80-24-04: Placard -Front Seat Occupancy
FAA order 80-24-04 is an airworthiness directive in force since December 4, 1980. The FAA's subject line: Placard -Front Seat Occupancy. It names Hughes 369 500 series helicopters, Md Helicopters Inc 369: about 231 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: cabin, seats and restraints.
What it applies to as the FAA lists it
- Kind of product
- Aircraft
- Makes
- MD Helicopters, Inc.
- Models
- 369, 369A, 369D, 369H, 369HE, 369HM, 369HS
- On this site
- Hughes 369 500 series helicopters 123 registered
Md Helicopters Inc 369 108 registered
Dates and paperwork
- In force since
- December 4, 1980
- Docket
- Unknown
- Status
- Current
- The FAA's document
- Read the order on the FAA's site
The order itself the regulatory text, as published
Show the full text (1,329 characters)
80-24-04 HUGHES HELICOPTERS: Amendment 39-3979. Applies to Model 369 Series Helicopters, certified in all categories, equipped with Automatic Engine Reignition System.
Compliance is required as indicated unless already accomplished.
To prevent the possibility of the middle front seat occupant accidentally deactivating the Automatic Engine Reignition System and also from blocking the crew's view of the automatic reignition "ARMED" and "RE-IGN" advisory lights, accomplish the following:
(a) Within thirty (30) consecutive calendar days or prior to flight in falling and/or blowing snow, whichever comes first, after the effective date of this AD, install a placard in close proximity to the Automatic Engine Reignition Arming switch and in plain view of the pilot which states "Middle front seat is not to be occupied during flight in falling and/or blowing snow" or equivalent words.
(b) Special flight permits may be issued in accordance with FAR 21.197 and .199 to operate aircraft to a base for the accomplishment of modification required this AD.
(c) Alternative inspections, modifications or other actions which provide an equivalent level of safety may be used when approved by the Chief, Engineering and Manufacturing Branch, FAA Western Region.
This amendment becomes effective December 4, 1980.
Related safety bulletins advice on the same designs, not orders
2021-11-29AIR-21-19 · AERIAL TOW EQUIPMENT, Side Pull Hook
2021-11-29AIR-21-19R1 · AERIAL TOW EQUIPMENT, Side Pull Hook
2012-10-03SW-12-45 · Garmin Model 400W/500W Series GPS-WAAS Navigation System
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 November 6, 2026. Connections as data: /graph/directive/80-24-04.json · aircraft systems.
