N8682B

Service difficulty reports · 85

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 = 'N8682B' 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 SWAA2022041284642Strap · corrodedDOT#35-186 AFT CARGO COMPARTMENT FLOOR 'T' STRAP CORRODED STA 887 RBL 22 TO LBL8 WL 156 / [01] REMOVED; LOCATED AND DRILLED; INSTALLED NEW AFT CARGO FLOOR SPLICE TEE STRAP AT BS 887 RBL22 TO LBL8 IAW SRM 51-40-02-0G-0 AND BOEING DWG# 146A7500 ID:0001 REV:B.;[0Mar 16, 2022 · N8682B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022040784636Strip · corrodedDOT#39-186 AFT CARGO COMPARTMENT #4 RH CAP STRIP CORRODED / [01] REMOVED COROSSION AND VERIFIED WITH 10X MAGINIFIER ALL COROSSION REMOVED IAW SRM 51-10-02-0G-0;[02] VERIFIED LIMITS; OUT OF LIMITS DUE TO NO PUBLISHED LIMITS IN SRM<BR>ORIGINAL THICKNESS .063'<BRMar 16, 2022 · N8682B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022040784637Strip · corrodedDOT#40-186 AFT CARGO COMPARTMENT #3 RH CAP STRIP CORRODED / [01] REMOVED COROSSION AND VERIFIED WITH 10X MAGINIFIER ALL COROSSION REMOVED IAW SRM 51-10-02-0G-0;[02] VERIFIED LIMITS; OUT OF LIMITS DUE TO NO PUBLISHED LIMITS IN SRM<BR>ORIGINAL THICKNESS .063'<BRMar 16, 2022 · N8682B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022040784643Strip · corrodedDOT#41-186 AFT CARGO COMPARTMENT #2 RH CAP STRIP CORRODED / [01] REMOVED COROSSION AND VERIFIED WITH 10X MAGINIFIER ALL COROSSION REMOVED IAW SRM 51-10-02-0G-0;[02] VERIFIED LIMITS; OUT OF LIMITS DUE TO NO PUBLISHED LIMITS IN SRM<BR>ORIGINAL THICKNESS .063'<BRMar 16, 2022 · N8682B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022040784638Strip · corrodedDOT#42-186 AFT CARGO COMPARTMENT #1 RH CAP STRIP CORRODED / [01] REMOVED COROSSION AND VERIFIED WITH 10X MAGINIFIER ALL COROSSION REMOVED IAW SRM 51-10-02-0G-0;[02] VERIFIED LIMITS; OUT OF LIMITS DUE TO NO PUBLISHED LIMITS IN SRM<BR>ORIGINAL THICKNESS .063'<BRMar 16, 2022 · N8682B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022040784644Floor Panel · corrodedDOT#43-186 AFT CARGO COMPARTMENT FLOOR PANEL 140DF CORRODED AROUND EDGES / [01] EVALUATED ALLOWABLE LIMITS: TOTAL ACCUMULATED DAMAGE LENGTH IS 20 INCHES MORE FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-1;[02] VERIFIED MATERIAL ID FOR NEW FLOOR PANEL IS 2024 T3 .07Mar 16, 2022 · N8682B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022040784639Floor Panel · corrodedDOT#44-186 AFT CARGO COMPARTMENT FLOOR PANEL 140CF CORRODED AROUND EDGES / [01] EVALUATED CORROSION ON AFT CARGO FLOOR PANEL 140CF CORROSION WAS FOUND TO BE OUT LIMITS EXCEEDS 20' IAW B737 SRM 53-00-53-1A-1;[02] MATERIAL ID FOR FLOOR PANEL 140CF IS 2024 T-3 .0Mar 16, 2022 · N8682B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022040784640Floor Panel · corrodedDOT#45-186 AFT CARGO COMPARTMENT FLOOR PANEL 140BF CORRODED AROUND EDGES / [01] EVALUATED PANEL 140BF FOUND THE TOTAL ACCUMULATED CORROSION EXCEEDS THE MAXIMUM 20'. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. WORK PERFORMED BY BERNARD BEMKE 27266;[02] VERMar 16, 2022 · N8682B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022040784645Floor Panel · corrodedDOT#46-186 AFT CARGO COMPARTMENT FLOOR PANEL 140AF CORRODED AROUND EDGES / [01] VERLFED MATERIAL LOSS CORROSION IS MORE THEN 20 INCHES MAXIMUM IS 20 INCHES IS OUT OF LIMITS I/A/W SRM 53-00-53-1A-1;[02] VERIFIED NEW MATERIAL FOR FLOOR PANEL 140AF FOR AFT CARGO Mar 16, 2022 · N8682B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022040784641Floor Panel · corrodedDOT#47-186 AFT CARGO COMPARTMENT FLOOR PANEL 140EF CORRODED AROUND EDGES / [01] EVALUATED PANEL 140EF FOUND THE TOTAL ACCUMULATED CORROSION EXCEEDS THE MAXIMUM 20'. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. WORK PERFORMED BY BERNARD BEMKE 27266;[02] VERMar 16, 2022 · N8682B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022040784648Scuff Plate · corrodedDOT#48-186 AFT CARGO COMPARTMENT FLOOR FWD HOCKY STICK SCUFF PLATE CORRODED / [01] VERIFIED AND REPLACED AFT CARGO COMPARTMENT FWD CARGO TIEDOWN PLATE ON PARTS RACK IAW IPC 25-52-10-04 AND BOEING DWG# 453A2600 ID:0026 REV:D;[02] VERIFIED STEP 1<BR>AUDIT CWMar 16, 2022 · N8682B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022040784646Scuff Plate · corrodedDOT#49-186 AFT CARGO COMPARTMENT FLOOR AFT HOCKY STICK SCUFF PLATE CORRODED / [01] VERIFIED AND REPLACED AFT CARGO COMPARTMENT AFT CARGO TIEDOWN PLATE ON PARTS RACK IAW IPC 25-52-10-04 AND BOEING DWG# 453A2600 ID:0026 REV:D;[02] VERIFIED STEP 1<BR>AUDIT CWMar 16, 2022 · N8682B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022040784647Strip · corrodedDOT#50-186 AFT CARGO COMPARTMENT 3EA CAP STRIPS CORRODED / [01] REMOVED COROSSION FROM 3 EA CAPSTRIPS AND VERIFIED WITH 10X MAGINIFIER ALL COROSSION REMOVED IAW SRM 51-10-02-0G-0;[02] VERIFIED LIMITS; OUT OF LIMITS DUE TO NO PUBLISHED LIMITS IN SRM<BR>ORIGINALMar 16, 2022 · N8682B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022041283724Floor Panel · corrodedDOT 050-023 FORWARD CARGO COMPARTMENT FLOOR PANEL 120AF IS CORRODED / [01] EVALUATED CORROSION; FOUND CORROSION EXCEEDS 20' FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-1;[02] VERIFIED PN: 2024-T3-071 A-TAG: A118124 IAW SRM 25-52-01-201-801;[03] VERIFIED STEPS 1 ANMar 15, 2022 · N8682B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022041283726Floor Panel · corrodedDOT 050-024 FORWARD CARGO COMPARTMENT FLOOR PANEL 120CF IS CORRODED / [01] FOUND CARGO FLOOR PANEL 120CF TO BE OUT OF LIMITS; MORE THAN 20' IN LENGTH OF ACCUMULATED DAMAGE IAW SRM 53-00-53-1A-1 PARA 5A FIG 102.;[02] VERIFIED MATERIAL FOR NEW FLOOR PANEL 120CF Mar 15, 2022 · N8682B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022041283720Floor Panel · corrodedDOT 050-026 FORWARD CARGO COMPARTMENT FLOOR PANEL 120DF IS CORRODED / [01] DAMAGE EXCEEDED 20' MAX ALLOWABLE LIMITS AND FOUND TO BE OUT OF LIMITS IAW B-737 SRM 53-00-53-1A-1 STEP 5 A B FIG. 102;[02] MATERIAL VERIFIED AS 0.071' 2024-T3 IAW B-737 SRM 25-52-01-83Mar 15, 2022 · N8682B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022041284129Angle · corrodedC-1 CARGO PIT; FLOOR PANEL L/H ZEE ANGLE; AREAS OF CORROSION ON UPPER SIDE AT LOWER SIDE WALL PANEL ATTACH FASTENER HOLES; BS 500+15 TO BS 500E+1; LBL 25; WL 156; AREAS MARKED IN BLACK; DOT: 148-002 / [01] REMOVED CORROSION ON Z ANGLE IAW SRM 51-10-02-0G-0 ITEMar 15, 2022 · N8682B · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022041284132Angle · corrodedC-1 CARGO PIT; BS 500I; LBL 25 TO RBL 25; WL 156; AREAS OF CORROSION ON UPPER SIDE OF AFT B/H TO FLOOR BEAM ATTACH ANGLE; AREAS MARKED IN BLACK; DOT: 148-004 / [01] REMOVED DAMAGE FLOOR BEAM ATTACH ANGLE IAW SRM 51-40-02-0G-0;[02] REMOVED CORROSION IAW SRM 51-Mar 15, 2022 · N8682B · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022040783725Floor Panel · corrodedDOT 050-024 FORWARD CARGO COMPARTMENT FLOOR PANEL 120BF IS CORRODED / [01] CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 PARA 5A AND FIG 102.;[02] VERIFIED MATERIAL FOR NEW FLOOR PANEL 120BF TO BE PN: 2024-T3-071 ATAG# A118124 IAW AMM 25-52-01-201-Mar 15, 2022 · N8682B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022040784128Floor Support · corrodedFWD CARGO PIT; FLOOR PANEL R/H ZEE ANGLE; BS 500+6 TO BS 500H+11; RBL25; WL 156; AREAS OF CORROSION ON ZEE ANGLE AT LOWER SIDE WALL PANEL ATTACH FASTENER HOLES; AREAS MARKED IN BLACK; DOT: 148-003 / [01] EVALUATED ALLOWABLE LIMITS .100% MATERIAL LOSS FOUND OUTMar 15, 2022 · N8682B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022041283715Battery Pack · inoperativeDOT 050-001 PASSENGER CABIN AISLE LIGHTS ARE INOP AT 5ABC; 8ABC; AND 12ABC / [01] REPLACED EMERGENCY LIGHTS POWER SUPPLY M2335 IAW AMM 33-51-06-960-806 AND BATTERY PACK M2335 IAW AMM 33-51-06-960-805. OPS CHECK GOOD.;[02] VERIFIED STEP 1. AUDIT C/WMar 14, 2022 · N8682B · Boeing 7378H4 · Emergency LightingSDR SWAA2022041283306Access Panel · elongatedDOT # A-111-001 PANEL # 521QB LEFT WING LOWER L/E ONE HOLE ELONGATED / [01] EVALUATED PANEL 521QB AND FOUND DAMAGE AROUND UPPER SURFACE OF MARKED FASTENER HOLE. FOUND TO BE REPAIRABLE. IAW B737-800 SRM 57-41-01-2R-1 PAR 1A & 2.B.(2) REV74. CLEAN AND PREP AREA Mar 13, 2022 · N8682B · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2022041283303Flap · delaminatedRIGHT WING OUTBOARD AFT FLAP HAS DELAM ON LOWER INBOARD SURFACE / [01] REMOVED RIGHT WING O/B AFT FLAP IAW AMM 27-51-22-000-801;[12] REMOVED FAILED DOUBLER AND PREPPED AREA FOR NEW REPAIR. IAW B737-800 SRM 51-70-10-2R-0 PAR 6&7. CLEAN AND PREP AREA. MADE NEW RMar 13, 2022 · N8682B · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2022012763530Lens · missingCEILING EXIT ROW LENSE MISSING ; / [01] REPLACED CEILING EXIT ROW LENS PER SIPJan 24, 2022 · N8682B · Boeing 7378H4 · Emergency LightingSDR SWAA2022011861861Battery Pack · inoperativeSEVERAL EMERGENCY LIGHTS ON FWD RH SIDE OF AC ARE INOP ; / [01] REMOVED AND REPLACED BATTERY PACK ON FWD RH EMERGENCY LIGHT POWER SUPPLY. OPS CHECK GOOD REF AMM 33-51-06Jan 15, 2022 · N8682B · Boeing 7378H4 · Emergency LightingSDR SWAA2021111141353Lens · looseOVER WING CENTER AISLE EXIT LIGHT LENS FELL OFF ; / [01] RE INSTALLED O/ WING CENTER AISLE EXIT LT LENSE PER SIPNov 7, 2021 · N8682B · Boeing 7378H4 · Emergency LightingSDR SWAA2021051070042Sign · detachedEXIT SIGN MID CABIN OVERHEAD FELL OFF. RESECURED EXIT SIGN (OVERHEAD EMERGENCY EXIT) PER S.I.P.May 6, 2021 · N8682B · Boeing 7378H4 · Emergency LightingSDR SWAA2021030352813O-Ring · leakingNO 2 ENGINE HYDRUALIC LOW PRESSURE LIGHT ILLUMINATED. B QUANTITY INDICATE 0. B PRESSURE IS STILL GOOD. PER QRH, NO. 2 ENGINE HYDRAULIC PUMP SWITCH TURNED OFF WHEN FLAPS WERE EXTEDED, TOTAL LOSS OF STSTEM B / FOUND 'O' RING LEAKING R/H SIDE MAIN WHEEL WELL 'B' Feb 27, 2021 · N8682B · Boeing 7378H4 · Hydraulic System, MainSDR SWAA2022031553530Radome · delaminatedNOSE RADOME WORN AND DELAMINATED THROUGH BOOT. LARGE AREAS OF PAINT MISSING OVER BOOT. / REMOVED & REPLACED RADOME IAW B737 MM 53-52-00 TRANSACTION #2644984POS:ONLY P/N OFF:1001002-7 P/N ON:1001002-2 S/N OFF:NRD-0529 S/N ON:WN0020/5311CAug 26, 2019 · N8682B · Boeing 7378H4 · Aerodynamic FairingsSDR SWAA2019021329559Glowstrip · brokenFORWARD GALLEY PHOTO LUMINESCENT TRACK LIGHTING BROKEN. R&R LIGHT PER AMM.Feb 12, 2019 · N8682B · Boeing 7378H4 · Emergency EquipmentSDR SWAA2018070223256Lens · looseAFT DOOR EXIT SIGN LENS LOOSE. REINSTALLED LENS PER SIP.Jun 30, 2018 · N8682B · Boeing 7378H4 · Emergency LightingSDR SWAA2018060422527Cover · looseFORWARD RT EMERGENCY EXIT LENS COVER LOOSE. SECURED COVER IAW MM.Jun 3, 2018 · N8682B · Boeing 7378H4 · Emergency LightingSDR SWAA2017101617128Lens · missingRIGHT AFT GALLEY EMERGENCY EXIT SIGN LENS MISSING. INSTALLED THE LENS IAW AMM.Oct 14, 2017 · N8682B · Boeing 7378H4 · Emergency LightingSDR SWAA2017080315476Light · damagedRT EMERGENCY LIGHT STRIP DAMAGED. R & R THE EMERGENCY LIGHT STRIP IAW MM.Aug 2, 2017 · N8682B · Boeing 7378H4 · Emergency LightingSDR SWAA2017013011528Lens · detachedOVERWING OVERHEAD EMERGENCY EXIT SIGN LENS FELL OUT. REINSTALLED LENS IAW SIP.Jan 27, 2017 · N8682B · Boeing 7378H4 · Emergency Lighting
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