Atlas / SAIB / ACE-95-03
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SAIB ACE-95-03 —
What is a SAIB?
A Special Airworthiness Information Bulletin is an FAA-issued advisory — not mandatory like an AD, but worth knowing about. SAIBs typically flag service bulletins, manufacturer recommendations, or emerging issues that don't (yet) rise to AD level.
Bulletin text
Verbatim from the FAA-published PDF. 97 paragraphs · 451 words.
No. ACE-95-03 October 2, 1995
Published by: FAA, AFS-613, P.O. Box 26460, Oklahoma City, OK 73125 This is issued for informational purposes only and any recommendation for corrective action is not mandatory.
INTRODUCTION:
The purpose of this Special Airworthiness Information Bulletin is to advise operators of SOCATA Model airplanes of the need to review the service bulletins listed below.
BACKGROUND:
The Small Airplane Directorate, Aircraft Certification Service, of the Federal Aviation Administration (FAA) conducted a review of specified SOCATA airplane service bulletins. The purpose of the review was to evaluate each service bulletin to determine the continued airworthiness safety aspect. The options considered by the FAA included: mandated compliance by initiation of an FAA Airworthiness Directive (AD), various forms of notices, or no further action required.
RECOMMENDATIONS:
The service bulletins identified in this document were not considered appropriate for AD action at this time, however, the FAA strongly suggests that all operators of the specified SOCATA Model airplanes review their compliance of the service bulletins listed below.
Service Bulletin DATE
TITLE (Model Affected) No.
51
10/90 Carburetor Air Bleed on Engine Cowling; TB 9/10
59
2/91
Propeller Deicing; TB 20/21
150/2
6/91
Nose Landing Gear Wheel Axle; Rallye
48/3
12/91 Fuel Tanks TB 9/10/20/21
10-071
1/93
Rudder Balance Weight; TB 20/21
10-074
1/94
Exhaust System; TBM 200
10-073
1/94
Exhaust System; TB 10
2 ACE-95-03
Service Bulletin DATE
TITLE (Model Affected) No.
10-083
8/94
Vertical Fin Rib Attachment; TB 9/10/200
10-084
8/94
Wing Ribs, Fuel Tank Area; TB 9/10/20/21/200
70-010
11/91 Right Hand Aileron Air Outlet; TBM 700
70-013
8/92
Pitch Control Bellcrank; TBM 700
70-024
12/92 Oil Cooler System; TBM 700
70-026
2/93
Battery Overheating; TBM 700
70-022
9/93
Inverter "ESS BUS TIE"; TBM 700
70-035
2/94
Reinforcement Frames C18B1S & C19; TBM 700
70-034
2/94
Horizontal Stabilizer Insert; TBM 700
70-030
3/94
EFIS Display Configuration; TBM 700
70-053
7/94
Excessive Travel in Elevator Trim System; TBM 700
70-017
9/94
Fuel Low Pressure Switch Electrical Connection;
TBM 700
70-037
10/94 Windshield De-icing; TBM 700
70-052
11/94 Wing Tip Draining; TBM 700
70-060
12/94 Oil Cooler Interference Problem; TBM 700
70-058
1/95
Inspection of the Flap Rail; TBM 700
61
1/91
Fuel Tank Outlet Filter; TB20 & TB21
152
6/94
Attachment Fitting of Nose Landing Gear;
Rallye
10-072
1/94
Exhaust System; TB9 & TB10
10-064
6/92
Fuel Tank Air Vent System; TB9, TB10,
TB200
10-067
3/93
Fuel Tank Air Vent System; TB20 & TB21
ACE-95-03 3
The service bulletins can be obtained from:
Aerospatiale, General Aviation 2701 Forum Dr., 1-10 Grand Prairie, TX 75052
FOR FURTHER INFORMATION CONTACT: Mike Kiesov, Aerospace Engineer, FAA, Project Support Branch (ACE-112), Small Airplane Directorate, 1201 Walnut Suite 900, Kansas City, Missouri, 64106, telephone (816) 426-6934.
The FAA-published PDF is the authoritative source. Open on drs.faa.gov ↗