N912WN

Service difficulty reports · 270

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 = 'N912WN' 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 SWAA2023091189433Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241AAF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATE FLOOR PANEL PER SRM 53-00-50-2R-0. ATTACHED CURE SHEET TO THIS FAULT RECORD.;[02] VERIFIED COAug 15, 2023 · N912WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023091189423Floor Panel · pulledAFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ADF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] VERIFIED CORRECTIVE ACTION #1;[03] VERIFIED MAug 15, 2023 · N912WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023091189436Floor Panel · pulledAFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] REPAIRED AREAS OF PULLED STRANDS ON UPPER SKIN OF AFT FLOOR PANEL 242TF IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.;[03] VERIFIED MEASUREMENTS TABLE.Aug 15, 2023 · N912WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023091189437Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE RECORDS TO THIS FAULT.;[02] VERIFIED RII STEPS COMPLETE;[03] VERIFIED MEASUREMENTAug 15, 2023 · N912WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023091388412Panel · crackedWING CENTER SECTION BREAK PANEL IS CRACKED AT FASTENER; BS 540; LBL 1; WL 207<[01] VERIFIED APPLICABILITY OF SRM 51-10-02-0G-0; NO DAMAGE LIMITS GIVEN IN SRM PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARA 9. REMOVED WING CENTER SECTION CRACK DAMAAug 11, 2023 · N912WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023091388413Panel · crackedWING CENTER SECTION BREAK PANEL IS CRACKED AT FASTENER; BS 540; RBL 1; WL 207<[01] REMOVED AND REPLACED WING CENTER SECTION BREAK PANEL; BS 540; RBL 1- RBL 25; WL 207 IAW SRM 51-40-02-0G-0 AND DWG 143A0060;[02] VERIFIED MEASUREMENTS TABLE.<BR>VERIFIED CORRECTIAug 11, 2023 · N912WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023091388414Attach Angle · crackedWING CENTER SECTION CABLE INTERCOSTAL ATTACH ANGLE IS CRACKED AT BS 685+11; RBL 24; WL 203<[01] NO DAMAGE LIMITS GIVEN IN SRM; PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR 9; FABRICATED NEW BRACKET FROM BAC1490-2782 7075-T0 CLAD .050 LOT# 148227Aug 11, 2023 · N912WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2023091388409Attach Angle · crackedWING CENTER SECTION CABLE INTERCOSTAL ATTACH ANGLE IS CRACKED AT BS 685+11; LBL 24; WL 203<[01] REMOVED CRACK DAMAGED BRACKET FROM BS 685+11 LBL 24 WL 203 IAW SRM 51-40-02-0G-0. NO DAMAGE LIMITS GIVEN IN SRM PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0Aug 11, 2023 · N912WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2023091188411Beam · corrodedWING CENTER SECTION INNER CHORD CREASE BEAM HAS CORROSION AT BS 616+22; LBL 63; WL 207<[01] UPDATE MEASUREMENTS AND STEPS 1-3;[02] REMOVED AND REPLACED WING CENTER SECTIN INNER CHORD CREASE BEAM AT 616+22; LBL 63; WL 207. IAW SRM 51-40-02-0G-0 AND BOEING DWG 1Aug 11, 2023 · N912WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2023091288122Seat Track · corrodedR/H CABIN SEAT TRACK HAS CORROSION ON TOP OF CROWN AND WELL; BS 380+6; 380+14; 400+12; 440+4; RBL 45; WL 208<[01] PARTIALLY COMPLETED STEP 1;[02] PARTIALLY COMPLETED STEPS 1 AND 2;[03] PARTIALLY COMPLETED STEPS STEP 5.<BR>UPDATES MEASUREMENTS TABLE;[04] UPDATEAug 10, 2023 · N912WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2023091288134Seat Track · corrodedR/H CABIN SEAT TRACK HAS CORROSION ON TOP OF CROWN AND WELL; BS 480+7; 597+13; 706+6; 727+14; RBL 25; WL 208 FAULT GENERATED IN ERROR. CORROSION BS ON SEPERATE TRACKS.<[01] FAULT RAISED IN ERROR. DAMAGE CORRECTED ON CCN: TTG8Q00MRHVJ AND TTG8Q00MRJS1;[02] VERIAug 10, 2023 · N912WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2023091288116Seat Track · corrodedR/H CABIN SEAT TRACK HAS CORROSION IN WELL; BS 500A+16; 706+6; 706+17; RBL 45; WL 208 FAULT GENERATED IN ERROR. CORROSION BS ON SEPERATE TRACKS.<[01] FAULT RAISED IN ERROR. DAMAGE CORRECTED ON CCN: TTG8Q00MRJAP AND TTG8Q00MRHJFE.;[02] VERIFIED CORRECTIVE ACTIOAug 10, 2023 · N912WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2023091288117Seat Track · corrodedR/H CABIN SEAT TRACK HAS CORROSION IN WELL; BS 500+7; 500+16; 500A+18; 639+8; RBL 25; WL 208 FAULT GENERATED IN ERROR. CORROSION BS ON SEPERATE TRACKS.<[01] FAULT RAISED IN ERROR. DAMAGE CORRECTED ON CCN: TTG8Q00MRJJ5 AND TTG8Q00MRHVC.;[02] VERIFIED CORRECTIVEAug 10, 2023 · N912WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2023091188142Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS535 S-25R WL155. MARKED<[01] REPAIRED AS PER EA-23-153-02485.;[02] TASK CARD COMPLETE.;[03] VERIFIED MEASUREMENT TABLE.Aug 10, 2023 · N912WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023091188143Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS535 S-26R WL153. MARKED<[01] VERIFIED COMPLETION TASK CARD AND MEASUREMENT TABLE.Aug 10, 2023 · N912WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023091387635Rib · crackedLEFTT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 2ND VERTICAL STIFFENER IS CRACKED.<[01] OK TO INSTALL T- SECTION; ANGLE AND SHIM GIVEN;[02] VERIFIED MEASUREMENT TABLE.<BR>TASK COMPLETEAug 9, 2023 · N912WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2023091387636Stiffener · crackedLEFTT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED.<[01] OK TO INSTALL T- SECTION; ANGLE AND SHIM GIVEN;[02] REMOVED CRACK DAMAGE ON LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 129.Aug 9, 2023 · N912WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2023091186742Panel · debondedPANEL 194FR OUTER SKIN IS DISBONDED. (MARKED)<[01] PANEL 194FR DIS BOND REPAIRED IAW 51-70-05-2R-2;[02] FINAL INSPECTION. JOB COMPLETE.Aug 8, 2023 · N912WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2023080786067Unknown · unknownBLEW #3 RH MLG TIRE ON TAKEOFF ROLL<[01] PERFORMED TIRE BURST CONDITIONAL INSPECTION PER AMM 05-51-54. DAMAGE DOCUMENTED ON LP# 2026258; 2026259; 2026260; 2026261 AND 2026262.Aug 3, 2023 · N912WN · Boeing 7377H4 · Tire TubeSDR SWAA2023072080444Power Supply · failedEMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK @ 17ABC<[01] REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY PER AMM 33-51-06Jul 20, 2023 · N912WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023061257325Battery Pack · inoperativeEMERGENCY LIGHTS AT 3DEF AND 6DEF INOP<[01] R&R FWD RH BATTERY PACK IAW AMM 33-51-06Jun 8, 2023 · N912WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023051548022Floor Panel · crackedRAMP REPORTS AFT CARGO FLOOR PANEL 140 BF HAS A CRACK.<[01] INSPECTED AND FOUND CRACK TO BE MORE THAN 2 INCHES FROM EDGE. REPAIRED CRACK ON FLOOR PANEL IN REFERENCE TO AMM 25-52-01. OK FOR CONTINUED SERVICE.May 12, 2023 · N912WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022110267132Assist Assy · brokenFWD DOOR ASSIST HANDLE BROKEN. / [01] R&R FWD ENTRY DOOR HANDLE REF AMM 52-11-32.Nov 1, 2022 · N912WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2022031182114Lens · inoperativeRH OVERWING LOWER EXIT SIGN LIGHTS INOP AND LENS DAMAGED / [01] RELAMPED AND REPLACED LENS IAW AMM 33-51-01Mar 10, 2022 · N912WN · Boeing 737* · Emergency LightingSDR SWAA2022013164118Panel · elongated193D PANEL HAS ELONGATED FASTENER HOLES ; 193D PANEL HAS ELONGATED HOLES. / [01] ACCOMPLISH EA 22-153-00260 ASSIGNED AS A SUBTASK.; [02] COMPLIED WITH TSR 202200634Jan 25, 2022 · N912WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2022013164119Panel · elongated194E PANEL HAS ELONGATED HOLES ; 194E PANEL HAS ELONGATED HOLES. / [01] REMOVED AND REPLACED 194E PANEL PER SRM 51-40-02. REF TSR 202200632.Jan 25, 2022 · N912WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2021121350989Bracket · brokenSUPPLEMENTAL INFORMATION: GIRT BAR BRACKET ON FWD PASSENGER ENTRY ; GIRT AR RACKET ON FWD PASSENGER ENTRY DOOR ROKE OFF REF TTG8Q009NK81 / [01] INSTALLED FASTENERS IAW SRM 51-40-02.Dec 7, 2021 · N912WN · Boeing 737 · Escape SlideSDR SWAA2021120950628None · brokenSUPPLEMENTAL INFORMATION: GIRT BAR BRACKET ON FWD PASSENGER ENTRY DOOR BROKE OFF ; / [01] C/W EA 21-125-03628 ; MUST BE REPAIRED WITHIN 10 CYCLES.Dec 5, 2021 · N912WN · Boeing 737 · Escape SlideSDR SWAA2021091416474Slide · out of adjustCUSTOMER WALK- R2 DOOR GIRT CURTAIN GRABS THE BOTTOM WHEN CLOSING WHEN CLOSING. NEEDS ADJUSTMENT/REPOSITIONING ; / [01] READJUSTED Z FOLD ON R-2 DOOR ESCAPE SLIDE GIRT BAR AS PER B737-700 AMM 25-66-01-400-804; [02] VERIFIED STEP 1Sep 10, 2021 · N912WN · Boeing 7377H4 · Escape SlideSDR SWAA2021091416131Retainer · brokenFWD CARGO DOOR ASSIST LANYARD HAS BROKEN CLIP ; / [01] REMOVED AND REPLACED FWD CARGO DOOR ASSIST LANYARD CLIP REF B 737-700 AMM 52-31-00-400-801; [02] VERIFIED STEP 1Sep 8, 2021 · N912WN · Boeing 7377H4 · Cargo/Baggage DoorsSDR SWAA2021091414617Intercostal · corroded***CORROSION*** FOUND CORROSION UNDER LT WING L/E PANEL 521DB ; / [01] REMOVED ACCESS PANELS FOR REPAIR #521CB;521EB;521FB AND 521GB AS PER B-737-700-AMM-57-41-02-000; [08] FABRICATED REPAIR Z ANGLE (-1) MATERIAL 0.100 THICK BARE ALUMINUM 2024-0 AS PER EA-21-1Sep 3, 2021 · N912WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2021091410885Angle · elongatedRIGHT VAPOR BARRIER WEB UPPER ANGLE HAS 12 HOLES THAT ARE ELONGATED ; / [01] PERFORMED HFEC ROTO INSP ON ELONGATED EXISTING FASTENER HOLES IAW B737 NDT PART 6; 51-00-00; PROCEDURE 16. NO CRACKS NOTED<BR>TOOL: NORTEC 600 B/C: 166317 DUE:10/12/2021<BR>TOOL: OLYMAug 23, 2021 · N912WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2021091549683Gusset · crackedFWD. CARGO COMPT. AFT BLKH. STA 500D;STR. 18L;FOUND GUSSET CRACKED. ; / [01] REMOVED DAMAGE GUSSET AT FWD. CARGO COMPT. AFT. BLKH. STA. 500D; S-18L. PER B737-7 SRM 51-40-02-0G-0.; [02] VERIFIED STEP 1; [03] OK TO INSTALL GUSSET; [04] INSTALLED NEW GUSSET P/N 1Aug 21, 2021 · N912WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091409670Scuff Plate · crackedFWD CARGO DOOR AFT SCUFF PLATE CRACKED ; / [01] RECEIVED NEW SERVICEABLE AFT SCUFF PLATE CORNER; P/N:143A8331-4; PO # 1684224. ISSUE TAG : WN4833. THIS PLATE WILL BE INSTALLED 0N CARD TTG8Q0067XQY.; [02] VERIFIED STEP 1Aug 20, 2021 · N912WN · Boeing 7377H4 · Cargo/Baggage DoorsSDR SWAA2021091409645Bracket · crackedFWD CARGO COMPT L/H STA 500C STR 25 UNDER ZEE ANGLE BRACKET APPEARED CRACKED ; / [01] CRACK VERIFIED AT 'Z'-ANGLE BRACKET LOWER AREA AT FWD CARGO COMPARTMENT L/H STA 500C STR 25;IAW NDTM PART 6;51-00-00 PROCEDURE 23. LENGTH OF CRACK-0.197'; [02] REMOVED & REPLAug 19, 2021 · N912WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091409642Angle · corrodedEVIDENCE OF CORROSION AT FWD CARGO COMPT R/H ZEE ANGLE UPPER SURFACE BETWEEN STA 500 AND STA 500A ; / [01] REMOVED THE CORROSION AT FWD CARGO COMPT R/H Z ANGLE UPPER SURFACE BETWEEN STA. 500 & 500A;REF.B737-700 SRM 51-10-02-0G-0.; [02] ORIG. [08] COMPLETED FABAug 19, 2021 · N912WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091409643Angle · corrodedCORROSION AT FWD CARGO COMPT R/H ZEE ANGLE UPPER SURFACE BETWEEN STA 500A AND STA 500D ; / [01] REMOVED THE CORROSION AT FWD. CARGO COMPT. R/H Z ANGLE UPPER SURFACE BETWEEN STA. 500A & 500D. REF. B737-700 SRM 51-10-02-0G-0.; [02] ORIG. MAT. OF Z ANGLE: 0.040';Aug 19, 2021 · N912WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091409667Pressure Deck · damagedFLIGHT DECK FLOOR AREA AROUND PANEL 211AF;FOUND DAMAGE AT PREVIOUS REPAIR WEB STA. 259.5 - 1.5;LBL 15.0'. ; / [01] INSTALL EWIS PROTECTION AT REPAIR AREA; AS PER B737-7 AMM 20-60-07-913-801.; [02] REPAIRED COCKPIT FLOOR PER EA M-21-153-00734/ 1503096; [03] REMAug 19, 2021 · N912WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2021091549669Pressure Deck · crackedHORIZONTAL PRESSURE DECK WEB CRACKED AT STA 671 AND RBL 43 ; / [01] PERFORMED HFEC AND CONFIRMED CRACK ON HORIZONTAL PRESSURE DECK WEB STA 671 RBL 43 IAW NDTM PART 6;51-00-00 PROCEDURE 23. CRACK LENGTH-1.181'.<BR>[NORTEC 600;B/C 166316;CALIB.DUE-10/21]; [02] IAug 19, 2021 · N912WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2021091409640Skin · crackedLEFT HORIZONTAL STABILIZER LOWER SURFACE SKIN HAS A CRACK AT STA 184.70 ;4.00' FROM TRAILING EDGE. CRACK LENGTH ;1.181' ( AREA MARKED). ; / [04] REMOVED PANEL 331BZ FOR ACCESS AT L/H HORIZT STAB FRONT SPAR REF B737-700 SRM 51-40-02-0G-0; 2 PER EA NO:21-155-024Aug 19, 2021 · N912WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2021091408430Floor Panel · deterioratedFLOOR PANEL 140BF DETERIORATED AND SHOWING BURRS ; / [01] FABRICATED AFT CARGO COMPARTMENT FLOOR PANEL 140BF REF B 737-700 AMM 25-52-01-201-801.Aug 18, 2021 · N912WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021091408436Floor Panel · warpedAFT CARGO FLOOR PANEL 120AF WARPED AND DEFORMED ; / [01] FABRICATED NEW FLOOR PANEL 120AF; MAT. USED: A90RG1W-48144; PO # 1724657; REF. B737-7 AMM 25-52-01-201-801.; [02] VERIFIED STEP 1Aug 18, 2021 · N912WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021091408438Floor Panel · deterioratedFLOOR PANEL 141AF DETERIORATED AND SHOWING BURRS ; FLOOR PANEL 140AF DETERIORATED AND SHOWING BURRS / [01] FABRICATED AFT CARGO COMPARTMENT SIDEWALL PANEL 140AF REF B 737-700 AMM 25-52-01-201-801. CORRECTION TO THIS STEP: ACCESS PANEL 140AF IS NOT A SIDEWALL PAug 18, 2021 · N912WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021091548858Bulkhead Web · crackedR/H WHEEL WELL VAPOR BARRIER CRACKED AT RBL 43' 5' FROM LOWER SECTION APPROX. 7' IN LENGTH ; / [01] MEASUREMENTS; [02] REMOVED DAMAGE PLIES; PREPARED DAMAGE AREA FOR REPAIR; STOP DRILL CRACKS; PERFORMED DRY OUT AS PER B737 SRM 51-70-04-2R-10 SECTION A;B;C AND Aug 18, 2021 · N912WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2021082308861Support Bracket · crackedRIGHT WING T/E FLAP DEFLECTION CONTOL RIB UPPER PANEL SUPPORT BRACKET HAS SMALL CRACK AT CONTROL RIB ATTACH POINT. REMOVED AND REPLACED R/W T/E FLAP DEFLECTION CONTROL RIG UPPER PANEL SUPPORT BRACKET IN REF SRM 51-40-02-0G-0.Aug 18, 2021 · N912WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2021060178405Computer · inoperativeDURING INITIAL CLIMB OUT; ELECTRIC TRIM BECAME INOP; BOTH SIDES. MANUAL TRIM NORMAL. ; / REMOVED AND REPLACED FCC B AND STAB TRIM RELAY; AMM 22-11-33 AND SWPM 20-81.May 28, 2021 · N912WN · Boeing 7377H4 · Autopilot SystemSDR SWAA2021060178767Relay · inoperativeDURING INITIAL CLIMB OUT; ELECTRIC TRIM BECAME INOP; BOTH SIDES. MANUAL TRIM NORMAL. ; / REMOVED AND REPLACED FCC B AND STAB TRIM RELAY; AMM 22-11-33 AND SWPM 20-81.May 28, 2021 · N912WN · Boeing 7377H4 · Stabilizer Control SystemSDR SWAA2021012143502Battery Pack · failedEMERGENCY LIGHT BATTERY PACKS AT FOLLOWING LOCATIONS FAILED CAPACITY CHECK M1675; M1673; M1672. R & R EMERGENCY LIGHT BATTERY PACKS AT M1675; M1673; M1672, PER AMM 33-51-06.Jan 19, 2021 · N912WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021050646120Seal · crackedRIGHT HAND HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED. / R&R RIGHT HAND HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL REF AMM 53-31-31.Apr 29, 2020 · N912WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2021050646119Seal · crackedLEFT HAND HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED. / R&R LEFT HAND HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL REF AMM 53-31-31.Apr 29, 2020 · N912WN · Boeing 7377H4 · Horizontal Stabilizer Structure
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