N506NA, cancelled Dec 22, 2009
Service difficulty reports · 25
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 = 'N506NA' AND deregistration_id = 'N506NA-2009-12-22' 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 = 'N506NA' AND deregistration_id = 'N506NA-2009-12-22' 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 ANCF2009060500045Unknown · odorPILOT REPORT: A STRONG SMELL AT SMOKE DURING CRUISE ON ALL THE ACFT, STRONGER ON BUSSINESS CLASS, IT WAS ABOUT 2 MINUTES DURING DESCENT. IAW AMM 05-51-56/PAGE 201 THE SMOKE OR FUMES CABIN INSP CHECK WAS PERFORMED, IAW FIM 21-00-21/101. IT WAS FOUND IN NORMAL CSDR ANCF200700031Connector · damagedAFTER TAKEOFF, GEN OFF EICAS MESSAGE WAS PRESENTED. ALSO LEFT BUSS ISOLATED MESSAGE WAS PRESENTED AND SEVERAL CAPTAIN INSTRUMENTS WERE LOST. THERE WAS NOT FLIGHT INSTRUMENT TRANSFER AND THE AUTOPILOT AUTOMATICALLY DISCONNECTED. GEN OFF CHECK LIST WAS ACCOMPSDR ANCF200700011Motor · inoperativeFLAPS FAIL TO MOVE, TRAILING EDGE LIGHT ILLUMINATED AND AICES MSG TE FLAPS DISAGREE AND FLAP ISLN VAL DISPLAYED. FLAPS OPERATE NORMAL USING TE ALTN SYSTEM. FLAP LEVEL VIBRATION WAS FELT DURING OPERATION WHEN TAXING OUT. IN ACCORDANCE WITH FIM 27-51-00 FIG 1SDR ANCF200600039Filler · damagedDURING TAKEOFF, ABOUT 400FT, EXPERIENCED RT ENGINE FAILURE WITH BUMPING. RT EGT REACHES 933 DEGREES (C) AFTER THAT THE RT ENGINE WAS SHUTDOWN, EMERGENCY PROCEDURE WAS PERFORMED. THE INSPECTION ON GROUND SHOWED THAT ANNULUS FILLER FROM POS 9 WAS RELEASED CAUSSDR ANCF200600013Control Unit · malfunctionedLEFT ENGINE N2 RPM WENT TO OVERSPEED. IAW AMM 75-32-01 PAGE 401, REPLACED BLEED VALVE CONTROL UNIT. OPS CHECK OK FOR SERVICE.SDR ANCF200600011Smoke · unknownRETURNED TO GATE, SMOKE WAS DETECTED IN THE PASSENGER CABIN. AS PER FIM 21-00-01 PAGE 109 ITEM 6 PROCEDURE 4 WAS PERFORMED CHECK TO THE LT & RT RECIRCULATION FAN FILTERS. AS PER AMM 21-25-02 PAGE 401 THE PREFILTER ON RT RECIRCULATION FAN WAS REPLACED AND FILSDR ANCF200400064Anti-Ice Valve · malfunctionedEICAS MSG L ENG ANTI ICE AND ENG ANTI-ICE VALVE CAME ON DURING TAKEOFF ROLL WITH MAX THRUST SET. IAW AMM 30-21-03 REPLACED ENGINE INLET THERMAL ANTI ICE V/V LTANTI ICE VALVE P/N 7646B000 S/N 040571-5.SDR ANCF200400061Actuator · failedBOTH FLAP POINTERS ARE ON HALF POSITION WITH THE FLAP LEVER UP. L/E SLAT DISAGREE LIGHT ILLUMINATED. L/E SLAT DISAGREE DISPLAY ON EICAS. VOICE RECORDER CB WAS PULL OUT AS SB REQUEST. IAW AMM 27-58-01 PAGE 501 ACCOMPLISHED RIGGING ON TRANSMITTER POSITION SLASDR ANCF200400060Lever · malfunctionedBOTH FLAP POINTERS ARE ON HALF WITH THE FLAP LEVER IN UP. L/E SLAT DISAGREE LIGHT ILLUM. L/E SLAT DISAGREE DISPLAY ON EICAS. (VOICE RECORDER CB PULL OUT ACCORDING TO SECURITY BULLETIN) IAW AMM 27-09-00 PAGE 201 FSEU N° 2 AND 3 WERE SWAPPED. NO FAULT NOTED OSDR ANCF200400059Warning Light · false activationEICAS MSG (AFT CARGO DOOR 2) AFTER CLOSE DOORS IAW AMM 52-71-00 FIG 103 PAGE BLOCK 1 PSEU BITE WAS PERFORMED FIM 32-09-03 FIG 103.SDR ANCF200400055Warning Light · illuminatedEICAS MSG GEAR DOORS DISPLAYED WITH GEAR HANDLE UP. DOOR AMBER LGT ILLUM. GEAR AMBER LGT AND ALL GREEN DN LGTS EXTIN IAW FIM 32-30-00 PAG. 129. AIRCRAFT WAS RAISED ON JACKS TO PERFOM MLG OPERATIONAL TEST AMM 07-11-01 AMM 29-11-00 TEST SASTIFACTORY.SDR ANCF200400039Controller · maladjustmentEICAS MSG CABIN ALTITUDE DISPLAYED, CABIN ALT AND CABIN ALTITUDE LIGHTS ILLUM. UNABLE TO RESTORE CABIN PRESS USING MANUAL MODE. AT 39000 FT CABIN ALTITUDE MSG DISPLAYED. THE CABIN ALTITUDE SHOW`S 12000 FT AND START THE DESCENT, THE DESCENT WAS ACCOMPLISHEDSDR ANCF200400038Radio · inoperativeRECEPTION ON L VHF COMM INOPERATIVE, TRANSMISSION O.K. AND R VHF INOPERATIVE AND DEFERRED. AFTER LANDING 2 VHF COMM BECOME NORMAL. IAW WDM 23-12-02 AND 23-12-02 VHF COMM CONTROL PANEL WIRING WAS CHECKED AND OPERATIONAL TEST WAS PERFORMED IAW AMM 23-12-00 PAGESDR ANCF200400007Solenoid · inoperativeTAKE OFF WAS DISCONTINUED AT 90KNS RT ENG EGT WAS IN YELLOW BAND, CONTINUE RAISING. ENG EGT WAS MORE THAN LIMIT WAS ACCOMPLISHED BLOCK 5.2,11,17 AND 24 TEST NR 3 LP/HP COMPR AIRFLOW CONTROL TEST IAW AMM. TAKE OFF PWR WAS PERFORMED IP BLEED V/VS SOLENOID AND SDR ANCF200400001Transceiver · failedWXR FAIL DISPLAYED ON HSI WXR TEST DISPLAY WXR FAIL RT. THE TRANSCEIVER RADAR WAS CHANGED IAW-AMM 34-43-01 PAG 401, TEST OK. P/N-OFF/ON-2041217-0415,S/N-OFF-2274, S/N-ON-6464.SDR 02090301Slat · delaminatedskin delamination and honeycomb missing trailing edge of slat inboard right wing. An uneventful landing was accomplished. Further investigation revealed delamination of fixed leading edge wing panel (aft of #6 leading edge slat) approx. 10'X24", and hole in upSDR 2002F00242Floor Support · corrodedFOUND CORROSION ON FLOOR SUPPORT BS 1675, RBL 56, WL 208. CLEANED UP CORROSION, FOUND TO BE BEYOND ACCEPTABLE LIMITS PER SRM 53-00-01. REMOVED AND REPLACED SUPPORT. (M)SDR 2001F00449Idg · defectiveON CLIMB-OUT, THE LEFT IDG LIGHT CAME ON. DISCONNECTED IDG AND RETURNED TO STATION. BPCU INTERROGATION INDICATED TRIP DUE TO LOW OIL PRESSURE. IDG REPLACED, OPS CHECK GOOD. (M)SDR 20010409SG006Fseu · failedDURING CLIMB, AT FLAP RETRACTION LE SLAT DISAGREE MESSAGE ON EICAS ILLUMINATED AND SLAT/FLAP POSITION INDICATOR INDICATED SLATS NOT RETRACTED. RETURNED TO DEPARTURE STATION AND ACCOMPLISHED UNEVENTFUL LANDING. INVESTIGATION REVEALED BOTH FSEU''S FAULTED PDU SDR 20010220SG001Slat · lack of lubeAFTER TAKEOFF UPON RETRACTION, ''LE SLAT DISAGREE'' EICAS MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO DEPARTURE STATION. LUBRICATED SLAT SYSTEM IAW FAULT ISOLATION MANUAL 27-81 AND AMM 12-21-08. OPS CHECK GOOD. (M)SDR 20010207SG005Pressure Switch · malfunctionedON TAXI IN TO THE GATE, RIGHT ENGINE FLAMED OUT AND EICAS STATUS MESSAGE R ENG LP PUMP CAME ON. REPLACED TRANSIENT PRESSURE UNIT. (M)SDR 20010206SG003Pressure Switch · failedON TAXI IN TO THE GATE, RIGHT ENGINE FLAMED OUT AND EICAS STATUS MESSAGE R ENG LP PUMP CAME ON. REPLACED TRANSIENT PRESSURE UNIT. (M)SDR 20010110CW001Pump · malfunctionedON APPROACH, 15MI OUT OF LAX, RT ENGINE SHUTDOWN WHEN THROTTLES PULLED BACK. RT ENG LLP PUMP, WAS OBSERVED. /REMOVED AND REPLACED RT ENGINE LOW PRESSURE FUEL PUMP.SYSTEM & LEAK CHECKED GOOD.SDR 20010111SG009Bleed Valve · fracturedAFTER SHUTDOWN, RT TURB OH DET 2, STATUS MESSAGE CAME ON. UPON INVESTIGATION, THE BLEED VALVE SKIRT WAS FOUND TO HAVE FRACTURED AND DEPARTED THE ENGINE, DAMAGING THE ACOUSTIC PANELS. REPLACED VALVE ASSEMBLY AND REPAIRED DAMAGED PANELS. (M)SDR 20001129AP006Duct · wornON CLIMB-OUT, NR 1 ENGINE HIGH STAGE AND ENGINE OVERHEAT EICAS MESSAGES CAME UP. ENGINE SHUTDOWN AND AN UNEVENTFUL LANDING WAS MADE. INVESTIGATION REVEALED SEAL RING BLOWNOUT ON HIGH STAGE DUCT JOINT. REMOVED AND REPLACED HIGH STAGE DUCT JOINT ASSEMBLY. (M
Back to N506NA, cancelled Dec 22, 2009