N801FR, cancelled Jan 7, 2013
Service difficulty reports · 44
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 = 'N801FR' AND deregistration_id = 'N801FR-2013-01-07' 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 = 'N801FR' AND deregistration_id = 'N801FR-2013-01-07' 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 F3LA2012053000764Girt Bar · out of adjustL2 DOOR SLIDE DOES NOT SHOW ARMED IN FLIGHT SHOWS ARMED ON GROUND. FOUND L2 DOOR GIRT BAR FITTINGS OUT OF ADJUSTMENT. ADJUSTED GIRT BAR FITTINGS IAW AMM 52-13-22-820-056-A.SDR F3LA2012053000762Actuator · failedSTRONG ELECTRICAL/OIL ODOR FUMES IN COCKPIT AND CABIN ON CLIMB. RETURNED TO DEPARTURE. NR 1 PACK OVERHEAT FAULT. SHUTDOWN PACK, BLOWING VERY HOT AIR. REMOVE AND REPLACE NR 1 ACM IAW AMM 21-52-21 PB 401. OPS CHECKED GOOD.SDR F3LA2012003080720Shear Plate · crackedC-CHECK: FUSELAGE LT SIDE AT FRAME 68, STRINGER 23, LEFT LATERAL SHEAR PLATE CRACKED. R & R PLATE IAW SRM 51-42-11, PAR 6.B.SDR F3LA2012003070719Floorbeam · corrodedC-CHECK: MAIN CABIN FRAME 68 FLOOR PANEL FASTENER HOLES BETWEEN V1292, FLOORBEAM HAS CORROSION. BLENDED OUT CORROSION IAW SRM 51-73-00 PARAGRAPH 5. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-14, FIGURE 101, SHEET 1.SDR F3LA2012003060717Floorbeam · corrodedC-CHECK: MAIN CABIN FLOORBEAM HAS CORROSION AROUND FASTENER HOLES FRAME 66 TO FRAME 68, -Y765. R & R FLOORBEAM IAW SRM 51-42-11, PARAGRAPH 5.SDR F3LA2012003060716Frame Splice · corrodedC-CHECK: AFT GALLEY AREA FRAME 70, -Y1292 SPLICE PLATE (SHEAR PLATE) HAS CORROSION. R & R AFT GALLEY SHEAR PLATE IAW SRM 51-42-11, PARAGRAPH 17-18 AND EO AO-53EO-31 434, KIT PIN F9-531207DOL R02.SDR F3LA2012022800712Battery · failedBATTIERY 10 WL FAILED CAPACITY TEST IAW CARD A332204-02. REPLACED EPSU BATTERY 10 WL IAW AMM33-51-38-400-002-A.SDR F3LA2012020700705Engine · making metalABORTED TAKEOFF. UNUSUAL VIBRATION NOTED ON START OF NR 2 ENGINE DURING TAXI. NO ECAMS NOTED. ON APPLICATION OF TAKE OFF THRUST, A LOUD COMPRESSOR STALL, FLAMES NOTED BY TOWER FROM ENGINE REAR. ECAM FOR NR 2 OIL FILTER CLOGGED. IMMEDIATELY SECURED NR 2 ENSDR F3LA2010111400550Battery Pack · dischargedBATTERY PACK 12W FAILED CAPACITY CHECK IAW TASK CARD A332204-02. REPLACED ESPU 12WL IAW AMM 33-51-38, PB 401.SDR F3LA2010072500474Encoder · faultyREFERENCE HEAVY MAINTENANCE NON ROUTINE N0526. EMERGENCY LIGHT OPERATIONAL TEST FAILED WITH A CLASS 1 MESSAGE EPSU (11WL) AND (12WL). FOUND HIGH AND LOW CODING SWITCHES ON TERMINATION/CONNECTION BOX 3000RH8-DEU B TO BE CODED ONE NOTCH OFF. SET CODING POTENTSDR F3LA2010072500473Light · inoperativeREFERENCE HEAVY MAINTENANCE NON ROUTINE N0499. DURING TEST FORWARD EMERGENCY LIGHT 61WL WOULD NOT ILLUMINATE. TROUBLESHOT SYSTEM IAW A318 TSM 25-62-00-810-813. FOUND TWO BULBS BURNT OUT. REPLACED BULBS IAW A318 AMM 33-51-15 PAGE BLOCK 401. OPERATIONAL TESSDR F3LA2010072500472Flap · damagedREFERENCE HEAVY MAINTENANCE NON ROUTINE N0001. TEMPORARY REPAIR TO LIGHTNING STRIKE DAMAGE ON RIGHT WING OUTBOARD FLAP TRAILING EDGE 4.25 INCHES FROM OUTBOARD EDGE AND 3.5 INCHES FROM TRAILING EDGE. DAMAGE MEASURED 1.75 X 0.50 INCH. INSTALLED PERMANENT REPASDR F3LA2009042100078Computer · inoperativePILOT REPORTED AFTER TAKEOFF THE AIRCRAFT DID NOT AUTO TRIM, CONSTANT FORWARD PRESSURE WAS REQUIRED TO MAINTAIN DESIRED PITCH. SAME RESULT ON BOTH STICKS. AIRCRAFT TRIMMED NOSE UP IF NO STICK INPUT RUNAWAY NOSE UP. MAINTENANCE REMOVED AND REPLACED THE NR 2 SDR F3LA2008111900718Fitting · out of adjustDURING C4 C-CHECK, INSPECTION NOTED THE R2 DOOR ARMED HANDLE WAS SPONGY WHEN IN THE ARMED POSITION. MAINTENANCE ADJUSTED THE R2 GIRT BAR FITTING AND PERFORMED OPERATION CHECK IN ACCORDANCE WITH A318 AMM 52-13-00-820-001.SDR F3LA2008111800717Battery · failedDURING C4 C-CHECK, INSPECTION NOTED THAT THE EMERGENCY LIGHT TEST THROUGH THE CENTRALIZED FAULT DISPLAY UNIT FAILED OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY IN ACCORDANCE WITH AMM 33-51-38-000-001.SDR F3LA2008111800716Hook · wornDURING C4 C-CHECK, INSPECTION NOTED THAT DURING INSTALLATION OF THE ESCAPE SLIDE THE L2 DOOR HANDLE WAS ABLE TO MOVE INTO THE CLOSED POSITION BEFORE THE DOOR WAS CLOSED. MAINTENANCE REMOVED AND REPLACED THE DOOR HOOK IN ACCORDANCE WITH AMM 52-13-21-420-052.SDR F3LA2008111700713Hinge Fitting · gougedDURING C4 C-CHECK, INSPECTION NOTED THE RIGHT NR 4 SPOILER ANTI-ROTATION WEB FLAT WAS GOUGED. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH ENGINEERING AUTHORIZATION A8-57R-30776.SDR F3LA2008111700712Hinge Fitting · gougedDURING C4 C-CHECK, INSPECTION NOTED THE RIGHT NR 3 SPOILER ANTI-ROTATION WEB FLAT WAS GOUGED. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH ENGINEERING AUTHORIZATION A8-57R-30776.SDR F3LA200700379Battery Pack · inoperativeFLIGHT CREW REPORTED EPSU "13WL" AFT LEFT MESSAGE. REPLACED EPSU BATTERY AT 13WL LOCATION IAW AMM 33-51-38-400-002. OPS CHECK GOOD.
SDR F3LA200700108Oxygen Mask · no testWHILE PERFORMING MASK DROP TEST, ROWS 15 AND AFT ON BOTH SIDES, 7, 8, AND 9 RT SIDE, R2 DOOR AND C LAV DID NOT DROP COMPLETELY. RESET MASKS AND PERFORMED TEST AGAIN IAW AMM 35-23-00-710-001. OPS CHECKED GOOD.SDR F3LA200700101Shear Plate · corrodedDURING C-3 CHECK, INSPECTION REPORTED LT SIDE OF CABIN FLOOR WEB 69 AND 70 HAD VERY LIGHT CORROSION AT NUT PLATES, MOSTLY ON LWR SIDE. REPLACED SHEAR PLATE IAW SRM 51-42-11.SDR F3LA200700091Web · corrodedDURING C-3 CHECK, INSPECTION REPORTED RT SIDE CABIN FLOOR WEB 69 AND 70 HAD VERY LIGHT CORROSION AT NUT PLATES, MOSTLY ON LWR SIDE. REPLACED SHEAR PLATE IAW SRM 51-42-11.SDR F3LA200700107Floorbeam · damagedDURING C-3 CHECK, INSPECTION REPORTED FWD SPLICE OF R2 DOOR SILL HAD TWO DOUBLE DRILLED HOLES, ONE COMPLETELY THROUGH THE FWD FLOORBEAM. REPLACED DAMAGED FLOORBEAM IAW SRM 51-42-11.SDR F3LA200700106Floor Panel · corrodedDURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF AT R-2 DOOR CORRODED ON BOTTOM OF PANEL. REPLACED FLOORBOARD 262FF IAW AMM 53-42-12-400-001.SDR F3LA200700098Rib · scratchedDURING C-3 CHECK, INSPECTION REPORTED LE OF VERTICAL STAB FIN HAD DEEP SCRATCH MARKS (TOOL MARKS) BETWEEN PANELS NR 322BL AND 322CL ON ATTACHMENT BRACKET WHERE PANEL 322BL ATTACHES. REPLACED RIB FOR VERT STAB LE BETWEEN PANELS 322BL AND 322CL IAW SRM 51-42-11SDR F3LA200700099Latch · missingDURING C-3 CHECK, INSPECTION REPORTED AFT OTBD NUTPLATE FOR THE AFT FILLER PLATE AROUND THE L2 DOOR GIRT BAR LATCH MISSING. REPLACED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 AND 7.SDR F3LA200700097Splice · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON OTBD UPPER ANGLE AFT ATTACHMENT HOLE UPON REMOVAL OF L2 DOOR SILL SPLICE ANGLES FWD OF FR66. REPLACED L2 DOOR SILL SPLICE ANGLES IAW SRM 51-42-11, FIG 6 AND 7.SDR F3LA200700096Sill · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUTPLATE HOLE UNDER THE FWD GIRT FITTING ON THE L2 DOOR SILL. REPLACED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 AND 7.SDR F3LA200700095Sill · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUTPLATE HOLES ON THE L2 DOOR SILL PLATE AT FR66. REPLACED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 AND 7.SDR F3LA200700094Sill · corrodedDURING C-3 CHECK, INSPECTION REPORTED L2 DOOR SILL PLATE HAD CORROSION FWD OF FR66. REPLACED L2 DOOR SILL IAW 51-42-11, FIG 6 AND 7.SDR F3LA200700093Sill · corrodedDURING C-3 CHECK, INSPECTION REPORTED L2 DOOR SILL THRESHOLD HAD CORROSION AROUND SEVERAL NUTPLATE HOLES. REPLACED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 AND 7.SDR F3LA200700092Floorboard · corrodedDURING C-3 CHECK, INSPECTION REPORTED FLOORBOARD 222FF (R1 ENTRY) CORRODED. REPLACED FLOORBOARD 222FF IAW AMM 53-12-12-400-001.SDR F3LA200700100Sill · corrodedDURING C-3 CHECK, INSPECTION REPORTED R2 DOOR SILL PLATE CORRODED FWD OF FR66. REPLACED R2 DOOR SILL IAW SRM 51-42-11.SDR F3LA200700090Floorbeam · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM -Y1292, AFT OF FR68. REPLACED FLOORBEAM AT FR68 STATION -Y1292 IAW SRM 51-42-11.SDR F3LA200700088Floorbeam · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM Y1292 FWD OF FR68. REPLACED FLOORBEAM AT Y1292 FWD OF FR68 IAW SRM 51-42-11, FIG 6 AND 7.SDR F3LA200700087Floorbeam · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE ON FLOORBEAM Y1292, AFT OF FR66. REPLACED FLOORBEAM AT Y1292 AFT OF FR66 IAW SRM 51-42-11, FIG 6 AND 7.SDR F3LA200700089Floorbeam · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM Y1292 AFT OF FR68. REPLACED FLOORBEAM AT Y1292 AFT OF FR68 IAW 51-42-11, FIG 6 AND 7.SDR F3LA200700086Bushing · corrodedDURING C-3 CHECK, INSPECTION REPORTED NLG UPPER TORSION LINK FROM STRUT CORRODED INSIDE ATTACH LUG. REMOVED CORROSION UNDER BUSHINGS OF NLG UPPER TORSION LINK ATTACH POINT AND REPLACED BUSHINGS IAW EA NR A8-32R-11869.SDR F3LA200700085Bolt · corrodedDURING C-3 CHECK, INSPECTION REPORTED WINGLET ATTACH HARDWARE RUSTY. REPLACED WINGLET ATTACH HARDWARE (MILD SURFACE CORROSION ON BOLT HEADS) ON LT WING IAW AMM 57-31-22-400-001.SDR F3LA200600048Computer · failedAIR TURNBACK. FLIGHT CREW REPORTED AILERON SERVO ECAM ON CLIMB. NORMAL LAW WAS LOST. RETURNED TO DEN AND PERFORMED AN OVERWEIGHT LANDING WITHOUT INCIDENT. REPLACED ELAC NR 2 PER TSM 27-93-00-810-855. OPS CHECKED GOOD PER AMM 27-93-34. PERFORMED AFS LAND SDR F3LA200500042Computer · failedFLIGHT CREW REPORTED A BURNING ELECTRICAL ODOR 20 MIN OUT FROM DEN FL390. APPROXIMATELY 20 SEC AFTER ODOR BEGAN, ECAM ANTI-ICE CAPT L & R STAT ILLUMINATED. REPLACED PROBE HEAT COMPUTER PER MM 30-31-34, PB 401. COMPLIED WITH MM 24-00-00-810-823 AND 30-31-20-SDR F3LA200500037Cooling Fan · failedFLIGHT CREW REPORTED LIVE TV SMOKE DETECTION WARNING HORN SOUNDED DURING FLIGHT. LIVE TV FAN C/B 2000VU POPPED AND WOULD NOT RESET. REPLACED AFT RACK COOLING FAN PER AMM 44-25-00, PAGE 471. OPS CHECK GOOD.SDR F3LA200400070Sleeve · damagedFLIGHT CREW REPORTED NOSE WHEEL VIBRATION ON GEAR RETRACTION. FOUND NOSE WHEEL LT BEARING AND SLEEVE DAMAGED. REMOVED SLEEVE AND INSPECTED AXLE FOR DAMAGE. NO DAMAGE NOTED. INSTALLED SERVICEABLE AXLE SLEEVE AT LT POSITION PER AMM 32-41-12-000-002 AND 32-41SDR F3LA200400005Windshield · crackedAIR TURNBACK, FLIGHT CREW REPORTED FIRST OFFICER'S WINDSHIELD CRACKED. DECLARED AN EMERGENCY, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FIRST OFFICER'S WINDSHIELD PER 56-11-11-000-001 AND 56-11-11-400-001. PERFORMED TEST OF WINDOW HEAT AND DEFOGGING PER 30
Back to N801FR, cancelled Jan 7, 2013