Boeing 747-2D3B
Service difficulty reports · 182
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 = '7472D3B' 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 = '7472D3B' 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 UIEA200400147Relay · inoperativeREJECTED TAKEOFF DUE TO TAKEOFF WARNING HORN AT 135KTS. STAB TRIM INDICATION SYSTEM TEST CUT OUT IAW MM 27-48-00. OPS NORMAL. STAB TRIM INDICATION AND CONTROL SYSTEM WITH MULTI GREEN BAND CUT OUT OPS NORMAL PER MM 27-48-00. REPLACED RELAY R-586 STAB TRIM GSDR UIEA200400139Sequence Valve · malfunctionedAFTER TAKEOFF, ON GEAR RETRACTION NOSE LANDING GEAR DOOR KEPT CYCLING. ATTEMPTED RE-CYCLE NO EFFECT. REMOVED AND REPLACED NOSE GEAR OPERATED DOOR SEQUENCE VALVE PER MM 32-34-08. PAGE 401-405 OPS AND LEAK CHECK NORMAL. (M)SDR P5CA0401131Valve · malfunctionedAFTER ENGINE START NR 1 ENGINE HAD NO RESPONSE TO THROTTLE MOVEMENT. ALL INSTRUMENTS INDICATED ENGINE AT IDLE POWER. CLEANED CDP LINE, NO HELP, REPLACED CIT SENSOR, ENGINE NOW RUNS HIGH EGT, FOUND PYLON VALVE AT FAULT, OPENED DMI NR 36-5-2.SDR UIEA200400123Bulb · failedPO380/10 DXB/CGK LOWER CARGO AFT FIRE LIGHT CAME ON DURING TAKEOFF: LOWER CARGO AFT FIRE LIGHT CAME (ON) AT ROTATION. APPROPRIATE DRILLS CARRIED OUT. AIRCRAFT RETURNED TO DEPARTURE. CHECKED LOWER AFT CARGO FOR FIRE OR DAMAGE, NO EVIDENCE. BULK CARGO IS EMSDR P5CA0401117Valve · malfunctionedDMI NR 32768, NR 1 PYLON VALVE INOPERATIVE, ALSO HIGH PRESSURE BLEED VALVE ON ENGINE NR 1. REMOVAL AND REPLACEMENT. REMOVED AND REPLACED PYLON VALVE DUE TO NOT CLOSING COMPLETELY , OPS CHECK AND LEAK CHECKS GOOD IAW MM 36-11-04.SDR P5CA0401116Valve · malfunctionedON ENGINE START-UP NR 1 ENGINE PYLON VALVE WILL NOT OPEN DURING MANUAL ENGINE START. REPOSITIONED PYLON VALVE IN ORDER TO ACHIEVE ENGINE START, OPS CHECK GOOD IAW MM 36-11-04.SDR P5CA0401105Manifold · leakingFUEL DRAINING FROM DRAIN MAST NR 3 ENGINE PORT ON ENGINE START. REPLACED NR 3 ENGINE VBR FUEL MANIFOLD ASSY AS PER MM 75-32-00. OPS & LEAK CHECK OK AS PER MM 71-00-00 TEST NR 3.SDR UIEA200400093Warning Light · false activationAFT CARGO FIRE WARNING LIGHT ILLUMINATED, CAUSING FIRE WARNING. CARRIED OUT PROCEDURE IAW QRH. RETURNED FOR LANDING. CARRIED OUT INSPECTION OF AFT CARGO IAW MM 26-16-00. NO EVIDENCE OF SMOKE OR FIRE DAMAGE. OFF LOADED CARGO FOR INSPECTION. ALL SYSTEM NORMSDR P5CA0401080Web · damagedON POST FLIGHT INSPECTION, FOUND FAIRING OVER RIGHT WING ROOT OPEN AND FOUND WEB PANEL DAMAGED. ACCOMPLISHED REPAIR OF WEB PANEL PER SRM 51-40-02. SURROUNDING AREA CLEANED AND INSPECTED. NO FURTHER DAMAGE.SDR P5CA0401073Door · damagedLT WING GEAR LWR O/B STRUT DOOR DAMAGED. REMOVED AND ROUTED TO SHOP, OK TO INSTALL. INSTALLED DOOR PER MM.SDR P5CA0401075Proximity Switch · failedLEFT "WING GEAR" ELECTRICAL HARNESS INSPECTION. REPLACED LEFT WING O/B (PRIM) PROX SWITCH (TILT) AND REPLACED LEFT WING GEAR INBD (ALT) TILT SWITCH. SECURED INBD PROX SWITCH MOUNT. CLEARANCE OK ON GEAR SWING.SDR P5CA0401074Panel · damagedLT WING ACCESS PANEL OB AND FWD OF NR 4 FLAP TRACK FIX FAIRING 3 X 3 INCH HOLE. REMOVED DAMAGED ACCESS PANEL FOR REPAIRS, INSTALLED SERVICEABLE PANEL IAW SRM.SDR P5CA0401071Tire · separatedTOWER REPORTED LOST TIRE ON LANDING. REPLACED NR 3 TIRE AND BRAKE, NR 4 TIRE.SDR UIEA200400036Pdu · smokeANC/DFW - PDU MAIN DECK POSITION 18R INOPERATIVE STARTED SMOKING. REMOVED PDU FOUND MOTOR INOPERATIVE. REMOVED CONNECTOR AND DEACTIVATED PDU. TRANSFERRED TO DI PAGE 55833 DMI C-4-003. (M)SDR IUEA200400028Connector · dirtyGT8971/5 DNA/BKK ATB AND IFSD DUE TO NR 1 ENGINE FALSE FIRE WARNING: NR 1 ENGINE FIRE INDICATION DURING CLIMB, ALL OTHER SYSTEMS NORMAL EXCEPT (B) LOOP WAS DEFERRED. (A) LOOP WAS INDICATION FAULT AND FIRE. ENGINE SHUTDOWN ACCOMPLISHED AND FUEL JETTISON 28.3SDR P5CA0401051Relief Valve · illuminatedAT APPROX 6,000 FT NR 4 ENG LOOP FAULT LT ILLUMINATED NACELLE TEMPS A&B OBSERVED RAPIDLY CLIMBING TO 9. REMOVED AND REPLACED HIGH PRESS VLV, HIGH PRESS BLEED VLV HARNESS. REMOVED AND REPLACED PRESSURE RELIEF VLV. ENG OPS CHECKED GOOD, NO DEFECTS NOTED PER MSDR P5CA0401050Connector · looseNR 1 ENG WILL NOT START. MANUAL START UNSUCCESSFUL. FOUND CONNECTOR LOOSE ON NR 1 ENG BLEED AIR VALVE. RECONNECTED PLUG, OPS CHECK OK PER MM 36-11-00.SDR P5CA0401034Start Valve · malfunctionedNR 4 ENG STARTER VALVE WOULD NOT CLOSE 50 PERCENT. REPLACED START VALVE, OPS CHECK OK PER MM 80-11-04.SDR P5CA0401035Panel · crackedLT WING UPPER LE PANEL CRACKED ON UPPER SURFACE (APPROX 30 INCHES,) LWR OB SURFACE HAS A 25 INCHES CRACK AND IS DISBONDED. PANEL REPLACED DURING FA-06 CHECK - NON-ROUTINE WORKCARD (T-160) NR 0034 REF.SDR P5CA0301000Check Valve · failedNR 1 ENG AT TOP OF DESCENT, FL 380, ENG. STALLED. ENG. RECOVERED AT FL 330 AND STALLED AGAIN. ENGINE SHUT DOWN. REMOVED AND REPLACED 8TH STAGE CHECK VALVE RUN UPPER LEAK CHECK, OK IAW MM 36-11-02 AND 71-00-43.SDR UIEA200300060Engine · making metalIN CRUISE, ENGINE NR 3 COMPRESSOR STALLS WITH N1, N2 AND EGT FLUCTUATION. PERFORMED ENGINE FIRE, SEVERE DAMAGE OR SEPARATION CHECK IAW FLIGHT HANDBOOK 3.70.1. SHUTDOWN ENGINE AND RETURNED. FUEL DUMPED 6,000 KGS. VISUAL INSPECTION OF NR 3 ENGINE, FOUND METASDR P5CA0300931Valve · malfunctionedNR 4 MAIN FUEL TANK - REFILL VALVE WILL NOT SHUT OFF. REMOVED AND REPLACED NR 4 MAIN FUEL TANK REFILL VALVE IAW AMM 28-21-13.SDR P5CA0300900Actuator · failedRT INBND BODY GEAR STEERING ACTUATOR FAILED, CAUSING LOSS OF NR 1 HYDRO SYS. REMOVED AND REPLACED RT INBND BODY GEAR STEERING ACTUATOR. LEAK CK AND GROUND OPS NORMAL IAW MM 32-51-05, SERVIVED NR 1 HYD SYS IAW 72-00.SDR UIEA200300037Skin · corrodedDURING C-CHECK, AS PER XEO 53-06/04/03 FOUND AFT BELLY SKIN WITH CORROSION AND DENTS UNDER PREVIOUS REPAIR AT THE FOLLOWING STATIONS 2200-2240 STRINGER 45R-48L AND STATION 1977-2008 STRINGER 45R-48L REPAIR CARRIED OUT PER BOEING TELEX SEP-SIN-03-00036H AND 811SDR UIEA200300036Floorbeam · crackedDURING C-CHECK, MAIN DECK FLOORBEAM WEB AND BEAM FOUND CRAKCED AT BS 320 AND APPROXIMATE AT RBL 40. FLOORBEAM AND WEB REPAIR CARRIED OUT PE IAI REPAIR SCHEME AND 8110-3. REPAIR AREA BS 320, RBL 38 TO BE VISUAL INSPECTED, AT THE FOLLOWING INTERVAL, 1500 HOURSSDR UIEA200300038Pressure Panel · crackedDURING C-CHECK, NOSE GEAR WHEEL TOP AT BS 366 LBL 11 FOUND CRACK FROM EDGE AND EXTENDED INBOARD APPROXIMATE 1 INCH IN LENGTH. DEFECT FOUND DURING L-CHORD REPLACEMENT AT STATION BS 340, LBL 11.33. REPAIR CARRIED OUT AS PER BOEING TELEX SEP-SIN-03-40H AND 8110SDR UIEA200300039Skin · corrodedDURING C-CHECK, CENTER TANK UPPER SKIN FOUND CORRODED AT BS 1060, RBL 106-122 UNDER FLOORBEAM LOWER CHORD. PERMANENT REPAIR PER REF, CORROSION WAS REMOVED BY BLENDING. BLENDED AREA WAS SHOP PEENED, REFINISHED AND BMS 5-95 SEALANT WAS USED TO FILL THE BLENDEDSDR P5CA0300891Fuel Sys · malfunctionedREPORTED FUEL LEAK BY TOWER ON CLIMBOUT WITH SMELL OF FUEL IN UPPER CRG DECK. FOUND LT SURGE TANK WITH FUEL SUMPED SURGED TANK. FOUND VOLUMETRIC SYS INOP. OPENED DMI 28-20-1. MALFUNCTION OF VOLUMETRIC SYS.SDR P5CA0300887Actuator · brokenLEFT BODY GEAR LIGHT "UNLOCKED" WOULD NOT COME ON IN PRIMARY OR ALTERNATE ON TAXI BACK LIGHTS CAME ON. ITEM TRANSFERRED TO DMI NR 30932 IAW DDPG 32-17-C BODY GEAR STEERING ACTUATORS VERIFIED LOCKED. REQUIRES FURTHER TROUBLE SHOOTINGSDR P5CA0300886Switch · malfunctionedON TOW OUT RT LANDING GEAR TURNED SIDEWAYS. OPS CHECKED BODY GEAR STEERING SYSTEM IAW MM 32-53-00. OPS CK OK A/C BACK TO CONFIGURATION. SUSPECT RT BODY GEAR UNLOCK SWITCHES MALFFUNCTIONED.SDR UIEA200300035Bulkhead · crackedDURING C-CHECK, FOUND CRACKS AT LT AND RT SIDES OF STATION 140, FORWARD PRESSURE BULKHEAD WEB, WL 205-227 AND WL 250-258. THE REPAIR TRIMS OUT THE CRACKS, HFEC INSPECTS THE TRIM. INSTALLED REPAIR DOUBLERS ON THE AFT SIDE PER REF AND MOD DOUBLERS ON THE FORWASDR P5CA0300784Control Unit · inoperativeON PUSHBACK RT WING FRONT ANTI-SKID LIGHT ILLUMINATED. DE-ACTIVATED NR 14 BRAKE & DEFERRED ITEM. ONE DEFECTIVE CHANNEL WITHIN CONTROL UNIT.SDR P5CA0300782Igniter · defectiveRETURN TO BLOCKS DUE TO NR 4 ENG FAILED TO START. REPLACED BOTH IGNITER PLUGS TESTED OK. DEFECTED IGNITER PLUG NR 2 POS NR 1 SYS PREV DEFERRED.SDR P5CA0200711Indicator · malfunctionedON LANDING & AFTER T/R'S STOWED, NR 3 ENGINE FUEL FLOW SPIKED. PRECAUTIONARY ENGINE SHUTDOWN PERFORMED IMMEDIATELY. F/F INDICATION REMAINED AT 12000 PLUS. PERFORMED BITE CHECK OF F/F SYSTEM. OPERATED NR 3 ENGINE, ALL PARAMETERS NORMAL PER MM 71-00-00 & MM SDR P5CA0200708Coupling · looseDURING CRUISE AT FL 310, #4 ENG OIL QTY WENT FROM 3.5 TO ZERO IN APPROX. 15 MIN. OIL PRESS STARTED FLUCTUATING; OIL TEMP IN GREEN BAND (PERFORMED PRECAUTIONARY SHUTDOWN) WINDMILL RPNM 26%, N2 23%, OIL TEMP BELOW GREEN, OIL PRESS 10 PSI. EMERGENCY DECLARED & SDR UIEA200200047Skin · crackedDURING CURRENT C CHECK, FOUND NR4 PYLON RIGHT HAND FORWARD ACCESS PLATE CUTOUT, BETWEEN NAC 211 AND 220, CRACKED. CRACKS INITIATED FROM THE CLIP NUT HOLES OF THE INNER LIP DOUBLER (4 PLACES). TRIMMED AWAY INNER DOUBLER AROUND THE ENTIRE CUTOUT. FABRICATED DSDR UIEA200200046Spar · corrodedDURING CURRENT C CHECK, FOUND CENTER WING LOWER REAR SPAR WEB CORRODED AT LBBL66 TO 75. BLENDED CORROSION. PERFORMED HFEC OPEN HOLE INSPECTION AND SURFACE INSPECTION OF BLENDED AREAS. NO DEFECTS FOUND. MEASURED CORROSION DEPTH, MEASUREMENTS EXCEEDED SRM LISDR UIEA200200045Web · crackedDURING CURRENT C CHECK, FOUND SHEAR WEB FLANGE AT BS 340 TO 360 STR 26R WITH CRACKS ALONG THE SKIN FASTENER ROW. CUT AND REMOVED THE CRACKED FLANGE AT THE WEB RADIUS. HFEC INSPECTION PERFORMED ON EXTERNAL SKIN AND WEB CUT LINE. NO ADDITIONAL CRACKS FOUND. SDR UIEA200200044Web · crackedDURING CURRENT C CHECK AT KLM FOUND SHEAR WEB FLANGE AT BS 340 TO 360 STR 26L WITH CRACKS ALONG THE SKIN FASTENER ROW. CUT AND REMOVED THE CRACKED FLANGE AT THE WEB RADIUS. HFEC INSPECTION PERFORMED ON EXTERNAL SKIN AND WEB CUT LINE. NO ADDITIONAL CRACKS FOSDR UIEA200200043Keelbeam · corrodedDURING CURRENT C CHECK AT KLM FOUND KEEL BEAM BOX WEB UPPER SURFACE ON BOTH LEFT/RIGHT SIDES OF BL 0 CORRODED. CUT AND REMOVED WEB FROM BS 1265 TO 1273. PERFORMED OPEN HOLE HFEC INSPECTION OF REMOVED FASTENER HOLES IN REPAIR AREA. NO ADDITIONAL CRACKS/CORROSDR UIEA200200026Switch · inoperativeON DESCENT A STRONG ELECTRICAL ODOR COMING OUT OF GASPERS. ELECTRICAL SMOKE OR FIRE CHECK LIST INITIATED. AFTER ITEM NR 6, SMOKE STOPPED. AIRCRAFT REMAINED IN THIS CONFIGURATION AND LANDED. C/A: FOUND MELTED INSULATION AT WING ILLUMINATION LIGHT SWITCH TERSDR UIE2002000026Switch · intermittentON DESCENT A STRONG ELECTRICAL ODOR COMING OUT OF GASPERS. ELECTRICAL SMOKE OR FIRE CHECK LIST INITIATED. AFTER NR 6, SMOKE STOPPED. AIRCRAFT IN THIS CONFIGURATION AND LANDED. FOUND MELTED INSULATION AT WING ILLUMINATION LIGHT SWITCH TERMINAL. LIGHT INTERSDR UIE2002F00008Switch · inoperativeON DESCENT A STRONG ELECTRICAL ODOR COMING OUT OF GASPERS. ELECTRICAL SMOKE OR FIRE CHECK LIST INITIATED. AFTER ITEM NR 6, SMOKE STOPPED. AIRCRAFT REMAINED IN THIS CONFIGURATION AND LANDED. C/A: FOUND MELTED INSULATION AT WING ILLUMINATION LIGHT SWITCH TESDR UIE2002F00003Clamp · looseAFTER TAKEOFF NR 3 ENGINE FIRE WARNING LIGHT CAME ON AND NACELLE HEAT FOR NR 3 ENGINE READ 8 ON BOTH SIDES. AFRTER LEVELING OFF AND REDUCING POWER, THE LIGHT WENT OUT. ENGINE SHUT DOWN PERFHB AIRCRAFT RETURNED TO AIRPORT. C/A: FOUND 14TH STAGE DUCT CLAMPS SDR UIEA0100Fire Warning · false indicationATB - DUE LOWER AFT CARGO FIRE LIGHT ON AT ROTATION. NR 1 BOTTLE DISCHARGED (FALSE INDICATION). LOWER AFT CARGO INSPECTED. NO SIGNS OF FIRE (NO CARGO IN SECTION). ITEM TRANSFERRED TO DMI PAGE 03049 AND DEFERRED PER MEL 26-14-2D AND ALL DDPG PROCEDURES FOLLSDR UIEA01100Fire Warning · false indicationATB DUE LOWER AFT CARGO FIRE LIGHT ON AT ROTATION NR 1 BOTTLE DISCHARGED, FALSE INDICATION. LOWER AFT CARGO INSPECTED. NO SIGNS OF FIRE (NO CARGO IN SECTION). ITEM TRANSFERRED TO DMI PAGE 03049 AND DEFERRED PER MEL 26-14-2D AND ALL DDPG PROCEDURES FOLLOWED.SDR UIEA01102Harness · missingDURING ROUTINE ENGINE INSPECTION FOUND NR 1 ENGINE LOWER EGT HARNESS MISSING. REPLACED NR 1 ENGINE EGT HARNESS AS PER MM 77-20-03. (M)SDR UIEA01091Skin · corrodedDURING INSPECTION FOUND CORROSION ON HORIZONTAL STABILIZER SKIN PANELS RIGHT STAB STATION 160 LOWER SKIN FRONT SPAR, RIGHT STAB STATION 173 AT SPLICE STRINGER LOWER SKIN AFT PANEL, LEFT STAB STATION 173 SPLICE STRINGER LOWER FORWARD SKIN AND AT LEFT STABILIZERSDR UIEA01090Fitting · corrodedDURING INSPECTION FOUND BS 1480 LEFT AND RIGHT INBOARD HORIZONTAL SUPPORT FITTINGS CORRODED AT THE ATTACHMENT TO THE BODY GEAR TRUNNION, VERTICAL SUPPORT FITTING. REMOVED BUSHINGS FROM BOLT HOLES. BLENDED LOCAL CORROSION. SPOT FACED AREA AROUND BOLT HOLES. SDR UIEA01076Web · crackedDURING INSPECTIN FOUND FRAME WEB CRACKED AT BS 380 FROM STRINGER 23L CUTOUT. TRIMMED AWAY CRACKED AREA. FABRICATED REPLACEMENT DOUBLER AND TWO ANGLES. INSTALLED PER STANDARD PRACTICES. CONTINUE CURRENT INSPECTION REQUIREMENTS PER SB 747-53A2265 UNTIL SB 53
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