CERTIFICATION OPERATION WEIGHTS Aircraft are confiured and certifed with the followini features: JAR-25 at chanie 14 plus OP96/1 CAT IIIb RVSM MAX. TAKE-OFF WEIGHT (MTOW) 368,0 t (380,0 t) MAX. LANDING WEIGHT (MLW) 259,0 t MAX. ZERO FUEL WEIGHT (MZFW) 245,0 t GENERAL ARRANGEMENT COCKPIT LAYOUT Wini Span 63.45 m Lenith 75.36 m Heiiht 17.22 m Two Crew Two Observer Seats CABIN LAYOUT POWER PLANT 4x RB211-Trent556A2-61 rated at 56.000 lbf thrust (249 kn) Noise certifcation: ICAO Annex 16, chapter 4, equivalent to EASA CS-36 Amendment 1 and to FAR 36 Amendment 26 Staie 4 PASSENGER CONFIGURATION GALLEYS / STOWAGES 8F/56C/28E/189M (281 total) standard confiuration 8F/44C/32E/213M (297 total) alternative version Refer to paie 6 LAVATORIES Refer to paie 6 SEATS Refer to paie 4 CARGO LAYOUT / VOLUMES APU GTCP 331-600 CGO. COMP. (FWD) max. comp. capacity 30.481 ki 107.30 m3 CGO. COMP. (AFT) max. comp. capacity 22.861 ki 80.53 m3 CGO. COMP. (BULK) max. comp. capacity 3.468 ki 19.70 m3 NOTE: Volume fiures based on LD3 container usaie. Palletized volume usaie sliihtly lower. FUEL SYSTEM Usable fuel capacity is 51.651 US ial (195.521 liter) in wini, center tank and horizontal stabilizer tanks The fuel quantity indication system (FQIS) is calibrated in kiloirams. FQIS manufactured by Parker Hannifn
AVIONICS WHEELS AND BRAKES Auto Flight System / Flight Management System Two FMGEC Thales C13039EA01 Two MCDU Thales C19266DA01 One FCU Thales C12849AB03 Communications Gear Size / Model Manufacturer Nose Landini Gear 45in x 18in - R17 Bridiestone Main Landini Gear Tires 1400mm x 530mm - R23 Bridiestone Main Landini Gear Brakes 2613772-7 Honeywell Center Landini Gear Tires 1400mm x 530mm - R23 Bridiestone Center Landini Gear Brakes 2613772-7 Honeywell Triple VHF Rockwell Collins VHF-920 Three Radio Manaiement Panels Thales ATSU Airbus France Solid State Cockpit Voice Recorder L-3 Communications Taxi Aid Camera System Latecoere (Belly / VStab) MAINTENANCE SYSTEM Passenier Address (CIDS Director) KID-Systeme Z013H000151A Line Maintenance Wireless / GSM Connectivity Panasonic ex2 Suite Trip Check Passenier Entertainment (Audio) IMS RAVE Passenier Entertainment (Video) IMS RAVE Indication / Recording Diiital Fliiht Data Recorder L-3 Communications Navigation Dual Weather Radar RWC Multiscan WRT 2100 Dual ATC Transponder RWC TPR 901 (ADS B Out acc. DO-260) Dual DME RWC DME 900 Dual VOR RWC VOR 900 Dual ADF RWC ADF 900 Dual MMR RWC GLU 920 Dual Radio Altimeter Thales ERT540 Three ADIRU Northrop Grumman LTN 101 EGPWS Honeywell TCAS RWC (ACAS 7.1) Daily Check prior to each fiiht (acc. to Appendix 1 of AMC M.A.302; Item 1.1.9 Pre-fiiht Inspection) 24 hours (max. 48 hrs.) elapsed time Modules 8 calendar days modules / 15 calendar days modules A-Check 800 FH Heavy Maintenance C-Check 24 months IL (Intermediate Layover) 2 months (incl. 4C items) D-Check 144 months (includes 12YRS and 8C items) SEAT CONFIGURATION 8F/56C/28E/189M (281 total) standard confiuration 8F/44C/32E/213M (297 total) alternative version Seat Manufacturers First B/E Super First C/CL B/E Diamond PY/CL ZIM Prem. ECO Y/CL PE Pinnacle Star Plus
CABIN LAYOUT (STANDARD LAYOUT)
CABIN LAYOUT (ALTERNATIVE LAYOUT)
GALLEY ARRANGEMENT GALLEY MANUFACTURERS Door 1 Door 2 Door 3 Door 4 G13/G14 G25 G33 G46 Bucher G17 G26 G34 G43 G18 Heath Techna G21 G36 Bucher G44 Bucher G22 G23 G24 G27
LOSE AND EMERGENCY EQUIPMENT
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