Dodson
1975 Boeing 737-242
S/N 21186
N103HA
AIRFRAME (as of May 22,2007)
Total Airframe Hours:
56,825.65 Hrs.
Total Airframe
Cycles: 51,228 Cycles
ENGINES
|
JT8D-9A S/N 674191 |
JT8D-9A S/N 674490 |
|
Total Hours: 38,948 |
Total Hours: 84,284 |
|
Total Cycles: 53,878 |
Total Cycles: 100,155 |
|
TS Repair: 380 |
TS Repair: 1,767 |
|
CS Repair: 183 |
CS Repair: 1,989 |
LANDING GEAR
|
Position |
Intervals |
Limit |
|
Nose |
20,000 hrs |
Life Limit/CPCP Program |
|
Left Main |
20,000 hrs |
|
|
Right Main |
20,000 hrs |
AIRFRAME CHECKS
C Check – 3000 hours – 2669.35 to next 1C-4C
D Check – 2100 hours – 10112.35 to next D/7C
Nordam Hush Kit, Selcal, 11 parameters DFDR, 122 “Y” Class Seating, Complete CPCP (nose landing gear will be compliant)
AVIONICS
|
SYSTEM |
QTY |
MANUFACTURER |
MODEL |
|
ADF |
2 |
Collins |
51Y-7 |
|
ATC |
2 |
Collins |
TRA-67A |
|
Air Data Computer |
1 |
Kollsman |
KS200 |
|
Auto Flight Control System |
1 |
Collins |
SP-77 |
|
DME System |
2 |
Bendix |
KDM700B |
|
Flight Data Acquisition Unit |
1 |
Teledyne Controls Lockheed 11 Para. |
2222601 |
|
Flight Data Recorder System |
1 |
1077A500-103 |
|
|
Flight Director |
2 |
Collins |
FD108 |
|
Ground Proximity Warning System |
1 |
Sunstrand |
Mark VII |
|
HF Communication System |
1 |
Collins |
622-3371-001 |
|
Marker Beacon Receiver |
1 |
Collins |
51z |
|
Radio Altimeter System |
1 |
Bendix |
ALA-51A |
|
Selective Calling (SELCAL) System |
1 |
Motorola |
NA 135 |
|
Traffic Collision Avoidance System |
1 |
Bendix |
TPA-81A |
|
VHF Communication System |
2 |
Collins |
618M3 |
|
VHF Navigation |
2 |
King |
51RV-2 |
|
Voice Recorder System |
1 |
Fairchild Burns |
A100 |
|
Weather Radar System |
1 |
Bendix |
RDR-1E |
|
Windshear Detection |
1 |
Sunstrand |
SEE GPWS |
|
Yaw Damper |
1 |
Sperry |
2588880-901 |
|
ELT 406Mhz System |
1 |
Artex |
C406-2 |
|
RVSM Mod Accomplished "A: Check - Ethiopian 2 April 2006 |
|||
CONFIGURATION
Equipment
122 Economy Seats
Overhead Bins
G1
G6 Entry Stowage
G4 Closet
G2 Stowage
Waistcoat Closet
2 Lavatories
AIRCRAFT DATA
Fuselage Line number 438
Interior Configuration 122
Extended Over Water Capacity – No
Noise Compliance – III (Hush Kit)
Approach Category: II
Display Type – Analog
OPERATING WEIGHT & FUEL CAPACITY
Maximum Taxi Weight: 117,500 lbs
Maximum Gross Takeoff Weight 117,500 lbs
Zero Fuel Weight: 95,000 lbs
Operators Empty Weight: 63,703 lbs
Fuel Capacity: 34,592 lbs (5,163 Us Gal)
PAST OPERATORS
Nordam, Midway, Canadian, Air South, Inc., Tramon Air, Hobo Air, Inc.
CONTACT: J. R. Dodson
The Preceding Preliminary Information Is For Discussion Purposes
Only, Is Subject To Verification By Purchaser,
Is Subject To Change Without Notice, And Is Not To Be Considered A
Representation Of This Aircraft.
Interested Parties Should Rely Upon Their Own Inspection Of The Aircraft And Its
Records.
Aircraft Is Offered Subject To Prior Sale Or Withdrawal From Market.
Contact
Information:
Dodson International
2155 Vermont Rd.
Rantoul, KS 66079
Email aircraftsales@dodson.com
Telephone 1 (785) 878-4000
Fax 1 (785) 878-4444