N776AS
Service difficulty reports not matched to an aircraft · 110
They name N776AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N776AS' AND registry_match IS NULL 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 = 'N776AS' AND registry_match IS NULL 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 ASAA0944356Jam-Nut · looseR 1 DOOR HARD TO CLOSE FROM INSIDE CABIN. PERFORMED INSPECTION OF R 1 DOOR MECHANISM PER AMM 52 41 00 206 001. FOUND JAM NUT ON TOP HINGE GUIDE ARM LOOSE. COMPLIED WITH PARALLEL ADJUSTMENT PER AMM 52 441 00 990 815 001. R 1 DOOR OPS NORMAL.SDR ASAA0843345Nut · looseL1 DOOR VERY STIFF HARD TO OPEN. PERFORMED VISUAL INSP OF L1 DOOR FOUND GUIDE ARM LOCK NUT LOOSE. TIGHTENED LOCK NUT IAW AMM 52 11 00 705 007 B00. PERFORMED FWD ENTRY DOOR TEST IAW AMM 52 11 00 755 051 B00. OPS CK GOOD. NO FURTHER DEFECTS NOTED AT THIS TISDR ASAA0843328Beam · crackedBS 601, STUB BEAM INNER HORD LOWER FASTENER HOLE CRACKED REPAIRED IAW EA 5310-02807.SDR ASAA0843327Skin · corrodedEXFOLIATION CORROSION FOUND ON UPPER WING SKIN AT FS 608.5 RBL 62 REPAIRED IAW EA 5710 01153.SDR ASAA0843326Skin · corrodedEXFOLIATION CORROSION FOUND ON UPPER WING SKIN AT FS 592 RBL 63 REPAIRED IAW EA 5710 01153.SDR ASAA0843325Skin · corrodedEXFOLIATION CORROSION FOUND ON UPPER WING PLANK AT FS591, RBL67 REPAIRED IAW EA 5710 01153.SDR ASAA0843324Skin · corrodedEXFOLIATION CORROSION FOUND ON UPPER WING PLANK AT FS 661, RBL 57 REPAIRED IAW EA-5710 01153.SDR ASAA0741629Shear Tie · crackedSHEAR TIE CRACKED. CUT OUT DAMAGED SECTION OF FRAME (SHEAR TIE) FABRICATED AND INSTALLED A REPAIR SHEAR TIE DOUBLER AND RADIUS FILLERS IAW SRM 53 00 07 FIG 201 REPAIR 5.SDR ASAA0741628Skin · puncturedTHE IB FORE FLAP IS PUNCTURED NEAR THE CENTER TRACK. REMOVED THE DAMAGED AREA OF LWR SKIN FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51 70 10 PARA 8 11 15 18 AND 20.SDR ASAA0741627Skin · chafedTHE RT OB MID FLAP IS CHAFED ON AN EXITING LE DOUBLER AT THE IB END. REMOVED THE EXITING REPAIR DOUBLER FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 57 53 01 FIG 201 REPAIR 8.SDR ASAA0741626Skin · crackedNR 2 SLAT SKIN LWR LIP IS CRACKED AROUND FASTENER HOLES JUST BELOW THE O B AUX TRACK. CUT OUT THE DAMAGED AREA OF SKIN FABRICATED AND INSTALLED A SKIN FILLER AND EXTERNAL SPLICE PLATE IAW SRM 57 40 01 FIG 206 REPAIR 6.SDR ASAA0741625Skin · damagedOUTWARD DING IN FUSELAGE SKIN REMOVED SKIN DAMAGE BY DRILLING A 0.1935" HOLE INSTALLED A BACR15BB6 RIVET IAW ASA EA 5330 02205 REV NEW AND AAR EA 112004 REV IR.SDR ASAA0741623Doubler · chafedRT IB FORE FLAP CHAFED ON AN EXITING REPAIR DOUBLER ON THE UPPER SIDE. REMOVED THE EXITING REPAIR DOUBLER AND FILLER FABRICATED AND INSTALLED A REPLACEMENT DOUBLER AND FILLER IAW SRM 51 70 10 PARA 7 8 11 15 18 AND 20.SDR ASAA0741622Skin · dentedLT IB FOR FLAP DENTED OUT OF LIMITS NEAR CENTER TRACK. REMOVED THE DAMAGED AREA OF LOWER SKIN FABRICATED AND INSTALLED A SKIN FILLER AND REPAIR DOUBLER IAW SRM 51 70 10 PARA 8 11 15 18 AND 20.SDR ASAA0741621Skin · delaminatedLT ELEV TAB UPPER SURFACE T E IS SPLIT 51" FROM I B END. PREPPED THE TAB UPPER SKIN SURFACE FOR BONDING CUT AND APPLIED REPAIR PLIES IAW SRM 51 70 05 PAPR 3.SDR ASAA0640270Skin · dentedSKIN DENTED. FABRICATED AND INSTALLED REPAIR PARTS PER EA 5330 02061 AND ER 06 1486.SDR ASAA0640265Skin · dentedFUSELAGE SKIN DENT. REPAIRED PER EA 5330 02064 AND EO 06 1319.SDR ASAA0640260Door Frame · crackedL1 DOOR FRAME CRACKED AT LOWER STOP FITTING FWD SIDE. REPAIRED PER EA 5310 02594.SDR ASAA0640254Skin · chafedCHAFE MARKS ON SKIN. INSTALLED REPAIR PER ASA EA 5360 01055.SDR ASAA0640255Floorbeam · corrodedFLOORBEAM CORRODED. REMOVED CORRODED AREA AND INSTALLED REPAIR PER EA 5310 02591.SDR ASAA0640234Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM. REPAIRED PER GOODRICH ER 06 1383 AND ASA EA 5310 02585.SDR ASAA0640229Floorbeam · corrodedFOUND TOP FLANGE OF FLOORBEAM CORRODED. REPAIRED PER SRM 51 70 11.SDR ASAA0640228Frame · crackedFOUND BSTA 907 STR 8L FRAME CRACKED. REPAIRED PER SRM 53 00 07.SDR ASAA0640225Floorbeam · corrodedFOUND TOP FLANGE OF FLOORBEAM AT BSTA 360 RBL 12 TO 25 WL 208 CORRODED. REPAIRED FLOORBEAM PER SRM 51 70 11.SDR ASAA0640221Sill · corrodedAFT SERVICE DOOR CREASE BEAM MOPSILL CORRODED. REMOVED AND REPLACED AFT SVC DOOR MOPSILL PER SRM 51 40 02.SDR ASAA0640207Web · crackedFOUND FLOOR WEB IS CRACKED. REMOVED AND REPLACED WEB.SDR ASAA0640199Crease Beam · corrodedFOUND CREASE BEAM CORRODED. REPLACED CREASE BEAM PER SRM 51 40 02.SDR ASAA0640198Frame · chafedFOUND FRAME FLANGE CHAFED. REPAIRED PER SRM 51 70 11.SDR ASAA0640195Angle · corrodedCORROSION ON THRESHOLD Z ANGLE. REMOVED AND REPLACED PER SRM 51 40 02.SDR ASAA0640193Frame · crackedCRACKED FRAME AT BIN RAIL ATTACHMENT. REPAIRED PER SRM 53 00 07SDR ASAA0640194Stringer Clip · crackedCRACKED STRINGER CLIP. REMOVED AND REPLACED PER SRM 51 40 02.SDR ASAA0640192Shear Tie · corrodedCORRODED SHEAR TIE. REPAIRED PER SRM 53 00 07.SDR ASAA0640191Shear Tie · corrodedCORRODED SHEAR TIE. REPAIRED PER SRM 53 00 07.SDR ASAA0640190Shear Tie · corrodedCORRODED SHEAR TIE. REPAIRED PER SRM 53 00 07.SDR ASAA0640189Shear Tie · corrodedCORRODED SHEAR TIE. REPAIRED PER SRM 53 00 07.SDR ASAA0640188Shear Tie · corrodedCORROSION ON SHEAR TIE. REMOVED AND REPAIRED PER SRM 53 00 07.SDR ASAA0640187Crease Beam · corrodedCORROSION AT RT SIDE CREASE BEAM. REMOVED AND REPLACED OUT OF LIMITS CORRODED CREASE BEAM PER SRM 57 48 02.SDR ASAA0640186Stringer Clip · chafedSTRINGER CLIP CHAFED. REMOVED AND REPLACED STRINGER CLIP PER SRM 51 40 02.SDR ASAA0640166Floorbeam · corrodedCORRODED FLOOR BEAM.SDR ASAA0640165Floorbeam · corrodedFLOOR BEAM FASTENER HOLES HAVE CORROSION.SDR ASAA0640164Stringer Clip · crackedSTRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM 51 40 02.SDR ASAA0540278Skin · dentedDENT FOUND AT LT WING IB T/E FORE FLAP. REPAIRED LT WING IB T/E FORE FLAP IAW SRM. (K)SDR ASAA0540277Skin · gougedLT WING UPPER SKIN GOUGED AT WING STA 223 BETWEEN STA 12 AND 13. BLENDED AREA, TREATED AND PRIMED IAW EA. (K)SDR ASAA0540276Skin · chafedNR 4 SLAT IB T/E CHAFED. REMOVED DAMAGE, FABRICATED FILLER SKIN AND DOUBLER AND INSTALLED REPAIR IAW SRM. (K)SDR ASAA0540268Skin · delaminatedLT WING OB FORE FLAP DELAMINATED AT IB END. REMOVED DAMAGED AREA OF LT OB FORE FLAP IAW SRM. (K)SDR ASAA0540267Skin · delaminatedRT WING OB AFT FLAP DELAMINATED AT IB TRAILING EDGE. REMOVED DAMAGED MATERIAL, INSTALLED CORE, SKIN, AND DOUBLER IAW SRM. (K)SDR ASAA0540266Skin · delaminatedNR 2 SLAT HAS DELAMINATED AT IB TRAILING EDGE. REPAIRED DAMAGED AREA OF NR 2 SLAT IAW SRM. (K)SDR ASAA0540269Shear Tie · crackedSHEAR TIE CRACKED AND CORRODED AT STR 28L B-STA 500G. FABRICATED SHEAR TIE, REMOVED AND REPLACED SHEAR TIE IAW SRM AND MFG DWG. (K)SDR ASAA0540265Shear Tie · corrodedSHEAR TIE BETWEEN STR 26L AND 25R, B-STA 947 HAS SURFACE CORROSION. REMOVED FABRICATED AND INSTALLED SHEAR TIE AND CLIP IAW SRM . (K)SDR ASAA0540264Skin · corrodedNR 5 SLAT IB TRAILING EDGE CHAFED. REMOVED DAMAGE, BONDED FILLER SKIN AND DOUBLER IAW SRM. (K)
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