N569WN

Service difficulty reports · 253

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 = 'N569WN' 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 SWAA2022112171187Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1675 INOP. / [01] REMOVED; REPLACED; AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY LIGHTS BATTERY PACK M1675 PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1Nov 15, 2022 · N569WN · Boeing 7377CT · Emergency LightingSDR SWAA2022111770636Battery Pack · inoperativeAFT LAB. B. EMERGENCY EXIT SIGN IS INOP / [01] RESEATED BATTERY PACK AND PERFORMED GOOD TEST OF BATTERY PACK AND EMERGENCY LIGHTS AS PER REF. AMM 33-51-06-960-805.;[02] CERTIFY ALL WORK PERFORMED AND GOOD OP CHECK AS PER AMM 33-51-06-960-805.;[03] VERIFIED CORNov 12, 2022 · N569WN · Boeing 7377CT · Emergency LightingSDR SWAA2022111770637Battery Pack · inoperativeA.S.D. HEADER PANEL EMERGENCY EXIT SIGN IS INOP / [01] RESEATED BATTERY PACK AND PERFORMED GOOD TEST OF BATTERY PACK AND EMERGENCY LIGHTS AS PER REF. AMM 33-51-06-960-805;[02] CERTIFY ALL WORK PERFORMED AND GOOD OP CHECK AS PER AMM 33-51-06-960-805.;[03] VERIFNov 12, 2022 · N569WN · Boeing 7377CT · Emergency LightingSDR SWAA2022111767052Scuff Plate · crackedFORWARD CARGO BAY FWD CORNER SCUFF PLATE CRACKED / [01] WELDED CRACK ON FWD CARGO BAY FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-30-15-2R PARA 4.B. (2) AND (4)<BR><BR>EQUIPMENT USED. WELDING MACHINE E10583; CAL DUE DATE 12/22;[02] Nov 1, 2022 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2022111764339Web · crackedINTERNAL HORZ. PRESSURE DECK STA 663 TO STA 675 - 2 CRACKS NOTED TO BE .5'. ONE AT BS 666 LBL 31; AND THE SECOND AT BS 673 LBL 35. / [01] CUT AND REMOVED THE DAMAGED PART OF THE WEB AT INTERNAL HORZ. PRESSURE DECK STA 663 TO STA 675 BETWEEN LBL 30 AND LBL 60 IOct 25, 2022 · N569WN · Boeing 7377CT · Fuselage Main, StructureSDR SWAA2022112261948Floor Panel · crackedFLOOR PANEL 834DZ IS CRACKED. NEW FLOOR PANEL INSTALLED IAW CARD TTG8Q00EWPU2.Oct 19, 2022 · N569WN · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2022111761391Gusset · crackedFWD CARGO BAY GUSSET CRACKED AT BS 500D STR 19L / [01] PRIOR TO REMOVAL ;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT;PER SRM 51-10-02 STEP 9.;[02] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLOct 18, 2022 · N569WN · Boeing 7377CT · Fuselage Main, Plate/SkinSDR SWAA2022111761394Gusset · crackedFORWARD CARGO BAY GUSSET CRACKED AT BS 500D STR 19R / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT;PER SRM 51-10-02 STEP 9.;[02] REMOVED GUSSET CRACKED AT BS500D;STR. 19R;IAW SRM 51-40-02.;[03] RECEIVED;LOCATEOct 18, 2022 · N569WN · Boeing 7377CT · Fuselage Main, Plate/SkinSDR SWAA2022111761396Fitting · crackedFWD 2 HINGE FITTINGS ARE CRACKED COMMON TO INSIDE SURFACE OF FAIRING PANEL 192CL (MARKED) / [01] REMOVED 1 FWD HINGE P/N:149A7234-1 PER AMM#52-48-42-000-801 STEPS 2.C.(1)-(4);[02] REMOVED 2ND HINGE P/N:149A7234-5 PER AMM#52-48-42-000-801 STEPS 2.C.(1)-(4);[03]Oct 18, 2022 · N569WN · Boeing 7377CT · Aerodynamic FairingsSDR SWAA2022111760102Floor Panel · pulledFLOOR PANEL 241AF UPPER SURFACE HAS LARGE AREAS OF PULLED STRANDS. / [01] IDENTIFIED FLOOR PANEL 241AF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.E(2). DAMAGE TO FLOOR PANEL IS BEYOOct 15, 2022 · N569WN · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2022111760098Floor Panel · pulledFLOOR PANEL 241DF UPPER SURFACE HAS LARGE AREAS OF PULLED STRANDS. / [01] IDENTIFIED FLOOR PANEL 241DF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. DAMAGE TO FLOOR PANEL IS BEYOND Oct 15, 2022 · N569WN · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2022111760094Floor Panel · pulledFLOOR PANEL 231XF UPPER SURFACE HAS LARGE AREAS OF PULLED STRANDS. / [01] IDENTIFIED FLOOR PANEL 231XF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.E(2). DAMAGE TO FLOOR PANEL IS BEYOOct 15, 2022 · N569WN · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2022112259778Panel · damagedRIGHT WING T/E PANEL 661BB HAD SEVERAL PULLED FASTENER HOLES. REPAIRED IAW SRM 51-70-04-2R-9 PARA 4 STEPS D & E .;Oct 13, 2022 · N569WN · Boeing 7377CT · Wing Main, Frame StructureSDR SWAA2022111759815Attach Angle · crackedCRACK ON FWD CARGO BAY FRAME TO BAFFLE ATTACH ANGLE AT LBL 24 BS 500B+19. / [01] REMOVED INTERCOSTAL FROM FCB BS 500B-500C LBL 24 IAW SRM 51-40-02-0G-0;[02] RECIVED; LOCATED AND DRILLED NEW ATTACH ANGLE AT BS 500B+19 LBL24; IAW B 737-700 SRM 51-40-05-0G-0 DWG Oct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Main, Plate/SkinSDR SWAA2022111759827Attach Angle · crackedCRACK ON FWD CARGO BAY FRAME TO BAFFLE ATTACH ANGLE AT LBL 24 BS 500C+1. / [01] REMOVED INTERCOSTAL FROM FCB BS 500C-500D LBL 24 IAW SRM 51-40-02-0G-0;[02] RECIVED; LOCATED AND DRILLED NEW ATTACH ANGLE<BR>N/P 143A7502-5 <BR>AT LBL 24 BS 500C+1 IAW SRM 51-40-05Oct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Main, Plate/SkinSDR SWAA2022111759814Attach Angle · crackedCRACK ON FWD CARGO BAY FRAME TO BAFFLE ATTACH ANGLE AT LBL 24 BS 400+19. / [01] REMOVED ATTACH ANGLE FROM FCB BS 400+19 LBL 24 IAW SRM 51-40-02-0G-0;[02] RECIVED; LOCATED AND DRILLED NEW ATTACH ANGLE AT BS 400+19 LBL24; IAW B 737-700 SRM 51-40-05-0G-0 DWG 134AOct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Main, Plate/SkinSDR SWAA2022111759788Shield · corrodedCORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 22 BS 767+3; BS 767+7; BS 767+11; BS 767+15; BS 767+19. / [01] PRIOR TO REMOVAL; FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT; IAW SRM 51-10-02-0G-0 STEP 9.;[02] VERIFIED CORRECTIVEOct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2022111759792Sidewall Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727+8; BS 727A+18; BS 727C+10; BS 727C+14; BS 727C+18; BS 727D+3; BS 727D+5; BS 727D+6; BS 727D+10; BS 727D+18. / [01] VERIFIED APPLICABILITY SRM 53-60-53-01-2 FOR IDENTIFICATION AND SRM 53-00-5Oct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2022111759795Sidewall Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727E+6; BS 727E+10; BS 727E+14; BS 747+2; BS 747+6; BS 747+10; BS 747+14; BS 767+3; BS 767+8. / [01] VERIFIED APPLICABILITY SRM 53-60-53-01-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABOct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2022111759794Sidewall Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727A+18; BS 727B+6; BS 727B+10; BS 727C+6; BS 727C+10; BS 727C+14; BS 727C+18. / [01] VERIFIED APPLICABILITY SRM 53-60-53-01-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE. REMOct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2022111759797Sidewall Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727D+3; BS 727D+5; BS 727D+6; BS 727D+8; BS 727D+10; BS 727D+19; BS 727E+2; BS 727E+6; BS 727E+10; BS 727E+12. / [01] VERIFIED APPLICABILITY SRM 53-60-53-01-2 FOR IDENTIFICATION AND SRM 53-00-53Oct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2022111759810Sidewall Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727E+14; BS 727E+18; BS 747+2; BS 747+8; BS 747+10; BS 747+14; BS 747+18. / [01] VERIFIED APPLICABILITY SRM 53-60-53-01-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE. REMOVED Oct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2022111759807Support · corrodedCORROSION ON AFT CARGO BAY AFT LOWER BULKHEAD SUPPORT AT RBL 20 BS 947. / [01] REMOVED AFT LOWER BULKHEAD SUPPORT IAW SRM 51-40-02-0G-0.<BR><BR>NO ALLOWABLE DAMAGE AND SO PART IS REPAIRABLE BY REPLACEMENT; IAW SRM 51-10-02-0G-0 STEP 9.;[02] VERIFIED CORRECTIVEOct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2022111759811Threshold · corrodedCORROSION ON AFT CARGO BAY THRESHOLD AT RBL 21 BS 787+8; RBL 23 BS 787+9; RBL 27 BS 787+13; RBL 27 BS 807+2; RBL 27 BS 807+4; RBL 27 BS 807+6; RBL 27 BS 807+9; RBL 27 BS 807+12. / [01] VERIFIED APPLICABILITY FOR IDENTIFICATION IAW SRM 53-60-15-01-1 AND SRM 53-Oct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2022111759809Threshold · corrodedCORROSION ON AFT CARGO BAY THRESHOLD AT RBL 27 BS 807+19; BS 827+1; BS 827+6; BS 827+8; BS 827+11; BS 827+13. / [01] VERIFIED APLICABILITY FOR IDENTIFICATION IAW SRM 53-60-15-01-1 AND SRM 53-60-15-1A-1 FOR ALLOWABLE DAMAGE;[02] REMOVED CORROSION ON AFT CARGO Oct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2022111759817Sidewall Support · corrodedCORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 400+2; BS 420+17; BS 440+14; BS 460+6; BS 460+18. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS SRM 53-00-53-1A-2.;[02] REMOVED CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT AT LBL24;BSOct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2022111759819Sidewall Support · corrodedCORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 480+14; BS 480+18; BS 500+4; BS 500+10; BS 500+14; BS 500+18; BS 500A+6; BS 500A+10; BS 500A+14; BS 500A+18. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS PER SRM 53-00-53-1A-2.;[02]Oct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2022111759820Sidewall Support · corrodedCORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 500B+2; BS 500B+6; BS 500B+10; BS 500B+14; BS 500C+6; BS 500C+10; BS 500C+14. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED CORROSION ON FCB FLOOROct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2022111759822Sidewall Support · corrodedCORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500A+18; BS 500B+2; BS 500B+6; BS 500B+10; BS 500B+18; BS 500C+2; BS 500C+6; BS 500C+10. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS;IAW SRM 53-00-53-1A-2.;[02] REMOVED CORROSION OOct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2022111759823Shield · corrodedCORROSION ON FWD CARGO BAY AFT DOOR SHIELD AT RBL 24 BS 480+18; BS 500+14. / [01] CORROSION ON FORWARD CARGO BAY AFT DOOR SHIELD LOCATED BTW BS 492.4 - BS 500A FOUND TO BE OUT OF LIMIT DUE TO NO ALLOWABLE DAMAGE ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAWOct 13, 2022 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2022111759310Stringer · crackedSTRINGER 7L IS CRACKED AT BS 296 / [01] VERIFY THE APPLICABILITY OF SRM 53-00-03-2R-1 REPAIR 1;[02] CRACK AT STRINGER 7 L BS 296 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-2R-1 REPAIR 1;[03] CUT AND REMOVED THE DAMAGED PART OF STRINGER 7L FROM BS 277+10 TO BS Oct 12, 2022 · N569WN · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2022111758884Stiffener · crackedR/H HORIZONTAL STABILIZER RIB 4 HAS 2 CRACKED STIFFENERS. (MARKED) / [01] UPDATED MEASUREMENTS CHART.[15] FABRICATED REPAIR PARTS FOR STIFFENER #2 ; (1) T-SECTION FROM 60-5872 7075 T76511 LOT# 1449876-1 (2) ANGLE FROM BAC 1490-2793 7075 T62 CLAD LOT# 1442205-1Oct 12, 2022 · N569WN · Boeing 7377CT · Horizontal Stabilizer, Spar/RibSDR SWAA2022111758873Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 10; W.L. 164. / [01] APPLICABILITY: SRM 57-10-10-2R-5-REPAIR 5 IS APPLICABLE TO THIS A/C;[02] PERFORMED CUT OUT THE UPPER ATTACH ANGLE LOWER COMPOSITE BULKHEAD AT BS 663 LBL14 IAW SRM 57Oct 11, 2022 · N569WN · Boeing 7377CT · Fuselage Main, StructureSDR SWAA2022112258401Skin · damagedFORWARD ENTRY DOOR SKIN IS CATCHING ON UPPER AFT CORNER OF CUTOUT WHEN CLOSING; DAMAGE PRESENT. FORWARD ENTRY DOOR SKIN IS CATCHING ON UPPER AFT CORNER OF CUTOUT WHEN CLOSING DAMAGE PRESENT. / [01] SRM 52-10-01-0I-1 IDENTIFICATION AND SRM 52-00-01-2R REPAIR 2 Oct 10, 2022 · N569WN · Boeing 7377CT · Passenger/Crew DoorsSDR SWAA2022062922654Tailpipe · faultyAFTER ENGINE SHUTDOWN RAMP REPORTS SMALL FIRE IN ENGINE #2 TAILPIPE. NO FIRE INDICATIONS IN COCKPIT. / [01] LP2338051 AP2804344 PERFORMED ENGINE FIRE CONDITIONAL INSPECTION REF AMM 05-51-49 NO DEFECTS NOTED. CENTER PLUG CAVITY HAS SMALL AMOUNT OF OIL. OIL USAGJun 25, 2022 · N569WN · Boeing 7377CT · Engine Collector/Tailpipe/NozzleSDR SWAA2022042697001Megaphone · faultyAFT MEGAPHONE INTERMITTENT / [01] R&R?D AFT MEGAPHONE PER MM 25-64-00Apr 22, 2022 · N569WN · Boeing 7377CT · Emergency EquipmentSDR SWAA2022031181764Cover · missingF/O SIDE OVER WING EXIT LIGHT COVER MISSING / [01] REINSTALLED LENS COVER PER AMM 33-51-01Mar 8, 2022 · N569WN · Boeing 737* · Emergency LightingSDR SWAA2022010658868Lens · missingOVER WING EXIT FO SIDE EXIT COVER MISSING. ; / [01] INSTALLED OVER WING EXIT F/O SIDE LIGHT LENS REF AMM 33-51-01Jan 6, 2022 · N569WN · Boeing 7377CT · Emergency LightingSDR SWAA2021102230873None · missingSUPPLEMENTAL INFORMATION: AIRCRAFT R SIDE HOVER WING EMERGENCY EXIT SIDEWALL EXIT PLACARD 1 OF 2 IS MISSING ; / [01] REINSTALLED SIDEWALL EXIT PLACARD IAW AMM 33-51-01.Oct 18, 2021 · N569WN · Boeing 737 · Emergency LightingSDR SWAA2021080503372Retainer · out of adjustFORWARD ENTRY DOOR ESCAPE SLIDE I DIFFICULT. ADJUSTED FORWARD ENTRY DOOR ESCAPE SLIDE HOLDER GIRT BAR HOLDER.Aug 3, 2021 · N569WN · Boeing 7377CT · Emergency EquipmentSDR SWAA2021060378650Lens · detachedRT. OVERWING EXIT COVER FELL OFF. ; / REINSTALLED RT. OVERWING EXIT LIGHT COVER. REFERENCE AMM 33-51-01. OPS CHECK GOOD.May 30, 2021 · N569WN · Boeing 7377CT · Emergency LightingSDR SWAA2021072837725Slider · crackedL/H HORIZONTAL STABILIZER UPPER FWD SLIDER IS CRACKED / REMOVED AND REPLACED LH UPPER SLIDER PER AMM. 53-31-31Dec 17, 2020 · N569WN · Boeing 7377CT · Horizontal Stabilizer StructureSDR SWAA2021072837726Slider · crackedR/H HORIZONTAL STABILIZER FWD UPPER SLIDER IS CRACKED / R&R'ED R/H HORIZONTAL STABILIZER FWD UPPER SLIDER IAW AMM 53-31-31Dec 17, 2020 · N569WN · Boeing 7377CT · Horizontal Stabilizer StructureSDR SWAA2021072837727Slider · crackedR/H HORIZONTAL STABILIZER FWD LOWER SLIDER IS CRACKED / REMOVED AND REPLACED R/H HORIZ STAB LOWER SLIDER PER AMM 53-31-31Dec 17, 2020 · N569WN · Boeing 7377CT · Horizontal Stabilizer StructureSDR SWAA2020113029754Skin · corrodedCORROSION ON FUSELAGE SKIN BS 886-888 BETWEEN STRS 2L-2R WL 308 RBL10-LBL10. REMOVED DAMAGE AT BS 886-888 BETWEEN STRS 2L-2R WL 308.5 RBL 10-LBL 10. DAMAGE FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-01-1A-1. REPAIRED AREA PER ATS ER 20-03531 REV IR AND SWA EANov 10, 2020 · N569WN · Boeing 7377CT · Fuselage Main, Plate/SkinSDR SWAA2021052529160Gusset · crackedFWD CARGO BAY BS 500D GUSSET IS CRACKED STR 21L/H / REMOVED DAMAGED GUSSET AT BS500D STR21L AND REPLACED IAW SRM CH 51-40-02 AND DRAWING # 143A7902 AND DRAWING # 143A9481.Nov 9, 2020 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021052529159Gusset · crackedFWD CARGO BAY BS 500D GUSSET IS CRACKED STR 19L/H / REMOVED & REPLACED GUSSET AT FWD CARGO BAY STR 19L/H BS500D IAW SRM 51-40-02-0G-0 & DWG 143A7902 REV.B 59191U 19NOV20Nov 9, 2020 · N569WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2020113028594Stringer Clip · damagedSTR 23 LT STRINGER CLIP AT BS 520 DAMAGED. REMOVED DAMAGED BS 520 STRINGER CLIP 23 LT, PER SRM 51-40-02 56639C 05NOV2020. LOCATED NEW STR CLIP BS 520-STR 23L, PER DWG 143A3210 & SRM 51-40-05 6908C 17NOV20. INSP 18 17NOV20 INSTALLED BS 520 STR 23L STR CLIP, Nov 5, 2020 · N569WN · Boeing 7377CT · Fuselage Main, Attach FittingsSDR SWAA2020113028869Beam · corrodedWHILE WORKING SEAT TRACK REPLACEMENT FOUND CORROSION IN MULTIPLE AREAS ON LONGITUDINAL BEAM BETWEEN BS 540 TO 727B LBL 45 WL 208. REMOVED CORROSION IN SEVERAL LOCATIONS ON LONGITUDINAL BEAM BS 540-BS727B LBL 45 MAX MATERIAL LOSS AT BS 630; 2' X 2' X .018'. RNov 5, 2020 · N569WN · Boeing 7377CT · Fuselage Main, StructureSDR SWAA2021071428407Floor Support · bentBENT INTERCOSTAL AT AREA AFT OF FWD CARGO BAY BS500D - BS520 RBL6 WL154. / REMOVED AND INSTALLED NEW INTERCOSTAL AT FCB B/S 500D-520; RBL 6 IAW SRM 51-40-02-0G-0; DWG# 143A7902.Nov 4, 2020 · N569WN · Boeing 7377CT · Fuselage Miscellaneous Structure
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