Source: https://www.federalregister.gov/documents/2001/07/27/01-18803/special-conditions-boeing-model-737-7bc-airplane-certification-of-cooktops
Timestamp: 2018-02-18 07:59:05
Document Index: 203449743

Matched Legal Cases: ['art 25', 'art 25', '§\u200921', 'art 34', 'art 36', '§\u200921', 'art 25', '§\u200921', '§\u200925', 'art 25']

Federal Register :: Special Conditions: Boeing Model 737-7BC Airplane; Certification of Cooktops
Special Conditions: Boeing Model 737-7BC Airplane; Certification of Cooktops
A Rule by the Federal Aviation Administration on 07/27/2001
The effective date of these special conditions is July 19, 2001. Comments must be received on or before September 10, 2001.
39085-39087 (3 pages)
Docket No. NM193
Special Conditions No. 25-183-SC
https://www.federalregister.gov/d/01-18803 https://www.federalregister.gov/d/01-18803
Start Preamble Start Printed Page 39085
These special conditions are issued for the Boeing Model 737-700 airplane modified by Piedmont Hawthorne-Associated Air Center. This modified airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. The modification incorporates the installation of an electrically heated surface, called a cooktop. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for addressing the potential hazards that may be introduced by cooktops. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Comments on these special conditions may be mailed in duplicate to: Federal Aviation Administration, Transport Airplane Directorate, Attention: Rules Docket (ANM-113), Docket No. NM193, 1601 Lind Avenue SW., Renton, Washington 98055-4056; or delivered in duplicate to the Transport Airplane Directorate at the above address. All comments must be marked: Docket No. NM193. Comments may be inspected in the Rules Docket weekdays, except Federal holidays, between 7:30 a.m. and 4 p.m.
Alan Sinclair, FAA, Airframe/Cabin Safety Branch, ANM-115, Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington 98055-4056; telephone (425) 227-2195; facsimile (425) 227-1149.
The FAA has determined that notice and opportunity for prior public comment hereon are impracticable because these procedures would significantly delay certification of the airplane and thus delivery of the affected aircraft. In addition, the substance of these special conditions has previously been subject to the public comment process with no substantive comments received. The FAA therefore finds that good cause exists for making these special conditions effective upon issuance.
Interested persons are invited to submit such written data, views, or arguments as they may desire. Communications should identify the rules docket number and be submitted in duplicate to the address specified above. The Administrator will consider all communications received on or before the closing date for comments. The special conditions described in this document may be changed in light of the comments received. All comments received will be available in the Rules Docket for examination by interested persons, both before and after the closing date for comments. A report summarizing each substantive public contact with FAA personnel concerning this rulemaking will be filed in the docket. Commenters wishing the FAA to acknowledge receipt of their comments submitted in response to these special conditions must include with those comments a self-addressed, stamped postcard on which the following statement is made: “Comments to Docket No. NM193.” The postcard will be date stamped and returned to the commenter.
On January 11, 2001, Piedmont Hawthorne—Associated Air Center, P.O. Box 540728, (8321 Lemmon Ave, Love Field), Dallas, Texas 75234, applied for a Supplemental Type Certificate (STC) to modify the Boeing Model 737-7BC airplane. The Model 737-7BC is one of the Boeing Business Jet (BBJ) variants of Model 737 airplanes. It is a large transport category airplane powered by two CFM 56 engines, with a maximum takeoff weight of 171,000 pounds. The modified 737-7BC airplane operates with a 2-pilot crew, up to 3 flight attendants, and can hold up to 18 passengers.
Under the provisions of 14 CFR 21.101, Piedmont Hawthorne—Associated Air Center must show that the Boeing Model 737-7BC airplane, as changed, continues to meet the applicable provisions of the regulations incorporated by reference in Type Certificate Data Sheet No. A16WE, or the applicable regulations in effect on the date of application for the change. The regulations incorporated by reference in the type certificate are commonly referred to as the “original type certification basis.” The regulations incorporated by reference in Type Certificate Data Sheet No. A16WE are part 25, as amended by Amendments 25-1 through 25-77, with reversions to earlier amendments, voluntary compliance with later amendments, special conditions, equivalent safety findings, and exemptions listed in the Type Certificate Data Sheet.
If the Administrator finds that the applicable airworthiness regulations (that is, part 25 as amended) do not contain adequate or appropriate safety standards for the Boeing Model 737-7BC airplane modified by Piedmont Hawthorne—Associated Air Center because of a novel or unusual design Start Printed Page 39086feature, special conditions are prescribed under the provisions of § 21.16.
In addition to the applicable airworthiness regulations and special conditions, this Boeing Model 737-7BC airplane must comply with the fuel vent and exhaust emission requirements of part 34 and the noise certification requirements of part 36.
Special conditions are initially applicable to the model for which they are issued. Should Piedmont Hawthorne-Associated Air Center apply at a later date for a supplemental type certificate to modify any other model included on the same type certificate to incorporate the same novel or unusual design feature, these special conditions would also apply to the other model under the provisions of § 21.101(a)(1).
As noted earlier, the modification of the Boeing Model 737-7BC airplane will include installation of a cooktop in the passenger cabin. Cooktops introduce high heat, smoke, and the possibility of fire into the passenger cabin environment. The current airworthiness standards of part 25 do not contain adequate or appropriate safety standards to protect the airplane and its occupants from these potential hazards. Accordingly, this system is considered to be a novel or unusual design feature.
Currently, ovens are the prevailing means of heating food on airplanes. Ovens are characterized by an enclosure that contains both the heat source and the food being heated. The hazards represented by ovens are thus inherently limited, and are well understood through years of service experience. Cooktops, on the other hand, are characterized by exposed heat sources and the presence of relatively unrestrained hot cookware and heated food, which may represent unprecedented hazards to both occupants and the airplane. Cooktops could have serious passenger and airplane safety implications if appropriate requirements are not established for their installation and use. These special conditions apply to cooktops with electrically-powered burners equipped with an automatic power shut off feature, which turn off the power to the cooktop whenever the cooktop cover is closed. This automatic shut off feature prevents the cooktop from being a hazard to the passengers and crew and from becoming a fire hazard when the cover is closed thus increasing the level of safety. Since the design proposed by Associated Air Center currently includes this power shut off feature it was not deemed necessary to include it in the design limitations, but it should be known that the automatic power shut off feature will be required for all future cooktop designs.
The use of an open flame cooktop (for example natural gas) is beyond the scope of these special conditions and would require separate rulemaking action. The requirements identified in these special conditions are in addition to those considerations identified in Advisory Circular (AC) 25-10, Guidance for Installation of Miscellaneous Non-required Electrical Equipment, and those in AC 25-17, Transport Airplane Cabin Interiors Crashworthiness Handbook. The intent of these special conditions is to provide a level of safety that is consistent with that on similar airplanes without cooktops.
As discussed above, these special conditions are applicable to the Boeing Model 737-7BC airplane modified by Piedmont Hawthorne-Associated Air Center. Should Piedmont Hawthorne-Associated Air Center apply at a later date for a supplemental type certificate to modify any other model included on the same type certificate to incorporate the same novel or unusual design feature, these special conditions would apply to that model as well under the provisions of § 21.101(a)(1).
This action affects only certain novel or unusual design features on the Boeing Model 737-7BC airplane modified by Piedmont Hawthorne-Associated Air Center. It is not a rule of general applicability and affects only the applicant who applied to the FAA for approval of these features on the airplane.
The substance of these special conditions has previously been subjected to the notice and comment period and has been derived without substantive change. It is unlikely that prior public comment would result in a significant change from the substance contained herein. For this reason, and because a delay would significantly affect the certification of the airplane, which is imminent, the FAA has determined that prior public notice and comment are unnecessary and impracticable, and good cause exists for adopting these special conditions upon issuance. The FAA is requesting comments to allow interested persons to submit views that may not have been submitted in response to the prior opportunity for comment described above.
Accordingly, pursuant to the authority delegated to me by the Administrator, the following special conditions are issued as part of the supplemental type certification basis for the Boeing Model 737-7BC airplane modified by Piedmont Hawthorne-Associated Air Center.
Two acceptable means of complying with this requirement are as follows: Start Printed Page 39087
Placarding must be installed that prohibits any burner from being powered when the cooktop is unattended (this would prohibit a single person from cooking on the cooktop and intermittently serving food to passengers while any burner is powered). In addition, a fire detector must be installed in the vicinity of the cooktop, which provides an audible warning in the passenger cabin; and a fire extinguisher of appropriate size and extinguishing agent must be installed in the immediate vicinity of the cooktop. A fire on or around the cooktop must not block access to the extinguisher. One of the fire extinguishers required by § 25.851 may be used to satisfy this requirement if the total complement of extinguishers can be evenly distributed throughout the cabin. If this is not possible, then the extinguisher in the galley area would be additional.
5. The surfaces of the galley surrounding the cooktop, which would be exposed to a fire on the cooktop surface or in cookware on the cooktop, must be constructed of materials that comply with the flammability requirements of part III of appendix F to part 25. This requirement is in addition to the flammability requirements typically required of the materials in these galley surfaces. During the selection of these materials, consideration must also be given to ensure that the flammability characteristics of the materials will not be adversely affected by the use of cleaning agents and utensils used to remove cooking stains.
Issued in Renton, Washington, on July 20, 2001.
[FR Doc. 01-18803 Filed 7-26-01; 8:45 am]