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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR 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 51-40-02SDR 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; DESDR 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;[0SDR 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 SRSDR 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 SRSDR SWAA2021071291959Battery Pack · inoperativeDURING OPS CHECK OF EMERGENCY LIGHTS FOUND FWD BATTERY PACK (M01675) INOP /SDR SWAA2021090877419Structure · crackedCRACK INDICATION FOUND AT WSTA 736.50 FASTENER HOLE OF RIB 26 MARKED IN BLACK. /SDR SWAA2021090876819Skin · buckledFOUND BUCKLING ON RIGHT WING LOWER SKIN PANEL; BETWEEN FUEL ACCESS PANELS; BEWEEN WSTA 564.5 AND 616.75 /SDR SWAA2021090876102Spar · damagedWHILE ACCOMPLISHING TASK 21-157-01428 FOUND 6.5' CREASE AT WBL639.5-WBL633 FWD OF OUTER LOWER SPAR WALL. /SDR 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 /SDR 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.SDR SWAA2021090876101Spar · buckledAFT SPR WALL HAS A 4' BUCKLE 13'-17' FROM CLOSURE RIB (WING TIP). /SDR SWAA2020113032738Strap · brokenAFT LEFT SIDE EMERGENCY FLASHLIGHT STRAP BROKEN. R & R STRAP, PER AMM 25-64-00.SDR SWAA2019060733417Megaphone · weakFORWARD MEGAPHONE WEAK. / REPAIRED MEGAPHONE PER AMM.SDR 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 001780SDR SWAA2019040531410Skin · delaminatedR/H WING OUTBOARD TRAILING EDGE AFT FLAP LOWER SKIN DELAMINATED. / R&R AFT FLAP PER AMM.SDR 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 # 201SDR SWAA2018082224512Skin · delaminatedRT WING OUTBOARD AFT FLAP UPPER SKIN DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA2018030120176Flashlight · inoperativeAFT LEFT INBOARD FLASHLIGHT INOPERATIVE. R & R THE FLASHLIGHT IAW CMM.SDR SWAA2017061914453Light · brokenLT FORWARD EMERGENCY EXIT LIGHT LENS COVER BROKEN. R&R LIGHT ASSEMBLY PER AMM.
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