N6826, cancelled Aug 3, 2009
Service difficulty reports · 35
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 = 'N6826' AND deregistration_id = 'N6826-2009-08-03' 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 = 'N6826' AND deregistration_id = 'N6826-2009-08-03' 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 EISA20000201Module · failedON ASCENT FLAPS AT 2 DEGREES, FORWARD LEADING EDGE AMBER LIGHT ILLUMINATED, F/E PANEL GREEN LIGHTS. EXTENDED AND RETRACTED FLAPS SEVERAL TIMES, ALL INDICATIONS NORMAL ON GROUND. FLAPS OP CHECK NORMAL.SDR EISA99140Connector · dirtyUPON GEAR EXTENSION THE RIGHT MAIN GEAR (RED) WARNING LIGHT ILLUMINATED. PERFORMED ABNORMALS SECTION 3 PAGE 50 PROCEDURE UNEVENTFUL LANDING. CLEANED AND REPOSITIONED CONNECTOR TO LANDING GEAR ACCY BOX AND PERFORMED TEST IAW MM 32-61-01. OPS CHECK GOOD. (M)SDR EISA98136Actuator · failedON TAKEOFF FROM BRUSSELS (BRU), A-SYSTEM HYDRAULIC QUANTITY WENT TO 2.0 GALLONS AND LOW LEVEL LIGHT ILLUMINATED. RETURNED FOR LANDING TO (BRU). GENERATED FROM PILOT REPORT. REMOVED AND REPLACED LEFT MAIN LANDING GEAR DOOR ACTUATOR IAW MM CHAPTER 32. OPS CSDR EISA98135Moisture Trap · contaminatedAIRBORNE RETURN TO SOUTHEND, ENGLAND (SNN), DUE TO FLUCTUATIONS ON ENGINE VALUES, NR 1 EPR, NR 1 N1, AND NR 1 N2, NR 1 FUEL FLOW. PILOT REPORT. CARRIED OUT T/S PER BOEING MM 72-00. INSPECTED INLET AND EXHAUST, REMOVED AND CLEANED PS4 MOISTURE TRAP. CREW CASDR EISA98105Fitting Boss · strippedIN-FLIGHT, NR 1 LOW OIL PRESSURE LIGHT ILLUMINATED, NR 1 OIL PRESSURE GAUGE READ JUST ABOVE LOWER RED RADIAL. OIL QUANTITY READ ZERO. PRECAUTIONARY SHUT DOWN OF NR 1 ENGINE. RETURNED TO BRUSSELS (BRU). GENERATED FROM PILOT REPORT. FOUND LEAKING FITTING ATSDR EISA98038Guide · chippedDURING C-CHECK, FOUND NR 2 SLAT GUIDE CHIPPED AT WS 620 LT TOP OF FLAT TRAILING EDGE. INSTALLED SLAT TRAILING EDGE DOUBLER PER SRM 57-50-03. (M)SDR EISA98037S-Duct · tornDURING C-CHECK, FOUND NR 2 ENGINE INTAKE 12 O'CLOCK POSITION HAS A TEAR IN SKIN AT OPENING NEXT TO ENGINE RING FLANGE. REMOVED DAMAGED AREA, FABRICATED REPAIR FILLER AND DOUBLER PER SRM 54-10-03. INSTALLED REPAIR PER SRM 54-10-03. (M)SDR EISA98036Skin · delaminatedDURING C-CHECK, FOUND TORN AND DELAMINATED LEFT INBOARD AFT FLAP TRAILING EDGE. REPAIR DELAMINATION ON LEFT INBOARD AFT FLAP BY INJECTION METHOD PR SRM 51-40-06. (M)SDR EISA98035Angle · crackedDURING C-CHECK, FOUND 50 INCH CRACK IN SUPPORT ANGLE FOR LEFT MAIN GEAR DOOR UPSTOP, FS 850. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER SRM 51-30-02. (M)SDR EISA98034Skin · delaminatedDURING C-CHECK, FOUND RT INBOARD AFT FLAP DELAMINATED TRAILING EDGE. REPAIR DELAMINATION BY INJECTION METHOD PER SRM 51-40-06. (M)SDR EISA98033Skin · crackedDURING C-CHECK, FOUND LEFT INBOARD AFT FLAP BOTTOM SKIN WITH CRACKS AND DENTS IN AREA 18 INCHES BY 24 INCHES. ACCOMPLISHED POTTING REPAIR PER SRM 51-40-06 AND INSTALLED FIBERGLASS OVERLAY PER SRM 51-40-08. (M)SDR EISA98032Skin · crackedDURIGN C-CHECK, FOUND RT INBOARD AFT FLAP BOTTOM SKIN WITH CRACKS AND DENTS IN AREA 18 INCHES BY 24 INCHES. ACCOMPLISHED POTTING REPAIR PER SRM 51-40-06 AND INSTALLED FIBERGLASS OVERLAY PER SRM 51-40-08. (M)SDR EISA98031Skin · holeDURING C-CHECK, FOUND CRACK AND HOLE, RT INBOARD AFT FLAP. REPAIRED HOLE WITH POTTING REPAIR PER SRM 51-40-06 FIBERGLASS OVERLAY APPLIED PER SRM 51-40-08. (M)SDR EISA98030Seat Track · corrodedDURING C-CHECK, FOUND CORROSION ON SEAT TRACK, LEFT SIDE FROM FS 750 TO 950E ON MAIN CARGO DECK. REMOVED TRACK AND INSTALLED NEW SEAT TRACK IAW SRM 53-10-05. (M)SDR EISA98029Angle · corrosionDURING C-CHECK, FOUND FS 178 BULKHEAD, FIRST ANGLE FROM BOTTOM HAS CORROSION. REMOVED ANGLE, FABRICATED ANGLE FROM 7075-T6 AND INSTALLED PER SRM 51-10-1. (M)SDR EISA98028Skin · delaminatedDURING C-CHECK, FOUND LEFT INBOARD AFT FLAP DELAMINATED AT TRAILING EDGE. REPAIRED DELAMINATION BY INJECTION METHOD PER SRM 51-40-06. (M)SDR EISA98027Skin · damagedDURING C-CHECK, FOUND LEFT INBOARD AFT FLAP HAS HOLE AND DENT ON BOTTOM SKIN. REPAIRED HOLE AND DENT IN BOTTOM SKIN WITH POTTING REPAIR PER SRM 51-40-06 AND MADE FIBERGLASS OVERLAY PER SRM 51-40-08. (M)SDR EISA98026Skin · delaminatedDURING C-CHECK, FOUND TRAILING EDGE DELAMINATION ON LEFT INBOARD AFT FLAP. REPAIRED DELAMINATION WITH FIBERGLASS OVERLAY PER SRM 51-40-08. (M)SDR EISA98025Skin · delaminatedDURING C-CHECK, FOUND INBOARD FLAP, AFT FLAP TRAILING EDGE DELAMINATED. REPAIRED DELAMINATION ON TRAILING EDGE WITH FIBERGLASS OVERLAY PER SRM 51-40-08. (M)SDR EISA98024Seat Track · corrodedDURING C-CHECK, FOUND CORROSION ON FLOORBEAM AND SEAT TRACK AT FS 560-580. SURFACE CORROSION REMOVED ON FLOORBEAM. FOUND IN LIMITS PER SRM 53-10-1. INSTALLED NEW SECTION OF SEAT TRACK. (M)SDR EISA98023Seat Track · corrodedDURING C-CHECK, FOUND FS 580 RT AND 620 CORROSION ON CENTER BEAM AND SIDE OF SEAT TRACK. REMOVED SURFACE CORROSION ON FLOORBEAM AND FOUND TO BE IN LIMITS. REMOVED AND REPLACED SEAT TRACK PER 53-10-1 DUE TO CORROSION OUT OF LIMITS. (M)SDR EISA98022Doubler · corrodedDURING C-CHECK, FOUND CORROSION ON COCKPIT SHEER DOUBLER JUST BELOW PILOTS WINDOW FS 253 LT. REMOVED CORROSION, FABRICATED DOUBLER AND INSTALLED DOUBLER PER SRM 51-40-2. (M)SDR EISA98021Vent Box · crackedDURING C-CHECK, FOUND WING STATION 171.5 RT WING, FUEL VENT BOX HAS CRACKED FLANGE AT UPPER CHORD. FABRICATED REPAIR PARTS PER SRM 57-10-4 AND INSTALLED REPAIR PER SRM 51-10-4 FIG 8. (M)SDR EISA98020Fuel Tank · leakDURING C-CHECK, FUOND FUEL LEAK NR 3 SLAT ACTUATOR CAN ON RT WING. REMOVED OLD SEALER AND RESEALED AT LEAK SOURCE PER 727 MM 28-11-0, PAGE 801. (M)SDR EISA98019Stringer · crackedDURING C-CHECK, FOUND LEFT WING STATION 629, CRACK ON UPPER STRINGER ATTACHMENT TO RIB, 7TH FROM FWD SPAR. DRILLED REPAIR ANGLES AND RADIUS BLOCKS AND INSTALLED REPAIR PER BOEING SB 727-57A-159. (M)SDR EISA98018Stringer · crackedDURING C-CHECK, FOUND LEFT WING STATION 519, 10TH STRINGER AFT OF FRONT SPAR HAS CRACK AT STRINGER TO RIB ATTACHMENT (UPPER STRINGER). DRILLED REPAIR ANGLES AND RADIUS BLOCKS AND INSTALLED PER BOEING SB 727-57A-159. (M)SDR EISA98017Skin · crackedDURING C-CHECK, FOUND RIGHT ELEVATOR HAS CRACK AND HOLE IN BOTTOM SKIN, OUTBOARD END. FABRICATED DOUBLER PER SRM 55-20-03. (M)SDR EISA98016Angle · crackedDURING C-CHECK, FOUND X-RAY INSPECTION OF RT ELEVATOR SHOWS A CRACK INDICATION AS SHOWN IN SHOTS R7, R1 AND R4. REMOVED ANGLE, FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-30-02. (M)SDR EISA98015Gusset · crackedDURING C-CHECK, FOUND FS 356, STRINGER 17L, GUSSET AND STRINGER CRACKED AT WIRE BUNDLE. FABRICATED PART PER SAMPLE AND INSTALLED PER SRM 51-40-2. (M)SDR EISA98014Frame · crackedDURING C-CHECK, FOUND FS 360, STRINGER 17L FRAME CRACKED AND BROKEN. FABRICATED DOUBLER AND INSTALLED PER SRM 53-10-4. (M)SDR EISA97208Hyd Pump · leakingLOSS OF A-SYSTEM HYDRAULICS DURING CLIMB-OUT. REMOVED AND REPLACED NR 2 ENGINE PUMP. CHKS GOOD IAW MM. (X)SDR EISA97079Door · damagedON POST FLIGHT INSPECTION, FOUND DAMAGED RIGHT MAIN GEAR DOOR (WING DOOR). (M)SDR EISA97035Aoa Vane · inopSTICK SHAKER ACTIVATED ON TAKEOFF FROM CPH (ATB). REPLACED AOA VANE. (M)SDR EISA97034Connectors · dirtySTICK SHAKER ACTIVATED ON TAKEOFF FROM CPH (ATB). PULLED LANDING GEAR ACCY BOX C/B'S. REMOVED L/G ACCY BOX CLEANED CONNECTORS. REINSTALLED L/B ACCY BOX, OPS CHECK GOOD ON THE GROUND. (M)SDR EISA97033Landing Accy Box · failedON TAKEOFF ROTATION FROM BRU, STICK SHAKER ACTIVATED AND REMAINED ON UNTIL LANDING AT BRU (ATB). REPLACED LANDING GEAR ACCY UNIT, OPS CHECK OK PR MM 34 AND 32. (M)
Back to N6826, cancelled Aug 3, 2009