C-130 (H) Master Question File: Flight Engineer
When performing a Stop-and-Go landing, runway remaining for takeoff must be greater than or equal to __________. Ref: AFI 11-2C-130 Vol 3 Pg: 131 Chap: 9 Para: 9.9.2.3
CFL
If involved in a mishap or incident, after landing and terminating the emergency, pull the ___________ power circuit breaker. Ref: AFI 11-2C-130 Vol 3 Pg: 109 Chap: 6 Para: 6.49
CVR and FDR
The order of preference of bailout exits are: Ref: TO 1C-130 E/H/K-1 Pg: 3A-81,3A-76,3A-75 Chap: 3
Cargo door and ramp, paratroop doors and forward crew door
Operating procedures, techniques, etc., which could result in damage to equipment if not carefully followed is a________. Ref: TO 1C-130 E/H/K-1 Pg: viii, vii, xv.
Caution
Prior to performing any procedure which involves removing all AC power: Ref: TO 1C-130 E/H/K-1 Pg: 3A-33,3A-32,3A-33 Chap: 3 Para: Warning
Configure the fuel system for tank to engine operation
Starts in cold weather conditions may result in start TIT less than normal starting limits. If all engine starts are similar in TIT: Ref: TO 1C-130 E/H/K-1 Pg: 7-6,7-8,7-7 Chap: 7 Para: Note
Consider this a normal start, no further action is required
Takeoff run is ________ and rate of climb decreased in high temperatures. Ref: TO 1C-130 E/H/K-1 Pg: 7-10,7-11,7-10 Chap: 7
Considerably increased
Do not select ________ unless the crossfeed system is pressurized by operating fuel boost pumps in other tanks. Ref: TO 1C-130 E/H/K-1 Pg: 3A-29,3A-28,3A-29 Chap: 3 Para: Warning
Crossfeed
If NTS is not indicated during an airstart, interruption of the start cycle after light off by an attempt to feather before the engine has reached a stabilized speed may result in: Ref: TO 1C-130 E/H/K-1 Pg: 3B-10,3B-10,3B-9 Chap: 3 Para: Caution
Decoupling and severe over speed
The two common types of wind shear phenomena found on final approach are: Ref: TO 1C-130 E/H/K-1 Pg: 2-82,2-87,2-85 Chap: 2
Decreasing headwind, increasing headwind
Do not ________ or open the ground test valve if ramp hydraulic actuators are preloaded or cargo loading operations are in progress. Ref: TO 1C-130 E/H/K-1 Pg: 2-18,2-19,2-20 Chap: 2 Para: Warning
Deplete hydraulic pressure
________ take-off with a known or suspected landing gear malfunction. Ref: TO 1C-130 E/H/K-1 Pg: 3A-59,3A-58,3A-58 Chap: 3 Para: Caution
Do not attempt a
In the event that utility or boost hydraulic pressure in excess of 3,450 psi is indicated: Ref: TO 1C-130 E/H/K-1 Pg: 3A-52,3A-51,3A-51 Chap: 3 Para: Caution
Do not turn off the individual hydraulic pump switches
If parking brake handle does not properly retract and requires additional force to fully seat: Ref: TO 1C-130 E/H/K-1 Pg: 3A-14,3A-14,3A-13 Chap: 3 Para: Note
Document in Form 781
For Manual Gear Extension, make sure the ratchet on the hand crank is set for ______ rotation before placing it on the emergency extension stub shaft. Ref: TO 1C-130 E/H/K-1 Pg: 3A-62,3A-60,3A-62 Chap: 3 Para: Warning
Down
For PROPELLER BRAKE FAILURE; if the propeller does counter-rotate, and the procedures are ineffective: Ref: TO 1C-130 E/H/K-1 Pg: 3A-25,3A-25,3A-25 Chap: 3 Para: Caution
Land as soon as practical
With the escape ladder installed, it is impossible to exit the airplane from the center overhead escape hatch using the ________ side of the ladder. Ref: TO 1C-130 E/H/K-1 Pg: 1V-3,1V-3,1V-4 Chap: 1V Para: Warning
Left
When 100 percent oxygen is being supplied, _________ oxygen is consumed per person as altitude ________. Ref: TO 1C-130 E/H/K-1 Pg: 1T-1,1T-2,1T-1 Chap: 1T Para: Note
Less/increases
During the landing approach, _______ before the throttles are retarded should give more equal power distrubution on all engines. Ref: TO 1C-130 E/H/K-1 Pg: 1B-18, 1B-23 Chap: 1B
Locking the TD valve
Unless otherwise directed, waiver authority for the contents of AFI 11-2C-130V3 is the __________ with mission execution authority. Ref: AFI 11-2C-130 Vol 3 Pg: 20 Chap: 1 Para: 1.4.2.
MAJCOM/A3/DO
Maximum effort operations with airplane configuration (fuel, cargo, etc.) that necessitate 300 FPM rate-of-sink should be restricted to wartime operation only. To perform during peacetime will require ________ approval. Ref: TO 1C-130 E/H/K-1 Pg: 5-24,5-23,5-26 Chap: 5 Para: Caution
Major Command
________ is operation at the speed which results in the minimum fuel flow for the given configuration, altitude, temperature, and gross weight. Ref: TO 1C-130E(H)1-1/H1-1 Generic Pg: 6A-1,6A-2 Chap: 6
Maximum endurance
If an in-flight door warning occurs and it cannot be determined what caused the door light to illuminate, the flight ________ at the discretion of the pilot (below the point where the light illuminates and with all personnel secured with safety belts). Ref: TO 1C-130 E/H/K-1 Pg: 3A-50,3A-49,3A-48 Chap: 3 Para: Warning
May be continued with partial pressurization
When landing with one or two engines inoperative, it is recommended that the in-flight ________ be compared to the ________ and the higher speed be used for approach. Ref: TO 1C-130E(H)1-1/H1-1 Generic Pg: 8-3 Note,9-4 Note
Minimum control speed/recommended approach speed
Negative thrust from propeller(s) retarded to the FLIGHT IDLE position will produce _____ drag than a feathered or windmilling propeller and _________ air minimum control speeds for the condition. Ref: TO 1C-130 E/H/K-1 Pg: 3B-5,3B-5,3B-5 Chap: 3 Para: Warning
More, increase
Do not perform touch-and-go landings during formation recoveries unless: Ref: AFI 11-2C-130 Vol 3 Pg: 234 Chap: 18 Para: 18.14[W]
Never
Early stage thermocouple decay may be difficult to identify, due to: _________. Ref: TO 1C-130 E/H/K-1 Pg: 1B-16, 1B-21 Chap: 1B Para: NOTE
No change in TIT and minimal increase in fuel flow and torque
Protection against asymmetrical operation is provided only during ________ hydraulic flap operation. Ref: TO 1C-130 E/H/K-1 Pg: 3A-56,3A-55,3A-55 Chap: 3 Para: Warning
Normal
When the crosswind component and_____________ fall within the caution area, the take-off or touchdown speed should be increased until the recommended area is reached or until the aircraft speed has been increased by 10 knots. Ref: TO 1C-130E(H)1-1/H1-1 Generic Pg: 3-11,3-13 Chap: 3
Normal take-off or touch down speed
If the landing gear selector valve DOWN button requires holding to lower the gear, hydraulic pressure will not be available for: Ref: TO 1C-130 E/H/K-1 Pg: 3A-61,3A-59,3A-59 Chap: 3 Para: Caution
Nose wheel steering
If flammable fumes are present, electrical equipment not required to complete the FUSELAGE FIRE/SMOKE AND FUME ELEMINATION procedure should: Ref: TO 1C-130 E/H/K-1 Pg: 3A-45,3A-44,3A-43 Chap: 3 Para: Warning
Not be turned on or off until the fumes are eliminated
The minimum flap retraction speed for a maximum effort takeoff is: Ref: TO 1C-130 E/H/K-1 Pg: 2-69,2-73,2-72 Chap: 2
Obstacle clearance speed plus 10 knots
A positive hydraulic pressure indication must be noted by the time the engine is _______. Normal operating pressure should be indicated within ________ after on speed. Ref: TO 1C-130 E/H/K-1 Pg: 2-49,2-50,2-50 Chap: 2 Para: Note
On speed/30 seconds
In emergencies, MIL-L-7808 and MIL-L-23699 may be mixed. The amount of emergency oil added should not exceed ________ tank capacity. Ref: TO 1C-130 E/H/K-1 Pg: 1Z-4,1Z-2,1Z-4 Chap: 1Z Para: Delta 2
One-half
If either the left or right wheel well overheat light illuminates after takeoff and the condition persists after isolation procedures have been accomplished, it may be indicative of: Ref: TO 1C-130 E/H/K-1 Pg: 3A-9,3A-8,3A-8 Chap: 3 Para: Caution
Overheated brakes
Ensure that the secure voice system mode switch is in the ________ position to provide normal operation (plain text) of the UHF radio when secure voice is not to be used. Ref: TO 1C-130 E/H/K-1 Pg: 1R-7,1R-6,1R-8 Chap: 1R Para: NOTE
P
The ___________ is the final authority in determining the overall suitability of an aircraft for the mission. Ref: AFI 11-2C-130 Vol 3 Pg: 43 Chap: 4 Para: 4.1
PIC
At the briefed stabilization point, the _____ will state the altitude (AGL) and announce "stable" or "go-around". Ref: AFI 11-2C-130 Vol 3 Pg: 63 Chap: 5 Para: 5.12.1.8.
PM
The __________ will provide the obstacle height, distance, and gradient information necessary for performance computations to the flight engineer. Ref: AFI 11-2C-130 Vol 3 Pg: 85 Chap: 6 Para: 6.16.
Pilot In Command (PIC)
At high airspeeds, abrupt movement of the throttles into the ground range could result in: Ref: TO 1C-130 E/H/K-1 Pg: 2-81,2-86,2-84 Chap: 2 Para: Warning
Pitchlock
If a Tachometer Generator Failure occurs on the engine selected as the master engine, first: Ref: TO 1C-130 E/H/K-1 Pg: 3A-28,3A-27,3A-28 Chap: 3
Place the synchrophaser master switch to OFF/other master
Allowable propeller fluctuations are: Ref: TO 1C-130 E/H/K-1 Pg: 5-44,5-40,5-43 Chap: 5
Plus/minus 0.5% either side of a stable RPM for a total of 1%
Normally, the quick don oxygen mask system is the _______ use equipment. Ref: TO 1C-130 E/H/K-1 Pg: 2-44,2-43,2-45 Chap: 2 Para: Note
Primary
________ should be on during takeoff and climb if temperature is 32 degrees F or lower and any visible moisture is present. Ref: TO 1C-130 E/H/K-1 Pg: 7-8,7-9,7-8 Chap: 7 Para: Caution
Propeller and engine anti-icing and deicing
If the feather override button fails to pop out within 6 seconds after the the propeller is feathered: Ref: TO 1C-130 E/H/K-1 Pg: 5-44,5-40,5-43 Chap: 5
Pull it out manually to shut off the pump. Maintenance action is required prior to flight
If severe wind shear is encountered on final and a recovery is flown, the navigator/engineer will monitor and call out ___________________. Ref: TO 1C-130E/H/K-1, Pg: 2-83, 2-89, 2-86 Para: Wind Shear Recovery
Radar Altimeter
When operating in tank-to-engine position with an inoperative fuel boost pump, avoid: Ref: TO 1C-130 E/H/K-1 Pg: 3A-29,3A-29,3A-29 Chap: 3 Para: Note
Rapid acceleration or nose low attitudes
Touch and go landings are only authorized when the crosswind component corrected for RCR is within the ___________ zone for the landing crosswind chart. Ref: AFI 11-2C-130 Vol 3 Pg: 127 Chap: 9 Para: 9.2.2.4.
Recommended
If a stop, sudden or severe braking application has occurred during turns: Ref: TO 1C-130 E/H/K-1 Pg: 2-57,2-58,2-59 Chap: 2 Para: Caution
Record in Form 781A
If start TIT is between 720-750 degrees C: Ref: TO 1C-130 E/H/K-1 Pg: 5-43,5-39,5-42 Chap: 5
Record in Form 781and perform a temperature controlling check IAW section 1B
When it is suspected or known that an aerospace vehicle or piece of equipment has been contaminated with a radiological, biological or chemical contaminant, a _________ will be entered and an annotation will be made in historical records for the lifecycle of the equipment. Ref: AFI 11-2C-130 Vol 3 Pg: 143 Chap: 10 Para: 10.5.9.
Red X
If a propeller fails to feather in flight, it is critical to restore oil to the ________ of the windmilling propeller as soon as possible. Ref: TO 1C-130 E/H/K-1 Pg: 3A-24,3A-24,3A-24 Chap: 3 Para: Caution
Reduction gearbox
When crewmembers are required to refuel, the flight engineer will act as the __________. Ref: AFI 11-2C-130 Vol 3 Pg: 166 Chap: 12 Para: 12.4.1.1
Refueling team supervisor
As soon as the airplane is parked during hot weather, chock wheels and ________ in order to avoid possible damage to brake components from excessive heat generated while taxiing. Ref: TO 1C-130 E/H/K-1 Pg: 7-10,7-11,7-11 Chap: 7
Release brakes
If a turbine overheat occurs in-flight: Ref: TO 1C-130 E/H/K-1 Pg: 3A-10,3A-10,3A-10 Chap: 3
Retard the throttle toward FLIGHT IDLE. If the condition persists, proceed with the ENGINE SHUTDOWN PROCEDURE
The correct procedure for high TIT on the ground is: Ref: TO 1C-130 E/H/K-1 Pg: 3A-10,3A-10,3A-10 Chap: 3
Retard the throttle toward GROUND IDLE, and place the temp datum control valve switch to the NULL position. If this fails to eliminate the over temperature condition, place condition lever to GROUND STOP
During landing, at the first indication of directional control difficulties during reversing, immediately: Ref: TO 1C-130 E/H/K-1 Pg: 2-86,2-90,2-88 Chap: 2 Para: Warning
Return all throttles to GROUND IDLE
The nose gear must be on the ground prior to _________. Ref: TO 1C-130 E/H/K-1 Pg: 2-87,2-91,2-90 Chap: 2 Para: Warning
Reversing
Do not enter/exit from the ________ side of the nose wheel well due to possible hazard of venting liquid oxygen. Ref: TO 1C-130 E/H/K-1 Pg: 1T-7,1T-6,1T-7 Chap: 1T Para: Warning
Right
Which of the following information is obtained from the FLIP? Ref: TO 1C-130E(H)1-1/H1-1 Generic Pg: 9-2,10-2 Chap: 9,10
Runway heading/Length , obstacle height/distance, climb gradients, and slope
The LAPES/CDS switches must remain _________ in the NORMAL/OFF (guarded) position except when required to be in ARM for operational check or mission requirements. Ref: TO 1C-130 E/H/K-1 Pg: 1S-26,1S-21,1S-25 Chap: 1S Para: Caution
Safetied
While accomplishing the POWER ON INSPECTION, if a light in the overheat test panel fails to illuminate during testing, bleed air systems: Ref: TO 1C-130 E/H/K-1 Pg: 2-15,2-13,2-14 Chap: 2 Para: Caution
Should not be pressurized until proper inspection and repairs have been made
In case of loss of oil pressure: Ref: TO 1C-130 E/H/K-1 Pg: 3A-28,3A-27,3A-28 Chap: 3
Shut down the engine in accordance with the Engine Shutdown Procedure
When Ditching, the severity of fuselage structural damage or failure depends on sea conditions and aircraft ___________ upon touchdown. TO 1C-130 E/H/K-1 Pg: 3A-88,3A-83,3A-84 Chap: 3 Para: Warning
Speed/descent rate
Normal operation of the NTS system does not commit the propeller to feather. However, a malfunctioning NTS system may completely feather the propeller or cause the engine to:______ Ref: TO 1C-130 E/H/K-1-1 Pg: 1B-3, 1B-4 Chap: 1B Para: NOTE
Stall/flameout
In case of emergency, oxygen usage may be continued until: Ref: TO 1C-130 E/H/K-1 Pg: 5-6,5-6,5-9 Chap: 5 Para: Note
System is empty
In addition to the procedures in __________ and ___________, the flight engineer will assist the pilot in maintaining the AFTO Form 781. Ref: AFI 11-2C-130 Vol 3 Pg: 168 Chap: 12 Para: 12.7.2.
T.O. 00-20-1/AFI 11-401
When corrected refusal speed exceeds take-off speed, use _________. Ref: TO 1C-130E(H)1-1/H1-1 Generic Pg: 3-16.2,3-18 Chap: 3
Take-off speed for refusal speed
Take-off and immediate landing data for the departure airfield will be completed prior to ________. The destination landing data will be computed prior to the completion of ________. Ref: TO 1C-130E(H)1-1/H1-1 Generic Pg: 9-1 Note,10-1 Note
Take-off/DESCENT checklist
When moving the flaps at low airspeed, an asymmetrical flap may go undetected until near or above ___________. Ref: TO 1C-130 E/H/K-1 Pg: 2-88, 2-93, 2-91 Chap: 2 Para: Warning
Takeoff speed
If a tailpipe fire occurs in-flight, follow the ENGINE SHUTDOWN PROCEDURE. If the fire persists: Ref: TO 1C-130 E/H/K-1 Pg: 3A-10,3A-10,3A-10 Chap: 3
The airplane should be accelerated as rapidly as possible, not exceeding maximum airspeed
If auxiliary feather motor operation is not indicated for a propeller: Ref: TO 1C-130 E/H/K-1 Pg: 2-53,2-54,2-54 Chap: 2 Para: Warning
The malfunction will be corrected prior to flight
If an individual landing gear position indicator becomes inoperative because of a faulty grounding circuit, the warning horn and warning light will indicate the position of: Ref: TO 1C-130 E/H/K-1 Pg: 1G-13,1G-12,1G-14 Chap: 1G Para: NOTE
The other two gear only
If throttle control cable failure is suspected, do not move the throttle prior to engine shutdown. To do so could cause: Ref: TO 1C-130 E/H/K-1 Pg: 3A-25,3A-25,3A-25 Chap: 3 Para: Warning
The propeller to go into reverse pitch or to full power
For GCAS ESCAPE during IMC Departure/Approach. Immediately and simultaneously rotate the airplane to at least 7° pitch-up, roll wings level and add maximum power to alter the airplanes flight path until _______________. Ref: TO 1C-130E/H/K-1 Pg: 2-71, 2-75, 2-74 Chap: 2 Para 1.a.
The warning has ceased and adequate terrain clearance is verified
The temperature datum control valve switches lock a fuel correction only when they are positioned at LOCKED/LKD while the: ______. Ref: TO 1C-130 E/H/K-1 Pg: 1B-9, 1B-10 Chap: 1B Para: NOTE
Throttle is in the temperature controlling range and the fuel correction lights are out
After confirmed fuel pump failure, fuel boost pump circuit breakers may be reset and the pump operated only: Ref: TO 1C-130 E/H/K-1 Pg: 3A-29,3A-28,3A-29 Chap: 3 Para: Warning
To prevent fuel starvation when a landing cannot be accomplished within the range of available fuel
Never place the throttles in the TAKEOFF position without monitoring the ________, since it is possible to exceed the maximum allowable torque. Ref: TO 1C-130 E/H/K-1 Pg: 2-67,2-71,2-70 Chap: 2 Para: Caution
Torque meters
Take-Off factor combines the parameters of: Ref: TO 1C-130E(H)1-1/H1-1 Generic Pg: 3-6,3-9 Chap: 3
Torque, field pressure altitude, runway temperature, TIT, and engine efficiency
Air Force policy is to conserve aviation fuel when it does not adversely affect ________, ______________, or _______________. Ref: AFI 11-2C-130 Vol 3 Pg: 207 Chap: 14 Para 14.2.
Training, flight safety, operational readiness
A PIC who accepts an aircraft with degraded equipment/systems is not committed to subsequent operations with the same degraded equipment. Ref: AFI 11-2C-130 Vol 3 Pg: 43 Chap: 4 Para: 4.2.
True
Aircrews will consider delaying engine start on all departures whenever practical to minimize fuel consumption. Ref: AFI 11-2C-130 Vol 3 Pg: 207 Chap: 14 Para 14.2.5
True
Any crewmember that observes both pilots heads-down at the same time (other than heads-down instrument flying) shall alert the PF without delay. Ref: AFI 11-2C-130V3 Pg: 64 Chap: 5 Para:5.14.4.
True
Do not conduct simulated aircraft systems emergency procedures training during any tactical training (operating in low level environment or during tactical approaches). Ref: AFI 11-2C-130 Vol 3 Pg: 128 Chap: 9 Para: 9.4.1.2
True
Do not takeoff under conditions of freezing rain. Ref: AFI 11-2C-130 Vol 3 Pg: 90 Chap: 6 Para: 6.21.2.1.
True
During normal fuel servicing operations, simultaneous fuel and oxygen servicing is not authorized. Ref: AFI 11-2C-130 Vol 3 Pg: 167 Chap: 12 Para: 12.4.1.10
True
Each crewmember must carry an operable flashlight for night flights. Ref: AFI 11-2C-130 Vol 3 Pg: 76 Chap: 6 Para: 6.2.8.
True
If departure is not possible, the aircrew must secure the aircraft to the best of their ability. In no case, will the entire crew leave the aircraft unattended. Crew rest will be subordinate to aircraft security when the airframe may be at risk. Ref: AFI 11-2C-130 Vol 3 Pg: 113 Chap: 7 Para: 7.5.2.3
True
If either the pilots' NVGs, SCNS, pressure altimeter, or radar altimeter fail, climb to MSA until resolving the problem. In addition, climb to MSA to resolve any T.O. 1C-130(x)/(x)-1 Section III procedures, commensurate with the tactical situation. Ref: AFI 11-2C-130 Vol 3 Pg: 217 Chap: 16 Para: 16.4.1.4
True
Under no circumstance will any crewmember act as the towing supervisor. Ref: AFI 11-2C-130 Vol 3 Pg: 94 Chap: 6 Para: 6.25.6
True
Unless servicing JP-4, simultaneous servicing of fuel while loading passengers, cargo, performing maintenance, aircrew members performing inspections, or operating aircraft systems is considered to be a normal fuel servicing operation. Ref: AFI 11-2C-130 Vol 3 Pg: 166 Chap: 12 Para 12.4.1.
True
When conducting flaps up landings, compute and post VMCA speeds for both configurations; flaps 50% and flaps up (normal boost). For example: VMCA, in ground effect, one engine inoperative - 105/122. Ref: AFI 11-2C-130 Vol 3 Pg: 168 Chap: 12 Para: 12.8.2
True
For malfunctions which result in asymmetric thrust, the airplane will attempt to ________ the malfunctioning power plant during airplane acceleration. Ref: TO 1C-130 E/H/K-1 Pg: 3A-15,3A-15,3A-14 Chap: 3 Para: Note
Turn toward
With engines running, never operate the propeller anti-icing or de-icing system for more than ________ cycles while the airplane is on the ground. Ref: TO 1C-130 E/H/K-1 Pg: 2-59,2-61,2-61 Chap: 2 Para: Caution
Two
With actual or suspected vapor contamination, the aircraft must be purged for __________ using Smoke and Fume Elimination procedures to eliminate the vapor hazard. Ref: AFI 11-2C-130 Vol 3 Pg: 143 Chap: 10 Para: 10.5.8.
Two hours
If a propeller malfunction occurs after refusal speed and there is no indication of fire, it is recommended that the engine be allowed to run until at least ________ is reached. Ref: TO 1C-130 E/H/K-1 Pg: 3A-21,3A-22,3A-21 Chap: 3 Para: Note
Two-engine inoperative air minimum control speed
This is used for the purchase of aviation fuel and ancillary ground services at commercial airports (and some military installations) worldwide. Ref: AFI 11-2C-130 Vol 3 Pg: 124 Chap: 8 Para: 8.6
U.S. Government Aviation Into-Plane Reimbursement (AIR) card
This is a closed-loop system of communication designed to significantly reduce typical automation selection errors between the PF, PM, and the navigator. Ref: AFI 11-2C-130V3 Pg: 65 Chap: 5 Para: 5.15.2.
Verbalize, Verify, and Monitor (VVM)
For Refusal Speed, in the event of an engine failure, the options available are based on ________. Ref: TO 1C-130E(H)1-1/H1-1 Generic Pg: 3-35,3-36.1 Chap: 3
Vmcg, Vr, and Vcef
Main tank boost pump switches ________ be turned off in-flight unless directed by a specific procedure in the flight manual. Ref: TO 1C-130 E/H/K-1 Pg: 2-65,2-68,2-67 Chap: 2 Para: Warning
Will not
The AERP system ________ protect the user against ammonia fumes or carbon monoxide gas and _______ be used without an oxygen source in an oxygen deficient atmosphere. Ref: TO 1C-130 E/H/K-1 Pg: 1T-6,1T-5,1T-6 Chap: 1T Para: Warning
Will not, shall not
Smoke developed in the cargo compartment ________ move forward into the flight station. The hatch ________ be opened to effectively eliminate smoke and fumes during all elimination emergencies. Ref: TO 1C-130 E/H/K-1 Pg: 3A-48,3A-47,3A-45 Chap: 3A Para: Warning
Will/must
The flight engineer should monitor engine instruments during shutdown for: Ref: TO 1C-130 E/H/K-1 Pg: 2-96,2-101,2-100 Chap: 2 Para: Note
Zero fuel flow and TIT and RPM decrease
Low Altitude Approach maneuvers may be flown on continuation training and operational missions with passengers aboard. In all cases plan to roll out on final at __________ speed no lower than _____ ft _____. Ref: AFI 11-2C-130 Vol 3 Pg: 224 Chap: 17 Para: 17.6
approach/150/AGL
NVG Airland. Coordinated actions during the final segment of an NVG __________ and _________ are critical. Ref: AFI 11-2C-130 Vol 3 Pg: 230 Chap: 17 Para: 17.12.1.2
approach/landing
EROs will not be conducted simultaneously through the __________ door and __________ door. Ref: AFI 11-2C-130 Vol 3 Pg: 225 Chap: 17 Para: 17.8.1.[W]
crew entrance door/paratroop doors/cargo ramp and door
The RCR factor ________ affect the 4-engine climbout, but ________ affect the 3-engine climbout. Ref: TO 1C-130E(H)1-1/H1-1 Generic Pg: 3-19,3-21 Chap: 3 Para: Note
does not / does
Any crewmember that experiences NVG problems will: Ref: AFI 11-2C-130 Vol 3 Pg: 82 Chap: 6 Para: 6.12.2.2
inform the rest of the crew
When computing climb-out performance, a headwind ________used for obstacle clearance, but the tailwind component ________ used to determine an effective obstacle distance. Ref: TO 1C-130E(H)1-1/H1-1 Generic Pg: 3-18,3-20 Chap: 3
is not / is
Analyze pre-drop gross weight to determine if obstructions can be cleared with __________. Ref: AFI 11-2C-130 Vol 3 Pg: 236 Chap: 18 Para: 18.18.3[W]
one engine inoperative
Minimum taxi interval is _____ aircraft length with four engines operating and _____ aircraft lengths with two engines operating. Ref: AFI 11-2C-130 Vol 3 Pg: 232 Chap: 18 Para: 18.4.1
one/two
When required to transfer a loaded weapon to another crew member, __________. Ref: AFI 11-2C-130 Vol 3 Pg: 118 Chap: 7 Para: 7.13.7
place the weapon on a flat surface
All maximum effort operations must fall in the ___________ area of charts (corrected for RCR) unless otherwise approved by OG/CC. Ref: AFI 11-2C-130 Vol 3 Pg: 67 Chap: 5 Para: 5.18.6.
recommended
Pilots will normally use __________ for takeoffs provided refusal speed (Vr) is equal to or greater than takeoff speed. Ref: AFI 11-2C-130 Vol 3 Pg: 72 Chap: 5 Para: 5.28
reduced power
The maximum number of persons on the flight deck will be the minimum commensurate with the mission requirements. At no time will this exceed _____ (unless otherwise specified in a MAJCOM supplement). Ref: AFI 11-2C-130 Vol 3 Pg: 111 Chap: 6 Para: 6.57.1
seven
Flight into areas of forecast or reported __________ is prohibited. Ref: AFI 11-2C-130 Vol 3 Pg: 89 Chap: 6 Para: 6.21.1
severe turbulence
Crewmembers will carry __________ on all flights Ref: AFI 11-2C-130 Vol 3 Pg: 75 Chap: 6 Para: 6.2.5.
two identification tags
Initial qualification or re-qualification for pilots ____________ be conducted with passengers onboard. Ref: AFI 11-2C-130 Vol 3 Pg: 127 Chap: 9 Para: 9.1.1
will not
During ERO procedures, use __________ and __________ to enhance safety at night as the situation dictates. Ref: AFI 11-2C-130 Vol 3 Pg: 225 Chap: 17 Para: 17.8.1.1.3
wing leading edge/taxi lights
Observe engine torque and TIT when placing each ________ switch in the ON position when accomplishing the Before Takeoff checklist. Ref: TO 1C-130 E/H/K-1 Pg: 2-65,2-67,2-67 Chap: 2 Para: Note
ENGINE INLET AIR DUCT ANTI-ICING
In any airplane configuration that could limit the normal climb capability of the airplane (such as engine out, ramp door open, etc) or operational situation where an RA maneuver is prohibited, the TCAS should be placed in: Ref: TO 1C-130 E/H/K-1 Pg: 1M-11,1M-8,1M-11 Chap: 1M Para: WARNING
Either A or C
Higher than normal ________ system pressure may be encountered in-flight. Ref: TO 1C-130 E/H/K-1 Pg: 2-80,2-85,2-83 Chap: 2 Para: Note
Emergency brake
Depletion of the emergency brake hydraulic system pressure with the brake select switch in normal is an indication of a(n) ________ failure. Ref: TO 1C-130 E/H/K-1 Pg: 2-23,2-27,2-24 Chap: 2 Para: Caution
Emergency brake selector valve
When pulling the condition lever to FEATHER, pull it all the way to the detent to assure that the propeller is fully feathered when the engine fuel is shut off. If the lever is left at a mid-position, and NTS is inoperative, a(n) Ref: TO 1C-130 E/H/K-1 Pg: 3A-4,3A-4,3A-4 Chap: 3 Para: Warning
Engine decoupling is possible
The hydromechanical fuel control senses ________, and varies fuel flow accordingly. Ref: TO 1C-130 E/H/K-1 Pg: 1B-4, 1B-5 Chap: 1B
Engine inlet air temperature and pressure, RPM, and throttle position
The engine hydraulic pump pressure warning light will illuminate whenever the pump output pressure drops below approximately 1,000 PSI or: ______ Ref: TO 1C-130 E/H/K-1 Pg: 1G-2 Chap: 1G
Engine pump switch is placed in the OFF position
After moving the condition lever to ground stop, do not move the lever from this position until ________. Ref: TO 1C-130 E/H/K-1 Pg: 2-48,2-48,2-48 Chap: 2 Para: Caution
Engine rotation has stopped
For GCAS ESCAPE MANEUVERS; Crewmembers will back up the pilot who is performing the escape maneuver. The __________ and ____________ will confirm escape maneuver is being properly flown. Ref: TO 1C-130 E/H/K-1 Pg: 2-71,2-75,2-74 Chap: 2 Para: Warning
Engineer, pilot monitoring
If on crossfeed during the ENGINE SHUTDOWN PROCEDURE, ________ before shutting off the fuel boost pump and closing the crossfeed valve for the affected engine. Ref: TO 1C-130 E/H/K-1 Pg: 3A-6,3A-5,3A-6 Chap: 3 Para: Note
Ensure source of fuel to operate engines
The CVR is operational anytime the ________ bus is powered by any source other than external power. Ref: TO 1C-130 E/H/K-1 Pg: 1U-7,1U-7,1U-12 Chap: 1U
Essential AC
The only sound response when severe wind shear is encountered during an approach is an immediate decision to _______________ Ref: TO 1C-130E/H/K-1 Pg: 2-84, 2-89, 2-87 Para: Warning
Execute a go around
If aborting for a propeller malfunction or any other malfunction which could result in asymmetric power causing directional control problems when the throttles are placed in the ground range, shut down the affected engine while throttle is in: Ref: TO 1C-130 E/H/K-1 Pg: 3A-15,3A-14,3A-14 Chap: 3 Para: Warning
FLIGHT IDLE
Raising of the flaps is permissible during stall recovery to decrease drag and assist in the recovery. Ref: TO 1C-130 E/H/K-1 Pg: 6-1,6-1,6-1 Chap: 6 Para: Warning
False
Do not hold the ice detector TEST switch in the No. 2 or No. 3 position longer than five seconds. The test cycle may be repeated once, but then wait ________ minutes for the ice detector to cool before performing this test again. Ref: TO 1C-130 E/H/K-1 Pg: 2-59,2-60,2-61 Chap: 2 Para: Caution
Five
__________ is the period of time starting at mission report time and ending immediately after the aircrew completes the final engine shutdown of the day. Ref: AFI 11-2C-130 Vol 3 Pg: 31 Chap: 3 Para: 3.7.1.
Flight Duty Period
Above crossover, if the engine instruments are not similar in ________, with throttles aligned, a propulsion system malfunction may exist. Ref: TO 1C-130 E/H/K-1 Pg: 2-67,2-71,2-69 Chap: 2 Para: Warning
Fuel flow, TIT, or torque
The throttles must not be moved out of the ________ detent during engine starting. Ref: TO 1C-130 E/H/K-1 Pg: 2-47,2-47,2-48 Chap: 2 Para: Caution
GROUND IDLE
In all combinations of two engine failures, monitor ________ to keep it within the range of available output. Ref: TO 1C-130 E/H/K-1 Pg: 3A-16,3A-16,3A-15 Chap: 3
Generator loading
In case of power failure, the crossfeed valves:______. Ref: TO 1C-130 E/H/K-1 Pg: 1D-4, 1D-3 Chap: 1D
Hold the last energized position
If a situation is encountered where the aircraft is on a Red X and qualified maintenance personnel are not available to clear it, the highest qualified flight engineer on scene may obtain authorization to sign off the Red X from the ___________, in accordance with TO 00-20-1. Ref: AFI 11-2C-130 Vol 3 Pg: 166 Chap: 12 Para: 12.3.
Home station MXG/CC or designated representative
During the POWER ON INSPECTION, movement of the flaps is essential at this time to enable detection of ________ or malfunctions during the walk-around inspection. Ref: TO 1C-130 E/H/K-1 Pg: 2-19,2-20,2-21 Chap: 2 Para: Note
Hydraulic leaks
Any time an IGNITION CONTROL circuit breaker is pulled on an inboard engine, the ________ for that engine is inoperative. Ref: TO 1C-130 E/H/K-1 Pg: 3A-27,3A-26,3A-26 Chap: 3 Para: Note
Ice detection system
Failure of the reverse current relay connecting the essential and isolated DC bus will be indicated by: Ref: TO 1C-130 E/H/K-1 Pg: 3A-37,3A-36,3A-37 Chap: 3
Illumination of the ISOL DC ON BATT/BAT DSCH light and/or a battery voltmeter indication of 24 volts or less
If a go-around is accomplished, retracting flaps from 100 to 50 percent will: Ref: TO 1C-130 E/H/K-1 Pg: 2-90,2-95,2-94 Chap: 2 Para: Warning
Increase stall speed
The use of brakes during reverse taxiing should be ________ to prevent the airplane from setting on the tail. Ref: TO 1C-130 E/H/K-1 Pg: 2-58,2-59,2-59 Chap: 2 Para: Caution
Avoided
The AF IMT 4108 will be completed whenever the navigator completes the __________. Ref: AFI 11-2C-130 Vol 3 Pg: 169 Chap: 12 Para: 12.9.2
AF IMT 4116, C-130 Flight Plan and Record
The __________ is a tool to notify appropriate authorities of any mishap involving crewmembers or aircraft. Ref: AFI 11-2C-130 Vol 3 Pg: 120 Chap: 8 Para: 8.4
AMC IMT 97, AMC In-Flight Emergency and Unusual Occurrence Worksheet
Under stable conditions, allowable oil pressure fluctuation is _________ psi (_________ psi excursion) for the power section. Ref: TO 1C-130 E/H/K-1 Pg: 5-42,5-38,5-41 Chap: 5 Para: Delta 1
+/- 10 psi/20 psi
Normal limit for the cabin differential gage: Ref: TO 1C-130 E/H/K-1 Pg: 5-3,5-3,5-5 Chap: 5
-1.2 to 15.8 In. Hg
Cabin differential pressure will be zero for landing. If the differential pressure is less than ________ Hg, no discomfort will be experienced if the air conditioning master switch is turned to a nonpressure position. Ref: TO 1C-130 E/H/K-1 Pg: 1J-10,1J-11,1J-12 Chap: 1J Para: NOTE
0.5
During propeller reversing check, if symmetrical torque differences are ________ inch pounds or more, record in AFTO Form 781. Ref: TO 1C-130 E/H/K-1 Pg: 5-8,5-8,5-11 Chap: 5
1,000
To compute ESA, add _____ feet (_____ feet in mountainous terrain) to the elevation of the highest obstruction to flight within _____ NMs either side of the planned route centerline. An ESA will be computed for the route and conspicuously annotated on the chart. Ref: AFI 11-2C-130 Vol 3 Pg: 219 Chap: 16 Para: 16.4.1.7
1,000/2,000/22
When landing with two engines inoperative, a go-around is not recommended: Ref: TO 1C-130 E/H/K-1 Pg: 3A-84,3A-79,3A-80 Chap: 3 Para: Warning
After the flaps are lowered
In terminal areas, __________ (if able) will monitor the command radio unless directed otherwise. Ref: AFI 11-2C-130 Vol 3 Pg: 63 Chap: 5 Para: 5.13.2.2.
All crewmembers
Airdrops will not be conducted below the following altitudes: Ref: AFI 11-2C-130 Vol 3 Pg: 219 Chap: 16 Para: 16.4.2
All of the above
Crews facing a hijacking threat will notify ground agencies by __________. Ref: AFI 11-2C-130 Vol 3 Pg: 117 Chap: 7 Para: 7.11
All of the above
Do not connect unauthorized equipment (laptop computers, video equipment, food preparation equipment, radios/tape players, CD players, etc.) to: Ref: AFI 11-2C-130 Vol 3 Pg: 59 Chap: 5 Para: 5.9.1.
All of the above
During EXTERIOR INSPECTION, if not previously checked by maintenance, a work stand/ladder will be required to check: Ref: TO 1C-130 E/H/K-1 Pg: 2-30,2-33,2-30 Chap: 2
All of the above
During pitchlocked propeller operation, the engine should be shutdown when: Ref: TO 1C-130 E/H/K-1 Pg: 3A-24,3A-24,3A-23 Chap: 3
All of the above
During the BEFORE EXTERIOR INSPECTION and before any electrical power is applied to the airplane, the engineer will: Ref: TO 1C-130 E/H/K-1 Pg: 2-5,2-4, 2-5 Chap: 2
All of the above
If cabin pressure increases at an excessive rate and cannot be reduced by normal means then: Ref: TO 1C-130 E/H/K-1 Pg: 3A-8,3A-9,3A-9 Chap: 3
All of the above
It is imperative for aircrews to review the airfield environment. Identify key features such as: Ref: AFI 11-2C-130V3 Pg: 63 Chap: 5 Para: 5.12.4.
All of the above
SQ/CCs shall not schedule an aircrew member to fly nor will an aircrew member perform aircrew duties: Ref: AFI 11-2C-130 Vol 3 Pg: 33 Chap: 3 Para: 3.8.
All of the above
With any flap extension, the maximum maneuver load factor is ________ G in unsymmetrical maneuvers. Ref: TO 1C-130 E/H/K-1 Pg: 5-13,5-13,5-16 Chap: 5 Para: Caution
1.5
After Slowdown, element leads will not exceed _____ degrees of bank. Ref: AFI 11-2C-130 Vol 3 Pg: 235 Chap: 18 Para: 18.18.2
10
Ensure INU power switch has been off for more than ________ seconds before turning SCNS power switch OFF. Ref: TO 1C-130 E/H/K-1 Pg: 4A-23,4A-24,4A-19 Chap: 4 Para: Note
10
If the inner and outer panes of a flight deck windshield should crack in-flight, reduce the cabin pressure to ___________. Ref: TO 1C-130 E/H/K-1 Pg: 3A-51,3A-50,3A-49 Chap: 3
10 inches or less
If movement of the flaps, after an outboard flap failure, must be attempted, return them in increments of ________ toward the position last selected before failure. During flap movement, check aileron control ________. Ref: TO 1C-130 E/H/K-1 Pg: 3A-55,3A-54,3A-54 Chap: 3 Para: Warning
10 percent/constantly
For a takeoff continued after engine failure, flap retraction should be accomplished in ______ percent increments with airspeed increasing approximately ________ knots between retraction increments. Ref: TO 1C-130 E/H/K-1 Pg: 3A-16,3A-16,3A-15 Chap: 3 Para: Note
10, 5
Power section oil pressure up to ________ PSI is allowable during start and warm-up. Ref: TO 1C-130 E/H/K-1 Pg: 5-2,5-2,5-4 Chap: 5
100
When oil temperature exceeds ________ degrees C. for any time duration, an entry will be made in the Form 781 to include duration and temperature. Ref: TO 1C-130 E/H/K-1 Pg: 5-2,5-2,5-2 Chap: 5 Para: Note
100
The stabilization point for precision approaches is at _______ feet above Threshold Elevation (THRE). For all other approaches (except tactical approaches), the stabilization point is at ______ feet above THRE unless otherwise briefed by the PF. Ref: AFI 11-2C-130 Vol 3 Pg: 62 Chap: 5 Para: 5.12.
1000/300
CDS Airdrops. It is not recommended to drop CDS at gross weights less than _____ pounds. Ref: AFI 11-2C-130 Vol 3 Pg: 252 Chap: 19 Para: 19.29.1
104,000
Normal limits for AC voltage: Ref: TO 1C-130 E/H/K-1 Pg: 5-2,5-4,5-7 Chap: 5
110 to 125 Volts
Complete all mission-related events (i.e., FCF/ACF checks, transition events, or tactical events) during the first _____ hours of the FDP. Ref: AFI 11-2C-130 Vol 3 Pg: 32 Chap: 3 Para: 3.7.1.5.2
12
Maximum gross weight for a no-flap landing is _____ lbs. Ref: AFI 11-2C-130 Vol 3 Pg: 131 Chap: 9 Para: 9.9.1.6.
120,000
Two-engine operation above ________ pounds gross weight or at high density altitude is marginal. Ref: TO 1C-130 E/H/K-1 Pg: 3A-17,3A-16,3A-16 Chap: 3 Para: Warning
120,000
Secondary fuel management will shorten the service life of the wings and should be avoided unless necessary for mission accomplishment. This becomes more critical when: Ref: TO 1C-130 E/H/K-1 Pg: 5-15,5-15,5-18 Chap: 5 Para: Note
All of the above
The C-130 is a category "C" aircraft. If approach speeds exceed _____ knots, the minimums for category "D" will be used. Ref: AFI 11-2C-130 Vol 3 Pg: 101 Chap: 6 Para: 6.42.1
140
In accordance with hot weather procedures, during descent (for landing) below ________ feet, manually open the oil cooler flaps and place the switches to the FIXED position. Ref: TO 1C-130 E/H/K-1 Pg: 7-10,7-11,7-10 Chap: 7
15,000
Temperature and pressure altitude will be obtained from __________. Ref: TO 1C-130E(H)1-1/H1-1 Generic Pg: 9-2,10-2 Chap: 9,10
All of the above
Do not exceed ________ KIAS with the ramp (or ramp and cargo door) open regardless of whether the paratroop doors are open or closed or the position of the air deflectors. Ref: TO 1C-130 E/H/K-1 Pg: 5-11,5-12,5-10 Chap: 5
150
Reduction gearbox oil pressure is permitted to go below ________ PSIG when RPM is below 100% if 150 PSIG can be maintained at 100% RPM with oil temperature normal. Ref: TO 1C-130 E/H/K-1 Pg: 5-42,5-37,5-41 Note 3 Chap: 5
150
Non-Current and/or unqualified NVG aircrews may fly NVG departures in weather down to ______. Ref: AFI 11-2C-130 Vol 3 Pg: 98 Chap: 6 Para: 6.33.1
1500/3
If elevator control should fail (hydraulic assistance is lost), achieve approximately level flight and ________ KIAS and land with 50% flaps recommended. Ref: TO 1C-130 E/H/K-1 Pg: 3A-54,3A-53,3A-53 Chap: 3
170
Fin stall can occur at all speeds between stall speed and approximately ________ KIAS in all flap configurations with power________. Ref: TO 1C-130 E/H/K-1 Pg: 6-2,6-2,6-2 Chap: 6
170/ON
With the exception of cruise flight, conversation below _________ will be limited to mission, departure, or approach essential items. Ref: AFI 11-2C-130 Vol 3 Pg: 64 Chap: 5 Para: 5.14.3
18,000 feet MSL
The PROPELLER LOW OIL WARNING light and the PROP LOW OIL QUANTITY light will illuminate when the oil quantity for any propeller drops approximately ______ below normal in the pressurized sump. Ref: TO 1C-130 E/H/K-1 Pg: 1B-13, 1B-12, 1B-18 Chap: 1B
2 quarts
Crewmembers will fit and adjust LPUs for overwater flights and will wear them on overwater missions below _______ feet. Ref: AFI 11-2C-130 Vol 3 Pg: 94 Chap: 6 Para: 6.27.3
2,000
Do not fly directly above (within _____ feet) thunderstorms or cumulonimbus clouds. Ref: AFI 11-2C-130 Vol 3 Pg: 90 Chap: 6 Para: 6.21.3.
2,000
If a decision is made by the pilot to ditch the airplane then a minimum of ________ pounds of fuel should remain at time of descent from altitude. Ref: TO 1C-130 E/H/K-1 Pg: 3A-89,3A-84,3A-85 Chap: 3
2,000
Aircraft damage may occur up to _____ from any thunderstorms. Ref: AFI 11-2C-130 Vol 3 Pg: 91 Chap: 6 Para: 6.21.3.1.4
20 NMs
When personnel on-load and off-load through the crew entrance door, station a crewmember (normally the loadmaster) on interphone with cord held taut at approximately ______-feet at an angle of _____-degrees from the aircraft axis. Ref: AFI 11-2C-130 Vol 3 Pg: 226 Chap: 17 Para: 17.8.1.6
20/45
Aircraft must be able to meet the published climb gradient for the departure runway with all engines operating. If no minimum climb gradient is published, _____ ft/nm to MSA will be used. Ref: AFI 11-2C-130 Vol 3 Pg: 86 Chap: 6 Para: 6.16.3.3.
200
When the leading edge temperature reaches approximately ________ the overheat warning light for that area is energized and the light illuminates. Ref: TO 1C-130 E/H/K-1 Pg: 1K-1,1K-2,1K-2 Chap: 1K
200 degrees F
Any crewmember seeing a deviation of _____ feet altitude or _____ knots in airspeed, or a potential terrain or obstruction problem, will immediately notify the PF. Ref: AFI 11-2C-130 Vol 3 Pg: 60 Chap: 5 Para: 5.11.2.2.
200/10
The normal limits on the DC voltmeter are ________ volts. Ref: TO 1C-130 E/H/K-1 Pg: 5-4,5-4,5-7 Chap: 5
25-30
Do not taxi an aircraft within _____ feet of obstructions without wing walkers monitoring the clearance between aircraft and obstructions. With wing walkers, avoid taxi obstructions by at least ____ feet. Ref: AFI 11-2C-130 Vol 3 Pg: 68 Chap: 5 Para: 5.19.1.
25/10
Maximum airspeed with the paratroop doors open and locked is: Ref: TO 1C-130 E/H/K-1 Pg: 5-12,5-12,5-10 Chap: 5
250 KIAS
The aircraft dash one preflight inspection will remain valid until either: Ref: AFI 11-2C-130 Vol 3 Pg: 93 Chap: 6 Para: 6.25.3.1
All of the above
The external fuel tank fuel boost pump pressure limits are ________ PSI. Ref: TO 1C-130 E/H/K-1 Pg: 5-3,5-3,5-5 Chap: 5
28 to 40
Minimum TOLD requirements for a termination landing are: Air Minimum Control Speeds, Obstacle Clearance Speed, 3 Engine Climb Speed, 100 & 50% Flap Landing Speeds and Distances, 0% Landing Approach Speed (Night or IMC), and __________. Ref: AFI 11-2C-130 Vol 3 Pg: 169 Chap: 12 Para: 12.8.3
3 Eng Ft/NM
For peace-time do not use runways less than __________ feet. Ref: AFI 11-2C-130 Vol 3 Pg: 65 Chap: 5 Para: 5.18.1
3,000
When flying at night, potential for spatial disorientation increases with: Ref: AFI 11-2C-130 Vol 3 Pg: 233 Chap: 18 Para: 18.10.2.5[W]
All of the above
Prior to raising the ramp, ensure that: Ref: TO 1C-130 E/H/K-1 Pg: 1G-7,1G-7,1G-8 Chap: 1G Para: CAUTION
All ramp locks are retracted and the ramp seal area is clear
In most cases degradation of an individual thermocouple assembly would affect each circuit equally. The indicating signal will be lower (______degC) than the actual temperature experienced by each thermocouple sensing element. Ref: TO 1C-130 E/H/K-1 Pg: 1B-6 Chap: 1B
3.5 to 22
A negative G condition may allow air to enter the engine oil supply line resulting in a loss of oil pressure approximately ________ later due to oil pump cavitation. Ref: TO 1C-130 E/H/K-1 Pg: 3A-28,3A-27,3A-28 Chap: 3 Para: Note
30 to 90 seconds
NVG Operations. IMC Approaches. The transfer of aircraft control for the landing will be no lower than _____. Ref: AFI 11-2C-130 Vol 3 Pg: 230 Chap: 17 Para: 17.12.1.4
300' AGL
If there is no positive indication of oil pressure on the engine and reduction gear by _________ % RPM, immediately discontinue the start. Ref: TO 1C-130 E/H/K-1 Pg: 2-49,2-49,2-50 Chap: 2 Para: Caution
35
When any doubt exists about which screen height to use, plan to cross the DER at _____ feet (minimum) unless you can ascertain a different screen height requirement from an appropriate authority. Ref: AFI 11-2C-130 Vol 3 Pg: 86 Chap: 6 Para: 6.16.3.2.
35
The engine low oil quantity warning light illuminates when an oil tank quantity level drops to approximately:______. Ref: TO 1C-130 E/H/K-1 Pg: 1B-11, 1B-12, 1B-15 Chap: 1B
4 gallons
A sheared shaft on the speed sensitive control with the throttle above 65 degrees travel may be indicated by: Ref: TO 1C-130 E/H/K-1 Pg: 3A-27,3A-27,3A-27 Chap: 3
All the above
If headwinds of more than 70 knots are encountered, increasing the cruise TAS by _________ knots for every _________ knots above 70 knots headwind will result in operating the airplane near the maximum nautical miles per pound of fuel. Ref: TO 1C-130E(H)1-1/H1-1 Generic Pg: 5-8,5-11 Chap: 5
4/10
The 28 volt external DC source should have a capacity of _____ amperes. Ref: TO 1C-130 E/H/K-1 Pg: 1F-3, Chap: 1F Para: NOTE
400
Regardless of specific emergency encountered: Ref: TO 1C-130 E/H/K-1 Pg: 3A-2,3A-3,3A-2 Chap: 3A
All the above
NVG Operations. For tactical VFR approaches, bank angle will not exceed _____ degrees and the aircraft will not descend below _____ AGL until rolled on final. Ref: AFI 11-2C-130 Vol 3 Pg: 230 Chap: 17 Para: 17.12.1.3.
45/150'
New TOLD will be required any time gross weight changes 5,000 pounds or more, outside temperature changes ________ degrees C or more, or pressure altitude changes 1,000 feet or more. Ref: TO 1C-130 E/H/K-1 Pg: 2-77,2-81,2-79 Chap: 2 Para: Note
5
For normal take-off, rotation speed is _________ than take-off speed to be used. Ref: TO 1C-130E(H)1-1/H1-1 Generic Pg: 3-22,3-24 Chap: 3 Para: Note
5 KIAS less
Maintain at least _____ separation from heavy rain showers. Ref: AFI 11-2C-130 Vol 3 Pg: 91 Chap: 6 Para: 6.21.3.3.2
5 NMs
Minimum runway length for 50% flap flight idle touch-and-go landing is _____ feet. Minimum runway length for all other touch-and-go landings is _____ feet. Ref: AFI 11-2C-130 Vol 3 Pg: 127 Chap: 9 Para: 9.2.2.2
5,000/6,000
Towed Parachutist. The PIC must consider density altitude, aircraft weight, position in formation, or other factors deemed important in determining what flap setting between _____ and _____ percent should be used. Ref: AFI 11-2C-130 Vol 3 Pg: 259 Chap: 19 Para: 19.39.4[W]
50/100
Formations. At no time will aircraft be operated within _____ feet of another aircraft. Ref: AFI 11-2C-130 Vol 3 Pg: 232 Chap: 18 Para: 18.7.1.
500
Day VMC En-Route. Fly no lower than ___________ (or __________ IAW paragraph 16.4.4.8) modified contour altitude above terrain using visual references and radar altimeter. Ref: AFI 11-2C-130 Vol 3 Pg: 217 Chap: 16 Para: 16.4.1.2
500 feet AGL, 300 feet AGL
Combat Off-load Method "A" Procedures. A taxiway or ramp at least ______ feet long is required, however, _____ feet is desired to provide a margin of safety. Ref: AFI 11-2C-130 Vol 3 Pg: 227 Chap: 17 Para: 17.8.2.1.1[C]
500/1000
NVG Enroute. Fly no lower than an indicated altitude of _________feet abouve the highest spot terrain elevation, or __________ feet plus one chart contour interval above the highest depicted terrain contour, whichever is higher, within the tactical corridor. Ref: AFI 11-2C-130 Vol 3 Pg: 217 Chap: 16 Para: 16.4.1.4.
500/400
Night VMC En-Route (Non-NVGs). Fly no lower than an indicated altitude of ________-feet above the highest obstruction to flight (man-made obstacle, terrain feature, or spot elevation), or _____-feet plus one chart contour interval above the highest depicted terrain contour, whichever is highest, within the tactical corridor to include the aircraft turn radius over each point. Ref: AFI 11-2C-130 Vol 3 Pg: 217 Chap: 16 Para: 16.4.1.3.
500/400
Plan MSA at an indicated altitude of _____-feet above the highest obstruction to flight (man-made obstacle, terrain feature, or spot elevation), or _____-feet plus one chart contour interval above the highest depicted terrain contour, whichever is highest, within _____ of route centerline to include the aircraft turn radius. Ref: AFI 11-2C-130 Vol 3 Pg: 218 Chap: 16 Para: 16.4.1.5
500/400/5 NMs
When the flight station air conditioning is on, the bleed air pressure indicator reads ________ than the actual pressure in the cross wing manifold. Ref: TO 1C-130 E/H/K-1 Pg: 1J-2,1J-2,1J-2 Chap: 1J Para: NOTE
6 PSI lower
Elevator trim tab travel is controlled by limit switches set at ________ degrees nose down and ________ degrees nose up. Ref: TO 1C-130 E/H/K-1 Pg: 1H-5,1H-5,1H-5 Chap: 1H Para: NOTE
6/25
In accordance with desert procedures; when propeller reversing is used during landing, start moving the throttles from MAXIMUM REVERSE to GROUND IDLE at approximately ________ KIAS and have the throttles at GROUND IDLE by the time 40 KIAS is reached. Ref: TO 1C-130 E/H/K-1 Pg: 7-12,7-13,7-12 Chap: 7
60
When operating with less than 6,000 pounds of total fuel in the main fuel tanks:______. Ref: TO 1C-130 E/H/K-1 Pg: 1D-11, 1D-9, 1D-10 Chap: 1D Para: CAUTION
All the above
During GROUND EVACUATION; if pyrotechnics are loaded on the airplane, evacuate a minimum of ______ feet from the airplane. Ref: TO 1C-130 E/H/K-1 Pg: 3A-11,3A-11,3A-11 Chap: 3 Para: Warning
600
After any full anti-skid braking operation above 130,000 pounds (aborted takeoff, engine-out/flaps-up landing, etc.), the approximate ground cooling time is ________ minutes. Ref: TO 1C-130 E/H/K-1 Pg: 1G-17,1G-16,1G-19 Chap: 1G Para: WARNING
65
If the BLADE DE-ICING ammeter falls below________, do not fly into icing conditions. Ref: TO 1C-130 E/H/K-1 Pg: 2-60,2-62,2-62 Chap: 2 Para: Warning
65 amperes
The recommended airspeed for penetration into thunderstorms is: Ref: TO 1C-130 E/H/K-1 Pg: 7-3,7-2,7-3 Chap: 7 Para: NOTE
65 knots above power-off stall speed not to exceed 180 KIAS
The ADS control panel ramp and door control switch must be set to OFF, and the ramp manual control knob, above the ramp control panel, must be set at the ________ position before operating the pump switch on the ramp control panel. Ref: TO 1C-130 E/H/K-1 Pg: 1G-7,1G-7,1G-8 Chap: 1G Para: WARNING
6N (neutral)
During low air density conditions (high temperature above approximately 28 degrees C/high altitude), if the engine accelerates smoothly with no indication of stall and TIT limits are not exceeded, time to stabilize on speed is ________ seconds. Ref: TO 1C-130 E/H/K-1 Pg: 2-48,2-48,2-48 Chap: 2 Para: Note
70
The landing gear warning horn cannot be silenced until the landing gear is down and locked or the flap lever is retracted above ________ %. Ref: TO 1C-130 E/H/K-1 Pg: 1H-6,1H-6,1H-6 Chap: 1H Para: NOTE
70
If start TIT is less than _________degrees C, record in AFTO Form 781. Maintenance action is required prior to flight. Ref: TO 1C-130 E/H/K-1 Pg: 2-50,2-50,2-51 Chap: 2 Para: Warning
720
The fuel low pressure warning light is turned on when fuel supply pressure at the point where fuel enters the engine pump falls below approximately ______ PSI. Ref: TO 1C-130 E/H/K-1 Pg: 1D-6, 1D-7 Chap: 1D
8.5
When down-shifting from normal to low-speed ground idle, the engineer will monitor the engine instruments and be prepared to shut down the engine by placing the condition lever to GROUND STOP if the temperature exceeds ________ degrees C or a stall occurs. Ref: TO 1C-130 E/H/K-1 Pg: 2-56,2-57,2-58 Chap: 2 Para: Caution
850
Normal speed ground idle RPM limits are ________ percent. Ref: TO 1C-130 E/H/K-1 Pg: 5-42,5-37,5-41 Chap: 5
94-102
The high pressure of the Halon fire extinguisher can spread a class ________ fire. Ref: TO 1C-130 E/H/K-1 Pg: 1V-1,1V-1,1V-1 Chap: 1V Para: Caution
A
If NTS advisory lights do not illuminate when shutting down engines from low-speed ground idle: Ref: TO 1C-130 E/H/K-1 Pg: 2-96,2-102,2-100 Chap: 2 Para: Note
A recheck of the NTS system must be made before the next flight
If indicated torque exceeds 19,600 inch pounds: Ref: TO 1C-130 E/H/K-1 Pg: 2-67,2-71,2-70 Chap: 2 Para: Caution
An entry in the FORM 781A is required noting the highest torque value observed and describing the runway and/or flight conditions
The electrical control system of the ramp and door is inactivated when the: Ref: TO 1C-130 E/H/K-1 Pg: 1S-25,1S-22,1S-24 Chap: 1S Para: Caution
Anchor line support arms are not in the UP position
__________ detecting the illumination of the radar altimeter Low Altitude Warning Light will immediately notify the pilot flying the aircraft. Ref: AFI 11-2C-130 Vol 3 Pg: 72 Chap: 5 Para: 5.26.1
Any crewmember
The battery is disconnected from all DC buses except the ______ when external DC power is used. Ref: TO 1C-130 E/H/K-1 Pg: 1F-3 Chap: 1F
Battery bus
Authority to use the Hostile Environment Kit and Repair Procedures is granted by OG/CC/CD for Operations; this authority is documented on the: Ref: AFI 11-2C-130 Vol 3 Pg: 173 Chap: 12 Para: 12.10.1
Both A and C
Cold weather procedures are generally considered to be applicable when the temperature is ________ and below. Ref: TO 1C-130 E/H/K-1 Pg: 7-3,7-5,7-4 Chap: 7
Both B and C
