N8623F

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 = 'N8623F' 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 SWAA2022013159073Angle · corrodedR/H CABIN R1 DOOR CREASE BEAM O/B ATTACH ANGLE CORRODED ; / [01] REMOVED CORROSION FROM ATTACH ANGLE AND VERIFIED MATERIAL LOSS ( FOUND OUT LIMITS THICKNESS REMOVED MORE THAN 50% ) IAW SRM 53-10-15-1A-2.; [02] REMOVED ATTACH ANGLE IAW SRM 53-10-15-1A-2: SRM 51Jan 6, 2022 · N8623F · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2022013158672Strip · corrodedDOT#03-186 AFT PIT 2EA RH CAP STRIPS CORRODED ; / [01] REMOVED CORROSION AND VERIFIED WITH 10X MAGINIFIER ALL CORROSION REMOVED IAW SRM 51-10-02-0G-0; [02] LIMITS VERIFIED; OUT OF LIMITS DUE TO NO PUBLISHED LIMITS IN SRM<BR>BOTH CAPSTRIPS ARE SAME ORIGINAL THIJan 5, 2022 · N8623F · Boeing 7378H4 · Cargo CompartmentsSDR SWAA2022013158673Strip · corrodedDOT#04-186 AFT PIT LH CAP STRIP #4 CORRODED ; / [01] REMOVED CORROSION AND VERIFIED WITH 10X MAGINIFIER ALL CORROSION REMOVED IAW SRM 51-10-02-0G-0; [02] LIMITS VERIFIED; OUT OF LIMITS DUE TO NO PUBLISHED LIMITS IN SRM<BR>ORIGINAL THICKNESS .063'<BR>REMAINING Jan 5, 2022 · N8623F · Boeing 7378H4 · Cargo CompartmentsSDR SWAA2022013158674Strip · corrodedDOT#05-186 AFT PIT LH CAP STRIP #3 CORRODED ; / [01] REMOVED CORROSION AND VERIFIED WITH 10X MAGINIFIER ALL CORROSION REMOVED IAW SRM 51-10-02-0G-0; [02] LIMITS VERIFIED; OUT OF LIMITS DUE TO NO PUBLISHED LIMITS IN SRM<BR>ORIGINAL THICKNESS .063'<BR>REMAINING Jan 5, 2022 · N8623F · Boeing 7378H4 · Cargo CompartmentsSDR SWAA2022013158696Floor Panel · pulledA-061 DOT 016. CABIN FLOORBOARD 221BF UPPER SURFACE FIBERS PEELING ; / [01] EVALUATED AND FOUND DAMAGED FIBERS ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED AREA FOR REPAIR IAW SRM 53-00-50-2RJan 5, 2022 · N8623F · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022013158695Floor Panel · brokenA-061 DOT 015. CABIN FLOORBOARD 221BF AFT INBD CORNER TIP BROKE ; / [01] EVALUATED AND FOUND DAMAGED FIBERS ON UPPER AND LOWER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED AREA FOR REPAIR IAW SRM 53-0Jan 5, 2022 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022013158698Floor Panel · damagedA-061 DOT 017. CABIN FLOORBOARD 221AF R/H OUTBD EDGE DAMAGED ; / [01] EVALUATED AND FOUND EDGE DAMAGE WITH DAMAGED FIBERS TO UPPER FACE SHEET AND REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53Jan 5, 2022 · N8623F · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022013158694Floor Panel · crackedA-061 DOT 018. CABIN FLOOR BOARD 222CF FACE SHEET CRACKED UPPER SURFACE ; / [01] EVALUATED AND FOUND MULTIPLE AREAS OF DAMAGED FIBERS TO UPPER FACE SHEET AND REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACJan 5, 2022 · N8623F · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022013158938Floor Panel · pulledCABIN FLOOR PANEL 231CF; UPPER SURFACE HAS PULLED FACE SHEET PLIES. ; / [01] EVALUATED AND FOUND DAMAGED FIBERS ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1 <BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2RJan 5, 2022 · N8623F · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022013158680Floorbeam · corrodedA-061 DOT 007. AFT CABIN FLOOR BEAM AT STA 986 RBL 15 TO RBL 18 WL 207 HAS CORROSION AT 2EA FASTENER HOLES LOWER SURFACE ; / [01] REMOVED DAMAGE FROM LOWER SURFACE OF 986 FLOOR BEAM AT 2EA FASTENER HOLES IAW SRM 51-10-02-0G-0.<BR>VERIFIED MATERIAL LOSS; ORIGINJan 5, 2022 · N8623F · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2022013158699Angle · crackedCUSTOMER REQUEST: RIGHT HAND PACK BAY HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STATION 663 RBL 10 IS CRACKED AT FASTENER OUTBOARD OF KEEL BEAM VERTICAL ANGLE. ; / [01] REMOVED DAMAGED SECTION OF ANGLE AND PERFORMED DVI OF REPAIR AREA; NO DEJan 5, 2022 · N8623F · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2022013158700Angle · crackedCUSTOMER REQUEST: LEFT HAND PACK BAY HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STATION 663 LBL 10 IS CRACKED AT FASTENER OUTBOARD OF KEEL BEAM VERTICAL ANGLE. ; / [01] REMOVED DAMAGED SECTION OF ANGLE AND PERFORMED DVI OF REPAIR AREA; NO DEFJan 5, 2022 · N8623F · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2022012858685Floorboard · pulledPASSENGER CABIN FLOORBOARD 241E UPPER SURFACE HAS PULLED FIBERS. A224-10 ; / [01] EVALUATED DAMAGE TO CABIN FLOORBOARD 241E; UPPER SURFACE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1. NO DELAMINATION NOTED.<BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737Jan 5, 2022 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022012858692Floorboard · pulledPASSENGER CABIN FLOORBOARD 242D UPPER SURFACE HAS PULLED FIBERS. A224-17 ; / [01] VERIFIED PANEL 242D TO HAVE DAMAGE TO UPPER PLIES AND 2 INSERTS DAMAGED. PANEL IS WITHIN LIMITS AND REPAIRABLE I/A/W BOEING 737-800 SRM 53-00-50-2R-0 (REPAIR-1) & SRM 53-00-50-2RJan 5, 2022 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022012858689Floorboard · pulledPASSENGER CABIN FLOORBOARD 242RF UPPER SURFACE HAS PULLED FIBERS. A224-15 ; / [01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUIND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-Jan 5, 2022 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022012858671Plate · corrodedDOT#02-186 AFT PIT DOOR THRESHOLD AFT CORNER PLATE CORRODED ; / [01] EVALUATED CORRODED PLATE NO ALLOWABLE LIMITS FOUND IN THE SRM FOUND PLATE OUT OF LIMITS; [02] VERIFIED ITEM 1; [03] VERIFIED NEW PART # AS 453A2611-1; IAW AIPC 25-52-10-04; ITEM # 450.. A-TAGJan 5, 2022 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022011058488Angle · corrodedFWD CARGO BAY Z-ANGLE CORRODED AT MULTIPLE NUTPLATE HOLES, WL 154, BS 500A+11 - 500E+7, LBL25. REMOVED CORROSION FROM THE Z ANGLE IAW SRM 51-10-02-0G-0. WITHIN LIMITS IAW SRM 53-00-53-1A-2 AND DWG 1496-444. REMOVED .002' OF .040' ORGINAL MATERIAL, .038' REMJan 5, 2022 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022011058478Angle · corrodedFWD CARGO BAY Z-ANGLE CORRODED AT MULTIPLE NUTPLATE HOLES, WL 154, BS 500E+10 - 500H+16, LBL 25. REMOVED CORROSION FROM FWD CARGO LT Z-ANGLE IAW SRM 51-10-02-0G-0. WITHIN LIMITS IAW SRM 53-00-53-1A-2 AND DWG 1496-444. REMOVED .003' OF .040' ORGINAL MATERIALJan 5, 2022 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022010658490Attach Angle · crackedFWD CARGO COMPARTMENT BAFFLE ATTACH CLIP BELOW Z-ANGLE IS CRACKED, FWD OF BS 500G FRAME, RBL 25. REMOVED CRACKED BAFFLE CLIP BELOW Z-ANGLE IAW SRM 51-40-02-0G-0. LOCATED & DRILLED HOLES IAW SRM 51-40-05-0G-0 & DWG 143A7505 REV-. INSTALLED BAFFLE CLIP IAW SRMJan 5, 2022 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022010658491Attach Angle · crackedFWD CARGO COMPARTMENT BAFFLE ATTACH CLIP BELOW Z-ANGLE IS CRACKED; FWD OF STA 500H FRAME; LBL25. REMOVED CRACKED BAFFLE CLIP BELOW Z-ANGLE IAW SRM 51-40-02-0G-0. LOCATED & DRILLED HOLES IAW SRM 51-40-05-0G-0 & DWG 143A7505 REV-. REMOVED & REPLACED BAFFLE ATTJan 5, 2022 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022010658492Baffle · crackedFWD CARGO COMPARTMENT BAFFLE ATTACH CLIP BELOW Z-ANGLE IS CRACKED; FWD OF STA 500H FRAME; RBL25. REMOVED THE CRACKED BAFFLE CLIP BELOW Z-ANGLE IAW SRM 51-40-02-0G-0. LOCATED & DRILLED HOLES IAW SRM 51-40-05-0G-0 AND DWG 143A7505 REV-. INSTALLED BAFFLE CLIPJan 5, 2022 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022010658493Attach Angle · crackedFWD CARGO COMPARTMENT BAFFLE ATTACH CLIP BELOW Z-ANGLE IS CRACKED; AFT OF STA 500H FRAME; LBL25. A177-016 ; /Jan 5, 2022 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022013158466Crease Beam · corrodedAFT GALLEY DOOR R-2 CREASE BEAM IS CORRODED. BS 975; WL208; RBL64. DOT 23 ; / [01] REMOVED CORROSION ON CREASE BEAM ANGLE IAW SRM 51-10-02-0G-0 ITEM 15; [02] EVALUATED ALLOWABLE LIMITS : ORIGINAL 'T' .080 REMAINING.060 LOSS .020 FOUND OUT OF LIMITS IAW SRM 53-Jan 4, 2022 · N8623F · Boeing 7378H4 · Fuselage Main, Longeron/StringerSDR SWAA2022013158472Floor Panel · pulledA22-012; CABIN FLOOR PANEL 241UF; UPPER SURFACE HAS PULLED FACE SHEET PLIES; MRK'D ; / [01] EVALUATED PANEL 241UF AND FOUND AREA'S OF PULLED FIBER'S ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B 737-800 SRM 53-00-50 2R -1 PAR 1A REV74. CLEAN AND PREP FOR REPJan 4, 2022 · N8623F · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022013158473Floor Panel · pulledA22-013; CABIN FLOOR PANEL 241VF; UPPER SURFACE HAS PULLED FACE SHEET PLIES; MRK'D ; / [01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1. TAP TEST GOOD.<BR><BR>CLEANED AND PRJan 4, 2022 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022013158471Floor Panel · pulledA22-010; CABIN FLOOR PANEL 231DF; UPPER SURFACE HAS PULLED FACE SHEET PLIES; MRK'D ; / [01] EVALUATED DAMAGE; UPPER FACE SHEET IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1. TAP TEST GOOD; NO DELAMINATION NOTED.<BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 5Jan 4, 2022 · N8623F · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022013158469Floor Panel · pulledA22-008; CABIN FLOOR PANEL 231FF; UPPER SURFACE HAS PULLED FACE SHEET PLIES; MRK'D ; / [01] EVALUATED AND FOUND DAMAGED FIBERS ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SJan 4, 2022 · N8623F · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022013158465Floor Panel · pulledA22-011; CABIN FLOOR PANEL 232CF; UPPER SURFACE HAS PULLED FACE SHEET PLIES; MRK'D ; / [01] EVALUATED AND FOUND DAMAGED FIBERS ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SJan 4, 2022 · N8623F · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022013158124Floor Panel · corrodedA125-20 - AFT CARGO BAY - FLOOR PANEL - 140BF - PERIMETER CORRODED ; / [01] MEASURED TOTAL ACCUMULATED LENGTH OF CORROSION DAMAGE TO BE = 27 ' LIMIT = 20'. PANEL 140BF IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102; [02] VERIFIED MATERIAL FOR NEW FLOOR PANEL TJan 4, 2022 · N8623F · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022013158125Floor Panel · corrodedA125-21 - AFT CARGO BAY - FLOOR PANEL - 140CF - PERIMETER CORRODED ; / [01] VERIFIED LIMITS; FOUND OUT OF LIMITS ( MORE THAN 20' LENGTH ) IAW 25-52-01-201-801.; [02] IDENTIFIED MATERIAL FOR PNL # 140CF AS: 2024 - T3-071 A TAG # A84104. IAW AMM 25-52-01-201-801Jan 4, 2022 · N8623F · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022013158140Channel · crackedA22-005; VERT STAB STA1016; LBL11; 5' ABOVE VERT STAB L/H ATTACH FTG; LATERAL SUPPORT CHANNEL CRACKED AT STRAIN RELIEF CUTOUT. ; / [01] REMOVED VERTICAL STAB LATERAL SUPPORT CHANNEL STA 1016 IAW SRM 51-40-02; [02] VERIFIED NEW PART TO BE MPN: 176A3101U26 ATAG:Jan 4, 2022 · N8623F · Boeing 7378H4 · Vertical StabilizerSDR SWAA2022012858138Lens · crackedA-061 DOT 002. R/H AFT EMERGENCY EXIT AFT HEADER PNL (232ZLW) LIGHT LENS CRACKED ; / [01] INSTALLED WINDOW LIGHT LED LENS IAW AMM 33-21-00-960-804 <BR><BR>STEP 9. C. (4)-(5)(C); [02] UPDATED PARTS INSTALLED INFO; [03] VERIFIED STEP 1; AUDIT C/WJan 4, 2022 · N8623F · Boeing 7378H4 · Passenger Compartment LightingSDR SWAA2022013157608Panel · crackedA-125-02 - AFT CARGO BAY - BULKHEAD PANEL - 142 NWB - CRACKED/TEMPORARY REPAIR INSTALLED ; / [01] REPLACED ON SHELF NEW BULKHEAD PANEL 142NWB. VERIFIED PART AS 453A2510-1; IAW AIPC 25-52-19-01B. ITEM # 35. A-TAG # WN12334.; [02] ALL WORK C/W<BR>AUDIT C/WJan 3, 2022 · N8623F · Boeing 7378H4 · Cargo CompartmentsSDR SWAA2022013157613Floor Panel · corrodedA-125-06 - FORWARD CARGO BAY - FLOOR PANEL - 120DF - PERIMITER CORRODE ; / [01] EVALUATED DAMAGE FOUND DAMAGE TO BE LONGER THEN 20' FOUND FLOOR PANEL TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1; [02] VERIFIED NEW FLOOR PANEL MATERIALS AS P/N <BR>2024-T3-071 ATAGJan 3, 2022 · N8623F · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022013157614Floor Panel · corrodedA-125-08 - FORWARD CARGO BAY - FLOOR PANEL - 120CF - PERIMETER CORRODED ; / [01] EVALUATED DAMAGE : CORROSION IS MORE 20 INCH FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-1; [02] VERIFIED MATERIAL ID : IS 2024 T3 .071 TAG #A105083 IAW AMM 25-52-01-201-801; [03] VERJan 3, 2022 · N8623F · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022013157615Floor Panel · corrodedA-125-09 - FORWARD CARGO BAY - FLOOR PANEL - 120AF - PERIMETER CORRODED ; / [01] VERIFIED LIMITS ON FWD PIT FLOOR PANEL 120AF. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. FIG 102.; [02] VERIFIED MATERIAL FOR REPLACEMENT PANEL AS .071; 2024-T3; IAW AMM 25-Jan 3, 2022 · N8623F · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022013157604Panel · crackedPANEL 194BL CORNER IS CRACKED AND BROKEN ; / [01] EVALUATED DAMAGE; PANEL CORNER IS REPAIRABLE IAW B737 SRM 53-60-70-2R-1 TABLE 203.<BR><BR>REMOVED DAMAGE; CLEANED AND PREPPED REPAIR AREA. BONDED REPAIR PLIES IAW B737 SRM 51-70-05-2R-10 REPAIR 10 PAR 4 STEPS AJan 2, 2022 · N8623F · Boeing 7378H4 · Aerodynamic FairingsSDR SWAA2021061582744Bracket · dentedGIRT BAR ON FORWARD ENTRY DOOR DIFFICULT TO STOW. / FOUND PARTIALLY DENT BRACKET. ADJUSTED BRACKET ON FWD ENTRY DOOR SLIDE CASE PER AMM 26-66-01.Jun 11, 2021 · N8623F · Boeing 7378H4 · Emergency EquipmentSDR SWAA2021021548382Girt Bar · out of positionRAMP REPORTS L1 GIRT BAR FIGHTING RETAINING CLIP / REPOSITIONED AND SECURED GIRT BAR PER AMM 25-66-01Feb 10, 2021 · N8623F · Boeing 7378H4 · Emergency EquipmentSDR SWAA2020123038835Grommet · looseGROMMET ON FOWARD ENTRY GIRT BAR FELL OFF. INSTALLED GROMMET PER SIP.Dec 28, 2020 · N8623F · Boeing 7378H4 · Emergency EquipmentSDR SWAA2020031242365Glowstrip · loosePHOTO LUMINESCENT STRIP @ 12D IS LOOSE CAUSES A TRIPPING HAZZARD SECURED PHOTO LUMINESCENT STRIP AT 12D USING SIPMar 10, 2020 · N8623F · Boeing 7378H4 · Emergency EquipmentSDR SWAA2020011340410Battery Pack · defectiveEMERGENCY LIGHT BATTERY PACK IN POSITION (M2816) WOULD NOT HOLD A CHARGE. / R&R BATTERY PACK PER AMM.Jan 8, 2020 · N8623F · Boeing 7378H4 · Emergency LightingSDR SWAA2021072629388Skin · delaminatedRIGHT HAND WING #8 SLAT UPPER SURFACE IS DELAMINATED AT 39' O/B AND 1.5' T/E / RIGHT HAND WING #8 SLAT UPPER SURFACE DELAMINATED AT 39' O/B AND 1.5' T/E REPAIRED IAW SRM 57-42-01-2R-4 AND IAW SRM 51-70-10-2R-2. DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 57-42-01-1Jan 4, 2020 · N8623F · Boeing 7378H4 · Leading Edge DevicesSDR SWAA2020011340409Skin · delaminatedR/H WING #8 SLAT UPPER SURFACE DELAMINATED AT 39" OUTBOARD AND 1.5" TRAILING EDGE. / REPAIRED SLAT IAW SRM.Jan 4, 2020 · N8623F · Boeing 7378H4 · Leading Edge DevicesSDR SWAA2020010329386Support · corroded***CORROSION*** FWD CARGO COMPARTMENT AFT BULKHEAD LOWER CENTER SUPPORT BS 500I RBL20-RBL 25 WL 156 / REMOVED + REPLACED FWD CARGO COMPARTMENT AFT BULKHEAD LOWER CENTER SUPPORT BS 500I RBL20 - RBL25 WL 156 IAW SRM 51-40-02-0G-0 + DWG 143A9481. 56379U 05JAN20Jan 3, 2020 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2021082229387Support · corroded***CORROSION*** FWD CARGO COMPARTMENT AFT BULKHEAD RH SUPPORT BS 500I RBL25 WL 156 / REMOVED AND REPLACED FWD CARGO AFT BULKHEAD R/H SUPPORT PART # 143A9485-34 PER BOEING DWG # 143A9481 AND SRM 51-40-02-0G-0 57903U 06JAN20Jan 3, 2020 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2020010840271Support · corrodedFORWARD CARGO COMPARTMENT AFT BULKHEAD RH SUPPORT CORRODED AT BS. 500I, RBL 25. / R&R SUPPORT PER DWG AND SRM.Jan 3, 2020 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2020010840270Support · corrodedFORWARD CARGO COMPARTMENT AFT BULKHEAD LOWER CENTER SUPPORT CORRODED AT BS. 500I, BETWEEN RBL 20 TO RBL 25. / R&R SUPPORT IAW SRM & DWG.Jan 3, 2020 · N8623F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022041248408Skin · crackedLEFT HAND LE SKIN I/B AFT EDGE HAS 4EA CRACKS AT SKIN COUNTERSINKS WING STA 218 / CUT AND REMOVED DAMAGED SECTION OF SKIN AT WS 218 L/H L/E SKIN. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 57-41-01-2R-3Dec 31, 2019 · N8623F · Boeing 7378H4 · Wing, Plate/SkinSDR SWAA2022030148405Flap · delaminatedLEFT HAND WING INBOARD MAIN FLAP LOWER O/B SURFACE DELAMINATED / REMOVED $ REPLACED L/H I/B MAIN FLAP IAW B737 AMM 27-51-11-000-801 & AMM 27-51-11-400-801. ADJUSTMENT CHECK IS GOOD IAW B737 AMM 27-51-11-820-801. (POS:LH; TAG NO:547763; P/N OFF:113A2100-71; S/NDec 31, 2019 · N8623F · Boeing 7378H4 · Trailing Edge Flaps
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