| Company Brand | company’s information |
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Address :Mapna Boulevard, 7th km Malard Road, Karaj, Iran Tel:026 36196000 Website: www.mapnamk.com
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| Reference Standard(s) | Specification | Product(s) |
|---|---|---|
| Doc. Code: S1AB1A01P01 Rev.: 03 Rev. Date: 96.10.11 | MESC No.: 20.67.34.107.3 material: IN792, hot gas path coating: MCrAlY Tip seal coating: abradable | First stage blade of Gas Turbine (HPT) model no.: SGT-600 |
| Doc. Code: S1AB3A01P01 Rev.: 02 Rev. Date: 94.11.07 | MESC No.: 20.67.34.106.3 material: IN792, Tip seal coating: abradable | Third stage blade of Gas Turbine (LPT) model no.: SGT-600 |
| Doc. Code: S1AV2A01P01 Rev.: 04 Rev. Date: 97.07.14 | MESC No.: 10.67.35 .131.3 material: IN939, hot gas path coating: MCrALY | Second stage vane of Gas Turbine (HPT) model no.: SGT-600 |
| Doc. Code: R1BB1A01P01 Rev.: 06 Rev. Date: 96.12.27 | MESC No.: 20.60.17.860.4 material: IN738LC, hot gas path coating: Sermaloy J | First stage blade of Gas Turbine (HPT) model no.: Rolls Royce 1534 |
| Doc. Code: S1AB1A01P01 Rev.: 03 Rev. Date: 96.10.11 | MESC No.: 20.64.78.518.2 material: IN738LC, coating: Sermaloy J | RUSTON TB4000, 3MW-First Stage Rotor Blade (CT) |
| Doc. Code: U2AB1A01P01 Rev.: 00 Rev. Date: 94.09.18 | MESC No.: 20.64.78.519.2 material: IN738LC | RUSTON TB4000,3MW-Second Stage Rotor Blade (CT) |
| Doc. Code: U2AB2A01P01 Rev.: 00 Rev. Date: 94.09.18 | MESC No.: 20.64.74.200.2 material: IN738LC | RUSTON TA-1750, 1.3MW-First Stage Rotor Blade |
| Doc. Code: U1AB1A01P01 Rev.: 01 Rev. Date: 95.05.11 | MESC No.: 20.64.74.202.2 material: IN738LC | RUSTON TA-1750,1.3MW-Second Stage Rotor Blade |
| Doc. Code: U1AB2A01P01 Rev.: 01 Rev. Date: 95.05.11 | MESC No.: 20.25.13.259.3 material: Ni90 | RUSTON EM-85, 6.5MW-First Stage Rotor Blade |
| Doc. Code: U3AB1A01P01 Rev.: 00 Rev. Date: 93.04.21 | MESC No.: 20.25.13.459.3 material: IN738LC | RUSTON EM-85, 6.5MW-First Stage Vane (CT) |
| Doc. Code: U3AV1A02P01 Rev.: 00 Rev. Date: 94.12.09 | MESC No.: 20.25.13.460.3 material: IN738LC | RUSTON EM-85, 6.5MW-First Stage Vane (CT) |
| Doc. Code: U3AV1A03P01 Rev.: 00 Rev. Date: 94.12.09 | MESC No.: 20.25.13.461.3 material: IN738LC | RUSTON EM-85, 6.5MW-First Stage Vane (CT) |
| Doc. Code: Z1AL0AA0P01 Rev.: 02 Rev. Date: 94.04.16 | material: Hayness 230 Coating: Sermaloy J | ZORYA DU80L, 25MW-Flame Tubes (LINER) |
| Doc. Code: L1ABDA01P01 Rev.:00 Rev. Date: 96.12.06 | MESC No.: 20.10.51.110.3 material: AISI 420 | SULZER S7, 10MW-Compressor Rotor Blade stage 4 |
| Doc. Code: C1AB1A01P01 Rev.: 00 Rev. Date: 94.09.28 | MESC No.: 20.70.22.290.3 material: IN738LC | SOLAR Centaur, 3MW-First Stage Rotor Blade |
| Doc. Code: C1AB2A01P01 Rev.: 00 Rev. Date: 94.09.28 | MESC No.: 20.70.22.292.3 material: IN738LC | SOLAR Centaur, 3MW-Second Stage Rotor Blade |
| Doc. Code: C1AV3AA0P01 Rev.: 00 Rev. Date: 92.07.07 | MESC No.: 20.70.22.314.3 material: N155 | SOLAR Centaur, 3MW -Third Stage Stator Blade |
| Doc. Code: C1AV1AA0P01 Rev.: 03 Rev. Date: 94.09.28 | MESC No.: 20.70.22.716.3 material: Mar M 509, Coating: Sermaloy J | SOLAR Centaur, 3MW-First Stage Stator Blade |
| Doc. Code: C1AV2AA0P01 Rev.: 02 Rev. Date: 94.09.28 | MESC No.: 20.70.22.718.3 material: FSX 414, Coating: Sermaloy J | SOLAR Centaur, 3MW-Second Stage Stator Blade |
| Doc. Code: R1BN0BA0P01 Rev.: 00 Rev. Date: 92.01.27 | MESC No.: 20.60.15.090.2 material: AISI 321, Coating: Hardfacing | ROLLS ROYCE Avon, 13MW-Intake Guide vane (Actuator) |
| Doc. Code: R1BN0AA0P01 Rev.: 00 Rev. Date: 92.01.27 | MESC No.: 20.60.15.092.2 material: AISI 321, Coating: Hardfacing | ROLLS ROYCE Avon,13MW-Intake Guide vane (Follower) |
| Doc. Code: R1AVFAA1P01 Rev.: 00 Rev. Date: 92.06.18 | MESC No.: 20.60.15.897.3 material: Airfoil: Al 2618, Shroud: Al 5754, Coating: Green Teflon | ROLLS ROYCE Avon, 13MW-Compressor Stator Blade stage 4(3 Airfoils) |
| Doc. Code: R1AVEAA1P01 Rev.: 00 Rev. Date: 92.06.18 | MESC No.: 20.60.15.918.3 material: Airfoil: Al 2618, Shroud: Al 5754, Coating: Green Teflon | ROLLS ROYCE Avon, 13MW-Compressor Stator Blade stage 3 (4 Airfoils) |
| Doc. Code: R1AVDAA1P01 Rev.: 00 Rev. Date: 92.06.18 | MESC No.: 20.60.15.928.3 material: Airfoil: Al 2618, Shroud: Al 5754, Coating: Green Teflon | ROLLS ROYCE Avon, 13MW-Compressor Stator Blade stage 2- Three Segments (Master) |
| Doc. Code: R1AVDAA1P01 Rev.: 00 Rev. Date: 92.06.18 | MESC No.: 20.60.15.920.3 material: Airfoil: Al 2618, Shroud: Al 5754, Coating: Green Teflon | ROLLS ROYCE Avon, 13MW-Compressor Stator Blade stage 2- Three Segments |
| Doc. Code: R1AVDAA1P01 Rev.: 00 Rev. Date: 92.06.18 | MESC No.: 20.60.15.937.3 material: Airfoil: Al 2618, Shroud: Al 5754, Coating: Green Teflon | ROLLS ROYCE Avon, 13MW-Compressor Stator Blade stage 2- Fourth Segments |
| Doc. Code: RAAVAAA1P01 Rev.: 00 Rev. Date: 92.08.28 | MESC No.: 20.60.15.990.3 material: AISI 321 | ROLLS ROYCE Avon, 13MW-Compressor Stator Blade stage 00 |
| Doc. Code: RAAVAAA1P01 Rev.: 00 Rev. Date: 92.08.28 | MESC No.: 20.60.15.992.3 material: AISI 321 | ROLLS ROYCE Avon, 13MW-Compressor Stator Blade stage 00 |
| Doc. Code: R1ABBAA0P01 Rev.: 00 Rev. Date: 93.10.25 | MESC No.: 20.60.16.320.3 material: Al 2618, Coating: Airfoil: Green Teflon, Tungsten Carbide Hardface Coating | ROLLS ROYCE Avon,13MW-Compressor Rotor Blade stage 0 |
| Doc. Code: R1ABCAA0P01 Rev.: 00 Rev. Date: 93.10.25 | MESC No.: 20.60.16.311.3 material: Al 2618, Coating: Airfoil: Green Teflon, Tungsten Carbide Hardface Coating | ROLLS ROYCE Avon, 13MW-Compressor Rotor Blade stage 01 |
| Doc. Code: R1ABFA01P01 Rev.: 00 Rev. Date: 97.08.28 | MESC No.: 20.60.16.283.3 material: Ti-6Al-4V | ROLLS ROYCE Avon, 13MW-Compressor Rotor Blade stage 04 |
| Doc. Code: R1ABGA01P01 Rev.: 00 Rev. Date: 97.08.28 | MESC No.: 20.60.16.275.3 material: Ti-6Al-4V | ROLLS ROYCE Avon,13MW-Compressor Rotor Blade stage 05 |
| Doc. Code: R1ABHA01P01 Rev.: 00 Rev. Date: 97.08.28 | MESC No.: 20.60.16.263.3 material: Ti-6Al-4V | ROLLS ROYCE Avon,13MW-Compressor Rotor Blade stage 06 |
| Doc. Code: R1ABJA01P01 Rev.: 00 Rev. Date: 96.11.19 | MESC No.: 20.60.16.248.3 Ti-6Al-4V | ROLLS ROYCE Avon, 13MW-Compressor Rotor Blade stage 07 |
| Doc. Code: R1ABKA01P01 Rev.: 00 Rev. Date: 96.11.19 | MESC No.: 20.60.16.234.3 Ti-6Al-4V | ROLLS ROYCE Avon, 13MW-Compressor Rotor Blade stage 08 |
| Doc. Code: R1ABLA01P01 Rev.: 00 Rev. Date: 96.11.19 | MESC No.: 20.60.16.219.3 Ti-6Al-4V | ROLLS ROYCE Avon,13MW-Compressor Rotor Blade stage 09 |
| Doc. Code: R1ABMA01P01 Rev.: 00 Rev. Date: 96.11.19 | MESC No.: 20.60.16.208.3 Ti-6Al-4V | ROLLS ROYCE Avon,13MW-Compressor Rotor Blade stage 10 |
| Doc. Code: R1ABNA01P01 Rev.: 00 Rev. Date: 96.11.19 | MESC No.: 20.60.16.197.3 Ti-6Al-4V | ROLLS ROYCE Avon,13MW-Compressor Rotor Blade stage 11 |
| Doc. Code: R1ABQA01P01 Rev.: 00 Rev. Date: 94.01.29 | MESC No.: 20.60.16.175.3 Ti-6Al-4V | ROLLS ROYCE Avon,13MW-Compressor Rotor Blade stage 13 |
| Doc. Code: R1ABRA01P01 Rev.: 00 Rev. Date: 94.01.29 | MESC No.: 20.60.16.164.3 Ti-6Al-4V | ROLLS ROYCE Avon, 13MW-Compressor Rotor Blade stage 14 |
| Doc. Code: R1BT0AA0P01 Rev.: 01 Rev. Date: 97.06.21 | MESC No.: 20.60.17.297.3 material: Ni 263, Coating: MCrAlY+TBC, Chromium Carbide Hardface Coting | ROLLS ROYCE Avon,13MW- Discharge Nozzles |
| Doc. Code: R1BV1AA0P01 Rev.: 01 Rev. Date: 91.11.23 | MESC No.: 20.60.17.352.3 material: X-40, Coating: Sermaloy J, Chromium Carbide Hardface Coating | ROLLS ROYCE Avon,13MW-First Stage Vane-Type 1534-Two segments (HP) |
| Doc. Code: R1BV1BA0P01 Rev.:01 Rev. Date: 91.11.23 | MESC No.: 20.60.17.354.3 material: X-40, Coating: Sermaloy J, Chromium Carbide Hardface Coating | ROLLS ROYCE Avon, 13MW-First Stage Vane-Type 1534-Three segments (HP) |
| Doc. Code: R1BV2BA0P01 Rev.: 02 Rev. Date: 97.12.01 | MESC No.: 20.60.17.392.3 material: IN738LC, Coating: Sermaloy J | ROLLS ROYCE Avon,13MW-Second Stage Vane-Three segments (IP) |
| Doc. Code: R1BV2AA0P01 Rev.: 02 Rev. Date: 97.12.01 | MESC No.: 20.60.17.405.3 material: IN738LC, Coating: Sermaloy J | ROLLS ROYCE Avon, 13MW-Second Stage Vane-Two segments (IP) |
| Doc. Code: R1BV3AA0P01 Rev.: 00 Rev. Date: 95.04.08 | MESC No.: 20.60.17.433.3 material: IN738LC, Coating: Sermaloy J | ROLLS ROYCE Avon,13MW-Third Stage Vane-Two segments (LP) |
| Doc. Code: R1BV3BA0P01 Rev.: 00 Rev. Date: 95.04.08 | MESC No.: 20.60.17.440.3 material: IN738LC, Coating: Sermaloy J | ROLLS ROYCE Avon, 13MW-Third Stage Vane-Three segments (LP) |
| Doc. Code: R1BB3AA0P01 Rev.: 0 Rev. Date: 95.07.17 | MESC No.: 20.60.17.952.3 material: Ni 105, Coating: Sermaloy J, Stellite 694 Hardface Welding | ROLLS ROYCE Avon, 13MW-Third Stage BLADE- LP |
| Doc. Code: R1CV1AA0P01 Rev.: 00 Rev. Date: 92.05.13 | MESC No.: 20.60.30.012.3 Material; IN738LC, Coating: Sermaloy J, Stellite 694 Hardface Welding | ROLLS ROYCE Avon, 13MW-First Stage Vane-Type 1535-Two segments (HP) |
| Doc. Code: R1CV1BA0P01 Rev.: 00 Rev. Date: 92.05.13 | MESC No.: 20.60.30.016.3 material: X-40, Coating: Sermaloy J, Chromium Carbide Hardface Coating | ROLLS ROYCE Avon,13MW-First Stage Vane-Type 1535-three segments (HP) |
| Doc. Code: A2AV1AA0P01 Rev.: 03 Rev. Date: 98.12.25 | material: IN738LC Coating: MCrAlY | BBC D13, 64MW-First Stage Vane |
| Doc. Code: A2AB1A01P01 Rev.: 01 Rev. Date: 94.02.21 | material: IN738LC Coating: MCrAlY | BBC D13, 64MW-First Stage Rotor Blade |
| Doc. Code: S1AV1AA0P01 Rev.: 01 Rev. Date: 92.11.28 | material: IN939 Coating: MCrAlY | Siemens SGT-600, 25MW-First Stage Vane |
| Doc. Code: S1AB3A01P01 Rev.: 2 Rev. Date: 94.07.07 | MESC No.: 20.67.34.106.3 material: IN792, Coating: Metco 101 Hardface Coating | Siemens SGT-600, 25MW-Third Stage Rotor Blade |
| Doc. Code: S1AB1A01P01 Rev.: 02 Rev. Date: 98.06.04 | MESC No.: 20.67.34.107.3 | Siemens SGT-600, 25MW-First Stage Rotor Blade |
| Doc. Code: S1AB2A01P01 Rev.: 02 Rev. Date: 98.06.04 | MESC No.: 20.67.34.107.3 material: IN792, Coating: MCrAlY, Metco 101 Hardface Coating | Siemens SGT-600, 25MW-Second Stage Rotor Blade |
| Doc. Code: G10AB1A01P01 Rev.: 02 Rev. Date: 94.08.18 | material: IN792, Coating: MCrAlY Metco 101 Hardface Coating | GE10-2, 10MW-First Stage Rotor Blade |
| Doc. Code: G10AB2A01P01 Rev.: 02 Rev. Date: 94.08.18 | material: GTD-111 Coating: MCrAlY+TBC Root Al Sealing | GE10-2, 10MW-Second Stage Rotor Blade |
| Doc. Code: G5BB2A01P01 Rev.: 04 Rev. Date: 95.03.01 | material: GTD-111, Coating: MCrAlY, Chromium Carbide Hardface Coating, Root Al Sealing | GE Frame 5-5002D, 32MW-Second Stage Rotor Blade |
| Doc. Code: G5BV1AA0P01 Rev.: 01 Rev. Date: 94.12.15 | material: U500, Coating: Stellite 12 Hardface Welding or HVOF Coating | GE Frame 5-5002D, 32MW-First Stage Vane |