LANDMARK AVIATION SUPER KING AIR 200 SERIES DUE ANYTIME PLACARDS ARE REMOVED OR AFTER PAINT AFTER INITIAL COMPLIANCE

Transcription

1 1 F /N riginal Issue hase Inspection C/W: 1&2 Next Due hase: 3& /10/ /09/08 hase Inspection C/W: 1&2 Next Due hase: 3& /10/ Complete hase Inspection 1 thru /10/ Aug-09 Complete hase Inspection 1 thru /10/ Next hase Next hase Next hase Next hase FAR /12/ Apr-08 FAR /12/ Apr-08 ELT Annual Inspection er FAR (d) /22/ /22/07??? ELT Battery - Date on Battery 238 Date on Battery: 4/1/2008 MSB Flight Control Gust Lock Inspection, hase AIRWRTHINESS DIRECTIVES - AIRFRAME AD R1 - Effect. 7/9/90 - Wing Bay Fuel anels - RECURRING AD N/A ER AIRCRAFT S/N AD R1 - Effect. 7/9/90 - Wing Bay Fuel anels - RECURRING AD /25/ AD Effect. 3/7/03 - Airstair Door & Emergency Exit - RECURRING AD DUE ANYTIME LACARDS ARE REMVED R AFTER AINT AFTER INITIAL CMLIANCE AD Effect. 3/1/05 - Stringer Inspection (Supersedes AD ) - Due 500 Cycles UNLESS CRACKS NTED - RECURRING AD ??? AIRWRTHINESS DIRECTIVES - ENGINES S/N L- R- N RECURRING R NEW AD'S AIRWRTHINESS DIRECTIVES - RS S/N L- R- N RECURRING R NEW AD'S AIRWRTHINESS DIRECTIVES - ALIANCES N RECURRING R NEW AD'S CHATER AIRWRTHINESS LIMITATINS S/N BB-2 THRU BB-1157, BB-1159 THRU BB-1166, BB-1168 THRU BB-1192; BL-1 THRU BL-72; BT-1 THRU BT-30; BN-1 THRU BN-4 Airworthiness Limitations for above Aircraft Serial Numbers are located in the Limitations Section & Emergency rocedures of the appropriate H and AFM CHATER AIRWRTHINESS LIMITATINS (MANUAL /N ) S/N BB-1158, BB-1167, BB-1193 & AFTER; BL-73 & AFTER; BT-31 & AFTER; BN-5 & AFTER

2 2 F /N riginal Issue Windshield Frame Screws Replace - Life Limited L Windshield Frame Screws Replace - Life Limited R Cabin Airstair Door Forward & Aft Side Latch Bolts Replace - Life Limited (A/C S/N BB-1158, BB- 1167, BB-1193 & After; BT-31 & After) Cabin Airstair Door Upper Hook Mechanism (Including ins, Brackets, Spring, Arm & Hooks) Replace - Life Limited (A/C S/N BB-1158, BB-1167, BB-1193 & After; BT-31 & After) B200C Cargo & Airstair Door Cam Lock Actuator Cables - Replace - Life Limit (A/C S/N BL-73 & After; BN-5 & After) Horizontal and Vertical Stabilizers - Retire Structure 45,000 Hours Wing Center Section - Life Limited 9,500 Hrs Unless Kit is installed - S/N BB-1158, BB-1167, BB BB-1203, BB BB-1295, BB BB-1301, BB-1303, BB-1304, BB BB-1308, BB B-1313, BB BB-1334; BL BL-127, BL-129, BL-131, BL-132; BT Wing Center Section - Life Limited 18,000 Hrs Unless Kit is installed - S/N BB-1158, BB-1167, BB BB-1203, BB BB-1295, BB BB-1301, BB-1303, BB-1304, BB BB-1308, BB B-1313, BB BB-1334; BL BL-127, BL-129, BL-131, BL-132; BT-33 SEE FLLWING NTE: Wing Center Section NT LIFE LIMITED (WITH KIT # & KIT # ED) RVIDED INSECTINS IN F SIRM ARE ERFRMED - SEE CHATER Wing Center Section - Life Limited 18,000 Hrs Unless Kit is installed -S/N BB BB-1337, BB BB-1375, BB BB-1382, BB BB-1433, BB BB-1512; BL BL-141; BT-35 - BT-38 SEE FLLWING NTE: Wing Center Section NT LIFE LIMITED (WITH KIT # ED) RVIDED INSECTINS IN F SIRM ARE ERFRMED - SEE CHATER Wing Center Section NT LIFE LIMITED - S/N BB-1513 & AFTER; BL-142 & AFTER; BT-39 & AFTER; BN-5 & AFTER NT LIFE LIMITED RVIDED INSECTINS IN F SIRM ARE ERFRMED - SEE CHATER

3 3 F /N riginal Issue utboard Wing Structure - Life Limited 30,000 Hours Unless Spar Cap is replaced w/ /N & -2 for A/C S/N BB BB-1337, BB BB-1375, BB BB-1382, BB BB-1433, BB BB-1539, BB BB-1542; BL BB-141; & rior A/C with Kit Installed Life Limited 30,000 Hours for A/C S/N BT-35 & AFTER; BN-5 & AFTER; & rior A/C with Kit Installed utboard Wing Structure NT LIFE LIMITED - S/N BB-1540, BB-1453 & AFTER; BL-141 & AFTER; & RIR A/C WITH NEW SAR CA /N & -2 ED NT LIFE LIMITED RVIDED INSECTINS IN F SIRM ARE ERFRMED - SEE CHATER Wing to Fuselage Attach Angles /N & Replace - Life Limited Upper Forward, Upper & Lower Aft Wing Bolts & Nuts - Replace /9/ /06/19 Upper Forward, Upper & Lower Aft Wing Bolts & Nuts - Replace Lower Forward Wing Bolt & Nut Replace 5 Years or Anytime Removed /9/ /08/09 NTE: FR SECIAL URSE AIRLANES - REFERENCE AIRWRTHINESS LIMITATINS MANUAL FR REQUIREMENTS Engine Fire Ext. Hydro (LH & RH) LISTED IN CHATER Engine Fire Ext. Cartridges Life Limit (LH & RH) LISTED IN CHATER xygen Cylinder - Hydro LISTED IN CHATER Cabin Fire Ext.- Hydro LISTED IN CHATER Emergency Exit (Self-Illuminating) - Replace 7 Years from DM R Inspect Annually Beginning 7 Yrs & Replace When the Brightness Level is Below 100 Micro Lamberts 2555 Date of Mfg. 8/9/ /08/11 Emergency Exit (Self-Illuminating) - Replace 7 Years from DM R Inspect Annually Beginning 7 Yrs & Replace When the Brightness Level is Below 100 Micro Lamberts 365 REEAT INSECTIN NT YET DUE Side Windows & Windows - with Cracked uter or Inner ly - Reference Airworthiness Limitations Manual Chart 4 for Limitations CHATER VERHAUL & RELACEMENT

4 4 F /N riginal Issue LANDING GEAR Actuators (Hydraulic)LH, RH, & Nose - n Condition /C Actuators (Mechanical) verhaul R Replace L Actuators (Mechanical) verhaul R Replace R Actuators (Mechanical) verhaul R Replace N Landing Gear Actuator Support Bearings (Sealed) /C Gear Wheels, Bearings & Tires (LH, RH, & Nose) Ref CMM for Limits Nose Gear Retract & Emergency Extension Chains (Mechanical) Replace per Chapter /C Main Gear Brakes Ref CMM for Limits Landing Gear Motor verhaul (Mechanical) Landing Gear Retract & Extension Teflon Hydraulic Hoses - Replace /9/ /07/14 Landing Gear Hydraulic System Filter & -Ring LISTED IN CHATER BRAKE SYSTEM Brake System Hoses (nly Hoses Exposed in Wheel Well) /9/ /08/09 ELECTRICAL SYSTEM CVR Underwater Locator Beacon ( BB-1476 & After, BL-141 & After, BT-39 & After, BN-5 & After) Replace Batteries Every 6 Years BATTERY EXIR. DATE ct-07??? CVR Underwater Locator Beacon (BB-1476 & After, BL-141 & After, BT-39 & After, BN-5 & After) Function Test Every 24 Months 730 8/16/ Aug-08 WERLANT ER &W SB 3003 REV Engine verhaul -42 CE-J0782 L Engine verhaul -42 CE-J0781 R Starter Generator verhaul L Starter Generator verhaul R il Cooler - Replace When Contaminated /C Engine il Filter - Replace L Engine il Filter - Replace R Air Filter - Replace L Air Filter - Replace R

5 5 F /N riginal Issue Flammable Fluid Carrying Hoses- Replace L /9/ /08/09 Flammable Fluid Carrying Hoses- Replace R /9/ /08/09 RELLER Make / Model ER ALICABLE SB ropeller verhaul S/N HH-1930 L /9/ /08/10 ropeller verhaul S/N ropeller verhaul S/N HH-1940 R /9/ /08/10 ropeller verhaul S/N ropeller verspeed Governor verhaul (SB 33580L) L ropeller verspeed Governor verhaul (SB 33580L) R ropeller rimary Governor verhaul (SB 33580L) L ropeller rimary Governor verhaul (SB 33580L) R FUEL SYSTEM Firewall Shut-ff Valve /C UTILITY SYSTEMS xygen System, assenger Shutoff Valve -rings LISTED IN CHATER Engine Fire Ext. (LH & RH) Hydro LISTED IN CHATER Engine Fire Ext. Cartridges (LH & RH) LISTED IN CHATER Instrument Air Filter - Replace /10/ SECIAL INSECTINS ER Hot Section Inspection er &W SB 3003 Rev L Hot Section Inspection er &W SB 3003 Rev R Engine il Filters - Replace LISTED IN CHATER Nacelle Fuel Cell & robe Inspection L /10/ /07/10 Nacelle Fuel Cell & robe Inspection L /10/ Nacelle Fuel Cell & robe Inspection R /10/ /07/10 Nacelle Fuel Cell & robe Inspection R /10/ Main Gear Shock Absorber Assy, Drag Brace Assy, Axle Assy & Torque Knee Inspection L /9/ /08/10 Main Gear 6 Year/8000 Cycle Inspection L Main Gear Shock Absorber Assy, Drag Brace Assy, Axle Assy & Torque Knee Inspection R /9/ /08/10 Main Gear 6 Year/8000 Cycle Inspection R

6 6 F /N riginal Issue Nose Gear Shock Absorber Assy, Drag Brace Assy, Axle Assy & Torque Knee Inspection N /9/ /08/10 Nose Gear 6 Year/8000 Cycle Inspection N Actuator Clevis Inspection L Actuator Clevis Inspection R Actuator Clevis Inspection N Main Landing Gear Wheels Inspection LISTED IN CHATER Flap Flexible Shaft Inspection L Flap Flexible Shaft Inspection R Wing Front Spar Cap Inspect & Check - Initial L /9/ /08/09 Wing Front Spar Cap Inspect & Check - Repeat L 365 REEAT INSECTIN NT YET DUE Wing Front Spar Cap Inspect & Check - Initial R /9/ /08/09 Wing Front Spar Cap Inspect & Check - Repeat R 365 REEAT INSECTIN NT YET DUE 3 Air Filter - Replace LISTED IN CHATER Fuselage Stringer Inspection - Ref. Chapter 53 LISTED IN CHATER Upper & Lower Windshield Corners Inspect Doublers & Clips of Fuselage (See Note) Initial Upper & Lower Windshield Corners Inspect Doublers & Clips of Fuselage (See Note) Repeat 1000 REEAT INSECTIN NT YET DUE NTE: Cracked arts found in area must be replaced within 500 Cycles per Ref. Chart IF CRACKED ARTS FUND - MUST RELACE WITHIN 500 CYCLES Edgelighted anel Assemblies Inspection /9/ /08/08 Edgelighted anel Assemblies Inspection Air-Conditioner Compressor Drive Belts - Check tension 50 Hrs after Installation of New Belt 50 NLY DUE 50 HURS AFTER ATIN F NEW BELT Cabin Door & Fuselage Frames Inspection 4 Corners of Door Frame & Upper Latch Hook Catches - Initial - (SEE NTE) Cabin Door & Fuselage Frames Inspection - Repeat (SEE NTE) 1000 REEAT INSECTIN NT YET DUE NTE: Cracked arts found in area must be replaced within 175 Cycles per Ref. Chart IF CRACKED ARTS FUND - MUST RELACE WITHIN 175 CYCLES

7 7 F /N riginal Issue edestal ower Lever Stop in Inspection Cockpit Fire Ext. Hydro Test (Date on Bottle) /9/ /06/16 Cabin Fire Ext. Hydro Test (Date on Bottle) /9/ /06/16 Cockpit Fire Ext. Annual Inspection 365 9/22/ /22/07??? Cabin Fire Ext. Annual Inspection 365 9/22/ /22/07??? Engine Fire Ext. Bottle - Hydro Test L /9/ /08/09 Engine Fire Ext. Bottle - Hydro Test R /9/ /08/09 Engine Fire Ext. Cartridge Service Life 4 Years from Installation L /9/ /08/08 Engine Fire Ext. Cartridge Service Life 4 Years from Installation R /9/ /08/08 Engine Fire Ext. Cartridge - Life Limit 6 Years from DM L /9/ /08/10 Engine Fire Ext. Cartridge - Life Limit 6 Years from DM R /9/ /08/10 Cargo Door Lower Attachment Lug (S/N BL-1 & After; BN-1 & After) - as required AS REQUIRED Eight Wing Attach Bolts Inspection - 5 Years (rior to S/N BB-1193, Except BB-1158 & BB-1167; rior to BB-31, prior to BL-73, prior to BN-5) /9/ /08/09 Wing Center Section Upper Surface Bonded anel Skin Inspection (AD R1) Ref Hydraulic System Filter, Landing Gear Inspection - Initial 200 INITIAL INSECTIN C/W Hydraulic System Filter, Landing Gear Inspection - Repeat Hydraulic System Filter, Landing Gear Inspection - Repeat Retract Gearbox & Clutch (Mechanical Gear) Inspect Actuators (Mechanical Gear) End lay Check LH, RH, & Nose Airstair Door, Cargo Door, and Escape Hatches Inspection Initial

8 8 F /N riginal Issue Airstair Door, Cargo Door, and Escape Hatches Inspection Repeat 1000 REEAT INSECTIN NT YET DUE Forward ressure Bulkhead Inspection Skin, Exterior Airframe Inspection - Initial Skin, Exterior Airframe Inspection - Repeat 1000 REEAT INSECTIN NT YET DUE Frames, Fuselage Subfloor (FS 84 - FS ) Inspection - Initial Frames, Fuselage Subfloor (FS 84 - FS ) Inspection - Repeat 1000 REEAT INSECTIN NT YET DUE Frame Web, (Stringer Cutouts FS FS 271, Lower Centerline to Stringer #4) Inspection - Initial Frame Web, (Stringer Cutouts FS FS 271, Lower Centerline to Stringer #4) Inspection - Repeat 1000 REEAT INSECTIN NT YET DUE Stringers 7,8,9, & 10 (FS 88 - FS 125) & Instrument anel Support Brackets Inspection Flight Control ulley Brackets & Castings Inspection - Initial Flight Control ulley Brackets & Castings Inspection - Repeat 5000 REEAT INSECTIN NT YET DUE Aft Fuselage Area & Rear ressure Bulkhead - xygen Bottle Mounting Brackets - utflow & Safety Valve Box Inspection - Initial Aft Fuselage Area & Rear ressure Bulkhead - xygen Bottle Mounting Brackets - utflow & Safety Valve Box Inspection - Repeat 500 REEAT INSECTIN NT YET DUE xygen Cylinder 3AA1800 (Lightweight Composite) Hydro Test Every 3 Yrs /30/ /29/09 xygen Cylinder 3AA1800 (Lightweight Composite) Cylinder Service Life 15 Yrs /09/ /06/19 xygen Regulator verhaul (Due when xygen Bottle is Hydrostatically Tested) /30/ /29/09

9 9 F /N riginal Issue CVR Underwater Locator Beacon (BB-1476 & After, BL-141 & After, BT-39 & After, BN-5 & After) Function Test Every 24 Months LISTED IN CHATER xygen System assenger Shutoff Valve (Auto deployment xygen System) Replace -Rings Every 2 Yrs 730 8/16/ Aug-08 Engine Mount Vibration Isolators - Replace 4000 Hours or Engine TB, whichever occurs first L Engine Mount Vibration Isolators - Replace 4000 Hours or Engine TB, whichever occurs first R Rudder Boost Filter (A/C without Autopilot)- Replace Every 200 Hours /10/ Lead Acid Battery Boost Charge - Battery Stored in A/C only- (BB-1632 & After; BT-39 & After; BL-141 & After; BN-5 & After) 90 BATTERY STRED IN A/C NLY Lead Acid Battery Emergency Capacity Test (BB-1632 & After; BT-39 & After; BL-141 & After; BN-5 & After) Initial (from Installation) 12 Months or 600 Hrs / Repeat 12 Months or 200 Hrs /10/ /09/08 Lead Acid Battery Emergency Cap Test - Initial 600 8/16/ Lead Acid Battery Emergency Capacity Test (BB-1632 & After; BT-39 & After; BL-141 & After; BN-5 & After) Repeat 12 Months or 200 Hours 365 REEAT INSECTIN NT YET DUE Lead Acid Battery Emergency Cap Test - Repeat 200 REEAT INSECTIN NT YET DUE Standby ower Supply Battery S835 Test /10/ /08/08 Cabin Altitude Warning ressure Switch Test /10/ /09/08 Barometric ressure Switch Check /10/ /09/08

10 10 F /N riginal Issue Air Data System - (RVSM A/C NLY) (S/N BB BB-1683, BB BB-1716, BB BB-1720, BB- 1722, BB-1723, BB-1725, BB-1726, BB BB & equipped with Collins EFIS-84 R EFIS- 85B(14) & if A/C has C/W SB ; BB-1802 & After; BL BL-148 if equipped with Collins EFIS-85B(14) & A/C has C/W SB ; BL- 149 & After) erform the Airworthiness Inspection Requirements 730 FR RVSM CMLIANT AIRCRAFT NLY ilot's Fuel Control anel & Lower Edgelighted anel, Coilot's Edgelighted Circuit Breaker anel Inspection /15/ /15/07??? FUSELAGE & ASSCIATED STRUCTURE LISTED IN CHATER R H SECTIN (ER S/N) WING & ASSCIATED STRUCTURE SAFELIFE LISTED IN CHATER R H SECTIN (ER S/N) CHATER CHART LISTED IN CHATER SECTIN N STATUS SHEET CHATER SIRM (Rev C1 dated 10/05) - S/N BB-1158, BB-1167, BB-1193 & AFTER; BL-73 & AFTER; BN-5 & AFTER; & BT-31 & AFTER Lower Forward (Main) Spar Lugs - Initial Lower Forward (Main) Spar Lugs - Repeat 6000 REEAT INSECTIN NT YET DUE /B Wing anel, Lower, Fwd Spar Cap /N (BB-1542 & After; BL-141 & After; & Earlier S/N's with this Spar Cap) - Initial /B Wing anel, Lower, Fwd Spar Cap /N (BB-1542 & After; BL-141 & After; & Earlier S/N's with this Spar Cap) - Repeat 3000 REEAT INSECTIN NT YET DUE Center Section Lower Fwd Spar Cap - Initial Center Section Lower Fwd Spar Cap - Repeat 3000 REEAT INSECTIN NT YET DUE Center Section Belly Skin - Initial Center Section Belly Skin - Repeat 3000 REEAT INSECTIN NT YET DUE Center Section Lower Aft Spar Cap without Kit Installed - Initial Center Section Lower Aft Spar Cap without Kit Installed - Repeat 1500 REEAT INSECTIN NT YET DUE

11 11 F /N riginal Issue Center Section Lower Aft Spar Fitting without Kit Installed - Initial Center Section Lower Aft Spar Fitting without Kit Installed - Repeat 1500 REEAT INSECTIN NT YET DUE utboard Wing anel Aft Spar Lower Fitting without Kit Installed - Initial utboard Wing anel Aft Spar Lower Fitting without Kit Installed - Repeat 1500 REEAT INSECTIN NT YET DUE UN ATIN F KIT /N THE FLLWING INSECTINS ARE DUE AS FLLWS - INITIALLY DUE 27,000 HURS AFTER KIT ATIN Center Section Lower Aft Spar Cap with Kit Installed - Initial Center Section Lower Aft Spar Cap with Kit Installed - Repeat 6000 REEAT INSECTIN NT YET DUE Center Section Lower Aft Spar Fitting with Kit Installed - Initial Center Section Lower Aft Spar Fitting with Kit Installed - Repeat 6000 REEAT INSECTIN NT YET DUE utboard Wing anel Aft Spar Lower Fitting with Kit Installed - Initial utboard Wing anel Aft Spar Lower Fitting with Kit Installed - Repeat 6000 REEAT INSECTIN NT YET DUE /B Wing anel Upper & Lwr Main Spar Caps Inspect - Initial /9/ /08/09 /B Wing anel Upper & Lwr Main Spar Caps Inspect - Repeat 365 REEAT INSECTIN NT YET DUE /B Wing anel Upper & Lwr Main Spar Caps Inspect - Replacement RELACEMENT REQUIREMENT LISTED IN CHATER SECTIN Lower Fwd Main Spar Clevis Fittings - Inspect /9/ /08/09 Lower Forward Wing Bolt INSECTIN N/A ER CHATER RELACEMENT REQUIREMENT LISTED IN CHATER SECTIN Wing Bolts the Upper Fwd, Upper & Lower Aft Wing Joining oints Inspection (Replacement Requirement listed in Chapter Section) /9/ /08/09

12 12 F /N riginal Issue Retorque Wing Bolts After Each Inspection of Wing Bolts or Anytime Removed - Due Next Scheduled Inspection /25/ Due Next Insp Flat Surfaces, Depressions, Counterbores, & Bolt Bores the Upper Fwd, Upper & Lower Aft Wing Joining oints Inspection /9/ /08/09 LUBRICATINS ANNUAL WING BLT LUBE /10/ /09/ HUR LUBRICATIN /10/ HUR LUBRICATIN 400 8/16/ HUR LUBRICATIN /10/ HUR LUBRICATIN HUR LUBRICATIN LEFT ENGINE LIFE LIMITED CMNENTS - ENGINE S/N ER &W SB 1st Stage Disk Hub Assy /N S/N nd Stage Disk /N S/N rd Stage Disk /N S/N Impeller /N S/N CT Disk /N S/N st Stage T Disk /N S/N nd Stage T Disk /N S/N RIGHT ENGINE LIFE LIMITED CMNENTS - ENGINE S/N ER &W SB 1st Stage Disk Hub Assy /N S/N nd Stage Disk /N S/N rd Stage Disk /N S/N Impeller /N S/N CT Disk /N S/N st Stage T Disk /N S/N nd Stage T Disk /N S/N STC'S

13 13 F /N riginal Issue