Boeing 747-409F
Service difficulty reports · 92
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 = '747409F' 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 = '747409F' 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 UIEA2024080300784Floor Panel · damagedMN DK FLOOR PANEL LH SIDE AFT OF SIDE CARGO DOOR HAS MULTIPLE PUNCTURES AND CRACKS.(<P>REFERENCE COBALT WO'S C1016 AND C1018 FOR PROPER SIGN OFFS. FAA FOR 8130-3 105868 FOR REPAIR OF MAIN DECK PANEL LH SIDE AFT OF SIDE CARGO DOOR. NO FURTHER DEFECTS PER SRM 53SDR UIEA2024080300783Floor Panel · damagedMAIN DECK CAROG FLOOR PANEL 144U5825-54 AT STA 1200 HAS THREE FASTENER HOLES DAMAGED.(<P>REFERENCE COBALT WO C1022 FOR SIGN-OFFS. FAA FORM 8130-3 106133 FOR REPAIR OF MAIN DECK CARGO FLOOR PANEL HAS THREE FASTENER HOLES DAMAGED. NO FURTHER DEFECTS NOTED PER SRSDR UIEA2024080300782Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 144U5825-64 AT STA 1200 HAS ONE FASTENER HOLE DAMAGED.(<P>REFERENCE COBALT WO C1021 FOR PROPER SIGN OFF. FAA FOR 8130-3 #106126 FOR REPAIR OF MAIN DECK CARGO FLOOR PANEL HAS FASTENER HOLE DAMAGED. NO FURTHER DEFECTS NOTED PER SRM 53SDR UIEA2024080300781Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 144U5803-32 AT STA 1200 HAS ONE FASTENER HOLE DAMAGED.(<P>REFERENCE COBAL WO C1023 FOR PROPER SIGN OFF. FAA FORM 8130-3 106134 FOR REPAIR OF MAIN DECK CARGO FLOOR PANEL HAS ONE FASTENER HOLE DAMAGED. NO FURTHER DEFECTS NOTED PER SRMSDR UIEA2024072300731Circuit Card · faultedENG 4 FIRE LOOP A & B INOP. WORK DONE PER AMM 26-10-01 & 26-11-00. INSTALLED NEW CIRCUIT CARD FOR ENG 4 OVHT DET LP A POSITION A19, ENG 4 FIRE DET LP A POSITION A16, ENG 4 FIRE DET LP B POSITION A17 & ENG 4 OVHT DET LP B POSITION A20. PERFORMED GROUND TEST IASDR UIEA2024122301181Oil Filter · warning messageON TAKEOFF ROLL "ENG 4 OIL FILT" EICAS. LOW SPEED 40 KIAS ABORT.(<P>REPLACED ENG OIL FILTER PER AMM 79-28-08 T/S PER FIM 79-00 FIG 103 NO DEFECTS FOUND. AIRCRAFT OK FOR SERVICE.</P>)SDR SAJF2020031609013Turbine Blades · damagedCREW SATCOM INFO AROUND 10,000 FEET A/C FEEL VIBRATION AND CHECK ENGINE-3 LPT VIBRATION SHOW 5.0 AT N2 98% N1 66%. CREW MANUAL SHUT DOWN ENG-3 PER QRH PROCEDURE AND ATB. 1.AFTER LANDING, VISUAL CHECK THE ENGINE EXHAUST AREA FOUND METAL CHIPS AND LPT 5TH BLADESSDR SAJF2016112500023Smoke Detector · false activationMAIN DECK FIRE WARNING ALARM DURING FLIGHT, AFTER 5 HRS THE "FIRE M/D AFT" EICAS MESSAGE ILLUMINATED. DEPLOYED PAX OXYGEN MASKS BUT NOT USED. CHECKED M/D WITHOUT ANY FIRE OR SMOKE EVIDENT. FLT CONTINUED TO DESTINATION. AFTER ARRIVAL , TROUBLESHOOTING FOUNDSDR SAJF2015062404028Rvdt · malfunctionedAFTER TAKEOFF, FLAP DRIVE, ADVS MSG DISPLAY, FLT QRH PROCEDURE CARRY OUT. IAW FIM 27-51 TASK878 TROUBLE SHOT PROCEDURE CARRY OUT. IAW AMM 27-58-01 PFM LT OTBD FLAP RVDT REPLACEMENT. ME SUGGEST BOTH OTBD FLAP EXAMINE THE ADJUSTMENT OF BALL SCREW UP STOP IAW SDR SAJF2014060303019Pump · leakingHYD 2 QTY LOW HYD QTY DROP TO 0.34 & CONTINUED TO DROP TO 0 BUT PRESS 3080 TEMP 50, 1.5 HRS LATER HYD PRESS ENG 2 MSG CAME ON, TURN OFF EDP, 1 HR 20 MINS BEFORE LD HYD PRESS SYS 2 MSG ON HYD PRESS READ 0. GND CHK FOUND LT WW WING GEAR LCCA SOLENOID VLV & ENG SDR SAJF201309102027Cabin Pressure · malfunctioned(B-18716) DURING CRUISE, CABIN ALT RAPID RISE, FOLLOW QRH PERFORM EMERGENCY DECENT, DUMP FUEL AND RETURN TO TPE AT 0605L. ACFT AFTER REACHING CRUISE ALT(FL300) SEVERAL MINUTES "CABIN ALT" WARNING APPEARED WITH WARNING SOUND (WARNING WILL TRIGGER WHEN CBN ALTISDR SAJF2013102023Strut · damaged(B-18720) AFTER LANDING, LT BODY GEAR WAS FOUND TILTED UP DURING TAXIING AND CONTACTED THE GEAR DOOR ON THE FUSELAGE. OPENSDR SAJF201205200017Skin · damaged(B-18701) ARRIVAL CHECK FOUND: RT INBD T/E FORE FLAP MISSING, MID FLAP UPPER SKIN BROKEN. RT FUSELAGE VARIOUS PLACES DAMAGED, 3 EA OBVIOUS PUNCTURES WERE FOUND. RT NR 3 THS L/E FAIRING BROKEN. RT NR 7 SPOILER BROKEN.SDR SAJF20130502015Flap System · stuck(B-18717) FLAP LT OTBD T/E FLAP STUCK AT 8.82 UNIT, RT OTBD T/E FLAP AT 7.01 UNIT, MSG FLAP DRIVE & ASYM COME ATB. FOLLOWING TROUBLESHOOTING, RVDT HAS BEEN REPLACED.SDR SAJF2013021702006Fuse · malfunctioned(B-18708) AFT LANDING CREW REPORTED NLG STEERING LOST DUE TO HYD QTY LOW 1 (DROP TO ZERO). GROUND CK HYD FLUID LEAK FROM RT BODY GEAR POS ACTUATOR HYD FUSE HOUSING. REPLACED HYD FUSE & LEAK CK OK, PART FM STATION SPARE. HYD LINE BLEED & FUSE RESET OK, HYD-1 SDR SAJF20130201004Cable · broken(B-18715) ACFT PUSH BACK IN POSITION, FLAP DOWN, FOUND LT OTBD AILERON INOPERATIVE. THE ACFT WAS TOWED BACK TO HANGAR FOR MAINT. GROUND CK FOUND LT AILERON CONTROL CABLE AB13 BROKEN AND CABLE AA11 FRAYED. PFM INSPECTION OF AILERON CONTROL QUADRANT, CABLE DRSDR SAJF20120625021B-Nut · loose(B18712) HYD-1 QTY LOW 'LESS THAN 0.34' MESSAGE DURING CRUISE. INSPECTION FOUND EDP NR 1 DAMPER CONNECT HOSE B-NUT LOOSE. INSPECTED HYD NR 1 PRESSURE MODULE DELTA P INDICATED NORMAL. REPLACED EDP NR 1 & CSAE DRAIN FILTER. ENG RUN UP TEST NORMAL.SDR SAJF201206101020Circuit Card · malfunctioned(B-18725) DURING CLIMB " EQUIP COOLING " EICAS MESSAGE CAME ON, CREW PFM QRH PROCEDURE, NO HELP. ACFT AIR TURNED BACK. GROUND CHECK CMC SHOWS ALL EQUIP COOLING VALVES AND FANS FAILED. REPLACED EQUIPMENT COOLING CARD (A15) IAW AMM 21-58-05. PFM EQUIP COOLINGSDR SAJF201206141017Engine · failed(B-18721) DURING CLIMB, EICAS MESSAGE "ENG 4 OIL PRESS" WITH OIL PRESSURE INDICATING 4 PSI, FOLLOWED QRH, ENGINE 4 SET TO IDLE, SHORTLY NOISE AND VIBRATION, THEN N1,N2 DROP, EICAS MESSAGE "ENG 4 FAIL", FOLLOW QRH ENG SHUTDOWN. GROUND CHECK FOUND METAL CHIPS SDR SAJF201203051010Oil System · contaminated(B-18708) SHORT AFT REACHING TOC, OIL QTY DROPPED TO 1, OIL TEMP RISING VERY SLOW, OIL PRESS DROPPED SLOWLY. BOTH STABILIZED BEFORE REACHING LIMIT, THR LEVER WAS RESTARED, NO MESSAGE APPEARED. GROUND CHECK FOUND OIL LUB & SCAV PUMP TGB & AGB INLET SCREEN WERSDR SAJF2012022601007Fire Warning · false activation(B18710) AIR TURN BACK, DUE TO MAIN DECK FIRE WARNING. NO FIRE EVIDENCE WAS FOUND AFTER ACFT TURNED BACK. CHECKED ELECTRONIC COMPARTMENT FOR ANY LEAKS AND THE CONDITION OF THE SEALANT OF THE FLOOR PANELS. THE RESULT IS NORMAL. WATER RESIDUAL AND PAPER TOWSDR SAJF201202041011Screw · dislodged(B18717) EXPERIENCED TWO CAN’T SHUTDOWN ENGINE EVENTS ON NR 3 ENGINE; FIRST ON JAN 27,2012 & SECOND ON FEB 4,2012). DURING TROUBLESHOOTING, GROUND CONFIRMED THAT THE HMU FUEL SHUTOFF VALVE STUCK IN OPEN POSITION & NR 2 HMUS WERE REPLACED. SHOP REPORT REVEALSDR SAJF2011122510048Structure · damaged(B-18708) EICAS MESSAGE, INBD T/E FLAP ASSY DURING APPROACH. AFTER LANDING GROUND CHECK FOUND LT INBD AILERON DAMAGED OVER LIMITS.SDR SAJF2011122000047Attach Fitting · fractured(B-18706) DURING EXTEND FLAP INSPECTION ON GROUND, FOUND LT WING T/E INBD FORE FLAP OTBD ATTACH FITTING FRACTURED, RESULTING IN PARTIAL INBD FORE FLAP, MID FLAP AND WING WEB ASSY DAMAGE.SDR SAJF2011111900045Tire · failed(B-18709) GROUND CHECK FOUND MAIN WHEEL NR 1 FWD BLOWN TIRE AFTER LANDING IAW AMM 32-45-01 R & R NR1, NR2 M/W ASSY FUNCTION CK NORMAL. TIRE PRE SERVICED TO NORMAL RANGE.SDR SAJF2011110900044Tire · ruptured(B-18707), DURING ACFT TAXIING OUT, STAFF FROM OTHER ORGANIZATION REPORTED THAT "ABNORMAL BANG SOUND WAS HEARD". DOWN LOAD CMC NO ACTIVE FAULTS FOR EXISTING FAULT & PRESENT LEG FAULT. CREW INFORMED ACFT NORMAL BY SATCOM. AFTER ACFT ARRIVED, GROUND CHECK FOUSDR SAJF201107010023Blades · failed(B-18711) AIRCRAFT ENROUTE, AFTER T/O AT FL015, NR 4 ENG HAD "BANG" SOUND AND SPOOL DOWN AND EGT OVER LIMIT. CREW FOLLOWED QRH TO SHUTDOWN ENGINE, DUMP FUEL AND AIR TURNED BACK. GROUND CHECK FOUND MANY METAL CHIPS IN TAILPIPE AND N1 ROTOR SEIZED. PRELIMINARYSDR SAJF20110609021Engine · failed(B-18712) ACFT ENROUTE, DURING CLIMB AT 1000 FT FLT CREW HEARD A NOISE, AT 5000 FT RETARDED NR 3 THRUST LEVER THEN NOISE GONE. CLIMB 7000 TO 9000 FT T/L ADVANCED BANG SOUND COME OUT AGAIN, THOUGH ALL ENGINE PARAMETERS ARE WITHIN LIMIT. FLT CREW CONFIRMED THE SDR SAJF201105150016Actuator · malfunctioned(B-18710), DURING TAKEOFF ROLL "BODY GEAR CTR" MSG DISPLAYED AT 50-60 KT, ACFT ABORTED TAKEOFF. CHECK CMC FOUND FAULT CODE 32057A RT B/G STEERING LT ACTUATOR UNCOMMAND EXTENSION. INVESTIGATION FOUND BLG STEERING ACTUATOR FAILURE DUE TO MOISTURE INGRESS INTO SSDR SAJF2011050400013Fitting · corroded(B-18706) CRACK FOUND AT LONGERON EXTENSION FITTING DURING PERFORMING 747-53A2515 SB INSPECTION, LOCATION OF THE CRACK IS AT LOWER GUSSET OUTWARD FLANGE OF SUBJECT FITTING. REPLACED FITTING.SDR SAJFCALS099035Drive Shaft · sheared(B18718) CREW INFO THROUGH ACARS "HYD-2 QTY LOW" MSG APPEARD, QTY CONTINUED DROPPING TO ZERO & "HYD PRESS ENG-2" MSG APPEARED, THEN QRH PROCEDURE COMPLETED. INITIAL INVESTIGATION FOUND NR 2 ENG EDP DRIVE SHAFT WAS SHEARED. RPLD NR2 ENG EDP. RPLD THE 2 FILTERSSDR SAJFCALS099025Valve · malfunctioned(B-18707) FUEL SPILL FROM RT WING SURGE TANK VENT PORT DURING REFUELING. FUEL TRANSFERRED & RT SURGE TANK DRAINED. AFTER THE ACFT RETURNED PERFORMED RT WING TANK VTO FUNCTIONAL TEST AND FND: - FUEL SPILLED INTO RT SURGE TANK BEFORE FILLED NR 4 MAIN TANK TO VTSDR SAJFCALS099024Controller · faulty(B-18706) AFTER TAKE OFF, FLIGHT CREW REPORTED THAT IT WAS UNABLE TO CONTROL F/D TEMPERATURE, RESULTING IN HIGH F/D TEMPERATURE.(43 CENTIGRADE) EICAS ECS-REAL PAGE SHOWED THAT PTC-A IN CONTROL & ALL 3 PACKS OUTLET TEMPERATURE ABOUT 57 CENTIGRADE. THERE WAS NOTSDR SAJFCALS099013Discharge Tube · fracturedFUEL LEAKAGE FROM LT WING SURGE TANK NACA. PURGED FUEL TANK. FOUND DISCHARGE TUBE FRACTURE AT MAIN TANK 2 FWD OVERRIDE JETTISON PUMP. REPLACED DISCHARGE TUBE & OPS TEST NORMAL. TASK CARDS 28-011-04-01/-02/-03/-04 CALL FOR DETAILED INSP OF IN-TANK TUBING &SDR SAJFCALS099009Skin · damagedSERVICE BACK, LARGE AMOUNT OF TAIL STRIKE WAS FOUND ON EXTERNAL SKIN FROM STA 2060 TO STA 2760 BETWEEN STR 49R AND 49L. THE DAMAGE TYPES CAN BE OBSERVED AS SKIN WEAR OUT, SKIN CRACK, RIVET WEAR OUT, AND POSSIBLE FRAME DEFORMED. SUBJECT ACFT SUFFERED TAIL STRISDR SAJFCALS099005Strut · misrepairedAIR TURNED BACK DUE TO NLG CAN NOT BE RETRACTED. MX RECORD SHOWN THAT TASK OF NLG SHOCK STRUT FULL SERVICE HAD BEEN PERFORMED ON JAN/23/2010 FOR CORRECTING TLB ENTRY. A FULLY LEAK TEST WAS ACCOMPLISHED WHEN ACFT BACK TO DEPARTURE. THERE WAS NO LEAKAGE FOUNDSDR SAJFCALS098032Bearing · migratedACFT WAS FOUND, BEARING MIGRATION AT RT HINGE OF NOSE CARGO DOOR DURING D01 CHECK 2. DUE TO SHORT OF TOOL TO REPAIR, PERIODIC CHECK ON BUSHING FLANGE IS REQUIRED IAW CHI-CHI-09-0301-04B UNTIL DEFECT IS CORRECTED. FIRST PERIODIC CHECK FOUND FUTHER DAMAGE ON RSDR SAJFCALS098029Actuator · inoperativePERFORMING 7A CHECK, FOUND RT MLG ALT EXTENSION, ELECTRIC ACTUATOR FUNCTION OUT (NO ROTATION)SDR 2009F00075Bearing · migratedCHINA AIRLINES AIRCRAFT B-18716 WAS FOUND BEARING MIGRATION AT RT HINGE OF NOSE CARGO DOOR DURING D01 CHECK. DUE TO SHORT OF TOOL TO REPAIR, A PERIODIC CHECK ON BUSHING FLANGE IS REQUIRED PER CHI-CHI-09-0301-04B UNTIL DEFECT IS CORRECTED. FIRST PERIODIC CHECSDR SAJFCALS098028Actuator · inoperativePERFORMING 8A CHECK, FOUND RT MLG ELECTRIC ACTUATOR, NOT FUNCTIONING.SDR 2009F00028Circuit Card · shortedIN FLT, CREW REPORTED "FIRE CARGO AFT" WARNING CAME OUT AND FIRE BOTTLES HAD BEEN DISCHARGED, AIR TURN BACK. GROUND INSP FOUND QUITE AMOUNT OF WATER CARRIED INTO THE ACFT BY THE CARGO ABOVE THE E/E BAY ON THE MAIN DECK SPILLED INTO THE E/E COMPARTMENT. THE LINSDR SAJFCALS098005Transmitter · malfunctionedDURING CLIMB, EICAS MSG "TE FALPS", "FLAPS DRIVE" IN VIEW. CREW SATCOM INFORM MOC AND PERFORM QRH THEN ACFT TURN BACK. CMC DOWNLINK FOUND OB TE FLAPS IND SHOW ASYMMETRY. REPLACED RT OTBD T/E FLAPS POS X’MIT AND OPERATION CHECK NML. PARTS SHIPPED FROM CI SP
Back to Boeing 747-409F