N270AX, cancelled May 31, 2012
Service difficulty reports · 22
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 = 'N270AX' AND deregistration_id = 'N270AX-2012-05-31' 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 = 'N270AX' AND deregistration_id = 'N270AX-2012-05-31' 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 CNMA20110026Connector · damagedNR 2 ENGINE FIRE INDICATION ILLUMINATED (LOOP A ONLY W/ ALL ASSOC WARNINGS - LOOP B WAS DEFERRED) PERFORMED ENGINE FIRE CL (QRH 4-1-1-1) NR 1 FIRE BOTTLE FIRED AND FIRE INDICATION WENT OUT W/ IN 30 SECONDS IAW CL. PERFORMED RECOMMENDED FIRE WARNNING TEST , TESSDR CNMA20100034Smoke Detector · false activationONE SMOKE DETECTOR LIGHT ON AND APPLICABLE CARGO FIRE LIGHT ON (FWD CARGO FIRE LIGHT ON DISCHARGED FIRE BOTTLES). REPLACED FWD CARGO NR3 SMOKE DETECTOR IAW AMN 26-14 AND TESTED GOOD. REPLACED AUX MWACS (MASTER WARNING CONTROL UNIT) IAW AMM 33-15 REPLACED TESTSDR CNMA20100032Support Fitting · corrodedCTR LANDING GEAR LT AND RT TRUNNION SUPPORT FITTING CORRODED ON TOP AROUND BOLT HOLES. CLEANED CORROSION IAW EO 5310E0973 ROTARY PEEN REWORK AREA IAW DPS 4.999-2. PERFORMED HFEC INSP IAW NDT MANUAL, PART 6 TO VERIFIY NO CORROSION REMAINS. REPLACED HARDWARE WISDR CNMA20100026Slide · defectiveDOOR 3L EVACUATION SLIDE REMOTE PRESURE PRESS TO TEST INDICATOR LIGHT STAYS ON CONTINUOUSLY. REPLACED L-3 DOOR SLIDE ASSY - OPS CHECK NORMAL. OK FOR SERVICE. M/M REF. 25-61.SDR CNMA20090019Slide · false indicationR4-DOOR SLIDE INOP (SLIDE LIGHT REMAINS ON). REPLACED R4 DOOR SLIDE - OPS CHECK NORMAL. MM REF. 25-61.SDR CNMA20090006Windshield · crackedAT FL 360, CAPT'S WINDSHIELD ANTI-ICE SYS BEGAN ARCING FOLLOWED BY WINDSHIELD CRACKING. QRH 4-10-2-5 PROCEDURE COMPLETED PRIOR TO WINDSHIELD FAILURE. REMOVED AND REPLACED CAPT'S WINDSHIELD IAW AMM 56-11 AND WINDSHIELD ANTI-ICING CONTROLLER IAW AMM 30-41. CASDR CNMA20090009Skin · damagedCOMPLY WITH EO D53-18 REPAIR OF SKIN AT S-27L STA 475 TO STA 495. COMPLETED EO D53-18 REPAIR OF SKIN AT S-2L STATION 475 TO 495 IAW EO D53-18 DWG 5330640-1.SDR CNMA20090008Tee Fitting · corrodedAREAS OF AFT BULKHEAD TEE AT FLOOR LEVEL HAVE CORROSION BEYOND SRM LIMITS. COMPLETED EO D53-17 REPAIR OF TEE AT AFT BULKHEAD STA 2007. CORROSION AT STA 2007, AFT BULKHEAD FLOOR LEVEL TEE REPAIRED BY DOC. 5320-625 ERA FOR LBL 69-70.5, DOC 5320-627 ERA FOR LBSDR CNMA20100002Floor Support · corrodedCORROSION ON MID FLOOR SUPPORT CHANNEL SUPPORT BS 1997-2007 RBL 25-27. DAMAGED FLOOR SUPPORT REMOVED. NEW FABRICATED PN: OAI-53-0009 IAW SRM VOL 3 53-16-01 FIG. 10C & GMM 4.45 INSTALLED WITH FASTENERS IAW SRM VOL 2 51-31-01 NAS517-2-6 B/N: 74919-03.SDR CNMA20080010Engine · malfunctionedNR 2 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED AT TOP OF CLIMB (29,000) INTERMITTENTLY. LIGHT BECAME SOLID AFTER 3 MINUTES. ENGINE SHUTDOWN IN FLIGHT IAW QRH PROCEDURE 4-1-2-19 AND CORRESPONDING CHECKLISTS. COMPLETED WORTAN 08-0368 R&R NR 2 ENGINE OIL STRASDR CNM2008F00002Compressor · stalledDURING CRUISE AT FL 300 NR 3 ENG COMPRESSOR STALLED N1 DROPPED TO APPROXIMATELY 70 PERCENT VIBRATION FELT IN NR 3 THROTTLE/ FUEL LEVEL/ FIRE HANDLE AS WELL AS AIRFRAME. (K)SDR CNMA20070008Drive Assy · malfunctionedAT 10,000 MSL AIRCRAFT SLOWED TO 250 KTS, AP OUT OF TRIM LIGHT ILLUMINATED GREATER THAN 5 SECONDS. AUTOPILOT DECOUPLED AND AC PITCHED NOSE DOWN EXCESSIVELY. TRIM SWITCHES FROM BOTH CONTROL COLUMNS DID MOVE LONG TRIM HANDLES BUT STAB INDICATOR REMAINED FIXED SDR CNMA20070006Channel · corrodedBS 2007, RBL 20-23, CORROSION ON CHANNEL SUPPORT UNDERNEATH GALLEY. CORRODED PORTION REMOVED NEW FABRICATED M/F S2920883-12000 AND INSTALLED WITH EXISTING FASTNERS IAW SRM VOL 2 51-31-01 AND CHERRY-MAX MS 2885/6-4/08.SDR CNMA20060028Battery Pack · inoperativeON PRE-FLIGHT, FOUND OVERWING EMERGENCY LIGHTS INOP. REPLACED OVERWING BATTERY PACK. OPS CKS OK IAW MM 33-51.SDR CNMA20060027Power Supply · no testEMERGENCY LIGHT TEST LT WILL NOT ILLUMINATE WHILE PERFORMING COM TEST. ALL LIGHT CHECK AS COMING ON WITH TEST. REMOVED AND REPLACED L3 BATTERY PACK AND CHARGER ASSY IAW AMM 33-50. REMOVED AND REPLACED L4 BATTERY CHARGER ASSY IAW AMM 33-50.SDR CNMA20060025Encoder · odor6 HOURS INTO FLT, THE CREW NOTICED AN ELECRICAL ODOR IN "C" ZONE SEATS 37-40 RIGHT SIDE OF ACFT. PULL ALL CB'S IN "C" ZONE ASSOC WITH LIGHTING / DECODERS. AFTER CB'S PULLED, ODOR STARTED GOING AWAY. REPLACED ENCODER IAW MM 23-33. OPS CK NORMAL.SDR CNMA20060019Blades · brokenDURING TAKEOFF ROLL NR 3 ENGINE EGT INDICATOR SHOWS RAPID EGT RISE AT TEMP 945 DEGREES AMBER LIGHT CAME ON AND TEMP EXCEEDED 950 DEGREES AND KEPT RISING. F/E REDUCED THRUST NR 3 ENGINE TO PREVENT OVERTEMP AND WHEN DIFFERENCE BETWEEN N1, NR3 ENGINE AND OTHERS RSDR CNMA20060018Manifold · crackedDURING THE TAKEOFF ROLL NR 3 ENG EGT BEGAN TO CLIMB ABOVE 950 DEGREES. THE ENGINEER PULLED NR 3 THROTTLE BACK ATTEMPTING TO BRING NR 3 EGT INTO LIMITS, THE CORRESPONDING DROP IN N1 WAS ALREADY AT 5 PERCENT LESS THAN THE N1 LIMIT AND THE EGT WAS STILL EXCEEDINSDR CNMA20060011Switch · intermittentEMERGENCY LIGHTING PRESS TO TEST SWITCH INTERMITTENT TESTING. REMOVED AND REPLACED PRESS TO TEST SWITCH IAW M/M 33-00, OPS CHECKS NORMAL.SDR CNMA20060009Lug · damagedFOUND DAMAGE TO THE NR 2 ENGINE LEFTHAND BOOTSTRAP LUG. PERFORMED REPAIR IAW REPAIR DRAWING 5420250-1 REV 1 DATED 5-6-2006 REF REPORT 5420250-ER REV 1 DATED 5-5-2006.SDR CNMA20060008Motor · noisyWITH AUTOPILOT ENGAGED VIBRATION COULD BE FELT IN FLOOR AND A (GRINDING) NOISE WAS DETECTED IN THE TAIL SECTION. REPLACED SEVERAL COMPONENTS INCLUDING GEARBOX ASSY, PRIMARY TRIM MOTOR, DRUM ASSY, HORIZONTAL STAB CHAIN DRIVE, FOUND DETERIORATED CONNECTOR TO THSDR 2005000009Pump · defectiveNR 1 ENGINE WOULD NOT MAKE TAKEOFF POWER. REMOVED AND REPLACED MAIN ENGINE FUEL PUMP NR 1 ENG IAW 73-12. REMOVED AND REPLACED MAIN FUEL FILTER IAW 73-11. REMOVED AND REPLACED MEC IAW 73-20 RAN ENGINE PER OMNI JET RUN HANDBOOK, OPS CHECKS GOOD AT THIS TIME.
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