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on the vertical stabilizer, even at speeds below the design maneuvering speed; and (3) explain that, on
some aircraft, as speed increases, the maximum available rudder deflection can be obtained with
comparatively light pedal forces and small pedal deflections. The FAA should also require revisions to
airplane and pilot operating manuals that reflect and reinforce this information. In addition, the FAA
should ensure that this training does not compromise the substance or effectiveness of existing training
regarding proper rudder use, such as during engine failure shortly after takeoff or during strong or
gusty crosswind takeoffs or landings. (A-02-01)
1.
Carefully review all existing and proposed guidance and training provided to pilots of
transport-category airplanes concerning special maneuvers intended to address unusual or emergency
situations and, if necessary, require modifications to ensure that flight crews are not trained to use the
rudder in a way that could result in dangerous combinations of sideslip angle and rudder position or
other flight parameters. (A-02-02)
2.
Require all manufacturers of transport-category airplanes to review and, if necessary, revise their
maintenance manual inspection criteria for severe turbulence and extreme in-flight maneuvers to
ensure that loads resulting from positive and negative vertical accelerations, as well as lateral
accelerations, are adequately addressed. (A-03-41)
3.
4. Require all manufacturers of transport-category airplanes to establish and validate maximum threshold
Executive Summary http://www.ntsb.gov/publictn/2004/AAR0404.htm
5 of 5 10/27/2004 8:39 AM
values for positive and negative vertical and lateral G accelerations beyond which direct manufacturer
oversight and intervention is required as a condition for returning the airplane to service. (A‑03-42)
Require all operators of airplanes that have experienced accelerations exceeding the threshold values
established as a result of Safety Recommendation A-03-42 (or that the operator has reason to believe
might have exceeded those thresholds), as determined from FDR and other available data, to notify the
FAA immediately of such high loading events and provide all related loads assessment and inspection
results. (A-03-43)
5.
Require manufacturers of transport-category airplanes to immediately notify the appropriate
certification authority of any event involving accelerations exceeding the threshold values (or that the
manufacturer has reason to believe might have exceeded those thresholds) necessitating the
intervention of the manufacturer, and provide all related loads assessment and inspection results.
(A-03-44)
6.
Require that within 2 years, all Airbus A300-600/A310 and Boeing 747-400 airplanes and any other
aircraft that may be identified as recording filtered data be retrofitted with a flight data recorder system
capable of recording values that meet the accuracy requirements through the full dynamic range of
each parameter at a frequency sufficient to determine a complete, accurate, and unambiguous time
history of parameter activity, with emphasis on capturing each parameter’s dynamic motion at the
maximum rate possible, including reversals of direction at the maximum rate possible. (A-03-50)
7.
Previously Issued Recommendations Classified in This Report:
Safety Recommendation A-96-120 (previously classified “Open—Acceptable Response”) is classified
“Open—Unacceptable Response.”
1.
U.S. Department
of Transportation
Federal Aviation Operations Specifications
Administration
TABLE OF CONTENTS
PART A - General
HQ CONTROL
DATE
EFFECTIVE
DATE
AMENDMENT
NUMBER
1 Issuance and Applicability 11/16/04 10/30/07 2
2 Definitions and Abbreviations 11/16/04 10/30/07 2
3 Ratings and Limitations 01/30/04 10/30/07 15
4 Summary of Special Authorizations and Limitations 09/23/98 10/30/07 4
5 Exemptions 02/20/98 (Not used)
7 Designated Persons 12/19/06 10/30/07 5
25 Electronic/Digital Recordkeeping System,
Electronic/Digital Signature, and Electronic Media
11/16/04 10/30/07 2
60 European Aviation Safety Authority Ratings for
Repair Stations Located Outside the United States
11/16/04 (Not used)
101 Additional Fixed Locations 11/16/04 (Not used)
449 Antidrug and Alcohol Misuse Prevention Program 01/22/04 10/30/07 2
Print Date: 11/12/2007 Certificate No.: I6XR049Y
AAR Aircraft Services Inc.
U.S. Department
of Transportation
Federal Aviation Operations Specifications
Administration
TABLE OF CONTENTS
PART D - Additional Maintenance Authorizations & Limitations
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