AIRWORTHINESS DIRECTIVE
CAA-AD-3-066R1/97
Date of issue: November 16, 1998
AIRCRAFT - ENGINE AIR INTAKE - MODIFICATION
Applicability: SAAB SF 340A -004 through -159 and SAAB 340B -160 through -219 and -402 through -436 equipped with Aerospace Composite Technologies (ACT) Engine Air Intakes.
Effective date: December 31, 1998
Compliance: Required as indicated in SAA AD 1-119R1.
Remarks: Where applicable, the requirements of this AD must be integrated into the Aircraft's Logbook(s). Address inquiries concerning this AD to: Civil Aviation Authority, Airworthiness
Division, Ruzyně Airport, 160 08 Prague 6, Czech Republic, tel.: 420 2 324086, fax: 420 2 364112.Ing. Pavel MATOUŠEK
Director of Airworthiness Division, CAA CZ
LUFTFARTSVERKET Aviation Safety Department SWEDISH AIRWORTHINESS DIRECTIVES (SAD)
SAD No 1-119R1 Cancels SAD No 1-119
Section 1. Swedish Manufactured Aeronautical Products
AIRWORTHINESS DIRECTIVE NO: 1-119R1
AIRCRAFT TYPE: SAAB SF 340A and SAAB 340B
SERIAL No’s AFFECTED: SAAB SF 340A -004 through -159 and SAAB 340B -160 through -219 and -402 through -436 equipped with Aerospace Composite Technologies (ACT) Engine Air Intakes.
Note: Effectivity changed
SUBJECT: Ice & Rain Protection - Engine Air Intake -Modification of the Detachable Center Inlet.
BACKGROUND: The design and manufacturing method of the detachable center inlet produces two apertures at the rear of the component. These holes must be closed to fully comply with fire resistance regulations.
REFERENCE DOCUMENTS: Saab AB Service Bulletin SAAB 340-30-073 Revision 1 dated October 1, 1998 and Attachment 1.
ACTIONS: Perform actions described in Saab AB Service Bulletin SAAB 340-30-073 Revision 1, dated October 1,1998, and Attachment 1, or later revision.
COMPLIANCE TIME: To be performed within two years from the effective date of this SAD.
EFFECTIVE DATE: 8 October, 1998