Vance Air Force Base, Okla., has grounded its
T-6A Texan II aircraft after several reports of hypoxia. (Master Sgt. David
Richards/Air Force)
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By: Stephen Losey
Two weeks after hypoxia scares led the 71st Flying
Training Wing at Vance Air Force Base in Oklahoma to ground its T-6A Texan II
aircraft, it remains unknown when flying operations will resume.
Vance stopped flying its T-6As on Nov. 15 after
“physiological incidents” happened during four flights since Nov. 1. The
incidents affected four instructor pilots and one student pilot there.
Flight operations for the T-1A Jayhawk and T-38 Talon at
Vance are still ongoing.
Vance public affairs chief Terri Schaefer said Wednesday
that the pilots “experienced mental disorientations in conjunction with classic
hypoxia systems.”
Hypoxia is too little oxygen in the body.
Schaefer said the cause of the hypoxia has not yet been
found. Aviators, medical personnel and industry experts are still reviewing the
incidents and looking for a solution, she said, but Vance is not sure when the
pause in T-6A flight operations will end.
In a Nov. 20 release announcing the groundings, Vance
said that “in each case, the aircraft’s backup oxygen system operated as
designed, and the pilot followed the correct procedures, landing the aircraft
safely,”
In all, over the last year there have been eight such
physiological events involving T-6A sorties at two bases, Vance and Naval Air
Station Pensacola in Florida.
“One event is too many,” Schaefer said in an email. “The
Air Force takes this issue seriously and will continue to investigate these events
with all major stakeholders in the T-6 enterprise to provide Vance AFB and all
other T-6 bases solutions, including changes to checklist procedures, that
protect our nation’s finest and ensure continued, safe and effective flying
training.”
Vance has also briefed its instructor pilots and students
on the hypoxia situation, and how the pilots in the incidents successfully
landed their planes afterwards.
Original post: airforcetimes.com
T-1A Jayhawk
Background
The first T-1A was delivered to Reese Air Force Base, Texas, in January 1992, and student training began in 1993.
Starting in 1993, undergraduate pilots who have graduated from their primary aircraft have proceeded to specialized training tailored for their follow-on assignments. The T-1A is used in advanced training for students identified to go into airlift or tanker aircraft. Those selected for bombers and fighters receive their advanced in the T-38.
The T-1A is used at Columbus AFB, Miss., Laughlin AFB, Texas, and Vance AFB, Okla. It is also used at Randolph AFB, Texas, to train instructor pilots and at Naval Air Station Pensacola, Fla., for combat systems officer training.
General Characteristics
Primary Function: Advanced trainer for airlift and tanker pilots
Builder: Raytheon Corp. (Beech)
Power Plant: Two Pratt and Whitney JT15D-5B turbofan engines
Thrust: 2,900 pounds each engine
Length: 48 feet, 5 inches (14.75 meters)
Height: 13 feet, 11 inches (4.24 meters)
Wingspan: 43 feet, 6 inches (13.25 meters)
Maximum Speed: 538 miles per hour (Mach .70)
Ceiling: 41,000 feet (12,500 meters)
Maximum Takeoff Weight: 16,100 pounds (7,303 kilograms)
Range: 2,222 nautical miles (2,900 nm flying long-range cruise)
Armament: None
Crew: Three (pilot, co-pilot, instructor pilot)
Date Deployed: February 1992
Unit Cost: $4.1 million
T-1A Jayhawk
The T-1A Jayhawk is a medium-range,
twin-engine jet trainer used in the advanced phase of specialized undergraduate
pilot training for students selected to fly airlift or tanker aircraft. (U.S.
Air Force photo).
Mission
The T-1A Jayhawk is a medium-range, twin-engine jet trainer used in the advanced phase of specialized undergraduate pilot training for students selected to fly airlift or tanker aircraft. It is also used to support navigator training for the U.S. Air Force, Navy, Marine Corps and international services.
Features
The swept-wing T-1A is a military version of the Beech 400A. It has cockpit seating for an instructor and two students and is powered by twin turbofan engines capable of an operating speed of 538 mph. The T-1A differs from its commercial counterpart with structural enhancements that provide for increased bird strike resistance and an additional fuselage fuel tank.
The T-1A Jayhawk is a medium-range, twin-engine jet trainer used in the advanced phase of specialized undergraduate pilot training for students selected to fly airlift or tanker aircraft. It is also used to support navigator training for the U.S. Air Force, Navy, Marine Corps and international services.
Features
The swept-wing T-1A is a military version of the Beech 400A. It has cockpit seating for an instructor and two students and is powered by twin turbofan engines capable of an operating speed of 538 mph. The T-1A differs from its commercial counterpart with structural enhancements that provide for increased bird strike resistance and an additional fuselage fuel tank.
T-1A CSO Aircraft Modifications – Image: cambertx.com
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T-1A CSO Instructor and Student station –
Image: cambertx.com
|
Background
The first T-1A was delivered to Reese Air Force Base, Texas, in January 1992, and student training began in 1993.
Starting in 1993, undergraduate pilots who have graduated from their primary aircraft have proceeded to specialized training tailored for their follow-on assignments. The T-1A is used in advanced training for students identified to go into airlift or tanker aircraft. Those selected for bombers and fighters receive their advanced in the T-38.
The T-1A is used at Columbus AFB, Miss., Laughlin AFB, Texas, and Vance AFB, Okla. It is also used at Randolph AFB, Texas, to train instructor pilots and at Naval Air Station Pensacola, Fla., for combat systems officer training.
General Characteristics
Primary Function: Advanced trainer for airlift and tanker pilots
Builder: Raytheon Corp. (Beech)
Power Plant: Two Pratt and Whitney JT15D-5B turbofan engines
Thrust: 2,900 pounds each engine
Length: 48 feet, 5 inches (14.75 meters)
Height: 13 feet, 11 inches (4.24 meters)
Wingspan: 43 feet, 6 inches (13.25 meters)
Maximum Speed: 538 miles per hour (Mach .70)
Ceiling: 41,000 feet (12,500 meters)
Maximum Takeoff Weight: 16,100 pounds (7,303 kilograms)
Range: 2,222 nautical miles (2,900 nm flying long-range cruise)
Armament: None
Crew: Three (pilot, co-pilot, instructor pilot)
Date Deployed: February 1992
Unit Cost: $4.1 million
Source: af.mil
AT-6B Light Attack Aircraft / Trainer: Details
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