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98-05-10: Aluminum Elbows

FAA order 98-05-10 is an airworthiness directive in force since March 18, 1998. The FAA's subject line: Aluminum Elbows. It names Robinson R44: about 1,939 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
On this site
Robinson R44 1,939 registered

Dates and paperwork

In force since
March 18, 1998
Published
March 3, 1998
Docket
97-SW-62-AD
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

This amendment adopts a new airworthiness directive (AD) that is applicable to Robinson Helicopter Company (Robinson) Model R44 helicopters. This action requires replacing the aluminum elbows that connect the oil cooler lines to the engine accessory case with steel elbows. This amendment is prompted by two reports of cracks that were discovered in aluminum elbows. The actions specified in this AD are intended to prevent failure of either the 45 degree or 90 degree aluminum elbows that connect the oil lines from the oil cooler to the engine accessory case, which would cause loss of engine oil, resulting in an engine failure and a subsequent forced landing.

The order itself the regulatory text, as published

Show the full text (3,180 characters)
98-05-10 ROBINSON HELICOPTER COMPANY: Amendment 39-10371. Docket No. 97-SW-62-AD. Applicability: Model R44 helicopters, serial numbers 0001 through 0330, certificated in any category. NOTE 1: This AD applies to each helicopter identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For helicopters that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must use the authority provided in paragraph (b) to request approval from the FAA. This approval may address either no action, if the current configuration eliminates the unsafe condition, or different actions necessary to address the unsafe condition described in this AD. Such a request should include an assessment of the effect of the changed configuration on the unsafe condition addressed by this AD. In no case does the presence of any modification, alteration, or repair remove any helicopter from the applicability of this AD. Compliance: Required within 50 hours time-in-service after the effective date of this AD, unless accomplished previously. To prevent failure of either the 45 degree or 90 degree aluminum elbows that connect the oil lines from the oil cooler to the engine accessory case, which would cause loss of engine oil, resulting in an engine failure and a subsequent forced landing, accomplish the following: (a) Remove any aluminum (blue-colored) AN823-8D (45 degree) or MS20822-8D (90 degree) elbows that connect the A723 oil cooler lines to the engine accessory case and replace them with airworthy MS20823-8 (45 degree) steel elbows or MS20822-8 (90 degree) steel elbows, as applicable. If the color is difficult to distinguish, use a magnet to determine if the elbow is aluminum or steel. Apply B270-6 thread sealant/lubricant to the replacement elbows' pipe threads. Torque the elbowsto 160 in-lbs. plus as much additional torque as is necessary to align for correct position with the oil line. NOTE 2: Robinson Helicopter Company R44 Service Bulletin SB-25, dated October 1, 1997, pertains to the subject of this AD and describes procedures for replacing both aluminum elbows with steel elbows. (b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Los Angeles Aircraft Certification Office. Operators shall submit their requests through an FAA Maintenance Inspector, who may concur or comment and then send it to the Manager, Los Angeles Aircraft Certification Office. NOTE 3: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Los Angeles Aircraft Certification Office. (c) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the FederalAviation Regulations (14 CFR 21.197 and 21.199) to operate the helicopter to a location where the requirements of this AD can be accomplished. (d) This amendment becomes effective on March 18, 1998.

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 28, 2026. Connections as data: /graph/directive/98-05-10.json · aircraft systems.