Boeing 747-228F
Service difficulty reports · 199
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 = '747228F' 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 = '747228F' 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 UIEA200600112Spar · corrodedCORROSION DAMAGE FOUND IN SUBJECT SPAR AFT FLANGE AT WBL 770. INTERIM REPAIR TO OUTBOARD TRAILING EDGE MIDFLAP, NR 3 SPAR LOWER CHORD ACCOMPLISHED AS PER BOEING MESSAGE 1-177581561 AND FAA FORM 8100-9. DETAIL VISUAL INSPECTION THE EXPOSED AFFECTED AREA, FOR SDR UIEA200600109Skin · crackedCRACKED RT OUTBOARD ELEVATOR PANEL AT ELEV STA 244 AND 306, P/N 65B05730-2. REPAIR ACCOMPLISHED AS PER BOEING MESSAGE 1-174409992 AND FAA FORM 8100-9.SDR UIEA200600107Web · crackedCRACKED WEB AND LOWER CHORD AT THE RT HORIZONTAL STABILIZER STA BL 421.50. WEB AND LOWER CHORD REPAIR CARRIED OUT AS PER BOEING MESSAGE 1-17410726 AND FAA FORM 8100-9.SDR UIEA200600104Web · crackedLT HORIZONTAL STAB, UPPER CHORD AT STAB BL 421.5 FOUND 1/2" CRACK AT AFT END. CHORD REPAIR CARRIED OUT AS PER BOEING MESSAGE 1-176012397 AND FAA FORM 8100-9.SDR UIEA200600085Frame · crackedRT STA 360 FRAME WEB AT STR 14E CUT OUT FOUND CRACKED 7.5". CRACKS WERE FOUND ON FRAME WEB. REPAIR DOUBLERS WERE INSTALLED IAW BOEING MESSAGE NR 1-175762603, AND FAA FORM 8100-9.SDR UIEA200600084Web · crackedCRACKED WEB AND UPPER CHORD AT THE LT HORIZONTAL STABILIZER STA BL421.50. TRIMMED OUT WEB AND UPPER CHORD CRACKS. HFEC INSPECTED AREA, NO ADDITIONAL FINDINGS. FABRICATED REPAIR DOUBLERS, SUPPORT ANGLES AND STRAPS. WET INSTALLED ALL PARTS IAW BOEING MESSAGESDR UIEA200600086Frame · crackedRT STA 300 FRAME WEB AT STA 14D CUT OUT FOUND CRACKED 7.1". CRACKS WERE FOUND ON FRAME WEB. REPAIR DOUBLER AND WAS INSTALLED IAW BOEING MESSAGE 1-175762603.SDR UIEA200600017Fitting · shearedFOUND SHEARED HI-LOKS IN NR 4 PYLON AFT DIAGONAL BRACE FITTING.SDR UIEA200500070Pan · crackedLT SIDE CANTED BULKHEAD AT BS 1245, LBL 60 CLOSURE PAN FOR AILERON CONTROL CABLE FEED THROUGH TO PRESSURE DECK FOUND WITH (2) CRACKED LINES. CLOSURE PAN REPAIRED IAW MFG MM. (K)SDR UIEA200500069Skin · crackedNR 1 PYLON LT ACCESS DOOR 452BL CUT OUT LOWER EDGE CRACKED. REPAIRED ACCOMPLISHED IAW MFG MM. (K)SDR UIEA200500068Frame · crackedNOSE WHEEL WELL STRUCTURE ON INTERIOR OF FUSELAGE CHORD CRACKED AT BS 340, WL 200, LBL 10. REPAIRED IAW MFG MM. (K)SDR UIEA200500067Pressure Panel · corrodedBS 1408, LBL 78 WHEEL WELL PRESSURE DECK CORRODED AT FASTENERS LOCATIONS. PRESSURE DECK REPAIRED IAW MM. (K)SDR UIEA200500066Precooler · crackedPYLONS NR1, 2, 3, AND 4, PRECOOLER EXHAUST CUT OUT LOWER EDGE CRACKED. REPAIRS ACCOMPLISHED IAW MM. (K)SDR UIEA200500065Pylon · crackedLT WING NR 1 PYLON STRUT DOOR 453BL UPPER CORNER CRACKED. (K)SDR UIEA200500064Pylon · crackedNR 4 PYLON OB SKIN FOUND (2) CRACKS ON ACCESS DOOR 482AR CUTOUT CRACK 1INCH TO 1.5 INCH ON BOTH SKIN AND DOUBLER. (K)SDR UIEA200500063Bulkhead · crackedBS 400 BULKHEAD WEB CUT OUT FOR NOSE GEAR RETRACT ACTUATOR PAN FOUND BOTH LOWER CORNERS CRACKED. (K)SDR UIEA200500047Relay · failedAFTER TAKE OFF, LEADING EDGE FLAPS NR 1 AND NR 3 WOULD NOT RETRACT. PRIMARY LEADING EDGE C/B OPEN. REPLACED R1102 RELAY IAW WDM 27-81-01. INSPECTED PDU`S DAMAGE, NONE FOUND. CLEANED ALL CONNECTORS AND RESEATED C/B. OPS CHECK CARRIED OUT SEVERAL TIMES IAW SDR UIEA200500018Module · failedFLT 8452 - AFTER TAKEOFF WITH GEAR RETRACTED, ANTI-SKID HYD LIGHT AND RED PARK LIGHT ILLUMINATED. A/C DIVERTED TO FRA. CLEANED CANNON PLUG AT PARKING BRAKE VALVE. SYSTEM CHECKS NORMAL. ALL INDICATIONS NORMAL PER MM 32-41-00. AS PRECAUTION MCC ISSUED ITEM SDR UIEA200400205Fairing · missingON WALK AROUND CHECK, FOUND LT AFT TIP FAIRING OF HORIZONTAL STABILIZER MISSING. EO ISSUED TO ACCOMPLISH TIME-LIMITED REPAIR WORK TO BE DONE PRIOR TO FURTHER FLIGHT. FABRICATED A TIME LIMITED REPLACEMENT FAIRING FROM 0.040 INCH THICK 2024-T3 CLAD SHEET. PERSDR UIEA200400203Connector · looseNR 4 LEADING EDGE FLAP WOULD NOT RETRACT OR EXTEND NORMALLY OR ELECTRICALLY. JETTISONED 60.0 K FUEL. FOUND FORWARD CONNECTOR LOOSE ON L/E DRIVE UNIT. RESECURED CONNECTOR IAW MM. OPS CHECK OK, NORMAL. (K)SDR UIEA200400150Seal · wornMXP-BOM - WITH NR 1 PACK ONLY ON OPERATION AT FL280 AND 310, CABIN ALTITUDE WILL CONTINUE TO CLIMB AT 10 TO 20 FPM. IN CRUISE WITH BOTH OUTFLOW VALVES FULL CLOSED AND DIFF PRESSURE DECREASING FROM 8.4 PSI WITH NO DROP IN DUCT PRESS, DUCT PRESSURE 42 PSI. AFTSDR UIEA200400143Valve · malfunctionedMXP-ALA - AT 1741Z ON TAKEOFF ROLL AT APPROXIMATELY 120 KNOTS EXPERIENCED THE NR 4 ENGINE FIRE INDICATION. N1 SET AT 106.0. PERFORMED A REJECTED IAW THE FHB. ONCE STOPPED, THE ENGINE FIRE CHECKLIST WAS ACCOMPLISHED. JUST PRIOR TO ROLLING, NR 4 ENGINE FIRE SDR 2004F00370Skin · corrodedDURNG FA02 A-CHECK ACCOMPLISHGIN ATLAS AIR ROUTINE WORK CARD 12M15002 INSPECTION OF RIGHT WING FOUND BULGE AT LOWER FRONT SPAR CAP, CORROSION IS REPORTED AS LEVEL 1 AND IS LOCAL. (M) T64RSDR 2004F00369Brace · crackedDURING FA02 A-CHECK ACCOMPLISHING ATLAS AIR ROUTINE WORK CARD 11FM15002, INSPECTION OF LEFT WING FOUND NR 4 FLAP CANOE FAIRING TO TRACK FORWARD OUTBOARD FITTING CRACKED IN HALF. (M) T64RSDR 2004FA0000693Brace · crackedDURING A-CHECK ACCOMPLISHING ATLAS AIR ROUTINE WORK CARD 11FM15002 INSPECTION OF LEFT WING FOUND NR 4 FLAP CANOE FAIRING TO TRACK FORWARD OUTBOARD FITTING CRACKED IN HALF. JETIIIB WORK ORDER 1063 NON-ROUTINE NR 132.SDR UIEA200400122Valve · erraticNR 4 ENGINE SHUTDOWN DURING DECENT: NR 4 ENGINE SHUTDOWN RUMBLE AND EGT RISING. AFTER RISING RELIGHT IS STARTED SURGING. SHUTDOWN AGAIN. NR 4 HIGH STAGE VALVE DEACTIVATED, CLOSE AND PERFORMED ENGINE RUN UP, CHECK NORMAL, ENGINE RUN BY FLT CREW AND NR 4 ENGSDR 2004F00427Windshield · crackedCAPTAINS NR 1 WINDOW STARTED ARCING FIVE HOURS INTO FLIGHT THEN CRACKED SHORTLY AFTER. COMPLIED WITH EMERGENCY/ABNORMAL CHECKLIST IAW QRH. REMOVED AND REPLACED CAPTAINS NR 1 L1 WINDOW IAW AMM 56-11-01. (M)SDR 2004F00184Windshield · crackedCAPTAINS NR 1 WINDOW STARTED ARCING FIVE HOURS INTO FLIGHT THEN CRACKED SHORTLY AFTER. COMPLIED WITH EMERGENCY/ABNORMAL CHECKLIST IAW QUICK REF QRH. REMOVED AND REPLACED CAPTAINS NR 1 L-1 WINDOW IAW AMM 56-11-01. (M)SDR UIEA200400090Bleed Valve · malfunctionedDURING CLIMB-OUT, NR 2 ENGINE COMPRESSOR STALLED. NR 2 ENGINE SUSTAINED 6 OR MORE HARD COMPRESSOR STALLS WHILE CLIMBING THROUGH 18,000 FT TO 24,000 FT. INSPECTED INTAKE/EXHAUST AREAS, NIL DISCREPANCIES. CHIP DETECTORS CLEAN REMOVED AND REPLACED SAME 8TH STASDR UIEA200400089Engine · malfunctionedPRIOR TO TAKEOFF, DUE TO ANTI-ICE ON, STAT 'C' RUN AT 60 PERCENT. N1 WAS NORMAL. WITH BRAKE RELEASE, TAKEOFF THRUST SET, ROLLING DOWN RUNWAY 13, ASI BELOW 60 KNOTS, NR 3 ENGINE HAD 'BACKFIRED WITH A LOUD NOISE', WITH REDUCTION IN N1 RPM OF ABOUT 10-15 PERCENSDR UIEA200400068Valve · inoperativeAZ9051 PVG/HKG NR 3 ENG BLEED OVERHEAT LIGHT CAME ON DURING TAKEOFF. FOLLOWED CHECKLIST IAW 3.36.5, NR 3 THRUST LEVER BACK TO IDLE LIGHT WILL EXTINGUISH. BUT LIGHT WILL COME BACK ON IF PUSH THRUST LEVER FORWARD MORE THAN 70 PERCENT N1. NR 3 THRUST LEVER USEDSDR UIEA200400007Duct · misalignedAIR TURNBACK DUE TO NR 3 ENGINE FIRE WARNING. NOTICED EGT AT 850 DEGREES, ON TAKEOFF AT 100 DEGREE HIGHER THAN NR 2 AND NR 4 ENGINES. REMOVED AND REPLACED T/R DRIVE DUCT ASSEMBLY IAW MM, PERFORMED PNEUMATIC LEAK TEST IAW MM, NO LEAKS FOUND. DISCOVERED TURBISDR UIEA200400005Connector · damagedOKO/SUU - NR 3 ENGINE FILTER BYPASS LIGHT CAME ON DURING CLIMB. RETARDING THROTTLE DID NOT OUT IT OUT. ENGINE SHUTDOWN PER FHB AT 0633Z. LIGHT REMAINED ON. REMOVED AND REPLACED OIL FILTER AND INSPECTED, NO CONTAMINATION FOUND. INSTALLED NEW FILTER, LEAK ASDR UIEA200400004Clamp · brokenLEFT WING OVERHEATED TWICE ON CLIMB-OUT AND THEN IN CRUISE. COMPLETED CHECKLIST TO ISOLATE LEFT WING WITH ONLY NR 2 ENGINE PYLON VALVES OFF, AND ISOLATION VALVE OPEN. FOLLOWING CLIMB FL320 TO FL350 WITH NR 1 AND NR 2 ENGINES BLEED VALVES CLOSED AND LEFT AND SDR UIEA200300072Control Cable · icedNR 3 ENGINE THROTTLE UNABLE TO SELECT IDLE DURING DESCENT. THROTTLE STUCK AT 4 DEGREE THROTTLE ANGLE AND 80 PERCENT N1. ENGINE SHUTDOWN USING ENGINE FAILURE/SHUTDOWN CHECKLIST. PERFORMED INSPECTION IAW 73-21-01 AND 76-11-03 THRUST CONTROL CABLE INSPECTED ALLSDR UIEA200300025Fitting · crackedDURING C-CHECK, FOUND RT KICK FITTING BOLT HOLES POSITION A, B AND K STILL SHOWING CRACK INDICATION AFTER 2ND OVERSIZE REAMING. PERMANENT REPAIR WITH DEVIATION TO REF 'A' SB PER REF 'B', 'C', AND 'D' BY OVERSIZING HOLE 'A', 'B'B AND 'K' THROUGH ALL COMPONENTSSDR UIEA200300024Fitting · crackedDURING C-CHECK AT SIN, FOUND LT NOSE CARGO DOOR PORTAL FRAME CRACKED ON FUSELAGE AT BS 281, WL 312 AND LBL 40, REF SRM 53-10-04 FIG 97. THE NOSE CARGO DOOR PORTAL FRAME CRACK WAS REPAIRED BY MODIFYING SRM 747-53-10-04 FIGURE PER REF TO MATCH THE REPAIR GEOMETSDR UIEA200300026Floor Panel · delaminatedDURING C-CEHCK AT SIN, FOUND FLOOR PANEL DELAMINATED AT FS 2040 TO STATION 2140, RIGHT SIDE RBL 33.00-75.00. REPAIR BOND A 2024-T3 REPAIR DOUBLER TO THE UNDERSIDE OF THE FLOOR PANEL, PER REF'A'. REPAIR PER REF 'A' IS TIME LIMITED. DER APPROVAL OF REF 'A' ENSDR UIEA200300031Skin · damagedDURING C-CHECK SERVICE IN SIAEC, NR 2 PYLON EXTERNAL SKIN FOUND WRINKLED AT INBOARD SIDE AREA OF PYLON VALVE FROM STATION 286 TO STATION 300, BETWEEN THE MID SPAR AND NR 5 STIFFENER. NDT AND CONDUCTIVITY CHECKS WERE ACCOMPLISHED AS PER CARDS A00043 AND A00044SDR UIEA200300015Clamp · looseNR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED & FIRE BELL ACTIVATED DURING CLIMB THROUGH 3000 FT. NR 1 ENGINE NACELLE TEMP INDICATES 'F' FOR BOTH 'A' AND 'B' LOOPS. ENG FIRE CHECKLIST ACCOMPLISHED. 80,000 KGS OF FUEL DUMPED. AFTER PULLING FIRE HANDLE LIGHT WSDR UIEA0008Actuator · failedFLT 64 - AIRCRAFT DIVERTED TO ATL DUE ON CLIMB-OUT WITH AILERONS AND RUDDER TRIM SET TO ZERO, REQUIRED 3.5 UNITS OF LEFT AILERON TO MAINTAIN LEVEL FLIGHT AND 6 UNITS OF RUDDER TRIM TO NEUTRALIZE AILERONS. MAINTENANCE AT ATL FOUND TWO RIVETS SHEARED IN THE AILSDR UIEA0002Frame · severedDURING C-CHECK AT AMS DISCOVERED CIRCUMFERENTIAL FRAME SEVERED AT STATION 2240 BETWEEN STRINGER 38R AND 39R. ACCOMPLISHED PERMANENT REPAIR TO FRAME STATION 2240 PER SRM 53-10-04 FIG 66. (M)SDR UIEA0003Frame · corrodedDURNG C-CHECK AT AMS, FOUND STATION 400 BULKHEAD UPPER CHORD LBL 40 WL 200 CORRODED (MAIN DECK LEVEL). CORROSION REMOVED BY TRIMMING THE FLOOR ANGLE. REPAIRED BY SPLICING IN REINFORCEMENT STRAPS AND ANGLES IAW KLM REPAIR 747-2000-019 AND BOEING ENGINEERING. SDR UIEA9921Fire Warning · activatedFLT GT020 - FIRE WARNING BELL AND LIGHT SOUNDED ON FORWARD COCKPIT LIGHT FOR CARGO AREA, BUT WENT OUT TOO FAST TO CHECK F/E PANEL. CHECK CARGO AREA FIRE TEST AND INDICATION AND NO ABNORMALITIES NOTED. (M)SDR UIEA9916Frame · corrodedINSPECTION OF STA 1319 FRAME REVEALED CORROSION ABOVE THE LEFT HAND LONGERON BEAM. THE AREA WAS REPAIRED IAW ATLAS AIR EO 4753A085. (X)SDR UIEA9709Engine · failedCREW REPORTS: FLT NR LAU 322/28, BOG/MIA - DEPARTED BOG ON 9-28-97 AND EXPERIENCED AN ABORTED TAKEOFF DUE NR 4 ENGINE FAN BLADE SEPARATION (2 EACH). IN ADDITION, EXHAUST TAIL PLUG EXITED THE ENGINE AND WAS RECOVERED FROM THE RUNWAY. FAN EXIT GUIDE VANES EXHSDR 97ZZZX1369Frame · crackedAD 96-26-04. INSPECTION OF FRAME, RIGHT BS 320, STR 39R, CRACK FOUND. INTERIM REPAIR CARRIED OUT IAW SRM 53-10-04, FIGURE 85.SDR 97ZZZX1368Frame · crackedAD 96-26-04. INSPECTION OF LEFT FRAME BS 300 AND BS 320. BS 300, STR 39 - STR 40, LEFT, CRACKED. BS 320, STR 41 - STR 42, LEFT, CRACKED. REPAIRED IAW ATLAS E.O. 4753A031.SDR UIEA9603Vane Control · inoperativeENGINE REPAIRED BY LUFTHANSA, FIRST FLIGHT AFTER INSTALLATION. NR 1 ENGINE STALL WHILE CLIMBING THROUGH 10,000 FEET. FLT NR GTI900/31, LUXEMBOURG-TURIN-ENGINE SHUT-DOWN. ENGINE RE-START ATTEMPT UNSUCCESSFUL. AIRCRAFT RETURNED TO LUXEMBOURG BORESCOPE HPC/HR
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