N592JB

Service difficulty reports · 66

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 = 'N592JB' 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.

SDR YENA20150531174Floor Support · corrodedDURING HEAVY MAINTENANCE, FLOORBEAM AT Y -1292 RT FROM FRAME 68 TO FRAME 69 HAS CORROSION. REMOVED CORROSION FROM FLOORBEAM 2.0" W X 3.0" L X .156" 100 PERCENT MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14. R & R FLOORBEAM IAW SRM 51-42-1.May 31, 2015 · N592JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA20150531173Floor Support · corrodedDURING HEAVY MAINTENANCE FLOORBEAM AT Y1292 LT FROM FRAME 68 TO FRAME 69 HAS CORROSION REMOVED CORROSION IN A 2.0" W X 3.0" L X .040" D FROM ORIGINAL MATERIAL THICKNESS OF .156" FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14. R & R FLOORBEAM 2 SECTIONS FROM FRAMEMay 31, 2015 · N592JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA20150531171Fitting · corrodedDURING HEAVY MAINTENANCE, LT BATH TUB FITTING HAS CORROSION AT FR 66, STR 23L. REMOVED CORROSION AT FRAME 66, REMOVED .065" FROM ORIGINAL MATERIAL THICKNESS OF .150" IN A 2.0"L X 2.0" W FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 1 CUT OUT CORRODED AREA AMay 31, 2015 · N592JB · Airbus A320232 · Fuselage Main, Attach FittingsSDR YENA20150531170Door Sill · corrodedDURING HEAVY MAINTENANCE LT L2 DOOR SILL PLATE HAS CORROSION AT FR 66 L-2 DOOR SILL PLATE. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14. LOCATED REPAIR ANGLE AND FILLER FIG 201, PRINCIPLE 7 IAW SRM 53-41-14. INSTALLED REPAIR ANGLE AND FILLER IAW SRM 51-42-11,May 31, 2015 · N592JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA20150203014Power Supply · failedDURING MAINTENANCE, EMERGENCY LIGHT SYSTEM TEST FAILED AS INDICATED AT AFT LIGHT EPSU. R & R AFT LIGHT EPSU BATTERY IAW AMM 33-51-38. SYS TEST AND OPS CHECK GOOD.Feb 3, 2015 · N592JB · Airbus A320232 · Emergency LightingSDR YENA20140407070Proximity Sensor · failedAIR RETURN TO DEPARTURE DUE TO AFT CARGO DOOR INDICATOR OPEN IN FLIGHT. R & R AFT CARGO DOOR PROXIMITY SENSOR IAW TSM 52-32-00-810-801. ADJUSTED AS REQUIRED. OPS CHECKED OK. ALL INDICATIONS NORMAL.Apr 7, 2014 · N592JB · Airbus A320232 · Door Warning SystemSDR YENA20131010211Landing Gear · malfunctionedAIR RETURN DUE TO NOSE GEAR WOULD NOT RETRACT ON TAKE OFF. CYCLED GEAR WITH NO CHANGE. LANDING GEAR SYSTEM DISAGREE ECAM MESSAGE. PERFORMED ADJUSTMENT CLEARANCE J2 ON NLG DRAG STRUT ASSY IAW AMM 32-21-16-400-002-A, CLEARANCE IS OK. PERFORMED MLG & NLG FUNCTOct 10, 2013 · N592JB · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR YENA20130108003Light · missingFLT 830 SDQ-JFK, ON MAINTENANCE CHECK FOUND ROW EMERGENCY LIGHT ASSEMBLY MISSING AT ROW 7ABC. INSTALLED MISSING LIGHT ASSEMBLY AT ROW 7 ABC. OPS CHECK PER 33-51-00.Jan 8, 2013 · N592JB · Airbus A320232 · Emergency LightingSDR YENA20121110639Idg · overheatedFLT 773 BOS-AUA, AIR RETURN DUE TO IDG NR 2 OVERHEAT AFTER TAKEOFF. ECAM ACCOMPLISHED IDG DISCONNECT. PERFORMED TSM TASK 24-21-00-810-823-A. FOUND NR 2 IDG THERMALLY DISCONNECTED. VISUALLY INSP IDG PYLON QUICK DISCONNECT AND FOUND NO EVIDENCE OF ARCING OR Nov 10, 2012 · N592JB · Airbus A320232 · AC Generator-AlternatorSDR YENA20120603518Light · inoperativeFLT 6414 MCO-TPA, ON HEAVY MAINTENANCE CHECK FOUND EMERGENCY LIGHT AT RIGHT OVERWING EXIT INOP. REMOVED AND REPLACED RT EMERGENCY LIGHT AT EMERGENCY EXIT IAW A320 AMM 33-51-16-000-001A. RE-INSTALLED WIRE LUG IAW A320 ESPM 20-44-20. RE-INSTALLED RIGHT EMERGEJun 6, 2012 · N592JB · Airbus A320232 · Emergency LightingSDR YENA20110917340Shutoff Valve · failedFLT 171 JFK-SMF, CREW DECLARED EMERGENCY AND DIVERTED TO OMA DUE TO ECAM CAB PR EXCESSIVE CABIN ALTITUDE. THE TECHNICIAN REMOVED AND REPLACED NR 2 ENGINE PRSOV. PERFORMED ENGINE GROUND RUN AS NORMAL REF AMM 36-11-52.Sep 17, 2011 · N592JB · Airbus A320232 · Pneumatic Distribution SystemSDR YENA20110811316Slide · defectiveFLT 29 JFK-TPA, FWD ENTRY DOOR SLIDE INOP DURING EMERGENCY LIGHT TEST GOT MESSAGE FWD EXTERIOR LIGHT LOAD L FAULT. T/S PER TSM 33-51-00-05, FOUND LT FWD SLIDE LIGHT AT FAULT. REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE PER AMM 25-62-44. ALL OPS TEST NORMAL.Aug 11, 2011 · N592JB · Airbus A320232 · Escape SlideSDR YENA20090820098Sensor · failedFLT 1784, BOG-JFK, AIR PACK 1 TRIPPED ON CLIMBOUT, UNABLE TO MAINTAIN CABIN, CABIN PRESSURE REACHED 11.2 PSID. DUE PACK NR 2 ON MEL, RETURN TO BOG. REMOVED AND REPLACED PACK 1 HEAT EXCHANGER O/H TEMP DET/OUT TEMP SENSOR. OPS CHECK OF PACK NR 1 NORMAL.Aug 21, 2009 · N592JB · Airbus A320232 · Cabin Temperature Control SystemSDR YENA20090810093Transmitter · failedFLT 1424 - LGB-SEA - OIL PRESSURE INDICATION WENT TO XX (AMBER) IN CLIMBOUT. NO SECONDARY INDICATIONS. CHECKED PER TSM 79-33-00-810-806, AMBER XX OIL DISPLAYED ON GROUND AT GATE. METERED WIRES FROM CONNECTOR 4003EN. VERIFIED 28VDC AND B GROUND PRESENT WHILAug 10, 2009 · N592JB · Airbus A320232 · Engine Oil PressureSDR YENA200526Electrical Box · unknownSMOKE SMELL ROW 8 RT SIDE. ACCOMPLISHED INFO NOTICE 2004-T023TR, OPS CHECKED NO FAULTS FOUND. REMOVED AND REPLACED SEB AT 8E AS PRECAUTIONARY AS STATED IN INFO NOTICE.Apr 4, 2005 · N592JB · Airbus A320232 · Entertainment SystemSDR YENA200465Actuator · wornFLAP SYS JAM IN CONF 3. TROUBLESHOOT PER TSM 27-51-00. FOUND NR 3 LT FLAP TRACK ACTUATOR TORQUE LIMITER POPPED. REMOVED AND REPLACED NR 3 LT FLAP ACTUATOR PER MM 27-54-49. ALL CHECKED OK FOR SERVICE.Dec 27, 2004 · N592JB · Airbus A320232 · Trailing Edge Flap Actuator
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