Boeing 747-2D7B
Service difficulty reports · 726
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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 aircraft_model_key = '7472D7B' 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 aircraft_model_key = '7472D7B' 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 UIEA200300013Sensor · malfunctionedJFK/MXP - INFLIGHT ENGINE SHUTDOWN. NR 1 ENGINE N1 EXCEEDANCE DURING DESCENT PROFILER WHILE A/T ENGATED AND THROTTLES MOVING FORWARD. N1 136.9 PERCENT FOR 11 SECONDS. EGT 666, N2 92.4, F/F 3218. NR 1 ENGINE SHUTDOWN IAW FHB. PERFORMED ENGINE OVERSPEED INSSDR UIEA200200068Frame · crackedDURING CURRENT C-CHECK AT IAI, FOUND CRACK IN FRAME WEB AT BS 1265 WL 199 L/S CRITICAL HOLE. CRACK LENGTH IS 1MM. DURING CRACK REMOVAL BY REAMING THE FRAME WEB AND INNER CHORD WERE MISDRILLED. FRAME WEB ONLEY OVERSIZED TO .419 INCH. PERFORMED OPEN HOLE INSSDR UIEA200200069Fitting · damagedDURING CURRENT C-CHECK AT IAI, FOUND NR 4 INBOARD MID FLAP CARRIAGE SUPPORT RIB FITTING WITH ELONGATED MOUNT HOLES. HOLES OVERSIZED TO OBTAIN A CLEAN ROUND HOLE. PERFORMED OPEN HOLE E/C CHECK TO INSURE CRACK FREE CONDITION. NO CRACKS FOUND. FABRICATED REPASDR UIEA200200061Line · crackedAIR TURN BACK, NR 1 HYDRAULIC SYSTEM LEAKING. QUANTITY STOPPED AT 2 GALLONS AFTER PLACING EDP SWITCH TO DEPRESS. ADP WORKED NORMAL AFTER 20 MINUTES IN CONTINUOUS ADP PRESSURE DROPPED TO ZERO. FOUND LINE CRACKED AT CLAMP IN SAILBOAT AREA. REMOVED AND REPLACSDR UIEA200200055Hinge Fitting · wornDURING CURRENT C-CHECK AT SIAEC, FOUND NR 3 ENGINE LEFT AFT FAN COWL HINGE SUPPORT FITTING WITH WEAR DAMAGE IN THE LUG BORE HOLE. REAMED LUG BORE HOLE OVERSIZED TO .610 INCH. PERFORMED MAGNETIC PARTICLE INSPECTION FOR CRACKING. NO CRACKS FOUND. FABRICATED SDR UIEA200200049Sensor · malfunctionedNOSE GEAR DOOR LIGHT (RED) AND GEAR LIGHT REMAINED ON AFTER GEAR LEVER WAS RAISED. ATTEMPTED TO CORRECT PER FHB PROCEDURES TO NO AVAIL. AIR TURN BACK REQUIRED. JETTISONED APPROXIMATELY 70,000 KGS OF FUEL. LIFTED THE AIRCRAFT AND TROUBLESHOT PER MM. ALL GESDR UIEA200200035Control Unit · failedON CLIMBOUT, NR 3 AND NR 4 BUS TIES OPENED. SPLIT BUS SYSTEM OPEN. NR 3 GENERATOR WAS DISCONNECTED. NR 4 GENERATOR CHECKED GOOD VOLTS/ FREQ. NR 3 BUS LOST POWER AND COULD NOT REPOWER. DUMPED 17.0 KGS OF FUEL PRIOR TO LANDING. REMOVED AND REPLACED RIGHT SDR UIEA200200029Tee Chord · crackedInternal inspection of #4 pylon found aft horizontial flange of R/H Tee Chord cracked at NC 270 Bulkhead in area of upper link fitting. Crack is located at the end fastener hole.SDR UIE2002F00007Panel · separatedTURN BACK DUE TO ENGINE NR 1 AND ENGINE NR 4 GAP PANELS SEPARATED FROM AIRCRAFT ON TAKE OFF ROLL. INSTALLED NR 1 ENGINE GAP PANEL ISW SRM. REPAIRED NR 4 GAP PANEL PER SRM. REINSTALLED GAP PANEL ON NR 4 ENGINE IAW MM. CHAPTER 5 INSPECTION NOT REQUIRED. ACCSDR UIEA02009Structure · crackedDURING CURRENT C-CHECK AT KLM/AMS WHILE PERFORMING SB 747-53A2450, IAW AD 2001-16-02 AND HFEC OPEN HOLE INSPECTION REVEALED CRACKS EMINATING FROM THE AFT STRAP ROW AT BS 2231, STRINGER 25L. CUT OUT BLENDED CRACK IN STRAP. HFEC INSPECTED ROUTED AREA AND ALL OSDR UIEA02008Structure · crackedDURING CURRENT C-CHECK AT KLM/AMS WHILE PERFORMING SB 747-53A2450, IAW AD 2001-16-02 AND HFEC OPEN HOLE INSPECTION REVEALED CRACKS EMINATING FROM THE AFT STRAP ROW AT BS 2231, STRINGER 24R AND 25R. CUT OUT BLENDED CRACKS IN STRAP. HFEC INSPECTED ROUTED AREASSDR UIEA02007Spar · corrodedDURING CURRENT C-CHECK AT KLM/AMS, FOUND LEVEL 1 CORROSION ON THE L/W VERTICAL FLANGE OF THE LOWER FRONT SPAR CHORD BETWEEN ILES 630.72 AND 638 (INBOARD OF NR 2 PYLON). TAPER LOCK FASTENERS IN THE AFFECTED AREA WERE REMOVED. CORROSION BLENDED AND FASTENER HOSDR UIEA02006Clamp · looseLIM/MIA - NR 4 ENGINE FIRE LIGHT CAME ON CLIMBING THROUGH 20.0. BOTH A/B LOOPS WERE AT 9.0. FIRE SWITCH PULLED. FIRE BOTTLE WAS NOT FIRED. HYDRAULIC PUMP NR 4 IN SUPPLY OFF POSITION OR 1 PLUS 30 MINUTES. PERFORMED NACELLE OVERTEMPERATURE INSPECTION ON NR SDR UIEA01103Damper · malfunctionedDURING CLIMB-OUT FROM MIA PASSING FL 33, FELT ABRUPT UNCOMMANDED YAW OF AIRCRAFT. LOWER RUDDER INDICES SHOWED DISPLACEMENT 5 DEGREES RIGHT OF CENTER. UPPER RUDDER INDICES SHOWED CENTERED. TURNED OFF LOWER YAW DAMPER, CONDITION STOPPED. INITIATED RETURN TO SDR 2001F00207Anti-Ice System · malfunctionedDURING CLIMB-OUT, THE CREW NOTICED A STRONG BURNING SMELL IN THE COCKPIT. TURNED OFF R2 AND 3 WINDOW HEAT AND THE SMELL DISSIPATED. PULLED CB'S FOR L2-R3 AND L3-R2 WINDOW HEAT. AFTER APPROXIMATELY 3 MORE HOURS THE ODOR RETURNED. THIS TIME SMOKE CAME FROM LSDR UIEA01061Door Actuator · failedNR 2 AIR CONDITIONING PACK OVERHEATED WITH A DOOR OUT OF SEQUENCE INDICATION. CAUSED FUMES IN AIR CONDITIONING SYSTEM. MANUALLY POSITIONED NR 2 PACK INLET DOOR CLOSED. REPLACED INLET DOOR ACTUATOR. (M)SDR UIEA01057Skin · crackedDURING HFEC INSPECTION PER SB 747-53A2488 FOUND LOWER LOBE AFT CARGO COMPT DOOR UPPER FORWARD CUTOUT WITH TWO CRACK INDICATIONS, ONE FROM FASTENER HOLE TO RADIUS CUTOUT, THE OTHER 7MM LONG FROM FASTENER HOLE. AREA TRIMMED OUT. FILLER AND STACK DOUBLER FABRICSDR UIEA01059Bulkhead · crackedDURING INSPECTION OF NR 4 PYLON, FOUND THE REAR ENGINE MOUNT BULKHEAD UPPER T-CHORD L/S CRACKED (R/S PREVIOUSLY REPAIRED). TRIMMED CRACK AREA AWAY. OVERSIZED HOLES IN AFFECTED AREA. HFEC INSPECTED HOLES TO ENSURE CRACK FREE AREA. NO CRACKS FOUND. INSTALLESDR UIEA01056Fitting · corrodedDURING INSPECTION OF REMOVED LANDING GEAR FOUND CORROSION PITTING ON THE INBOARD TRUNNION SUPPORT BUSHING CAP OF THE LEFT BODY LANDING GEAR EXCEEDING SRM LIMITS. CORROSION CLEANED UP BY BLENDING AFFECTED AREAS. AREAS PLOTTED, MEASURED AND TREATED PER STANDARSDR UIEA01055Doubler · wornDURING INSPECTION OF NR 3 PYLON ACCESS PLATE CUTOUT (473AR) NAC STATION 290 WL 145, THE CONTACT AREA OF THE INNER SKIN TO LATCHES WAS FOUND WORN (THREE PLACES). AREAS TRIMMED OUT. HFEC INSPECTED AREAS FOR CRACKS, NONE FOUND. FABRICATED AND INSTALLED CRES-STSDR UIEA01058Fitting · crackedDURING HFEC INSPECTION PER SB 53A2390R1, FOUND BS 1480 L/S SPLICE PLATE FITTING HOLES NR 9 AND 10 WITH CRACK INDICATIONS. REMOVED LONGERON EXTENSION STRAP. REAMED HOLES TO REMOVE CRACKS. CONFIRMED NO CRACKS. FABRICATED BUSHINGS AND INSTALLED PER STANDARD PSDR UIEA01039Display · failedDURING CRUISE FLIGHT, RIGHT ENGINE INSTRUMENT DISPLAY FAILED, NR 2 EGT SPIKED UP AND FLIGHT CREW REPORTED SMOKE IN COCKPIT AND ELECTRICAL BURNING ODOR. SMOKE CLEARED AND FLIGHT CONTINUED TO DESTINATION. REMOVED AND REPLACED RIGHT ENGINE INSTRUMENT DISPLAY SCSDR UIEA01031Frame · crackedDURING HFEC INSPECTIN PER D6-7170 PART 6, 51-00-00, INSPECTION FOUND BS 2231 FRAME CRACK INDICATION AT STRINGER 25L. CRACK CONFIRMED. CRACK AREA TRIMMED OUT. FILLERS AND STRAP DOUBLERS FABRICATED. INSTALLED PER SRM 51-30-02 AND STANDARD PRACTICES. REF SB SDR UIEA01034Frame · damagedDURING ROUTINE INSPECTION, FOUND UPPER CHORD WITH CRITICAL HOLE ELONGATED AT BS 1265L AT WL 197. STACK UP DOUBLERS REMOVED. AREA CHECKED, PREVIOUS CRACKS CONTAINED. ALL HOLES IN STACK UP DOUBLERS OVERSIZED. OVERSIZED FASTENERS INSTALLED PER STANDARD PRACTISDR UIEA01035Angle · crackedDURING ROUTINE INSPECTION, FOUND CEILING ZEE CHORD ANGLE CRACKED IN LEFT BODY GEAR WHEEL WELL AT BS 1438 AND LBL 107. TRIMMED AWAY DAMAGED AREA. FABRICATED FILLER AND REPAIR ANGLES. INSTALLED PER STANDARD SRM PRACTICES. (M)SDR UIEA01036Skin · crackedDURING HFEC INSPECTION, FOUND UPPER FORWARD CORNER OF AFT LOWER LOBE CARGO COMPT CRACKED .87 INCHES AT BS 1815, STRINGER 27R. TRIMMED OUT CRACKED AREA. FABRICATED FILLER AND REPAIR STACK UP DOUBLERS PER SRM 53-30-03 FIG 60, TYPE II. INSTALLED PER SRM REPAIRSDR UIEA01037Skin · corrodedDURING INSPECTION, FOUND SKIN CORROSION AT 4L MED LOWER AFT CORNER CUT OUT. TRIMMED AWAY CORRODED AREA. FABRICATED FILLER AND REPAIR STACK UP DOUBLERS. INSTALLED FASTENERS PER STANDARD SRM 51-30-02 PRACTICES. (M)SDR UIEA01038Frame · crackedDURING INSPECTION, FOUND FRAME CRACKED STATION 800 STRINGER 17L ADJACENT TO 2L MED. STOP DRILL NOT REQUIRED DUE CRACK RAN OFF END OF FRAME. FABRICATED REPAIR STACK UP DOUBLERS. INSTALLED PER STANDARD SRM PRACTICES. REF SB 53-10-04 FIG 114. (M)SDR UIEA01029Skin · crackedDURING ROUTINE HFEC INSPECTION, FOUND SKIN CRACKED .33 INCH AT RADIUS CUT OUT, UPPER FORWARD CORNER OF LOWER LOBE AFT CARGO COMPARTMENT DOOR FRAME, BS 1815, AT STRINGER 15R. TRIMMED AWAY CRACK AREA FABRICATED FILLER AND REPAIR DOUBLERS PER SRM 53-30-03 FIG 6SDR UIEA01028Frame · dentedDURING ROUTINE INSPECTION, FOUND BS 1780 FRAME DENTED AND DEFORMED AT STRINGER 15R. TRIMMED AWAY DAMAGED AREA. FABRICATED FILLER, NEW SHEAR TIE, REPAIR DOUBLE AND SPLICES. INSTALLED PER STANDARD PRACTICES. (M)SDR UIEA01030Panel · delaminatedDURING ROUTINE INSPECTION, FOUND LEFT SIDE UNDER WING VAPOR BARRIER PANEL DELAMINATED IN SEVERAL AREAS FROM LBL 29.98 TO 103.95. DELAMINATED AREAS SANDWICHED WITH ALUMINUM PLATES AND THROUGH BOLTED. REPAIR AREA TO BE REINSPECTED FOR STRUCTURAL INTERGRITY ANDSDR UIEA00051Tire · failedFLT 8612 - FRA/JFK - ATB - CREW REPORTED EXCESSIVE VIBRATION AFTER V1. UPON INSPECTION OF RUNWAY, FRA AIRPORT AUTHORITIES FOUND PIECES OF HONEYCOMB PANEL, FLAP PANEL AND TIRES. AIRCRAFT RETURNED TO FRA. LANDING WAS UNEVENTFUL. UPON ARRIVAL ON THE RAMP AT FSDR UIEA00046Skin · corrodedDURING INSPECTION OF LEFT WING LEADING EDGE INTERIOR BAY, THE LOWER WING SKIN WAS FOUND CORRODED BOTH SIDES OF FSSO 1381.5. CORRODED AREA OF LEFT WING SKIN WAS CUT OUT, AREA TREATED, ECI CHECKED, FLAT PEENED. FILLER AND DOUBLER MANUFACTURED. INSTALLED IAW ASDR UIEA00040Structure · crackedDURING VISUAL INSPECTION OF FUSELAGE, THE MED NR 1L FORWARD LOWER REVEAL (STA 434) WAS FOUND CRACKED 1 INCH IN LENGTH HORIZONTALLY BELOW STOP NR 1 ON LOWER REVEAL. STOP DRILLED IAW SRM 51-10-01 AND BOEING TELEX AND 81180-3. TO BE REPLACED PRIOR TO 1,500 CYCLSDR 20010103AP008Frame · crackedDURING VISUAL INSPECTION OF AFT FUSELAGE INTERNAL RIGHT SIDE WALLS FOUND BENT KICKPLATE AT BS 1800. AFTER OPENING SIDE WALLS FOUND BS 1800 FRAME CRACK 3.5 INCHES BETWEEN STRINGER 10R AND 11R. FOUND FRAME STATION 1820 INNER CHORD DENTED BELOW STRINGER 12R. PSDR UIEA00042Frame · crackedDURING VISUAL INSPECTION OF AFT FUSELAGE INTERNAL RIGHT SIDE WALLS FOUND BENT KICKPLATE AT BS 1800. AFTER OPENING SIDE WALLS FOUND BS 1800 FRAME CRACK 3.5 INCHES BETWEEN STRINGER 10R AND 11R. FOUND FRAME STATION 1820 INNER CHORD DENTED BELOW STRINGER 12R. PSDR UIEA00041Spar · corrodedDURING VISUAL INSPECTION OF CENTER WING REAR SPAR, FOUND WEB CORROSION TO THE UPPER CHORD AT BS 1241 LBL 4. REMOVED CORROSION FROM WEB SURFACE IAW SRM 57-10-01. REMOVED FASTENERS IN UPPER CHORD. PERFORMED HFEC INSPECTIONS OF WEB AND FASTENER HOLES, NO CRACKSDR UIEA00039Skin · corrodedDURING VISUAL INSPECTION OF RT WING LOWER SURFACE, FOUND BULGING OF FIXED LEADING EDGE PANEL AT WING STATION 1322, FSSO 1339. REMOVED FASTENER AND FRONT SPAR FITTING. FOUND LOWER SKIN UPPER SURFACE PAD AREA CORRODED FORWARD OF FRONT SPAR. REMOVED CORROSION SDR UIEA00038Skin · corrodedDURING VISUAL INSPECTION OF LEFT WING LOWER SURFACE, FOUND SKIN CORROSION AROUND FASTENER HEADS AT WING STATION 1300 COMMON TO THE MID SPAR. REMOVED FASTENER, REMOVED CORROSION FROM SKIN SURFACE IAW SRM 57-30-01. PERFORMED HFEC INSPECTION OF SKIN AND FASTENESDR UIEA00037Fitting · crackedDURING VISUAL INSPECTION OF NR 1 PYLON, SUPPORT FITTING (P/N 65B94161-1) AT NAC 222 WAS DISCOVERED LOOSE. FURTHER INSPECTION AND DISASSEMBLY REVEALED THE ATTACHING BOLTS ON THE UPPER AND LOWE LEFT SIDE ATTACH POINTS WRE WORN AND THE SUPPORT FITTING BUSHINGS ESDR 20000816AP004Frame · crackedAT C-CHECK WHILE CONDUCTING A THROUGH VISUAL STRUCTURES INSPECTIONS, FOUND VERTICAL SUPPORT FRAMES OF RADAR SUPPORT ANTENNA CRACKED AT BS 140. LEFT SIDE CRACKED 3 INCHES FROM LOWER CLIP AREA. RIGHT SIDE CRACKED .5 INCH THROUGH ONE FASTENER AT LOWER CLIP. RESDR UIEA00029Structure · crackedLT LA7143 - MIA/ASU-ATB, AFTER TAKEOFF, CREW ADVISED THAT THEY WERE UNABLE TO PRESSURIZE THE AIRCRAFT. AFTER ABNORMAL CHECKLIST ACCOMPLISHED, CHECK OF MAIN DECK REVEALED NO ABNORMALITIES. DUMPED 80 KGS OF FUEL AND RETURNED TO MAI WAS UNEVENTFUL. MAINTENANCESDR UIEA00024Frame · crackedFOUND CRACK FROM FRAME WEB AT STATION 1265 RIGHT WL 199 CRITICAL HOLE FASTENER. STOP DRILLED CRACK, INSTALLED A STEEL FRAME WEB DOUBLER, INTERCOSTAL DOUBLER AND ATTACH ANGLE PER AMOC TO PARAGRAPH A AND C OF AD2000-02-01. (M)SDR UIEA00023Frame · crackedFOUND AFTER HFEC INSPECTION, CRACK FROM FRAME WEB AT STATION 1265 LEFT WL 199 HOLE A. REMOVED INTERIM REPAIR. STOP DRILLED CRACK, INSTALLED A FRAME WEB DOUBLER, INTERCOSTAL DOUBLER AND ATTACH ANGLE PER AMOC TO PARAGRAPH A AND C OF AD2000-02-01. (M)SDR UIEA00022Skin · crackedNOSE GEAR CUTOUT CORNER CRACKED AT STATION 240 STRINGER 40R. FOUND NO SECONDARY CRACKS. REPAIRED BY INSTALLING DOUBLER PER SB 747-53-2272. (M)SDR UIEA00021Fitting · misdrilledFOUND STATION 1480 STRINGER 39R FOUND TWO HOLES INSTALLED IN THE RADIUS. REMOVED CORNER FITTING, REDRILLED AND SLEEVED HOLES, REINSTALLED FITTING. INSTALLED FASTENERS PER SB 747-53A2390. (M)SDR UIEA200010Frame · crackedDOOR L5 FRAME CRACK INDICATION ON LOWER FORWARD FRAME NEAR DOOR FITTING CUTOUT. CONFIRMED CRACK INDICATION WITH FPI.. REPLACED FRAME P/N 65B05000-263 PER SRM 51-10-01. (M)SDR UIEA0004Fire Loop · inoperativeFLT 6137 - AMS-DXB - NR 2 ENGINE FIRE WARNING FAULT LIGHT CAME ON DURING THE TAKEOFF ROLL, ''B'' LOOP INDICATED 8 UNITS. WHEN AIRCRAFT BLOCKED IN, NR 2 ENGINE ''B'' LOOP FIRE WARNING READ 8 UNITS. FOR TROUBLESHOOTING FIRE WARNING CARDS WERE SWAPPED, BUT NO HSDR UIEA9996Bolt · looseINSPECTION OF NR 2 INBOARD AFT FLAP TRACK CARRIAGE BOGIE PIN ASSY REVEALED SAFETY BOLT MIGRATED OVER .50 INCH. NO PIN MIGRATION DUE PIN HELD IN PLACE BY ROLLER SUPPORT ROD. THIS CONFIGURATION DOES NOT REQUIRE SAFETY WIRE FROM BOLT TO PIN. REMOVED BOLT, INSPESDR UIEA9989Fire Warning · activatedFLT GT394 - CTS-ANC - DURING CRUISE, APU 'A' LOOP FIRE WARNING ILLUMINATED INTERMITTENTLY, WARNIGN HORN DID NOT SOUND. APU FIRE WARNING WAS SELECTED TO THE BOTH POSITION. SYSTEM CHECK WAS PERFORMED AND 'B' LOOP FAILED TEST. 'A' LOOP WAS SELECTED AND TESTED O
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