Investigation brief · generated 2026-10-09 · source: NTSB public docket and accident database
BOEING 717-200 — Pleasant Grove, NC, USA, 2009-10-26
NTSB number
ERA10LA041
Operator
Air Tran Airways
Registration
N935AT
Highest injury
Serious injury
Regulation
Part 121
Damage
—
Cohort
Part 121 airline
Recorder data
Tier 1 — decoded recorder tables
Every sentence below is taken directly from NTSB records — the accident database, the docket's recorder reports and the Board's findings — with its source noted. Nothing is paraphrased or inferred.
NTSB summary
During cruise descent the captain of the scheduled airline flight handed over control of the airplane to the first officer to make a public address announcement regarding turbulence. He had just turned on the fasten seatbelt sign when they received a resolution advisory (RA) from the onboard traffic alert and collision avoidance system (TCAS). The captain then took back control of the airplane and initiated an avoidance maneuver. During the avoidance maneuver, a flight attendant sustained serious injuries and a child passenger sustained a minor injury.
Review of air traffic control radar data and data from the onboard flight data recorder revealed that 1.5 seconds after the TCAS RA occurred, the captain initiated a series of excessive control inputs which resulted in a positive vertical acceleration of approximately 1.6g. One second after the positive vertical acceleration the airplane sustained a maximum negative vertical acceleration of approximately .2g. A second after the negative vertical acceleration the airplane sustained another positive load of 1.4g after which the acceleration was dampened out. According to the TCAS manufacturer's published guidance, a flight crew should "promptly but smoothly" follow a TCAS RA and since the maneuvers are coordinated between aircraft, the crew should never maneuver in the opposite direction of the advisory. The advisories are always based on the "least amount of deviation from the flight path" while providing safe vertical separation. Typical RAs that would require a maneuver by a flightcrew only requires crew response within 5 seconds and g-forces of ±.25g. Review of the airline's training and guidance materials for the two different types of airplanes the airline operated revealed that this information was included in the training and guidance material for one of the airplane types in their fleet but was not included in the training and guidance materials for the accident airplane type.
The captain's excessive maneuver in response to a traffic alert and collision avoidance system (TCAS) alert, which resulted in a serious injury to a flight attendant. Contributing to the accident was the operator's inadequate TCAS training and guidance.
Verbatim, NTSB determination.
Sequence of events (FDR factual report)
Time
Event
Page
1201 EDT (approximate)
Aircraft maneuvered to avoid another airplane during cruise-descent near Pleasant Grove, NC
1
N/A
TCAS resolution advisory occurred
3
1.5 seconds after TCAS RA
Positive vertical acceleration of approximately 1.6 g's recorded
3
1 second after positive vertical acceleration peak
Aircraft sustained a maximum negative vertical acceleration of approximately 0.2 g's
3
1 second after negative vertical acceleration
Aircraft sustained another positive load of 1.4 g's after which the acceleration was dampened out
3
Extracted by claude-sonnet-5; 0 of 1 stated events verified against the raw recorder data.