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Boeing 737-800 Flight Crew Training Manual Questions

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Boeing 737-800 Flight Crew Training Manual Questions

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25 Questions

1. Which two factors that affect stopping distance are most effective during the high speed portion of the landing?

2. During an ILS approach, when should Flaps 5 be selected?

3. Under which conditions is use of the autobrake system recommended?

Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Page: 6.52Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39

4. What are the guidelines for maximum crosswind during landing under the following runway conditions: (1) dry, (2) wet, (3) standing water/slush, (4) snow (no melting), and (5) ice (no melting)?

Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Page: 6.52Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39

5. If THR HLD is not annunciated during takeoff, what is the appropriate crew action?

Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39The THR HLD mode protects against thrust lever movement if a system fault occurs. Lack of the THR HLD annunciation means the protective feature may not be active. If THR HLD annunciation does not appear, no crew action is required unless a subsequent system fault causes unwanted thrust lever movement. As with any autothrottle malfunction, the autothrottle should then be disconnected and desired thrust set manually. | Page: 3.7When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16

6. How can the accuracy of the FMC-calculated descent profile be improved if anti-ice is to be used?

When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16The use of anti-ice and the increased thrust required increases the descent distance. Therefore, proper descent planning is necessary to arrive at the initial approach fix at the correct altitude, speed, and configuration. The anticipated anti-ice use altitude should be entered on the DESCENT FORECAST page to assist the FMC in computing a more accurate descent profile. | Page: 4.23Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39

7. During climb, until what point should flaps up maneuvering speed be maintained?

When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44Maintain flaps up maneuvering speed until clear of obstacles or above minimum crossing altitudes. If there are no altitude or airspeed restrictions, accelerate to the crossing altitudes. If there are no altitude or airspeed restrictions, accelerate to the desired climb speed schedule. The sooner the airplane can be accelerated to the climb speed schedule, the more time and fuel efficient the flight. | Page: 4.2

8. What is typically displayed on the PF's CDU during takeoff?

When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39The PF normally displays the takeoff reference page on the CDU. Display of the takeoff reference page allows the crew to have immediate access to V-speeds during takeoff in the event that V-speeds are inadvertently removed from the airspeed display. | Page: 3.4

9. What is the alternate approach for setting MCP altitude in departures and arrivals with closely spaced constraints?

When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39When approved by the operator, the following MCP altitude setting technique may be used during published instrument departures, arrivals, and approaches where altitude constraints are closely spaced to the extent that crew workload is adversely affected and unwanted level-offs are a concern: • for departures, set the highest of the closely-spaced constraints • for arrivals, initially set the lowest of the closely spaced altitude constraints or the FAF altitude, whichever is higher. | Page: 1.46

10. Why is the brake temperature monitoring system not useful for detecting immediate changes in temperature?

When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39The optional brake temperature monitoring system may be used for additional flight crew guidance in assessing brake energy absorption. This system indicates a stabilized value approximately fifteen minutes after brake energy absorption. Therefore, an immediate or reliable indication of tire or hydraulic fluid fire, wheel bearing problems, or wheel fracture is not available. The brake temperature monitor readings may vary between brakes during normal braking operations. | Page: 6.47

11. Should A/T and/or F/D be on or off during takeoff?

Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44Autothrottle and flight director use is recommended for all takeoffs. However, do not follow F/D commands until after liftoff. | Page: 3.5When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39

12. What is the VDP of a non-ILS approach?

Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39'For a non-ILS approach, the Visual Descent Point (VDP) is defined as the position on final approach from which a normal descent from the MDA(H) to the runway touchdown point may be initiated when suitable visual reference is established. If the airplane arrives at the VDP, a stabilized visual segment is much easier to achieve since little or no flight path adjustment is required to continue to a normal touchdown.VDPs are indicated on some non-ILS approach charts by a ''V'' symbol. The distance to the runway is shown below the ''V'' symbol. | Page: 5.71'When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44

13. How does immediate initiation of reverse thrust after landing affect the brake system?

When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Immediate initiation of reverse thrust at main gear touchdown and full reverse thrust allow the autobrake system to reduce brake pressure to the minimum level. Since the autobrake system senses deceleration and modulates brake pressure accordingly, the proper application of reverse thrust results in reduced braking for a large portion of the landing roll. The importance of establishing the desired reverse thrust level as soon as possible after touchdown cannot be overemphasized. This minimizes brake temperatures and tire and brake wear and reduces stopping distance on very slippery runways. The use of minimum reverse thrust as compared to maximum reverse thrust can double the brake energy requirements and result in brake temperatures much higher than normal. | Page: 6.44Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39

14. With airspeed increasing during climb, when should sequential flap retractions be initiated? What speed should be minimally maintained for flaps up maneuvering?

When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39Flaps should be retracted when airspeed reaches the maneuvering speed (number) for the existing flap position. For flaps up maneuvering, maintain at least 'UP' speed. | Page: 3.33

15. What is the appropriate brake technique during taxi?

Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Avoid prolonged brake application to control taxi speed as this causes high brake temperatures and increased wear of brakes. If taxi speed is too high, reduce speed with a steady brake application and then release the brakes to allow them to cool. Braking to approximately 10 knots and subsequent release of the brakes results in less heat build-up in the tires and brakes than when the brakes are constantly applied. | Page: 2.6Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44

16. During taxi, how are turns of 90 degrees or more made?

When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44Initiate the turn as the intersecting taxiway centerline (or intended exit point) approaches approximately the center of the number 3 window. Initially use approximately full nose wheel steering wheel displacement. Adjust the steering wheel input as the airplane turns to keep the nose wheels outside of the taxiway centerline, near the outside radius of the turn. Nearing turn completion, when the main gear are clear of the inside radius, gradually release the steering wheel input as the airplane lines up with the intersecting taxiway centerline or intended taxi path. | Page: 2.8

17. What air speed bugs are present on the speed tape during landing?

When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16VREF and VREF + 15 (VREF + 20 for airplanes with CDS Block Point 2004 and later) are displayed upon entry of landing flaps/speed in the FMC. The maneuvering speed for the current flap position and the next flap position are automatically displayed on the airspeed display. | Page: 1.23Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44

18. How is a delayed flap approach (for noise abatement) performed?

Intercept the glide slope with gear down and flaps 15 at flaps 15 speed. The thrust required to descend on the glide slope may be near idle. Approaching 1,000 feet AFE, select landing flaps, allow the speed to bleed off to the final approach speed, then adjust thrust to maintain it. Do the Landing checklist. | Page: 5.19Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16

19. During departures and arrivals, how are MCP altitudes normally set?

The following MCP altitude setting technique is normally used during published instrument departures, arrivals, and approaches when waypoints with altitude constraints are not closely spaced: • during climbs, maximum or hard altitude constraints should be set in the MCP. Minimum crossing altitudes need not be set in the MCP. The FMC alerts the crew if minimum altitude constraints will not be satisfied • during descent, set the MCP altitude to the next constraint or clearance altitude, whichever will be reached first • just prior to reaching the constraint, when compliance with the constraint is assured, and cleared to the next constraint, reset the MCP to the next constraint. | Page: 1.46When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39

20. What are the RVR values for low-visibility takeoffs with and without guidance systems and centerline lighting?

Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39With proper crew training and appropriate runway lighting, takeoffs with visibility as low as 500ft/150m RVR may be authorized (FAA). With takeoff guidance systems and centerline lighting that meets FAA or ICAO criteria for Category III operations, takeoffs with visibility as low as 300ft/75m RVR may be authorized. | Page: 3.20When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44

21. Which airspeed bugs are present on the speed tape during takeoff?

When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44When V1, VR and gross weight are entered into the FMC, airspeed bugs are automatically displayed at V1, VR and the minimum flap retraction speed for the next flap position. Command speed is set at V2 using the MCP. An airspeed bug is automatically set 15 knots above command speed. V2 + 15 provides 40° bank capability (25° + 15° overshoot) for all takeoff flaps. | Page: 1.23Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39

22. What are the two parts of the definition of V1?

• V1 means the maximum speed in the takeoff at which the pilot must take the first action (e.g., apply brakes, reduce thrust, deploy speedbrakes) to stop the airplane within the accelerate-stop distance and• V1 also means the minimum speed in the takeoff, following a failure of an engine at which the pilot can continue the takeoff and achieve the required height above the takeoff surface within the takeoff distance. | Page: 3.24When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44

23. In a Fail Operational airplane, an Autoland annunciation changes or system fault occurs above AH that requires higher weather minimums (reversion to LAND 2 or NO AUTOLAND). What should be done?

When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39For fail operational airplanes, if an autoland annunciation changes or system fault occurs above AH that requires higher weather minimums (reversion to LAND 2 or NO AUTOLAND), do not continue the approach below these higher minimums unless suitable visual reference with the runway environment is established. | Page: 5.18Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44

24. What is the normal status of the hydraulic system and nose wheel steering during pushback?

Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44Pushback or tow out is normally accomplished with all hydraulic systems pressurized and the nose wheel steering locked out. | Page: 2.2When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39

25. In a fail operational airplane, which Autoland approaches are authorized if one engine is inoperative?

With an engine inoperative, autoland operations are authorized for flaps 30 only. AFDS management and associated procedures are similar to those used during the normal ILS approach. If flaps 30 performance is not satisfactory, a flaps 15 engine inoperative landing is required. Autoland operations are not authorized with flaps 15. After LAND 3 or LAND 2 is annunciated, use of the autothrottle for an approach with an engine inoperative is recommended for authorized operators. | Page: 5.32Use of the autobrake system is recommend whenever the runway is limited, when using higher than normal approach speeds, landing on slippery runways, or landing in a crosswind. | Page: 6.44Factors that affect stopping distance include: height and speed over the threshold, glide slope angle, landing flare, lowering the nose to the runway, use of reverse thrust, speedbrakes, wheel brakes and surface conditions of the runway. Reverse thrust and speedbrake drag are most effective during the high speed portion of the landing. Deploy the speedbrake lever and activate reverse thrust with as little time delay as possible. | Page: 6.39When maneuvering to intercept the localizer, decelerate and extend flaps to 5. Attempt to be at flaps 5 and flaps 5 maneuvering speed before localizer capture. | Page: 5.16

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About | Explore | User Guide | Topics | Subjects | Doubt Solver | Career Aptitude Test | Answers | Free Tools | What Should We Know?
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