Source: https://www.law.cornell.edu/cfr/text/14/part-27/subpart-G?quicktabs_7=2
Timestamp: 2015-03-02 03:34:02
Document Index: 381759345

Matched Legal Cases: ['art 27', 'art 27', 'art 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', 'art 27', 'art 27', 'art 27', '§ 27']

14 CFR Part 27, Subpart G - Operating Limitations and Information | LII / Legal Information Institute
CFR › Title 14 › Chapter I › Subchapter C › Part 27 › Subpart G 14 CFR Part 27, Subpart G - Operating Limitations and Information
There are 3 Updates appearing in the Federal Register for 14 CFR 27. View below or at eCFR (GPOAccess)
§ 27.1501 — General.
§ 27.1503 — Airspeed limitations: general.
§ 27.1505 — Never-exceed speed.
§ 27.1509 — Rotor speed.
§ 27.1519 — Weight and center of gravity.
§ 27.1521 — Powerplant limitations.
§ 27.1523 — Minimum flight crew.
§ 27.1525 — Kinds of operations.
§ 27.1527 — Maximum operating altitude.
§ 27.1529 — Instructions for Continued Airworthiness.
§ 27.1541 — General.
§ 27.1543 — Instrument markings: general.
§ 27.1545 — Airspeed indicator.
§ 27.1547 — Magnetic direction indicator.
§ 27.1549 — Powerplant instruments.
§ 27.1551 — Oil quantity indicator.
§ 27.1553 — Fuel quantity indicator.
§ 27.1555 — Control markings.
§ 27.1557 — Miscellaneous markings and placards.
§ 27.1559 — Limitations placard.
§ 27.1561 — Safety equipment.
§ 27.1565 — Tail rotor.
Rotorcraft Flight Manual and Approved Manual Material
§ 27.1581 — General.
§ 27.1583 — Operating limitations.
§ 27.1585 — Operating procedures.
§ 27.1587 — Performance information.
§ 27.1589 — Loading information.
Title 14 published on 2014-01-01The following are only the Rules published in the Federal Register after the published date of Title 14.For a complete list of all Rules, Proposed Rules, and Notices view the Rulemaking tab.2014-08-19; vol. 79 # 160 - Tuesday, August 19, 201479 FR 48946 - Special Conditions: Robinson Model R66 Helicopter, § 27.1309, Installation of HeliSAS Autopilot and Stabilization Augmentation System (AP/SAS)
typeregulations.gov FR Doc.2014-19539 RIN Docket No.FAA-2014-0596 Special Conditions No.27-035-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is August 7, 2014. We must receive your comments on or before October 3, 2014. 14 CFR Part 27 SummaryThese special conditions are issued for the modification of the Robinson Helicopter Company Model R66 helicopter. This model helicopter will have a novel or unusual design feature after installation of the HeliSAS helicopter autopilot/stabilization augmentation system (AP/SAS) that has potential failure conditions with more severe adverse consequences than those envisioned by the existing applicable airworthiness regulations. These special conditions contain the added safety standards the Administrator considers necessary to ensure the failures and their effects are sufficiently analyzed and contained.
typeregulations.gov FR Doc.2014-19540 RIN Docket No.FAA-2014-0595 Special Conditions No.27-031-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is August 7, 2014. We must receive your comments on or before October 3, 2014. 14 CFR Part 27 SummaryThese special conditions are issued for the modification of the Airbus Helicopters Deutschland GmbH (Airbus Helicopters) Model EC135 series helicopters. These model helicopters will have a novel or unusual design feature after installation of the S-TEC Corporation (S-TEC) HeliSAS helicopter autopilot/stabilization augmentation system (AP/SAS) that has potential failure conditions with more severe adverse consequences than those envisioned by the existing applicable airworthiness regulations. These special conditions contain the added safety standards the Administrator considers necessary to ensure the failures and their effects are sufficiently analyzed and contained.
2014-08-14; vol. 79 # 157 - Thursday, August 14, 201479 FR 47553 - Special Conditions: Robinson Model R44 and R44 II Helicopters, Installation of HeliSAS Autopilot and Stabilization Augmentation System (AP/SAS)
typeregulations.gov FR Doc.2014-19211 RIN Docket No.FAA-2014-0560 Special Conditions No.27-033-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is August 4, 2014. We must receive your comments on or before September 29, 2014. 14 CFR Part 27 SummaryThese special conditions are issued for the modification of the Robinson Helicopter Company Model R44 and R44 II helicopters. These model helicopters will have a novel or unusual design feature after installation of the HeliSAS helicopter autopilot/stabilization augmentation system (AP/SAS) that has potential failure conditions with more severe adverse consequences than those envisioned by the existing applicable airworthiness regulations. These special conditions contain the added safety standards the Administrator considers necessary to ensure the failures and their effects are sufficiently analyzed and contained.
Title 14 published on 2014-01-01The following are ALL rules, proposed rules, and notices (chronologically) published in the Federal Register relating to 14 CFR 27 after this date.2014-08-19; vol. 79 # 160 - Tuesday, August 19, 201479 FR 48946 - Special Conditions: Robinson Model R66 Helicopter, § 27.1309, Installation of HeliSAS Autopilot and Stabilization Augmentation System (AP/SAS)