N296PQ
Service difficulty reports · 115
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 = 'N296PQ' 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 = 'N296PQ' 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 REXA2018080100651Battery Pack · dischargedFLASHLIGHT BEHIND COPILT SEAT IS NOT BLINKING RED. INSTALLED NEW BATTERY PACK IAW AMM 25-61-02. CHECK GOOD OK FOR SERVICE.SDR REXA2018012500048Sign · damagedAFT FACING EXIT SIGN DAMAGED. R & R THE SIGN IAW AMM 33-51-05. OPS CHECKED GOOD.SDR REXA2017122901300Fan · failedRECIRCULATION FAN FAULT STATUS MESSAGE, STRONG ODOR OF BURNING. FOLLOWED QRH, MESSAGE PERSISTED. R & R THE RT RECIRCULATION FAN AND FILTER IAW AMM 21-22-12, AND J/C 900-21-180-702. OPS CHECKED GOOD.SDR REXA2017090600984Smoke Detector · false activationAFT LAVATORY SMOKE WARNING MESSAGE DURING DECENT. FA REPORTED NO EVIDENCE OF SMOKE/FIRE/FUMES. REMOVED AND REPLACED THE AFT LAV SMOKE DETECTOR IAW 26-16-01. PERFORMED AN OPS TEST IAW AMM 26-16-00-710-801, OPS TEST PASSED.SDR REXA2017010600031Intercostal · corrodedINTERCOSTAL ON STRINGER 26R HAS CORROSION BETWEEN BS 364 AND 349. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM-51-42-06 AND 51-42-21.SDR REXA2017010600030Intercostal · corrodedINTERCOSTAL LEFT OF STRINGER 27 HAS CORROSION BETWEEN FRAMES BS 364 AND 349, IN THE FWD E & E BAY. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM-51-42-01 & 51-42-21.SDR REXA2017010600029Riser · crackedPAX DOOR STEP AFT RISER CRACKED. REMOVED THE CRACK BY PERFORMING CUTOUT AND INSTALLED A REPAIR IAW SRM 52-11-04.SDR REXA2017010600028Riser · crackedPAX DOOR STEP AFT RISER CRACKED. REMOVED THE CRACK BY PERFORMING EDGE BLEND AND RESTORED FINISH. FOUND TO BE WITHIN LIMITS. IAW SRM 52-11-04.SDR REXA2017010500027Strap · crackedEXTERNAL LOWER AFT RT WING TO BODY FAIRING 196DR AFT INBD STRAP ANGLE CRACKED. REMOVED AND REPLACE THE FARING STRAP ANGLE IAW SRM 51-42-10.
"SDR REXA2017010400026Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED THE DRAG ANGLE IAW SRM 52-11-04.SDR REXA2016102602013Oxygen Mask · unwanted deploySEAT 16C/D OVERHEAD OXYGEN MASKS DEPLOYED. ALL SYSTEMS NORMAL. OXYGEN NOT ACTIVATED. RESTOWED MASKS IAW T/R 35-0513 AMM 35-21-09. DEPLOYED AND PERFORMED DVI OF MASK AND LATCHING ASSY IAW AMM 35-21-09. REPACKED AND PERFORMED OPS CHECKS OF PAX OXYGEN DEPLOYSDR REXA2016070601247Light · detachedLEFT SIDE GALLEY EMERGENCY LIGHTING IS LOOSE. SECURED LEFT SIDE GALLEY EMERGENCY LIGHT IAW AMM 33-51-00, OPS CHECKED GOOD, OK FOR SERVICE.SDR REXA2015110401004Fire Bottle · lowON SAFETY STICKER INSPECTION, FOUND FIRE EXTINGUISHER IN ENTRANCE FWD CABINET TO BE UNDERWEIGHT DURING QC WEIGHT INSPECTION. R & R FWD ENTRANCE CABINET FIRE EXTINGUISHER IAW AMM 26-23-01, PN OFF & ON 30H673, SN OFF Y510335 & SN Y-643436.
SDR REXA2014120501163Flashlight · inoperativeFORWARD FLIGHT ATTENDANT EMER FLASHLIGHT INOPERATIVE, NEXT TO SERVICE DOOR. DEFERRED FWD FLASHLIGHT IAW MEL 25-61-4A MX 4488 NOTIFIED. MMO2 UPDATED, PLACARD INSTALLED. R & R FWD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY PN ON & OFF P2-07-0001-214
IAW 25-61-01. SDR REXA2014012600132Unknown · malfunctionedWHILE CLIMBING THROUGH 31,000 FT. WE RECEIVED CAB DIFF WARNING. ABNORMAL PROCEDURES FOLLOWED & WARNING CLEARED SHORTLY AFTER INITIATING A DESCENT TO LOWER ALT. ACFT PRESS WAS CONTROLLED MANUALLY. UNDER DIRECTION OF MOC PERFORMED FAULT ISOLATION OF DIFF PRES
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