N8680C

Service difficulty reports · 95

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 = 'N8680C' 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 SWAA2023041325391Panel · delaminatedDURING WALK AROUND FOUND DELAMINATION ON PANEL 192BL. FWD EDGE OF LH FRONT SPAR TO REAR SPAR UNDERWING PNL 192BL. DAMAGE MEASURED 8 IN LONG BY 1.25 IN WIDE DELAMINATION CROSSED 1 FASTENER HOLE AND IS 1 PLY DEEP.<[01] REFERENCE FAULT TTG8Q00KCJUV AND EA 23-153-Apr 10, 2023 · N8680C · Boeing 7378H4 · Service DoorsSDR SWAA2023022105134Sign · brokenEMERGENCY EXIT OVERWING CENTER SIGN BROKE<[01] REINSTALLED EMERG EXIT SIGN PER SIP.Feb 19, 2023 · N8680C · Boeing 7378H4 · Emergency LightingSDR SWAA2023011992565Lens · missingFRONT SIDE OF EMERGENCY EXIT ROW SIGN IS MISSING. REPLACED LENS ON FRONT SLIDE OF EMERGENCY EXIT ROW SIGN OPS CHECKED GOOD IAW MM 33-51-00.Jan 18, 2023 · N8680C · Boeing 7378H4 · Emergency LightingSDR SWAA2022102563698Slide · dislodgedL1 DOOR SLIDE FELL OUT OF CONTAINER / [01] REINSTALLED SLIDE IAW AMM 25-66-01Oct 23, 2022 · N8680C · Boeing 7378H4 · Escape SlideSDR SWAA2022080237515Lens · missingOVERHEAD EMERGENCY EXIT SIGN OVER EXIT ROW MISSING FRONT PART WITH LETTERING / [01] REPLACED EMERGENCY EXIT SIGN LENS REF AMM 33-51-01.Aug 1, 2022 · N8680C · Boeing 7378H4 · Emergency LightingSDR SWAA2022032985059Battery Pack · inoperativeALL EMERGENCY LIGHTS POWERED BY M1673 ARE INOP / [01] REPLACED EMERGENCY LIGHT BATTERY PACK M1673 IAW AMM 33-51-06-960-805 AND WDM 33-51-14. OPS CHECK GOOD.;[02] VERIFIED STEP 1. AUDIT C/WMar 17, 2022 · N8680C · Boeing 7378H4 · Emergency LightingSDR SWAA2022032985062Battery Pack · inoperativeALL EMERGENCY LIGHTS POWERED BY M1670 ARE INOP / [01] REPLACED EMERGENCY LIGHT BATTERY PACK M1670 IAW AMM 33-51-06-960-805 AND WDM 33-51-13. OPS CHECK GOOD.;[02] VERIFIED STEP 1. AUDIT C/WMar 17, 2022 · N8680C · Boeing 7378H4 · Emergency LightingSDR SWAA2022032985060Battery Pack · inoperativeALL EMERGENCY LIGHTS POWERED BY M1675 ARE INOP / [01] REPLACED EMERGENCY LIGHT BATTERY PACK M1675 IAW AMM 33-51-06-960-805 AND WDM 33-51-12. OPS CHECK GOOD.;[02] VERIFIED STEP 1. AUDIT C/WMar 17, 2022 · N8680C · Boeing 7378H4 · Emergency LightingSDR SWAA2022032985061Battery Pack · inoperativeALL EMERGENCY LIGHTS POWERED BY M2816 ARE INOP / [01] REPLACED EMERGENCY LIGHT BATTERY PACK M2816 IAW AMM 33-51-06-960-805 AND WDM 33-51-12. OPS CHECK GOOD.;[02] VERIFIED STEP 1. AUDIT C/WMar 17, 2022 · N8680C · Boeing 7378H4 · Emergency LightingSDR SWAA2022032979987Floor Panel · corrodedFWD CARGO COMP.FLOOR PANEL 120BF CORRODED AROUND THE FASTNER HOLE / [01] EVALUATED DAMAGE ON FLOOR PNL #120 BF; FOUND OUT OF LIMITS DUE CORROSION LENGTH LIMITS IS MORE TNAN 20 INCHES IAW SRM 53-00-53-1A-1 FIG. 102.;[02] IDENTIFIED MATERIAL FOR FLOOR PNL FABRICMar 3, 2022 · N8680C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022032979978Floor Panel · corrodedFWD CARGO COMP.FLOOR PANEL 120CF CORRODED AROUND THE FASTNER HOLE / [01] EVALUATED CORROSION DAMAGE AROUND FASTENER HOLES FOUND TO BE OUT OF LIMITS EXCEEDS 20' IAW<BR>SRM 53-00-53-1A-1 5.A. (1)(B) FIG. 102<BR>AMM 25-52-01-201-801;[02] VERIFIED MATERIAL IAW AMMMar 3, 2022 · N8680C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022032979986Floor Panel · corrodedFWD CARGO COMP.FLOOR PANEL 120DF CORRODED AROUND THE FASTNER HOLE / [01] EVALUATED DAMAGE FOUND TO BE OUT OF LIMITS IAW <BR>SRM 53-00-53-1A-1 5. A. (1) (B) 1) FIG 102<BR><BR>VERIFIED MATERIAL ALCLAD 2024 T3 .071' A TAG A115238<BR>IAW AMM 25-52-01-201-801 1. C.Mar 3, 2022 · N8680C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022032979991Floor Panel · corrodedA22-34; AFT PIT FLOOR PANEL 140BF; CORROSION AROUND THE PERIMETER (SECONDARY STRUCTURE) / [01] FOUND PANEL 140BF TO BE OUT OF LIMITS DUE TO DAMAGE BEING MORE THAN 20' IAW SRM 53-00-53-1A-1;[02] VERIFIED MATERIAL FOR FLOOR PANEL 140 BF PART # 2024-T3-071 ATAG #Mar 3, 2022 · N8680C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022032979983Floor Panel · corrodedA22-32; AFT PIT FLOOR PANEL 140EF; CORROSION AROUND THE PERIMETER (SECONDARY STRUCTURE) / [01] EVALUATED CORROSION FOUND MORE THAN 20' OF DAMAGE; OUT OF LIMITS IAW SRM 53-00-53-1A-1.;[02] VERIFIED NEW MATERIAL AS 2024 T3 .071' SHEET; A-TAG A115239; IAW AMM 25-Mar 3, 2022 · N8680C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022032979990Intercostal · corrodedA22-37; AFT PIT STA747-767; RBL22; WL157; INTERCOSTAL HAS CORROSION ON BOTH SURFACES OF UPPER FLANGE / [01] REMOVED DAMAGE INTERCOSTAL IAW SRM 51-40-02-0G-0;[02] VERIFIED STEP 1 IS COMPLETE;[03] EVALUATED ALLOWABLE LIMITS:100% MATERIAL LOSS FOUND OUT OF LIMITSMar 3, 2022 · N8680C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022032979984Floor Panel · corrodedA22-33; AFT PIT FLOOR PANEL 140AF; CORROSION AROUND THE PERIMETER (SECONDARY STRUCTURE) / [01] FOUND PANEL 140AF TO BE OUT OF LIMITS DUE TO THE DAMAGE BEING MORE THAN 20'.IAW SRM 53-00-53-1A-1;[02] VERIFIED NEW FLOOR PANEL MATERIAL AS P/N 2024-T3-071 ATAG##A11Mar 3, 2022 · N8680C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022032979982Floor Panel · corrodedA22-31; AFT PIT FLOOR PANEL 140CF; CORROSION AROUND THE PERIMETER (SECONDARY STRUCTURE) / [01] EVALUATED CORROSION ON AFT CARGO FLOOR PANEL 140CF FLOOR PANEL WAS FOUND TO BE OUT OF LIMITS EXCEEDED 20' IAW B737 SRM 53-00-53-1A-1;[02] MATERIAL ID FOR AFT CARGO FMar 3, 2022 · N8680C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022032979977Angle · corrodedA-061 DOT 033 FWD CARGO PIT L/H Z ANGLE HAS CORROSION ON UPPER SURFACE FROM STA 500A+15' TO STA 500I LBL 23 WL 155 / [01] REMOVED CORROSION IAW SRM 51-10-02 10X MAGNIFY ORIGINAL THICKNESS .040 .010 MATERIAL REMOVED OUT OF LIMITS .030 IAW SRM 53-00-53-1A-2 AAR Mar 3, 2022 · N8680C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022032979916Baffle · crackedA-061 DOT 035 FWD CARGO PIT BAFFLE CLIP CRACKED FWD SIDE OF FRAME AT STA 500E RBL 23 WL 155 / [01] REMOVED CRACKED BAFFLE CLIP IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW BAFFLE CLIP PN: 143A7502U158 ATAG A111434 IAW DWG 143A7505 REV. -;[03] VERIFIED STMar 3, 2022 · N8680C · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022032979913Angle · corrodedA-061 DOT 030 FWD CARGO PIT R/H Z ANGLE CORROSION UPPER SURFACE FROM STA 500C+16' TO STA 500I RBL 23 WL 155 / [01] REMOVED CORROSION IAW SRM 51-10-02 10X MAGNIFY ORIGINAL THICKNESS .040 .010 MATERIAL REMOVED OUT OF LIMITS.030 IAW SRM 53-00-53-1A-2 AAR TOOL NO.Mar 3, 2022 · N8680C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022032979918Support · corrodedA-061 DOT 029 FWD CARGO PIT AFT FLOOR STRUCTURE AT STA 500I LBL 23 TO RBL 23 WL 155 CORRODED UPPER SURFACE / [01] REMOVED CORROSION IAW SRM 51-10-02 10X MAGNIFY MAXIMUM MATERIAL REMAINING .056 .050 MATERIAL REMAINS OUT OF LIMITS IAW SRM 53-30-08-1A-1 AAR TOOL Mar 3, 2022 · N8680C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022032979884Channel · corrodedA22-19 AFT PIT STA 727G+10-767; RBL22; WL157; Z-CHANNEL HAS HEAVY CORROSION AT AND AWAY FROM FASTENER HOLES ON UPPER SURFACE AND A COUPLE MRK'D IN BLACK ON LOWER SURFACE / [01] REMOVED CORROSION ON Z- CHANNEL IAW SRM 51-10-02-0G-0 ITEM 15;[02] EVALUATED ALLOWAMar 3, 2022 · N8680C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022032879633Pan · crackedR2 DOOR;LINER BOTTOM SUPPORT PANEL 842DZ AFT BRACKET CRACKED / [01] REMOVED DAMAGED PAN ASSY FROM R2 DOOR IAW SRM 51-40-02-0G-0.;[02] NEW PART VERIFIED; PAN ASSY P/N 411A2119-194; IAW IPC 52-41-31-10 AND BOEING DWG 411A2119 ID:0090 REV A;[03] ATAG FOR NEW PARTMar 2, 2022 · N8680C · Boeing 7378H4 · Galley DoorsSDR SWAA2022032979627Strap · corrodedA22-22; AFT PIT STA 772; BL0; FLOOR SPLICE STRAP; UPPER SURFACE; CORROSION AT 1EA FASTENER HOLE; MRK'D. (SECONDARY STRUCTURE) ATA-53-98 / [01] VERIFIED REPLACEMENT PART AS 149A9401-4; IAW AIPC 53-42-11-26; ITEM # 955. REMOVED AND REPLACED ON A/C IAW AMM 25-52-Mar 2, 2022 · N8680C · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2022032979615Shield · corrodedA22-20; AFT PIT STA 767-787; RBL22; WL157; SIDE SHIELD HAS CORROSION ON UPPER AND LOWER SURFACES; MRK'D. / [01] EVALUATED ALLOWABLE LIMITS : 100% MATERIAL LOSS FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1;[02] VERIFIED ITEM 1;[03] REMOVED DAMAGE SIDE SHIELD IAW SMar 2, 2022 · N8680C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022032979619Channel · corrodedA22-18; AFT PIT STA 727I+10-827; LBL22; WL157; Z-CHANNEL HAS CORROSION ADJACENT TO 21 EA FASTENER HOLES UPPER AND A COUPLE ON LOWER MRK'D WITH BLACK B. / [01] REMOVED CORROSION ON Z- CHANNEL IAW SRM 51-10-02-0G-0 ITEM 15;[02] EVALUATED ALLOWABLE LIMITS: .040 OMar 2, 2022 · N8680C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022032979612Slide · out of positionL2 DOOR SLIDE DRAGS ON THRESHOLD WHEN CLOSING DOOR / [01] REPOSITION AFT ENTRY DOOR SLIDE I/A/W MT 725-61-06 STEP 11;[02] STILL NEEDS RIG CHECK ON A/C;[03] VERIFIED STEPS 1 & 2;[04] VERIFIED SLIDE DOES NOT INTERFERE WHEN CLOSING ON AIRCRAFT IAW MT 725-61-06.;[Mar 2, 2022 · N8680C · Boeing 7378H4 · Escape SlideSDR SWAA2022032979227Panel · corrodedA-061 DOT 013 R/H WING FUEL QTY PNL UNDER PNL 621GB CORRODED AT CUTOUT FOR TANK #1 FUEL QTY GAUGE / [01] REMOVED CORROSION FROM FUEL QTY PANEL ON R/H WING IAW SRM 51-10-02-0G-0 SECTION 15. VERIFIED WITH 10X MAGNIFICATION.;[02] VERIFIED STEP 1;[03] MEASURED FORMar 1, 2022 · N8680C · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2022032880495Plate · crackedA-061 DOT 018 R/H WING T/E WIGGLE PLATE INBD 0F #7 FLAP TRACK LOOSE / [01] REMOVED WIGGLE PLATE I.A.W SRM 51-40-02-0G-0;[02] VERIFIED NEW PLATE AS PART #115A3760-42 I.A.W BOEING DWG 115A3700 REV:- ATAG#A117635;[03] DRILLED NEW WIGGLE PLATE I.A.W SRM 51-40-05-0Mar 1, 2022 · N8680C · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2022032978894Plate · crackedA-061 DOT 005 L/H WING WIGGLE PLATE OUTBD OF SAIL TAIL PHENOLIC CRACKED / [01] REMOVED DAMAGE PARTS IAW SRM 51-40-02-0G-0;[02] RECEIVED NEW WIGGLE PLATE P/N 115A3760Y29 TAG # WN 14076 IAW IPC 57-50-00-17;[03] LOCATED AND DRILL HOLES ON NEW PLATE IAW SRM 51-40-Feb 28, 2022 · N8680C · Boeing 7378H4 · Wing, Control SurfacesSDR SWAA2022032978889Attach Angle · crackedA-061 DOT 003 L/H WING ATTACH ANGLE FOR UPPER FIXED TRAILING EDGE PNL BETWEEN #5 AND #6 FWD ATTACH ANGLE CRACKED / [01] REMOVED DAMAGE ATTACH ANGLE IAW SRM 51-40-02-0G-0;[02] VERIFIED NEW ATTACH ANGLE P/N 115A2156-7 TAG # A117676 IAW DWG 115A2512;[03] VERIFIEDFeb 28, 2022 · N8680C · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2022032978890Attach Angle · crackedA-061 DOT 002 L/H WING ATTACH ANGLE FOR UPPER FIXED TRAILING EDGE PANEL BETWEEN #5 AND #6 SPOILERS CRACKED / [01] REMOVED DAMAGE ATTACH CLIP IAW SRM 51-40-02-0G-0;[02] VERIFIED NEW ATTACH CLIP P/N 115A6260-1 TAG#A117854 IAW DWG 115A6200;[03] VERIFIED STEPS 1 AFeb 28, 2022 · N8680C · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2022032978892Skin · delaminatedDOT A-24-3. LEFT WING O/B AFT FLAP HAS LARGE AREA OF DELAMINATED SKIN ON LOWER INBOARD CORNER. / [01] REMOVED L/H O/B AFT FLAP IAW AMM 27-51-22-000-801.;[02] BOND TEST IAW B737 NDT PT 4; 51-00-05. NO DEFECTS NOTED. TOOL#40082; DUE 11OCT22;[03] REMOVED FASTENERFeb 28, 2022 · N8680C · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2021112947647Light · missingMID CABIN EMERGENCY EXIT SIGN FORWARD SIDE MISSING ; / [01] REPLACED MID CABIN EMERGENCY EXIT SIGN FORWARD SIDE PER AMM 33-51-01.Nov 24, 2021 · N8680C · Boeing 7378H4 · Emergency LightingSDR SWAA2021102531950None · looseEMERGENCY EXIT SIGN OVERWING OVERHEAD; COVER FELL OFF. / RESECURED EMERGENCY EXIT SIGN COVER @ OVERWING OVERHEAD PER AMM 33-51-01Oct 19, 2021 · N8680C · Boeing 7378H4 · Emergency LightingSDR SWAA2021072095822Lens · looseMID CABIN OVERHEAD EXIT SIGN FELL OFF. / INSTALL EXIT SIGN LENS PER AMM 33-51-01Jul 16, 2021 · N8680C · Boeing 7378H4 · Emergency LightingSDR SWAA2021060378568Lens · detachedFLIGHT ATTENDENT REPORTS OVERWING EXIT SIGN FELL OFF. / RESCURED OVERWING EXIT LENS IAW S.I.P. REF AMM 33-51-04.May 30, 2021 · N8680C · Boeing 7378H4 · Emergency LightingSDR SWAA2020120133021Light · inoperativePHOTO ILLUMINESCENT STRIP NEXT TO ROW 1 AND 2 D;E;F DO NOT GLOW. R & R STRIP NARROW PHOTOLUMINESCENT BLUE AND OPERATIONS CHECK NORMAL, PER AMM 33-51-15.Nov 30, 2020 · N8680C · Boeing 7378H4 · Emergency LightingSDR SWAA2018100325719Glowstrip · inoperativeRT STRIP OF PHOTOLUMINESCENT EMERGENCY PATH LIGHTING INOP BETWEEN ROW 1 TO ROW 2. R&R STRIP PER AMM.Oct 2, 2018 · N8680C · Boeing 7378H4 · Emergency EquipmentSDR SWAA2017111517808Bulb · inoperativeR2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BULB IAW AMM.Nov 14, 2017 · N8680C · Boeing 7378H4 · Emergency LightingSDR SWAA2017083116019Strap · crackedFLASHLIGHT STRAP CRACKED. R&R STRAP PER MM.Aug 29, 2017 · N8680C · Boeing 7378H4 · Emergency EquipmentSDR SWAA2017051613714Megaphone · inoperativeMEGAPHONE INOPERATIVE. R & R THE MEGAPHONE IAW MM.May 12, 2017 · N8680C · Boeing 7378H4 · Emergency EquipmentSDR SWAA2016092708220Latch · out of adjustL2 DOOR SLIDE LATCH OUT OF ADJUST. ADJUSTED THE LATCH IAW SIP.Sep 26, 2016 · N8680C · Boeing 7378H4 · Escape SlideSDR SWAA2016071353750Girt Bar · out of adjustL1 DOOR EMERGENCY SLIDE GIRT BAR CLIPS OUT OF ADJUST. ADJUSTED THE GIRT BAR IAW MM.Jul 10, 2016 · N8680C · Boeing 7378H4 · Emergency EquipmentSDR SWAA2016052452045Lens · brokenRIGHT AFT OVERWING EMER EXIT LIGHT LENS BROKEN. R & R LENS IAW MM.May 23, 2016 · N8680C · Boeing 7378H4 · Emergency Lighting
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