Elevator Mass Balance V1, 01 thr. 34 -/- -/- -/- -/- -/- -/- LBA: LTA-Nr ; FAA: AD
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1 EASA.21J.073 Type EA-300, incl. Models (TCDS N EASA.A.362) Page: 1 of 5 SB Main Undercarriage U- Spring mounting Clamp V1, 03, 05, 06, -/- 15 thr. 26 -/- SB Elevator Mass Balance V1, 01 thr. 34 -/- LBA: LTA-Nr ; FAA: AD SB SB Issue C SB Rudder Control Cable Compression Sleeve Wing Root Rib/Aux. Spar Attachment Upper Longeron Cutout- Bridge all all LBA: LTA-Nr ; FAA: AD V1, 01 thr thr. 12 LBA: LTA-Nr /2 V1, 01 thr thr. 17 LBA: LTA-Nr. D R1 EASA: FAA: AD SB SB SB SB SB SB N withdrawn -/- -/- -/ Attachment of engine control V1, 01 thr thr. 23 -/- bowden Cables Canopy Latches -/- 01 thr. 24 LBA: LTA-Nr FAA: AD Pitot Static Drain Installation V1, 01 thr thr. 12 -/ Air Inlet Screen V1, 01 thr thr. 21 LBA: LTA-Nr Fire Protection Cowling Area V1, 01 thr thr. 22 LBA: LTA-Nr and Firewall SB Fuel Selector -/- 01 thr. 24 -/-
2 EASA.21J.073 Type EA-300, incl. Models (TCDS N EASA.A.362) Page: 2 of 5 SB SB Hydraulic Brakes V1, 01 thr thr. 25 -/ Seat Attachment V1, 01 thr thr. 22 -/- SB Issue F Upper Longeron Insp. 01 thr thr thr thr thr thr thr /- -/- -/- EASA: AD N FAA: AD LBA: D R1 85 thr and 92 SB Rudder pedal safety control stop all, if electric actuated pedals installed, prior 11/ thr thr. 15 -/- -/- -/- -/- LBA: LTA-Nr ; FAA: AD 98-CE-53-AD SB SB N withdrawn -/- -/- -/ Front Seat Belt Safety Cover -/- -/- -/- 01 thr. 15 -/- -/- -/- LBA: LTA-Nr R2 Installation FAA: AD SB Issue D Fuselage Structure Tail Spring Support -/- -/- 012, 014 thr. 170, 172, 173, 1171 and 1174 thr thr. 31 and 1032 thr /- -/- -/- EASA: AD N LBA: LTA-Nr. D R1 FAA: AD Transport Canada: Validated SB SB Front seat installation of lap belt guide Securing the wire stirrup of the gascolator bowl -/- -/- -/- 01 thr. 23 -/- -/- -/- LBA: LTA-Nr R2; FAA: AD thr thr thr thr. 29 -/- -/- -/- -/-
3 EASA.21J.073 Type EA-300, incl. Models (TCDS N EASA.A.362) Page: 3 of 5 SL Fuel selector valve leakage -/- all all all -/- -/- -/- LBA: LTA-Nr FAA: AD SB Replacement Fuel Hose to Filler Cap -/- 01 thr thr. 167, 172 and 01 thr. 31 -/- -/- -/- -/- SL Sep. 04 Technical Publications -/- -/- -/- SB Issue C Inspection/repair of Main Landing Gear Mounting Attachment -/- -/- -/- 01 thr. 31 and 1032 thr /- -/- -/- -/- SB Change Long Range Tanksto Standard Tanks Configuration 64 thr thr thr. 167, 172 and SB Bottom fuselage cover/firewall sealing V1, 01 thr thr thr. 167, 1171, 172, and 1174 thr thr. 31 -/- -/- -/- LBA: LTA-Nr. D ; FAA: AD
4 EASA.21J.073 Type EA-300, incl. Models (TCDS N EASA.A.362) Page: 4 of 5 EA-300/SC EA-300/LT EA-300/LC EXTRA 300LT SB Engine fuel pump vent V1, 01 thr thr. 31, thr. 167, 1171, 172 (or 1172),, 1174 thr and 1201 thr SB Repositioning of Single Oil Cooler -/- the single oil cooler system before May 2006 the single oil cooler system before May 2006 SB Safety clamps on located in subpanels -/- SL Propeller blade lag screw all all all all all all all -/- replacement (addresses MT- Propeller SB N 30 [R2])
5 EASA.21J.073 Type EA-300, incl. Models (TCDS N EASA.A.362) Page: 5 of 5 EA-300/SC EA-300/LT EA-300/LC EXTRA 300LT SB Throttle control cables -/- 01 thr. 31, 1032, 1034, thr. 167, 1171, 172 (or 1172), 173 (or 1173), 1174 thr thr. 31, 1032 thr SC003 thr. SC054 LT001 thr. LT030 LC001 thr. LC043 SB V-tubes in rear fuselage structure 62 -/- -/-
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