B December-2018
|
|
- Ada McDowell
- 5 years ago
- Views:
Transcription
1 B December2018 IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 24 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THYAHM560_FOREWORD" PAGE NO ATION ISSUE REV SHEET FOR DATE NO NO PAGES PAGE DESRIPTION ontents Apr11 General Info Apr11 A1,A2 ontact Address Apr11 B1,B2 Passenger & baggage weights/ crew weights Apr11 DOW and DOI specifications / Special Information Apr11 Load&Trim Sheet Information Dec18 24 Updated List Of Effective Pages Basic Index and MA formula/ Stabilizer Dec ,3 Trim Setting/A/ Registration., Wt Index Details 04.01A 22Jul10 12 Stabilizer Trim Setting table Dec18 24 Updated A/ Basic Weight & Index Table 04.02A 20Dec18 24 Updated Pantry Standard W/I Table(atering) Oct Aircraft Weight Limitations Jun G Limits for Loadsheet Purpose Dec Effect of Fuel / APU Taxi Fuel Weight Mar rew Seats Location & Distribution Jul Galley & Pantry Jul Passenger abin Jul lass / abin Sections Dec Seating Layout ode Letters July16 11 Seat Plan Layout May ,1 Details For ompartment Trim & 3,14 Bay/Section Trim, Ballast Dec08 01 D1, D2,D3 Ideal Trim Line, ULD / Special Load May12 Load&Trim Sheet (TJKJ,JKK,JKO) Page No:04.00
2 REVISION NOTES: B December2018 REV NO REVISION DESRIPTION 24 TJKO BW/BI values have been updated due to potable water s weight s change and pantry standart weight /ındex table for all Anadolu Jet Flights has been added. 23 TJKO G Limits have been updated. 22 TJKK,JKJ left THY fleet 21 TJKJ,JKK,JKO BW/BI changed due to modification 20 TJKJ,JKK BW/BI changed due to weighing 19 TJKO BW/BI changed due to weighing 19 TJKN left THY fleet 18 LM values are updated Pantry codes amended. Passenger cabin modified by addition of seat row Total index value of 3 cockpit crew amended. Number of cockpit crew seats and average location table amended for JS. Page No:04.00
3 EDPSYSTEM B December2008 Sheet 2 abin onfiguration(s) A / TYPE arrier ALL B TK 2. BASI INDEX AND MA FORMULA 2.1. Examples and definitions Index W (Station Ref.Sta.) K % MA W Station Ref.Station calculated K I MA LEMA ( (I K) Ref.Sta. LEMA W MA 100 = Weight, actual [kg] = Station, Horizontal distance in inches or meters from station zero = Reference Station/axis. Selected station around which all index values are = onstant used as a plus value to avoid negative index figures = onstant used as a Denominator to convert moment values into index values = Index value corresponding to respective weight = Length of Mean Aerodynamic hord in inches or meters = Horizontal Distance in inches or meters from the station zero to location of the leading EDGE of the MA Index formula Ref.Station. at = inches from zero K (onstant) = 45 (onstant) = MA Information Length of MA = inches LEMA at = inches from zero 2.4. Stabilizer Trim Setting Stabilizer Trim Setting tables are on page 04.01A. These are for Flaps 1 & 5 only. EDPSYSTEM Sheet 3 abin onfiguration(s) A / TYPE arrier ALL B TK 3. AIRRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS DRY OPERATING WEIGHT X BASI WEIGHT X A list of weight and index values for each aircraft registration is given on next page. Page No:04.01
4 B July2010 STABILIZER TRIM SETTING VALUES ENGINE THRUST RATING : LB Page No:04.01A
5 B December2018 A/ BASI & DRY OPERATING WEIGHT & INDEX TABLE Numbe A/c Type MSN A/ Reg. r of Seats Basic*(crew(0/0) How to calculate DOW/DOI? Weight Index B737700W TJKO Basic Weight/Index (Full potable water tank) + ockpit rew Total Weight/Index + abin rew Total Weight/Index + Pantry Weight/Index = Dry Operating Weight/Index If actual is different, then make necessary adjustments A/ Reg A/ Limitations MTAXI KG TJKO MTOW KG MLDW KG MZFW KG OKPIT REW TOTAL EFFET / ockpit rew No/Locations ockpit rew No/Locations WEIGHT INDEX 2 OKPIT REW (2 FrontSeat) OKPIT REW (2 FrontSeat + 1JumpSeat) ABIN REW TOTAL EFFET / abin rew No/Locations abin rew No/Locations WEIGHT INDEX 3 ABIN REW (1 Fwd + 2 Aft) ABIN REW (2 Fwd + 2 Aft) PANTRY EFFET / Pantry ode/lass, onfig, App. PANTRY (ATERING) STANDARD W/I TABLE IS ON PAGE 04.02A BW/BI value in the above table already includes potable water with FULL tank (160 kg/ 1.7 Index).If potable water tanks are different, adjust DOW & DOI in proper ratios. INFLUENE OF POTABLE WATER ON DOW/DOI %75 POTABLE WATER %50 POTABLE WATER %25 POTABLE WATER Subtract 40 KG / Subtract 0.4 Index Subtract 80 KG / Subract 0.8 Index Subtract 120 KG / 1.3 Subtract Index *Basic Wt/Index includes: ockpit & A/ Documents, Potable Water Tanks Full, Skylife Magazine, Tare empty Weight of all Trolleys & Galley Equipment (hotcup, hotjug, etc). If some items or Equipment are NOT carried make necessary adjustments. Dry Operating Weight/Index does NOT include Toolkit Box. heck if they are carried in cargo compartment. It should be shown as Load in compartments (distribution) on loadsheet as Equipment in compartment. TOOLKIT BOX = 23 KG REW BAGGAGE (in BULK argo ompartment) : For Longhaul flights and for flights that crew stays overnight at destination, additional REW BAGGAGE, standard bag weight of 10 kg per crew member is carried. This load is NOT included in above DOW/DOI, and it should be shown as 'LOAD IN OMPARTMENT DISTRIBUTION" in Loadsheet. * Refer to DOWDOI_TableB file for several possible standard cockpit/cabin crew, pantry codes & potable water tanks fill ratio. DOI calculation remark : During Index alculations due to DS system rounding (or truncating), approximately +/ 0.3 index difference is acceptable. Page No:04.02
6 Pantry ode B December2018 PANTRY STANDART WEIGHT/INDEX TABLE (ATERING) Galley weight TOTAL Fwd Aft WEIGHT INDEX Destination / Departure N ALL INTERNATIONAL FLIGHTS D DOMESTI FLIGHTS ONE WAY G DOMESTI FLIGHTS RETURN PANTRY REMARKS: 1 All weights are in kg. I Valid for all Anadolu Jet Flights Pantry Galley weight TOTAL ode Fwd Aft WEIGHT INDEX Destination / Departure U ,4 DOMESTI FLIGHTS ONE WAY V ,7 DOMESTI FLIGHTS RETURN PANTRY W ,0 ALL INTERNATIONAL FLIGHTS Page No:04.02A
7 EDPSYSTEM B July2016 Sheet 4 abin onfiguration(s) A / TYPE arrier B TK 4. LIMITATIONS 4.1. Aircraft Weight Limitations Maximum weights for: Aircraft Design Takeoff Wet off Dry Landing Design Take Design MSN Ramp/Taxi Zero Fuel Reg. TJKO kg kg kg kg LM (Last Minute hanges) Information : Last Minute hanges (LM) to the mass and balance sheet are only permitted when the changes of the load (either minus or plus) in last minutes are within the following limits. B : 800 kg Total Weight (Passengers,argo,Mail or any combination) These changes must be shown as pax, cargo, mail, baggage etc. in the Load & Trim Sheet. The effect of LM in aircraft G must be checked. Aircraft G after LM must not exceed forward and aft operational G Limits. In Addition to LM Weight, LM Index influence should be shown on Load & Trim Sheet in a suitable space under LM title preferably next to LM weight. Page No:04.03
8 EDPSYSTEM B Oct2018 Sheet 5 abin onfiguration(s) A / TYPE arrier B TK G Limits for Loadsheet Purpose FORWARD Special condition if applicable Specify applicability ZERO FUEL HEK Weight(kg) Special condition if applicable TAKEOFF HEK Special condition if applicable LANDING HEK Index Value AFT Special condition if applicable Specify applicability ZERO FUEL HEK Weight(kg) Index Value Special condition if applicable TAKEOFF HEK Special condition if applicable LANDING HEK Page No:04.04
9 EDPSYSTEM B Dec2008 Sheet 6 abin onfiguration(s) A / TYPE arrier ALL B TK 5. EFFET OF FUEL Fuel Loading Fuel Usage Standard Procedure X Nonstandard Procedure FUEL DENSITY: 0.79 KG/L FUEL WEIGHT (KG) INDEX VALUE MAIN TANKS =>>> FULL MAIN & ENTER TANKS FULL =>>> REMARKS: FUEL LOADING PROEDURE IS AS FOLLOWS 1. Load main tanks 1 & 2 equally until they are full. 2. Load additional fuel in the center tank. Fuel usage procedure is just the opposite of loading procedure VOLUMETRI APAITY MAIN TANKS LT MAIN TANKS LT ENTER TANK LT TOTAL LT 5.2 APU / TAXI FUEL WEIGHT Due to local taxiing distances and local needs for APU running, total taxi Fuel may be different in your local station. It may be calculated by using the following fuel flow figures; Taxi Fuel Flow = 12 kg/minute APU Fuel Flow = 105 kg/hour Page No:04.05
10 EDPSYSTEM B Dec2008 Sheet 7 abin onfiguration(s) A / TYPE arrier ALL B TK 6. REW 6.1. Number of cockpit crew seats and average location Length of arm from reference Index influence station Maximum number of cockpit seats +/ +/ (inch) per 1 kg Number of cabin crew seats and location ABIN rew seats locations Max. Length of arm from Index influence No. of seats reference station +/ +/ (inch) per 1 kg FWD ENTRY DOOR AFT ENTRY DOOR rew Distribution / rew ode rew ode Number of abin rews at ockpit abin rew Location rew Total Total No Location of No FWD AFT rew Baggage 2/ BULK ARGO 2/ OMPT. Page No:04.06
11 EDPSYSTEM B Jul2010 Sheet 8 abin onfiguration(s) A / TYPE arrier ALL B TK 7. GALLEY AND PANTRY Galleys Length of arm from reference Index influence Galley locations station +/ +/ (Inch) per 1 kg G G FWD(G1+G2) G4B AFT(G4B) Remarks: FWD, AFT average Galley locations can be used for simplicity 7.2 Pantry Weight / Pantry ode Pantry Weight / Pantry ode table is given on A/ BASI WEIGHT & INDEX TABLE. 7.3 SEATING ONDITIONS LOADSHEET OUTPUT State below how the seating conditions should be shown in the respective loadsheet box. Give example. Enclose a passenger distribution table if used. Page No:04.07
12 EDPSYSTEM B Jul2010 Sheet 9 abin onfiguration(s) A / TYPE arrier B TK 8. PASSENGER ABIN 8.1 Passenger Seats LASS ODES lass 1: lass 2 : Y lass 3 : Name of cabin section NUMBER OF SEATS lass lass lass Total per cabin section Name of cabin section NUMBER OF SEATS lass lass lass Total per cabin section ABIN ONFIGURATION 124Y ABIN ONFIGURATION 12/112Y OA OA OB OB O O Total per Total per class class Page No:04.08
13 EDPSYSTEM B Jul2010 Sheet 9 abin onfiguration(s) A / TYPE arrier ALL B TK 8.2 lass/abin Sections lass/abin Section Length of arm from reference station Index influence +/ inch +/ per 1 kg OA 308, OB O Page No:04.09
14 EDPSYSTEM 8.3 Seating Layout B Jul2010 Sheet 10 A / TYPE arrier B TK Show the passenger seating layout for the configurations given in the box at the top by inserting the seat row numbers and letters in the following table. For special seats use the description codes listed below : B = Bassinet position = rew seat E = Emergency exit G = Groups H = Incapacitated passenger I = Infant preference rows/seats J = Rear facing seats K = Near galley L = Leg space seat M = Wheel chair N = No Smoking O = Over wing seat P = Stretcher location Q = Quiet zone S = Smoking T = Near toilet U = Unaccompanied minor V = Seat left vacant/offered last W = No Movie X = No facility seat (e.g. no distinction between smoking and nonsmoking) Y = Not fitted Z = Buffer zone. = Aisle Alfa/haracters A, D, F, R, Blank not used Note : Seat designators to be in accordance with Recommended Pratice Page No:04.10
15 EDPSYSTEM B July2016 Sheet 11 abin onfiguration(s) A / TYPE arrier TJKO B TK Seatplan Layout / Facilities and Row Index Influence SETION ROW NO 1 A B Index Influence per Seat Row per1kg ABIN ONFIGURATION 124Y ABIN ONFIGURATION 12/112Y Rows Rows fromtoto: from A B D E F A B D E F 13 NI N Y. Y N NI 13 NI N Y. Y N NI 611 NI N N. N N NI 611 NI N N. N N NI 12 Y NE NE. NE NE Y 12 Y NE NE. NE NE Y 13 NE NE NE. NE NE NE 13 NE NE NE. NE NE NE 1424 NI N N. N N NI 1424 NI N N. N N NI MOVEABLE ERTAIN LASS DIVIDER is shown as: THE AISLE is shown as :. Page No:04.11
16 EDPSYSTEM B Nov2009 Sheet 12 abin onfiguration(s) A / TYPE arrier B TK 9. DETAILS FOR OMPARTMENT TRIM MAXIMUM APAITY INDEX INFLUENE OMPARTMENT DESRIPTION GROSS VOLUME* NUMBER WEIGHT (M 3 ) (kg) +/ per 1 kg 1 FWD HOLD FWD HOLD AFT HOLD AFT HOLD Volume information required for bulk compartments only. 9.1 ombined Load Limitations : None 9.2 umulative Load Limitations : None EDPSYSTEM Sheet 13 abin onfiguration(s) A / TYPE arrier B TK 10. DETAILS FOR BAY / SETION TRIM MAX. APAITY Index influence BAY / SETION GROSS WEIGHT (kg) VOLUME (M 3 ) +/ per 1 kg NOT APPLIABLE 10.1 Unsymmetrical load limitations: NOT APPLIABLE EDPSYSTEM Sheet 14 abin onfiguration(s) A / TYPE arrier B TK 11. BALLAST FIXED PROVISIONS FOR ARRYING BALLAST? REMARKS : BALLAST IS NOT REQUIRED Page No:04.12
17 B Dec2008 EDPSYSTEM D Sheet 1 A / TYPE arrier B TK 1. G LIMITS 1.1. Planning Limits GLimits for loadplanning purpose shall be agreed between carrier and system operator. 1.2 Ideal Trim Line at ZFW for Fuel Saving Purposes The IDEAL TRIM LINE shown in the balance graph below is a loadplanning limit only. In the interest of fuel economy the load in the compartments shall whenever possible. be distributed in such a way that the LIZFW is aft of this line. The respective breakpoints (weight / index) of the ideal trim line shall be entered in the table below. WEIGHT INDEX VALUE EDPSYSTEM D Sheet 2 A / TYPE arrier B TK 2. UNIT LOAD DEVIES DETAILS Maximum apacity Type ode Tare weight Gross Weight VOLUME (m 3 ) Remarks NOT APPLIABLE EDPSYSTEM D Sheet 3 A / TYPE arrier B TK 3. SPEIAL LOAD Apply Turkish Airlines & IATA regulations. When necessary contact Turkish Airlines Station Manager. Page No:04.13
B777F 06-Apr-2018 IATA AHM560 DATA LIST OF EFFECTIVE PAGES REV 02
B777F 06-Apr-2018 IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 02 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THY-AHM560_Pages_00.00-02.04.pdf" ATION PAGE ISSUE SHEET REV NO FOR PAGE
More informationSHEET NO Aug15 78 Updated - List Of Effective Pages / Revision Highlights
PAGE NO A340-300 14-Aug-2015 IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 77 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THY-AHM560_FOREWORD.pdf" ISSUE DATE REV NO ATION FOR PAGES
More informationAHM560 Data for Check-in & Loadcontrol Contents Apr General Info Apr A1,A2 Contact Address.
PAGE NO A340-300 04-Aug-2017 IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 85 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THY-AHM560_FOREWORD.pdf" ISSUE DATE REV NO ATION FOR PAGES
More informationA Dec-2016 IATA AHM560 DATA LIST OF EFFECTIVE PAGES REV 38
IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 38 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THY-AHM560_FOREWORD.pdf" ATION ISSUE REV SHEET PAGE NO FOR PAGE DESRIPTION DATE NO NO PAGES
More informationA F 8-Oct-2018 IATA AHM560 DATA LIST OF EFFECTIVE PAGES REV 16
A330-243F 8-Oct-2018 IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 16 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THY-AHM560_Pages_00.00-02.04.pdf" ATION PAGE ISSUE SHEET REV NO FOR
More informationA F 19-Dec-2017 IATA AHM560 DATA LIST OF EFFECTIVE PAGES REV 13
A330-243F 19-Dec-2017 IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 13 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THY-AHM560_Pages_00.00-02.04.pdf" ATION PAGE ISSUE SHEET REV NO FOR
More informationA May-2018 IATA AHM560 DATA LIST OF EFFECTIVE PAGES REV 57
A330-300 21-May-2018 IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 57 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THY-AHM560_FOREWORD.pdf" ATION ISSUE REV SHEET PAGE NO FOR PAGE DESRIPTION
More informationCondor / Condor Berlin Thomas Cook Airlines Belgium Thomas Cook Airlines UK
Ground Operations Manual Thomas Cook Airlines Belgium Thomas Cook Airlines UK Page 1 12 Aircraft Data B767-300 12.1 Load Control Condor B767-300 (76C)...3 12.1.1 Aircraft Data Condor B767-300 (76C)...3
More informationAHM560 Data for Check-in & Loadcontrol ACTION FOR PAGES PAGE NO ISSUE DATE SHEET NO REV NO PAGE DESCRIPTION
PAGE NO A318-112J 19-Apr-2018 IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 01 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THY-AHM560_FOREWORD" ISSUE DATE REV NO ATION FOR PAGES SHEET
More informationSUPPLIER'S CONTACTS AHM565 EDP SYSTEM SEMI PERMANENT DATA. Contact and Message Information Supplier Contacts. Sheet 1 Carrier
Contact and Message Information Supplier Contacts A Sheet 1 1 SUPPLIER'S CONTACTS Completed sheets and changes of basic data and procedure must be forwarded to: MAILING ADDRESS: (INC. TEL & FA) Click Here
More informationCHAPTER 22 WEIGHT CONTROL OF AIRCRAFT
May 2016 Page 1 of 8 CHAPTER 22 WEIGHT CONTROL OF AIRCRAFT 1. Introduction 1.1. The mass and centre of gravity of aircraft should be determined prior to the initial issuance of the Certificate of Airworthiness.
More information2.1 General Characteristics. 2.2 General Dimensions. 2.3 Ground Clearances. 2.4 Interior Arrangements. 2.5 Cabin Cross Sections
2.0 AIRPLANE DESCRIPTION 2.1 General Characteristics 2.2 General Dimensions 2.3 Ground Clearances 2.4 Interior Arrangements 2.5 Cabin Cross Sections 2.6 Lower Cargo Compartments 2.7 Door Clearances JUNE
More informationFLIGHT DISPATCH MANUAL AIRCRAFT WEIGHT AND BALANCE
PAGE: 1 Table of Contents Table of Contents... 1 CHARTER 6.-... 2 6.1 General... 2 6.1.1 Basic load requirement... 2 6.1.2 Weight... 2 6.1.3 Balance... 2 6.2 Definitions... 3 6.3 Weight limitations...
More informationFOR REFERENCE ONLY NOT FOR FLIGHT
PA-46-350P, MALIBU SECTION 6 6.7 GENERAL LOADING RECOMMENDATIONS For all airplane configurations, it is the responsibility of the pilot in command to make sure that the airplane always remains within the
More informationNOTE: DATA PRELIMINARY
2.0 AIRPLANE DESCRIPTION 2.1 General Characteristics 2.2 General Dimensions 2.3 Ground Clearances 2.4 Interior Arrangements 2.5 Cabin Cross Sections 2.6 Lower Cargo Compartments 2.7 Door Clearances REV
More informationTYPE CERTIFICATE DATA SHEET A3WE
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A3WE Revision 19 BOEING 727 Series 727-100 Series 727C Series 727-100C Series 727-200 Series 727-200F Series February 20, 1991 TYPE CERTIFICATE
More informationWEIGHT, BALANCE & EQUIPMENT LIST
WEIGHT, BALANCE & EQUIPMENT LIST For Aircraft Fitted with 65litre Fuel Tank P/No 4217092 Table of Contents 6.1. Introduction 2 6.2. Aircraft Weight Record 2 6.3. Loading System 3 6.3.1. General 3 6.3.2.
More informationAIRCRAFT BALANCING FOR THE PURPOSE OF AIR TRAFFIC SAFETY
AIRCRAFT BALANCING FOR THE PURPOSE OF AIR TRAFFIC SAFETY Igor Štimac, B.Eng. Zagreb Airport Ltd. Pleso bb, 10000 Zagreb, Croatia e-mail: istimac@zagreb-airport.hr Jurica Ivanišević, B.Eng. Zagreb Airport
More informationAccident Prevention Program
Accident Prevention Program WEIGHT AND BALANCE An Important Safety Consideration for Pilots Aircraft performance and handling characteristics are affected by the gross weight and center of gravity limits.
More informationGlossary. basic empty weight (GAMA). Standard empty weight plus optional equipment.
Glossary General Aviation Manufacturers Association (GAMA) 14 CFR, Part 121. The Federal regulations governing domestic, flag, and supplemental operations. 14 CFR, Part 135. The Federal regulations governing
More informationTECHNICAL SPECIFICATION BOEING LY-PGC
AIRCRAFT TECNICAL SPECIFICATION 1 of 5 TECHNICAL SPECIFICATION Date: 11-Jul-18 BOEING 737-400 LY-PGC Operated by GETJET AIRLINES AIRCRAFT TECNICAL SPECIFICATION 2 of 5 GENERAL Aicraft Type: B737-400 Aicraft
More informationTECHNICAL SPECIFICATION
AIRCRAFT TECNICAL SPECIFICATION 1 of 5 TECHNICAL SPECIFICATION Date: 11-Jul-18 BOEING 737-400 LY-MGC Operated by GETJET AIRLINES AIRCRAFT TECNICAL SPECIFICATION 2 of 5 GENERAL Aicraft Type: B737-400 Aicraft
More informationATR FREIGHTER VERSIONS. AN EASY CONVERSION AVAILABLE SINCE 2002, TO EXTEND ATR s
ATR FREIGHTER VERSIONS AN EASY CONVERSION AVAILABLE SINCE 2002, TO EXTEND ATR s economic advantages to the cargo market ATR FREIGHTER CONVERSION AN ADAPTED PLATFORM FOR EASY FREIGHTER CONVERSION XXXXXXXXXXXXXXXXXX
More informationLS-Data. Manual. Altenrhein Luftfahrt GmbH Office Park 3 Top 312 / Postfach 90 A-1300 Wien Flughafen
LS-Data Manual Altenrhein Luftfahrt GmbH Office Park 3 Top 312 / Postfach 90 A-1300 Wien Flughafen Contents: 1. General... 2 2. Requirements... 2 3. Log In... 3 4. Cockpit crew... 4 4.1. New flight...
More information767 Airplane Characteristics for. Airport Planning. Boeing Commercial Airplanes. D SEPTEMBER 2005 i
767 Airplane Characteristics for Airport Planning Boeing Commercial Airplanes SEPTEMBER 2005 i 767 AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING LIST OF ACTIVE PAGES Page Date Page Date Page Date Original
More informationFOR REFERENCE ONLY NOT FOR FLIGHT
PIPER AIRCRAFT CORPORATION SECTION 6 6.7 GENERAL LOADING RECOMMENDATIONS For all airplane configurations, it is the responsibility of the pilot in command to make sure that the airplane always remains
More informationChapter 5 Center of Gravity Change After Repair or Alteration
Chapter 5 Center of Gravity Change After Repair or Alteration The largest weight changes that occur during the lifetime of an aircraft are those caused by alterations and repairs. It is the responsibility
More informationAirport Compatibility
747X Quiet Longer Range Family Airport Compatibility April, 2002 Specific airport compatibility questions concerning commercial aircraft should be forwarded to: Airport Technology Boeing (Seattle, WA)
More informationEuropean Aviation Safety Agency
TCDS EASA.IM.A.042 Gippsland Aeronautics Page 1 of 13 Issue 6 - Series 05-Jul-2011 European Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET EASA.IM.A.042 - Series Type Certificate Holder: Airvan
More informationAirplane Performance. Introduction. Copyright 2017 Boeing. All rights reserved.
Introduction Airplane Performance The statements contained herein are based on good faith assumptions and provided for general information purposes only. These statements do not constitute an offer, promise,
More informationWorldwide Aircraft Services, Inc
Worldwide Aircraft Services, Inc Worldwide Aircraft Services, Inc. Springfield / Branson Regional Airport 2755 N. General Aviation Ave., Springfield, Missouri 65803 (417) 865-1879 # 0r Fax (417) 865-6884
More informationWeight and Balance. Chapter 10. Introduction. Weight Control
Chapter 10 and Balance Introduction Compliance with the weight and balance limits of any aircraft is critical to flight safety. Operating above the maximum weight limitation compromises the structural
More information/-400ER Freighters
s 64.44 m (211 ft 5 in ) 22.17 m (72 ft 9 in) 70.66 m (231 ft 10 in ) 19.40 m (63 ft 8 in) 11.00 m (36 ft 1 in ) Part of a complete Boeing freighter solution Revenue payload, 1,000 kg (1,000 lb) (330)
More informationTWO SISTERSHIPS BEECHCRAFT 1900D. Available for Sale
TWO SISTERSHIPS BEECHCRAFT 1900D Available for Sale 25 OCTOBER 2017 These superbly maintained commercial aircraft are available for immediate sale by their owner Registered in Central Asia Fully AD/SB-compliant
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION FAA TYPE CERTIFICATE DATA SHEET NO. A55NM
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A55NM Revision 7 328 Support Services GmbH Dornier Model 328-300 September 8, 2016 FAA TYPE CERTIFICATE DATA SHEET NO. A55NM This data sheet
More informationAircraft General Specifications
Aircraft General Specifications Boeing Serial Number: 737-522 This document has been prepared on the basis of information as made available. It provides basic information to prospect clients and is neither
More informationGuyana Civil Aviation Authority. ATR Form M Instructions
Guyana Civil Aviation Authority ATR Form M Instructions P a g e 2 Submission of ATR Forms The ATR Forms were developed in MS Excel so as to be used to submit data electronically. Completed electronic ATR
More informationAircraft Details. Airframe Status (as of 03-May-2018)
Aircraft Details Approach Category IIIa ETOPS Capability t Capable TSN / CSN(03-May-2018) 39,561 / 41,195 Engine Model PW150A DOM 28-Sep-2001 Max Certified Thrust Rating 5,071 Lbs ise Compliance II Current
More informationDiamond Aircraft Industries GmbH N.A. Otto-Str.5 A-2700 Wiener Neustadt Austria
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A47CE Revision 12 DIAMOND DA 40 DA 40 F DA 40 NG FEB 21, 2014 TYPE CERTIFICATE DATA SHEET NO. A47CE This data sheet which is part of Type Certificate
More informationFLIGHT AND OPERATING MANUAL SUPPLEMENT FMS305902, REVISION 1 SEAPLANES WEST INC.
FLIGHT AND OPERATING MANUAL SUPPLEMENT FMS305902, REVISION 1 AEROCET 3500/3500L FLOAT INSTALLATION ON CESSNA 182E THROUGH 182N AIRCRAFT AIRCRAFT MODEL: AIRCRAFT REGISTRATION: AIRCRAFT SERIAL NUMBER: TRANSPORT
More informationWeight and Balance. Chapter 9. Introduction. Weight Control
Chapter 9 and Balance Introduction Compliance with the weight and balance limits of any aircraft is critical to flight safety. Operating above the maximum weight limitation compromises the structural integrity
More informationWeight and Balance User Guide
Weight and Balance User Guide Selecting the Weight and Balance tab brings up the Departure and Destination screen, used for initiating the process for a standalone WB report. Select the tail to be used
More informationJanuary 2018 Air Traffic Activity Summary
January 2018 Air Traffic Activity Summary Jan-2018 Jan-2017 CY-2018 CY-2017 Passengers 528,947 505,421 4.7% 528,947 505,421 4.7% Passengers 537,332 515,787 4.2% 537,332 515,787 4.2% Passengers 1,066,279
More informationCRUISE TABLE OF CONTENTS
CRUISE FLIGHT 2-1 CRUISE TABLE OF CONTENTS SUBJECT PAGE CRUISE FLIGHT... 3 FUEL PLANNING SCHEMATIC 737-600... 5 FUEL PLANNING SCHEMATIC 737-700... 6 FUEL PLANNING SCHEMATIC 737-800... 7 FUEL PLANNING SCHEMATIC
More informationDornier OE-LIR MSN 3115
Dornier 328-100 OE-LIR MSN 3115 SPECIFICATION SUMMARY Manufacturer Date Current Hours Current Cycles 2000 24925 24253 Prepared by Matthias Miller, with best knowledge of 30th May 2017 CONTENTS 1 GENERAL...3
More informationInvestigation Report. Bundesstelle für Flugunfalluntersuchung. Identification. Factual information
Bundesstelle für Flugunfalluntersuchung German Federal Bureau of Aircraft Accidents Investigation Investigation Report EX007-0/02 April 2004 Identification Kind of occurrence: Serious incident Date: 29
More informationAirport Compatibility Brochure 737 MAX
Airport Compatibility Brochure 737 MAX Specific airport compatibility questions concerning Boeing commercial aircraft should be forwarded to: June 2017 BOEING is a trademark of Boeing Management Company.
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET NO. EASA.A.644 for WT9 Dynamic LSA Type Certificate Holder Aerospool, spol. s r. o. Letisková 10, 971 03 Prievidza Slovak Republic For models: Club TE.CERT.00048-001 European
More information@AIRBUS A /-600 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING
@AIRBUS A340-500/-600 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING AC The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents
More informationBDSF SPECIAL FREIGHTER CONVERSION
phone: 407.517.0300 email: freighters@cargoleasing.com web: www.cargoleasing.com 767-300BDSF SPECIAL FREIGHTER CONVERSION Aircraft Length vs 767-200 FWD PLUG (121 ) AFT PLUG (132 ) MAIN DECK CARGO DOOR
More informationRV10 Weight and Balance
RV10 Weight and Balance Author: Greg Hale -------- ghale5224@aol.com Rev. Date: 4/15/2008 11:43:34 AM The RV10 weight and balance program was designed for the Van's RV10 aircraft. The program includes
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION FAA TYPE CERTIFICATE DATA SHEET NO. A45NM
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A45NM Revision 8 328 Support Services GmbH Dornier Model 328-100 September 9, 2016 FAA TYPE CERTIFICATE DATA SHEET NO. A45NM This data sheet
More informationSubpart H. 2042/2003
AIRWORTHINESS NOTICE Issue of Certificate of Airworthiness No 12 Issue 3 May 2014 1 Purpose and scope The Civil Aviation Directive CAD-AIRW/8(1)-1 incorporates the Annex Part 21 to the European Commission
More informationREQUEST FOR PROPOSAL (RFP) SCHEDULE FOR ACMI (WET) LEASE OF TWO AIRCRAFT. (Ref: RFP Notice No ; Date: 22 November 2018)
01. INTRODUCTION REQUEST FOR PROPOSAL (RFP) SCHEDULE FOR ACMI (WET) LEASE OF TWO AIRCRAFT (Ref: RFP Notice No. 30.34.2600.011.178.660.2018; Date: 22 November 2018) Biman Bangladesh Airlines Ltd. (Biman)
More information717 Aeroplane JAA Data Sheet
The Following Content of this Data Sheet is Complete In Accordance With the Concurrent and Cooperative Certification Process (CCC) Working Procedure, Draft Issue 8 dated 17-May-1994 and JAA Administrative
More informationREPORT A-024/2012 DATA SUMMARY
REPORT A-024/2012 DATA SUMMARY LOCATION Date and time Sunday, 1 July 2012; 08:45 UTC 1 Site La Juliana Aerodrome (Seville, Spain) AIRCRAFT Registration Type and model Operator HA-NAH SMG-92 Turbo Finist
More informationTRAFFIC COMMERCIAL AIR CARRIERS
INTERNATIONAL CIVIL AVIATION ORGANIZATION AIR TRANSPORT REPORTING FORM (01/00) Page of Contact person for inquiries: Organization: Tel.: Fax: E-mail: State: Air carrier: Month(s): Year: 20 TOTAL ALL SERVICES
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION. TYPE CERTIFICATE DATA SHEET No. A00006WI
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A00006WI Revision 6 HAIC Y12 IV Y12E February 7, 2013 TYPE CERTIFICATE DATA SHEET No. A00006WI This data sheet, which is part of Type Certificate
More informationBy providing more capacity than any other twin-engine freighter, the 777F brings new levels of efficiency to the long-haul market.
By providing more capacity than any other twin-engine freighter, the 777F brings new levels of efficiency to the long-haul market. 04 aero quarterly qtr_02 09 777 Freighter: Efficiency for Long-Haul Operators
More information1.0 SCOPE AND INTRODUCTION. 1.1 Scope. 1.2 Introduction. 1.3 A Brief Description of the
1.0 SCOPE AND INTRODUCTION 1.1 Scope 1.2 Introduction 1.3 A Brief Description of the 747-400 DECEMBER 2002 1 1.0 SCOPE AND INTRODUCTION 1.1 Scope This document provides, in a standardized format, airplane
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET A2NM
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A2NM Revision 15 BOEING 757-200 Series 757-200PF Series 757-200CB Series September 1, 1998 TYPE CERTIFICATE DATA SHEET A2NM This data sheet,
More informationType Acceptance Report
TAR 13/21B/8 PIPER PA-20 Aircraft Certification Unit TABLE OF CONTENTS EXECUTIVE SUMMARY 1 1. INTRODUCTION 1 2. ICAO TYPE CERTIFICATE DETAILS 1 3. TYPE ACCEPTANCE DETAILS 1 4. NZCAR 21.43 DATA REQUIREMENTS
More informationVersion 8.5 PENTAGON 2000 SOFTWARE. Flight Operations Module
Version 8.5 PENTAGON 2000 SOFTWARE Pentagon 2000 Software 15 West 34 th Street 5 th Floor New York, NY 10001 Phone 212.629.7521 Fax 212.629.7513 TITLE: PART: Quality MODULE: BUILD 8.5.54.113.18 RESPONSIBILITY:
More informationCESSNA SECTION 5 PERFORMANCE
CESSNA SECTION 5 TABLE OF CONTENTS Page Introduction............................................5-3 Use of Performance Charts................................5-3 Sample Problem........................................5-4
More informationCHAPTER 3 PREFLIGHT ACTION TABLE OF CONTENTS
CHAPTER 3 PREFLIGHT ACTION TABLE OF CONTENTS Cessna 172 Flight Standards Manual GENERAL...2 Preflight Action Philosophy...2 Flight Crew Preflight Procedures...2 Blank TOLD Card (both sides)...3 Blank Flight/Weather
More informationWeight Arm Moment. Empty Airplane Front Seats. Back Seats. Fuel. Baggage TOTAL
Homework Exercise to prepare for Class #9. Answer these on notebook paper then correct or improve your answers (using another color) by referring to the answer sheet. 1. What is the term for the reference
More informationHow to Program the PMDG 737 NGX FMC
How to Program the PMDG 737 NGX FMC Greg Whiley Aussie Star Flight Simulation Greg Whiley Aussie Star Flight Simulation 2 For flight simulation use only How to Program the PMDG 737-800 NGX FMC The Flight
More informationTHE ULTIMATE IN COMFORT. YOUR PERFECT BUSINESS PARTNER. PERFORMANCE DATA. 3,400 nm (6,297 km)
N991EC YOUR PERFECT BUSINESS PARTNER. Even when it comes to making what might seem more difficult journeys for an executive jet, the Legacy 600 won t let you down. You can rest assured it has outstanding
More informationPRE-SOLO KNOWLEDGE TEST Diamond Eclipse DA20-C1
PRE-SOLO KNOWLEDGE TEST Diamond Eclipse DA20-C1 Name Date 1 List the airspeeds and their definitions for your airplane. Visual Indication on the Definition Indicator (color) V SO V S1 V R V X T/O V X CRUISE
More informationP.001.FPG FUEL PLANNING GUIDE. First Edition
P.001.FPG FUEL PLANNING GUIDE First Edition Edited by: Approved by: Wilhelm Andrei Bubeneck Division Training Coordinator Lucian Cristea Division Director P.001.FPG Version 1.0 September 15, 2014 Page
More informationIATA FUEL EFFICIENCY CAMPAIGN
IATA FUEL EFFICIENCY CAMPAIGN Juergen Haacker Director, Operations Montreal, IATA Fuel Efficiency Campaign Jet fuel price driving airline fuel efficiency Increased 5% from 2003-2005 Industry is on track
More informationSAN LUIS OBISPO COUNTY REGIONAL AIRPORT ANNUAL AIRLINE PASSENGER SUMMARY SUMMARY BY YEAR AND MONTH 4/11/2018
ANNUAL AIRLINE PASSENGER SUMMARY SUMMARY BY YEAR AND MONTH 4/11/ JAN FEB MAR IL E Y T 35,023 36,435 38,282 38,390 37,848 35,589 38,325 37,433 32,324 31,169 32,771 33,627 30,978 24,586 23,382 2017 24,586
More informationValley Fliers 1402 Auburn Way North, #223 Auburn WA 98002
Valley Fliers 1402 Auburn Way North, #223 Auburn WA 98002 Instructor: Check Out Date: Phase 1: Pre-Flight Name: Certificate Number: Certificate Type: Ratings: Total Flight Time: Last 90 Days: Club check
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A24CE A24CE Revision 67 200 (A100-1 (U-21J)) 200C 200CT 200T A200 (C-12A) or (C-12C) A200C (UC-12B) A200CT (C-12D)
More informationaerogate Directory of Services and Prices 2018 Living ideas Connecting lives
aerogate Directory of Services and Prices 2018 Living ideas Connecting lives Passenger Handling & Flight Ops Effective from 1st January 2018 Contents Page Contact Details 2 1. Passenger Handling and Operations
More informationTYPICAL ERRORS. Making a keystroke or transposition
F light crews consider many factors when determining correct takeoff reference speeds, or V speeds, for a particular airplane on a particular runway. These include gross weight (GW); center of gravity;
More informationCHAPTER 2 AIRCRAFT INFORMATION SUMMARY TABLE OF CONTENTS
CHAPTER 2 AIRCRAFT INFORMATION SUMMARY TABLE OF CONTENTS General...2 Kinds of Operations...2 Structural and weight limitations...2 Maneuvering limitations...3 Flight load factor limitations...3 Power plant
More informationIN SERVICE FROM 2017 ONWARDS A /-200 P2F. Next-Generation Widebody Conversion
IN SERVICE FROM 2017 ONWARDS A0-00/-200 P2F Next-Generation Widebody Conversion A0-00/-200 P2F Proven design, high-level workmanship and expertise. A NEW GENERATION PROVEN EXPERIENCE Based on the success
More informationREQUEST FOR PROPOSAL (RFP) SCHEDULE FOR ACMI (WET) LEASE OF TWO AIRCRAFT
1. INTRODUCTION REQUEST FOR PROPOSAL (RFP) SCHEDULE FOR ACMI (WET) LEASE OF TWO AIRCRAFT (Ref: RFP Notice No. 30.34.2600.011.RFP176.126.2018, Date: 04 April 2018) Biman Bangladesh Airlines Ltd. invites
More informationJohn Leahy Chief Operating Officer, Customers Airbus Annual Press Conference
John Leahy Chief Operating Officer, Customers Airbus Annual Press Conference 13 January 2014 A year of new industry records 2013 result Previous records Airbus records Airbus orders 1,619 gross 1,608 (Airbus
More informationGOVERNMENT OF INDIA OFFICE OF THE DIRECTOR GENERAL OF CIVIL AVIATION OPP SAFDURJUNG AIRPORT, NEW DELHI
GOVERNMENT OF INDIA OFFICE OF THE DIRECTOR GENERAL OF CIVIL AVIATION OPP SAFDURJUNG AIRPORT, NEW DELHI CIVIL AVIATION REQUIREMENTS SECTION 8 AIRCRAFT OPERATIONS SERIES ' D', PART I ISSUE I, DATED 3 rd
More informationA318/A319/A320/A321 PERFORMANCE TRAINING MANUAL STANDARD PERFORMANCE PART OF TRANSITION COURSE WITH FOVE TOOL
A318/A319/A320/A321 PERFORMANCE TRAINING MANUAL STANDARD PERFORMANCE PART OF TRANSITION COURSE WITH FOVE TOOL Rtr: U0Q2SP0 This document must be used for training purpose only. Under no circumstances
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A20WE BOEING Revision 45 747-100 Series 747-200B Series 747-200F Series 747-200C Series 747SR Series 747SP Series 747-100B Series 747-300 Series
More informationUniversity of Colorado, Colorado Springs Mechanical & Aerospace Engineering Department. MAE 4415/5415 Project #1 Glider Design. Due: March 11, 2008
University of Colorado, Colorado Springs Mechanical & Aerospace Engineering Department MAE 4415/5415 Project #1 Glider Design Due: March 11, 2008 MATERIALS Each student glider must be able to be made from
More informationOffers for Sale Q400. Serial Number 4162 TTSN 10,168 TCSN 11,241
Offers for Sale Q400 Serial Number 4162 TTSN 10,168 TCSN 11,241 Check Status: Aircraft will receive a fresh C1 / C2 and 6 year inspection immediately prior to return Cabin Interior: 72 B/E Aerospace Model
More informationPictures shown are artist s renderings Artist rendering
Pictures shown are artist s renderings A TRULY 21 ST CENTURY JET. The Legacy 600 makes perfect business sense in today s market. A Super Mid-Size jet with incredible comfort and reliability. Even when
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A51NM East Falcon Drive Mesa, Arizona 85215
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A51NM Marsh Aviation Company S2F-3T May 21, 1999 TYPE CERTIFICATE DATA SHEET NO. A51NM This data sheet, which is a part of Type Certificate
More informationA Human Factors Approach to Preventing Tail Strikes. Captain Vern Jeremica Senior Safety Pilot Boeing Commercial Airplanes May 2004
A Human Factors Approach to Preventing Tail Strikes Captain Vern Jeremica Senior Safety Pilot Boeing Commercial Airplanes May 2004 1 Presentation Overview Tail strike statistics as of 2003 Engineering/procedural
More informationAirport Compatibility Brochure 737 MAX. March 2014 PRELIMINARY
Airport Compatibility Brochure 737 MAX March 2014 BOEING is a trademark of Boeing Management Company. Copyright 2013 Boeing. All rights reserved. PRELIMINARY Specific airport compatibility questions concerning
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET NO. EASA.A.573 for Virus SW 121 Type Certificate Holder Pipistrel d.o.o. Ajdovščina Goriška cesta 50A 5270 Ajdovščina Slovenia, Europe For models: Virus SW 121 TE.CERT.00048-001
More informationEuropean Aviation Safety Agency
TCDS No.: EASA.IM.A.S.02479 Boeing 737 Page 1 of 7 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET No. EASA.IM.A.S.02479 for IAI/Bedek Aviation Group Boeing 737-400 SF Special Freighter
More informationF I N A L R E P O R T ON SERIOUS INCIDENT OF THE AIRCRAFT SR-20, REGISTRATION D-ELLT, WHICH OCCURED ON MAY , AT ZADAR AIRPORT
THE REPUBLIC OF CROATIA Air, Maritime and Railway Traffic Accident Investigation Agency Air Traffic Accident Investigation Department CLASS: 343-08/17-03/03 No: 699-04/1-18-15 Zagreb, 8 th June 2018 F
More informationForward Galley with Crew Rest Configuration Total Time Since New: 3,645.7 Hours
Gulfstream G550 #5109 Forward Galley with Crew Rest Configuration Total Time Since New: 3,645.7 Hours Cycles: : 1,120 AIRFRAME Manufacturer: Gulfstream Model: GV-SP (G550) Registration: N818HK Year built:
More informationCAR AIR CONTINUING AIRWORTHINESS (GENERAL AVIATION OPERATIONS)
CONTINUING AIRWORTHINESS (GENERAL AVIATION OPERATIONS) FOREWORD CONTENTS REVISION RECORD LIST of EFFECTIVE PAGES This Page Intentionally Left Blank FOREWORD The Civil Aviation and Maritime Navigation Authority
More informationGuidelines for Life Limited Part (LLP) Movement History Sheet
Guidelines for Life Limited Part (LLP) Movement History Sheet 1. Background 1.1. History Transfer of LLPs between owners/operators has in the past caused issues and time consuming tasks. Operators have
More informationContent of Description
APPENDIX B : DESCRIPTION OF FLIGHT ATTENDANT PRACTICAL TEST STANDARD PTS 8081-11 Content of Description 1. OBJECTIVE OF FLIGHT ATTENDANT PRACTICAL TEST. 2. FLIGHT ATTENDANT PRACTICAL TEST AREAS. I. PREFLIGHT
More informationAirport Monthly Air Transport Movements Guidance Notes CAA Business Intelligence
General s This form is to be completed monthly by s with an annual volume of more than 150,000 terminal passengers and/or more than 30 million kilograms of cargo. Data is due 21 calendar days following
More informationTopanga Air Finance Years of Experience at your Service. Boeing B737-5Y0. Total Flight Hours:
Boeing B737-5Y0 Aircraft Make: B737-5Y0 Total Flight Hours: 49 693 Total Flight Cycles: 36 965 As Of: 31-mar-11 General Requirements - Noise Compliant Stage III - Approach Category Cat III A (currently
More informationSpecifications GLOBAL Serial Number 9523
Specifications GLOBAL 6000 Serial Number 9523 AIRCRAFT EXECUTIVE SUMMARY A GREAT PEDIGREE Sparfell & Partners is pleased to offer, for immediate sale, this immaculate 2012 Global 6000. Executive Summary
More informationAs Authorized Marketing Agents for SAS, Bombardier Presents for Sale Q400 Aircraft
As Authorized Marketing Agents for SAS, ombardier Presents for Sale Q400 Aircraft - 4012 Rev. 6 Aircraft Summary: The Q400 is an extraordinary modern technology turboprop, offering airlines exceptional
More information