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NTSB Safety Recommendations A-10-62 through -86



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                   NTSB SAFETY RECOMMENDATION
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National Transportation Safety Board
Washington, DC 20594

May 21, 2010

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NTSB Safety Recommendation A-10-62 through -86

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The National Transportation Safety Board makes the following 
recommendations to the Federal Aviation Administration: 
Work with the military, manufacturers, and National 
Aeronautics and Space Administration to complete the 
development of a technology capable of informing pilots 
about the continuing operational status of an engine. (A-10-
62) 

Once the development of the engine technology has been 
completed, as asked for in Safety Recommendation A-10-62, 
require the implementation of the technology on transport-
category airplane engines equipped with full-authority 
digital engine controls. (A-10-63) 

Modify the 14 Code of Federal Regulations 33.76(c) small and 
medium flocking bird certification test standard to require 
that the test be conducted using the lowest expected fan 
speed, instead of 100-percent fan speed, for the minimum 
climb rate. (A-10-64) 

During the bird-ingestion rulemaking database (BRDB) working 
group's reevaluation of the current engine bird-ingestion 
certification regulations, specifically reevaluate the 14 
Code of Federal Regulations (CFR) 33.76(d) large flocking 
bird certification test standards to determine whether they 
should 1) apply to engines with an inlet area of less than 
3,875 square inches and 2) include a requirement for engine 
core ingestion. If the BRDB working group's reevaluation 
determines that such requirements are needed, incorporate 
them into 14 CFR 33.76(d) and require that newly 
certificated engines be designed and tested to these 
requirements. (A-10-65) 

Require manufacturers of turbine-powered aircraft to develop 
a checklist and procedure for a dual-engine failure 
occurring at a low altitude. (A-10-66) 

Once the development of the checklist and procedure for a 
dual-engine failure occurring at a low altitude has been 
completed, as asked for in Safety Recommendation A-10-66, 
require 14 Code of Federal Regulations Part 121, Part 135, 
and Part 91 Subpart K operators of turbine-powered aircraft 
to implement the checklist and procedure. (A-10-67) 

Develop and validate comprehensive guidelines for emergency 
and abnormal checklist design and development. The 
guidelines should consider the order of critical items in 
the checklist (for example, starting the auxiliary power 
unit), the use of opt outs or gates to minimize the risk of 
flight crewmembers becoming stuck in an inappropriate 
checklist or portion of a checklist, the length of the 
checklist, the level of detail in the checklist, the time 
needed to complete the checklist, and the mental workload of 
the flight crew. (A-10-68)

Require 14 Code of Federal Regulations Part 121, Part 135, 
and Part 91 Subpart K operators to include a dual-engine 
failure scenario occurring at a low altitude in initial and 
recurrent ground and simulator training designed to improve 
pilots? critical-thinking, task-shedding, decision-making, 
and workload-management skills. (A-10-69) 

Require 14 Code of Federal Regulations Part 121, Part 135, 
and Part 91 Subpart K operators to provide training and 
guidance to pilots that inform them about the visual 
illusions that can occur when landing on water and that 
include approach and touchdown techniques to use during a 
ditching, with and without engine power. (A-10-70) 

Work with the aviation industry to determine whether 
recommended practices and procedures need to be developed 
for pilots regarding forced landings without power both on 
water and land. (A-10-71) 

Require applicants for aircraft certification to demonstrate 
that their ditching parameters can be attained without 
engine power by pilots without the use of exceptional skill 
or strength. (A-10-72) 

Require Airbus operators to amend the ditching portion of 
the Engine Dual Failure checklist and any other applicable 
checklists to include a step to select the ground proximity 
warning system and terrain alerts to OFF during the final 
descent. (A-10-73) 

Require Airbus operators to expand the angle-of-attack-
protection envelope limitations ground-school training to 
inform pilots about alpha-protection mode features while in 
normal law that can affect the pitch response of the 
airplane. (A-10-74) 

Require all 14 Code of Federal Regulations Part 139-
certificated airports to conduct wildlife hazard assessments 
(WHA) to proactively assess the likelihood of wildlife 
strikes, and, if the WHA indicates the need for a wildlife 
hazard management plan (WHMP), require the airport to 
implement a WHMP into its airport certification manual. (A-
10-75) 

Work with the U.S. Department of Agriculture to develop and 
implement innovative technologies that can be installed on 
aircraft that would reduce the likelihood of a bird strike. 
(A-10-76) 
Require Airbus to redesign the frame 65 vertical beam on 
A318, A319, A320, and A321 series airplanes to lessen the 
likelihood that it will intrude into the cabin during a 
ditching or gear-up landing and Airbus operators to 
incorporate these changes on their airplanes. (A-10-77) 

Conduct research to determine the most beneficial passenger 
brace position in airplanes with nonbreakover seats 
installed. If the research deems it necessary, issue new 
guidance material on passenger brace positions. (A-10-78)

Require, on all new and in-service transport-category 
airplanes, that cabin safety equipment be stowed in 
locations that ensure that life rafts and/or slide/rafts 
remain accessible and that sufficient capacity is available 
for all occupants after a ditching. (A-10-79) 

Require quick-release girts and handholds on all evacuation 
slides and ramp/slide combinations. (A-10-80) 

Require 14 Code of Federal Regulations Part 121, Part 135, 
and Part 91 Subpart K operators to provide information about 
life lines, if the airplane is equipped with them, to 
passengers to ensure that the life lines can be quickly and 
effectively retrieved and used. (A-10-81) 

Require that aircraft operated by 14 Code of Federal 
Regulations Part 121, Part 135, and Part 91 Subpart K 
operators be equipped with flotation seat cushions and life 
vests for each occupant on all flights, regardless of the 
route. (A-10-82) 

Require 14 Code of Federal Regulations Part 121, Part 135, 
and Part 91 Subpart K operators to brief passengers on all 
flotation equipment installed on an airplane, including a 
full demonstration of correct life vest retrieval and 
donning procedures, before all flights, regardless of route. 
(A-10-83) 

Require modifications to life vest stowage compartments or 
stowage compartment locations to improve the ability of 
passengers to retrieve life vests for all occupants. (A-10-
84) 

Revise the life vest performance standards contained in 
Technical Standard Order-C13f to ensure that they result in 
a life vest that passengers can quickly and correctly don. 
(A-10-85) 

Conduct research on, and require 14 Code of Federal 
Regulations Part 121, Part 135, and Part 91 Subpart K 
operators to implement, creative and effective methods of 
overcoming passengers? inattention and providing them with 
safety information. (A-10-86)



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http://www.ntsb.gov/recs/letters/2010/A-10-062-086.pdf

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The complete recommendation letter is available on the Web 
at the URL indicated above.

The letter is in the Portable Document Format (PDF) and can 
be read using the Acrobat Reader 5.0 or later from Adobe 
(http://www.adobe.com/prodindex/acrobat/readstep.html). 
	
An archive of recommendation letters is available at 
http://www.ntsb.gov/recs/letters/letters.htm. 
Electronic versions of letters may or may not include 
enclosures; however, related publications, accident 
briefs, and aviation accident synopses may be found 
on the NTSB website.

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