Tecnam P2010 Aircraft Maintenance Manual 1st Edition Rev 4 (Doc. 2010/101)

Description

Tecnam P2010 Aircraft Maintenance Manual 1st Edition Rev 4 (Doc. 2010/101)

The Tecnam P2010 Aircraft Maintenance Manual 1st Edition Rev 4 (Doc. 2010/101) is the ATA Specification 100 maintenance publication issued as Doc.No.2010/101 by Costruzioni Aeronautiche TECNAM srl. Revision 4 of the first edition is dated 7 August 2020. Technical content is approved under the authority of DOA Ref. EASA.21J.335. The manual gives systems description so a maintenance crew can learn the airplane and the scheduled and unscheduled tasks needed to keep a P2010 airworthy.

File Details

• Manual type: Aircraft Maintenance Manual (AMM)
• Brand / model: Tecnam P2010
• Document number: Doc.No.2010/101
• Edition / revision: 1st Edition – Rev. 4
• Publication date: 7 August 2020
• Language: English
• Page count: 1745
• File format: PDF

Airplane and Powerplant Coverage

The P2010 is a strut-braced high-wing, four-seat, single-engine airplane with fixed tricycle landing gear. Fuselage and fin structures are carbon-fibre composite. Wings, horizontal tail, ailerons, flaps, rudder and the internal landing-gear attachment beams are aluminium alloy. Each wing attaches with two bolts and a single strut. Integral fuel tanks sit in the wing boxes behind the main spar at 120 litres per side (240 litres total), with 4.06 litres unusable in each tank (8.12 litres total unusable).

Baseline engine data in the Tecnam P2010 Aircraft Maintenance Manual 1st Edition Rev 4 (Doc. 2010/101) is the Textron Lycoming IO-360-M1A: fuel-injected, direct-drive, four-cylinder horizontally opposed, air-cooled, 361 cubic inches, 5.125 in bore, 4.375 in stroke, 8.5:1 compression, 134.0 kW (180 hp) at 2700 rpm continuous. The standard propeller is the MT Propeller MT-188R-145-4G two-blade fixed-pitch unit, 1880 mm diameter, laminated-wood body with epoxy fiberglass and a stainless-steel leading-edge sheath. Maximum take-off weight is listed as 1160 kg (2557 lb), baggage 40 kg (88 lb), wingspan 10.3 m, length 7.97 m, height 2.64 m, wing area 13.9 m².

Chapter 93 supplements cover later design changes embodied on individual airplanes: variable-pitch propeller (2010/002), alternative avionics (2010/003), Garmin GFC 700 autopilot (2010/001), new seats (2010/045), Lycoming IO-390-C3B6 215 hp engine with Garmin G1000 NXi and related nacelle, oil cooler, exhaust and MT propeller changes (2010/078), GFC 700 on IO-390 aircraft (MOD2010/133), G1000 NXi on IO-360 aircraft (2010/136), and the 14 000 ft maximum operating altitude increase with continuous-flow oxygen equipment (MOD 2010/194). Engine overhaul and detailed internal engine work remain in the applicable Lycoming manuals referenced throughout.

Chapters Covered

• 01 Introduction — foreword, ATA breakdown, abbreviations, occurrence reporting
• 02 Conversion charts — factors and litre/US gallon, in-lb/Nm and ft-lb/Nm tables
• 03 Airplane general description — structure, engine/propeller, landing gear, fuel, brakes, pitot-static, general features
• 04 Airworthiness Limitations (EASA approved) — life-limited items and NDI intervals
• 05 Time Limits and Maintenance Schedule — replacement/overhaul limits, inspection program, lubrication, unscheduled inspections (lightning, hard landing, overweight)
• 06 Dimensions and Inspection Caps — three-view dimensions, access panels, engine cowling
• 07 Jacking — jack points and adapters
• 08 Leveling and Weighing — longitudinal/lateral level, weighing record
• 09 Towing and Taxiing
• 10 Parking, Mooring, Storage and Return to Service
• 11 Placards and Markings — exterior and interior identification
• 12 Servicing — fuel, oil, battery, seats, brake fluid, cleaning
• 20 Standard Practices – Airframe — torque values, control-cable tension
• 21 Heating and ventilation — cabin heat, defrost, cold-air diffusers
• 22 Autopilot — GFC 700 description, servos, cable tension (supplements)
• 23 Communications
• 24 Electrical system — 28 Vdc busses, alternator, battery, relays
• 25 Equipment and furnishings — seats, belts, ELT, first-aid kit, cabin panels
• 26 Fire protection — extinguisher and engine-bay fire protection
• 27 Flight controls — aileron, flap, stabilator trim, rudder, travel limits, balancing
• 28 Fuel system — tanks, pumps, selector, quantity senders, gascolator, vents
• 30 Ice protection — LH pitot heat
• 31 Indicating system — instrument panel and Garmin EIS
• 32 Landing gear system — MLG leaf springs, NLG, wheels/tires, hydraulic brakes
• 33 Lights — interior, NAV/strobe, landing/taxi
• 34 Navigation — pitot-static, Garmin G1000 / G1000 NXi LRU removal, software, leak tests
• 51 Standard Practices and Structures — materials chart, composite/metal repair limits, sealants
• 52 Doors — cabin doors, emergency exits, baggage door
• 53 Fuselage — composite shells, vortex generators, Level 1/2 inspections
• 55 Stabilator and Rudder — removal, installation, travel
• 56 Windows — windshield and side-window replacement/repair
• 57 Wings — wing/aileron/flap removal, strut joints, eddy-current inspection
• 61 Propeller — fixed-pitch and variable-pitch MT units, governor
• 71 Power Plant — cowlings, engine mount, air intakes/filter, drains
• 72 Engine — IO-360-M1A and IO-390-C3B6 removal/installation, preservation
• 74 Ignition — switches and reference to Lycoming ignition work
• 78 Exhaust — pipes, muffler, heat exchanger
• 79 Oil system — tank, cooler, filter, breather (including MOD 2010/178 cooler support)
• 80 Starting
• 92 Wiring diagrams — installation rules and drawing appendix
• 93 Supplements S1, S2, S3, S5, S6, S12, S13, S16

Taken as a whole, the Tecnam P2010 Aircraft Maintenance Manual 1st Edition Rev 4 (Doc. 2010/101) is the airframe and installed-systems shop book: description and operation, troubleshooting blocks, and maintenance practices for structure, flight controls, landing gear, fuel, electrics, avionics and powerplant interfaces, plus the inspection calendar and EASA-approved airworthiness limitations. Vendor CMMs and the Lycoming/MT Propeller manuals remain the source for internal engine and propeller overhaul.

Scheduled Inspections and Structural Checks

Chapter 05 sets replacement and overhaul times and the recurring inspection program, including lubrication charts and gascolator frequency. Chapter 04 (EASA approved) includes high-frequency eddy-current inspection of the wing-strut joints and wing front-spar area at the stated interval. Composite fuselage work is split into Level 1 and Level 2 inspections in Chapters 05-40 and 05-50, with ultrasonic guidance and allowed-repair limits in Chapter 51. Unscheduled inspections cover lightning strike, hard landing and similar events, with engine follow-up directed to the Lycoming manuals.

Servicing chapters walk through refuelling and tank drainage, approved fuels for the IO-360-M1A (Lycoming SI 1070 series, including AVGAS 100LL and listed MOGAS grades) and AVGAS 100LL for the IO-390-C3B6, oil change and filter replacement, Gill Teledyne G-247 battery service, brake-reservoir level, seat removal and cleaning, and engine/airframe cleaning. Jacking, leveling, weighing (datum at the leading-edge vertical), towing, mooring and storage/return-to-service procedures sit in Chapters 07–10.

IMAGES PREVIEW

Systems Work a Technician Will Actually Perform

Flight-control practices give aileron travel UP 19° / Down 14° (±2°), flap travel UP 0° / Down 40° (±1°), cable-tension values in pounds, turnbuckle safety wiring, and aileron balancing after repair or paint. Landing-gear practices cover MLG and NLG removal, leaf-spring and damper work, 6.00-6 main tires at 36 psi (2.5 bar), brake bleed/fill, parking-valve replacement and NLG pivot-friction check. Fuel-system practices cover quantity-sender replacement with PR 1776 B2 tank sealant, electric and engine-driven pumps, selector valve, vents and internal tank inspection through the upper caps.

The 28 Vdc electrical system uses Essential, Main and Avionic busses, a Kelly Aerospace ALU-8521LS 24 V / 70 A belt-driven alternator with Plane-Power R1224 regulator, and a 24 V 19 Ah Gill-Teledyne G-247 battery. Practices include alternator and V-belt work, battery removal through the baggage compartment, and relay replacement. Navigation and indicating chapters document Garmin G1000 GDU 1040 installations and, in the supplements, G1000 NXi GDU 1050/1054 suites, GIA 63W/64W, GDC air-data computers, GMU 44, GEA 71/71B, pitot-static leak tests and software/configuration loading. Autopilot supplements add GSA 80/81 roll, pitch and pitch-trim servos, TO/GA switch work and servo-cable tension.

Keep the P2010 Airworthy With Documented Procedures

Use the Tecnam P2010 Aircraft Maintenance Manual 1st Edition Rev 4 (Doc. 2010/101) when you need the published travel limits, torque values, inspection intervals, fuel and oil servicing steps, structural NDI, landing-gear and control-system R&I, electrical and Garmin LRU practices, and the supplement data that matches a modified airplane. Working from those figures and sequences—not memory—keeps airworthiness limitations, cable tensions and composite repairs inside the published envelope.

Delivery is an instant PDF download after payment. Open it on a shop computer, tablet or phone, and print the pages you need for the hangar. No shipping wait and no printed-book bulk for a 1745-page AMM.