N8685B

Service difficulty reports · 84

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 = 'N8685B' 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 SWAA2024050171829Web · corrodedAFT WET AREA- CORROSION ON FLOOR WEB AT STA 986 +3; LBL +33 MARKED; BLENDED CORROSION PER SRM 51-10-02. REMOVED .030' OF MATERIAL. REMAINING THICKNESS IS .010'. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-51-1A-1. BLENDED CORROSION PER SRM 51-10-02. REMOVEDApr 7, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050171827Floorbeam · corrodedAFT WET AREA- CORROSION ON FLOORBEAM AT HOLE- STA 987; RBL +44. REMOVED CORROSION IAW SRM 51-10-02. DAMAGE REMOVAL APPROX .065' OUT OF LIMITS PER SRM 53-70-51-1A-1. CUT & REMOVED DAMAGED PART OF FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6, ALTERNATIVE 4. VERApr 7, 2024 · N8685B · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2023121127776Seal · crackedRH HORIZONTAL STABILIZER FRONT SPAR UPPER SLIDING SEAL IS CRACKED.<[01] REMOVED AND REPLACED RH HORIZONTAL STABILIZER FRONT SPAR UPPER SLIDING SEAL PER AMM 53-31-31.Dec 5, 2023 · N8685B · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2023121127777Flap · delaminatedRH WING OUTBD AFT FLAP INBD SIDE IS DELAMINATED L=19.5X W=10.75<[01] REMOVED AND REPLACED R/H WING OUTBOARD AFT FLAP PER AMM 27-51-22 OPS RIG CK NORMAL;[02] REMOVED AND REPLACED R/H WING OUTBOARD AFT FLAP PER AMM 27-51-22 OPS RIG CK NORMALDec 5, 2023 · N8685B · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2023110919425Battery Pack · inoperativeMULTIPLE EMERGENCY LIGHTS ARE INOP THROUGHOUT THE CABIN AND EXTERIOR. / [01] REMOVED AND REPLACED AFT LEFT BATTERY PACK; ROW 21 ABC; AND ROW 21 DEF BATTERY PACKS IN REFERENCE TO AMM 33-51-06. EMERGENCY LIGHTING SYSTEM OPS CHECKS GOOD.Nov 8, 2023 · N8685B · Boeing 7378H4 · Emergency LightingSDR SWAA2023081487880Battery Pack · inoperativeRH FWD OVERWING & TWO RH FWD AISLE EMERGENCY LIGHTS ARE INOP<[01] REPLACED R/H FWD AISLE EMERGENCY BATTERY IAW AMM 33-51-06. OPS CHECK GOODAug 10, 2023 · N8685B · Boeing 7378H4 · Emergency LightingSDR SWAA2023051147292Sign · inoperativeL1 DOOR EXTERIOR LIGHT; LOWER WALL AND EMERGENCY EXIT SIGN ON L1 DOOR INOP<[01] R/R LH FWD EMERGENCY LIGHT POWER SUPPLY BATTERY PACK IAW AMM 33-51-06May 10, 2023 · N8685B · Boeing 7378H4 · Emergency LightingSDR SWAA2023033021427Battery Pack · inoperativeEMERGENCY EXIT LIGHT OVER AFT GALLEY SERVICE DOOR INOP<[01] R&R EMERGENCY LIGHT CHARGER AND BATTERY PACK AT R/H POSITION IN AFT GALLEY FDR CEILING COMPARTMENT IAW AMM 33-51-06Mar 28, 2023 · N8685B · Boeing 7378H4 · Emergency LightingSDR SWAA2022051201095Support Angle · corrodedAFT PIT FWD SHIELD SUPPORT ANGLE AT STA 767+7 WL 155 RBL 22 HAS CORROSION ON UPPER SURFCE / [01] REMOVED CORRODED FWD SHIELD SUPPORT ANGLE BS 767-787 RBL 22 IAW SRM 51-40-02-0G-0;[02] VERIFIED NEW FWD SHIELD SUPPORT ANGLE BS 767-787 RBL 22 IAW DWG 146A0081 REVApr 30, 2022 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022051200952Strap · corrodedDOT#68-186 AFT PIT FLOOR SPLICE STRAP CORRODED STA 887 LBL 3 TO RBL 4 WL 156 / [01] VERIFIED REPLACEMENT PART AS P/N 149A9401-39; ITEM #650;IAW AIPC 53-42-11-26. A-TAG # WN15356.;[02] REMOVED DAMAGED PART FROM A/C IAW AMM 25-52-10-000-801.;[03] VERIFIED STEPS Apr 29, 2022 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022051200956Angle · crackedDOT#67-186 AFT PIT LAV TANK LOWER BKHD STANTION (LEEK) ANGLE CRACKED STA 867 LBL 11 WL 156 / [01] REMOVED AND REPLACED CRACKED CLIP IN AFT CARGO COMPARMENT AT AFT BULKHEAD STA 850; LBL 11 IAW SRM 51-40-02-0G-0 AND BOEING DWG 149A8102 ID:0015 REV:A;[02] VERIFIEApr 29, 2022 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022051200955Shield · corrodedDOT#66-186 AFT PIT FWD SHIELD CORRODED STA 767+7 RBL 22 WL 156 / [01] REMOVED CORROSION FROM FWD SHIELD; ORIG T= .050' LOSS OF .008' REM T= .042' FOUND TO BE OUT OF LIMITS IAW SRM 53-60-151A-1 TOOLING INFO AAR 32351 CAL DUE 12/12/22;[02] VERIFIED STEP 1;[03] RApr 29, 2022 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022051200954Angle · corrodedDOT#65-186 AFT PIT Z ANGLE CORRODED STA 727I+7' TO 807 LBL 22 WL 156 / [01] REMOVED CORROSION. EVALUATED MATERIAL LOSS; ORIGINAL T .040; REMAINING .030; LOSS OF .010. OUT OF LIMITS IAW B737 SRM 53-00-53-1A-2.FIG 103 VIEW A-A. AAR TOOL #32351 CAL DUE 12/10/22.;Apr 29, 2022 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022051200353Floor Panel · corrodedFWD CARGO FLOOR PANEL 120 AF HAS CORROSION ALONG EDGE A225-003 / [01] BLENDED DAMAGE ON FWD CARGO FLOOR PANEL 120AF; DAMAGE EXCEEDS MAXIMUM ALLOWABLE DAMAGE OF 20 INCHES. FOUND TO BE OUT OF LIMITS I/A/W B737-800 SRM 53-00-53-1A-1;[02] VERIFIED MATERIAL TO BE UApr 28, 2022 · N8685B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022051200354Floor Panel · corrodedFWD CARGO FLOOR PANEL 120 BF HAS CORROSION ALONG EDGE A225-004 / [01] EVALUATED CORROSION EXCEED MORE 20 INCH MAXIMUM ALLOWED FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102;[02] VERIFIED STEP 1;[03] VERIFIED STEPS 1 AND 2;[04] VERIFIED. MATERIAL ID FOR FLOOApr 28, 2022 · N8685B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022051200355Floor Panel · corrodedFWD CARGO FLOOR PANEL 120 DF HAS CORROSION ALONG EDGE A225-005 / [01] REMOVED CKORROSION IAW SRM 53-00-53-1A-1. ORIGINAL THICKNESSS .071'; LOSS .020' REMAINING MATERIAL .051'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. AAR TOOL 32351 CAL DUE DATE 12/10/2Apr 28, 2022 · N8685B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022051200773Angle · corrodedFWD CARGO RH Z ANGLE CORRODED WL 156; BS 500A TO 500I ; RBL 25 A225-00I / [01] REMOVED CORROSION IAW SRM 51-10-02 10X MAGNIFY ORIGINAL THICKNESS.040 .010 MATERIAL REMOVED .030 MATERIAL REMAINS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 AAR TOOL NO.36644 DApr 28, 2022 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022051200772Shield · corrodedFWD CARGO AFT SHIELD CORRODED WL 156; BS 500 TO 500A ; RBL 25 A225-004 / [01] REMOVED CORROSION IAW SRM 51-10-02 10X MAGNIFY ORIGINAL THICKNESS .040 .015 MATERIAL REMOVED .052 MATERIAL REMAINS OUT OF LIMITS IAW SRM 53-00-53-1A-2 AAR TOOL NO.36644 DUE DATE 08/2Apr 28, 2022 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022051200771Support Angle · corrodedFWD CARGO AFT BLKD LOWER SUPPORT ANGLE CORRODED WL 156; BS 500I; RBL 25 TO LBL25 A225-003 / [01] REMOVED CORROSION IAW SRM 51-10-02 10X MAGNIFY MINIMUM ALLOWABLE MATERIAL REMAINING .056 .050 MATERIAL REMAINS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-08-1A-1 AAR Apr 28, 2022 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022051200776Angle · corrodedFWD CARGO LH Z ANGLE CORRODED WL 156; BS 500B - 8' TO 500I ; LBL 25 A225-006 / [01] REMOVED CORROSION IAW SRM 51-10-02 10X MAGNIFY ORIGINAL THICKNESS.040 .003 MATERIAL WAS REMOVED .037 MATERIAL REMAINS FOUND TO BE IN LIMITS IAW 53-00-53-1A-2 AAR TOOL NO.36644 Apr 28, 2022 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022051200769Stringer Clip · crackedSTRINGER CLIP CRACKED AT LOWER RIVET (FRAME ATTACH) BS 500I; WL 153; S26RH. UNDER Z ANGLE A225-001 / [01] REMOVED S26R STR CLIP SRM SRM 51-40-02-0G-0;[02] VERIFIED NEW STR CLIP AS P/N 143A1010-48 ATAG A02631 IAW DWG 143A1234 REV A;[03] VERIFIED STEP 2;[04] LOCApr 28, 2022 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022051200770Stringer Clip · crackedSTRINGER CLIP CRACKED AT LOWER RIVET (FRAME ATTACH) BS 500I; WL 153; S26LH. UNDER Z ANGLE A225-002 / REMOVED SECTION OF L/H Z-ANGLE STA 500D TO STA 500 I FOR ACCESS IAW SRM 51-40-02-0G-0;DISPLACED L/H SIDE AFT END OF BAFFLE STA 500I AT STR 26 FOR ACCESS IAW SRApr 28, 2022 · N8685B · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022051700349Panel · corrodedAFT CARGO FLOOR BOARD 140 AF CORRODED ALONG EDGE A225-003 / [01] EVALUATED PANEL AND FOUND PUNCTURE AND CORROSION EXCEEDING 20'. THIS IS OUT OF LIMITS IAW SRM 53-00-53-1A.;[02] VERIFIED ITEM 1<BR>VERIFIED MATERIAL AS 2024 T3 .071' IAW AMM 25-52-01-201-801;[03]Apr 27, 2022 · N8685B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022051200347Floor Panel · corrodedAFT CARGO FLOOR BOARD 140 EF CORRODED ALONG EDGE A225-001 / [01] CORROSION ON PANEL 140EF EXCEEDS THE 20' MAX LIMIT. PANEL FOUND OUT OF LIMITS IAW B-737 AMM 25-52-00-200-803.;[02] MATERIAL VERIFIED AS 0.071' 2024-T3 IAW B-737 AMM 25-52-01-201-801. A-TAG A12258Apr 27, 2022 · N8685B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022051200348Floor Panel · corrodedAFT CARGO FLOOR BOARD 140 BF CORRODED ALONG EDGE A225-002 / [01] EVALUATED CORRODED AREA ON FLOOR PNL 140BF FOUND LENGTH OF CORROSION MORE THEN 20' IS OUT OF LIMITS I.A.W SRM 53-00-53-1A-1;[02] VERIFIED MATERIAL FOR NEW PNL AS 2024-T3 .071 <BR>A TAG#A122584 I.Apr 27, 2022 · N8685B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022051200350Floor Panel · corrodedAFT CARGO FLOOR BOARD 140 DF CORRODED ALONG EDGE A225-004 / [01] EVALUATED CORROSION DAMAGE; FOUND TO BE OUT OF LIMITS DUE TO TOTAL ACCUMULATED DAMAGE BEING MORE THAN THE 20' MAX ALLOWED IAW SRM 53-00-53-1A-1;[02] MATERIAL VERIFIED FOR NEW PNL FAB; 2024-T3 .07Apr 27, 2022 · N8685B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022051200351Floor Panel · corrodedAFT CARGO FLOOR BOARD 140 CF CORRODED ALONG EDGE A225-005 / [01] REMOVED CORROSION IAW SRM 53-00-53-1A-1. ORIGINAL THICKNESS .071' LOSS .020'; REMAINING MATERIAL .051' OUT OF LIMITS IAW SRM 53-00-53-1A-1. AAR TOOL 32351 CAL DUE DATTE 12/10/22.;[02] VERIFIED MAApr 27, 2022 · N8685B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022051200352Bulkhead · crackedAFT CARGO FORWARD BULKHEAD 142 NWB CRACKED A225-006 / [01] VERIFIED AND REPLACED AFT CARGO FWD BULKHEAD PANEL # 142NWB ON PARTS RACK IAW IPC 25-52-19-01B AND BOEING DWG# 453A25110 ID:0001 REV:C;[02] VERIFIED STEP 1 COMPLETE<BR>AUDIT C/WApr 27, 2022 · N8685B · Boeing 7378H4 · Fuselage Main, BulkheadSDR SWAA2022012062428Web · crackedLEFT WING OUTBD SUPPORT CLIP FROM DEFLECTION CONTROL RIB TO AFT WEB BRACKET CRACKED. ; / [01] REMOVED AND REPLACED CLIP REF SRM 51-40-02Jan 19, 2022 · N8685B · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2021032256990Access Door · brokenEXTERNAL AIR DOOR HINGE BROKEN ( MX NOTE ) DOOR SPEED TAPE CLOSED / R&R'D THE FWD FAIRING ACCESS DOOR; REF AMM 52-49-01. REF LOG PAGE 0458850Mar 18, 2021 · N8685B · Boeing 7378H4 · Service DoorsSDR SWAA2021020446592Skin · crackedHFEC CRACK INDICATION ON DAMAGE BLENDED AREA AT BS 787+11' STR 3R. (ORIGINAL RIGHT UP NR # D352660) / ACCOMPLISHED PERMANENT REPAIR PER EA# 21-153-00223Feb 2, 2021 · N8685B · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2020122838229Handle · looseFWD MEGA PHONE NOT WORKING AND HANDLE IS LOOSE. REPLACED MEGA PHONE PER SIP.Dec 22, 2020 · N8685B · Boeing 7378H4 · Emergency EquipmentSDR SWAA2020081909106Blade · dentedDAMAGE FOUND DURING WALK AROUND ON #1 ENG BLADE # 16. DENT/GOUGE LOCATED 2 DIFFERENT LOCATIONS ON LEADING EDGE BLADE SEQ. REPLACEMENT / REMOVED AND REPLACED #1 ENG BLADE #16 IAW MT 772-21-19 AND AMM 72-21-02 A/C OK FOR SERVICE ACCOMPLISHED MT 772-21-22P/N OFF Aug 15, 2020 · N8685B · Boeing 7378H4 · Turbine Engine Air Inlet SectionSDR SWAA2016102509072Glowstrip · inoperativeRT FORWARD CABIN PHOTO LUMINESCENT LIGHT INOP AT ROW 1. R&R STRIP PER AMM.Oct 25, 2016 · N8685B · Boeing 7378H4 · Emergency Equipment
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