N135LC
Service difficulty reports · 16
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 = 'N135LC' 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 = 'N135LC' 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 2A6R2026031675004Ehsi · wrong partDURING REINSTALLATION OF THE EHSI (ELECTRONIC HORIZONTAL SITUATION INDICATOR), THE INSTALLING TECHNICIAN NOTED THAT THE LOCKING TEETH RETAINER ON THE UNIT'S J3 CONNECTOR WOULD NOT LOCK AS EXPECTED WHEN CONNECTING THE AIRFRAME P3 D-SUB CONNECTOR. IT WAS ALSO NOSDR 2A6R2026021975003Floor Panel · dentedDAMAGE WAS DISCOVERED TO THE CABIN FLOOR UPPER SKIN PANEL IN THE FORM OF MULTIPLE DENTS. THE DENTS WERE FILLED WITH AN EA9309.3NA RESIN/MICRO BALLOON MIXTURE AND .025” 2024-T3 REPAIR DOUBLERS WERE FABRICATED AND INSTALLED OVER TOP OF THE REPAIR AREA. A DETAILESDR 2A6R2026021975002Floor Panel · dentedDENT DAMAGE MEASURING 13.5” LONG AND 2.5” WIDE WITH A MAXIMUM DEPTH OF 0.065” WAS DISCOVERED ON THE L/H SIDE OF THE COCKPIT FLOOR SKIN NEAR F.S 2,675MM APPROXIMATELY 0.5” FROM THE EDGE OF THE CENTER CONSOLE. THE DAMAGED AREA WAS POTTED WITH EA9309.3NA ADHESIVESDR 2A6R2026020275001Attach Angle · corrodedCORROSION DAMAGE OF 0.016”- 0.020” IN DEPTH WAS DISCOVERED ON THE LOWER R/H BROOM CLOSET ATTACHMENT ANGLE (L533M1052317). REPLACEMENT ANGLE BRACKETS WERE NOT AVAILABLE WITHIN THE SCHEDULED RETURN TO SERVICE DATE. THEREFORE, A REPLACEMENT ANGLE WAS FABRICATED USDR 2A6R2022090264802Frame · crackedDURING 1000 HOUR INSPECTION, CRACK DAMAGE WAS DISCOVERED ON THE RH FRAME 5 AT THE SIDE WALL ATTACHMENT AT THE UPPER MOUNT LOCATION FOR THE AFT MEDICAL WALL AT APPROXIMATELY FUSELAGE STATION 4,709MM WATER LINE 2,375MM. THE CRACK IS APPROXIMATELY 0.75” IN LENGTSDR 2A6R2022090264801Tail Boom · chafedDURING 1000 HOUR INSPECTION, FOUND TAILBOOM CHAFE MARK ON BOTTOM CENTER SURFACE ROUGHLY 3FT AFT OF FWD RING FRAME THAT APPEARS TO BE THRU MULTIPLE PLIES. PERFORMED REPAIR ON TAILBOOM CHAFE DAMAGE ON BOTTOM CENTER SURFACE AFT OF FWD RING FRAME USING ECS0031-12SDR QMLA2020021172009Engine · failedON 7 FEB 20 AT 1957 HOURS WHILE ATTEMPTING TO LAND ON THE DOLLY, PILOT HEARD LOUD BANG FOLLOWED BY VIBRATIONS IN THE AIRFRAME, NOT IN THE FLIGHT CONTROL, AND SEVERE GRINDING NOISES. I LOOKED IN AT THE CAD TO SEE WHAT WAS GOING ON AND NOTICED FLAMES OUT THE LEFSDR QMLA2012093012163Frame · corrodedTHE TAIL BOOM JUNCTION RING FRAME X9227 WAS FOUND TO BE CORRODED. THE TAIL BOOM ASSY WAS REMOVED AND SHIPPED TO ACFT MFG. REPLACED RING FRAME WITH A NEW RING FRAME X9227.SDR QMLA2012093012162Skin · corrodedFUSELAGE SKIN HAS VARIOUS AREAS OF CORROSION AT THE GROUND PLUG. COMPLETED REPAIR BY FRABICATING A FILLER USING 0.020" THICK 2024-T3 ALUMINUM ALLOY. FABRICATED A DOUBLER USING 0.025" THICK 2024-T3 ALUMINUM ALLOY. POSITIONED DOUBLER AND MATCHED DRILLED EXISTINGSDR QMLA2012093012161Floor Panel · crushedTHE CABIN FLOOR HAS MULTIPLE AREAS OF DAMAGE/CRUSHED HONEYCOMB. REMOVED UPPER SKIN FROM DAMAGED AREAS. POTTED THE EXPOSED CORE AREA TO ACHIEVE A FLAT AND SMOOTH SURFACE, TO EVEN WITH THE EXISTING SKIN. FABRICATED A DOUBLER USING 0.032" THICK 2024-T3 ALUMINUM SDR BAQA094141Clock · intermittentCLOCK WORKS INTERMITTENTLY AND THEN STOPS, WORKS THEN STOPS. REPLACED WITH SERVICABLE UNIT, 04/19/2004.SDR BAQA093734Indicator · ratchetingINDICATOR IS RATCHETY AND STICKY. REPLACED WITH SERVICABLE UNIT. 03/11/2004SDR BAQA091997Mount · collapsedMAIN ROTOR GEARBOX MOUNT COLLAPSED. REPLACED WITH SERVICEABLE UNIT. 01/15/2004SDR BAQA091483Chip Detector · looseCHIP DETECTOR STAKE IN PLUG LET GO ALLOWING CONNECTOR END TO ROTATE. ERIC SAID TO SCRAP ON SITE. FAX SCRAP CERT. AND MMIR TO HIM. THIS WAS DONE 12/10/03.SDR BAQA091587Control Unit · intermittentINSTRUMENT LIGHTS INTERMITTENT, FLASH ON AND OFF ONCE EVERY 1 OR 2 FLIGHTS. REPLACE SERVICEABLE UNIT. 12/18/2003SDR BAQA091485Indicator · inoperativeN2 NEEDLE INOPERATIVE. REPLACED WITH CANNED UNIT FROM AN AIRCRAFT.
Back to N135LC