N758SA, cancelled Dec 23, 2015
Service difficulty reports · 28
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 = 'N758SA' AND deregistration_id = 'N758SA-2015-12-23' 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 = 'N758SA' AND deregistration_id = 'N758SA-2015-12-23' 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 Q2SA2012072875813Skin · failedDURING POST-FLIGHT, FOUND A HOLE AND CRACK DAMGE AT SECTION 48 LH SIDE BETWEEN STATION 2638 AND 2658 AND S-11L AND S-13L. STRINGER (P/N 65B 02976-1) CHORD (P/N 65B02515-113) AND ANGLE (P/N 65B02712-139) ASSEMBLIES WERE FOUND TO BE DAMAGED BEYOND ALLOWABLE LIMISDR TX9Y20111214011Cargo Track · crackedFORWARD CARGO TRACK FORWARD RIGHT CORNER WAS FOUND CRACKED. REPAIRED AS PER SRM 53-10-05 FIG 5 REV 120.SDR TX9Y20111208008Structure · corrodedLT WING T/E INBOARD MID FLAP T/E LOWER CHORD WAS FOUND CORROSION. THREE CORROSION AREAS WERE FOUND ON LEFT T/E INBOARD MID FLAP (P/N:65B02025-35) T/E LOWER CHORD (P/N:65B02098-1) HORIZONTAL FLANGE LOWER SURFACE. THE REPAIR WAS CARRIED OUT PER BOEING MESSAGE SDR TX9Y20111208009Mount · corrodedNR 4 ENG AFTER UPPER ENG MOUNT UPPER SURFACE WAS FOUND RUSTED HEAVILY. NR 4 ENGINE AFTER ENGINE MOUNT WAS REPLACED AS PER AMM 71-21-03 REV 86.SDR TX9Y20111208010Skin · crackedDURING REMOVING TWO ADDITIONAL DOUBLERS, THREE HOLE CRACK ON THE LEFT DOUBLER FUSELAGE SKIN AND TWO HOLE CRACK ON THE RIGHT DOUBLER FUSELAGE SKIN WERE FOUND. FOR EXISTING REPAIR DOUBLERS WHICH COMMON TO NOSE WHEEL WELL AFTER CORNER SKIN BETWEEN STA 400 TO STASDR TX9Y20111207007Longeron · crackedDURING INSPECTION OF NR 3 ENGINE RT SIDE COWL, ONE CRACK AND ONE DEEP CHAFING DAMAGE WERE FOUND AT LOWER LONGERON (P/N:65B94280-199). THE REPAIR WAS PERFORMED AS PER BOEING MESSAGE NUMBER TEC-SOF-11-0102.SDR TX9Y20111206004Skin · dentedFUSELAGE SKIN (STA2200-STA2400,STR27-STR28) WAS FOUND ONE ORIGINAL REPAIR RIVET AND DENT. FUSELAGE SKIN DOUBLER WAS REPAIRED AS PER SRM 53-30-03 FIG 4 REV 120.SDR TX9Y20111205003Failsafe · corrodedDURING DATUM AIRCRAFT INPUT,A CORROSION (SIZE ABOUT:3.3"*0.8") WAS FOUND ON BULK CARGO FRAME LOWER LOBE FAIL SAFE CHORD (P/N:65B04347-149,STA2200) HORIZONTAL FLANGE AT STR 40R. THE REPAIR WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0099. THE REPAIR WASDR TX9Y20111202001Skin · dentedBULK CARGO DOOR SKIN FORWARD LOWER CORNER WAS FOUND A DENT. THE SKIN SMOOTHED OUT WAS FOUND OUT LIMITS. BULK CARGO DOOR SKIN DENT AREA WAS REPAIRED AS PER SRM 52-00-03 FIG 9 REV 120.SDR TX9Y20111202002Doubler · crackedNR 9 SPOILER HINGE DOUBLER AND NR 11 SPOILER HINGE DOUBLER WERE FOUND CRACKED. NR 9 SPOILER AND NR 11 SPOILER WERE REPLACED AS PER AMM 27-61-02 REV 86.SDR Q2SA758012Engine · failedFLIGHT MAS6145, WHILE PREPARING FOR TAKEOFF, EXPERIENCED AN UNCONTAINED ENGINE FAILURE.SDR Q2SA795002AActuator · missingACFT 795 DEPARTED AS FLT SOO113, BOTH TAXI & TAKEOFF OPS WERE NORMAL. MLG HANDLE SELECTED TO "UP" POSITION AFTER LIFTOFF. BOTH RED "DOOR OPEN" & "RED "GEAR" LIGHTS REMAINED ILLUMINATED. FO CONTINUED FLYING & CLIMBED ON COURSE. CAPTAIN & FE COMPLETED QRH PROCEDSDR Q2SA758011Engine · leakingDURING THE TAKEOFF ROLL IN OMDB NR 1 EGT GAUGE BRIEFLY WENT TO 0, THEN RETURNED TO NORMAL. DURING THE CLIMB TO FL 300 IT WAS NOTICED, NR 1 EGT WAS RUNNING SIGNIFICANTLY HOTTER (APPROXIMATELY 80 DEG C) THAN THE OTHERS. AT THE TOP OF CLIMB, THE NR 1 EGT KEPT CSDR 2010FA0000346Hinge Fitting · crackedHORIZ STABILIZER LT 2 PLACES 0.9 INCH AND 0.8 INCH & RT 2 PLACES 1.1 INCH AND 0.85 INCH, HINGE FITTING CRACKED.SDR 2010FA0000345Stiffener · crackedPYLON NR 2 INBD NR 3 STIFFENER CRACK 0.67 INCH BETWEEN NAC STA 248 AND NAC STA 259 ON THE RT SIDE.SDR 2010FA0000344Skin · corrodedFWD CARGO LOWER FUSELAGE SKIN AT STA 1000 WAS CORRODED LEVEL 2.SDR 2010FA0000343Doubler · crackedMAIN ENTRY DOOR NR 1 UPPER OUTER SKIN DOUBLER CRACK, 0.35 INCH AT UPPER HINGE DOOR.SDR 2010FA0000342Stiffener · crackedPYLON NR 1, INBD NR 3, STIFFENER CRACK.SDR Q2SA758010Doubler · crackedMAIN ENTRY DOOR NR 1 UPPER OUTER SKIN DOUBLER CRACK AT UPPER HINGE DOOR.SDR Q2SA758009Stiffener · crackedPYLON NR 1 INBOARD NR 3 STIFFENER CRACK.SDR Q2SA758008A/C Pack · vibrationDEPARTURE FROM VAKK TO VMCC: AFTER TAKEOFF NR 1 AIR CONDITIONING PACK STARTED SEVERE RUMBLING NOISE AND EMITTED AN ODOR. AIRCRAFT QUICK HANDBOOK PROCEDURE ACCOMPLISHED. REMOVED AND REPLACED ACM AND DUCT ASSEMBLY. OPERATIONAL AND LEAK CHECK ACCOMPLISHED ANDSDR Q2SA758007Fuel Filter · failedON TAKEOFF CLIMBOUT OF KJFK, ENGINE NR 1 AND ENGINE NR 4 FUEL FILTER BYPASS INDICATION LIGHTS CAME ON AND STAYED ON, CREW ELECTED TO TERMINATE FLIGHT, DUMPED 156,000 LBS OF FUEL, RETURNED TO KJFK AND LANDED SAFELY. AFTER LANDING MAINTENANCE CREW IN KJFK REPLASDR Q2SA758006Slide · unwanted deployPRIOR TO DEPARTURE FROM KJFK, LEFT UPPER DECK EMERGENCY EXIT SLIDE INADVERTENTLY DEPLOYED. REMOVED SLIDE IN ACCORDANCE WITH AMM 25-68-02. TRANSFERRED TO DEFERRED MAINTENANCE ITEM NR 18844 PER MEL 25-11, CAT. C. PLACARD INSTALLED.SDR Q2SA758005Pms · inactiveCLIMB-OUT OF EBLG, PERFORMANCE MANAGEMENT SYSTEM (PMS) LIGHT ILLUMINATED IN FLIGHT AND AUTOPILOTS "A" AND "B" WOULD NOT FOLLOW FLIGHT MANAGEMENT SYSTEM (FMS) COMMAND. AIR TURN BACK TO EBLG. NO FUEL DUMPED. OPERATIONALLY CHECKED IN ACCORDANCE WITH DELCO OPERSDR Q2SA758004Thrust Reverser · deployedON CLIMB-OUT FROM ADDIS ABABA, ETHIOPIA (HAAB), AIRCRAFT PERFORMED AN AIR TURN BACK DUE TO INDICATION OF NR 4 ENGINE THRUST REVERSER TRYING TO DEPLOY IN FLIGHT. CREW WAS ALERTED BY THRUST REVERSER VALVE LIGHT AND TRANSIT LIGHT ILLUMINATING. CREW RETURNED TO SDR Q2SA758003Engine · damagedDURING TAKEOFF AFTER V1 FROM HAAB, BIRD INGESTION INTO NR 3 ENGINE. AIR TURNBACK TO HAAB. FUEL DUMP OF 50,000 LBS. INSPECTION AFTER LANDING CONFIRMED DAMAGE TO NR 3 ENGINE FAN BLADES, AS WELL AS EVIDENCE OF BIRD STRIKE ON NR 2 ENGINE. NR 1, 3, 4, 6, 11, 13SDR Q2SA758002Access Panel · crackedPOST FLIGHT WALK-AROUND, FOUND HYDRAULIC ACCESS PANEL ON NR 1 ENGINE SAIL BOAT FAIRING OPEN. FOUND CRACK AT NR 1 ENGINE INBOARD SAIL BOAT DOOR, AT THE FORWARD HINGE. HYDRAULIC ACCESS PANEL OPENED IN FLIGHT.SDR 758001Trim System · failedASTU WAS ON DEFERRAL. REMOVED AND REPLACED ASTU PRIOR TO DEPARTURE OUT OF PANC IAW AMM 22-14-01. AFFECTED BOTH AUTOPILOT A AND B SYSTEMS AND COULD NOT ENGAGE BOTH AUTOPILOT IN FLIGHT. RETURNED TO PANC. ASTU OPERATIONAL CHECK ACCOMPLISHED ON GROUND AND FAILE
Back to N758SA, cancelled Dec 23, 2015