AIRCRAFT STATUS REPORT NOTE: AIRCRAFT PAINT SCHEME AND REGISTRATION SHOWN FROM PREVIOUS OPERATOR FOKKER 50 SERIAL NUMBER: 20244 PREPARED BY: AVMAX AIRCRAFT LEASING INC. 2055 PEGASUS ROAD, N.E. CALGARY, ALBERTA CANADA T2E 8C3 E-MAIL : www.avmax.com The information contained in this document is the copyrighted property and proprietary information to Avmax Aircraft Leasing Inc. (“Avmax”), and is disclosed in strict confidence. It is the sole property of Avmax and shall not be used, disclosed or reproduced without the express written consent of Avmax. Avmax unequivocally excludes all inferred or implied terms, conditions and warranties arising out of this document and excludes all liability for loss and damages arising there from. All rights reserved. AVMAX AIRCRAFT LEASING INC. PAGE 1 FOKKER 50 01-MAR-2017 (REV 7) MSN: 20244
Transcript
AIRCRAFT
STATUS REPORT
NOTE: AIRCRAFT PAINT SCHEME AND REGISTRATION SHOWN FROM PREVIOUS OPERATOR
FOKKER 50
SERIAL NUMBER: 20244
PREPARED BY: AVMAX AIRCRAFT LEASING INC. 2055 PEGASUS ROAD, N.E. CALGARY, ALBERTA CANADA T2E 8C3 E-MAIL : www.avmax.com
The information contained in this document is the copyrighted property and proprietary information to Avmax Aircraft Leasing Inc. (“Avmax”), and is disclosed in strict confidence. It is the sole property of Avmax and shall not be used, disclosed or reproduced without the express written consent of Avmax. Avmax unequivocally excludes all inferred or implied terms, conditions and warranties arising out of this document and excludes all liability for loss and damages arising there from. All rights reserved.
2.1 PRINCIPAL AIRCRAFT DATA ............................................................................................................. 3 2.2 AIRFRAME STATUS .......................................................................................................................... 3 2.3 PRINCIPAL OPERATING WEIGHTS (LB) – HIGH GROSS WEIGHT VARIANT................................................ 3 2.4 OPERATIONAL SPECIFICATIONS ...................................................................................................... 4 2.5 FUEL DATA – NOTE .......................................................................................................................... 4 2.6 CABIN CONFIGURATION ................................................................................................................. 4
3.0 AIRCRAFT TECHNICAL STATUS ....................................................................................................... 5
3.1 AIRCRAFT MAINTENANCE PROGRAM ............................................................................................. 5 3.2 CURRENT MAINTENANCE STATUS .................................................................................................. 5
4.0 ENGINE STATUS .............................................................................................................................. 7
4.1 LEFT ENGINE – PW125B .................................................................................................................. 7 4.2 RIGHT ENGINE – PW125B ............................................................................................................... 8 4.3 LEFT PROPELLER – DOWTY................................................................................................................ 9 4.4 RIGHT PROPELLER - DOWTY .............................................................................................................. 9
5.0 AUXILIARY POWER UNIT (APU) ................................................................................................... 10
6.1 NOSE LANDING GEAR ................................................................................................................... 10 6.2 LEFT MAIN LANDING GEAR ........................................................................................................... 11 6.3 RIGHT MAIN LANDING GEAR ........................................................................................................ 12
7.0 ADDITIONAL INFORMATION ........................................................................................................ 13
7.1 MAJOR MODIFICATIONS INSTALLED ................................................................................................ 13
8.0 AVIONICS STATUS ........................................................................................................................ 14
1.0 INTRODUCTION On behalf of Avmax Aircraft Leasing Inc, this report details the aircraft status in respect of aircraft type Fokker 50 (HGW), manufacturer’s serial number 20244 (the ‘Aircraft’). This information is provided for informational purposes only, is not part of any proposal, and creates no legal or contractual commitment either express or implied. The Aircraft offered is subject to prior sale, lease or withdrawal from the market without notice and the engines and gear are subject to change. The accuracy of the information contained herein, is based on the knowledge and information available to the individual who has composed and/or updated this document as of the date specified. As such all data is subject to verification by any potential purchaser or lessee by way of inspection of the aircraft and it’s records.
2.0 AIRCRAFT SPECIFICATION 2.1 PRINCIPAL AIRCRAFT DATA
AIRCRAFT TYPE: FOKKER AIRCRAFT VARIANT: FOKKER 50 (HGW) MANUFACTURER’S SERIAL NUMBER: 20244 DATE OF MANUFACTURE: 1992 CURRENT REGISTRATION: TF-JMS
2.2 AIRFRAME STATUS
AS AT 01-MAR-2017
TOTAL HOURS SINCE NEW: 41,444.5 TOTAL CYCLES SINCE NEW: 52,887
2.3 PRINCIPAL OPERATING WEIGHTS (LB) – HIGH GROSS WEIGHT VARIANT
MAXIMUM TAKE-OFF WEIGHT: 45,900 MAXIMUM LANDING WEIGHT: 43,500 MAXIMUM ZERO FUEL WEIGHT: 41,000 BASIC EMPTY WEIGHT: 28,810 [PROVIDED BY PREVIOUS OPERATOR]
INSTRUMENTATION STANDARD: STANDARD FOKKER 50 EFIS AVIONICS RVSM CAPABLE: NOT REQUIRED AT AIRCRAFT SERVICE CEILING (FL250) SATCOM INSTALLED: NO OTHER SINGLE FMS – UNIVERSAL UNS-1L
2.5 FUEL DATA – NOTE
TOTAL FUEL CAPACITY: 9,090 LB LONG RANGE TANKS: NO
2.6 CABIN CONFIGURATION
POSITION MANUFACTURER MODEL / TYPE IN-SEAT VIDEO STANDARD QTY PASSENGER SEATS
ECONOMY FEEL NO 30 INCH PITCH 50
GALLEYS AFT CABIN BIEMANS -- G1 & G2 2
LAVATORIES DESIGNATION LOCATION MANUFACTURER MODEL – P/N FLUSH TYPE
POWER TURBINE DISC STAGE 1 3038513 A002AL36 30,000 8,187 21,813
POWER TURBINE DISC STAGE 2 3033914 A002C86L 30,000 8,187 21,813
HP TURBINE BLADES 3115601-01 125030+1 15,000 8,187 6,813 NOTE: DATA PROVIDED BY PREVIOUS OPERATOR, AND IS UN-AUDITED, WITH FRESH HSI.
TURBOMACHINERY: MANUFACTURE DATE OCT-1990 TURBOMACHINERY: LAST SHOP VISIT 02-JUN-2015 REDUCTION GEARBOX: MANUFACTURE DATE NOV-1991 REDUCTION GEARBOX: LAST SHOP VISIT 02-JUN-2015
POWER TURBINE DISC STAGE 1 3038513 A002N1F5 30,000 7,487 22,513
POWER TURBINE DISC STAGE 2 3033914 A001Y3PD 30,000 13,158 16,842
HP TURBINE BLADES 3115601-01 125057+1 15,000 7,487 7,513 NOTE: DATA PROVIDED BY PREVIOUS OPERATOR, AND IS UN-AUDITED. ENGINE SHOWN AFTER FRESH HSI AT VECTOR AEROSPACE.
TURBOMACHINERY: MANUFACTURE DATE JAN-1991 TURBOMACHINERY: LAST SHOP VISIT 28-DEC-2016 REDUCTION GEARBOX: MANUFACTURE DATE FEB-1991 REDUCTION GEARBOX: LAST SHOP VISIT 28-DEC-2016
