N616AW, cancelled Oct 29, 2014
Service difficulty reports · 106
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 = 'N616AW' AND deregistration_id = 'N616AW-2014-10-29' 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 = 'N616AW' AND deregistration_id = 'N616AW-2014-10-29' 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 A6WA200460066Acm · odorNR 2 PACK WAS INADVERTENTLY SWITCHED ON FOR APPROX 10 MINUTES ENROUTE. PILOTS NOTICED ODOR IN COCKPIT, PACK SWITCHED OFF AND A PUFF OF WHITE SMOKE CAME OUT OF VENT IN COCKPIT THEN SMOKE ODOR DISSIPATED. MAINTENANCE REMOVED AND REPLACED RIGHT HAND AIR CYCLE MSDR A6WA200460052Oxygen Mask · misinstalledDURING INSPECTION, ALL PASSENGER O2 DROP DOWN MASKS WERE FOUND STOWED INCORRECTLY. MAINTENANCE RESTOWED ALL PASSENGER O2 DROP DOWN MASKS, CORRECTLY IAW AMM 35-20-45.SDR A6WA200460032Wire · shortedSHORTLY AFTER TAKEOFF, LOST ALL RADIO COMMUNICATION. RETURNED TO RDU, LANDED UNDER LANDING WEIGHT. MAINTENANCE REPAIRED SHORTED KEY WIRE TO YOKE MIC JACK SYSTEM. OPS CHECK GOOD. (M)SDR A6WA200360005Cable · unserviceableNR 2 THRUST LEVER WILL NOT MOVE BELOW CRUISE AT 31K (31,000 FEET), OK AFTER 14K (14,000 FEET). REMOVED AND REPLACED UPPER PYLON TELEFLEX CABLE. ON INSPECTION OF THE UNSERVICEABLE TELEFLEX CABLE. CONFIRMED THAT A CRIMP ALONG THE LENGTH OF THE CABLE CAUSED IT SDR A6WA200260078Bleed Band · out of toleranceUPON APPLICATION OF TAKEOFF POWER, NR 2 ENGINE DID NOT RESPOND WHILE TGT WENT TO 950 DEGREES FOR AN ESTIMATED 5 SECONDS BEFORE SECURING. MAINTENANCE FOUND NR 2 ENGINE BLEED BAND OUT OF TOLERANCE. ADJUSTED AS REQUIRED AND PERFORMED 4 POINT RUN. ALL RUNS WITHSDR A6WA200260005Cage · crackedREAR CARGO DOOR UPPER AFT INNER SEAL RETAINER CAGE IS CRACKED APPROX 2 INCHES IN LENGTH. REPLACED UPPER AFT INNER CAGE IAW SRM 51-42-00. REPAIRS CARRIED OUT PER BARA/AVR/5007/00. (M)SDR A6WA200260010Frame · chafedNR 3 ENGINE FORWARD INBOARD COWL DOOR HAS CHAFE MARKS ON FORWARD MOST FRAME. REPAIRED IAW BAE RIL HC711H9089. (M)SDR A6WA200260007Door · crackedNR 4 ENGINE INBOARD AFT COWL DOOR HAS A CRACK NEXT TO DRAIN TUBE. REPAIRED CRACK IAW BAE PROCEDURE REF NR NWH/RJ/0726-02 AND RIL HC7IIH9012. (M)SDR A6WA200260008Retainer · damagedELECTRICAL EQUIPMENT BAY DOOR RETAINING ANGLE ON FORWARD FRAME DAMAGED. ANGLE REPAIRED IAW BAE PROCEDURE REF NR CH/RJ/0734-02. (M)SDR A6WA200260006Structure · chafedFOUND LEFT AFT PAX DOOR AIRSTAIR HOOK CUTOUT HAS CHAFING FROM HOOK. REPAIRS CARRIED OUT IAW BAE PROCEDURE REF NR CH/RJ/0735/02. (M)SDR A6WA200260004Skin · dentedDENT IN A VERTICAL DIRECTION AT STRINGER 26L BETWEEN FRAME 12 AND 13. FABRICATED A REPAIR PATCH. PERFORMED A DETAILED VISUAL INSPECTION TO ENSURE SOUND CRACK FREE STRUCTURE REMAINS.SDR A6WA200260011Panel · dentedDENTS FOUND IN LEFT AND RIGHT WINGS TRAILING EDGE PANELS BETWEEN RIB 14A AND 15B. INSPECTION CARRIED OUT IAW MFG MM.SDR A6WA200260013Trim Tab · dentedDENTS FOUND IN LEFT AILERON TRIM TAB. INSPECTION CARRIED OUT IAW MM.SDR A6WA200260012Bracket · crackedLEFT INBOARD SPOILER OUTBOARD END BRACKET CRACKED AT FORWARD TOP EDGE. CARRIED OUT IAW MFG NWH/RJ/0723-02.SDR A6WA200260009Attach Angle · crackedFLOOR BEAM TO CROSSMEMBER ATTACH ANGLE CRACKED AT STA 183.15 FORWARD SIDE AND LBL 47 OUTBOARD SIDE. CROSSMEMBER ATTACH ANGLE REPLACED IAW SRM.SDR A6WA200000082A/C Pack · odorSMOKY SMELL IN CABIN AFTER TAKEOFF, CREW SHUT OFF APU AIR AND SWITCHED TO ENGINE AIR, OPERATED ON NR 2 PACK AND SMOKY SMELL DISSIPATED. MAINTENANCE PERFORMED DUCT CONTAMINATION CLEARING PROCEDURE COULD NOT DUPLICATE SMELL, SYSTEM OPERATES NORMALLY ON ALL ENGISDR 98ZZZM936Door Warning · activatedAFTER GEAR RETRACTION, LEFT MAIN GEAR INTRANSIT LIGHT 'RED' REMAINED ON AND RED LT IN GR HANDLE. COULD NOT DUPLICATE MEGGED AND UPLOCK HARNESSES. GEAR UPLOCK, 50M OHM EACH DOOR UPLOCK .5M OHM. REMOVED AND REPLACED HARNESS, FROZE SENSORS, CLEANED SENSORS, ONSDR 98ZZZX1234Pan · brokenCAPTAIN'S SEAT ASSY SEAT PAN BROKEN AT FWD RT CORNER. PAN ALSO HAS SEVERAL OTHER CRACKS. MADE NEW SEAT PAN IAW PS1 DRAWING AW-25-10-9707-06 INSTALLED PER DRAWING ALSO.SDR 98ZZZX1205Hinge · crackedDURING ADJUSTMENT/CHECK OF RT NR 2 CARRIAGE FLAP CANOE, FOUND HINGE ASSY CRACKED AT TOP FORWARD TRANSVERSE BEAD. DRESSED OUT CRACKED AREA (JM/RJ085-97). C/W FLUORSCENT DYE PENETRANT AND EDDY CURRENT INSPECTIONS. INSPECTED ENTIRE HINGE ASSY FOR CRACKS, NO DESDR 98ZZZX1208Bracket · crackedPSU RAIL RT OTBD, STAND-OFF BRACKET AT FRAMES 39-40 CRACKED AND RIVETS LOOSE. REPLACED BRACKET.SDR 98ZZZX1209Bulkhead Frame · chafedTHERE IS AN L-SHAPED CHAFE MARK ON FRAME 32 PRESSURE BULKHEAD, NEAR CENTERLINE BEHIND RT MLG DOOR UPLOCK ASSY. NEEDS INVESTIGATION. BLENDED ABOVE AREA IAW BAE FAX JM/FJ0844-97. REPROTECTED, PRIMED AND PAINTED.SDR 98ZZZX1201Bracket · crackedFORWARD PASSENGER DOOR - DOOR HANDLE SUPPORT BRACKET CRACKED. CHECKED WITH ET CRACK DEFECT NOTED. ITEM MARKED WITH TAG. MFG ABOVE BRACKET PER BAE DRAWING AND PS1 PN AW524H970206-000. INSTALLED PER SRM AND BAE FAX DJR/RJ0318-97 2 EACH UNF BOLTS.SDR 98ZZZX1229Rib · crackedATW - LT WING TIP REMOVEABLE RIB PANEL HAS A FEW CRACKS IN IT. PATCHED SAID CRACKS IAW BAE STD PRACTICES AND AIR WISC MM PSI REF: AW-57-20-9412-06.SDR 98ZZZX1199Intercostal · crackedREAR FUSELAGE AREA - CENTER FLOOR SUPPORT INTERCOSTAL CRACKED UNDER GUSSET PLATE BETWEEN FRAMES 41 AND 43. MARKED WITH GREEN DOT. REPAIRED INTERCOSTAL IAW BAE FAX REF DJR/RJ0839-97.SDR 98ZZZX1194Frame · crackedATW - RIGHT SIDE OF ECS BAY AT FRAME NR 47 HAS A CRACK IN THE SHEAR ANGLE AT STR 9 THAT IS APPROX .25 INCH LONG IN THE BEND RADIUS. NOTE: VERIFIED WITH EDDY CURRENT. REPAIR SHEAR ANGLE IAW BAE REPAIR INSTRUCTIONS HC539H9014.SDR 98ZZZX1207Angle · crackedREAR CARGO BAY FLOOR SUPPORT ANGLE CRACKED AT SCREW HOLE FRAME 34. SPLICED 8 INCH SECTION TO SUPPORT ANGLE PER SRM 51-71-11, DAMAGED AREA REMOVED.SDR 98ZZZX1221Stiffener · crackedATW - RIGHT WING TOP T/E SKIN STIFFENER CRACKED AT FWD END JUST INBD OF RIB NR 8. REPAIRED STIFFENER, REF FAX JM/RJ0317/97, AND JM/RJ0818-97.SDR 98ZZZX1219Intercostal · brokenATW - FORWARD CARGO INTERCOSTAL BROKEN BETWEEN FRAMES 23 AND 23 LT SIDE. REPAIRED INTERCOSTAL IAW BAE 146 SRM AND REINSTALLED IAW BAE 146 SCM. REF: 51-71-11. REPAIRED, OK FOR SERVICE.SDR 98ZZZM372Stiffener · crackedRT WING TOP TE SKIN STIFFENER CRACKED AT FWD END BETWEEN RIBS 8/9, JUST OUTBOARD OF RIB 8. REPAIRED CRACKED STIFFENER IAW FAX NR'S JM/RJO317/97 AND NR JM/RJO818-97. (M)SDR 98ZZZM369Stiffener · crackedLT WING, TRAILING EDGE AND SHROUD UPPER SKIN STIFFENER IS CRACKED AT FORWARD END IN AREA BETWEEN WING RIBS 7 AND 8. REPAIRED STIFFENER REF FAX JM/RJ0818-97. (M)SDR 98ZZZM365Stiffener · crackedRT WING TOP TE SKIN STIFFENER CRACKED AT FWD END AT RIB NR 9, JUST INBOARD OF RIB 9. REPAIRED CRACKED STIFFENER IAW FAX NR'S JM/RJ0317/97 AND NR JM/RJO317/97 AND NR JM/RJO818-97. (M)SDR 98ZZZX1195Frame · crackedATW - RIGHT SIDE OF STRUCTURE AFT OF FR 50 HAS A FRAME THAT IS CRACKED LOCATED ABOVE UPPER HINGE BLADE FOR AIRBRAKE BACKSIDE OF FR 50. CRACK IS UNDER OUTER CORNER OF GUSSET PLATE ACROSS THAT RIVET HOLE AND GOES INWARD TO INNER AND EDGE OF FRAME. REPLACED UPPSDR 98ZZZM366Frame · crackedLEFT SIDE OF STRUCTURE AFT OF FRAME 50 HAS A FRAME ABOVE THE UPPER HINGE BLADE FOR SPEED BRAKE THAT HAS A CRACK ACROSS THE 3RD RIVET HOLE DOWN ON OUTER FLANGE THAT ATTACHES TO SKIN. VERIFIED WITH EDDY CURRENT. REPLACED LEFT UPPER WEB DIAPHRAM. (M)SDR 98ZZZM364Web · crackedRT SIDE OF STRUCTURE AFT OF FRAME NR 50 HAS A WEB THAT RUNS VERTICALLY FROM THE REAR FLANGE OF FRAME NR 50 DOWN TO THE LOWER BLADE OF THE SPEED BRAKE HINGE THAT HAS A SMALL CRACK ACROSS THE UPPER TOP RIVET HOLE AT OUTER FLANGE. CRACK VERIFIED WITH EDDY CURRENSDR 98ZZZX1202Inserts · corrodedFORWARD LAV MODULE, METAL INSERTS IN FLOOR CORRODED. REPLACED AS NEEDED. INSTALLED PERMACEL AFTER REPLACMENT OF INSERTS. REPLACED INSERTS AS NEEDED AND INSTALLED NEW PERMACEL ON UNDER SIDE OF FORWARD LAV MODULE.SDR 98ZZZX1236Bracket · crackedNR 2 ENGINE SHOULDER COWL TERMINAL BOARD FWD BRACKET CRACKED. REPLACED NR 2 ENG SHOULDER COWL TERMINAL BOARD FWD BRACKET.SDR 98ZZZX1233Bracket · brokenFWD CLOSET WALL BEHIND FO'S SEAT, LOWER CORNER ATTACH BRACKET BROKEN. FABRICATED AND REPLACED FWD CLOSET WALL BRACKET BEHIND FO'S SEAT (LOWER ATTACH BRACKET).SDR 98ZZZX1227Sill · corrodedAFT VESTIBULE SILL PLATE FOR SERVICE DOOR SIDE HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED AFT VESTIBULE SERVICE DOOR SILL PLATE.SDR 98ZZZX1224Angle · crackedATW - RT WING T/E LOWER SKIN STIFFENER AFT TAG ANGLE CRACKED BETWEEN RIBS 3 AND 4. REPLACED ANGLE.SDR 98ZZZX1223Angle · crackedRT WING T/E LOWER SKIN STIFFENER AFT TAG ANGLE CRACKED AT RIB NR 4. REPLACED ANGLE.SDR 98ZZZX1222Angle · crackedATW - RT WING T/E LOWER SKIN STIFFENERS AFT TAG ANGLE CRACKED BETWEEN RIBS 5 AND 6. REPLACED ANGLE.SDR 98ZZZX1206Seal Cage · crackedREAR CARGO DOOR LOWER AFT SEAL CAGE CRACKED. REPLACED LOWER AFT SEAL CAGE.SDR 98ZZZX1226Bolts · looseATW - AIR WISC EO E92/083/657 RECC ATTACH BOLTS AND NUTS ON RT SIDE, A, B, C, D ARE LOOSE ON THE REAR SPAR ROOT ATTACHMENT FITTING AT WING RIB 2. REPLACED FASTENERS IAW BAE REPAIR INSTRUCTIONS HC53H9043. BOLTS A, C, D ORIG SIZE. BOLT B FIRST OVERSIZE, RESEASDR 98ZZZX1225Mounting · crackedATW - RT LIFT SPOILER VALVE MOUNTING PLATE CRACKED. REMOVED AND REPLACED RT SPOILER VALVE MOUNTING PLATE. NO DISCONNECTING OF VALVE REQUIRED.SDR 98ZZZX1237Cowl · chafedNR 2 ENGINE LT FWD COWL DOOR AFT FRAME CHAFED AT LATCH AREA AND AT MID-AREA DUE TO CONTACT WITH HYDRAULIC LINE. REPLACED CAP STRIP ON NR 2 ENG LT FWD COWL DOOR AFT FRAME.SDR 98ZZZX1216Floor · buckledREF FAX LM/115-97, LM/116-97, JM/RJ0096-97, AND DJR/RJ0098-97. MLG PRESS FLOOR BETWEEN FRAMES 29 AND 32 OTBD SEAT RAILS 19 INCHES, 20 INCHES OTBD CENTERLINE HV BUCKLE APPROX .125 INCH DEEP. DV DUE EA 500 CYC. REPORT FINDINGS AI (R) REMOVE FLOOR STS. CUR 230SDR 98ZZZX1231Bracket · crackedATW - LT WING BRACKET FOR HYD LINES THAT PASS THROUGH THE AFT END OF THE SPOILER HINGE RIB AT WING RIB NR 5 IS CRACKED. REPLACED BRACKET.SDR 98ZZZX1220Angle · crackedFREIGHT ANGLE AT FRAME 19D CRACKED CENTER SECTION. REPLACED FREIGHT ANGLE AT FRAME 19D IAW BAE 146 SRM.SDR 98ZZZX1213Jobolts · damagedREPLACED JOBOLTS ON RT WING CENTER TANK RIB 2 INBOARD PER RIL HC571H9033. PERFORMED RIL HC571H9033 TO RIB 2 INBD CENTER TANK. REPLACED JOBOLTS WITH MRL FASTENERS.SDR 98ZZZX1203Support · crackedFRONT CARGO BAY CENTER CARGO FLOOR SUPPORT AT 19C CORRODED AND CRACKED. AREA MARKED. REPLACED FREIGHT ANGLE AT FR 19C IAW BAE 146 SRM.
Back to N616AW, cancelled Oct 29, 2014