(THIS FORM IS TO BE RETAINED IN THE AIRCRAFT LOG) AIRCRAFT MAKE / MODEL: Hawker 800A AIRCRAFT TIME IN SERVICE: 6484.0 AIRCRAFT REGISTRATION NUMBER: N803CE AIRCRAFT LANDINGS: 5457 AIRCRAFT SERIAL NUMBER: 258271 1. Complied with (A1 A6, B1-B12, C1-C12 and D1- D12) 300/600/1200/2400 Hour Inspection and (E1-E12, F1-F12, and G) 12/24/48 Month Routine Airframe Inspection in accordance with the Raytheon Aircraft Flexible Maintenance Schedule 2. Complied with No. 1 and No.2 Engine 150 to 200 and 300 to 400 hour inspection (057120, 057110). 3. Complied with the following APU Inspections in accordance with Hamilton Sundstrand SB-T-62T-49-77 Revision 10 dated August 29, 2005 and Customer supplied CAMP cards: a) 6 month / 125 hour / 250 cycle Inspection (490010) b) 6 month / 250 hour/ 500 cycle Inspection (490020) c) 12 month / 500 hour / 1000 cycle Inspection (490030) d) 12 month / 1000 hour / 2000 cycle Inspection (490040) 4. Complied with No.1 and No.2 Thrust Reverser 150 and 300 hour inspection in accordance with the Raytheon Aircraft Flexible Maintenance Schedule and using customer supplied CAMP cards. 781021 Inspect No.1 Engine thrust reverser (150-200) 781070 Inspect No.1 Engine thrust reverser (300-400) 781022 Inspect No.2 Engine thrust reverser (150-200) 781071 Inspect No.2 Engine thrust reverser (300-400) 5. Complied with the following Service Bulletins and Airworthiness Directives. a) 2006-12-20 to prevent loss of all primary electrical power, which could result in the airplane operating only under emergency power. b) SB 24-3793 dated May 1, 2006 Electrical Power Inspection and Replacement of UMA 100 Limiter 5.1 The following Mandatory Service Bulletins have been found to be (NOT APPLICABLE) a) 21-3377 Revision 1 Dated 7-1-00 AIR CONDITIONING - Installation Of Improved Air Conditioning Duct Sleeves And Clamps Mod. 25F963A Mod. 25F963B (A.D. 2001-13-05) (Not Applicable) b) 21-3414 Revision 1 Dated 7-1-00 AIR CONDITIONING - Removal Of Air Conditioning Duct Sleeve Bedding Strips Mod. 25G032A Mod. 25G032B Mod. 25F032C (A.D. 2001-13-05) (Not Applicable) c) 24-319 Dated 2-15-95 ELECTRICAL POWER Emergency Power Supply Unit To Revise Jet Pack Battery Output Voltage Monitoring. Mod 25A624A Effectivity: 258211 (Not Applicable By Serial Number) d) 31-3055 Revision 1 Dated 2-1-99 INSTRUMENTS - Removal Of The Fuel Flow Electrical Signal To The Fairchild F1000 Flight Data Recorder (FDR). (Not Applicable) e) 32-166 Dated 1-27-76 LANDING GEAR - Brake Control Valve - Failure Of Knife Edges (A.D. 77-13-02) (Not Applicable) f) 32-167 Dated 1-27-76 DUNLOP EMERGENCY BRAKE REDUCING VALVE - Failure Of Knife Edges (A.D. 77-13-11) (Not Applicable) g) 32-3386 Dated 6-1-00 LANDING GEAR - Main Landing Gear Door Uplock Thread Inspection (A.D. 2001-15-25) (Not Applicable By Serial Number) h) 33-3586 Revision 1 Dated 11-1-04 LIGHTS Pulselite System Bus Wiring Modification (Not Applicable) i) 33-3682 Dated 3-14-05 LIGHTS Reactivation Of Precise Flight Pulelite System (Not Applicable By Serial Number) j) 34-137 Dated 11-28-79 NAVIGATION - Introduction Of Revised Setting Module For Altitude Alerting Unit Mod. No. 7583 (Not Applicable) k) 35-A25 Dated 10-13-77 SUPPLY VALVE - Insecurity Of Threaded Insert In Gland Bush (A.D. 77-26-01) (Not Applicable) l) 35-3171 Dated 9-1-98 OXYGEN To Introduce Replacement Oxygen Fitting In Lieu Of Fitting Incompatible With The Oxygen System Effectivity: All (Not Applicable) m) 53-85 Revision 1 Dated 5-23-95 FUSELAGE - To Introduce Improved Fluid Drainage In The Fuselage. Mod.253566D (A/C S/N 258186 Only) (Not Applicable By Serial Number) 6. Complied with the following AFMS, NTM / NDT techniques. 320032 Inspect main landing gear fairing strut NTM 32-10-103 510003 Inspect flight compartment skin and window structure above windshields NTM 53-10-105A 520008 Main entrance door X-Ray NTM 52-80-102 550006 Elevators X-Ray the internal structure NTM 55-20-101 & 55-20-102 550011 Rudder X-Ray the internal structure NTM 55-40-101
570007 Inspect X-Ray wing bottom skins and stringers between the front and rear spars, rib 0 to rib1 and between the center spar and rear spar from rib 1 to rib 4 NTM 57-30-101 570014 Ailerons inspect hinge brackets NTM 57-50-107 570017 Inspect flap and flap vanes NTN 57-50-105, 106 570024 Inspect aileron horn balance weight NTM 57-50-107 7. Complied with the following Raytheon Aircraft Flexible Maintenance Schedule codes, customer supplied CAMP cards 120001 Lubricate area G-150 hour 240025 Inspect APU starter/generator 243002 No.2 Starter/Generator overhaul 32R123 Inspect and reshim main gear scissor links on all three gear 351061 Test passenger Oxygen masks 510002 Inspect font pressure bulkhead 510009 Inspect entry door surround 530001 Inspect skin exterior under the dorsal intake, forward of frame 19 530002 Inspect fuselage skin under wing-to-fuselage 530003 Inspect wing to fuselage attachment links, brackets and bolts 530011 Inspect left side front face of rear pressure bulkhead 550001 Inspect horizontal stabilizer to vertical stabilizer rear attachment fittings 550007 Inspect elevators 550008 Lubricate connecting rods, elevator trim tabs 550009 Inspect rudder 550010 Lubricate connecting rods, rudder trim tab and anti-servo tab 550015 Inspect elevator mass balance weights and spigots 570008 Inspect main landing gear and side stay attachment fittings 570009 Inspect wing top skin, left and right, in the area of the wing fence 570013 Inspect left lower, left upper, right lower and right upper airbrake 570012 Inspect wing rear spar, rear face 570015 Inspect ailerons 570016 Lubricate connecting rods, aileron trim and servo tabs 570028 Inspect wing leading edges (post mod 253538B) 570030 Inspect aileron at outboard hinge casting 579301 Inspect wing fairing (Avionics) seal 731120 Replace No.1 and No.2 fuel filters 243162 Check No. 3 battery electrolyte 243163 Check No. 4 battery electrolyte 243164 Check No. 5 battery electrolyte 256013 Inspect life vests 8. Removed, replaced, repaired, inspected and/or reinstalled the following items. a) Brake Assembly, No.1 removed P/N: AHA1897 S/N: YO23 installed P/N: AHA1897 S/N: QN162 reference FAA Form 8130-3 dated July 31, 2006, Tracking No.WO32187 b) Brake Assembly, No.2 removed P/N: AHA1897 S/N: SM039 installed P/N: AHA1897 S/N: ZV104 reference FAA Form 8130-3 dated July 11, 2006, Tracking No.WO31964 c) Fuel filter, No.1 and No.2 engine removed P/N: 897830-1 installed new P/N: same reference FAA Form 8130-3 dated March 13, 2006, Tracking No. 10362979 d) Oxygen Bottle, No.3 removed P/N: 176531-35 S/N: 366325 installed inspected P/N: same S/N: same reference FAA Form 8130-3 dated July 31, 2006, Tracking No.1 154039 Note: Next Hydro Test Due July 2011 e) Rods, thrust reverser left 4ea removed P/N: 5453003-7 installed inspected 4ea P/N: same f) Rods, thrust reverser right 4ea removed P/N: 5453003-7 installed inspected 4ea P/N: same g) Starter/Generator, No.2 removed P/N: 23080-064 S/N: 6141 installed overhauled P/N: 23080-064 S/N: 6141 reference FAA Form 8130-3 dated August 7, 2006, Tracking No. SE2R 74863 h) Switch, Cabin lighting removed P/N: HSP-017 S/N: 05952806 installed repaired P/N: same S/N: same reference FAA Form 8130-3 dated July 31, 2006, Tracking No. AI 39033 i) Switch, Cabin lighting removed P/N: HSP-018 S/N: 05953804 installed repaired P/N: same S/N: same reference FAA Form 8130-3 dated August 4, 2006, Tracking No. AI 39119 j) Switch, hydraulic reservoir over heat detector removed P/N: 150T283 S/N: 1277 installed inspected P/N: same S/N: same reverence FAA Form 8130-3 dated July 25, 2006, Tracking No. M4660-4 k) Windshield, Copilots A removed P/N: 24016-416 S/N: L351272 installed new P/N: 24016-416 S/N: L355447 reference EASA Form 1 dated July 1, 2006, Tracking No. 249506 l) Windshield, Copilots B removed P/N: 24016-92 S/N: 238752 installed new P/N: 24016-92 S/N: L355199 reference EASA Form 1 dated July 7, 2006, Tracking No. 249512 m) Battery, No.1 removed P/N: S/N: Installed new P/N: S/N: reference FAA Form 8130-3 dated, Tracking No. n) Battery, No.2 removed P/N: S/N: Installed new P/N: S/N: reference FAA Form 8130-3 dated, Tracking No.
o) Battery, No3 removed P/N: CA-126 S/N: 9703959 installed inspected P/N: same S/N: same reference FAA Form 8130-3 dated August 7, 2006, Tracking M4659 p) Battery, No4 removed P/N: CA-126 S/N: 9902756 installed inspected P/N: same S/N: same reference FAA Form 8130-3 dated August 7, 2006, Tracking M4659 q) Battery, No3 removed P/N: CA-126 S/N: 9902877 installed inspected P/N: same S/N: same reference FAA Form 8130-3 dated August 7, 2006, Tracking M4659 r) Controller, removed P/N: 7011345-901 S/N: 95050955 installed repaired P/N: same S/N: same reference FAA Form 8130-3 dated August 8, 2006, Tracking No. 300463557 s) Life Vest, P/N: P0201-105 S/N: A37724 inspected reference FAA Form 8130-3 dated August 2, 2006, Tracking No. AN16697 t) Life Vests, 7ea P/N: P0723E105P S/N: 33816, 33832, 33868, 33881, 33919, 33986 and 34011 inspected reference FAA Form 8130-3 dated August 2, 2006, Tracking No. AN16696 u) Life Vest, 2ea P/N: P01074-101 S/N: 271742 and 707755 inspected reference FAA Form 8130-3 dated August 2, 2006, Tracking No. 1000460 9. The following wing attaching links and bolts have been inspected reference FAA form 8130-3 dated July 24, 2006, July 25, 2006 and July 26, 2006 a) Left forward upper wing link bolt P/N: 25-8WS3109-3 b) Left forward inboard wing link bolt P/N: 25-8WS3107-1 c) Left forward lower wing link bolt P/N: 25-8WS3109-1 d) Left forward horizontal wing link P/N: 25-8WS3105-1 e) Left forward vertical wing link P/N: 25-8WS3101-1 f) Right forward wing link P/N: 25-8WS3103-1 g) Right forward upper wing link bolt P/N: 25-8WS3109-3 h) Right forward lower wing link bolt P/N: 25-8WS3109-3 i) Left aft upper wing link bolt P/N: 25-8WS3005-1 j) Left aft lower wing link bolt P/N: 25-8WS3005-1 k) Left aft wing link P/N: 25-8WS3003-1 l) Right aft upper wing link bolt P/N: 25-8WS3005-1 m) Right aft lower sing link bolt P/N: 25-8WS3005-1 n) Right aft wing link P/N: 25-8WS3003-1 10. This Aircraft is in compliance with all applicable Airworthiness Directives through Bi-Weekly 2006-16. NOTE: All components removed, replaced and/or reinstalled were rigged, operationally checked and leak checked in accordance with current revisions of the Hawker 800 Maintenance Manual, with respect to work performed, this aircraft is approved for return to service. For more information on work performed, reference Work Order No. M 4660, M4659, E, E and WO on file at this facility. (.Airframe Log- ) (MC-RSM-013A (Revision 2, 05/06)) 91.409 (f) (3) INSPECTION PROGRAM THE AIRCRAFT IS DETERMINED TO BE
(THIS FORM IS TO BE RETAINED IN THE ENGINE LOG) AIRFRAME HOURS: 6484.0 AIRFRAME LANDINGS: 5457 ENGINE MODEL: TFE731-5/-5AR/-5 ENGINE TIME: 6250.1 ENGINE SERIAL NUMBER: P-91653 (No.1) ENGINE CYCLES: 5208 1. Complied with No. 1 Engine 150 to 200 and 300 to 400 hour inspection. 2. Removed, replaced, repaired, inspected and/or reinstalled the following items. a) Fuel filter, No.1 and No.2 engine removed P/N: 897830-1 installed new P/N: same reference FAA Form 8130-3 dated March 13, 2006, Tracking No. 10362979 b) Adapter, Starter/Generator removed P/N: 3072869-2 NSN installed new P/N: same NSN reference FAA Form 8130-3 dated June 6, 2006, Tracking No. B0600667255 All Maintenance, Operational, Functional and Leak Checks were complied with in accordance with HS125-800 Maintenance Manual and 731-5R Light Maintenance Manual Report No. 72-02-75, Revision 3, dated January 16, 2004. For more information on work performed, reference Work Order No. M4660, M4669 on file at this facility. (.Engine- -Log- ) (MC-RSM-013B (Revision 2, 05/06)) 91.409 (f)(3) INSPECTION PROGRAM THE ENGINE IS DETERMINED TO BE
(THIS FORM IS TO BE RETAINED IN THE ENGINE LOG) AIRFRAME HOURS: 6484.0 AIRFRAME LANDINGS: 5457 ENGINE MODEL: TFE731-5/-5AR/-5 ENGINE TIME: 6052.2 ENGINE SERIAL NUMBER: P-91659 (No.2) ENGINE CYCLES: 5059 1. Complied with No.2 Engine 150 to 200 and 300 to 400 hour inspection. 2. Removed, replaced, repaired, inspected and/or reinstalled the following items. a) Fuel filter, No.1 and No.2 engine removed P/N: 897830-1 installed new P/N: same reference FAA Form 8130-3 dated March 13, 2006, Tracking No. 10362979 All Maintenance, Operational, Functional and Leak Checks were complied with in accordance with HS125-800 Maintenance Manual and 731-5R Light Maintenance Manual Report No. 72-02-75, Revision 3, dated January 16, 2004. For more information on work performed, reference Work Order No. M4660, M4669 on file at this facility. (.Engine- -Log- ) (MC-RSM-013B (Revision 2, 05/06)) 91.409 (f)(3) INSPECTION PROGRAM THE ENGINE IS DETERMINED TO BE
(THIS FORM IS TO BE RETAINED IN THE APU LOG) AIRFRAME HOURS: 6484.0 AIRFRAME LANDINGS: 5457 APU MODEL: T-62T-40C8D1 APU HOURS: 1440.9 APU SERIAL NUMBER: SP-E945336 APU STARTS 3660 1. Complied with the following APU Inspections in accordance with Hamilton Sundstrand SB-T-62T-49-77 Revision 10 dated August 29, 2005 and Customer supplied CAMP cards: a) 6 month / 125 hour / 250 cycle Inspection (490010) b) 6 month / 250 hour/ 500 cycle Inspection (490020) For more information on work performed, reference Work Order No. M4659, M4660 on file at this facility. (.APU Log- ) (MC-RSM-013C (Revision 2, 05/06)) 910409 (f)(3) INSPECTION PROGRAM THE APU IS DETERMINED TO BE