N218WN

Service difficulty reports · 281

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 = 'N218WN' 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 SWAA2026102116002Lamp · inoperativeRIGHT FWD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. R & R THE LAMP IAW AMM 33-51-04. OPS CHKD SATISFACTORY.Oct 17, 2026 · N218WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026100556763Collector · abnormalNR 1 ENGINE CANDLING AFTER SHUT DOWN FOR ABOUT 5-7 MINUTES. REMOVED AND REPLACED IAW AMM 71-00-00-800-803-F00, INSPECTION AFTER AN ENGINE FIRE USE OF FIRE EXTINGUISHING AGENTS OR HIGH NACELLE TEMPERATURE.Oct 3, 2026 · N218WN · Boeing 7377H4 · Engine Collector/Tailpipe/NozzleSDR SWAA2026092906455Lamp · inoperativeEMERGENCY EXIT LIGHT AT R1 DOOR WAS INOPERATIVE. REMOVED AND REPLACED THE LAMPS IAW AMM 33-51-04-960-801.Sep 25, 2026 · N218WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026090301846Strut · crackedNR 1 ENGINE TURBINE REAR FRAME HAD A CRACK ON STRUT NR 15 AT C2, LOCATION MEASURING 0.0895" CW EA M-21-172-00808 NR 1 ENG TURBINE REAR FRAME TO REINSP EVERY 4700CYCAug 30, 2026 · N218WN · Boeing 7377H4 · Engine Mount SectionSDR SWAA2026081077807Light · inoperativeFO EMERGENCY EXIT DOOR INTERNAL EMERGENCY LIGHT INOPERATIVE. R & R IAW AMM 33-51-04-960-801.Aug 5, 2026 · N218WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026062314655Seat · faultedSEAT 15 DEF WONT STAY UP. TIGHTENED AFFECTED SEAT ROW AS REQUIRED IAW CMM 25-21-45.Jun 21, 2026 · N218WN · Boeing 7377H4 · Passenger Compartment EquipmentSDR SWAA2026061511252Sign · brokenMID-CABIN CEILING EXIT SIGN BROKEN. REMOVED AND REPLACED OVERWING CEILING EMERGENCY EXIT SIGN IAW AMM 33-51-01.Jun 10, 2026 · N218WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025091113796Battery · no testFA REPORTS AFT EMERGENCY FLASH LIGHT WONT TEST. REPLACED AFT INBOARD FLASHLIGHT BATTERY. OPS CHECK OKAY. REF AMM 25-64-00Sep 11, 2025 · N218WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2025082206432Acm · seizedWITH MAX COOLING FROM THE APU; AFTER ABOUT 10 MINUTES; SMOKE FILLED THE CABIN AND AN ACRID SMELL WAS NOTICED. THE PACKS AND RECIRC FAN WERE TURNED OFF AND THE SMOKE DISAPATED.<[01] DURING INSPECTION OF FAULT FOUND RIGHT ACM SEIZED.;[02] PERFORMED SMOKE OR FUMEAug 19, 2025 · N218WN · Boeing 7377H4 · Cabin Cooling SystemSDR SWAA2025051670801Flashlight · inoperativeFWD FLASHLIGHT (FA) INOP<[01] R+R FWD FA FLASHLIGHT PER AMM 33-55-00.<BR>OPS CHECKS GOOD.May 13, 2025 · N218WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2025040721696Lens · out of adjustR1 OVERDOOR EXIT SIGN LENS FALLING<[01] R&R OVERDOOR EXIT SIGN ASSY PER AMM 33-51-01Apr 4, 2025 · N218WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025032608223Handle · brokenL-2 DOOR ASSIST HANDLE IS BROKEN IN TWO HALVES. REPLACED L-2 DOOR ASSIST HANDLE IAW AMM-52-13-31-400-802 ITEM G STEP 2.Mar 22, 2025 · N218WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2025032607422Battery Pack · inoperativeEMERGENCY EXIT BATTERY PACK M1668 WILL NOT CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT BATTERY M1668 IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.<BR>WN50148;[02] VERIFIED ITEM 1<BR>C/WMar 19, 2025 · N218WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025032601595Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 231UF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLETE.;[03] COMPLETE AND AUDIT COMPLETE.Mar 3, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025032601596Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 231LF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLETE.;[03] COMPLETE AND AUDIT COMPLETE.Mar 3, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025032601597Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 231KF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLETE.;[03] COMPLETE AND AUDIT COMPLETE.Mar 3, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025032601326Attach Angle · crackedCENTER TANK REAR SPAR LEFT HAND LOWER ATTACH ANGLE COMMON TO STA663 VAPOR BARRIER WEB IS CRACKED AT FASTENER HOLE OUTBOARD OF LBL 6.13; WL 169<[01] REMOVED AND REPLACED CENTER TANK REAR SPAR LEFT HAND LOWER ATTACH ANGLE IAW B737-700 SRM 57-10-10-2R-5;[02] EDITMar 2, 2025 · N218WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2025032601193Skin · cracked#2 TANK UPPER SKIN (INTERNAL) BETWEEN RIB 21 AND RIB 22; AFT UPPER STRINGER END IS CRACKED.<[01] CRACK ON #2 FUEL TANK (INTERNAL). AFT UPPER STRINGER; BETWEEN RIBS 21 AND 22 WAS REPAIRED IAW EA 25-157-00566-WIP1 AND EA 25-157-00566;[02] C/WMar 1, 2025 · N218WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2025032600387Floor Panel · pulledDOT A24-12 AFT CABIN FLOOR PANEL 241ADF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLETE.;[03] COMPLETE AND AUDIT COMPLETE.Feb 27, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025032600477Floor Panel · pulledDOT A24-12 FORWARD CABIN FLOOR PANEL 222DF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLETE.;[03] COMPLETE AND AUDIT COMPLETE.Feb 27, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025032600043Support Angle · corroded(147-91) R1 DOOR CREASE BEAM SUPPORT ANGLE HAS CORROSION AT STA 332.1-10' TOP SIDE (MARKED)<[01] REMOVED DAMAGE IAW SRM 53-10-15-1A-2 STEP: 4.C<BR>01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME -Feb 26, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025032600040Floor Panel · pulled(151- DOT 015) PULLED FIBERS ON TOP SIDE OF CABIN FLOOR PANEL 241DF.<[01] ALL STEPS EA 25-153-00560; WORK ACCOMPLISHED IAW B737 SRM 53-00-50-2R-1.;[02] COMPLETE.;[03] COMPLETE AND AUDIT COMPLETE.Feb 26, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025032600041Floor Panel · pulled(151- DOT 016) PULLED FIBERS ON TOP SIDE OF CABIN FLOOR PANEL 242DF.<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLETE AND AUDIT COMPLETE.;[03] COMPLETE AND AUDIT COMPLETE.Feb 26, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025032600045Floor Panel · pulled(151- DOT 017) PULLED FIBERS ON TOP SIDE OF CABIN FLOOR PANEL 241EF.<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLETE.;[03] COMPLETE;[04] COMPLETE AND AUDIT COMPLETEFeb 26, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025032600042Floor Panel · pulled(151- DOT 018) PULLED FIBERS ON TOP SIDE OF CABIN FLOOR PANEL 242CF.<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLETE.;[03] COMPLETE;[04] COMPLETE AND AUDIT COMPLETE.Feb 26, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025032699636Panel · cracked(147-80) L/H HORZ PANEL 333AT GAP COVER FIN HAS CRACK<[01] REMOVED AND REINSTALLED GAP COVER SEAL TO F.O.M ON PANEL 333AT; THEN THE GAP COVER FIN WAS REMOVED DUE TO A CRACK; AND A NEW FIN WAS INSTALLED ON PANEL 333AT. MAINTENACE WAS DONE PER SRM 51-40-02-0G-0 Feb 25, 2025 · N218WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2025032699171Strap · corrodedDOT#07 A-043 AFT CARGO COMPARTMENT FLOORBOARD STRAP CORRODED AT STA 887 RBL 20 TO LBL 10 WL 156<[01] REMOVED AND REPLACED ON SHELF AFT CARGO COMPARTMENT FLOORBOARD STRAP AT STA 887 RBL 20 TO LBL 10 WL 156 IAW SRM 51-40-02-0G-0;[02] REMOVED AND REPLACED ON SHELFeb 24, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025032698984Pressure Deck · crackedA177-001 HORIZONTAL PRESSURE DECK WEB STA 665; RBL 43; WL 202 HAS A .50' CRACK IN WEB. VERIFIED WITH HFEC AND MARKED ENDS IN BLACK.<[01] 04 - REPAIRED HORIZONTAL PRESSURE DECK WEB BETWEEN RBL 38.5 TO RBL 60 AND BETWEEN STA 663.75 TO STA 675PER [SRM 53-40-51-2RFeb 24, 2025 · N218WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2025032699172Angle · corrodedDOT#08 A-043 AFT CARGO COMPARTMENT AFT BKHD LOWER STAINTION ANGLE CORRODED AT STA 947.5 RBL 20 TO LBL 10 WL 156<[01] REMOVED CORROSION AFT CARGO COMPARTMENT AFT BKHD LOWER ANGLE IAW SRM 51-10-02-0G-0 ITEM 15 EVALUATED ALLOWABLE LIMITS .090 ORIG 'T' .045 REMAINFeb 24, 2025 · N218WN · Boeing 7377H4 · Cargo CompartmentsSDR SWAA2025032699175Escape Rope · frayedRIGHT EMERGENCY ESCAPE HATCH ESCAPE ROPE STARTING TO FRAY<[01] REPLACED RIGHT EMERGENCY ESCAPE HATCH ESCAPE ROPE I/A/W AMM 25-61-10-400-802 STEP 6;[02] REMOVED & INSTALLED RIGHT EMERGENCY ESCAPE HATCH ESCAPE ROPE I/A/W AMM 25-61-10-000-802 & AMM 25-61-10-400-8Feb 24, 2025 · N218WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2025032699174Skin · delaminatedDOT#09 A-043 LH WING; OTBD AFT FLAP INBD LOWER CORNER DELAMINATED<[01] REPAIRED LH WING OUTBD AFT FLAP INBD CORNER IAW B737 SRM 57-53-01-2R-1 AND SRM 51-70-10-2R-0.;[02] VERIFIED ITEM 1<BR>C/WFeb 24, 2025 · N218WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2025033198409Support Bracket · cracked(A125-13) AFT CARGO BAY; PANEL SUPPORT BRACKET ATTACHED TO FWD BULKHEAD CRACKED; BS727; RBL04; WL162<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] AUDIT C/WFeb 23, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025032698397Threshold · corroded(A125-01) AFT CARGO BAY; DOOR LOWER THRESHOLD CORRODED; BS787+8' - BS847; RBL21-RBL29; WL156<[01] REMOVED CORROSION AND EVALUATED .045 ORIG 'T' .033 REMAINING .012 LOSS FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1 REMOVED AND REPLACED IAW SRM 51-40-02-0G-0 AND DWFeb 23, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025032698398Shield · corroded(A125-02) AFT CARGO BAY; DOOR FWD SHIELD CORRODED; BS767 - BS787+8'; RBL21; WL156<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] COMPLETE<BR>AUDIT C/W;[03] COMPLETE;[04] CFeb 23, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025032698399Floor Support · corroded(A125-03) AFT CARGO BAY; FLOOR LATERAL UNION CORRODED; BS767+5'; RBL22-LBL22; WL156<[01] REMOVED AND REPLACED ON SHELF AFT CARGO BAY; FLOOR LATERAL UNION P/N 146A9401-4 ISSUE TAG WN49235 IAW IPC 53-42-11-30; SRM 51-40-02-0G-0;[02] VERIFIED TASK COMPLETE<BR><BRFeb 23, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025032698405Angle · corroded(A125-04) AFT CARGO BAY; DOOR FWD SHIELD; UNDERLYING STRUCTURE - ANGLE CORRODED; BS767 - BS787+8'; RBL22; WL156<[01] VERIFIED 100% MATERIAL LOSS FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1 REMOVED AND REPLAED ANGLE IAWSRM 51-40-02-0G-0 AND DWG 146A8123 REV:-;[02Feb 23, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025032698925Skin · pulled(147-73 ) R/H WING L/E INBOARD OF THE NACELLE STRUT SKIN HAS PULLED FASTENERS (MARKED) AFT END<[01] 04 - REPAIRED PER [SRM 57-41-01-2R-7-A01177 (REPAIR 7 - WING INBOARD FIXED LEADING EDGE SKIN - LOOSE OR MISSING FASTENER REPAIR - CAT A REPAIR - PERMANENT)];[02Feb 23, 2025 · N218WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2025032698926Skin · pulled(147-74) R/H WING L/E SKIN INBOARD OF THE NACELLE STRUT HAS PULLED FASTENER (MARKED) AFT AND I/B END<[01] 01 - REMOVED AND REPLACED PER [SRM 57-41-01-2R-7-A01177 (REPAIR 7 - WING INBOARD FIXED LEADING EDGE SKIN - LOOSE OR MISSING FASTENER REPAIR - CAT A REPAIRFeb 23, 2025 · N218WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2025032698406Angle · corroded(A125-07) AFT CARGO BAY; Z-ANGLE CORRODED; BS727 - BS767; RBL22; WL156<[01] BLENDED CORROSION ON AFT CARGO Z-ANGLE BS727 - BS767; RBL22 ACCOMPLISHED 10X MAG IAW SRM 51-10-02 VERIFIED MATERIAL LOSS TO BE ORIG .040'; LOSS .008'; REMAINING .032' FOUND TO BE OUT OFeb 23, 2025 · N218WN · Boeing 7377H4 · Cargo CompartmentsSDR SWAA2025032698407Angle · corroded(A125-08) AFT CARGO BAY; Z-ANGLE CORRODED; BS727 - BS847; LBL22; WL156<[01] BLENDED CORROSION ON AFT CARGO Z-ANGLE BS727 - BS847; LBL22 VERIFIED TO 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED AFT CARGO L/H Z-ANGLE STA 727 - STA 847 IAW SFeb 23, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025032698383Baffle · cracked(A204 DOT 45) FORWARD CARGO STA 500 TO 500A; STR 26L; Z-ANGLE BAFFLE PLATE IS CRACKED IN 2EA PLACES.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)] AND BOEING DWG: 143A7505 REVFeb 22, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025032698384Baffle · cracked(A204 DOT 46) FORWARD CARGO. STA 440+10; STR 26L; Z-ANGLE BAFFLE PLATE IS CRACKED AT FASTNER HOLE.<[01] REMOVED BAFFLE IAW SRM 51-40-02-0G-0 RECEIVED REPLACEMENT BAFFLE PN 143A7510-9 TAG WN3413 AND VERIFIED IT TO BE CORRECT REPLACEMENT PART IAW BOEING DWG 143AFeb 22, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025032698389Stringer Clip · cracked(A204 DOT 54) FORWARD CARGO. STA 500D; STR 19L; STRINGER CLIP GUSSET IS CRACKED IN RADIUS COMMON TO BULKHEAD SUPPORT.<[01] REMOVED AND REPLACED STA 500D; STR 19L; STRINGER CLIP GUSSET I.A.W. SRM 51-40-02-0G-0 AND BOEING DWG 143A7902; SHEET 172; REV -;[02] VERIFeb 22, 2025 · N218WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2025032698394Stringer Clip · cracked(A204 DOT 55) FORWARD CARGO; STA 500D; STR 21L; STRINGER CLIP GUSSET CRACKED COMMON TO BULKHEAD SUPPORT.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]<BR>APPLIED CIC IAW AMM 5Feb 22, 2025 · N218WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2025032698385Angle · corroded(A204 DOT 47) FORWARD CARGO STA 500A TO 500D; LBL 21; WL 159; Z-ANGLE HAS CORROSION AROUND NUTPLATE HOLES.<[01] 04 - REPAIRED PER [SRM 53-00-53-2R-5-A00957 (REPAIR 5 - CARGO COMPARTMENT SIDEPLATE REPAIR BETWEEN FLOOR PANEL SPLICES - PERMANENT)];[02] VERIFIED SFeb 22, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024111858841Battery Pack · failedPASSENGER CABIN EMERGENCY EXIT LIGHT BATTERY PACK M1675 FAILED CAPACITY TEST.<[01] R&R PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERY PACK M1675 IAW AMM 33-51-06.Nov 12, 2024 · N218WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024111858820Panel · cracked-CABIN FLOORBOARD PNL BREAKS CRACKED STA. 540 BETWEEN FLOORBOARDS 231XF AND 231UF BOTH SIDES LEFT AND RIGHT.<[01] R&R CABIN FLOORBOARD PANEL BREAKS/INTERCOSTALS LH & RH SIDES AT STA. 540 BETWEEN FLOORBOARDS 231XF & 231UF IAW SRM 51-40-02. STILL NEEDS FLOORBOARNov 12, 2024 · N218WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024111858821Girt Bar · looseR1 DOOR SLIDE AFT GIRT BAR BRACKET RIVET LOOSE<[01] REMOVED AND REPLACED RIVETS FOR R1 DOOR SLIDE AFT GIRT BAR BRACKET PER SRM 51-40-02.Nov 12, 2024 · N218WN · Boeing 7377H4 · Escape SlideSDR SWAA2024111858822Girt Bar · out of adjustL1 DOOR SLIDE GIRT NOT SECURED WITH VELCRO<[01] RE-SECURED L1 DOOR SLIDE GIRT WITH VELCRO PER AMM 25-66-01.Nov 12, 2024 · N218WN · Boeing 7377H4 · Escape SlideSDR SWAA2024111858835Seal · crackedR/H HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL IS CRACKED 4 PARALLEL TO SLIDING SEAL LEADING EDGE.<[01] R&R RH HORIZONTAL STABILIZER FRONT UPPER SLIDING SEAL REF. AMM 53-31-31.Nov 12, 2024 · N218WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
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