N313AW, cancelled Oct 13, 2011
Service difficulty reports · 261
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 = 'N313AW' AND deregistration_id = 'N313AW-2011-10-13' 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 = 'N313AW' AND deregistration_id = 'N313AW-2011-10-13' 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 AWXA200400438Skin · delaminatedMCN - MAJOR REPAIR - DURING C-17 CHECK FOUND THE L/H OUTBOARD AFT FLAP SEPARATING AT THE AFT INBOARD CORNER WS 230.68. MAINTENANCE PERFORMED A BOND REPAIR IAW B737-300 SRM 51-70-10, FIG. 10.SDR AWXA200301003Flashlight · inoperativeFLIGHT CREW REPORTED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300713Battery · dischargedEMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300005Floorbeam · crackedDURING C-16 CHECK, A .5000 INCH CRACK WAS FOUND ON LOWER FLOORBEAM TIE STRAP AT BS 340, STR 45 LT, JUST ABOVE AIR STAIR RAIL OUTBOARD END. MAINTENANCE STOP DRILLED END CRACK ON LOWER FLOORBEAM TIE STRAP AT BS 340; FABRICATED A REPAIR PLATE; REMOVED VERTICAL STSDR AWXA200300004Floorbeam · crackedDURING C-16 CHECK, A .5000 INCH CRACK WAS FOUND ON LOWER FLOORBEAM TIE STRAP AT BS 340 JUST ABOVE AIR STAIR RAIL RBL 24.75. MAINTENANCE STOP DRILLED HOLE ON LOWER FLOORBEAM TIE STRAP AT BS 340; FABRICATED A REPAIR PLATE; AND INSTALLED REPAIR PART IAW SRM.SDR AWXA200201245Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 663, STR 10 R/H. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 663, STR 10 R/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED REPASDR AWXA200201244Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 616, STR 2 R/H. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 616, STR 2 R/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED REPAIRSDR AWXA200201243Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 616, STR 1. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 616, STR 1; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED REPAIR PART IASDR AWXA200201242Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 616, STR 2 L/H. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 616, STR 2 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED REPAIRSDR AWXA200201241Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A 3/8" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 663, STR 10 L/H. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 663, STR 10 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED RESDR AWXA200300002Skin · crackedDURING C-16 CHECK, CORROSION AND 3 EACH .2500 INCH CRACKS WERE FOUND ON LOWER EXTERIOR FUSELAGE SKIN (LT AND RT KEELBEAM) AT BS 727+5 - BS 727+10, STR 27 LT - STR 27 RT. MAINTENANCE CUT SKIN FOR ACCESS TO KEEL BEAM; TRIMMED OUT DAMAGED AREAS OF OUTBOARD LOWERSDR AWXA200201257Skin · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A 1/2" CRACK WAS FOUND ON FUSELAGE SKIN AT THE UPPER HINGE CUTOUT OF THE L-2 DOOR, BS 951, STR 10 L/H. MAINTENANCE CUTOUT CRACKED AREA OF SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIRSDR AWXA200201249Slat · delaminatedYVR - MAJOR REPAIR - DURING C-16 CHECK THE #5 SLAT WAS FOUND DELAMINATED AT THE OUTBOARD UPPER TRAILING EDGE SURFACE. MAINTENANCE REMOVED THE #5 SLAT AND REPAIRED DAMAGE IAW B737-300 SRM 51-70-10 REPAIR 22 & 23. REINSTALLED #5 SLAT IAW BMM 27-81-21, PG. 401-41SDR AWXA200201258Control Cable · brokenDURING C-16 CHECK, FLAP FOLLOW UP CABLES WFFA, WFFB WERE FOUND TO HAVE LOW TENSION IAW TABLE 4, W/C 12B27001. WHILE APPLYING TENSION TO CABLES, CABLE WFFA BROKE .1250 INCH INSIDE THE TERMINAL DUE TO NUMEROUS BROKEN WIRE STRANDS. MAINTENANCE REMOVED AND REPLACSDR AWXA200201250Slat · delaminatedYVR - MAJOR REPAIR - DURING C-16 CHECK THE #4 SLAT WAS FOUND DELAMINATED AT THE INBOARD UPPER TRAILING EDGE SURFACE. MAINTENANCE REMOVED THE #4 SLAT AND REPAIRED DAMAGE IAW B737-300 SRM 51-70-10 REPAIR 22 & 23. REINSTALLED #4 SLAT IAW BMM 27-81-21, PG. 401-419SDR AWXA200200759Light · inoperativePHX - EEL - FLIGHT ATTENDANT REPORTED THAT EMERGENCY EXIT LIGHT IN FIRST CLASS WAS INOPERATIVE. REPLACED BULLNOSE LIGHT ASSEMBLY PER BMM 33-51-21-201, OPERATIONAL CHECK GOOD.SDR AWXA200200097Windshield · crackedGEG - DIVERSION - FLT 592 - O - EN ROUTE FROM GEG TO PHX AT FL 330 CABIN PRESSURE DIFFERENTIAL OF 7.8 PSI CAPTAINS WINDSHIELD OUTER PANE SHATTERED. EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED SAFELY TO BOI. MAINTENANCE ARRIVED AT BOI FROM PHX AND REPLACED TSDR AWXA200100610Wire · detachedYVR - EEL - "C" - DURING C-15 CHECK DISCOVERED BLACK WIRE PULLED OUT OF SPLICE IN FLOOR CONDUIT ON L/H SEAT MOUNTED ESCAPE PATH LIGHTING SEAT ROW 17. MAINTENANCE RE-SPLICED WIRE PER STANDARD WIRING PRACTICES MANUAL 20-30-12, PG. 3.SDR AWXA0001247Receiver · malfunctionedLAS - AIR TURNBACK 1/7/01 - ON APPROACH IN SLC THE CAPT''''''''S GLIDE SLOPE INDICATION WENT FULL DEFLECTION AND THE 1ST OFFICER''''''''S FULL DEFLECTION DOWN. TWO APPROACHES TRIED WITH THE SAME RESULT. THE AIRCRAFT RETURNED TO LAS AND BOTH GLIDE SLOPE INDICASDR AWXA0001033Seat Track · crackedSEAT TRACK ATTACH FRAME AT STA 727A TO 727B WL 207 RBL 45 CRACKED. REPAIRED IAW AWA ER 03-5310-00335-JS2SDR AWXA0001028Floorbeam · corrodedCORROSION ON FLOORBEAM AT STA 294 LBL 3 FOUND DURING CPCP INSPECTION EVALUATED AS LEVEL 1. CORROSION REMOVAL IAW SRM BEYOND LIMITS; REPAIRED FLOORBEAM IAW SRM 53-10-51 PG 220-222 FIG 205 SHT.3-4; PREPPED AND PAINTED IAW MM51-21-00SDR AWXA0001027Floorbeam · corrodedCORROSION ON FLOORBEAM AT STA 328 LBL 49 AND GOUGES IN FLOORBEAM UPPER CHORD AT RBL 22 AND 35; FOUND DURING CPCP INSPECTION EVALUATED AT LEVEL 1 CORROSION. CORROSION REMOVAL IAW SRM BEYOND LIMITS, GOUGES CLEANED UP IAW SRM 53-10-51 BEYOND LIMITS; REPAIRED FLOOSDR AWXA0001001Frame · crackedD: SEVERAL CRACKS FOUND BS 178 WL 185, 195, AND 207 AT AND BETWEEN LEFT AND RIGHT BL 5.6 AND 24.00 IN SIDE CHORDS, WEB AND FLOOR PANEL STRUCTUREC: REPAIRED ALL IAW EO 53-12-07SDR AWXA0001000Skin · damagedFUSELAGE SKIN FOUND DAMAGD STA 500A STR 3L. FABED AND INSTALLED REPAIR PARTS IAW SRM 53-00-01 FIG 202SDR AWXA0000997Skin · damagedD; FUSELAGE SKIN FOUND DAMAGD STA 500A STR 31C: FABED AND INSTALLED REPAIR IAW SRM 53-00-01 FIG 202SDR AWXA0000998Frame · crackedSEVERAL CRACKS FOUND BS 178 WL 185, 195, 207 AT AND BETWEEN LEFT AND RIGHT BL 5.6 AND 24.00 IN SIDE CHORDS, WEB AND FLOOR PANEL STRUCTURE. REPAIRED ALL IAW EO 53-12-07.SDR AWXA9900413Bulkhead · crackedC-CHECK, CABIN STA 663.75 LBL 32, WHEEL WELL PRESSURE DECK HAD 1 .4375 CRACK. HFEC VERIFIED CRACK. REMOVED DAMAGED AREA, FABRICATED DOUBLER, TREATED, PRIMED, AND INSTALLED PARTS PER ER 03-5310-99288-EY1. FABRICATED REPAIR DOUBLER FROM 2024T3 X .050 R700212,SDR AWXA9900412Seat Track · corrodedC-CHECK, CORROSION ON SEAT TRACK AT RIGHT OUTBD FS 500B-500D OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK PER SRM 51-40-02, FABRICATED SEAT TRACK FROM BAC 1520-792/7178T6 PER SRM 53-30-52 R659935, TREATED AND PRIMED PER SRM 51-20-01 AND INSTALLED PER SRM 51-40-SDR AWXA9900411Skin · creasedC-CHECK, TWO SMALL DENTS 5 FEET FWD OF FWD CARGO DOOR, FS 380 STR 24R. CREASE IN BOTTOM OF DENTS OUT OF LIMITS. REMOVED DAMAGE, NDT REVEALED NO CRACKS. FABRICATED REPAIR PARTS FROM 2024T3 X.063 R699111 2024T3 X.050 R697963. INSTALLED CONICAL WASHERS, ALODSDR AWXA9900410Skin · gougedC-CHECK, RIGHT O/B MID FLAP AT I/B TRACK IS GOUGED ON LWR L/E SURFACE. REMOVED DAMAGED AREA, FABRICATED REPLACEMENT DOUBLER FROM .032301 CRES 1/2 HARD MATERIAL, IAW SRM 57-53-01. TREATED AND PRIMED IAW SRM 51-20-01. INSTALLED DOUBLER IAW SRM 57-53-01.SDR AWXA9900409Skin · crackedC-CHECK, CRACK IN FUSLAGE SKIN AT LWR AFT CORNER OF R1 DOOR HAD CRACKS EXTENDING FROM 2 FASTENER HOLES. REMOVED FASTENERS AND REAMED HOLES TO .25 IAW SRM 53-10-01, HFEC REVEALED INTERIOR CRACKS, EXTERIOR CRACKS ARE CONTAINED AT FASTENER HOLES. INSTALLED FLUSSDR AWXA9900408Intercostal · corrodedC-CHECK, AFT PIT STA 787-793, STR 25R INTERCOSTAL HAD CORROSION ON UPPER FLANGE AT NUT PLATE ATTACH AREAS. REMOVED CORRODED INTERCOSTAL, FABRICATED, TREATED, AND PRIMED REPAIR PART AND INSTALLED PER SRM 53-60-15, 51-40-12 AND 51-10-1.SDR AWXA9900336Fan · failedDURING DESCENT, FA REPORTED ELECTRICAL SMELL IN AFT GALLEY, CYCLING RECIRC FAN MADE DIFFERENCE INSTANTLY. REPLACED RECIRC FAN PER MM 21-21-22 PG 401. NONE RELATED RECOMMENDATION.SDR AWXA9900069Panel · leakingEMERGENCY LANDING, INFLIGHT RIGHT WING FUEL LEAK. NON REV PILOT REPORTED FLUID LEAK ON RT WING UNDETERMINED QTY, TYPE, AND SOURCE. CAPTAIN INITIATED AN EMERGENCY LANDING. REMOVED AND REPLACED UPPER PANEL ON WING JUST AFT OF PYLON, LEAK CK GOOD, NO LEAKS.SDR AWXA9700666Compressor · failedAIR TURNBACK FOR SMOKE IN CABIN AND AFT LT LAV SMOKE DETECTOR SOUNDING. FOUND OIL IN HIGH PRESSURE COMPRESSOR OF NR 2 ENGINE. REMOVED AND REPLACED ENGINE. REPLACED SMOKE DETECTOR AS NO SMOKE WAS NOTED IN CABIN ONLY OIL SMELL.SDR AWXA9700484Air Distribution · odorBURNED SMELL NOTED BY CABIN AND FLIGHT DECK CREW. RECIRCULATION FAN TURNED OFF AND SMELL DIMINISHED. RAN RECIRCULATION FAN AT GATE DURING TURN. NO BURN SMELL, OPS CHECK NORMAL.SDR AWXA9700431Check Valve · inoperativeAIR TURNBACK, AFTER ROTATION, SMELLED A HOT ELECTRIC SMELL. SHUT DOWN RECIRCULATION FAN AND SMELL WENT AWAY. APPROXIMATELY 15 MIN INTO FLIGHT, COOLING EXHAUST LIGHT ILLUMINATED. SWITCHED TO ALTERNATE FAN AND RESET CIRCUIT BREAKERS WITH NOT EFFECT. REMOVED SDR AWXA9700312Control Cable · misriggedLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOLLOWED QRH PROCEDURES AND RETRACTED GEAR. FOUND TELEFLEX CABLE AND AIR SAFETY SENSOR NOT RIGGED PER MM. CORRECTED PER MM 32-09-01.SDR AWXA9700051Carriage Assy · wornCREW REPORTED DURING FLAP SELECT 15 TO 40 DEGREES, THE A/C ROLLED TO THE LEFT WHICH REQUIRED 7 UNITS OF RT RUDDER TRIM TO LEVEL. LANDING WAS MADE WITHOUT INCIDENT. UNITED MAINTENANCE COULD FIND NO OBVIOUS DEFECTS, MADE REQUIRED LOGBOOK ENTRY FOR MAINTENANCESDR 97ZZZX113Drag Brace · damagedDRAG BRACE SENT FOR REPAIR. BEARING MIGRATED FROM LOCATION CAUSING DAMAGE TO BRACE DURING GEAR ACTUATION. BEARING INSTALLED AND TESTED PER BAC OHM 32-01-03. CAUSE OF MIGRATION IS UNKNOWN.SDR AWXA960517Skin · crackedDURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND SEVERAL SMALL CRACKS IN OUTER SKIN COMING FROM RIVETS AT CENTER INBOARD STOP MOUNT ON NR 1 SLAT. REPAIRED PER DWG 65C30133PT2. (M)SDR AWXA960516Floor Beam · corrodedDURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 344, LBL 28 TO LBL 56 IN NUMEROUS PLACES. REMOVED UPPER CHORD, FABRICATED AND INSTALLED REPLACEMENT AT BS 344, IAW SRM 53-10-51. (M)SDR AWXA960515Mopsill · corrodedPAE - FLT 7818 - DURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND CORROSION ON FORWARD ENTRY DOOR MOPSILL, STATION 304-328, LBL 42. REMOVED AND REPLACED FORWARD MOPSILL, STATION 304-328, LBL 42 PER SRM 51-10-02. (M)SDR AWXA960518Floor Beam · corrodedPAE - FLT 7818 - DURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 328 - LBL 28. REPAIRED FLOOR BEAM AT BS 328, LBL 28 TO 65 PER SRM 53-10-51. (M)SDR AWXA960266Actuator · failedLAS/SNA - FLT 0806 - AIR TURNBACK. ON TAKEOFF FROM LAS AT 200 FEET, HAD A STICK SHAKER FOR 25 SECONDS AT 170 KIAS. LEADING EDGE FLAP ANNUNCIATOR LIGHTS FLASHING BETWEEN TRANSIT EXT. AND L/E DEVICES OVERHEAD ANNUNCIATOR PANEL SHOWED NR 5 SLAT GOING BETWEEN EXSDR AWXA960113Window · crackedLAS - FLT 192 - AIR TURN BACK, CLIMBING THROUGH 18000 MSL, CAPTAINS WINDSHIELD BEGAN ARCING BADLY. THEN HEARD A DISTINCT POP AND IMMEDIATELY NOTICED A LARGE CRACK. REMOVED AND REPLACED LEFT WINDOW PER T/C R1B56001. REPLACED LEFT WINDOW CONTROLLER PER GPP. SDR 96ZZZM678Controller · malfunctionedLAS - FLT 192 - AIR TURN BACK, CLIMBING THROUGH 18000 MSL, CAPTAINS WINDSHIELD BEGAN ARCING BADLY. THEN HEARD A DISTINCT POP AND IMMEDIATELY NOTICED A LARGE CRACK. REMOVED AND REPLACED LEFT WINDOW PER T/C R1B56001. REPLACED LEFT WINDOW CONTROLLER PER GPP. SDR AWXA960012Wire · brokenPHX - FLT 0226 - DURING ROUTINE MAINTENANCE CHECK, FOUND INTERIOR EMERGENCY LIGHTING FOR AFT DOOR EXIT PATHWAYS INOPERATIVE. REPAIRED AND REPINNED WIRE AT PIN 2. SYSTEM OPS CHECKED GOOD. (X)SDR AWXA9500713Hose · failedPHX - FLT 460 - DURING FINAL APPROACH TO PHX, THE B-SYSTEM HYDRAULIC QUANTITY STARTED DECREASING. B-SYSTEM WAS SHUT DOWN AND AIRCRAFT CONTINUED TO PHX, LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC PRESSURE LINE FROM PUMP TO HYDRALIC PRESSURE MODUSDR AWXA9500598Skin · damagedPHX - DURING SCHEDULED C9 INSPECTION, FOUND LIGHTNING STRIKE DAMAGE TO SKIN THAT EXCEEDED SRM LIMITS AT STATION 364 STRINGER 6L. CLEANED AREA AND REPAIRED PER SRM 53-00-01, FIGURE 201. (M)
Back to N313AW, cancelled Oct 13, 2011