Quantcast Takeoff Path - One Engine Inoperative.

Share on Google+Share on FacebookShare on LinkedInShare on TwitterShare on DiggShare on Stumble Upon
Custom Search
 
  
 
TM 1-1510-224-10 setting.      The   accelerate-go   distance   (flaps   up)   would exceed the available runway length, so a flaps-approach takeoff must be calculated if it is desired to allow for the accelerate-go    distance    (which    is    not    a    regulatory requirement, but a recommended practice). i. Takeoff Path - One Engine Inoperative. Graphs  are  provided  to  estimate  the  horizontal  distance required  to  reach  a  height  of  1500  feet,  or  the  minimum climb  gradient  required  to  clear  an  obstacle  along  the take-off flight path.  If clearance of obstacles beyond the runway   is   required,   these   results   may   restrict   takeoff weight accordingly. The  takeoff  distance  extends  from  brake  release  to reference zero, which is the point at which the aircraft is 50  feet  above  the  runway.    The  net  takeoff  flight  path begins at liftoff and consists of the following segments: 1. The first segment climb extends from liftoff to    the    point    where    the    landing    gear completes     the     retraction     cycle.          The airspeed is maintained at V2. 2. The  second  segment  climb  begins  at  the end  of  the  first  segment  and  extends  to 500  feet  above  the  runway.    The  airspeed during the second segment is V2. 3. The acceleration and flap retraction segment  consists  of  an  acceleration  from V2  to  VENR  at  a  constant  height  of  500 feet.      If   a   flaps-   approach   takeoff   was made, begin flap retraction at VENR. 4. The third segment climb begins when one- engine-inoperative climb speed is reached and  flaps  are  fully  retracted  at  500  feet, and    extends    to    1500    feet    above    the runway.  Air-speed is maintained at VENR during this segment. j. Takeoff    Path    Profile    (Flaps    Approach,    One Engine  Inoperative).    The  following  examples  illustrate the use of the flaps-approach takeoff path graphs.  Enter the  graphs  at  15C   FAT,   3499   feet   pressure   altitude, 16,000   pounds   takeoff   weight,   1.9%   downhill   runway gradient, and a 10-knot headwind component. (1) Example 1 - close-in obstacle clearance: given: Obstacle  Height  Above  Aircraft  at  Brake  Release      88 feet Obstacle Distance from Brake Release          16,294 feet Figure 7A-1.  Takeoff Path Profile - One Engine Inoperative 7A-12

Aviation News
DOT Celebrates 25th Anniversary of ADA
A look at our recent past and a peek into...
faa.gov
Four Corners of the Country
July 30- The July/August 2015 issue of FAA Safety Briefing...
faa.gov
UH-X Order Could Boost 412 Commercial Sales
Japan’s order for 150 military versions of Bell Helicopter’s 412EPI...
aviationtoday.com
Australian Air Force Acquires First Boeing Growler
Amazon’s rendering of a segregated UAS airspace. Photo: Amazon [Avionics...
aviationtoday.com
Northrop Grumman CEO Looks to UAS to Grow Revenues
[Avionics Today 07-29-2015] Northrop Grumman Chief Executive Officer Wesley Bush...
aviationtoday.com
Engility Wins Contract to Support US Air Force GPS
[Avionics Today 07-28-2015] The U.S. Air Force has awarded TASC,...
aviationtoday.com
US Navy Awards Harris Corporation $29 Million Avionics Contract
F/A 18 Super Hornet. Photo: Boeing [Avionics Today 07-28-2015] The...
aviationtoday.com
First Bell 525 Delivery Slated for 2017
The 525 Relentless won’t be delivered to its first operators...
aviationtoday.com
Australian Military Training System Approved for Airbus Helicopters H135
Airbus Helicopters has achieved Factory Acceptance of HATS01, the first...
aviationtoday.com
Airbus Helicopters H135 Receives Factory Acceptance for HATS
Airbus Helicopters has achieved Factory Acceptance of HATS01, the first...
aviationtoday.com
Rockwell Collins Sees Softening Aftermarket Amid Rising Connectivity
Rockwell Collins connectivity segment looks to offset other market softness....
aviationtoday.com
Harris and CPqD to Monitor CNS Systems for Brazilian Air Force ATC
[Avionics Today 07-27-2015] Brazilian Air Force Air Traffic Control (ATC)...
aviationtoday.com
Harris Exec Outlines Electronic Warfare Strategy
Andy Dunn, vice president of business development at Harris. Photo:...
aviationtoday.com
Northrop Grumman Lays Out Fifth Generation C4ISR Framework
[Avionics Today 07-24-2015] Northrop Grumman Corporation has set out a...
aviationtoday.com
New Technologies to Boost Future Military HUD Sales
[Avionics Today 07-24-2015] A new Technavio report on the Head-Up...
aviationtoday.com
Rockwell Collins to Upgrade Communications for E-4B
E-4B aircraft. Photo: Boeing [Avionics Today 07-23-2015] Boeing has selected...
aviationtoday.com
UTC CEO Speaks to ‘Market Softness’ Amid Sikorsky Sale
United Technologies Corporation CEO Gregory Hayes. Photo: UTC [Avionics Today...
aviationtoday.com
Boeing Shows Off Global Xpress for Military Networks
[Avionics Today 07-22-2015] Boeing is completing the first tests of...
aviationtoday.com
Sikorsky Sale vs. Spinoff? Simple Math
The decision to sell Sikorsky Aircraft rather than spin it...
aviationtoday.com
UTC Releases Disappointing Second Quarter Profits
Photo: UTC [Avionics Today 07-21-2015] Following the company’s announcement to...
aviationtoday.com

 


Privacy Statement - Copyright Information. - Contact Us

Integrated Publishing, Inc.
9438 US Hwy 19N #311 Port Richey, FL 34668

Phone For Parts Inquiries: (727) 755-3260
Google +