N828AX, cancelled Jul 21, 2009
Service difficulty reports · 107
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 = 'N828AX' AND deregistration_id = 'N828AX-2009-07-21' 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 = 'N828AX' AND deregistration_id = 'N828AX-2009-07-21' 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 ABXA010180Fitting · crackedZ-FITTING CRACKED AT STA 1200 LONGERON 33R-34R.SDR ABXA010179Fitting · crackedZ-FITTING CRACKED IN AFT LOWER CARGO BAY AT FS 1680 FROM L34R TO L35R.SDR ABXA010554Pressure Panel · corrodedCORROSION ON THE UPPER SURFACE OF THE PRESSURE WEB AND ON FINGER DOUBLER. ALSO RIVET HEADS WERE SHEARED OFF BETWEEN FS 920-980. REPAIRED AREA AND REPLACED THE DOUBLER IAW DC-8 SRM 51-1-8, 53-2-0, AND REA D853-40413-MR, AND DAC DRAWING NR 5645332.SDR ABXA010237Stanchion · corrodedTHE FWD CARGO RT TUNNEL STANCHION WAS CORRODED ON THE LOWER RIGHT SIDE AT STA 360. MAINTENANCE INSPECTED AND REPLACED THE STANCHION IAW DAC DRAWING 3706753 AND DC-8 SRM.SDR ABXA010228Stanchion · corrodedRIGHT TUNNEL STANCHION CORRODED AT FUSELAGE STATION 360, FORWARD CARGO BAY RIGHT SIDE. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 51-1-8, 53-2-0.SDR ABXA010178Fitting · crackedBATH TUB FITTING CRACKED IN FORWARD CARGO PIT AT FS 300 L27 - L28.SDR ABXA010555Pressure Panel · corrodedCORROSION AND SEVERAL RIVET HEADS SHEARED OFF BETWEEN FS 900-940, ON UPPER SURFACE OF PRESSURE WEB AT BUTT LINE 00. REPAIRED AREA AND REPLACED DOUBLER AND GUSSET IAW DC-8 SRM 51-1-20, 51-1-11, 51-3-0, 51-1-21, 51-1-8, 53-20, AND DAC DRAWING NR 5645332, AND REASDR ABXA010552Doubler · bulgedBULGING FINGER DOUBLER AND RIVET HEADS WERE SHEARED ON THE UPPER SURFACE OF THE PRESSURE WEB BETWEEN FUSELAGE STATION 880 AND BUTT LINE 00. REPAIRED AREA AND INSTALLED NEW FINGER DOUBLER IAW DC-8 SRM 51-1-21, 51-1-8, 53-2-0, 51-9-0, 51-1-20D, 51-1-11, AND DRAWSDR ABXA010177Fitting · crackedLEFT FRAME FITTING AT FS 700 BELOW LONGERON L21 WAS CRACKED.SDR ABXA010289Intercostal · crackedRIGHT MAIN LANDING GEAR WHEEL WELL AT FS 975, LONGERON 28 RIGHT INTERCOSTAL WAS CRACKED AT FORWARD END. FABRICATED INTERCOSTAL IAW DC-8 DWG 5646444. ALODINED IAW DC-8 SRM 51-1-8. PRIMED IAW DC-8 SRM 51-1-8. INSTALLED IAW DC-8 SRM 51-1-20D.SDR ABXA010176Intercostal · crackedINTERCOSTAL AT LONGERON 25R FS 960 IN THE RIGHT MAIN LANDING GEAR WHEEL WELL IS CRACKED.SDR ABXA010175Intercostal · crackedINTERCOSTAL CRACKED AT FS 975 AT LONGERON 28R.SDR ABXA010288Attach Angle · corrodedRIGHT MAIN LANDING GEAR WHEEL WELL AT FS 880 KEEL BEAM TO WEB ATTACH ANGLE WAS CORRODED. REMOVED SURFACE CORROSION IAW DC-8 SRM 51-1-8. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. FOUND BLEND OUT TO BE WITHIN LIMITS IAW DC-8 SRM 53-2-0.SDR ABXA010227Attach Angle · corrodedKEEL BEAM TO WEB ATTACHMENT ANGLE IN THE RIGHT MAIN LANDING GEAR WHEEL WELL WAS CORRODED. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 51-1-8 AND 51-2-0.SDR ABXA010174Bulkhead · crackedTHE RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD OUTBOARD LOWER BULKHEAD PANEL WAS CRACKED.SDR ABXA010173Fitting · crackedRIGHT MAIN LANDING GEAR WHEEL WELL TRAPEZOID FITTING AT STA 860 WAS CRACKED.SDR ABXA010172Fitting · crackedRIGHT WING JACK POINT CRACKED AT XRS 139.SDR ABXA000529Door · missingDURING POSTFLIGHT INSPECTION, MAINTENANCE NOTED THE LEFT OUTBD MAIN LANDING GEAR DOOR WAS MISSING FROM THE AIRCRAFT. THE STRUT HOLDING ON THE LEFT OUTBD UPPER GEAR DOOR WAS CRACKED. THE DOOR AND ASSOCIATED BRAKETS WERE REPLACED IAW DC-8 MM 32-12-01 AND 32-12-SDR ABXA000463Panel · contaminatedDRINK WAS SPILLED ON COCKPIT FLOOR. A BURNING SMELL WAS DETECTED SHORTLY THEREAFTER AND A SPARK BY THE FLIGHT ENGINEER''S PANEL. FOLLOWED EMERGENCY CHECKLIST FOR ELECTICAL FIRE/SMOKE OF VARIOUS ORIGIN. CLEANED SPILLED DRINK FROM AREA AROUND FLIGHT ENGINEER'SDR ABXA000371Connector · looseNOSE GEAR GREEN LIGHT (DOWN LIGHT) WOULD NOT ILLUMINATE WITH GEAR HANDLE DOWN. MISSED APPROACH. ACCOMPLISHED ABNORMAL PROCEDURES, LANDING WAS UNEVENTFUL. REPLACED CONNECTORPI-215 IAW DC8 MM 32-61-01. OPS CHECKED GOOD.SDR ABXA000361Connector · looseWHEN LANDING GEAR WAS EXTENDED FOR LANDING, THE LANDING GEAR GREEN LIGHT FOR THE NOSE GEAR DID NOT COME ON. MAINTENANCE FOUND CANNON PLUG HAD COME OFF NOSE GEAR DOWNLOCK SWITCH. CLEANED AND RESECURED PLUG, CHECKED GOOD.SDR ABXA9900805Connector · contaminatedWHEN THROTTLE WAS RETARDED FOR DESCENT, NR 1 LOW OIL PRESSURE LIGHT CAME ON. THROTTLE WAS PULLED BACK TO IDLE, LOW OIL PRESSURE LIGHT STAYED ON. OIL PRESSURE WAS 41 PSI, TEMP 75 DEGREES AND QUANTITY WAS 4.2 GALLONS. SHUT ENGINE DOWN IAW ABNORMAL PROCEDURES.SDR ABXA9900331Bulb · failedDURING CRUISE, NOTICED ODOR (BURNING SMELL) COMING FROM AREA OF FIRST OFFICER'S GLARESHIELD FLOURESCENT LIGHT. REPLACED LIGHT BULBS AND REMOVED GLUE FROM LIGHT ASSY AREA. OPS CHECKED GOOD.SDR ABXA9900303Switch · defectiveDURING DESCENT INTO ONT, WITH POWER REDUCED TO IDLE, NR 1 ENG LOW OIL PRESS LIGHT ILLUMINATED. OIL PRESS IND 42 PSI. SHUT NR 1 ENGINE DOWN, OIL PRESS WAS 7 PSI DURING DESCENT AND APPROACH FOR 8 MINUTES. INSPECTED MAIN OIL FILTER, NO CONTAMINATION FOUND. CHSDR ABXA9800041Indicator · defectiveNR 3 ENGINE OIL PRESSURE FLUCTUATED BETWEEN 36 AND 45 PSI. SHUT DOWN NR 3 IAW DC8 ENGINE SECURING CHECKLIST. REPLACED NR 3 ENGINE OIL PRESSURE INDICATOR IAW DC8 MM 79-32-0, OPS CHECKED NORMAL.SDR ABXA9701903Spoiler · delaminatedSPOILER LOWER SURFACE HAS 40 PERCENT DELAMINATION. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.SDR ABXA9701771Angle · corrodedVERTICAL STABILIZER, TO FUSELAGE ATTACH ANGLE CRACKED AND GOUGED ON RT AFT SIDE AT REAR SPAR. REPAIRED IAW DC8 SRM 53-2-5, 51-1-8 AND ABX REA D853-19535MR.SDR ABXA9701770Skin · corrodedFOUND CORROSION ON LWR FUSELAGE SKIN FS 610 TO FS 710. REPLACED SKIN IAW ABX REA D853-19477MR.SDR ABXA9701769Keel Beam · corrodedSTA 798 KEEL BEAM HAS CORROSION UNDER CANTED PANEL 745C. REMOVED CORROSION AND INSTALLED DOUBLERS IAW ABX REA D853-19066MR.SDR ABXA9701768Longeron · corrodedSTA 1380, LONGERON 21L (CUSP) CORRODED ON BOTTOM SIDE. REPAIRED IAW ABX REA D853-19054MR.SDR ABXA9701767Longeron · corrodedSTA 1680 LONGERON 21 TO 25 LT CORRODED. REPAIRED IAW DC8 SRM 51-1-8, 53-2-0, 51-1-21 AND ABX REA D853-18569.SDR ABXA9701766Web · corrodedFS 1766 VERTICAL WEB CORRODED. REPAIRED IAW ABX D853-19061MR.SDR ABXA9701765Angle · corrodedCANTED WING BOX SHEAR WEB L-ANGLE CORRODED AT STA 857 FROM C/L TO RBL 15. REPAIRED IAW ABX D853-19085MR.SDR ABXA9701764Frame · corrodedCARGO DOOR JAMB FRAME AT FS 280 AND LONGRON 32R CORRODED. REPAIRED IAW ABX REA 853-1913MR.SDR ABXA9701763Frame · corrodedFRAME AT FS 320 LT IS CRACKED AND BROKEN AT BOTTOM. REPAIRED IAW ABX D853-19887MR.SDR ABXA9701772Frame · corrodedCORROSION FOUND ON THE FWD UPPER WEB OF -5 ANGLE AND ON THE LOWER FLANGE OF -3 FRAME AT L35R AND L35L. REPAIRED IAW ABX REA D853-20466, DAC DWG 5750885 AND SRM 51-1-20D.SDR ABXA9701762Spar · crackedFOUND CRACKS INSIDE UPPER/LOWER FLAP SUPPORT ATTACH HOLES IN WING REAR SPAR AND BULKHEAD INSTALLATION STRUCTURE AT XRS=428. REPAIRED IAW ABX REA D857-20371MR.SDR ABXA9701761Longeron · corrodedCORROSION FOUND ON INNER SURFACE OF LONGERON 34R AT STA 695, BELOW NUT PLATE RESULTED IN BLENDOUT EXCEEDING SRM LIMITS. REPAIRED IAW ABX REA D853-20438MR.SDR ABXA9701832Stinger · delaminatedDURING INSPECTION, FOUND THRUST REVERSER STINGER ASSY HAD SEVERE DELAMINATION AND WIDE SPREAD CORROSION. REPAIRED UNIT COMPLETE.SDR ABXA9701831Stinger · delaminatedDURING INSPECTION, FOUND SEVERE DELAMINATION AND WIDESPREAD CORROSION ON LOWER THRUST REVERSER STINGER. REPAIRED UNIT COMPLETE.SDR ABXA9701543Longeron · corrodedSTA 1380 LONGERON 21L (CUSP) CORRODED ON BOTTOM SIDE. REPAIRED IAW ABX REA D853-19054 MR.SDR ABXA9701542Tr Track · wornNR 4 PYLON THRUST REVERSER UPPER CENTER TRACK WORN AT AFT FLANGES. WELDED TRACK IAW ABX DWG C89R01, COUNTER BORED TRACK IAW DWG 9753006 AND INSTALLED TRACK IAW DC8 SRM 51-3-0.SDR ABXA9701541Spar Cap · delaminatedLEFT LEADING EDGE AUX TANK UPPER SPAR CAP DELAMINATED AND CORRODED XFS 20 AND XFS 40. INSTALLED NEW L/E UPPER SPAR CAP IAW DC-I SRM 51-1-21 AND 51-1-20D.SDR ABXA9701540Skin · corrodedBELLY SKIN CORRODED. REPLACED BELLY SKIN IAW DAC DWG 5779925 AND DC8 SRM 51-1-8.SDR ABXA9701539Web · crackedRT AFT LOWER WEB AT STA 931 HAS CRACKED DOUBLER AND VERTICAL STIFFENER IS CRACKED. FABRICATED DOUBLER WEB REPAIR IAW 51-9-0 AND DAC DWG 564 3402, AND DC8 SRM 51-1-20D AND 51-1-21.SDR ABXA9701538Sub Floor · corrodedCORROSION ON SUB FLOOR STA.52, 24 INCHES FROM LT CUSP UNDER CAPTAIN'S SEAT TRACK. INSTALLED DOUBLER REPAIR IAW ABX REA D853-20446MR AND SRM 51-1-20.SDR ABXA9701537Panel · crackedFOUND SEVERAL CRACKS AT ATTACH HOLES ON LEFT WING PANEL 505F. INSTALLED REPAIR DOUBLER IAW ABX REA 0857-20439MR.SDR ABXA9701536Frame · elongated holesSTA 1310 FRAME HAS ELONGATED HOLES BETWEEN LONGERON 21L AND 20L. REPAIRED IAW ABX REA 0853-20461MR.SDR ABXA9701347Frame · corrosionFOUND CORROSION AND GOUGE DAMAGE ON LOWER FRAME FLANGE OF CARGO DOOR JAMB FRAME AT FS 340, LONGERON 35R. REPAIRED IAW ABX REA D853-19132-MR.SDR ABXA9701346Panel · crackedFOUND DENT AND CRACK ON FUSELAGE PANEL AT FS 1580 AND L 21L AND 22L. REPAIRED IAW DC-8 SRM 51-1-20D, 51-1-21D AND 51-1-12.
Back to N828AX, cancelled Jul 21, 2009