SPECIAL AIRWORTHINESS INFORMATION BULLETIN
Aircraft Certification Service
Washington, DC
U.S. Department of Transportation
Federal Aviation Administration
AIR-21-19 R1

March 14, 2022

This is information only. Recommendations aren’t mandatory.

Introduction

This Special Airworthiness Information Bulletin (SAIB) alerts owners, operators, and maintenance personnel of an airworthiness concern on MD Helicopters Inc. (MDHI) Model 369D, 369E, 369F, 369FF, 500N, and 600N helicopters with Colorado Helicopters, Inc. Supplemental Type Certificate (STC) SH5230NM Side Pull Hook Assembly installed. This is a revision to AIR-21-19 SAIB.

At this time, the airworthiness concern is not an unsafe condition warranting an airworthiness directive (AD) action under Title 14 of the Code of Federal Regulations (14 CFR) part 39.

Background

The Federal Aviation Administration (FAA) became aware that the breakaway pin installed in the breakaway swivel of the side pull hook link installation could be replaced with the wrong pin or a bolt prior to operations. The side pull hook link includes a breakaway swivel, a calibrated breakaway pin, and a retaining ring (See Figure 1 below). The side pull hook link installation is certified for a maximum pull load of 1,900 pounds and is safeguarded by the calibrated breakaway pin connecting the two pieces of the swivel. If the side pull hook link installation is overloaded, the breakaway pin is designed to shear and allow the load line to fall away without upsetting the helicopter. Installation of other than the approved breakaway pin could result in helicopter damage, upset, and even loss of control if the maximum pull load of 1,900 pounds is exceeded. The swivel is installed in between the hook link assembly, which attaches to the helicopter, and the line attached to the load. The pin is 1.15 inch ±.003 inch long with one end painted GREEN (not BLUE) and fills the hole through the swivel. The pin has two smaller diameters allowing it to break in shear at a specified load. It does NOT contain any threaded features and does not protrude from the swivel. The pin is held in place with a steel retaining ring installed in a groove around the circumference of the swivel. If further verification is necessary, then FAA certified maintenance personnel should disassemble the side pull hook link to conduct a visual inspection. This inspection is a visual verification of the shear diameters and lack of threads, and is accomplished by removal of the steel ring and pin. Additionally, you may measure the shear diameter (the smallest diameter of the pin in two places) to be .149 inch +.000/-.003 inches, not larger.

Consequently, on November 29, 2021, the FAA issued SAIB AIR-21-19, which included recommendations to address this concern. After the SAIB was issued, the FAA became aware the SAIB recommendations contained errors. The SAIB is revised accordingly.

Recommendations

The FAA recommends all owners/operators of the affected aircraft listed in the introduction of this SAIB conduct a one-time inspection ensuring FAA certified maintenance personnel remove the retaining ring, breakaway pin, and inspect the breakaway pin for the correct color (GREEN), appearance, and shear diameter prior to the next side pull operation. If the pin matches the description above and has no signs of damage, reinsert the pin and reinstall the retaining ring prior to flight. If the pin does not match the description above, or shows signs of damage, it should be replaced with pin part number 91106-018 prior to the next side pull operation.

Additionally, the FAA continues to recommend all pilots of the affected aircraft listed in the introduction of this SAIB visually inspect the breakaway pin, per Figure 2, immediately before any side pull operations. If the pin is not secured by the retaining ring, or is not green on one end, or does not fill the hole through the swivel, or shows signs of damage, it should be replaced with pin part number 91106-018 prior to the next side pull operation.

For Further Information Contact

Ronnea Derby, Aerospace Engineer, FAA, Denver ACO Branch, 26805 E 68th Ave., Denver, CO 80249, United States; phone: (303) 342-1093; fax: (303) 342-1088; e-mail: Ronnea.L.Derby@faa.gov.

ILLUSTRATION (Figure 1)

ILLUSTRATION (Figure 2)