N215WN

Service difficulty reports · 291

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 = 'N215WN' 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 SWAA2022100552521Lamp · inoperativeROW 7DEF SIDEWALL LIGHT INOP / [01] THIS IS ORIGINATING LOG PAGE THIS CLEARS MEL 33-2-03 SP1B REF 737 AMM 33-21 -32 RELAMPED ROW 7 DEF SIDE WALL LIGHT OPS CK GOODOct 3, 2022 · N215WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022092051699None · inoperativeFWD RIGHT CABIN WET AREA EMERGENCY LIGHTS ARE INOP / [01] REMOVED AND REPLACED FWD BATTERY PACK M1647 STA 322 IAW AMM 33-51-06-960-805. OPERATIONAL CHECK GOOD.;[02] VERIFIED STEP 1; CHECK PASSED; JOB COMPLETE; AUDIT C/WSep 9, 2022 · N215WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022091551557Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 232SF TOP SIDE HAS PULLED FIBERS THE LENGTH OF THE PANEL 2' INBD OF L/H SIDE. DOT 203-31 / [01] WORK ACCOMPLISHED ON NON-ROUTINE TTG8Q00EPIKD;[02] VERIFIED STEP 1Sep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551554Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 2417BF TOP SIDE HAS PULLED FIBERS FROM THE AFT EDGE TO THE MIDDLE OF THE PANEL 1' INBD OF R/H SIDE. DOT 203-15 / [01] WORK ACCOMPLISHED ON W.O. TTG8Q00EP1YH;[02] VERIFIED STEP 1Sep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551553Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241BF TOP SIDE HAS PULLED FIBERS FROM THE FWD EDGE TO THE MIDDLE OF THE PANEL 2' INBD OF L/H SIDE. DOT 203-14 / [01] WORK ACCOMPLISHED ON W.O. TTG8Q00EP1YH;[02] VERIFIED STEP 1Sep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551543Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241AF TOP SIDE HAS PULLED FIBERS FROM THE AFT EDGE TO THE MIDDLE OF THE PANEL 2' INBD OF L/H SIDE. DOT 203-11 / [01] DAMAGE TO UPPER SURFACE OF FLOOR BOARD 241AF WAS ACCOMPLISHED ON TTG8Q00EP1H0;[02] VERIFIED STEP 1Sep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551541Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241AF TOP SIDE HAS PULLED FIBERS THE LENGTH OF THE PANEL 17' INBD OF L/H SIDE. DOT 203-10 / [01] DAMAGE TO UPPER SURFACE OF FLOOR BOARD 241AF WAS ACCOMPLISHED ON TTG8Q00EP1H0;[02] VERIFIED STEP 1Sep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551540Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241AF TOP SIDE HAS PULLED FIBERS FROM THE AFT EDGE TO THE MIDDLE OF THE PANEL 23' INBD OF R/H SIDE. DOT 203-09 / [01] DAMAGE TO UPPER SURFACE OF FLOOR BOARD 241AF WAS ACCOMPLISHED ON TTG8Q00EP1H0;[02] VERIFIED STEP 1Sep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551539Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241AF TOP SIDE HAS PULLED FIBERS THE LENGTH OF THE PANEL 17' INBD OF R/H SIDE. DOT 203-08 / [01] DAMAGE TO UPPER SURFACE OF FLOOR BOARD 241AF WAS ACCOMPLISHED ON TTG8Q00EP1H0;[02] VERIFIED STEP 1Sep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551537Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241AF TOP SIDE HAS PULLED FIBERS THE LENGTH OF THE PANEL 8' INBD OF R/H SIDE. DOT 203-07 / [01] DAMAGE TO UPPER SURFACE OF FLOOR BOARD 241AF WAS ACCOMPLISHED ON TTG8Q00EP1H0;[02] VERIFIED STEP 1Sep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551536Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 232SF TOP SIDE HAS PULLED FIBERS THE LENGTH OF THE PANEL DOWN THE CENTER. DOT 203-30 / [01] EVALUATED PANEL 232SF AND FOUND AREA'S OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLESep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551528Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 242AF TOP SIDE HAS PULLED FIBERS THE LENGTH OF THE PANEL 9' INBD OF L/H SIDE. DOT 203-24 / [01] EVALUATED DAMAGE TO FLOOR PANEL 242AF FOUND WITHIN REPAIRABLE LIMITS OF B737-700 SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED UPPER SURFACE OSep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551532Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 242BF TOP SIDE HAS PULLED FIBERS THE LENGTH OF THE PANEL 1' INBD OF L/H SIDE. DOT 203-05 / [01] EVALUATED FLOOR PANEL 242BF FOUND WITHIN REPAIRABLE LIMITS OF SRM REPAIR 53-00-50-2R-1;[02] PREPPED FLOOR PANEL 242BF FOR WET LAY-UP REPSep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551533Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 242BF TOP SIDE HAS PULLED FIBERS THE LENGTH OF THE PANEL 2' INBD OF R/H SIDE. DOT 203-06 / [01] EVALUATED UPPER SURFACE OF FLOOR PANEL 242BF FOUND WITHIN REPAIRABLE LIMITS OF SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED FLOOR PANEL 242BFSep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551544Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 232RF TOP SIDE HAS PULLED FIBERS THE LENGTH OF THE PANEL 1' INBD OF R/H SIDE. DOT 203-27 / [01] EVALUATED AND FOUND MULTIPLE AREAS OF PULLED FIBERS ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 RESep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551548Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 231YF TOP SIDE HAS PULLED FIBERS THE LENGTH OF THE PANEL 2' INBD OF R/H SIDE. DOT 203-21 / [01] EVALUATED AND FOUND MISSING FIBERS ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR>Sep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551551Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 231XF TOP SIDE HAS PULLED FIBERS THE LENGTH OF THE PANEL 8' INBD OF R/H SIDE. DOT 203-01 / [01] EVALUATED AND FOUND MISSING FIBERS ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR>Sep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551552Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 231XF TOP SIDE HAS PULLED FIBERS THE LENGTH OF THE PANEL 15' INBD OF L/H SIDE. DOT 203-02 / [01] EVALUATED AND FOUND MISSING FIBERS ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BRSep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551524Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241AF TOP SIDE HAS PULLED FIBERS FROM THE AFT EDGE TO THE MIDDLE OF THE PANEL 10' INBD OF R/H SIDE. DOT 203-16 / [01] EVALUATED AND FOUND MULTIPLE AREAS OF PULLED FIBERS ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAISep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022091551527Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 242AF TOP SIDE HAS PULLED FIBERS THE LENGTH OF THE PANEL 2' INBD OF R/H SIDE. DOT 203-23 / [01] EVALUATED DAMAGE TO FLOOR PANEL 242AF FOUND WITH-IN REPAIRABLE LIMITS OF SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED UPPER SUFACE OF FLOOR PSep 9, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022092151510None · delaminatedRIGHT WING OUT BOARD AFT FLAP; LOWER INBD SURFACE IS DELAMINATED / [01] EVALUATED DAMAGE; LOWER INBD SURFACE DELAMINATION IS REPAIRABLE IAW B737 SRM 57-53-01-2R-4.<BR><BR>REMOVED DELAMINATED SKIN; CLEANED AND PREPPED AREA IAW B737 SRM 51-70-10-2R-0 REPAIR GENESep 8, 2022 · N215WN · Boeing 737 · Trailing Edge FlapsSDR SWAA2022051206296Floor Panel · crackedAFT CARGO FLOOR PANEL 140BF HAS A CRACK IN CENTER THAT MEASURES 8 INCHES LONG. / [01] REMOVED DAMAGED FLOOR PANEL; FABRICATED NEW 140BF FLOOR PANEL; AND INSTALLED PER AMM 25-52-10.May 10, 2022 · N215WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022032485726Clamp · brokenWHEN APU BLEED WAS TURNED ON A LOUD BANG WAS HEARD AND SMOKE BEGAN ENTERING THE CABIN / [01] C/W CONDITIONAL INSPECTION PER AMM 05-51-56-200-801; FOUND APU BLEED AIR DUCT CLAMP INBD OF AFT PRESSUE BULKHEAD BROKEN. R & R CLAMP PER SIP. LEAK CK GOODMar 20, 2022 · N215WN · Boeing 737* · APU Cowling/ContainmentSDR SWAA2022013164843Slide · inoperativeFORWARD ENTRY DOOR SLIDE GAUGE INDICATES LOW PRESSURE OUT OF THE GREEN BAND ; / [01] REPLACED L1 DOOR SLIDE PER MT#725-61-06Jan 27, 2022 · N215WN · Boeing 7377H4 · Escape SlideSDR SWAA2022013163641Light · failedAFT L/H EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK ; / [01] REMOVED AND REPLACED PATTERN PACK PER M/M 33-51-06.Jan 25, 2022 · N215WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022013163642Light · failedEMERGENCY LIGHTING BATTERY PACK AT R/H OVERWING EXIT FAILED CAPACITY CHECK ; / [01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.Jan 25, 2022 · N215WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021122053595Light · inoperativeBOTH LEFT AND RIGHT OVERWING EXIT SIDEWALL LIGHTS ARE INOP. PERFORMED EMERGENCY LIGHTS OPERATIONAL CHECK(TEST) IAW AMM 33-51-00 OPS CHECK GOOD.Dec 15, 2021 · N215WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021110338517Lens · missing# 22 BULLNOSE EMERGENCY LIGHT LENS COVER MISSING ; / [01] OK TO CONTINUE PER MEL 33-15-02. SP 1. LOG PAGE # 1901907; [02] INSPECTED AND FOUND LENS MISSING AND RETAINER/HOUSING DIS-BONDED FROM BULLNOSE PANEL. NO PARTS IN STOCK AT THIS TIME. REMOVED AND REPLACEDOct 30, 2021 · N215WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021062285511Girt Bar · out of adjustAFT SERVICE DOOR SLIDE GIRT REQUIRES ADJUSTMENT ; / SECURED AFT SERVICE ESCAPE SLIDE AND GIRT PER AMM 25-66-01.Jun 18, 2021 · N215WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2021062286328Girt Bar · out of adjustAFT SERVICE DOOR SLIDE GIRT REQUIRES ADJUSTMENT ; / SECURED AFT SERVICE ESCAPE SLIDE AND GIRT PER AMM 25-66-01.Jun 18, 2021 · N215WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2021062285507Girt Bar · out of adjustFWD ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT ; / ADJUSTED SLIDE GIRT PER AMM 25-66-01Jun 18, 2021 · N215WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2021062285503Seal · crackedR/H HORIZONTAL STAB UPPER SLIDING SEAL CRACKED ; / R&R R/H HORIZONTAL STAB. UPPER FORWARD SLIDING SEAL REF AMM 53-31-31.Jun 18, 2021 · N215WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2021031554756Bulb · burned outCUSTOMER WALK: LH EMERGENCY EXIT LOWER LIGHT HAS BURNT OUT BULB / RELAMPED LH EMERGENCY EXIT LOWER LIGHT AS PER REF B737 AMM 33-51-01-960-801. OPS CHECK FOUND NORMAL.Mar 12, 2021 · N215WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021031551834Baffle · crackedFOUND BAFFLE UNDER 'Z' CHANNEL SIDE PLATE CRACKED DURING INSTALLATIO LOCATED STA 500 TO 500A / (DATA ENTRY) REMOVED AND INSTALLED NEW BAFFLE AT LEFT SIDE UNDER 'Z' CHANNEL (SIDEPLATE) BETWEEN STA 500 AND 500A IN REFERENCE SRM 51-40-02-0G-0 AND DOCUMENT NUMBER Feb 28, 2021 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021031549796Web · corrodedFWD CARGO DOOR THRESHOLD PLATE WEB IS CORRODED WL 154 / REMOVED AND INSTALLED NEW THRESHOLD PLATE WEB. AT FWD CARGO COMPART DOOR REF B737-700 SRM 51-40-02-0G-0 D/W: 143A8120-17 OLD THRESHOLD WEB FOUND OUT OF LIMITS REF B737-700 SRM 53-30-15-1A-1.Feb 18, 2021 · N215WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2021031549798Support · corrodedFWD CARGO FLOOR SUPPORT AT STRINGER 25R 500-TO 500A IS CORRODED. / REMOVED CORROSION AT FWD CARGO FLOOR SUPPORT STA 500-500A STR 25R REF B737-700 SRM 51-10-02-0G-0; FOUND TO BE OUT OF LIMITS REF B737-700 SRM 53-00-53-1A-1; REMOVED AND REPLACED FLOOR SUPPORT REFeb 18, 2021 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021031549799Support Channel · corrodedFWD CARGO FLOOR SUPPORT 'Z' CHANEL AT STRINGER 25 RIGHT FROM 500A TO 500D IS CORRODED; WL 154. REMOVED AND REPLACED SIDE PLATE ('Z' CHANNEL) OF FWD CARGO STR 25R FROM STA 500A TO 500D IN REFERENCE SRM 5140020G0 AND DOCUMENT NUMBER 143A7500Feb 18, 2021 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021031549804Support · corrodedFWD CARGO FLOOR SUPPORT AT 420-440 STRINGER 25 RIGHT IS CORRODED. / REMOVED AND REPLACED FLOOR SUPPORT AT FWD CARGO STA 420 TO STA 440 AND STR 25 RIGHT IN REFERENCE SRM 51-40-02-0G-0 AND DOCUMENT NUMBER 143A8126.Feb 18, 2021 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021031549878Support Channel · corrodedAFT CARGO FLOOR SUPPORT AT 25R 'Z' CHANNEL IS CORRODED AT 727C TO 767. REMOVED AND REPLACED 'Z' CHANNEL FOR AFT CARGO COMPARTMENT FROM STA 727 STA 767 AS PER B737 SRM 514002060 AND DWG REF 146A 7502 VERIFIED SQUEEZED OUT AND 100% FASTENER INSTALLATION AS PER BFeb 18, 2021 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021031549882Support Strap · corrodedAFT CARGO FLOOR SUPPORT AT BS 887 25L-25R IS CORRODED. WL 168 / REMOVED AND REPLACED FLOOR SUPPORT STRAP FOR AFT CARGO STA BS 887 25L-25R AS PER 51-40-02-0G-0 AND DWG REF 146A7500Feb 18, 2021 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021031549884Support Angle · bentAFT CARGO BS 727 LOWER SUPPORT ANGLE FOR SIDE WALL PANEL IS BENT P/N 453A2611-26; / RECEIVED NEW ANGLE FOR AFT CARGO LOWER SUPPORT SIDEWALL PANEL REPLACEMENT. PART TO BE INSTALLED UPON CLOSE UP OF AFT CARGO COMPARTMENT REF JPANEL-141-CLOSE 2017037-1000-0076Feb 18, 2021 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021031549805Housing · brokenAFT LOWERED CEILING PANEL EXIT LIGHT HOUSING BROKEN / REPLACED AFT LOWERED CEILING PANEL EXIT LIGHT HOUSING IN REF B737-700 AMM 33-51-01-960-802Feb 18, 2021 · N215WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021030849880Channel · corrodedAFT CARGO LEFT SIDE FLOOR SUPPORT STRINGER 25L 'Z' CHANNEL FROM 727B TO 847 IS CORRODED. REMOVED AND REPLACED AFT CARGO FLOOR SUPPORT 'Z' CHANNEL FROM BS 727B TO 847. LBL 21 AS PER B737-7 SRM 51-40-02-0G-0 AND DWG REF 142A7502 ACCOMPLISHED SPLICE REPAIR BETWEEFeb 18, 2021 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021030849881Support · corrodedAFT CARGO FLOOR SUPPORT AT 727D+6 IS CORRODED AT 25L TO 25R_WL 155.5 / CLEANED AND EVALUATED CORROSION FOR FLOOR SUPPORT STRAP AT BS 727D+6' AS PER B737-7 SRM 51-10-02-0G-0. CORROSION FOUND TO BE OUT OF LIMITS AS PER B737-7 SRM 53-00-53-1A-2 FIG D. RECEIVED NEFeb 18, 2021 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021030849877Floor Support · corrodedAFT CARGO FLOOR SUPPORT AT BS 767+5 FROM 25L TO 25R IS CORRODED. CLEANED AND EVALUATED CORROSION FOR FLOOR SUPPORT STRAP AS BS 767+5 AS PER B737-7 SRM 51-10-02-0G-0. CORROSION FOUND TO BE OUT OF SERVICEABLE LIMITS AS PER B737-7 SRM 53-00-53-IA-2 FIG D. RECEIVEFeb 18, 2021 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021030849875Web · corrodedAFT CARGO DOOR THRESHOLD WEB IS CORRODED. / CLEANED CORROSION ON THRESHOLD WEB ON AFT CARGO DOOR AS PER B737-7 SRM 51-10-02-0G-0; PERFORMED NDT ON REWORKED AREA ORIGINIAL MAT 0.050'; MAT REMAINING 0.040'; MAT LOSS 0.010' FOUND TO BE OUT OF LIMITS AS PER B737-7Feb 18, 2021 · N215WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2021030849874Channel · corrodedFWD CARGO FLOOR SUPPORT 'Z' CHANNEL STRINGER 25L FROM 420 TO500D HAS AREAS OF LIGHT CORROSION MISSING PRIMER PAINT REMOVED AND INSTALLED NEW 'Z' CHANNEL (SIDE PLATE) AT STR25L FROM STA 396 TO STA 500D IN REF. SRM 51-40-02-0G-0 AND DOCUMENT NUMBER 143A7501.Feb 18, 2021 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021030849876Support · corrodedAFT CARGO FLOOR SUPPORT AT 767-787 STRINGER 25R IS CORRODED / CLEAN CORROSION AT AFT CARGO FLOOR SUPPORT AT STA 767-787-25R AS PER B737-700 SRM 51-10-02-0G-0; PERFORM NDT ON REWORKED AREA AND MIN MAT THICKNESS WS 0.040' MAT REMOVED 0.010' FOUND OUT OF LIMITS AFeb 18, 2021 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021031549610Gusset · crackedFWD CARGO LH GUSSET CRACKED AT STA 520; STR 19L; WL 200. / REMOVED AND INSTALLED NEW GUSSET AT FWD CARGO L/H STA 520; STR 19L IN REF SRM 51-40-02-0G-0 AND DOCUMENTED NUMBER 143A9481Feb 17, 2021 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021031549608Gusset · crackedFWD CARGO RH GUSSET CRACKED AT STA 520; STR 19R; WL 200. / REMOVED AND REPLACED GUSSET ON FWD CARGO COMPT AT STA 520; STR 19R; WL200 AS PER B737-700 SRM 51-40-02-0G-0Feb 17, 2021 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
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