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 SWAA2021060470111Angle · corrodedDOT# A45-010; AFT CARGO PIT; RH Z-ANGLE HAS CORROSION; WL: 154; RBL: 20; STA: 727 TO 727C+10. ; / REMOVED CORROSION IAW RH STA 727-727C VERIFIED WITTH 10X MAGNIFY GLASS IAW SRM 53-00-53-1A-2. VERIFIED MATERIAL LOSS ORIGINAL THICKNESS .040' LOSS .008'; REMAININMay 7, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021060470107Splice Plate · corroded185-016 AFT CARGO;FLOOR PANEL SPLICE PLATE CORRODED AROUND FASTNER HOLES STA 887 LBL 16-RBL 16 WL 158 ; / REMOVED CORR0SION FROM AFT CARGO FLOOR SUPPORT PANEL SPLICE AT STA 887 LBL 16 RBL 16 VERIFIED OUT OF LIMITS DUE TO NO PUBLISHED LIMITS VERIFIED NEW PART PMay 7, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021060469795Stiffener · crackedRIGHT HORIZONTAL STAB RIB STA 92.70; RIB STIFFENER #3 IS CRACKED 1' ABOVE LOWER FLANGE. CRACK VERIFIED BY HFEC. DOT 177A-001 ; / CUT OUT DAMAGED AREA ON R/H HORZ STAB RIB ON #3STIFFENER I.A.W SRM55-10-09-2R-4.<BR>FABRICATED AND DRILLED REPAIR KIT I.A.W SRM55-1May 7, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2021052470119Cargo Track · corrodedDOT# A45-020; AFT CARGO PIT; FLOOR SUPPORT RAIL HAS CORROSION; WL: 156; RBL: 8; STA: 767+6. ; / REMOVED CORROSION FROM FLOOR SUPPORT RAIL AT STA 767+6' RBL 8 MEASURED MATERIAL LOSS USING TOOL #1714 CAL DUE 10/6/21 ORIGINAL MATERIAL THICKNESS .071 LOSS OF .031 May 7, 2021 · N220WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021052470113Cargo Track · corrodedDOT# A45-013; AFT CARGO PIT; FLOOR SUPPORT RAIL HAS CORROSION; WL: 156; RBL: 14; STA: 767 TO 807. ; / REMOVED CORROSION IAW B737 SRM 51-10-02-0G-0. ORIGINAL T .071' REMAINING .058'; LOSS OF .013. OUT OF LIMITS IAW B737 SRM 53-00-53-1A-2 FIG 103 VIEW A-A. AAR TMay 7, 2021 · N220WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021052470110Angle · corrodedDOT# A45-009; AFT CARGO PIT; RH Z-ANGLE HAS CORROSION; WL: 156; RBL: 20; STA: 727C+10 TO 767. ; / VERIFIED NEW Z-ANGLE MATERIAL AS PN BAC1496-377-7075 T6. A TAG A73414; IAW BOEING 737 SRM 53-60-53-01-2 FIGURE 2.; VERIFIED NEW PART EFFECTIVITY.; CONTINUED TO LOMay 7, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021052470108Angle · corrodedDOT# A45-012; AFT CARGO PIT; LH Z-ANGLE HAS CORROSION; WL: 156; LBL: 21; STA: 727C+10 TO 807+10. ; / VERIFIED NEW PART EFFECTIVITY.; CONTINUED LOCATING AND DRILLING NEW Z-ANGLE IAW SRM 53-00-53-2R-5.; VERIFIED IN PROCESS STEPMay 7, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021052470106Angle · corrodedDOT# A45-011; AFT CARGO PIT; LH Z-ANGLE HAS CORROSION; WL: 154; LBL: 20; STA: 727 TO 727C+10. REMOVE Z-ANGLE LH BS 727-727C + 10' IAW SRM 51-40-02-0G-0.; VERIFIED MATERIAL FOR Z-ANGLE AS PN BAC1496-377 7075 T6; 'A' TAG A81056 IAW SRM 53-60-53-01-2 FIG 2.; VEMay 7, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021052470105Floor Support · corrodedDOT# A45-008; AFT CARGO PIT DOOR CUTOUT; RH INTERCOSTAL HAS CORROSION ON UPPER AND LOWER SURFACE; WL: 156; RBL: 19; 767 TO 767+8. ; / REMOVED CORROSION ON R/H INTERCOSTAL AT STATION 767 ORIGINAL THICKNESS .056 REMOVED .016 REMAINING .040 INTERCOSTAL WAS FOUND May 7, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021052470104Shield · corrodedAFT CARGO PIT; RH FLOOR SHIELD HAS CORROSION; WL:156; RBL:22; STA: 767-787. REMOVED CORROSION ON AFT CARGO FORWARD FLOOR SHIELD ORIGINAL THICKNESS .050 REMAINING .030 REMOVED .020 SHIELD WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60--15-1A-1 TOOL 36649 DUE 8-4May 7, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021052470102Web · corrodedDOT# A45-006; AFT CARGO PIT; DOOR CUTOUT THRESHOLD WEB; UPPER SURFACE HAS CORROSION. WL: 156; RBL: 26; STA: 787+11 TO 827+10. ; / REMOVED CORROSION IAW SRM 51-10-02-0G-0; ORIGINAL T .045' REMAINING .036' LOSS OF .009'. OUT OF LIMITS IAW B737 SRM 53-60-15-1A-1 May 7, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021060469392Rib · crackedDOT 18_A22: LEFT HORIZONTAL STAB RIB STA 120.30; LOWER FLANGE CRACKED JUST FWD OF #4 STIFFENER ; / REMOVED AND REINSTALLED LEFT HORIZONTAL STAB RIB STA 120.30 IAW SRM 51-40-02-0G-0; DWG 002A0001. REPAIRED IAW EA 21-155-01399; VERIFIED STEP 30 RII; AUDIT COMPLEMay 6, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2021060469791Bracket · crackedVERTICAL STAB PANEL 324AL LOWER BRACKET IS CRACKED DOT A-21-13 ; / INSTALLED NEW RETAINER ON PANEL 324AL IAW B737 SRM 51-40-02-0G-0; DWG 172A6123 REV A; REMOVED AND REPLACED RETAINER ON PANEL 324AL IAW SRM 51-40-02-0G-0; DWG 172A6123 REV A; COMPLETED INSPECTIOMay 6, 2021 · N220WN · Boeing 7377H4 · Vertical StabilizerSDR SWAA2021060469785Web · corrodedDOT# 31 A-186 FWD PIT SILL WEB CORRODED STA 440-480 RBL 28 WL156 ; / AUDIT CW; VERIFIED STEP C/W; VERIFIED ITEM #5<BR>AUDIT CWMay 6, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021060469784Floor Panel · corrodedDOT#30 A-186 FWD PIT FLOOR CORRODED STA 420+16 LBL18 WL 156 ; / UPDATED MEASUREMENTS; VERIFIED MEASUREMENTS; ALL WORK C/W <BR>AUDIT C/WMay 6, 2021 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021060469783Shield · corrodedDOT#26 A-186 FWD PIT FWD SHILD CORRODED STA 420-440 RBL24 WL156 ; / VERIFIED STEPS 2; 3; 10; 11 AND 21 COMPLETE; REMOVED CORROSION LOSS OF .010 IS OUT OF LIMITS DUE TO NO DOCUMENTED LIMITS REMOVED AND REPLACED SHIELD IAW SRM 51-40-02 AND DWG 143A0080; VERIFIEDMay 6, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021060469782Cargo Track · corrodedDOT#25 A-186 FWD PIT FLOOR RAIL CORRODED STA 40[+2 LBL 18 WL 156 ; / UPDATED MEASUREMENTS; VERIFIED MEASUREMENTS; ALL WORK C/W <BR>AUDIT C/WMay 6, 2021 · N220WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021060469778Seat Track · corrodedDOT 23-A22; CABIN SEAT TRACK STA 463-466; LBL25; WL208; LIGHT CORROSION IN BASE OF SEAT TRACK ; / CORRECTIVE ACTION SHOULD READ: FAULT RAISED IN ERROR DUPLICATE WRITE UP TO TTG8Q004YCAQ; VERIFIED CORRECTIVE ACTION SHOULD READ: FAULT RAISED IN ERROR DUPLICATE WMay 6, 2021 · N220WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021060469777Seat Track · corrodedDOT 22-A22; CABIN SEAT TRACK STA 400-404; LBL22.5; WL208; LIGHT CORROSION IN BASE OF SEAT TRACK ; / UPDATED MEASUREMENTS; CERTIFIED STEP C/W; VERIFIED <BR>AUDIT C/WMay 6, 2021 · N220WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021060469772Cargo Track · corrodedDOT#32 A-186 FWD PIT FLOOR RAIL CORRODED STA 480+16 LBL 18 WL 156 ; / UPDATED MEASUREMENTS; VERIFIED MEASUREMENTS; ALL WORK C/W<BR>AUDIT C/WMay 6, 2021 · N220WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021060469770Cargo Track · corrodedDOT# 27 A-186 FWD PIT FLOOR RAIL CORRODED STA 400+ 18 RBL 14 WL156 ; / UPDATED MEASUREMENTS; VERIFIED MEASUREMENTS; ALL WORK C/W <BR>AUDIT C/WMay 6, 2021 · N220WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021060469764Stiffener · crackedDOT 21-A-22; RIGHT HORIZONTAL STAB RIB STA 129.50; RIB STIFFENER #3 CRACKED 1' ABOVE LOWER FLANGE ; / C.I.CED AREA I.A.W MM51-21-91-620-802; REMOVED RIB TO REPAIR CRICKET # 3 STIFFENER AT R /H HORZ STAB STA129.5 I.A.W ARM 51-40-02-0G-0<BR>REMOVED DAMAGED AREA May 6, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2021060469763Stiffener · crackedDOT 20-A-22; RIGHT HORIZONTAL STAB RIB STA 92.70; RIB STIFFENER #2 CRACKED 1' ABOVE LOWER FLANGE ; / C.I.CED RIBI.A.W MM51-21-91-620-802; REINED RIB AT R/H HORZ STAB STA92.70 TO REPAIR #2 RIB STIFFENER I.A.W SRM51-40-02-0G-0.<BR>REMOVED DAMGE AT #2 RIB STIFFENMay 6, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2021060469393Stiffener · crackedDOT 19_A22: LEFT HORIZONTAL STAB; RIB STA 120.30; RIB STIFFENER #3 CRACKED 1' ABOVE LOWER FLANGE. ; / REMOVED DAMAGE FROM L/H HORIZ STAB RIB STA 120.3; RIB STIFFENER #3 CRACKED 1' ABOVE LOWER FLANGE IAW B737 SRM 55-10-09-2R-4. REPAIRED PER 55-10-09-2R-4 CIC APMay 6, 2021 · N220WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2021060469389Seat Track · corrodedDOT0 21-A061 SEAT TRACK BASE HAS CORROSION FROM STA 727E+18' TO STA 747+1' RBL 45 WL ; / UPDATE MEASUREMENTS; I.A.W SRM 53-00-52-1A-1<BR>UPDATED STEP 7; VERIFIED STEPS 7; 8; AND 9<BR>AUDIT C/WMay 6, 2021 · N220WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021060469781Door Frame · crackedR1 DOOR SURROUND;FWD TOP CORNER INSIDE THE FRAME BEHIND THE T/T LATCH RECEIVER EVIDENCE OF A CRACK AT FASTNER (MARKED) ; / TASK COMPLETE; FINAL AUDIT C/W; FINAL AUDIT C/WMay 6, 2021 · N220WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2021051473157Panel · damagedDOT#48 A-186 FWD PIT PNL 120CF DAMAGE AT FASTENER HOLES ; / FOUND FWD CARGO PANEL 120 CF TO BE OUT OF LIMTS IAW SRM 53-00-53-1A-1 STEP 5 B 1; VERIFIED ITEM 1May 6, 2021 · N220WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021060469371Skin · damagedSKIN DAMAGE AT STA 1008 1.5' ABOVE STR 15L ; / N/A MEASUREMENT TABLE DUE TO NO DENT IN AREA; VERIFIED DENT TABLE MEASUREMENTS ARE N/A'D DUE TO DENT BEING PREVIOUSLY REPAIRED; VERIFIED AND AUDITED.May 5, 2021 · N220WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021060469370Floor Panel · damagedCABIN FLOOR PANEL 241CF EDGE HAS DAMAGE. DOT A-21-09 ; / VERIFIED STEPS 1;2;3 TAP TESTED GOOD; REPAIRED EDGE DAMAGE ON CABIN FLOOR PANEL 241CF I/A/W SRM 53-00-50-2R-10 TAP TEST GOOD; VERIFIED ITEM 5. TAP TEST GOOD<BR>AUDIT C/WMay 5, 2021 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021060469369Floor Panel · damagedCABIN FLOOR PANEL 231ZF EDGE HAS DAMAGE. DOT A-21-08 ; / RII STEPS; BONDED REPAIR AT EDGE DAMAGE ON FLOORBOARD PANEL 231ZF I/A/W SRM 53-00-50-2R-1 3A-N &REV 73); RII C/W FINAL INSPECTION; AUDIT C/WMay 5, 2021 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021060469368Floor Panel · damagedCABIN FLOOR PANEL 231WF EDGE HAS DAMAGE. DOT A-21-07 ; / APPLIED POTTING COMPOUND TO INBOARD FWD AND AFT CORNERS CORE ONLY. CURED FOR 5 HOURS AT 125 DEGREES WITH HEAT LAMP I/A/W 53-00-50-2R-10 (3) A-G REV73; REPAIRED INBOARD FWD AND AFT EDGE DAMAGE ON CABIN FLMay 5, 2021 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021060469367Floor Panel · damagedCABIN FLOOR PANEL 241FF HAS EDGE DAMAGE. DOT A-21-11 ; / REPAIRED EDGE DAMAGE ON FLOOR PANEL 241FF WITH POTTING COMPOUND I/A/W SRM 53-00-50-2R-10 STEP 3A-G (REV 73); VERIFIED STEPS 1-4; AUDIT CWMay 5, 2021 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021060469366Floor Panel · peelingCABIN FLOOR PANEL 241CF HAS PEELED FIBERS. DOT A-21-10 ; / REPAIRED PEELED FIBERS ON CABIN FLOOR PANEL 241CF I/A/W SRM 53-00-50-50-2R-1 (3) A-M (REV73) TAP TEST GOOD; VERIFIED ITEMS 1;2;3;4; AND 7<BR>AUDIT C/W; CLOSING INDEPENDENT INSPECTION THAT WAS SELECTED May 5, 2021 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021060469386Floor Panel · pulledDOT 005-A061 CABIN FLOOR BOARD 232SF UPPER SURFACE PULLED FIBERS ; / REPAIRED CABIN FLOOR BOARD 232SF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1; OK; STEP 4 & 5 OK AUDIT COMPLETEMay 5, 2021 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021060469385Floorboard · damagedDOT 001-A061 CABIN FLOOR BOARD 232SF AFT INBD CORNER DAMAGED ; / EVALUATED AND FOUND DAMAGE TO CORE AT AFT I/B CORNER AS MARKED. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-10 REV 73.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-10 STEP 3 A-D. <BR><BR>APPLIEDMay 5, 2021 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021060469384Floorboard · damagedDOT 003 A061 CABIN FLOOR BOARD 241EF HAS DAMAGE TO THE LEADING EDGE ; / BONDED REPAIR ON LEADING EDGE AREA ON FLOORBOARD PANEL 241EF I/A/W SRM 53-00-50-2R-1 STEP 3A-N (REV 73); REPAIRED LEADING EDGE DAMAGE ON FLOORBOARD 241EF I/A/W SRM 53-00-50-2R-1 STEP 3A-N May 5, 2021 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021060469383Floorboard · pulledDOT 006-A061 CABIN FLOOR BOARD 242AF UPPER SURFACE PULLED FIBERS ; / BONDED REPAIR PLIES; CURED 3 HOURS AT 150 DEGREES IAW SRM 53-00-50-2R-1 REV. 73 STEPS 3J;K;L;M AND SRM 53-00-50-2R-0 REPAIR GENERAL REV. 73. TOOLING--OVEN B0-06 DUE 5-26-21. TAP TEST GOOD.; RMay 5, 2021 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021060469382Floorboard · damagedDOT002-A061 CABIN FLOOR BOARD 242AF AFT INBD CORNER DAMAGED ; / INSTALLED INSERTS IAW BOEING DRAWING 144A5810-189 REV. A AND BAC5085 STEP 8.4.2.2 CURED 1 HOUR AT 150 DEGREES. TOOLING--AAR 30347 DUE 4-29-22; REPAIRED DAMAGE TO AFT EDGE OF FLOORBOARD 242AF IAW SMay 5, 2021 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021060469381Floorboard · pulledDOT 008-A061 CABIN FLOOR BOARD 242DF UPPER SURFACE PULLED FIBERS ; / REPAIRED CABIN FLOOR BOARD 242DF UPPER SURFACE PULLED FIBERS IAW SRM 53-00-50-2R-1 AND 53-00-50-2R-0 REPAIR GENERAL.; OK; VERIFIED STEP 3 AND 4 COMPLETE AND AUDIT COMPLETEMay 5, 2021 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021060469380Floorboard · pulledDOT 009_A061 CABIN FLOOR BOARD 241AF UPPER SURFACE HAS PULLED FIBERS ; / REPAIRED DAMAGE TO UPPER SURFACE OF PANEL 241AF. IAW B 737-700SRM 53-00-50-2R-1;SRM 53-00-50-2R-0; OK; STEP 4 & 5 OK. AUDIT COMPLETEMay 5, 2021 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021060469374Seat Track · corrodedDOT 020-A061 SEAT TRACK BASE HAS CORROSION FROM STA 727C+16' TO STA 727D+10 RBL 45 WL 208 ; / UPDATE MEASUREMENTS; VERIFIED STEP 7 AND 8 COMPLETE AND AUDIT COMPLETE; OKMay 5, 2021 · N220WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021060468449Bulkhead Web · crackedAFT CARGO; FWD BULKHEAD PNL 141LW CRACKED; DOT A-193-11 / VERIFIED PART AS 453A2510-20; SI#7254212; ITEM# 45; IAW AIPC 25-52-19-01A. PANEL TO BE INSTALLED ON W/O 42133-1000-0233.; A TAG # FOR PART IS WN1222; ALL WORK C/W<BR>AUDIT C/WMay 4, 2021 · N220WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2021052469360Floor Panel · corrodedAFT PIT PANEL 140CF HAS CORROSION AROUND FASTENER HOLES LEFT AND RIGHT SIDES A172-0003 ; / VERIFIED STARTING FABRICATION OF PANEL; STARTED FABING FLOOR PANEL. 140CF IAW AMM 25-52-01-201-801; EVALUATED CORROSION ON AFT CARGO FLOOR PANEL 140CF FLOOR PANEL WAS FOMay 4, 2021 · N220WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2020060387851Battery Pack · dischargedEMERGENCY LIGHTS IN FWD GALLEY INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IN FWD GALLEY OVERHEAD LT SIDE IAW AMM 33-51-06.May 30, 2020 · N220WN · Boeing 7377H4 · Emergency LightingSDR SWAA2020051175668Seat Track · wornF/OS FLTDECK SEAT AFT INBD SEAT TRACK WORN TO CHECK LIMITS / REMOVED AND REPLACED FLTDECK SEAT TRACK PER AMM 25-11-11May 6, 2020 · N220WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2020051175667Seat Track · wornCAPTS FLTDECK SEAT AFT INBD SEAT TRACK WORN TO CHECK LIMITS / REMOVED AND REPLACED FLTDECK SEAT TRACK PER AMM 25-11-11May 6, 2020 · N220WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2020051175656Glowstrip · wornPASSENGER CABIN FWD GALLEY TO ROW 2DEF PHOTO ILLUMINES STRIPS WORN AND HAVE MOISTURE UNDER COVER BOTH SIDES / R&R PHOTO ILLUMINES STRIPS PER AMM 25-27-31May 6, 2020 · N220WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2021081706096Skin · cracked193B PANEL HAS SEVERAL DAMAGE ON OUTER SURFACE- SKIN (DENTS;CRACKS & HOLES) / REPLACED 193B PANEL PER AMM 53-51-21Jan 28, 2020 · N220WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2019121639602Cover · detachedR/H OVERWING EMERGENCY EXIT SIGN LENS FELL OFF. / INSTALLED COVER PER AMM.Dec 6, 2019 · N220WN · Boeing 7377H4 · Emergency LightingSDR SWAA2019110138447Light · inoperativeR/H OVERWING EXIT EXTERIOR EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.Oct 31, 2019 · N220WN · Boeing 7377H4 · Emergency Lighting
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