N961WN

Service difficulty reports · 187

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 = 'N961WN' 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 SWAA2023060244173Rib · crackedR/H HORIZ STAB L/E 341B AS A CRACKED RIB AT L/E STA 151.75 (MARKED)<[01] NDI HFEC VERIFY RIB IS CRACKED AT R/H HORIZ STAB LE STA 151.75 IAW SRM 51-10-02-0G-0;[02] HFEC INSPECTED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>CRACK NOTED WITHIN INSPECTION AMay 1, 2023 · N961WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2023060143738Frame · crackedSTA 312 FRAME CRACKED IN RADIUS AT FED HEADER SUPPORT.<[01] ACCOMPLISED REPAIR PER EA#M-22-153-01244 ON FAULT#TTG8Q00KVLNJ;[02] 'EA-GENERAL' REPAIR REFERENCE IS SELECTED PER EA#M-22-153-01244 STEP 10;[03] VERIFIED CORRECTIVE ACTION 1 AND 2<BR><BR>VERIFIED MEASMay 1, 2023 · N961WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2023060143737Panel · crackedBREAK BEAM CRACKED IN RADIUS; STA 540; LBL 1; WL 208.<[01] LOCATED AND DRILLED NEW PASSENGER CABIN BREAK PANEL BS 540 ; BL 0 TO LBL 25 WL 208 IAW SRM 51-40-05 AND DWG # 143A5240 ; OK TO INSTALL;[02] VERIFIED CORRECTIVE ACTION ITEM 1. OKAY TO INSTALL BREAK PANEMay 1, 2023 · N961WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023060144172Rib · crackedR/H HORIZ STABL/E 341BHAS A CRACKED RIB AT L/E STA 105.26 (MARKED)<[01] NDI HFEC VERIFY RIB IS CRACKED AT R/H HORIZ STAB LE STA 105.26 IAW SRM 51-10-02-0G-0;[02] HFEC INSPECTED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>CRACK NOTED WITHIN INSPECTION ARMay 1, 2023 · N961WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2023060143257Floor Panel · pulledFLOOR PANEL 231DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 231DF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1525675-1; LOCATED AND INSTALLED ALL INSERTS USING BMS5-107 LOT#AK2KP8383K-1 THEN CURED USING HEAT LAMP AND THERMOMEApr 29, 2023 · N961WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023060143258Floor Panel · pulledFLOOR PANEL 231EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231EF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #Apr 29, 2023 · N961WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023060143259Floor Panel · pulledFLOOR PANEL 231GF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 231GF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1525675-1; APPLIED TAPE AND INSTALLED INSERTS USING BMS5-107 LOT#AK2KP8383K-1 THEN CURED USING HEAT LAMPS AND THERMOApr 29, 2023 · N961WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023060143267Floor Panel · pulledFLOOR PANEL 231JF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 231JF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1525675-1; APPLIED TAPE AND INSTALLED INSERTS USING BMS5-107 LOT#AK2KP8383K-1 THEN CURED USING HEAT LAMPS AND THERMOApr 29, 2023 · N961WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023060143268Floor Panel · pulledFLOOR PANEL 231UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED NEW FLOOR PANEL 231UF OUT OF BMS 4-23 TY2 LOT#1525675-1. INSTALLED INSERTS USING BMS 5-107 LOT#AK2KP8383K-1 AND CURED UNDER HEAT LAMP USING THERMOMETER ID:ATS2208 DUE:10/23. PART MARKED Apr 29, 2023 · N961WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023060143271Floor Panel · pulledFLOOR PANEL 241KF UPPER SKIN HAS ARAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241KF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 5 TABLE 5. DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. DAMAGE TO FLOOR PANEL IS BEYOND ECONOMICAL RApr 29, 2023 · N961WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023060143262Floor Panel · pulledFLOOR PANEL 241SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 241SF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1525675-1; LOCATED AND INSTALLED ALL INSERTS USING BMS5-107 LOT#AK2KP8383K-1 AND CURED USING HEAT LAMP AND THERMOMETApr 29, 2023 · N961WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023060143263Floor Panel · pulledFLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 241UF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1525675-1; LOCATED AND INSTALLED ALL INSERTS USING BMS5-107 LOT#AK2KP8383K-1 AND CURED USING HEAT LAMP AND THERMOMETApr 29, 2023 · N961WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023060143264Floor Panel · pulledFLOOR PANEL 242MF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIGURE 5 TABLE 5 SECTION 46.UPPER SKIN STRAND DAMAGE EXCEEDS THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-50-1A-1. PARA 4. F. <BR>MULTIPLE AREAS OF STRAApr 29, 2023 · N961WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023060142663Floor Panel · crackedFWD FLOOR PANEL 221BF O/B TANG IS CRACKED.<[01] IDENTIFIED PANEL 221BF IAW SRM 53-00-50-0I-1 FIG 2; TABLE 2 FOUND CRACKE ALONG BOTH UPPER AND LOWER SKINS OF TANG TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4. F.<BR><BR>COMPLETELY REMOVED TANG; PREApr 28, 2023 · N961WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023060142675Floor Panel · pulledAFT FLOOR PANEL 241YF UPPER SKIN HAS AN AREA OF PULLED STRANDS.<[01] IDENTIFIED FLOORBOARD MATERIAL IAW SRM 53-00-50-0I-1 SHEET 1 FIG 6 TABLE 6<BR><BR>PANEL UPPER SKIN DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR 4.F.<BR><BR>PANEL SKIN DAApr 28, 2023 · N961WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023060142672Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL 241AAF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6. DAMAGE TO UPPER SURFACE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. FLOOR PANEL 241AAApr 28, 2023 · N961WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023060142677Skin · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 242UF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6.<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. <BR><BR>DAMAGE IS REPAIRABLE IAWApr 28, 2023 · N961WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023060143253Support · corrodedMULTIPLE AREAS OF CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727+5-807 WL 155-157.<[01] VERIFIED APPLICABILITY SRM 53-60-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.<BR><BR>REMOVED CORROSION ON AFT CARGO BAY FLOApr 28, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023060143254Support · corrodedMULTIPLE AREAS OF CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727C-767 WL 154-155.<[01] VERIFIED APPLICABILITY SRM 53-60-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2.<BR><BR>REMOVED CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORTApr 28, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023060143255Shield · corrodedMULTIPLE AREAS OF CORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 21 BS 767-787+5 WL 155.<[01] NO ALLOWABLE DAMAGE LIMITS IN SRM. REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARAGRAPH # 9;[02] VERIFIED CORRECTION ACTION ITEM 1.;[03] RECEIVED NEW SHIELD PApr 28, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023060143256Threshold · corrodedMULTIPLE AREAS OF CORROSION ON AFT CARGO BAY THRESHOLD AT RBL 21-27 BS 787+8-847 WL 156.<[01] VERIFIED APLICABILITY FOR IDENTIFICATION<BR>IAW SRM 53-60-15-01-1<BR>AND SRM 53-60-15-1A-1 FOR ALLOWABLE DAMAGE<BR><BR>REMOVED CORROSION ON AFT CARGO BAY THRESHOLD<BRApr 28, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023060142649Intercostal · crackedCRACK ON PASSENGER CABIN INTERCOSTAL AT BL 0 BS 277+8 WL 208.<[01] REMOVED INTERCOSTAL PER SRM 51-40-05 LOCATED AND DRILLED NEW P/N 141A5410U3AAR PER DWG #141A5410-3 OK TO INSTALL;[02] VERIFIED CORRECTIVE ACTION ITEM 1; OK TO INSTALL.;[03] PARTIAL INSTALLED INApr 27, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023060142650Fitting · corrodedCORROSION ON PASSENGER CABIN L/H FITTING AT LBL 59 BS 344 WL 208.<[01] FOUND NO ALLOWABLE LIMITS ON IAW SRM 53-10-15-1A-1;[02] FOUND NO ALLOWABLE LIMITS ON IAW SRM 53-10-51-1A-1;[03] REMOVED FITTING PER B737-700 SRM 51-40-02;[04] VERIFIED CORRECTIVE ACTION ITEApr 27, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023060142658Strap · corrodedCORROSION ON PASSENGER CABIN FLOOR STRAP AT RBL 18 BS 1016+12 WL 208.<[01] REMOVED CORROSION ON FLOOR STRAP IAW SRM 51-10-02-0G-0; MEASURES L=1.020'' X W=0.825'' ORIGINAL THICKNESS=0.050'' PER DWG# 147A5744; TOOL USED CALIPER ID: ATS2739 S/N:A22004232 DUE DATEApr 27, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023060241688Panel · crackedRT WING L/E PANEL 621PB FWD CORNER IS CRACKED (MARKED)<[01] IDENTIFIED PANEL 621PB IAW SRM 57-41-01-0I-4 FIGURE 3 TABLE 3 ITEM 1.<BR>DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A(5).<BR>DAMAGE TO BE REPAIRED IAW SRM 51-70-05-2R-6 PEApr 26, 2023 · N961WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2023060141783Bracket · corrodedROW 44 ADAPTOR RING AFT GROUND BRACKET CORRODED<[01] REPLACED GROUND BRACKET ON ADAPTER RING; PER SRM 5214-010.;[02] VERIFIED CORRECTIVE ACTION 1;[03] CORRECTED TABLE;[04] VERIFIED MEASUREMENTS TABLE.Apr 26, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023060145130Vapor Barrier · crackedLH VAPOR BARRIER PERVIOUS REPAIR IS CRACKED AT BODY STATION 666 FROM WL20 TO WL 24. LH VAPOR BARRIER PERVIOUS REPAIR IS CRACKED AT BODY STATION 663 FROM WL20 TO WL 24.<[01] IDENTIFIED PART AND MATERIAL IAW SRM 57-10-10-0I-2; FIGURES 1-2; TABLE 2; ITEM [4].<BR>Apr 24, 2023 · N961WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2023060131155Door · out of adjustL1 DOOR REQUIRES ADJUSTMENT.<[01] FED ADJUSTMENT ACCOMPLISHED ON TC# TTG8Q00KN6UM STEP 2.;[02] VERIFIED. TASK CARD COMPLETE.Apr 24, 2023 · N961WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2022120577995Bottle · low pressureAFT SERVICE DOOR SLIDE NOT IN GREEN BAND, REMOVED AND REPLACED ESCAPE SLIDE PER AMM 25-66-01.Dec 2, 2022 · N961WN · Boeing 7377H4 · Escape SlideSDR SWAA2022091352331None · damagedAFT RT EMERGENCY EXIT SIGN DAMAGED / [01] REMOVED AND REPLACED AFT RT EMERGENCY EXIT SIGN PER AMM 33-51-03Sep 12, 2022 · N961WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022072832001Battery Pack · inoperativeEMERGENCY LIGHT BATT PACK M1675 AT FWD LEFT CABIN IS WEAK/INOP / [01] REPLACED M1675 FWD LEFT SIDE BATTERY PACK IAW AMM 33-51-06-960-805. TESTS GOOD;[02] VERIFIED STEP 1; OPS CHECKED PASSED; JOB COMPLETE; AUDIT C/WJul 21, 2022 · N961WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022072930833Barrier · crackedLOWER RIGHT VAPOR BARRIER CRACKED ON OUTBOARD END. / [01] EVALUATED RIGHT VAPOR BARRIER AND FOUND 3EA CRACKS AT RBL 45;57&72. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 57-10-10-2R-2 PAR 1A& NOTE REV76. CLEAN AND PREP. IAW B737-700 SRM 51-70-04-2R-10 PAR4A-C REVJul 18, 2022 · N961WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2022072928612Angle · crackedDOT#04-186 LH A/C BAY STA 663 UPPER AFT ANGLE CRACKED AT FASTANER LBL 9 WL 172 / [01] REMOVED DAMAGED SECTION PER B737 SRM 57-10-10-2R-5;[02] RECEIVED -1 REPLACEMENT ANGLE FROM BACKSHOP ON WORK ORDER 43976-000-0001 AND -2 SPLICE ANGLE ON WORK ORDER 43976-000-0Jul 13, 2022 · N961WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2022072929764Barrier · deterioratedCUSTOMER REQUEST: RIGHT HAND VAPOR BARRIER HAS DETERIORATED REPAIR / [01] VERIFIED FSBRICATION OF VAPOR BARRIER IN BACK SHOP ON N/R 43976/0000/0005 I.A.W BOEING DWG 111A4111 REV:B;[02] VERIFIED STEP 1; VERIFIED FABRICATION OF VAPOR BARRIER IN BACK SHOP ON N/R Jul 12, 2022 · N961WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2022072928242Web · crackedLEFT HAND 663 VAPOR BARRIER WEB IS CRACKED AT LBL 30 / [01] EVALUATED DAMAGE; LEFT HAND VAPOR BARRIER WEB IS REPAIRABLE IAW B737 SRM 57-10-10-2R-2.<BR><BR>CLEANED AND PREPPED AREA IAW B737 SRM 51-70-04-2R-10 PAR 4 STEPS A;B; AND C. <BR><BR>VERIFIED REPAIR MATEJul 12, 2022 · N961WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2022051707807Light · inoperativeEMERGENCY LIGHT AFTY OF L-1 DOOR INOP / [01] RELAMPED OPS CHK GOODMay 13, 2022 · N961WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022042696992Light · inoperativeR1 DOOR EMERGENCY LIGHT INOP. / [01] RELAMPED R1 DOOR EXTERNAL EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD AT THIS TIME.Apr 23, 2022 · N961WN · Boeing 737 · Emergency LightingSDR SWAA2021070288372Engine · sparksPASSENGERS REPORTED FLAMES/SPARKS IN REAR RIGHT ENGINE AND A POPPING NOISE ON TAKE OFF. NO REPORTED SMOKE IN CABIN. NO ABNORMAL ENGINE INDICATION. NO OVERHEAT OR FIRE INDICATION IN COCKPIT. BWI FIRE ; RESCUE REPORTED NORMAL ENGINE TEMPERATURES BOTH FRONT AND RJun 28, 2021 · N961WN · Boeing 7377H4 · Engine (Turbine/Turboprop)SDR SWAA2021062985352Megaphone · faultedAFT MEGAPHONE NEEDS REPLACEMENT ; / [01] REMOVED AND REPLACED AFT MEGAPHONE; REPLACED BATTERIES AND INSTALLED NEW INSPECTION PLACARD WITH CURRENT DATE AND NEW INSPECTION DATE PER AMM 25-64-00; OPS CK. GOOD; [02] INSPECTED PERFORMED WORKJun 17, 2021 · N961WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2021062988712Battery · faultyAFT MEGAPHONE NEEDS REPLACEMENT ; / [01] REMOVED AND REPLACED AFT MEGAPHONE; REPLACED BATTERIES AND INSTALLED NEW INSPECTION PLACARD WITH CURRENT DATE AND NEW INSPECTION DATE PER AMM 25-64-00; OPS CK. GOOD; [02] INSPECTED PERFORMED WORKJun 17, 2021 · N961WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2021061582681Scuff Plate · crackedAFT CARGO FWD CORNER SCUFF PLATE IS CRACKED ; / LOCATED HOLES ON NEW CORNER SCUFF PLATE PER SRM 51-40-02.; INSPECTED PERFORMED WORK; REMOVED AND REPLACED FWD CORNER SCUFF PLATE PER SRM 51-10-02;AND SRM 51-40-02. INSPECTED PERFORMED WORK REMOVED AND REPLACED FJun 11, 2021 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021062982678Cap · corrodedAFT CARGO #2 RH FLOOR CAP STRIP CORRODED. / [01] REMOVED AND REPLACED FLOOR CAP STRIP PER AFT CARGO CORROSION PROTECTION TASK CARD 5360-E-16462 <BR>NG; TTG8Q004CF1E. PN 453A2611-11.; [02] INSPECTED PERFORMED WORKJun 10, 2021 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021061781251Light · deterioratedPHOTO LUMINESCENT STRIPS AT L/H STA 342 -376 & R/H STA 328-346 ARE DETERIORATED AND UNSERVICEABLE. ; / THE PHOTO LUMINESCENT STRIPS TO BE REPLACED ON TASK CARD TTG8Q002RAAG.; CORRECTIVE ACTION IN LINE 1 IS WRITTEN IN ERROR. THE PHOTO LUMINESCENT STRIPS TO BE RJun 8, 2021 · N961WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021061681250Light · deterioratedPHOTO LUMINESCENT STRIPS BOTH L/H & R/H STA 520 -737B ARE DETERIORATED AND UNSERVICEABLE. INSTALLED PER TASK CARD 733-080-00-01. TTG8Q002RA7H;INSTALLED PER TASK CARD 733-080-00-01. TTG8Q002RA7H. C/W INSPECTION.Jun 8, 2021 · N961WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021062978475Cargo Track · corrodedFORWARD CARGO AFT BULKHEAD R/H RAIL HAS CORROSION AROUND SEVERAL FASTENER HOLES. ; / [01] LOCATED NEW PART; DRILLED HOLES PER SRM 51-40-02 .; [02] FWD CARGO AFT BULKHEAD R/H RAIL P/N # 143A9485Y34 ; WILL BE INSTALL ON TASK # TTG8Q0049ACU .; [03] FWD CARGO AFT May 28, 2021 · N961WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021062978474Cargo Track · corrodedFORWARD CARGO AFT BULKHEAD L/H RAIL HAS CORROSION AROUND SEVERAL FASTENER HOLES. ; / [01] LOCATED DRILLED HOLES ON NEW BULKHEAD RAIL PER SRM 51-40-02 .; [02] BULKHEAD RAIL P/N # 143A9485U30 . WILL BE INSTALL ON TASK # TTG8Q0049ACU .; [03] REPLACED PART PER SRMMay 28, 2021 · N961WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021062975871Shield · corrodedAFT CARGO; R/H TRANSITION ANGLE STA 770; RBL 23 CORRODED ON UPPER SURFACE (ORIGINAL FAULT TTG8Q00541UD SIGNED OFF IN ERROR) ; / [01] REMOVED DAMAGE; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [02] REMOVED AND REPLACED SHIELD PER SRM 51-40-02.; [03] INSPMay 22, 2021 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021061675112Angle · corrodedCORROSION; AFT CARGO COMPARTMENT R/H TRANSITION ANGLE HAS NUT PLATE HOLE CORROSION STA. 727E+2'; RBL 22'. ; / FOUND DAMAGE TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;REMOVED AND REPLACED TRANSITION ANGLE FROM STA 727+4 TO STA 767 RBL 23 PER SRM 51-40-02.;REMOVMay 20, 2021 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021062975077Angle · corrodedAFT CARGO; L/H TRANSITION ANGLE STA 844; LBL 23 CORRODED ON UPPER SURFACE ; / [01] REMOVED DAMAGE AND FOUND IT TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [02] REMOVED ZEE-ASSY. FROM PARTS INFORMATION.; [03] INSTALLED NEW TRANSITION ANGLE PART # 146A7502-51 FRMay 19, 2021 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021062975075Angle · corrodedAFT CARGO; R/H TRANSITION ANGLE STA 782; RBL 23 CORRODED ON UPPER SURFACE ; / [01] TRANSITION ANGLE FROM STA 727+4 TO STA 867; WILL BE REMOVED AND REPLACED DUE TO OUT OF LIMITS DAMAGE REF FAULT BARCODE (TTG8Q005441X).; [02] TRANSITION ANGLE FROM STA 727+4 TO SMay 19, 2021 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
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