AIRCRAFT TECHNICAL SPECIFICATION
AIRCRAFT DETAILS
CERTIFICATION
POWERPLANT
APU
OPERATING WEIGHTS
Serial Number
Variable Number
Line Number
Date of Manufacture
OPERATING LIMITS
MANDATORY & OPTIONAL INSTALLATIONS
Model Boeing 747-467F 11 July 1995 114,392 FH / 19,408 FC
Utilisation up to 1 July 2025
Operation
OEM Delivery Certification
Existing Certification
Manufacturer
Engine Type & Model
Thrust Rating
Noise rating
Manufacturer
APU Type & Model
Maximum Taxi Weight
Maximum Take Off Weight
Maximum Landing Weight
Maximum Zero Fuel Weight
Operating Empty Weight
Fuel Capacity
Last Weight Date
Max TO / Landing Altitude
Max Operating Altitude
ADS-B OUT
CAT III
FAA TCDS A20WE
EASA TCDS IMAC01058
Rolls Royce
RB211-524H2-19 59,450 lbs
Stage III
Pratt& Whitney PW901A
397,800 kg / 877,000 lbs 396,893 kg / 875,000 lbs 302,092 kg / 666,000 lbs 288,031 kg / 635,000 lbs 162,234 kg / 357,665 lbs
163,118 kg / 359,614 lbs
November 2024 10,000 FT
45,100 FT
VHF 8.33 Spacing Compliant Compliant
FM Immunity Compliant
RVSM Compliant
TCAS Version 7.1 Installed
EGPWS Installed
ELT Fixed (1),Portable (2)
Elementary Surveillance Installed
Enhanced Surveillance Installed
15 Knot Tail Wind Certified Compliant
10 Minute Take Off Thrust Rating Compliant SATCOM Installed
RNP 1,5,10 Compliant
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UPPER DECK CABIN LAYOUT
PASSENGER SEATS BE Aerospace 6 Seats
CREW REST Boeing 2 Sleep Bunks
GALLEY Including:
MAIN DECK CONFIGURATION
LOWER DECK CONFIGURATION
Atlas type (1)
Oven (1)
Coffeemaker (1)
Hot cup (1)
Showa PN 60191-000006
Inventum PN 72068000
Grimes PN 411-0001-141
Driessen PN DLH1834-001
Containers (5) Driessen PN DLH306-14
Boeing/Goodrich System 30 ULDs 96’ or 88’ x 125’ Temperature controlled
Boeing/Goodrich System 5 ULDs 96’ or 88’ x 125’ (fwd) 4 ULDs 96’ or 88’ x 125’ (aft) Temperature controlled
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Disclaimer: While every effort has been made to ensure consistency of the aircraft’s configuration, this document does not constitute an offer or a contract. This specification is for information only and shall not constitute any right or obligations.
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Disclaimer:
MAINTENANCE STATUS
AIRFRAME
Utilisation (to 1 July 2025) 114,392 FH / 19,408 FC
A-CHECK Interval 1,000 hrs
1C-CHECK Interval 10,000 hrs / 24 months
1C-CHECK Last Performed 112,984 FH / 19,187 FC / Nov-2024 Next Due 122,984 FH / Nov-2026
D-CHECK Interval 72 months
D-CHECK Last Performed Next Due 18 May 2020 18 May 2026
LANDING GEAR
ENGINE #1
ENGINE #2
ENGINE #3
ENGINE #4
APU
NLG Last Performed / Next Due June 2020 / June 2030
LH WLG Last Performed / Next Due June 2020 / June 2030
RH WLG Last Performed / Next Due June 2020 / June 2030
LH BLG Last Performed / Next Due June 2020 / June 2030
RH BLG Last Performed / Next Due June 2020 / June 2030
Rolls Royce RB211-524H2-19 13667
Time / Cycles Since New 89,798 / 10,687 Time / Cycles Since Shop Visit 24,316 / 3,357 Date of Last Shop Visit 23 September 2014
Rolls Royce RB211-524H2-19 13694
Time / Cycles Since New 70,834 / 9,190 Time / Cycles Since Shop Visit 21,186 / 2,581
Date of Last Shop Visit 24 June 2011
Rolls Royce RB211-524H2-19 13031
Time / Cycles Since New 121,063 / 15,614 Time / Cycles Since Shop Visit 8,011 / 1,169
Date of Last Shop Visit 13 July 2019
Rolls Royce RB211-524H2-19 13023
Time / Cycles Since New 125,617 / 16,519 Time / Cycles Since Shop Visit 16,540 / 2,345
Date of Last Shop Visit 02 February 2016
PCE900588
APU TT / TC 30,248* / 21,031*
APU TSLSV / CSLSV 8,362* / 8,587* *APU data as of Nov 2024 only
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Disclaimer: While every effort has been made to ensure consistency of the aircraft’s configuration, this document does not constitute an offer or a contract. This specification is for information only and shall not constitute any right or obligations.
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Disclaimer: While every effort has been made to ensure consistency of the aircraft’s configuration, this document does not constitute an offer or a contract. This specification is for information only and shall not constitute any right or obligations.