1991 BEECHCRAFT BONANZA A36 N77PG S/N E-2680

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1 1991 BEECHCRAFT BONANZA A36 N77PG S/N E-2680 Airframe, Engine & Prop Logs, AD List, Form 337s Airworthiness Certificate Weight & Balance Exclusively offered by Shoreline Aviation, Inc JETS (5387) shorelineaviation.net

Engine Total Time Since New 1195 TSTOH, Factory Cylinder Assemblies 142 Prop Total Time Since New 1195 Prop Total Time Since Overhaul 105 1991 BEECHCRAFT A36 BONANZA N77PG Serial# E-2680 AVIONICS

2 Engine Total Time Since New 1195 TSTOH, Factory Cylinder Assemblies 142 Prop Total Time Since New 1195 Prop Total Time Since Overhaul BEECHCRAFT A36 BONANZA N77PG Serial# E-2680 AVIONICS King Silver Crown equipped (Avionics by Beechcraft) Garmin GNS 430 GPS King KMA-24 Audio Panel w 3LMB King K-65 NavComm King KN-63 DME King KR-87 ADF w King KI-227 (Slaved Heading Card) ADF Indicator King KT-79 Transponder King KEA-130 Encoding Altimeter King KFC-150 Autopilot/Flight Director w Slaved HSI and Compass System & Yaw Damper King KAS-297 Altitude Alert and Preselect System 3M W1000 Stormscope OPTIONS 3 Blade HOT PROP Ventilation Blower Shadin Mini Flow Computer Isocom 4-place Intercom System 3 Light Strobe System Ground Clearance Switching Super Soundproofing Club Seating Tannis Engine Heater w Cover Standby Pressure System Co-Pilot Altimeter Standby Generator Co-Pilot DG 100 amp Alternator Co-Pilot Artificial Horizon Hobbs Meter Co-Pilot Brakes Heated Pitot JPI EDM 700, with Fuel Flow Rosen Sun Visors GAMI Fuel Injectors Executive Writing Desk Map Light Internally Lighted Instruments True Airspeed Indicator King KFC-150 Yaw Damper ELT, 406 MHz Winter Baffles Beryl D'Shannon molded Engine Baffles upgrade kit Exterior: Allover Matterhorn White, Regal Blue and Velvet Black and Chamois Trim, Freshly Waxed Interior: Buff Leather Seat and Sidewall Trim, Spotlight Lightwaves Fabric Seat Inserts, Ocean Leather Horizontal Trim Panel, Beige Velvet Carpet & Scuff Area. Club Seating With Executive Writing Desk. Interior Is In Excellent Condition. New Headliner Installed by Beech 815 Hours Total Time Airframe. Comments: Annual Inspection Completed 8/16, Next Due 8/17. IFR Certification Due 9/18. This Low Time A36 Shows Beautifully! Price: $229,000 US- Specifications Subject To Verification By Inspection CONTACT: ANN POLLARD MOBILE: OFFICE: Marshfield Airport KGHG 93 Old Colony Lane Marshfield, MA

73 Page 1 of 3 N77PG 09/29/2016 AD NOTES COMPLIANCE RECORD Airframe - Hawker Beechcraft Corporation - A36 s/n: E-2680 Propeller - McCauley - D3A32C409 s/n: Appliance - Air Filter - Paper Induction Appliance - Governors - McCauley m/n: D s/n: Appliance - Ignition Switches - Bendix Appliance - Safety Belts - Davis FDC6400 Series Appliance - Safety Belts - AM Safe p/n: Appliance - Autopilots - King KFC-150 Appliance - GPS - Garmin GNS 430 Date & AD# Applicable S.B. # & Subject Method of Compliance Comp. Recurring One Time Next Hrs/Date Authorized Signature & Number Center seat tracks DNA per serial # R1 Security of control wheel DNA per serial # Engine fuel interruption DNA per serial # Landing gear uplock rollers Superceded by Landing gear strut piston DNA per serial # Landing gear shock piston DNA per serial # Aft facing seats DNA per serial # Strobe light system DNA per serial # Engine Oil DNA - affected STC is not installed R1 Y type shoulder harness DNA per serial # Screws in control system DNA per serial # Emergency egress provisions DNA per serial # R1 Seat recline actuator handle DNA per serial # Firewall material DNA per serial #.

74 Page 2 of 3 N77PG 09/29/2016 Date & AD# Applicable S.B. # & Subject Method of Compliance Comp. Recurring One Time Next Hrs/Date Authorized Signature & Number Seat tracks DNA per serial # Elevator trim tab actuators DNA per serial # Shoulder harnesses Superseded by Fresh air blower housing DNA per serial # Wing spar frame cracks Superceded by Forward rudder spar cracks Superceded by Landing gear circuit 3/19/93 - C/W Beech SB Page See Airframe Log # Loran deviation signal 3/16/93 - Complied with Beech SB Page See Airframe Log Rudder spar cracks DNA per serial # Spar failure DNA per serial # Door handle's lock release button 11/13/97 - Inspected door handles per Beech SB no defects noted. See airframe Log R1 Lack of fuel flow to the engine This AD has been withdrawn Flight control mechanism DNA per serial # Inspect for the installation of firewall sealant and install DNA per serial #. firewall sealant Correct the misrouted rudder control cable DNA per serial # Install missing rivets in the right hand fuselage panel Superceded by Prevent the tailpipe from detaching from the turbocharger DNA - affected STC is not installed Protect the blower motor circuit 5/13/99 - New 1 amp avionics circuit breaker installed. page See airframe log Prevent separation of the flap flex shaft assembly DNA per serial #. Also, no affected flap drive cables were installed during the dates listed in the AD CORRECTION - Detect and correct missing rivets in the 01/06/01 - Inspected fuselage rivets per Beech SB page 50 right hand fuselage panel assembly and added three rivets found not installed. See airframe log Decrease the possibility of gear-up landings caused by DNA per serial #. seizure of the uplock rollers To prevent failure of the circuit breaker toggle switch 4/21/09 - Installed all new circuit breaker/switches

75 Page 3 of 3 N77PG 09/29/2016 Date & AD# Applicable S.B. # & Subject Method of Compliance Comp. Recurring One Time Next Hrs/Date Authorized Signature & Number To detect and correct an incorrect washer installed in the pilot and copilot shoulder harnesses DNA per serial # AM Safe restraint system DNA per part # of the installed shoulder harnesses King Radio autopilots DNA per serial # King Radio autopilots DNA - affected STC is not installed Bendix flight control systems DNA per aircraft model Prevent external noise to the GNS 430 units course DNA per serial #. deviation indicator (CDI) Paper induction air filters 2/3/ New air filter installed. John E. Sheehan A&P IA McCauley governors DNA per prop. gov. model # Bendix switches DNA - TCM igition switch installed R1 Bendix switches DNA - TCM ignition switch installed Davis Safety belts DNA per seat belt model # R1 Davis safety belts DNA per date of mfg Davis safety belts DNA - installed belts are 45 degree release Maintenance by T&W Propellers Inc. DNA - propeller not returned to service by T&W Propeller Maintenance by Southern California Propeller Service DNA - propeller not returned to service by So. Cal. Propeller To detect unsafe conditions that could result in a propeller DNA - propeller not returned to service by Oxford blade separating from the hub and loss of control of the Propeller in the UK. airplane To prevent blade or hub failure that could result in separation of a propeller 8/9/ Placarded panel per para. (f). Completed blade insp. per para. (h)(1) - no defects noted. Para (h)(3) due ea. 100 hrs. or next Annual - whichever is first. Para. (h)(2) due at next prop. O/H or major disassembly. Para. (h)(4) hrs (remove prop. from service). see mothod of compliance

76 Page 1 of 3 77PG 09/29/2016 AD NOTES COMPLIANCE RECORD Engine - Continental Motors - IO-550-B s/n: Appliance - Connecting Rods - Engine Components Incorporated (ECi) Appliance - Cylinder assembly - Superior Air Parts Appliance - Cylinder assembly - Engine Components Incorporated (ECi) Appliance - Magnetos - Slick L & R m/n's: 6310 L s/n: R s/n: Appliance - Pistons - Superior Air Parts Date & AD# Applicable S.B. # & Subject Method of Compliance Comp. Recurring One Time Next Hrs/Date Authorized Signature & Number CORRECTION - To prevent fatigue failure of the connecting rod and a possible uncommanded shutdown of the engine Cylinder assemblies To prevent cylinder separation that can lead to engine failure R1 To prevent cylinder separation that can lead to engine failure To prevent loss of engine power due to cracks in the cylinder assemblies To prevent loss of engine power due to cracks in the cylinder assemblies To prevent loss of engine power due to cracks at the head-to-barrel interface in the cylinder assemblies and possible engine failure caused by separation of a cylinder head To prevent loss of engine power due to cracks at the head-to-barrel interface and possible engine failure caused by separation of a cylinder head Slick magnetos DNA - affected engine parts are O.E.M. DNA - affected engine parts are O.E.M. DNA - affected engine parts are O.E.M. DNA - affected engine parts are O.E.M. Superseded by DNA - affected engine parts are O.E.M. Superseded by DNA - affected engine parts are O.E.M. DNA per magneto model #'s Slick magnetos DNA per magneto part #'s Slick magnetos DNA per magneto part #'s Magneto impulse coupling DNA per engine model # To prevent engine failure due to migration of the magneto DNA per engine model #. impulse coupling stop pin

77 Page 2 of 3 77PG 09/29/2016 Date & AD# Applicable S.B. # & Subject Method of Compliance Comp. Recurring One Time Next Hrs/Date Authorized Signature & Number PMA approved pistons DNA - affected engine parts are O.E.M PMA piston pin DNA - affected engine parts are O.E.M R3 Cylinder assemblies DNA per serial # Starter adaptor shaftgear DNA - affected component (freon compressor) not installed Oil filter DNA - affected component (TCM "Protech" oil filter) not installed Starter adapter shaftgear DNA - affected component (freon compressor) not installed Champion oil filter DNA per oil filter part # Incorrect oil pick-up tube DNA per serial # Cylinder valve retainer DNA per date of mfg. DNA per serial # Fuel pumps DNA per serial #. DNA per date of mfg. PL Exhaust roller rocker arms DNA - affected STC is not installed. PL Crankshaft failure Superceded by Crankshaft failure DNA per serial #. DNA per date of mfg. PL Crankshaft connecting rod journal fracture Superceded by Fracture of the crankshaft connecting rod journal DNA per engine and crankshaft serial #'s Prevent loss of engine power DNA - affected engine parts are O.E.M To prevent the separation of the cylinder head DNA - affected engine parts are O.E.M Correction - To prevent loss of engine power due to cracks 09/17/09 - R+R #4 cylinder - see log entry. No other affected in the cylinder head, possible engine failure, and fire in the cylinders found to be installed. engine compartment To address rapid wear on the face of hydraulic lifters Superseded by To prevent excessive hydraulic lifter wear DNA - no affected lifters were installed during the dates listed in the A.D To prevent an in-flight shutdown due to a failed fuel servo DNA-affected engine part is OEM Thomas D. Hall diaphragm IA

78 Page 3 of 3 77PG 09/29/2016 Date & AD# Applicable S.B. # & Subject Method of Compliance Comp. Recurring One Time Next Hrs/Date Authorized Signature & Number Superior Air Parts Investment Cast Cylinder Assemblies DNA - affected engine parts are O.E.M.

97 1991 BEECHCRAFT A36 BONANZA N77PG S/N E-2680 Airworthiness Certificate Weight & Balance SPECIFICATIONS AND RECORDS SUBJECT TO VERIFICATION BY INSPECTION

98 SPECIFICATIONS AND RECORDS SUBJECT TO VERIFICATION BY INSPECTION

99 74 GALLONS USABLE FUEL

100 SPECIFICATIONS AND RECORDS SUBJECT TO VERIFICATION BY INSPECTION

101 SPECIFICATIONS AND RECORDS SUBJECT TO VERIFICATION BY INSPECTION

102 SPECIFICATIONS AND RECORDS SUBJECT TO VERIFICATION BY INSPECTION

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1976 CESSNA 421C N98522

1976 CESSNA 421C N98522 IDENTIFICATION Year Mfr/Dlv 1976 / 1976 Registration # N98522, Expires 10/31/19 Purchase Date 3/20/08 Location PTK/KPTK/Oakland County International Airport, Pontiac, M-U.S. STATUS FOR SALE, ASKING: $345K