N960WN

Service difficulty reports · 180

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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 = 'N960WN'
  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 SWAA2026011259295Floor Support · crackedPASSENGER DECK FLOOR SUPPORT BS 540, LT OF CENTERLINE, CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.Jan 8, 2026 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026011259290Floor Support · crackedFORWARD CARGO BAY, A/C DISTRIBUTION BAY, MAIN PASSENGER DECK FLOOR SUPPORT, BS 540 RT IS CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.Jan 8, 2026 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026011259282Seal · crackedRH ELEVATOR UPPER SLIDER SEAL CRACKED. R&R RH HORIZONTAL STAB UPPER FWD SLIDING SEAL IAW AMM 53-31-31.Jan 8, 2026 · N960WN · Boeing 7377H4 · Elevator Miscellaneous StructureSDR SWAA2025102225663Battery Pack · inoperativeFWD GALLEY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG.Oct 19, 2025 · N960WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025061782051Light · inoperativeCR RR LEFT OVER WING EMERGENCY EXIT DOOR LIGHT INOPERATIVE. VERIFIED LEFT OVER WING EMERGENCY EXIT DOOR LIGHT. OPS CHECK IS GOOD IAW SWA BOEING 737-700 AMM 33-51-04-960-802.Jun 15, 2025 · N960WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025061781247Battery Pack · inoperativeEMERGENCY LIGHTS INOPERATIVE RH STOW BIN POSITION 8;11 AND 13. REMOVED AND REPLACED RH EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK IS GOOD.Jun 12, 2025 · N960WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025050566533Battery Pack · inoperativeRH OVER WING EMERGENCY EXIT LIGHTS 3EA INOP<[01] CHARGED RH OVER WING EXIT LIGHT POWER SUPPLY BATTERY PACK OPS OK IAW AMM 33-51-06May 2, 2025 · N960WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025050566532Battery Pack · inoperativeLH OVER WING EMERGENCY EXIT LIGHTS 3EA INOP<[01] R&R LH OVER WING EMERGENCY EXIT LIGHT POWER SUPPLY BATTERY PACK OPS OK IAW AMM 33-51-06May 2, 2025 · N960WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025021896623Battery Pack · inoperativeTWO EMERGENCY LIGHTS ON EXTERIOR AFT LOWER BELLY NOT WORKING<[01] REMOVED AND REPLACED THE BATTERY PACK ON STA L/H 747 FOR TWO EMERGENCY LIGHT ON EXT AFT LOWER BELLY REF AMM 33-51-06; OPS CHECK GOOD.;[02] ADDING PART REQUIREMENT DOCUMENTED ON TTG8Q00YG68X:<BR>Feb 16, 2025 · N960WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024123081569Floor Panel · crackedRAMP REPORTS CRACK IN AFT CARGO FLOOR<[01] REMOVED AND REPLACED AFT CARGO PANEL 241KF IN REF TO EA M-21-153-00666Dec 29, 2024 · N960WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024112161119Panel · crackedFWD CARGO PANEL 120CF HAS CRACK ABOUT 6IN LONG.<[01] REPAIRED CRACK ON FWD CARGO PANEL 120 CF PER AMM 25-52-01.Nov 18, 2024 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024072315412Limiter · inoperativeLOSS OF B SYSTEM WHEN SETTING FLAPS TO 5 FOR LANDING<[01] REMOVED AND REPLACED TRAILING EDGE FLAP FLOW LIMITER IN REF TO AMM 27-51-67.;[02] REF TTG8Q00URRTA R/R HYD PUMP.Jul 22, 2024 · N960WN · Boeing 7377H4 · Trailing Edge Flap Control SystemSDR SWAA2024072315908Limiter · leakingLOSS OF B SYSTEM WHEN SETTING FLAPS TO 5 FOR LANDING<[01] REMOVED AND REPLACED TRAILING EDGE FLAP FLOW LIMITER IN REF TO AMM 27-51-67.;[02] REF TTG8Q00URRTA R/R HYD PUMP.Jul 22, 2024 · N960WN · Boeing 7377H4 · Trailing Edge Flap Control SystemSDR SWAA2024040570771Fairing · pulled#6 FLAP SUPPORT AFT FAIRING HAS FASTENERS PULLED THRU<[01] 04 - REPAIRED PER [SRM 57-53-70-2R-2-A01234 (REPAIR 2 - FLAP SUPPORT FAIRING - NUMBERS 3 AND 6 INBOARD TRAILING EDGE FLAP - ALTERNATIVE 1 - 500 CYC DVI - INTERIM REPAIR)];[02] VERIFIED WORK PERFORMED IApr 5, 2024 · N960WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2024020547507Engine · failedON CLIMB OUT #2 ENG LOUD BANG ; LOSS OF THRUST ENGINE FAIL MESSAGE; NO N2 ROTATION. ON ENGINE SHUTDOWN EGT RED BOXED.<[01] R&R #2ENG PER MT 771-00-01;[02] R&R #2ENG PER MT 771-00-01. RII 67658Feb 1, 2024 · N960WN · Boeing 7377H4 · Engine (Turbine/Turboprop)SDR SWAA2023072481290Tire · damagedON CLIMB OUT AT APROX; 12.000 FEET WE FELT A POP AND SHUDDER FROM UNDERNEATH AIRCRAFT; ALL SYSTEMS AND INDICATIONS WERE NORMAL. - CONTINUE TO FAULT DESCRIPTION SECTION 15 MINUTES LATER THE MASTER CAUTION ILLUM WITH SYS A HYDRAULIC QTY LOSS. AFTER LANDING DISCOJul 21, 2023 · N960WN · Boeing 7377H4 · Tire TubeSDR SWAA2023062872172Battery Pack · inoperativeLIGHTS ASSOCIATED WITH M1670 BATTERY INOP LIGHTS ASSOCIATED WITH M1670 BATTERY INOP. SUSPECTED BAD BATTERY CHARGER. REMOVED AND REPLACED M1670 BATTERY PACK WITH SERVICEABLE UNIT AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-06-960-805. COMPLETION OF STEJun 28, 2023 · N960WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023062771029Light · inoperativeFWD SERVICE DOOR SLIDE LIGHT IS INOP<[01] REPLACED LAMP FOR FWD SERVICE SLIDE LIGHT AND PERFORMED GOOD TEST PER AMM 33-51-04-960-801.;[02] VERIFIED CORRECTION ACTION ITEM 1; CARD COMPLETE.Jun 25, 2023 · N960WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023062771030Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1672 ARE INOP<[01] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1672 AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-06-960-805.;[02] CERTIFIED ACTION 1;[03] FOR PARTS REQUIREMENTS.;[04] VERIFIED CORRECTIVE Jun 25, 2023 · N960WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023062771034Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1673 ARE INOP. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1673 IAW AMM 33-51-06-960-805. PERFORMED GOOD CONTINUITY CHECK ON CONNECTOR D11330 AND AISLE LAMPS ON BS 720, WL 274, LBL 30, & AISLE LIGHT BS 850 Jun 25, 2023 · N960WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023062870253Sign · brokenLAV B EXIT INDICATOR IS BROKEN<[01] REPLACED LAV B EXIT INDICATOR IAW AMM 33-51-01-960-801. OPS CHECK REQUIRED;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] VERIFIED CORRECTIVE ACTION 1.;[04] FAULT CORRECTION DOCUMENTED ON TTG8Q00LV2LC.<BR>PERFORMED GOOD OPS TEJun 21, 2023 · N960WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023062961090Light · brokenEXIT LIGHT FOR OVERWING EXIT'S ATTACHED TO OVERHEAD DIFFUSER IS BROKEN.<[01] REMOVED AND REPLACED EXIT LIGHT HOUSING ASSY FOR OVER WING EXITS PER AMM 33-51-01-960-802.;[02] CERTIFIED CORRECTIVE ACTION 1;[03] VERIFIED ALL STEPS COMPLETED.Jun 20, 2023 · N960WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023062957824Seat Track · crackedBS 727B; LBL 45.5 SEAT TRACK FASTENER LOCATION B CRACK NOTED IN FLOOR BEAM LAYER<[01] UPSIZED HOLE 1/32 IAW SRM 51-40-05. REQUIRES NDI TO VERIFY CRACK FREE CONDITION.;[02] CERTIFIED CORRECTIVE ACTION 1;[03] ACCOMPLISHED HFEC INSPECTION OF FASTENER HOLE INDICATJun 10, 2023 · N960WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2023062956973Seat Track · crackedCRACKED SEAT TRACK FASTENER AT PASSENGER CABIN BS727B LBL45 WL208. FWD FASTENER.<[01] UPDATED MEASUREMENTS TABLE AND STEP 1.;[02] CERTIFIED CORRECTIVE ACTION 1 AND STEP 1 PARTIAL;[03] UPDATED MEASUREMENTS TABLE;[04] VERIFIED MEASUREMENT TABLE;[05] REMOVED CABIJun 7, 2023 · N960WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2023062954606Floor Panel · pulledFLOOR PANEL 232RF UPPER SKIN HAS PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 232RF USING BMS 4-23TY2 LOT#1525675-1. INSTALLED INSERTS USING BMS 5-107 LOT#AK2KP8383K-1; CURED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2023; APPLIED Jun 1, 2023 · N960WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062954982Angle · crackedCRACKED INTERCOSTAL AT PASSENGER CABIN BS500D+6 BL0 WL208.<[01] REMOVED PASSENGER CABIN UPPER ANGLE INTERCOSTAL FROM BS500D - BS420; BL 0; PER SRM 51-40-02-0G-0.<BR>RECEIVED FROM TOOL ROOM NEW INTERCOSTAL UPPER ANGLE P/N 143A5410-170; LOCATED AND DRILL PER SRMJun 1, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062954980Intercostal · crackedCRACKED INTERCOSTAL AT PASSENGER CABIN BS380+14 LBL13 WL208.<[01] DRILLED FASTENERS AND REMOVED INTERCOSTAL IAW SRM 51-40-02;[02] CERTIFY;[03] UPDATED MEASUREMENT TABLE;[04] RECEIVED NEW ANGLE PER CUSTOMER RO: N923207-SWA;[05] VERIFIED CORRECTIVE ACTION 4;[06]Jun 1, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062954983Intercostal · crackedCRACKED INTERCOSTAL AT PASSENGER CABIN BS380+14 BL0 WL208.<[01] REMOVED PASSENGER CABIN UPPER ANGLE INTERCOSTAL FROM BS380 - BS400; BL 0; PER SRM 51-40-02-0G-0<BR>RECEIVED FROM TOOL ROOM NEW INTERCOSTAL UPPER ANGLE P/N 143A5410-170; LOCATED AND DRILL PER SRM 5Jun 1, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062955086Scuff Plate · crackedAFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACK ON AFT CARGO DOOR FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B. (2) AND (4)<BR>EQUIP USED: WELDING MACHINE E10583; CAL DUE 01/20Jun 1, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062955087Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACK ON AFT CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B. (2) AND (4)<BR>EQUIP USED: WELDING MACHINE E10583; CAL DUE 01/202Jun 1, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062954981Intercostal · crackedCRACKED INTERCOSTAL AT PASSENGER CABIN BS380+10 RBL40 WL208.<[01] RECEIVED NEW ANGLE PER CUSTOMER RO: N923207-SWA;[02] VERIFIED CORRECTIVE ACTION 1;[03] REMOVED CRACKED INTERCOSTAL AT PASSENGER CABIN BS380+10 RBL40 WL208 IAW SRM 51-40-02;[04] LOCATED AND DRILLJun 1, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062954100Sidewall Support · damagedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS DISBONDED NUTPLATE AT STA 727D+8; WL 155.5; LBL 21.<[01] WORK TO BE COMPLETED BY CUST SYSTEM ID : TTG8Q00LC60R<BR>THIS FLOOR TO SIDEWALL SUPPORT IS REPAIRED BY REPLACEMENT;[02] VERIFIED CORRECTIVE ACTION 1May 31, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070353513Bracket · crackedAFT CARGO COMPARTMENT AT THE 727 BULKHEAD HAS BROKEN BRACKET AT STA: 727; WL:14.5; BL:3.5 CORRECTION WL: 163 RBL:3.5<[01] MEASURMENT UPDATE; NO ALLOWABLE DAMAGE LIMIT FOUND IN SRM. PART TO BE REPAIRED BY REPLACMENT;[02] REMOVED CRACKED 727 BULKHEAD BRACKET AT May 30, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070354094Supercharger · corrodedAFT CARGO RIGHT FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT: STA:727B+14; 727C+14; 727C+6; 727D+3; 727D+8; 727D+11; 727D+14; 727D+18; 727E+2; 727E+6 WL: 156; RBL:20 T0 22<[01] VERIFIED APPLICABILITY OF SRM 53-60-53-01-2 IDENTIFICATION 2 AND SRM 53-00-53-1A-2 ALMay 30, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070354095Support · corrodedAFT CARGO COMPARTMENT RIGHT FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT STA: 727E+10; 727E+14; 727E+18; 747+2; 747+6; 747+10; 747+15; 747+18 WL:156; RBL: 20 TO 24<[01] VERIFIED APPLICABILITY OF SRM 53-60-53-01-2 IDENTIFICATION 2 AND SRM 53-00-53-1A-2 ALLOWABLE May 30, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070354092Support · corrodedAFT CARGO COMPARTMENT LEFT FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT STA: 727+6; 727E+6;747; 747+2; 747+10; 747+14; 767; 767+3; 767+4.5; 787. WL 156: LBL 20 TO 24<[01] REMOVED CORROSION ABOUT 1' X 1' AT <BR>STA 727+6 0.005'(OUT OF LIMIT)<BR>STA 727E+6 0.002'<May 30, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070354096Shield · corrodedAFT CARGO COMPARTMENT CARGO BAY FWD SHIELD HAS CORROSION FROM STA:767+3 THRU RBL:787+4; RBL:26; WL:156<[01] NO ALLOWABLE DAMAGE FOUND FOR THIS PART IN B737-700 SRM 53-00-53-1A-2 AFT CARGO FLOOR STRUCTURE ALLOWABLE DAMAGE.<BR>REPAIR BY REPLACEMENT IAW SRM 51-10May 30, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062954093Bracket · brokenAFT CARGO COMPARTMENT AT THE 727 BULKHEAD HAS BROKEN BRACKET AT STA: 727; WL:163; RBL:3.5<[01] TRANSFERED MEASUREMENTS FROM FAULT TTG8Q00LBLDX.;[02] INSTALLED NEW ACB BULKHEAD BRACKET AT BS 727; WL 163; RBL 3.5 IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG May 30, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070352620Bracket · crackedRIGHT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET (212A1116) ACCESS PANEL 192CR BS540+6 RBL8. MARKED<[01] REMOVED CRACKED R/H ECS BAY DUCT SUPPORT BRACKET AT BS540+6 RBL 8 AND REPLACED WITH NEW BRACKET PER SRM 51-40-02-0G-0 AND AIPC 36-13-01-01;[02] VERIFIED CORRMay 25, 2023 · N960WN · Boeing 7377H4 · Wing, Center BoxSDR SWAA2023070352136Structure · corrodedCORROSION ON L1 DOOR MOP SILL AT STA 328+6; +7.5; & +14.5; WL 208.1; LBL 60.<[01] PART REPLACED ON FAULT TTG8Q00L8VCT;[02] VERIFIED MEASUREMENT TABLE<BR><BR>VERIFIED CORRECTIVE ACTION 1May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070352623Shield · corrodedFWD CARGO BAY SHIELD HAS CORROSION BS 500+13; RBL 26; WL 156<[01] PART HAS NO LIMIT FOR DAMAGE. BLEND IS 1'L X 1'W REMOVED 0.010. PART IS FOUND TO BE (OUT LIMITS) REPAIR BY REPLACEMENT. IAW SRM 51-10-02;[02] REMOVED AFT SHIELD FROM FWD CARGO IAW SRM 51-40-02;[May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070352635Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK RBL45 BS410;440;473 WL208.<[01] VERIFIED APPLCABILITY PER SRM 53-00-52-1A-1. REMOVED CORROSION FROM CABIN SEAT TRACK AT BS 440 RBL45 W208 L:3' W:.45' D:.25' ON CROWN FOUND SEAT TRCK TO BE OUT OF LIMIT PER SRM 53-00-52-1AMay 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Internal Mounting StructureSDR SWAA2023070352621Stringer · corrodedAREA AFT OF FWD CARGO BAY STR 23 IS CORRODED AT THE AFT FASTENER; STR 23; RBL 45<[01] REMOVED CORROSION ON FCB STRINGER 23R BS 539 L=0.500'X W=0.500'D=0.036' FROM ORIGINAL THICKNESS 0.036' DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103 DETAIL B.[05]May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023070352637Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK RBL45 BS500+4; BS500C+9 WL208.<[01] VERIFIED APPLCABILITY PER SRM 53-00-52-1A-1. REMOVED CORROSION FROM CABIN SEAT TRACK AT BS500+4 RBL45 W208 L:3' W:.45' D:.22' ON CROWN; FOUND SEAT TRACK TO BE OUT OF LIMIT PER SRM 53-0May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Internal Mounting StructureSDR SWAA2023070352626Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK RBL45 BS727C+16; 727E+8; 787+9 WL208.<[01] VERIFIED APPLCABILITY PER SRM 53-00-52-1A-1. REMOVED CORROSION FROM CABIN SEAT TRACK AT BS727C+16 RBL45 W208 L:3' W:.45' D:.25' ON CROWN; FOUND SEAT TRACK TO BE OUT OF LIMIT PERMay 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070352641Seat · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK LBL25 BS371 WL208.<[01] VERIFIED APPLICABILITY FOR 737-700 SRM 53-00-52-1A-1.<BR>REMOVED CORROSION FROM PASSENGER CABIN SEAT TRACK AT LBL 25 WL 208 BS371 L: 2' W: .90' D:.060' ON WELL; FOUND SEAT TRACK TO BE OUT LIMITS PMay 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070352642Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK LBL45 BS380; 473 WL208.<[01] VERIFIED APPLICABILITY FOR 737-700 SRM 53-00-52-1A-1.<BR>REMOVED CORROSION FROM PASSENGER CABIN SEAT TRACK AT LBL 45 WL 208 BS 380 L: 1' W: .90' D:.050' ON WELL; FOUND SEAT TRACK TO BE OUT LIMay 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062952125Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL WITH BMS4-23 TYPE II LOT 1525675-1 AND BMS5-107 CLASS 1 LOT AK2KP8383K-1 RESIN; CURED RESIN UNDER A HEAT LAMP USING THERMOMEMay 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062952126Floor Panel · pulledFLOOR PANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL WITH BMS4-23 TYPE II LOT 1525675-1 AND BMS5-107 CLASS 1 LOT AK2KP8383K-1 RESIN; CURED RESIN UNDER A HEAT LAMP USING THERMOMEMay 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062952127Floor Panel · pulledFLOOR PANEL 242BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 242BF FLOOR PANEL FROM BMS4-17 TYPE 6 LOT#1526676-1; LOCATED AND INSTALLED INSERTS USING BMS5-107 LOT#AK2KP8383K-1 AND CURED USING HEAT LAMP AND THERMOMETER AMay 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Floor Panel
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