N960WN

Service difficulty reports · 180

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 = 'N960WN' 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 SWAA2023062952128Floor Panel · pulledFLOOR PANEL 241LF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL FROM BMS4-23 TYPE II LOT 1525675-1; DETERMINED INSERT HOLE LOCATIONS; UPSIZED INSERTS HOLES INSTALLED INSERTS WITH BMS5-107 May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062952129Floor Panel · pulledFLOOR PANEL 241MF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL FROM BMS4-17 TYPE VI LOT 1526676-1; DETERMINED INSERT HOLE LOCATIONS; UPSIZED INSERTS HOLES INSTALLED INSERTS WITH BMS5-107 May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062952130Floor Panel · pulledFLOOR PANEL 241PF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL FROM BMS4-17 TYPE VI LOT 1526676-1; DETERMINED INSERT HOLE LOCATIONS; UPSIZED INSERTS HOLES INSTALLED INSERTS WITH BMS5-107 May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062952131Floor Panel · pulledFLOOR PANEL 241RF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241RF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 5 TABLE 5. MOST OF THE UPPER SURFACE HAS LARGE AREAS OF PULLED STRANDS OR DELAMINATION. AREAS EXCEED ALLOWABLE DAMAGE LIMITS 53-00May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062952121Floor Panel · pulledFLOOR PANEL 241SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241SF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 5 TABLE 5. MOST OF THE UPPER SURFACE HAS LARGE AREAS OF PULLED STRANDS OR DELAMINATION. AREAS EXCEED ALLOWABLE DAMAGE LIMITS 53-00May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062952122Floor Panel · pulledFLOOR PANEL 241TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241TF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 5 TABLE 5. MOST OF THE UPPER SURFACE HAS LARGE AREAS OF PULLED STRANDS OR DELAMINATION. AREAS EXCEED ALLOWABLE DAMAGE LIMITS 53-00May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062952123Floor Panel · pulledFLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 241UF 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 PanelSDR SWAA2023062952132Floor Panel · pulledFLOOR PANEL 241VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 241VF 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 PanelSDR SWAA2023062952133Floor Panel · pulledFLOOR PANEL 242NF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 242NF 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 PanelSDR SWAA2023062952134Floor Panel · pulledFLOOR PANEL 242QF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 242QF 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 PanelSDR SWAA2023062952629Stringer · crackedAFT AREA OF FWD CARGO BAY STR 25 IS CRACKED AT AFT FASTENER ; RBL 29<[01] EVALUATED CRACK MEASUREMENTS ON FCB STRINGER 25R BS 539 DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103 DETAIL A;[02] VERIFIED APPLICABILITY FOR STR 25R IAW SRM 53-00-03-2R-1 FMay 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023062952630Stringer · crackedAFT AREA OF FWD CARGO BAY STR 26 IS CRACKED AT AFT FASTENER; LBL 25<[01] EVALUATED CRACK MEASUREMENTS ON FCB STRINGER 26L BS 539 DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103 DETAIL A;10] LOCATED AND DRILLED REPLACEMENT STRINGER SECTION AND HAT SECMay 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023062952636Attach Angle · crackedFWD CARGO BAY INTERCOASTAL ATTACH ANGLE IS CRACKED BS 440; LBL28; WL 154<[01] REMOVED FWD CARGO BAY INTERCOASTAL ATTACH ANGLE BS 440 LBL28 WL154. LOCATED AND DRILLED NEW ANGLE P/N 143A7502U155 LOT: 1519478-4 PO: 907139/4. IAW SRM 51-40-02-0G-0; SRM 51-30-01-0GMay 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2023062952137Intercostal · crackedCRACKED INTERCOSTAL AT STA 277+7 & 277+13.5; WL 208; RBL 1.<[01] REMOVED INTERCOSTAL FOR REPLACED BS 277 TO 794 WL 208 RBL 1.<BR>IAW SRM 51-40-02-0G-0;[02] LOCATED IN DRILLED NEW INTERCOSTAL BS 277 TO 294 W2L 208 RBL 1. IAW SRM 51-40-05-0G-0 <BR>OK TI INSTALL;May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062952632Attach Angle · crackedPASSENGER CABIN FSD FWD LOWER ATTACH ANGLE BS292 RBL 54 WL 208 CRACKED<[01] REMOVED FSD FWD LOWER ATTACH ANGLE IAW SRM 51-40-02;[02] CERTIFY;[03] PASSENGER CABIN FSD LOWER ATTACH ANGLE TO BE OUT LIMITS PER SRM 51-10-02. RECEIVED NEW ANGLE FROM TOOL ROOM P/N 14May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2023062952633Web · crackedPASSENGER CABIN FED FWD WEB BS294.5 STR 15 CRACKED<[01] UPDATED MEASUREMENT TABLE;[02] FOUND FED FWD WEB BS294.5 STR 15 CRACK TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS AVAILABLE;[03] REMOVED STRAP AT BS 294+1-303+2 STR 15 L/H ; AND ATTACHING CLIP AT BS294May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062952644Frame · crackedPASSENGER CABIN FED UPPER FRAME BS 312 STR 5L CRACKED<[01] COMPLETE MEASUREMENT TABLE;[02] VERIFIED MEASUREMENT TABLE;[03] REPAIRED ON FAULT TTG8Q00L9MWU;[04] VERIFIED CORRECTIVE ACTION 3May 25, 2023 · N960WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2023062951868Floor Panel · brokenAFT CABIN FLOOR PANEL 241ADF HAS A BROKEN AFT O/B CORNER<[01] IDENTIFIED PANEL IAW SRM 53-00-50-0I-1 FIGURE 6. DAMAGE TO THE PANEL IS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.B AND WILL BE REPAIRED IAW SRM 53-00-50-2R-4. REMOVED AN APPROX. 1.7May 24, 2023 · N960WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062952120Channel · crackedFWD ENTRY DOOR MOP SILL IS CRACKED AT B.S. 303; LBL 55; WL 207<[01] REMOVED FWD ENTRY DOOR MOP SILL IS CRACKED AT B.S. 277 - 360; LBL 55; WL 207;[02] RECEIVED FROM TOOL ROOM NEW FED MOPSILL P/N 141A8112-1.<BR>LOCATED; DRILLED AND COUNTERSUNK NEW FED MOPSILL IAMay 24, 2023 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070351428Frame · broken#1 ENGINE I/B FAN COWL OIL ACCESS DOOR CLOSE OUT SHIELD FRAME IS BROKEN.<[01] REMOVED #1 ENGINE I/B FAN COWL OIL ACCESS DOOR CLOSE OUT SHIEL FRAME PER SRM 51-40-02-0G-0 4. E. FIG.8 AND 5. C. (1) FIG.10;[02] REPLACED NEW #1 ENGINE I/B FAN COWL OIL ACCESS DOOR CMay 23, 2023 · N960WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous StructureSDR SWAA2023062950997Panel · delaminatedPANEL 194FR HAS A DELAMINATION ON THE OUTER SKIN (MARKED)<[01] IDENTIFIED PANEL IAW SRM 53-60-70-0I-1 FIGURE 2 ITEM [2] DAMAGE TO THE PANEL IS BEYOND ALLOWABLE LIMITS IAW SRM 53-60-70-1A-1 PARAGRAPH 4.A.(6).(B) AND WILL BE REPAIRED IAW SRM 51-70-05-2R-2 PER SRMay 22, 2023 · N960WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2023042429612Light · inoperativeCREW REPORTS R/H EMERG EXIT SIDEWALL WINDOW LIGHT INOP.<[01] OK TO CONTINUE PER MEL 33-2-03; SP-1B.;[02] REMOVED AND REPLACED BOTH LAMP AND FUSE IAW AMM 33-51-01; NO HELP. ATTEMPTED TO REPLACE BALLAST FOUND TRIM STUD ROUNDED OUT; UNABLE TO REMOVE NUT.;[03] REPApr 20, 2023 · N960WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023040621139Panel · crackedRH WING LOWER PANEL 651CB IS CRACKED; AFT INBOARD SIDE NEAR NUT PLATE.<[01] R&R RH WING OWNER PANEL 651CB PER AMM 32-11-00Mar 27, 2023 · N960WN · Boeing 7377H4 · Wing, Control SurfacesSDR SWAA2023033020926Bracket · brokenAFT SUPPORT BRACKET AT 194BR BROKEN<[01] REPLACED THE AFT SUPPORT BRACKET UNDER PANEL 194BR PER SRM 51-40-02.Mar 25, 2023 · N960WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2023033020927Bracket · brokenFWD SUPPORT BRACKET AT 194BR BROKEN<[01] REPLACED THE FWD SUPPORT BRACKET UNDER 194BR PER SRM 51-40-02.Mar 25, 2023 · N960WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2023022003867Floor Panel · deterioratedFWD. CARGO COMPARTMENT; THE AFT CARGO FLOOR BOARD IS COMING APART<[01] REMOVED AND REPLACED FWD. CARGO COMPARTMENT; THE AFT CARGO FLOOR PANEL PER AMM 25-52-10.Feb 17, 2023 · N960WN · Boeing 7377H4 · Cargo CompartmentsSDR SWAA2022112875635Slide · out of adjustFORWARD PASSENGER DOOR SLIDE INDICATING IN RED ARCH / [01] REMOVED SLIDE PER MT725-61-06;[02] REMOVED AND REPLACED FWD ENTRY SLIDE PER MT 725-61-06.Nov 26, 2022 · N960WN · Boeing 7377H4 · Escape SlideSDR SWAA2022110166753Slide · out of limitsAFT SERVICE DOOR SLIDE GAUGE OUT OF LIMITS / [01] R&RD AFT SERVICE DOOR SLIDE IAW MT 725-61-06Nov 1, 2022 · N960WN · Boeing 7377H4 · Escape SlideSDR SWAA2022101157950None · faultyCEILING LIGHT ROW 1 INOP CAPTAINS SIDE. RELAMPED ROW 1 RECESSED CEILING LIGHT PER AMM 33-22-00.Oct 9, 2022 · N960WN · Boeing 7377H4 · Passenger Compartment LightingSDR SWAA2022090850503Battery Pack · inoperativeFWD SERVICE DOOR TOP EMERGENCY LIGHT INOP AND OUTSIDE EMERGENCY LIGHT INOP / [01] R&R FWD RH BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD AT THIS TIME.Sep 6, 2022 · N960WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022072531041Fastener · looseFWD SERVICE DOOR GIRT BAR RETAINING HOOK LOOSE. / [01] R & R?D FASTNER ON RETAINING CLIP PER SRM 51-40-02<BR>AND C/W MT 725-61-06-FSJul 19, 2022 · N960WN · Boeing 7377H4 · Escape SlideSDR SWAA2022051707392Battery Pack · inoperative1 EMER FLASHLIGHT INOP @ AFT F/A STATION / [01] R & R?D AFT GALLEY BOTH FLASH LIGHTS BATTERY PACK PER AMM 25-64-00.May 13, 2022 · N960WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2022040791279Slide · out of positionFWD ENTRY DOOR SLIDE CAME OUT OF CASE SLIDE DID NOT DEPLOY / [01] REMOVED AND REPLACED L! DOOR ESCAPE SLIDE PER AMM 25=66-01.Apr 4, 2022 · N960WN · Boeing 7377H4 · Escape SlideSDR SWAA2022021169870Light · inoperativeMOST AFT R/H SIDE EXTERIOR EMERGENCY LIGHT INOP. ; / [01] RE-LAMPED THE AFT SERVICE DOOR EXTERIOR SLIDE EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.Feb 7, 2022 · N960WN · Boeing 737* · Emergency LightingSDR SWAA2021081104919Slide · low pressureFWD SERVICE DOOR SLIDE PRESSURE IS LOW. ; / [01] REMOVED AND REPLACED FWD SERVICE ESCAPE SLIDE IAW MT 725-61-06 WORK ACCOMPLISHED ON W/O TTG8Q0062YY1 AND TTG8Q0062YXBAug 7, 2021 · N960WN · Boeing 7377H4 · Escape SlideSDR SWAA2021061481237Skin · gougedFUSELAGE SKIN GOUGED AT BS 847 - BS 852; 4IN BELOW STR 20R; WL 177 / ENTERED CALIBRATION INFO; APPLIED TOP FINISH TO REPAIR AREA. IAW AMM 51-21-00-100-801; VERIFIED APPLIED TOP FINISH TO REPAIR AREA. IAW AMM 51-21-00-100-801 <BR><BR>CARD COMPLETEJun 8, 2021 · N960WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021061480407Bulb · burned outLH EMERGENCY EXIT SIDEWALL LIGHT HAS BURNT OUT BULBS ; / RELAMPED AND PERFORMED A GOOD INSTALLATION TEST OF THE LH EMERGENCY EXIT DOORS EXIT LIGHT PER AMM 33-51-01-960-801; VERIFIED RELAMPED AND PERFORMED A GOOD INSTALLATION TEST OF THE LH EMERGENCY EXIT DOORSJun 3, 2021 · N960WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021061480406Bulb · inoperativeAFT ENTRY DOOR SLIDE LIGHT INOP ; / REMOVED AND REPLACED BULB AND PREFORMED GOOD OP CHECK OF SLIDE/OVERWING LIGHT AS PER AMM 33-51-04-960-801; VERIFIED BULB REPLACEMENT AND OPS CHECK PER AMM.Jun 3, 2021 · N960WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021061478459Support · corrodedAFT CARGO BAY RH AFT BULKHEAD SUPPORT CORRODED. LOWER SURFACE. BS947; RBL23; WL182 ; ADDITIONAL CORROSION FOUND DURING INSPECTION FOR OK TO INSTALL CENTER BULKHEAD SUPPORT. / NO SRM ALLOWABLE DAMAGE FOUND; PN# 149A8118-29 REPAIRED BY REPLACEMENT OF THE PART - May 29, 2021 · N960WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2021061478456Seal · crackedL/H HORIZ STAB UPPER FWD SLIDE SEAL IS CRACKED ; / CERTIFIED; VERIFIED INSTALLATION OF SLIDE SEAL IAW AMM 53-31-31; SRM 51-40-02.; PERVIOUS TO INSTALLING HARDWARE REMOVED UPPER L/H SLIDE SEAL IAW M/M 53-31-31-000-802May 28, 2021 · N960WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2021061478458Gusset · crackedGUSSET CRACKED AT STR19 L/H BS500D WL170 / VERIFIED LOCATING AND DRILLING OF NEW GUSSET IAW SRM 51-40-05; DWG 143A7902. OK TO INSTALL.; INSTALLED GUSSET AT B/S 500D STR 19 L/H LO# 1457203-12 IAW SRM 51-40-02 AND DWG 143A7902 REV:-; VERIFIED INSTALLATINO OF GUSMay 28, 2021 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021061478457Gusset · crackedGUSSET CRACKED AT STRINGER 19 R/H BS500D 154 ; GUSSET CRACKED AT STRINGER 19 R/H BS500D WL170 / INSTALLED GUSSET AT B/S 500D STR 19 R/H LOT#1453293-4 IAW SRM 51-40-05 AND DWG 143A7902 REV:-; REFERENCE ADDED FOR INSTALLATION PER SRM 51-40-02; VERIFIED INSTALLATMay 28, 2021 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021061477090Baffle · crackedFWD CARGO BAY BAFFLE CRACKED BS 500A-500B LBL21 WL157 / VERIFIED INSTALLATION OF BAFFLE AND REPAIR SPLICE PER DWG 143A7505 AND SRM 53-30-53-2R-1; RE-VERIFIED INSTALLATION OF BAFFLE AND REPAIR SPLICE PER DWG 143A7505 AND SRM 53-30-53-2R-1.; RE-VERIFIED INSTALLAMay 25, 2021 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021061476238Baffle · damagedFWD CARGO BAY BAFFLE DAMAGED AT FASTENER HOLE BS 500 - BS 500A LBL 22 WL 157 ; / VERIFIED LOCATED HOLES AND DRILLED PER SRM 51-40-05. OK TO INSTALL; INSTALLED FCB BAFFLE BS 500- BS 500A; LBL 22; WL 157 IAW BOEING DWG 143A7505; BOEING DWG 143A1212 AND SRM 51-40May 23, 2021 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021061475858Baffle · crackedFWD CARGO BAY BAFFLE CRACKED BS 400- BS 420 LBL 21 WL 157 ; / INSTALLED FCB BAFFLE BS 400-420; LBL 21; WL 157 PER SRM 51-40-02-0G-0; DWG# 143A7505.; VERIFIED BAFFLE INSTALLATION; BS 400-420; LBL 21; WL 157 PER SRM 51-40-02-0G-0; DWG# 143A7505; VERIFIED JOB IS May 22, 2021 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021061475563Support · corrodedCORROSION ON FORWARD CARGO BAY AFT R/H BULKHEAD SUPPORT BS 500D RBL 28 WL 154 ; / UPDATED MEASUREMENT TABLE; VERIFIED; VERIFIED CARD COMPLETE.May 21, 2021 · N960WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2021061475557Support · crackedFWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT CRACKED AT FASTENER HOLE BS 500A LBL 21 WL 157 ; / VERIFIED APPLIED PRIMER ON FLOOR TO SIDEWALL SUPPORT AND SPLICE ANGLE PER AMM 51-21-72-370-801.; INSTALLED FLOOR TO SIDEWALL SUPPORT SPLICE ANGLE PER SRM 53-00-53-2RMay 20, 2021 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021061474626Floor Panel · damagedPASSENGER CABIN FLOOR PANEL; 232SF; IS DAMAGED ON UPPER SURFACE AT AFT END. ; / DUE TO EXTENT OF DAMAGE TO FLOOR PANEL 232SF; FABRICATED NEW PANEL FROM BMS 4-23 TY.2 LOT#1456675-1; INSTALLED INSERTS WITH BMS 5-107 LOT#AK0DP4051K; CURED USING THERMOMETER ID ATSMay 18, 2021 · N960WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021061474206Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK AT B.S. 706+2 - 706+8; R.B.L. 24.5; W.L. 208.1. ; / INDEPENDENT INSPECTION NOT REQUIRED; APPLIED CHEMICAL CONVERSION AND PRIMER PER SRM 53-00-52-1A-1 STEP 2 B. (1) (2); VERIFIED APPLICATION OF CHEMICAL CONVERSION AND PRIMay 17, 2021 · N960WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021061474204Floorbeam · crackedCRACKED FLOOR SUPPORT AT B.S. 540; B.L. 0 - R. B.L. 24.5; W.L. 208.1. ; / VERIFIED ALL STEPS FOR COMPLETION.; VERIFIED COMPLETE; 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT). 1. AARON BARBOSA (TECHNICIAN), 22-MAY-20May 17, 2021 · N960WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
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