N660CP
Service difficulty reports · 21
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 = 'N660CP' 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 = 'N660CP' 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 SROM20200810002Skin · crackedTWO CRACKS IN LT HORIZONTAL STABILIZER LOWER SKIN, HSS 157, 9 AND 16 FROM THE AFT SPAR. REPAIRED THE SKIN IAW SRM 55-10-01-2R-11, REV 70.SDR SROM20200810001Skin · crackedCRACK IN LH HORIZONTAL STABILIZER LOWER SKIN, STAB STA. 101, 19” FORM THE FORWARD SPAR. REPAIRED CRACK IN LH HORIZONTAL STABILIZER LOWER SKIN AT STA. 101, 19” FROM THE FORWARD SPAR IN ACCORDANCE WITH B737-700 SRM 55-10-01-2R-11 REV. 70.SDR SROM2020051300000Battery Pack · dischargedEMERGENCY LIGHTS ROW 14 AND 16 AIRCRAFT LEFT INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK AT ROW 14 AND 16 LH IAW B737-700 AMM 33-51-00. OPS CHECK OK.SDR 2019FA0000385Battery Pack · dischargedRH OVERWING EMERGENCY LIGHTS INOP.SDR SROM2019F00225Battery · dischargedEMERGENCY EXIT SIGN/LIGHT AT LH OVERWING EXIT WILL NOT STAY LIT.SDR 2016F00108Frame · dentedINSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES, SO A SERVICE REQUEST WAS RAISED INCLUDING A REQUEST TO ALLOW TO REMAIN IN SERVICE & A RSDR 2016F00111Frame · dentedINSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME, PN 146A1285-70, AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES, SO A SERVICE REQUEST WAS RAISED INCLUDING A REPAIR SCHEME SUGGESTED BYSDR 2016F00113Intercostal · deformedDURING INSPECTION, DAMAGE WAS NOTED IN THE UPPER FLANGE OF THE INTERCOSTAL RUNNING BETWEEN BS 787 & BS 807 AT STRINGER 22L. FABRICATED & INSTALLED REPLACEMENT INTERCOSTAL.SDR SROM2016F00098Shear Tie · dentedINSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA AND THERE ARE NOR SRM REPAIRS FOR SHEAR TIE FRAMES.SDR 2016F00110Frame · dentedINSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES, SO A SERVICE REQUEST WAS RAISED INCLUDING A REQUEST TO ALLOW TO CONTINUE IN SERVICE AS SDR SROM2016042600118Frame · dentedINSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA AND THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES SO A SERVICE REQUEST WAS RAISED WITH MFG INCLUDING A REQUEST TO ALLOW TO CONTINUE IN SSDR 2016F00109Frame · dentedINSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES, SO A SERVICE REQUEST WAS RAISED INCLUDING A REQUEST TO ALLOW TO CONTINUE IN SERVICE AS SDR 2016F00117Frame · dentedINSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES, SO A SERVICE REQUEST WAS RAISED, INCLUDING A REPAIR SCHEME SUGGESTED BY ENGINEERING.SDR SROM091220141Warning Light · false activationDURING TAKEOFF ROLL, FORWARD ENTRY DOOR LIGHT ILLUMINATED AT 80 KNOTS. REJECTED TAKEOFF, RETURNED TO GATE. INSPECTED AND TESTED FORWARD ENTRY DOOR IAW FAULT ISOLATION MANUAL 52-10-08. NO FAULTS FOUND. ACFT RELEASED FOR SERVICE. SUBSEQUENT FLIGHT REPORTED, NSDR SROM0418201403Intercostal · crackedFOUND CRACK IN INTERCOSTAL NEXT TO FLOOR PANEL ATTACH NUTPLATE.SDR SROM0418201402Floor Panel · crackedFLOOR PANEL FOUND CRACKED.SDR SROM0418201401Floor Panel · crackedFLOOR PANEL FOUND CRACKED.SDR SROM201311210001Downlock Switch · out of toleranceDURING CLIMB OUT, AFTER GEAR RETRACTION, FORWARD PANEL GEAR INDICATOR SHOWED RT MAIN GEAR STILL DOWN AND LOCKED. OVERHEAD GEAR INDICATOR SHOWED ALL 3 GEAR UP AND LOCKED. RETURNED TO DEPARTURE. LANDED UNEVENTFUL. FOUND RT GEAR PRIMARY DOWN LOCK PROXIMITY SWISDR SROM2010017Compressor Blade · nickedNR 2 ENG BIRD STRIKE AND INGESTION AT THE 9 O’CLOCK POSITION. BLOOD AND FEATHERS FOUND ON BLADES IN BYPASS PATH AND BOOSTER INLET. CONDITIONAL INSP COMPLIED WITH IAW AMM 05-51-18 AND 71-00-00. NO DEFECTS NOTED. ENGINE BORESCOPE INSP OF HIGH PRESSURE COMPRESSSDR SROM20100001Autopilot Sys · disconnectedSPEED TRIM FAIL LIGHT ILLUMINATED AND YAW DAMPER WON'T ENGAGE DURING TAKEOFF. MADE UNEVENTFUL RETURN TO DEPARTURE AIRPORT. PERFORMED YAW DAMPER SYS TEST IAW AMM 22-23-00, NO DEFECTS NOTED. PERFORMED DFCS BITE PROCEDURE AND DFCS ADJUSTMENT/TEST IAW AMM 22-11-SDR SROM20090001Windshield · crackedMULTIPLE BIRD STRIKES ON DEPARTURE, RETURNED TO AIRPORT. REPLACED F/O WINDSHIELD. REPLACED 5 RIVETS UNDER INBD STRAFE OF NR 2 ENGINE NOSE COWL. CLEANED MULTIPLE BIRD REMAINS FROM RT FUSELAGE NOSE AND TAIL OF ACFT. PERFORMED BIRD STRIKE INSP IAW AMM 05-51-1
Back to N660CP