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FAA orders · airworthiness directive · historical

2019-12-18: Engine Air Intake System

FAA order 2019-12-18 is an airworthiness directive in force since July 5, 2019. The FAA's subject line: Engine Air Intake System. It names Robinson R44: about 1,944 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Robinson Helicopter Company
Models
R44 II
On this site
Robinson R44 1,944 registered

Dates and paperwork

In force since
July 5, 2019
Published
July 5, 2019 (signed June 25, 2019)
Docket
FAA-2019-0361
Replaced by
2020-18-08
Status
Historical
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is adopting a new airworthiness directive (AD) for Robinson Helicopter Company (Robinson) Model R44 II helicopters. This AD requires inspecting the engine air induction hose (hose) and replacing any hose that is not airworthy. This AD was prompted by multiple reports of separation between the outer and inner layers of the hoses. The FAA is issuing this AD to address the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (3,840 characters)
Adoption of the Amendment \n\n\n\tAccordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: \n\nPART 39--AIRWORTHINESS DIRECTIVES \n\n0 1. The authority citation for part 39 continues to read as follows: \n\n\n\tAuthority: 49 U.S.C. 106(g), 40113, 44701. \n\n\n\nSec. 39.13 (Amended) \n\n0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): \n\n2019-12-18 Robinson Helicopter Company: Amendment 39-19673; Docket No. FAA-2019-0361; Product Identifier 2019-SW-015-AD. \n\n(a) Effective Date \n\n\n\tThis AD is effective July 5, 2019. \n\n(b) Affected ADs \n\n\n\tNone. \n\n(c) Applicability \n\n\n\tThis AD applies to Robinson Helicopter Company Model R44 II helicopters certificated in any category. \n\n(d) Subject \n\n\n\tJoint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code: 7160, Engine Air Intake System. \n\n(e) Unsafe Condition \n\n\n\tThis AD was prompted by a report of separation between the outer and inner layers of a hose. This condition, if not addressed, could result in blockage of air flow to the engine, engine stoppage, and subsequent loss of control of the helicopter. The FAA is issuing this AD to prevent the unsafe condition on these helicopters. \n\n(f) Compliance \n\n\n\tComply with this AD within the compliance times specified, unless already done. \n\n(g) Required Actions \n\n\n\t(1) For helicopters with an engine air induction hose (hose) part number A785-31 installed after April 30, 2018 or helicopter serial numbers 14248 through 14268 and 14270 through 14286, within 10 hours time-in-service (TIS): \n\n((Page 32030)) \n\n\n\t(i) Inspect the inside of the hose for separation between the outer and inner layers, and flex the hose in all directions while listening for a crinkling sound, which is an indication of separation. \n\t(ii) If there is any separation or a crinkling sound, replace the hose before further flight. \n\t(iii) If there is no separation and no crinkling sound, replace the hose within 50 hours TIS. \n\t(2) After the effective date of this AD, do not install on any helicopter a hose part number A785-31 marked with code 1Q18. \n\n(h) Alternative Methods of Compliance (AMOCs) \n\n\n\t(1) The Manager, Los Angeles ACO Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the certification office, send it to the attention of the person identified in paragraph (i)(1) of this AD. Information may be emailed to: [email protected]. \n\t(2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. \n\n(i) Related Information \n\n\n\t(1) For more information about this AD, contact Roger Gretler, Aviation Safety Engineer, Los Angeles ACO Branch, Compliance & Airworthiness Division, FAA, 3960 Paramount Blvd., Lakewood, CA 90712; phone 562-627-5251; email [email protected]. \n\t(2) For information about AMOCs, contact [email protected]. \n\t(3) For copies of the service information referenced in this AD, contact: Robinson Helicopter Company, 2901 Airport Drive, Torrance, CA 90505; phone 310-539-0508; fax 310-539-5198; or at https://robinsonheli.com/robinson-r44-service-bulletins/. You may view this referenced service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177. \n\n(j) Material Incorporated by Reference \n\n\n\tNone.

Related safety bulletins advice on the same designs, not orders

2024-10-292024-05 · Engine/Transmission Coupling, Gearmotor Assembly
2022-11-212022-21 · EMERGENCY FLOTATION SECTION, Pop-Out Float Under-inflation.
2022-04-11AIR-22-08 · MAIN ROTOR DRIVE SYSTEM,TAIL ROTOR DRIVE SYSTEM
2022-03-03AIR-22-03 · Robinson Helicopter Company Model R22, R44, and R66 Helicopters; Emergency Locator Transmitter Retention
2021-08-24AIR-21-14 · Robinson R44 and R66 HeliSAS Autopilot/Garmin Primary Flight Display (PFD) Interface

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 30, 2026. Connections as data: /graph/directive/2019-12-18.json · aircraft systems.