Boeing 747-238B
Service difficulty reports · 371
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 = '747238B' 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 = '747238B' 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 CALA9700006Stringer · crackedINSPECTION FOUND CRACKS IN STRINGER 2R AND 2AR AT BS 741. THERE WERE A TOTAL OF FOUR CRACKS MEASURING 2.5, 1.18, 1.38, AND 0.62 LONG. THE STRINGERS WERE REPAIRED IAW ECRA 5310-03383.SDR CALA9700007Skin · corrodedINSPECTION FOUND CORROSION IN SKIN LAP SPLICE AT SEVERAL LOCATIONS FROM BS 520 TO 741, STRINGER 6L. THE SKIN WAS REPAIRED IAW ECRA 5330-02472.SDR CALA9700015Fitting · crackedINSPECTION FOUND SPLICE FITTING AND UPPER SPLICE PLATE CRACKED AT LT WING REAR SPAR. THE CRACKS WERE 0.040 AND .25 INCH LONG. THE SPLICE PLATE AND SPLICE FITTING WERE REPLACED IAW EA 5710-01199 AND BOEING SB 57-2110.SDR CALA9700003Doubler · corrodedINSPECTION FOUND CORROSION ON LT WING OUTBOARD TRAILING EDGE MID FLAP OUTBOARD DOUBLER. THE DOUBLER WAS REPAIRED IAW ECRA 5750-02581.SDR CALA9700002Lug · wornINSPECTION FOUND LT WING NR 4 MOVEABLE FLAP TRACK FAIRING DRIVE ARM LOWER OUTBOARD HINGE OUTBOARD LUG WORN. THE WORN AREA WAS REPAIRED IAW ECRA 5750-02580.SDR CALA9700001Frame · crackedINSPECTION FOUND A 1.75 INCH CRACK IN RT FRAME AT BS 220, STRINGER 32A. THE FRAME WAS REPAIRED IAW ECRA 5310-03374.SDR CALA9700022Stringer · crackedINSPECTION FOUND A .125 INCH CRACK IN STRINGER 3R AT MAIN DECK BS 2180 TO 2190. THE STRINGER WAS REPAIRED IAW SRM 53-10-03, FIGURE 6.SDR CALA9700017Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN STRINGER 9R AT BS 990 MANUFACTURING SPLICE LOCATION. THE STRINGER WAS REPAIRED IAW ECRA 5310-03384.SDR CALA9700016Skin · crackedINSPECTION FOUND A 0.040 CRACK AT THE RT WING EXTERNAL SPLICE FITTING AND A .1875 INCH CRACK AT THE MATING STRUCTURE WING CENTER SECTION UPPER SKIN PANEL. THE SPLICE FITTING WAS REPLACED IAW EA 5710-01199. THE SKIN PANEL WAS REPAIRED IAW ECRA 5710-01769.SDR CALA9700005Stringer · crackedINSPECTION FOUND A 0.87 INCH CRACK AT INBOARD VERTICAL FLANGE FASTENER HOLE OF STRINGER 9R AT THE MANUFACTURING SPLICE LOCATION, BS 1740. THE STRINGER WAS REPAIRED IAW ECRA 5310-03373.SDR CALA9700024Skin · delaminatedINSPECTION FOUND LT WING INBOARD MID FLAP PANEL NR 577KT SKIN DELAMINATED. A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-06, FIGURE 15.SDR CALA9700014Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN FRAME AT MAIN DECK BS 360, LT SIDE, BETWEEN STRINGER 15 AND 16. THE FRAME WAS REPAIRED IAW ECRA 5310-03376.SDR CALA9700012Frame · crackedINSPECTION FOUND A .75 INCH CRACK IN FRAME AT BS 360 ON RT SIDE, STRINGER 14E. THE FRAME WAS REPAIRED IAW ECRA 5310-03375.SDR 96UAL900853Light · inoperativeEMERGENCY EXIT LIGHT STRIP AT SEAT 34 H, J, K INOP. REPLACED EEL POWER FEEDER AND EEL LAMP SEGMENTS.SDR CALA9700025Fitting · corrodedINSPECTION FOUND LT AND RT WING TO BODY KICK FITTINGS CORRODED. THE BODY KICK FITTINGS WERE REPAIRED IAW ECRA 5340-01283.SDR CALA9700021Spar Web · crackedINSPECTION FOUND A .1875 INCH CRACK AT FASTENER HOLE OF NR 2 PYLON WING FRONT SPAR VERTICAL WEB AT INBOARD NACELLE RIB POST ATTACH AREA, WS 688. THE FRONT SPAR VERTICAL WEB WAS REPAIRED PER BOEING DRAWING 112U8040, FCD 5710-01758 AND SRM 51-10-01.SDR CALA9700004Splice · crackedINSPECTION FOUND STRINGER SPLICE CORRODED WITH A 1.8 INCH CRACK ALONG FLANGE AT BS 1480, STRINGER 1L. THE STRINGER SPLICE WAS REPLACED IAW ECRA 5310-03380.SDR 96UAL900849Light · inoperativeEMERGENCY BUSTLE LIGHT IS INOP AT DOOR 1 LEFT LIGHT FAILED. REPLACED SLIDE LIGHT ASSEMBLY.SDR CALA9700026Skin · corrodedINSPECTION FOUND CORROSION AT RT WING LOWER SKIN FORWARD OF FRONT SPAR LOWER CHORD AND EXTENDING AFT OF FRONT SPAR BETWEEN WS 1454 AND WS 1548. THE AREA WAS REPAIRED IAW ECRA 5710-01766.SDR CALA9700018Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD SHEAR TIE AT LT WING NR 2 MAIN TANK WS 670, UPPER STRINGER 27 AND A .5 INCH CRACK WAS FOUND AT SHEAR TIE OF RIB CHORD, LOWER STRINGER 19. THE RIB CHORD AT UPPER STRINGER 27 WAS REPAIRED IAW SB 57-2273. THE RIB CHORDSDR CALA9700013Frame · crackedINSPECTION FOUND A 2 INCH CRACK IN FRAME AT THE OUTBOARD FRAME WEB BETWEEN STRINGER 26R AND 27AR, BS 280. THE FRAME WAS REPAIRED IAW ECRA 5310-03370.SDR CALA9700011Frame · crackedINSPECTION FOUND A .75 INCH CRACK IN FRAME AT BS 380, STRINGER 23R. THE FRAME WAS REPAIRED IAW ECRA 5310-03367.SDR CALA9700023Bulkhead Chord · crackedINSPECTION FOUND A .125 INCH CRACK AT FASTENER HOLE COMMON TO THE AFT BULKHEAD VERTICAL CHORD LT FITTING OF NR 2 PYLON. THE CHORD ASSEMBLY WAS REPLACED IAW BOEING DRAWING 65B90413 AND SRM 51-10-01.SDR CALA9700020Bulkhead · crackedINSPECTION FOUND A .125 INCH CRACK AT NR 3 PYLON FASTENER HOLE COMMON TO THE AFT BULKHEAD VERTICAL CHORD LT FITTING. THE NR 3 PYLON LT BULKHEAD ASSEMBLY WAS REPLACED IAW SRM 51-10-01 AND BOEING DRAWING 65B90413.SDR CALA9700019Bulkhead · crackedINSPECTION FOUND A 2 INCH CRACK AT UPPER POSITION OF NR 4 PYLON AFT BULKHEAD INBOARD CHORD. THE CHORD AND AFT BULKHEAD ASSEMBLY WERE REPLACED IAW SRM 57-10-01 AND SB 747-54A2159.SDR 96UAL900800Pump · leakingLOST NR 4 HYDRAULIC SYSTEM FLUID. *S/D* FOUND HYDRAULIC FLUID LEAKED FROM ENGINE DRIVEN PUMP. REPLACED ENGINE DRIVEN PUMP, CASE DRAIN FILTER AND PRESSURE FILTER.SDR 96UAL900782Light · inoperativeDOOR 1R EMERGENCY BUSTLE LIGHT INOP. REPLACED LIGHT ASSY.SDR TWRA96327Bearing Tube · cloggedAFTER STARTING NR 4 ENGINE, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. FURTHER EVALUATION NEEDED ON THE ENGINE. MAINTENANCE FOUND NR 3 BEARING TUBE CLOGGED. RETRIEVED CARBON DEPOSIT ON NR 3 COMPARTMENT. REMOVED AND REPLACED EVC AS PER TC 75-361. RAN ENGINESDR TWRA96321Socket · failedDURING DAILY CHECK, FOUND EMERGENCY LIGHT OUT BY SEAT 43C AND 64H. REMOVED AND REPLACED SOCKET SYSTEMS CHECKED NORMAL PER MM 33-51-00. (M)SDR 96UAL900744Duct · rupturedUNABLE TO MAINTAIN CABIN PRESSURE. PNEUMATIC CROSS-OVER DUCT RUPTURED IN-FLIGHT. DUCT FAILED NEAR A WELD. CAUSE UNKNOWN. DUCTS REPLACED. PART TOTAL CYCLES, 2,804.SDR 96UAL900712Light · inoperativeEMERGENCY LIGHT ABOVE MAIN ENTRY DOOR 2 LEFT IS INOP. LIGHT BURNED OUT, REPLACED LIGHT ASSEMBLY.SDR 96UAL900711Battery Pack · dischargedFORWARD RIGHT HAND OVERWING EMERGENCY LIGHT ASSEMBLIES INOP. BATTERY PACK DEAD, REPLACED BATTERY PACK.SDR TWRA96313Wire · brokenDURING DAILY CHECK, FOUND RIGHT WING THIRD OVERWING EVAC LIGHT IS INOP. FOUND BROKEN WIRE. REPAIRED WIRE, OPS CHECKED GOOD PER MM 33-51-00 PAGE 501. (M)SDR 96UAL900685Engine · bird strikeON TAKEOFF ROLL, HEARD LOUD BANG AND VIBRATION. ABORTED TAKEOFF AT 138 KNOTS. FOUND NR 3 ENGINE INGESTED BIRDS.SDR TWRA96309Light · inoperativeDURING DAILY CHECK, FOUND EMERGENCY LIGHT INOP AT L4 DOOR. REMOVED AND REPLACED LIGHT ASSY. OPS CHECKED NORMAL PER MM 33-51-00. (M)SDR TWRA96310Wire · brokenDURING DAILY CHECK, FOUND D-ZONE EVAC FLOOR LIGHT AT SEAT 43C INOP. FOUND BROKEN WIRE, RESPLICED WIRE. OPS CHECKED GOOD PER MM 33-51-00. (M)SDR 96UAL900670Engine · failedNR 2 ENGINE FILTER BYPASS LIGHT ON, BREATHER TEMPERATURE PEGGED AT 226 DEGREES AND ENGINE SHUT DOWN. *S/D* ENGINE REPLACED. TEARDOWN OF ENGINE REVEALED EVIDENCE OF FIRE IN NR 3 BEARING COMPARTMENT. CAUSE OF FIRE UNKNOWN.SDR 96UAL900650Light · inoperativeDOOR 4 RIGHT, EMERGENCY CEILING LIGHT IS INOPERATIVE. REPLACED LIGHT.SDR 96UAL900639Flap · corner missingOUTBOARD CORNER OF NR 16 KRUEGER PLAP WAS FOUND MISSING. DETAILED INVESTIGATION OF THE REMAINING FLAP STRUCTURE FOUND NO DELAMINATION OR CRACKS. INSTALLED DOUBLER REPAIR.SDR TWRA96262Bulb · failedDURING DAILY CHECK, FOUND FLOOR EMERGENCY LIGHT INOP AT 5C, 39H, 42C. RELAMPED, OPS CHECKED OK PER MM 33-51-00. (M)SDR TWRA96258Wire · brokenDURING DAILY CHECK, FOUND EMERGENCY EVAC LIGHT INOP AT ROW 7H. RESPLICED WIRE. OPS CHECKED NORMAL AS PER MM 33-51-00. (M)SDR TWRA96250Bulb · failedDURING DAILY CHECK, FOUND EVAC LIGHT FLOOR AT SEAT 25H BLINKS AND REMAINS OUT SEVERAL SECONDS. RELAMPED, OPS CHECK OK PER MM 33-51-00 PG 501. (M)SDR TWRA96254Lens · missingDURING DAILY CHECK, FOUND FLOOR EVAC LIGHT AT SEAT 22H INOP. REPLACED LENS AND BULB. OPS CHECKED OK PER MM 33-51-00 PG 501. (M)SDR TWRA96253Bulb · failedDURING DAILY CHECK, FOUND RT WING NR 4 OVERWING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED NR 4 FORWARD ON RIGHT SIDE OVERWING LIGHT. OPS CHECKED OK PER MM 33-51-00 PG 501. (M)SDR TWRA96247Bulb · failedDURING DAILY CHECK, FOUND 38H FLOOR EMERGENCY LIGHT IS INOP. RELAMPED, OPS CHECKED OK PER MM 33-51-00. (M)SDR 96ZZZM1253Bulb · failedDURING DAILY CHECK, FOUND FLOOR EVAC LIGHT AT SEAT 22H INOP. REPLACED LENS AND BULB. OPS CHECKED OK PER MM 33-51-00 PG 501. REFERENCE TWRA96254.SDR TWRA96244Lens · missingDURING DAILY CHECK, FOUND UPPER DECK AFT OF 73K, FLOOR EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT LENS AND BULB. OPS CHECKED OK PER MM 33-51-00 PG 501. (M)SDR TWRA96243Lens · missingDURING DAILY CHECK, FOUND FLOOR EMERGENCY LIGHT INOP AT 4H, 42C, 45C AND 50 C. REPLACED LENS AND BULB. OPS CHECKED NORMAL AS PER MM 33-51-00 PG 501. (M)SDR 96ZZZM1280Bulb · failedDURING DAILY CHECK, FOUND FLOOR EMERGENCY LIGHT INOP AT 4H, 42C, 45C AND 50 C. REPLACED LENS AND BULB. OPS CHECKED NORMAL AS PER MM 33-51-00 PG 501. REFERENCE TWRA96243.SDR 96ZZZM1279Bulb · failedDURING DAILY CHECK, FOUND UPPER DECK AFT OF 73K, FLOOR EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT LENS AND BULB. OPS CHECKED OK PER MM 33-51-00 PG 501. REFERENCE TWRA96244.
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