for sale: two saab 340b aircraft serial numbers: 184 ... specifications.pdffor sale: two saab 340b...
TRANSCRIPT
For Sale:
Two SAAB 340B Aircraft
Serial Numbers:
184 & 191
Registration Numbers:
N300CE & N301CE
By:
1 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
AIRCRAFT TECHNICAL SPECIFICATIONS
General
Aircraft Manufacturer SAAB Aircraft
Aircraft Type SAAB 340B
Serial Number 184
Date of Manufacture April 1990
Country of Registration USA
Registration Number N300CE
Engine Type General Electric CT7-9B
Operating Weights
Maximum Take-off Weight 29,000 Lbs.
Maximum Landing Weight 28,500 Lbs.
Maximum Zero Fuel Weight 26,500 Lbs.
Operating Empty Weight 19,522 Lbs.
Fuel Capacity 5,690 Lbs.
Interior Configuration
Current Configuration Passenger
Number and Location Of Galleys 1 Forward
Number and Location of Lavatories 1 Forward
2 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
Operator Information
Current Operator Chicago Express
Average Daily Utilization (Check Reliability Report) 5.4 Hours/Day
Historical Yearly Utilization 1,874 Hours/Year 2,291 Cycles/Year
Type Of Operation (Scheduled Passenger, Cargo) Scheduled Passenger
Operators Main Base Chicago, Illinois
Operating Environment (Coastal, Desert, Continental) Continental US/Northeast
Aircraft History
Previous Operator American Eagle
3 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
Aircraft Technical Specifications
Data Effective Date: January 11, 2005
Total Aircraft Hours 29,116
Total Aircraft Cycles 34,369
Airframe Maintenance Program Summary
“A/B” Check Every
400 Hours
4,000 Hour Check Every
4,000 Hours
8,000 Hour Check Every 8,000 Hours
12 Month Check Every 12 Months
Current Status of Intermediate and Heavy Maintenance Visits Last Accomplished Next Due In
“4,000 Hour” Check 9-16-04 3,333 Hours
“8,000 Hour” Check 6-29-03 4,533 Hours
12 Month Check 1-29-04 24 Days
4 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
COMPONENT STATUS
Engines Data Effective Date: January 13, 2005
Engine Type: GE CT7-9B
Current Location
Serial Number TT/TC TSLSV Limit
Item Cycles
Remaining
Left Engine 785353 23,199 Hours 29,260 Cycles
4,558 Hours
Stage 2 FWD Cool
Plate
2,365 Cycles
Right Engine 785528 21,789 Hours 26,017 Cycles 544 Hours Turbine
Inter Seal 6,181 Cycles
Notes: Engine Serial Number 785353 is installed on aircraft Tail Number N301CE Engine Serial Number 785528 is installed on aircraft Tail Number N300CE
Landing Gear
Data Effective Date: January 13, 2005
Position and Location Serial Number
Interval Between Overhaul
Cycles Remaining
Nose LK9101190 15,000 Cycles 10,600 Cycles
Left Body LK9104546 15,000 Cycles 4,357 Cycles
Right Body LK8908035 15,000 Cycles 3,859 Cycles
5 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
Propellers
Data Effective Date: January 13, 2005
#1 Position Component
Serial Number
Interval Between Overhaul
Remaining Percent Remaining
LT Hub 130 7,000 Hours 5,315 Hours 76 %
Blade 1 879462 7,000 Hours 5,728 Hours 82%
Blade 2 875395 7,000 Hours 6,712 Hours 96%
Blade 3 863665 7,000 Hours 2,344 Hours 33%
Blade 4 866035 7,000 Hours 4,164 Hours 59%
#2 Position Component
Serial Number
Interval Between Overhaul
Remaining Percent Remaining
RT Hub 391 7,000 Hours 2,555 Hours 37%
Blade 1 885887 7,000 Hours 2,555 Hours 37%
Blade 2 876767 7,000 Hours 3,810 Hours 54%
Blade 3 887265 7,000 Hours 4,164 Hours 59%
Blade 4 869072 7,000 Hours 4,986 Hours 71%
6 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
Airframe History of Major Damage? No: X* Yes: ______ *According to operator supplied data.
FAA approvals per: N/A
Interior Configuration Data
Total Number of Passenger Seats 34
Class Breakout Single Class
Number and Location of Galleys 1 Forward
Number and Location of Lavatories 1 Forward
Number of Crew Seats 3 Cockpit, 1 Cabin
Aircraft Paint Scheme Blue and White
7 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
Additional
Cargo Loading System No
FAR 121 Compliant Yes
TCAS Yes
Windshear No Extended Range Over Water Operation
(ETOPS) No
FAR part 36, Stage III Noise Compliant Yes Reduced Vertical Separation Minimums
(RVSM) No
How Are Operators Manuals Maintained (Hard Copy, CD ROM, Tape) 1 Master Hardcopy / CD ROM
Able Obtain Organizational Chart No
LOPA Drawing Supplied No
Deferred Maintenance
Total Number of deferred maintenance items: One. Do the deferred maintenance items exceed US $25,000? No.
Airworthiness Directives
All ADs are believed to be up to date. AD list provided upon request.
8 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
Effective: 1/13/05
Cycle Life Cycle Life Cycle Life Cycle LifeLimit Remaining Limit Remaining
GG Turbine Shaft 28,200 19,245 28,200 10,057Rear Shaft 31,800 20,554 31,800 18,400
Tie Rod 40,000 33,831 40,000 23,035Compressor Impeller 18,600 9,645 18,600 12,613
Stage 1 Blisk 26,900 8,605 26,900 8,893Stage 2 Blisk 20,800 3,192 20,800 6,994
Stage 3-4 Blisk 18,000 11,831 18,000 12,013Stage 5 Blisk 35,100 16,084 35,100 10,765
Stage 2 RR Cool Plate 15,000 8,831 15,000 14,229Stage 2 Disk 15,000 8,831 15,000 11,454
Stage 2 Fwd. Cool Plate 13,200 2365* 13,200 12,429Stage 1 RR Cool Plate 15,000 8,831 15,000 14,229
Stage 1 Disk 15,000 2,840 15,000 11,454Stage 1 Fwd. Cool Plate 15,000 8,831 15,000 6,663
Stage 3 Disk 18,600 12,431 18,600 11,823Stage 4 Disk 18,600 12,431 18,600 17,829
PT Dive Shaft 30,000 5,744 30,000 22,048Turbine Inter Seal 16,000 9,831 16,000 6181*
SUM TOTAL 390,800 201,588 390,800 224,928AVERAGES 21711.11 11199.33 21711.11 12496.00
51.58% 57.56%
*Limiting Component
N300CE ENGINE DISK LIFE
ENGINE S/N 785353 ENGINE S/N 785528
Item
9 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
Avionics List
Nomenclature Manufacturer MODEL QTY.Stall Warning Comp Rosemont 20AK1/2 2ADC Collins ADC-81 1ACARS Collins DLM-700C 1Radio Altimeter Colllins ALT-55 1Display Processor Collins Not Visible 2VHF Comm Collins VHF-22A 2Master Warning Dowty 1ADF Receiver Collins ADF-60 2Flight Control Comp Collins FCC-85B 1VOR/ILS Collins VIR-32 2DME Collins DME-42 2TCAS Computer Collins TTR-920 1ATC (Mode S) Collins TDR-94D 2Multi-function Proc Collins MPU*** 1Attitude Heading Comp Collins AHC-85 2Emergency Power Supp Jet PS-835D 1FDAU Teledyne 70-251 1Passenger Address Collins 346D2B 1DFDR Not Visible 1CVR Not Visible 1Printer (Flight Deck) Not Visible 1Radar Transceiver Not Visible 1
Water Heater Deactivated
AVIONICS INVENTORY (Hands-on by ACI)
13-Jan-05SAAB 340B Serial # 184 Reg# N300CE
DEACTIVATED OR PROVISIONED SYSTEMS
10 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
AIRCRAFT TECHNICAL SPECIFICATIONS
General
Aircraft Manufacturer SAAB Aircraft
Aircraft Type SAAB 340B
Serial Number 191
Date of Manufacture May 1990
Country of Registration USA
Registration Number N301CE
Engine Type General Electric CT7-9B
Operating Weights
Maximum Take-off Weight 29,000 Lbs.
Maximum Landing Weight 28,500 Lbs.
Maximum Zero Fuel Weight 26,500 Lbs.
Operating Empty Weight 19,522 Lbs.
Fuel Capacity 5,690 Lbs.
Interior Configuration
Current Configuration Passenger
Number and Location Of Galleys 1 Forward
Number and Location of Lavatories 1 Forward
11 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
Current Operator Information
Current Operator Chicago Express
Average Daily Utilization (Check Reliability Report) 5.8 Hours/Day
Average Yearly Utilization 2,055 Hours/Year 2,369 Cycles/Year
Type Of Operation (Scheduled Passenger, Cargo) Scheduled Passenger
Operators Main Base Chicago, Illinois
Operating Environment (Coastal, Desert, Continental) Continental US/Northeast
Aircraft History
Previous Operator American Eagle
12 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
Aircraft Technical Specifications
Data Effective Date: January 11, 2005
Total Aircraft Hours 30,826
Total Aircraft Cycles 35,545
Airframe Maintenance Program Summary
“A/B” Check Every
400 Hours
4,000 Hour Check Every
4,000 Hours
8,000 Hour Check Every 8,000 Hours
12 Month Check Every 12 Months
Current Status of Intermediate and Heavy Maintenance Visits Last Accomplished Next Due In
“4,000 Hour” Check 6-5-04 2,626 Hours
“8,000 Hour” Check 2-5-03 3,442 Hours
12 Month Check 4-11-04 100 Days
13 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
COMPONENT STATUS
Engines Data Effective Date: January 13, 2005
Engine Type: GE CT7-9B
Current Location
Serial Number TT/TC TSLSV Limit Item Cycles
Remaining
Left Engine 785571 20,511 Hours 24,730 Cycles 2,857 Hours
Stage 2 Fwd. Cool
Plate
5,733 Cycles
Right Engine 785628 16,783 Hours 21,572 Cycles 4,014 Hours PT Drive
Shaft 1,708 Cycles
Note: Engine Serial Number 785571 is on aircraft tail number N307CE Engine Serial Number 785628 is on aircraft tail number N302CE
Landing Gear
Data Effective Date: January 13, 2005
Position and Location Serial Number
Interval Between Overhaul
Cycles Remaining
Percent Remaining
Nose LK9100395 15,000 Cycles 7,664 Cycles 51%
Left Body LK9201763 15,000 Cycles 2,100 Cycles 14%
Right Body LK9000236 15,000 Cycles 2,100 Cycles 14%
14 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
Propellers
Data Effective Date: January 13, 2005
#1 Position Component Serial Number
Interval Between Overhaul
Remaining Percent Remaining
LT Hub 858 7,000 Hours 2,438 Hours 35 %
Blade 1 879599 7,000 Hours 2,672 Hours 38%
Blade 2 887561 7,000 Hours 6,785 Hours 97%
Blade 3 876978 7,000 Hours 3,767 Hours 54%
Blade 4 866245 7,000 Hours 954 Hours 14%
#2 Position Component Serial Number
Interval Between Overhaul
Remaining Percent Remaining
RT Hub 20001215 7,000 Hours 5,897 Hours 84%
Blade 1 875412 7,000 Hours 1,408 Hours 20%
Blade 2 869077 7,000 Hours 774 Hours 11%
Blade 3 887490 7,000 Hours 6,391 Hours 91%
Blade 4 886382 7,000 Hours 3,160 Hours 45%
15 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
Airframe History of Major Damage? No: X* Yes: ______
*According to operator supplied data.
FAA approvals per: N/A
Interior Configuration Data
Total Number of Passenger Seats 34
Class Breakout Single Class
Number and Location of Galleys 1 Forward
Number and Location of Lavatories 1 Forward
Number of Crew Seats 4 (3 Cockpit, 1 Cabin)
Aircraft Paint Scheme Blue and White
16 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
17 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
Additional
Cargo Loading System No
FAR 121 Compliant Yes
TCAS Yes
Windshear No
Extended Range Over Water Operation (ETOPS) No
FAR part 36, Stage III Noise Compliant Yes
Reduced Vertical Separation Minimums (RVSM) No
How Are Operators Manuals Maintained (Hard Copy, CD ROM, Tape) 1 Master Hardcopy / CD ROM
Able Obtain Organizational Chart No
LOPA Drawing Supplied No
Deferred Maintenance
Total Number of deferred maintenance items: None noted upon logbook inspection. Do the deferred maintenance items exceed US $25,000? No.
Airworthiness Directives
All ADs appear to be up to date. AD list provided upon request.
18 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
Effective: 1/14/05
Cycle Life Cycle Life Cycle Life Cycle LifeLimit Remaining Limit Remaining
GG Turbine Shaft 28,200 24,282 28,200 11,270Rear Shaft 31,800 18,027 31,800 18,250Tie Rod 40,000 19,352 40,000 23,070
Compressor Impeller 18,600 14,682 18,600 13,129Stage 1 Blisk 26,900 22,982 26,900 21,429Stage 2 Blisk 20,800 16,882 20,800 15,329
Stage 3-4 Blisk 18,000 14,082 18,000 12,529Stage 5 Blisk 35,100 31,182 35,100 29,629
Stage 2 RR Cool Plate 15,000 7,533 15,000 9,529Stage 2 Disk 15,000 7,533 15,000 4,548
Stage 2 Fwd. Cool Plate 13,200 5733* 13,200 7,729Stage 1 RR Cool Plate 15,000 7,533 15,000 4,693
Stage 1 Disk 15,000 7,533 15,000 3,509Stage 1 Fwd. Cool Plate 15,000 7,533 15,000 9,529
Stage 3 Disk 18,600 14,682 18,600 11,130Stage 4 Disk 18,600 14,682 18,600 11,130
PT Dive Shaft 30,000 10,324 30,000 1708*Turbine Inter Seal 16,000 7,761 16,000 8,530
SUM TOTAL 390,800 246,585 390,800 214,962AVERAGES 21711.11 13699.17 21711.11 11942.33
63.10% 55.01%
Limiting Component*
N301CE ENGINE DISK LIFE
ENGINE S/N 785571 ENGINE S/N 785628
Item
19 of 19 ACI and owner expressly disclaim any and all liability for information, express or implied, contained in or omitted from this Fact Sheet. Nothing contained herein is, or shall be relied upon, as a representation made by ACI or owner. Only specific written representations made by owner in a written definitive agreement shall have any legal effect, subject to such limitations and restrictions as may be specified in such agreement.
Avionics List
Nomenclature Manufacturer MODEL QTY.Stall Warning Comp Rosemont 20AK1/2 2ADC Collins ADC-81 1ACARS Collins DLM-700C 1Radio Altimeter Colllins ALT-55 1Display Processor Collins Not Visible 2VHF Comm Collins VHF-22A 2Master Warning Dowty 1ADF Receiver Collins ADF-60 2Flight Control Comp Collins FCC-85B 1VOR/ILS Collins VIR-32 2DME Collins DME-42 2TCAS Computer Collins TTR-920 1ATC (Mode S) Collins TDR-94D 2Multi-function Proc Collins MPU*** 1Attitude Heading Comp Collins AHC-85 2Emergency Power Supp Jet PS-835D 1FDAU Teledyne 70-251 1Passenger Address Collins 346D2B 1DFDR Not Visible 1CVR Not Visible 1Printer (Flight Deck) Not Visible 1Radar Transceiver Not Visible 1
Water Heater Deactivated
AVIONICS INVENTORY (Hands-on by ACI)
13-Jan-05SAAB 340B Serial # 191 Reg# N301CE
DEACTIVATED SYSTEMS