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.

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 ANDFeb 4, 2024 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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 Feb 4, 2024 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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.Feb 3, 2024 · N465WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR 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; M166Jan 11, 2024 · N465WN · Boeing 7377H4 · Emergency LightingSDR 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 GOODJan 10, 2024 · N465WN · Boeing 7377H4 · Emergency LightingSDR 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 EMAug 14, 2023 · N465WN · Boeing 7377H4 · Hydraulic Power Accumulator, MainSDR 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 51-40-02Oct 28, 2022 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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.Oct 17, 2022 · N465WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR 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 #1Mar 10, 2022 · N465WN · Boeing 737* · Emergency LightingSDR 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 IDENTIFMar 9, 2022 · N465WN · Boeing 737* · Emergency LightingSDR 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 SAMar 9, 2022 · N465WN · Boeing 737* · Leading Edge DevicesSDR 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 Mar 8, 2022 · N465WN · Boeing 737* · Emergency LightingSDR 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 GOODMar 7, 2022 · N465WN · Boeing 737* · Emergency LightingSDR 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 INTERCOSFeb 27, 2022 · N465WN · Boeing 737* · Fuselage Miscellaneous StructureSDR 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-0Feb 24, 2022 · N465WN · Boeing 737* · Fuselage Main, Plate/SkinSDR 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 29Feb 22, 2022 · N465WN · Boeing 737* · Fuselage Main, FrameSDR 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.;[0Feb 16, 2022 · N465WN · Boeing 737* · Fuselage Main, Plate/SkinSDR 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.;[0Feb 16, 2022 · N465WN · Boeing 737* · Fuselage Main, Plate/SkinSDR 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.;[0Feb 16, 2022 · N465WN · Boeing 737* · Fuselage Miscellaneous StructureSDR 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 (CRAFeb 15, 2022 · N465WN · Boeing 737* · Fuselage Miscellaneous StructureSDR 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 Feb 14, 2022 · N465WN · Boeing 737* · Fuselage Main, Plate/SkinSDR 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 79Feb 12, 2022 · N465WN · Boeing 737* · Fuselage Main, StructureSDR 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 53-80-7Feb 11, 2022 · N465WN · Boeing 737* · Empennage StructureSDR 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 53-21-00-2Feb 11, 2022 · N465WN · Boeing 737* · Fuselage Floor PanelSDR 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.CFeb 11, 2022 · N465WN · Boeing 737* · Wing, Center BoxSDR 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=0.70Feb 11, 2022 · N465WN · Boeing 737* · Fuselage Main, StructureSDR 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=2Feb 11, 2022 · N465WN · Boeing 737* · Fuselage Miscellaneous StructureSDR 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 ENTRIEFeb 11, 2022 · N465WN · Boeing 737* · Fuselage Miscellaneous StructureSDR 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] REMOFeb 11, 2022 · N465WN · Boeing 737* · Fuselage Miscellaneous StructureSDR 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. THFeb 11, 2022 · N465WN · Boeing 737* · Fuselage Miscellaneous StructureSDR 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 REMAININGFeb 11, 2022 · N465WN · Boeing 737* · Fuselage Main, StructureSDR 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.Feb 10, 2022 · N465WN · Boeing 737* · Fuselage Floor PanelSDR 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 8Feb 10, 2022 · N465WN · Boeing 737* · Fuselage Floor PanelSDR 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 CORREFeb 10, 2022 · N465WN · Boeing 737* · Fuselage Miscellaneous StructureSDR 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 Feb 10, 2022 · N465WN · Boeing 737* · Fuselage Main, StructureSDR 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 CONDITIOFeb 10, 2022 · N465WN · Boeing 737* · Fuselage Main, FrameSDR 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]Feb 10, 2022 · N465WN · Boeing 737* · Fuselage Miscellaneous StructureSDR 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.;[02Feb 10, 2022 · N465WN · Boeing 737* · Fuselage Miscellaneous StructureSDR 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 OFFeb 10, 2022 · N465WN · Boeing 737* · Fuselage Main, Floor BeamSDR 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 ACTIONFeb 10, 2022 · N465WN · Boeing 737* · Fuselage Main, StructureSDR 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 CORRECTIVEFeb 10, 2022 · N465WN · Boeing 737* · Fuselage Miscellaneous StructureSDR 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 CORRECTIFeb 10, 2022 · N465WN · Boeing 737* · Fuselage Miscellaneous StructureSDR 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 Feb 10, 2022 · N465WN · Boeing 737* · Fuselage Main, StructureSDR 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 CORRECFeb 10, 2022 · N465WN · Boeing 737* · Fuselage Main, StructureSDR 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#1453731-1Feb 10, 2022 · N465WN · Boeing 737* · Fuselage Miscellaneous StructureSDR 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 Feb 10, 2022 · N465WN · Boeing 737* · Wing Miscellaneous StructureSDR 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.Feb 10, 2022 · N465WN · Boeing 737* · Wing Miscellaneous StructureSDR 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 CORRFeb 10, 2022 · N465WN · Boeing 737* · Fuselage Main, Floor BeamSDR 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;Feb 10, 2022 · N465WN · Boeing 737* · Fuselage Miscellaneous StructureSDR 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:B190Feb 10, 2022 · N465WN · Boeing 737* · Fuselage Miscellaneous Structure
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