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 UIEA00049Engine · flamed outFLT 9027 - BOM-MAA - NR 2 ENGINE FLAME OUT AT FL370. ALL ENGINE INDICATIONS WERE NORMAL AND ENGINE WAS RUNNING FINE. ACCOMPLISHED IN FLIGHT RESTART AT FL290. MAINTENANCE CHECKED ENGINE INLET AND EXHAUST AREA AND NO DEFECTS WERE FOUND. INSPECTED ENGINE TUBISDR UIEA00026Frame · crackedDURING A CHECK, FOUND FUSELAGE FRAME STATION 1760 CRACKED AT APPROX WL 250R ON MAIN DECK. FRAME CRACK STOP DRILLED AND REPAIR DOUBLERS INSTALLED PER SRM 51-10-04. (M)SDR UIEA0020Floorbeam · crackedDURING SB747-53A2416 INSPECTION OF BS 1265, A CRACK WAS DISCOVERED EMANATING FROM A FRAME WEB FASTENER HOLE ON THE MAIN DECK FLOORWEB AT WL 199, LBL 120. REPAIRED ACCOMPLISHED BY INSTALLING A FRAME WEB DOUBLER, INTERCOSTAL DOUBLER AND AN ATTACHING ANGLE IAW ASDR UIEA0017Skin · damagedDURING INTERNAL INSPECTION OF PYLON NR 1, NR 2, NR 3 STRUCTURE SURROUNDING THE PRECOOLER EXHAUST EXIT AREA FOUND METAL DISCOLORED AND EXTERNAL SKIN CREASED. OVER TEMPERATURE ANALYSIS INDICATED TEMPER LOSS AND HEAT RELATED DAMAGE. AFFECTED STRUCTURE AND SKIN SDR UIEA0011Intercostal · crackedFOUND NR 3 LEFT/RIGHT MAIN ENTRY DOOR FRAME CRACKED AT BS 1265. LEFT CRACKED 1.6875 INCH ON EACH SIDE OF RIVET. PER BOEING SB 747-53A2416 TRIMMED OUT CRACKED AREA AND FILLER REPAIRED FRAME. REFERENCE KLM DRAWING KLM-AMS-99-0913RE FOR REPAIRS UP TO 3 INCHES.SDR UIEA0012Fitting · corrodedRIGHT STATION 1480 BULKHEAD CORROSION REPAIR COMMON TO STRINGER 38R. FOUND HOLES NR 2, 3, 5, 7, AND NR 10 CRACKED. REAMED HOLES OVERSIZE, ALL WITHIN LIMITS PER SB 747-53A2390. OVERSIZED FASTENERS INSTALLED. (M)SDR UIEA0013Fitting · crackedLEFT STATION 1480 BULKHEAD CORROSION REPAIR COMMON TO STRINGER 38L. FOUND HOLES NR 3, 4, 7, 8, 9, 10 AND NR 11 CRACKED. REAMED HOLES OVERSIZE, AND INSTALLED BUSHING REPAIRS AT LOCATION NR 3, 7, 8, 9, 11. OVERSIZED FASTENERS INSTALLED PER SB 747-53A2390. (MSDR UIEA0014Splice · damagedLEFT STATION BULKHEAD CHORD SPLICE FITTING 65B14682-3 FOUND TOOLING MARKS DURING DISASSEMBLY. PER BOEING TELEX TLS-TPE-00-00047F, BLEND ALL TOOLING MARKS. ALL TOOL MARKS BLENDED. (M)SDR UIEA0015Spar · corrodedSURFACE CORROSION DETECTED CENTER SECTION REAR SPAR LEFT/RIGHT. CORROSION MAPPED, MEASURED, CLEANED AND TREATED BY BOEING FIELD TEAM. ALL WITHIN LIMITS. AREAS OF REWORK ARE; LEFT FASTENERS NR 7, 8, 9, RIGHT FASTERNERS NR 2, 3, 4, 5, 6, 7, 8, 9, 13, 14, 23 ASDR 20000505AP036Spar · corrodedFOUND CORROSION ON WING CTR SECTION REAR SPAR RBL 99, COMMON TO REAR BULKHEAD FITTING AND INBOARD WEB OF LEG TO TWO BOLT HOLES WHILE PERFORMING SB 747-57-2263. CLEANED, TREATED, MEASURED CORROSION. APPLIED FINISH. ALL WITHIN ACCEPTABLE LIMITS. (M)SDR UIEA9947Manifold · crackedORD/MXP - FLT AZ9163/02 - DURING CLIMB-OUT AT 4,000 FEET, NR 4 ENGINE NACELLE TEMPERATURES INDICATED 7.6 DEGREES ON BOTH 'A' AND 'B' LOOPS. TEMPERATURE DECREASED WHEN THROTTLE WAS RETARDED. CLOSED BLEED VALVE ACCORDING TO FHB PROCEDURE. AS NR 4 THROTTLE WAS SDR UIEA9911Csd · failedFLT 7127 - MIA/VCP - NR 4 CSD OIL LIGHT 'ON', CSD OIL TEMPERATURE HIGH (OUT OF RANGE 150 PLUS). ATTEMPT TO DISCONNECT CSD UNSUCCESSFUL. CSD RPM '0', PMG VOLTS '70'. FOLLOWED ALL DISCONNECT PROCEDURES THEN SHUTDOWN NR 4 ENGINE. ON ARRIVAL AT VCP MAINTENANCE FSDR UIEA9901Fire Detector · malfunctionedAPU FIRE WARNING CAME ON SEVERAL TIMES. DISCHARGED BOTTLE AS PRECAUTION. MAINTENANCE AT ANC INSPECTED APU COMPARTMENT, NO DAMAGE OR FIRE NOTED. PLEASE NOTE, APU PREVIOUSLY DEFERRED DUE WILL NOT ACCELERATE ABOVE 60 PERCENT. APU FIRE WARNING SYSTEM DEFERRED SDR UIEA9805Turbine · failedANC - AFTER TAKEOFF AT FL 310, NR 2 ENGINE FLAMED OUT IN CRUISE. ATTEMPTED RE-START ENGINE AND NO HELP. NO N2 INDICATION. AIRCRAFT DUMPED FUEL AND HAD UNEVENTFUL RETURN TO ANC. DURING INSPECTION OF ENGINE AT ANC, FOUND EVIDENCE OF METAL IN THE TAIL PIPE ANSDR UIEA9803Probe · missingDURING MAINTENANCE SERVICE AT MIA, DISCOVERED THE EGT PROBE AND WELDED BOSS AT THE 12 O'CLOCK POSITION ON NR 4 ENGINE CASE NEAR THE AFT ENGINE MOUNT WAS MISSING. EXHAUST AIR ESCAPING THROUGH THE RESULTING HOLE IN THE CASE CAUSED DAMAGE TO THE AREA AND STRUT. SDR CALA9801232Light · inoperativeINSPECTION FOUND L-1 DOOR MOUNTED SLIDE LIGHT INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-06.SDR CALA9800889Skin · puncturedINSPECTION FOUND A PUNCTURE IN FUSELAGE SKIN ABOUT 2 INCHES BELOW BOTTOM OF FORWARD CARGO DOOR AT BS 580-600. REPAIRED IAW SRM 53-30-03.SDR UIEA9802Engine · failedATB - FLT C1315 - ANC/TPE - NR 3 ENGINE FAILURE (FLAMEOUT) DURING CRUISE, FL 290, .84M..ENGINE VIBRATION NORMAL. ACCOMPLISHED ENGINE FAILURE SHUTDOWN CHECKLIST. AFTER CHECKLIST, N1 = 26.8, N2 = 0, F/F = 100, OIL PRESSURE = 0. FUEL DUMPED AND RETURNED TO ANCSDR CALA9800104Garlock Seal · leakingTHE NR 3 ENGINE OIL QUANTITY DECREASED TO ZERO WHILE EN ROUTE. THE NR 3 ENGINE WAS SHUTDOWN AND THE AIRCRAFT LANDED AT HNL WITHOUT INCIDENT. MAINTENANCE FOUND OIL LEAKING FROM CSD DRIVE PAD. THE GARLOCK SEAL AND ALL OIL SEALS WERE REMOVED AND REPLACED IAW MSDR CALA9701433Stiffener · crackedCRACK ON STIFFENER AND DISTORTION ON WEB AT FLOORBEAM UNDER TO UPPER CHORD STATION 1560 AND 1580 BETWEEN LBL 11 AND RBL 11. FABRICATED NEW STIFFENER AND INSTALLED IN ACCORDANCE WITH SRM 53-10-23 AND 51-40-01.SDR CALA9701434Stringer · corrodedDEEP CORROSION AND SHEARED RIVETS ON STR 51L AT FUSELAGE BILGE AFT CARGO STA 2260. INSTALLED NEW STRINGER AND REPAIRED IN ACCORDANCE WITH SRM 53-10-03 AND SRM 51-30-02.SDR CALA9701383Slide · inoperativeTHE UPPER DECK CREW DOOR EMERGENCY SLIDE ONLY PARTIALLY INFLATED DURING TEST WHILE AIRCRAFT WAS IN C-CHECK. MAINTENANCE NOTED THAT THE SLIDE BOTTLE HAD DISCHARGED. *S/D* INSPECTION OF THE SLIDE BY THE VENDOR FOUND DAMAGE TO THE PACKBOARD ASSEMBLY, THE INFLASDR UIEA9708Vsi Indicator · internal leakCREW REPORTS: MAINTENANCE LOG ITEM NR 1 - AFTER TAKEOFF, CAPTAIN'S AND FIRST OFFICER'S ALTIMETER SPLIT. WITH INCREASE IN ALTITUDE, THE SPLIT BECAME WORSE. CAPTAIN'S ALTIMETER 24,500 FEET, FIRST OFFICER'S ALTIMETER 20,000 FEET. MAINTENANCE LOG ITEM NR 2 - ASDR CALA9701102Skin · crackedINSPECTION FOUND A .875 INCH CRACK WITH CORROSION IN FUSELAGE SKIN AT BS 2220 BETWEEN STRINGERS 50R AND 51R. A SKIN REPAIR WAS INSTALLED IAW SRM 53-30-03, FIGURE 1 AND THE STRINGERS WERE REPAIRED IAW SRM 53-10-03, FIGURE 1.SDR CALA9700052Power Supply · inoperativeINSPECTION FOUND LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE, POSITION L3. THE POWER SUPPLY WAS REPLACED AND OPERATION CHECKED GOOD.SDR CALA9601814Stringer · corrodedINSPECTION FOUND STRINGER 50L CORRODED AT STA 1700 IN AFT CARGO COMPARTMENT. THE CORRODED SECTION WAS REMOVED AND A NEW STRINGER SECTION AND TWO SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-03, FIGURE 7.SDR CALA9601815Stringer · corrodedINSPECTION FOUND CORROSION AT STRINGER 51L, STA 1700 IN AFT CARGO COMPARTMENT. THE CORRODED SECTION WAS REMOVED, A NEW STRINGER SECTION AND TWO SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-03, FIGURE 7.SDR CALA9601813Support · corrodedINSPECTION FOUND CORROSION ON GALLEY SUPPORT BETWEEN STA 1350 AND 1360, LBL 11 TO 33. THE SUPPORT WAS REMOVED, A REPLACEMENT SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-07.SDR CALA9601812Angle · corrodedINSPECTION FOUND CORROSION AT T-ANGLE, STA 1380 BETWEEN LBL 11 AND RBL 11. THE ANGLE AND FILLER WERE REMOVED, REPLACEMENT PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-07.SDR CALA9601810Support · corrodedINSPECTION FOUND CORROSION ON GALLEY SUPPORT AT STA 1320 BETWEEN RBL 11 TO 33. THE SUPPORT AND FILLER WERE REMOVED, A NEW SUPPORT AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-07.SDR CALA9601809Support · corrodedINSPECTION FOUND CORROSION ON GALLEY SUPPORT AT BS 1300 BETWEEN LBL 11 TO RBL 11. THE SUPPORT AND FILLER WERE REMOVED, A NEW SUPPORT AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-07, 51-10-01 AND 51-10-02.SDR CALA9601821Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED NEAR SEAT TRACK AT STA 520, LBL 11.33. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-07, 51-10-01 AND 51-10-02.SDR CALA9601819Support · corrodedINSPECTION FOUND CORROSION ON FLOOR SUPPORT AT STA 540 TO 560 BETWEEN RBL 11.33 TO LBL 33.88. THE FLOOR SUPPORT WAS REMOVED AND A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 53-10-07 AND 51-30-02.SDR CALA9601811Floorbeam · corrodedINSPECTION FOUND CORROSION ON FLOORBEAM AT STA 480 TO 500, RBL 40. THE CORROSION WAS REMOVED, A REINFORCEMENT ANGLE AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-01, 53-10-07 AND 51-10-02.SDR CALA9601804Angle · corrodedINSPECTION FOUND FLOOR ANGLE CORRODED AT STA 1940, RBL 10. THE CORROSION WAS REMOVED AND A REINFORCEMENT REPAIR WAS INSTALLED IAW SRM 53-10-07, 51-10-01 AND 51-10-02.SDR CALA9601807Floor Support · corrodedINSPECTION FOUND CORROSION ON FLOOR SUPPORT AT STA 2350, LBL 40. THE FLOOR SUPPORT WAS REMOVED AND A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 53-10-07.SDR CALA9601806Splice · corrodedINSPECTION FOUND CORROSION ON STRINGER SPLICE, STRINGER 50 AND ON FILLER UNDER SPLICE AT STA 1980 IN AFT CARGO COMPARTMENT. THE SPLICE AND CORROSION WERE REMOVED, A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-01 AND 51-30-02.SDR CALA9601805Angle · corrodedINSPECTION FOUND FLOOR ANGLE CORRODED AT STA 1980, LBL 10. THE CORROSION WAS REMOVED, A REINFORCEMENT STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 53-10-07, 51-10-01 AND 51-10-02.SDR CALA9601825Angle · corrodedINSPECTION FOUND FLOOR ANGLE CORRODED AT STA 2350, BL 0 TO RBL 38. THE ANGLE WAS REMOVED AND A NEW FLOOR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-07, 51-10-01 AND 51-10-02.SDR CALA9601824Angle · corrodedINSPECTION FOUND FLOOR ANGLE CORRODED AT STA 900 BETWEEN LBL 11 AND RBL 11. THE FLOOR ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-07.SDR CALA9601808Angle · corrodedINSPECTION FOUND CORROSION ON FLOOR ANGLE AT STA 2280 NEAR DOOR R-5. THE ANGLE WAS REMOVED, A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 53-10-23 AND 51-10-02.SDR CALA9601822Angle · corrodedINSPECTION FOUND FLOOR ANGLE CORRODED BETWEEN STA 2280 AND 2340, LBL 40. A NEW FLOOR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-02.SDR CALA9601818Angle · corrodedINSPECTION FOUND CORROSION ON FLOOR SUPPORT ANGLE AT STA 835 BETWEEN LBL 11 AND RBL 11. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-07.SDR CALA9601898Angle · crackedINSPECTION FOUND A 1 INCH CRACK ON SUPPORT ANGLE ATTACHED TO FRAME AT BS 1540 BETWEEN STRINGER 37 TO 38L. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-02.SDR CALA9601823Angle · corrodedINSPECTION FOUND FLOOR ANGLE CORRODED AT STA 2350 BETWEEN BL 0 TO LBL 38. A NEW FLOOR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-02.SDR CALA9601820Angle · corrodedINSPECTION FOUND CORROSION ON FLOOR ANGLE AT STA 2280, RBL 11. THE FLOOR ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-07 AND 51-10-02.SDR CALA9601826Angle · corrodedINSPECTION FOUND ANGLE CORRODED AT STA 870 BETWEEN RBL 11 AND LBL 11. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-01.SDR CALA9601802Bulkhead · crackedINSPECTION FOUND A .4375 INCH CRACK AT RT CORNER OF BULKHEAD BS 400. A CRACK OF UNIDENTIFIED LENGTH WAS FOUND AT LT CORNER OF BULKHEAD BS 400. THE AREAS WERE REPAIRED IAW ECRA 5310-03369.SDR CALA9601803Spar · corrodedINSPECTION FOUND CORROSION ON REAR SPAR AFT FACE AT WS 405. THE AREA WAS REPAIRED IAW SRM 5720-01551.SDR CALA9601799Power Supply · inoperativeINSPECTION FOUND OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. THE EMERGENCY EXIT LIGHT POWER SUPPLY WAS REMOVED AND REPLACED.
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