Term
|
Definition
|
|
Term
| Oil low light on without pressing the LOX/FUEL/OIL QTY Button? |
|
Definition
| Less than 20% oil remaining |
|
|
Term
|
Definition
At idle: 30 psi
Below 90%: 35 psi
Normal range: 40-50 psi
Max all RPM: 50 psi (1-4-3) |
|
|
Term
| Boost pump test in flight? Why or why not? |
|
Definition
| No, due to the possibility of flaming-out an engine the centrifugal pump has failed. |
|
|
Term
| Fuel Press for wings/drops- all configurations. |
|
Definition
Configuration Wing Drops
On deck 0psi 0psi
On deck ORIDE 7psi 25psi
In flight clean 7psi 25psi
In flight dirty 0psi 0psi
In flight clean/dirty ORIDE 12psi 25psi
Wing dump on 12psi 25psi 25 |
|
|
Term
| Yellow "DU" means? How do you extend? |
|
Definition
| Display unit overheat, should continue to operate for 30 min. Reduce brightness and modes to extend life. |
|
|
Term
| Three mandatory fuel transfer processes for 4 or 5 full drops? |
|
Definition
EXTERNAL XFER switch in either INBD or OUTBD until thos drop tanks empty.
Place the switch in NORM for the remainder of the flight.
If all drop tanks contain fuel, the EXTERNAL XFER switch shall be set to NORM only under the following conditions.
When fuel is being dumped.
For a brief period immediately after launch to check fuel transfer. |
|
|
Term
| Low fuel light at 6.5 units means? |
|
Definition
| At 6.5 AOA approximately 2500lbs of fuel remain. A higher AOA will delay illumination until 1800lbs remain in the aft fuselage cell. |
|
|
Term
| Fuselage dumping time range and down to? |
|
Definition
| Fuselage dump pumps can dump fuel to 3700-2700lbs in 3.5-4 min at 4-4.5 AOA, high AOA or faster airspeed will decrease remaining fuel closer to 2700lbs. Wing dumps can dump approximately 6300lbs in 5min at 4-4.5 AOA, the last 400 lbs takes 3min due to drain time. |
|
|
Term
| If multiple CBs pop, can your reset if operational necessity dictates? |
|
Definition
| Multiple CB's cannot be reset due to the risk of fire from Kapton insulated wiring. |
|
|
Term
| RAT powers___ and ____ which powers the DC essential? |
|
Definition
| The RAT will power the AC essential bus and the emergency T/R which powers the DC essential bus. |
|
|
Term
|
Definition
| Up to 20,000 waypoints can be loadd on the DTM/PDTM from JMPS. |
|
|
Term
| Which anti-collision light works on deck? |
|
Definition
| The upper anti-collison will work on deck as the lower one is extingushed when the gear is down and locked. |
|
|
Term
| Secondary hyd components? |
|
Definition
| The Flaps*, Slats*, Landing Gear*, Flaperon Pop-ups, Wingfold, Winglocks, NWS, Hook retract, Strut Lock, and Normal Wheel Brakes* are powered by the secondary combined hydraulic system. *indicated a secondary means of operation. |
|
|
Term
| Requirements for flaperon popups? |
|
Definition
| Flaperons will pop-up to the 41 degree position if the pop-up switch is the ARM position, wings spread and locked, left WOW switch activated to the on-deck position, and the throttles retarted to idle. |
|
|
Term
| ASR affect on flight control surface travel? |
|
Definition
| When ASR is selected rudder travel is extended to +/-35 degrees and the stabilizer travel is increased to 1.5 degrees up and 24 degrees down. |
|
|
Term
| What hapens if the flap selector lever and emergency flap switch do not agree? |
|
Definition
| The Emergency Flap Switch has priority and will override the flap selector handle. Once the Emergency Flap Switch is placed in OFF to brake flap motor, hte flaps/slats will be driven to the osition of the flap selector handle if hydraulic pressure is available. |
|
|
Term
| CDNU FOM. What is best, what is worst- at what point does CDNU stop passing steering info? |
|
Definition
| FOM 1 is the best FOM 9 then worst, the CDNU stops using depending on hte mode selected. ENROUTE at FOM 8, TERMINAL at FOM 7, and APPROACH at FOM 5. |
|
|
Term
|
Definition
| The Standard Central Air DATA Computer (SCADC) replaced the Air DATA Computer (ADC) and providese pressure altitude change and Mach number change to the AFCS, TAS and Pressure altitude to the CMC SYK-14, MODE C altitude to IFF, TAS and Pressure altitude to CDNU, PRI/SEC EGI navigation set to the NAV system. |
|
|
Term
| When and why do you dump cabin press to lower gear? |
|
Definition
| Above 8000FT dump cabin pressure before lowering the landing gear to prevent jamming the nose gear. |
|
|
Term
| T/F- The last 4-7 applications of the aux hyd accumulator are for aux brake applications. |
|
Definition
| The last 4-7 applications of the aux brakes are reserved for emergency/parking brake applications. |
|
|
Term
| T/F- With ADF selected, push to talk disables? |
|
Definition
| Selecting ADF disables push to talk. |
|
|
Term
| Why does the Electronic Airflow Light come on? |
|
Definition
| The ELECTRONIC AIRFLOW caution light illuminates when the downstream pressure in the cooling duct falls below 5psi. |
|
|
Term
| How do you display steering info on hte EHSI? |
|
Definition
| To display steering on the EHSI select MAP mode with FMS as the primary NAV source and set FMS1 at needle 1. |
|
|
Term
| How do you do an RSG bit? |
|
Definition
| Set the RADAR power swiitch to BIT/STBY and select RSG using the BIT switch. The azimuth cursor must be stabilized on hte A/C datum line, STC DP full counter clockwise, and RCVR GAIN full clockwise. |
|
|
Term
| Alignment time required for an Attitude Reference? |
|
Definition
| The EGI's require 15sec of alignment for valid attitude. |
|
|
Term
| Three items required for CV alignment? |
|
Definition
| The CV heading, CV speed, and current LAT/LONG position are required to perform a manual CV alignment. |
|
|
Term
| Grounding points for refueling? |
|
Definition
| During ground refueling earth ground the A/C at the nosewheel well static point, ground fuel unit to A/C nosewheel well static ground and earth, and ground fuel nozzle to A/C. Figure 3-2 also shows the tail bumper static ground oint as a valid grounding point. |
|
|
Term
| T/F- During prolonged use of Mach Hold, the aircraft will climb. |
|
Definition
| During extended periods of MACH hold operation at a constant trottle setting, the A/C will climb slowly due to weight loss through fuel consumption. |
|
|
Term
| How many reversionary wayoints in the CDNU? |
|
Definition
| 2OO reversionary waypoints can be downloaded from the DTM/PDTM into the CDNU. |
|
|
Term
| HARM can be carried on which stations? |
|
Definition
| HARM can be carried on stations 1, 2, 4, and 5. |
|
|
Term
| VERT REF switch in Secondary, attitudeinformation is pulled from? |
|
Definition
| The SEC EGI is selected and providing attitude information. |
|
|
Term
| TACAN BIT shows what on the EHSI? |
|
Definition
| The TCN bit shows 004 degrees and 1.8 DME within 5-6sec on hte EFIS and a GO light within 22sec on the TCN panel. |
|
|
Term
|
Definition
Acceleration: 832C for 8 min
Max Power: 804C for 30 min
Max Continuous: 720C Continuous
Starting: 474C Momentary |
|
|
Term
|
Definition
| The DSDC receives pitch and roll information from the PRI/SEC EGI's and supplies it to the AFCS, RADAR, and Signal generator (SG). It also receives range and bearing information from the TACAN. |
|
|
Term
|
Definition
1. Intentional Spins
2. Intentional zero-airseed maneuvers
3. Normal flight with ASR on
4. Full deflection abrupt control reversals
5. Abrupt control movement with BLIVOT installed
6. Zero-G maneuvers in excess of 10sec due to oil starvation
7. Negative-G maveuver in excess of 30 sec due to fuel starvation |
|
|
Term
|
Definition
| Max tire rotation speed is 175kts ground speed. |
|
|
Term
| How many GPS satellites are required for altitude information? |
|
Definition
| A minimum of 4 satellites are required to obtain altitude information. |
|
|
Term
| T/O RPM is normally ____-____ but can be lower when temp is below 30*F? |
|
Definition
|
|
Term
| Pilot's only cue of stall in the dirty configuration? |
|
Definition
| Lateral control effectiveness decreases during the approach to stall and can serve as a cue to the impending stall if lateral control inputs are made. A stall warning horn at 21 units AOA may be the only stall-warning cue perceived by the pilot. |
|
|
Term
| Is TACAN information available on the EFIS display when running on RAT power? |
|
Definition
| TACAN information will be displayed and will be valid on the EFIS displays on RAT power as long as the PRI EGI is operating. If both EGI's have failed TCN information will be relative to the A/C. |
|
|
Term
| Weight/airspeed limits for gear blowdown and why? |
|
Definition
| 150 KIAS and 40k lbs. 150 KIAS for gear extension speed and because the A/C will stall at airspeeds below 150 above 43,000 lbs if flaps/slats not extended. |
|
|
Term
| Can the pilot pull the trigger in HARM Practice mode when carrying a live missile or CATM? |
|
Definition
| The pilot can pull the trigger in HARM practice mode or when using a CATM as long as there is not a live missile on board. |
|
|
Term
| What should you do upon takeoff during cold weather? |
|
Definition
| Before T/O insure all instruments are sufficiently warmed. After T/O, cycle the gear to free gear from the possibility of freezing in the wheel wells. |
|
|
Term
| Will Halon deployment extinguish a fire better at lower airspeeds? |
|
Definition
| Due to higher retention times at lower speeds there is a higher probability of fire extinction. |
|
|
Term
|
Definition
| Gages located in the NWW are the Landing Gear Emergency Air Pressure (2450psi) and forward adn aft canopy jettison. A-aux canopy, B-blow down, C-canopy |
|
|
Term
| Emergency O2 on ejection lasts how long? |
|
Definition
| The emergeny Oxygen supply will last approximately 15min depending on altitud and breathing rate. |
|
|
Term
| Seat man separation <11.5k occurs when? |
|
Definition
| A barostat delays drogue shoot release until 13,000 +/- 1500FT, therefore ejections below 11,500FT have no delay and parachute release is immediate. |
|
|
Term
| CDNU CLR button. Press it once, press it twice, Press and hold? |
|
Definition
| The CLR key on the CDNU is used to delete characters on the edit line. Pressed once it will delete the last character entered. When pressed and held it will delete character one at a time. Pressed twice in succession will clear the entire enty. |
|
|
