N179US, cancelled Jun 30, 2006
Service difficulty reports · 63
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 = 'N179US' AND deregistration_id = 'N179US-2006-06-30' 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 = 'N179US' AND deregistration_id = 'N179US-2006-06-30' 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 A6WA200560016Fuel Control · unserviceableCLIMBING THRU 9000 FT NR 1 ENGINE STARTED TO WIND DOWN. BOTH N1 AND N2 WERE DROPPING, TGT APPEARED TO BE RISING. SECURED ENGINE, PERFORMED IMMEDIATE ACTION CHECKLIST C/W QRH. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. (K)SDR A6WA200160048Structure · wornWEAR DAMAGE TO THE LOWER L/E OF THE LT FLAP IN THE RECESSED AREA BETWEEN RIBS 25 AND 31. MAINTENANCE REPAIRED WEAR DAMAGE IAW BAE FAX BARA/AVR/6894/04-DC.SDR A6WA200460009Hook · damagedDAMAGE TO DOOR HOLD OPEN HOOK AREA ON THE DOOR, AND ASSOCIATED RECEPTICLE ON THE FUSELAGE, FORWARD PASSENGER DOOR. MAINTENANCE REPLACED UPPER HINGE AND HOLD OPEN LATCH HOUSING. REPAIRED DAMAGE TO THE FORWARD PASSENGER DOOR IAW BAE FAX REF NR BARA/AVR/6690/04SDR A6WA200260046Control Valve · malfunctionedDURING CLIMB, EXPERIENCED SLIGHT HAZE IN COCKPIT FOLLOWING SHUTDOWN OF NR 1 AND NR 2 PACKS, HAZE DISSIPATED. MAINTENANCE RAN BOTH PACKS, VERIFIED NR 1 PACK INOPERATIVE. REMOVED AND REPLACED PACK TEMP CONTROL VALVE. (M)SDR A6WA200260021Frame · crackedCRACKS AND CORROSION TO LOWER HALF OF FRAME 18 FROM 18L TO STR 18R.SDR A6WA200100023Engine · power lossON CLIMBOUT IN ICING CONDITIONS, NR 1 ENGINE POWER DECAYED WITH TAIL AND WING ANTI-ICE ON N1 WENT TO 82 PERCENT, N2 WENT TO 84 PERCENT. MAINTENANCE INSPECTED ALL CHIP DETECTORS, BLEED BAND ACTUATOR, OPS CHECK GOOD. NO DEFECTS NOTED.SDR A6WA200000080Aileron · malfunctionedAILERON OUT OF TRIM LIGHT ON M/A TURNED OFF A/P MASTER SWITCH, ALL FLIGHT CONTROLS AND TRIM WORK OK. MAINTENANCE OPERATIONAL TEST OK, COULD NOT DUPLICATE.SDR A6WA200000060Skin · dentedDENT AT FRAME 20-20A STRINGER 18 LT SIDE. REPAIRED DENT AT FRAME 20-20A STRINGER 18 LT SIDE IAW BAE FAX REF BARA/AVR/5135/00 AND RIC HC536H9251. NO FURTHER REINSPECTS REQUIRED.SDR A6WA0000015Pump · malfunctionedWHILE EN ROUTE, MWS LIGHT CAME ON, HYD PANEL SHOWED LOW PRESSURE AND LOW QUANTITY YELLOW SYSTEM. REMOVED AND REPLACED NR 3 ENGINE DRIVEN HYDRAULIC PUMP. (M)SDR A6WA9900059Bracket · crackedLEFT GLIDESLOPE ANTENNA BRACKET IS CRACKED. REPLACED ANTENNA BRACKET. (X)SDR A6WA9900060Structure · crackedAFT CARGO DOOR, AFT UPPER HINGE POINT IS CRACKED. REPAIRED CRACKS IAW BAE REPAIR NR HC523H9001. RE-PROFILED AFT BOTTOM SEAL CAGE. (X)SDR A6WA9900078Seat · crackedSEAT PAN ON SEAT 3C IS CRACKED. REPLACED SEAT PAN 3C. (X)SDR A6WA9900077Seat · crackedSEAT PANS 4A AND 4C ARE CRACKED. REPLACED SEAT PANS 4A AND 4C. REF: OPERATOR CONTROL NR 99ZZZX3107. (X)SDR A6WA9900076Seat · crackedSEAT PAN 7C IS CRACKED. REPLACED SEAT PAN 7C. (X)SDR A6WA9900075Seat · crackedSEAT PAN 9A IS CRACKED. REPLACED SEAT PAN 9A. (X)SDR A6WA9900074Seat · crackedSEAT PAN 10A AND 10C ARE CRACKED. REPLACED SEAT PANS 10A AND 10C. REF: OPERATOR CONTROL NR 99ZZZX3109. (X)SDR A6WA9900073Seat · crackedSEAT PAN 1D IS CRACKED. REPLACED SEAT PAN 1D.SDR A6WA9900072Seat · crackedSEAT PANS 7D AND 7F ARE CRACKED. REPLACED SEAT PAN 7D AND 7F. REF: OPERATOR CONTROL NR 99ZZZX3108. (X)SDR A6WA9900071Seat · crackedSEAT PAN 8F IS CACKED. REPLACED SEAT PAN 8F. (X)SDR A6WA9900070Seat · crackedSEAT PAN 10D IS CRACKED. REPLACED SEAT PAN 10D. (X)SDR A6WA9900069Seat · crackedSEAT PAN 13D IS CRACKED. REPLACED SEAT PAN 13D. (X).SDR A6WA9900068Seat · crackedSEAT PAN 15D IS CRACKED. REPLACED SEAT PAN 15D. (X)SDR 99ZZZX3109Seat · crackedSEAT PAN 10A AND 10C ARE CRACKED. REPLACED SEAT PANS 10A AND 10C. REF: OPERATOR CONTROL NR A6WA9900074.SDR 99ZZZX3108Seat · crackedSEAT PANS 7D AND 7F ARE CRACKED. REPLACED SEAT PAN 7D AND 7F. REF: OPERATOR CONTROL NR A6WA9900072.SDR 99ZZZX3107Seat · crackedSEAT PANS 4A AND 4C ARE CRACKED. REPLACED SEAT PANS 4A AND 4C. REF: OPERATOR CONTROL NR A6WA9900077.SDR A6WA9900067Stiffener · crackedFROM EO E95/003/653 STIFFENERS ON FORWARD SIDE FRA 29 STA 25.94 LEFT AND RIGHT AND 31.13 LEFT AND RIGHT HAVE ONE A-BOLT HOLE CRACKED. EO E95/005/653 NEEDS COMPLIANCE AT CRACKED LOCATIONS. REPAIRED STIFFENERS AT FRA 29 STATIONS LEFT AND RIGHT 25.94 AND 31.13 SDR A6WA9900066Fastener · damagedPERFORMED RIL HC571H9033 LEFT RIB 2 OUTBOARD JO-BOLTS. C/W RIL HC571H9033 TO LEFT RIB 2 JO-BOLT REPLACEMENT. (X)SDR A6WA9900065Fastener · damagedPERFORMED RIL HC571H9033 LEFT RIB 2 INBOARD JO-BOLTS. C/W RIL HC571H9033 TO ABOVE LEFT RIB 2 JO-BOLT REPLACEMENT. (X)SDR A6WA9900064Fastener · damagedPERFORMED RIL HC571H9033 LT CENTER TANK RIB 0 JO-BOLTS. C/W RIL HC571H9033 TO LEFT CENTER TANK RIB 0 JO-BOLT REPLACEMENT. (X)SDR A6WA9900063Fasteners · damagedPERFORMED RIL HC571H9033 RT RIB 2 OUTBOARD JO-BOLTS. C/W RIL HC571H0933 RT WING SIDE OF RIB 2 JO-BOLT REPLACEMENT. (X)SDR A6WA9900062Fastener · damagedPERFORMED RIL HC571H9033 ON RT RIB 2 INBOARD JO-BOLTS. C/W RIL HC571H0933 RT RIB 2 CENTER TANK SIDE JO-BOLT REPLACEMENT. (X)SDR A6WA9900061Fastener · damagedPERFORMED RIL HC571H9033, RT RIB 0 JO BOLTS. C/W RIL - HC571H9033 TO RT CENTER TANK RIB 0 JO-BOLT REPLACEMENT. (X)SDR A6WA9900058Door · crackedFORWARD LAVATORY SERVICE DOOR CRACKED NEAR HINGE AREA. REPAIRED IAW BAE FAX REF NR BARA/AVR/3589/99. (X)SDR A6WA9900042Flow Valve · failedDURING E.O. INSPECTION, VALVE FAILED STEP 3. FLAP VALVE MOVED COMPLETELY FREE WITH NO DAMPING ACTION ABOUT THE HOLLOW RIVET. REMOVED AND REPLACED VALVE ASSY. (X)SDR 98ZZZX3966Bolt · crackedATW - NLG UPPER ACTUATOR MOUNT BOLT HEAD HAS CRACKED INDICATION. VERIFIED BY NDT 8-31-98 ID NR 042. REPLACED BOLT (INNER) ONE-HALF DIAMETER AT NL9 UPPER ATTACH POINT FOR ACTUATOR IAW BAE 146 MM. REF W/C 7050 FOR RETRACTION TEST.SDR 98ZZZX3965Diaphragm · crackedATW - REF W/C 7030, NLG DIAPHRAGM AT ATTACHMENT POINT OF NLG RAM HAS BEEN FOUND CRACKED AT 6 O'CLOCK POSITION. CRACK EXTENDS DOWNWARD FROM AND INTO THE PIN HOLE .125 INCH. REPORTED TO AVRO/BAE RDO AND AWAITING FOR REPAIR ACTION. REPAIRED NLG DIAPHRAGM (LT) SDR 98ZZZX3969Longeron · chafedATW - AIRBRAKE ACTUATOR HAS CHAFED RIGHT FUSELAGE UPPER LONGERON APPROXIMATELY .030 INCH DEEP. REPAIRED RT FUSELAGE UPPER LONGERON AT AIRBRAKE ACTUATOR IAW BAE FAX DJR/RJ0681-98, AVRO FAX DJR/RF0638-96, AND PRODUCTION DRAWING NR HC539H0229.SDR 98ZZZX3955Bulkhead · corrodedATW - BULKHEAD AFT OF FRAME 50 (ABOVE AIRBRAKE ACTUATOR) IS CRACKED IN RT LOWER CORNER AND ABOUT 4 INCHES FROM LEFT CORNER. ALSO, RIVETS LOOSE IN BOTH CORNERS. REPAIRED RT AND LT CORNER AREAS OF BULKHEAD JUST AFT OF FRAME 50 IAW BAE FAXES DJR/RJ0602-98, JIM/SDR 98ZZZX3972Seat Track · wornATW - SEAT TRACK RAIL, STA 252.33, FRAMES 20-20A, LT INBOARD CORRODED AND WORN BEYOND LIMITS. REPLACED FORWARD SECTION OF SEAT RAIL 87 INCHES TOTAL AND SPLICED PER SRM 53-00-32, PAGE 202.SDR 98ZZZX3964Bracket · corrodedATW - REF EO E92/067/632 REV A, LEFT HINGE BRACKET MISSING BUSHING, HOLE OVER SIZE, CORROSION AROUND HOLE IAW ITEM 6 SECT I. REMOVED LEFT HINGE BRACKET WRK 1032. INSTALLED SERVICEABLE LT HINGE BRACKET WITH REPLACEMENT HARDWARE AS REQUIRED.SDR 98ZZZX3963Skin · lightning strikeATW - DURING LIGHTNING STRIKE INSPECTION, NOTED ONE MINOR SKIN PIT BETWEEN FRAMES 4 AND 5, STR 19L. CLEANED AND PREPPED AREA. DAMAGE MEASURED AT .014 INCH DEPTH. PER BAE FAX, INSTALLED A .1250 INCH RIVET SL4070-32. BAE FAX DJR/RJ0682-98.SDR 98ZZZX3961Skin · lightning strikeATW - DURING LIGHTNING STRIKE INSPECTION, NOTED ONE MINOR SKIN PIT BETWEEN FRAMES 5 AND 7 APPROXIMATELY STR 19L. CLEANED AND PREPPED AREA. DAMAGED MEASURED AT .007 INCH DEPTH. PER BAE FAX, INSTALLED A .1250 INCH RIVET SL4070-32, BAE FAX DJR/RJ06820-98.SDR 98ZZZM831Bracket · damagedREF EO E92/067/632 REV A, RIGHT HINGE BRACKET HAS DEEP IMPACT DAMAGE AROUND BOLT HOLE AND CORROSION IAW ITEM 10 SECTION I. REMOVED RIGHT HINGE BRACKET WRK 1032. INSTALLED SERVICEABLE HINGE BRACKET WITH REPLACEMENT HARDWARE AS REQUIRED. (M)SDR 98ZZZX3990Skin · gougedATW - PER FAX DS/W/TJ/28015/97 AND DJR/RJ0912-96. SEVERAL GOUGES TO DENTS AFT OF FRAME 20 AND ABOVE LAP SEAM AT STR 19 MUST BE REPAIRED BY TCA OF 22593 TCA TO CORRESPOND WITH DUE TIME OF C-CHECK CURRENTLY SCHEDULED FOR 5-31-98. REPAIRED IAW BAE FAX REF NR DJSDR 98ZZZX3974Longeron · crackedATW - FRAME 29 TOP LANDING GEAR LONGERONS CRACKED NR 3 AND NR 19 OUTBOARD OF BOTH OUTBOARD SEAT TRACK RAILS. REPAIRED AT FRAME 19, FLOOR BEAMS NR 3 AND NR 19 AT FORWARD OUTBOARD POSITIONS IAW BAE REPAIR DRAWING NR HC536H9211 AND BAE FAX NR DJR/RJ0207-97. (X)SDR 98ZZZX3968Intercostal · corrodedATW - FORWARD VEST INTERCOSTALS, SILL PLATES NEED CLEANING AND SEALANT, INSPECTED FOR CORROSION. CLEANED AND INSPECTED. REMOVED MINOR CORROSION AND TREATED METAL, PRIMED, PAINTED, AND SEALED FORWARD VEST INTERCOSTALS AND SILL PLATES.SDR 98ZZZX3975Door Sill · corrodedATW - SURFACE CORROSION ON AFT PASSENGER DOOR SILL PLATE. CLEANED CORROSION, TREATED, PRIMED, PAINTED AND SEALED DOOR SILL. (X)SDR 98ZZZX3962Skin · corrodedATW - LEFT FORWARD PASSENGER DOOR HAS 2 EACH CRACKS IN THE HANDLE BOX AREA. REPLACED BOTH BOX ANGLES IAW FAX DJR/RJ0318-97 AND BAE SRM. ANGLES MADE PER PS1.SDR 98ZZZX3967Control Cable · corrodedATW - THE CENTER SECTION MAIN AILERON INTERCONNECT CABLES ARE CORRODED AT THE WING ROOT AREA. REMOVED AND REPLACED MAIN AILERON INTERCONNECT CENTER CABLES. GEN W/C FOR FUNCTIONAL TEST.SDR 98ZZZX3960Control Cable · corrodedATW - THE RIGHT MAIN AILERON CENTER SECTION OF CABLES ARE CORRODED AT THE LOWER PULLEY IN THE WING ROOT JUST AFT OF FRAME NR 29. REMOVED AND REPLACED THE RIGHT AILERON CENTER SECTION MAIN AILERON CONTROL CABLES. GEN W/C FOR FUNCTIONAL TEST.
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