N826AX, cancelled Nov 21, 2007
Service difficulty reports · 217
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 = 'N826AX' AND deregistration_id = 'N826AX-2007-11-21' 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 = 'N826AX' AND deregistration_id = 'N826AX-2007-11-21' 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 ABXA050366Floorbeam · corrodedFOUND MAIN CABIN, STA 70, RIGHT BUTT LINE 43-51, LOWER SIDE OF FLOORBEAM CORRODED OUT OF LIMITS. FOUND LOWER SIDE OF FLOORBEAM CORRODED OUT OF LIMITS AT STA 70, RIGHT BUTT LINE 43-51. FABRICATED FILLER AND DOUBLER AND INSTALLED. ALL WORK IAW DC8 SRM 51-1-8,SDR ABXA050352Floorbeam · corrodedFOUND MAIN CABIN, STA 920, RIGHT BUTT LINE 31, FLOORBEAM CORRODED AT NUTPLATES. REMOVED CORROSION STA 920, RIGHT BUTT LINE 31. MATERIAL LOSS OUT OF LIMITES. FABRICATED REPAIR ANGLES AND INSTALLED IAW DWG K04881 OUT OF 7075 "0", PO NR 1108502 0.063", HEAT TRSDR ABXA050351Floorbeam · corrodedFOUND MAIN CABIN, STA 680, RIGHT BUTT LINE 26, LOWER SIDE OF FLOORBEAM CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, ORIGINAL MATERIAL THICKNESS 0.178", REMAINING THICKNESS 0.107" AND OUT OF LIMITS IAW DC8 SRM 53-2-0. VERIFIED REPAIR AINGLE AS AND10134-1407SDR ABXA050296Skin · corrodedFUSELAGE SKIN, STA 1100 TO 1120 AT RT AFT BODY FAIRING, SKIN CORRODED. REMOVED CORROSION AND INSTALLED REPAIRS BETWEEN STA 1100 LONGERON 29 RT TO STA 1120 LONGERON 30 RT IAW REA D853-52518-MR AND SRM 51-1-8, PG 20.SDR ABXA050365Longeron · corrodedFORWARD CARGO BAY, CORROSION IN LONGERON 36, STA 598 OUT OF LIMITS. REPAIRED LONGERON 36 IAW DC8 SRM 53-2-2 AND SPLICE WITH NEW SECTION FROM EXTRUSION P/N: S2645716 IAW DC8 SRM 53-2-2-, PG 6.SDR ABXA050339Stiffener · corrodedLOWER AFT CARGO FORWARD BULKHEAD LEFT SIDE FRAME CORRODED AT BOTTOM STA 980, 30 LEFT. REMOVED OLD STIFFENER IAW DC8 SRM 51-3-1 AND 51-1-21 WHICH HAD CORROSION OUT OF LIMITS IAW DC8 SRM 53-2-0 AND REPLACED WITH NEW STIFFENER PO NR 1122166 IAW DC8 SRM 51-1-21 ASDR ABXA050338Air Duct · dentedNR 4 ENGINE L/S TRANSITION AIR DUCT HAD SEVERAL DENTS. 2 DENTS AT 9 AND 11 O'CLOCK POSITIONS OUT OF LIMITS IAW DC8 SRM 51-1-9A. CLEANED UP AREA OF DENTS AT 9 AND 11 O'CLOCK POSITIONS AND REPAIRED IAW DC8 SRM 51-1-9A. 2 MORE DENTS AT 11 O'CLOCK POSITION ARE WISDR ABXA050337Case · wornNR 2 ENGINE EXHAUST NOZZLE 6 O'CLOCK POSITION, CASE WORN. REMOVED DAMAGED EXISTING DOUBLERS IAW DC8 SRM 51-1-21. FABRICATED NEW DOUBLERS IAW SSRM DWG NR 78-841 FROM 0.051 301 1/2HD PO NR 1121624, PRIMED CONTACT SURFACE IAW DC8 51-1-8. INSTALLED NEW DOUBLER SDR ABXA050336Pressure Panel · corrodedDOUBLER CORRODED TOP OF RIGHT WHEEL WELL PRESSURE DECK IN MAIN CARGO, STA 980, RIGHT BUTT LINE 30. REMOVED, FABRICATED, AND INSTALLED DOUBLER AT TOP OF RIGHT WHEEL WELL PRESSURE DECK IN MAIN CARGO STA 980 RIGHT BUTT LINE 30 IAW DC8 SRM 51-1-21, 51-1-14, 51-9-SDR ABXA050316Doubler · corrodedCORRODED DOUBLER IN MAIN CARGO BELOW FLOOR LEVEL AGAINST ABOVE LEFT WHEEL WELL PRESS DECK, STA 940, LEFT BUTT LINE 67. REMOVED, FABRICATED AND REPLACED DOUBLERS IN MAIN CARGO BELOW FLOOR LEVEL AGAINST ABOVE LEFT PRESS DECK STA 940, LEFT BUTT LINE 67 IAW DC8 SSDR ABXA050315Cowling · scoredNR 1 ENGINE, OUTBOARD FORWARD COWL HOLD OPEN ROD HAD SCORED INNER SIDE OF COWL. REMOVED PREVIOUS REPAIR, FABRICATED NEW DOUBLER, AND APPLIED COMPOSITIE REPAIR IAW DC8 SRM 51-1-9A, TREATED DOUBLER IAW LWR 200302015 AND PRIMED IAW DC8 SRM 51-1-8.SDR ABXA050314Attach Angle · crackedFORWARD CARGO BAY DENT ON GILLINER ATTACH ANGLE, STA. 160, BETWEEN LONGERON 36 LEFT TO 35 LEFT. REMOVED DENT IN FORWARD CARGO BAY GILLINER ATTACH ANGLE STA 160, LONGERON 36 LEFT - 35 LEFT, FOUND TO BE CRACKED, REPAIRED. REMOVED GILLINER ATTACH ANGLE IAW DC8 SDR ABXA050312Frame · tool damageFORWARD CARGO BAY DRILL START IN FRAME RADIUS, STA 120, ABOVE LONGERON 31 RIGHT, RIGHT BUTT LINE 33. ORIGINAL MATERIAL 7075-T6 0.090" PER DC8 SRM 53-4-1, PG 125. FABRICATED REPAIR ANGLE FROM 7075-0 FIG 2, HEAT TREATED IAW DC8 SRM 51-1-4, SHIM FROM 7075-T6 0.SDR ABXA060018Fitting · crackedAFT CARGO, RT SIDE, STA. 1580 HAD CRACKED FITTING, RBL 58, LONGERON 21 RT. REMOVED AND REPLACED CRACKED FITTING AT STA. 1580, RBL 58 IAW SRM 51-1-21 AND 51-3-1.SDR ABXA050335Floorbeam · corrodedMAIN DECK AFT ACCESSORY COMPARTMENT, STA 1660, LEFT BUTT LINE 44, LONGERON 22 LEFT, FLOORBEAM HAD CORROSION. CLEANED UP SURFACE CORROSION WITH NEGLIGIBLE MATERIAL LOSS EXCEPT FOR AROUND ONE FASTENER HOLE. REPAIRED CORROSION DAMAGE IAW DC8 SRM 51-1-8, PG 20, SDR ABXA060017Angle · corrodedCORROSION LOWER ANGLE ON PRESSURE WEB ON FWD BULKHEAD STA. 857, FORWARD OF RT. WHEEL WELL, APPROXIMATELY LONGERON 24. WING TO BODY ANGLE AT STA. 857 CORRODED BEYOND LIMITS. ANGLE REMOVED FROM LBL13 - RBL 57.5 AND NEW SECTION INSTALLED IAW SRM 51-1-20.SDR ABXA050364Angle · corrodedFOUND CORNER ANGLE ON PRESSURE WEB CORRODED ON FORWARD BULKHEAD IN RIGHT WHEEL WELL, STA 857, RIGHT BUTT LINE 48. NEW CORNER ANGLE FABRICATED IAW REA D853-52555. ANGLE INSTALLED IAW DC8 SRM 51-1-20 AT STA 857, RIGHT BUTT LINE 48.SDR ABXA050348Skin · damagedLOWER FUSELAGE SKIN, STA 400, LONGERON 31 RIGHT, FASTENER HEADS SHEARED. REMOVED DAMAGED FASTENERS, NOTED CORROSION ON INTERNAL FINGER DOUBLER AT STA 440 LONGERON 31 RIGHT. REPAIRED FINGER DOUBLER IAW REA D853-52523. ELONGATED AND OVER-SIZED HOLES AT STA 44SDR ABXA050349Fitting · crackedUPPER FORWARD MOST SUPPORT ANGLE WAS CRACKED IN 2 PLACES ON TOP OF L-24 FITTING IN RIGHT WHEEL WELL. REMOVED AND REPLACED CRACKED FITTING TOP OF L-24 RIGHT WHEEL WELL STA 880, P/N: 5750198-502 IAW DC8 SRM 51-1-20D.SDR ABXA050350Fitting · corrodedFOUND STA 900, L-24, CORROSION ON FORWARD SECTION AND AFT OF FITTING AT ATTACH POINT TO L-24. REMOVED AND REPLACED FITTING WITH NEW PART IAW DC8 SRM 51-10-1. POSITIONED, DRILLED UP HOLES, REAMED AND INSTALLED FITTING AT STA 879 (900) L-24 IN LEFT WHEEL WELL SDR ABXA060015Cusp Web · corrodedCORROSION ON CUSP LINE EXTRUSION, STA. 1020 TO STA. 114O, LONGERON 21 RT. CORRODED BEYOND LIMITS. REMOVED AND REPLACED CUSP EXTRUSION IAW SRM 53-2-5, FIG. 15 AND 15A.SDR ABXA060016Floorbeam · corrodedCORROSION RUNNING THE ENTIRE FLOORBEAM, FORMER AND FASTENERS AT STA. 1640, LONGERON 22 RT, UNDERSIDE AFT. CORRODED BEYOND LIMITS AT RBL 53-60. REMOVED END CAP AND DOUBLER L/S. REMOVED CORROSION IAW SRM 53-2-0, PG 2P, FIG 1F AND INSTALLED END CAPS AND DOUBLER. SDR ABXA050347Support Fitting · crackedSUPPORT FITTING WAS CRACKED ON LONGERON 24 RIGHT IN RIGHT MAIN LANDING GEAR WHEEL WELL AT APPROXIMATELY STA 940. REMOVED SUPPORT FITTING BRACKET ON LONGERON 24 STA 940 RIGHT MAIN LANDING GEAR, NEW BRACKET FABRICATED BY OUTSIDE VENDOR, REF REA D853-52521, PO NSDR ABXA050363Keelbeam · corrodedCORROSION FOUND ON SURFACE OF KEEL BEAM IN MID CARGO BAY BILGE AREA, STA 610 TO 710 APPROXIMATELY BUTT LINE 0. MULTIPLE BLENDED AREAS ON BOTH HORIZONTAL LEGS RANGING FROM 0.010" MIN TO MAX BLEND DEPTH OF 0.141". REMOVED CORROSION ON UPPER SURFACE OF KEEL BEASDR ABXA050154Longeron · corrodedCORROSION DISCOVERED ALONG LONGERON 24 RIGHT, BEHIND THE INBOARD SPLICE FITTING AT STA 980 IN THE RIGHT WHEEL WELL. REMOVED CORROSION FROM THE LONGERON AND FITTING BY BLENDING. ALL REWORKED AREAS ARE WITHIN SRM LIMITS.SDR ABXA050037Wire · brokenRIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE WITH GEAR DOWN - RED GEAR UNSAFE LIGHT NOT ON - HORN DID NOT SOUND. RECYCLED NO HELP. FOUND WIRES G321E24 AND G324N24 BROKEN INSIDE THE CONDUIT BETWEEN P1-1398 AND S3-4. REPLACED BOTH WIRES AND WIRE G32SDR ABXA050036Connector · damagedRIGHT MAIN LANDING GEAR GREEN LIGHT WOULD NOT COME ON WHEN THE GEAR WAS EXTENDED. CYCLED THE GEAR TWICE AND THE LIGHT STARTED WORKING. FOUND CORROSION ON P1-1398 AND S1-210. REMOVED AND REPLACED CONNECTOR P1-1398 AND RIGHT LANDING GEAR DOWN SWITCH S1-120. SDR ABXA040234Arm · looseDURING DESCENT THRU 10,000, AIRCRAFT BEGAN A ROLL TO LEFT, AUTOPILOT DISCONNECTED AND AIRCRAFT CONTINUED TO ROLL UNTIL RIGHT AILERON WAS APPLIED. DURING ROLL EVENT, AIRCRAFT HAD A MILD SHAKING. MAINTENANCE FOUND LATERAL CONTROL SPOILER POWER CONTROL VALVE ARSDR ABXA040199Battery · inoperativeDURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE EMERGENCY LIGHTS BATTERY PACK ASSEMBLY IAW DC8 MM 33-50-01.SDR ABXA040124Skin · corrodedAFT ACCESSORY INNER SKIN AT LONGERON 27 RIGHT, LONGERON 26 RIGHT, STA 1660 - 1680 WAS CORRODED. REPAIRED AREA IAW REA D853-4866MR.SDR ABXA040129Skin · corrodedMAIN CABIN CENTER WING BOX HAD CORROSION AT LEFT BUTT LINE 8, STA 850. REPAIRED AREA IAW REA D857-48869MR.SDR ABXA040119Longeron · crackedLONGERON 24 LEFT CRACKED, LOWER INNER FLANGE OF BOTTLE BOLT CAVITY. REPAIRED LONGERON 23 LEFT IAW DC-8 SRM 53-2-2 AND REA D853-48861MR.SDR ABXA040118Keelbeam · corrodedMID SHIP ACCESSORY COMPARTMENT, FS 640 - 660, L-36 KEEL BEEM EXTENSION CORRODED. REMOVED CORROSION IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR DOUBLER IAW ABX REA D853-48863MR, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8.SDR ABXA040125Frame · corrodedAFT LOWER CARGO STA 1140, ABOVE LONGERON 35 RIGHT, RIVNUT INSTALLED THROUGH PORTION OF FASTENER HEAD. REPAIRED AREA IAW REA D853-48864MR.SDR ABXA040126Fastener · wrong partATTACH ANGLE TO FLOOR SUPPORT CENTER WING BOX, RIGHT SIDE 857, ANGLE HAD IMPROPER FASTENER INSTALLED. REPAIRED AREA IAW REA D857-48854MR.SDR ABXA040128Fitting · crackedLONGERON 24 LEFT, STA 980, UPPER LIP CRACKED. REPAIRED AREA IAW REA D853-48872MR.SDR ABXA040123Spar Cap · crackedTOP SIDE OF CENTER WING BOX, STA 857, LEFT BUTT LINE 24, UPPER SPAR CAP HAD A 3 INCH CRACK. REPAIRED AREA IAW DC-8 SRM 51-1-24, 51-1-20D AND 31-3-1.SDR ABXA040122Web · corrodedMAIN CABIN FS 280 AND RIGHT CUSP HAD CORROSION. REPAIRED AREA IAW REA D853-48860MR.SDR ABXA040121Pressure Panel · corrodedRIGHT WHEEL WELL, CORROSION ON SPOILER CABLE BRACKET FOOT END AROUND ATTACH BOLTS, JUST ABOVE LONGERON 24, FS 920. REPAIRED AREA IAW DC-8 REA D853-48868MR.SDR ABXA040120Fitting · corrodedAIR CONDITION ACCESSORY COMPARTMENT AT STA 70, LONGERON 34 RIGHT TO LONGERON 35 RIGHT, BULKHEAD ATTACH FITTING CORRODED. REPAIRED CHORD AND LONGERON FITTING IAW DC-8 SRM 51-1-24, 53-2-5 AND 51-1-8.SDR ABXA040130Floorbeam · corrodedRIGHT PRESSURE DECK MAIN CABIN LOWER SIDE OF FLOORBEAMS AT STA 920 AND 940 ARE EXFOLIATED. REPAIRED AREA IAW REA D853-48871MR AND REA D853-48873MR.SDR ABXA040127Attach Angle · corrodedATTACH ANGLE TO UPPER PRESSURE DECK FLOOR FROM STA 960 - 980, 100 INCHES FROM RIGHT CUSP, HAD CORROSION. REPAIRED AREA IAW REA D853-48865MR.SDR ABXA030438Latch · wornRED GEAR UNSAFE LIGHT AND LEFT GEAR DOOR NOT LATCHED LIGHT CAME ON. BOTH LIGHTS WENT OUT AFTER PERFORMING ALTERNATE UPLATCH CHECK ABNORMAL, THRU FLAP EXTENSION. GEAR CYCLED. CHECKED GEAR DOOR LATCH MECHANISM, CHECKED TARGET, CLEANED AND LUBED SWITCH AND CYCSDR ABXA030138Lock · brokenAFTER PRE-DEPARTURE CHECK WAS COMPLETED. CREW WAS UNABLE TO OPEN COCKPIT DOOR. FOUND DOOR LOCK PLUNGER BROKEN IN LOCKED POSITION. INSTALLED SLIDE LOCK ON FLIGHT COMPARTMENT SIDE OF COCKPIT DOOR. VERIFIED THAT LOCK WAS OPERABLE FROM INSIDE THE COCKPIT. REPLACEDSDR ABXA020150Bracket · defectiveHOT CUP CAUSED A BURNING ODOR AND SMOKE FROM PRONGS ON THE HOT CUP. REPLACED HOT CUP AND BRACKET ASSEMBLY. OPS CHECKED GOOD IAW DC-8 MM.SDR ABXA020221Floorbeam · bentAFT CARGO, STATION 1320, RIGHT BUTT LINE 33, FLOORBEAM WAS BENT. REPAIRED AREA IAW ABX REA D853-43921MR AND DC-8 SRM 51-1-8.SDR ABXA020099Skin · damagedL1 DOOR FORWARD LOWER AND AFT CORNER REPAIRS. REPAIRED AREA IAW ABX REA D853-43922-MR, DC-8 SRM 53-2-0, 51-1-20D, 51-1-21, AND 51-3-0.SDR ABXA020100Beam · corrodedMAIN CABIN STATION 940, RIGHT BUTT LINE 68, CORROSION UNDER BEAM AND SHEAR WEB PANEL, LOWER SIDE CORNER. REPAIRED AREA IAW REA D853-43931-MR.SDR ABXA020098Fitting · corrodedRIGHT WING STATION 219, FLAP LINK SUPPORT (CANOE) WAS CORRODED AND PITTED UNDER AFT TRACK PLATES. REMOVED CORROSION FROM FLAP LINK SUPPORT FITTING AND FABRICATED REPAIR FILLERS IAW DC-8 SERVICE BULLETIN 27-164. REMOVED CORROSION FROM LEFT AND RIGHT SIDE SUPPSDR ABXA020097Web · corrodedMAIN CABIN STATION 960, CORROSION UNDER BEAM AND SHEAR WEB BY LEFT BUTT LINE 68. REPAIRED AREA IAW ABX REA D853-43930-MR.
Back to N826AX, cancelled Nov 21, 2007