N242WN

Service difficulty reports · 327

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 = 'N242WN' 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 SWAA2024031252836Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PULLED STRANDS ON AFT FLOOR PANEL 241XF UPPER SKIN HAVE BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.Feb 16, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024031252837Floor Panel · pulledAFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ZF UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED REPAIR OF FLOOR PANEL 241ZF UPPER SKIN IAW SRM 53-00-50Feb 16, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024031252821Floor Panel · pulledAFT FLOOR PANEL 241ABFF UPPER SKIN HAS AREAS OF PULLED STRANDS. PANEL SHOULD BE 241ABF<[01] AREAS OF PULLED STRANDS ON FLOOR PANEL 241ABF WERE REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>DOWNLOADED CURE SHEETS AND TAPE.;[02] VERIFIED FLOOR PANEL 241ABF WAS REPAIREDFeb 16, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024031252839Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ACF UPPER AND LOWER SKIN DAMAGED AREAS HAVE BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED REPAIR OF FLOOR PANEL 241ACF PER SRFeb 16, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024031252822Floor Panel · pulledAFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON AFT FLOOR PANEL 241ADF UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.Feb 16, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024031252823Floor Panel · pulledAFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242TF UPPER SKIN AREAS OF PULLED STRANDS WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED REPAIR OF FLOOR PANEL 242TF UPPER SKIN IAW SRM 53-00-50-2R-1.;[03] WORKSCOPE IS COMPLFeb 16, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024031252825Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1Feb 16, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024031252842Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] REPAIRED AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 221CF IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Feb 16, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024031252843Floor Panel · pulledFWD FLOOR PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 221EF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1.Feb 16, 2024 · N242WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2024031252830Floor Panel · pulledFWD FLOOR PANEL 222AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222AF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.Feb 16, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024031252832Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222CF UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BAC DWG 141A5810 ID: 245.;[02] INFORMATION ENTERED ON ITEM 1 WAS ENTERED IN ERROR. THIS IS AN INSPECTOR BLOCK.;[03] FWD FFeb 16, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024031252833Floor Panel · pulledFWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222DF WITH UPPER SKIN PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BAC DWG 141A5810 ID:185.;[02] VERIFIED CORRECTIVE ACTION 1.Feb 16, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024031253146Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS460 - BS500C LBL23 WL156.<[01] VERIFIED STEP 15 IN PARTIAL.;[02] VERIFIED STEP 16 COMPLETE.;[03] REJECT - INSTALLATION OF SIDEWALL SUPPORT; FOUND CRACK AT INTERCOSTAL FASTENER ATTACHMENT POINT; BS460; WL156; LBL2Feb 16, 2024 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024031452452Skin · debondedPANEL 194CL OUTER SKIN HAS 2 TIGHTLY GROUPED DISBONDS NEAR CENTER OF PANEL. (MARKED)<[01] PANEL 194CL OUTER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 51-70-05-2R-2.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED PANEL 194CL OUTER SKIN HAS BEEN REPAIRED IAFeb 15, 2024 · N242WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2024031452669Web · corrodedCORROSION ON 1016 WEB AT AFT WET AREA BS1016+13 LBL7 WL208. MARKED<[01] REMOVED CORROSION ON 1016 WEB AT AFT WET AREA BS 1016+13 LBL 7; WL 208 AND REWORKED PER EA 24-153-00486.;[02] TASK CARD COMPLETEFeb 15, 2024 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024031452670Strap · corrodedCORROSION ON TENSION STRAP AT AFT WET AREA BS1016; BS1016+11; RBL3 WL208. MARKED<[01] CORROSION ON TENSION STRAP AT AFT WET AREA BS 1016+11 RBL 3 WL 208 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED AFT WET AREA TENSION STRAP IAW SRM 51-40-02-0G-0 AND DWG 14Feb 15, 2024 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024031452815Angle · crackedRIGHT WING FIXED T/E PANEL JUST AFT OF THE PYLON ATTACH ANGLE CRACKED JUST IB OF DEFLECTION RIB. MARKED<[01] REMOVED AND REPLACED RIGHT WING FIXED T/E ATTACH ANGLE JUST AFT OF PYLON AND I/B OF DEFLECTION RIB IAW SRM 51 -40-02-0G-0 PARA. 4.;[02] VERIFIED COMPLEFeb 15, 2024 · N242WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2024031252665Floorbeam · corrodedCORROSION ON FLOOR BEAM AT AFT WET AREA BS986 RBL43 WL208. MARKED<[01] CORROSION ON BS 986 FLOOR BEAM AT RBL 43; WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R-6.;[02] CORRECTED MEASUREMENT;[03] CUSTOMER CARD COFeb 15, 2024 · N242WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024031252666Floorbeam · corrodedCORROSION ON FLOOR BEAM AT AFT WET AREA BS986 LBL43 WL208. MARKED<[01] COMPLETED STEP 8; PARTIAL STEP 9.;[02] COMPLETED STEP 9.;[03] VERIFIED STEPS 11;13 COMPLETE.;[04] REMOVED CORROSION FROM AFT WET AREA FLOOR BEAM BS 986 LBL 43 WL 208 FOUND TO BE OUT OF LIMIFeb 15, 2024 · N242WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024031252671Skin · crackedDURING HFEC INSPECTION OF LH HORIZONTAL STABILIZER LOWER SKIN (TTG8Q00BDWA5); CRACK FOUND AT STA:193.90; 18' FROM FWD EDGE; MEASURED L: 1.0' MARKED<[01] REPAIRED LH HORIZONTAL STABILIZER LOWER INSPAR SKIN AT STA 193.90 18' FROM FWD EDGE IAW SRM 55-10-01-2R-11;Feb 15, 2024 · N242WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2024031352136Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0.;[02] ADDITION TO ITEM 1: IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 SHEET:8.;[03] VERIFIED CORRECTIVE ACTION ITEMFeb 14, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024031352137Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241DF IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION 1.Feb 14, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024031352135Floor Panel · pulledFLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241EF IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION 1.Feb 14, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024031352138Floor Panel · pulledFLOOR PANEL 241FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241FF WITH PULLED STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0013;[02] VERIFIED FLOOR PANEL 241FF WAS REPLACED BY FABRICATING A NEW PANEL Feb 14, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024031352139Floor Panel · pulledFLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242CF WITH PULLED STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0006;[02] JOB COMPLETE.Feb 14, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024031451950Inlet · cracked#2 ENGINE INLET COWL OUTER LIP SKIN HAS A CRACKED RIVET HEAD AT THE 10:00 POSITION SPLICE SECOND ONE IN FROM THE AFT SIDE OF LIP SKIN.<[01] UPDATED PARTS;[02] REMOVED AND REPLACED #2 ENGINE INLET COWL IAW 71-11-01-000-802-F00 AND 71-11-01-400-802-F00 STEP 5.H.Feb 13, 2024 · N242WN · Boeing 7377H4 · Nacelle/Pylon, Plate/SkinSDR SWAA2024031352128Pressure Deck · crackedWHEEL WELL PRESSURE DECK CRACKED; BS665; RBL40; WL200<[01] BEADED PRESSURE DECK WEB WILL BE REPAIRED WITH CUSTOMER CARD TTG8Q00RJ75C.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.Feb 13, 2024 · N242WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2024031352130Pressure Deck · crackedWHEEL WELL PRESSURE DECK CRACKED; BS672; RBL41; WL200<[01] BEADED PRESSURE DECK WEB WILL BE REPAIRED WITH CUSTOMER CARD TTG8Q00RJ75C.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.Feb 13, 2024 · N242WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2024031352131Pressure Deck · crackedWHEEL WELL PRESSURE DECK CRACKED; BS666; RBL41; WL200<[01] BEADED PRESSURE DECK WEB WILL BE REPAIRED WITH CUSTOMER CARD TTG8Q00RJ75C.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.Feb 13, 2024 · N242WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2024031352129Pressure Deck · crackedWHEEL WELL PRESSURE DECK CRACKED; BS666; RBL42; WL200<[01] BEADED PRESSURE DECK WEB WILL BE REPAIRED WITH CUSTOMER CARD TTG8Q00RJ75C.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.Feb 13, 2024 · N242WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2024031251943Pressure Deck · crackedCRACK FOUND DURING HFEC INSPECTION OF HORIZONTAL PRESSURE DECK WEB (TTG8Q00BCA3K) AT RBL 41 BS663+2. L:0.4IN MARKED<[01] REPAIRED BEADED PRESSURE DECK BETWEEN BS 663.5 TO BS 675; RBL 30 TO RBL 60 WL 202 IAW SRM 53-40-51-2R-2 REPAIR 2. FIGURE 202.;[02] VERIFIEDFeb 13, 2024 · N242WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2024031251942Pressure Deck · crackedCRACK FOUND DURING HFEC INSPECTION OF HORIZONTAL PRESSURE DECK WEB (TTG8Q00BCA3K) AT LBL 34.5 BS663+1.5. L:0.5IN MARKED<[01] REPAIRED HORIZONTAL PRESSURE DECK AT LBL 34.5 BS663+1.5 PER SRM 53-40-51-2R-2 REPAIR 2. FAULT COMPLETE.;[02] VERIFIED ALL RII STEPS AREFeb 13, 2024 · N242WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2024031252132Pressure Deck · crackedWHEEL WELL PRESSURE DECK CRACKED; BS665; LBL35; WL200<[01] PRESSURE DECK AT BS 665 LBL 35 WL 200 REPAIRED ON FAULT TTG8Q00RJ619. FAULT COMPLETE.;[02] VERIFIED RII ITEMS WERE COMPLETED ON FAULT TTG8Q00RJ619.;[03] VERIFIED COMPLETION ON FAULT TTG8Q00RJ619. CARD Feb 13, 2024 · N242WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2024011139649Floor Panel · crackedFWD CARGO FLOOR AFT OF DOOR HAS CRACK IN IT. REPLACED FWD CARGO FLOOR PANEL REF AMM 25-52-10.Jan 10, 2024 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023112021649Battery Pack · failedEMERGENCY LIGHT BATTERY PACKS POS M1675 AND M1674 FAILED CAPACITANCE CHECK<[01] R/R EMERGENCY LIGHT BATTERY PACKS AT POSITIONS M1675 AND M1674 REF AMM 33-51-06.Nov 15, 2023 · N242WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023112021657Tail Cone · delaminatedTAIL-CONE RH SIDE HAS A DENT MEASURING 10 LONG 2 WIDE AND .106 DEEP. DENT HAS AREAS THAT ARE DELAMINATED.<[01] APPLIED SPEED TAPE TO TAIL CONE RH SIDE AND COMPLIED WITH EA - 23-153-03378.Nov 15, 2023 · N242WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2023111721856Tail Cone · delaminatedTAIL CONE RH SIDE HAS A DENT 12 FWD OF ELEVATOR INDEX PLATE MEASURING 3 LONG 3 WIDE AND .087 DEEP. DENT IS DELAMINATED. DAMAGE IS WITHIN 4 OF PREVIOUS DENT.<[01] C/W EA: 23-153-03381;[02] EDIT STEP 3 TO INDICATE 'YES'Nov 15, 2023 · N242WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2023071176370Handle · looseALL FOUR DOOR LINER ASSIST HANDLES ARE LOOSE.<[01] RESECURED ALL FOUR DOOR LINER ASSIST HANDLE IAW AMM-25-99-99-SWA-001 PAGE 6 STEP B ITEM (C);[02] VERIFIED ITEM 1.<BR>AUDITED.Jul 8, 2023 · N242WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2023071775840Web · crackedDURING DVI INSPECTION FOUND L/H VAPOR BARRIER WEB CRACKED AT STA 663 WL 167 LBL47<[01] EVALUATED DAMAGE; CRACKS ARE REPAIRABLE IAW B737 SRM 57-10-10-2R-2. TAP TEST GOOD; NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 51-70-04-2R-10Jul 6, 2023 · N242WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2023071875272Bracket · crackedDOT A24-07 RH WING I/B L/E WING TO BODY FAIRING / L/E SUPPORT STRUCTURE ANGLE CRACKED AT FASTENER HOLE. MARKED<[01] REMOVED CRACKED ANGLE IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05-0G-0 AND BOEING DWG# 116A3110 ID:0005 REV:B. WORK PEJul 5, 2023 · N242WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2023071275275Floor Panel · delaminatedDOT A160-46; FLOOR PANEL 241BF HAS DELAMINATION<[01] WORK ACCOMPLISHED ON NON-ROUTINE TTG8Q00M1DKDJul 5, 2023 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023071275283Floor Panel · delaminatedDOT A160-44; FLOOR PANEL 231ZF HAS DELAMINATION OF TOP PLYS<[01] WORK ACCOMPLISHED ON NON-ROUTINE TTG8Q00M1D0EJul 5, 2023 · N242WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023071874510Angle · crackedL/H VAPOR BARRIER UPPER ANGLE IS CRACKED AT STA663 WL 167 AT LBL 10 I/B<[01] ACCOMPLISHED HFEC SURFACE AND OPEN HOLE IAW B737 NDT P6 51-00-00 P16 AND P23 TOOL 44291 DUE 03NOV23 NO CRACKS NOTED;[02] AUDIT C/WJul 3, 2023 · N242WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2023071775271Angle · crackedR/H VAPOR BARRIER UPPER ANGLE HAS CRACK AT STA663 WL 167 AT RBL 45<[01] RECEIVED REPAIR ANGLES FROM BACK SHOP 2024-0 .071 W/O 44942-1000-0004 AND 2024-0 .063 W/O 44942-1000-0001;[02] VERIFIED ITEM 1;[03] ACCOMPLISHED HFEC SURFACE AND OPEN HOLE IAW B737 NDT P6 Jul 2, 2023 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023071773765Bulkhead Web · crackedR/H VAPOR BARRIER WEB AT STA 663 HAVE CRACK AT RBL 45 AND RBL 37<[01] EVALUATED DAMAGE; CRACK IS REPAIRABLE IAW B737 SRM 57-10-10-2R-2 REPAIR 2. NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 51-70-04-2R-10 PAR 4 STEPS A; B; AND C.Jul 2, 2023 · N242WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2023052250514Slide · out of adjustR1 DOOR SLIDE UNSEATED FROM HOLDER<[01] INSPECTED R1 DOOR SLIDE; RE-SECURED GIRT BAR INTO RETAINING CLIPS NO DEFECTS NOTED PER AMM 25-66-01.May 19, 2023 · N242WN · Boeing 7377H4 · Escape SlideSDR SWAA2023041024008Panel · elongatedPANEL 193B HAS SEVERAL ELONGATED HOLES.<[01] REMOVED AND REPLACED WITH NEW PANEL PER AMM 53-51-01.;[02] INSPECTION VERIFIED CORRECTIVE ACTION STEP 1.Apr 6, 2023 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022090148406Slide · out of adjustFWD ENTRY SLIDE MORE THAN ONE NEEDLE WIDTH INTO THE RED / [01] R&R FWD ENTRY SLIDE PER AMM 25-66-01Aug 30, 2022 · N242WN · Boeing 7377H4 · Escape SlideSDR SWAA2022082947453Slide · lowFORWARD ENTRY DOOR SLIDE PRESSURE IN THE RED / [01] INSPECTED SLIDE PRESSURE IAW AMM 25-66-01; FOUND WITHIN LIMITS AT THIS TIMEAug 28, 2022 · N242WN · Boeing 7377H4 · Escape SlideSDR SWAA2022040690568Girt Bar · out of positionL2 DOOR SLIDE GIRT BAR NEEDS TO BE REPOSITIONED 2022-129940 / [01] INSTALLED CORRECTLY L2 DOOR SLIDE GIRT BAR IAW B737-700 AMM 25-66-01-000-804;[02] CORRECTED ACTION<BR>INSTALLED CORRECTLY L2 DOOR SLIDE GIRT BAR IAW B737-700 AMM 25-66-01-400-803;[03] INSTALLEDApr 1, 2022 · N242WN · Boeing 7377H4 · Escape Slide
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