Search results for: 'APS105-00200'

Description:

RIVET

Manufacturer:

MCFARLANE AVIATION

PartNum:

APS105-00200

UnitMeasure:

EA

Description:

RIVET

Manufacturer:

AVIATION PRODUCTS

PartNum:

APS105-00200-100

UnitMeasure:

EA

Description:

RIVET, 100PK

Manufacturer:

MCFARLANE AVIATION

PartNum:

APS105-00200-100

UnitMeasure:

EA

Description:

RIVET, 100PK

Manufacturer:

MCFARLANE AVIATION

PartNum:

APS105-00200-100

UnitMeasure:

EA

Description:

RIVET

Manufacturer:

AVIATION PRODUCTS

PartNum:

APS105-00200-PKG

UnitMeasure:

EA

ReplacedPartNumber:

Parker Hannifin P/N 105-00200

ApprovalBasis:

Identicality Per 14 CFR Part 21.303 Drawing: APS105-00200 Rev: B Dated: 2/14/02 or later FAA approved revisions

Models:

DA20, DA40, DA42

ReplacedPartNumber:

Parker Hannifin Corp P/N 105-00200

ApprovalBasis:

Identicality Per 14 CFR Part 21.303 Dwg No. APS105-00200 Rev. B Dated 2/14/02 or later FAA approved revisions

Models:

Cirrus SR20

ReplacedPartNumber:

Parker Hannifin (Cleveland) P/N 0105-00200

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No APS105-00200 Rev D Date 07/21/2014 or later FAA-approved revisions

Models:

65 (When STC SA673GL is installed), 65-90, 65-A90, 65-A90-1 (JU-21A), 65-A90-4 (RU-21E, RU-21H), B90, C90GT, C90GTi, E90, H90 (When STC SA619GL is installed), JRB-6 (When STC SA788GL is installed), D18C, D18S, E18S, E18S-9700, G18S, H18, C-45G, TC-45G, RC45J, C-45H, TC-45H, TC-45J, JRB-6, 3N, 3NM, 3TM (When STC SA1222GL has been installed)) Viking Air Limited (DHC-6-1, DHC-6-100, DHC-6-200, DHC-6-300 (When STC SA1065GL is installed)

ReplacedPartNumber:

Parker Hannifin (Cleveland) P/N 105-00200

ApprovalBasis:

Identicality per 14 CFR 21.303, DWG. No. APS105-00200 Rev. D Date July 21, 2014 Or later FAA approved revisions

Models:

Pty) Ltd (GA8, GA8-TC320

ReplacedPartNumber:

Parker Hannifin (Cleveland) P/N 105-00200

ApprovalBasis:

Identicality per 14 CFR 21.303 DWG No APS105-00200 Rev -C Date 4-16-2007 or later FAA-approved revisions

Models:

G36

ReplacedPartNumber:

Cleveland Wheels & Brakes P/N 105-00200 Rapco, Inc. P/N RA105-002 Aviation Products Systems Inc. P/N APS105-00200

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No. RA105-00200 Rev. - Date 05/15/2012*

Models:

A-9B | AT-300, AT-301, AT-302, AT-400, AT-400A, AT-401, AT-401A, AT-402, AT-501, AT-502, AT-503, AT-503-A | 17-30A, 17-31A, 17-31ATC | G-164, G-164A, G-164B, G-164B-15T, G-164B-20T, G-164-34T, G-164B (with 73 inch wing gap), G-164C, G-164D, G-164D (with 73 inch wing gap) | R 3000/160 | 150F,150G, 150H, 150J, 150K, 150L, A150L, 152, A152, F150F, F150G, F150H, F150J, F150K, FA150K, FA150L, FRA150L, F152, FA152, 172F, 172G, 172H, 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S, F172F, F172G, F172H, F172K, 177A, 177B, 177RG, F177RG, 180G, 180H, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182S, R182, TR182, FR182, 185C, 185D, 185E, A185E, A185F, 188, 188A, 188A, 188B, A188, A188A, A188B, T188C, 206, 206H, P206, P206A, P206B, P206C, P206D, P206E, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G, T206H, TP206A, TP206B, TP206C, TP206D, TP206E, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G, 207, 207A, T207, T207A, 210-5A (205A), 210C 210D, 210E, 210F, 210G, 210H, 210J, 210K, 210L, 210M, P210N, 210R, P210R, T210F, T210G, T210H, T210J, T210K, T210L, T210M, T210N, T210R, 336 337, 337A, 337B, 337C, 337D, T337B, T337C, T337D, 120, 140, 140A, 170, 170A, 170B, 172, 172A, 172B, 172C, 172D, 172E, 175, 175A, 175B, 175C, P172D, 180, 180A, 180B, 180C, 180D, 180E, 180F, 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G (When STC SA13GL is installed), 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K, 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F, 206, P206, U206, U206F, U206G, TU206E, TU206F, TU206G (When STC SA63GL is installed), 180, 180A, 180B, 180C, 180D, 180E, 180F, 180H, 180J, 185, 185A, 185B, A185E, A185F, 206E, 206F, TU206E, TU206F, 210, 210A, 210B, 210C, 210K, 210L, 210M, T210C, T210K, T210L, T210M (When STC SA52GL or SA62GL is installed), P210N (When STC SA54GL is installed) | SR20, SR22, SR22T | 112, 112B, 112TC, 112TCA, 114, 114A, 114B, 114TC | BO-209-150 FF, BO-209-150 FV, BO-209-150 RV, BO-209-160 FV, BO-209-160 RV | DA 40, DA 40F, DA 42, DA 42 NG, DA 42 M-NG | DA20-A1, DA20-C1 | MA-1, MA-1B | FFA) (AS 202/18A4 BRAVO | FBA Centennial 100 | F.20 | 2T-1A, 2T-1A-1, 2T-1A-2 | 19A, B19, M19A, 23, A23, A23A, A23-19, A23-24, B23, C23, A24, A24R, B24R, C24R, 35-C33, 35-C33A, G33, F33, F33A, F33C, B35BTC, 36, A36, A36TC, 76, 19A, M19A, A23, A23A, B23, C23, A23-24, A24, A24R (When STC SA718Gl is installed), 35, A35, B35, C35, D35, E35, G35, 35R, 35-33, 35-A33, 35-C33, 35-C33A, 35-D33, E33A, F33, F33A, F33C, G33, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, A36 (When STC SA11GL is installed) | Laviasa (PA-25, PA-25-235, PA-25-260 | H-250, H-295 (USAF U10D), H-391 (USAF UL-24), H-395 (USAF L-28A or U10B) | M-4-180C, M-4-180S, M-4-180T, M-4-180V, M-4-210C, M-4-210S, M-4-210T, M-4-210, M-4-220C, M-4-220S, M-4-220T, M-4-220, M-5-200, M-5-210C, M-5-210TC, M-5-220C, M-5-235C, M-6-180, M-6-235, M-7-235A, M-7-235B, M-7-235C, M-7-235, M-7-260C, M-7-260, M-7-420AC, M-7-420A | M20C, M20E, M20F, M20G, M20J, M20K, M20M | FU24-954, FU24A-954, 750XL | PA-18, PA-18A, PA-18AS, PA-18A-150, PA-22-108, PA-23, PA-23-160, PA-23-235, PA-24, PA-24-250, PA-24-260, PA-28-140, PA-28-150, PA-28-151, PA-28-161, PA-28-180, PA-28-181, PA-28-235, PA-28-236, PA-28R-180, PA-28R-200, PA-28-201T, PA-28R-201, PA-28RT-201, PA-28RT-201T, PA-32-260, PA-32-300, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32-301, PA-32-301T, PA-34-200, PA-34-200T, PA-34-220T, PA-36-285, PA-36-300, PA-36-375, PA-38-112, PA-44-180, PA-22, PA-22-135, PA-22-150, PA-22-160 (When STC SA91AL is installed) | 305A, 305C, 305D, 305F | LA-4, LA-4-180, LA-4-200, Lake Model 250 | Navion A, Navion B, Navion D, Navion E, Navion D, Navion F, Navion G, Navion G (When STC SA36GL is installed | A-1, S-1S, S-1T, S-2, S-2A, S-2S, S-2B, S-2C | MD3-160 | TB 9, TB 10, TB 20, TB 21, TB 200 | UC-1 | S-1B2 | GC-1A, GC-1B (When STC SA2GL is installed) | F19, F21, F21A, F22 | S-2B, S-2C, 600-S2C, S2R-R1340, S2R-R1820, S2R-T11, S2R-T15, S2R-T34, S2R-T45, S2R-T65, S2RHG-T34, S2RHG-T65 S-2R (When STC SA162GL is installed) | AA-1, AA-1A, AA-1B, AA-1C, AA-5, AA-5A, AA-5B | M10, A-2, A2-A, 415-C, 415-CD, E, G, F-1, F-1A (From TCDS holder and when STC SA12GL or SA127GL is installed.) | P68 Observer, P68B, P68C, P68C-TC | YMF | DHC-1B-2S3, DHC-1B-2S5 (When STC SA748S0 or SA1011S0 is installed) | 201A, 201B, 201C, 620

ReplacedPartNumber:

McCauley/Parker Hannifin P/N 105-00200

ApprovalBasis:

Identicality per 14 CFR 21.303 DWG No APS105-00200 Rev C Date 4/16/2007 or later FAA-approved revisions

Models:

As modified per STC SA01156CH 182P, 182Q, 182R, 182S, 182T, F182P, F182Q) (As modified per STC SA01320CH 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K, A185E, A185F, 185, 185A, 185B, 185C, 185D, 185E) Maule Aerospace Technology, Inc. (As modified per STC SA01412CH M-6-235, M-7-235, M-7-235B, M-7-235C, M-7-260, M-7-260C, M-7-420A, M-7-420AC, MT-7-235, MT-7-260, MX-7-235) (As modified per STC SA01185CH 206, 206H, P206, P206A, P206B, P206C, P206D, P206E, T206H, TP206A, TP206B, TP206C, TP206D, TP206E, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G) (As modified per STC SA01272CH A185E, A185F) (As modified per STC SA169CE 185, 185A, 185B, 185C, 185D, 185E, A185E) (As modified per STC SA805CE A185E) (As modified per STC SA18GL TU206F, TU206G, U206F, U206G) (As modified per STC SA666CE 206, P206, P206A, TP206A, TU206A, TU206B, TU206C, TU206D, TU206E, U206, U206A, U206B, U206C, U206D, U206E) (As modified per STC SA7GL 185A, A185F) (As modified per STC SA332CE 206, P206 , P206A, TP206A, TU206A, TU206B, TU206C, TU206D, TU206E, U206, U206A, U206B, U206C, U206D, U206E) Viking Air Limited (As modified per STC SA309CH DHC-2 MK.III) Viking Air Limited (As modified per STC SA610GL DHC-2 MK I) Pilatus Aircraft Limited (As modified per STC SA227CH PC-6/B2-H4) Quest Aircraft Design, LLC (As modified per STC SA02848CH Kodiak 100) (As modified per STC SA1311GL 208) Viking Air Limited (As modified per STC SA331CH DHC-3) Air Tractor Inc. (As modified per STC SA01795CH AT-802, AT-802A) Viking Air Limited (As modified per STC SA2CH DHC-6-100, DHC-6-200, DHC-6-300

ReplacedPartNumber:

McCauley/Parker Hannifin P/N 105-2

ApprovalBasis:

Identicality per 14 CFR 21.303 DWG No APS105-00200 Rev C Date 4/16/2007 or later FAA-approved revisions

Models:

As modified per STC SA00900CH 172D, 172E, 172F (USAF T-41A), 172G, 172H (USAF T-41A), 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S, 175A, 175B, 175C, P172D, R172K, FR172E, FR172F, FR172G, FR172H, FR172J, FR172K, F172D, F172E, F172F, F172G, F172H, F172K, F172L, F172M, F172N, F172P) Maule Aerospace Technology, Inc. (As modified per STC SA01411CH MX-7-180B, MX-7-180C, MX-7-235, MX-7-420) (As modified per STC SA1483GL 206, P206, P206A, P206B, P206C, P206D, P206E, TP206A, TP206B, TP206C, TP206D, TP206E, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G) (As modified per STC SA1569GL A185E, A185F

ReplacedPartNumber:

Grove P/N 105-2

ApprovalBasis:

Identicality per 14 CFR 21.303 DWG No APS105-00200 Rev C Date 4/16/2007 or later FAA-approved revisions

Models:

As modified per STC SA00900CH 172D, 172E, 172F (USAF T-41A), 172G, 172H (USAF T-41A), 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S, 175A, 175B, 175C, P172D, R172K, FR172E, FR172F, FR172G, FR172H, FR172J, FR172K, F172D, F172E, F172F, F172G, F172H, F172K, F172L, F172M, F172N, F172P) Maule Aerospace Technology, Inc. (As modified per STC SA01411CH MX-7-180B, MX-7-180C, MX-7-235, MX-7-420

ReplacedPartNumber:

Grove P/N 105-2

ApprovalBasis:

Identicality per 14 CFR 21.303 DWG No APS105-00200 Rev - (N/C) Date 3/13/1995 or later FAA-approved revisions

Models:

A-1, A-1A, A-1B, A-1C-180, A-1C-200 as modified by STC SA00637CH) Cessna Aircraft Company (172, 172A, 172B, 172C, 172D, 172E, 172F, 172G, 172H, 172I, 172K, 172L, 172M, 172N, 172P, 175, as modified by STC SA00674CH) Cessna Aircraft Company (170A, 170B as modified by STC SA00804CH) Piper Aircraft, Inc. (PA-12, PA-12S modified by STC SA00901CH) Piper Aircraft, Inc. (PA-18A-135, PA-18AS-135, PA-18S-135, PA-18S-150, PA-18-150, PA-18AS-150, PA-18A-150, PA-18-135(Army L-21B) as modified by STC SA00713CH) American Champion Aircraft Corp (8GCBC as modified by STC SA00763CH

ReplacedPartNumber:

Cleveland Wheels & Brakes P/N 105-00200 Rapco, Inc. P/N RA105-002 Aviation Products Systems Inc. P/N APS105-00200

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No. RA105-00200 Rev. - Date 05/15/2012*

Models:

A-9B) Air Tractor, Inc. (AT-300, AT-301, AT-302, AT-400, AT-400A, AT-401, AT-401A, AT-402, AT-501, AT-502, AT-503, AT-503-A) Alexandria Aircraft LLC (17-30A, 17-31A, 17-31ATC) Allied Ag Cat Productions, Inc. (G-164, G-164A, G-164B, G-164B-15T, G-164B-20T, G-164-34T, G-164B (with 73 inch wing gap), G-164C, G-164D, G-164D (with 73 inch wing gap)) APEX Aircraft (R 3000/160) Cessna Aircraft Company (150F,150G, 150H, 150J, 150K, 150L, A150L, 152, A152, F150F, F150G, F150H, F150J, F150K, FA150K, FA150L, FRA150L, F152, FA152, 172F, 172G, 172H, 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S, F172F, F172G, F172H, F172K, 177A, 177B, 177RG, F177RG, 180G, 180H, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182S, R182, TR182, FR182, 185C, 185D, 185E, A185E, A185F, 188, 188A, 188A, 188B, A188, A188A, A188B, T188C, 206, 206H, P206, P206A, P206B, P206C, P206D, P206E, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G, T206H, TP206A, TP206B, TP206C, TP206D, TP206E, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G, 207, 207A, T207, T207A, 210-5A (205A), 210C 210D, 210E, 210F, 210G, 210H, 210J, 210K, 210L, 210M, P210N, 210R, P210R, T210F, T210G, T210H, T210J, T210K, T210L, T210M, T210N, T210R, 336 337, 337A, 337B, 337C, 337D, T337B, T337C, T337D, 120, 140, 140A, 170, 170A, 170B, 172, 172A, 172B, 172C, 172D, 172E, 175, 175A, 175B, 175C, P172D, 180, 180A, 180B, 180C, 180D, 180E, 180F, 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G (When STC SA13GL is installed), 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K, 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F, 206, P206, U206, U206F, U206G, TU206E, TU206F, TU206G (When STC SA63GL is installed), 180, 180A, 180B, 180C, 180D, 180E, 180F, 180H, 180J, 185, 185A, 185B, A185E, A185F, 206E, 206F, TU206E, TU206F, 210, 210A, 210B, 210C, 210K, 210L, 210M, T210C, T210K, T210L, T210M (When STC SA52GL or SA62GL is installed), P210N (When STC SA54GL is installed)) Cirrus Design Corporation (SR20, SR22, SR22T) CPAC, Inc. (112, 112B, 112TC, 112TCA, 114, 114A, 114B, 114TC) Daimler Chrysler Aerospace AG (BO-209-150 FF, BO-209-150 FV, BO-209-150 RV, BO-209-160 FV, BO-209-160 RV) Diamond Aircraft Industries GmbH (DA 40, DA 40F, DA 42, DA 42 NG, DA 42 M-NG) Diamond Aircraft Industries Inc. (DA20-A1, DA20-C1) The EMROTH Company dba EMAIR (MA-1, MA-1B) Flugzeugwerke Altenrhein AG (FFA) (AS 202/18A4 BRAVO) Found Brothers Aviation Limited (FBA Centennial 100) GENERAL AVIA Costruzioni Aernautiche (F.20) Great Lakes Aircraft Company (2T-1A, 2T-1A-1, 2T-1A-2) Hawker Beechcraft Corporation (19A, B19, M19A, 23, A23, A23A, A23-19, A23-24, B23, C23, A24, A24R, B24R, C24R, 35-C33, 35-C33A, G33, F33, F33A, F33C, B35BTC, 36, A36, A36TC, 76, 19A, M19A, A23, A23A, B23, C23, A23-24, A24, A24R (When STC SA718Gl is installed), 35, A35, B35, C35, D35, E35, G35, 35R, 35-33, 35-A33, 35-C33, 35-C33A, 35-D33, E33A, F33, F33A, F33C, G33, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, A36 (When STC SA11GL is installed)) Lavia Argentina S.A (Laviasa (PA-25, PA-25-235, PA-25-260) Helio Aircraft, LLC. (H-250, H-295 (USAF U10D), H-391 (USAF UL-24), H-395 (USAF L-28A or U10B)) Maule Aerospace Technology, Inc. (M-4-180C, M-4-180S, M-4-180T, M-4-180V, M-4-210C, M-4-210S, M-4-210T, M-4-210, M-4-220C, M-4-220S, M-4-220T, M-4-220, M-5-200, M-5-210C, M-5-210TC, M-5-220C, M-5-235C, M-6-180, M-6-235, M-7-235A, M-7-235B, M-7-235C, M-7-235, M-7-260C, M-7-260, M-7-420AC, M-7-420A) Mooney Aviation Company Inc (M20C, M20E, M20F, M20G, M20J, M20K, M20M) Pacific Aerospace Limited (FU24-954, FU24A-954, 750XL) Piper Aircraft, Inc. (PA-18, PA-18A, PA-18AS, PA-18A-150, PA-22-108, PA-23, PA-23-160, PA-23-235, PA-24, PA-24-250, PA-24-260, PA-28-140, PA-28-150, PA-28-151, PA-28-161, PA-28-180, PA-28-181, PA-28-235, PA-28-236, PA-28R-180, PA-28R-200, PA-28-201T, PA-28R-201, PA-28RT-201, PA-28RT-201T, PA-32-260, PA-32-300, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32-301, PA-32-301T, PA-34-200, PA-34-200T, PA-34-220T, PA-36-285, PA-36-300, PA-36-375, PA-38-112, PA-44-180, PA-22, PA-22-135, PA-22-150, PA-22-160 (When STC SA91AL is installed)) Regal Air, Inc. (305A, 305C, 305D, 305F) Revo, Incorporated (LA-4, LA-4-180, LA-4-200, Lake Model 250) Sierra Hotel Aero, Inc. (Navion A, Navion B, Navion D, Navion E, Navion D, Navion F, Navion G, Navion G (When STC SA36GL is installed) Sky International, Inc. (A-1, S-1S, S-1T, S-2, S-2A, S-2S, S-2B, S-2C) SME Aero, Inc. (MD3-160) SOCATA (TB 9, TB 10, TB 20, TB 21, TB 200) STOL Aircraft Corporation (UC-1) STOL Aviation LLC (S-1B2) Swift Museum Foundation, Inc. (GC-1A, GC-1B (When STC SA2GL is installed)) Taylorcraft 2000, LLC. (F19, F21, F21A, F22) Thrush Aircraft, Inc (S-2B, S-2C, 600-S2C, S2R-R1340, S2R-R1820, S2R-T11, S2R-T15, S2R-T34, S2R-T45, S2R-T65, S2RHG-T34, S2RHG-T65 S-2R (When STC SA162GL is installed)) True Flight Holdings LLC. (AA-1, AA-1A, AA-1B, AA-1C, AA-5, AA-5A, AA-5B) Univair Aircraft Corporation (M10, A-2, A2-A, 415-C, 415-CD, E, G, F-1, F-1A (From TCDS holder and when STC SA12GL or SA127GL is installed.)) Vulcanair S.p.A (P68 Observer, P68B, P68C, P68C-TC) The Waco Aircraft Company (YMF) William E. Lannon (DHC-1B-2S3, DHC-1B-2S5 (When STC SA748S0 or SA1011S0 is installed)) Weatherly Aircraft Company (201A, 201B, 201C, 620

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

100

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

108 | -1 | -2 | -3 | -5 | 415-D | -E | -G | CD | A-2 | A2-A | M10

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

201 | A | B | C | 620 | -A | -B | -B-TG | -TP

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

Air Tractor AT-300 | -301 | -302 | 302A | - 400A | -400 | -402 | -501 | -502 | -503 | -401 | -401A | 503A

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

M-4 -180 | -180C | -180S | -180T | -180V | -210 | -210C | -210S | -210T | -220 | 220C | -220 S | -220T | M-4 | M-4C | 4S | 4T | M-5-180C | -200 | 210C | -210TC | -220C | -235C | M-6-280 | -235 | M-7-235 | -235A | 235B | -235C | -260 | -260C | -420AC | -420A | M-8-235 | M-9-235 | MT-7-235 | -260 | -420 | MX-7-160 | -160C | -180AC | -180A | -180B | -180C | -180 | -235 | -420 | MXT-7-160 | -180 | -180A

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

C22J

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

AS202-18A4

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

G164 | 164A | G164B | G164C | G164D

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

CC1A | CC1B

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

P2002 | P206T | T2010

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

120 | 140 | 140 | 150 | 150A | 150B | 150C | 150D | 150E | 150F | 150G | 150H | 150J | 150K | 150L | 150M | F150 | FA150 | FR150 | FRA150 | FA152 | A150K | A150L | A150M | 152 | A152 | 170 | 170A | 170B | 172 | 172A | 172B | 172C | 172D | 172E | 172F (T-41A) | 172G | 172H | 172I | 172K | 172L | 172M | 172N | 172P | 172Q | 172R | 172S | F172 | FR172 | 172RG | 175 | 175A | 175B | 175C | 177 | 177A | 177B | 177RG | F177RG | 180 | 180A | 180B | 180C | 180D | 180E | 180F | 180G | 180H | 180J | 180K | 182 | 182A | 182B | 182C | 182D | 182E | 182F | 182G | 182H | 182J | 182K | 182L | 182M | 182N | 182P | 182Q | 182R | 182S | 182T | 185 | 185A | 185B | 182C | 185D | 185E | 188 | 188A | 188B | 205 | 205A | 206 | 206H | P206 | P206A | P206B | P206C | P206D | P206E | U206 | U206A | 206H | U206B | U206V | U206D | U206E | U206F | U206G | TP206A | TP206B | TP206C | T206H | TP206D | TP206E | TU206A | TU206B | TU206C | TU206D | TU206E | TU206F | TU206G | 207 | 207A | T207 | T207A | 210 | 210A | 210B | 210C | 210D | 210E | 210F | T210F | 210G | T210G | 210H | 210J | T210J | 210K | T210K | 210L | T210L | 210M | T210M | 210N | P210N | 210R | P210R | T210R | 305 | 336 | 337A | B | C | D | M19 | 19A | 23 | A23 | 24 | A23-24 | A24 | A24R | C33 | 24R | G33 | F33A | F33C | 35 | A35 | B35 | C35 | D35 | E35 | F35 | G35 | 35R | 35-33 | 35-A33 | 35B33 | 35-C33 | 35-C33A | E33A | F33 | F33A | F33C | H35 | J35 | K35 | M35 | N35 | P35 | S35 | V35 | V35A | V35B | V35BTC | 36 | A36 | A36TC | B36TC | 76 | 77

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

UC-1

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

PA25 | 235 | 260

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

100 | 125 | 150 | 160 | 180 | 220 | 235 | TB9 | TB10 | TB20 | TB212 | TB200

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

2T1A | 2T1A1 | 2T1A2

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

MD3-160

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

SF205 | 260 | 260C | 260M | 260W | 260TP | 260SW | 211 | 600TP

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

LA-4 | 4-200 | 4-250

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

PA28-140 | 150 | 151 | 160 | 161 | 180 | 181 | 235 | 236 | PA28R-180 | -200 | -201 | -201T | PA32-260 | 300 | PA32R-300 | PA32RT- 300 | -300T | -301 | -301T | PA34-200 | -200T | 220T | PA44-180 | PA18-150 | PA18A-150 | PA22-108 | PA23-160 | -235 | PA24-180 | -250 | -260 | -400 | PA38-112 | J3 | PA-11 | PA11 | PA12 | PA14 | PA16 | PA17 | PA-18 | PA-20 | PA22 | PA36 | PA38- 112

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

S1 | S-2 | A-1

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

S1B2

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

Lark 100 | 180

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

MA1B

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

T67M260 | -T3A

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

220 | 300

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

F20 | F20TP

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

DHC121 | 122 | 122A | DHC1B2S3 | 1B2S5

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

M10 | M20 | A | B | C | D | E | F | G | J | K | L | M | R | S | TN | U | V | M22

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

YMF-5

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

S2R-600 | -800 | -R1340 | -R1820 | -T11 | - T15 | -T34 | -T41 | -T65

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

17-30A | 17-31A | 17-31ATC | 300A

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

G103 | G103C | G109 | G109A | G115 | G115A | B | C | C2 | D | D2 | EG | G120A

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

L19

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

FU24-954 | FU24A-954 | 750XL | 08-600 | CT/4E

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

P68 | B | C | C-TC | AP68TP-300 | TP-600 | R | V1.0

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

112 | A | B | TC | TCA | 114 | A | B | TC

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

B0208 | 209

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

N22 | N22B | N24

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

H250 | H295 | 391 | 395

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

7ECA | 7GCAA | 7GCBC | 7KAB | 7SRS | 7ACA | 8GCBC | 8KCAB | T-250

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

AA1 | A | B | C | AA5 | A | B

ReplacedPartNumber:

105-00200

ApprovalBasis:

Test and Computations per 14 CFR § 21.303DWG No: APS105-00200Rev: EDate: 04/26/2016 or later FAA-approved revisions

Models:

19 | F19 | F21 | F21A | F21B | F22 | F22A | F22B | F22C

Description:

RIVET

Description:

RIVET

Description:

RIVET

Description:

RIVET

Description:

RIVET

Description:

RIVET

Description:

RIVET

Description:

RIVET

Description:

RIVET

Description:

RIVET

Description:

RIVET

Description:

RIVET

Description:

RIVET