SR-71-A NORMAL PROCEDURES
ABBREVIATED CHECKLIST
APPROACH
- Display mode select - SET (ANS/TACAN/ILS)
- Defog - SET
- Altimeter - SET
- INS altitude - UPDATE (RSO)
- Crossfeed - OPEN
- Brake switches - SET, ANTISKID ON
- Below Mach 0.5, Limiter - PULLED & LIGHT OFF
- UHF power - SET
- Defog - SET
- Landing light - ON
BEFORE LANDING
- Approach and landing speed - COMPUTED
- CG - CHECKED (between 17%-22% for all subsonic operations)
- Gear - 5-10 miles from the runway, MAX 300 KIAS -DOWN & CHECKED
- Hydraulic pressure - CHECK
- Right refrig - OFF
- Ckpit air - OFF (fwd, RSO).
- Annunciator panel - CHECKED
LANDING
- Chute - DEPLOY
- Steering - ENGAGE
- Brakes - CHECKED
- Chute - JETTISON (over 55 knots)
TOUCH AND GO
- Final approach - 190 KIAS
- Touchdown - 170 KIAS
GO AROUND
- Throttles - MILITARY THRUST (Maximum thrust is necessary)
- Landing gear lever - UP (after positive rate of climb is established)
NOTE I:
The excess thrust available to perform a go-around varies with airspeed, gross weight, airplane configuration, field elevation and ambient temperature. As extremes of these variables are approached, the ability to perform a successful go-around with military thrust decreases, thus requiring afterburner. Refer to appendix for charts showing variation in performance to be expected with changes in these operating conditions.
NOTE II:
Fuel required for a missed approach and instrument go-around (typical GCA pattern) is approximately 3,000 pounds. A closed pattern go-around requires approximately 1,000 pounds.
WARNING
DO NOT ATTEMPT A GO-AROUND AFTER DRAG CHUTE CONTROL HAS BEEN ACTUATED.