N8628A

Service difficulty reports · 168

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 = 'N8628A' 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 SWAA2025082909593Girt Bar · out of positionAFT ENTRY DOOR SLIDE APPEARS OUT OF POSITION. REPOSITIONED AFT ENTRY DOOR GIRT FLAP IAW AMM 26-66-01.Aug 28, 2025 · N8628A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2025071490326Elec Connector · disconnectedFWD LEFT ENTRY DOOR OVER DOOR EXIT SIGN LIGHT INOPERATIVE. TROUBLESHOOT PER WDM 33-51-12 AND AMM 33-51-06. REPLACED FUSE NO HELP. FUSE BACK TO NORMAL REPLACED BATTERY NO HELP BATTERY BACK TO NORMAL. FOUND D40040P CONNECTOR WAS DISCONNECTED. CONNECTED THE CJul 11, 2025 · N8628A · Boeing 7378H4 · Light System WiringSDR SWAA2025061681718Battery Pack · inoperativeLH FWD 3 PAX AISLE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMER LIGHT POWER SUPPLY BATTERY PACK FOR FWD LEFT AISLE LIGHTS (M2335) PER AMM 33-51-06. OPS TEST GOOD.Jun 14, 2025 · N8628A · Boeing 7378H4 · Emergency LightingSDR SWAA2025050566946Slide · exposedFWD SERVICE DOOR EMERENCY SLIDE EXPOSED<[01] ADJUSTED SERVICE DOOR SLIDE PER S.I.P. (ADJUSTED FLAP VELCRO COVER) HARD SLIDE COVER NOT OPEN OR REMOVED.May 2, 2025 · N8628A · Boeing 7378H4 · Escape SlideSDR SWAA2025030400863Battery Pack · inoperativeAFT OF WING RH AND LH EMERGENCY SLIDE LIGHT IS OUT<[01] REMOVED AND REPLACED M1670/M1671 EMERGENCY BATTERY PACK AND PERFORMED A GOOD INSTALLATION TEST IAW AMM 33-51-06-960-805 AND AMM 33-51-00-710-801.;[02] VERIFIED CORRECTIVE ACTION #1Mar 1, 2025 · N8628A · Boeing 7378H4 · Emergency LightingSDR SWAA2024080221153Slide · noneFA REPORTS FWD SERVICE DOOR SLIDE VELCRO COVER FOR PULL HANDLE TUCKED UP IN SLIDE. INSPECTED FWD SERVICE DOOR SLIDE PULL HANDLE COVER PER AMM 22-66-00. NO DEFECTS NOTED AT THIS TIME.Aug 1, 2024 · N8628A · Boeing 7378H4 · Escape SlideSDR SWAA2024040467303Strip · corrodedALL FWD CARGO CAP STRIPS HAVE CORROSION ON LOWER SURFACE.<[01] REMOVED AND REPLACED CAP STRIPS PER AMM 25-52-10.;[02] C/W INSPECTION AS REQUIRED.Mar 24, 2024 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024040566987Balance Weight · corrodedL/H WING L/E SPLIT SCIMITAR WINGLET BALLAST WEIGHT IS CORRODED.<[01] REMOVED FASTENERS IN WEIGHTS TO F.O.M.;[02] REMOVED WING TIP PANEL ABOVE WEIGHTS TO F.O.M.;[03] CLEANED PER BAC5748 NO CORROSION NOTED OK TO CONTINUE WITH EA M-27-157-00365.;[04] C/W INSPECTIMar 23, 2024 · N8628A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2024040564333Web · crackedR/H WING T/E UPPER SHELF PANEL AT APPROX. OBSS 277 WEB IS CRACKED AT O/B FASTNER. REPLACED WEB (ANGLE) PER SRM 51-40-02. REPLACED WEB (ANGLE) PER SRM 51-40-02. TOP ROW OF RIVETS COMMON TO UPPER SHELF PANEL REQUIRE INSTALLATION . INSTALLED TOP ROW OF RIVETS Mar 16, 2024 · N8628A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2024040564489Fairing · damagedL WING #2 MAIN FLAP TRACK FAIRING TAILCONE HAS ELONGATED FASTENERS HOLES.<[01] ADDED STEP 1.;[02] REMOVED AND REPLACED #2 FLAP TRACK TAIL CONE FARING PER SOPM 20-50-01<BR>01 - REMOVED AND REPLACED PER [SOPM SOPM REPREF NOT FOUND (SOPM REPAIR REFERENCE NOT FOUNMar 16, 2024 · N8628A · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2024040564485Skin · delaminatedLH OTBD AFT FLAP HAS DELAMINATION ON INBD LOWER SURFACE.<[01] REMOVED LH OTBD AFT FLAP.;[02] REMOVED AND REPLACED L/H O/B AFT FLAP PER AMM 27-51-22.;[03] INSPECTED WORK ACCOMPLISHED IN C/A #2 (RII)Mar 16, 2024 · N8628A · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2024040464340Panel · crackedLEFT WING T/E DEFLECTION CONTROL RIB UPPER PANEL ATTACH FLANGE IS CRACKED IN HALF. DISASSEMBLED AND REMOVED DAMAGE PER SRM 57-51-02-2R-3. PERFORMED NDT INSPECTION PER NDT PART 6 51-00-00 PROCEDURE 23. NO DEFECTS NOTED. FLAP PEENED REPAIR AREA AND FABRICATEMar 16, 2024 · N8628A · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2023110617605Handle · brokenFWD SERVICE DOOR GRAB HANDLE BROKEN<[01] REMOVED AND REPLACED FWD SERVICE DOOR GRAB HANDLE REF AMM 52-41-31. SECURITY CHECKED GOOD.Nov 3, 2023 · N8628A · Boeing 7378H4 · Service DoorsSDR SWAA2023091499660Seal · cracked-LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] R&R LH HORIZONTAL STAB FWD UPPER SLIDING SEAL REF. AMM 53-31-31.Sep 13, 2023 · N8628A · Boeing 7378H4 · Horizontal Stabilizer StructureSDR SWAA2023091499661Seal · cracked-RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] R&R RH HORIZONTAL STAB FWD SLIDING SEAL REF. AMM 53-31-31.Sep 13, 2023 · N8628A · Boeing 7378H4 · Horizontal Stabilizer StructureSDR SWAA2023082291453Trunnion · damagedLEFT GEAR FORWARD TRUNNION FITTING'S FOUR BUSHINGS ALL HAVE CADMIUM PLATING MISSING.<[01] REMOVED AND REPLACED BUSHINGS PER. AMM REF. 20-10-02 AND DVI 757-RCB-04-01 (DVI - MLG FWD TRUNNION FITTING (-700 AND -800)).Aug 19, 2023 · N8628A · Boeing 7378H4 · Fuselage, Landing Gear Attach FittingsSDR SWAA2023082291452Trunnion · damagedRIGHT GEAR FORWARD TRUNNION FITTING'S FOUR BUSHINGS ALL HAVE CADMIUM PLATING MISSING.<[01] REMOVED AND REPLACED BUSHINGS PER. AMM REF. 20-10-02 AND DVI 757-RCB-04-01 (DVI - MLG FWD TRUNNION FITTING (-700 AND -800)).Aug 19, 2023 · N8628A · Boeing 7378H4 · Fuselage, Landing Gear Attach FittingsSDR SWAA2023081486627Scuff Plate · crackedFWD CARGO DOOR AFT CORNER SCUFF PLATE IS CRACKED AS MARKED<[01] WELDED CRACKED SCUFF PLATE IN BACK SHOP ON N/R 45067/0000/0001 I.A.W SRM 53-30-15-2R-1;[02] VERIFIED ITEM 1.<BR>AUDIT C/W.;[03] UPDATE MEASUREMENTAug 7, 2023 · N8628A · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2023081484862Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACK M1695 FOR R/H OVERWING EXIT AND CENTER CEILING EXIT LIGHT IS INOP<[01] REMOVED EMERGENCY LIGHT BATTERY PACK M1695 R/H I.A.W AMM 33-51-06-960-805;[02] OK TO INSTALL BATTERY PACK;[03] INSTALLED EMERGENCY LIGHT BATTERY PACK M1695 FOR Aug 2, 2023 · N8628A · Boeing 7378H4 · Emergency LightingSDR SWAA2023081484857Scuff Plate · crackedFWD CARGO FWD CORNER SCUFF PLATE REQUIRES WELD REPAIR TO FIT SKIN REPAIR PROFILE<[01] REPAIRED FWD CARGO FWD CORNER SCUFF PLATE ON SHOP W/O 45067/0000/0002 IAW SRM 53-30-15-2R-1;[02] VERIFIED STEP 1<BR>AUDIT C/WAug 1, 2023 · N8628A · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2023081484858Scuff Plate · crackedFWD CARGO CENTER SCUFF PLATE REQUIRES WELD REPAIR TO FIT SKIN REPAIR PROFILE<[01] REPAIRED FWD CARGO CENTER SCUFF PLATE ON SHOP W/O 45067/0000/0004 IAW SRM 53-30-15-2R-1;[02] VERIFIED STEP 1<BR>AUDIT C/WAug 1, 2023 · N8628A · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2023040322573Power Supply · inoperativeSEVERAL EMERGENCY LIGHTS @ FWD ENTRY DOOR INOP.<[01] R&R FWD ENTRY DOOR SIDE EMERGENCY LIGHT POWER SUPPLY REF. AMM 33-51-06 OPS CHECKS NORMALMar 31, 2023 · N8628A · Boeing 7378H4 · Emergency LightingSDR SWAA2023030812865Slide · out of adjustL1 DOOR SLIDE CAME OUT OF CASE<[01] REINSTALLED L1 DOOR SLIDE IN CASE PER MT 725-61-06Mar 5, 2023 · N8628A · Boeing 7378H4 · Escape SlideSDR SWAA2023011791875Megaphone · inoperativeFORWARD MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-64-00.Jan 15, 2023 · N8628A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2022122785178Lamp · inoperativeLEFT WING FWD O/W EXIT DOOR EXTERIOR LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-04. OPS CHECKED GOOD.Dec 24, 2022 · N8628A · Boeing 7378H4 · Emergency LightingSDR SWAA2022111068855Slide · out of adjustAIRCRAFT LEFT AFT EMERGENCY SLIDE EXPOSED / [01] NO DEFECTS NOTED IAW M/M 25-66-01Nov 7, 2022 · N8628A · Boeing 7378H4 · Escape SlideSDR SWAA2022041995045Light · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY M1672 INOP / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1672 AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION #1Apr 17, 2022 · N8628A · Boeing 7378H4 · Emergency LightingSDR SWAA2022041995044Light · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY M1695 INOP / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1695 AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION #1Apr 17, 2022 · N8628A · Boeing 7378H4 · Emergency LightingSDR SWAA2022041995043Light · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY M1670 INOP / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1670 AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION #1Apr 17, 2022 · N8628A · Boeing 7378H4 · Emergency LightingSDR SWAA2022041989148Floor Panel · pulledPASSENGER CABIN FLOOR PANEL HAS PULLED STRANDS ON UPPER SURFACE SKIN DAMAGE IS ON FLOOR PANEL 221BF / [01] IDENTIFIED PASSENGER CABIN FLOOR PANEL 221BF IAW SRM 53-00-50-0I-1 FIGURE 2; SHEET 1; TABLE 2. <BR>DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRMMar 28, 2022 · N8628A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022041989149Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 231FF HAS PULLED STRANDS ON UPPER SURFACE / [01] IDENTIFIED PASSENGER CABIN FLOOR PANEL 231FF IAW SRM 53-00-50-0I-1 FIGURE 3; SHEET 1; TABLE 3.<BR>DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR 4F.<BR>REPAIMar 28, 2022 · N8628A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022042188673Floor Panel · corrodedPASSENGER CABIN FLOOR PANEL 221CF; HAS NUMEROUS CORRODED INSERTS. / REMOVED (17 EA) CORRODED THROUGH INSERTS ALONG THE PERIMETER AND CENTER OF PANEL IAW SRM 53-00-50-2R-0 PARA 5. B. (2) <BR><BR>FOUND CORE DAMAGE AT EDGE OF PANEL AT INSERT LOCATIONS P1; P2; P10Mar 27, 2022 · N8628A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022042188676Floor Panel · corrodedPASSENGER CABIN FLOOR PANEL 221AF; HAS SEVERAL CORRODED INSERTS / REMOVED SEVERAL CORRODED INSERTS IAW SRM 53-00-50-2R-0 PARA 5. B. (2) <BR><BR>FOUND CORE DAMAGE AT EDGE AT INSERT LOCATION P23. DAMAGES IS OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F. Mar 27, 2022 · N8628A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022042188677Floor Panel · corrodedPASSENGER CABIN FLOOR PANEL 222AF HAS SEVERAL CORRODED INSERTS / REMOVED (12 EA) CORRODED THROUGH INSERTS ALONG THE INBD AND AFT EDGES IAW SRM 53-00-50-2R-0 PARA 5. B. (2) FOUND DAMAGE ON TOP FACESHEET AT INSERT LOCATIONS P2; P3; P34 AND P35. DAMAGES IS OUT OFMar 27, 2022 · N8628A · Boeing 737 · Fuselage Floor PanelSDR SWAA2022042088222Channel · corrodedCORROSION ON FWD ENTRY DOOR MOPSILL STA 303-338; LBL 53-LBL 59; WL 208. / [01] FOUND FWD ENTRY MOPSILL TO HAVE 100% MATERIAL LOSS STA 303; LBL 53; WL 208. OUT OF LIMITS PER SRM 53-10-15-1A-1; SRM 51-10-02-0G-0; REPLACEMENT OF PART.;[02] VERIFIED CORRECTIVE ACTMar 25, 2022 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022042088218Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA 948-949; RBL 50-52; WL 208. / [01] REMOVED AFT LAV FLOOR SUPPORT BS 948 RBL 52 IAW SRM 51-40-02-0G-0.;[02] VERIFIED APPLICABILITY OF SRM 53-70-51-1A-1;[03] REMOVED CORROSION ON FLOOR SUPPORT BS 948-949 RBL 50-52 WL 208 AT AREA OFMar 25, 2022 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022042088217Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA 949; RBL 26.5; WL 208. / [01] REMOVED AFT LAV FLOOR MOUNT BS 947 RBL 25 IAW SRM 51-40-02-0G-0.;[02] VERIFIED APPLICABILITY OF SRM 53-70-15-1A-1;[03] REMOVED CORROSION ON FLOOR SUPPORT BS 949 RBL 26.5 WL 208 AT EDGE REMOVED MATERIMar 25, 2022 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022042088215Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA 948.5; 951; LBL 24; WL 208. / [01] VERIFIED APPLICABIITY OF SRM 53-70-15-1A-1;[02] REMOVED CORROSION ON FLOOR SUPPORT BS 948.5; 951 LBL 24 WL 208 AT AREA OF 1'X0.5' REMOVED MATERIAL .060' FOUND TO BE OUT OF LIMITS DEPTH GAUGE USEMar 25, 2022 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022042088230Floorbeam · corrodedCORROSION ON 344 FLOORBEAM FWD UPPER FLANGE AT RBL 1; WL 208. / [01] REMOVED CORROSION ON 344 FLOORBEAM; FWD UPPER FLANGE AT RBL 1; WL 208 PER SRM 51-10-02-0G-0. AREA BLENDED IS 1.7' BY 1.2' PER SRM 51-10-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION STEP 1 TO BE CMar 25, 2022 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022042088225Floorbeam · corrodedCORROSION ON UNDERSIDE OF FWD UPPER FLANGE OF 947 FLOORBEAM; LBL 53; WL 208. / [01] REMOVED CORROSION ON TOP AND UNDERSIDE ON FWD FLANGE OF 947 FLOORBEAM; LBL 53; WL 208. AREA BLENDED ON TOP IS 1' BY 1'; AREA BLENDED ON BOTTOM IS 1' BY 1.4'; OVERSIZED FLOOR PAMar 25, 2022 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022042088232Channel · corrodedCORROSION ON FWD SERVICE DOOR MOPSILL STA 294-332; RBL 52-55; WL 208. / [01] REMOVED CORROSION ON FWD SERVICE DOOR MOPSILL STA 294-332; RBL 52-55; WL 208. MAX MATERIAL REMOVED WAS .027' 1' BY 2' FROM .080'. OUT OF LIMITS PER SRM 53-10-15-1A-2; SRM 51-10-02-0G-Mar 25, 2022 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022042088223Support · corrodedCORROSION ON FWD ENTRY GIRT BAR SUPPORT FITTING STA 312; LBL 53; WL 209. / [01] SRM 53-10-15-1A-1 IS NOT APPLICABLE FOR GIRT BAR FITTING SUPPORT; OUT LIMITS AND REPLACEMENT OF PART PER SRM 51-10-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] MEASURED DEPTH WMar 25, 2022 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022042088231Angle · corrodedCORROSION ON FWD ENTRY MOPSILL TO SCUFFPLATE ATTACH ANGLE STA 315-338; LBL 60; WL 209. / [01] REMOVED CORROSION ON FWD ENTRY MOPSILL TO SCUFFPLATE ATTACH ANGLE STA 315-338; LBL 60; WL 209. MAX MATERIAL REMOVED WAS .023' 1' BY 2' FROM .080'. OUT OF LIMITS PER SMar 25, 2022 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022042088233Angle · corrodedCORROSION ON FWD SERVICE DOOR MOPSILL TO SCUFFPLATE ATTACH ANGLE STA 309-319; RBL 60; WL 209. / [01] REMOVED CORROSION ON FWD SERVICE DOOR MOPSILL TO SCUFFPLATE ATTACH ANGLE STA 309-319; RBL 60; WL 209. MAX MATERIAL REMOVED WAS .034' 1' BY 3' FROM .090'. OUT OMar 25, 2022 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022042088234Floorbeam · corrodedCORROSION ON 328 FLOORBEAM; FWD UPPER FLANGE; RBL 22; WL 208. / [01] REMOVED 3 EA SEAT TRACK FASTENERS AT 328 FLOOR BEAM UPPER FLANGE; RBL 22; WL 208 FOR ACCESS PER SRM 51-40-02-0G-0.;[02] REMOVED CORROSION ON 328 FLOORBEAM UPPER FLANGE; RBL 22; WL 208 PER SRMMar 25, 2022 · N8628A · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2022041988221Support Angle · crackedCRACKED INTERCOSTAL UPPER SUPPORT ANGLE STA 380-400; RBL 9; WL 208. / [01] REMOVED DAMAGED INTERCOSTAL UPPER SUPPORT ANGLE STA 380-400; RBL 9; WL 208 PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL UPPER SUPPORT ANGLE STA 380-400; RBL 9; WL 208Mar 25, 2022 · N8628A · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2022041988228Attach Angle · crackedCRACKED INTERCOSTAL UPPER ATTACH ANGLE STA B380-400; LBL 13; WL 208. / [01] REMOVED; LOCATED AND DRILLED NEW INTERCOSTAL UPPER ATTACH ANGLE BS380 - BS400 LBL 13 WL 208 IAW SRM 51-40-05-0G-0 AND DWG 143A5400. OK TO INSTALL;[02] VERIFIED CORRECTIVE ACTION 1.<BR>Mar 25, 2022 · N8628A · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2022041988227Intercostal · crackedCRACKED INTERCOSTAL STA 277-294; RBL 1; WL 208. / [01] REMOVED INTERCOSTAL STA 277-294 RBL 1 WL 208 IAW SRM 51-40-02-0G-0 ITEM 7 DWG N 141A5400;[02] LOCATED AND DRILLED NEW INTERCOSTALL P/N 141A5410-3 STA 277-294 RBL 1 WL 208 IAW SRM 51-40-02-0G-0 ITEM 7 DWG NMar 25, 2022 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022041988220Intercostal · crackedCRACKED INTERCOSTAL STA 344-360; LBL 11; WL 208. / [01] REMOVED DAMAGED INTERCOSTAL STA 344-360; LBL 11; WL 208 PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL STA 344-360; LBL 11; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG# 141A5400;Mar 25, 2022 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022041988229Intercostal · crackedCRACKED INTERCOSTAL UPPER STTACH ANGLE STA 344-360; LBL 50; WL 208. / [01] UPON INVESTIGATION FOUND CRACKED INTERCOASTAL UPPER ATTACH ANGLE IS LOCATED AT BS 380 - 400; LBL 50; WL 208;[02] VERIFIED CRACK TO BE AT BS 380 TO BS 400; LBL 50; NOT AT BS 344-360 LBL Mar 25, 2022 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous Structure
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