N612AW, cancelled Jan 31, 2008
Service difficulty reports · 82
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 = 'N612AW' AND deregistration_id = 'N612AW-2008-01-31' 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 = 'N612AW' AND deregistration_id = 'N612AW-2008-01-31' 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 A6WA200460054Oxygen Mask · missingROWS 14 AND 16 DEF HAVE NR O2 MASKS INSTALLED IN PSU BOXES. MAINTENANCE INSTALLED PASSENGER ALL O2 MASKS AS REQUIRED IAW 35-20-45.SDR A6WA200460033Line · rupturedFOUND RIGHT MLG FAILED TO RETRACT AFTER TAKEOFF, REV UNSAFE LIGHT ILLUMINATED, CYCLED MLG DOWN, RETUREND TO RDU FOR FERRY FLIGHT BACK TO ATW. INSPECTED AND FOUND RT MLG FLEX LINE FOR RETRACTOR BRAKES RUPTURED WITH HYDRAULIC FUSE BLOWN, REPLACED LINE. RESET HSDR A6WA200460023Skin · damagedFOUND LEFT INBOARD LEADING EDGE HAS WEAR DAMAGE OT THE INBOARD LEADING EDGE WHERE THE STALL BAR ATTACHES. MAINTENANCE REQUESTED REPAIRS FROM BAE SYSTEMS REF AVMAX FAX 612-190-006. (M)SDR A6WA200460024Skin · gougedFOUND RIGHT HORIZONTAL STABILIZER TOP SKIN SMALL GOUGE IN THE UPPER SKIN OF THE RIGHT HORIZONTAL STABILIZER BETWEEN RIBS 9 AND 10. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 612-1909007. (M)SDR A6WA200360027Panel · chafedCHAFE DAMAGE TO LEFT STABILIZER PANEL 275CL. MAINTENANCE BLENDED AND POLISHED DAMAGE AREA IAW BAE FAX BARA/AVR/3037/03-DC. (M)SDR A6WA200260043Tab · dentedDENTS TO RT ELEVATOR AND TABS X 34 RECEIVED CONCESSION.SDR A6WA200260042Tab · dentedDENTS TO LEFT ELEVATOR AND TABS X 8 RECEIVED CONCESSION.SDR A6WA200260041Structure · dentedRIGHT FLAP INBOARD AND OUTBOARD TABS DENTED, RECEIVED CONCESSION.SDR A6WA200260040Skin · dentedDENTS RIGHT FUSELAGE X 4 RECEIVED CONCESSION.SDR A6WA200260039Door · dentedDENTS RT MAIN LANDING GEAR X 26 RECEIVED CONCESSION.SDR A6WA200260038Door · dentedDENTS LEFT MAIN LANDING GEAR DOOR X 18 RECEIVED CONCESSION.SDR A6WA200260037Tab · dentedDENT LEFT FLAP INBOARD TAB X RECEIVED CONCESSION.SDR A6WA200260036Tab · dentedDENTS RIGHT AILERON INBOARD AND OUTBOARD TABS X 32 RECEIVED CONCESSION.SDR A6WA200260035Tab · dentedDENTS LEFT AILERON TABS X 9 RECEIVED CONCESSION.SDR A6WA200100047Control Box · failedNR 1 ENGINE FAILED IN FLIGHT, NO LEAKS NOTED OR DAMAGE NOTED. MAINTENANCE REMOVED AND REPLACED THE HIGH AND LOW PRESSURE FUEL FILTERS, FUEL CONTROL AND PRIMARY OVERSPEED CONTROL BOX.SDR A6WA200100039O-Ring · failedLOST ALL GREEN HYDRAULIC QUANTITY ON GEAR EXTENSION. MAINTENANCE REMOVED AND REPLACED O-RING ON PTU PLUG.SDR A6WA200100016A/C Pack · failedAT 20,000 FEET NR 1 PACK VALVE LIGHT CAME ON, FLIGHT CREW TRIED TO RESET COULD NOT. THE RECIRCULATION VALVE WENT FREST COULD NOT RESET. NR 2 PACK VALVE LIGHT CAME ON, LOST PRESSURE. RESTORED CABIN PRESSURE AT 10,000 FEET PACK WORKED. MAINTENANCE PRESSURIZESDR A6WA200000064Service difficultySTRONG OIL SMELL IN CABIN WHEN APU AIR INTRODUCED INTO SYSTEM OK ON ENGINE AIR. MAINTENANCE PERFORMED CONTAMINATED DUCT CLEANING PROCEDURE. APU VACUUM TEST GOOD.SDR A6WA0000011Engine · failedFLT 5510 - ORD-ATW - NR 1 ENGINE FAILED ON TAKEOFF OUT OF ORD. REMOVED AND REPLACED NR 1 ENGINE. (M)SDR 99ZZZM426Skin · wornNR 2 ENGINE LEFT AFT AFT COWL DOOR INNER SKIN WORN THROUGH. PATCHED ABOVE DAMAGE PER PSI USING TA2 AND CHERRYMAXNUETS.SDR 99ZZZM432Door · lack of lubeCOCKPIT DOOR DIFFICULT TO OPEN FROM CABIN SIDE. LUBED AND RESHIMMED DOOR, OPS CHECK OK. (M)SDR 99ZZZM544Control Cable · corrodedLEFT MAIN AILERON CONTROL CABLES ARE CORRODED AT PULLEY BETWEEN FUSELAGE FRAME NR 24 AND 25. REMOVED AND REPLACED LEFT MAIN AILERON CENTER CONTROL CABLES, TENSIONED AND SAFETIED. (M)SDR 99ZZZM427Valve · failedCABIN OXYGEN MASKS AT RIGHT SIDE ROW 2 DEF VALVE PISTON FAIL TEST. REMOVED AND REPLACED VALVE AT SEAT 2 DEF, OPS CHECK GOOD. (M)SDR 98ZZZM937String · misinstalledOXYGEN CABIN DROP DOORS FOR MASKS AT POS RIGHT 7 DEF, RT 8 DEF, RT 12 DEF AND LT 5 ABC STRING HINGES ARE NOT LONG ENOUGH FOR DOOR TO SWING OPEN FULLY. ADJUSTED AND CHANGED STRINGS AT RT SIDE 7 DEF, 8 DEF, 12 DEF AND LT 5 ABC. ALL DOORS SWING FREE. OK FOR SESDR 98ZZZM908Laynard · wornOXYGEN MASK AT 20 RT REBREATHER FEL HAS HOLES AND PIN STRING FRAYED, 11 LT. REBREATHER FELT HAS HOLES. REPLACED FELTS RT 20, 11 LT. REPLACED LANYARD 20 RT. CHECKS OK. (M)SDR 99ZZZM547Strip · crackedNR 4 ENGINE FORWARD OUTBOARD COWL DOORIS CRACKED AT INNER DOOR MIDDLE CAPPING. STRIP NEAR DRAIN LINE CLAMP. REPAIRED CAPPING STRIP PER BAE SRM 51-71-11 AND 12. (M)SDR 99ZZZM546Door · crackedNR 4 ENGINE INBOARD FAN DOOR, 3RD DOOR RIB, CRACKED AT LOWER CORNER AREA NEAR VENT TUBE. REPAIRED CRACK BY PATCHING IAW BAE AIR/WISC SRM STD PRACTICES AND FOUND SERVICABLE. (M)SDR 99ZZZM545Door · crackedNR 4 ENGINE INBOARD FAN DOOR, FORWARD INNER TITANIUM FIRESHIELD CRACKED AT CORNERS. REPAIRED CRACK BY PATCHING IAW BAE/AIR WISC SRM STD PRACTICES AND FOUND SERVICEABLE. (M)SDR 99ZZZM537Stiffener · crackedRIGHT WING TE SHROUD LOWER SKIN STIFFENER CRACKED INBOARD OF RIB 10. REMOVED AND REPLACED LOWER SKIN STIFFENER PER SRM. (M)SDR 98ZZZX3992Angle · missingATW - FORWARD CARGO BAY: CENTER FORWARD CARGO FLOOR SUPPORT ANGLE AT FRAME 19D, SECTION MISSING. REPLACED FORWARD CARGO BAY CENTER FLOOR SUPPORT ANGLE AT FRAME 19D.SDR 98ZZZX3954Rib · crackedATW - NR 1 (BOTTOM) RIB ON RUDDER IS CRACKED WITH A SMALL PIECE BROKEN OUT. REPLACED RIB PER REPAIR INSTRUCTIONS HC554H9005.SDR 98ZZZX3956Skin · damagedATW - RIGHT MLG DOOR FORWARD LOWER CORNER DAMAGE DUE REPAIR IN 2,000 FLIGHTS PER AVRO FAX JM/0642-97. SEE SRM FOR SKIN REPAIR CRITERIA CURRENT TCA 25066 DUE REPAIR BY 27566 TCA. SEE FAX JM/RJ0317-98 FOR 500 FLIGHT EXTENSION TO 27566 TCA. REPAIRED FORWARD LOSDR 99ZZZM543Stiffener · crackedLT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END, INBOARD OF RIB NR 10. REPLACED LEFT TE WING SHROUD TOP SKIN STIFFENER INBOARD OF NR 10 RIB AT THIS TIME. (M)SDR 99ZZZM542Stiffener · crackedLT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END, OUTBOARD OF RIB NR 8. REPLACED LEFT WING TE SHROUD TOP SKIN STIFFENER OUTBOARD OF RIB NR 8.SDR 99ZZZM540Stiffener · crackedLEFT WING TE SHROUD LOWER SKIN STIFFENERS, TWO HAVE TAG ANGLE CRACKED AT AFT END, BETWEEN RIBS 8/9. REPLACED TWO ANGLES ON TE SHROUD LOWER SKIN STIFFENERS BETWEEN RIBS 8/9 AT THIS TIME.SDR 99ZZZM538Stiffener · crackedLEFT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END INBOARD OF RIB NR 6. REPLACED TOP SKIN STIFFENER BETWEEN RIBS 5 AND 6 JUST INBOARD OF RIB 6 AT THIS TIME. (M)SDR 99ZZZM433Angle · crackedRIGHT WING TE TOP SKIN STIFFENER AFT TAG ANGLE CRACKED AT LOWER FLANGE BETWEEN RIBS 5 AND 6 OF SHROUD. REMOVED AND REPLACED AFT TAG ANGLE BETWEEN RIBS 5/6 FOR THE TOP SKIN STIFFENER. (M)SDR 99ZZZM541Stiffener · crackedLT WING TE SHROUD TOP SKIN STIFFENER CRACK AT FORWARD END (BETWEEN RIBS 7/8). REPLACED LEFT WING TE SHROUD TOP SKIN STIFFENER BETWEEN RIB 7/8 AT THIS TIME.SDR 99ZZZM435Stiffener · crackedRIGHT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 7/8 OF SHROUD. REMOVED AND REPLACED STIFFENER PER SRM. (M)SDR 99ZZZM434Stiffener · crackedRIGHT WING TOP SKIN TE STIFFENER CRACKED AT FORWARD END, INBOARD OF RIB 9, SHROUD AREA. REMOVED AND REPLACED STIFFENER PER SRM. (M)SDR 98ZZZX3957Skin · dentedATW - REF W/C DATED 10-19-96, LT AFT FUSELAGE HAS DENT LOCATED 24 INCHES AFT OF LT PRESSURE BULKHEAD AND 6 INCHES BELOW 'N' NUMBERS. DENT IS 5 INCHES LONG BY MIN/D MAX - 1 INCHES/.078 INCH. REPAIRED DENT IAW BAE FAX DJR/RJO437-98.SDR 99ZZZM539Bracket · crackedLEFT WING TE, HYDRAULIC LINE CLAMP BRACKET CRACKED AT FALSE SPAR RIB NR 5. REPLACED HYDRAULIC LINE CLAMP BLOCK BRACKET AT RIB 5 AT THIS TIME. (M)SDR 99ZZZM431Control Cable · corrodedTHE CENTER FUSELAGE INTERCONNECT CABLES ARE CORRODED AT RIGHT WING ROOT. REMOVED AND REPLACED BOTH CENTER FUSELAGE INTERCONNECT CABLES AND ADJUSTED IAW MM 27-11-00. W/CS GENERATED FOR FUNCTIONAL TEST OF AILERON CONTROLS AND DISCONNECT. (M)SDR 99ZZZM430Fitting · leakingCOCKPIT OXYGEN SYSTEM HAS A LEAK. FAILED LEAK CHECK. REMOVED AND REPLACED 'T' FITTING BETWEEN SUPPLY GAUGE AND PRESSURE REDUCING VALVE UNDER RIGHT SIDE PANEL. COMPLIED WITH LEAK CHECK. ALL IAW MM. (M)SDR 99ZZZM429Sill · corrodedFORWARD VESTIBULE, PAX AND SERVICE DOOR, SILL PLATE HAV SOME CORROSION AROUND SCREW HOLES AND OTHER SMALL AREAS. MINOR SURFACE CORROSION REMOVED FROM SILL PLATES, ALODINED AND PRIMED. (M)SDR 99ZZZM428Intercostal · corrodedGUSSET PLATE AND FORWARD REST FLOOR SUPPORT INTERCOSTAL, LEFT OF CENTER, AT FRAME 18 IS CORRODED. INSTALLED NEW GUSSET PLATE.SDR 98ZZZX3958Cage · dentedATW - FORWARD CARGO DOOR AFT LOWER SEAL CAGE IS DENTED AND CRACKED. REPLACED FORWARD CARGO DOOR AFT LOWER SEAL CAGE.SDR 98ZZZM868Manifold · leakingNR 1 ENGINE FUEL LEAK AT BOTH MANIFOLDS AT START. REPLACED LEFT AND RIGHT FUEL MANIFOLDS, REF WORK CARD NR 29.SDR 98ZZZM867Manifold · leakingNR 1 ENGINE FUEL LEAK AT BOTH MANIFOLDS AT START. REPLACED LEFT AND RIGHT FUEL MANIFOLDS, REF WORK CARD NR 29.SDR 98ZZZX3991Intercostal · corrodedATW - AFT VESTIBULE FLOOR SUPPORT STRUCTURE, FIRST INTERCOSTAL INBOARD OF AIRSTAIR RAILS, LT SIDE HAS A RIVET WITH CORROSION AROUND IT. DRILLED OUT RIVET, REMOVED MINOR SURFACE CORROSION, USED PROTECTIVE TREATMENT ON BARE SURFACE, PRINTED AND COVERED SURFACE
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