Zone

Crash of a Piper PA-61 Aerostar (Ted Smith 601) in Houston: 1 killed

Date & Time: Nov 2, 1988 at 0302 LT
Registration:
N60819
Flight Type:
Survivors:
No
Schedule:
Baton Rouge – Conroe
MSN:
61-0759-8062149
YOM:
1980
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2887
Captain / Total hours on type:
190.00
Aircraft flight hours:
3202
Circumstances:
The aircraft collided with power lines and trees while on final approach. The reported weather immediately following the accident was an indefinite ceiling zero, sky obscured, and visibility 1/16 of a mile in fog. No preimpact failures or malfunctions of the aircraft were found. The pilot had diverted from his intended destination due to fog. The pilot, sole on board, was killed.
Probable cause:
Pilot's decision to fly the approach visually with outside reference to the lights and inadvertently descending below the decision height off the proper glide path.
Occurrence #1: in flight collision with object
Phase of operation: approach - faf/outer marker to threshold (ifr)
Findings
1. (f) weather condition - fog
2. (f) weather condition - obscuration
3. (c) in-flight planning/decision - poor - pilot in command
4. (c) decision height - below - pilot in command
5. (c) proper glidepath - not maintained - pilot in command
6. (f) object - wire, transmission
7. (f) object - tree(s)
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain in Baton Rouge: 3 killed

Date & Time: Oct 31, 1982 at 0505 LT
Registration:
N41045
Flight Phase:
Survivors:
No
Schedule:
Baton Rouge - Charleston
MSN:
31-8252020
YOM:
1982
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
1784
Captain / Total hours on type:
336.00
Aircraft flight hours:
290
Circumstances:
The aircraft crashed and burned shortly after taking off in darkness on an IFR flight plan. The weather was reported as indefinite ceiling, zero obscuration, visibility 1/4 mile with fog, wind 120° at 5 knots. A number of witnesses heard the aircraft, both before and after takeoff. The consensus of their statements indicated that one engine lost power while the other continued running at a high power setting. An investigation revealed that an intense post crash fire had consumed most of the aircraft. There was evidence that the plane had crashed in a steep nose down, right wing low attitude and did not move after impact. The right propeller was found in a feathered position. The left propeller blades were curled and twisted. Both engines were disassemble, but no evidence of a mechanical failure was found. The gear and flaps were retracted and the cowl flaps were closed. All three occupants were killed.
Probable cause:
Occurrence #1: loss of engine power
Phase of operation: takeoff - initial climb
Findings
1. (c) reason for occurrence undetermined
----------
Occurrence #2: loss of control - in flight
Phase of operation: maneuvering - turn to landing area (emergency)
Findings
2. (f) light condition - dark night
3. (f) weather condition - below approach/landing minimums
4. (f) weather condition - low ceiling
5. (f) weather condition - fog
6. (c) airspeed (VMC) - not maintained - pilot in command
7. (c) aircraft handling - not maintained - pilot in command
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Douglas DC-9-14 in Baton Rouge

Date & Time: Mar 17, 1980 at 1645 LT
Type of aircraft:
Operator:
Registration:
N9103
Survivors:
Yes
Schedule:
Houston - Baton Rouge
MSN:
45796/74
YOM:
1966
Crew on board:
4
Crew fatalities:
Pax on board:
46
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
15732
Captain / Total hours on type:
8720.00
Circumstances:
The airplane landed in rain falls with a 18 knots tailwind about 2,000 feet down runway 13 which is 5,800 feet long. Unable to stop within the remaining distance, the airplane overran and came to rest in a ditch about 350 feet further and 200 feet to the right of the extended centreline. All 50 occupants escaped without injuries while the aircraft was damaged beyond repair. At the time of the accident, the total weight of the airplane was 71,000 lbs.
Probable cause:
Overshoot on landing and subsequent overrun and collision with ditch because ATC cleared the aircraft to wrong runway for existing conditions. The following contributing factors were reported:
- Improper in-flight decisions on part of the pilot-in-command,
- Improper operation of brakes and flight controls on part of the pilot-in-command,
- Rain,
- Wet runway,
- Downwind,
- Haze,
- Aircraft over 25,000 lbs upon landing on runway 13, restricted to zero tailwind/10 knots crosswind when wet,
- Runway 22 available,
- Spoilers not used after touchdown.
Final Report:

Crash of a Curtiss C-46 in Baton Rouge

Date & Time: Nov 24, 1964 at 1045 LT
Type of aircraft:
Operator:
Registration:
N9885F
Flight Type:
Survivors:
Yes
Schedule:
Atlanta-New Orleans
MSN:
32878
YOM:
1944
Flight number:
DL029
Crew on board:
2
Crew fatalities:
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7209
Captain / Total hours on type:
478.00
Aircraft flight hours:
19842
Circumstances:
Weather at New Orleans was below landing minima, so the flight was diverted to Baton Rouge. Weather at Baton Rouge was a ceiling 300 feet overcast, visibility 1,5 miles in light rain and fog, wind 360deg/5 knots. Runway 13 ILS minima were 300 feet ceiling and 3/4 mile visibility, weather was below circling minima. However, the approach was continued and the plane touched down fast 2,500 feet past the runway threshold. Approaching the end of the runway, the pilot attempted to ground loop, but the plane just turned 20° and slid off the runway. Both pilots were evacuates while the aircraft was damaged beyond repair.
Probable cause:
"Failure of the captain to execute a go around during a landing overshoot under existing unfavourable wind and adverse runway conditions. Ineffective braking caused by hydroplaning. The copilot completed the approach and the captain took over control after touchdown.
Final Report: