Boeing 747-230B
Service difficulty reports · 618
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 = '747230B' 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 = '747230B' 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 EIA2007149Lamp · looseDURING FLIGHT, NR 2 MAIN CARGO DETECTOR CAME ON; THERE WAS NO CARGO LOADED. BEACON LAMP FOUND LOOSE, TIGHTENED AND DETECTOR OPS NORMAL. A SYSTEM NO DEFECT. MAIN DECK NR 2 SMOKE DETECTOR SYSTEM OPS NORMAL PER MM 26-14-00.SDR EIA2007142Floorbeam · damagedLT STA 1345 BL 117 O/B FLOORBOARD SUPPORT HAS ELONGATED HOLE (UNDER FLOOR BOARD). REPAIRED LT STA 1345 BL 117 O/B FLOORBOARD SUPPORT PER ECRA 488-53-024-2A.SDR EIA2007141Floorbeam · damagedRT STA 1345 BL 117 O/B FLOORBOARD SUPPORT HAS ELONGATED HOLE (UNDER FLOOR BOARD). REPAIRED RT STA 1345 BL 117 O/B FLOORBOARD SUPPORT PER ECRA 488-53-024-2A.SDR EIA2007144Floorbeam · loose2 FASTENERS MISSING AND 2 NOT TIGHTENED ON UPPER TEE OF FLOORBEAM STA 1460 BELOW CARGO TIE DOWN FITTING RBL 57 (BELOW FLOOR PANEL). REPAIRED STA 1460 FLOORBEAM AT RBL 57 PER ECRA 488-53-025-2.SDR EIA2007140Skin Panel · gougedNR 3 PYLON OUT BOARD ACCESS DOOR NR 473AR THE DOOR RING HAS DEEP GOUGE AT INNER SIDE. REPAIRED NR 3 PYLON OUTBOARD ACCESS DOOR NR 473AR PER ECRA 488-54-019-2.SDR EIA2007148Bulb · inoperativeUPPER DECK AFT EMERGENCY AISLE LIGHT INOP. REPLACED BOTH BULBS AND OPS CHECKED PER B747MM 33-51-07.SDR EIA2007139Battery Pack · no testEMERGENCY LIGHT IN UPPER DECK LOUNGE DID NOT COME ON DURING TEST. INSTALLED BATTERY PACK POWER SUPPLY MODULE PER B747 MM 33-51-04 PAGE 201-204, OPS CHECKED PER B747 MM 33-51-04 PAGE 204-205.SDR EIA2007138Frame · crackedNR 2R DOOR FRAME STA 800 STR 18R WEB CRACKED. REPAIRED PER EOA ECRA 488-53-023-2 PAGE 1.SDR EIA2007146Rib · looseLEFT WING LEADING EDGE HAS RIVETS LOOSE AT FORMER RIB INBOARD OF NR 3 KREUGER FLAP. REPAIRED LEFT WING LEADING EDGE AT FORMER RIB INBOARD OF NR 3 KREUGER FLAP PER ECRA 488-57-020-2.SDR EIA2007145Closeout Panel · gougedNR 3 PYLON INBOARD DOOR 473AL RING IS GOUGED INSIDE. REPAIRED NR 3 PYLON INBD ACCESS DOOR CUT OUT FOR ACCESS PANEL 473AL PER ECRA 488-54-018-2 PART 1.SDR EIA2007135Pressure Panel · crackedNOSE WHEEL WELL TOP WEB IS CRACKED BETWEEN STA 280-300 LBL 20 AT LEFT BRAKE PAD MOUNT. REPAIRED NOSE WHEEL WELL TOP WEB BETWEEN STA 280-300 LBL 20 PER B747 SRM 53-10-04 PG 713-721.SDR EIA2007136Skin · dentedOUTWARD DENT IN FUSELAGE SKIN STA 2364 STRINGER 15 RIGHT. CUT OUT DAMAGE AREA FABRICATED -1 AND -2 REPAIR PARTS, INSTALLED FILLER AND DOUBLER PER B747 SRM 53-30-03 FIG 47 AND 51-30-02. ALL WORK ACCOMPLISHED AT BS 2346 STRINGER 15R.SDR EIA2007143Floorbeam · damagedRT 840 BL 46 SCREW IS DOUBLE DRILLED AND DEEP DRILL STARTS ON FLOORBEAMS. REPAIRED RT STA 840 BL 46 FLOORBEAM PER ECRA 488-53-014-2.SDR EIA2007137Skin · dentedOUTWARD DENT IN FUSELAGE SKIN STA 2364 STRINGER 15L. REPAIRED SKIN AT STA 2364 STRINGER 15L PER B747 SRM 53-30-03 FIG 47.SDR WRNA200700027Engine · unserviceableAFTER TAKEOFF, DURING CLIMB NR 1 ENGINE EXPERIENCED MULTIPLE STALLS. POWER WAS REDUCED, 160,000 POUNDS OF FUEL WERE DUMPED. AIRCRAFT RETURNED TO FIELD AND MADE A SAFE LANDING. ENGINE WAS VISUALLY AND BORESCOPE INSPECTED PER BOEING MM 72-00-00 PAGE 680Q WITHSDR EIA2007105Tension Tie · damagedBS 880 TENSION TIE BEAM RT SIDE COMMON TO FRAME HAS ONE HOLE OUT OF LIMITS PER EO 53-747-1818-06 REV A. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 487-53-045-2.SDR EIA2007104Tension Tie · crackedTENSION TIE FRAME BS 940 RT SIDE FUSELAGE CABLE THRU HOLES ENLONGATED AND FASTENER HOLES CRACKED OUT. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 487-53-048-2.SDR EIA2007106Skin · crackedUPPER EDGE OF NR 2 PYLON ACCESS PANEL 463AR OPENING IS CRACKED AND WORN. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 487-54-043-2.SDR EIA2007103Skin · crackedNR 4 PYLON O/B ACCESS PANEL CUTOUT FLANGE CRACKED, PYLON STATION 213.6. REMOVED DAMAGE, NDTD AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 487-54-046-2.SDR EIA2007107Floor Panel · corrodedMAIN DECK BS 800 FWD OUTBOARD END OF PANEL 83 HAS CORROSION BETWEEN FLOOR BEAM AND SEAT TRACK. REMOVED CORROSION, NDTD AREA, FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-10-07 FIG 10.SDR EIA2007108Stringer · corrodedHEAVY EXFOLATION CORROSION STRINGER 46L BS 770 TO BS 790. REMOVED CORROSION, NDTD AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 487-53-050-2.SDR EIA2007116Floor Panel · gougedMAIN CABIN FLOOR PANEL GOUGED 2 PLACES BS 358 RBL 6. DAMAGED FLOOR PANEL IS WEB OF NOSE WHEEL WELL BOX TOP PANEL. REMOVED GOUGES, AREA OUT OF LIMITS PER B747 SRM 53-10-01 PAGES 2-6. REPAIRED AREA STATION 340 RBL 6 B747 SRM 53-10-04 FIGURE 119.SDR EIA2007117Strap · gougedNR 3 PYLON LEFT SIDE AFT ACCESS 473CL FED VERTICAL FRAME, HORIZONTAL STRAP AND ANGLE SUPPORT HAS GOUGE. REMOVED GOUGE AND INSTALLED REPAIR ON NR 3 PYLON LEFT SIDE AFT ACCESS 473CL FWD VERT FRAME HORIZ STRAP AND ANGLE SUPPORT PER B747 SRM 54-11-03 FIG 1.SDR EIA2007115Stringer · corrodedHEAVY EXFOLIATION CORROSION ON STRINGER 47R AT STATION 790, FORWARD PIT BILGE. REMOVED CORROSION AT STRINGER 47R STATION 790, FOUND TO BE OUT OF LIMITS 100 PERCENT MATERIAL LOSS. REMOVED DAMAGE AREA PER B747 SRM 51-30-02 FIGURE 1, NDT CHECKED NO CRACKS NOTEDSDR EIA2007113Skin · damagedLEFT HORIZONTAL STABILIZER STATION 210 UPPER SIDE OF THE WEB STIFFENER AT LEFT ACCESS CUT-OUT HAS TOOLING MARKS 2 EA. INSTALLED REPAIR PLATE, FILLER AND 2 EACH WEB STIFFENERS AT LEFT HORIZONTAL STABILIZER STATION 210 PER B747 SRM 55-10-06 PAGES 8-9 AND 51-30-SDR EIA2007110Spar · damagedHOLE NR 2 LEFT SIDE HORIZONAL STAB REAR SPAR CHORD IS REAMED TO .405" STILL SHOWS DEFECT AT LIMIT PER SB747-55A2050. REMOVED AND REPLACED LT HORIZONAL STAB HINGE FITTING PER B747 SRM 51-30-02 PAGES 8/9, 51-30-05 PAGE 5, 51-10-01 AND 51-30-04 FIG 1.SDR EIA2007109Stringer · damagedFUSELAGE INTERIOR FRAME TO FRAME ANGLE STATION 960 STRINGER 15L HAS MISDRILLED FASTENER HOLES. DAMAGE REMOVED, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 4887-53-044-2.SDR EIA2007114Frame · crackedFRAME WEB CRACKED AT STAND OFF HOLE STA 320 W/L 175 LBL 20 IN LT TUNNEL. REPAIRED CRACK AT STAND OFF HOLE AT STA 320 W/L 175 LBL 20 LT TUNNEL PER B747 53-10-02 PAGE 90 FIGURE 6, 51-20-01 PAGES 11, 14-29, 51-30-05 PAGE 5 TABLE 1, 51-10-02 PAGES 6-8 ITEM G, 51-SDR EIA2007111Frame · crackedFRAME WEB CRACKED AT STAND-OFF HOLE STA 300 WL 175 LBL20 IN LT TUNNEL. REPAIRED CRACKED STAND-OFF HOLE AT STA 300 WL 175 LBL 20 IN TUNNEL PER B747 SRM 53-10-20 PAGES 90-91 FIGURE 6, 51-20-01 PAGES 11,14-29, 51-30-05 PAGE 5 TABLE 1, 51-10-02 PAGES 6-8 ITEM G, SDR EIA2007112Stop Fitting · crackedDOOR STOP NR 9 ON LT MAIN ENTRY DOOR CRACK NOTED DURING ACCOMPLISHMENT OF EO, LOCATED AT BS 488 FRAME WEB TOOLING HOLE. REPAIRED MAIN ENTRY DOOR FRAME STA 488 PER SRM B747 53-10-04 FIG 121.SDR EIA2007069Drive Assy · malfunctionedNR 1 LT LEADING EDGE DRIVE FAILED TO RETRACT PNEU OR ELEC AFTER T/O FROM JFK AIRCRAFT RETURNED TO JFK. AWAITING CORRECTIVE ACTIONSDR UIEA200700203Skin · delaminatedRT WING O/B MID FLAP UPPER SURFACE LEADING EDGE AT WING STA 1000.00 TO WING STA 995.00 IS DELAMINATED 2.5IN WIDE 4.5IN LONG. REPAIRED RT WING O/B MID FLAP UPPER SURFACE DELAMINATION IAW SRM 51-10-01 EO4757A353.SDR WRNA200700023Flap · delaminatedDURING B-CHECK, RIGHT INBOARD FORE FLAP WAS FOUND WITH DAMAGE, A 42 INCH LONG X 19 INCH WIDE PREVIOUS REPAIR, 45 INCHS FROM OUTBOARD END, DEPARTED FORE FLAP WITH 40% MATERIAL LOSS. ACCOMPLISHED REPAIR PER 747 SRM 51-40-12.SDR 2007FA0000228Sensor · malfunctionedDURING TAKEOFF, THE LANDING GEAR HANDLE WILL NOT GO TO UP OR RETRACT POSITION. AIRCRAFT RETURNED TO BASE. PERFORMED TROUBLESHOOTING ON THE LANDING GEAR SYSTEM AND FOUND THAT LT WING GEAR TRUCK ROTATION SENSOR AT FAULT. ADJUSTED THE LT WING GEAR TRUCK ROTATISDR EIA2007019Clamp · openON TAKEOFF ROLL, NR 4 ENGINE NACELLE TEMP "A" LOOP TEMP WAS READING 8.2 UNITS WITH P2 PANEL AMBER LIGHT "FIRE DET" LIGHT ILLUM. ABORTED TAKEOFF. MX FOUND LOOP CLAMP OPEN WITH "A" LOOP (L/H BOTTOM) CONTACTING BEARING OIL SCAVENGE LINE. INSPECTED FIRE LOOP ANSDR EIA2007015Cable · brokenAFTER TAKEOFF, IN CLIMB, AT F1120 PILOTS FIRE WARNING ANNUNCIATOR ILLUMINATED WITH FLIGHT ENGINEER'S NR 1 ENG A & B LOOPS AT TOP OF BAND. ENGINE WAS SHUT DOWN AND RT FIRE BOTTLE DISCHARGED. FIRE DETECTION RETURNED TO NORMAL AND AIRCRAFT RETURNED TO TLV. TROSDR 740006Flex Duct · blownNR 4 ENGINE HAS 2 KNOB THROTTLE SPLIT. HIGH EGT, HIGH FUEL FLOW, HIGH OIL TEMPERATURE, HIGH FIRE DETECTION TEMPERATURE AND HIGH STAGE VALVE OPEN. RETURNED TO RKSI. TROUBLESHOOT IAW AMM 71-00-42. PERFORMED BLEED SYSTEM LEAK CHECK IAW AMM 71-00-00. FOUND HISDR 740005Cable · frozenNR 4 ENGINE PARAMETERS INDICATED LOSS OF POWER AT CRUISE ALTITUDE OF 25,000 FEET. EGT HIGH, N1 AND N2 LOW, FUEL FLOW HIGH AND ENGINE SURGES +/- 3 PERCENT. DUMPED 96,000 LBS OF FUEL AND DIVERTED TO RKSI. FOUND FROZEN VSV FEEDBACK CABLE. REMOVED AND REPLACEDSDR Q2SA740004Bolt · shearedGEAR WILL NOT RETRACT AFTER TAKEOFF. BOTH RIGHT BODY GEAR TILT LIGHTS CAME ON. AIR TURN BACK TO PANC. FOUND RIGHT BODY GEAR TRUCK POSITION ACTUATOR FORWARD ATTACH BOLD SHEARED. INSPECTED AND NO OTHER DISCREPANCIES FOUND. REMOVED AND REPLACED RIGHT BODY GESDR EIA2007006Battery Pack · inoperativeLT CREW SERVICE DOOR UPPER JAMB EMERGENCY LIGHT DOES NOT REMAIN LIGHTED WITH EMERGENCY LIGHT SW ON. REPLACED BATTERY PACK, OPS CHECK NORMAL PER MM 33-55-00.SDR Q2SA509001Sense Line · cloggedNR 4 ENGINE ROLL BACK TO 93.5 PERCENT N1 AT FLIGHT LEVEL 310. EGT AT 641 DEGREES, N2 AT 94.5 PERCENT AND FUEL FLOW AT 5648. AFTER LANDING NO RESPONSE FROM THROTTLE LEVER. DUMPED 140,000 LBS FUEL. AIRCRAFT EN ROUTE ZSPD TO PANC, DIVERTED TO RKSI. NR 4 ENGISDR EIA2007001Smoke Detector · malfunctionedFIRE BELL SOUNDED 3 TIMES DURING LEVEL FLIGHT, ACCOMPANIED WITH WARNING LIGHTS ON P-10 AND P-12 PANELS, AND MAIN DECK CARGO SMOKE DETECTOR NR 5 ON FE P-4 UPPER." TRANSFERRED TO DMI.328. REMOVED AND REPLACED NR 5 A AND B SMOKE DETECTORS AND SMOKE DETECTOR AMP SDR WRNA200600041Housing · crackedDURING CRUISE, AT 33,400 FEET, NR 3 ENGINE OIL QUANTITY AND OIL PRESSURE DROPPED RAPIDLY TOWARDS -0- PERFORMED PRECAUTIONARY SHUTDOWN. FLIGHT CONTINUED TO DESTINATION AND MADE A SAFE LANDING. INVESTIGATION REVEALED RADIAL DRIVE LEAKING, REPLACED RADIAL DRIVESDR EIAA2006381Stringer Splice · misrepairedDURING INSPECTION, FOUND STRINGER 27L AT BS 440-460 TO HAVE A PREVIOUS NON-SRM REPAIR. REMOVED DAMAGED SECTION AND FABRICATED AND INSTALLED SECTION PER BOEING SRM 51-30-02, PG 2-3;51-20-01 PGS 11,14 - 20; AND 51-10-02 PGS 7 - 8.SDR EIA2006382Skin · dentedSKIN DENT, BS 502, STR38 - 39R. REMOVED DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR PER B747 SRM 53-30-03 FIG 1.SDR EIA2006383Skin · dentedFUSELAGE SKIN DENT AT STR 28, BS 450. REMOVED INTERNAL FRAME STRUCTURE AND DAMAGED PORTION OF STR 28L PER B747 SRM 53-10-03, FIG 3; 53-10-20, FIG 11;51-10-02, PGS 7-8;51-10-01, PG 9; 51-30-02, PGS 2, 3, 8, 9.SDR EIA2006377Skin · dentedDURING CHECK FOUND DENT IN SKIN AT BS 510, STR 28L. REMOVED DAMAGE, NDT'D AREA, FABBED AND INSTALLED REPAIR PER B747 SRM 53-30-03 FIG 47.SDR EIA2006378Stringer · damagedWHILE REPAIRING DENT AT BS 510 FOUND HOLES IN STR 27L AT STA 500 OVER 1/4 IN DIAMETER. REMOVED DAMAGED STR27L STA 500-520, FABBED NEW AND INSTALLED PER B747 SRM 51-30-02, 53-11-20 AND 51-20-01.SDR EIA2006375Hydraulic System · leakingEN ROUTE FROM CHS TO PIK, NR 1 HYD SYSTEM QUANTITY LOSS. EDP AND ADP DEPRESSURIZED, NO HELP, FIREWALL VALVE SHUT OFF, NO HELP. CONTINUED TO PIK, WILL REQUIRE ALTERNATE GEAR OPERATION FOR EXTENSION. WILL REQUIRE TOW FROM RUNWAY DUE TO NOSE GEAR STEERING INOPSDR Q2SA740003Valve · malfunctionedHAD INDICATION OF NR 1 ENGINE FIRE AT FL 250. ACCOMPLISHED ENGINE FIRE CHECKLIST IAW QRH. SHUTDOWN ENGINE, ACTIVATED FIRE EXTINGUISHER, DUMPED FUEL AND RETURNED TO ZSPD. FOUND PRESSURE RELIEF VALVE (PRV) WILL NOT STAY CLOSED. REMOVED AND REPLACED PRV AND LEA
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