[Federal Register Volume 65, Number 10 (Friday, January 14, 2000)]
[Rules and Regulations]
[Pages 2295-2296]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 00-1056]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Parts 121, 125
[Docket No. FAA-1999-6140; Amendment Nos. 121-271 and 125-32]
RIN 2120-AG88
Revisions to Digital Flight Data Recorder Requirements for Airbus
Airplanes; Correction
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final Rule; correction.
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SUMMARY: The FAA published a final rule in the Federal Register on
August 24, 1999, (64 FR 46117). The rule amended the flight data
recorder regulations by adding language to allow certain Airbus
airplanes to record certain data parameters using resolution and
sampling requirements that differed slightly from the regulation. This
document makes certain corrections to Appendix E to Part 125, Airplane
Flight Recorder Specifications.
EFFECTIVE DATE: August 17, 1999.
FOR FURTHER INFORMATION CONTACT: Gary E. Davis, Air Carrier Operations
Branch (AFS-201), Flight Standards Service, Federal Aviation
Administration, 800 Independence Avenue, SW., Washington, DC 20591,
telephone (202) 267-8166.
SUPPLEMENTARY INFORMATION: On August 24, 1999, the FAA published an
amendment to the flight data recorder requirements of 14 CFR Parts 121
and 125 (64 FR 46117). In the amendment to Appendix E to Part 125,
Airplane Flight Recorder Specifications, one parameter listing was
inadvertently omitted. This action corrects that omission.
Correction
In FR Doc. 99-21783, published on August 24, 1999 (64 FR 46117),
make the following correction:
On page 46122, third column, in Appendix E to Part 125, Airplane
Flight Recorder Specifications, insert parameter 21, in numerical
order, to read as follows:
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Appendix E to Part 125--Airplane Flight Recorder Specifications
The recorded values must meet the designated range, resolution, and
accuracy requirements during dynamic and static conditions. All data
recorded must be correlated in time to within one second.
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Accuracy Seconds per
Parameters Range (sensor sampling Resolution Remarks
input) interval
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*
21. Leading Edge Flap or Cockpit Control
Selection \11\................................
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*
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[[Page 2296]]
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Issued in Washington, DC on January 12, 2000.
Donald P. Byrne,
Assistant Chief Counsel, Regulations Division.
[FR Doc. 00-1056 Filed 1-13-00; 8:45 am]
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