Boeing 747-200
Service difficulty reports · 651
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 = '747200' 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 = '747200' 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 UPS06447030Strap · crackedINSPECTION TYPE:C M/D RIGHT BS 800 FRAME INNER FLANGE BETWEEN S26R-17R FOUND 1EA FASTENER LOCATION CRACKED AT FRAME STRAP. CRACK LENGTH 1.25 INCH. REPAIRED AS PER RS R53-10-35484 AND UPS EO B747-5310-24451-A.SDR UPS06447021Support Fitting · crackedINSPECTION TYPE:C AFT CARGO COMPT BS 1910 LBL 46 FIXED END STOP O/B SUPPORT FITTING FOUND CRACKED. CRACK LENGTH .375 INCH. AFT CARGO COMPT BS 1910 LBL 46 FIXED END STOP O/B SUPPORT FITTING REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.SDR UPS06447015Beam · corrodedINSPECTION TYPE:C FWD CARGO DOOR INTERNAL LINER ATTACH BEAM A/NUT AREA FOUND SURFACE CORRODED FS 580 FWD AS MARKED. CORROSION BLEND OUT 0.070" X 1" X 1" EXCEES SRM LIMIT. FWD CARGO DOOR INTERNAL LINER ATTACH BEAM FWD OF BS 580 LOWER AREA REPAIRED AS PER SRM SDR UPS06447000Frame · crackedINSPECTION TYPE:C M/D LEFT BS 434 FRAME AT S26L FOUND 2EA HOLE CRACKED AT FRAME WEB AND AFT WEB DOUBLER. CRACK LENGTH 0.040 INCH. M/D LEFT BS 434 FRAME WEB & DOUBLER REPAIRED BETWEEN STR 23 TO STR 30 AREA AS PER SRM 53-10-04 FIG 99.SDR UPS06446999Web · corrodedINSPECTION TYPE:C FWD CARGO COMPT TORQUE BOX UPPER ACCESS PANEL UPPER SURFACE FOUND SURFACE CORROSION AT STA 660-680 RBL 50 TO RBL 57. CORROSION BLEND OUT 0.055" X 1" X 4" EXCEED SRM 53-10-01 FIG 1 LIMITS, WEB REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 5SDR UPS06446978Frame · crackedINSPECTION TYPE:C M/D RIGHT BS434 FRAME S26R AREA FOUND 2EA HOLE CRACKED AT AFT WEB DOUBLER. CRACK LENGTH .125 AND .0625 INCH. M/D RIGHT BS 434 FRAME WEB DOUBLER REPAIRED AT BETWEEN STR 23 TO S30 AREA AS PER SRM 53-10-04 FIG 9.SDR UPS06446977Fitting · crackedINSPECTION TYPE:C LT WING NR 2 L/E PDU FWD SUPPORT ATT NOSE BEAM UPPER CHORD FOUND CRACK AS MARK, NR 7 VC FLAP I/B. CRACK LENGTH .625 AND 2.5 INCH. LT WING NR 2 L/E PDU FWD SUPPORT ATT NOSE BEAM UPPER CHORD AT BETWEEN AILES 949 - 962 AREA REPAIRED AS PER SRMSDR UPS06446971Attach Bracket · crackedINSPECTION TYPE:C M/D BS 434 FRAME ATT BRACKET AT S26R FWD FOUND CRACKED. CRACK LENGTH .25 INCH. BRACKET REPLACED AS PER SRM 51-10-01 PG 9, 51-30-05 AND INSTALLED AS PER SRM 51-30-02.SDR UPS06446968Frame · crackedINSPECTION TYPE:C M/D LEFT BS 434 FRAME ABOVE S26L AREA FOUND 1EA HOLE CRACK AT FRAME INNER CHORD. CRACK LENGTH .0625 INCH. FRAME CHORD REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.SDR UPS06446897Stiffener · crackedINSPECTION TYPE:C NWW TOP PANEL BS 260-280 BL 0 STIFFENER FOUND CRACK AT PREVIOUS REPAIRED AREA. CRACK LENGTH .25 INCH. NWW TOP PANEL BS 260-280 BL 0 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.SDR UPS06446896Stiffener · crackedINSPECTION TYPE:C NWW TOP PANEL BS 280-300 LBL 10 STIFFENER RADIUS AREA FOUND CRACK APPROX .75 INCH. NWW TOP PANEL BS 280-300 LBL 10 STIFFENER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.SDR UPS06447017Bolt · shearedINSPECTION TYPE:C LEFT BLG WHEEL WELL LBL 15 SUSPECT 1EA MOUNT BOLT FOUND SHEARED AS MARKED AT STA 1350 KEEL BEAM. BORE HOLE REAMED TO 0.776 INCH. BOLT REPLACED AS PER MM 20-51-01 AND BOLT HOLE INSPECTED AFTER NEW FITTING REPLACED AND INSTALLED AS PER SRM 51SDR UPS06446972Clip · crackedINSPECTION TYPE:C N/G WHEEL WELL LT SIDEWALL PANEL VERTICAL BEAM TYPICAL CLIP FOUND CRACK AS MARK AT STA 280 WL 163 LBL 30. CRACK LENGTH .25 INCH. N/G WHEEL WELL LT SIDEWALL PANEL VERTICAL BEAM CLIP REPLACED AND INSTALLED AT BS 280 WL 163 LBL 30 AREA AS PER SDR UPS06446892Clip · crackedINSPECTION TYPE:C N/G WHEEL WELL RT SIDEWALL PANEL VERTICAL BEAM TYPICAL CLIP FOUND CRACK AS MARK AT RBL 30 STA 280 WL 182. CRACK LENGTH .25 INCH. N/G WHEEL WELL RT SIDEWALL PANEL VERT BEAM CLIP AT BS 280 WL 182 REPLACED AND INSTALLED AS PER SRM 51-10-01 PG SDR UPS06446996Rib · crackedINSPECTION TYPE:C LEFT WING - SURGE TANK WS 1516 RIB LWR STR 6 & 9 SUSPECT CRACK. CRACK LENGTH 1.125 INCH. LEFT WING WS 1516 RIB LWR STR -9 AREA REINSPECTED BY NDT, NO CRACK REVEALED AND STR -6 AREA REPAIRED AS PER SRM 57-10-05 FIG 4.SDR UPS06446995Rib · crackedINSPECTION TYPE:C RIGHT WING SURGE TANK WS 1516 RIB UPPER CHORD STR 8 FOUND CRACKED. CRACK LENGTH 0.625 INCH. RIGHT WING SURGE TANK WS 1516 RIB UPPER CHORD STR 8 AREA REPAIRED AS PER SRM 57-10-05 FIG 3.SDR UPS06446994Rib · crackedINSPECTION TYPE:C RIGHT WING SURGE TANK WS 1516 RIB LOWER CHORD STR 6 AND STR 8 FOUND CRACKED. CRACK LENGTH 0.75 INCH & 1 INCH. RIGHT WING SURGE TANK WS 1516 RIB LOWER CHORD STR 6 TO THE FWD END AREA REPAIRED AS PER SRM 57-10-05 FIG 4.SDR WRNA200600011Fuel Control · malfunctionedAFTER TAKEOFF NR 4 ENGINE EGT STARTED FLUCTUATING AND STARTED TO CLIMB PAST 900 DEGREES, REDUCED POWER TO 1.29 EPR. AFTER POWER REDUCTION TEMPERATURE WAS STILL 850 DEGREES, EPR WAS LOWER (1.25) THAN OTHER J ENGINES. ACFT RETURNED TO MIA AND MADE A SAFE LANDISDR WRNA200600009Packing · damagedIN CRUISE OIL PRESSURE LIGHT FLASHING, EGT, N1, N2, OIL TEMP NORMAL OIL PRESSURE 40 PSI, OIL QTY. PERFORMED ENGINE FAILURE PRECAUTIONARY SHUTDOWN CHECKLIST. DIVERTED TO CLOSEST AIRPOR. ENGINE WINDMILLING FLT TIME 20 - 25 MINS, PART OF THAT TIME ENGINE OIL PSDR WRNA200600008Engine · shutdownPRECAUTIONARY SHUTDOWN NR 4 ENGINE DUE TO LOSS OF OIL PRESSURE, ALL OTHER INDICATIONS NORMAL. WINDMILLING OIL PRESSURE STAYED ABOVE 10 PSI. PERFORMED INLET & EXHAUST VISUAL INSPECTION, NO DEFECTS. PERFORMED WINDMILL INSPECTION PER MM 72-00-00 PG 682 W/X 3F SDR WRNA200600007Engine · shutdownNUMBER 4 ENGINE COMPRESSOR STALL BELOW 60 KTS, SHUTDOWN ENGINE, EGT WENT TO 1090 FOR 3 SECONDS. PERFORMED BORESCOPE INSPECTION OF LPC, HPC, COMBUSTION CHAMBER ASSY, HPT AND LPT, IAW 72-00-00 PG 601, NO DEFECTS NOTED. PERFORMED OVER TEMPERATURE VISUAL INSPECTSDR UPS06446386Rib · crackedINSPECTION TYPE:C LT WING O/B MID FLAP SLIDING TRACK RIB FOUND CRACKED, CRACK LENGTH 1 INCH. LT WING O/B MID FLAP SLIDING TRACK RIB REPLACED AS PER SRM 51-10-01 PG 9.SDR UPS06446315Doubler · crackedINSPECTION TYPE:C U/D BS 480 BTN S11L & S12L FRAME DOUBLER FOUND CRACKED, CRACK LENGTH .5 INCH. U/D BS 480 BTN S11L - S12L FRAME DOUBLER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.SDR UPS06446249Frame · crackedINSPECTION TYPE:C COCKPIT BS 360 STR 10AL FRAME INNER CHORD FOUND CRACKS FROM 1EA FASTENERS HOLE AS MARKED, CRACK LENGTH .125 INCH. COCKPIT BS 360 STR 10-15L FRAME INNER CHORD REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.SDR UPS06446343Fitting · wornFOUND FUS BS 1000 S39R END FTG CROSS MOUNT BOLT AREA WORN OUT. BS 1000 STR 39R END FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND EO B747-5310-18579-F FIG 10.SDR UPS06446341Fitting · wornFOUND BS 1000 S37R END FTG CROSS MOUNT BOLT AREA WORN OUT. BS 970- BS 983 STR 37R REPAIRED AS PER SRM 53-10-03 FIG 1 AND STR 37R END FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & EO NR B747-5310-18579 APPENDIX 'F' FIG 10.SDR UPS06446248Splice · damagedINSPECTION TYPE:C U/D - BS 420-425 STR 10L STRINGER SPLICE FASTENER HOLES FOUND ELONGATED. BS 420-425 STR 10L STRINGER SPLICE REPLACED AS PER SRM 51-10-01 PG 9.SDR UPS06446217Panel · debondedINSPECTION TYPE:C RIGHT WING O/B AFT FLAP TOP PNL 688KT AFT EDGE MIDWAY AREA DEBONDED. DEBONDED AREA ACCOMPLISHED METAL HOT BOND REPAIR AS PER SRM 51-40-24 FIG 2.SDR UPS06446311Clip · crackedBS 480 STR 11L FRAME FWD AND AFT FACE ATT CLIP FASTENER HOLES FOUND ELONGATED. CRACK LENGTH 3/8". FWD AND AFT ATT CLIPS 2 REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.SDR UPS06446310Splice · crackedFOUND BS 500 STR12L STRINGER SPLICE FOUND CRACKED. CRACK LENGTH 3/8". STRINGER SPLICE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.SDR UPS06446308Stringer Clip · crackedBS 500 STR12L FRAME FWD FACE ATT TIE CLIP FOUND CRACK. CRACK LENGTH 1/4". TIE CLIP REPLACED AS PER SRM 51-10-01 PG9 AND INSTALLED AS PER SRM 51-30 -02.SDR UPS06446251Support Fitting · crackedINSPECTION TYPE:C FWD CARGO COMPT - REAR STOP FITTING SUPPORT FRAME FOUND CRACKED AT STA 960 TO STA 970 RBL 25 SEAT TRACK ATT SURFACE, CRACK LENGTH 5 INCHES. SUPPORT FITTING REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.SDR UPS06446230Floorbeam · misdrilledINSPECTION TYPE:C U/D BS 380 FWD FLANGE RBL 61, 66 AND 71 SHORT EDGE MARGIN FOUND. U/D BS 380 FLOORBEAM UPPER CHORD FWD FLANGE RBL 56" TO RBL 76" AREA REPAIRED AS PER EO NR B747-5320-12407 FIG 2 PLAN B.SDR UPS06446229Floorbeam · misdrilledINSPECTION TYPE:C U/D BS 380 FWD FLANGE RBL 51, 52.5, 53.5 AND 55 SHORT EDGE MARGIN FOUND. U/D BS 380 FLOORBEAM UPPER CHORD FWD FLANGE AT RBL 51". REPAIRED AS PER EO B747-5320-12407 FIG 2 PLAN B & RBL 52.5", 53.5" AND 55" AREA. REPAIRED AS PER EO B747-5320-SDR UPS06446378Spar · crackedINSPECTION TYPE:C RT WING FRONT SPAR WEB AT FSSI 688 FOUND 2EA FASTENER HOLES CRACKED, CRACK LENGTH .5 INCH & .125 INCH. RT WING FRONT SPAR WEB REPAIRED AS PER RS R57-21-35443 JUST BETWEEN FSSI 670 & FSSI 695 AND UPS EO B747-5720-23833-A.SDR UPS06446238Stringer · crackedINSPECTION TYPE:C BS 980-1000 S38L FOUND CRACK AT STRINGER 3EA FASTENER HOLES APPROX 1/16" LONG. FWD CARGO COMPT BS 970 TO BS 1000 S38L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.SDR UPS06446216Panel · dentedINSPECTION TYPE:C RIGHT WING - I/B AFT FLAP UPPER O/B FLAP PANEL 678IT FOUND DENT MARK AT LOWER SURFACE. DENT AREA ACCOMPLISHED METAL HOT BOND REPAIR AS PER SRM 51-40-22 FIG 3.SDR UPS06446388Angle · crackedINSPECTION TYPE:C E/E COMPT BS 400 LBL 27 NWW REAR PANEL INTERCOSTAL VERTICAL ANGLE FOUND CRACKED, CRACK LENGTH .3125 INCH. VERTICAL ANGLE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.SDR UPS06446387Angle · crackedINSPECTION TYPE:C E/E COMPT - BS 400 RBL 27 NWW REAR PANEL INTERCOSTAL VERTICAL ANGLE FOUND CRACKED, CRACK LENGTH .375 INCH. VERTICAL ANGLE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.SDR UPS06446380Skin · crackedINSPECTION TYPE:C AFT CARGO DOOR CUTOUT FWD HINGE MOST FWD LOWER FASTENER HOLE FOUND CRACK AT SKIN RUNNING FWD APPROX 0.030 INCH. AFT CARGO DOOR CUTOUT FWD HINGE MOST FWD LOWER FASTENER HOLE AT SKIN AREA REPAIRED AS PER RS R53-61-35445 CONTINUE OPEN HOLE INSPSDR UPS06446344Fitting · corrodedFWD CARGO COMPT REF NRC NR 5726 LT BATH FITTING ATT SURFACE FOUND HEAVY CORROSION AT STA 983 STR 38L PRESSURE BULKHEAD (AFTER FTG REMOVED ). CORROSION BLEND OUT 0.100" BY 2" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS, BS 1000 STR 38L UPPER BATH TUB FTG REPLACED SDR UPS06446322Support · crackedINSPECTION TYPE:C RT WING - O/B MID FLAP ACCESS PANEL 687NT AFT SUPPORT O/B AREA CRACKED, CRACK LENGTH 12 INCHES. RT WING - O/B MID FLAP ACCESS PANEL 687NT AFT SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 3.SDR UPS06446314Doubler · crackedINSPECTION TYPE:C COCKPIT - BS 500 STR 11L FRAME DOUBLER FOUND CRACK AT O/B AREA, CRACK LENGTH .5 INCH. COCKPIT BS 500 STR 11L TO STR 16L FRAME DOUBLER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.SDR UPS06446306Access Panel · corrodedL/W O/B AFT FLAP ACCESS PANEL NR 588KT AFT SUPPORT I/B AREA CORROSION CRACK REVEALED. CORROSION BLEND OUT 0.055" BY 1" BY 3" EXCEED SRM 57-50-01 FIG 3. LIMIT AFT SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 4 AND HFEC INSP C/OUT AS PER NTM PART6 51-00-0 FIG 4. SDR UPS06446294Flap Track · chafedO/B MID FLAP I/B SLIDE TRACK I/B WEB AFT AREA DEEP CHAFING REVEALED. RHW O/B MID FLAP O/B SLIDE TRACK I/B WEB REPAIRED AS PER SRM 51-40-02 FIG 1.SDR UPS06446288Plate · crackedE/E COMPT BS 400 BL0 FX INTERCOSTAL SPLICE PLATE FOUND CRACKED. CRACK LENGTH 1.75". SPLICE PLATE REPLACE AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30- 02SDR UPS06446372Frame · crackedBS480 STR 11L FOUND O/B AREA FOUND CRACK. CRACK LENGTH 7/8" TO 1". BS 480 S10L AND ABOVE U/B FLOORBEAM AREA FRAME REPAIRED AS PER RS R53-10-35447 CONTINUED INSPECTION REQUIRE WHILE PERFORMING SB747-53A2265 INSPECTIONS AND REPLACEMENT WITH SB747-53-2272 MOD RSDR UPS06446370Frame · crackedBS 500 STR 11L FRAME O/B AREA FOUND CRACK. CRACK LENGTH 3/4". BS 500 BETWEEN STR 8L TO STR 13L FRAME REPAIRED AS PER SRM 51-40-03 FIG2.SDR UPS06446369Frame · crackedBS480 STR11-12R FRAME O/B AREA FOUND CRACKED. CRACK LENGTH 5/8" TO 1". BS480 BETWEEN STR 10R AND ABOVE U/D FLOORBEAM AREA FRAME REPAIRED AS PER RS R53-10-35447. CONTINUED INSPECTION REQUIRE WHILE PERFORMING SB747-53A2265 INSPECTIONS AND REPLACEMENT WITH SB7SDR UPS06446364Frame · crackedCOCKPIT BS 360 STR 10L TO STR 10AL FRAME O/B AREA FOUND CRACK, CRACK LENGTH 1" & 0.125". COCKPIT BS360 STR9L TO STR10AL FRAME REPAIRED AS PER RS R53-12-35434 CONTINUED INSPECTIONS REQUIRE WHILE PERFORMING SB 747-53A2265 INSPECTIONS AND REPLACEMENT WITH SB747-
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