N444WN

Service difficulty reports · 336

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 = 'N444WN' 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 SWAA2023081459859Rib · crackedL/H HORIZONTAL STABILIZER FRONT SPAR L/E MOVEABLE FAIRING 331B INB INTERNAL RIB # 1 CRACKED RADIUS MKD DOT<[01] REMOVED L/H HORIZ STABILIZER RIB ASSY LE STA 78.29 AS PER B737-700 SRM 51-40-02-0G-0.;[02] REMOVED CRACKED CHORD FROM LH HORIZ RIB ASSY LE 78.29 AS Jun 16, 2023 · N444WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2023081459832Stiffener · crackedAFT CARGO FWD BULKHEAD STA 727 RBL 10 STIFFENER CRACK.<[01] ACCOMPLISHED EA 23-153-02252;[02] CERTIFIED JOB STEPS ACCOMPLISHED PER EA 23-153-02252.Jun 16, 2023 · N444WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2023081459845Bracket · crackedAFT CARGO COMPARTMENT FWD BULKHEAD STA 727 LOWER CENTER POSITION BRACKET PANEL SUPPORT CRACK.<[01] REMOVE AND REPLACED AFT CARGO COMPARTMENT FWD BULKHEAD STA 727 LOWER CENTER POSITION BRACKET; REF B737 SRM 51-40-02-0G-0;[02] VERIFIED / INSPECTED NEW BRACKET ISJun 16, 2023 · N444WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2023081459838Channel · corrodedCORROSION FOUND AFT CARGO RH 'Z' CHANNEL AT STA 727B + 6 RBL 21 WL 155.5 HAS SPOT OF CORROSION.<[01] REPAIR WAS ACCOMPLISHED IN THE ITEM TTG8Q00LP0BE;[02] NOTE OF WORK TRANSFER TO ' TTG8Q00LP0BE : / TRANSFER OF WORK PEFORMED ALSO WILL CARRY OVER TO SAME ( TT #Jun 16, 2023 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023081459839Channel · corrodedCORROSION FOUND AFT CARGO RH 'Z' CHANNEL AT STA 727C + 2 RBL 21 WL 155.5 HAS SPOT OF CORROSION.<[01] REPAIR WAS ACCOMPLISHED IN THE ITEM TTG8Q00LP0BE;[02] TRANSFER OF WORK ; AS PER ENTRY #1 ' TTG8Q00LPOBE ' INSP. VERIFIED AS SUCH. THIS N/R IS NOW CLOSEDJun 16, 2023 · N444WN · Boeing 7377H4 · Fuselage Structure (General)SDR SWAA2023081459848Channel · corrodedCORROSION FOUND AFT CARGO RH 'Z' CHANNEL FROM STA 747 TO STA 767 RBL 21 WL 155.5 HAS SPOTS OF CORROSION.<[01] REPAIR WAS ACCOMPLISHED IN THE ITEM TTG8Q00LP0BE;[02] TRANSFER OF WORK ACCOMPLISHED ; AS PER ENTRY #1 ' TTG8Q00LPOBE ' DID PERFORM THE REPAIRE & INSTAJun 16, 2023 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023081459503Support Bracket · crackedFWD CARGO COMPARTMENT L/H FLOOR SUPPORT BRACKET CRACKED UNDER Z CHANNEL S-26L STA 500A MKD DOT<[01] REMOVED L/H FLOOR SUPPORT BRACKET AT FWD CARGO COMP UNDER Z CHANNEL S-26L STA 500A PER B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1;[03] REMOVED AND REPLACEJun 15, 2023 · N444WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2023081459504Support Bracket · crackedFWD CARGO COMPARTMENT L/H 2EA SUPPORT BRACKETS CRACKED @ S-26L STA 500C FWD & AFT OF SUPPORT FRAME MKD DOTS<[01] REMOVED L/H 2EA SUPPORT BRACKETS AT FWD CARGO COMP S-26L STA 500C FWD & AFT OF SUPPORT FRAME PER B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1;[Jun 15, 2023 · N444WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2023081459509Vapor Barrier · crackedLOWER FUSELAGE CENTER WING BULKHEAD R/H VAPOR BARRIER UPPER CHORD ATTACHED ANGLE CRACKED AT RBL 40 STA 663.75<[01] OK TO INSTALL NEW VAPOR BARRIER UPPER CHORD ATTACHED ANGLE.;[02] REMOVED; FABRICATED AND INSTALLED NEW R/H VAPOR BARRIER UPPER CHORD ATTACHED ANGJun 15, 2023 · N444WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2023081459510Vapor Barrier · crackedLOWER FUSELAGE CENTER WING BULKHEAD L/H VAPOR BARRIER UPPER CHORD ATTACHED ANGLE CRACKED @ LBL 5 STA 663.75 MKD DOT<[01] ACCOMPLISHED CAP SEAL AND FILLET SEAL ARROUND REPAIR EDGES AS PER B737-700 SRM 57-10-10-2R-5.;[02] REPAIRED L/H VAPOR BARRIER UPPER ATTACH Jun 15, 2023 · N444WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2023081459502Gusset · crackedFWD CARGO COMPARTMENT R/H SIDE WALL GUSSET CRACKED @ S-19R STA 500D<[01] REMOVED AND REPLACED R/H SIDE GUSSET AT STA 500D STR 19R PER B737-700 SRM 51-40-02-0G-0 AND DRAWING 143A7902;[02] VERIFIED 1.;[03] VERIFIED REMOVAL OF RH SIDE GUSSET ON STEP #1;[04] CERTIJun 15, 2023 · N444WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2023081459501Gusset · crackedFWD CARGO COMPARTMENT L/H SIDE WALL GUSSET CRACKED @ S-19L STA 500D<[01] COMPLETED INSTALLATION FWD CARGO COMP. LEFT SIDE GUSSET ASSY STA 500D STR 19L PER B737-700 SRM 51-40-02-0G-0 AND DRAWING 143A7902. (PERFORMED BY. E.G # 1184)Jun 15, 2023 · N444WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2023081459829Bracket · crackedR/W REAR SPAR T/E DEFLECTOR CONTROL RIB PANEL LOWER HORIZONTAL BULB SEAL RETAINER O/B END SUPPORT BRACKET CRACKED @ FASTENER'S TAIL MKD DOT<[01] REMOVED AS REPLACED CLIP PN 115A6260-2 AS PER B737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.Jun 15, 2023 · N444WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2023081459114Floor Panel · crackedMAIN CABIN CENTER AREA FLOOR PANEL 242CF TOP FIBERGLASS SKIN WITH CRACK APROX. 5'<[01] REPAIRED FLOOR PANEL #242CF AT DAMAGED AREA PER B737 SRM 53-00-50-2R-1 PARA 3.M. MATERIALS USED RESIN P/O#1783720; CLOTH P/O#1738579Jun 14, 2023 · N444WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023081458710Skin · crackedSLAT #3 ACTUATOR ATTACHMENT FASTENER HOLE CRACKED.<[01] REPAIRED SLAT #3 SKIN AT ACTUATOR AREA AS PER SRM 57-42-01-2R-8;[02] VERIFIED REPAIR OF SLAT #3 SKIN AT ACTUATOR.Jun 13, 2023 · N444WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2023081458532Bracket · crackedAFT ENTRY DOOR FWD SLIDE MOUNTING BRACKET SHOCK MOUNT CRACKED.<[01] REMOVED AND REPLACED AFT ENTRY DOOR FWD SLIDE MOUNTING BRACKET SHOCK MOUNT; REF SRM 51-40-02-0G-0;[02] VERIFIED AFT ENTRY DOOR FWD SLIDE MOUNTING BRACKET SHOCK MOUNT REPLACEMENT.Jun 12, 2023 · N444WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2023050141784Unknown · unknownINADVERTANT GEAR EXTENSION AT 260 KTS FOLLOWED BY IMMEDIATE GEAR RETRACTION AT 265 KTS<[01] C/W LANDING GEAR OPERATION ABOVE DESIGN SPEED COND INSP PER M/M 05-51-47. NO DEFECTS NOTEDApr 26, 2023 · N444WN · Boeing 7377H4 · Landing Gear SystemSDR SWAA2022091953027None · inoperativeRIGHT EMERGENCY OVER WING DOOR CABIN SIDE LIGHT INOP ( RELAMP NO HELP) / [01] OK TO CONTINUE PER MEL 33-2-03 SP1B<BR><BR>MDDR 89474;[02] R&R RIGHT EMERGENCY LIGHT BALLAST; OPS CHECK GOOD IAW AMM 33-21-00; AMM 25-21-20; AND SOPM 20-50-01.Sep 15, 2022 · N444WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022081541586Panel · delaminatedGENERAL VISUAL INSPECTION OF THE INTERIOR SURFACE OF THE 193B FAIRING PANEL REVEALS AREAS OF DELAMINATION; PRESENT ON THE FAIRING PANEL AT FASTENER LOCATIONS NUMBER 3; 5; 9; 19; 20; 34; 35; 36; 37; 38 / [01] DRILLED AND COUNTERSUNK HOLES ON NEW PANEL PER AMM 5Aug 14, 2022 · N444WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2022081140394Girt Bar · missingLEFT AFT GIRT BAR STOP RING MISSING / [01] REMOVED AND REPLACED LEFT AFT DIRT BAR STOP RING PER AMM 25-66-01.Aug 10, 2022 · N444WN · Boeing 7377H4 · Escape SlideSDR SWAA2022072833667Light · missingL1 DOOR LOWER EXIT SIGN MISSING DIRECTIONAL ARROW. / [01] REMOVED AND REPLACED L1 LOWER DOOR EXIT SIGN REF AMM 33-51-00;[02] INSPECTEDJul 26, 2022 · N444WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022071327495Frame · crackedREF. LP# 2334140; CRACK FOUND ON FWD EDGE OF GROUND POWER DOOR CUT OUT. CRACK IS .1875 LONG 3 FROM LOWER FWD DOOR CUT OUT RADIUS. / [01] REPAIRED DAMAGE PER SRM 53-10-15?1A-4 PARAGRAPH 2.;[02] C/W REPAIR PER SRM 53-10-15-1A-4 ;AND TSR 2022005407; AND EA 22-153Jul 9, 2022 · N444WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2022061618435Girt Bar · misinstalledFORWARD SERVICE DOOR GERT BAR DIFFICULT TO OPERATE / [01] FOUND GERT BAR IMPROPERLY INSTALLED; REINSTALLED GERT BAR PER AMM 25-66-01.Jun 14, 2022 · N444WN · Boeing 7377H4 · Escape SlideSDR SWAA2022022877144Battery Pack · inoperativeLT. OVERWING EMERGENCY EXIT EXTERIOR EMERGENCY LIGHT AND ASSOCIATED EMERGENCY LIGHTS POWERED BY EMERGENCY EXIT LIGHT BATTERY PACK M1668 INOP. / [01] REPLACED POWER SUPPLY M1668 BATTERY PACK IAW AMM 33-51-06.Feb 24, 2022 · N444WN · Boeing 737* · Emergency LightingSDR SWAA2022011059166Skin · crackedREF LOGPAGE 1731634 #5 CRACK LEFT UNDERWING PANEL #115A2720. REMOVED LEFT UNDERWING PANEL 115A2720 PER AMM 57-50-02.Jan 4, 2022 · N444WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2021110540214Slide · out of positionAFT SERVICE SLIDE OUT OF POSITION ; / [01] REPACK AFT SERVICE SLIDE PER AMM 25-66-01Nov 3, 2021 · N444WN · Boeing 7377H4 · Escape SlideSDR SWAA2021081807061Bulb · burned outFWD SERVICE DOOR EMERGENCY EXIT SIGN L1186 HAS BURNT OUT BULBS ; / [01] RELAMPED FWD SERVICE DOOR EMERGENCY EXIT SIGN L1186 AND PERFORMED A GOOD FUNCTIONAL TEST PER AMM 33-51-01-960-801; [02] VERIFIED CORRECTIVE ACTION 1 PER AMM 33-51-01-960-801Aug 13, 2021 · N444WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021081807062Bulb · burned outL/H OVERWING EMERGENCY EXIT SIGN L1365 HAS BURNT OUT BULBS ; / [01] RELAMPED L/H OVERWING EMERGENCY EXIT SIGN L1365 AND PERFORMED A GOOD FUNCTIONAL TEST PER AMM 33-51-01-960-801; [02] VERIFIED CORRECTIVE ACTION 1 PER AMM 33-51-01-960-801Aug 13, 2021 · N444WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021081807063Bulb · burned outR/H OVERWING EMERGENCY EXIT SIGN L751 HAS BURNT OUT BULBS. RELAMPED R/H OVERWING EMERGENCY EXIT SIGN L751 AND PERFORMED A GOOD FUNCTIONAL TEST PER AMM 33-51-01-960-801; [02] VERIFIED CORRECTIVE ACTION 1 PER AMM 33-51-01-960-801Aug 13, 2021 · N444WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021081804395Megaphone · inoperativeMEGAPHONE IN AFT L/H WINDSCREEN DOES NOT WORK. ; / [01] REPLACED AFT LT WINDSCREEN MEGAPHONE IAW MT 725-031-00-05Y MM25-64-00; [02] VERIFIED AFT MEGAPHONE REPLACEMENT PER MT 725-031-00-05Y MM25-64-00Aug 5, 2021 · N444WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2021081899983Retainer · corrodedCORROSION ON FWD GIRT BAR FITTING TIE DOWN BS312 LBL57 WL208 ; / [01] NO ALLOWABLE DAMAGE FOUND IN SRM. REPAIR WILL BE BY REPLACEMENT.; [02] NO ALLOWABLE DAMAGE FOUND IN SRM. REPAIR WILL BE BY REPLACEMENT.; [03] OK TO INSTALL.; [04] OK TO INSTALL FWD GIRT BAR Jul 30, 2021 · N444WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2021081899984Retainer · corrodedCORROSION ON AFT GIRT BAR FITTING TIE DOWN BS344 LBL61 WL208 ; / [01] NO ALLOWABLE DAMAGE FOUND IN SRM. REPAIR WILL BE BY REPLACEMENT.; [02] NO ALLOWABLE DAMAGE FOUND IN SRM. REPAIR WILL BE BY REPLACEMENT.; [03] OK TO INSTALL.; [04] OK TO INSTALL. AFT GIRT BARJul 30, 2021 · N444WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2021081899981Splice Strap · corrodedCORROSION AFT CARGO BAY ON FLOOR PANEL SPLICE BS887 RBL 10 TO LBL 6 WL 156 ; / [01] CORROSION ON SPLICE WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. SPLICE WILL BE REMOVED AND REPLACED PER SRM 51-10-02-0G-0 PARAGRAPH 9.; [02] INSPECTED Jul 29, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081897458Stub Frame · crackedFWD GALLEY DOOR CUTOUT UPPER FWD STUB FRAME CRACKED AT BS294 STRINGER 8RT ; / [01] REMOVED CRACKED UPPER FWD STUB FRAME IAW SRM 51-40-02; [02] UPDATED MEASUREMENT TABLE; [03] LOCATED AND DRILLED NEW FWD GALLEY DOOR CUTOUT UPPER FWD STUB FRAME AT BS294 STR 8R IJul 22, 2021 · N444WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2021082696770Structure · corrodedCORROSION ON TOP SURFACE OF AFT CHORD AT BS 260.7; WL 207; RBL 9 ; / [01] REMOVED CORROSION ON TOP SURFACE OF AFT CHORD AT BS 260.7; WL 207; RBL 9. DIMENSIONS OF DAMAGE REMOVAL FOUND TO BE 1.6' X 0.7'. DAMAGED PART HAS NO ALLOWABLE DAMAGE ENTRY; THEREFORE; DAMJul 21, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081897116Support Bracket · crackedCRACKED PULLEY SUPPORT BRACKET ANGLE BS 686+10 RBL 1 WL 207 ; / [01] REMOVED CRACKED PULLEY SUPPORT BRACKET PER SRM 51-40-02.; [02] FABRICATED NEW SUPPORT BRACKET FROM 2024TO#0.50 LOT # 1292371 MATERIAL PER DWG#273A9112; [03] FABRICATED NEW SUPPORT BRACKET FROJul 21, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081896774Intercostal · corrodedCORROSION ON TOP SURFACE OF INTERCOSTAL AT BS 262; WL 207; LBL 9.7 ; / [01] REMOVED CORROSION ON TOP SURFACE OF INTERCOSTAL AT BS 262; WL 207; LBL 9.7. DIMENSIONS OF DAMAGE REMOVAL FOUND TO BE 2.3' X 0.9' PER SRM 53-10-51-1A-1.; [04] REQUEST NDI TO PERFORM HFEJul 21, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081896771Intercostal · corrodedCORROSION ON TOP SURFACE OF INTERCOSTAL AT BS 264; WL 207; LBL 10.4 ; / [01] REMOVED CORROSION ON TOP SURFACE OF INTERCOSTAL AT BS 264; WL 207; LBL 10.4. DIMENSIONS OF DAMAGE REMOVAL FOUND TO BE 1.5' X 0.85' PER SRM 53-10-51-1A-1[05] REQUEST NDI TO PERFORM HFEJul 21, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081896772Structure · corrodedCORROSION ON TOP SURFACE OF AFT CHORD AT BS 260.7; WL 207; LBL 5.5 ; / [01] REMOVED CORROSION ON TOP SURFACE OF AFT CHORD AT BS 260.7; WL 207; LBL 5.5. DIMENSIONS OF DAMAGE REMOVAL FOUND TO BE 3' X 0.7'. DAMAGED PART HAS NO ALLOWABLE DAMAGE ENTRY; THEREFORE; DJul 21, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081896760Nut Plate · corrodedCORROSION ON NUTPLATE STRIP BS 787 TO BS 794 WL 156 RBL 21 ; / [01] CORROSION ON NUTPLATE STRIP FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] REMOVED NUTPLATE ASSEMBLY PER SRM51-40-02; [03] VERIFIED EVALUATION FOUND TO BE OUT OF LIMITS Jul 20, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895131Web · corrodedCORROSION ON ACB DOOR CUTOUT SUB-THRESHOLD WEB AT BS 818; RBL 28; WL 156 ; / [01] CORROSION ON WEB WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-60-15-1A-1 FIG 103 DETAIL D.; [02] VERIFIED CORRECTIVE ACTION #1<BR> WEB FOUND TO BE Jul 16, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895127Strap · corrodedCORROSION BS795 RBL21 BELOW AFT CARGO DOOR THRESHOLD STRAP ON NUT PLATE RETAINER STRIP / [01] REMOVED TWO N/P STRIPS PER SRM 51-40-02; [02] OUT OF LIMITS NO ALLOWABLE LIMITS GIVEN REPLACEMENT OF PART PER SRM 51-10-02-0G-0; STEP 9; [03] VERIFIED PART IS OUT OF Jul 16, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895143Web · corrodedCORROSION ON FCB DOOR SUB-THRESHOLD WEB BS 483; RBL 28; WL156 ; / [01] CORROSION ON WEB WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-30-15-1A-1 FIG 103 DETAIL D; [02] REMOVED FWD CARGO BAY SUB THRESHOLD WEB PER SRM 51-40-02-0G-0;Jul 16, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021072095140Angle · corrodedCORROSION ON BS 947 LOWER TRANSITION ANGLE LBL 12; WL 156. CORROSION ON SUPPORT FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS AGE GIVEN THE SRM. REMOVED TRANSITION ANGLE IAW SRM 51-40-02-0G-0, LOCATED AND DRILLED A NEW TRANSITION ANGLE IAW SRM 51-40-05-0G-0 &Jul 16, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021072095130Angle · corrodedCORROSION ON BS 947 LOWER TRANSITION ANGLE RBL 15; WL 156 ; / [01] CORROSION ON SUPPORT FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS AGE GIVEN THE SRM. NEW PART WILL BE INSTALLED ON FAULT # TTG8Q005U2RBJul 16, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021072095141Web · corrodedCORROSION ON ACB DOOR CUTOUT SUB-THRESHOLD WEB AT BS 797; RBL 22; WL 156. FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-60-15-1A-1 FIG 103 DETAIL D. WEB WILL BE REMOVED AND REPLACED PER SRM 51-10-02-0G-0 PARAGRAPH 9.Jul 16, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895098Stringer Clip · crackedCRACK IN STRINGER CLIP BS294 STR13L ; / [01] REMOVED CRACKED STRINGER CLIP AT BS 294 STR 13L PER SRM 51-40-02.; [02] FABRICATED NEW ANGLE FROM BAC1489-360#7075T62; LOT# 1464682-1 IAW DWG 141A1311 SH 1 REV:C; [03] INSPECTED FABRICATED NEW ANGLE FROM BAC1489-360Jul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2021081895077Bear Strap · crackedCRACK NOTED IN FWD GALLEY DOOR (R1) BEAR STRAP BS-293.5 APPROXIMATELY 4' BELOW STR-8R ; / [01] STARED REMOVING FASTENERS AT BS 291.5 FRAME FOR SKIN AND BEARSTRAP REPAIR PER SRM 51-40-02; [02] VERIFIED; [03] REMOVED ALL FASTENERS IN THE REPAIR AREA AT BS291.5 FJul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021081895086Channel · corrodedCORROSION ON MOPSILL AT ASD BS 947-987 RBL 50 WL 208 ; / [01] REMOVED CORROSION ON MOPSILL BS 983-984 RBL 50 WL 208 PER SRM 51-10-02-0G-0. REMOVED AMOUNT 1X1X .014 ORIGINAL THICKNESS .080. FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-1-A00707. DIAL DEPTH GUAGJul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895092Channel · crackedFWD ENTRY MOPSILL INNER CHORD CRACKED AT BS 303 LBL 50 WL 208 ; / [01] REMOVED FWD ENTRY DOOR MOPSILL INNER CHORD PER SRM 51-40-02-0G-0. MATERIAL THICKNESS IS 0.090.; [02] LOCATED AND DRILLED NEW FED MOPSILL PER DWG# 141A8110; DWG# 141A9810; SRM 51-40-05; SRM Jul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
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