Boeing 747-2B5F
Service difficulty reports · 39
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 = '7472B5F' 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 = '7472B5F' 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 TX9Y20110928006Valve · malfunctionedAIRCRAFT DEPARTED AIRPORT TO PERFORM A FUNCTIONAL TEST FLT, AFTER HEAVY CHECK. ON CLIMBOUT, ACFT DEVELOPED PROBLEMS WITH THE NR 1 ENGINE NACELLE OVERHEAT RUNNING HIGH WHICH INDICATED ON BOTH A AND B DETECTION SYSTEM INDICATORS, ALSO AT THIS TIME A "BURNING ODSDR TX9Y20110924002Structure · damagedDURING ACCOMPLISHMENT OF SB 747-54-2230 R0, FIGURE 14 ON THE STRUT STRUCTURE ASSEMBLY AT NR 3 PYLON, CRACK DAMAGE AT NUMEROUS HOLES WAS FOUND IN THE CAP SKIN ASSEMBLY, THE BULKHEAD STRAP AND THE FRONT SPAR CHORD. DAMAGE WAS ALSO FOUND IN THE BULKHEAD FRAMES ASDR TX9Y20110924001Structure · damagedDURING ACCOMPLISHMENT OF SB 747-54-2230 R0, FIGURE 14 ON THE STRUT STRUCTURE ASSEMBLY AT NR 2 PYLON, CRACK DAMAGE AT NUMEROUS FASTENER HOLES WAS FOUND IN THE CAP SKIN ASSEMBLY, THE BULKHEAD STRAP AND THE FRONT SPAR CHORD. DAMAGE WAS ALSO FOUND IN THE BULKHEADSDR TX9Y20110921001Frame · damagedDURING INSPECTION, A DAMAGE WAS FOUND COMMONT TO A TOOL HOLE OF BULKHEAD AT STA1140, S-18R TO S-19R. AND NO ALLOWANCE DAMAGE LIMIT WAS PROVIDED IN SRM. A REPAIR THAT BLENDED OUT THE DAMAGED FRAME WEB AT A TOOLING HOLE AND REFINISHED THE SURFACE PER BOEING MESDR 2011F00162Mount · crackedDURING EDDY CURRENT CHECK, PYLON NR 3 REAR ENGINE MOUNT BULKHEAD OTBD UPPER AFT FRAME FOUND WITH CRACK. CRACK LENGTH APPROX 10MM. FINDING DISCOVERED DURING 'C1 & C2' CHECK. (OPEN)SDR 2011F00161Skin · crackedPYLON NR 3 UPPER SKIN EDGE AND FASTENER HOLES FOUND WITH CRACK DURING EDDY CURRENT CHECK. FINDING DISCOVERED DURING 'C1+C2' CHECK FROM 08 JUN 2011 TO 22 JULY 2011. (OPEN)SDR 2011F00160Mount · crackedCRACK DETECTED DURING LOW FREQUENCY EDDY CURRENT CHECK ON NR3 PYLON REAR ENGINE MOUNT BULKHEAD UPPER CAP SKIN STRAP ADJACENT TO FRONT SPAR FITTING. FINDING DISCOVERED DURING 'C1+C2' CHECK FROM 08 JUN 2011 TO 22 JULY 2011. (OPEN)SDR 2011F00159Mount · crackedCRACKS FOUND ON NR 2 PYLON REAR ENGINE MOUNT UPPER BULKHEAD INBD AND OTBD FRAME HORIZ FLANGE. EACH CRACK APPROX 0.500" IN LENGTH. FINDING DISCOVERED DURING 'C1 & C2' CHECK.SDR Q2SA2011F00081Valve · malfunctionedWITH NR 4 CROSS FEED VALVE INDICATING "OPEN", NR 4 TANK (QTY) WENT DOWN AS IF CROSSFEED VALVE WAS CLOSED. NR 4 TANK BOOST PUMP LOW PRESSURE LIGHTS DID NOT FLASH, ENGINE NR 4 FLAMED-OUT. DESCENDED TO FL 300 AND RECYCLED NR 4 CROSSFEED VALVE, ALL ENGINE INDICASDR Q2SA708003Hydraulic Line · rupturedSHORTLY AFTER TAKEOFF THE CREW CALLED IN TO NOTIFY, HAD LEFT BODY GEAR PRIMARY/ALT LIGHT ON PER QRH AND ARE RETURNING TO ORD, 110 THOUSAND POUNDS OF FUEL WAS DUMPED AS A PRECAUTION BEFORE LANDING. DURING GROUND INSPECTION, MAINTENANCE WAS UNABLE TO IDENTIFY ASDR Q2SA704002Unknown · malfunctionedAT CRUISE, NUMBER 4 ENGINE WOULD NOT ACCELERATE; ACCOMPLISHED QRH PROCEDURE: ABNORMAL ENGINE RESPONSE TO THROTTLE SETTING. ACCOMPLISHED PNEUMATIC MANIFOLD INSPECTION OF NUMBER 4 ENGINE. ALL CHECKS NORMAL PER AMM 36-11-01. ITEM TRANSFERRED TO DI 21818 PER MSDR 2010FA0000437Skin · crackedNR 3 ENG PYLON AFT LWR SPAR FIREWALL SKIN 1.5 INCH CRACK.SDR 2010FA0000436Skin · crackedNR 3 ENG LT PYLON ACCESS PANEL CRACKED.SDR 2010FA0000435Door · crackedNR 2 PYLON LT SIDE PRESSURE RELIEF DOOR CRACK (0.35 INCH).SDR 2010FA0000438Skin · dentedAPU LT ACCESS DOOR SKIN DENT. INSTALL EXTERNAL REPAIR DOUBLER.SDR 2010FA0000434Skin · crackedNR 3 ENG LT SIDE COWL SKIN CRACK. INSTALL EXTERNAL REPAIR DOUBLER.SDR 2010FA0000433Stiffener · crackedCRACK WAS FOUND ON THE STIFFENER OF THE NR 3 PYLON. INSTALLATION SPLICE REPAIR ANGLES.SDR 2010FA0000432Skin · crackedNR 4 PYLON AFT FAIRING DOOR LT SIDE CRACKED. BONDING EXTERNAL REPAIR DOUBLER.SDR 2010FA0000431Longeron · crackedNR 3 ENG LT SIDE COWL UPPER LONGERON CRACK. INSTALL REPAIR DOUBLER.SDR 2010F00082Frame · cracked(KADY) CRACK AT FLANGE OF INNER CHORD OF BS 2598 BULKHEAD. MAJOR REPAIR ACCOMPLISHED BY TRIM OUT THE CRACKED CHORD AND INSTALL REPAIR PART INCLUDING SPLICE ANGLE.SDR 2010F00079Skin · cracked(KADY) CRACK WAS FOUND ON THE SKIN OF THE NR 3 ENGINE RT SIDE COWL AT NAC STA 225.95.SDR 2010FA0000360Skin · worn(KADY) WEAR DAMAGE WAS FOUND ON THE CAP SKIN OF THE NR 4 PYLON AT NAC STA 210.00-221.90 NAC WL 187.63-190.68.SDR 2010FA0000359Skin · worn(KADY) WEAR DAMAGE WAS FOUND ON THE CAP SKIN OF THE NR 1 PYLON AT NAC STA 210.00-221.90 WL 187.63-190.60.SDR 2010FA0000358Frame · cracked(KADY) A CRACK WAS FOUND ON THE FRAME AT STA 1680, S13R-S14R.SDR 2010FA0000357Floorbeam · damaged(KADY) AN ELONGATED FASTENER HOLE WAS FOUND ON THE UPPER DECK FLOORBEAM UPPER CHORD AT STA 380, LBL 22/12.SDR 2010FA0000333Cowling · delaminated(KADY) DELAMINATION ON THE NR 2 ENG NOSE COWL. MINOR REPAIR ACCOMPLISHED BY FABRICATE REPAIR DOUBLER, STRAP AND CURE AFTER BOND.SDR 2010FA0000332Seat Track · worn(KADY) ENLARGE THE MAIN DECK SEAT TRACK PIN HOLE AT SEC 44 AND 46. MAJOR REPAIR ACCOMPLISHED BY OVERSIZE REAM AND INSTALL FREEZE PLUG BUSH.SDR 2010FA0000331Seat Track · corroded(KADY) CORROSION AT SEAT TRACK BS 1500, RBL 98.58. MAJOR REPAIR ACCOMPLISHED BY BLEND OUT OF CORROSION AND FABRICATE AND INSTALL A REPAIR STRAP.SDR 2010FA0000356Seat Track · worn(KADY) ENLARGE THE MAIN DECK SEAT TRACK PIN HOLE AT SEC 42. MAJOR REPAIR ACCOMPLISHED BY OVERSIZE REAM AND INSTALL FREEZE PLUG BUSH.SDR 2010F00085Skin · damaged(KADY) AN ENLARGED HOLE WAS FUND ON THE OTBD SKIN AT NAC STA 286.50.SDR 2010FA0000355Skin · corroded(KADY) CORROSION AT NR 1 PYLON OTBD CAP SKIN. MINOR REPAIR ACCOMPLISHED BY BLEND OUT THE CORROSION AND APPLY FINISH TREATMENT.SDR 2010F00083Skin · corroded(KADY) CORROSION AT NR 4 PYLON OTBD CAP SKIN. MINOR REPAIR ACCOMPLISHED BY BLEND OUT THE CORROSION AND APPLY FINISH TREATMENT.SDR 2010F00084Skin · cracked(KADY) CRACK WAS FOUND NR 3 PYLON INBD SKIN.SDR 2010FA0000354Floorbeam · cracked(KADY) CRACK AT FLOORBEAM WEB AT UPPER DECK BS 340, 400, AND 500. MAJOR REPAIR ACCOMPLISHED BY TRIM OUT THE CRACKED FLOORBEAM AND INSTALL REPAIR FILLER AND REPAIR DOUBLER.SDR 2010FA0000351Skin · worn(KADY) WORN AT OUTER SKIN AND FLANGE OF FRAME. MINOR REPAIR ACCOMPLISHED BY TRIM OF DAMAGED SKIN AND FRAME AND INSTALL FILER AND REPAIR ANGLE AND REPAIR DOUBLER.SDR 2010FA0000353Skin · worn(KADY) WORN AT OUTER SKIN AND STIFFENER OF NR 4 LT SIDE COWL. MONOR REPAIR ACCOMPLISHED BY TRIM OUT THE DAMAGED SKIN AND STIFFENER AND INSTALL REPAIR DOUBLER.SDR 2010FA0000352Skin · punctured(KADY) PUNCTURE OF NR 4 ENGINE LT SIDE FAN COWL INNER SKIN. MINOR REPAIR ACCOMPLISHED BY TRIM OUT THE DAMAGED SKIN AND INSTALL FILLER AND REPAIR DOUBLER.SDR 2010FA0000350Fairing · cracked(KADY) NR 1, 3 AND 4 ENG SLOT SEAL FAIRING FASTENER HOLES WORN. MINOR REPAIR ACCOMPLISHED BY OVERSIZE, THE AFFECTED HOLES AND INSTALL NEW GROMMET ASSY.SDR Q2SA708001Fuel Control · malfunctionedATB AT ANC DUE TO ENGINE PROBLEM. NR 4 ENGINE STALLED DURING CLIMB AT 33,600 FT. REDUCED THRUST TO IDLE. IDLE PARAMETERS N1 37 PERCENT, N2 61 PERCENT, EPR ERRATIC, EGT 483, FF 800. ALL BLEEDS ON, 2 AIR CONDITIONING PACKS ON. 2 AIR CONDITIONING PACKS ON. R
Back to Boeing 747-2B5F