N942WN

Service difficulty reports · 184

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 = 'N942WN' 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 SWAA2026101473533Floor Panel · crackedFWD CARGO FLOOR PANEL 120CF CRACKED. REMOVED & INSTALLED A NEW FWD CARGO FLOOR PANEL IAW AMM 25-52-10.Oct 10, 2026 · N942WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026101389481Floor Panel · crackedGROUND CREW FOUND SMALL CRACK IN BIN C FLOOR FAULT. OK TO CONTINUE PER MEL 25-16-01 XA. REMOVED AND REPLACED THE FLOOR PANEL 120BF IAW AMM 25-52-10.Oct 9, 2026 · N942WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026072729522Skirt · debondedPASSENGER CABIN FWD SERVICE DOOR ESCAPE SLIDE SKIRT RUBBER TORN AND DISBONDED. R & R THE SLIDE IAW AMM 25-66-01.Jul 21, 2026 · N942WN · Boeing 7377H4 · Escape SlideSDR SWAA2026072713137Battery Pack · no testFWD LT EMERGENCY BATTERY PACK AT M1675 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK PER AMM 33-51-06.Jul 21, 2026 · N942WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026060308625Light · faultyF/O SIDE EMER EXT LIGHT FLICKERS. OK TO CONTINUE PER MEL 33-2-03 SP1B. REMOVED AND REPLACED F/O SIDE EMERGENCY EXIT SIDE WALL LIGHT IN REF TO AMM 33-21-00. OPS TEST GOOD. THIS CLEARS MEL.Jun 1, 2026 · N942WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026031679934Slide · displacedAFT RT SERVICE DOOOR SLIDE DISPLACED. REPOSITIONED SLIDE PER MT 725-61-06.Mar 14, 2026 · N942WN · Boeing 7377H4 · Escape SlideSDR SWAA2025102928336Socket · dirtyFWD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. CLEANED LAMP SOCKET CONTACTS AND VERIFIED NORMAL OPERATION OF FWD SERVICE DOOR EXTERIOR EMERGENCY LIGHT LAMP IAW AMM 33-51-00.Oct 25, 2025 · N942WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025060969973Keelbeam · crackedCRACK INTERNAL STRUCTURE KEEL BEAM LOCATED BETWEEN BS 727 TO BS 727A AND STR 27R AT AFT CARGO COMPARTMENT 2025-310172<[01] ON STEP 7 AND 8. TOOL USED: ET INSTRUMENT. P/N: NORTEC 600D. S/N: 60007161486. DUE DATE: 06-SEP-25.;[02] TOOLS USED: TEMPERATURE CONTROLLMay 12, 2025 · N942WN · Boeing 7377H4 · Fuselage Main, KeelSDR SWAA2025060969974Angle · crackedCRACK ANGLE LOCATED BS907 TO BS 927 BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT 2025-310174<[01] REPLACED ANGLE AND FASTENERS LOCATED BS907 TO BS927 BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G AND DWG: 147A7221 SHEET: 28 REV: - <May 12, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025060969975Angle · crackedCRACK ANGLE LOCATED BS947.5 AND S-26L AT AFT CARGO COMPARTMENT 2025-310173<[01] REPLACED ANGLE (FITTING) AND FASTENERS LOCATED BS947.5 AND S-26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0; DWG # 149A8103 SHEET 7 REV: A.<BR>SEMay 12, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025060970160Scuff Plate · crackedCRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2025-310178<[01] TOOL USED DIGITAL CALIPER P/N:500-193-30; S/N: 0000291; DUE DATE: 01-NOV-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000 ; S/N : 1753759 ; DUE DATE: 30/JUN/25;[03] REPAIRED THMay 12, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025060970159Rib · crackedCRACK RIB LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER 2025-310176<[01] TOOL USED: TEMPERATURE CONTROLLED: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26.;[02] REPLACED RIB AND FASTENERS LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER I.A.W B737May 12, 2025 · N942WN · Boeing 7377H4 · Vertical Stabilizer, Spar/RibSDR SWAA2025060969745Angle · crackedCRACK ANGLE - CLIP LOCATED BS400 AFT SIDE LBL 24 FWD CARGO COMPARTMENT 2025-310106<[01] INSTALLED CLIP LOCATED BS 400 AFT SIDE LBL 24 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 AND DWG# 143A7505 SHEET 117 AND REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02]May 11, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025060969744Support Channel · corrodedCORROSION CHANNEL SUPPORT LOCATED BETWEEN BS500A AND BS500B LBL24 WL 156.5 AT FWD CARGO COMPARTMENT 2025-310101<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N 45MG S/N 232019809 DUE DATE: 08-OCT-25.;[02] REPAIRED CHANNEL SUPPORT (SUPPORT ZEE) LOCATED BETWEEN BS480 AMay 11, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025060969746Support Channel · corrodedCORROSION CHANNEL SUPPORT LOCATED BETWEEN BS500 AND BS500A RBL24 WL 156.5 AT FWD CARGO COMPARTMENT 2025-310110<[01] REPLACED CHANNEL SUPPORT (SHIELD) AND FASTENERS LOCATED BETWEEN BS500 TO BS500A RBL 24 WL 156.5 AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM May 11, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025060969747Access Panel · crackedCRACK BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB 2025-310153<[01] REPLACED BLADE ON ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0.<BR>MEASURED CRACK IS L: 0.181 INCHES; TOOL USED DIGITAL CALIPER P/N: 8647A42;May 11, 2025 · N942WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2025060969317Angle · crackedCRACK ON ANGLE - CLIP LOCATED BS500B AND LBL21 FWD CARGO COMPARTMENT 2025-310010<[01] REPLACED CLIP LOCATED BS 500B AND LBL 21 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 AND DWG# 143A7505 SHEET 118 AND REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACMay 9, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025060969320Angle · crackedCRACK ON ANGLE - CLIP LOCATED BS500C AND LBL21 FWD POSITION FWD CARGO COMPARTMENT 2025-310011<[01] REPLACED CLIP LOCATED BS 500C AND LBL 21 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 AND DWG# 143A7505 SHEET 117 AND REV -. SEE INDIVIDUAL SIGN OFF BELOWMay 9, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025060969314Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 120.30 AND 28 INCH FROM FRONT SPAR LT HORIZONTAL STAB 2025-310000<[01] TOOL USED ON STEP 3: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 220272712 DUE DATE: 28-JAN-26;[02] PERFORMED REPAIR ON INSPAR RIB LOCATED STAB STA 120.30 May 9, 2025 · N942WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2025060969311Rib · crackedCRACK INSPAR RIB LOACTED STAB STA 129.50 AND 9 INCH FROM REAR SPAR LT HORIZONTAL STAB 2025-310001<[01] ON STEP 3 AND 4. TOOL USED: ET INSTRUMENT. P/N: NORTEC 600D. S/N: 210136503. DUE DATE: 24-JUL-25.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600May 9, 2025 · N942WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2025060969312Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 129.50 AND 9 INCH FROM REAR SPAR AT RT HORIZONTAL STABILIZER 2025-310003<[01] STEP 3 AND STEP 4. EDDY CURRENT EQUIPMENT USED P/N: NORTE 600D; S/N: 220273012 AND DUE DATE: 22-JAN-26.;[02] STEP 7. EDDY CURRENT EQUIPMENT USED P/NMay 9, 2025 · N942WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2025060969178Floorbeam · crackedCRACK ON BREAK PANEL LOCATED BS 540 LBL 1 AT CENTER WING BOX 2025-309994 CRACK ON BREAK PANEL LOCATED BS 540 BTW BL0 TO LBL 24.75 AT CENTER WING BOX<[01] REPLACED BREAK PANEL AND FASTENERS LOCATED BS 540 BTW BL0 TO LBL 24.75 AT CENTER WING BOX IAW B737-700 SRMMay 9, 2025 · N942WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2025060969179Angle · crackedCRACK ANGLE LOCATED BS 695 LBL1 AT CENTER WING BOX 2025-309996<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 29 JAN 26; TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 DUE DATE 28 JAN 26.;[02] REPLACED ANGLE AND FASTEMay 9, 2025 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025060969180Floorbeam · crackedCRACK ON BREAK PANEL LOCATED BS 540 RBL 1 AT CENTER WING BOX 2025-309995 CRACK ON BREAK PANEL LOCATED BS 540 BTW BL0 TO RBL 24.75 AT CENTER WING BOX<[01] REPLACED BREAK PANEL AND FASTENERS LOCATED BS 540 RBL 1 AT CENTER WING BOX IAW B737-700 SRM 51-40-02-0G; BMay 9, 2025 · N942WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2025060968101Handle · deterioratedDETERIORATED ASSIST HANDLE NUT ON FORWARD ENTRY DOOR LINING AT FORWARD GALLEY AREA (4EA). REPLACED ASSIST HANDLE NUT ON FORWARD ENTRY DOOR LINING AT FORWARD GALLEY AREA (4EA) IAW AMM 52-11-31-400-802 STEP 3.G.(4). THE INSTALLATION IS DOCUMENTED ON TTG8Q010CWFMay 7, 2025 · N942WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2025060968098Light · deterioratedDETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA). REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) I.A.W B737-700 AMM 33-51-15-400-802.May 6, 2025 · N942WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025060968093Skin · crackedCRACK LOWER SURFACE ACTUATOR AREA LEADING EDGE ON SLAT 6 AT RT WING. REPAIRED LOWER SURFACE ACTUATOR AREA LEADING EDGE ON SLAT 6 AT RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1.May 6, 2025 · N942WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2025031404536Girt Bar · out of adjustGIRT BAR ON AFT CAPTAINS SIDE HANGING OUT TOO FAR <[01]. REINSTALLED GIRT BAR IAW MM 25-66-01.Mar 12, 2025 · N942WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2025012889974Battery Pack · inoperativeEMERGENCY LIGHTS ABOVE ENTRY DOOR AND FWD 2 AISLE LIGHT ON RH SIDE INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1674 IN REF TO AMM 33-51-06. ALL AFFECTED EMERGENCY LIGHTS OPS CHECK GOOD AT THIS TIME.Jan 27, 2025 · N942WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024091737107Attach Bracket · crackedRIGHT MAIN LANDING GEAR CENTER DOOR BOTTOM FWD ATTACH BRACKET CRACKED AT THE BARREL NUT.<[01] OK TO CONTINUE PER CDL 32-10-3; SP1B<BR>AUTHORIZATION CODE: #213893Sep 13, 2024 · N942WN · Boeing 7377H4 · Landing Gear DoorsSDR SWAA2024081325102Handle · brokenMAIN CABIN DOOR ASSIST HANDLE BROKEN<[01] R&R L-1 DOOR ASSIST HANDLE PER A.M.M. 25-21-31 & I.P.C. 52-11-51-12.Aug 10, 2024 · N942WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2024081325061Handle · brokenFWD ENTRY DOOR ASSIST HANDLE BROKEN.<[01] RESECURED DOOR ASSIST HANDLE IAW AMM 52-11-31.Aug 9, 2024 · N942WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2024052085442Sign · detachedPLASTIC EXIT SIGNS POPPED OFF HOLDER MID-CABIN<[01] INSTALLED PLASTIC EXIT SIGN COVERS IAW AMM 33-51-01. EXIT SIGN COVERS SECURITY CONFIRMED.May 14, 2024 · N942WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023091499302Flap · delaminatedL/H WING OUTBOARD AFT FLAP IS DELAMINATED ON UPPER INBOARD SURFACE. DELAMINATING IS 6.50 LONGITUDINALLY; 5.25 LATERALLY; 1.25 AWAY FROM TRAILING EDGE AND 1.25 AWAY FROM INBOARD EDGE.<[01] REMOVED AND REPLACED OUTBOARD AFT FLAP IAW B737 AMM 27-51-22. COMPLETE USep 12, 2023 · N942WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2023062771129Handle · looseCUSTOMER WALK R-2 DOOR ASSIST HANDLE LOOSE<[01] SECURED R2 DOOR ASSIST HANDLE AS PER B737 AMM 52-13-31-400-802.;[02] VERIFIED AND INSPECTED STEP #; SECURED R2 DOOR ASSIST HANDLE AS PER B737 AMM 52-13-31-400-802.Jun 25, 2023 · N942WN · Boeing 7377H4 · Fixed Inner DoorsSDR SWAA2023062770284Light · inoperativeR2 DOOR EXTERIOR EMERGENCY LIGHT INOP.<[01] REPLACED LAMP SLIDE/OVERWING EMERGENCY LIGHT AS PER REF AMM 33-51-041-960-801 TEST PASS;[02] REPLACED LAMP SLIDE/OVERWING EMERGENCY LIGHT AS PER REF AMM 33-51-04-960-801 TEST PASS;[03] VERIFIED FINAL CORRECTIVE ACTIOJun 22, 2023 · N942WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023062770285Battery Pack · inoperativeL2 EMERGENCY AND AFT CENTER EXIT LIGHT INOP<[01] CLEANED BATTERY PACK AND CONNECTOR AS PER REF AMM 20-60-06-100-801 AND PERFORMED EMERGENCY LIGHT OPERATIONAL TEST AS PER REF AMM 33-51-00-710-801; TEST PASS;[02] VERIFIED FINAL CORRECTIVE ACTION.Jun 22, 2023 · N942WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023070358411Channel · corrodedMODERATE TO FLACKING LEVALS OF CORROSION FOUND ON UNDER SIDE OF RT.SIDE Z-CHANNEL FROM STA 807- STA 787 AT FASTENER HOLE LOCATIONS. ( MRKED ). R/H AFT CARGO COMPARTMENT STA 727 - STA 767 CHANNEL UNDER SIDE AT FASTENER HOLES HAS CORROSION.<[01] INSTALLED NEW ZEJun 13, 2023 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070358413Channel · corrodedMODERATE TO FLACKING LEVALS OF CORROSION FOUND ON UNDER SIDE OF LT. SIDE OF THE Z-CHANNEL FROM STA 807- STA 767 AT FASTENER HOLE LOCATIONS. ( MRKED ).<[01] REMOVED AND REPLACED ZEE CHANNEL ON L/H AFT CARGO COMPARTMENT PER REF. SRM 51-40-02-0G-0 AND DRAWING # 1Jun 13, 2023 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062958410Channel · corrodedMODERATE TO FLACKING LEVALS OF CORROSION FOUND ON UNDER SIDE OF LT. SIDE Z-CHANNEL FROM STA 887- STA 844 AT FASTENER HOLE LOCATIONS. ( MRKED ). MODERATE TO FLACKING LEVALS OF CORROSION FOUND ON UNDER SIDE OF LT. SIDE -CHANNEL FROM STA 807- STA 847 AT FASTENER Jun 13, 2023 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062758409Channel · corrodedMODERATE TO FLACKING LEVALS OF CORROSION FOUND ON UNDER SIDE OF RT.SIDE Z-CHANNEL FROM STA 767- STA 747 AT FASTENER HOLE LOCATIONS. ( MRKED ).<[01] REMOVED CORROSION ON R/H Z-CHANNEL FROM STA. 767 - STA. 747 PER REF. SRM 51-10-02-0G-0; AFTER FURTHER EVALUATIONJun 13, 2023 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062758412Channel · corrodedMODERATE TO FLACKING LEVALS OF CORROSION FOUND ON UNDER SIDE OF LT. SIDE OF Z-CHANNEL SECTION FROM STA 807- STA 847 AT FASTENER HOLE LOCATIONS. ( MRKED ).<[01] REMOVED CORROSION ON L/H Z-CHANNEL FROM STA. 807 - STA. 847 PER REF. SRM 51-10-02-0G-0; AFTER FURTHEJun 13, 2023 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062858776Angle · crackedCRACK INDICATION FOUND AT L/H VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 42 HOLE. CRACK INDICATION FOUND AT L/H VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 42 HOLE.<[01] INSTALLED REPAIR AT L/H VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 42 PER REF SRM 57-10-10-2R-5 REPAJun 12, 2023 · N942WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2023070357861Door · corrodedCORROSION AT AFT LAV EXTERIOR SERVICE DOOR EXTERNAL SKIN FWD CORNER MKD DOT<[01] REF TASK CARD TTG8Q00LJR0Z FOR TOILET SERVICE DOOR REPLACEMENT.;[02] VERIFIED STEP #1. TRANSFER CARD.Jun 11, 2023 · N942WN · Boeing 7377H4 · Service DoorsSDR SWAA2023062957860Stiffener · crackedLOWER FUSELAGE CENTER WING STIFFENER CRACKED AT R/H VAPOR BARRIER O/B A/C AIR EXIT EXHAUST DUCT RBL 25 STA 663.75<[01] REMOVED DAMAGE STIFFENER AND INSTALLED NEW STIFFENER ON R/H VAPOR BARRIER STA. 663.75 RBL 25; PER REF. SRM 51-40-02-0G-0 AND DRAWING # 111A10Jun 11, 2023 · N942WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2023062957859Stiffener · crackedLOWER FUSELAGE CENTER WING STIFFENER CRACKED AT L/H VAPOR BARRIER O/B A/C AIR EXIT EXHAUST DUCT LBL 25 STA 663.75<[01] REMOVED AND REPLACED STIFFENER AT LOWER FUSELAGE CENTER WING L/H VAPOR BARRIER O/B A/C AIR EXHAUST DUCT LBL 25 STA 663.75 REF.737-700-SRM 51-Jun 11, 2023 · N942WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062858775Angle · crackedLOWER FUSELAGE CENTER WING R/H VAPOR BARRIER UPPER CHORD ATTACHED ANGLE CRACKED @ RBL 7 STA 663.75 MKD DOT LOWER FUSELAGE CENTER WING R/H VAPOR BARRIER UPPER CHORD ATTACHED ANGLE CRACKED @ RBL 9.25 STA 663.75 MKD DOT<[01] ACCOMPLISHED REPAIR AT RT. VAPOR BARRIJun 11, 2023 · N942WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2023070360058Balance Weight · erodedVERTICAL STAB. T/E RUDDER BALANCE WEIGHT AT CENTER POSITION HAS SEVERAL EROSION. VERTICAL STAB. T/E RUDDER BALANCE WEIGHT AT CENTER POSITION HAS SEVERAL CORROSION.<[01] REMOVED RUDDER BALANCE WEIGHT IN REFERENCE CMM 55-40-09. AND INSTALLED RUDDER BALANCE WEIGHJun 10, 2023 · N942WN · Boeing 7377H4 · Vertical Stabilizer Miscellaneous StructureSDR SWAA2023070357465Skin · crackedCRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90; 17' FROM FRONT SPAR ;I/B ROW. CRACK LENGTH: 1.468' CRACK FOUND AT LEFT HORIONTAL STABILIER LOWER SKIN AT STAB STA 193.90 17&#34; FROM FRONT SPAR I/B ROW. CRACK LENGTH: 1.468&#34;<[01] INSJun 9, 2023 · N942WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2023062957471Vapor Barrier · crackedLEFT VAPOR BARRIER SIGNS OF CRACKS.<[01] STEPS # 4 & 5 WERE CHANGED TO COMPLETE FOR COMPLETION OF ALL WORK STEPS ON THIS COARD ARE NOW COMPLETED.;[02] VERIFIED ALL WORK STEPS HAVE BEEN ACCOMPLISHED AS REQUIERD PER WORK INSTRUCTIONS ON JOB CARD.Jun 9, 2023 · N942WN · Boeing 7377H4 · Fuselage Main, Bulkhead
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