1991 EUROCOPTER BK117 B 2

1991

EUROCOPTER

BK117 B-2

Used

Engine I Lycoming LTP 101-750B-1 S/N: LE-45732AEF P/N Remaining term / cycles Axial rotor 4-101-006-39 12512.6 hrs / 17104.9 cyc Impeller 4-101-052-64 13770.3 hrs / 22991.7 cyc Compr. shaft 4-101-007-12 13770.3 hrs / 22991.7 cyc G.P. disc 4-111-062-03 8776.7 hrs / 5123.6 cyc G.P. sealing plate 4-111-063-02 8776.7 hrs / 5123.6 cyc G.P. spacer 4-111-018-05 8776.7 hrs / 5123.6 cyc P.T. rotor 4-141-290-18 7584.6 hrs / 4278.9 cyc Accessories P/N Remaining term Fuel control 4-301-283-08 1382.3 hrs Fuel pump 4-301-377-02 1103.0 hrs O/S Governor 4-301-212-05 72.7 hrs T1 Sensor 4-301-099-11 2369,2 hrs Air flow module 4-301-102-17 1965.3 hrs Engine II Lycoming LTP 101-750B-1 S/N: LE-48201BEF P/N Remaining term / cycles Axial rotor 4-101-006-39 14738.3 hrs / 24530.5 cyc Impeller 4-101-052-64 12005.4 hrs / 15757.5 cyc Compr. shaft 4-101-007-12 8294.6 hrs / 8990.5 cyc G.P. disc 4-111-015-19 3647.1 hrs / 4014.4 cyc G.P. sealing plate 4-111-019-08 13647.1 hrs / 22714.4 cyc G.P. spacer 4-111-018-09 13647.1 hrs / 27714.4 cyc P.T. rotor 4-141-290-18 7984.0 hrs / 2427.8 cyc Accessories P/N Remaining term Fuel control 4-301-413-04 1346.9 hrs Fuel pump 4-301-377-02 1615.7 hrs O/S Governor 4-301-212-05 1955.2 hrs T1 Sensor 4-301-411-02 2090.1 hrs Air flow module 4-301-102-12 2138.3 hrs Avionik VHF-S/E AR6201 Becker VHF-S/E AR6201 Becker VHF-NAV KNR634A Bendix/King VHF-NAV KNR634A Bendix/King UHF-NAV KNR634A Bendix/King UHF-NAV KNR634A Bendix/King MARKER KNR634A Bendix/King MARKER KNR634A Bendix/King DME KDM706 A Bendix/King MODE-S XPDR GTX330 Garmin TCAD RAYN TAS610 RDR-Altimeter KRA405 Bendix/King ELT 110-406HM NAV Artex ALT.ENC./ADC 10420-11968E Aerosonic GPS BR NAV KLN90B(B-RNAV) Bendix/King Engines Manufacturer Honeywell International Inc. Type/Model 2x Model LTS 101-750B-1 Dimensions Length 789 mm Height 644 mm Width 470 mm Dry weight 127 kg Take off power 410 kW Maximum continuous power 410 kW EASA Type Certification Application Date Feb 10th, 1987 EASA Type Engine Certification EASA.IM.E.228 Manufacturer Messerschmitt-Bölkow-Blohm GmbH Type/Model MBB-BK 117 B-2 Dimensions Fuselage Width 1.60 m Height 3.36 m Length 5.89 m Main rotor Diameter 11.00 m Tail rotor Diameter 1.96 m Fluid Capacities Fuel 607 l Fuel usable 598 l Oil (per engine) 4.33 l Technical Characteristics Max. air speed Vne 278 km/h 150 kts Max. operating altitude (up to 3,000 kg) 4,572 m 15,000 ft Max. operating altitude (above 3,000 kg) 3,048 m 10,000 ft Minimum flight crew one pilot (on right seat) Maximum passenger seating capacity 7 passengers Maximum baggage/ cargo loads 1,200 kg 600 kg/m2 EASA Type Certification Application Date Sep 28th, 2003 EASA Type Certification EASA.R.010 Stand Inspektion Engine I Lycoming LTP 101-750B-1 S/N: LE-45732AEF P/N Remaining term / cycles Axial rotor 4-101-006-39 12512.6 hrs / 17104.9 cyc Impeller 4-101-052-64 13770.3 hrs / 22991.7 cyc Compr. shaft 4-101-007-12 13770.3 hrs / 22991.7 cyc G.P. disc 4-111-062-03 8776.7 hrs / 5123.6 cyc G.P. sealing plate 4-111-063-02 8776.7 hrs / 5123.6 cyc G.P. spacer 4-111-018-05 8776.7 hrs / 5123.6 cyc P.T. rotor 4-141-290-18 7584.6 hrs / 4278.9 cyc Accessories P/N Remaining term Fuel control 4-301-283-08 1382.3 hrs Fuel pump 4-301-377-02 1103.0 hrs O/S Governor 4-301-212-05 72.7 hrs T1 Sensor 4-301-099-11 2369,2 hrs Air flow module 4-301-102-17 1965.3 hrs Engine II Lycoming LTP 101-750B-1 S/N: LE-48201BEF P/N Remaining term / cycles Axial rotor 4-101-006-39 14738.3 hrs / 24530.5 cyc Impeller 4-101-052-64 12005.4 hrs / 15757.5 cyc Compr. shaft 4-101-007-12 8294.6 hrs / 8990.5 cyc G.P. disc 4-111-015-19 3647.1 hrs / 4014.4 cyc G.P. sealing plate 4-111-019-08 13647.1 hrs / 22714.4 cyc G.P. spacer 4-111-018-09 13647.1 hrs / 27714.4 cyc P.T. rotor 4-141-290-18 7984.0 hrs / 2427.8 cyc Accessories P/N Remaining term Fuel control 4-301-413-04 1346.9 hrs Fuel pump 4-301-377-02 1615.7 hrs O/S Governor 4-301-212-05 1955.2 hrs T1 Sensor 4-301-411-02 2090.1 hrs Air flow module 4-301-102-12 2138.3 hrs Actual Aircraft Data (as of December 9th, 2020) S/N 7241 German civil registration D-HSAS Year built 1991 Total aircraft flight hours 9308.50 Fh Total landings 21124 Engine I TT 8623.57 Fh Engine II TT 7407.50 Fh Last Inspections Performed Due in / at Airworthiness Review Certificate Nov 2020 Nov 2021 50 FH-Inspection 9283.7 Fh 9333.7 Fh 100 FH-Inspection 9283.7 Fh 9383.7 Fh 600 FH-Inspection acc. to MM 9283.7 Fh 9883.7 Fh (600 Fh or 48 mon.) Jul 2020 Jul 2022 6000 FH-Inspection acc. to MM 8873.8 Fh 14873.8 Fh (6000 Fh or 96 mon.) Jun 2018 Jun 2024 Transponder check Jul 2020 Jul 2022 Emergency locator transmitter check Jul 2020 Jul 2021 Airframe Component Forecast Operation Hours Main transmission P/N Performed / Remaining term 117-120061 8873.8 Fh / 5565.3 Fh Main rotor head P/N Performed / Remaining term 117-141081 8873.8 Fh / 5565.3 Fh Main rotor blade P/N Performed / Remaining term 117-151521 8873.8 Fh / 5565.3 Fh 117-151521 8873.8 Fh / 5565.3 Fh 117-151521 8873.8 Fh / 5565.3 Fh 117-151521 8873.8 Fh / 5565.3 Fh Tail rotor gearbox P/N Performed / Remaining term Intermediate 4639 002 005 8873.8 Fh / 5565.3 Fh Tail rotor 4639 003 007 8873.8 Fh / 5565.3 Fh Tail rotor P/N Performed / Remaining term 105-317391 8873.8 Fh / 5565.3 Fh Tail rotor blade P/N Performed / Remaining term B641M1001101 8873.8 Fh / 5565.3 Fh B641M1001101 8873.8 Fh / 5565.3 Fh Hydraulic system P/N Performed / Remaining term 117-45020V002 8873.8 Fh / 5565.3 Fh The running times refer to the 6000 FH-Inspection. Remaining terms of individual components may differ.