N224WN

Service difficulty reports · 281

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 = 'N224WN' 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 SWAA2023082883227Panel · crackedL/H WING I/B FLAP TRACK ACCESS PANEL # 194CL HAS BULGING/CRACKED FASTENER HOLES<[01] REPAIRED DAMAGE TO PANEL 194CL PER SRM 51-70-04-2R-9 PARA 4.E; SRM 51-70-04-2R-9 PRIMED AND TOP COAT PER AMM 51-21-72-370-51-21-73-370-803804. REPAIR COMPLETE.;[02] VERIFIED CJul 27, 2023 · N224WN · Boeing 7377H4 · Wing, Control SurfacesSDR SWAA2023082890331Access Panel · crackedR/H WING LOWER MID T/E ACCESS PANEL # 661CB HAS BULGING/CRACKED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGED AREA AS MARKED AT PANEL #661CB AS PER B737 SRM 51-70-04-2R-1 AND 51-70-04-2R-0 PARAGRAPH 4-L-M-N ; MATERIAL USED PO#1775890 ; PO#2011230 ANDJul 27, 2023 · N224WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2023082890332Access Panel · crackedR/H WING LOWER MID T/E ACCESS PANEL # 661AB HAS BULGING/CRACKED FASTENER HOLES<[01] REMOVED PANEL 661AB;[02] ENTERED IN ERROR.;[03] APPLIED TOPCOAT ON R/H WING LOWER MID T/E ACCESS PANEL #661AB REF B 737 AMM 51-21-73-370-803;[04] APPLIED PERMANENT REPAIR ON DAJul 27, 2023 · N224WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2023082390330Floor Panel · crackedLEFT FLIGHT COMPARTMENT CONTROL STAND ACCESS PANEL # 211B CRACKED.<[01] APPLIED TOPCOAT ON LEFT FLIGHT COMPARTMENT CONTROL STAND ACCESS PANEL #211B REF B 737 AMM 25-00-00-370-801;[02] CORRECTION TO STEP 1: REPAIRED DAMAGE AREA ON LEFT FLIGHT COMPARTMENT CONTROJul 27, 2023 · N224WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023082382557Intercostal · crackedFWD CABIN BETWEEN STA 294.5 AND STA 303.9 AT S-16L WL 215.3 INERCOSTAL IS CRACKED AS MARKED. 124-021<[01] REMOVED AND REPLACED NEW INTERCOSTAL AT FWD CABIN BETWEEN STA 294.5 TO STA 303.9 S-16L WL 215.3 SRM 51-40-02-0G-0 AND DWG 141A8180;[02] VERIFIED CORRECTIVJul 26, 2023 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023082482324Floor Support · corrodedFWD CABIN FLOOR SUPPORT AT 294.5 TO 312 11 INCHES LEFT OF CENTER LINE IS CORRODED<[01] REMOVED AND INSTALLED NEW INTERCOSTAL AT FWD CABIN STA 294.5 TO STA 312 LBL 11 SRM 51-40-02-0G-0 AND DWG141A5600<BR>REMOVED EWIS PROTECTION AT FLOOR AREA PER AMM 20-60-07-90Jul 25, 2023 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023082482095Threshold · corrodedR-2 DOOR THRESHOLD INNER CORD IS CORRODED. R-2 DOOR THRESHOLD INNER CORD IS CORRODED. STA.951 TO STA 992.8 RBL 50' AND WL 2081<[01] S;[02] REMOVED AND REPLACED R-2 DOOR INNER CHORD PER REF. SRM 51-40-02-0G-0 AND DRAWING # 147A 8501.;[03] VERIFIED REPLACEMENT OJul 25, 2023 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023082382323Intercostal · crackedFWD CABIN FLOOR SUPPORT INTERCOSTAL IS CRACKED AT B/S 283 TO 294.5 AT CENTERLINE<[01] REMOVED AND INSTALLED FWD CABIN FLOOR SUPPORT INTERCOSTAL AT B/S 283 TO 294.5 AT CENTERLINE REF SRM 51-40-02-0G-0 REF SRM 51-40-05-0G-0 REF AMM 20-60-07-913-801 DWG 141A5410;Jul 25, 2023 · N224WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2023082382315Floor Panel · corrodedFWD CABIN FLOOR PANEL 222BF HAS CORRODED INSERTS<[01] RECEIVED NEW FLOOR PANEL 222BF PANEL WILLBE INSTALL ON TT J8O00LYL2F;[02] CORRECTION FOR STEP 1 : RECEIVED NEW FLOOR PANEL 222BF PANEL WILL BE INSTALL ON TTG8Q00LYL2F;[03] VERIFIED CORRECTIVE ACTIONS.Jul 25, 2023 · N224WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023082382318Floor Panel · corrodedFWD CABIN FLOOR PANEL 221CF HAS CORRODED INSERTS<[01] RECEIVED NEW FLOR PANEL <BR>WILL BE INSTALLED ON TTG8Q00LYLJO;[02] CORRECTION TO STEP 1: RECEIVED NEW FLOR PANEL<BR>WILL BE INSTALLED ON TTG8Q00LYLJ0;[03] VERIFIED 2.Jul 25, 2023 · N224WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023082481530Retainer · crackedLT WING FIXED T/E AT ORSS 274 SUPPORT STRUCTURE VERTICAL SEAL RETAINER IS CRACKED. 124-011<[01] REMOVED AND REPLACED SEAL RETAINER SUPPORT AT L/H WING T/E ORSS 274 IN REF B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP # 1.Jul 23, 2023 · N224WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2023082381230Flashlight · damagedMAIN CABIN FWD L/H WINDSCREEN FLASHLIGHT CRACK<[01] REMOVED AND REPLACED MAIN CABIN FWD L/H WINDSCREEN FLASHLIGHT ASPER DWG#25600001;[02] VERIFIED CORRECTIVE ACTION.Jul 21, 2023 · N224WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2023021499293Light · inoperativeFOUND R/H OVER WING EMERGENCY EXIT WINDOW LIGHT BALLAST BAD<[01] REMOVED R/H OVER WING EMERGENCY EXIT DOORWAY LINING IAW AMM 25-21-70-000-801;[02] REMOVED LIGHT ASSY BALLAST FROM R/H OVER WING EXIT AND INSTALLED NEW LIGHT ASSY BALLAST ON R/H OVER WING EXIT IAWFeb 5, 2023 · N224WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023020898858Stringer · crackedFOR TRACKING PURPOSES ONLY. BOEING AOG REPAIR. CRACK ON LH WING UPPER NO. 8 STRINGER (PN 112A3208-5) AT WSTA 574; WL 231<[01] AS PER EA 23-157-00135; EDGE TRIM REPAIR DOCUMENTED ON BOEING FRR-03.?;[02] UPDATED MEASUREMENTS;[03] C/W;[04] C/W<BR>AUDIT C/WFeb 4, 2023 · N224WN · Boeing 7377H4 · Wing, Longeron/StringerSDR SWAA2023021480434Web · crackedR/H STA 663 VAPOR BARRIER WEB GROUND SERVICE MODULE HYDRAULIC BRACKET HAVE A CRACK<[01] LOCATED; DRILLED AND REPLACED CRACKED -2 BRACKET ASSY FOR R/H 663 VAPOR BARRIER ON PARTS RACK IAW SRM 51-40-05-0G-0 AND BOEING DWG #276A9183 ID:0001 REV:-;[02] VERIFIED TASDec 10, 2022 · N224WN · Boeing 7377H4 · Fuselage Main, KeelSDR SWAA2023021478503Web · crackedR/H VAPOR BARRIER WEB CRACKED AT STA 663 RBL 40 WL 167<[01] VAPOR BARRIER BEEN FABRICATED AND REPLACED ON N/R TTG8Q00GFSMU;[02] VERIFIED STEP 1; JOB COMPLETE; AUDIT C/WDec 4, 2022 · N224WN · Boeing 7377H4 · Fuselage Main, KeelSDR SWAA2023021477038Attach Angle · crackedCRACK FOUND ON UPPER ATTACH ANGLE STA 663 LBL 8 (WL 167)<[01] VERIFIED ITEM I OF STEP 3 AND ITEM 1 OF STEP 5;[02] VERIFIED ITEM 3 OF STEP 5;[03] MISS SPELLED EXTERNAL NOT ENTERNAL;[04] AUDIT C/WNov 30, 2022 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023021477039Attach Angle · crackedCRACK FOUND ON UPPER ATTACH ANGLE STA 663 RBL 40 (WL 167)<[01] VERIFIED ITEM 1 OF STEP 7;[02] VERIFIED ITEM 3 OF STEP 7;[03] VERIFIED ITEM 4 OF STEP 7;[04] VERIFIED ITEN 2 OF STEP 9;[05] MISS SPELLED INTERNAL NOT ENTERNAL;[06] CAP SEALED EXTERNAL FASTNERS COMMNov 30, 2022 · N224WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2023021376323Floor Panel · pulledDOT A24-2 MID CABIN FLOOR PANEL 242AF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE.<[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 AREAS IAW B737 SRM 53-00-Nov 28, 2022 · N224WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023021376324Floor Panel · pulledDOT A24-3 MID CABIN FLOOR PANEL 241BF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE.<[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 AREAS IAW B737 SRM 53-00-Nov 28, 2022 · N224WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023021376329Floor Panel · pulledDOT A24-4 MID CABIN FLOOR PANEL 241AF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE.<[01] EVALUATED AND FOUND MISSING FIBERS ON UPPER SURFACE LENGTH OF BOARD. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPENov 28, 2022 · N224WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023021376325Floor Panel · pulledDOT A24-5 MID CABIN FLOOR PANEL 232SF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE.<[01] EVALUATED AND FOUND MISSING FIBERS ON UPPER SURFACE AFT SIDE OF BOARD. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPNov 28, 2022 · N224WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023021376330Floor Panel · pulledDOT A24-6 MID CABIN FLOOR PANEL 232RF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE.<[01] EVALUATED AND FOUIND MISSING PLIES ON UPPER SURFACE LENGTH OF PANEL. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPENov 28, 2022 · N224WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023021376326Floor Panel · pulledDOT A24-7 MID CABIN FLOOR PANEL 231ZF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE.<[01] EVALUATED PANEL 231ZF AND FOUND UPPER SURFACE WITH PULLED FIBERS. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP FOR REPAIR. IAW B737-700 SRM 5Nov 28, 2022 · N224WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023021376327Floor Panel · pulledDOT A24-8 MID CABIN FLOOR PANEL 231YF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE.<[01] EVALUATED PANEL 231YF AND FOUND PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW B737-700 SRM 53-00-50-2R-1 Nov 28, 2022 · N224WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023021376328Floor Panel · pulledDOT A24-9 MID CABIN FLOOR PANEL 231XF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE.<[01] EVALUATED PANEL 231XF AND FOUND PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP FOR REPAIR. IAW B737-700 SRM 53-Nov 28, 2022 · N224WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023011068196Light · inoperativeEMERGENCY LIGHTS AT SEAT LOCATIONS 14 CBA; 22 FED AND 23 CBA ARE INOP.Nov 5, 2022 · N224WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023011062557Stringer · crackedLT WING (#1 TANK) AFT VENT STRINGER IS CRACKED AT STRINGER U-11 JUST I/B OF RIB #6 WSTA 228.25 AND EXTENDING O/B BEYOND RIB #6. JACKED AIRCRAFT IAW AMM 07-11-01-580-815. SHORING REQUIRES AN OK TO CONTACT AT FUSELAGE STATIONS 360; 662; & 1016. LH WING STATIOct 20, 2022 · N224WN · Boeing 7377H4 · Wing, Longeron/StringerSDR SWAA2022101961433Light · inoperativeAFT RIGHT CABIN EMERGENCY LIGHTS ARE INOP /Oct 18, 2022 · N224WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022101961432Light · inoperativeAFT LEFT CABIN EMERGENCY LIGHTS ARE INOP /Oct 18, 2022 · N224WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022101961431Light · inoperativeMISC CENTER LEFT AND RIGHT CABIN EMERGENCY LIGHTS ARE INOP / [01] FAULT RAISED IN ERROR;[02] AUDIT C/WOct 18, 2022 · N224WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022101961430Light · inoperativeMISC FOWARD LEFT WET AREA EMERGENCY LIGHTS ARE INOP /Oct 18, 2022 · N224WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022102055649Light · inoperativeAFT AREA ENTRY LIGHT IS INOP / [01] REPLACED AFT ENTRY LIGHT BALLAST I.A.W. AMM 33-29-00-960-804.<BR>WN22831<BR><BR>SIGNING FOR ISAI VALADEZ EMP#35642;[02] C/W STEP 1 <BR>OPS CHECK REQ'D;[03] PERFORMED GOOD OPS CHECK OF ENTRY LIGHT IAW AMM 33-29-00-960-804 STESep 26, 2022 · N224WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023011016127Support · corrodedR/H PRESSURE WEB SUPPORT STRUCTURE STA 663 TO 684.668 WL 202 RBL 65 HAS AREA OF CORROSION ON AFT END. REMOVED CORROSION IAW SRM 51-10-02-0G-0; EVALUATED MATERIAL LOSS - ORIGINAL THICKNESS .125'; LOSS .007'; REMAINING .118'. REPAIRED RH PRESSURE WEB SUPPORT Sep 21, 2022 · N224WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2023011016125Shear Tie · corrodedR/H PRESSURE DECK SHEAR TIE AT STA 665 TO 669 RBL 65 TO RBL 70 WL 202 HAS AREA OF CORROSION. REMOVED CORROSION IAW SRM 51-10-02-0G-0; EVALUATED MATERIAL LOSS - ORIGINAL THICKNESS .063'; LOSS OF .006'; REMAINING .057'. NO ALLOWABLE MATERIAL LOSS LIMITS. RECESep 21, 2022 · N224WN · Boeing 7377H4 · Fuselage Internal Mounting StructureSDR SWAA2023011016130Intercostal · corrodedRH INTERCOSTAL SHELF HAS LIGHT CORROSION ON LOWER O/B FLANGE. REMOVED CORROSION IAW SRM 51-10-02-0G-0. EVALUATED MATERIAL LOSS. ORIGINAL THICKNESS .180'; LOSS .010'; REMAINING .170'. REMOVED CORROSION AND REPAIRD RH INTERCOSTAL SHELF LOWER O/B FLANGE IAW EA 22Sep 21, 2022 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023011016128Bracket · corrodedR/H WHEEL WELL STA 663 TO 695 RBL 70 SHELF SECONDARY BRACKET SHUT OFF VALVE SUPPORT CORROSION FOUND ON BONDING MATING SURFACE<[01] REMOVED CORROSION IN BRACKET IAW SRM 51-10-02-0G-0 ITEM 15;[02] MEASURED MATERIAL 'T' ORIGINAL .071 REMAINING .067 LOSS .004 TOOLSep 21, 2022 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022102016124Web · corrodedR/H PRESSURE WEB SUPPORT CLIP AT STA 663 RBL 63 WL 202 HAS AREA OF CORROSION / [01] REMOVED CORROSION IAW SRM 51-10-02-0G-0; EVALUATED MATERIAL LOSS - ORIGINAL THICKNESS .063'; LOSS .007; REMINING .056'.<BR>TOOL# AAR29270 CAL DUE 12/09/22.;[02] NO ALLOWABLE MASep 21, 2022 · N224WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2022102016126Web · delaminatedR/H PRESSURE WEB STA 663 TO 684.668 RBL 65 TO RBL 70 WL 202 HAS AREA OF DELAM ON FWD END / [01] VERIFIED NEW WEB P/N 144A7732U1 ATAG WN23125 IAW E/A 22-153-03009-WIP1 STEP 2.;[02] VERIFIED MATERIAL;[03] LOCATED AND DRILLED NEW WEB IAW SRM 51-40-05-0G-0 AND BOESep 21, 2022 · N224WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2022102051881Handle · out of adjustDOT A-24-1 FORWARD GALLEY SERVICE DOOR INTERIOR HANDLE HAS EXCESSIVE PLAY. / [01] RESURED FORWARD GALLEY SERVICE DOOR INTERIOR HANDLE I/A/W AMM 52-41-11-400-801 STEP 3 F [5] 3];[02] VERIFIED STEP 1<BR>AUDIT CWSep 9, 2022 · N224WN · Boeing 7377H4 · Galley DoorsSDR SWAA2022102052876Pickle Fork · cracked(RH) STEP 2 OF EA 22-153-02730-WIP1 IS INCOMPLETE. REMOVE STRINGER 17 INTERCOSTAL PER 737-700 SRM 51-40-02. REFER TO FIGURE 1-1; REF 144A5901 AND 144A5900 / [01] REMOVED FLOOR WEB ASSY STA 643 - STA 663 IAW B737-700 SRM 51-40-02;[02] REMOVED FLOOR WEB ASSY STASep 9, 2022 · N224WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2022101951721Battery Pack · inoperativeFWD RIGHT CABIN WET AREA EMERGENCY LIGHTS ARE INOP / [01] REMOVE AND INSTALLED BATTERY PACK IAW AMM 33-51-06-960-805;[02] REMOVE AND INSTALLED BATTERY PACK IAW AMM 33-51-06-960-805; OPS CHECK GOOD.;[03] VERIFIED ITEM 2<BR>AUDIT C/WSep 9, 2022 · N224WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022111551613Fitting · crackedDUE TO CRACK FINDING IN THE L/H BS 663 FRAME FITTING; THE R/H FRAME FITTING IS BEING REPLACED (PICKLE FORK) PN 144A2400-38. ASSY P/N 144A2400-36#B / [01] STARTED REMOVE FASTENERS RH FRAME STA 663 LH IAW B737-700 SRM 51-40-02;[02] VERIFIED ACTION 1;[03] REMOVEDSep 8, 2022 · N224WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2022090649758None · crackedFOUND CRACK AT THE L/H PICKLE FORK FITTING #6 FASTENER AT S-L18A. VERIFIED WITH HFEC 737 NDT PART 6 51-00-00 PROCEDURE 23. STARTED REMOVE FASTENERS LH FRAME STA 663 IAW B737-700 SRM 51-40-02. REMOVED 663 FRAME SPLICE PLATE FWD OF FRAME, AND REMOVED I/B OF FSep 3, 2022 · N224WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2022081241191Girt Bar · looseGIRT BAR ON FOWARD SERVICE DOOR LOOSE / [01] RESECURED FWD SERVICE DOOR GIRT BAR IAW AMM 25-66-01Aug 11, 2022 · N224WN · Boeing 7377H4 · Escape SlideSDR SWAA2022053111931Door · out of adjustFLIGHTATTENDANTS ARE REPORTING THAT FORWARD ENTRY DOOR IS HARD TO CLOSE; AND THAT IT TOOK THEM A FEW TIMES TO CLOSE IT CORRECTLY. / [01] ADJUSTED GUIDE ARM. OPS CK GOOD. POSITIVE LATCH OVER AND SMOOTH CLOSER. REF AMM 52-11-21.May 26, 2022 · N224WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2022052409885Cover · missingEMERGENCY EXIT ROW SIGN COVER MISSING ON A/C LEFT / [01] INSTALLED LEFT EMERGENCY EXIT EXIT ROW EXIT SIGN COVER AS PER REF AMM 33-51-01May 20, 2022 · N224WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022022877163Handle · brokenFWD. SERVICE DOOR HANDLE BROKE. / [01] R&R FWD. SERVICE DOOR ASSIST HANDLE PER S.I.P.Feb 23, 2022 · N224WN · Boeing 737* · Galley DoorsSDR SWAA2022022475714Light · inoperativeINFO ONLY - DURING PREFLIGHT - FOUND EMERGENCY PANEL LIGHT C/B OUT / [01] NOTED BY MAINT.Feb 20, 2022 · N224WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021120248918Light · inoperativeR/H OVER WING EXTERIOR EMERGENCY LIGHT INOP. ; / [01] RELAMPED PER AMM 33-51-04; OPS CHECK GOOD.Dec 1, 2021 · N224WN · Boeing 7377H4 · Emergency Lighting
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