N220WN

Service difficulty reports · 358

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 = 'N220WN' 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 SWAA2022112973122Floor Panel · damagedDOT A24-10 MID CABIN FLOOR BOARD 231XF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE. / [01] EVALUATED DAMAGE; TOP SIDE OF PANEL IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1; TAP TEST GOOD NO DELAMINATION NOTED. <BR><BR>CLEANED; PREPPED DAMAGED AREAS IAW BNov 18, 2022 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022112973123Floor Panel · damagedDOT A24-11 MID CABIN FLOOR BOARD 242BF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE. / [01] EVALUATED DAMAGE; TOP SIDE OF PANEL IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1; TAP TEST GOOD NO DELAMINATION NOTED. <BR><BR>CLEANED; PREPPED DAMAGED AREAS IAW BNov 18, 2022 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022112973125Floor Panel · damagedDOT A24-12 MID CABIN FLOOR BOARD 241BF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE. / [01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 5Nov 18, 2022 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022112973303Attach Angle · crackedA-240 DOT 001 #2 ENGINE OUTBD FAN COWL ATTACH ANGLE AFT SIDE OF OIL SERVICE DOOR OPENING CRACKED. / [01] REMOVED #2 ENG OUTBD FAN COWL ATTACH ANGLE IAW SRM 51-40-02;[02] VERIFIED ACTION 1;[03] OK TO INSTALL NEW #2 ENGINE OTBD FAN COWL ATTACH ANGLE;[04] INSTALLNov 18, 2022 · N220WN · Boeing 7377H4 · Nacelle/Pylon, Attach FittingsSDR SWAA2022112972974Attach Angle · crackedCRACK FOUND ON UPPER ATTACH ANGLE STA 663 LBL 8 (WL 167) / [01] VERIFIED ITEM 2 OF STEP 5;[02] VERIFIED ITEM 2 OF STEP 8;[03] VERIFIED STEP 9;[04] LEAK CHECKED REPAIR AREA NO LEAK NOTED I.A.W MM 28-11-00-400-801;[05] NO LEAKS NOTED<BR>AUDIT C/WNov 17, 2022 · N220WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2022112972975Attach Angle · crackedCRACK FOUND ON UPPER ATTACH ANGLE STA 663 RBL 8 (WL 167) / [01] VERIFIED ITEM 2 OF STEP 8;[02] VERIFIED STEP 9;[03] LEAK CHECKED REPAIR AREA NO LEAK NOTED I.A.W MM 28-11-00-400-801;[04] LEAK CHECK GOOD<BR>AUDIT C/WNov 17, 2022 · N220WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2022111671444Slide · looseSLIDE LOOSE ON R-2 DOOR. R-2 DOOR SLIDE CHECKED FOR SECURITY IAW MMMM 25-66-01. OK FOR SERVICE.Nov 14, 2022 · N220WN · Boeing 7377H4 · Escape SlideSDR SWAA2022092716658None · crackedFOUND #2 SLAT UPPER SKIN CRACKED @ SLAT STATION 327 DURING BIRD STRIKE INSPECTION DENT IS L= 10.0 W= 2.5CRACK IS 2.25 / [01] REMOVED #2 LE SLAT IAW AMM 27-81-21. NEEDS INSTALL AND RIG CHECK.;[02] INSPECTED CAN HOUSING AND FOUND NO DEBRIS OR FOD. INSPECTED HARDSep 23, 2022 · N220WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2022081741980Fairing · damagedLOWER PYLON FAIRING BELOW ACCESS PANEL 434BL SHOWS FRETTING WEAR FROM PYLON DRAIN TUBE / [01] REMOVED AND REPLACED LOWER PYLON FAIRING AT PYLON DRAIN TUBE PER SRM 51-40-02 AND SRM 51-40-05.Aug 15, 2022 · N220WN · Boeing 7377H4 · Nacelle/Pylon StructureSDR SWAA2022030779023Bracket · crackedLH WING T/E CAVITY TO I/B FLAP SEAL SUPPORT BRACKET IS CRACKED BEHIND #1 PYLON / [01] REMOVED AND REPLACED LH WING T/E CAVITY TO I/B FLAP SEAL SUPPORT BRACKET PER SRM 51-40-02 AND AMM 20-50-11Mar 1, 2022 · N220WN · Boeing 737* · Wing Miscellaneous StructureSDR SWAA2022030379014Bracket · crackedLH MLG CENTER DOOR FWD LOWER ATTACH POINT BRACKET IS CRACKED /Mar 1, 2022 · N220WN · Boeing 737* · Landing Gear DoorsSDR SWAA2022030379020Web · crackedRH MLG CENTER DOOR FWD LOWER MOUNTING ATTACH WEB HAS A 1.0' CRACK /Mar 1, 2022 · N220WN · Boeing 737* · Landing Gear DoorsSDR SWAA2021120649281None · faultySUPPLEMENTAL INFORMATION: AT FL370 APU LIGHT LOW OIL PRESSURE ILLUMINATED SHUT DOWN PER QRH OTS - APU & #2 GEN INOP_APU - COMPLIED WITH FIM 49-90 803 TASK. SERVICED OIL TANK. NO CURRENT FAULTS.R&R APU BTC CO803 IN REF TO AMM 24 - 21 - 41 R&R #2 ENGINE BTC CO80Dec 1, 2021 · N220WN · Boeing 737 · Alternator-Generator DriveSDR SWAA2021120650021None · faultySUPPLEMENTAL INFORMATION: AT FL370 APU LIGHT LOW OIL PRESSURE ILLUMINATED SHUT DOWN PER QRH OTS - APU & #2 GEN INOP_APU - COMPLIED WITH FIM 49-90 803 TASK. SERVICED OIL TANK. NO CURRENT FAULTS.R&R APU BTC CO803 IN REF TO AMM 24 - 21 - 41 R&R #2 ENGINE BTC CO80Dec 1, 2021 · N220WN · Boeing 737 · Alternator-Generator DriveSDR SWAA2021120650020None · faultySUPPLEMENTAL INFORMATION: AT FL370 APU LIGHT LOW OIL PRESSURE ILLUMINATED SHUT DOWN PER QRH OTS - APU & #2 GEN INOP_APU - COMPLIED WITH FIM 49-90 803 TASK. SERVICED OIL TANK. NO CURRENT FAULTS.R&R APU BTC CO803 IN REF TO AMM 24 - 21 - 41 R&R #2 ENGINE BTC CO80Dec 1, 2021 · N220WN · Boeing 737 · Alternator-Generator DriveSDR SWAA2021060477927Rib · crackedRH HORIZONTAL LE PANEL 331B; 3RD RIB LE STA 95.96 FROM INBD EDGE; HAS A CRACK AT UPPER MOST AFT FASTENER ; PANEL 341B NOT 331B / APPLIED CIC TO RIB IAW AMM 51-21-91; REMOVED AND REPLACED RH STAB LE RIB CHORD AT LE STA 95.96 IAW DWG 186A1303 REV 1; SRM 51-40-02May 28, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2021060477926Lamp · inoperativeR/H OVERWING EXIT EMERGENCY EXIT LOCATOR LIGHT L1358 IS INOP ; / REPLACED LAMPS IN R/H OVERWING EXIT EMERGENCY EXIT LOCATOR LIGHT L1358; OPS CHECK GOOD IAW AMM 33-51-01-960-801.<BR>ATAG A69819; ALL WORK C/W<BR>AUDIT C/WMay 27, 2021 · N220WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021060476890Battery Pack · inoperativeLEFT OVERWING ESCAPE LIGHT (L6) INOP / REPLACED BATTERY PACK AND BATTERY PACK CHARGER M1668 IAW AMM 33-51-06-960-805 AND AMM 33-51-06-960-806. LEFT OVERWING ESCAPE SLIDE LIGHT OPS CHECK GOOD.; ALL WORK C/W<BR>AUDIT C/WMay 25, 2021 · N220WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021060479805Charger · inoperativeLEFT OVERWING ESCAPE LIGHT (L6) INOP / REPLACED BATTERY PACK AND BATTERY PACK CHARGER M1668 IAW AMM 33-51-06-960-805 AND AMM 33-51-06-960-806. LEFT OVERWING ESCAPE SLIDE LIGHT OPS CHECK GOOD.; ALL WORK C/W<BR>AUDIT C/WMay 25, 2021 · N220WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021060476887Battery Pack · inoperativeLEFT OVERWING ESCAPE LIGHT (L7) INOP ; RIGHT OVERWING ESCAPE LIGHT (L7) INOP / REPLACED BATTERY PACK AND BATTERY PACK CHARGER M1669 IAW AMM 33-51-06-960-805 AND AMM 33-51-06-960-806. RIGHT OVERWING ESCAPE SLIDE LIGHT OPS CHECK GOOD.; REPLACED BATTERY PACK AND May 25, 2021 · N220WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021060479806Charger · inoperativeLEFT OVERWING ESCAPE LIGHT (L7) INOP ; RIGHT OVERWING ESCAPE LIGHT (L7) INOP / REPLACED BATTERY PACK AND BATTERY PACK CHARGER M1669 IAW AMM 33-51-06-960-805 AND AMM 33-51-06-960-806. RIGHT OVERWING ESCAPE SLIDE LIGHT OPS CHECK GOOD.; REPLACED BATTERY PACK AND May 25, 2021 · N220WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021060476458Rib · crackedLH HORZ STAB RIB 120.30; CRACKED O/B LOWER FLANGE AT FWD END IN RADIUS ; / APPLIED CIC TO REPAIR AREA & OEM RIB IAW AMM 51-21-91; REMOVED DAMAGE ON L/H HORIZ STAB RIB 120.3 FWD LOWER O/B END IAW B737 SRM 55-10-09-2R-5. ACCOMPLISHED REPAIR PER EA 21-155-01399-WMay 25, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2021060477924Rib · crackedLH HORIZ STAB RIB AT ST A 120.3 FWD LOWER FLANGE COMMON TO SKIN I/B FASTENER HOLE CRACKED 3RD FROM FWD (MARKED) ; / COMPLETED EA 21-155-01399 FINAL; FINAL AUDIT C/WMay 15, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2021060473219Skin · debondedRIGHT WING INBOARD MAIN FLAP TRAILING EDGE SKIN DISBONDED AT OUTBOARD END / REPAIRED AREA OF DELAMINATION ON I/B R/W MAIN FLAP LOWER SKIN. IAW B737-700 SRM 57-53-01-2R-7;SRM 51-70-10-2R-4; SRM 51-70-10-2R-0; AMM 51-21-99-300-801.; STEP 12 OK; SUMMARY STATEMENTMay 15, 2021 · N220WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2021060475326Skin · crackedLH HORIZ STAB RIB AT ST A 120.3 FWD LOWER FLANGE COMMON TO SKIN I/B FASTENER HOLE CRACKED 3RD FROM FWD (MARKED) ; / ACCOMPLISHED EA 21-155-01399-WIP1; VERIFIED EA 21-155-01399-WIP1 ALL STEPS COMPLETE; FINAL AUDIT C/WMay 15, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2021060473220Rib · crackedLH HORIZ STAB RIB AT ST A 120.3 FWD LOWER FLANGE COMMON TO SKIN I/B FASTENER HOLE CRACKED 3RD FROM FWD (MARKED) ; / REMOVED DAMAGED AREA FROM LH HORIZ STAB RIB AT STA 120.3 FWD LOWER FLANGE COMMON TO SKIN I/B FASTENER HOLE PER B737 SRM 51-10-02-0G-0. REPAIRED May 15, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2021060477923Skin · crackedRIGHT HORIZONTAL STAB RIB STA 129.5 FWD UPPER FLANGE COMMON TO UPPER SKIN CRACKED ; / AUDIT C/WMay 14, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2021060472685Stub Frame · crackedR1 DOOR CUTOUT STA 291+9; FWD UPPER STUB FRAME ABOVE UPPER HINGE HAS CRACK IN FASTENER HOLE COMMON TO UPPER HOLE IN SEAL DEPRESSOR. MARKED ; / REMOVED AND REPLACED R1 IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A8370 REV C DOOR UPPER STUB FRAME; VERIFIED STEP 9; AMay 14, 2021 · N220WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2021060473158Rib · crackedRIGHT HORIZONTAL STAB RIB STA 129.5 FWD UPPER FLANGE COMMON TO UPPER SKIN CRACKED ; / REMOVED DAMAGE; FABRICATED REPAIR PARTS AND INSTALLED REPAIR TO RH HORIZONTAL STAB RIB STA 129.5 FWD UPPER FLANGE IAW EA 21-155-01361; VERIFIED ITEM 29 AND 30; AUDIT C/WMay 14, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2021060474863Skin · crackedRIGHT HORIZONTAL STAB RIB STA 129.5 FWD UPPER FLANGE COMMON TO UPPER SKIN CRACKED ; / VERIFIED TRIMMED DAMAGED AREA I.A.W EA21-155-01361 STEP1 COMPLETE; EA C/W; AUDIT C/WMay 14, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2021060473159Floor Support · crackedSTA 927-947 RBL 25 INTERCOSTAL FOUND CRACKED ; / REMOVED AND REPLACED INTERCOSTAL BS 927-947 RBL 20 IAW DWG 147A7500 REV C; SRM 51-40-02-0G-0. RESTORED CIC IAW AMM 51-21-91-620-802; ALL WORK C/W; AUDIT C/WMay 14, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021060472687Angle · crackedFWD CARGO COMPT STA 500B - 500C LBL25 BAFFLE IS BENT AND AFT ANGLE IS CRACKED. DOT A-21-071 ; / VERIFIED ITEM 4.<BR>OK TO INSTALL.; INSTALLED BAFFLE STA 500B-C FWD PIT IAW SRM 51-40-02 & BOEING DWG 143A7510 REV B; INSPECTION CW CORROSION PROTECTION CW REF SWA May 14, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021060472686Strap · corrodedAFT CARGO COMP. AFT BULKHEAD LOWER BULKHEAD STRAP CORRODED STA.947 APPROX STR 21R TO STR 25R WL 158 ; / FOUND MATERIAL LSS TO BE 100%; REMOVED AND REPLACED AFT CARGO AFT BULKHEAD RH SUPPORT RAIL BS 947 IAW SRM 51-40-02-0G-0; DWG 149A8117 REV -; RESTORED CIC IAMay 14, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021051772683Stiffener · crackedRIGHT HORIZONTAL STABILIZER; RIB STA 92.7; RIB STIFFENER #1 CRACKED ABOVE LOWER FLANGE. CUT OUT DAMAGE AREA ON #1 STIFFENER STA.92.70 HORIZONTAL STAB RIB IAW SRM 55-10-09-2R-4 REPAIR4 VERIFIED MATERIAL ID FOR REPAIR PARTS 55100003-01 TAG #WN 4752 IAW DWG 5510May 13, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2021051772682Rib · crackedDOT-125-01 RIGHT HORIZONTAL STABILIZER RIB STA 129.5; FWD LOWER FLANGE CRACKED.May 13, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2021060477922Rib · crackedDURING REMOVAL OF RIGHT HAND HORIZONTAL STAB STA 92.70 RIB WAS CRACKED AT UPPER FORWARD CORNER ; / VERIFIED STEPS ALL STEPS COMPLETE. IAW EA 21-155-01364-P1 AND FINAL<BR>FINAL AUDIT C/WMay 12, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2021060472106Rib · crackedDURING REMOVAL OF RIGHT HAND HORIZONTAL STAB STA 92.70 RIB WAS CRACKED AT UPPER FORWARD CORNER ; / ADDING P1 AND FINAL TO ITEM 12. EA 21-155-01364-WIP 1 REV P1 AND FINAL COMPLETE; VERIFIED COMPLETION OF EA 21-155-01364-WIP1 REV P1 AND FINAL; VERIFIED STEPS 12;May 12, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2021060474864Rib · crackedDURING REMOVAL OF RIGHT HAND HORIZONTAL STAB STA 92.70 RIB WAS CRACKED AT UPPER FORWARD CORNER ; / SUMMARY EA 21-155-01364 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK OF THE FAULT.<BR><BR>NOTE: THE TYPICAL WORK STEP ENG SIGN OFF WAS OMITTED FROM THE WMay 12, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2021060470136Door · gougedAPU COWL DOOR; 38' AFT OF FWD EDGE; RIGHT SIDE FRAME; DEEP GOUGE. ; / N/A'D REQUIRED STEPS; VERIFIED ITEMS 9 AND 10<BR>AUDIT C/W; VERIFIED ITEMS 9 AND 10<BR>AUDIT C/WMay 8, 2021 · N220WN · Boeing 7377H4 · Auxiliary Power Unit (APU) DoorsSDR SWAA2021052470141Angle · corrodedCORROSION ON LOWER SURFACE OF Z ANGLE WL 156 RBL 20 STA 727C TO 767 AROUND NUT PLATES ; / VERIFIED LIMITE ON R/H Z-ANGLE; STA 727C TO STA 767. ORIG 'T' .040. REM 'T' .031; LOSS .009. FOUND TO BE OUT OF LIMITS IAW. SRM 51-10-02-0G-0; VERIFIED MATERIAL LOSS IS OMay 8, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081370121Strap · corrodedDOT# A45-014; AFT CARGO PIT DOOR CUTOUT; INTERCOSTAL LOWER ATTACH STRAP HAS CORROSION; WL: 156; RBL: 19; STA: 787+12. ; / [01] REMOVED STRAP FROM STATION 787+12 TO REMOVE CORROSION IAW B737 SRM 51-40-02; [02] REMOVED CORROSION ON STRAP AT STATION 787+12 ORIGINMay 7, 2021 · N220WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2021081370126Attach Angle · corrodedDOT# A45-027; AFT CARGO PIT; RH INTERCOSTAL UNDER Z-ANGLE HAS CORROSION; WL:156; RBL:22; STA: 747-767. ; / [01] REMOVED CORROSION ON R/H INTERCOSTAL AT STATION 747-767 ORIGINAL THICKNESS .032 REMOVED .007 REMAINING .025 INTERCOSTAL WAS FOUND TO BE OUT OF LIMITMay 7, 2021 · N220WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2021060470128Splice Plate · crackedDOT-42-A22; CABIN STA 538; RBL1; FLOOR BBOARD SPLICE PLATE CRACKED @ INBD/AFT CORNER. ; / AUDIT CW; AUDIT CW; FOUND COMPLETEMay 7, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021060470125Attach Angle · corrodedAFT CARGO PIT; RH ATTACH ANGLE ON LOWER SURFACE OF FLOOR SHIELD HAS CORROSION; WL:156; RBL:22; STA: 767+4. ; / REMOVED CORROSION ON ATTACH ANGLE AT STATION 767+4 ORIGINAL THICKNESS .050 VERIFIED BY TOOL 36649 DUE 8-4-21MATERIAL REMOVED .012 REMAINING .038 ANGLMay 7, 2021 · N220WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2021060470124Cargo Track · corrodedDOT# A45-021; AFT CARGO PIT; FLOOR SUPPORT RAIL HAS CORROSION; WL: 156; RBL: 2.5; STA: 767+6. ; / REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-53-2R-2 APPLIED CIC TO AREA IAW AMM 51-21-91-620-802; May 7, 2021 · N220WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021060470122Attach Angle · crackedDOT# A45-015; AFT CARGO PIT; RH Z-ANGLE; LOWER SIDE ATTACH CLIP IS CRACKED IN RADIUS; WL: 155; RBL: 21; STA: 727+5. ; / CLIP REMOVAL & INSTALLATION ACCOMPLISHED ON FAULT TTG8Q004YWGX; FABRICATED NEW CLIP P/N 146A7505-4; ON SHOP W/O 42136-1600-0004. LOCATED ANDMay 7, 2021 · N220WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2021060470117Cargo Track · corrodedDOT# A45-019; AFT CARGO PIT; FLOOR SUPPORT RAIL HAS CORROSION; WL: 156; RBL: 13; STA: 767+6. ; / REMOVED AND REPLACED TRACK SECTION RBL 13.8 BS 747+10-887 IN FAULT TTG8Q004YWLS; C/W; AUDIT C/WMay 7, 2021 · N220WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021060470116Cargo Track · corrodedDOT# A45-018; AFT CARGO PIT; FLOOR SUPPORT RAIL HAS CORROSION; WL: 156; LBL: 2.5; STA: 767+6. ; / REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-53-2R-2 APPLIED CIC TO AREA IAW AMM 51-21-91-620-802; May 7, 2021 · N220WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021060470114Support Angle · corroded185-019 AFT CARGO COMP.AFT BULKHEAD BOTTOM ANGLE CORRODED AROUND FASTNER HOLES STA.947 LBL 16-RBL 16 WL 158 ; / REMOVED CORROSION FROM AFT BULKHEAD LOWER SUPPORT RAIL. ORIGINAL T.080' REMAINING .062' LOSS OF .018' OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 VIMay 7, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021060470112Shield · corroded185-015 AFT CARGO;RH FLOOR SHIELD CORRODED AROUND FASTNER HOLES STA 847-867 RBL 16 WL 158 ; / INSTALLED NEW SHIELD IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A0081 REV A; VERIFIED INSTALLATION ON STEP 8; VERIFIED ITEMS 8 & 9.<BR>AUDIT COMPLETE.May 7, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
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