N413WN, cancelled Jun 5, 2026

Service difficulty reports · 307

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 = 'N413WN' AND deregistration_id = 'N413WN-2026-06-05'
  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 SWAA2025072393464Lens · looseEMERGENCY EXIT LIGHT LENS LOOSE ROW 3 DEF, SECURED LENS WITH TAPE. OK TO CONTINUE PER MEL 3-15-02 SP-1B . REINSTALLED EMERGENCY LIGHT LENS AT ROW 3DEF PER AMM 33-51-03. OPS CHECK GOOD.Jul 20, 2025 · N413WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025063086111Floor Panel · crackedFWD CARGO BIN HAS FWD CRACK ON FLOOR<[01] PREFORMED REPAIR OF FWD CARGO AFT FLOOR PANEL (120CF) PER SRM 53-00-53-1A-1 TO BE REINSPECTED EVERY 400 CYCLE MUST REPLACE AT 4;000 CYCLESJun 27, 2025 · N413WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025063085969Floor Panel · crackedFWD CARGO BIN HAS FWD CRACK ON FLOOR <[01]. OK TO CONTINUE AS PER MEL 25-16-01 SP1B AUTH NO 263657; [02] PERFORMED REPAIR ON FWD CARGO PIT AFT FLOOR PANEL 120CF PER SRM 53-00-53 SEE NON-ROUTINE TTG8Q013EBJT FOR CORRECTIVE ACTION AND TLD.Jun 26, 2025 · N413WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025050767579Girt Bar · out of adjustAFT FLT ATT NDT REPORTS CAPT SIDE GIRT BAR CATCHING ON DOOR FRAME. ADJUSTED GIRT BAR IAW AMM 25-66-01.May 5, 2025 · N413WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2025041725075Seat · loosePASSENGER CABIN SEAT ROWS 1DEF; 2DEF; 3DEF; 5ABC; 8ABC AND 11DEF LOOSE IN SEAT TRACKS <[01]. ADJUSTED SEAT ROWS 1DEF; 2DEF; 3DEF; 5ABC; 8ABC; & 11DEF IN REF TO CMM 25-21-42.Apr 16, 2025 · N413WN · Boeing 7377H4 · Passenger Compartment EquipmentSDR SWAA2024121878927Girt Bar · out of adjustCAPT AFT DOOR OPENED FROM OUTSIDE WITH GIRT BAR ATTACHED<[01] INSPECTED AFT DOOR SLIDE ON CAPT SIDE IN REFERENCE TO AMM 25-66-00 NO FAULTS NOTEDDec 17, 2024 · N413WN · Boeing 7377H4 · Escape SlideSDR SWAA2024090934916Cover · out of adjustAFT GALLEY SLIDE DOES NOT STOW PROPERLY<[01] READJUSTED AFT ENTRY DOOR SLIDE COVER PER SIP. NO OTHER DEFECTS NOTED.Sep 6, 2024 · N413WN · Boeing 7377H4 · Escape SlideSDR SWAA2024072516217Slide · dislodgedFLIGHT CREW LEFT GIRT BAR ARMED ON FWD SERVICE DOOR AND SLIDE CAME OUT AND PARTLY UNPACKED.<[01] REMOVED AND REPLACED FWD SERVICE DOOR SLIDE IAW AMM 25-66-01 AND MT 734-00-03.Jul 24, 2024 · N413WN · Boeing 7377H4 · Escape SlideSDR SWAA2024050783114Girt Bar · looseAFT ENTRY SLIDE GIRT BAR LOOSE<[01] RE-ADJUSTED GIRT BAR AND AFT ENTRY SLIDE REF MT 725-61-06May 6, 2024 · N413WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2023082490844Rib · crackedL/H HORIZONTAL STABILIZER REMOVABLE L/E; #4 (FROM I/B) UPPER RIB CRACKED. (MARKED)<[01] SRM 55-10-09-0I-1 IDENTIFICATION AND SRM 53-10-09-1A-1 ALLOWABLE DAMAGE ARE APPLICABLE.<BR>RIB LE.STA 95.96 CRACKED; FOUND TO BE OUT OF LIMITS PER 55-10-09-1A-1 PARAGRAPH 4Aug 17, 2023 · N413WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2023082490845Rib · crackedR/H HORIZONTAL STABILIZER REMOVABLE L/E; #2 (FROM I/B) LOWER RIB CRACKED. (MARKED)<[01] SRM 55-10-09-0I-1 IDENTIFICATION AND SRM 53-10-09-1A-1 ALLOWABLE DAMAGE ARE APPLICABLE.<BR>RIB LE.STA 78.29 CRACKED FOUND TO BE OUT OF LIMITS PER 55-10-09-1A-1 PARAGRAPH 4.Aug 17, 2023 · N413WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2023082489571Stiffener · crackedREJECTED: L/H H-STAB RIB #7 STIFFENER #4 UPPER RADIUS CRACKED: SRM APPLICABILITY VALIDATION FOR REPAIR; AND NDT/VISUAL INSPECTIONS NOT PERFORMED AFTER DAMAGE REMOVAL.<[01] L/H H-STAB RIB #7 STIFFENER #4 UPPER RADIUS CRACKED: ACCOMPLISHED ON COSTUMER CARD TTG8QAug 14, 2023 · N413WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2023082487322Support Bracket · crackedRT WING T/E PANEL 651FB FWD CENTER SUPPORT BRACKET IS CRACKED<[01] REMOVED AND REPLACED CRACKED FWD SUPPORT BRACKET ON PNL 651FB PER SRM 51-40-02-0G-0;[02] ADD REFERENCE SOPM 20-50-02;[03] VERIFIED CORRECTIVE ACTION #1.Aug 9, 2023 · N413WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2023082487069Stringer · crackedAREA AFT OF FORWARD CARGO BAY; STR 23R IS CRACKED AT AFT FASTENER BS 520+18<[01] PARTIAL STEP 1;[02] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 23-153-02467';[03] TASK CARD COMPLETEAug 8, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023082487068Stringer · crackedAREA AFT OF FORWARD CARGO BAY; STR 26R IS CRACKED AT AFT FASTENER BS 520+18<[01] PARTIAL STEP 1;[02] REPAIRED AREA AFT OF FORWARD CARGO BAY; STR 26R FROM BS 500D+11 TO BS 540 IAW SRM 53-00-03-2R-1;[03] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE;[04] VEAug 8, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023082487066Stringer · crackedAREA AFT OF FORWARD CARGO BAY; STR 23L IS CRACKED AT AFT FASTENER BS 520+18<[01] COMPLETED STEPS 1;2;3 AND 5;[02] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 23-153-02474;[03] VERIFIED CORRECTIVE ACTION #2.<BR>VERIFIED MEASUREMENTS.Aug 8, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023082486832Stiffener · crackedL/H H-STAB RIB #5 STIFFENERS 2 & 3 LOWER RADII ARE CRACKED.<[01] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 129.50 RIB 2ND AND 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[02] HFEC REQUEST ON THE CUT OUT EDGES; WEB AND EXISTING FASTENERS HOLES WAug 8, 2023 · N413WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2023082486834Stiffener · crackedCRACK INDICATION ON L/H H-STAB RIB #7 STIFFENER #4 UPPER RADIUS.<[01] REJECTED: L/H H-STAB RIB #7 STIFFENER #4 UPPER RADIUS CRACKED: THE SRM APPLICABILITY VALIDATION FOR REPAIR; AND NDT/VISUAL INSPECTIONS NOT PERFORMED AFTER DAMAGE REMOVAL. GENERATED TTG8Q00MUAug 8, 2023 · N413WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2023082486833Stiffener · crackedR/H H-STAB RIB 4 #3 STIFFENER LOWER RADIUS IS CRACKED.<[01] REMOVED THE DAMAGED PART AT RH HORIZONTAL STABILIZER STA 120.30 RIB 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[02] HFEC REQUEST ON THE CUT OUT EDGES; WEB AND EXISTING FASTENERS HOLES WITHIN THE REPAug 8, 2023 · N413WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2023082387321Scuff Plate · crackedAFT CARGO BAY FORWARD CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACK ON AFT CARGO BAY FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2) AND (4)<BR>EQUIPMENT USED; WELDING MACHINE E10583; CALIBRATION DUEAug 8, 2023 · N413WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023082387067Stringer · crackedAREA AFT OF FORWARD CARGO BAY; STR 27R IS CRACKED AT AFT FASTENER BS 520+18<[01] PARTIAL STEP 1;[02] REPAIRED AREA AFT OF FORWARD CARGO BAY; STR 27R FROM BS 500D+11 TO BS 540 IAW SRM 53-00-03-2R-1;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLEAug 8, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023082387065Stringer · crackedAREA AFT OF FORWARD CARGO BAY; STR 24L IS CRACKED AT AFT FASTENER BS 520+18<[01] COMPLETED STEPS 1;2;3 AND 5;[02] REPAIRED AREA AFT OF FORWARD CARGO BAY; STR 24L FROM BS 500D+10 TO BS 540 IAW SRM 53-00-03-2R-1 REPAIR 1;[03] VERIFIED CORRECTIVE ACTION 2 AND MEAAug 8, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023082387064Stringer · crackedAREA AFT OF FORWARD CARGO BAY; STR 26L IS CRACKED AT AFT FASTENER BS 520+18<[01] COMPLETED STEPS 1;2;3 AND 7;[02] REMOVED DAMAGED SECTION OF STR 26L BETWEEN BS 500D+10 TO 540 AND INSTALLED HAT SECTION SPLICE AND NEW STRINGER SECTION IAW SRM 53-00-03-2R-1 (REPAAug 8, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023082486619Panel · crackedWING CENTER SECTION BREAK PANEL IS CRACKED AT BS 540; RBL 1; WL 208<[01] REMOVED AND INSTALLED NEW BREAK PANEL AT WING CENTER SECTION BS 540; PER SRM 51-40-02 AND DWG 143A0060.;[02] VERIFIED CORRECTIVE ACTION #1.<BR>VERIFIED MEASUREMENTS.Aug 7, 2023 · N413WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023082486620Attach Angle · crackedWING CENTER SECTION CABLE INTERCOSTAL LOWER ATTACH ANGLE IS CRACKED AT BS 685+7; RBL 24; WL 203<[01] VERIFIED CORRECTIVE ACTION PARTIAL ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE; EXCEPT MISSING AMT SUMMARY OF WORK PER MPM.;[02] REMOVED AND REPLACED WING CENTAug 7, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2023082486621Attach Angle · crackedWING CENTER SECTION CABLE INTERCOSTAL LOWER ATTACH ANGLE IS CRACKED AT BS 685+7; LBL 24; WL 203<[01] VERIFIED CORRECTIVE ACTION PARTIAL ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE; EXCEPT MISSING AMT SUMMARY OR WORK PER MPM.;[02] TYPO: MISSING SUMMARY OF WORK.Aug 7, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2023082386622Frame · crackedBS 312 FRAME IS CRACKED IN THE LOWER RADIUS AT FED HEADER SUPPORT<[01] REPAIRED BS 312 FRAME LOWER RADIUS IAW EA # M-22-153-01244;[02] VERIFIED MEASUREMENT TABLE.<BR>VERIFIED CORRECTIVE ACTION COMPLETE. CARD COMPLETEAug 7, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2023082886355Panel · pulled/R/W T/E PANEL 661CB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] R/W T/E PANEL 661CB WITH SEVERAL PULLED FASTENER HOLE ON AFT END WAS REPAIRED IAW SRM 51-70-04-2R-9.;[02] DAMAGE WAS REPAIRED IAW SRM 51-70-04-2R-9.VERIFIED CURE TAPES UPLOADED.JOB Aug 6, 2023 · N413WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2023082886356Panel · pulledR/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] CONDUCTIVE COATED THE TOOLSIDE REPAIR SURFACE; CURED CONDUCTIVE COATING; AND PERFORMED A SATISFACTORY RESISTIVITY TEST WITH MULTIMETER ID:ATS1658 CAL DUE: 04/2024 IAW AMM 51-21-71-37Aug 6, 2023 · N413WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2023082886357Panel · pulledR/W T/E PANEL 661AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] R/W T/E PANEL 661AB WITH SEVERAL PULLED FASTENER HOLE ON AFT ENDWAS REPAIRED IAW SRM 51-70-04-2R-9.;[02] DAMAGE WAS REPAIRED IAW SRM 51-70-04-2R-9.VERIFIED CURE TAPES UPLOADED.JOB COAug 6, 2023 · N413WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2023082486362Track · brokenL/H HORIZ STAB UPPER AFT SLIDE SEAL TRACK FOR IS BROKEN<[01] VERIFIED OK TO INSTALL L/H HORIZ STAB UPPER AFT SLIDE SEAL TRACK.;[02] REMOVED AND REPLACE L/H HORIZ STAB UPPER AFT SLIDE SEAL TRACK IAW AMM 20-50-11 AND AMM 51-21-99-300-801<BR><BR>TW ID: PER2271. CAug 6, 2023 · N413WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2023082385853Battery Pack · unknownREMOVE AND REPLACE EMERGENCY EXIT LIGHT BATTERIES PRIOR TO AIRCRAFT DEPARTURE<[01] DOCUMENTATION OF INSTALLED PARTS;[02] ALL STEPS COMPLETE;[03] VERIFIED ALL PARTIAL STEPS COMPLETE; CARD COMPLETE; EXCEPT AMT MISSING FINAL ?SUMMARY OF WORK ACCOMPLISHED? PER MPMAug 4, 2023 · N413WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022093049110Panel · damaged193B MOUNTING HOLE LOCATIONS 1; 14 ; AND 19 HAVE ELONGATED OVERSIZED HOLES / [01] INSTALLED WASHERS AT HOLE LOCATIONS 1; 14; AND 19 PER EA 22-153-02942.Sep 29, 2022 · N413WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2022051908866Lens · loose17ABC CLEAR LENS AT BULLNOSE LOOSE / [01] SECURED LENS IN PLACE WITH BIN TAPE <BR>OK TO CONTINUE PER MEL 25-10-01 SP1B<BR>AUTH 66639;[02] REINSTALLED AREA IGHT LENS AT ROW 17ABC IAW AMM 33-51-03May 17, 2022 · N413WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022010357368Ballast · inoperativeRH EMERGENCY OVER WING EXIT SIDE WALL LIGHT OUT ; FLORESCENT LIGHT ON THE EMERG DOOR. OK TO CONTINUE PER MEL 33-2-03 SP1B. R & R BALLAST IAW MM 33-21-00.Dec 31, 2021 · N413WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021122254435Cover · looseEMERGENCY LIGHT COVER AT 5DEF FELL OFF ; / [01] SECURED LIGHT COVER AT 5DEF IAW AMM 33-51-03 OPS CHECK GOODDec 18, 2021 · N413WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021121452162Tie Rod · brokenSUPPLEMENTAL INFORMATION: L/H FIXED LOWER TE PANEL 551FB HAS BROKEN SUPPORT STUTS AT LEADING EDGE INBOARD SIDE. ; / [01] R/R TWO BROKEN TIE RODS ON INBOARD FIXED TRAILING EDGE LOWER PANEL PER AMM 57-50-02Dec 12, 2021 · N413WN · Boeing 737 · Wing, Control SurfacesSDR SWAA2021112446110Light · inoperativeSUPPLEMENTAL INFORMATION: LEFT WING EMERGENCY EXIT DOOR OUTSIDE EMERGENCY LIGHT INOP ; / [01] RELAMPED LEFT OVERWING EMERGENCY LIGHT IAW AMM 33-51-04Nov 21, 2021 · N413WN · Boeing 737 · Emergency LightingSDR SWAA2021102232413None · crackedGIRT TUBE END CRACKED OUT / [01] R&R GIRT TUBE IAW CMM 25-66-17.; [02] C/WSep 27, 2021 · N413WN · Boeing 7377H4 · Escape SlideSDR SWAA2021092018033Door · out of adjustON LANDING FWD ENTRY DOOR HANDLE POPPED UP A LITTLE AND FWD ENTRY LIGHT CAME ON. 2 OUT OF 3 LANDINGS. / [01] ADJUSTED FWD ENTRY DOOR OPS CHECK GOOD PER AMM 52-11-00Sep 16, 2021 · N413WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2021091616781Lamp · inoperativeEMERGENCY LIGHT ROW 4ABL INOP. ; / [01] RELAMPED EMERGENCY LIGHT AT ROW 4ABC PER B7373 AMM 33-51-03-960-801. INSTALLATION TEST; TESTED NORMAL.; [02] VERIFIEDSep 12, 2021 · N413WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021091615326Scuff Plate · crackedAFT CARGO DOOR FORWARD CORNER SCUFF PLATE FOUND CRACKED. ; / [01] LOCATED AND DRILLED NEW AFT CARGO DOOR FORWARD SCUFF PLATE IAW SRM 51-40-05-0G-0. SCUFF PLATE WILL BE INSTALLED ON CUSTOMER CARD #TTG8Q0035HUM.; [02] VERIFIED 1Sep 8, 2021 · N413WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091614807Battery Pack · inoperativeASSOCIATED EMERGENCY LIGHTS BY LH OVER WING EXIT DOOR WITH BATTERY PACK M1668 ARE INOP. ; OCIATED EMERGENCY LIGHTS BY LH OVER WING EXIT DOOR WITH BATTERY PACK M1668 ARE INOP. / [01] REPLACED BATTERY PACK AT M1668 L/H OVER WING AND PERFORMED OPS CHECK AS PER B7Sep 4, 2021 · N413WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021091613659Support Bracket · brokenRT WING AT LWR REAR SPAR NEAR OB FWD CORNER OF PNL 651BD HAS PNL SUPPORT BRKT BROKEN 8-98 ; / [01] REMOVED AND REPLACED SUPPORT BRACKET AT RT WING AT LOWER REAR SPAR IN IAW SRM 51-40-02-0G-0 P/N #115A5552U2; [02] VERIFIED 1Aug 31, 2021 · N413WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2021091610592Lug · corrodedCORROSION-- RH HORIZONTALSTABILIZER CENTER SECTION REAR SPAR LOWER CLEVIS E FWD LUG HAS CORROSION IN BORE. ; / [01] ''PERFORMED EA 21-155-02335. REFER TO FAULT TTG8Q0065NR8''.; [02] VERIFIED STEP 1Aug 23, 2021 · N413WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2021091610591Lug · corrodedCORROSION-- RH HORIZONTAL STABILIZER CENTER SECTION REAR SPAR LOWER CLEVIS E AFT LUG HAS CORROSION ON FWD FACE. ; / [01] ''PERFORMED EA 21-155-02335. REFER TO FAULT TTG8Q0065NR8''.; [02] VERIFIED STEP 1Aug 23, 2021 · N413WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2021091609154Spar · corrodedCORROSION FOUND ON RH REAR SPAR LOWER LUG K HAS CORROSION ON BOTH FACE OF THE LUG. ; / [01] REPAIR ACCOMPLISHED PER EA 21-155-02337. REFER TO FAULT TTG8Q0065LLA.; [02] VERIFIED STEP 1Aug 20, 2021 · N413WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2021091608697Baffle · crackedFWD CARGO RT SIDE PLATE BAFFLE CRACKED BTW STA 400 AND 420 ; / [01] REMOVED CRACKED BAFFLE OF FWD. CARGO COMP. STA. 400 TO 420. R/H.; [02] LOCATED AND DRILL NEW PLATE BAFFLE IAW. B-737-700 SRM. 51-40-05-0G-0; [03] VERIFIED 1-2. OK TO INSTALL NEW BAFFLE.; [04] Aug 19, 2021 · N413WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091607868Fitting · corrodedLH O/B REAR SPAR FITTING OF VERTICAL STABILIZER(FTG-LH FWD MAIN)HAS PITTING CORROSION. ; / [01] REMOVED LH O/B REAR SPAR FITTING OF VERTICAL STABILIZER - LH FWD MAIN IN IAW SRM 51-40-02-0G-0; [02] VERIFIED 1. OK TO LOCATE AND DRILL NEW FITTING.; [03] PARTIALLYAug 16, 2021 · N413WN · Boeing 7377H4 · Vertical Stabilizer, Attach FittingsSDR SWAA2021091606993Clevis · corroded**CORROSION** R/H HORIZONTAL STABILIZER REAR SPAR LOWER AFT CLEVIS 'E'; HAS CORROSION. DOT # 208-151 ; / [01] COMPLETED REPAIR OF RIGHT HORIZONTAL STABILIZER REAR SPAR LOWER AFT CLEVIS 'E' PER EA 21-155-02335 AND PER ENGINEERING WORK INSTRUCTIONS WIP1; WIP2. WAug 14, 2021 · N413WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
Back to N413WN, cancelled Jun 5, 2026