73-19-10: Elevator Control Horn
FAA order 73-19-10 is an airworthiness directive in force since August 29, 1979. The FAA's subject line: Elevator Control Horn. It names Ag-Cat Corporation G-164, Schweizer Aircraft Corp G-164: about 69 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: flight controls.
What it applies to as the FAA lists it
- Kind of product
- Aircraft
- Makes
- Allied Ag Cat Productions, Inc.
- Models
- G-164A, G-164B, G-164B-15T, G-164B-20T, G-164B-34T, G-164B (with 73 inch wing gap)
- On this site
- Ag-Cat Corporation G-164 5 registered
Schweizer Aircraft Corp G-164 64 registered
Dates and paperwork
- In force since
- August 29, 1979
- 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 (2,316 characters)
73-19-10 GRUMMAN AIRCRAFT: Amendment 39-1719 as amended by Amendments 39-1757 and 39-1828 is further amended by Amendment 39-3544. Applies to G-164A S/N's 1 through 1659A and G-164B S/N's 1B through 56B certificated in all categories and all G-164A and G-164B aircraft in which the elevator control horn assembly and torque tube end fittings have not been modified per Gulfstream American Service Note No. 23 or FAA-approved equivalent.
Compliance required as indicated.
1. Within the next 25 hours in service or two weeks, whichever occurs first, unless already accomplished within the last 75 hours in service, inspect the bolts attaching the Elevator Control Horn, P/N A 1841-3, to the left and right side elevator, P/N A1201-5A and A1201-4A respectively, for a standard (ref. AC 43.13-1 Chg. 7) torque rating and for corrosion and thereafter at intervals not to exceed 100 hours in service or 60 days, whichever occurs first.
2. If any looseness is detected, the bolts must be removed and inspected for wear.
3. Replace any worn or corroded bolts with bolts of the same part number or NAS 1304-12 bolts or an equivalent as approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region, except that the aircraft may be flown in accordance with FAR 21.197.
4. The bolts referenced in paragraph 3, must be replaced at intervals not exceeding 1000 hours in service or one year, whichever occurs first.
5. Upon submission of substantiating data by an owner or operator through an FAA Maintenance Inspector, the Chief, Engineering and Manufacturing Branch, FAA Eastern Region, may adjust the inspection intervals specified in this AD.
6. The repetitive inspection intervals required by paragraph 1 may be discontinued upon accomplishment of the modification in Grumman Gulfstream Service Note No. 23 dated 8/1/76, or an FAA-approved equivalent.
7. Any equivalent parts or alterations must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.
(Grumman American Aviation Corporation AgCat Service Bulletin No. 51 pertains to this subject.)
Amendment 39-1719 was effective September 21, 1973.
Amendment 39-1757 was effective December 20, 1973.
Amendment 39-1828 was effective May 6, 1974.
This Amendment 39-3544 is effective August 29, 1979.
Related safety bulletins advice on the same designs, not orders
2015-10-07CE-16-02 · Engine Mounts: Allied Ag Cat Airplanes with Honeywell TPE331 Conversions; engine mount cracking and...
2011-06-10CE-11-40 · Flight Controls: Rudder
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 5, 2026. Connections as data: /graph/directive/73-19-10.json · aircraft systems.
