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Crash of a Cessna 525 CitationJet CJ1 in Marietta: 4 killed

Date & Time: Apr 4, 1998 at 1032 LT
Type of aircraft:
Registration:
N111LR
Flight Phase:
Survivors:
No
Schedule:
Chamblee - Harrisburg
MSN:
525-0222
YOM:
1997
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
1824
Captain / Total hours on type:
86.00
Aircraft flight hours:
181
Aircraft flight cycles:
125
Circumstances:
A Cessna 525 and a Cessna 172 collided in flight about 3,400 feet mean sea level on converging courses, with the 525 heading north and the 172 heading southwest. The converging speed was about 300 knots. The 525 departed under instrument flight rules, received vectors, and was initiating a climb on course. Training in the 525 emphasizes maximum use of the autopilot to afford greater outside scanning by the single pilot. The 525 was in radio contact with terminal approach control and the pilot's acknowledgement of the climb clearance was interrupted by the collision. The 172 had departed a local airfield, located just outside the 30 mile Mode C veil airspace of a terminal airport, and proceeded southwest. The collision occurred as the 172 was approaching Class D airspace of a military tower, and the pilot was initiating radio contact with the military tower. The terminal approach controller in contact with the 525 stated he did not observe the primary target of the 172, and conflict alert software was not installed. The 172 did not display a transponder signal and the transponder switch was subsequently found in the 'off' position. A cockpit visibility study indicated that from a fixed eye position the 172 was essentially hidden behind aircraft structure of the 525 for the 125 seconds before impact. The 172 could be seen by shifting the pilot's eye position. The 525 was viewable in the left lower section of the 172's windscreen. Both airplanes were operating in visual flight conditions.
Probable cause:
The failure of both pilots to see and avoid conflicting traffic, and the failure of the 172 pilot to operate the transponder as required by current regulations. Factors were the controller's failure to observe the traffic conflict, the lack of radar conflict alert capability, and the training emphasis on maximum autopilot usage with the autopilot controller placed at the rear of the cockpit center mounted pedestal.
Final Report:

Crash of a Beechcraft C90 King Air in Chamblee: 2 killed

Date & Time: Oct 1, 1989 at 1642 LT
Type of aircraft:
Operator:
Registration:
N43GT
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Chamblee - Orlando
MSN:
LJ-652
YOM:
1975
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
2000
Captain / Total hours on type:
400.00
Aircraft flight hours:
4272
Circumstances:
After taking off, the pilot established radio contact with departure control and reported a directional gyro problem. Seconds later, he reported that he was losing all instruments. Departure control attempted to provide no-gyro vectors. The pilot was instructed to make a frequency change. Soon thereafter, radio and radar contact were lost and the aircraft crashed. Before crashing the aircraft was observed in a rolling attitude. Wreckage was found scattered over a 600 feet by 150 feet area. An exam revealed the right wing had separated in flight. There was evidence that the right wing had failed in an upward (positive) direction. The pilot's attitude gyro was damaged during impact, but no rotational damage was noted. The pilot's attitude indicator and copilot's turn indicator were air driven, the pilot's turn indicator was dc powered and the copilot's attitude indicator was ac powered. The maintenance log did not have a current static/altimeter and transponder check. Both occupants were killed.
Probable cause:
Malfunction of one or more flight instruments for an undetermined reason, failure of the pilot to maintain control of the aircraft with partial panel instruments after becoming spatially disoriented, and his exceeding the design stress limits of the aircraft. The weather (low ceiling) and malfunctioning directional gyro were related factors.
Final Report:

Crash of a Beechcraft 60 Duke in Valdosta: 1 killed

Date & Time: Jul 13, 1973 at 0747 LT
Type of aircraft:
Operator:
Registration:
N7282D
Flight Type:
Survivors:
Yes
Schedule:
Chamblee - Valdosta
MSN:
P-84
YOM:
1969
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1555
Captain / Total hours on type:
57.00
Circumstances:
On approach to Valdosta Airport, the pilot encountered poor weather conditions with low clouds and fog. Too high on the localizer, he failed to execute a missed approach and attempted circling approach below published minimums when he lost control of the airplane that crashed in flames. A passenger was killed while both other occupants were injured.
Probable cause:
Improper IFR operation on part of the pilot. The following factors were reported:
- The pilot failed to maintain flying speed,
- Low ceiling and fog,
- Poorly planned approach.
Final Report: