N156CA, cancelled Sep 6, 2005
Service difficulty reports · 70
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 = 'N156CA' AND deregistration_id = 'N156CA-2005-09-06' 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 = 'N156CA' AND deregistration_id = 'N156CA-2005-09-06' 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 SWIA200110134Flap Track · dirtyON APPROACH TO OXR, HAD FLAP DISAGREEMENT (INBOARD FLAPS TWO BARS). RETURNED TO LAX.CLEANED FLAP TRACKS. CYCLED FLAPS, COULD NOT DUPLICATE.SDR SWIA200110125Annunciator · malfunctionedFLAPS SET 45 DEGREES ON FINAL, CONTINUITY FAULT ILLUMINATED FOR OUTBOARD PAIR OF FLAPS.REPLACED ANNUNCIATOR/I WITH VERSION II PER MM 27-50-00. OPS CHECK OK ON GROUND TESTS.SDR SWIA200110120Annunciator · malfunctionedRECEIVED FLAP CONTROL FAULT WARNING WHEN SELECTING FLAPS TO 15 DEGREES. RESET WAS SUCCESSFUL AFTER PRESSING RESET TWICE.REPLACED FLAP ANNUNCIATOR IAW MM 27-50-05. OPS CHECK GOOD.SDR SWIA200110019Flap Track · defectiveFLAP DISAGREEMENT AFTER TAKEOFF WHEN MOVING FLAPS FROM 15 DEGREES TO 0 DEGREES. APPEARS TO BE NACELLE FLAPS REPEATEDLY. PERFORMED FLAP INSPECTION AND FLAP TROUBLESHOOTING. REMOVED LEFT INBOARD FLAP. REPLACED ALL ROLLERS IAW 27-50-12 AND REPLACED OUTBOARD TSDR SWIA972619Potentiometer · failedFLAP DISAGREEMENT LIGHT MOMENTARILY ILLUMINATED AFTER TAKEOFF. FAULT CODE STORED IN MEMORY BANK INDICATED FLAP SELECTOR POTENTIOMETER FAILED. REPLACED FLAP SELECTOR. OPS CHECK GOOD ON GROUND CHECK. P/N: 120-42642-507 S/N ON: 120028RSDR SWIA972544Indicator · failedHIGH SPEED AURAL WARNING SOUNDED DURING TAKEOFF, RIGHT AFTER POWER LEVERS WERE SET FOR TAKEOFF TORQUE. REPLACED NR 1 AIRSPEED INDICATOR WITH SERVICEABLE UNIT IAW MM 34-12-01. OPS CHECK GOOD. COMPLIED WITH PITOT/STATIC CHECK IAW MM 34-11-00. NO LEAKS NOTED SDR SWIA972448Switch · out of adjCARGO DOOR OPEN INDICATIONS ON CLIMBOUT, RED LIGHT ON MAP AND TRIPLE CHIME. RETURNED TO SEA. ADJUSTED CARGO DOOR MICROSWITCH. OPS CHECK GOOD.SDR SWIA972352Pressure Switch · malfunctionedOIL PRESSURE RED LIGHT ILLUMINATES AND ORAL WARNING OIL PRESSURE GAUGE FLUCTUATED BETWEEN 45-55. RETURNED TO LAX. REMOVED AND REPLACED LEFT ENGINE OIL PRESSURE SWITCH WITH SERVICEABLE SWITCH. PERFORMED ENGINE RUN OIL PRESSURE INDICATION WAS NORMAL WITH NO FSDR SWIA972412Warning Light · illuminatedLEFT OIL PRESSURE LIGHT ILLUMINATED CLIMBING THROUGH 16,500 FEET. FOLLOWED QRH PROCEDURES RETURNED BACK TO SBA. LIGHT EXTINGUISH THEREAFTER. INSPECTED LEFT ENGINE, SERVICED ENGINE OIL, CLEANED CANNON PLUG ON OIL PRESS SWITCH AND RAN ENGINE AT 100 PERCENT TOSDR SWIA972263Door · damagedIN DESCENT FROM FL240 CABIN FILLED WITH SMOKE. DIVERTED TO PDX. REPLACED LEFT RAM AIR DOOR IAW MM 21-26-01. OPS CHECK GOOD.SDR SWIA972208Smoke · detectedLIGHT SMOKE IN CABIN ON DESCENT TO RDD. RAN MEMORY/FLOW CHECK LIST (NO OXY OR SMOKE GOGGLES), RECIRC/GASPER OFF, THEN RIGHT, THEN LEFT PAC AND STOPPED SMOKE. DID FULL RAMP CHECK OF PACKS, UNABLE TO DUPLICATE. INSPECTED BOTH PACKS AND RAM AIR VALVES FOR DISCRSDR SWIA972081Regulator · out of adjPILOT REPORTED LOSS OF OIL PRESSURE (DROPPED IN YELLOW BAND) AND LOSS OF POWER (LEFT). DIVERTED TO EUGENE. ADJUSTED OIL PRESSURE REGULATOR PER MM 72-1-50. OPS AND LEAK CHECKS GOOD. REPLACED LEAKING FUEL OIL HEATER PER MM 72-01-40. OPS AND LEAK CHECKS ONSDR SWIA971957Control Unit · failedLANDING GEAR WOULD NOT RETRACT. RETURNED TO SEA. REMOVED AND REPLACED LANDING GEAR CONTROL MODULE IAW MM 32-31-01. P/N ON: 120-38594-501, S/N: 120027, S/N OFF: 120085.SDR SWIA971458Tq Indicator · malfunctionedLARGE RIGHT ENGINE TORQUE FLUCTUATIONS FROM 60 PERCENT TO 84 PERCENT ON CLIMB THROUGH 5000. RETURNED TO PDX. RAN RIGHT ENGINE BUT COULD NOT DUPLICATE PROBLEM.SDR SWIA971418Valve · failedEN ROUTE TO CLD LEFT DUCT LEAK LIGHT ILLUMINATED. FOLLOWED QRH AND LIGHT DID NOT EXTINGUISH. SHUT DOWN LEFT ENGINE AND RETURNED TO LAX. RAN AIRCRAFT AND DUPLICATED DISCREPANCY. ISOLATED REGULATOR/RELIEF VALVE AS FAULTY. INSTALLED SERVICEABLE VALVE AND RANSDR SWIA971348O Ring · failedLEFT ENGINE DUCT LEAK LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. COMPLIED WITH QRH AND RETURNED TO PSP AND CONTACTED MAINTENANCE. FOUND O-RINGS WORN ON COUPLER SLEEVE CAUSING LEFT ENGINE BLEED AIR DUCT TUBE ASSEMBLY TO LEAK AT LEADING EDGE AND AT WING TO FUSELSDR SWIA971343Warning · activatedAFTER TAKEOFF, CONTROL FAULT ILLUMINATED. QRH DID NOT CLEAR FAULT. RETURNED FOR LANDING AT SMF. OPERATED FLAPS UP AND DOWN COUPLE OF TIMES, NO DISCREPANCY NOTED. COULD NOT DUPLICATE PROBLEM.SDR SWIA971294Ias Indicator · leakingON TAKEOFF, FO'S AIRSPEED, ALTIMETER AND VSI VERY ERRATIC. ALTIMETER AS MUCH AS 1,500 FEET BEHIND CAPTAINS. AIRSPEED INDICATOR 0 KNOTS MOST OF THE TIME. RETURNED TO SEA. COPILOTS IAS INDICATOR HAS A STATIC LEAK. REMOVED AND REPLACED COPILOTS IAS INDICATORSDR SWIA971285Actuator · malfunctionedON APPROACH HAD US DO A GO-AROUND. ON GO-AROUND, NOSE GEAR A AND B REMAINED ON, (NO GROUND LIGHTS). NOSE GEAR WOULD NOT COME UP. REPLACED NOSE GEAR ACTUATOR FOR TROUBLESHOOTING. ALSO, REPLACED BAD ROD-END ASSY. SWUNG GEAR SEVERAL TIMES. ALL CHECKS GOOD.SDR SWIA971258Actuator · failedIN DESCENT FLIGHT MAP TRIM FAIL AP DISCONNECT. AIRCRAFT PITCHED UP. DIFFICULT TO CONTROL PITCH. TO DESCEND, IT TOOK ALL NOSE DOWN TRIM AND FORWARD YOKE PRESSURE, (AP TRIM SEVO NOT ILLUMINATED WHEN LOOK AT IT). INSPECTED AND FOUND LEFT ELEVATOR TRIM ACTUATOSDR SWIA971252Trim Tab · out of positionDURING DESCENT, AUTO PILOT DISCONNECTED. FOUND TRIM WHEEL AT FORWARD LIMIT AND TRIM INDICATOR AT 1-8 UNITS DOWN. AIRCRAFT SPEED REDUCTION REQUIRED TO REDUCE STICK FORCES TO NORMAL. ACCOMPLISHED ELEVATOR TRIM TAB DEFLECTION CHECK PER MM 27-32-00, TRAVEL WITHSDR SWIA971251Control Panel · failedDURING INITIAL CLIMB AT 1000 FT, ELECTRIC TRIM RAN AWAY FORWARD TO STOP. ROLLED TRIM BACK AND IT RAN FORWARD TO STOP AGAIN, EACH TIME SOUNDING AUTO PILOT AURAL WARNING. THE AUTO PILOT WAS NOT ON AT THE TIME. TRIED TO TURN RIGHT, WAS UNABLE BECAUSE AUTO PILOSDR COMA9810040Wire · shortedNAVIGATION LIGHTS CIRCUIT BREAKER TRIPPED. REPAIRED SHORTED WIRE RIGHT HAND WING.SDR COMA9810034Battery · dischagedEMERGENCY FLOOR LIGHTING IS INOP. REPLACED EMERGENCY BATTERIES.SDR COMA9710497Frame · crackedDURING 1C INSPECTION, TASK 419-012 REVEALED A CRACK IN LEFT NACELLE UPPER HALF-FRAME. REPLACED HALF-FRAME USING AERODESIGN REPORT 2524-2.SDR COMA9710496Frame · crackedDURING 1C INSPECTION, TASK 419-012 REVEALED A CRACK IN LEFT NACELLE UPPER HALF FRAME. THE CRACK WAS .52 LONG AND STARTED AT A NUTPLATE FASTENER. THE NUTPLATE IS ONE OF FOUR INSTALLED TO ATTACH THE EXHAUST DUCT MOUNT BRACKET. REPAIRED HALF-FRAME USING AERODESDR COMA9710487Sequence Valve · out of adjustTHE RIGHT HAND MLG DOES NOT RETRACT. ADJUSTED THE RIGHT HAND MLG DOORS SEQUENCE VALVES.SDR COMA9710308Aural Warning · soundedTAKEOFF TRIM AURAL WARNING SOUNDED DURING TAKEOFF. TRIM WAS CONFIRMED AT TAKEOFF SETTING. COULD NOT DUPLICATE DISCREPANCY. RESET AURAL WARNING UNIT, SYSTEM TEST NORMAL.SDR COMA9710235Blade · delaminatedPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR HUB MAJOR INSPECTION. UPON FURTHER INSPECTION, THE NR 3 BLADE WAS FOUND TO HAVE A DELAMINATION OF 40 SQ INCHES LOCATED ON THE CAMBER SIDE OF THE BLADE AND BEGINNING AT BLADE STATION 38. BLADE WAS REMOVED FROM SERVSDR COMA9710234Blade · delaminatedPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR HUB MAJOR INSPECTION. UPON FURTHER INSPECTION, THE NR 2 BLADE WAS FOUND TO HAVE A DELAMINATION OF 74 SQ INCHES LOCATED ON THE CAMBER SIDE OF THE BLADE AND BEGINNING AT BLADE STATION 32. BLADE WAS REMOVED FROM SERVSDR COMA9710227Antenna · failedWEATHER RADAR DISPLAY INOPERATIVE DURING CLIMB OUT. REPLACED THE WEATHER RADAR ANTENNA.SDR COMA9710177Stop Tab · bentPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION THE FEATHER STOP TAB S/N 248 WAS FOUND TO BE BENT APPROXIMATELY 0.125. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND HELD FOR PROPOSED FUTURE REPAIR.SDR COMA9710176Bearing Insert · wornPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION THE BLADE PIN BEARING INSERT WAS FOUND TO BE WORN IN AN OVAL FASHION. FURTHER INSPECTION SHOWED THAT THE INSERT HAD WORN TO .083 AT THE THINNEST POINT AND .0SDR COMA9710175Bearing Insert · wornPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION THE BLADE PIN BEARING INSERT WAS FOUND TO BE IN AN OVAL FASHION. FURTHER INSPECTION SHOWED THAT THE INSERT HAD WORN TO .082 AT THE THINNEST POINT AND .099 ATSDR COMA9710171Antenna · failedWEATHER RADAR IS INOP. REPLACED THE RADAR ANTENNA.SDR COMA9710168Hydraulic Syst · reqd serviceTHE LT (GREEN) HYDRAULIC SYSTEM LOW QUANTITY WARNING WAS ON DURING GEAR RETRACTION. THE RESERVOIR QUANTITY WAS AT THE BOTTOM OF THE GREEN RANGE. SERVICED HYDRAULIC SYSTEM TO FULL LEVEL, SYSTEM OPERATION NORMAL.SDR COMA9710077Coupler · inoperativeILS COURSE MOVES PLUS OR MINUS 1 DOT ON FINAL. REPLACED INBOARD COUPLER, OPERATIONAL CHECK GOOD.SDR COMA9710016Filter · cloggedFUEL FILTER IMPENDING BYPASS WARNING DURING FLIGHT. REPLACED RT ENGINE FUEL FILTERS.SDR COMA9610403Separator · crackedWING AND STABILIZER INBD DE-ICE BOOTS ARE INOP. REPLACED A CRACKED BLEED AIR WATER SEPARATOR.SDR COMA9610355Skin · corrodedDURING 2C INSPECTION, FOUND FUSELAGE INNER SKIN FOUND CORRODED AT PAX DOOR CUTOUT, BENEATH BOTTOM FWD DOOR CUTOUT REINFORCEMENT DOUBLER. THE DAMGE WAS REPAIRED PER AERODESIGN REPORT NR 2118-1, REV IR, DATED 12-3-96.SDR COMA9610354Sill · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR STRUCTURE RT SILL CORRODED. REPLACED SILL WITH NEW PART PER EMB120 SRM STANDARD PRACTICES CHAPTER 51.SDR COMA9610353Butt Strap · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR STRUCTURE RT BUTT STRAP CORRODED. REPLACED BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.SDR COMA9610352Butt Strap · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FWD CENTER FLOOR SUPPORT STRUCTURE BUTT STRAP CORRODED. REPLACED CENTER BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.SDR COMA9610351Butt Strap · corrodedDURING 2C INSPECTION, FOUND FWD FUSELAGE FLOOR SUPPORT STRUCTURE LT BUTT STRAP CORRODED. REPLACED LT BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.SDR COMA9610350Crossbeam · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR SUPPORT LT CROSSBEAM CORRODED. REPLACED CROSSBEAM WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.SDR COMA9610349Sill · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR SUPPORT STRUCTURE LT SILL CORRODED. REPLACED LT SILL PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.SDR COMA9610348Butt Strap · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR SUPPORT STRUCTURE LT BUTT STRAP CORRODED. REPLACED LT BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51 AND AERODESIGN REPORT 31671-2, REV IR, DATED 12-4-96.SDR COMA9610347Stringer · corrodedDURING 2C INSPECTION, FOUND FUSELAGE STRINGER 18L CORRODED AT FWD END, FS 4088.0. REPAIRED STRINGER PER AERODESIGN REPORT NR 1990-2, REV IR DATED 9-15-96.SDR COMA9610346Crossbeam · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FLOOR SUPPORT RT CROSSBEAM AT FRAME 16 HAD CORROSION. REPLACED RT CROSSBEAM WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.SDR COMA9610345Butt Strap · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP CORRODED. REPLACED CENTER BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.
Back to N156CA, cancelled Sep 6, 2005