T-2C FLIGHT PROCEDURES
1.1. PRESTART CHECKS
1.1.1. The student performs Prestart Checks.
1.1.2. IP places battery switch on.
184.108.40.206. IP "ICS check, fire lights."
220.127.116.11. STUDENT "Loud and clear, four fire lights, running down the wings."
1.1.3. The student runs down the wings and checks the rear cockpit warning and caution lights.
18.104.22.168. STUDENT "8 over 9 warning and caution lights, Pre-Start Checks complete, ____lbs.
left and ____lbs. right wing fuel."
22.214.171.124.1. 8 lights:
126.96.36.199.1.1. 4 fire lights
188.8.131.52.1.2. Gear handle light
184.108.40.206.1.3. Wheels warning light
220.127.116.11.1.4. Hook handle light
18.104.22.168.1.5. Eject select light
22.214.171.124.2. 9 lights:
126.96.36.199.2.1. Caution lights
1.2. START / POSTSTART
1.2.1. The aircraft is started using either the battery or external power via an auxiliary power
unit. The majority of aircraft starts utilize an APU, however students need to always be prepared
for a battery start. At least one start in the FAM stage is done on battery power.
188.8.131.52. APU Start
184.108.40.206.1. IP signals PC to apply 28 VDC external power.
220.127.116.11.2. IP signals PC and initiates start sequence on #2 (right) engine.
18.104.22.168.2.1. IP "Starting #2."
22.214.171.124.3. During the start sequence, the student monitors engine instruments and the PC
for abnormal start indications. Upon successful start and thumbs up signal from PC:
126.96.36.199.3.1. STUDENT "Thumbs up from the PC."
188.8.131.52.3.2. IP "Roger, starting #1."
184.108.40.206.3.3. STUDENT "Thumbs up from the PC." (Upon successful start and thumbs
up signaled by PC.)
220.127.116.11.4. IP signals PC to disconnect external power.