SAIB 2024-05
Current · Issued 10/29/2024 · Robinson Helicopter Company R44 | R44 II · FAA DRS
Engine/Transmission Coupling, Gearmotor Assembly Open on drs.faa.gov ↗
The FAA-published PDF is the authoritative source.
Bulletin text · verbatim from the FAA PDF · 13 paragraphs · 339 words
FAA Aviation Safety SPECIAL AIRWORTHINESS INFORMATION BULLETIN SUBJ: Engine/Transmission Coupling, Gearmotor Assembly SAIB: 2024-05 Date: 10/29/2024 This is information only. Recommendations aren’t mandatory.
Introduction
This Special Airworthiness Information Bulletin (SAIB) alerts all owners, operators, maintenance technicians, and inspectors of an airworthiness concern on Robinson Helicopter Company (RHC) Model R44 and R44 II helicopters due to potential loosening of the gearmotor assembly (gearmotor), part number (P/N) D276-1 or D276-3, on belt-tension actuators. This concern also applies to C051-1 and C051-2, Revision AC and prior, belt-tension actuator assemblies sold as spares that include gearmotor P/N D276-1 or D276-3.
At this time, the airworthiness concern is not an unsafe condition that would warrant airworthiness directive (AD) action under Title 14 of the Code of Federal Regulations (14 CFR) part 39.
Background
The FAA has received reports of loose P/N D276-1 and D276-3 gearmotors on RHC Model R44- series helicopters from both domestic and international operators. Investigation has determined the cause to be related to poor dimensional control of certain internal countersunk head screws and the potential absence of thread locking adhesive in a population of gearmotors that left the manufacturer.
RHC updated the R44-series maintenance manual in September 2023 to add a gearmotor assembly torque stripe verification to the 100-hour / annual inspection procedures. Additionally, RHC released R44 Service Bulletin SB-115, dated October 27, 2023 (RHC SB-115); this service bulletin specifies a one-time verification of gearmotor security and application of a torque stripe for future visual inspections.
Recommendations
The FAA recommends the following the actions: (1) Inspect the gearmotor assembly for looseness, replace if necessary, and apply the torque stripe for future visual inspections, in accordance with the SB. (2) At every 100-hour/Annual Inspection, follow the Gear Motor Assembly Torque Stripe inspection procedure within RHC R44 MM, dated September 2023.
For Further Information Contact
Eric Moreland, Aerospace Engineer, FAA, 3960 Paramount Boulevard, Lakewood, CA 90712; phone: (562) 627-5364; email: [email protected].
For Related Service Information Contact
Robinson Helicopter Company, Technical Support Department, 2901 Airport Drive, Torrance, CA 90505; phone: (310) 539-0508; website: robinsonheli.com.