Federal Aviation Administration April 21, 2005 – Federal Register Recent Federal Regulation Documents

Airworthiness Directives; Airbus Model A320 Series Airplanes
Document Number: 05-7997
Type: Proposed Rule
Date: 2005-04-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A320 series airplanes. This proposed AD would require installing insulator and cable ties to the electrical cables of the S routes at the gaps in the raceway in the wing trailing edge and the wing tip and wing root areas. This proposed AD is prompted by the results of fuel system reviews conducted by the manufacturer. We are proposing this AD to prevent injection of high voltage current into the low voltage wiring that passes through the fuel tanks, which could result in a possible fuel tank explosion.
Special Conditions: Garmin International Inc.; Cessna Model 182T/T182T Airplane; Installation of Electronic Flight Instrument System and the Protection of the System From High Intensity Radiated Fields (HIRF)
Document Number: 05-7977
Type: Rule
Date: 2005-04-21
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for Garmin International Inc., 1200 E. 151st St., Olathe, KS 66062, for a Supplemental Type Certificate on the Cessna Model 182T/T182T airplanes. These airplanes, as modified by Garmin, will have a novel or unusual design feature(s) associated with the installation of a Garmin GFC-700 digital autopilot system. These special conditions address the protection of these systems from the effects of high intensity radiated field (HIRF) environments. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.
Advisory Circular: Change 1 to 23-21, Airworthiness Compliance Checklists Used To Substantiate Major Alterations for Small Airplanes
Document Number: 05-7976
Type: Notice
Date: 2005-04-21
Agency: Federal Aviation Administration, Department of Transportation
This notice announces the issuance of change 1 to Advisory Circular (AC) 23-21, Airworthiness Compliance Checklists Used to Substantiate Major Alterations for Small Airplanes. The most significant change is a revision in all locations to the signature required so the aircraft may be returned to service after major alteration. The Aviation Safety Inspector in the Flight Standards District Office must now sign instead of an Airframe and Powerplant mechanic. Other changes were minor.
Notice of Intent To Rule on Application To Impose a Passenger Facility Charge (PFC) at Fort Lauderdale International Airport, Fort Lauderdale, FL
Document Number: 05-7975
Type: Notice
Date: 2005-04-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to rule and invites public comment on the application to impose a PFC at Fort Lauderdale International Airport under the provisions of the Aviation Safety and Capacity Expansion Act of 1990 (Title IX of the Omnibus Budget Reconciliation Act of 1990) (Pub. L. 101-508) and part 158 of the Federal Aviation Regulations (14 CFR part 158).
Notice of Submission Deadline for International Slots for the Winter 2005/2006 Scheduling Season
Document Number: 05-7974
Type: Notice
Date: 2005-04-21
Agency: Federal Aviation Administration, Department of Transportation
On October 1, 1999, the FAA amended the regulations governing takeoff and landing slots and slot allocation procedures at certain High Density Traffic Airports as a result of the ``Open Transborder'' Agreement between the Government of the United States and the Government of Canada. One element of this final rule established that the deadline for submission of requests for international slots will be published in a Federal Register notice for each scheduling season. The purpose of the amendment is for the FAA deadline for international slots requests to coincide with the International Air Transport Association deadline for submission of international requests. In accordance with this amendment, the FAA announces in this notice that the deadline for submitting requests for international slots at John F. Kennedy International Airport (JFK) for allocation under 14 CFR 93.217 is May 12, 2005. Additionally, the FAA has designated Chicago's O'Hare International Airport (O'Hare) as a Level 2, Schedules Facilitated Airport under the IATA Guidelines. As such, the FAA requests carriers intening to conduct international service to O'Hare submit their intended schedules following the same procedures used for submitting requests for slots at JFK.
Notice of Intent To Rule on Application 05-05-C-00-SGF To Impose and Use the Revenue From a Passenger Facility Charge (PFC) at Springfield-Branson Regional Airport, Springfield, MO
Document Number: 05-7973
Type: Notice
Date: 2005-04-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to rule and invites public comment on the application to impose and use the revenue from a PFC at Springfield- Branson Regional Airport under the provisions of the Aviation Safety and Capacity Expansion Act of 1990 (Title IX of the Omnibus Budget Reconciliation Act of 1990) (Pub. L. 101-508) and part 158 of the Federal Aviation Regulations (14 CFR part 158).
Notice of Intent To Rule on Application 05-05-C-00-LAS To Impose and Impose and Use Passenger Facility Charge (PFC) at McCarran International Airport, and Use the PFC Revenue at McCarran International, Henderson Executive, and North Las Vegas Airports, Las Vegas, NV
Document Number: 05-7972
Type: Notice
Date: 2005-04-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to rule and invites public comment on the application to impose and impose and use a PFC at McCarran International Airport, and use the revenue of a PFC at McCarran International Airport, Henderson Executive Airport, and North Las Vegas Airport under the provisions of the Aviation Safety and Capacity Expansion Act of 1990 (Title IX of the Omnibus Budget Reconciliation Act of 1990) (Pub. L. 101-508) and part 158 of the Federal Aviation Regulations (14 CFR part 158).
Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG-800B Sailplanes
Document Number: 05-7790
Type: Rule
Date: 2005-04-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA adopts a new airworthiness directive (AD) for all Glaser-Dirks Flugzeugbau GmbH (DG Flugzeugbau) Model DG-800B sailplanes equipped with a SOLO 2625 engine or a Mid-West AE 50T engine. This AD requires you to modify the coolant pump and fuel pump electrical circuits, remove the non-resettable digital engine indicator (DEI) circuit breaker (4-ampere) and replace with a resettable 5-ampere circuit breaker, secure (for sailplanes with a SOLO 2625 engine) the choke butterfly valve axis, install edge protection at the sharp edges of the resettable 5-ampere DEI circuit breaker, and incorporate changes in the FAA-approved sailplane flight manual. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to prevent electrical failure of the fuel and coolant pumps if a non-resettable circuit breaker trips. This could result in power loss with the inability to restart the fuel pump during a critical phase of flight (for example, takeoff under own power).
Airworthiness Directives; CENTRAIR 101 Series Gliders
Document Number: 05-7784
Type: Rule
Date: 2005-04-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA adopts a new airworthiness directive (AD) for certain CENTRAIR 101 series gliders. This AD requires you to replace non- strengthened rudder pedals with reinforced rudder pedals. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. We are issuing this AD to replace the non-strengthened rudder pedals and to prevent failure of the rudder controls. This failure could lead to loss of directional control of the glider.
Airworthiness Directives; McDonnell Douglas Model DC-8-33 and -43 Airplanes; Model DC-8F-54 and DC-8F-55 Airplanes; and Model DC-8-50, -60, -60F, -70, and -70F Series Airplanes
Document Number: 05-7684
Type: Rule
Date: 2005-04-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to certain McDonnell Douglas series airplanes. That AD currently requires repetitive inspections of the electrical connectors of the explosive cartridge wiring of the engine fire extinguisher containers to verify if the identification number labels are installed and legible; repetitive electrical tests of all explosive cartridge wiring of the engine fire extinguisher containers to verify proper installation and function; and corrective actions if necessary. This new AD requires an inspection of the emergency shut off wire assembly; installation of lanyards on the electrical connectors for the engine fire extinguishing agent containers and for the auxiliary power unit fire extinguishing agent containers if applicable; and related investigative/corrective actions, as applicable. This AD is prompted by reports of cross-wired electrical connectors of the engine fire extinguishing agent containers. We are issuing this AD to detect and correct cross-wired electrical connectors of the fire extinguishing system, which could release fire extinguishing agent into the incorrect engine nacelle in the event of an engine fire.
Airworthiness Directives; Pilatus Aircraft Limited Models B4-PC11, B4-PC11A, and B4-PC11AF Sailplanes
Document Number: 05-7563
Type: Rule
Date: 2005-04-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA adopts a new airworthiness directive (AD) for all Pilatus Aircraft Limited (Pilatus) Models B4-PC11, B4-PC11A, and B4- PC11AF sailplanes. This AD requires you to repetitively inspect the control-column support for cracks and, if any cracks are found, replace the control-column support with a new support. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. We are issuing this AD to detect and correct cracks in the control-column support, which could result in failure of the support. This failure could lead to loss of the primary flight control system.
This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.