Crash of a Piper PA-31T-620 Cheyenne II in Saint Louis: 1 killed

Date & Time: Jan 18, 1988 at 1903 LT
Type of aircraft:
Registration:
N200RS
Survivors:
Yes
Schedule:
Alexander City – Saint Louis – Quincy
MSN:
31-7520011
YOM:
1975
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
14000
Circumstances:
The passenger said that the approach appeared normal until the pilot turned on the landing lights while in the overcast. Seconds after, the aircraft impacted trees, careening out of control, and snapping power lines; then striking a house roof before coming to rest on the ground. The airplane began to burn as it went through the power lines. The weather at the time was at or above IFR landing minimums. The flight had been in a holding pattern for forty five minutes prior to commencing the approach. All of the aircraft's systems and powerplants, as well as the FAA approach facilities, were determined to be in working order. The pilot was killed and all three passengers were seriously injured.
Probable cause:
The National Transportation Safety Board determines the probable cause(s) of this accident to be:
Proper glide path not maintained by p.i.c., decision height not identified By the pic, missed approach not performed by the pic. Turning on lights in overcast.
Findings
Occurrence #1: undershoot
Phase of operation: approach - faf/outer marker to threshold (ifr)
Findings
1. (f) weather condition - obscuration
2. (f) weather condition - fog
3. (f) weather condition - rain
4. (c) proper glidepath - not maintained - pilot in command
5. (c) ifr procedure - not followed - pilot in command
6. (c) decision height - not identified - pilot in command
7. (f) visual/aural perception - pilot in command
----------
Occurrence #2: in flight collision with object
Phase of operation: approach - faf/outer marker to threshold (ifr)
Findings
8. (f) object - tree(s)
9. (f) object - wire, transmission
10. (f) object - residence
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: approach - faf/outer marker to threshold (ifr)
Final Report:

Crash of a Cessna 414A Chancellor in Midland: 1 killed

Date & Time: Jan 4, 1988 at 0949 LT
Type of aircraft:
Operator:
Registration:
N6576C
Flight Phase:
Survivors:
No
Schedule:
Midland - Roswell
MSN:
414A-0018
YOM:
1978
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
11000
Captain / Total hours on type:
34.00
Aircraft flight hours:
2952
Circumstances:
The aircraft collided with power lines and the ground shortly after takeoff during instrument conditions. The only evidence of a malfunction or failure which was found was the gyro for the pilot's attitude indicator which had no indication of rotation at impact. The previous pilot stated that he normally pulled the ac circuit breaker after landing, that the breaker supplied voltage to the pilot's attitude indicator, and that he told the new pilot of this procedure which was not on the aircraft's checklist. This was the new pilot's first instrument flight in this aircraft. The accident occurred in a residential area.
Probable cause:
Occurrence #1: loss of control - in flight
Phase of operation: climb
Findings
1. (c) flight/nav instruments,attitude gyro - disconnected
2. (c) attitude indicator - not corrected - pilot in command
3. (c) spatial disorientation - pilot in command
4. (f) weather condition - fog
5. (f) weather condition - low ceiling
6. (c) preflight planning/preparation - inadequate - pilot in command
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Findings
7. Terrain condition - residential area
8. Object - wire, transmission
Final Report:

Crash of a Mitsubishi MU-2B-20 Marquise in White Plains

Date & Time: Dec 7, 1987 at 1725 LT
Type of aircraft:
Registration:
N866Q
Survivors:
Yes
Schedule:
Concord - White Plains
MSN:
121
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5525
Captain / Total hours on type:
1695.00
Aircraft flight hours:
5526
Circumstances:
The cross country business flight was uneventful from Concord, New Hampshire to white Plains, New York under clear sky. During final approach, the pilot extended the gear but did not notice that the circuit breaker had opened and the gear was not lowered. The aircraft landed gear up and the gear doors partially open. The gear warning horn did not operate. The pilot stated that he failed to check for 3 green lights.
Probable cause:
Occurrence #1: gear not extended
Phase of operation: landing
Findings
1. (c) landing gear, normal retraction/extension assembly - inoperative
2. (c) gear extension - not attained - pilot in command
3. Landing gear, gear warning system - inoperative
4. (c) electrical system, circuit breaker - popped/tripped
5. (f) checklist - not followed - pilot in command
Final Report:

Crash of a Cessna 402B in Arthur's Town: 1 killed

Date & Time: Dec 5, 1987 at 1635 LT
Type of aircraft:
Registration:
N422TA
Survivors:
No
Schedule:
Nassau - Arthur's Town
MSN:
402B-0357
YOM:
1973
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Crashed under unknown circumstances while approaching Arthur's Town Airport. The pilot, sole on board, was killed.

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 Cessna 421B Golden Eagle II in Stansted: 6 killed

Date & Time: Oct 20, 1987 at 1200 LT
Registration:
G-HAST
Flight Phase:
Survivors:
No
Schedule:
Stansted – Tatenhill
MSN:
421B-0828
YOM:
1974
Location:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
500
Captain / Total hours on type:
200.00
Circumstances:
The aircraft was on an IFR flight from Stansted Airport to Tatenhill Aerodrome with a pilot and five passengers on board. Shortly after takeoff from runway 23 at Stansted the pilot reported that he had a problem and wished to return. Stansted ATC cleared him for a left hand circuit and return. As the aircraft turned left hand towards a downwind leg the left bank was observed to suddenly increase and it turned onto its back before descending vertically and crashing into a wooded area to the southwest of the airport. Immediately after the impact there was a fierce fire; all the occupants were killed instantaneously.
Probable cause:
Examination confirmed that the right hand propeller and engine has been delivering power normally before impact, but that the left propeller and engine had not been producing power. The left engine drive fuel pump had also suffered fire damage, and the rubber seals were leaking. Upon disassembly it was found that the aneroid unit within the pump was corroded and could not have functioned. The possible adverse effects of the corrosion within the fuel pump aneroid unit to engine performance were investigated using another similar engine in a test facility. It was found that this condition caused the engine to misfire and run roughly at high power settings, but that the engine ran normally at low power. The tests, whilst not totally representative of the conditions on the accident flight, showed no tendency for the engine to fail completely, although sudden full throttle applications grossly aggravated the rough running. Thus no reason for the apparent marked power loss associated with the left engine fitted to G-HAST has been established.
Final Report:

Crash of a Piper PA-61 Aerostar (Ted Smith 601P) in Corona

Date & Time: Sep 14, 1987 at 1130 LT
Registration:
N902RG
Flight Phase:
Survivors:
Yes
Schedule:
Corona – Carlsbad
MSN:
61-0666-7963311
YOM:
1979
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4634
Captain / Total hours on type:
120.00
Aircraft flight hours:
1295
Circumstances:
The airplane was refueled before it departed on the accident flight; the pilot did not supervise the fueling. Shortly after takeoff, the pilot advised the Ontario departure controller that both engines were experiencing a power loss and that he suspected jet fuel contamination. The airplane collided with a berm during the ensuing forced landing. The investigation revealed that the FBO fueled the airplane with 131.3 gallons of Jet A fuel. Investigators did not locate any witnesses who saw the pilot preflight the airplane. The pilot sustained severe head injuries and could not recall if he had preflighted the airplane - the right front seat passenger was not present when the pilot boarded the aircraft.
Probable cause:
Occurrence #1: loss of engine power (partial) - nonmechanical
Phase of operation: climb - to cruise
Findings
1. All engines
2. (c) fluid, fuel grade - incorrect
3. (c) refueling - improper - fbo personnel
4. (f) inadequate initial training - fbo personnel
5. (c) preflight planning/preparation - improper - pilot in command
----------
Occurrence #2: forced landing
Phase of operation: descent - emergency
----------
Occurrence #3: on ground/water collision with object
Phase of operation: landing - roll
Findings
6. Terrain condition - berm
Final Report:

Crash of a Partenavia P.68C Victor off New Orleans

Date & Time: Sep 11, 1987 at 0629 LT
Type of aircraft:
Registration:
N1352W
Survivors:
Yes
Schedule:
Hammond - New Orleans
MSN:
232
YOM:
1982
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
15164
Captain / Total hours on type:
30.00
Aircraft flight hours:
913
Circumstances:
The pilot began an ILS runway 18R approach at night to the Lakefront Airport. He reported that after the aircraft broke out of the clouds at 1,700 feet, he transitioned to a visual approach. He stated that as he continued, the approach seemed normal, except the VASI lights seemed too far down the runway. He remembered that just before impact, the VASI was providing a red over red indication, but he did not worry as he perceived the aircraft was over the end of the runway and he was about to flare. At about that time, the aircraft impacted with water, well short of the runway. As the aircraft sank, the pilot escaped thru a hole in the windshield. Subsequently, he was found by passing fishermen. The pilot believed he had gotten a false perception of the runway location due to reflection of lights off of calm lake water.
Probable cause:
Occurrence #1: undershoot
Phase of operation: approach - vfr pattern - final approach
Findings
1. (f) light condition - dark night
2. (f) terrain condition - water, glassy
3. (c) in-flight planning/decision - improper - pilot in command
4. (c) unsafe/hazardous condition warning - disregarded - pilot in command
5. (c) distance - misjudged - pilot in command
6. (f) visual/aural perception - pilot in command
7. (c) altitude - misjudged - pilot in command
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: approach - vfr pattern - final approach
Findings
8. Terrain condition - water
Final Report:

Crash of a Beechcraft B200 Super King Air in Jasper

Date & Time: Jun 23, 1987 at 0619 LT
Registration:
N859DD
Survivors:
Yes
Schedule:
Birmingham - Jasper - Allentown
MSN:
BB-859
YOM:
1981
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11000
Captain / Total hours on type:
2000.00
Aircraft flight hours:
2966
Circumstances:
The pilot obtained a weather briefing for his proposed flight from Birmingham, AL to Jasper, AL to Allentown, PA. He did not file a flight plan for the 35 mile flight from Birmingham to Jasper, however, he did file a flight plan for the proposed flight from Jasper to Allentown. He stated that he 'felt like he got a little slow and the tail stalled' during his VFR landing approach at Jasper. The aircraft contacted the ground at the east end of the east-west runway on a northerly track. The aircraft continued on the northerly track for 288 feet before colliding with trees. The aircraft was destroyed by the post crash fire. Witnesses reported fog in the area and the pilot reported that he had encountered patches of fog on the flight from Birmingham.
Probable cause:
Occurrence #1: in flight collision with terrain/water
Phase of operation: approach
Findings
1. (f) weather condition - fog
2. (f) light condition - dawn
3. (c) proper alignment - not attained - pilot in command
4. (c) airspeed - not maintained - pilot in command
5. (c) stall - inadvertent - pilot in command
6. (f) go-around - not performed - pilot in command
----------
Occurrence #2: in flight collision with object
Phase of operation: approach
Findings
7. (f) object - tree(s)
Final Report:

Crash of a Beechcraft B60 Duke in Wall

Date & Time: May 27, 1987 at 0851 LT
Type of aircraft:
Operator:
Registration:
N4314W
Flight Phase:
Survivors:
Yes
Schedule:
San Angelo – San Antonio
MSN:
P-264
YOM:
1974
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2553
Captain / Total hours on type:
250.00
Aircraft flight hours:
2645
Circumstances:
Aircraft was destroyed during an attempted off airport emergency landing following a dual engine failure while leveling off at cruise flight. Pilot stated that left engine, then right engine surged and quit as he was leveling off at 9,000 feet msl. At the time of the engine failures the fuel totalizer was reading 60 gallons, but the aircraft fuel gauges were reading empty. Pilot broke out of overcast at 3,500 msl (about 1,200 feet agl) and was unable to find a suitable clear area to land before committing to an emergency landing in trees. Gear was down, flaps were up and neither engine was feathered at impact. Pilot stated that he knew he was out of gas when both engines quit and that he did not attempt an air start. Both occupants were seriously injured.
Probable cause:
Occurrence #1: loss of engine power (total) - nonmechanical
Phase of operation: cruise - normal
Findings
1. (c) fluid,fuel - exhaustion
2. (c) refueling - disregarded - pilot in command
3. (c) fuel consumption calculations - not performed - pilot in command
4. (c) complacency - pilot in command
----------
Occurrence #2: forced landing
Phase of operation: descent - emergency
Findings
5. Weather condition - low ceiling
6. Emergency procedure - not performed - pilot in command
7. Propeller feathering - not performed - pilot in command
----------
Occurrence #3: in flight collision with object
Phase of operation: landing - flare/touchdown
Findings
8. (f) object - tree(s)
9. (f) terrain condition - high obstruction(s)
10. (f) terrain condition - none suitable
Final Report: