N8686A

Service difficulty reports · 71

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 = 'N8686A' 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 SWAA2022041287876Transition Panel · corrodedAFT CARGO COMPARTMENT RH TRANSITION ANGLE HAS CORROSION 767 - 794 (MARKED) / [01] R/H TRANSITION ANGLE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED TRANSLATION ANGLE.;[03] REMOVED AND REPLACED R/H TRANSITION ANGLE FROM STA 767-794.Mar 25, 2022 · N8686A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022041287697Support Angle · crackedR/H WING TRAILING EDGE PANEL#651FB HAS 1EA SUPPORT ANGLE CRACKED. (MARKED) / [01] REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-40-02.;[02] 1. MICHAEL BALLERT (TECHNICIAN); 31-MAR-2022 12:34 UTC<BR>REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-40-02Mar 24, 2022 · N8686A · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2022041287468Transition Panel · corrodedFORWARD CARGO COMPARTMENT CORROSION FOUND ON RH TRANSITION ANGLE UPPER SURFACE FORM STA 500A-500B; RBL 24; AND WL 156 / [01] FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] REMOVED R/H TRANSITION ANGLE FROM STA 500A TO STA 500I; PICKED UP HOLES; DEMar 23, 2022 · N8686A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022041287466Support Angle · corrodedFORWARD CARGO COMPARTMENT CORROSION FOUND ON AFT BULKHEAD FLOOR SUPPORT ANGLE UPPER SURFACE AT STA 500I; LBL 24 TO RBL 24; AND WL 156. / [01] FOUND TO BE OUT OF LIMITS IAW SRM 53-30-08-1A-1 REMOVED ANGLE PER SRM 51-40-02; DRILLED NEW PART; AND OK TO INSTALL;[0Mar 23, 2022 · N8686A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022041287176Angle · chafedVERTICAL STABILIZER PANEL MATING SURFACES ON THE RIGHT FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAVE AREAS OF CHAFFING FROM CONTACT OF CLOSURE PANELS / [01] REMOVED FWD AND AFT RH SIDE SKATE ANGLES IAW SRM 51-40-02.;[02] INSTALLED RH FWD SKATE ANGLE IAW SRMar 23, 2022 · N8686A · Boeing 7378H4 · Vertical StabilizerSDR SWAA2022041287175Angle · chafedVERTICAL STABILIZER PANEL MATING SURFACES ON THE LEFT FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAVE AREAS OF CHAFFING FROM CONTACT OF CLOSURE PANELS. / [01] REMOVED LEFT AFT SKATE ANGLE PER SRM 51-40-02.;[02] REMOVED AND REPLACED L/H AFT SKATE ANGLE PER SRMar 23, 2022 · N8686A · Boeing 7378H4 · Vertical StabilizerSDR SWAA2021071291959Battery Pack · inoperativeDURING OPS CHECK OF EMERGENCY LIGHTS FOUND FWD BATTERY PACK (M01675) INOP /Jul 7, 2021 · N8686A · Boeing 7378H4 · Emergency LightingSDR SWAA2021090877419Structure · crackedCRACK INDICATION FOUND AT WSTA 736.50 FASTENER HOLE OF RIB 26 MARKED IN BLACK. /May 27, 2021 · N8686A · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2021090876819Skin · buckledFOUND BUCKLING ON RIGHT WING LOWER SKIN PANEL; BETWEEN FUEL ACCESS PANELS; BEWEEN WSTA 564.5 AND 616.75 /May 25, 2021 · N8686A · Boeing 7378H4 · Wing, Plate/SkinSDR SWAA2021090876102Spar · damagedWHILE ACCOMPLISHING TASK 21-157-01428 FOUND 6.5' CREASE AT WBL639.5-WBL633 FWD OF OUTER LOWER SPAR WALL. /May 24, 2021 · N8686A · Boeing 7378H4 · Wing SparSDR SWAA2021090876099Skin · buckledRT. WING LOWER AFT EDGE INSPAR SKIN HAS A 2.0 BUCKLE 10' FROM CLOSURE RIB (WING TIP). APEX OF BUCKLE IS .020' FROM FARED /May 24, 2021 · N8686A · Boeing 7378H4 · Wing, Plate/SkinSDR SWAA2021090876100Skin · buckledRT WING LOWER AFT EDGE INSPAR SKIN HAS A 3.5' BUCKLE 14.5' FROM CLOSURE RIB (WING TIP). APEX OF BUCKLE IS .080 FROM FARED.May 24, 2021 · N8686A · Boeing 7378H4 · Wing, Plate/SkinSDR SWAA2021090876101Spar · buckledAFT SPR WALL HAS A 4' BUCKLE 13'-17' FROM CLOSURE RIB (WING TIP). /May 24, 2021 · N8686A · Boeing 7378H4 · Wing SparSDR SWAA2020113032738Strap · brokenAFT LEFT SIDE EMERGENCY FLASHLIGHT STRAP BROKEN. R & R STRAP, PER AMM 25-64-00.Nov 26, 2020 · N8686A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2019060733417Megaphone · weakFORWARD MEGAPHONE WEAK. / REPAIRED MEGAPHONE PER AMM.Jun 5, 2019 · N8686A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2022022453896Flap · delaminatedR/H WING OUTBOARD TRAILING EDGE AFT FLAP LOWER SKIN DELAMINATED AT OTEF 56.83; MEASURING 4.5 INCHES LONG BY 3.7 INCHES WIDE / REMOVED AND REPLACED RH OTBD AFT FLAP PER AMM 27-51-22RT OTBD P/N OFF 113A3700-20; P/N ON 113A3700-22; S/N OFF 001257; S/N ON 001780Apr 5, 2019 · N8686A · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2019040531410Skin · delaminatedR/H WING OUTBOARD TRAILING EDGE AFT FLAP LOWER SKIN DELAMINATED. / R&R AFT FLAP PER AMM.Apr 5, 2019 · N8686A · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2022021853891Skin · delaminatedRIGHT WING OUTBOARD AFT FLAP UPPER SKIN IS DELAMINATED 3 INCHES IN DIAMETER 4 INCHES FROM INBOARD EDGE X 3 INCHES FROM AFT EDGE / SEALED DAMAGED AREA WITH SPEED TAPE ON R/H WING O/B AFT FLAP REF SRM 57-53-01-1A-4. SEE EC/TC REPAIR 57EA-05596 TSR TRACKING # 201Aug 21, 2018 · N8686A · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2018082224512Skin · delaminatedRT WING OUTBOARD AFT FLAP UPPER SKIN DELAMINATED. REPAIRED AFT FLAP PER SRM.Aug 21, 2018 · N8686A · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2018030120176Flashlight · inoperativeAFT LEFT INBOARD FLASHLIGHT INOPERATIVE. R & R THE FLASHLIGHT IAW CMM.Mar 1, 2018 · N8686A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2017061914453Light · brokenLT FORWARD EMERGENCY EXIT LIGHT LENS COVER BROKEN. R&R LIGHT ASSEMBLY PER AMM.Jun 17, 2017 · N8686A · Boeing 7378H4 · Emergency Lighting
Back to N8686A