N208WN

Service difficulty reports · 417

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 = 'N208WN' 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 SWAA2021092408577Frame · crackedCRACKED FRAME AT E&E COMPARTMENT BS328 3' BELOW S-20R WL182. ; / [01] CRACK FOUND ON FRAME AT E&E COMPARTMENT BS328+3'' BELOW S-20R; WL182 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ON SRM PART MUST BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR.9.C. IAug 18, 2021 · N208WN · Boeing 737* · Fuselage Main, FrameSDR SWAA2021082308618Cargo Track · corrodedCORROSION ON TRACK TIEDOWN AT AFT CARGO BAY BS790 LBL17 WL158. REMOVED CORROSION ON AFT CARGO TRACK, AREA MEASUREMENTS D=0.058' X L=1.9' X W=0.8'. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARAGRAPH 4B(2) FIGURE 103 DETAIL A B C D AND E. REMOVED THE Aug 18, 2021 · N208WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021092708216Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 927+12; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] REMOVED 1 EA FASTENER PER SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.5' W=0.5'.PERFORMED VISUAL INSPECTION WITH A 10Aug 17, 2021 · N208WN · Boeing 737 · Fuselage Main, Plate/SkinSDR SWAA2021092708212Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 927+6; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] REMOVED 1 EA FASTENER PER SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.5' W=0.5'.PERFORMED VISUAL INSPECTION WITH A 10-Aug 17, 2021 · N208WN · Boeing 737 · Fuselage Main, Plate/SkinSDR SWAA2021092708188Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 907+9; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] REMOVED 1 EA FASTENER AT DISCREPANCY AREA PER SRM 51-4[06] EVALUATED DAMAGED REMOVAL AT DISCREPANCY AREA L=0.5' W=0.6' ORIG. THICKAug 17, 2021 · N208WN · Boeing 737 · Fuselage Main, Plate/SkinSDR SWAA2021092708225Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 927+13; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] REMOVED 1 EA FASTENER PER SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.5' W=0.5'.PERFORMED VISUAL INSPECTION WITH A 10Aug 17, 2021 · N208WN · Boeing 737 · Fuselage Main, Plate/SkinSDR SWAA2021092708224Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 927+5; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] INSTALLED EWIS PROTECTION AT BS927-BS947 BL 0 PER AMM 20-60-07; [02] REMOVED 1 EA FASTENER PER SRM 51-40-02. REMOVED CORROSION AT Aug 17, 2021 · N208WN · Boeing 737 · Fuselage Main, Plate/SkinSDR SWAA2021092708219Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 927+8; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] REMOVED 1 EA FASTENER PER SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.5' W=0.5'.PERFORMED VISUAL INSPECTION WITH A 10-Aug 17, 2021 · N208WN · Boeing 737 · Fuselage Main, Plate/SkinSDR SWAA2021092708208Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 907+14; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] REMOVED 1 EA FASTENER AT DISCREPANCY AREA PER SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.5 W= 0.5 PERFORMED VISUAL IAug 17, 2021 · N208WN · Boeing 737 · Fuselage Main, Plate/SkinSDR SWAA2021092708207Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 907+12; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] REMOVED 1 EA FASTENER AT DISCREPANCY AREA PER SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.5 W= 0.5 PERFORMED VISUAL IAug 17, 2021 · N208WN · Boeing 737 · Fuselage Main, Plate/SkinSDR SWAA2021092708189Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 907+10; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] REMOVED 1 EA FASTENER AT DISCREPANCY AREA PER SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.6 W= 0.5 PERFORMED VISUAL IAug 17, 2021 · N208WN · Boeing 737 · Fuselage Main, Plate/SkinSDR SWAA2021092708183Skin · corrodedCORROSION AROUND FASTENER AT BS 887+16, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED ONE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARAGRAPH 15 A 6A. NO ADDITAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708215Skin · corrodedCORROSION AROUND FASTENER AT B.S. 927+11; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [11] INSTALLATION OF 1 EACH FASTENER WAS ACCOMPLISHED ON EA# 21-153-02635-WIP1; [12] REFER TO FAULT TTG8Q006DPMC WHERE EA 21-153-02635 WAS ADDED AS A SUBTASK; [Aug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708220Skin · corrodedCORROSION AROUND FASTENER AT BS 927+9, BL 0, WL 306.5 ON SKIN UNDER DORSAL FIN. ] REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS, CORROSION WAS REMOVED IAW SRM 51-10-02 PARAGRAPH 15Aug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708217Skin · corrodedCORROSION AROUND FASTENER BS 927+14, BL 0, WL 306.5 ON SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS TO MAKE SURE ALL OF THE CORROSION WAS REMOVED IAW SRM 51-Aug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708218Skin · corrodedCORROSION AROUND FASTENER AT BS 927+15, BL 0, WL 306.5 ON SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS, CORROSION WAS REMOVED IAW SRM 51-10-02 PARAGRAPH 15.Aug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708213Skin · corrodedCORROSION AROUND FASTENER AT BS 927+7, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02 PARAGRAPH 15.A.6.A. NO ADDITAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708214Skin · corrodedCORROSION AROUND FASTENER AT BS 927+10, BL 0, WL 306.5 ON SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS, CORROSION WAS REMOVED IAW SRM 51-10-02, PARAGRAPH 15Aug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708210Skin · corrodedCORROSION AROUND FASTENER AT BS 907+17, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER AT DISCREPANCY AREA IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS, NO CORROSION IAW SRM 51-10-Aug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708209Skin · corrodedCORROSION AROUND FASTENER BS 907+15, BL 0, WL 306.5 ON SKIN UNDER DORSAL FIN. REMOVED THE FASTENER AT DISCREPANCY AREA IAW SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.5 W= 0.5 PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS TO MAKE SUREAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708206Skin · corrodedCORROSION AROUND FASTENER AT BS 907+11, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS IAW SRM 51-10-02 PARAGRAPH 15.A.6.A. NO ADDITIOAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708204Skin · corrodedCORROSION AROUND FASTENER AT BS 907+13, BL 0, WL 306.5 FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION & PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS IAW SRM 51-10-02 PARAGRAPH 15.A.6.A. NO ADDITIONAL DAMAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708205Skin · corrodedCORROSION AROUND FASTENER AT BS 907+16, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. . REMOVED CORROSION, PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS IAW SRM 51-10-02 PARAGRAPH 15.A.6.A. NO ADDITIONAL DAMAGE NOTED. HFEC INSPECTED SKIN BLEAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708203Skin · corrodedCORROSION AROUND FASTENER AT BS 907+7, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS IAW SRM 51-10-02 PARA 15 A 6 A. NO ADDITIONAL DAMAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708202Skin · corrodedCORROSION AROUND FASTENER AT BS 907+5, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARAGRAPH, 15 A 6 A. NO ADDITIAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708187Skin · corrodedCORROSION AROUND FASTENER AT BS 907+8, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARA 15 A 6 A. NO ADDITIONAL DAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708186Skin · corrodedCORROSION AROUND FASTENER AT BS 907+6, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER AT DISCREPANCY AREA IAW SRM 51-40-02. REMOVED CORROSION PERFORMED A VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARAGRAPH 15 Aug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708185Skin · corrodedCORROSION AROUND FASTENER AT BS 907+4, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE ONE FASTENER IAW SRM 51-40-02. REMOVED CORROSION, PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARAGRAPH 15 A 6 A. NO ADDIAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708201Skin · corrodedCORROSION AROUND FASTENER AT BS 887+15, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED A VISUAL INSPECTION WITH A 10- POWER MAGNIFYING, IAW SRM 51-10-02, PARA 15 A 6 A. NO ADDITIONAL DAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708199Skin · corrodedCORROSION AROUND FASTENER AT BS 887+12, BL 0, WL 306.5, ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER SRM 51-40-02. REMOVED CORROSION AND PERFORMED A VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02 PARA 15 A 6 A. NO ADDITIONALAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708200Skin · corrodedCORROSION AROUND FASTENER AT BS 887+14, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS, CORROSION WAS REMOVED IAW SRM 51-10-02, PARAAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708198Skin · corrodedCORROSION AROUND FASTENER AT BS 887+11, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED A VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS. CORROSION REMOVED IAW SRM 51-10-02, PARAAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708197Skin · corrodedCORROSION AROUND FASTENER AT BS 887+10, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARA 15 A 6 A. NO ADDITIOAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708196Skin · corrodedCORROSION AROUND FASTENER AT BS 887+9, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARA15 A 6 A. NO ADDITIONALAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708195Skin · corrodedCORROSION AROUND FASTENER AT BS 887+8, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARA 15 A 6 A. NO ADDITIONAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708193Skin · corrodedCORROSION AROUND FASTENER AT BS 887+6, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02 PARA 15 A 6 A. NO ADDITIONAL DAMAGE NOTED. REMOVED THE FASTENER IAAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708190Skin · corrodedCORROSION AROUND FASTENER AT BS 887+3, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED CORROSION , PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARA 15 A 6 A . NO ADDITIONAL DAMAGE NOTED. REMOVED THE FASTENER IAWAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708192Skin · corrodedCORROSION AROUND FASTENER AT BS 887+5, BL 0, WL 306.5, ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARA 15 A 6 A. NO ADDITIONAL DAMAGE NOTED. REMOVED THE FASTENER IAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708191Skin · corrodedCORROSION AROUND FASTENER AT BS 887+4, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED CORROSION AND PERFORMED A VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARA 15 A 6 A. NO ADDITIONAL DAMAGE NOTED. REMOVED THE FASTENER Aug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708184Skin · corrodedCORROSION AROUND FASTENER AT BS 887+17, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED ONE FASTENER IAW SRM 51-40-02. REMOVED CORROSION. PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARAGRAPH 15 A 6 A. NO ADDIAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092708182Skin · corrodedCORROSION AROUND FASTENER AT B.S. 887+13; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED ONE FASTENER IAW SRM 51-40-02. REMOVED CORROSION. PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02 PARAGRAPH 15.A.6.A. NO AAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021082308194Skin · corrodedCORROSION AROUND FASTENER AT BS 887+7, BL 0, WL 306.5, ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED CORROSION, L= 0.7' W=0.7'. PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS TO INSURE ALL CORROSION REMOVED IAW SRM 51-10-02 PARAGRAPH 15.A.6.A .NOAug 17, 2021 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021092707817Support Bracket · crackedCRACKED PNEUMATIC DUCT CLAMP SUPPORT BRACKET AT STA 540 + 5; RBL 6; WL 160. ; / [01] REMOVED AND INSTALLED NEW/SERVICEABLE PNEUMATIC DUCT CLAMP SUPPORT BRACKET AT STA 540+ 5; RBL6; WL 160 IAW SOPM 20-50-01; [02] REMOVED AND INSTALLED NEW/SERVICEABLE PNEUMATIC Aug 16, 2021 · N208WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081806708Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK BS727B - BS727C RBL45 WL208. REMOVED CORROSION ON PASSENGER CABIN SEAT TRACK, REWORKED AREA L=19' W=1' MAX MATERIAL LOSS= 0.013' WAS FOUND WITHIN THE LIMIT IAW SRM:53-00-52-1A-1 STEPS:4.A(2)A FIG.103. APPLIED A CHEMIAug 14, 2021 · N208WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021092706621Panel · pulledPANEL 661BB HAS SEVERAL PULLED FASTENER HOLES ; / [01] IDENTIFIED PANEL 661BB IAW SRM 57-51-01-0I-1 FIGURE 3; SHEET 1; TABLE 3; ITEM 9. DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PAR 4B(5B). REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-05-Aug 13, 2021 · N208WN · Boeing 7377H4 · Wing, Control SurfacesSDR SWAA2021092406624Post · corrodedFWD LAVATORY I/B AFT POST IS CORRODED ; / [01] REPAIRED CORRODED FORWARD LAVATORY INBOARD AFT DOOR POST IAW CMM 25-42-39 PG. 607.03 - 607.06 SECTION 4G; [02] ADDED MORE INFO FOR MEASUREMENTS.; [03] VERIFIED CORRECTIVE ACTIONS 1 AND 2.; [04] CORRECTED ERROR IN Aug 13, 2021 · N208WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2021092706135Door · crackedSUPPLEMENTAL INFORMATION: FWD SERVICE DOOR #4 BEAM CRACKED AT I/B SIDE OF RADIUS. / REMOVED FWD SERVICE DOOR PER AMM 52-41-00-000-801 UPDATED PARTS REMOVAL AND MEASURES TABLE.Aug 11, 2021 · N208WN · Boeing 737 · Galley DoorsSDR SWAA2021092706136None · crackedSUPPLEMENTAL INFORMATION: FWD SERVICE DOOR #5 BEAM CRACKED AT I/B SIDE OF RADIUS. / NO FAULT FOUND - ENTERED IN ERRORAug 11, 2021 · N208WN · Boeing 737 · Galley DoorsSDR SWAA2021092706129Floor Support · crackedCRACKED FLOOR SUPPORT AT B.S. 540; B.L. 0 - R.B.L. 24.5; W.L. 208.1. ; / [01] REMOVED FLOOR SUPPORT AT BS 540 BL 0 RBL 24.5 WL 208.1 IAW SRM 51-40-01-0G-0 ITEM D; [02] RECIVED NEW FLOOR SUPPORT P/N 143A-5240-36 LOCATED AND DRILLED NEW FLOOR SUPPORT AT BS 540BLAug 11, 2021 · N208WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021092706140Rib · crackedLT HORIZONTAL STABILIZER INSPAR RIB, AT HSS 129.50, 2ND VERTICAL STIFFENER IS CRACKED. REMOVED DAMAGED STIFFENER IAW SRM 55-10-09-2R-4. HFEC INSPECTION OF THE CUT OUT EDGES OF THE STIFFENER, WEB, AND EXISTING FASTENERS HOLES IAW SRM 55-10-09-2R-4. ET INSPAug 11, 2021 · N208WN · Boeing 7377H4 · Horizontal Stabilizer Structure
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