Boeing 747-87UF
Service difficulty reports · 1,102
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 = '74787UF' 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 = '74787UF' 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 UIEA2025052500686Stringer · crackedM/D - STA 760-780 S-9L STRINGER FOUND CRACK.(<P>M/D - STA 760-780 S-9L STRINGER CRACK REPAIRED IAW RI-53-21-17628 REV A. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2025052500687Stringer · crackedM/D - STA 780-800 S-9L STRINGER FOUND CRACK.(<P>M/D - STA 780-800 S-9L STRINGER CRACK REPAIRED IAW RI-53-21-17628 REV A. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2025052500688Stringer · crackedM/D - STA 840-860 S-9L STRINGER FOUND CRACK.(<P>M/D - STA 840-860 S-9L STRINGER CRACK REPAIRED IAW RI-53-21-17628 REV A. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2025052500689Stringer · crackedM/D - STA 860-880 S-10L STRINGER FOUND CRACK.(<P>M/D - STA 860-880 S-10L STRINGER CRACK REPAIRED IAW RI-53-21-17609 REV A. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2025052600690Stringer · crackedAFT OF STA 2360 S14R FOUND CRACKED.(<P>AFT OF STA 2360 S14R CRACK REPAIRED IAW RI-53-81-17624 REV A. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2025052600691Stringer · crackedAFT OF STA 2360 S2R FOUND CRACKED.(<P>AFT OF STA 2360 S2R CRACK REPAIRED IAW RI-53-81-17574 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025052600692Stringer · cracked2 EA CRACKS WERE FOUND ON STRINGER O/B SIDE APPROX 1/8" AND 11/16" AS MARKED AFT OF BS 2360 STR 2L.(<P>2 EA CRACKS FOUND ON STRINGER O/B SIDE APPROX 1/8" AND 11/16" AS MARKED AFT OF BS 2360 STR 2L WERE REPAIRED IAW RI-53-81-17607 REV A. NO FURTHER DEFECTS NOTESDR UIEA2025052600693Stringer · crackedAFT OF STA 2360 S6L FOUND CRACKED.(<P>AFT OF STA 2360 S6L CRACK REPAIRED IAW RI-53-81-17595 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025052600694Stringer · crackedM/D - STA 1940-1960 S-9R STRINGER FOUND CRACK.(<P>M/D - STA 1940-1960 S-9R STRINGER CRACK REPAIRED IAW B747-8F SRM 53-60-03 REPAIR 4 ALTERNATIVE 2 REV 145. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025052700696Stringer · crackedM/D - STA 980+160 - 1000 S-12R STRINGER FOUND CRACK.(<P>M/D - STA 980+160 - 1000 S-12R STRINGER CRACK REPAIRED IAW RI-53-20-17599 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025052700697Stringer · crackedM/D - STA 1660-1680 S-9R STRINGER FOUND CRACK.(<P>M/D - STA 1660-1680 S-9R STRINGER CRACK REPAIRED IAW RI-53-60-17615 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025052700698Stringer · crackedAFT OF STA 2598, S3L FOUND CRACKED.(<P>AFT OF STA 2598, S3L CRACK REPAIRED IAW RI-53-81-17593 REV A. NO FUTHER DEFECTS NOTED.</P>)SDR UIEA2025051900639Warning Message · activatedCABIN ALTITUDE WARNING MSG AT 39,100". C/W IAI AND CHECKLIST(<P>CMC REVIEWED, NIL RELATED FAULT MSG. REF IFIM 31-98-00-810-801 CORRECTIVE ACTION C/W CPCS CENTER A & B CMC TEST OK. REF AMM 21-31-03</P>)SDR P5CA2025041600013Shear Tie · damagedFUSELAGE SECTION 46 - FUSELAGE SKIN (P/N: 146U3867-5) - PUNCTURE BETWEEN STA 2000 AND S38L TO S39L - CATEGORY B REPAIR.(<P>SHEAR TIE REPLACED AS PER SRM 51-10-02. NEW SHEAR TIE HOLES TRANSFERRED AS PER SRM 51-40-05. NEW SHEAR TIE INSTALLED AS PER SRM 51-40-02.SDR P5CA2025041900014Web · crackedEMP - RH HORIZONTAL STAB TIP FAIRING I/B CLOSURE WEB, FOUND CRACK.(<P>CRACK - WEB REPLACED AS PER SRM 51-10-01. NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05. NEW WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042100015Skin · damaged#18 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2025042100016Skin · damaged#19 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042100017Skin · damaged#20 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042100018Skin · damaged#7 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042100019Skin · damaged#8 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2025042100020Skin · damaged#9 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2025042200021Beam · crackedLHW NO.11 K-FLAP AT WS 569 D-BEAM LWR ATT BOLT AREA, FOUND CRACK.(<P>CRACK AREA REPAIRED AS PER RI NO: RI-57-41-17558 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042200022Channel · crackedLH HORIZONTAL STAB TIP T/E FAIRING FWD U CHANNEL CRACK.(<P>U CHANNEL REPLACED AS PER RI NO: RI-55-10-17562 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042300023Seat Track · damagedM/D STA 1510, 1530, 1550 LBL 11 SEAT TRACK SLOT HOLE ELONGATED.(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-9 REPAIR 9 FIG 201 AND RI NO: RI-53-65-17570 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042300024Web · crackedEMP - RH HORIZONTAL STAB TIP FAIRING CLOSURE WEB LWR CHORD CRACK.(<P>LWR CHORD REPAIRED AS PER SRM 55-10-09-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042300025Rib · crackedEMP - RH HORIZONTAL STAB TIP FAIRING INTERNAL AREA MOST AFT RIB, FOUND CRACK.(<P>RIB REPLACED AS PER SRM 51-10-02. NEW RIB HOLES TRANSFERRED AS PER SRM 51-40-05. NEW RIB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2025042300026Beam · crackedRHW I/B L/E D-BEAM AT I/B PDU AREA O/B FOUND CRACK ILES 520.(<P>CRACK AREA REPAIRED AS PER RI-57-41-17559 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042300027Support Beam · damagedRHW ILE 450 I/B SUPPORT BEAM UPPER FTG FOUND HOLE ELONGATED.(<P>SUPPORT BEAM REPAIRED AS PER SRM 57-41-09-2R-2 REPAIR 2 FIG 203 DETAIL IV AND RI-57-41-17586 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042300028Skin · damaged#21 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025040200010Valve · malfunctionedAIR TURNBACK DUE TO LOSS OF CABIN PRESSURE.(<P>R+R SMOKE OVERIDE VALVE PER AMM 21-58-06, OPS CHECK GOOD.</P>)SDR UIEA2025031300281Pdu · faultedFLAPS DRIVE CAUTION MSG.(<P>REMOVE & REPLACE #4 PDU FEEDBACK SWITCH ASSY PER AMM 27-88-01. REMOVED AND REPLACED #4L PDU PER AMM 27-81-03 APC 27-81-03-51. OPS CHECK GOOD. NO MESSAGES OR FAULTS NOTED.</P>)SDR UIEA2025022000153Warning Message · false activationBLOCK TURN BACK. LOW SPEED REJECT T/O DUE TO T/O WARNING STAB TRIM. MCC NOTIFIED, NO EICAS MESSAGE, NO CURRENT FAULT, NO EXISTING FAULT, HORIZONTAL STABILIZER TRIM CONTROL SYSTEM AND ADJUSTMENT TEST IAW AMM 27-41-00/501.SDR UIEA2025021900152Structure · damagedTE RUDDER DAMAGE.(<P>REPAIRED IAW SRM 51-70-05 AND EA 1955A028. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025011800085Outflow Valve · failedDURING CLIMB ON, THE CABIN WOULD NOT PRESSURIZE, STOPPED CLIMB AT 10,000, CAB ALT WAS 10300. DELTA P WAS 0.1 COULD NOT CONTROL THE CABIN PRESSURE IN MANUAL OR AUTO.(<P>REMOVED AND REPLACED R/H OUTFLOW VALVE IAW B747 AMM 21-31-01 UP TO SUBTASK 21-31-01-430-016.SDR P5CA2025010200001Panel · puncturedFUSELAGE - SEC 46 LOWER AFT CARGO COMPARTMENT FLOOR PANEL PUNCTURE - DAMAGED NEAR STA 1540 TO 1560.(<P>FUSELAGE - SEC 46 STA 1540-1560 RBL 45" TO RBL 55" LOWER AFT CARGO COMPARTMENT FLOOR PANEL PUNCTURE - DAMAGED AREA REPAIRED IAW RI-53-12-17630 REV.A </P>)SDR P5CA2024121600050Pcb · faultedMASTER WARNING LIGHTS (RED) AND BELL WERE ACTIVATING EVERY 90 SECONDS WITH NO EICAS OR OTHER RED LIGHTS ILLUMINATING.(<P>REMOVED AND REPLACED MASTER MONITOR A & MAWEA PCC IAW B747 AMM 31-51-02. OPS CHECK GOOD. PART EFFECTIVITY VERIFIED PER IPC 31-51-02-01.</P>SDR UIEA2024120601168Line · loose#1 ADP FAILED, LOSS OF HYDRAULIC FLUID. #1 EDP ON DEFERRAL PRIOR TO FLIGHT.(<P>R/R EDP PER AMM 29-11-05 & IPC 29-11-05-05, RETURN LINE FOUND LOOSE, LEADING TO FLUID LOSS. SCAVENGE FILTER CHECKED FOR DEBRIS, NONE FOUND. R/R RETURN MOD FILTER PER MCC REQUEST. FISDR P5CA2024111900049Engine · unknownDURING TAKEOFF WHILE POWER PUSHED UP TO STABILIZATION, THRUST ON ENG #3 AND #4 LAGGED AT 25-30% WHILE ENGINES #1 AND #2 CAME UP NORMALLY TO APPROXIMATELY 45% N1(<P>FOUND NO FAULT MAINTENANCE MESSAGE ON PLF OR EF. PERFORMED POWER ASSURANCE TEST AND FOUND THE RESDR P5CA2024110800048Pcb · failedREJECTED TAKE OFF @ 110 KNOTS MASTER WARING ON EICAS.(<P>REMOVED & REPLACED MAWEA PRINTED CIRCUIT CARD (MASTER MONITORS) AMM 31-51-02/401, HIGH ENERGEY STOP INSPECTION C/W IAW AMM 05-51-10-202-001</P>)SDR P5CA2024092900046Stringer · crackedAPU COMPT STA 2598 RH STRG 42R AFT BULKHEAD FOUND CRACK(<P>APU COMPT STA 2598 AFT BULKHEAD RH STGR 42R STRINGER REPLACEMENT IAW EO 4853A157 PART 2 STEP 2 AE AND SRM 51-10-02 AND 51-40-02 REV 43 20 JUN 2024. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2024092800045Support Rod · crackedRHW L/E CAVITY #7 'A' SUPPORT ROD UPPER L/E RIB TAB CRACKED(<P>RHW L/E CAVITY #7 'A' SUPPORT ROD UPPER L/E RIB TAB REPAIRED IAW SRM 57-41-09-2R-2 REPAIR 2 AND RI-57-41-17102 REV A. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2024092800044Support · crackedRHW L/E CAVITY #4 "A" UPR SUPPORT ROD ATT TAB (COUNT FROM I/B) FOUND CRACKED(<P>RHW L/E CAVITY #4 "A" UPR SUPPORT ROD ATT TAB (COUNT FROM I/B) REPAIRED IAW SRM 57-41-09-2R-2 REPAIR 2 AND RI-57-41-17103 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2024092800043Door · chafedAPU - LH COMPT DOOR FWD EDGE CHAFING WORN(<P> APU - LH COMPT DOOR FWD EDGE REPAIRED IAW SRM 52-40-01-2R-6 REV 43 DATE 20 JUN 2024. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2024092800042Stringer · crackedSTA 2360 STR 2R AFT OF PRESSURE BULKHEAD STRINGER FOUND CRACK(<P>STA 2360 STR 2R AFT OF PRESSURE BULKHEAD STRINGER REPAIRED IAW RI-53-80-17141 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2024092800041Skin · delaminated#22 V/C FLAP BULLNOSE FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-04 REPAIR 5. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2024092700040Channel · crackedLH HORI. STAB. T/E TIP FAIRING U CHANNEL FOUND CRACK(<P>REPLACED U CHANNEL IAW RI 55-10-17081 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2024092700039Stringer · crackedSTA 2360 STR 6R FWD OF PRESSURE BULKHEAD STRINGER FOUND CRACK(<P>STA 2360 STR 6R FWD OF PRESSURE BULKHEAD STRINGER REPAIRED IAW RI-53-60-17133 REV.A. NO FURTHER DEFECTS</P>)SDR P5CA2024092700038Stringer · crackedBS 2360 FWD OF THE PRESSURE BULKHEAD STR 6L FOUND CRACK(<P>BS 2360 FWD OF THE PRESSURE BULKHEAD STR 6L STRINGER REPAIRED IAW RI-53-60-17132 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2024092700037Stringer · crackedBS 2360 FWD OF THE PRESSURE BULKHEAD STR 9R FOUND CRACK(<P>BS 2360 FWD OF THE PRESSURE BULKHEAD STR 9R REPAIRED IAW RI-53-60-17135 REV A. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2024092700036Stringer · crackedSTA 2360 STR 1L AFT OF PRESSURE BULKHEAD STRINGER FOUND CRACK(<P>STA 2360 STR 1L AFT OF PRESSURE BULKHEAD STRINGER REPAIRED IAW RI-53-60-17138 REV.A. NO FURTHER DEFECTS NOTED</P>)
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