N776AM, cancelled Apr 14, 2017
Service difficulty reports · 19
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 = 'N776AM' AND deregistration_id = 'N776AM-2017-04-14' 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 = 'N776AM' AND deregistration_id = 'N776AM-2017-04-14' 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 ASMF201611015Carbon Seal · leakingCAPTAIN REPORTED THAT DURING APPROACH, THE LEFT ENGINE OIL QUANTITY DECREASED TO 3 QTS WITH ENGINE PARAMETERS NORMAL. THE AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL PERFORMED LEFT ENGINE LEAK CHECK IAW AMM 71-00-00-700-823, AMM 79-00-00-200-800,SDR ASMF20160620011Transceiver · failedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO EICAS MESSAGE WXR FAIL. MAINTENANCE PERFORMED THE AIR/GROUND INTERFACE TEST IAW AMM 34-43-02, DETECTING WXR FAIL FLAG AND WXR SYS STATUS; SO THE LT TRANSCEIVER WAS REPLACED AND SYSTEM TEST WAS PERFORMED IAW AMMSDR ASMF201602009Windshield · crackedAIRCRAFT RETURNED FROM FLIGHT DUE TO, DURING CLIMB THE RT WINDSHIELD GOT CRACKED. PERFORMED THE QRH 1.9 PROCEDURE, CONFIRMING THE FAILURE. ACFT WAS SENT TO THE HANGAR & MX REPLACED THE LT L1 WINDSHIELD ASSEMBLY IAW MM 56-11-01 & WINDOW HEAT SYS TEST WAS PERFSDR ASMF201511008Actuator Valve · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE RT ENG FAIL LIGHT TURNED ON WITHOUT ABNORMAL INDICATIONS & DURING THE RT ENG SHUTDOWN, THE EGT EXCEEDANCE WAS SHOWN. PERFORMED FIM 73-11 TASK 815 & FIM 73-22 TASK 815 & 820 PROCEDURES & IDLE POWER OPERATSDR ASMF201510028Tire · puncturedAIRCRAFT RETURNED TO PLATFORM DUE TO MSG IN EICAS & STATUS OF LOW PRESS IN TIRE NR 11. PERFORMED REVISION DETECTING THE TIRE NR 11 WITH PRESS DROPPED OFF TO 26 PSI DUE TO DRILLING. WHEEL NR 11 WAS REPLACED IAW AMM 32-45-00, ALL CORRECT.SDR ASMF201507018Wire · damagedAIRCRAFT RETURNED TO PLATFORM, DURING LT ENG START, THE FAILURE CODE 73 21 52 51 & 732 152 51 WERE SHOWED & LT ENG NOT STARTED BY TWO ATTEMPTS. PERFORMED REVISION TO LT ENG, DETECTING LT HIGH PRESS FUEL SOV POSITION IN DISAGREE WITH COMMAND POSITION. THE FIMSDR ASMF201310005Radome · deformedDURING TRANSIT CHECK, FOUND RADOME DEFORMED. FOUND OUT OF LIMITS IAW SRM 57-12-00. RADOME REPLACED IAW AMM 57-12-02.SDR ASMF201306003Wedge · crackedDURING TRANSIT CHECK, THE T/E WEDGE RT OTBD FLAP WAS DAMAGED PROMOTING A CRACK OF 6.00" LENGTH AND 5.75" WIDE AT BS 214, ON UPPER & LOWER RT OTBD FLAP. MX PERSONNEL ISSUED THE NON ROUTINE CARD A0205977. THE T/E WEDGE RT OTBD FLAP WAS REPAIRED IAW SRM 57-53-0SDR ASMF201210009Engine · intermittentACFT REJECTED TAKE AT 70 KNOTS WITH A GROSS WEIGHT OF 268 000 KG DUE TO RIGHT ENGINE STRONG EXPLOSION WITHOUT ADVISE ON ENGINE PARAMETERS OR EXCEEDS IN CREW CABIN WAS LISTENING. MX PERFORMED FIM 71-05 TASK 807 PROCEDURE; A RT ENGINE STALL INSPECTION IAW MM 71SDR ASMF201207009Panel · puncturedDURING TRANSIT CHECK, DAMAGE WAS DETECTED IN THE NOSE COWLING SKIN ACOUSTIC PANEL OF THE LT ENGINE, A PUNCTURE 1 X 0.75 INCH BEING OUT OF LIMITS IAW SRM 54-11-01. THE DAMAGE WAS REPAIRED IAW AMX-12-0324-02B, TESTED CORRECT.SDR ASMF201110002Unknown · smokeDURING CLIMB, SMOKE IN THE PASSENGER CABIN ON THE PREMIER CLASS AND THE FIRST 20 ROWS WAS VISIBLE ALONG THE CEILING; SO FLIGHT CREW ACCOMPLISHED THE QRH 8.5 PROCEDURE. ACFT RETURNED, MX PERSONNEL PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW MMSDR ASMF201104002Pump · leakingCAPTAIN REPORTED THAT DURING CRUISE, THE HYD QTY LOW LT AND HYD PRESS PRI LT LIGHTS TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 13.3 AND 13.22 PROCEDURES, CONFIRMING THE FAILURE AND CONTINUING TO DESTINATION. MX PERSONNEL, A REVISION, DETECTING HYD LEAK IN THSDR ASMF201007006Wheel · damagedDURING PUSH BACK THE TOW FITTING WAS BROKEN. MX PERFORMED GENERAL VISUAL INSP TO THE NLG IAW MM 05-51-01 DETECTING DAMAGE OUT OF LIMIT IN THE RT NOSE LANDING WHEEL. TECH REPLACED BOTH NOSE LANDING WHEELS IAW MM 32-45-02, TESTED CORRECT.SDR ASMF201007003Access Door · damagedDURING TRANSIT CHECK A BIRD STRIKE WAS DETECTED BETWEEN SLAT NR 9 AND 10. MX PERFORMED A BIRD STRIKE INSP IAW 05-51-18 DETECTING DAMAGES IN ANTI ICE RELEASE ACCESS DOORS SLAT. THE RT WING SLAT LEADING EDGE NR 9 WAS REPLACED IAW DWG NR 114W4565 AND INSTALLED FASDR ASMF201004001Blades · damagedDURING A BORESCOPE INSP OF THE HPC 1, 4 AND 9 STAGES BLADES OF THE RT ENGINE WAS DETECTED. 1 BLADE OF THE HPC 1ST STAGE WITH L/E TIP CURLED 90 DEGREES OUT OF LIMITS IAW 72-00-00, PARA 5H (L) (7), PAGE 625; WITH DIMENSIONS OF 3.5 INCHES LENGTH AND 1.25 INCHES WSDR ASMF20090402Skin · damagedDURING TRANSIT CHECK, MX FOUND 3 SCRATCHES OF .5 INCHES ON THE FUSELAGE SKIN, AT THE COVER RECEPTACLE EXTERNAL POWER. A SCRATCH AT STA 342 WITH THICKNESS FOUND 0.020 INCHES, AT STA 348 WITH THICKNESS FOUND 0.089 INCHES, AND AT STA 351 WITH THICKNESS FOUND 0.06SDR ASMF 20081201Tire · separatedDURING TAKE OFF, CAPTAIN REPORTED STRONG VIBRATION IN MLG. MX PERSONNEL DETECTED TREAD LOSS IN THE WHEEL POSITION NR 1 IN THE LT MLG, CRACK IN THE LT FLAP LOWER SKIN AT STA 261 AND A DENT OF 8 IN LONG X 4 IN WIDTH 0.200” DEPTH IN THE LOWER ACCESS PANEL 511JB SDR ASM2008F00005Hose · damagedDURING TRANSIT CHECK, MAINT DETECTED DAMAGE AND HYDRAULIC LEAK ON SUPPLY HOSE ASSEMBLY TO RT ENGINE EDP. THE HOSE ASSY, PN AE70970110 WAS REMOVED AND REPLACED AND PERFORMED LEAK CHECK IAW AMM 29-11-05, NO LEAKS WERE FOUND. (K)SDR ASM2008F00001Blade · bentDURING TRANSIT CHECK, THE MAINTENANCE PERSONNEL PERFORMED A BOROSCOPIC INSPECTION DETECTING BLADES TIP BENDED IN THE FIRST STAGE OF HIGH PRESSURE COMPRESSOR ROTABLE SECTION AND A IGV SCRATCHED IN THE RT ENG, OUT OF LIMITS IAW MM 72-00-00. THE RT ENG WAS REPLA
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