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 UIEA200800147Skin · damagedRIGHT WING REAR SPAR UPPER SKIN AT WS 1490 FOUND EXISTING EXCESSIVE BLEND OUT AS MARKED. CHECKED THE BLENDOUT AREA AND FOUND AS PER ATLAS EO 4757A338 THE BLENDOUT IS PERMITTED.SDR UIEA200800146Skin · damagedRIGHT WING REAR SPAR UPPER SKIN AT WS 1390 FOUND EXISTING EXCESSIVE BLEND OUT AS MARKED. CHECKED THE BLENDOUT AREA AND FOUND AS PER ATLAS EO 4757A338 THE BLENDOUT IS PERMITTED.SDR UIEA200800026Skin · crackedMAIN ENTRY DOOR L-1, EXTERIOR LOWER HINGE CUT-OUT, PREVIOUS DOUBLER REPAIR, LOWER CORNER IS CRACKED AT STA 452.5 L. REMOVED CRACKED DOUBLER, FABRICATED NEW DOUBLER AS PER SB 747-52-2144 REV 2. VERIFIED STOP DRILLED ENDED CRACK USING HFEC INSP. AS PER 747 NDTSDR UIEA200800025Skin · corrodedLT WING O/B FLAP, AFT FLAP UPPER SKIN ON PANEL, AN AREA OF 5.0 INCH BY 2.0 INCH IS CORRODED AT WBL 625 LT. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 5, SHEETS 7 AND 9, PREPREG LAYUP 250 DEGREES F CURE PER SRM 51-40-12. REF: ATLAS AIR EO SDR UIEA200800024Panel · crackedLT WING UPPER FIXED T/E PANELS AT STA WBL 445, 11.0 INCHES FROM TRAILING EDGE AND WBL 515, 6.0 INCHES FROM TRAILING EDGE HAVE A 1.0 INCH CRACK. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 2 SHEETS 3 AND 5, PREPREG LAYUP 250 DEGREES F CURE PSDR UIEA200700498Steering Sys · inoperativeTAKEOFF REJECTED DUE TO T/O WARNING HORN BECAUSE RIGHT BODY GEAR UNLOCKED LIGHT ILLUMINATED ON T/O ROLL. SYSTEM SELECTED TO PRIMARY MODE. PERFORMED OPS CK OF BODY GEAR STEERING SYSTEM. FOUND RIGHT ALT BODY GEAR ACTUATOR SWITCH INOP. REMOVED AND REPLACED ASSDR UIEA200700476Floorbeam · damagedON REMOVAL OF MCD CEILING PANELS AROUND STA 600 FOUND UPPER FLOORBEAM LOWER CHORD AT BS 620 RBL 52 HAS SUSTAINED IMPACT DENT OF 5" LONG 1.5" WIDE 0.187" DEEP. STRUCTURAL DISCREPANCY RAM PART 1 COMPLETED. HFEC ACCOMPLISHED TO DAMAGED AREA PER NDT PARA 6 51-0SDR UIEA200700475Floorbeam · damagedAFTER REMOVAL OF MCD CEILING PANEL AT STA 620 FOUND UPPER FLOORBEAM LOWER CHORD AT BS 620 LBL 52 WL 300.8 HAS IMPACT DENT. 4.5" LONG 1.5" WIDE. HFEC ACCOMPLISHED TO DAMAGED AREA PER NDT PARA 6 51-00-00 FIG 23. NO CRACK INDICATION FOUND. LOWER CHORD REPAIRESDR UIEA200700461Unknown · smokeAT FL 380 (6.50 HOURS INTO FLIGHT) SMELLED ELECTRICAL SMOKE FROM UPPER DECK. COMPLETED ELECTRICAL SMOKE CHECKLIST LOCATED ODOR FROM GALLEY AREA. REMOVED POWER FROM GALLEY SMOKE ODOR WENT AWAY. INSPECTED GALLEY AREA FOR DEFECTS PERFORMED DETAILED WIRING INSSDR UIEA200700460Transmitter · malfunctionedDIVERSION, DUE TO LOSS OF CREW O2. REPLACED UPPER AND LOWER CREW O2 BOTTLES IAW AMM 12-15-08. REPLACED UPPER AND LOWER CREW O2 PRESS XMITTERS, LEAK CHECKED OKAY.SDR UIEA200700327Structure · debondedLT WING GEAR LOWER STRUT DOOR, AFT LOWER END, PREVIOUS REPAIR, EDGE IS SEPARATING. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 12 SHEET 1, 2 AND 3. ALSO, REFERENCE ATLAS AIR XEO NR 52-082907.SDR UIEA200700328Structure · dentedNR 2 ENGINE OUTBOARD REVERSER EXTERIOR SKIN HAS A 7.5 INCH BY 6.0 INCH DENT IN UPPER AREA OF TRANSLATING COWL. PERMANENT REPAIR ACCOMPLISHED AS PER GE CF6-50 ENGINE MANUAL 78-32-01, REPAIR 003. ALSO, REFERENCE ATLAS AIR XEO NR 78-082907.SDR UIEA200700321Seat Track · brokenAFT CARGO COMPARTMENT HAS SEAT TRACK CROWN BROKEN BETWEEN STA 1872 AND STA 1881 LBL 47. REPAIRED SEAT TRACK IAW SRM 53-10-05.SDR UIEA200700322Web · crackedAFT CARGO COMPARTMENT FLOOR WEB STA 1900 LBL 49 HAS SMALL CRACK. DAMAGED AREA OF WEB CUT OUT AND DOUBLER INSTALLED IAW SRM 53-10-04 FIG 71.SDR UIEA200700320Door · puncturedNR 1 PYLON OUTBOARD TRAILING EDGE DOOR INNER FACE PUNCTURED BY HOLD OPEN ROD WHEN DOORS ARE CLOSED 1.5 BY 1.5. PERM REPAIR CARRIED OUT IAW SRM 51-40-20 PAGE 1 250 DEGREES F.SDR UIEA200700291Unknown · unknownRTO: T/O + 15 MINUTES NR 2 ENGINE NACELLE TEMPS WENT TO 9.2 "A" LOOP AND 8.1 "B" LOOP FAULT LIGHT CAME ON. FAULT LIGHT ON FWD PANEL WAS ON. ACCOMPLISHED FWB PROCEDURES. TOOK 20 MINUTES FOR OVERHEAT TO COOL AFTER NR 2 THROTTLE TO IDLE.SDR UIEA200700292Structure · damagedAFTER LANDING LEFT WING UPPER SURFACE, INBOARD OF NR 2 ENG JUST AFT OF LEADING EDGE, PATCH MISSING. EXPOSED DAMAGE HONEYCOMB, MATERIAL EXPOSED WITH PORTIONS OF HONEY COMB MISSING AND BULGED UP FROM SURFACE AREA. INTERIM REPAIR WAS ACCOMPLISHED IAW XEO NR 57-0SDR UIEA200700244Skin · crackedFLAT SIDED SKIN AT BS 340 STRINGERS 6-8L FOUND 9 EACH HOLES CRACKED AT SKIN. FLAT SKIN CRACKED HOLES REPAIRED AS PER BOEING MESSAGE 1-343396688-2 AND FAA 8100-9SDR UIEA200700243Skin · crackedNR 3 PYLON ACCESS PANEL 473BL CUTOUT CRACKED AT FORWARD UPPER CORNER. NR 3 PYLON ACCESS PANEL 473BL CUTOUT SKIN REPAIR AS PER BOEING MESSAGE 1-351455345-3 AND FAA FORM 8100-9.SDR UIEA200700245Skin · crackedNR 3 PYLON OVAL PANEL 473AR CUTOUT CRACKED LOWER AFT SKIN. NR 3 PYLON OVAL PANEL 473AR CRACKED SKIN REPAIRED AS PER BOEING MESSAGE 1-351859671-9 AND FAA FORM 8100-9.SDR UIEA200700246Skin · crackedBS 2605 FOUND DENT AND CRACK BETWEEN STRINGER 46R AND 49R AREA JUST BETWEEN 2 PREVIOUS DOUBLERS. SKIN REPAIRED AS PER BOEING MESSAGE 1-343200877-4 AND FAA FORM 8100-9.SDR UIEA200700242Shear Tie · crackedBS 920R FRAME TO TENSION TIE CONNECTION FOUND HOLE NR 4 CRACKED. BS 920R FRAME TO TENSION TIE CONNECTION REPAIRED AS PER BOEING MESSAGE 1-340126164-4 AND 8100-9.SDR UIEA200700241Shear Tie · crackedBS 900R FRAME TO TENSION TIE CONNECTION FOUND CRACKED HOLE NR 9 AT FORWARD CHANNEL. BS 900R FRAME TO TENSION TIE CONNECTION REPAIRED AS PER BOEING MESSAGE 1-343193942-4 AND FAA FORM 8100-9.SDR UIEA200700240Shear Tie · crackedBS 880R FRAME TO TENSION TIE CONNECTION FOUND CRACKED HOLE NR 5 AT FRAME. BS 880R FRAME TO TENSION TIE CONNECTION CRACKED FRAME REPAIRED AS PER BOEING MESSAGE 1-339629649-2 AND FAA FORM 8100-9.SDR UIEA200700239Shear Tie · crackedBS 860R FRAME TO TENSION TIE CONNECTION FOUND HOLE NR 9 HOLE CRACKED AT FORWARD CHANNEL. BS 860 FRAME TO TENSION TIE CONNECTION CRACKED FORWARD CHANNEL REPAIRED AS PER BOEING MESSAGE 1-339630379-21-1 AND FAA 8100-9.SDR UIEA200700238Shear Tie · crackedBS 840R FRAME TO TENSION TIE CONNECTION FOUND NR 14 AND 19 HOLE CRACKED. BS 840 FRAME TO TENSION TIE CONNECTION REPAIRED AS PER BOEING MESSAGE 1-340418286-2 AND FAA FORM 8100-9.SDR UIEA200700237Altimeter · out of limitsA A/P PORPOISED 200-300' ABOVE AND BELOW SELECTED ALTITUDE AT FL 410 IN CRUISE. A/P OK. TRANSFERRED TO DMI M07-117IAW MEL 22-1-2B CAT C. A/C IS CAT II RESTRICTED.SDR P5CA0701523Filter · cloggedON TAKEOFF, NR 2 ENGINE FLAMED OUT. ENGINE HAD SUCCESSFUL RESTART. INLET AND EXHAUST FEELING AND COMPRESSOR CHECKED SATIS NR 2 FUEL TANK WAS SUMPED THEN REPLACED NR 2 ENGINE FUEL FILTER. NO FURTHER PROBLEMS.SDR UIEA200700206Hose · burstNR 1 ENGINE HAD VISIBLE SMOKE COMING FROM THE TAIL PIPE JUST PRIOR TO BLOCK IN. ALL INDICATIONS IN FLIGHT DECK WERE NORMAL. FOUND NR 1 ADP PRESS LINE BURST. REMOVED AND REPLACED THE LINE CLEANED RESIDUAL FLUID FROM THE COWLING AND SERVICED THE HYD FLUID. OSDR UIEA200700180Frame · crackedM/D BS 1740 S-13R-S14R FRAME FOUND CRACKED AND DEFORMED. M/D BS 1740 S13R-S14R DAMAGE FRAME REPAIRED FROM S11R TO S15R/16R AS PER BOEING MSG 1-309862807-8.SDR UIEA200700175Panel · crackedKEEL BEAM PANEL NR 191KK CRACKED AT RT FWD HINGE CUT-OUT AS MARK. CRACKED HINGE CUT-OUT SKIN REPAIRED AS PER SRM 51-40-02.SDR UIEA200700167Bear Strap · delaminatedM/DECK R3 DOOR AFT UPPER CORNER AREA BEAR STRAP DELAMINATED. DELAMINATED BEAR STRAP CORROSION REMOVED, OUT OF LIMIT, REPAIRED AS PER BOEING MSG 1-30886570-4.SDR UIEA200700168Bear Strap · crackedM/DECK LT MED NR 3 CUT-OUT AFT UPPER CORNER SMALL STEEL DOUBLER 1 HOLE CRACK AT BEAR STRAP APPROX 0.030" LONG (AFTER CORNER REMOVED). CRACKED HOLE REPAIRED AS PER BOEING MSG 1-309886570-4, WORK DETAILS REF N.R C51491.SDR UIEA200700169Spar · crackedEMP LT HORIZ STAB HINGE FTG AREA FOUND NR 25 HOLE CRACK AT REAR SPAR UPPER CHORD APPROX 3/16" RUNNING O/B LOWER DIRECTION. REPAIRED AS PER BOEING MSG 1-305519321-7.SDR UIEA200700166Bear Strap · delaminatedM/DECK L3 DOOR AFT UPPER CORNER AREA DELAMINATED BEAR STRAP. OUT OF LIMIT DELAMINATION BEAR STRAP REPAIRED AS PER BOEING MSG 1-309886570-4.SDR UIEA200700200Keelbeam · corrodedKEEL BEAM PNL NR 191KK EXTERNAL AND INTERIOR SURFACE CORROSION REVEALED. KEEL BEAM PANEL NR 191KK OUT OF LIMIT HINGE AREA REPAIRED AS PER SRM 51-40-03 FIG 1 AND SKIN REPAIRED AS PER SRM 51-40-02 FIG 1.SDR UIEA200700199Keelbeam · corrodedKEEL BEAM PNL NR 191HH EXTERNAL AND INTERIOR SURFACE CORROSION REVEALED. KEEL BEAM PANEL NR 191HH HINGE ATTACHMENT AREA OUT OF LIMIT, REPAIRED AS PER SRM 51-40-03 FIG 1.SDR UIEA200700181Frame · crackedLT S14 AREA FRAME CRACKED. CRACKED FRAME WEB REPAIRED AS PER SRM 51-40-03 FIG 1.SDR UIEA200700151Support Channel · crackedLT STAB 344QBL PANEL AFT SUPPORT AREA FOUND CRACKED. REPLACED SUPPORT CHANNEL PER BOEING MESSAGE 1-307217093-2.SDR UIEA200700149Channel · crackedRT STAB ACCESS PANEL 344 QBR OUTBOARD AFT CORNER PANEL SUPPORT FOUND CRACKED. REPLACED OUTBOARD AFT CORNER SUPPORT CHANNEL PER BOEING MESSAGE 1-307272180-2.SDR UIEA200700174Support · corrodedFAIRING SUPPORT FRAME AT STA 880 LWR SIDE LBL 2 AND RBL 2 FOUND CORRODED. OUT OF LIMIT LWR CHORD REPAIRED AS PER SRM 53-50-04.SDR UIEA200700173Support · corrodedFX - AIR COND BAY FAIRING SUPPORT FOUND CORRODED AT BS 1160, LBL58-LBL68. CORROSION OUT OF LIMIT, FAIRING SUPPORT CHORD REPLACED AS PER SRM 51-10-01 PP AND INSTALL AS PER SRM 81-30-02.SDR UIEA200700170Panel · crackedM/DECK BS 1241-1250 LBL 75-97 CLOSE-OUT PANEL NEAR TRIM AIR DUCT FOUND CRACK. TRIM AIR DUCT CLOSE-OUT PANEL. REPLACED AS PER SRM 53-23-29 PART IV.SDR UIEA200700172Stringer · corrodedFX - STRINGER FOUND CORROSION CRACKED AT STA2260-S-51L. CORROSION CRACKED STRINGER, REPAIRED AS PER SRM 53-10-02.SDR UIEA200700202Keelbeam · corrodedKEEL BEAM PNL NR 191JJ INTERIOR SURFACE CORROSION REVEALED AT SEVERAL LOCATIONS. KEEL BEAM PANEL NR 191JJ INTERIOR SUPPORT REPLACED AS PER SRM 51-10-01 PP AND INSTALLED AS PER SRM 51-30-02.SDR UIEA200700186Plate · damagedM/D BS 940 LT TENSION TIE STEEL PLATE FASTENER HOLE 1 FOUND SHORT EDGE MARGIN. M/D BS 940 LT TENSION TIE STEEL PLATE REPAIRED AS PER BOEING MSG 1-30-3983211-2-1 AND 4 FIG 3.SDR UIEA200700178Doubler · crackedRT BS 900 TENSION TIE AREA HOLE NR 5 FOUND CRACKED AT FRAME DOUBLER, INSULATION BLANKET HOLE FOUND CRACKED AT FRAME DOUBLER BETWEEN S-8R TO S-9R AND S-10R TO S-10AR. FRAME DOUBLER REPAIRED AS PER BOEING MSG 1-306586780-2.SDR UIEA200700176Plate · damagedM/DECK BS940 RT TENSION TIE STEEL PLATE FASTENER HOLE 2 FOUND SHORT EDGE MARGIN AT UPPER ROW MOST O/B. REPAIRED AS PER BOEING MSG 1-303983211-1-2, FIG 3.SDR UIEA200700160Support · corrodedFX - AIR COND BAY FAIRING SUPPORT FOUND CORRODED AT BS 1050 LBL 12, LBL 28 (191AL FRG ATTACH AREA). OUT OF LIMIT FAIRING SUPPORT LWR CHORD LWR FLANGE REPAIRED AS PER SRM 53-50-06 FIG 2.SDR UIEA200700155Seat Track · corrodedUPPER DECK STATION 685 RBL 27 SEAT TRACK CORRODED AS MARKED. REMOVED CORROSION PER SRM 53-10-05
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