ATR 42-300 Regional Turboprop Aircraft | YOM 1997 | PW121 Engines (1 Aircraft | Airworthy Configuration)
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ATR 42-300 Regional Turboprop Aircraft | YOM 1997 | PW121 Engines (1 Aircraft | Airworthy Configuration) Share with Buyers
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Welcome to Salvex Marketplace: Get surplus, salvage, and discounted ATR-42/72 parts for commercial repurposing.
Item Description
FOR SALE
Airworthy ATR 42-300 regional turboprop aircraft manufactured in 1997 and configured with Pratt & Whitney Canada PW121 engines. The aircraft is configured for 48-passenger operations and includes substantial remaining landing gear overhaul interval, recent C-check status, and detailed engine and propeller records.
Aircraft Model: ATR 42-300
Manufacturer: ATR
Year of Manufacture: 1997
Quantity: 1 Aircraft (Airworthy Condition)
Passenger Capacity: 48 Passengers
Maximum Cruise Altitude: 25,000 Feet
Cruise Speed: Mach 0.55
Fuel Capacity: 4,500 kg
Airframe Summary
Aircraft TSN: 31,397:25 Hours
Aircraft CSN: 52,390 Cycles
Maximum Taxi Weight: 17,070 kg
Maximum Zero Fuel Weight: 15,540 kg
Maximum Landing Weight: 16,400 kg
Primary Aircraft Compatibility
ATR 42-300
Additional Applications
Regional Passenger Operations
Cargo Conversion Programs
Government & Special Mission Operations
Charter & ACMI Operations
Engine Configuration
Engine Position #1
Engine Type: Pratt & Whitney Canada PW121
TSN: 18,827:57 Hours
CSN: 22,525 Cycles
Time Since Last HSI: 1,075:09 Hours
Lowest LLP Remaining: 7,932 Cycles
Engine Position #2
Engine Type: Pratt & Whitney Canada PW121
TSN: 9,079:04 Hours
CSN: 8,517 Cycles
Time Since Last HSI: 59:46 Hours
Lowest LLP Remaining: 4,431 Cycles
Primary Engine Compatibility
Pratt & Whitney Canada PW121
Landing Gear Status
Manufacturer: Messier-Dowty
Next Landing Gear Overhaul Due: September 23, 2030
Remaining Time to Overhaul
2,075 Days Remaining
17,984 Cycles Remaining
Landing Gear Positions
LH Main Landing Gear: PN D22685040-10/-12-16/-18
RH Main Landing Gear: PN D22686040-9-X-11-15-16/-18
Nose Landing Gear: PN D22698100-3-8
Aircraft Inspection Status
C Check Interval: Every 8,000 Hours
Last C Check: 31,337:39 Hours
Next C Check Due: 39,337:39 Hours
Remaining to Next C Check: Approximately 8,000 Hours
Propeller Configuration
Propeller Model: Hamilton Standard 802255-1
Position #1
Propeller Main Unit TSN: 20,708:16 Hours
TSO: 59:46 Hours
Hub PN 782701-5
Hub TSO: 59:46 Hours
Position #2
Propeller Main Unit TSN: 15,797:00 Hours
TSO: 59:46 Hours
Hub PN 782701-5
Hub TSO: 59:46 Hours
Propeller blades include multiple SFA13M1R0A and SFA13U1P0A blade assemblies with recent overhaul status.
Documentation reflects:
Airworthy aircraft status
ATR 42-300 passenger configuration
Pratt & Whitney PW121 engines
Detailed landing gear records
Engine LLP status information
Propeller maintenance records
C-check tracking
Registration valid through October 2026
Compass swing valid through July 2026
| Quantity | : | 1 Aircraft |
| Product Location | : | South America |
| Condition | : | Airworthy |
| Condition Description | : | Airworthy
Being sold "AS IS, WHERE IS". Buyer is responsible for shipping and handling. |
| Manufacturer | : | |
| | : | |
| Trader | Sudheesh Sudhakaran +1 832 548 5660 | |
| Seller | : | |
| Seller Industry | : | |
Seller Terms
- Salvex and the seller have the right to reject any and all offers.
- This product is sold AS IS, WHERE IS.
- Buyer is responsible for all taxes, duties, loading and freight charges.
- Seller does not offer any warranties or manufacturer warranties.
- Upon receipt of cleared funds, Seller will provide the Buyer a Release Order for item pick up. Title transfers from Seller to Buyer upon issuance of the Release Order.
- It is Buyer's responsibility to verify quantities and condition at the time of pick up. Once the product has been removed from Seller's location, there will be no adjustments based on quantity or condition.
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