AD 2024-19-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | SOCATA | Various | Airworthiness Directives; DAHER (Type Certificate Previously Held by SOCATA) Airplanes |
| aircraft | Socata | Various | Airworthiness Directives; DAHER (Type Certificate Previously Held by SOCATA) Airplanes |
Unsafe Condition
chafing and cracking of the nose landing gear (NLG) wheel axle, which could lead to failure of the NLG with consequent damage to the airplane and/or injury to occupants.
Required Actions
repetitively inspecting the NLG wheel axle and, if chafing, cracking, or damage was found, installing the newly designed NLG wheel axle and attachment screws, which would terminate the actions specified in the AD. Additionally, repetitively replacing the NLG wheel axle attachment screws.
Compliance Time
Within 50 hours TIS after the effective date of this AD, or within 2,000 hours TIS total on the airplane, or within 2,000 hours TIS since the last time the attachment screws were replaced, whichever occurs later, and repetitively thereafter at intervals not to exceed 2,000 hours TIS after the last replacement.
Affected Aircraft
DAHER AEROSPACE Model MS 880 B, MS 880 B-D, MS 881, MS 883, MS 884, MS 885, MS 886, MS 887, MS 890 A, MS 890 B, MS 892 A.150, MS 892 B.150, MS 892 E.150, MS 892 E-D.150, MS 893 A, MS 893 B, MS 893 E, MS 893 E-D, MS 894 A, MS 894 E, RALLYE 100 S, RALLYE 100 S-D, RALLYE 100 ST, RALLYE 100 ST-D, RALLYE 110 ST, RALLYE 150 ST, RALLYE 150 ST-D, RALLYE 150 T, RALLYE 150 T-D, RALLYE 150 SV, RALLYE 150 SVS, RALLYE 180 T, RALLYE 180 TS, RALLYE 180 T-D, RALLYE 235 A, RALLYE 235 F, RALLYE 235 E, and RALLYE 235 E-D airplanes.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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