2001 EMBRAER ERJ-145LR


2001 EMBRAER ERJ-145LR

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  • Year: 2001
  • Model: ERJ-145LR
  • Serial Number: MSN 145523
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Description

General Specs Passenger Seats: 50 Configuration: Commuter – Forward Galley / Aft Lavatory Interior: New Carpet & Upholstery (Refurbished) Exterior: White Paint Scheme (Recent Application) Avionics Suite: Honeywell Maximum Certified Weights Max Takeoff Weight: 22,600 kg / 49,810 lbs Max Landing Weight: 19,800 kg / 43,639 lbs Max Zero Fuel Weight: 18,400 kg / 40,553 lbs Max Taxi Weight: 22,700 kg / 50,030 lbs Engines – Rolls-Royce AE3007A1P LEFT ENGINE (CAE-310125): TSN: 42,032.95 Hrs | CSN: 33,659 TSLSV: 2,298.75 Hrs | CSLSV: 2,049 Limiting Component: 11th Stage Compressor Wheel (4,201 FC remaining) RIGHT ENGINE (CAE-312010): TSN: 37,088.71 Hrs | CSN: 31,422 TSLSV: 2,042.59 Hrs | CSLSV: 1,833 Limiting Component: HPT Spacer (5,433 FC remaining) Avionics & Systems ADS-B Out – Honeywell (2x, PN: 7510733-623) TCAS 7.1 – Honeywell EGPWS – Honeywell FMS V6.1 – Honeywell (2x) GPS – Honeywell CVR – Allied Signal FDR – Honeywell ELT – Artex Modifications and Service Bulletins Cockpit security door installed (STC ST01409LA – January 2003) Coffee brewers installed (STC ST09858SC – July 2004) Bleed system insert installed (STC ST03994A – February 2015) MiniQAR installed (STC ST02472AT – June 2015) ADS-B Out installed (EMB SB 145-34-0118 – May 2015) FADEC upgraded to software version B9.4.1 (EMB SB 145-73-0043 – April 2016) Nose landing gear modifications for increased weight (EMB SB 145-32-0111 Rev.04 – September 2017) Structural reinforcement for increased weights (EMB SB 145-53-0068 – September 2017) Aircraft modified to meet increased MTOW and MZFW (EMB SB 145-00-0032 – September 2017) FMS upgraded from NZ 5.2 to NZ 6.1.1 (March 2025) Maintenance Status 2A Check performed at 42,176.52 hours – 208.75 hours remaining 2C Check last done at 37,496.22 hours – 5,471.55 hours remaining 30-Month Check last done at 44,931.55 hours – 1,963.78 hours remaining 3C Check due at 57,431.55 hours – 14,463.78 hours remaining 4A Check last done at 44,431.55 hours – 1,463.78 hours remaining 48-Month Check due December 2026 60-Month Check due August 2027 120-Month Check due August 2032 Landing Gear Status Nose gear last overhauled August 2024 – 20,000 flight cycle interval Left main gear last overhauled July 2019 – 20,000 flight cycle interval Right main gear overhaul data not listed Shock absorber life limited to 14,949 flight cycles or 47.5 months Features & Highlights Fresh interior upgrades completed White paint scheme in excellent condition Fully ADS-B Out compliant FMS and FADEC software upgrades completed Weight increase modifications implemented Well-maintained with full records available

Airframe
Total Time 1631 Hours
Total Landing 5939
Range 312 NM
Max Take Off Weight 5732 lb
Basic Operating Weight 0 lb
Complete Logs Yes
Airframe Notes NON-AIRWORTHY Note: This helicopter is sold exclusively as part of a package with the 1997 AS355 N (HK-4795). They will not be sold separately.
Engine1
Engine1 Manufacturer Safran
Engine1 Model Arrius 1A
Engine1 Serial Number 2007
Engine Time 1571
Engine1 Notes TT: 1571 - CY NG: 1970 - CY NTL: 2550
Engine2
Engine2 Manufacturer Safran
Engine2 Model Arrius 1A
Engine2 Serial Number 2048
Engine2 Time 2500
Engine2 Notes TT: 2500 - CY NG: 3486 - CY NTL: 4627
Inspections Status
Inspection Status Note The maintenance is carried out in accordance with the maintenance manual for these helicopters. Periodic inspections are performed based on flight hours and calendar time, as detailed in the status report.
Airworthy NO