AIRWORTHINESS DIRECTIVE
CAA-AD-4-072/97R2
Canceled CAA-AD-4/072/97R1
Date of issue: March 14, 2000
AIRWORTHINESS DIRECTIVES FOR ENGINES, PROPELLERS AND VENDOR EQUIPMENT
Applicability: SAAB SF340A and SAAB 340B.
Effective date: April 20, 2000
Compliance: Required as indicated in SAD No. 1-1094R4.
Remarks: The compliance of this AD must be recorded in Aircraft Logbook, where applicable the requirements of this AD must be integrated into Aircraft Technical Documentation. Address inquiries concerning this AD to: Civil Aviation Authority, Airworthiness Division, Ruzyne Airport, 160 08 Prague 6, Czech Republic, tel: 420 2 33320922, fax: 420 2 20562270.
Ing. Pavel MATOUŠEK
Director of Airworthiness Division
CAA CZ
SWEDISH AIRWORTHINESS DIRECTIVES (SAD) No: 1-094R4
Cancels 1-094R3
AIRCRAFT TYPE: SAAB SF340A and SAAB 340B
SERIAL No's. AFFECTED: All serial numbers
SUBJECT: Airworthiness Directives for engines, propellers and other vendor equipment
BACKGROUND: Procedures and regulations regarding issuance of Swedish Airworthiness Directives (SAD) are defined in Swedish Civil Aviation Regulations, BCL-M 1.11.
This regulation stipulates that LFV shall issue an SAD in each case a foreign Airworthiness Directive has been issued by the state of manufacture for an engine, propeller or other vendor equipment that is used in an aircraft which has been certificated by LFV and LFV has agreed that the required action is appropriate.
This regulation has with a few exceptions not been followed up to now. This means that an operator may formally, with reference to BCL-M 1.11, elect not to comply with foreign Airworthiness Directives. On the other hand, the Swedish regulations for maintenance, BCL-M 3.2 stipulates that each maintenance organization for transport category aircraft must have access to and follow all Airworthiness Directives issued by the state of manufacture. However, the wording in this regulation is ambiguous and can be misinterpreted as being limited to airframe Airworthiness Directives only.
This SAD is issued to
a) Eliminate the possibility of misinterpretation of the wording in the regulations regarding mandatory compliance with Airworthiness Directives issued by the state of manufacture for engines, propellers and other vendor equipment
b) As a service publish a list of vendor Airworthiness Directives published by the State of Manufacture (or Design)
REFERENCE DOCUMENTS: Swedish Civil Aviation Regulations, BCL-M 1.11 and M 3.2
ACTIONS:
Perform all applicable actions required by Airworthiness Directives issued by the state of manufacture (or Design) for the engines, propellers and other vendor equipment that are part of the SAAB SF340A and SAAB 340B type design. An alternate means of compliance or exemption may be approved by LFV, Aviation Safety Department.
COMPLIANCE TIME: As defined in the foreign Airworthiness Directive
EFFECTIVE DATE: 17 February, 2000
Enclosure to SAD 1-094R4
List of foreign Airworthiness Directives applicable to the SAAB SF340A and/or SAAB 340B
The following foreign Airworthiness Directives are issued by the state of manufacture (or Design) for engines, propellers and other vendor equipment that are part of the SAAB SF340A and/or type design.
Please observe that the list may be incomplete and is published as a service only. Each operator is responsible to check applicable Airworthiness Directives for his airplane.
Comments are invited for revision of the enclosure with updated data.
|
Authority |
AD Number |
Subject |
LFV Disposition |
|
CAA UK |
018-10-90 |
FIRE FIGHTING ENTERPRISES: Cabin portable fire extinghuiser |
Swedish Airworthiness Directive LVD No 2329 released |
|
CAA UK |
005-04-92 |
FLIGHT EQUIPMENT AND ENGINEERING SEATS MODEL 121: Visual inspection of 111/115 seats for cracking |
|
|
CAA UK |
004-09-92 |
FIRE FIGHTING ENTERPRISES: Cabin portable fire extinghuiser- Discharge head assembly |
Swedish Airworthiness Directive L VD No 2453 released |
|
CAA UK |
006-03-93 |
FLIGHT EQUIPMENT & ENGINEERING: Inspection and where necessary replacement of aisle section |
|
|
CAA UK |
017-03-93 |
FLIGHT EQUIPMENT & ENGINEERING SEATS MODEL 121: Replacement of inboard section |
|
|
CAA UK |
006-01-94 |
DOWTY AEROSPACE PROPELLERS: Inspection of counterweight arms for forging folds |
Overhaul instructions applies |
|
CAA UK |
005-10-94 |
DOWTY AEROSPACE GLOUCESTER PROPELLERS: Propellers - Hub wall cracking |
|
|
CAA UK |
002-11-96 |
DOWTY AEROSPACE GLOUCESTER: Propeller - Blade pitch seizure |
|
|
CAA UK |
006-10-99 |
DOWTY AEROSPACE GLOUCESTER: Propellers - Hub wall cracking |
|
|
FAA |
74-08-09 |
PAPER AND LINEN RECEPTABLES |
Included in MRB Doc. |
|
FAA |
88-07-08 |
GENERAL ELECTRIC: Prevent engine power turbine over speed |
SAD No 1-021 released |
|
FAA |
90-07-08R1 |
S.E.L.A. LABORATORIE: Cabin fluorecent lighting system |
|
|
FAA |
91-10-01 |
COLLINS TCAS II Modification of Collins TTR-920 computer |
|
|
FAA |
91-15-15 |
E.I. DUPONT de NEMOURS & Co: Crewmember Protective Breathing Equipment |
Performed by SAAB USA |
|
FAA |
93-04-02 |
ROCKWELL INTERNATIONAL/-COLLINS: TDR-94D Mode S Transponders |
|
|
FAA |
93-06-06 |
HAMILTON STANDARD: Possible exessive wear of propeller control unit |
|
|
FAA |
93-14-12 |
ESSX PB arid R CORPORATION: Crewmember Protective Breathing Equipment |
|
|
FAA |
93-23-05 |
GENERAL ELECTRIC AIRCRAFT ENGINES: Inspection and replacement of, if necessary of certain gas generator turbine rotor assembly |
|
|
FAA |
93-24-16 |
PURITAN BENNET AERO SYSTEMS: Crewmember Protective Breathing Equipment (PBE) |
|
|
FAA |
93-25-17 |
GENERAL ELECTRIC: Gas generator turbine disks and cooling plates |
|
|
FAA |
94-06-05 |
HAMILTON STANDARD: New torquening procedures for the propeller hub retainging nuts |
|
|
FAA |
94-01-06 |
COLLINS: TCAS II Processors |
|
|
FAA |
95-05-03 |
HAMILTON STANDARD: Perform an ultrasonic shear wave inspection for cracks in the blade taper bore |
|
|
FAA |
94-17-16 |
GENERAL ELECT RIC AIRCRAFT ENGINES: To prevent failure of the propeller shaft |
|
|
FAA |
94-24-10 |
SAAB AIRCRAFT AB: Flight Equipment and Engineering Seats Model 121, inspection/repair of seat backrest |
|
|
FAA |
95-05-03 |
HAMILTON STANDARD: Ultra shear wave inspection of blade taper bore |
|
|
FAA |
95-22-01 |
AEROSPACE LIGHTING CORPORATION: Cabin fluorescent lighting system |
|
|
FAA |
95-22-12 |
HAMILTON STANDARD: Inspection of PCU servo BIS for tooth wear |
|
|
FAA |
96-08-0l R1 |
HAMILTON STANDARD: Ultrasonic shear wave inspection for cracks at the blade butt end |
|
|
FAA |
96-08-02 |
HAMILTON STANDARD: Ultra shear wave inspection of blade taper bore |
|
|
FAA |
96-25-20 |
HAMILTON STANDARD: Inspection of transfer tube assemblies and propeller control units (PCU) for wear |
|
|
FAA |
96-26-01 |
GENERAL ELECTRIC AIRCRAFT ENGINES: Reduced cyclic life limit of GGT Stage 2 forward cooling plates |
|
|
FAA |
97-25-07 |
GENERAL ELECTRIC AIRCRAFT ENGINES: Inspection of Stage 1 GGT Disks |
|