Embraer 135
43 for sale, 5 with a US-dollar asking price. Asking prices, not sales.
What does a Embraer 135 ask?
$13,000,000 is the median of 5 US-dollar asking prices; the middle half ask $9,995,000–$13,850,000.
43 for sale now. Asking prices, not sales.
How far does a Embraer 135 fly?
Across its 13 catalog variants, book ranges run 1,480–3,200 nm; the EMB-135 flies furthest.
Still air, no reserves; catalog confidence high.
What does a Embraer 135 cost to keep?
It depends on how you fly it and where you keep it, so Sprinkle doesn’t give one figure. Work it out on your own numbers.
Go to the cost calculator →Asking price by year built
Each dot is one aircraft's asking price; the line is each year's median, the band its low–high. 2013–2015: 4 for sale, 2 priced.
The figures by year
| Year | For sale | Priced | Median ask | Low–high |
|---|---|---|---|---|
| 1999 | 1 | 0 | — | — |
| 2000 | 1 | 0 | — | — |
| 2003 | 2 | 1 | — | $3,500,000–$3,500,000 |
| 2004 | 3 | 0 | — | — |
| 2006 | 9 | 1 | — | $9,995,000–$9,995,000 |
| 2007 | 3 | 0 | — | — |
| 2008 | 4 | 0 | — | — |
| 2009 | 2 | 0 | — | — |
| 2010 | 3 | 0 | — | — |
| 2011 | 4 | 1 | — | $13,850,000–$13,850,000 |
| 2012 | 3 | 0 | — | — |
| 2013 | 1 | 0 | — | — |
| 2014 | 3 | 2 | — | $13,000,000–$16,995,000 |
Medians from 5 priced aircraft up. Asks outside 0.6–1.6× their year's median are left out.
Recently listed
View all 43 for sale →
Range by variant
Book ranges from the catalog: still air, full fuel, no reserves, at the confidence shown. Plan with your own numbers.
- EMB-1353,200 nm · high confidence
- EMB-135BJ3,200 nm · low confidence
- EMB-135BJ (Legacy 600)3,200 nm · medium confidence
- EMB-135BJ (Legacy 650)3,200 nm · medium confidence
- EMB-145XR2,000 nm · high confidence
- EMB-1451,620 nm · medium confidence
- EMB-145EP1,620 nm · medium confidence
- EMB-145ER1,620 nm · high confidence
- EMB-145LR1,620 nm · medium confidence
- EMB-145MP1,620 nm · medium confidence
- EMB-135ER1,480 nm · medium confidence
- EMB-135KL1,480 nm · high confidence
The Embraer 135 in brief
43 Embraer 135 listings are for sale across the sites Sprinkle reads as of Nov 12, 2026, built 1999–2014.
The middle half were built 2006–2011.
How the Embraer 135 performs
The longest book range across its variants is 3,200 nautical miles: still air, no reserves.
It seats up to 50 passengers.
Buying a Embraer 135
The middle half of US-dollar asks run $9,995,000–$13,850,000, around a median of $13,000,000, from 5 priced listings. Asking prices, not sales.
The middle half of those that publish airframe time show 3,575–7,263 hours, from 16 listings.
Before an offer, check
- A pre-buy inspection by a mechanic who knows the type, chosen by you, not the seller.
- Complete logbooks for the airframe, engines and propellers, with any gaps explained.
- Damage history and any repairs, against the logbooks and the registry record.
- Engine time against the overhaul interval, and the shop that did the last overhaul.
- Airworthiness directives and service bulletins: which apply, and how each was closed.
Figures from the listings Sprinkle reads, read Nov 12, 2026. A market read from asking prices, not an appraisal.
About the Embraer 135
- Manufacturer
- Embraer, Brazil
- Category
- Jet airplane
- Variants in the catalog
- 15: EMB-135, EMB-135BJ, EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER, EMB-135KE, EMB-135KL, EMB-135LR…
- Passengers, at most
- 50
- The farthest the maker says the aircraft can fly on full fuel, in still air with standard reserves. Real trips with passengers and wind come up shorter.
- 3,200 nm
- Cruise speed, fastest
- Not published
- The highest altitude at which the aircraft can still climb at 100 feet per minute. Most trips cruise well below it.
- 41,000 ft
- The heaviest the aircraft is certified to weigh at takeoff, with people, bags and fuel on board.
- 22,000 kg (48,502 lb)
- The aviation authority’s approval of an aircraft design, such as the FAA’s or EASA’s. Each model flies under one.
- FAA
From Sprinkle's aircraft catalog. Figures are the highest across the model's variants.
The Embraer 135 fleet
- Registered fleet
- 1,232
- Median age
- 23 years
- Registration changes, past 12 months
- 9
- Most built in the
- 2000s
From the national aircraft registers Sprinkle reads. Read Nov 12, 2026.
Embraer 135 type certificates
- EMB-145 FAA T00011AT
- approved Dec 10, 1996 · Federal Aviation Regulation (FAR) Part 21, including Amendments through 21-69, effective August 16, 1991; Part 25 including Amendments through 25-84, effective July 10, 1995,with the following additions: Special Condition No. 25-ANM-118: “High Intensity Radiated Fields (HIRF) Protection” (FARs 21.16, 25.1309, 25.1333 and 25.1431) Special Condition No. 25-ANM-131: “Thrust reverser systems” used as optional equipment. (FAR 21.16; for aircraft without thrust reversers, the effect of wet runway surfaces on accelerate-stop distances must be accounted for in accordance with criteria contained in NPRM 93-8 and its associated guidance; takeoff limitations for operation on wet runway surfaces must be predicated on the wet runway accelerate-stop criteria contained in NPRM 93-8) · MTOW 19,200 kg · 50 passengers · Two - Allison Engine Company Model AE 3007A · Type certificate data sheet (opens in a new tab)
- EMB-145ER FAA T00011AT
- approved Dec 10, 1996 · Federal Aviation Regulation (FAR) Part 21, including Amendments through 21-69, effective August 16, 1991; Part 25 including Amendments through 25-84, effective July 10, 1995,with the following additions: Special Condition No. 25-ANM-118: “High Intensity Radiated Fields (HIRF) Protection” (FARs 21.16, 25.1309, 25.1333 and 25.1431) Special Condition No. 25-ANM-131: “Thrust reverser systems” used as optional equipment. (FAR 21.16; for aircraft without thrust reversers, the effect of wet runway surfaces on accelerate-stop distances must be accounted for in accordance with criteria contained in NPRM 93-8 and its associated guidance; takeoff limitations for operation on wet runway surfaces must be predicated on the wet runway accelerate-stop criteria contained in NPRM 93-8) · MTOW 20,600 kg · 50 passengers · Two - Allison Engine Company Model AE 3007A, AE3007A1/1, AE3007A1/2, AE3007A1, or Model AE3007A1P · Type certificate data sheet (opens in a new tab)
- EMB-145MR FAA T00011AT
- approved May 7, 1998 · Federal Aviation Regulation (FAR) Part 21, including Amendments through 21-69, effective August 16, 1991; Part 25 including Amendments through 25-84, effective July 10, 1995,with the following additions: Special Condition No. 25-ANM-118: “High Intensity Radiated Fields (HIRF) Protection” (FARs 21.16, 25.1309, 25.1333 and 25.1431) Special Condition No. 25-ANM-131: “Thrust reverser systems” used as optional equipment. (FAR 21.16; for aircraft without thrust reversers, the effect of wet runway surfaces on accelerate-stop distances must be accounted for in accordance with criteria contained in NPRM 93-8 and its associated guidance; takeoff limitations for operation on wet runway surfaces must be predicated on the wet runway accelerate-stop criteria contained in NPRM 93-8) · MTOW 20,700 kg · 50 passengers · Two - Allison Engine Company Model AE 3007A1/1, AE 3007A1/2, AE3007A1 or AE3007A1P · Type certificate data sheet (opens in a new tab)
- EMB-145LR FAA T00011AT
- approved May 7, 1998 · Federal Aviation Regulation (FAR) Part 21, including Amendments through 21-69, effective August 16, 1991; Part 25 including Amendments through 25-84, effective July 10, 1995,with the following additions: Special Condition No. 25-ANM-118: “High Intensity Radiated Fields (HIRF) Protection” (FARs 21.16, 25.1309, 25.1333 and 25.1431) Special Condition No. 25-ANM-131: “Thrust reverser systems” used as optional equipment. (FAR 21.16; for aircraft without thrust reversers, the effect of wet runway surfaces on accelerate-stop distances must be accounted for in accordance with criteria contained in NPRM 93-8 and its associated guidance; takeoff limitations for operation on wet runway surfaces must be predicated on the wet runway accelerate-stop criteria contained in NPRM 93-8) · MTOW 22,100 kg · 50 passengers · Two - Allison Engine Company Model AE 3007A1/1, AE 3007A1/2, AE3007A1 or AE3007A1P · Type certificate data sheet (opens in a new tab)
- EMB-135LR FAA T00011AT
- approved Jul 15, 1999 · Federal Aviation Regulation (FAR) Part 21, including Amendments through 21-74, effective March 12, 1997; Part 25 including Amendments through 25-84; 25-85; FAR 25.1517 from 25-86; 25-88; 25-90; FAR 25.331, 25.335(b)(2), 25.345, 25.351, 25.363, 25.371, 25.415, 25.491, 25.499 and 25.561 from 25-91; 25-93; FAR 25.807 from 25-94; and 25-97. Special Condition No. 25-ANM-118: “High Intensity Radiated Fields (HIRF) Protection” (FARs 21.16, 25.1309, 25.1333 and 25.1431) Special Condition No. 25-ANM-131: “Thrust reverser systems” used as optional equipment. (FAR 21.16; for aircraft without thrust reversers, the effect of wet runway surfaces on accelerate-stop distances must be accounted for in accordance with criteria contained in NPRM 93-8 and its associated guidance; takeoff limitations for operation on wet runway surfaces must be predicated on the wet runway accelerate-stop criteria contained in NPRM 93-8) · MTOW 19,000 kg · 37 passengers · Two - Allison Engine Company Model AE 3007A1/3 · Type certificate data sheet (opens in a new tab)
- EMB-135ER FAA T00011AT
- approved Jul 15, 1999 · Federal Aviation Regulation (FAR) Part 21, including Amendments through 21-74, effective March 12, 1997; Part 25 including Amendments through 25-84; 25-85; FAR 25.1517 from 25-86; 25-88; 25-90; FAR 25.331, 25.335(b)(2), 25.345, 25.351, 25.363, 25.371, 25.415, 25.491, 25.499 and 25.561 from 25-91; 25-93; FAR 25.807 from 25-94; and 25-97. Special Condition No. 25-ANM-118: “High Intensity Radiated Fields (HIRF) Protection” (FARs 21.16, 25.1309, 25.1333 and 25.1431) Special Condition No. 25-ANM-131: “Thrust reverser systems” used as optional equipment. (FAR 21.16; for aircraft without thrust reversers, the effect of wet runway surfaces on accelerate-stop distances must be accounted for in accordance with criteria contained in NPRM 93-8 and its associated guidance; takeoff limitations for operation on wet runway surfaces must be predicated on the wet runway accelerate-stop criteria contained in NPRM 93-8) · MTOW 19,000 kg · 37 passengers · Two - Allison Engine Company Model AE 3007A1/3 · Type certificate data sheet (opens in a new tab)
- EMB-145MP FAA T00011AT
- approved Jul 3, 2003 · Federal Aviation Regulation (FAR) Part 21, including Amendments through 21-69, effective August 16, 1991; Part 25 including Amendments through 25-84, effective July 10, 1995,with the following additions: Special Condition No. 25-ANM-118: “High Intensity Radiated Fields (HIRF) Protection” (FARs 21.16, 25.1309, 25.1333 and 25.1431) Special Condition No. 25-ANM-131: “Thrust reverser systems” used as optional equipment. (FAR 21.16; for aircraft without thrust reversers, the effect of wet runway surfaces on accelerate-stop distances must be accounted for in accordance with criteria contained in NPRM 93-8 and its associated guidance; takeoff limitations for operation on wet runway surfaces must be predicated on the wet runway accelerate-stop criteria contained in NPRM 93-8). FAR 25 amendment 92 (final rule of the NPRM 93-8) was the means of compliance to the Special Condition. Equivalent Level of Safety Findings: - Use of 1g stall criteria (various FARs); - Cockpit underfloor access hatch and rear fuselage electronic compartment access hatch (FAR 25.783(f)); - Flight critical thrust reverser (FAR 25.933(a)(1)(ii)); - Turbine engine tailpipe fire detection (FAR 25.1203(a)); - Digital only display of turbine engine high/intermediate pressure rotor speed (N2) (FAR 25.1305(c)); -APU instrumentation and monitoring requirements (FAR 25.1305 and 25.1501(b)); and - Cabin Altitude Warning System – High Altitude takeoff and landing Operations – (FAR 25.841(b)(6)) for EMB-145XR and EMB-145LR. ELOS Memo AT0134IB-T-S-1. Optional Requirements: Optional compliance to the icing requirements of FAR 25.1419 was demonstrated. Compliance to the ditching requirements of FAR 25.801 have not been demonstrated. The EMB-145 ( ) models are approved with the thrust reversers removed. Noise standard : FAR 36 - including amendment 36-1 through 36-21, effective January 21, 1996. Fuel venting and exhaust emission : FAR 34 - including amendment 34-1 through 34-2 effective January 21, 1996. · MTOW 20,990 kg · Two Rolls Royce Corporation AE 3007A, AE3007A1/1, AE3007A1/2, AE3007A1, or Model AE3007A1P · Type certificate data sheet (opens in a new tab)
- EMB-145EP FAA T00011AT
- approved Oct 14, 2003 · Federal Aviation Regulation (FAR) Part 21, including Amendments through 21-69, effective August 16, 1991; Part 25 including Amendments through 25-84, effective July 10, 1995,with the following additions: Special Condition No. 25-ANM-118: “High Intensity Radiated Fields (HIRF) Protection” (FARs 21.16, 25.1309, 25.1333 and 25.1431) Special Condition No. 25-ANM-131: “Thrust reverser systems” used as optional equipment. (FAR 21.16; for aircraft without thrust reversers, the effect of wet runway surfaces on accelerate-stop distances must be accounted for in accordance with criteria contained in NPRM 93-8 and its associated guidance; takeoff limitations for operation on wet runway surfaces must be predicated on the wet runway accelerate-stop criteria contained in NPRM 93-8). FAR 25 amendment 92 (final rule of the NPRM 93-8) was the means of compliance to the Special Condition. Equivalent Level of Safety Findings: - Use of 1g stall criteria (various FARs); - Cockpit underfloor access hatch and rear fuselage electronic compartment access hatch (FAR 25.783(f)); - Flight critical thrust reverser (FAR 25.933(a)(1)(ii)); - Turbine engine tailpipe fire detection (FAR 25.1203(a)); - Digital only display of turbine engine high/intermediate pressure rotor speed (N2) (FAR 25.1305(c)); -APU instrumentation and monitoring requirements (FAR 25.1305 and 25.1501(b)); and - Cabin Altitude Warning System – High Altitude takeoff and landing Operations – (FAR 25.841(b)(6)) for EMB-145XR and EMB-145LR. ELOS Memo AT0134IB-T-S-1. Optional Requirements: Optional compliance to the icing requirements of FAR 25.1419 was demonstrated. Compliance to the ditching requirements of FAR 25.801 have not been demonstrated. The EMB-145 ( ) models are approved with the thrust reversers removed. Noise standard : FAR 36 - including amendment 36-1 through 36-21, effective January 21, 1996. Fuel venting and exhaust emission : FAR 34 - including amendment 34-1 through 34-2 effective January 21, 1996. · MTOW 20,990 kg · 50 passengers · Two Rolls Royce Corporation AE 3007A, AE3007A1/1, AE3007A1, or Model AE3007A1P · Type certificate data sheet (opens in a new tab)
From the regulators' type-certificate data sheets. Figures shown only where the reading is high-confidence.
Embraer 135 manuals and documents
From Sprinkle’s library for this model. PDFs open from Sprinkle’s own files.
What one would cost to fly
Put in your own figures; the totals update as you type.
A year at these figures
$1,637,911
- A month
- $136,493
- A flight hour, all in
- $6,552
- Flying (fuel and reserve)
- $325,000
- Fixed
- $156,000
- Loan
- $1,156,911
Fields marked Typical hold a rule-of-thumb figure for a jet: an assumption, not Sprinkle's data. Replace them with your own.
Not a quote: Sprinkle doesn't hold insurance, hangar or maintenance costs. Asking prices, not sales.
From the listings Sprinkle reads for this model. Read Nov 12, 2026.