N465WN
Service difficulty reports · 285
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N465WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N465WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA2024030748506Sidewall Support · corrodedCORROSION FOUND AT SECTION 2 AROUND NUTPLATE HOLES AT FLOOR TO SIDEWALL SUPPORT; RBL 21; BS 500A-500C; WL 150<[01] REMOVED AND REPLACED SIDEWALL SUPPORT FROM BS 500A TO BS 500D IAW DWG 143A7500 AND SRM 51-40-02.;[02] UPDATED CORRECTIVE ACTION 1.<BR>REMOVED ANDSDR SWAA2024030648505Sidewall Support · corrodedCORROSION FOUND AT SECTION 2; LBL 21; BS 500-500C; WL 150 FAULT CORRECTION-CORROSION FOUND AT SECTION 2 AROUND NUTPLATE HOLES AT FLOOR TO SIDEWALL SUPPORTF<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BETWEEN BS.396 - 500D; LBL21 WL 156.5 IAW B-737-700 SDR SWAA2024030748232Doubler · corrodedFUSELAGE LWR SKIN DOUBLER HAS SURFACE CORROSION @ STA 685 + 10; BETWEEN STR-1 AND STR-2R; MARKED; PICS ATTACHED.<[01] NO ALLOWABLE DAMAGE LIMITS ENTRIES FOUND IN SRM FOR THIS ITEM. COVER PLATE ITEM 7340372 REPAIRED BY REPLACEMENT. PER SRM 51-10-02 PARAGRAPH 9.SDR SWAA2024011139844Battery Pack · failedEMERGENCY LIGHT BATTERIE PACKS FAILED CAPACITY TEST AT LOCATIONS M1672;M1669; M1675; M1670 EMERGENCY LIGHT BATTERIE PACKS FAILED CAPACITY TEST AT LOCATIONS M1672M1669 M1675 M1670<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERIE PACKS AT LOCATIONS M1672; M166SDR SWAA2024011139573Battery Pack · inoperativeAFT LH SIDE OF CABIN EMERGENCY LIGHTS ARE INOP<[01] REMOVED AND REPLACED AFT GALLEY CEILING EMERGENCY BATTERY PACK PER AMM 33-51-06 OPS CHECK GOODSDR SWAA2023081489219Limiter · crackedLOSS OF HYD B ON DEP. RAN CHECKLIST; TURN OFF B-PUMP IN UNDER A MIN. QTY WAS ZERO<[01] FOUND LEAK ON SYS B HYD FLOW LIMITING VALVE. UPON REMOVAL; FOUND UNION ADAPTER CRACKED BETWEEN THREADS CAUSING ALL SYSTEM B HYD FLUID TO DRAIN. REMOVED AND REPLACED SYS B EMSDR SWAA2022102865398Support Web · crackedFLOOR BEAM SUPPORT WEB CRACKED 3INCHES AT NUT PLATE BETWEEN STA 312-328 AT LBL 46.5 JUST BELOW FLOOR PANEL / [01] REMOVED AND REPLCACED INTERCOSTAL SUPPORT WEB PER SRM 51-40-02SDR SWAA2022101860669Skin · crackedREPAIR EA - 22-153-03096(N465WN - - REPAIR - EXTERNAL GROUND POWER RECEPTACLE (EGPR) DOOR CUTOUT DAMAGE/CRACK - PERMANENT) / [01] PERFORMED REPAIR IAW EA 22-153-030096 AND WO TTG8Q00FHNJL.SDR SWAA2022031581852Lamp · inoperativeL/H OVERWING EXTERIOR EMERGENCY LIGHT IS INOP / [01] REMOVED; REPLACED AND PERFORMED GOOD OPERATIONAL CHECK OF L/H OVERWING EXTERIOR EMERGENCY LIGHT LAMP PER AMM 33-51-04-960-801;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2022031581851Wire · inoperativeEMERGENCY EXIT LIGHT IDENTIFIER LOCATED ON AFT GALLEY IS INOP. / [01] WHILE TROUBLESHOOTING FOUND GROUND WIRE PULLED OUT OF DISCONNECTABLE REMOVABLE CONTACT SPLICE (D10088). RE-TERMINATED WIRE AND PERFORMED GOOD OPERATIONAL TEST OF EMERGENCY EXIT LIGHT IDENTIFSDR SWAA2022031581372Slat · out of adjustWHILE ADJUSTING #1 SLAT FOUND #2 SLAT OUT OF ADJUSTMENT / [01] INSTALLED PRE-LOAD SHIMS PER AMM 27-81-00-820-803 STEP 4G(4).;[02] ADJUSTED AND OPS CHECKED #2 SLAT PER AMM 27-81-00-820-803 STEP 4H(4)-4I(5). ADJUSTMENT AND OPS CHECK GOOD. VERIFIED TORQUES AND SASDR SWAA2022031581370Light · brokenPASSENGER CABIN EMERGENCY EXIT LIGHT ON CEILING BETWEEN OVERWING EXIT DOORS IS DAMAGED AND BROKEN (HOUSING AND LENS) / [01] REMOVED AND REPLACED PASSENGER CABIN EMERGENCY EXIT LIGHT ASSY AND LENSES ON CEILING BETWWEN OVERWING EXIT DOORS. OPERATIONAL TEST GOOD SDR SWAA2022031580960Wire · cutLH OVERWING LIGHT L00751 CONNECTOR HAS WIRE CUT FROM PIN 1 (D12452). / [01] DISPLACED OVERWING UPPER PANEL L/H 231YJW FOR ACCESS I.A.W AMM 25-21-20-000-801;[02] RETERMINATED LIGHT SIDE OF CONNECTOR D12452 PER SWPM 20-61-28 AND WDM 33-51-13 AND PERFORMED A GOODSDR SWAA2022031578378Angle · corrodedAFT CARGO BAY =CORROSION ON ATTACH ANGLE FROM INTERCOSTAL TO FWD SHEILD AT BS 768-786 RBL 21 / [01] PRIOR TO REMOVAL;FOUND PAT O HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-OG-0 STEP 9.;[02] REMOVED ANGLE CORRODED FROM INTERCOSSDR SWAA2022031577397Baffle · crackedFWD CARGO BAY BAFFLE HAS A CRACK AT TOP FWD CORNER AT BS500A-500B LBL 25 WL154 / [01] REMOVED IN FWD CARGO BAY BAFFLE BTW. BS 500A - BS500B LBL 25 WL 154 IAW SRM 51-40-02-0G-0. NO HAVE DAMAGE ALLOWABLE IN SRM MUST BE REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0SDR SWAA2022031576290Stub Frame · crackedFOUND CRACK ON FWD GALLEY DOOR FORWARD STUB FRAME BS 269.4; WL 208 RBL 55 FOUND CRACK ON FWD GALLEY DOOR FORWARD STUB FRAME BS 269.4 WL 208 RBL 55 / [01] VERIFIED APPLICABILITY OF REPAIR ON THE STUB FRAME OF THE FORWARD GALLEY DOOR SURROUND STRUCTURE AT STA 29SDR SWAA2022031573552Gusset · crackedGUSSET CRACKED BS 500D STR 21L FWD CARGO BAY / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-OG-0 STEP 9.;[02] REMOVED GUSSET CRACKED AT BS 500D STR.21 L FWD CARGO BAY;IAW SRM 51-40-02-OG-0.;[0SDR SWAA2022031573553Gusset · crackedGUSSET CRACKED BS 500D STR 19R FWD CARGO BAY / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-OG-0 STEP 9.;[02] REMOVED GUSSET CRACKED AT BS 500D STR. 19R FWD CARGO BAY;IAW SRM 51-40-02-OG-0.;[0SDR SWAA2022031573551Gusset · crackedGUSSET CRACKED BS 500D STR 19L FWD CARGO BAY / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-OG-0 STEP 9.;[02] REMOVED GUSSET CRACKED AT BS 500D STR. 19L FWD CARGO BAY;IAW SRM 51-40-02-OG-0.;[0SDR SWAA2022031573550Intercostal · crackedDAMAGED INTERCOASTAL @ B.S. 1138 (CRACKED) / [01] INTERCOSTAL (CRACKED) AT BS 1138; RBL 15;WL 250 FOUND TO BE OUT OF LIMITS DUE TONO ALLOWABLE DAMAGE FOUND IN SRM; IT'LL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9.C.;[02] REMOVED INTERCOSTAL (CRASDR SWAA2022031572355Skin · corrodedCORROSION AROUND FASTENERS ON FUSELAGE SKIN FROM B.S. 1016-1088; L.B.L. 15-R.B.L.15; W.L. 306.5. / [01] REMOVED CORROSION FROM AROUND FASTENERS AT FUSELAGE UPPER SKIN BS 1016 TO BS 1088; LBL15 -RBL15; WL 306.5 IN AREA OF 20' X 1.5' ORIGINAL MATERIAL THICKNESS SDR SWAA2022031572031Web · corrodedCORROSION ON VERTICAL WEB UNDER SUB THRESHOLD WEB IN AFT CARGO BAY; BS 795; RBL 20; WL 154 / [01] REMOVED FASTENERS AT WEB BS 794.37 TO 847 RBL 20 WL154 IAW SRM 51-40-02-0G-0;[02] REMOVED CORROSION ON VERTICAL WEB UNDER SUB THRESHOLD WEB IN AFT CARGO BAY BS 79SDR SWAA2022031572029Tail Cone · debondedTAIL CONE R/H SIDE HAS DISBOND AT BS 1156+9' AND 6' FROM TAIL CONE ACCESS DOOR CUTOUT LOWER CORNER / [01] IDENTIFIED TAIL CONE MATERIAL IAW SRM 53-80-70-0I-1 TABLE 2 FIGURE 2 ITEM 1. DAMAGE AT DISCREPANT LOCATION EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-80-7SDR SWAA2022031571215Floor Panel · damagedFLOOR PANEL 241ABF HAS DAMAGED INSERTS. / [01] REMOVED 22EA. THRU INSERTS; AND 4EA. BLIND INSERTS; ALL ACCORDING TO SRM 53-00-50-2R-0; PARA. 2.B.(2).;[02] DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 241ABF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-2SDR SWAA2022031572025Support Bracket · crackedCRACKED DUCT SUPPORT BRACKET AT STA 542; RBL 8; WL 155. / [01] REMOVED AND REPLACE DUCT SUPPORT BRACKET P/N 212A1116-1 LOT# 1480405-1. AT BS 540.40; RBL 8 WL. 165.98 I.A.W. SRM 51-10-02-0G-0. ITEM 9.C. SRM 51-40-02-0G-0;AMM 20-50-11-910-801.DWG#212A1110. REV.CSDR SWAA2022031571209Web · corrodedCORROSION ON AFT CARGO BAY DOOR CUTOUT SUB-THRESHOLD WEB; STA 787+8 TO STA 827+6; RBL 20 TO RBL 25; WL 158. / [01] REMOVED CORROSION ON AFT CARGO BAY SUB THRESHOLD WED AT BS.787+8 TO 827+6;AT DISCREPANCY AREA FOUND TO BE OUT LIMITS AT BS. 787+8 L=1.900' W=0.70SDR SWAA2022031571211Support · corrodedCORROSION ON AFT CARGO BAY FLOOR R/H FLOOR TO SIDEWALL SUPPORT AT STA 887+18 TO STA 887+19; RBL 21 WL 171. / [01] REMOVED CORROSION ON SEVERAL AREAS FROM UPPER SURFACE FLOOR TO SIDEWALL SUPPORT RBL 21; BS887+18 TO BS887+19; MAX.MAT. LOSS MEASURES : L=2.' X W=2SDR SWAA2022031571214Support · corrodedCORROSION ON AFT CARGO BAY AFT BULKHEAD SUPPORT; STA 947.5; RBL 12 TO LBL 3 WL 179 / [01] REMOVED ON AFT CARGO BAY LOWER BULKHEAD ANGLE SUPPORT AT STA 947.5 RBL 12 TO LBL 3 WL 179 IAW SRM 51-40-02 AND SRM 51-10-02-0G PARA 9.C WILL BE REPLACEMENT NO HAVE ENTRIESDR SWAA2022031571212Angle · corrodedCORROSION ON AFT CARGO BAY SIDEWALL ATTACH ANGLE; LOCATED ON FUSELAGE FRAME 907. STA 887+19; RBL 25; WL 172. / [01] REMOVED CORROSION ON ATTACH ANGLE ON FUSELAGE FRAME WAS NO FOUND ALLOWABLE DAMAGE ;PART MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH#9.;[02] REMOSDR SWAA2022031571213Support · corrodedCORROSION ON AFT CARGO BAY FLOOR R/H FLOOR TO SIDEWALL SUPPORT AT STA 907+15; RBL 21 WL 174.6. / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT STA907+ RBL21 WL174.6 THE LOWEST REMAINING THICKNESS 0.033' ON BLENDED AREA L=2'X W=1'XD=0.007 ORIG. MAT. THSDR SWAA2022031474952Skin · damagedEXTERNAL SKIN HAD A PREVIOUS BLEND AT BS 360+5' AND 5' BELOW STR 27L. HFEC INSPECTED DENTED AREA IAW NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND. EVALUATED PREVIOUS BLEND AT DISCREPANCY AREA L=1.9' W=0.8' ORIGINAL THICKNESS 0.063' MATERIAL REMAININGSDR SWAA2022031571098Floor Panel · corrodedFLOOR PANEL 241AAF HAS CORRODED INSERTS. / [01] DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 241AAF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-26 ITEM 150;[02] PANEL REPLACED PER SRM 51-10-02-0G-0.SDR SWAA2022031571101Floor Panel · corrodedFLOOR PANEL 241AEF INSERTS ARE CORRODED AND THE BOARD IS BROKEN. / [01] DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 241AEF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-26 ITEM 301.<BR>INSTALLED ALL INSERTS USING BMS 5-107 LOT#AK0DP4051K IAW BOEING PL 8SDR SWAA2022031571080Strap · corrodedCORROSION ON WEB STRAP BS 1015 TO BS 1031 LBL-3 WL-208. / [01] DAMAGE FOUND AT CABIN FLOOR WEB STRAP BS 1015; LBL 3; WL 208 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM; PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9C;[02] VERIFIED CORRESDR SWAA2022031571078Web · corrodedBS 987 WL 208 RBL 40 FLOOR WEB IS CORRODED. / [01] DAMAGE FOUND AT CABIN FLOOR WEB BS 987; RBL 40; WL 208 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM; PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9C;[02] VERIFIED CORRECTIVE ACTION ITEM SDR SWAA2022031571068Frame · crackedCRACK IN RADIUS OF FRAME AT B.S. 312; STRINGER 5 JUST ABOVE FORWARD ENTRY DOOR CUT OUT. / [01] TRIMED OUT AREA AT RADIUS OF FRAME AT BS 312 STRINGER 5-L JUST ABOVE FWD ENTRY DOOR CUT OUT PER L=.55 W=.35 PER SRM 51-10-02;[02] REQUEST NDI FOR CRACK FREE CONDITIOSDR SWAA2022031571058Intercostal · crackedCRACKED FLOOR SUPPORT AT B.S. 313-328; R.B.L. 34; W.L. 208.1. / [01] DAMAGE FOUND ON FLOOR SUPPORT AT B.S 313-328 RBL 34 ; WL 208.1 P/N 141A5410-12 FOUND TO BE OUT LIMITS ON SRM 51-10-51-1A-1 WILL BE REPAIRED BY REPLACEMENT I.A.W SRM 51-10-02-0G-0 PAR 9C.;[02]SDR SWAA2022031571057Support · crackedCRACKED FLOOR SUPPORT AT B.S. 277-294.5; R.B.L. 1; W.L. 208.1. / [01] DAMAGE FOUND ON FLOOR SUPPORT AT B.S 277-294.5 RBL 1 ; WL 208.1 P/N 141A5410-3 FOUND TO BE OUT LIMITS ON SRM 51-10-51-1A-1 WILL BE REPAIRED BY REPLACEMENT I.A.W SRM 51-10-02-0G-0 PAR 9C.;[02SDR SWAA2022031571059Floorbeam · crackedCRACKED FLOOR BEAM AT B.S. 294.5; R.B.L. 59; W.L. 208. FORWARD SIDE OF UPPER FLOOR BEAM FLANGE. / B.S 294.5 FLOOR BEAM AT RBL 59 WL 208 FOUND TO BE OUT OF LIMITS DUE TO A CRACK IAW SRM 51-10-02-0G-0;[03] B.S 294.5 FLOOR BEAM AT RBL 59 WL 208 FOUND TO BE OUT OFSDR SWAA2022031571081Web · corrodedCORROSION ON WEB BS 1026 TO BS 1033 LBL-6 WL-208. / [01] DAMAGE FOUND AT CABIN FLOOR WEB BS 1026; LBL 6; WL 208 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM; PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9C;[02] VERIFIED CORRECTIVE ACTIONSDR SWAA2022031571082Strap · corrodedCORROSION ON FLOOR WEB STRAP BS 1029 RBL-3 WL-208. / [01] DAMAGE FOUND AT CABIN FLOOR WEB STRAP BS 1029; RBL 3; WL 208 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM; PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9C;[02] VERIFIED CORRECTIVESDR SWAA2022031571084Strap · corrodedCORROSION ON FLOOR WEB STRAP BS 1027 RBL 17 WL 208. / [01] DAMAGE FOUND AT CABIN FLOOR WEB STRAP BS 1027; RBL 17; WL 208 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM; PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9C;[02] VERIFIED CORRECTISDR SWAA2022031571094Web · corrodedCORROSION ON FLOOR WEB RBL-38 WL-208. LOCATION OF DEFECT IS BS 990. / [01] LOCATION OF DEFECT IS BS 990.;[02] DAMAGE FOUND AT CABIN FLOOR WEB BS 990; RBL 38; WL 208 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM; PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM SDR SWAA2022031571085None · corrodedCORROSION ON THE INNER CREASE BEAM BS 922 TO BS 952 LBL-50 WL-208. / [01] REMOVED CORROISION ON AED INNER CORD BS 922-BS 952 LBL 50 WL 208 MAX MAT. LOSS 5'X2'X.015' ORIGINAL THICKNESS .080' FOUND TO BE OUT OF LIMITS I.A.W SRM 53-70-15-1A-1;[02] VERIFIED CORRECSDR SWAA2022031571095None · corrodedCORROSION ON THE BS 986.5 FLOOR BEAM UPPER FLANGE AT FASTENER HOLES LBL-45 TO RBL-45 WL-208. / [01] PARTIALLY COMPLETED STEPS 1 & 2;[23] FABRICATED -1 T-CHORD FROM BAC1505-101474 7050-T76511 LOT#1412519-1; -2 ANGLES FROM BAC1490-2811#7075T62 CLAD LOT#1453731-1SDR SWAA2022031571069Attach Angle · crackedLEFT WING; TRANSVERSE WEB O/B ATTACH ANGLE CRACKED AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT / [01] REMOVED AND REPLACED LEFT WING; TRANSVERSE WEB O/B ATTACH ANGLE AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT P/N 115A6260-1 IAW SRM 51-40-02 SDR SWAA2022031571063Plate · crackedLEFT WING; WAFFLE PLATE CRACKED JUST I/B OF #1 PYLON AFT TIP / [01] REMOVED AND REPLACED L/H WING WAFFLE PLATE I/B #1 PYLON IAW SRM 51-40-02.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.SDR SWAA2022031571097Crease Beam · corrodedCORROSION ON THE INNER CREASE BEAM BS 937 TO BS 1000 RBL-50 WL-208 / [01] REMOVED CORROISION ON ASD INNER CORD BS 937-BS 1000 RBL 50 WL 208 MAX MAT. LOSS 16'X2'X.018' ORIGINAL THICKNESS .080' FOUND TO BE OUT OF LIMITS I.A.W SRM 53-70-15-1A-1;[02] VERIFIED CORRSDR SWAA2022031571206Support · corrodedAFT CARGO BAY CORROSION L/H FLOOR TO SIDEWALL SUPPORT BS 761 LBL 21. / [01] REMOVED CORROSION ON L/H FLOOR TO SIDEWALL SUPPORT AT BS 761 LBL21 WL157 MEASURES L: 1.2' W: .8' D: 0.10' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 STEP 4.A(2) TOOL ID:NCX000697;SDR SWAA2022031571202Track · crackedAFT CARGO BAY FLOOR SUPPORT TRACK CRACKED AT BS 727E RBL-13. / [01] EVALUATE DAMAGE ON AFT CARGO BAY FLOOR SUPPORT TRACK; CRACK AT BS 727E RBL 13 WL 157; CRACK LENGTH .6' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 STEP 4.B(1)(A); TOOL ID:ATS2318; S/N:B190
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