King Air 200 Series Report - Title Page
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1 - Title Page Serial Number: Registration Number: Total Time: Total Landings: Date of C of A: Date Last Weighed: Paint Scheme: Date This Shop Visit: 12/28/2007 Projection: Hours Cycles Cal. Days Hours & Cycles current as of: 1/29/2008 Airframe: 659 Airframe HOBBS: Engines: 2/18/2005 2/8/2005 Exterior Interior Today's date: Prepared By: 4/9/2008 Holt Engines L/H Serial Number: L/H del R/H Serial Number: R/H del PCE-PJ0834 PT6A-42 PCE-PJ0833 PT6A-42 TSN: TSO: TSHI: CSN: 659 CSO: TSN: TSO: TSHI: CSN: 659 CSO: Propellers L/H Serial Number: L/H del HH-2115 HC-E4N-3G TSN: TSO: R/H Serial Number: R/H del HH-2116 HC-E4N-3G TSN: TSO: Manuals POH/AFM Current Revision: Flight Manual Supplements: Wiring Diagrams: Weight and Balance Current: Yes No Notes: Avionics PRO LINE FAA Form 337's Repairs: Alterations: How Many Notes: Certificates Airworthiness: Registration: Yes No (does N# serial number match) (current owner) Inspection Program: FAR (e)(f)(3) 1 of 1 4/9/2008
2 Maintenance Sched. Ref. Hours Cycles / Hours Cycles Days ATA 05 - INSPECTIONS Phase Phase Phase Phase Phase 1 w/ Additional Proline items ,564.0 Phase 2 w/ Additional Proline items ,564.0 Phase 3 w/ Additional Proline items ,564.0 Phase 4 w/ Additional Proline items 800 1/29/ , /31/2010 ATA 08 - LEVELING & WEIGHING Weight Aircraft & Update AFM. FAR ATA 12 - SERVICING 200 Hr. Lubrication Items. Ch Hr. Lubrication Items. Ch , Hr. Lubrication Items. 800 Hr. Lubrication Items. Ch. 12 Ch , , ,200 Hr. Lubrication Items. Ch. 12 1, ,200.0 Annual Wing Bolt Lubrication. ATA 21 - AIR CONDITIONING Ch /4/ /31/2008 Cabin Altitude Warning Switch Check 12 12/4/ /31/2008 A/C Belt Tension Check 50 Pneumatic Flow Control Filter Replace P/N Pneumatic Flow Control Filter Clean P/N ATA 22 - AUTOFLIGHT Pro Line Autopilot Servo Clutch Test 12,000 11, 12,000.0 ATA 23 - COMMUNICATIONS CVR ULB Clean/Ping Test 3/16/ /31/2009 CVR ULB Battery Replacement 891 Expiration Date 9/30/2010 ATA - ELECTRICAL POWER L/H Starter Generator Ovh. 89 1, ,311.8 R/H Starter Generator Ovh. P1125 1,000 L/H Starter Generator QAD Inspection. R/H Starter Generator QAD Inspection. 1,000 1, ,311.8 Main Battery RG380E/44K /23/ , /31/2008 Cap Check BB-1632 & After Main Battery RG-380E/44K Concorde Replacement STC ONLY 1, Main Battery RG-380E/44K Concorde 0 12 Cap Check STC ONLY ATA 25 - EQUIP/FURNISHINGS ELT Inspection FAR (d) 12 12/4/ /31/2008 ELT Battery Replacement. FAR c Expiration Date Life Vest Recertification 4/30/ of 6 4/9/2008
3 ATA 26 - FIRE PROTECTION L/H Eng. Fire Extinguisher R/H Eng. Fire Extinguisher Left Eng. Fire Ext. Squib. Right Eng. Fire Ext. Squib. Cockpit Fire C352TS Extinguisher W Maintenance Sched. Ref. Hours Cycles / Hours Cycles Days Hydro Test Hydro Test Service Life 4 Life Limit 6 Date of Mfg Service Life 4 Life Limit 6 Date of Mfg Hydro Test 12 1/1/ /31/2015 Mid-Life Insp 6 1/1/ /31/2009 Insp/Weight 1 1/29/ Cabin Fire C352TS Hydro Test 12 1/1/ /31/2015 Extinguisher W Mid-Life Insp 6 1/1/ /31/2009 Insp/Weight 1 1/29/ ATA 27 - FLIGHT CONTROLS Flight Control Pulley Bracket & Casting Insp.0 L/H Flap Flexible Shaft Inspection 4,341.0 R/H Flap Flexible Shaft Inspection. 4,341.0 Rudder Boost Filter Replacement. 200 ATA 28 - FUEL L/H Nacelle Fuel Cell & Probe Inspect. 2, /23/2007 2, ,996.4 R/H Nacelle Fuel Cell & Probe Inspect. 2, /23/2007 2, ,996.4 ATA 32 - LANDING GEAR NLG & MLG Trunnion Bolt & Drag Brace holes 8, , L/H MLG Shock Absorber Inspection 8, , R/H MLG Shock Absorber Inspection 8, , L/H MLG Drag Brace Inspection 8, , R/H MLG Drag Brace Inspection 8, , L/H MLG Axle & Torque Knee Inspect 8, , R/H MLG Axle & Torque Knee Inspect 8, , NLG Trunnion Shock Absorber Inspect 8, , NLG Drag Brace Inspection 8, , NLG Axle & Torque Knee Inspection 8, , NLG Actuator Clevis Inspection 1, ,000 L/H MLG Actuator Clevis Inspection 1, ,000 R/H MLG Actuator Clevis Inspection 1, ,000 L/H Brake Hose Replacement. 5 R/H Brake Hose Replacement. 5 2 of 6 4/9/2008
4 BFG Nose Wheel Corrosion Inspection Maintenance Sched. Ref. CMM Hours Cycles / # Since NDT #1 Wheel NDT Inspection CMM Total # Since NDT NDT Date #2 Wheel NDT Inspection CMM Total # Since NDT NDT Date #3 Wheel NDT Inspection CMM Total # Since NDT NDT Date #4 Wheel NDT Inspection CMM Total # Since NDT NDT Date HYDRAULIC LANDING GEAR ITEMS Landing Gear Hydraulic System Filter & O-ring Replacement. 1,200 1, NLG Replace Teflon Hoses L/H MLG Replace Teflon Hoses R/H MLG Replace Teflon Hoses MECHANICAL LANDING GEAR ITEMS NLG Actuator End Play Check 1, L/H MLG Actuator End Play Check 1, R/H MLG Actuator End Play Check 1, L/H MLG Mechanical Actuator Overhaul 8, R/H MLG Mechanical Actuator Overhaul 8, NLG Mechanical Actuator Overhaul 8, Landing Gear tor Overhaul 8, Landing Gear Retract Gear Box Insp 8, ATA 33 - LIGHTS Pilot's & Co-Pilots Fuel & LWR CB Panel Insp 12 12/4/2007 Edgelighted Panel Inspection. 2,000 4 Emer. Exit Signs Illum SP (Replacement) (Inspection) 7 1 MFG. Date Inspection Date 9/1/2004 ATA 34 - NAVIGATION Pilots Pitot/Static Sys Recertification Copilots Pitot/Static Sys Recertification FAR FAR Pilot's Trans FAR Cert. & Test 1MRKB 1/9/2007 Co-pilots Trans FAR Cert. & Test 1/9/2007 Pilots Altimeter FAR Certification. Co-Pilots Alt. FAR Certification. Standby FAR Altimeter 932 #1 Air Data FAR Comp. Cert. 1MRYJ #2 Air Data FAR Comp. Cert. 1N22P Total Hours Cycles Days 1, , /28/ /28/ /28/ /31/2008 1, 319 2, /28/ /31/2011 1MRKM 292 NDT Date of 6 4/9/2008
5 Maintenance Sched. Ref. Hours Cycles / Hours Cycles Days Air Data System For RVSM Compliant Aircraft-Airworthiness Inspection Aeromech RVSM STC Read Note ICA ICA requirements items 1-4 ST01278SE Aeromech RVSM STC Read Note ICA ICA requirements items 1-4 ST01070SE (PS835) - Periodic Check 6 (PS835) - Cap Test Pro Line ESIS PS835 - Periodic Check L /29/ /31/2008 Pro Line ESIS PS835 - Cap Test 12 1/29/ ATA 35 - OXYGEN Oxygen Bottle Hydro 36 8/23/ /31/2010 Composite Replace 15 8/31/ /31/2019 Oxygen Bottle Hydro 36 Light Weight Replace Oxygen Bottle Ltw. Regulators 9377 Overhaul 36 8/23/ /31/2010 Oxygen Bottle Std. Weight Hydro Oxygen Bottle Std. Regulator Overhaul Barometric Pressure Switch Check 12 12/4/ /31/2008 Oxygen Shut-off Valve O-ring Replace 2/2/ /28/2009 ATA 37 - VACUUM Instrument Air Filter Replacement ,364.0 ATA 52 - DOORS Cabin Door Fwd & Aft Side Latch Bolts Replace 4,341 Cabin Door Upper Hooks Replace Airstair Door 4,.0 Escape Hatches 4,.0 Cargo Door 1,000 Cargo & Airstair Cam Lock Actuator Cables B200C Only 8,000 ATA 53 - FUSELAGE Forward Pressure Bulkhead Inspect 2,500 1,841 2,500 Aft Fuselage & Aft Press Bulkhead Insp L/H Windshield Doublers & Clips Insp R/H Windshield Doublers & Clips Insp Exterior Skin Inspection. Fuselage Frame FS 84 - FS Inspect Frame Web FS FS 271 Inspect Cabin Door & Fuselage Frame Inspect Stringers FS 88 - FS 125 & Panel Brackets Fuselage Stringers 5-11Aft of Bulkhead AD Fuselage Stringers 8,9 & 10 aft of Bulkhead AD ,000 Stringer Cutouts - A/C w/ External Doublers AD ,500 Stringer Cutouts - A/C w/ Internal Doublers Stringer Cutouts - BB1463 thru BB-1471 AD ,500 2,500 Raisbeck Aft Body Strakes Inspection STC of 6 4/9/2008
6 ATA 55 - STABILIZERS Horizontal Stabilizer Replacement Vertical Stabilizer Replacement. ATA 56 - WINDOWS Maintenance Sched. Ref. Ch. 4 Ch. 4 Hours Cycles / 4 44, 4 44, Hours Cycles Days L/H Windshield Attach Screw Replace Ch. 4 R/H Windshield Attach Screw Replace Ch. 4 ATA 57 - WINGS Raisbeck Nacelle/Wing Locker Inspect STC 200 L/H Wing Bolt Torque Check 200 R/H Wing Bolt Torque Check 200 L/H Wing Ctr Section Bonded Panel Insp R/H Wing Ctr Section Bonded Panel Insp /23/2007 8/23/ , , /28/2009 2/28/2009 L/H OB Wing Spar Cap Visual Insp R/H OB Wing Spar Cap Visual Insp L/H Wing Clevis Fitting Inspection R/H Wing Clevis Fitting Inspection L/H Wing NDT Inspection R/H Wing NDT Inspection L/H Lower Fwd Bolt & Nut Replace R/H Lower Fwd Bolt & Nut Replace L/H Upper FWD & AFT, LWR AFT Replace R/H Upper FWD & AFT, LWR AFT Replace , 14, /29/0 2/29/0 L/H Lwr Fwd Spar Lugs NDT Inspect 1 14, 1.0 R/H Lwr Fwd Spar Lugs NDT Inspect 1 14, 1.0 L/H Outboard Wing Lwr FWD Spar Cap NDT 1 14, 1.0 R/H Outboard Wing Lwr FWD Spar Cap NDT 1 14, 1.0 L/H Wing Ctr Sec. Lwr Fwd Spar Cap NDT 18,000 17, 18,000.0 R/H Wing Ctr Sec. Lwr Fwd Spar Cap NDT 18,000 17, 18,000.0 Wing Center Section Belly Skin NDT 22,500 21, ,500.0 Wing Ctr Sec Lwr Aft Spar Cap NDT 27,000 26, 27,000.0 Wing Ctr Section Lwr Aft Spar Fitting NDT 27,000 26, 27,000.0 L/H OB Wing Panel Aft Spar Lwr Fitting NDT 27,000 26, 27,000.0 R/H OB Wing Panel Aft Spar Lwr Fitting NDT 27,000 26, 27,000.0 Wing to Fuselage Attach Angles Replace Ch. 4 30,000 29, 30,000.0 L/H Wing Lower Fwd Fitting Counterbores Read Note & Barrel nut holes eddy current. BB-2 thru ,200 R/H Wing Lower Fwd Fitting Counterbores Read Note & Barrel nut holes eddy current. BB-2 thru ,500 READ NOTES FOR THE FOLLOWING ITEMS L/H Wing Ctr Sec & OB Wing Replace Ch. 4 9,500 R/H Wing Ctr Sec & OB Wing Replace Ch. 4 9,500 L/H Wing Center Section Replacement. Ch. 4 18,000 R/H Wing Center Section Replacement. Ch. 4 18,000 L/H Wing Center Section Replacement Ch. 4 18,000 R/H Wing Center Section Replacement Ch. 4 18,000 L/H Outboard Wing Structure Replace Ch. 4 30,000 R/H Outboard Wing Structure Replace Ch. 4 30,000 5 of 6 4/9/2008
7 ATA 61 - PROPELLERS L/H Hartzell R/H Hartzell R/H McCauley ATA 71 - POWERPLANT Maintenance Sched. Ref. Hours Cycles / Hours Cycles Days Hartzell Steel Hub SL ,000 Hartzell Steel Hub SL ,000 L/H Hartzell HC-E4N-3G Hartzell Alum Hub HH-2115 SL , , , /28/2011 R/H Hartzell HC-E4N-3G Hartzell Alum Hub HH-2116 SL , , , /28/2011 L/H McCauley Hartzell Alum Hub SL , Hartzell Alum Hub SL , L/H Overspeed Woodward Gov Overhaul SB ,500 5, ,500.0 R/H Overspeed Woodward Gov Overhaul SB ,500 5, ,500.0 L/H Eng. Replace Flamm Fluid Hoses R/H Eng. Replace Flamm Fluid Hoses 5 5 L/H Eng. Vibration Isolator unt Insp. 4,000 3, 4,000.0 R/H Eng. Vibration Isolator unt Insp. 4,000 3, 4,000.0 ATA 76 - ENGINE CONTROLS Pedestal Power Lever Stop Pin Insp. 1, ,200.0 ADDITIONAL ICAs (add as needed) Raisbeck Ram Air Recovery Inspect ICA of 6 4/9/2008
8 - Left Engine Engine Position: Left Aircraft Engine Install: Engine Total Time: Registration No: Eng. Install: Engine Total Cycles: 659 Engine Engine Install: Aircraft Total Time: PCE-PJ0834 Engine del: Eng. Install: Aircraft Total Cycles: PT6A Inspections Comments Hours Cycles / Hours Cycles Days ATA 61 - PROPELLERS Primary Prop H Woodward SB Governor Overhaul. 4,500 3, ,500.0 ATA 72 - ENGINES P3 Air Filter Replacement ,000 Engine Driven Fuel Pump See Note # 1 3,0 2, ,0.0 Engine TBO See Note # 2 3,0 2, ,0.0 Hot Section Inspection See Note # 3 1,800 1, ,800.0 Engine Time Component Time Component Total Component Component Engine Installation Time Life Limit Time Hrs. Cyc. Hrs. Cyc. Hrs. Cyc. Hrs. Cyc. Hrs. Cyc. Hrs. Cyc. 1st Stage Compressor TXA1A nd Stage Compressor A001KP5Y rd Stage Compressor A001LNNC Impeller TXA1A CT Disk A001L8F st Stage PT Disk A001L6AD , ,000 2nd Stage PT Disk A001L61W , ,000 ATA 73 - ENGINE FUEL/CONTROL Fuel Nozzle Clean/Flow Acft. Phase 2 & ,164.0 ATA 79 - OIL Oil Filter Replacement Gearbox Scavenge Screen , ,000 Computer Tracked Total Engine Time Difference Computer Tracked Total Engine Cycles Difference 659 Comments See Note # 4 See Note # 6 See Note # 7 See Note # 8 NOTES: 1. Service Bulletin P&WC 3003R20 dated July 16, 2002 used for TBO. Due at Engine TBO- PT6A-38: 2000 Hrs.; -41: 2500 Hrs.; -41 Post SB 3075,3089,3097 Pre-SB 33: 3000 Hrs.; -41 Post SB 3089, 3097, 33: 30 Hrs.; -42: 3000 HRs.; -42 Post SB 33: 30 Hrs.; -42A: 30 HRS. 2. Service Bulletin P&WC 3003R20 dated July 16, 2002 used for TBO. PT6A-38: 2000 Hrs.; -41: 2500 Hrs.; -41 Post SB 3075, 3089, 3097, Pre-SB 33: 3000 Hrs. -41 Post SB 3089, 3097, 33: 30 Hrs.; -42: 3000 HRs.; -42 Post SB 33: 30 Hrs.; -42A: 30 HRS. 3. Service Bulletin P&WC 3003R20 dated July 16, 2002 used for Hot Section Inspection. PT6A-38: 1000 Hrs.; -41: 1250 Hrs.; -41 Post SB 3075, 3089, 3097 Pre-SB 33: 1500 Hrs.; -41 Post SB 3089, 3097, 33: 1800 Hr.; -42: 1500 Hrs.; -42 Post SV 33: 1800 Hrs.; -42A: 1800 Hrs. 4. P/N's , , , for PT6A-38, -41 Life Limit is Cycles. P/N's , for PT6A-41, -42 Life Limit is 5,500 Cycles. P/N Life Limit is 5000 Cycles. 5. P/N's , , for PT6A-38, -41 Life Limit is 30,000 Cycles. P/N for PT6A-41, -42, -42A Life Limit is Cycles. 6. P/N Life Limit is 12,000 Cycles. P/N Life Limit is Cycles. P/N's & Life Limit is Cycles. 7. P/N's , , Life Limit is 8,000 Cycles. P/N Life Limit is 4,500 Cycles. P/N Life Limit is 30,000 Cycles. 8. P/N's , , Life Limit is 8,000 Cycles. P/N Life Limit is 4,500 Cycles. P/N Life Limit is 30,000 Cycles. 9. Pratt & Whitney Canada SB 3002R dated September 03, 1975, Revised September 10, 2002 used for Rotor Components Service Life 1 of 1 4/9/2008
9 - Right Engine Engine Position: Right Aircraft Registration No: Engine PCE-PJ0833 Engine del: PT6A-42 Engine Install: Eng. Install: Engine Install: Eng. Install: Engine Total Time: Engine Total Cycles: 659 Aircraft Total Time: Aircraft Total Cycles: 659 Inspections ATA 61 - PROPELLERS Primary Prop H Governor Overhaul. ATA 72 - ENGINES P3 Air Filter Replacement Engine Driven Fuel Pump Engine TBO Hot Section Inspection 1st Stage Compressor TXA1A5105 2nd Stage Compressor A001KP5R 3rd Stage Compressor A001LNNB 3033 Impeller EAAA000H425 CT Disk A001L8F2 1st Stage PT Disk A001L8HC 2nd Stage PT Disk A001L61T ATA 73 - ENGINE FUEL/CONTROL Fuel Nozzle Clean/Flow ATA 79 - OIL Oil Filter Replacement Gearbox Scavenge Screen Comments Woodward SB See Note # 1 See Note # 2 See Note # 3 Acft. Phase 2 & 4 4,500 1,000 3, ,000 Hours Cycles / 3,0 1,800 1, ,800.0 Engine Time Component Time Component Total Component Installation Time Life Limit Time Hrs. Cyc. Hrs. Cyc. Hrs. Cyc. Hrs. Cyc. Hrs. Cyc Hours Cycles Days 3, , , ,000 4, ,0.0 3, , ,000 Engine Time Hrs. Cyc. Computer Tracked Total Engine Time Difference Computer Tracked Total Engine Cycles Difference Comments See Note # 4 30, ,000 See Note # 7 NOTES: 1. Service Bulletin P&WC 3003R20 dated July 16, 2002 used for TBO. Due at Engine TBO- PT6A-38: 2000 Hrs.; -41: 2500 Hrs.; -41 Post SB 3075,3089,3097 Pre-SB 33: 3000 Hrs.; -41 Post SB 3089, 3097, 33: 30 Hrs.; -42: 3000 HRs.; -42 Post SB 33: 30 Hrs.; -42A: 30 HRS. 2. Service Bulletin P&WC 3003R20 dated July 16, 2002 used for TBO. PT6A-38: 2000 Hrs.; -41: 2500 Hrs.; -41 Post SB 3075, 3089, 3097, Pre-SB 33: 3000 Hrs. -41 Post SB 3089, 3097, 33: 30 Hrs.; -42: 3000 HRs.; -42 Post SB 33: 30 Hrs.; -42A: 30 HRS. 3. Service Bulletin P&WC 3003R20 dated July 16, 2002 used for Hot Section Inspection. PT6A-38: 1000 Hrs.; -41: 1250 Hrs.; -41 Post SB 3075, 3089, 3097 Pre-SB 33: 1500 Hrs.; -41 Post SB 3089, 3097, 33: 1800 Hr.; -42: 1500 Hrs.; -42 Post SV 33: 1800 Hrs.; -42A: 1800 Hrs. 4. P/N's , , , for PT6A-38, -41 Life Limit is Cycles. P/N's , for PT6A-41, -42 Life Limit is 5,500 Cycles. P/N Life Limit is 5000 Cycles. 5. P/N's , , for PT6A-38, -41 Life Limit is 30,000 Cycles. P/N for PT6A-41, -42, -42A Life Limit is Cycles. 6. P/N Life Limit is 12,000 Cycles. P/N Life Limit is Cycles. P/N's & Life Limit is Cycles. 7. P/N's , , Life Limit is 8,000 Cycles. P/N Life Limit is 4,500 Cycles. P/N Life Limit is 30,000 Cycles. 8. P/N's , , Life Limit is 8,000 Cycles. P/N Life Limit is 4,500 Cycles. P/N Life Limit is 30,000 Cycles. 9. Pratt & Whitney Canada SB 3002R dated September 03, 1975, Revised September 10, 2002 used for Rotor Components Service Life 659 See Note # 6 30,000 See Note # 8 1 of 1 4/9/2008
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