2001 EMBRAER EMB 135

2001

EMBRAER

EMB-135

145513

Used

IFR

Highlights: • C-Check and 60 month Inspection currently in progress • ADS-B

33010

29967

Total Time Since New 33,010 (April 2019) Total Landings Since New 29,967 (April 2019) Date of Manufacturer 24th Sept 2001 Approach Category I Noise Compliance III ETOPS Capability Not Capable Winglets No Observer Crew 1 Cabin Crew 1 Stretcher capable No Interior Placards & Signs Single language (English) Model as per Type Certificate ERJ-135KL/140LR Seat Summary 44 economy Class seats Secure Cockpit Door fitted Yes Certification FAR-25 DESIGN WEIGHTS Weights Max Structural Design Per AFM Max Taxi Weight - 46,737 Max Take Off Weight - 46,515 Max Zero Fuel Weight - 37,698 Max Landing Weight - 41,225 Basic Empty Weight 26,653 Date of Last Weighing 24-Jan-17 Weights and Balance System Fitted No

None

Description Rolls Royce AE3007-A1/3 Serial Number(s) 311857 311850 Date of manufacturer 25/05/2001 21/05/2001 Status Date 22/06/2018 22/06/2018 Max Certified Thrust Rating 8,338 lbs 7,580 lbs Current Operating Thrust rating 7,201 lbs 7,057 lbs Total Hours Since New 31,578:56 29,265:21 Total Cycles Since New 25,410 25,901 TSLSV 31,578:56 29,265:21 CSLSV 25,410 25,910 Cycles Limiter (LLP) LPT Disks Fan Drive Shaft Cycles to Limiter (LLP) 9,590 7,503 On watch No No On watch Comment None None Comments Not installed (1st April 2019)

Yes

Description Hamilton Sundstrand - Model APS-500R/T-62T-40C14 Serial Number SP-E0314547 APU Total Time Since New 13,134 Cycles Since New 26,543 Status date 5/06/2018 Last Heavy Shop Visit 5/06/2018

Transceiver-Hf/Com 1 Allied Signal 064-1015-61 1 Transceiver-Vhf/Com 2 Decoder Selcal 1 Recorder SSFDR 1 Recorder CVR 1 Integrated NAV/ADF/DME 2 Wu 660 Radar Receiver/Transmitter 1 Receiver/Exciter Krx 1053 1 Rad Alt Rec/Trans 1 Autopilot Controller 1 Radio Management Unit 2 Air Data Computer 1 Integrated Avionics Comp 1 Navigation Computer 1 Flight Guidance Control 1 Radar R.T.S. 1 Antenna 1 Mk3 CMU 1 Enhanced Ground Prox 1 Flight Data Recorder 1 Cockpit Voice Recorder 1 Inertial Ref Unit 1 Global Nave Sensor 1 ADS-B

COMMUNICATIONS Component Qty Manufacturer Notes ACARS MU (or CMU) 1 Universal VHF System Integration Narrow Width Printer Located on Central Pedestal Dedicated VHF MCDU Interface No ACMS Parameters Present No Pilot Control Data Link CVR 1 Allied Signal 120 Miniute Duration Cockpit Switch Solid State Fixed ELT 1 Artex Automatic Not 406KHz Cockpit Switch Integrated VHF Comm Unit 2 Honeywell FM Immune 8.33KHz Pre-Recorded Announcement 1 Pioneer Radio Management Unit 2 Honeywell VHF Transceiver 1 Collins FM immune 8.33KHz HF ATC Transponder 2 Honeywell KHF 1050 Communication System (Receiver Transmitter) 1 Remarks • Cockpit switch for the CVR is erase and test. • Digital audio panel, 2 each. • CVR control panel has an erase and test switch. • Pre-recorded announcements are made with a Pioneer CD Player. IN-FLIGHT-ENTERTAINMENT & EMERGENCY LOCATOR TRANSMITTER (ELT) Component Qty Manufacturer Manual/Automatic 406MHz Cockpit Switch Fixed ELT 1 Socata Group Automatic Yes Yes Passenger Entertainment Audio None Passenger Entertainment Video None   NAVIGATION Component Qty/notes Manufacturer ADF Control Panel 1 Honeywell ADF Transceiver 2 Honeywell Air Data Computer 2 Honeywell ATC Transponder Type Mode S TCAS Control Panel No Distance Measuring Equipment 2 Honeywell Flight Management Computer 2 Honeywell GPWS 1 Honeywell GPWS Type EGPWS Mod 6 Call out Menu Yes Reactive Windshear Yes Position Data Source FMC Inertial Navigation System 2 Honeywell Radio Altimeter Transceiver 1 Honeywell TCAS 1 Honeywell Change 7.0 Software Yes TCAS Display EFIS Honeywell FM Immune Yes Honeywell Predictive Windshear No GPS Receiver Honeywell 2 Honeywell IM-600 configuration module 2 Honeywell IC-600 Integrated Computer 2 Honeywell FMS 2 Honeywell Aural Warning Computer (Upgraded) 1 Honeywell Additional Navigation Details RVSM Compliant Yes GPS Navigation Yes – Honeywell NZ-2000 FMS/GPS with WAAS/LPV Data Loader Installed FMS Dual (Honeywell) Jet Connect Iridium Satcom Honeywell Remarks: • The VHF Communication Units include the ATC Transponders. • INS System is AHRS. • The VHF NAV Unit includes the NAV / DME / ADF. Radio Management Unit controls VHF Communication and VHF NAV including ADF. FUEL SYSTEMS Fuel Qty Indication Units Pounds Tank Capacity 5,186 Kgs AUX Tanks No Dipstick Calibration Inches INDICATING AND RECORDING SYSTEMS Component Qty Manufacturer Flight Data Acquisition Unit 2 Honeywell Flight Data Recorder 1 Allied Signal LANDING GEAR Nose Left Main Right Main Manufacturer Liebherr Aerospace EDE EDE Part Number 1170C0000-02 2309-3002-515 2309-3002-516 Serial No 417 306 306 Status Date 43,272 43,272 43,272 Time Since New (TSN) 30,484 33,064 33,064 Cycles Since New (CSN) 28,967 29,629 29,629 Overhaul Cycles Interval 20,000 20,000 20,000 Overhaul Months Interval 144 144 144 Gear Status Exchanged Exchanged Exchanged Last Installation Date 2011-05-23 2011-04-08 2011-04-08 Last Overhaul Date 2011-04-23 2011-03-29 2011-03-29 Time Since Last Overhaul 8,236:30 8,380:39 8,380:39 Cycles Since Last Overhaul 9,715 9,919 9,919 WHEELS AND BRAKES Component Qty Manufacturer Position Brakes 4 B F Goodrich Wheels 2 B F Goodrich Nose Wheels 4 B F Goodrich Main

44

Component Qty Manufacturer/notes Economy Class Seats 44 C & D Aerospace Centre Life Raft Storage No Lavatory 1 Recirculation-Flush Handicapped Enabled Lavatory 0 Baby Changing Table 1 Power Outlet No Power Control Unit Installed No Seat Mounted Video No CARGO Deck Main Cubic Capacity 9 m³ Compartment Class C Cargo Loading System None Heating No There are no air stairs installed

MAJOR INSPECTION STATUS Inspection Next Due 1A 9 Aug 2019 2A 17 Nov 2019 3A 25 Feb 2020 4A 4 June 2020 5A 12 Sept 2020 12 month 30 April 2020 30 month 30 Oct 2020 60 month Being completed 120 month 28 April 2028 C Being completed 2C 21 Oct 2024 3C 18 July 2027 Remarks: Assuming 150 FH every 30 days and current maintenance is completed 1st May 2019 ADDITIONAL MAINTENANCE INFORMATION Aircraft Subject to Sampling Under Structural Inspection Program Full MPD Revision 15 Structural Check Required to Meet Redelivery Conditions No Last Aircraft Maintenance Status Date 2018-06-22 Time Since New (TSN) 31,346 FH Cycles Since New (CSN) 28,330 FL Engine Maintenance Program Engine Condition Monitor By Rolls Royce DeRate Policy No