Abort Start (pg. 3-3)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
All BF Procedures
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Annunciator Causes Red (pg. 3-58)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Annunciator Causes Amber (pg. 3-58)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Annunciator Causes Green (pg. 3-58)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Annunciator Causes FDR (pg. 3-58)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Land As Soon As Possible (pg. 3-3)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
An emergency shall be declared and landing accomplished at nearest suitable field (immediately) considering:
* severity of the emergency
* weather conditions
* field facilites
* ambient lighting
* command guidance
Engine related
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Land As Soon As Practical (pg. 3-3)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Emergency conditions are less urgent, and although mission is CANX, emer is such that immediate landing may not be necessary
Non engine related
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Suitable Landing Area (pg. 3-3)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Hard surface runway, taxiway, or under/overrun. Landing on unpaved surfaces or ditching is not recommended
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Batt Bus Fail Effect on Config/Confirming/TP Stalls
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Plan to extend Ldg Gr w/ EMER LDG GR HANDLE; Emer flaps will be powered by Main batt through Hot Batt Bus (if not failed); If BATT BUS fails but main batt has not failed, flaps will retract; Ldg Gr/Flap indicators will not be powered
Note: STBY Gyro will operate for at least 9 minutes after Batt Bus has failed if off flag appears
Note: OBOGS/Pressurization will be inop
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Gen Bus Fail Effect on Config/Confirming/TP Stalls
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
W/ Gen Bus fail but operational Gen, BUS TIE Switch remains in NORM to keep Batt/Batt Bus alive; Normal Gear/flap operations available; Airspeed/Altimeter will fail necessitating use of Standbys
Note: speed brake, AOA, TAD, VSI, RMU, GPS, EHSI, and warning tones will be inop
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
AOA Comp Fail Effect on TP Stalls
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Hydro Fail Effect on Config/Confirming/TP Stalls
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Normal gear/flaps/speedbrake/NWS ops unavailable when HYDR FL LO and pressure is < 1800 psi; Loss of hydro press w/out annunciator may indicate engine driven pump failure; EMER LDG GR Handle must be used (flap & gear
retraction will be unavailable)
Note: EHYD PX LO indiactes emergency ldg gr and flaps are inop
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
General EP Knowledge (Ch 3)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Engine Oil Quantity Limits (pg. 5-3, condensed checklist N-27/28)
Note: N-27 is US NAVY ONLY, while N-28 is USAF ONLY
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Capacities (CL N-27/28):
* Tank = 10 Quarts
* Oil systems = 18.5 Quarts
* Oil Specification = MIL-PRF-23699
Note: N-27 is US NAVY ONLY, while N-28 is USAF ONLY
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Battery/Starter Limits (pg. 5-3,8)
(Volts, duty cycle, gen limits)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Prop Limits (pg. 5-8)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
VMO, MMO, VG, VO (pg. 5-8,9)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
0 G Limit/Neg G Limit (pg. 5-9,10)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Prohibited Maneuvers (pg. 5-10)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Acceleration Limits (pg. 5-10)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Weight Limits (pg. 5-11)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Barrier Limits (pg. 5-11)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
En-route Limits (pg. 5-13)
Source: 1T-6A-1 T-6A Flight Manual (Dash One)
Icing
* When operating in areas of known icing Probes Anti-ice switch shall be ON
* At first icing indication, crews will ascend or
descend from icing layer
* Aerobatics after icing encounter are prohibited
until ice has melted or sublimated
* Maneuvers w/ icing are limited to 30° AOB & 0 to 2 G’s
* For landing config & landing phase, w/ ice
accumulation, approach speed must be increased by 10 KIAS
Source: 1T-6A-1 T-6A Flight Manual (Dash One)