N147AW, cancelled Oct 17, 2014
Service difficulty reports · 54
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 = 'N147AW' AND deregistration_id = 'N147AW-2014-10-17' 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 = 'N147AW' AND deregistration_id = 'N147AW-2014-10-17' 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 KNNA147071110KACYHydraulic Line · leakingTHE "A" SYSTEM QUANTITY AND PRESSURE DROPPED TO ZERO ON DESCENT TO KACY (ATLANTIC CITY IAP, NJ). COMPLETED CHECKLIST 6.77 OF THE AFM.SDR KNNA20090001Seal · failedNR 1 ENGINE OIL QUANTITY DROPPED TO ZERO DURING FLIGHT FOLLOWED BY DROP IN OIL PRESSURE LEADING TO ENGINE SHUT DOWN AND DECLARATION OF AN EMERGENCY. IT WAS DISCOVERED DURING TROUBLE SHOOTING THAT BOTH THE STARTER SEAL AND THE FUEL PUMP SEALS WERE LEAKING. BSDR PIDR07001Skin · crackedCRACK IN THE FUSELAGE SKIN AT BS 727B+4 AT STR 17 RT WAS REPAIRED BY REPLACING THE DAMAGED SECTION OF SKIN FROM BS 727 TO BS 757 FROM STR 14 RT TO STR 20 RT DUE PROXIMITY OF ADJACENT REPAIRS. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH PACE AIRLINES REPAIR PROSDR PIDR07002Skin · crackedCRACK IN FUSELAGE SKIN AT BS 727A+14.5 AT STR 17 LT WAS REPAIRED BY REPLACING SECTION OF SKIN FROM BS 727A +8 TO BS 767 FROM STR 16 LT TO STR 18 LT DUE TO PROXIMITY OF ADJACENT REPAIRS. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH PACE AIRLINES REPAIR PROCEDURESDR PIDR07003Stringer · damagedSTRINGER 16 RT AT BS 727B HAS A DAMAGED FASTENER HOLE. REPAIRED IN ACCORDANCE WITH SRM 53-10-3 FIGURE 2.SDR KNNA200700011Frame · misdrilledFOUND MISDRILLED HOLE AT SKIN OF SIDE FRAME, WL 212 LT, STA 179. FOUND PROVIDE INSTRUCTIONS ON REPAIR OF MISDRILLED FASTENER HOLE BS 178 W/L 212.SDR KNNA200700018Frame · crackedFOUND STA 178, LT SIDE FRAME IS CRACKED AT W/L 195. PROVIDE INSTRUCTION ON REPAIR CRACK BY INSTALLING A SPLICE OVER THE (LEFT SIDE) SIDE CHORD AT WL 212.SDR KNNA200700017Vertical Beam · crackedFOUND LBL 5.7 VERTICAL BEAM IS CRACKED BOTH FLANGES AT STA 178 BULKHEAD. PROVIDE INSTRUCTIONS ON REPAIR OF LBL 5.7 VERTICAL CHORD AT STA 178.SDR KNNA200700015Bulkhead · crackedFOUND STA 178 BULKHEAD IS CRACKED AT WL-234, LBL-8 TO LBL-9. PROVIDE INSTRUCTION ON REPAIR OF BULKHEAD AT STA 178 LBL 8 - LBL 9 AND LBL-10-LBL 12.SDR KNNA200700014Frame · crackedFOUND STA 178 RT SIDE FRAME IS CRACKED AT WL 207. PROVIDE INSTRUCTION TO REPAIR CRACK BY INSTALLING A SPLICE OVER THE (RIGHT SIDE) SIDE CHORD AT WL 212.SDR KNNA200700012Bulkhead · crackedFOUND STA 178 BULKHEAD IS CRACKED AT STA 178 W/L 213.5, RBL1, W/L 224, LBL-1-RBL1, W/L 227, RBL 1. PROVIDE INSTRUCTIONS ON REPAIR OF BULKHEAD AT STA 178 W/L 213.5, RBL 1,SDR KNNA200700010Bulkhead · crackedFOUND STA 178 BULKHEAD IS CRACKED AT W/L 234,RBL 9-RBL 10. FOUND PROVIDE INSTRUCTIONS ON REPAIR OF BULKHEAD AT STA 178 RBL 9-RBL 10 .SDR KNNA200700013Skin · damagedE/E BAY ACCESS DOOR EXTERIOR SURFACE, RT EDGE BEND. PROVIDE INSTRUCTIONS ON REPAIR OF E/E BAY DOOR .SDR KNNA200700016Stringer Splice · activeFOUND CRACKED CHORD OF STRINGER 14L AT BS 663.75. PROVIDE INSTRUCTION ON REPAIR OF S14L AT BS 663.75.SDR KNNA200300001Skin · crackedAIRCRAFT AT MAINT. BASE FOR "A3" CHECK COMPLIANCE. IN C/W TASK CARD A-07A A 1.8 INCH CRACK WAS FOUND IN EXTERIOR FUSELAGE SKIN AT LT BS 757 BELOW STR 17. A NON-ROUTINE T030446 AND ACO 035313R00 WAS ISSUED TO DOCUMENT SRM REPAIR CH 53-30-3 FIG 25. CRACK IN SKSDR 2001F00633Tire · separatedLOSS OF A SYSTEM HYDRAULICS. LEFT INBOARD TIRE LOST TREAD DURING TAKEOFF ROLL. PIECES OF THE TIRE TREAD DAMAGED HYDRAULIC LINES AND CONTROL CABLES LOCATED IN THE LEFT WHEEL WELL. ALSO, DAMAGE FROM FLYING RUBBER TO LEFT FORE FLAP, MID FLAP AND TRAILING EDGE SDR AWXA9900373Power Supply · inopCONDITION: NON-ROUTINE-- EMER LTNG LOG 3203678DISCREPANCY: EMERGENCY LIGHTS ROW 6 THROUGH 14 INOPCORRECTIVE ACTION: REPLACED POWER SUPPLY AND BATTERYCURRENT HISTORY: 6 WRITE-UPS SINCE 07/01/99 NONE RELATEDSDR AWXA9900137Engine · failedAIR TURNBACK, ENGINE SHUT DOWN. ON CLIMBOUT OIL TEMP ON NR 1 ENG WAS IN THE RED BAND. ENGINE WAS SHUTDOWN INFLIGHT PER QRH. DRAINED 1 GALLON ENGINE OIL FROM NR 1 ENG. RAN ENGINES AT T/O POWER, OPS NORMAL AT THIS TIME. AIRCRAFT WAS RELEASED FOR REVENUE SERSDR AWXA9800237Pcu · leaksINBOUND TO LAX, LOST 'B' SYSTEM HYDRAULIC FLUID. DECLARED EMERGENCY. REMOVED AND REPLACED RUDDER PCU FOR LEAKING. ADDITIONAL INFORMATION TO FOLLOW, TO INCLUDE TEARDOWN REPORT.SDR AWXA9800229Actuator · malfunctionedCABIN FLOORBEAM STA 696 LBL 63 FLOORBEAM WEB IS CRACKED, MARKED NR 38. RESEARCHED, NOT A REPAIR IN THE SRM MAPPED AREA AND SENT TO ENGINEERING REF LOG 5082720.SDR AWXA9800163Connector · looseNR 2 FIRE WARNING LIGHT AND BELL WENT OFF ABOUT 50 MILES PRIOR TO LAND QRH PROCEDURES COMPLETE AND ENGINE SECURED. BOTH FIRE BOTTLES EXPENDED INTO NR 2 ENGINE. BELL CONTINUED TO SOUND AND FIRE LIGHT CONTINUED TO ILLUMINATE LONG AFTER LANDING AND TAXI IN. RESDR AWXA9800146Skin · crackedD-FUSELAGE CRACK AT STA 727 NEAR STRINGER 17 RT SIDE C-CONFIRMED BY HFEC AND REPAIRED PER SRM 53-30-03 FIG 1.SDR 99ZZZX1821Valve · misoverhauledRED, TI-TEMP RTV HAS BEEN APPLIED IN THE THROAT OF THE HOUSING AROUND THE BUTTERFLY SEAL SEAT. THIS BUTTERFLY SEAL IS DESIGNED TO FLOAT IN THE HOUSING, BUT IN THIS CASE, THE SEAL WAS PRESSED INTO THE BEAD OF SEALANT. SUBMITTER STATED THIS IS NOT AN ASSEMBLY SDR AWXA9800003Wire · looseSEAT 1L EMERGENCY LIGHT INOP. RECONNECTED WIRE HARNESS, OPS GOOD. STC NR SA3432NMSDR AWXA9700707Light · loosePST DECK EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, GRD OPS OK. STC NR SA3432NMSDR AWXA9700613Megaphone · inoperativeDURING ROUTINE MAINTENANCE CHECK, FOUND AFT EMERGENCY MEGAPHONE INOP. REMOVED AND REPLACED MEGAPHONE.SDR AWXA9700557Light · cover missingDURING ROUTINE MAINTENANCE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY, OPS TEST GOOD. STC - SA3432NMSDR AWXA9700556Solenoid · failedL/G HANDLE WOULD NOT MOVE PAST OFF ON TAKEOFF. CYCLED HANDLE DOWN AND BACK TO NO AVAIL. USED RED TRIGGER TO RETRACT GEAR. REMOVED AND REPLACED LANDING GEAR LEVER LOCK SOLENOID.SDR AWXA9600769Wire · brokenDURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHT AT ROW 13 INOPERATIVE. REPAIRED SEAT WIRING. OPS GOOD. STC - SA3432NM.SDR 97ZZZX111Drag Brace · damagedDRAG BRACE SENT TO BFG FOR REPAIR. FOUND BEARING MIGRATED FROM LOCATION CAUSING DAMAGE TO BRACE DURING GEAR ACTUATION. BEARING INSTALLATION RECORDS NOT AVAILABLE TO BFG AT THIS TIME. CAUSE UNKNOWN. (REP STA NR B4GR448J).SDR AWXA960608Fuel Heat Vlv · loose wiringTUS - FLT 2062 - PILOT SHUT DOWN NR 1 ENGINE DUE TO HIGH OIL TEMP. PILOT CYCLED FUEL HEAT VALVE SUSPECTING IT MAY BE PARTIALLY OPEN, VALVE APPARENTLY FAILED TO CLOSE AS INDICATED BY DISAGREE LIGHT WHEN SELECTED OFF. COULD NOT REMEDY THE HIGH OIL TEMP SO ENGISDR AWXA9600667Light · inopPHX - FLT 2455 - DURING ROUTINE MAINTENANCE INSPECTION, FOUND L-1 DOOR EMERGENCY EXIT LIGHT (OUTER DOOR) DOES NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONS CHECK GOOD. (M)SDR AWXA960598Connector · loosePHX - FLT 2245 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT OVERWING WINDOW EXIT INOP. RECONNECTED CONNECTOR ON BATTERY PACK. OPS CHECK GOOD. (M)SDR AWXA960422Wire · brokenPHX - FLT 2081 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 11 EMERGENCY LIGHT INOP. REPAIRED WIRE. OPS CHECK OK. (M)SDR AWXA960014Duct Assy · crackedPHX/SJC - FLT 0870 - DURING CLIMB-OUT, NR 1 ENGINE FIRE LIGHT CAME ON. (NR 1 OVHT DET CURRENTLY ON MEL 26-02.) THE FIRE DET SYSTEM WOULD NOT TEST IN EITHER NORM OR FIRE. THE FIRE OVERHEAT SYSTEM DID START TO TEST IN NORM AND FIRE. AIRCRAFT RETURN TO PHX NOSDR AWXA9500790Track · wornPHX - FLT NR 417 - PHX/COS - AIR TURN BACK - AIRCRAFT ROLLED TO THE LEFT AND REQUIRED 15 TO 20 DEGREE RIGHT AILERON TO CORRECT. SITUATION CORRECTED AFTER FLAPS RETRACTED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 5 LEADING EDGE SLAT AUXILLIARY SDR AWXA9500773Wire · brokenPHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 1L. REPAIRED WIRES, OPS CHECK GOOD. (M)SDR AWXA9500730Pitot Tube · heat inopPHX/DEN - FLT NR 499 - AIR TURNBACK DUE TO LEFT ELEVATOR PITOT HEAT LIGHT ILLUMINATED DURING CRUISE. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT ELEVATOR PITOT TUBE. OPS AND LEAK CHECK GOOD. AIRCRAFT RSDR AWXA9500668Eel Battery Pack · dischargedPHX - DURING ROUTINE MAINTENANCE CHECK, FOUND LEFT EMERGENCY EXIT LIGHT IDENTIFIER INOPERATIVE. REMOVED AND REPLACED AFT OVERHEAD BATTERY PACK, SYSTEM OPS CHECK GOOD. (M)SDR AWXA9500663Skin · crackedPHX - DURING SCHEDULED C13 INSPECTION, FOUND 1 INCH CRACK IN FUSELAGE SKIN AT L2 DOOR LOWER HINGE CUTOUT LOWER FORWARD CORNER. FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 53-30-03, FIGURE 34. (M)SDR AWXA9500661Panel · crackedPHX - DURING SCHEDULED C13 INSPECTION, FOUND A .75 INCH CRACK IN LEFT SIDE OF KEEL BEAM SKIN AT STATION 685 BL 0. FABRICATED AND INSTALLED REPLACEMENT PANEL PER SRM 51-10-1 AND SRM 51-30-02. (M)SDR AWXA9500660Shear Tie · corrodedPHX - DURING SCHEDULED C13 INSPECTION, FOUND CORROSION BEYOND LIMITS ON SHEAR TIE AT STATION 930, OUTBOARD OF STRINGER 28L IN AFT CARGO PIT. FABRICATED AND INSTALLED SHEAR TIE PER SRM 53-10-4, FIGURE 8. (M)SDR AWXA9500659Stringer · corrodedPHX - DURING SCHEDULED C13 INSPECTION, FOUND CORROSION BEYOND LIMITS ON STRINGER 28L BS 910 IN AFT CARGO PIT. FABRICATED AND INSTALLED NEW STRINGER PER SRM 53-10-3 FIGURE 1. (M)SDR AWXA9500658Floor Beam · corrodedPHX - DURING SCHEDULED C13 INSPECTION, FOUND AFT CABIN FLOOR BEAM AT STATION 947 RBL 5 TO RBL 6 CORRODED BEYOND LIMITS. REPAIRED BEAM PER SRM 53-10-9. (M)SDR AWXA9500657Angle · crackedPHX - DURING SCHEDULED C13 INSPECTION, FOUND CRACK IN LT SIDE OF ZERO FLOOR SUPPORT ANGLE AT STATION 540 BL 0. INSTALLED NEW SUPPORT ANGLE PER SRM 51-10-1 AND SRM 51-30-2. (M)SDR AWXA9500656Hinge Cutout · crackedPHX - DURING SCHEDULED C13 INSPECTION, FOUND A CRACK IN L1 DOOR SKIN AT UPPER HINGE CUTOUT UPPER CORNER. ROUTED OUT CRACK PER SRM 52-00-2, PAGE 34. (M)SDR AWXA9500655Skin · crackedPHX - DURING SCHEDULED C13 INSPECTION, FOUND TWO CRACKS IN RT SIDE OF KEEL BEAM SKIN. A 2 INCH CRACK FOUND AT STATION 685 BL ZERO AND A 1.5 INCH CRACK FOUND AT STAITON 706 BL ZERO. FABRICATED PANEL 7075 T6 .080 INCH AND INSTALLED PER SRM 51-10-1 PAGE 5 AND SSDR AWXA9500654Stringer · corrodedPHX - DURING SCHEDULED C13 INSPECTION, FOUND STRINGER 28L AT BS 910 CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED STRINGER PER SRM 53-10-3. (M)SDR AWXA9500653Stringer · crackedPHX - DURING SCHEDULED C13 INSPECTION, FOUND CRACK IN FUSELAGE FRAME AT BS 360 BETWEEN STRINGER 20L AND STRINGER 21L. STOP DRILLED CRACK AND REPAIRED PER EO 53-11-04. (M)SDR AWXA9500652Floor Beam · corrodedPHX - DURING SCHEDULED C13 INSPECTION, FOUND AFT GALLEY FLOOR BEAM TOP CAP AT STATION 986.5 RBL 17 CORRODED BEYOND LIMITS. REMOVED AND REPLACED T-CAP PER SRM 53-10-09. (M)
Back to N147AW, cancelled Oct 17, 2014