N812AX, cancelled Jun 16, 2008
Service difficulty reports · 85
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 = 'N812AX' AND deregistration_id = 'N812AX-2008-06-16' 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 = 'N812AX' AND deregistration_id = 'N812AX-2008-06-16' 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 ABXA070265Hinge Pin · shearedDURING MAINTENANCE ON WO 600267980, UPPER FORWARD CARGO DOOR FORWARD HINGE PIN WAS SHEARED. REMOVED AND REPLACED FORWARD HINGE PIN IAW DC8 AMM 20-10-0.SDR ABXA060222Spar · corrodedLEFT WING REAR SPAR AFT FACE HAD CORROSION AT WING ROOT XRS 5. ACCOMPLISHED REPAIR IAW REA D857-53586-MR, REV. IR AT LEFT WING REAR SPAR.SDR ABXA060221Skin · damagedRIGHT ELEVATOR LOWER SKIN AT XS 77.0, HAD "OIL CAN" CONDITION AT HINGE NR 2 SMALL ACCESS HOLE. ACCOMPLISHED REPAIR IAW REA D855-53583-MR, REV. IR AT RIGHT ELEVATOR.SDR ABXA060220Skin · damagedUPPER CARGO MAIN CARGO DOOR FUSELAGE CUT OUT PLATING DAMAGE, SEVERAL AREAS MISSING STA. 160 - 180, LONGERON 6 LEFT. ACCOMPLISHED REPAIR AT DOOR CUT OUT IAW REA D853-53588-MR, REV. IR.SDR ABXA060219Skin · corrodedLEFT INBOARD HORIZONTAL STABILIZER LEADING EDGE SECTION OUTBOARD UPPER SURFACE AT XSTA 177, HAD INTERGRANULAR CORROSION AT SCREW HOLE AREA. INSTALLED REPAIR AT LEFT INBOARD STABILIZER LEADING EDGE SECTION OUTBOARD UPPER SURFACE IAW REA D855-53575-MR, REV. B.SDR ABXA060217Skin · crackedCRACK IN RIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN 8" FROM INBOARD EDGE, STA. XFS 304. STOP DRILLED CRACK AND INSTALLED REPAIR IAW REA D857-53580, REV. IR.SDR ABXA060218Skin · crackedRIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN HAD 3 EACH CRACKS AT APPROX. XFS 410 - 423. REPAIRED CRACKS IAW REA D857-53581, REV. IR.SDR ABXA060195Skin · crackedRIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN HAD 3 EACH CRACKS AT XFS 410 - 423. REPAIRED CRACKS IAW REA D857-53581, REV IR.SDR ABXA060194Skin · crackedCRACK IN RIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN 8 INCHES FROM INBOARD EDGE STA XFS 304. STOP DRILLED CRACK AND INSTALLED REPAIR IAW REA D857-53580, REV IR.SDR ABXA060216Longeron · corrodedEXFOLIATION CORROSION IN LONGERON 27 LEFT, STA. 1220 - 1240. ACCOMPLISHED REPAIR IAW REA D853-53585-MR, REV. IR, ON LONGERON 27 LEFT, STA. 1220 - 1240.SDR ABXA060215Skin · corrodedLEFT HORIZONTAL STABILIZER OUTBOARD LEADING EDGE UPPER STRUCTURE HAD INTERGRANULAR CORROSION ON AFT TRAILING EDGE FROM XFS 178 - 341. ACCOMPLISHED REPAIR OF LEFT HORIZONTAL STABILIZER LEADING EDGE IAW REA D855-53574-MR, REV. A.SDR ABXA060213Panel · corrodedRIGHT HORIZONATL STABILIZER LEADING EDGE OUTBOARD SECTION UPPER TRAILING EDGE INTERGRANULAR CORROSION AT 3 LOCATIONS: XFS260, 316 & 332. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW REA D855-53089-MR, REV. B.SDR ABXA060214Skin · crackedTHREE CRACKS ALONG THE UPPER EDGE OF CUT OUT, IN THE INNER SKIN OF THE AFT CARGO DOOR. TRIMMED OUT CRACKS IAW REA D852-53568.SDR ABXA060211Skin · corrodedRIGHT HORIZONTAL STABILIZER INBOARD LEADING EDGE SECTION AT UPPER TRAILING EDGE MID AREA AT XSTA 140, HAD INTERGRANULAR CORROSION AROUND SCREW HOLES. INSTALLED REPAIR IAW REA D855-53086-MR, REV. A, ON RIGHT HORIZONTAL STABILIZER INBOARD LEADING EDGE SECTION ATSDR ABXA060212Panel · corrodedRIGHT HORIZONTAL STABILIZER OUTBOARD LEADING EDGE SECTION AT INBOARD UPPER LEADING EDGE HAD INTERGRANULAR CORROSION AT HILOC HOLE. INSTALLED REPAIR IAW REA D855-53090-MR, REV. IR AT RIGHT STABILIZER LEADING EDGE AT XSTA 178.75.SDR ABXA060192Skin · corrodedRIGHT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD SECTION UPPER TRAILING EDGE HAD INTERGRANULAR CORROSION AT 3 LOCATIONS: XFS 260, 316 AND 332. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW REA D855-53089-MR, REV B.SDR ABXA060193Skin · crackedTHREE CRACKS ALONG THE UPPER EDGE OF CUTOUT, IN THE INNER SKIN OF THE AFT CARGO DOOR. TRIMMED OUT CRACKED IAW REA D852-53568.SDR ABXA060191Skin · corrodedRIGHT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD UPPER SKIN HAD INTERGRANULAR CORROSION AT XFS 178.750. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW REA D855-53088-MR, REV A.SDR ABXA060207Skin Panel · corrodedPERMANENT REPAIR OF CORROSION ON LONGERON L36 (KEEL BEAM) PER COI 50571 AND SKIN PANELS AT STA. 670 AND 683 PER COI 50570 AND COI 50572. REPAIR ACCOMPLISHED IAW REA D853-53093 - MR, REV. A, ON KEEL BEAM AND SKIN PANELS AT STA. 665 - 700.SDR ABXA060208Longeron · damagedREMOVE AND REPLACE EXISTING DISCREPANT LONGERON 24 RIGHT IN RIGHT WHEEL WELL, STA. 857 - 980, DUE TO PREVIOUS DAMAGE WITH AN INTERIM REPAIR IAW REA D853-52752-MR. REMOVED AND REPLACED LONGERON 24 RIGHT IN RIGHT WHEEL WELL IAW REA D853-53079-MR, REV. A.SDR ABXA060209Skin · corrodedLEFT WING LEADING EDGE UPPER AFT EDGE OF OUTER MOST LEADING EDGE ASSEMBLY AT XFS 291 - 422 LEFT, HAD EXFOLIATION AROUND SCREWS. ACCOMPLISHED REPAIR IAW REA D857-53573-MR, REV. A, AT LEFT WING OUTER MOST LEADING EDGE ASSEMBLY.SDR ABXA060206Longeron · corrodedFORWARD CARGO COMPARTMENT LNOGERON 31 LEFT HAD CORROSION AT STA. 520. ACCOMPLISHED REPAIR IAW REA D853-53595-MR, REV. IR, ON LONGERON 31 LEFT.SDR ABXA060205Longeron · corrodedCORROSION AT LONGERON 31 LEFT, F.S. 560 - 600. ACCOMPLISHED REPAIR OF LONGERON 31 LEFT, F.S. 560 - 600 IAW REA D853-53592-MR, REV. IR.SDR ABXA060210Skin · corrodedRIGHT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD UPPER SKIN HAD INTERGRANULAR CORROSION AT XFS 178.750. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW REA D855-53088-MR, REV. A.SDR ABXA060204Longeron · corrodedSEVERAL AREAS OF CORROSION ON LONGERON 24 LEFT, F.S. 857 - 980 IN LEFT WHEEL WELL. REPLACED LONGERON 24 LEFT, F.S. 857 - 980 IN LEFT WHEEL WELL IAW REA D853-53080-MR, REV.A.SDR ABXA060203Skin · corrodedRIGHT FUSELAGE SKIN HAD BULGE AND RIVETS POPPED OFF AT STA. 1600, LONGERON 27 RIGHT. EXISTING REPAIR REMOVED AND SKIN AND INNER DOUBLER CUT TO REMOVE ALL CORROSION. COMPLETED REPAIR IAW REA D853-53635-MR.SDR ABXA060190Skin · corrodedRIGHT FUSELAGE SKIN HAD BULGE AND RIVETS POPPED OFF AT STA 1600, LONGERON 27 RIGHT. EXISTING REPAIR REMOVED, AND SKIN AND INNER DOUBLER CUT TO REMOVE ALL CORROSION. COMPLETED REPAIR IAW REA D853-53635-MR.SDR ABXA060081Fuel Control · defectiveNR 3 ENGINE FAILED TO ACCELERATE IN-FLIGHT. EET 20 DEGREES N2 48%, FF AT 1000 LBS. ATTEMPTED RE-LIGHT TO NO AVAIL. SHUT DOWN NR 3 ENGINE AT 0518Z, 4 PSI INDICATED ON OIL PRESSURE. REMOVED AND REPLACED FUEL CONTROL UNIT ON NR 3 ENGINE AND TRIMMED NR 3 ENGINSDR ABXA060056Fitting · crackedFITTING AT LONGERON 24, FS 879, CRACKED. REPAIRED FITTING IAW REA D853-53104.SDR ABXA050293Longeron · corrodedCORROSION FOUND ON LONGERON 24 RIGHT AT STATION 879. REA D853-52752MR PERFORMS AN INTERIM REPAIR TO THE LONGERON.SDR ABXA050292Skin · corrodedCORROSION FOUND ON THE WING TO FUSELAGE SKIN AT STATION 670 AND LONGERON 36. REA D853-52756MR PERFORMS AN INTERIM REPAIR SIMILAR TO SRM 53-2-1, FIG. 7, AS OPERATIONAL SCHEDULING DID NOT ALLOW FOR A PERMANENT REPAIR.SDR ABXA050289Window · lack of lubeCAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. LUBRICATED CAPTAIN'S CLEARVIEW WINDOW ASSEMBLY IAW DC-8 MM 56-00-00. OPS CHECKED GOOD.SDR ABXA050094Skin · corrodedFUSELAGE SKIN COMMON TO THE FACTORY ANTENNA DOUBLER, CORRODED. FABRICATED SKIN AND DOUBLER FOR ANTENNA AND INSTALLED IAW REA D853-51782 ON WO NR 600221026.SDR ABXA040352Lamp · inoperativeEMERGENCY EXIT LIGHTS ARMED AMBER LIGHT INOPERTATIVE. RELAMPED, OPS CHECKED GOOD IAW DC-8 MM 33-50-02.SDR ABXA040299Fitting · crackedINTERCOSTAL END FITTING AT STA 1140, LONGERON 35 LEFT WAS CRACKED. REPLACED END FITTING IAW DC-9 SRM 51-1-20D.SDR ABXA040300Fitting · crackedINTERCOSTAL END FITTING AT STA 1160, LONGERON 35 RIGHT WAS CRACKED. END FITTING WAS REPLACED IAW DC-8 SRM 51-1-20D.SDR ABXA040301Skin · corrodedAFT FUSELAGE SKIN FORWARD OF NR 3 CARGO DOOR HAD BULGED REPAIR. REPAIRED AREA IAW REA D853-50277MR.SDR ABXA040264Longeron · crackedLT MAIN LANDING GEAR WHEEL WELL LONGERON 24 CRACKED ON LOWER FLANGE AT BOTTLE BOLT CAVITY. REPAIRED AREA IAW REA D853-49163MR.SDR ABXA040263Fitting · crackedFITTING CRACKED AT MOST FORWARD FASTENER HOLES. FABRICATED REPAIR PARTS IAW REA D853-49975MR. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED IAW SRM 51-1-20B.SDR ABXA040111Fuel Control · defectiveNR 4 ENGINE, AFTER SETTING POWER FOR CRUISE, NR 4 ENGINE ROLLED BACK .15 EPR. EGT, FUEL FLOW N1 AND N2 ALL DROPPED. THROTTLE DID NOT MOVE. REPLACED NR 4 ENGINE FUEL CONTROL UNIT IAW 73-20-01. REPLACED NR 4 LOW PRESSURE FUEL FILTER. PERFORMED LEAK CHECK OFSDR ABXA040110Bleed Valve · defectiveAFTER TAKEOFF 2000 FEET, HEARD SHARP LOUD BANG/POP. NR 2 EPR DROPPED .18 AND BACK. FELT SLIGHT LEFT YAW. REPLACED NR 2 ENGINE COMPRESSOR BLEED VALVE AND CONTROL IAW 75-30-03-2-0002. NR 2 ENGINE LOW PRESSURE BLEED VALVE CHECKED GOOD IAW DC8 AMM 71-00-00. RSDR ABXA030029Link · brokenDURING SERVICE CHECK, FOUND THE NR 5 INBOARD GROUND SPOILER WITH 2 EACH CENTER CRANK ASSEMBLIES AND INBOARD SPOILER OVERCENTER LINK BROKEN. REMOVED THE LEFT WING NR 5 SPOILER PANEL AND REPLACED BOTH SPOILER CRANK ASSEMBLIES IAW AMM. OPS CHECKED GOOD. INSTALLEDSDR ABXA020272Frame · crackedMAIN CABIN FRAME AT STA 240 RIGHT SIDE WAS CRACKED AT FLOOR LEVEL. INSTALLED DOUBLER REPAIR AT STA 240 MAIN CABIN RIGHT SIDE IAW DRAWING K04888 AND DC-8 SRM.SDR ABXA020271Frame · crackedMAIN CABIN FRAME AT STA 220 RIGHT SIDE WAS CRACKED AT FLOOR LEVEL. INSTALLED DOUBLER REPAIR AT STA 220 RIGHT AT FLOOR LEVEL IAW DRAWING K04888 AND DC-8 SRM.SDR ABXA020267Skin · crackedFUSELAGE RIGHT AFT DOOR X-RAY SHOWED CRACK AT AFT UPPER CORNER OF DOOR CUTOUT. INSTALLED REPAIR DOUBLER AT RIGHT AFT DOOR UPPER CORNER IAW DC-8 DRAWING SRO 8530024 AND DC-8 SRM 53-2-0.SDR ABXA020273Skin · crackedA/C EXHAUST DUCT SKIN WAS CRACKED AT THE FORWARD UPPER CORNER AT FS 50, STRINGER 28 LEFT. CUT OUT DAMAGE AND INSTALLED REPAIR IAW DRAWING SR08530020 AND DC-8 SRM.SDR ABXA020290Floorbeam · corrodedCORROSION FOUND ON NOSE LANDING GEAR WELL HORIZONTAL PRESSURE PANEL, BETWEEN FS 12 TO FS 27. ALSO FOUND CORROSION ON FLOORBEAM LOWER FLANGE AT FS 12, BUTT LINE '0'. REPAIRED AREA IAW REA 853-41975MR.SDR ABXA020270Door Frame · crackedCRACK AT FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW DC-8 SRM 53-2-0.SDR ABXA020269Door Frame · damagedEXISTING REPAIR AT PASSENGER DOOR FORWARD UPPER CORNER DID NOT CONFORM TO DRAWING ES00863. REMOVED AND REPLACED REPAIR IAW DC-8 SRM 53-2-0.SDR ABXA020268Longeron · crackedFUSELAGE LONGERON 11 RIGHT HAD A 1 INCH CRACK AT FS 1660. REPAIRED LONGERON 11 IAW REA D853-41973MR.
Back to N812AX, cancelled Jun 16, 2008