AIRWORTHINESS
LIMITATIONS
LIST OF EFFECTIVE PAGES
CHAPTER PAGE DATE
04-LEP 1 Apr. 95
2 Aug. 94
04-TC 1 Apr. 95
2 Aug. 94
04-00-00 (CA) 1 Apr. 95
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4 Apr. 95
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TABLE OF CONTENTS
SUBJECT CHAPTER PAGE VALIDITY
AIRWORTHINESS LIMITATIONS 04-00-00 1 - 9999
General (CA) 3
Structure service life 3
Engine service life 3
Propeller service life 3
HARTZELL propeller 3
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SOCATA MODEL TB 20 MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS
THE DGAC APPROVES THAT THE AIRWORTHINESS LIMITATIONS IN THIS CHAPTER ANSWER THE APPLICABLE AIRWORTHINESS REGULATION DETAILED IN FRENCH AIRWORTHINESS DATA SHEET No. 165.
THIS CHAPTER SPECIFIES INSPECTION AND MAINTENANCE REQUIRED UNDER PARTS 43.16 AND 91.403 OF THE FEDERAL AVIATION REGULATIONS.
Original version dated Sept. 1991, DGAC Approval reference BUREAU VERITAS MAE/AVI/TAB-200/91-JC/GV, dated 05 DEC. 1991.
Revision 04 dated Apr. 95, DGAC Approval reference 962720 SFACT/N dated June 11th, 1996.
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1. GENERAL
The airworthiness limitations section is DGAC approved and specifies inspection and maintenance required under parts 43.16 and 91.403 of the Federal Aviation Regulations.
2. STRUCTURE SERVICE LIFE
COMPONENT PART NUMBER SERVICE LIFE
(flight hours)
L.H. wing structure assembly TB 20 11000X)0( 10000
R.H. wing structure assembly _ TB 20 11000XXX 10000
XXX corresponds to the different changes of wing structures
3. ENGINE SERVICE LIFE
Refer to AVCO LYCOMING Operator's Manual (latest revision) or to fascicle 3.1/4 Vol. III of GSAC (Groupement pour la Securite de ('Aviation Civile, ex-BUREAU VERITAS., Aeronautics Division) (latest revision).
4. PROPELLER SERVICE LIFE A. HARTZELL propeller
Refer to manual of HARTZELL manufacturer (at latest revision) and HARTZELL Service Letter Nr 61 (latest revision) or to fascicle 4.1/2 Vol. III of GSAC (Groupement pour la Securite de ('Aviation Civile, ex-BUREAU VERITAS, Aeronautics Division) (latest revision).
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