empty. This was the 2nd flight since the deice tank had been serviced. The manufacturer's info indicated the supply tank should have provided about 3 to 4 hours of filter deicing operation. One of the pilots was killed.
Probable cause:
Inadequate preflight by the pilot(s), water contamination of the fuel, low level of deice fluid (methanol) in the deice tank, and subsequent ice blockage of the fuel filters. Darkness was a related factor.
Final Report:

Crash of a BAe 125-3A in Houston

Date & Time: Aug 13, 1989 at 1750 LT
Type of aircraft:
Operator:
Registration:
N66HA
Flight Type:
Survivors:
Yes
Schedule:
Savannah - Houston
MSN:
25126
YOM:
1967
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5180
Captain / Total hours on type:
10.00
Aircraft flight hours:
3966
Circumstances:
During landing, upon nose wheel contact with the runway, directional control was lost and the aircraft exited the runway hard surface and crossed a ditch collapsing the nose gear. The crew stated that full left rudder and differential braking would not stop the right drift, and that the aircraft was in grass uncontrollable by the time the steering tiller was reached. The nose wheel steering system was extensively damaged by the impact sequence when the nose wheel well aft bulkhead was forced into the steering assembly. The pilot stated that if he had been 'spring loaded to the tiller' that he could have possibly kept the aircraft off the grass.
Probable cause:
Failure of the nose wheel steering system for undetermined reasons, and the pilot-in-command's hesitation reaching for the nose wheel steering tiller. A contributing factor was his lack of experience in a DH-125.
Final Report:

Crash of a Hawker-Siddeley HS.125-600A in Houston: 1 killed

Date & Time: Jan 18, 1988 at 1010 LT
Type of aircraft:
Operator:
Registration:
XA-KUT
Survivors:
Yes
Schedule:
Laredo - Houston
MSN:
256028
YOM:
1974
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
10000
Captain / Total hours on type:
4000.00
Aircraft flight hours:
2812
Circumstances:
Before takeoff, a pilot of XA-KUT was briefed that the Houston Hobby (HOU) weather was IFR with '. . . Indefinite ceiling zero sky obscured visibility's 1/16 of a mile and fog . . .' He was also advised IFR conditions were forecast until 0900 cst, gradually improving to marginal VFR by 1100 cst with 1,000 feet broken, 5 miles visibility and fog. The flight took off at 0900 cst. At HOU, arrival was delayed due to weather. The crew requested an ILS approach, with intentions of diverting if a missed approach was made. The RVR was variable. After being cleared for an ILS runway 04 approach, the pilot was advised the RVR had dropped to 1,400 feet. After changing to tower frequency, the flight was cleared to land and was told again the RVR was 1,400 feet. When the aircraft was on final approach, the pilots were advised of a low altitude alert. However, the aircraft continued below the decision height (dh), hit a 70 feet power line (approximately 6,500 feet short of the runway) and crashed. No preimpact malfunction of the aircraft or its systems was found. The ILS was flight checked, but only a minor discrepancy (concerning the outer marker width) was noted. The dh was 200 feet agl, minimum RVR for the approach was 2,400 feet. The copilot was killed and seven other occupants were injured, three seriously.
Probable cause:
Occurrence #1: in flight collision with object
Phase of operation: approach - faf/outer marker to threshold (ifr)
Findings
1. Weather condition - low ceiling
2. Weather condition - fog
3. Weather condition - obscuration
4. (f) weather condition - below approach/landing minimums
5. (c) ifr procedure - improper - pilot in command
6. (c) decision height - not identified - pilot in command
7. (f) object - wire, transmission
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Hawker-Siddeley HS.125-400A in Lexington: 2 killed

Date & Time: Dec 5, 1987 at 1450 LT
Type of aircraft:
Registration:
N400PH
Survivors:
Yes
Schedule:
Dallas - New York
MSN:
25180
YOM:
1968
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
20565
Aircraft flight hours:
5710
Circumstances:
While en route at FL370, the pilots declared an emergency, reported a fire in the right engine and requested vectors to the nearest suitable airport. They were vectored toward the Lexington-Blue Grass Airport and circled to descend. Shortly after declaring an emergency, the pilots reported they secured the right engine and extinguished the fire light. As the aircraft was on final approach to land, the local controller (using binoculars) confirmed that both the gear and flaps were extended. However, as the aircraft continued onto a short final approach, an increase in its pitch attitude was noted. It then dropped below the level of the runway threshold and impacted in a pasture short of the runway. After initial impact, the aircraft went thru a stone fence, hit 2 utility poles, crossed a highway, came to rest at the perimeter fence and burned. An auto was damaged by debris; 2 occupants received minor injuries. An investigation revealed the aircraft impacted with the gear extended, but the flaps and flap handle were found in the up position. An examination of the right engine revealed its outer exhaust cone was cracked in the vicinity of a fire detection loop. No other preexisting mechanical problems were evident. Both pilots were killed and both passengers were seriously injured.
Probable cause:
Occurrence #1: airframe/component/system failure/malfunction
Phase of operation: cruise - normal
Findings
1. (f) exhaust system, exhaust cone/tailpipe (jet engine) - cracked
2. (f) exhaust system, exhaust cone/tailpipe (jet engine) - leak
3. (f) engine compartment - overtemperature
----------
Occurrence #2: loss of engine power
Phase of operation: cruise
Findings
4. 1 engine
5. Emergency procedure - intentional
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: approach - vfr pattern - final approach
Findings
6. Precautionary landing - initiated
7. (c) raising of flaps - inadvertent
8. (c) stall/mush - inadvertent - pilot in command
Final Report:

Crash of a BAe VU-93 in Carajás: 9 killed

Date & Time: Sep 8, 1987 at 1908 LT
Type of aircraft:
Operator:
Registration:
2129
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Carajás – Brasília
MSN:
25290
YOM:
1973
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
Shortly after takeoff, while in initial climb, the aircraft lost height and crashed in a huge explosion. All nine occupants were killed, among them Marcos de Barros Freire, Brazilian minister of Agrarian Reform.

Crash of a BAe 125-600B in Casablanca: 10 killed

Date & Time: Dec 15, 1986
Type of aircraft:
Registration:
5N-AWS
Survivors:
No
Site:
MSN:
256042
YOM:
1975
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
10
Circumstances:
On approach to Casablanca-Nouasseur Airport, the crew failed to realize his altitude was insufficient when the aircraft crashed into houses located 2 km short of runway. All eight occupants were killed as well as two people on the ground.

Crash of a Hawker-Siddeley HS. 125-1A-522 in Bedford: 2 killed

Date & Time: Aug 2, 1986 at 1806 LT
Type of aircraft:
Registration:
N50HH
Flight Type:
Survivors:
No
Schedule:
Toledo – Bedford
MSN:
25022
YOM:
1965
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
6544
Captain / Total hours on type:
605.00
Circumstances:
The pilot canceled IFR 8 miles from the airport to continue on a visual approach and landing. Witnesses stated a strong thunderstorm had just passed over the airport. Wind info issued to the pilot by unicom were west at 20 knots. Witnesses observed the aircraft approach runway 31 and execute a go-around before touchdown. The aircraft circled left to a runway 06 (almost direct downwind) approach. Touchdown occurred about 2/3 down the 3,100 feet long runway. The engines were heard to spool up to high power (no thrust reversers) but the aircraft did not become airborne. It overran the runway into rough terrain and caught fire. Investigation showed the landing gear was down, flaps were at approach setting and speed brakes were fully deployed. Both pilots were killed.
Probable cause:
Occurrence #1: overrun
Phase of operation: landing
Findings
1. (f) wrong runway - selected - pilot in command
2. (f) weather condition - tailwind
3. (c) proper touchdown point - not attained - pilot in command
4. (c) go-around - delayed - pilot in command
5. (f) speed brakes - improper use of - pilot in command
----------
Occurrence #2: on ground/water encounter with terrain/water
Phase of operation: landing
Findings
6. (f) terrain condition - rough/uneven
Final Report:

Crash of a BAe 125-700B in Kaduna: 7 killed

Date & Time: Dec 31, 1985
Type of aircraft:
Operator:
Registration:
5N-AXP
Flight Type:
Survivors:
No
Schedule:
Abuja - Kaduna
MSN:
257203
YOM:
1983
Location:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The crew was cleared to descent to 4,500 feet when the aircraft went out of control and crashed in an open field located 32 km short of runway. The aircraft was destroyed upon impact and all seven occupants were killed.
Probable cause:
The exact cause of the accident was not determined with certainty. However, it is believed that the loss of control was the consequence of the combination of the following factors:
- Lack of altitude awareness on part of the crew,
- Crew distraction,
- Poor judgment on part of the crew,
- Possible optical illusion or wrong perception on approach due to intensity of the approach lights.