Boeing 747-47UF
Service difficulty reports · 3,116
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 = '74747UF' 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 = '74747UF' 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 UIEA2026031800096Frame · crackedDURING HFEC OPEN HOLE INSPECTION AT NON STRETCHED UPPER DECK TENSION TIE AND FRAMES STA 760 LHS FOUND 01 EA HOLE CRACKED ON STEEL PLATE AS MARKED.(<P>NON STRETCHED UPPER DECK TENSION TIE AND FRAMES STA 760 LHS WORK ACCOMPLISHED IAW EN#3186-26 REV 0. NO FURTHESDR UIEA2026031800097Skin · dentedLOWER FUSELAGE SKIN STA 517 S36R FOUND DENT. LOWER FUSELAGE SKIN STA 517 S36R WORK ACCOMPLISHED IAW EN 3188-26 REV 0. NO FURTHER DEFECTS NOTED.SDR UIEA2026031800098Skin · dentedDENT AT LOWER HALF OF FUSELAGE EXTERNAL SKIN AT STA 463 S33L - S34L. DENT AT LOWER HALF OF FUSELAGE EXTERNAL SKIN AT BS 463 S33L - S34L WORK ACCOMPLISHED IAW EN #3167-26 REV 0. NO FURTHER DEFECTS NOTED.SDR UIEA2026031800099Skin · dentedDENT ON FUSELAGE EXTERNAL SKIN AT STA 2595 S25R - S26R.(<P>DENT AT OF FUSELAGE EXTERNAL SKIN AT STA 2595 S25R - S26R, WORK ACCOMPLISHED IAW EN #3185-26 REV 0. NO FURTHER DEFECTS NOTED. PN 65B02698-18.SDR UIEA2026031800100Spar Web · corrodedRIGHT WING GEAR W/W CENTER WING REAR SPAR WEB JETTISION PUMP CUTOUT FOUND CORROSION. RT WING GEAR W/W CENTER WING REAR SPAR WEB JETTISION PUMP CUTOUT WORK ACCOMPLISHED IAW EN #3157-26 REV 0. PN 111U1007-11. NO FURTHER DEFECTS NOTED.SDR UIEA2026031800101Spar Web · corrodedLH WING GEAR W/W CENTER WING REAR SPAR WEB JETTISON PUMP CUTOUT FOUND CORROSION.(<P>LH WING GEAR W/W CENTER WING REAR SPAR WEB JETTISON PUMP CUTOUT WORK ACCOMPLISHED IAW EN 3156-26 REV 0. NO FURTHER DEFECTS NOTED. PN 111U1007-11.</P>)SDR UIEA2026031800102Structure · corrodedDURING HFEC INSPECTION AT LOWER FUSELAGE AREA 2, FOUND CORROSION INDICATION AT STA 1718 - STA 1740 S45L. LOWER FUSELAGE AREA 2 STA 1718 - STA 1740 S45L WORK ACCOMPLISHED IAW EN #3190-26 REV 0. NO FURTHER DEFECTS NOTED.SDR UIEA2026031600091Support · crackedDURING INSPECTION OF RH T/E FOREFLAP #6, FOUND INBD & OTBD BOGIE SUPPORT PINS CRACKED. PLEASE REPLACE(<P>R/R BOGIE SUPPORT PINS IAW AMM 27-51-43 REV 116. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026031600092Support · crackedDURING INSPECTION OF RH T/E FOREFLAP #6, FOUND INBD AND OTBD BOGIE SUPPORT PINS CRACKED. PLEASE REPLACE(<P>R/R BOGIE SUPPORT PINS IAW AMM 27-51-43 REV 116. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026031600093Support · crackedDURING INSPECTION OF RH INBD T/E FOREFLAP #5, FOUND CRACKS IN THE HEAD OF BOGIE SUPPORT PIN. PLEASE REPLACE PIN(<P>R/R BOGIE SUPPORT PIN IAW AMM 27-51-43 REV 116. NO FURTHER DEFECTS NOTED.SDR UIEA2026022200065Adc · faultedALT DISAGREE EICAS MSG LEVEL FLIGHT AT FL280 GREATER THAN 200' L 27760 R/R CAPT LH AIR DATA COMPUTER IAW AMM 34-12-01/401 AND IPC 25-71-31-01A. OPS CHECK GOOD</P>)SDR UIEA2026021300050Engine · failed16 SECONDS AFTER T/O OUT OF XHM, SOMETHING WAS INGESTED INFLIGHT INTO ENG NR 1, CREW HEARD A LOUD BANG. ENG NR 1 PARAMETERS STARTED TO DECLINE. VIB STARTED AND THRUST DROPPED, ENG WAS SHUT DOWN, AND FLIGHT DECLARED PAN PAN AND DIVERTED TO PVG. ENGINE 1 REMOVSDR UIEA2026020700045Web · crackedAFT CARGO BAY, WEB BELOW FLOOR SUPPORT AT BS 1880, LBL A8 FOUND CRACKED. AFT CARGO COMPT WEB, WEB TRIMMED OUT AND REPAIR CARRIED OUT IAW SRM 51-70-13-2R-1, REPAIR 1, REV 105.SDR UIEA2026012800018Torque Box · crackedAFT CARGO BS 1680 RT TORQUE BOX PANEL FOUND CRACKED. AFT CARGO BS 1660-1680, RBL 30" TO RBL 45.5" TORQUE BOX UPPER SKIN WEB REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-2. NO FURTHER DEFECTS NOTED.SDR UIEA2026010800006Control Panel · smokeSMOKE (ELECTRICAL SMELL) POURED OUT OF CTR PEDESTAL JUST BETWEEN WXR PANEL AND FUEL CONTROL SWS. FOUND WXR PANEL TO BE EMITTING SMOKE. R & R WXR PANEL AS PER AMM 34-43-02 & AIPC 34-43-01. OPS CHK GOOD. NO SMOKE EMITTING FROM PANEL IN COCKPIT.SDR UIEA2026010300003Plug · leakingDIVERSION ENGINE 3 OIL QUANTITY LOSS. INSPECTED #3 ENG AND FOUND OIL LEAKING FROM #3 IDG. DEACTIVATION BLANKING PLATE, REMOVED BLANKING PLATE AND FOUND DRIVE SEAL PLUG MISSING & INSTALLED DRIVE SEAL PLUG PER MEL 24-11-01A. RAN ENG IAW AMM 71-00-00, LEAK CHECKSDR UIEA2025121901352Skin · crackedLEFT WING OTBD AFT FLAP BOTTOM SKIN AT INBD AREA FOUND CRACKED. LT WING O/B AFT FLAP BOTTOM SKIN AT I/B AREA PERFORMED TIME-LIMITED REPAIR IAW EA 1957A259 PART 1 REV.0. NO FURTHER DEFECTS NOTED.SDR UIEA2025122001355Angle · crackedFOUND 1 INCH LENGTH CRACK ON RH LONGERON BOX FRAME (PN: 65B15001-80) REPAIRED PER EA 4453A258 PART 1, REQUIRE TO PERFORM REPEAT INSPECTION PER EA 4453A258 PART 2. (14340)(<P>WHEN ACCOMPLISHED REPEAT INSPECTION PER EA 4453A258 PART 2, FOUND CRACK ON CLIP AND RSDR UIEA2025121201341Elec Connector · damagedNO NAI INDICATION FOR ENG 1 NAI VALVE IS ON DEFERRAL DMI 243009 AND LOCKED OPEN, & CONNECTOR IS REMOVED. RAN ENGINE IAW 71-00-00, VALVES OPS NORMAL. RESET PUSHED PIN ON PLUG 40289P PIN 15 & OPS CHK OK PER AMM 30-21-00 & 71-00-00.SDR UIEA2025112901330Elec Connector · faultedON DEPARTURE AT 1000' AGL, HYD QTY LOW 4 EICAS ADVISORY MESSAGE, RAN NNC 13.29, SECURED NR 4 HYDRAULIC SYSTEM OFF. T/S PER WDM 29-33-12-2 TO PERFORM WIRING CHKS BTWN HYQUIM D7848CA TO #4 HYD SYS TRANSMITTER DT404, CHKS GOOD & INSULATION RESISTANCE CHCKS NORMSDR UIEA2025112401322Coupler · faultedLEFT/RIGHT HF WILL NOT TRANSMIT. R & R RT & LT HF COUPLER PER AMM 23-11-03 & AIPC 23-11-03-05A. OPS CHK OK. LSDR UIEA2025112201321Start Valve · warning messageSTARTER CUTOUT MSG. R & R ENG NR 1 ENG START VALVE IAW AMM 80-11-01. OPS CHECKED GOOD, NO FAULTS NOTED. ENG 1 START VALVE STATUS MSG CLEARED.SDR UIEA2025102801283Icu · faultedCABIN ALT AUTO EICAS MSG. C/W QRH. RETURNED TO ANC(<P>FOUND MX MSG 21234, CHECK FAIL. R/R ICU PER AMM 21-31-10 & IPC 21-31-10-01 ITEM 236, TEST PASSED. R/R DIODES M3349 & 47008 PER SWPM 20-00-00, TEST PASSED. DMI 240995 CLOSED.SDR UIEA2025100901263Pump · faultedHYD 4 QTY LOW-ADVISORY, HYD PRESS ENG 4-STATUS, HYD RESVR PRESS 4-STATUS-DURING FLIGHT. WHEN ARRIVED BLEEDING HYDRAULIC FLUID VERIFIED FROM JFK STATION TECHS. SERVICED HYD SYS AS REQ'D DUE TO ENG 4 EDP R & R REF AMM 12-12-01 R114. FOUND ENG 4 EDP HOUSING CRACSDR UIEA2025101001265Pump · failedLOST #4 HYDRAULIC SYS ENROUTE TO JFK. EMERGENCY WAS DECLARED. REMOVED & REPLACED #4 ENGINE DRIVEN PUMP IAW AMM- 29-11-05. LEAK & OPS CHECK GOOD.SDR UIEA2025100201253Transceiver · failedWX RT SYS & RT WXR FAIL STATUS MSG DISPLAYED. ATB, R & R RT WXR R/T RACK IAW AMM 34-43-03. OPS CHECK GOOD. R & R RH WXR TRANSCEIVER IAW 34-43-02, SYSTEM TEST OKAY.SDR UIEA2025100401257Transceiver · failedWEATHER FAIL ND MESSAGE & WXR ATT(<P>R/R LH WXR TRANSCEIVER IAW AMM 34-43-02 AND WXR RADAR PEDESTAL IAW 34-43-00. SYSTEM TEST GOOD PER 34-43-00</P>)SDR UIEA2025092501245Pdu · burnedPDU NR 1 FOUND BURNED. REMOVED PDU NR 1, INSTALLED BLANKING PLATE, AND DEFERRED PDU NR 1. PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-56-200-801, NO FURTHER DEFECTS FOUND. TRANSFER TO DMI 238867 PER MEL 25-57-01 CAT D DUE DATE 23JAN26.SDR UIEA2025092401243Support Fitting · crackedR/H BODY LANDING GEAR WHEEL WELL AREA SUPPORT FITTING CRACK (STA 1372). PERFORMED TIME LIMITED REPAIR PER EA-4453A258 PART 1. NO FURTHER DEFECTS NOTED.SDR UIEA2025083001150Solenoid · faultedENG 4 FUEL VALVE EICAS, ENG 4 FUEL VALVE STATUS, #4 ENG WOULD NOT SHUT DOWN UPON FUEL CONTROL SWITCHING OFF POSN. L13 CB FOUND IN OUT POSITION.(<P>R/R SOLENOID FUEL SOV PER AMM 73-21-20 & IPC 73-21-14-01 ITEM 67. PFM #4 ENG IDLE RUN CHK, NO LEAK FND.</P>)SDR UIEA2025082701144Skin · damagedRIGHT LOWER AFT FUSELAGE SKIN DAMMAGE FWD OF AFT LOWER CARGO DOOR. REPAIR TO DAMAGE AT FS 1802, STR 35R C/W IAW EO 4453C592 PART 1 CATEGORY C IAW SRM 53-00-01. REPEAT VISUAL INSP DUE EVERY 250 F/C. TRANSFERRED TO NON-MEL 237259. LP 1915290 M14: PERMANENT REPASDR UIEA2025082601142Pump · faultedHYD OVHT SYS 4 EICAS MESSAGE. R & R TEMP TRANSMITTER IAW AMM 29-32-02. OPS/LK CHK OK. R & R EDP IAW AMM 29-11-05. OPS CHECKED OK PER AMM 29-11-05. IDLE RUN CHKS OK PER AMM 71-00-00-705-152-J00. REF IPC 29-11-05-048.SDR UIEA2025080701091Splice · damagedDEVIATION - PERFORM EO 4453B761 PART 1-2 SPLICE FITTING INSPECTION FOUND L/H UP FITTING ONE HOLE SIZE UNCORRECT AT STA 2598 S-11 AREA(<P>1. ACCOMPLISHED EI #T2025A53M-1475 REV 1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2025080701092Bulkhead · not reportedDEVIATION - PERFORM STA 2598 BULKHEAD MODIFICATION FOUND DEVIATION AT DOUBLER(<P>1. ACCOMPLISHED EI #T2025A53M-1411 REV 1 AND EI #T2025A53M-1440 REV 1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2025080701093Support Fitting · crackedCRACK - FITTING L/H WING #5 SPOILER ACTUATOR SUPPORT FITTING(<P>1. ACCOMPLISHED IAW WORK SHEET #50468 (SRM 57-51-13-2R-1 REV 104). 2. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2025080701094Seat Track · crackedCRACK - FOUND CRACK ON SEAT TRACKS AT RBL 11.33 STA 2095(<P>1. ACCOMPLISHED WORK SHEET #50496 AND DWG #65B38253, SH1 REV, AP, SHS1, REV A, SH52, REV A, SH53, REV, AND SRM 53-00-52-2R-12, REV 104. 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2025080701095Web · crackedCRACK- WEB OUTBD FACE OF L/H WING T/E INBD AILERON INBD WEB WBL 445(<P>1. ACCOMPLISHED IAW EI #T2025A57M-1399 REV 1. 2. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2025080701096Seat Track · corrodedCORROSION - FOUND CORROSION ON SEAT TRACK AT LBL 11.33 STA 1770, STA 1790 AND STA 1875(<P>1. ACCOMPLISHED WORK SHEET #50495 AND DWG #65B38253, SH-1, REV AL, 65B3853, SH-50, REV A, AND 65B3853, SH-49, REV AND SRM 53-00-52-2R-12 REV 104. 2. JOB COMPLETED AND COSDR UIEA2025080701097Fitting · crackedCRACK - FITTING L/H WING #6 SPOILER MID HINGE SUPPORT FITTING(<P>1. ACCOMPLISHED IAW WORK SHEET #50469 AND EI #T2025A57M-14262 REV 1 AND SRM 57-51-13-2R-1 REV 104. 2. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2025080701098Repair · not reportedEXISTING REPAIR - FOUND EXISTING REPAIR AT FWD CGO INNER SKIN, BETWEEN STA 580 - STA 596. ACCOMPLISHED EI #T2025A52M-1521 REV 1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2025080701099Seat Track · brokenBROKEN - SEAT TRACK M/D CGO COMPT BETWEEN STA 1520 AND STA 1540 RBL 11.33. ACCOMPLISHED EI #T2025A53M-1428 REV 1 AND DWG #65B38253, SH 1 REV AL, 14440802, SH 2, REV B.SDR UIEA2025080701100Support Fitting · crackedCRACK ON L/H PORTAL LATCH #4 SUPPORT FITTING OF NOSE CGO DOOR AT C3 FRAME, WL200(<P>1. REPAIR PORTAL LATCH #4 SUPPORT FITTING IAW WORK SHEET #50489 AND EI #T2025A53M-1524 REV 2 AND SRM 53-10-07-2R-3 REV 104. 2. INSTALL FASTENERS IAW SRM 51-40-02-0G-0 REV 104 ASDR UIEA2025080701101Bracket · corrodedFND AFT CGO FLOOR BRACKET CORROSION AT STA 1871 LBL 20(<P>1. REMOVED THE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 104. 2. INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 104 AND DWG #65B60128, SH 8, REV B. 3. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2025080701102Bracket · corrodedFND AFT CGO FLOOR BRACKET CORROSION AT STA 1880 LBL 20. REMOVED THE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 104. INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 104 AND DWG #65B60128 SH-8 REV B. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR UIEA2025080701103Lamp · inoperativeFOUND U/D SLIDE LIGHT INOPERATIVE IAW AMM 33-51-10-962-001 REV 113 REPLACED U/D SLIDE LIGHT LAMP 2EA. 2. IAW AMM 33-51-10-962-001 REV 114 PERFORMED EMERGENCY LIGHT (U/D SLEEVE) INSTALLATION TEST AND THE RESULT WAS SATISFACTORY</P>)SDR UIEA2025080701105Actuator · no testFOUND R/H BODY GEAR ACTUATOR ROTARY FUNCTIONAL TEST FAIL(<P>1. IAW AMM 32-35-01-004-001 REV 114 & AMM 32-35-01-404-007 REV 114 STEP A TO FCU RPL R/H BLG ALTERNATE ELEC ACTUATOR. 2. IAW AMM 32-35-00-715-059 REV 114 PERFORM R/H BODY GEAR ALTERNATE EXTENSION TESTSDR UIEA2025080501089Engine · faultedLOW SPEED REJECTED, #1 ENG 2.5-3.0 BELOW REQ T/O THRUST. EGT #1 EXCEED 952 SOLID RED BOX AROUND EGT. RED BOX FOR 5 SECONDS(<P>MX IN WORK WHILE IN AOGM FOR RTO ENG 1 EGT LIMIT. AOGM ETR: 10AUG25</P>)SDR UIEA2025073001071Software · faultedL NAV WON'T ENGAGE. RELOADED ALL ASSOCIATED SOFTWARE INTO BOTH LT & RT FMC IAW AMM 34-61-00. ALL GROUND TEST PASSED. VERIFIED ALL SOFTWARE CORRECT CONFIG.SDR UIEA2025071500954Smoke Detector · false activationEQUIPMENT SMOKE STATUS MESSAGE AFTER EQUIPMENT COOLING MESSAGE. REMOVED AND REPLACED EQUIPMENT COOLING SMOKE DETECTOR IAW AMM 26-16-51. PERFORMED GROUND TEST .</P> / <P>TEST PASSED MESSAGE CLEARED.SDR UIEA2025061400773Tire · failed#10 MLG TIRE FAILURE ON LANDING. R/R #9 & #10 MLG WHEEL ASSY PER AMM 32-45-01/401 & AIPC 32-45-03-02. FOUND DAMAGE ON RIGHT BODY GEAR DOOR (OUTBOARD). REPLACED DOOR PER AMM 32-14-02. RIGHT BODY GEAR STRUT DOOR DAMAGED. REPLACED PER AMM 32-14-06. DAMAGE AT R/H
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