Boeing 747-243B
Service difficulty reports · 506
Newest first. General aviation reporting is voluntary.
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 = '747243B' 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 = '747243B' 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 UIEA200600005Controller · malfunctionedNR 3 PACK CONTROL CIRCUIT BREAKER ON P6 PANEL TRIPPED AFTER TAKEOF. STRONG ELECTRICAL ODOR DETECTED NEAR POSITION E-L. SMELL DISIPATED AFTER 3 HOURS. CIRCUIT BREAKER NOT RESETSDR UIEA200500033Seat Track · damagedMAINTENANCE PICK UP DURING DAILY CHECK, FOUND MAIN DECK SEAT TRACK DAMAGED AT STATION 1730. CUT OUT DAMAGED AREA AND REPAIRED PER SRM 53-10-05 FIG 1A. (M)SDR UIEA200400202Shutoff Valve · leakingDURING CRUISE, LOSS OF FLUID NR 4 HYD SYSTEM. SYSTEM DEPRESSURIZED AT 2.0 GALS QUALITY. EDP TO SUPPLY OFF. FOUND NR 4 RUDDER CONTROL SHUTOFF VALVE FAILED. (LEAKED) REMOVED AND REPLACED NR 4 RUDDER SHUTOFF VALVE. OPS AND LEAD CHECK GOOD IAW MM. (K)SDR UIEA200400200Sensor · failedIMMEDIATELY AFT T/O, STALL WARNING, STICK SHAKER ACTIVATED ASSOCIATED WITH STALL WARNING. (POWER OFF) LIGHT ILLUMINATION ON PILOTS OVERHEAD PANEL. REMOVED AND REPLACED LT ANGLE OF ATTACK SENSOR. OPS CHECK NORMAL IAW MM.SDR UIEA200400178Actuator · malfunctionedON TAKEOFF OUT OF BOG, A NOISE WAS HEARD RIGHT AT ROTATION. ALL SYSTEMS INDICATED NOTHING ABNORMAL. HOWEVER, WHEN THE GEAR WAS RETRACTED THE RIGHT BODY GEAR PRI AND ALT DOOR LIGHTS WERE ON ALONG WITH THE RED DOOR OPEN AND RED GEAR LIGHTS. THE LIGHTS EXTINGUSDR UIEA200400174Connector · inoperativeAIRCRAFT EMERGENCY LIGHT FLICKER MOST OF THE FLIGHT. FOUND SEVERAL PUSHED BACK PINS AT CONNECTOR EMERGENCY LIGHT PANEL. ACCOMPLISHED GROUND CHECK OK PER MM 33-51-10. (M)SDR UIEA200400172Indicator · failedCAPTAINS ADI FAILED. INSTRUMENT WARNING LIGHT AND ATTITUDE LIGHT, UNABLE OT SWITCH TO NR 3 INU DUE TO BEING INOPERATIVE. REMOVED AND REPLACED CAPTAINS ADI IAW MM 34-41-05, OPS NORMAL. REMOVED AND REPLACED NR 1 AND NR 3 INU IAW MM 34-41-03 CHECKS ALL SYSTEM SDR UIEA200400175Relay · inoperativeEMERGENCY LIGHT FLICKER DURING FLIGHT. FOUND RELAYS ON EMERGENCY LIGHTS UNSECURED, RESECURED RELAYS OPS CHECK OK IAW MM 33-51-07. REMOVED AND REPLACED BOTH RELAYS ON EMERGENCY LIGHT CNTL PANEL LIGHTS OPS OK PER MM 33-51-07. (M)SDR UIEA200400156Line · brokenAFTER TAKEOFF NR 4 ENGINE FIRE WARNING SOUND. PEAK EGT 976 FOR 11 SECONDS. GOT A RED BALL, SHUTDOWN THE ENGINE IAW FHB FIRE INDICATION WENT OUT WHEN NR 4 ENGINE FIRE SWITCH WAS PULLED. PERFORMED NR 4 ENGINE VISUAL INSPECTION NO EVIDENCE OF FIRE. PERFORMED SDR UIEA200400145Skin · scratchedDURING SCHEDULE MAINTENANCE, FUSELAGE SKIN DAMAGE WAS FOUND ADJACENT TO THE CARGO DOOR. THE SKIN DAMAGE WAS REMOVED BY BLENDING OUT THE DAMGAE. NO FASTENERS WRE AFFECTED BY THE BLEND OPERATION. HFEC SURFACE INSPECTED TO ENSURE NO DEFECTS EXIST. BOEING ADVISDR UIEA200400144Floorbeam · crackedDURING INCORPORATION OF SB 747-53A2459, FOUND CRACK AND OR ELONGATED FASTENER HOLES COMMON TO FRAMES AND UPPER DECK FLOORBEAM UPPER CHORDS AT BS 340/360. FLOORBEAM UPPER CHORDS AND WEBS REPAIRED PER SRM. AT BS 340, STOP DRILLED AND REPAIRED FRAME WEB. OPEN SDR UIEA200400141Relief Valve · leakingRHI/MXP - NR 1 ENGINE WOULD NOT ATTAIN REQUIRED THRUST FOR T/OFF. WOULD ONLY ATTAIN 108.5 AGAINST THE STOP. ALL OTHER INDICATIONS NORMAL. NR 3 ENG WOULD NT ATTAIN REQUIRED THRUST FOR T/OFF. WOULD ONLY ATTAIN 110.0 AGAINST THE STOP. ALL OTHER INDICATIONS NSDR UIEA200400136Connector · damagedAFTER TAKEOFF, NR 4 ENGINE INTERMITTENT FIRE WARNING 'A' LOOP FLUCTUATED. HOWEVER, 'B' LOOP DMI INOPERATIVE. SHUTDOWN NR 4 ENGINE JETTISION FUEL AND RETURNED. CLEANED AND CHECKED ALL CONNECTOR OF NR 4 ENGINE 'A' LOOP. NO FAULT FOUND AND GROUND TEST OK AS PSDR UIEA200400114Acm · unserviceableAFTER TAKEOFF, NR 3 AIR CONDITIONING PACK STARTED MAKING LOW RUMBLING SOUND. SMELLED BURNING ODOR, TURNED NR 3 PACK OFF FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED NR 3 AIR CYCLE MACHINE. GROUND OPERATION CHECK NORMAL IAW MM.SDR UIEA200400113Fuel Filter · contaminatedNR 1 ENGINE FAILED DURING CRUISE, FLIGHT LEVEL 350, .84 MACH, NORMAL FLIGHT. FOLLOWED PROCEDURES AND ATTEMPTED TO RESTART ENGINE WITH NO SUCCESS. ACCOMPLISHED ENGINE INLET AND EXHAUST INSPECTION ALL NORMAL. REPLACED NR 1 ENGINE FUEL FILTER IAW MM, LEAK CHECKSDR UIEA200400111Handle · malfunctionedDUE TO GEAR DOOR OPEN INDICATION: AFTER GEAR RETRACTION, RED DOOR OPEN LIGHT REMAINED ILLUMINATED. RAN SECTION 3 PROCEDURES, LT WING GEAR DOOR OPEN LIGHT ILLUMINATES WITH PRIMARY AND ALTERNATE DOOR SELECTION SWITCHES. DOOR IS OPEN WITH AIRCRAFT RUMBLE. UP OSDR UIEA200400112Beam · crackedLT WING FIXED LEADING EDGE NOSE BEAM UPPER CHORD AND LOWER CHORD AND WEB CRACKED AT ILES 1116.00. REMOVED FASTENERS IAW SRM, REMOVED DAMAGED UPPER AND LOWER CHORD BY CUTOUT METHOD IAW SRM REMOVED WEB IAW SRM. FABRICATED UPPER, AND LOWER CHORDS FROM SRM. FABSDR UIEA200400110Antenna · inoperativeATB DUE TO BOTH RADARS INOPERATIVE: AFTER LEVEL OFF, BOTH RADAR SCREENS INOPERATIVE. SHOWED BLUE AZIMUTH LINES, BUT NO RANGE OR SWEEP. REPLACED RADAR ANTENNA. OPERATION CK IAW MM, ALL NORMAL. NOTE: NO FUEL DUMPED.SDR P5CA0401085Accumulator · leakingAFTER ENG START, NR 1 AND 4 LOST HYD SYSTEM QTY. REPLACED BRAKE ACCUMULATOR AS PER MM 32-41-23. OPS AND LEAK CK NORMAL. RESTARTED NR 1 AND 4, HYD SYSTEM TO PROPER LEVEL.SDR UIEA200400087Cadc · inoperativeMIA-JFK - APPROXIMATELY 45 MINUTES DURING CRUISE, NR 1 CADC POWER C/B OPENED. C/B RESET PER FHB PROCEDURES. C/B OPENED AGAIN AND WAS LEFT OPENED FOR DURATIONOF FLIGHT. NY MAINTENANCE CONTROL DIVERT A/C TO MIA. REMOVED AND REPLACED NR 1 CADC OPERATION CHECKSDR UIEA200400069Rib · crackedFOUND INTERIOR RIB CRACKED AT NAC STA 318.20 RIGHT SIDE NR 3 PYLON LOWER AREA. DEFECT RECTIFIED AS PER TARNSIT W/O 71181467000001 IAW BOEING DRAWING 65B94117 REV E, 65B89043 REV D, 65B89044 REV B, AND BOEING SEP-SIN-04-00049H. (M)SDR UIEA200400070Rib · crackedFOUND INTERIOR RIB CRACKED AT NAC STA 300 LEFT SIDE NR 3 PYLON LOWER AREA. DEFECT RECTIFIED AS PER TRANSIT W/O 71181467000001 IAW BOEING DRAWING 65B94117 REV E, 65B89043 REV D, 65B89044 REV B, AND BOEING SEP-SIN-04-00049H. (M)SDR UIEA200400072Skin · corrodedFOUND WING TOP SIDE SKIN CORROSION WSTA 440.62 STRINGER 19. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M)SDR UIEA200400075Skin · corrodedFOUND LEFT WING TOP SIDE SKIN CORRODED WSTA 1392 STRINGER 15. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M)SDR UIEA200400076Skin · corrodedFOUND LEFT WING LOWER SKIN CORROSION AROUND SURGE TANK SUMP DRAIN VALVE AT WS 1487. CORROSION BLENDED OUT AND REPAIRED AS PER FAA FORM 8110-3 DATED 19 JAN 2004, COPY ATTACHED FOR DETAILS OF HFEC INSPECTION REF COPY OF ATTACHED SJC A00064. (M)SDR UIEA200400073Skin · corrodedFOUND LEFT WING TOP SIDE SKIN CORROSION WS 1434 STRINGER 13. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M)SDR UIEA200400071Skin · corrodedFOUND LEFT WING TOP SIDE SKIN CORROSION WSTA 697 STRINGER 27. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M)SDR UIEA200400074Skin · corrodedFOUND LEFT WING TOP SIDE SKIN CORRODED WSTA 1454 STRINGER 15. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M)SDR UIEA200400078Keelbeam · corrodedFOUND RIGHT WING GEAR WHEEL WELL KEELBEAM TOP SURFACE AT BS 1265, CORRODED AROUND FASTENERS LOCATION. KEEL BEAM CORRODED TOP WEB SURFACE REPLACEMENT CARRIED OUT AS PER SRM 51-10-01 AND SRM 51-30-02. (M)SDR UIEA200400080Angle · crackedFOUND RT WING T/E UPPER FIXED PANEL LONGITUDINAL SUPPORT BEAM FORWARD L-ANGLE CRACK AT WBL 130.0. REPLACED CRACKED SUPPORT ANGLE WRT SRM 51-30-02. (M)SDR UIEA200400079Angle · crackedFOUND RT WING T/E LOWER ACCESS PANEL SUPPORT BEAM AFT L-ANGLE CRACK AT WS 670. REPLACED CRACKED PANEL SUPPORT BEAM ATTACH CLIP 'L' ANGLE WRT SRM 51-30-02. (M)SDR UIEA200400077Frame · corrodedFOUND RT WING GEAR WHEEL WELL BS 1350 BULKHEAD LOWER CHORD HORIZONTAL FLANGE AT RBL 50, LOWER SURFACE CORRODED. CORROSION REMOVED IAW SRM 51-10-01 FOUGN TO BE WITHIN LIMITS IAW SRM 53-10-01 FIG 1. AREA REPROTECTED IAW SRM 51-10-02. REMAINING THICKNESS 1.140SDR UIEA200400059Skin · corrodedFOUND LT WING TOP SKIN CORROSION WS 1280 STRINGER 14. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1 AREA WAS REPROTECTED AND PRIMED IAW SRM 57-30-01. (M)SDR UIEA200400064Rib · crackedFOUND KEELBEAM VERTICAL SUPPORT ANGLES AT STATION 1000 LT AND RT SIDES CRACKED. SUPPORT ANGLES REPLACED IAW SRM 51-10-01 AND SRM 51-30-02. (M)SDR UIEA200400063Spar · crackedFOUND LEFT WING UPPER MID SPAR WEB SURFACE FROM MSS 446.41 TO MSS 475.62 FOUND 2 CRACKS OF 5MM AND 16MM IN LENGTH REF TO NDT REPORT NR 276/03. CARRIED OUT HFEC INSPECTION ON THE CUTOUT SURFACE WEB AS PER NTM PART 6 51-00-00 FIG 4. NIL CRACK INDICATED. CRACKSDR UIEA200400062Bushing · crackedFOUND LEFT WING WALKING BEAM SUPPORT FITTING ASSEMBLY. FORWARD BEARING HOUSING OUTBOARD UPPER/FWD BOLT HOLE LOCATION ON REAR SPAR STIFFENER WAS FOUND WITH A CRACKED BUSHING HOLE AND BUSHING WAS ALSO FOUND WORN. CRACKED HOLE REPAIRED AS PER SB 747-57-2226 REVSDR UIEA200400061Skin · corrodedFOUND LEFT WING TOP SKIN CORROSON WS 323.82.00 STRINGER 27. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1 AREA WAS REPROTECTED AND PRIMED IAW SRM 57-30-01. (M)SDR UIEA200400066Angle · crackedFOUND RIGHT WING T/E UPPER FIXED PANEL HORIZONTAL SUPPORT BEAM L-ANGLE CRACKED AT WING STATION 400. REPLACED CRACKED ANGLE WRT SRM 51-30-02. (M)SDR UIEA200400065Rib · crackedFOUND INTERIOR RIB CRACKED AT NAC STATION 220 RIGHT SIDE. DEFECT RECTIFIED AS PER TRANSIT W/O 71181467000001 IAW BOEING DRAWING 65B94117 REV E, 65B89043 REV D, 65B89044 REV B, AND BOEING RES SIN-04-00049H. (M)SDR UIEA200400058Panel · corrodedFOUND LEFT WING STATION 715, WBL 433, BULGE ON THE T/E F/G PANEL RABBET AREA AT REAR SPAR WING TOP SKIN. CORROSION FOUND ON WING TOP SKIN AFT OF REAR SPAR CORROSION BLENDED OUT WITHIN LIMITS OF SRM 57-30-01. AREA REPROTECTED AND PRIMER APPLIED IAW 57-30-01. SDR UIEA200400057Panel · corrodedFOUND LEFT WING STATION 715, WBL 433, BULGE ON THE T/E F/G PANEL RABBET AREA AT REAR SPAR WING STOP SKIN. CORROSION FOUND ON WING TOP SKIN AFT OF REAR SPAR CORROSION BLENDED OUT WITHIN LIMITS OF SRM 57-30-01. AREA REPORTECTED AND PRIMER APPLIED IAW 57-30-01.SDR UIEA200400060Skin · corrodedFOUND LEFT WING TOP SKIN CORROSION WS 1280 STRINGER 18. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1 AREA WAS REPROTECTED AND PRIMED IAW SRM 57-30-01. (M)SDR UIEA200400067Stringer · corrodedFOUND AFT CARGO STRINGER AT STATION 1750 RIGHT SIDE STRINGER 44 FOUND CORRODED. STRINGER REPAIRED AT STATED LOCATION CARRIED OUT AS PER SRM 53-10-03 FIG 1. (M)SDR UIEA200400052Seat Track · damagedUPPER DECK SEAT TRACK CROWN HAS 2 OF THE LIPS SHEARED OFF AT STATION 660 LBL 46.65. DAMAGED SEAT TRACK SECTION TRIMMED OUT AND REPAIR SECTION SPLICED ON IAW SRM 53-10-05. (M)SDR UIEA200400054Rib · crackedFOUND LEFT WING LE PARTIAL RIB AT ILES 414.5 HAS A 4.5 INCH CRACK LONGITUDAL ACROSS ITS WEB JUST BEHIND THE FORWARD RIB SECTION. CRACKED WEB REPAIRED PER SRM 51-40-02. (M)SDR UIEA200400056Panel · corrodedFOUND LEFT WING TOP SKIN FIXED T/E FIBERGLASS PANEL BULGING AT RABBET AREA AFT OF REAR SPAR BETWEEN WBL 198.6 TO 204.6. CORROSION FOUND ON WING TOP SKIN AFT OF REAR SPAR CORROSION BLENDED OUT WITHIN LIMITS OF SRM 57-30-01. AREA REPROTECTED AND PRIMER APPLIEDSDR UIEA200400055Rib · crackedFOUND RT WING LEADING EDGE RIB AT ILES 330 FOUND WITH A 1.25 INCH LONG CRACK ON THE WEB ALONG THE LOWER ANGLE AT AFT EDGE. REPLACED CRACKED LEADING EDGE RIB WEB WRT SRM 51-30-02. (M)SDR UIEA200400053Cap · crackedFOUND RT WING LEADING EDGE NOSE CAP AT LES 1042 FOUND 4.25 INCH LONG SPANWISE CRACK PROPERGATED FROM WING ANTI-ICE DUCT. RIGHT WING LEADING EDGE NOSE BEAM CRACKED WEB REPAIRED AS PER FAA FORM 8110-3 REF SJC NR A00063. (M)SDR UIEA200400040Fan · inoperativeDURING TAXI IN, SMELL OF SMOKE FROM THE AIR CONDITIONING SYSTEM. FLIGHT DECK FAN SWITCHED OFF WITH NO FURTHER SMELL. AFTER SHUTDOWN, UNABLE TO SWITCH FAN BACK ON. CIRCUIT BREAKER PULLED AND ITEM TRANSFERRED DMI M04-064. REMOVED AND REPLACED FLIGHT COMPARTMSDR UIEA200400027Panel · looseMXP/BOM ATB DUE TO SIDE CARGO DOOR OPEN LIGHT ON: SIDE CARGO DOOR OPEN LIGHT CAME ON DURING TAKEOFF AND REMAINED ON AFTER TAKEOFF. FOUND SECURING PANEL ON LATCH DOOR MECHANISM WITH LOOSE SCREWS. TIGHTENED SCREWS, EXERCISED DOOR AND CHECKED OPERATION, FOUND
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