N962WN

Service difficulty reports · 194

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 = 'N962WN' 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 SWAA2021080295684Bulkhead Web · damagedL/H VAPOR BARRIER FASTENER ATTACH HOLES ON O/B END (APPROX. 39) ARE OVERSIZED ; / PART/MATERIAL IDENTIFIED PER SRM 57-10-10-0I-2 FIG 2 TABLE 2 ITEM 4 .<BR>30' OF THE O/B EDGE BAND OVERSIZE HOLES EXCEED THE ALLOWABLE LIMITS AS GIVEN IN SRM 57-10-10-1A-2 PARA 4 Jul 14, 2021 · N962WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2021080394625Skate Angle · chafedCHAFE DAMAGE ON THE R/H VERTICAL STAB TO FUSELAGE SKATE ANGLES / [01] REMOVED R/H SKATE ANGLES IAW SRM 51-40-02; [02] LOCATED; DRILLED AND COUNTERSINK NEW L/H SKATE ANGLE P/N 148A8310U4 PO#823628 /1 IAW SRM 51-40-05;SRM 51-40-08 AND DWG 148A8300 REV.A; [03] NOJul 13, 2021 · N962WN · Boeing 7377H4 · Vertical StabilizerSDR SWAA2021080394626Skate Angle · corrodedCHAFE DAMAGE ON THE L/H VERTICAL STAB TO FUSELAGE SKATE ANGLES / [01] REMOVED LH SKATE ANGLES PER SRM 51-40-02.; [02] LOCATED; DRILLED AND COUNTERSINK NEW L/H SKATE ANGLE P/N 148A8310U3 PO#829514 /1 IAW SRM 51-40-05;SRM 51-40-08 AND DWG 148A8300 REV.A; [03] NOJul 13, 2021 · N962WN · Boeing 7377H4 · Vertical StabilizerSDR SWAA2021080394611Floorbeam · corrodedCORROSION ON FLIGHT DECK LATERAL BEAM BS 259.5; LBL 1; WL 208 (MARKED) ; / [01] REMOVED CORROSION IN A 1.3' X 0.4' AREA; MAX DEPTH .005' PER SRM 51-10-02-0G-0; MEASURED WITH CAL ID: ATS2472 SN: UNKNOWN CAL DATE: 06/2021. ORIGINAL THICKNESS IS .094' PER DWG 141Jul 13, 2021 · N962WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2021080294610Beam · corrodedCORROSION ON FLIGHT DECK LATERAL BEAM BS 259.5; LBL 5; WL 208 (MARKED) ; / [01] REMOVED CORROSION IN A 1.2' X 0.6' AREA; MAX DEPTH OF BLENDOUT .006' PER SRM 51-10-02-0G-0; MEASURED WITH MICROMETER CAL ID: IS000461 S/N: 67126205 CAL DATE: 01/2021. ORIGINAL THICJul 13, 2021 · N962WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2021080294621Beam · corrodedCORROSION ON FLIGHT DECK LATERAL BEAM BS 270; RBL 2.5; WL 208 (MARKED) ; / [01] REMOVED CORROSION IN A 1.5' X 0.6' AREA; MAX DEPTH .008' PER SRM 53-10-51-1A-1;FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1.; [02] REMOVED NUTPLATE AT BS 270; RBL 2.5; WL 208 PEJul 13, 2021 · N962WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2021080294609Attach Angle · damagedREJECT- L/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE DAMAGE REMOVAL CUTLINE IS NOT TRIMMED AS SHOWN IN SRM 57-10-10-2R-5; FIGURE 202 REPAIR 5 ; / [01] CUT OUT L/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE DAMAGE IAW SRM 57-10-10-2R-5; [02] VERIFIED; [03] VERIFIEDJul 13, 2021 · N962WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2021080394613Sidewall Support · corrodedCORROSION BS727E +6- +12 LBL 24 WL157 FLOOR TO SIDEWALL SUPPORT / [01] REMOVED CORROSION FROM L/H ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+6 MEASURED 2'L X 1'W AND 0.020' DEEP. ORIGINAL THIKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2; [02] VERIFIEJul 12, 2021 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080294604Plate · corrodedCORROSION BS767 RBL 24 WL157 PLATE THAT TIES TOP OF FRAME TO FWD SHIELD CORRODED / [01] REMOVED PLATE COMMON TO FRAME AT BS 767 RBL 24 WL 157 PER SRM 51-40-02.; [02] VERIFIED REMOVAL; [03] NO ALLOWABLE DAMAGE PER SRM. REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-Jul 12, 2021 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080294606Shield · corrodedCORROSION BS767-787 RBL24 WL157 SHIELD UPPER SURFACE / [01] REMOVED AFT CARGO BAY SHIELD BS767-787 RBL24 WL157 IAW SRM 51-40-02; [02] NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM FOR ACB FWD SHIELD; PART TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02; [03] VERIFIEDJul 12, 2021 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080294605Intercostal · corrodedCORROSION BS767-787 TR25R INTERCOSTAL UPPER CHORD CORRODED IN SEVERAL PLACES COMMON TO NUT PLATES / [01] REMOVED CORROSION ON INTERCOSTAL UPPER CHORD AT BS 767 TO BS 787; RBL 25 ; WL 157 ; WORK AREA IS 18.5' X 0.950' X 0.009' ; ORIGINAL THICKNESS IS 0.050' ; RJul 12, 2021 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080294598Support · corrodedCORROSION BS727C+14-18 RBL 24 WL157 FLOOR TO SIDEWALL SUPPORT / [01] REMOVED ACB FLOOR TO SIDEWALL SUPPORT R/H FROM BS 727-767 RBL 24 WL 157 PER SRM 51-40-02.; [02] VERIFIED REMOVAL; [03] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT AT BS 727C+14 RBL23 MEAJul 12, 2021 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080294617Retainer · corrodedCORROSION BS790 RBL24 WL157 ON NUT PLATE RETAINER / [01] REMOVED CORROSION ON NUT PLATE RETAINER AT BS 790 ; RBL 24 ;WL 157 ; WORK AREA IS 5.0' X 0.900' X 0.005 ; ORIGINAL THICKNESS IS 0.040 ; REMAINING THICKNESS IS 0.035 ; FOUND TO BE OUT OF LIMITS IAW SRM 53Jul 12, 2021 · N962WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2021080294599Support · corrodedCORROSION BS727C+10 LBL 24 WL157 FLOOR TO SIDEWALL SUPPORT / [01] REMOVED ACB FLOOR TO SIDEWALL SUPPORT L/H FROM BS 727-787 LBL 24 WL 157 PER SRM 51-40-02.; [02] VERIFIED REMOVAL; [03] REMOVED CORROSION FROM ACB FLOOR TO SIDEWALL SUPPORT BS727C+10 LBL24 MEASURJul 12, 2021 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080294607Web · corrodedCORROSION BS792-810 RBL28 WL157 UPPER SURFACE OF SUB THRESHOLD CORRODED IN SEVERAL PLACES / [01] REMOVED ACB SUBTHRESHOLD WEB BS 792-847 RBL 21-28 WL 157 PER SRM 51-40-02; [02] VERIFIED REMOVAL; [03] REMOVED CORROSION ON SUB THRESHOLD AT BS792-810 RBL28 WL157;Jul 12, 2021 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080293322Attach Angle · crackedL/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE CRACKED LBL 40 WL 164 ; / CUT OUT DAMAGE ANGLE IAW SRM 57-10-10-2R-5 FABRICATED; LOCATED AND DRILLED REPAIR PARTS IAW SRM 57-10-2R-5. MATERIAL ID:<BR>ITEM [1] 2024T3#0.063 CLAD; LOT #1457316-1 <BR>ITEM[2] 2024T3#0.07Jul 10, 2021 · N962WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2021080293269Floor Panel · damagedFWD CARGO BAY FLOOR PNL 120AF DAMAGED ; / [01] FABRICATED NEW FCB FLOOR PANEL 120AF FROM 090 CONOLITE; LOT# 1454533-1 PER AMM 25-52-01-201-801; [02] ADDED DWG REFERENCE 453A1610; [03] VERIFIED FABRICATION OF NEW PANEL PER AMM 25-52-01-201-801 AND DWG 453A1610Jul 9, 2021 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080293263Floor Panel · damagedAFT CARGO BAY FLOOR PNL 140AF DAMAGED ; / [01] FABRICATED NEW ACB FLOOR PANEL 140AF FROM 090 CONOLITE; LOT# 1458090-1 PER AMM 25-52-01-201-801 AND DWG 453A2610; [02] ADDED MEASUREMENT INFORMATION; [03] VERIFIED FABRICATION OF NEW PANEL PER AMM 25-52-01-201-801Jul 9, 2021 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080293264Floor Panel · damagedAFT CARGO BAY FLOOR PNL 140BF DAMAGED ; / [01] FABRICATED NEW ACB FLOOR PANEL 140BF FROM 090 CONOLITE; LOT# 1458090-1 PER AMM 25-52-01-201-801 AND DWG 453A2610; [02] ADDED MEASUREMENT INFORMATION; [03] VERIFIED FABRICATION OF NEW PANEL PER AMM 25-52-01-201-801Jul 9, 2021 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080293270Floor Panel · damagedFWD CARGO BAY FLOOR PNL 120CF DAMAGED ; / [01] FABRICATED NEW FCB FLOOR PANEL 120CF FROM 090 CONOLITE; LOT# 1458090-1 PER AMM 25-52-01-201-801 AND DWG 453A1610; [02] ADDED MEASUREMENT INFORMATION; [03] VERIFIED FABRICATION OF NEW PANEL PER AMM 25-52-01-201-801Jul 9, 2021 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080293284Floor Panel · delaminatedFLOOR PANEL 242CF - UPPER FORWARD L/H CORNER IS DELAMINATED ; / [01] IDENTIFIED FLOOR PANEL 242CF IAW SRM 53-00-50-0I-1 FIGURE 4; SHEET 1; TABLE 4. DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR 4F. DUE TO THE EXTENT OF DAMAGE OPTED TJul 9, 2021 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080293285Floor Panel · damagedFLOOR PANEL 242BF - LOWER AFT L/H CORNER IS DAMAGED ; / [01] IDENTIFIED FLOOR PANEL 242BF IAW SRM 53-00-50-0I-1 FIGURE 4; SHEET 1; TABLE 4. DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR 4F. DUE TO THE EXTENT OF DAMAGE OPTED TO FABRICJul 9, 2021 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080293286Floor Panel · pulledFLOOR PANEL 231XF - UPPER SKIN HAS MULTIPLE STRANDS PULLED STARTING FROM LEADING EDGE OF PANEL ; / [01] IDENTIFIED FLOOR PANEL 231XF IAW SRM 53-00-50-0I-1 FIGURE 4; SHEET 1; TABLE 4. DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR 4F. Jul 9, 2021 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080293267Floorbeam · crackedFLOOR SUPPORT BS 540; RBL 25 - BL 0; WL 208 CRACKED AT I/B FASTENER HOLE ; / [01] REMOVED AND INSTALLED FLOOR SUPPORT AT BS 540 RBL 25 TO BL 0 WL 208 PER SRM 51-40-02 AND BOEING DWG 143A0060. FLOOR SUPPORT STILL REQUIRES MATCH DRILL OF FLOOR PANEL FASTENER HOLJul 9, 2021 · N962WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2021080293282Floorbeam · crackedFLOOR SUPPORT BS 540; LBL 25 - BL 0; WL 208 CRACKED AT I/B FASTENER HOLE ; / [01] REMOVED AND INSTALLED FLOOR SUPPORT AT BS540 LBL 25 TO BL 0 WL 208 PER SRM 51-40-02 AND BOEING DWG 143A0060. FLOOR SUPPORT STILL REQUIRES MATCH DRILL OF FLOOR PANEL FASTENER HOLEJul 9, 2021 · N962WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2021080292521Bulkhead · crackedCRACKED LOWER L/H COMPOSITE BULKHEAD AT BS663 LBL35 WL149. ; / [01] DAMAGE IS OUT OF ALLOWABLE LIMITS PER SRM 57-10-10-1A-2; PAR 1.C. DAMAGE TO BE REPAIRED PER SRM 51-70-04-2R-10 AS DIRECTED BY SRM 57-10-10-2R-2; PAR 1.B AND NOTE VERIFIED INSTALLED REPAIR PLIEJul 7, 2021 · N962WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2021032257076Handle · looseFORWARD SERVICE DOOR HANDLE IS LOOSE / TIGHTENED BOLTS ON FWD SERV DOOR HANDLE IAW MM 52-41-31 OPS CKS OKMar 18, 2021 · N962WN · Boeing 7377H4 · Galley DoorsSDR SWAA2020110227084Battery Pack · inoperativeEMERGENCY LIGHTS AT LT EXIT ROW INOPERABLE. REMOVED AND REPLACED BATTERY PACK AT ROW 15 ABC FOR EMERGENCY LIGHTS, IAW AMM 33-51-06.Oct 29, 2020 · N962WN · Boeing 7377H4 · Emergency LightingSDR SWAA2020032332187Light · inoperativeSIDEWALL LIGHT OUT AT 11 ABC (EMERGENCY EXIT). / RELAMPED PASSENGER CABIN SIDEWALL LIGHT AT 11ABC IAW AMM 33-51-11.Mar 17, 2020 · N962WN · Boeing 7377H4 · Emergency LightingSDR SWAA2020031942586Light · inoperativeSIDEWALL LIGHT OUT AT 11 ABC (EMERGENCY EXIT). RELAMPED PASSENGER CABIN SIDEWALL LIGHT AT 11ABC IAW AMM 33-51-11.Mar 17, 2020 · N962WN · Boeing 7377H4 · Emergency LightingSDR SWAA2019072435271Connector · defectiveR2 DOOR HEADER EMERGENCY EXIT LIGHT INOP AT M1673. R&R CONNECTOR D10746 IAW SWPM AND WDM.Jul 21, 2019 · N962WN · Boeing 7377H4 · Light System WiringSDR SWAA2019072435262Fuse · blownR2 DOOR HEADER EMERGENCY EXIT LIGHT INOP AT M1673. R&R FUSES IAW SWPM AND WDM.Jul 21, 2019 · N962WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022031273236Support Angle · crackedLEFT MLG WHEEL WELL STA 663 LBL25 WL 150; VERTICAL SUPPORT ANGLE IS CRACKED AT BOTTOM END. / REMOVED & REPLACED LEFT MLG WHEEL WELL STA 663 LBL 25 WL 150 VERTICAL SUPPORT STIFFENER IAW SRM 51-40-02-0G-0; 51-40-05-0G-0 & DWG 111A1000 REV-Jul 13, 2019 · N962WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2022031173209Support Bracket · crackedPASSENGER CABIN AT R1 DOOR CUTOUT STA 306-326 RBL 60; THRESHOLD SUPPORT BRACKET IS CORRODED. / BLENDED CORROSION WITH A MATERIAL LOSS OF .012' IS FOUND TO BE 'OUT OF LIMITS' AS PER B 737-700 SRM 53-10-15-1A-2 REMOVED AND REPLACED ATTACH ANGLE AS PER B 737-700 Jul 11, 2019 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022031173212Angle · corrodedAFT CARGO COMP.RH Z-ANGLE HAS CORROSION AROUND SEVERAL FASTNER HOLES 727-727E / REMOVED AND REPLACED RH Z ANGLE FROM STA 727-767 ON SA-M 112 #X982183 IAW SRM 51-40-02-0G-0 AND DWG 146A7502 REV. -Jul 11, 2019 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022031173213Angle · corrodedAFT CARGO COMP.RH Z-ANGLE HAS CORROSION AROUND SEVERAL FASTNER HOLES STA.727E-767 / REMOVED AND REPLACED RH Z ANGLE FROM STA 727-767 ON SA-M 112 #X982183 IAW SRM 51-40-02-0G-0 AND DWG 146A7812 REV.-Jul 11, 2019 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022031173214Strap · corrodedAFT CARGO COMP.FLOOR BOARD STRAP CORRODED AROUND FASTNER HOLES STA. 767 / REMOVED AND REPLACED AFT CARGO FLOOR BOARD STRAP ASSEMBLY AT STA 767 IAW SRM 51-40-02-0G-0 AND DWG 146A 7500 RESTORED CIC TO DISTURBED AREA IAW AMM 51-21-91-620-802 PN: 146A9401-4 ATAG: Jul 11, 2019 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022031173226Floor Panel · crackedFLOOR PANEL 242XF CRACKED / INSTALLED NEW FLOOR PANEL; WORK ACCOMPLISHED ON J.PANEL CARD - 241-CLOSEJul 11, 2019 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2019071935135Threshold · corrodedAFT CARGO COMPARTMENT THRESHOLD WEB CORRODED AROUND SEVERAL FASTENER HOLES BETWEEN BS. 794 TO BS. 847, BETWEEN RBL 20 TO RBL 24. R&R WEB IAW SRM, AMM & DWG.Jul 11, 2019 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2019071835038Crease Beam · corrodedL2 DOOR CUTOUT CREASE BEAM INNER CHORD CORRODED BETWEEN BS. 965 TO BS. 985, LBL 53. R&R CREASE BEAM INNER CHORD IAW DWG AND SRM.Jul 11, 2019 · N962WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2019071835037Crease Beam · corrodedR2 DOOR CUTOUT CREASE BEAM INNER CHORD CORRODED BETWEEN BS. 960 TO BS. 985, RBL 53. R&R INNER CHORD IAW SRM AND DWG.Jul 11, 2019 · N962WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2019071834946Floorboard · damagedPASSENGER CABIN FLOORBOARD 221EF HAS UPPER PLY DAMAGED, BETWEEN BS. 270 TO BS. 420. REPAIRED FLOORBOARD PANEL IAW SRM.Jul 11, 2019 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2019071834948Crease Beam · corrodedL1 DOOR INNER CREASE BEAM ANGLE CORRODED ON UPPER SURFACE AT BS. 303.9, LBL 53. R&R L1 DOOR INNER CHORD (CREASE BEAM) PER SRM AND DWG.Jul 11, 2019 · N962WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2019071834945Floorboard · damagedPASSENGER CABIN FLOORBOARD 221DF HAD UPPER PLY AND INSERT DAMAGE BETWEEN BS. 270 TO BS. 420. REPAIRED FLOORBOARD IAW SRM.Jul 11, 2019 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2019071634928Floor Support · crackedLONGITUDINAL FLOOR SUPPORT CRACKED AT BS. 312+4.5, RBL 33.5. R&R FLOOR SUPPORT ANGLE IAW SRM & DWG.Jul 11, 2019 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2019071634927Floor Support · crackedLONGITUDINAL FLOOR SUPPORT CRACKED AT BS. 277+7.5, BL 0. R&R FLOOR SUPPORT IAW DWG, SRM, & AMM.Jul 11, 2019 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2019071634926Floorboard · damagedAFT CABIN FLOORBOARD 242RF HAD UPPER PLY DAMAGE, BETWEEN BS. 887 TO BS. 1016. REPAIRED FLOORBOARD 242RF IAW SRM.Jul 11, 2019 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2019071634925Floorboard · damagedPASSENGER CABIN FLOOR BOARD 221BF HAD UPPER PLY DAMAGE, BETWEEN BS. 270 TO BS. 420. REPAIRED UPPER FACE SHEET IAW SRM.Jul 11, 2019 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022031173194Seal · crackedRIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL IS CRACKED / REMOVED RIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL AND FWD AND AFT CENTER TRACK STRIP IAW 737 AMM 53-31-31-000-802 RECEIVED AND VERIFIED NEW PART P/N 181A8025-2 IAW IPC 53-31-31-03 INSJul 10, 2019 · N962WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2022031173196Seal · crackedLH HORIZONTAL STAB; UPPER FWD SLIDING SEAL IS CRAKED AT FWD SIDE ALONG GUIDE TRACK / REMOVED CRACKED LH HORIZONTAL STAB UPPER FORWARD SLIDING SEAL IAW 737 SRM 51-40-02-0G-0 AND 737 AMM 53-31-000-802. RECEIVED AND VERIFIED NEW SLIDING SEAL IAW 737 IPC 53-31-31-Jul 10, 2019 · N962WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
Back to N962WN