ATA 00 - INTRO

• STA 0 is located 254 cm in front of the radome

• 300 is stabilizer major zone, 400 is the pylons

• A/C major zones:

- 100 = Lower fuselage

- 200 = Upper fuselage

- 300 = Stabilizer / Tail section

- 400 = Pylon / Nacelle

- 500 = L/H Wing

- 600 = R/H Wing

- 700 = Landing Gear

- 800 = Doors

• Z is a panel identification in the internal, W is side wall panel

• For jacking procedure we do align the plane using attitude monitor or MCDU alpha

call-up

• Maximum steering angle is 95 degrees (Pin inserted), Tiller steering is 75 degrees

• 14CA1 FIN number stands for flight control and autopilot, M are mechanical

components

• AMM Page Block 400 is Removal/Installation – Deactivation/Reactivation procedures,

PB 700 is cleaning

• PFR (Post Flight Report) is the first entry point on TSM (TroubleShooting Manual)

• A/C basic structure is made of aluminum alloys with stainless and Titanium in some

areas

• Composite materials are used for primary and secondary structure and represent

15% of the A/C weight (CFRP, AFRP, GFRP)

• FR36 and FR42 belong to the wing center section box

• Fuselage frames are connected to stringers via “cleats”

• Wing section ribs 1 to 13: 7 non load carrying fuel tank access panels are installed (Clamped)

• Wing section ribs 14 to 27: 14 load carrying fuel tank access panels are installed (Bolted)

• Vertical and Horizontal Stabilizers are mainly made by composite materials