Airworthiness Directive 2025-20-11

one-time
Official AD 2025-20-11 · FR doc 2025-19354 · 2025-10-02 · airframe

Airworthiness Directives; Textron Aviation Inc. Airplanes

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for certain Textron Aviation Inc. (Textron) Model B200GT, B200CGT, B300, and B300C airplanes. This AD was prompted by a report of rudder control pushrod failure during a production ground run, caused by sheared rivets off of a rudder control pushrod. This AD requires a visual inspection of the attaching rivets of the pilot and copilot rudder control pushrods for incorrect rivets and replacement if necessary. The FAA is issuing this AD to address the unsafe condition on these products.

Which aircraft AD 2025-20-11 applies to

MakesTextron Aviation Inc.
ModelsB200GT, B200CGT, B300, B300C, B200
Serial-conditional — narrows to serials BY-335–BY-335, BY-356–BY-356, BY-443–BY-443, BY-453–BY-453, BY-454–BY-454, BZ-4–BZ-9, FL-1173–FL-1175, FL-1177–FL-1177, FL-1181–FL-1181, FL-1184–FL-1186, FL-1189–FL-1189, FL-1193–FL-1193, FL-1197–FL-1202, FL-1210–FL-1210, FL-1211–FL-1211, FL-1213–FL-1213, FL-1218–FL-1218, FL-1220–FL-1222, FL-1225–FL-1225, FL-1228–FL-1230, FL-1232–FL-1232, FL-1233–FL-1233, FL-1240–FL-1242, FL-1244–FL-1244, FL-1245–FL-1245, FL-1249–FL-1251, FL-1253–FL-1253, FL-1257–FL-1259, FL-1262–FL-1262, FL-1265–FL-1265, FL-1266–FL-1266, FL-1269–FL-1269, FL-1271–FL-1271, FL-1275–FL-1275, FL-1276–FL-1276, FL-1277–FL-1277, FL-1280–FL-1280, FL-1284–FL-1284, FL-1286–FL-1286, FL-1287–FL-1287, FL-1290–FL-1290, FL-1291–FL-1291, FL-1293–FL-1293, FL-1296–FL-1296, FL-1305–FL-1305, FL-1310–FL-1310, FL-1315–FL-1317, FL-1319–FL-1319, FL-1320–FL-1320, FM-78–FM-86, FM-88–FM-88, FM-90–FM-92, FM-94–FM-94, FM-96–FM-107, FM-110–FM-110.

Serial ranges apply per model: Model B200GT S/Ns BY-335, BY-356, BY-443, BY-453, BY-454; Model B200CGT S/Ns BZ-4 through BZ-9; Model B300 S/Ns FL-1173 through FL-1320 (multiple non-contiguous ranges, see serial_ranges); Model B300C S/Ns FM-78 through FM-110 (multiple non-contiguous ranges, see serial_ranges).

Whether AD 2025-20-11 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2025-20-11 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

Look up a tail number →Read the full directive (Federal Register)

Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.