N100YC PC12/45/47 STATUS REPORT

Transcription

1 100 HOUR INSPECTION 150 N/A N/A N/A ANNUAL INSPECTION Jun-11 3-Jun-12-1 CHAPTER AIRWORTHINESS LIMITATIONS STRUCTURAL LIMITATIONS - Note SB applies to MSN 193 and Beyond flying hours or landings (whichever comes first) refer to Supplement Structural Inspection Document (SSID) at Para. 5 and 12-A A-280A-A. FUSELAGE AND ASSOCIATED STRUCTURE - PRE-SB FUSELAGE AND ASSOCIATED STRUCTURE - POST-SB NOT APPLICABLE AIRCRAFT IS PRE SB WING STRUCTURE PRE-SB WING STRUCTURE Post-SB NOT APPLICABLE AIRCRAFT IS PRE SB TAIL STRUCTURE PRE-SB TAIL STRUCTURE POST-SB NOT APPLICABLE AIRCRAFT IS PRE SB ENGINE ROTOR COMPONENTS SERVICE LIFE LIMITS- PRATT & WHITNEY CANADA SB (latest revision) SHAFT, COMPRESSOR ROTOR (P/N ) (S/N A000319X) SB ROTOR, COMPRESSOR 1ST STAGE (P/N ) (S/N A00048Y3) SB ROTOR, COMPRESSOR 2ND STAGE (P/N ) (S/N A0004A6K) SB ROTOR, COMPRESSOR 3RD STAGE (P/N ) (S/N 3H900) SB ROTOR, COMPRESSOR 4TH STAGE (P/N ) (S/N 4H005) SB IMPELLER, CENTRIFUGAL (P/N ) (S/N 4H458) SB DISK, COMPRESSOR TURBINE (P/N ) (S/N A0004NB6) SB DISK, POWER TURBINE 1ST STAGE (P/N ) (S/N A0004LTT) SB DISK, POWER TURBINE 2ND STAGE (P/N ) (S/N A0004FHM) SB ENGINE MOUNT FRAME - PRE SB ENGINE MOUNT FRAME - POST SB NOT APPLICABLE AIRCRAFT IS PRE SB ENGINE MOUNT FRAME - REPLACE ALL BOLTS, WASHERS AND NUTS PITCH TRIM ACTUATOR (P/N , S/N 196, ALT. P/N ) INSTALLED WITH TSN: 6948, CSN FLAP ACTUATOR (P/N; , 308,309) (BLACK ANODIZED) (RH OUTBD FLAP ACTUATOR ONLY, ALL OTHERS ARE P/N ) OXYGEN BOTTLE Sep Sep NLG DRAG LINK RH PART (P/N ) (PRE SB ) CARGO DOOR LOWER LUG FITTINGS (QTY 3) BACKREST TUBES ON CREW SEATS WITH RECLINE SYSTEM (SEAT P/Ns: ,112,121 AND 122) N/A N/A N/A 6/13/

2 BACKREST TUBES ON CREW SEATS WITHOUT A RECLINE SYSTEM (SEAT P/Ns: ,132,133 AND 134) CREW SEATS P/N: and 132 installed PITCH TRIM ACTUATOR ATTACHMENT PARTS, FAIL SAFE PLATES AND THEIR ATTACHMENT PARTS (IPC ) NOSE LANDING GEAR TORQUE TUBE (P/N: ) DOES NOT APPLY N/A BY P/N: MISCELLANEOUS LIMITATIONS COCKPIT SIDE WINDOWS AND CABIN WINDOWS - REPLACE IF CRACKED OR STRESS CRAZING CAN BE FELT. IF CHIPPED REFER TO DATA MODULE 12-A A-904A-A WINDSHIELD LH AND RH - IF CRACKED IN INNER LAMINATION -REPLACE HORIZONTAL STABILIZER TRIM - FUNCTIONAL TEST OF TRIM RUNAWAY AURAL WARNING SYSTEM (FAA CMR) REPLACE IF CRACKED OR STRESS CRAZING CAN BE FELT. IF CHIPPED REFER TO DATA MODULE 12-A A-904A-A Jun Jun NLG DRAG LINK RH PART (P/N OR ) Initial 2000 hrs 2500 landings (installed) whichever comes first, then 300 hrs or 400 landings whichever comes first FIRE EXTINGUISHER HYDROSTATIC TEST (I NSTALLED NEW UNIT ON 10/04/2011 WITH MANUFACTURE DATE: DEC ) Dec Dec OXYGEN BOTTLE HYDROSTATIC TEST & REGULATOR O/H - REFER TO LATEST AVOX SERVCE INFORMATION ON SIL LATEST REVISION ( May May PITCH TRIM ACTUATOR (P/N ) - OVERHAUL DOES NOT APPLY BY P/N INSTALLED PITCH TRIM ACTUATOR (P/N &.203) - OVERHAUL Sep Sep WING MAIN SPAR FASTENER HOLES STRAP RIB 6 - (See Notes 1 and 2 below) Eddy current inspection, AMM 12-A A-353D-A May NOTE 1: The inspection is applicable to all aircraft except MSN 170, 222, 233, 234, 237, 240, 244, 250, and 324 which have performed the inspection as part of a fleet leader inspection survey and aircraft that have performed Service Bulletin Revision 1 or later. NOTE 2: Wings with more than flying hours or landings, whichever comes first, must perfrom the inspection within the next 500 flying hours or 500 landings, whichever comes first. OVERHAUL AND REPLACEMENT SCHEDULE IF CRACKED IN INNER LAMINATION - REPLACE 24 -Electrical Power STARTER GENERATOR (P/N , ,, , , Jun GENERATOR 2 DRIVE ASSEMBLY AFT BEARING (PRE SB ) DOES NOT APPLY BY POST SB GENERATOR 2 DRIVE ASSEMBLY AFT BEARING (POST SB AND MSN ) Equipment and Furnishings 6/13/

3 ELT BATTERY - AFTER ONE HOUR OF USE OR AS SHOWN ON BATTERY LABEL May-09 5-Sep CREW SEAT CUSHION (P/N: 0A INSTALLED ON IPECO SEAT P/Ns: AND 136) DOES NOT APPLY BY SEAT P/N CREW SEAT BELTS Oct-11 4-Oct PASSENGER SEAT BELTS AND EXTENSIONS Oct-11 4-Oct FIRE EXTINGUISHER CONTENTS CHECK Fire Protection 12 3-Jun-11 3-Jun Flight Controls FLAP POWER DRIVE UNIT (P/Ns: AND 002) FLAP POWER DRIVE UNIT (P/Ns: ) DOES NOT APPLY BY PDU P/N FLAP LINEAR ACTUATORS (WHITE COLORED) (P/Ns: /303/304/305 AND 306) FLAP LINEAR ACTUATORS (BLACK COLORED) (P/Ns: /308 AND 309) (RH OUTBD FLAP ACTUATOR ONLY, ALL OTHERS ARE P/N ) FLAP FLEXIBLE DRIVE SHAFTS (P/Ns: / 204 / 205 AND 206) DOES NOT APPLY DOES NOT APPLY ENGINE DRIVEN PUMP Fuel Hydraulics HYDRAULIC POWER PACK Indicating/Recording CAWS CACU CLOCK BATTERY (2 YEARS INSTALLED) MSN 321 AND DOES NOT APPLY BY AIRCRAFT SERIAL NUMBER 61 -Propeller PROPELLER (REFERENCE HARTZELL SL 61) (INSTALLED) Oct Oct Power Plant ENGINE SHOCK MOUNT ASSEMBLIES - AT ENGINE OVERHAUL BUT NOT LATER THAN 5000 FLYING HRS Engine ENGINE OVERHAUL - REFER TO P&WC SB ENGINE ACCESSORIES - TBO hrs - REFER TO P&WC SB Engine Fuel and Control P3 AIR FILTER REF P&WC EMM FUEL PUMP OUTLET FILTER Oil OIL FILTER (PRE PWC SB 14267, & SB ) OIL FILTER (POST PWC SB 14267, & SB ) DOES NOT APPLY DOES NOT APPLY DOES NOT APPLY OIL COOLER - OVERHAUL OIL SYSTEM SERVICING REF; P&WC SB AND EMM SERVICE AS REQUIRED TIME LIMITED INSPECTION REQUIREMENTS 6/13/

4 AIRCRAFT - Do the corrosion inspection (ref.12-a a- 901A-A) (SEVERE CLIMATE CONDITIONS ) 6 26-Jan Jul CHAPTER 21- AIR CONDITIONING COLD AIR UNIT RE-OIL (REF 12-A A-902A-A) Nov HEAT EXCHANGER MATRIX INSPECTION/CHECK (REF. 12- A A-313A-A) Nov OVERTEMPERATURE SWITCH - REMOVE AND TEST (REF 12-A A-903A-A) (5 YEARS INSTALLED) Oct Oct DUCT OVERTEMPERATURE SWITCH: REMOVE AND TEST. (REF 12-A A-920A-A) Oct Oct WATER SEPARATOR CONDENSER CLEANING (REF 12-A A-250A-A) Nov SECONDARY HEATERS THERMAL PROTECTION SWITCHES (MSN WITHOUT A MODIFIED AUXILIARY HEATING SYSTEM) TEST (REF: 12-A A-903A-A) SECONDARY HEATERS THERMAL PROTECTION SWITCHES (MSN WITH A MODIFIED AUXILIARY HEATING SYSTEM) TEST (REF: 12-A A-903A-A) DOES NOT APPLY 600 DOES NOT APPLY CABIN ALTITUDE SWITCH - FUNCTIONAL TEST (REF 12-A A-903A) (5 YRS INSTALLED) Jun-11 3-Jun CABIN DIFFERENTIAL PRESSURE SWITCH - FUNCTIONAL TEST (REF 12-A A-903A-A) (5 YRS INSTALLED) Jun-11 3-Jun PRESSURIZATION OUTFLOW & SAFETY VALVE CLEAN REMOVE AND CLEAN (REF 12-A A-250A-A) Apr Apr PRESSURIZATION SYST: ADJUSTMENTS / TESTS (REF 12- A A-903A-A) Apr Apr VAPOR CYCLE COMPRESSOR MOTOR DRIVE BELT CHECK FOR TENSION (REF 12-A A-903A-A) VAPOR CYCLE COMPRESSOR MOTOR BRUSHES - BRUSH INSPECTION (REF 12-A A-313A-A) CHAPTER 22- AUTO FLIGHT SERVO MOUNT (PITCH, ROLL & YAW) CLUTCH CHECK (REF 12-A A-313A-A) Jun Jun CHAPTER 24- ELECTRICAL POWER NICAD BATTERIES OR BATTERIES (IF 2ND INSTALLED) (P/N; )REMOVE AND SERVICE (REF 12-A A-920A-A AND CMM) DOES NOT APPLY LEAD ACID BATTERY NICAD BATTERIES OR BATTERIES (IF 2ND INSTALLED) (P/N; )REMOVE AND SERVICE (REF 12-A A-920A-A AND CMM) DOES NOT APPLY LEAD ACID BATTERY 6/13/

5 LEAD ACID BATTERY OR BATTERIES IF 2ND BATTERY INSTALLED. REMOVE AND DO A CAPACITY CHECK (REF 12- A A-920A-A AND CMM) STC SA00776LA CONCORDE LEAD ACID BATTERY RG-380E/44 (Installed during production ) GILL BATTERY P/N , S/N G INSTALLED HRS. INITIAL 800 HR / 12 MTH THEN 400 HR / 6 MTH per GILL CMM Jan Apr STARTER-GENERATOR BRUSH WEAR CHECK - (REF 12-A A-313A-A) Nov GENERATOR 2 (P/N: MOD B) BRUSH CHECK (REF 12-A A-313A-A) DOES NOT APPLY DOES NOT APPLY DOES NOT APPLY GENERATOR 2 (P/N: MOD A OR C AND ABOVE ) BRUSH CHECK (REF 12-A A-313A-A) GENERATOR 2 DRIVE ASSEMBLY HOUSING (PRE SB ) INSPECTION/CHECK (REF 12-A A-313A-A) DOES NOT APPLY DOES NOT APPLY DOES NOT APPLY GENERATOR 2 DRIVE ASSEMBLY HOUSING POST SB and MSN ) INSPECTION/CHECK (REF 12-A A-313A-A) EMERGENCY POWER SUPPLY (IF INSTALLED) STC SA00296DE EMERGENCY POWER SYSTEM (Installed during production) REMOVE AND CAPACITY TEST (REF 12- A A-920A-A) May May-12-4 GENERATOR 1 AND 2 GROUND POINTS - EXAMINE CORROSION PROTECTION LAYER (REF 12-A A-A) May May CHAPTER 27- FLIGHT CONTROLS BONDING LEADS TO ALL FLIGHT CONTROL SURFACES - EXAMINE HOURS OR LANDINGS THEN HOURS OR LANDINGS FLIGHT CONTROL CABLES INCLUDING AUTOPILOT AND STICK PUSHER CABLES EXAMINE - (REF 12-A A- 313A-A) May May ELEVATOR CONTROL CABLES TENSION - CHECK AFTER REPLACEMENT OF ANY ELEVATOR CONTROL SYSTEM CABLES (AUTOPILOT, STICK PUSHER, AND OR ELEVATOR) (REF 12-A A-903A-A) AT NEXT SCHEDULED INSP. BUT NOT LATER THAN 150 HRS DOES NOT APPLY AT THIS TIME FLAP FLEXIBLE DRIVE SHAFTS - REMOVE, CLEAN, INSPECT AND LUBRICATE (POST SB )(P/Ns: AND 202) (REF 12-A A-902A-A) Sep FLAP ACTUATOR (WHITE COLORED) (P/NS: , 303, 304, 305 AND 306) LUBRICATE (REF 12-A A- 902A-A) Jun Jun FLAP ACTUATOR (BLACK ANODIZED) (P/NS: , 308 AND 309) LUBRICATE (REF 12-A A-902A-A) (RH OUTBD FLAP ACTUATOR ONLY, ALL OTHERS ARE P/N ) Jun Jun /13/

6 FLAP ACTUATOR (WHITE COLORED) (P/NS: , 303, 304, 305 AND 306) BACKLASH CHECK (REF 12-A A-313A-A) Jun Jun FLAP ACTUATOR (BLACK ANODIZED) (P/NS: , 308 AND 309) BACKLASH CHECK (REF 12-A A- 313A-A) (RH OUTBD FLAP ACTUATOR ONLY, ALL OTHERS ARE P/N ) Jun Jun FLAP ELECTRICAL SYSTEM (MSN PRE-SB27-013) DO FLAP ELECTRICAL SYSTEM MAINT PRACTICE TESTS (REF 12-A A-901A-A) May CHAPTER 28- FUEL FUEL LOW LEVEL WARNING SYSTEM - OPS TEST (MSN REF 12-A A-903A-A) MSN (REF 12-A A-903B-A) Oct Oct FUEL CROSS VENT AND OUTWARD CHECK VALVE - OPERATIONAL TEST (REF 12-A A-903A-A) Jan CHAPTER 30- ICE AND RAIN PROTECTION AIRFOIL DE-ICERS - APPLY AGEMASTER No. 1 REF MANUFACTURER INSTRUCTIONS Jan Jul CHAPTER 32- LANDING GEAR MAIN AND NOSE WHEEL BEARINGS - LUBRICATE (REF 12- A A-902A-A) (TIRE CHANGE OR 12MTH) Jun-11 3-Jun-12-1 MAIN LANDING GEAR AXLES AND BUSHES (PC12/45 AND /47 AC) INSPECTION/CHECK (REF 12-A A-313A) Jun Jun NOSE LANDING GEAR OVERHAUL HOURS OR LANDINGS THEN EVERY 8300 HOURS OR LANDINGS OR 6 YEARS NLG STEERING MECHANISM HOURS OR LANDINGS THEN EVERY 8300 HOURS OR LANDINGS OR 6 YEARS CHAPTER 34- NAVIGATION STATIC SYSTEM - SINGLE SYSTEM (REF 12-A A- 903A-A) DUAL SYSTEM STC SA00322DE 2ND PITOT - STATIC SYSTEM (Installed during production ) (REF 12-A A-903A-A) Sep Sep ALTIMETER - CHECK CALIBRATION (REF ) Sep Sep STANDBY MAGNETIC COMPASS - CHECK SWING (REF 12- A A-903A-A) Apr Apr ATTITUDE HEADING REFERENCE SYSTEM (AHRS) - CHECK SWING (REF 12-A A-903A-A) Apr Apr TRANSPONDER SYSTEM (SINGLE AND DUAL) - FUNCTIONAL TEST (REF 12-A A-903A-A) OR 12- A A-040A-A) Sep Sep PASSENGER OXYGEN MASKS - INSPECTION/CHECK (REF 12-A A-313A-A) CHAPTER 35- OXYGEN Jan Jan CHAPTER 52- DOORS 6/13/

7 PASSENGER / CREW DOOR PIANO HINGE - EDDY CURRENT HOURS OR LANDINGS THEN HOURS OR LANDINGS (REF 12-A A-353A-A) PASSENGER / CREW DOOR SKIN - EDDY CURRENT HOURS OR LANDINGS THEN HOURS OR LANDINGS OR 6 YEARS (REF 12-A A- 353A-A) CARGO DOOR PIANO HINGE EDDY CURRENT HOURS OR LANDINGS THEN HOURS OR LANDINGS (REF 12-A A-353A-A) CARGO DOOR SKIN - EDDY CURRENT HOURS OR LANDINGS THEN HOURS OR LANDINGS OR 6 YEARS (REF 12-A A-353A-A) PASSENGER / CREW DOOR EXAMINE WITH TRIM REMOVED (REF 12-A A-920A-A OR 12-A A-920A-A) TOP STEP AREA IF INSULATION MAT FOR CORROSION - CONTACT PILATUS FOR REPAIR IF FOUND. EXAMINE HINGES (REF 12-A A-313A-A) (SEVERE CORROSIVE ENVIROMENT) May May CARGO DOOR EXAMINE WITH TRIM REMOVED (REF 12-A A-920A-A OR 12-A A-920A-A) EXAMINE DOOR HINGE AND PINS (REF 12-A A- 313A-A) (SEVERE CORROSIVE ENVIROMENT ) May May CHAPTER 53-FUSELAGE FRONT PRESSURE BULKHEAD - EXAMINE WITH INSUALTION ON ENGINE AND COCKPIT SIDES REMOVED. (SEVERE CORROSIVE ENVIROMENT ) May May FUSELAGE INTERNAL BOTTOM SURFACE - EXAMINE FRAMES 10,21,24 36 AND FRAMES ADJACENT TO DOOR AND EMERGENCY EXIT WITH INSULATION REMOVED. (SEVERE CORROSIVE ENVIROMENT ) May May STRUCTURE AROUND WINDOWS - EXAMINE - (SEVERE CORROSIVE ENVIROMENT ) May May DOOR FRAMES & EMERGENCY EXIT FRAME - EXAMINE IF INSULATION INSTALLED IN DOOR FRAMES AND IS WET REMOVE AND DISCARD NO LONGER INSTALLED ON PRODUCTION. (SEVERE CORROSIVE ENVIROMENT ) May May REAR PRESSURE BULKHEAD - EXAMINE WITH TRIM REMOVED - (SEVERE CORROSIVE ENVIROMENT ) May May FRAME 40 - EDDY CURRENT INSPECTION - 12-A A-353A-A HOURS OR LANDINGS THEN HOURS OR LANDINGS CHAPTER 55-STABILIZERS HORIZONTAL STABILIIZER INTERNAL SURFACES AND HORIZONTAL /VERTICAL STABILIZER INTERFACE - EXAMINE AS FAR AS POSSIBLE WITH PANELS REMOVED (SEVERE CORROSIVE ENVIROMENT ) May May /13/

8 VERTICAL STABILIZER INTERNAL SURFACES - (SEVERE CORROSIVE ENVIROMENT ) May May VERTICAL STABILIZER FORWARD ATTACHMENT TO FRAME 40 - EDDY CURRENT INSPECTION - 12-A A-353A-A HOURS OR LANDINGS THEN HOURS OR LANDINGS - (MODERATE CORROSIVE ENVIROMENT ) RUDDER TRIM TAB - EXAMINE - 12-A A-310A-A HOURS OR LANDINGS THEN HOURS OR LANDINGS OR 6 YEARS CHAPTER 56-WINDOWS COCKPIT SIDE WINDOWS - INSPECTION/CHECK (REFER TO DM 12-A A-313A-A) May May CHAPTER 57-WINGS WING INTERNAL SURFACES & FLAP COMPARTMENT - EXAMINE AS FAR AS POSSIBLE WITH ALL PANELS REMOVED - (SEVERE CORROSIVE ENVIROMENT) May May LANDING GEAR COMPONENTS - EXAMINE ESPECIALLY MAIN AND REAR SPAR PARTS - (SEVERE CORROSIVE ENVIROMENT ) May May WING TO FUSELAGE ATTACHMENTS - EXAMINE ATTACHMENT FITTINGS WITH WINGS REMOVED (REF 12-A A-313A-A) Oct Oct AILERON TRIM TAB - EXAMINE (REF 12-A A- 310A-A) HOURS OR LANDINGS THEN HOURS OR LANDINGS OR 6 YEARS WING TIPS - EXAMINE (REF 12-A A-310A-A) HOURS OR LANDINGS THEN HOURS OR LANDINGS OR 6 YEARS WING SKIN AROUND DRAIN HOLES - EXAMINE (REF 12-A A-353A-A) HOURS OR LANDINGS THEN 2500 HOURS OR 3000 LANDINGS CHAPTER 61- PROPELLER PROPELLER LUBRICATE (REF 12-A A-902A-A) Jun Jun CHAPTER 71-Power Plant POWER PLANT - TORQUE LIMITER TEST PERFORMANCE TEST (REF 12-A A-903A-A TABLE 501) THIS IS PART OF POWER PLANT ANNUAL INSPECTION REQUIREMENTS Jun Jun OIL PRESSURE TRANSDUCER ELECTRICAL CONNECTOR (PRE-SB ) CLEAN (REF 12-A A-250A-A) DOES NOT APPLY DOES NOT APPLY DOES NOT APPLY ENGINE TORQUE AND STICK PUSHER TORQUE TRANSDUCER ELECTRICAL CONNECTOR - CLEAN (12-A A-250A-A) Jun Jun COMPRESSOR PERFORMANCE RECOVERY WASH (REF. 12-A A-250A-A) REF. P&WC EMM COMPRESSOR DESALINATION WASH - REF 12-A A- 250A-A AND REF P&WC EMM Apr May COMPRESSOR TURBINE DESALINATION WASH - REF 12-A A-250A-A AND REF P&WC EMM Apr May /13/

9 CHAPTER 72- Engine ENGINE HOT SECTION - (REF P&WC SB14603 LATEST REVN) ENGINE BORESCOPE - (REF P&WC EMM BLOCK 601) FIRST STAGE COMPRESSOR - EXAMINE (REF P&WC EMM ) POWER TURBINE BLADES - IN SERVICE INSPECTION (REF P&WC EMM BLOCK 601) PRE SB BLADES WITH MORE THAN 1500 HRS TSN EVERY 200HRS DOES NOT APPLY POST SB POWER TURBINE BLADES - IN SERVICE INSPECTION (REF P&WC EMM BLOCK 601) P0ST SB BLADES WITH MORE THAN 4000 HRS TSN EVERY 200HRS CHAPTER 73- Engine Fuel & Control FUEL PUMP INLET SCREEN - CLEAN (REF P&WC EMM ) FUEL PUMP COUPLING SHAFT (ONLY IF SUNDSTRAND FUEL PUMP INSTALLED) EXAMINE FOR FRETTING CORROSION N/A BY ARGO TECH PUMP INSTALLED FUEL MANIFOLD ADAPATOR AND NOZZLE ASSEMBLIES - EXAMINE (REF P&WC EMM TABLE 602) Jun P3 AIR FILTER - CLEAN (REF P&WC EMM ) CHAPTER 74- Ignition SPARK IGNITERS - EXAMINE (REF 12-A A-920A- A AND P&WC EMM ) Jun Jun CHAPTER 76 - Engine Controls PROPELLER FEATHERING MICROSWITCHES - FUNCTIONAL TEST (REF 12-A A-903A-A) Jun Jun CHAPTER 79 - Oil REDUCTION GEARBOX CHIP DETECTOR AND ACCESSORY GEARBOX CHIP DETECTOR IF POST SB INSPECT (REF 12-A A-920A-A AND P&WC EMM ) Jun Jun SUMMARY OF AIRCRAFT - CORROSION INSPECTIONS (SEVERE 2000 HRS / 24 MONTH ) (MODERATE 4000 HRS / 48 MONTH) (MILD 6000 HRS / 72 MONTHS) AIRCRAFT EXTERIOR CORROSION INSPECTION 6 26-Jan Jul AIRCRAFT INTERIOR CORROSION INSPECTION 12 3-Jun-11 3-Jun-12-1 PASSENGER DOOR May May CARGO DOOR May May FRONT PRESSURE BULKHEAD May May FUSELAGE INTERNAL BOTTOM SURFACE May May STRUCTURE AROUND WINDOWS May May DOOR FRAMES & EMERGENCY EXIT FRAME May May REAR PRESSURE BULKHEAD May May HORIZONTAL STAB INTERNAL SURFACES/INTERFACES May May VERTICAL STABILIZER INTERNAL SURFACES May May WING INTERNAL SURFACES & FLAP COMPARTMENT May May /13/

10 LANDING GEAR COMPONENTS May May INSTALLATIONS / MODIFICATIONS / ALTERATIONS STC SA00322DE 2ND PITOT - STATIC SYSTEM (Installed during production ) Sep Sep STC SA00296DE EMERGENCY POWER SYSTEM (Installed during production ) 12 3-Jun-11 3-Jun-12-1 STC SA00776LA CONCORDE LEAD ACID BATTERY RG- 380E/44 (Installed during production ) GILL BATTERY P/N , S/N G INSTALLED HRS. INITIAL 800 HR / 12 MTH THEN 400 HR / 6 MTH per GILL CMM Nov May STC SA00297DE COPILOT FLIGHT INSTRUMENTS (Installed during production ) 10-Nov-11 KING KCS-55A COMPASS SYSTEM AND KI525A - H S I (Installed Nov. 10, 1999) Field Approval NO RECURRING MAINTENANCE REQUIREMENTS BF GOODRICH SKYWATCH SKY497 SYSTEM (Installed Nov. 10, 1999). Ref. SKY497 INSTALLATION MANUAL P/N Field Approval 12 3-Jun-11 3-Jun-12-1 TOWBAR and FUEL SAMPLER HOLDER (Installed Nov. 11, 1999) Ref. Drawing PC12030, PC12031A and , Dated June 25, Jun-11 3-Jun-12-1 STC SA00886WI-D BENDIX/KING KGP-560 GA-EPGWS TERRAIN WARNING SYSTEM (Installed Dec. 21, 2004 ) FOLLOW ON STC 12 2-Jun-11 2-Jun-12-2 KANNAD 406 Mhz EMERGENCY LOCATING TRANSMITTER (Installed May 15, 2008 ). Field Approval ref. FAR (c)(d) 12 3-Jun-11 3-Jun-12-1 SARSAT BEACON REGISTRATION (NOAA) May May PAINT CODES P/N MFG: Acry-Glo Medium Concord Blue HT10717 MFG: Acry-Glo Cobolt Blue HT10593 MFG: Acry-Glo Las Vegas Gold HT10494 INTERIOR CODE: EX-6S-2 6/13/