N609AW, cancelled Dec 13, 2012
Service difficulty reports · 70
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 = 'N609AW' AND deregistration_id = 'N609AW-2012-12-13' 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 = 'N609AW' AND deregistration_id = 'N609AW-2012-12-13' 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 A6WA200560002Brake · inoperativeGREEN HYDRAULIC SYSTEM LOW, YELLOW SYSTEM HIGH. ABORTED TAKE-OFF AT LESS THAN 5 KTS. MAINTENANCE SERVICED AS REQUIRED. MAINTENANCE REMOVED AND REPLACED NR 4 BRAKE ASSEMBLY. (K)SDR A6WA200360006Lever · out of rigNR 3 THRUST LEVER NEEDS TO BE RE-RIGGED. UNABLE TO SET BELOW 40 PERCENT N1. (M)SDR A6WA200260002Connector · failedENROUTE, NR 1 GENERATOR FAILED, NO VOLTS OR HZ, NR 1 AC BUSS AND AC ESSENTIAL BUSS FELL OFF LINE. NR 4 GEN FELL OFF LINE MOMENTARILY WITH AC NR 2 BUSS OFF LINE ALSO. RESET NR 4 GENERATOR BUT ONLY ABLE TO REGAIN AC NR 2 BUSS. STARTED APU, APU GENERATOR SHOWSDR A6WA200100021Warning Light · illuminatedFAULT LIGHT ILLUMINATED FLAPS STUCK AT 18 DEGREES. MAINTENANCE CLEARED FAULT USING BAE SUPPLEMENT. RAN FLAPS, OPS CHECKED GOOD.SDR A6WA200000074Connector · dirtyDURING TAXI BRAKES SEEM INAFFECTIVE ON YELLOW HYDRAULIC SYSTEM. SWITCHED TO GREEN SYSTEM AND BACK TO YELLOW SYSTEM BRAKING NORMAL. MAINTENANCE REMOVED THE ANTI-SKID CONTROL BOX AND CLEANED CONNECTION OPERATIONAL CHECK GOOD. VISUALLY OBSERVED BRAKES ON YELLOW ASDR A6WA200000068Scoop · crackedNR 1 ENGINE OUT BOARD DOOR NACA SCOOP AND ATTACHMENTS CRACKED. MAINTENANCE REPAIRED FAN DOOR NACA SCOOP AS REQUIRED ALSO REPAIRED APLITTER ANGLE IAW SRM AND FAX BARA/AVR/5228/00.SDR A6WA200000067Pin · crackedWHILE PERFORMING INSPECTION OF NLG RETRACTION BOSS FOUND EVIDENCE OF VISUAL FRETTING OF ATTACH PIN. FURTHER INSPECTION REVEALED TORQUE AT 20 FT LBS AND SIGNS OF CRACKING VISUALLY CONFIRMED BY NDT SIDEWALL BAD. MAINTENANCE REPLACED NOSE DIAPHAGM PER RIL HC53H9SDR A6WA9900039Girt Bar · disengagedAFT PASSENGER CABIN DOOR AFTER OPENING, GIRT BAR DISENGAGED FROM DOOR. FOUND NO PARTIAL DEPLOYMENT OF SLIDE, RE-ENGAGED GIRT BAR TO DOOR. RECONNECTED SLIDE AUTODEPLOY LANYARD. OPS CHECKED DOOR AND GIRT BAR. OPS CHECKS SATISFACTORY. ACFT TT: 23,562 HOURSDR 98ZZZX3959Actuator · leakingATW - FLT 581 - YELLOW HYDRAULIC FLUID LOST, WITH ASSOCIATED FLUID AT REAR AIRSTAIR AND LAVATORY. FOUND AFT AIRSTAIR, FORWARD ACTUATOR LEAKING, CLEANED, CAPPED OFF LINE AND DEFERRED AND PLACARDED, C/W OVERWEIGHT LANDING INSPECTION.SDR 99ZZZM493Skin · chafedFUSELAGE SKIN CHAFED APPROX 13 INCHES LONB BY FORWARD RIGHT WING ROOT FAIRING BETWEEN FRAMES 25/26. REF W/C 6075 FOR BLEND AND NDT. FIT EXTERNAL PATCH OVER CHAFED AREA UNDER RT WING ROOT FAIRING ON FUSELAGE SKIN BETWEEN FRAMES 25/26 PER SRM 53-00-12 FIGURE 2SDR 99ZZZM534Prox Switch · failedWITH GEAR HANDLE SELECTOR UP, LEFT MAIN GEAR INDICATES GEAR INTRANSIT, RID LIGHT IN GEAR HANDLE ALSO ILLUMINATED. NO AURAL GEAR WEARING. STANDBY GEAR INDICATORS ALL OFF. REMOVED AND REPLACED LEFT MLG LEG UPLOCK HARNESS AND PROXIMITY SWITCH IAW BAE 146MM, TESDR 99ZZZM561Arm · failedDURING GEAR RETRACTION AT EGE, HEARD A VERY LOUD BANG FROM NOSE WHEEL AREA ACCOMPANIED BY WHEEL ROTATION SOUNDS. GEAR RETRACTION AND EXTENSION NORMAL. REPLACED LEFT EMEREGNCY LOWERING GEAR ASSISTING ARM ASSY. RETRACTED GEAR, FREE FALL OPS CHECKED GOOD. CLOSDR 99ZZZM500Bolts · looseFOUND LOOSE JOBOLTS AT VARIOUS LOCATIONS AT WING TANK RIB '0' AND RIB 2 LT/RT. COMPLETED LOOSE JOBOLT REPLACEMENT AT RIB 0 AND RIB 2 LT/RT PER RIL HC571H9033. NOTE, 6 POSITIONS WERE OVERSIZED.SDR 99ZZZM563Stall Bar · looseLEFT WING INBOARD SECTION OF STALL BAR LOOSE, PULLING OVER SCREW HEADS. REMOVED LT WING STALL TRIGGER AND REPAIRED PER FAX REF DJH/RJO268-98 USING FAX GCB/RJ1344-94. REINSTALLED STALL TRIGGER. (M)SDR 99ZZZM492Stall Bar · out of positionRIGHT WING SHORT SECTION OF STALL BAR PULLING OVER CORNER SCREWS. REMOVED LEFT WING STALL TRIGGER AND REPAIR PER FAX REF DJH/R JO268 USING FAX GCB/RJ1344-94 AND REINSTALLED STALL TRIGGER. (M)SDR 99ZZZM511Wire · brokenNR 1 ENGINE POWER LEVER FIRE WARNING LIGHT DOES NOT ILLUMINATE DURING FIRE TEST, WIRE BAD. REMOVED AND REPLACED BOTH WIRES IN POWER LEVER FIRE WARNING. TESTED PER MM. (M)SDR 99ZZZM507Bulkhead Strip · corrodedFORWARD LAVATORY BULKHEAD I2109 LOWER METAL STRIP ON BOTTOM OF BULKHEAD IS CORRODED. INSTALLED LOWER METAL STRIP ON FORWARD LAVATORY BULKHEAD I2109 OLD UNIT PREVIOUSLY REMOVED. (M)SDR 99ZZZM564Stiffener · crackedLEFT WING TE TOP SKIN, TWO STIFFENERS CRACKED AT FORWARD END BETWEEN RIB 8/9. REPLACED LEFT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN RIB 8/9 (P/N HC572H0626-0000). REPAIRED LEFT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN RIB 8/9 (P/N HC572H0627-002) SDR 99ZZZM562Angle · crackedLEFT FORWARD PAX DOOR HANDLE BOX AREA 2 CRACKED ANGLES. REPLACED LEFT FORWARD PAX DOOR HANDLE BOX AREA ANGLES REF P/N'S ABOVE. REPAIR ACCOMPLISHED IAW BAE DRAWINGS HC521H0508 AND HC521H0507 AND BAE FAX REF DJR/RJO318-97. (M)SDR 99ZZZM502Bolt · wornRIGHT AIRBRAKE UPPER ATTACH POINT BOLT PLATING IS WORN OFF, BOLT WAS FROZEN IN BEARING. REMOVED AND REPLACED HINGE PIN AND BUSH. INSTALLED DURING AIRBRAKE INSTALLATION. SEE W/C NR 3019 FOR INSTALLATION. (M)SDR 99ZZZM567Stiffener · crackedRIGHT WING TE TOP SKIN STIFFENER CRACKED AT AFT END BETWEEN RIBS 3/4. REMOVED AND REPLACED STIFFENER. (M)SDR 99ZZZM498Skin · chafedRIGHT MLG DOOR INTERNAL SKIN, FORWARD EDGE, APPROX 1ST 6 INCHES DOWN HAS EVIDENCE OF CHAFING ON FRAME NR 29 WHEN L/G IS UP AND LOCKED. BLENDED OUT CHAF IN DRUM, MINOR DAMAGE WITHIN LIMITS, PRC COATED FOR ABRASION. (M)SDR 99ZZZM491Pulley · seizedRIGHT WING LOWER AILERON TRIM CABLE PULLEY SEIZED OUTBOARD OF NR 4 FLAP TRACK. REMOVED AND REPLACED TRIM CABLE PULLEY'S AS NEEDED IAW MM. (M)SDR 99ZZZM490Attach Links · corrodedRIGHT WING TO FUSELAGE AFT ATTACH LINKS HAVE SURFACE CORROSION ON ENDS (PAINT MISSING). CLEANED, PRIMED AND PAINTED ENDS. (M)SDR 99ZZZM566Bracket · crackedRIGHT WING TE HYD LINE CLAMP BRACKET CRACKED AT FALSE SPAR ABOVE NR 2 FLAP TRACK. REPLACED RIGHT WING TE HYD LINE CLAMP BRACKET. (M)SDR 99ZZZM499Bolts · loosePERFORM RIL HC571H9033 LT RIB 2 OUTBOARD JOBOLTS. PERFORMED RIL HC571H9033 ON LEFT RIB 2 OUTBOARD JOBOLTS. (M)SDR 99ZZZM568Stiffener · crackedRIGHT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 8/9. REPLACED RT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN 7/8. (M)SDR 99ZZZM487Stiffener · crackedRIGHT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 7/8 (OUTBOARD STIFFENER). REPLACED RT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN RIB 7/8. (M)SDR 99ZZZM569Skin · chafedRIGHT FLAP UPPER SKIN BETWEEN RIB 29/30 HAS .020 INCH DEEP BY 1 INCH LONG CHAFE. BLENDED CHAFE MARK TO A SMOOTH PROFILE AS NEEDED IAW BAE FAX DJR/RJO236-98. DV AND NDT INSPECTION C/W IAW BAE FAX DJR/RJO236-98, AREA CRACK FREE. APPLIED SURFACE REPROTECTION ASDR 99ZZZM565Skin · chafedRIGHT FLAP TAB UPPER SKIN AT RIB 34 HAS TWO .011 INCH DEEP CHAFED AREAS, (.005 TO .008). BLENDED CHAFE MARKS TO SMOOTH PROFILE AS NEEDED IAW BAE FAX DJR/RJO234-98. DV AND NDT INSPECTION C/W IAW BAE FAX DJR/RJO234-98, AREA CRACK FREE. APPLIED SURFACE REPROTESDR 99ZZZM497Skin · chafedLEFT MLG DOOR INTERNAL SKIN FORWARD EDGE APPROX 1ST 6 INCHES FROM TOP EDGE HAS EVIDENCE OF CHAFING ON FRAME NR 29 WHEN GEAR IS UP AND LOCKED. TRANSFER TO W/O BX1879 FOR REPAIR. (M)SDR 99ZZZM489False Spar · crackedRIGHT WING TE FALSE SPAR CRACKED JUST INBOARD OF INBOARD LIFT SPOILER JACK. REPAIRED PER FAX JM/RJ0240-98, PER DRAWING HC572H9036. OPPOSITE HAND TO DRAWING. (M)SDR 99ZZZM501Bolt · scratchedUPPER RUDDER ACTUATOR AFT ATTACHMENT BOLT HAS SCRATCH THAT GOES BELOW PLATING. REMOVED AND REPLACED UPPER RUDDER ACTUATOR AFT ATTACHMENT BOLT IAW AMM. (M)SDR 99ZZZM504Bearing · wornRUDDER TOP 'A FRAME HINGE POINT HAS A BAD BEARING. 'A' FRAME REMOVED FOR REPAIR. INSTALLED SERVICEABLE RUDDER TOP 'A' FRAME IAW BAE MM. (M)SDR 99ZZZM494Door · damagedRIGHT MLG DOOR LOWER FORWARD CORNER IS DEFORMED OUTWARD APPROX .167 FROM CONTOUR, APPROX 3.55 IN LENGTH. REPAIRED IAW BAE SRM 52-81-11, FIG 204, TYPE 2. (M)SDR 99ZZZM488Mount · crackedRIGHT WING ROOT, LIFT SPOILER CONTROL VALVE MOUNT PLATE CRACKED. REMOVED AND REPLACED PLATE. (M)SDR 99ZZZM510Control Cable · corrodedLEFT CLAD INTERCONNECT CABLE FOR AILERONS SHOWS EVIDENCE OF CORROSION AT DIFFERENTIAL SECTOR BETWEEN RIBS 14/15. REMOVED AND REPLACED LEFT CLAD INTERCONNECT CABLE (AILERON) IAW BAE MM. GENERATED W/C TO PERFORM AILERON FUNCTIONAL CHECKS AND PRIORITY 2 WC TO RSDR 99ZZZM508Control Cable · corrodedRIGHT WING AILERON INTERCONNECT CABLES AT WING ROOT PULLEY CORRODED. REMOVED AND REPLACED FUSELAGE INTERCONNECT CABLES (AILERON) IAW BAE MM. GENERATED WC TO PERFORM AILERON FUNCTIONAL CHECK AND PRI 2 WC TO RE-CHECK TENSION AT 4000 FLT INTERVAL. (M)SDR 99ZZZM506Cable Guard · seizedRIGHT WING ROOT, OUTBOARD CABLE GAURD SEIZED AND BOTH PULLEYS WORN FOR CENTER SECTION AILERON INTERCONNECT CABLES. REMOVED AND REPLACED PULLEYS EXTRACTED SEIZED GUARD AND REPLACED WITH NEW GUARD, RIGHT WING ROOT. (M)SDR 99ZZZM570Seal · bentFORWARD CARGO DOOR BOTTOM HALF SEAL CAGE IS DISTORTED, BENT IN NUMEROUS AREAS. REPLACED FORWARD CARGO DOOR BOTTOM AFT SEAL CAGE P/N HC523J0 063-202. STRAIGHTENED BEND IN PORTION OF BOTTOM FORWARD SEAL CAGE. (M)SDR 99ZZZM496Seal · damagedREAR CARGO DOOR LOWER SEAL CAGE IS BENT, DEFORMED IN SEVERAL AREAS. REPLACED REAR CARGO DOOR LOWER SEAL CAGE. (M)SDR 99ZZZM505Bearing · wornRUDDER BEARING BAD AT MAIN (RIB 6) 'A' FRAME SUPPORT. ALLOW AND EXCESSIVE UP AND DOWN FLOAT OF RUDDER ASSY .25 INCH APPROX. REMOVED AND REPLACED RUDDER MAIN 'A' FRAME (RIB 6) HINGE BEARING. (M)SDR 99ZZZM503Control Cable · corrodedLEFT AND RIGHT ELEVATOR CABLES ARE CORRODED AT PULLEYS IN VERTICLE STAB. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR CABLES FROM REAR PRESS BULKHEAD TO COMPENSATORS AND ADJUSTED IAW MM 27-31-00. W/C GENERATED FOR FUNCTION TEST. (M)SDR 99ZZZM509Sill · crackedAFT PASSENGER DOOR, AFT SIDE OF DOOR SILL PLATE IS CRACKED ABOUT 1 INCH LONG. REMOVED DAMAGED SILL PLATE, DRILLED AND FITTED NEW SILL PLATE ON AFT PASSENGER DOOR, AFT SIDE INSTALLED NEW SILL PLATE AND PAINTED RIVET HEADS AND BUCKTAILS. (M)SDR 99ZZZM495Bracket · crackedUPPER ATTACH ANGLE BRACKET FOR MLG BAY DIAPHRAM HAS A CRACK. REPLACED UPPER ATTACH ANGLE BRACKET FOR MLG BAY DIAPHRAM. (M)SDR 97ZZZX3147Air Distribution · fumesORD - FLT 504 - NOTICED FUMES IN CABIN ON GROUND WHILE ON APU AIR. RAN BOTH PACKS TO FULL HOT. NO FUMES NOTED.SDR 97ZZZX2992Hydraulic Line · leakingORD - FLT 504 - SUSPECT HYDRAULIC FLUID FUMES IN AIRCRAFT. FOUND LEAKING NLG DOWN LINE. REPLACED LINE, GREEN SYSTEM.SDR 97ZZZM402Doubler · crackedRIGHT STIFFENER (STATION 47.20) AT FRAME 29 IN HYDRAULIC BAY HAS CRACKED DOUBLER PLATE AT BOTTOM END OF STIFFENER. REPLACED RIGHT STIFFENER (STATION 47.20) AT FRAME 29 IAW BAE DRAWING NR HC536H0090 AND AIR FAX NR DS/W/TS/25913/96.SDR 97ZZZM403Trim Chain · corrodedLEFT AILERON TRIM SCREWJACK CHAIN APPEARS TO BE CORRODED. LEFT TRIM CABLE TURNBUCKLES LOOSE. REMOVED AND REPLACED LEFT AILERON TRIM CHAIN IAW 27-12-17. A DJUSTED CABLES AND COMPLIED WITH FUNCTION TEST IAW 27-12-00. CHECKS OK. (M)SDR 97ZZZM404Floorbeam · crackedTHREE FLOORBEAMS ARE CRACKED AT FRAME 29 BEAM 3, 13 AND 19. REPAIRED CRACKS IAW BAE DRAWING HC536H9211 AND FAX AIRAMS/T/BAE/25858/96.
Back to N609AW, cancelled Dec 13, 2012