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Monday, 10 November 2008

Significant Regulatory & Related Activity

 

28 October 2008               Federal Aviation Administration (FAA)

FR Doc E8-25476             Docket No. FAA-2006-26722

Security Related Considerations in the Design & Operation of Transport Category Airplanes

Final Rule

This rule marks the end stage of a January 2007 Notice of Proposed Rulemaking dealing with airliners of more than 60 passenger seats or a takeoff weight of more than 100,000 pounds, proposing that new airplanes be designed to limit the effects of an explosive or incendiary device by:

1. Providing means to protect the flight deck and the passenger compartment from smoke, fumes, and noxious gases.

2. Requiring that fire suppression systems for cargo compartments be designed to withstand certain impacts and loads.

3. Designating a ‘least risk bomb location’ where a bomb discovered in-flight could be placed, so if it were to explode, flight-critical systems and structures would be protected as much as possible.

4. Ensuring redundant airplane systems for continued flight and landing following an explosion, primarily through separation of redundant critical systems (a 5-foot separation was proposed).

5. Designing the cabin in such a way so that it is more difficult to conceal weapons and explosives.

Summary of the final rule: The rule specifies design standards to protect the flight deck from forcible intrusion by persons or from penetration by small arms fire or fragmentation devices. It also requires the design to provide means to limit the effects of detonation by (1) limiting entry of smoke, fumes, and noxious gases into the flight deck and/or the passenger cabin; (2) meeting specified standards for all components of fire suppression systems in cargo compartments; (3) establishing a ‘least risk bomb location’; (4) physically separating certain redundant airplane systems; and (5) providing interior features that make it easier to detect explosives or weapons by a simple search of the cabin.

The rule generated 31 comments from aircraft manufacturers, airline associations, pilots unions and security experts, among others. Among the objections were the following complaints:

From Boeing and the Air Transport Association (representing most airlines in the U.S.): They claimed the rule wasn’t properly coordinated and, in any event, should be deferred or withdrawn.

Several commentators recommended the proposed requirements should also apply to all-cargo airplanes. The FAA disagreed, saying screening of personnel who board these aircraft should be sufficient.

A number of commentators recommended that the proposed requirements be applied not only to newly-manufactured aircraft but also should be retrofitted onto existing models. The FAA rebuffed this suggestion, saying bluntly: “We have no plan to extend any of these requirements to the existing fleet or existing type designs.”

A security expert, Billie Vincent, President & CEO of Aerospace Services International, Inc., recommended that a system of covert closed-circuit television (CCTV) be installed to monitor the cockpit, the cabin and the exterior of the airplane, with the ability to tap into the imagery at a ground station.

Vincent wrote:

“The purpose of these recommendations is to create a situation where cockpit crews have full views of the passenger cabin and the exterior of the aircraft. The intent of these systems is to provide the cockpit crew with as much intelligence as possible about events in the interior and exterior of the aircraft without having to leave the cockpit …

“The purpose of the capability to tap into the CCTV system from the ground is to provide the crisis managers  and the U.S. Hostage Rescue Teams with data from inside a hijacked/hostage aircraft. Under the current situation the crisis managers and the Hostage Rescue Teams have to operate with a dearth of information on what is happening inside a hijacked airplane.”

The FAA claimed “there are numerous concerns (especially as to violations of privacy) associated with the use of such systems, and at this point the potential benefits of requiring video monitoring do not outweigh the concerns.” The argument the FAA made here was similar to the one the agency made in vetoing any rulemaking action on the National Transportation Safety Board’s recommendation for cockpit imagery recorders. And, as in the case of cockpit imagery recorders, the FAA has lost an opportunity to require CCTV on all future airliners.

Regarding separation of flight-critical systems, the FAA said:

“We considered the installation of systems near the fuselage contour, for example, in the crown of the airplane … In this area, a system could not be displaced beyond the contour of the fuselage, since the fuselage skin will not significantly deflect without failure. In those cases, the maximum displacement in the direction of the fuselage skin can be limited to that which would result in displacement outside the fuselage contour.”

The FAA claimed that the final rule passes the test of a cost versus benefits analysis:

“The cost of a fatal aircraft accident involving a terrorist bombing and hijacking can exceed one billion dollars. In addition to the direct costs of such an accident are associated costs of Congressional hearings, bankruptcy proceedings, and other litigation following an accident.”

Total costs for design, certification, and the added fuel burn associated with the extra weight are placed at $ 1.4 billion.

Total benefits in terms of resistance to terrorist attack and the “get home” ability of a bombed aircraft are placed at $ 2.7 billion.

Thus: $ 2.7/$ 1.4 billion yields a favorable cost-benefit ratio of almost 2:1.

Retrofitting the existing fleet of aircraft could well have pushed the total cost over $ 2.7 billion. In this case, a negative cost-benefit would have resulted and the final rule might not have been issued.

The rule is effective 28 November 2008. It does not apply to the Airbus A380 double-decker, as that airplane has been certificated and is now flying in revenue service. The rule may apply to Boeing’s new B787, as that airplane is still short of making its first flight.

(Comments on the NPRM may be found at www.regulation.gov; enter FAA-2006-26772 to get to the applicable entries in the docket.)

 

16 October 2008               FAA

FR Doc E8-24549             Docket No. FAA-2008-1096

AD 2008-21-09

Final Rule, request for comments, concerning Bombardier Challenger CL-600 jets in icing conditions

Supersedes an existing airworthiness directive (AD 2008-08-06) issued 14 April 2008. The earlier AD required revising the airplane flight manuals (AFMs) to include new cold weather operations limitations and procedures. That AD was considered “interim action” and this new directive (AD 2008-21-09) requires flight crew training regarding enhanced take-off procedures and winter operations.

Unsafe condition: This AD results from reports of uncommanded roll during take-off. This AD is issued to prevent loss of control on take-off resulting from even small amounts of frost, ice, snow, or slush on the wing leading edges or forward upper wing surfaces.

The new AD becomes effective 31 October 2008.

FAA’s justification and determination of the effective date: “We are rapidly approaching the ice/snow season and the pilot training regarding enhanced takeoff procedures and winter operations must be accomplished before the season begins. Because of our requirement to promote safe flight of civil aircraft and thus, the critical need to prevent uncommanded roll during take-off and the short compliance time involved with this action, this AD must be issued immediately.”

Comments on the new AD must be received by 17 November 2008.

Note: This action deals with model CL-600 airplanes which feature flaps but have a “hard” leading edge, that is, no slats. The absence of slats requires higher takeoff speeds. The “hard” leading edge is considered especially vulnerable to ice contamination. A stretch model, the CRJ-700, features a new wing with leading edge slats.

7 October 2008               FAA

FR Doc E8-23668           Docket No. FAA-2008-1065

Notice of Proposed Rulemaking (NPRM), concerning a proposed airworthiness directive for Boeing B727 airplanes

The action proposed results from the Special Federal Aviation Rule (SFAR 88) that mandated the manufacturers to review their fuel tank safety, identify gaps and propose fixes. SFAR 88 was published a few years ago, and more than 100 airworthiness directives (ADs) have been issued for all types of transport category aircraft as part of an effort to minimize ignition sources in fuel tanks. Recall that TWA flight 800, downed by an explosion of its center wing fuel tank (CWT) in 1996, was believed to have been caused by electrical arcing that led to a spark inside the fuel tank and the resulting explosion that killed all 230 aboard.

ADs are still dribbling out of the SFAR 88 design reviews, and this appears to be another, requiring ground fault interrupter (GFI) relays for the main fuel tanks.

As the FAA says “We are proposing this AD to prevent an electrical fault in the fuel pump system, which might cause a connector or end cap to burn through and a subsequent fire or explosion inside the fuel pump or wing spar area. We are proposing this AD to prevent uncommanded operation of the auxiliary fuel tank pumps, which can cause them to run dry. This condition will increase pump temperature and could supply an ignition source to fumes in the fuel tank, which can result in a fire or explosion.”

The B727 was built before 1992 and therefore is not covered by the FAA ruling of July 2008 that requires retrofit of a Flammability Reduction Means (FRM), which is generally understood to mean an inerting gas in the fuel tank. With inert nitrogen-enriched air in the void spaces of the fuel tank, even the presence of an electrical spark or other heat source will not ignite an explosion. The FRM obviates the “single point failure” of an errant ignition source by building in a means of negating the effect of heat sources in the fuel tank. (See Aviation Safety & Security Digest, ‘Significant Regulatory & Related Activity,’ archive, August 2008.)

This particular action hopes to eliminate a heat source, as the FAA has determined that FRM will not be required of those older aircraft. A previous SFAR 88 action regarding B727 fuel tanks and electrical conduits was not sufficient to prevent a fuel tank explosion that blew off the wing of a Transmile B727 freighter on the ground at Bangalore, India, in 2006. The National Transportation Safety Board (NTSB) recently removed fuel tank inerting from its “Most Wanted” list of safety improvements, but did not explain the justification for this action with hundreds of older jets exempted and the design of fuel tanks without FRM clearly being a violation of Section 25.1309 Code of Federal Regulations. (See Aviation Safety & Security Digest, ‘Most Wanted List Updated to Account for Reality,’ home page.)

Even with the action proposed by this AD, the B727 fleet runs the risk of a single point failure and another fuel tank explosion.

The FAA’s proposed action affects some 200 B727s at a total fleet cost of between $9 million to $18 million. The FAA allows 60 months (5 years) for GFI retrofit, which works out to an annual effort of some 40 airplanes.

One is prompted to ask why a compliance time of 5 years is allowed on an airplane with a recognized and allowed single point failure, on an airplane where previous SFAR 88 fixes have been ineffective (Transmile), and for a SAFETY FIX. As one commentator quipped, “Why not just say, ‘Time to implement change is WHENEVER THE OPERATOR GETS A CHANCE OR FEELS LIKE IT’?”

Comments due 21 November 2008.

 
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