90-23-08: Continuous Ignition System
FAA order 90-23-08 is an airworthiness directive in force since December 3, 1990. The FAA's subject line: Continuous Ignition System. It names Messerschmitt-Boelkow-Blohm BO-105: about 11 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
- Airbus Helicopters Deutschland GmbH
- Models
- BO-105C, BO-105S
- On this site
- Messerschmitt-Boelkow-Blohm BO-105 11 registered
Dates and paperwork
- In force since
- December 3, 1990
- Docket
- 89-ASW-68
- 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 (2,225 characters)
90-23-08 MESSERSCHMITT-BOLKOW-BLOHM (MBB): Amendment 39-6778. Docket No. 89-ASW-68.
Applicability: All MBB Model BO105C and BO105S series helicopters, certified in any category, that operate in snow conditions.
Compliance: Required as indicated, unless already accomplished.
To prevent engine flameout resulting from ingestion of layers of wet snow in engine inlets, accomplish the following:
(a) Install a continuous ignition system in accordance with MBB Service Bulletin, SB-BO 105-80-108, "Optional Equipment-Retrofit of Continuous Ignition System," dated May 11, 1990.
(b) Incorporate into the applicable Rotorcraft Flight Manual (RFM) the FAA- approved flight manual Revision No. 2/16, dated October 1, 1989, which includes the following paragraphs 2.8.2.4 and 2.8.2.5:
2.8.2.4 Snow Conditions
Operation in snow is prohibited, except when the Continuous Ignition System) OPT 19 is installed and switched on. Prior to takeoff, snow and ice must be removed, particularly from the following areas:
- cabin roof
- transmission cowling interior in front of engine air intakes
- transmission compartment interior
- engine inlet deflector shield.
NOTE: After engine operation in snow make an entry in the logbook. Maintenance action is required in accordance with the Allison Operation and Maintenance Manual.
2.8.2.5 Engine Inlet Deflector Shield
The engine inlet deflector shield must be installed at all times.
The procedures shall be done in accordance with MBB Service Bulletin SB-BO 105-80- 108, which incorporates the following pages: 1, 2, and 8, Rev. 1, dated May 11, 1990; 3-7 and 9, Original, dated June 12, 1989. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from MBB Helicopter Corporation, 900 Airport Road, P.O. Box 2345, West Chester, PA 19380. Copies may be inspected at the Office of the Assistant Chief Counsel, FAA, 4400 Blue Mound Road, Fort Worth, Texas, or at the Office of the Federal Register, 1100 L Street, NW., Room 8301, Washington, DC.
This amendment (39-6778, AD 90-23-08) becomes effective on December 3, 1990.
Related safety bulletins advice on the same designs, not orders
2008-08-27SW-08-42 · Emergency Float with Liferaft Kits (kits)
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/90-23-08.json · aircraft systems.
