Boeing 747-451
Service difficulty reports · 2,469
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 = '747451' 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 = '747451' 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 DALA1125926313Light · inoperativeDURING A MAINTENANCE VISIT, THE EMERGENCY LIGHT AT DOOR 4R WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. SYSTEM OPERATION WAS NORMAL AFTER THE LIGHT ASSEMBLY WAS REPLACED.SDR DALA1125916313Light · inoperativeDURING A MAINTENANCE VISIT, THE EMERGENCY LIGHT AT DOOR 1L WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. SYSTEM OPERATION WAS NORMAL AFTER THE LIGHT ASSEMBLY WAS REPLACED.SDR DALA1124066309Light · inoperativeDURING A MAINTENANCE VISIT, THE EMERGENCY DOOR MOUNT LIGHT AT 2L WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY DOOR MOUNT LIGHT AT 2L. SYSTEM OPERATION WAS NORMAL AFTER THE EMERGENCY DOOR MOUNT LIGHT WAS REPLACED.SDR DALA1124016309Light · inoperativeDURING A MAINTENANCE VISIT, THE EMERGENCY DOOR 4L DOOR MOUNT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE DOOR MOUNT LIGHT. SYSTEM OPERATION WAS NORMAL AFTER THE DOOR MOUNT LIGHT WAS REPLACED.SDR DALA1124006309Fuse · blownDURING A MAINTENANCE VISIT, THE EMERGENCY SLIDE LIGHT AT UPPER RIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FUSE. SYSTEM OPERATION WAS NORMAL AFTER THE FUSE WAS REPLACED.SDR DALA1124336304Skin · wornFUSELAGE SKIN AND VERT STAB LT SEAL INTERFACE HAVE WEAR.STA 2521-2628. MAX DEPTH:0.016" PER ER/A 489971-14AD BLEND OUT THE WEAR AND DAMAGE IS WITHIN LIMITS PER ER/A 489971-14AD. JOB COMPLETED. 8T2010900043 2011-07-26. ORIG MAT 0.063". DAMAGE DIM.L:16"W:0.1"SDR DALA1124326304Seal · wornFUSELAGE SKIN AND RT VERT STAB SEAL INTERFACE HAVE WEAR. STA 2521-2628. MAX DEPTH: 0.014" BLEND OUT, MEASURE AND RECORD SIZE, CHECK LIMITS PER SRM 53-00-0 1 ALLOWABLE DAMAGE1. 515462 LIU CHUN FU 149342. PER ER/A 489971-14AD BLEND OUT THE WORN AND DAMAGE IS WSDR DALA1124316304Seal · wornFUSELAGE SKIN AND VERT STAB RT SEAL INTERFACE HAVE WEAR STA 2280-2416. MAX DEPTH: 0.005" BLEND OUT, MEASURE AND RECORD SIZE, CHECK LIMITS PER SRM 53-00-0 1 ALLOWABLE DAMAGE 1. 515462 LIU CHUN FU 149342 PER ER/A 489971-14AD BLEND OUT THE WORN. AND DAMAGE IS WITSDR DALA1124306304Skin · wornFUSELAGE SKIN AND LT VERT STAB SEAL INTERFACE HAVE A WORN.STA22 80~2416.MAX DEPTH: 0.005" PER ER/A 489971-14AD BLEND OUT THE WORN. DAMAGE IS WITHIN LIMITS PER ER/A 489971-14AD. JOB COMPLETED. ORIG MAT 0.063" DAMAGE DIM. L: 14" W: 0.1" D: 0.005" ASSOCIATEDSDR DALA1127696304Skin · deformedLT NR 1 MAIN ENTRY DOOR SKIN EXTERNAL SURFACE DEFORMATION BS452 S-20L. L=1.5" HINGE CUTOUT AREA DONE THE SKIN REPAIR ER/A 489972-14 REV ORIG SEC 1, CATEGORY B. CLOSED LOG, DUPLICATE LOG PAGE. SEE LOGPAGE 0333797 FOR FOLLOW ON ACTION. MONITORED ASSY ACFT: Y LSDR DALA1127606304Skin · crackedLT NR1 ENTRY DOOR SKIN EXTERIOR SURFACE CRACK. L=0.5", BS444, S-23L. SKIN REPAIR IAW ER/A 489972-14 REV ORIG SEC 1.SDR DALA1125886304Skin · crackedLT DOOR SKIN EXTERIOR SURFACE CRACK. L=0.5", BS 44, S-23L. SKIN REPAIR IAW ER/A 489972-14, CAT B REPAIR. INSP 22,000 TOTAL DOOR FLIGHT CYCLES. INTERVAL: 3,000 DOOR FLIGHT CYCLES METHOD: INTERNAL AND EXTERNAL DVI IAW SRM 52-10-01, REPAIR 3. SEC II. A NEW FAA ASDR DALA1125546304Skin · crackedLT NR 1 MAIN ENTRY DOOR SKIN EXTERIOR SURFACE CRACK. L=0.5" BS444. S-23L. SKIN REPAIRED IAW ER/A 489972-14, REV ORIG.SDR DALA1125536304Skin · deformedLT NR 1 MAIN ENTRY DOOR SKIN EXTERNAL SURFACE DEFORMATION AT BS 452, S-20L, L=1.5" HINGE CUTOUT AREA. SKIN REPAIR IAW ER/A489972-14, REV ORIG COMPLETED.SDR DALA1122906315Power Supply · inoperativeDURING A MAINTENANCE VISIT, THE EMERGENCY FLOOR PROXIMITY LIGHTS AT ZONE B ON THE RIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE POWER SUPPLY TO BE DEFECTIVE AND REPLACED IT. SYSTEM OPERATION WAS NORMAL AFTER THE POWER SUPPLY WAS REPLACED.SDR DALA1122896311Wire · disconnectedDURING A MAINTENANCE VISIT, THE EMERGENCY ESCAPE PATH FLOOR TRACK LIGHT FROM SEAT 22H TO DOOR 2R WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE WIRE DISCONNECTED AT SEAT 22H AND RECONNECTED THE WIRE. SYSTEM OPERATION WAS NORMAL AFTER THE WIRE WAS RECONNSDR DALA1121326307Power Supply · inoperativeMAINTENANCE VISIT THE OVERWING RIGHT EMERGENCY LIGHTS L1870 AND L1165 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY M7920. SYSTEM OPERATION WAS NORMAL AFTER THE POWER SUPPLY WAS REPLACED.SDR DALA1121316301Power Supply · inoperativeDURING A MAINTENANCE VISIT THE OVERWING RIGHT EMERGENCY LIGHT L1870 AND L1165 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY M7920. SYSTEM OPERATION WAS NORMAL AFTER THE POWER SUPPLY WAS REPLACED.SDR DALA1120566306Wire · disconnectedDURING A MAINTENANCE VISIT, THE EMERGENCY ESCAPE PATH FLOOR TRACK LIGHTING AT SEATS 51 AND 52 WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE WIRE DISCONNECTED AT SEAT 52C AND RECONNECTED IT. SYSTEM OPERATION WAS NORMAL AFTER THE WIRE WAS RECONNECTED.SDR DALA1119796310Wire · inoperativeDURING A LINE CHECK, MAINTENANCE FOUND THE LEFT MOST FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPAIRED A WIRE AT THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD.SDR DALA1118906304Power Supply · inoperativeDURING A MAINTENANCE VISIT, THE EXTERIOR EMERGENCY LIGHTS AFT OF THE INBOARD FLAP RIGHT WING WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE 3R DOOR POWER SUPPLY. SYSTEM OPERATION WAS NORMAL AFTER THE POWER SUPPLY WAS REPLACED.SDR DALA1118856304Light · inoperativeDURING A MAINTENANCE VISIT, THE EMERGENCY SLIDE LIGHT AT DOOR 2R WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE 2R DOOR SLIDE LIGHT. SYSTEM OPERATION WAS NORMAL AFTER THE LIGHT WAS REPLACED.SDR DALA1118576305Light · disconnectedCREW FOUND THE EMERGENCY PATH LIGHT, GALLEY UNIT NR 1, AFT CENTER TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE LIGHT ASSEMBLY. SYSTEM OPERATION WAS NORMAL.SDR DALA1117086309Frame · crackedDURING HFEC INSPECTION FOUND 2 INCH LONG CRACK AT BX 2674.85 WL 305. FWD SIDE OF FRAME. CUT OUT DAMAGE, FABBED REPAIR OUT OF 2024T3 .050", TREATED AND INSTALLED PER SRM 51-70-11 FG 201 ID TAG INSTALLED PER PS 900 5-1 INSPECTION RII MTC COMPLETE.SDR DALA1116136315Frame · damagedFOUND HEAT DAMAGE ON BULK CARGO LOWER LOBE FRAME WEB AT STA 2160, LBL23, AREA:1.97" X 1.38" DO THE FRAME WEB REPAIR IAW ER/A488632-14 REV ORIG INSP THRESHOLD: 20000 TOTAL FLIGHT CYCLES.SDR UALA2011030301046Light · missing22H SEAT MOUNTED EEL LIGHT MISSING. REPLACED EEL LIGHT AT 22H. OPS OKAY.SDR DALA1115166305Wire · disconnectedDURING A MAINTENANCE VISIT THE EMERGENCY FLOOR AT ZONE A WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED WIRES AT SEAT 4J. SYSTEM OPERATION CHECKED NORMAL AND AIRCRAFT GOOD FOR SERVICE.SDR DALA1114446315Bearing · corrodedCORROSION WAS FOUND ON OTBD SIDE UNDER-WING FITTING BEARING OF NR 3 STRUT TO WING DSB BEARING.SDR DALA1114436315Bearing · corrodedCORROSION WAS FOUND ON INBD SIDE STRUT AFT BULKHEAD FITTING BEARING OF NR 3 STRUT TO WING DSB BEARING.SDR DALA1114426315Fitting · corrodedCORROSION WAS FOUND ON O/B SIDE STRUT AFT BULKHEAD FITTING BEARING OF NO 3 STRUT TO WING. DSB BEARING CORRECTED PER CARD 5441-01068-03C.SDR DALA1114406306Connector · brokenDURING A MAINTENANCE VISIT, THE FLOOR PROXIMITY EMERGENCY LIGHTS AT A-ZONE LEFT SIDE WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE ELECTRICAL CONNECTOR BROKEN NEAR SEAT 4B. MAINTENANCE REPAIRED THE WIRE AT 4B EMERGENCY PROXIMITY LIGHT ASSEMBLY. SYSTEMSDR DALA1116926315Skin Panel · damagedDURING L CHECK, FUSELAGE SKIN PANELS HAS WEAR DAMAGE AT THE VERTICAL STABILIZER SEAL INTERFACE.SDR DALA1113776309Connector · disconnectedDURING MAINTENANCE VISIT, THE EMERGENCY PATH LIGHT AT GALLEY G3C LEFT WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE CONNECTORS AT THE EMERGENCY LIGHT AT PATH HAVE DISCONNECTED. MAINTENANCE REPAIRED THE CONNECTORS. SYSTEM OPERATION WAS NORMAL AFTER THE SDR DALA1113126309Power Supply · inoperativeDURING MAINTENANCE VISIT, THE RIGHT OVERWING EMERGENCY LIGHTS NR 1 AND NR 2 POSITION WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY FOR THE EMERGENCY LIGHT ABOVE DOOR 3L. SYSTEM OPERATION WAS NORMAL AFTER THE POWER SUPPLY WAS REPLACED.SDR DALA1111456302Skin · crackedDURING L-CHECK, FUSELAGE SKIN CRACKING WAS FOUND ON THE NOSE WHEEL WELL AFT CORNERS. ACCOMPLISHED SECT II INSP WITHIN 6000 CYCLES AFTER SECTION I. REPEAT SECTION II INSPECTIONS AT 1500 CYCLE INTERVALS. PERFORMED FUSELAGE EXTERIOR SKIN REPAIR IAW ER/A 48862SDR DALA1111426316Skin · wornVERTICAL STABILIZER SEAL INTERFACE INSPECTION LT SIDE FOUND LIGHT WEAR BETWEEN STA 2380-2397. BLENDED AREA, MAX MATERIAL REMOVED IS.006"HFEC NO CRACKS WITHIN LIMITS IAW SRM53- 00-01, FIG 101. TREATED, PRIMED AND APPLIED TEFLON COATING IAW AA5331-01190-02, ERSDR DALA1113926302Sill · crackedRT NR 1 DOOR UPPER SILL CRACK,BS460,S-17R L=1.5 INCHES PERFORMED THE UPPER SILL WEB REPAIR PER ER/A488625-14 REV ORIG C /W ER/A488625-14 REV ORIG RII COMPLETED. PERFORMED THE UPPER SILL WEB REPAIR PER ER/A 488625-14AD REVORIG. C/W ER/A 488625-14AD REV ORIG RSDR DALA1111516315Connector · damagedDURING A LINE CHECK, MX FOUND THE EMERGENCY PATH LIGHTS AT SEAT 10B INOPERATIVE. MX REPAIRED THE CONNECTOR. OPS CHECK WAS GOOD.SDR DALA1111506313Light · inoperativeDURING A LINE CHECK, MX FOUND THE EMERGENCY PATH LIGHT AT SEAT 9J INOPERATIVE. MX REPLACED THE LIGHT ASSY. OPS CHECK WAS GOOD.SDR DALA1111466302Skin · wornWEAR WAS FOUND AT FUSELAGE SKIN AND VERTICAL STABILIZER SEAL INTERFACE. STA 2521-2628. MAX DEPTH: 0.027" IAW ER/A 488622-14AD, REV 0 AND SRM 53-00-01, REPAIR 15, FIG 201 PERFORMED MED FUSELAGE SKIN-BUTT JOINT EXTERNAL REPAIR, THIS IS A CATEGORY" B" REPAIRSDR DALA1111416316Skin · wornVERTICAL STABILIZER SEAL INTERFACE INSP RT SIDE. FOUND LIGHT WEAR DAMAGE STA 2538-STA 2557. BLENDED AREA MAX MATERIAL REMOVED IS .003". HFEC NO CRACKS, WITHIN LIMITS IAW SRM 53-00-01, FIG 101. TREATED, PRIMED AND APPLIED TEFLON COATING IAW AA5331-01190-02SDR DALA1111406316Skin · gougedVERTICAL STABILIZER SEAL INTERFACE INSP LT SIDE FOUND WEAR BETWEEN STA 2280-2300 WITH GOUGE AT STA 2298. BLENDED AREA, MAX MATERIAL REMOVED IS .015". HFEC NO CRACKS WITHIN LIMITS IAW SRM5300-00-01, FIG 101, NOTE K. TREATED, PRIMED AND APPLIED TEFLON COATINSDR DALA1111396316Skin · wornVERTICAL STABILIZER SEAL INTERFACE INSP RT SIDE. FOUND WEAR DAMAGE FROM STA 2598-STA2628. BLENDED AREA, MAX MATERIAL REMOVED IS .006".HFEC NO CRACKS. WITHIN LIMITS IAW SRM 53-00-01, FIG 101. TREATED, PRIMED AND APPLIED TEFLON COATING IAW AA5331-01190-02. SDR DALA1111386316Fuse · inoperativeDURING A MX VISIT, THE EMERGENCY EXIT LIGHT AT DOOR 4R WAS FOUND INOPERATIVE. MX REPLACED THE FUSE IN POWER SUPPLY M7922 IAW AMM.SDR DALA1110846316Skin · damagedVERT STAB SEAL INTERFACE INSP JOB CARD 5331-01190-02 RT SIDE FOUND LIGHT WEAR DAMAGE FROM STA 2280-STA 2350. BLENDED AREA. MAX MATERIAL REMOVED IS .008" HFEC NO CRACKS WITHIN LIMITS IAW SRM 53-00-01, FIG 101. TREATED, PRIMED, APPLIED TEFLON COATING IAW AA SDR DALA1110836316Skin · damagedVERTICAL STABILIZER SEAL INTERFACE 01190-02, RT SIDE. FOUND LIGHT WEAR DAMAGE FROM STA 2360-STA 2397. BLENDED AREA, MAX MATERIAL REMOVED IS .009" HFEC NO CRACKS, WITHIN LIMITS IAW SRM 53-00-01, FIG 101. TREATED, PRIMED, AND APPLIED TEFLON COATING IAW AA53SDR DALA1110826316Skin · damagedVERT STAB SEAL INTERFACE INSP RT SIDE, FOUND LIGHT WEAR DAMAGE FROM STA 2557-STA 2598. BLENDED AREA, MAX MATERIAL REMOVED IS .006". HFEC NO CRACKS WITHIN LIMITS IAW SRM 53-00-01, FIG 101. TREATED, PRIMED AND APPLIED TEFLON COATING IAW AA 5331-01190-02. ERSDR DALA1111376316Skin · wornVERTICAL STABILIZER SEAL INTERFACE INSP LT SIDE FOUND WEAR BETWEEN STA 2560-2630. BLENDED AREA, MAX MATERIAL REMOVED IS .004. HFEC NO CRACKS WITHIN LIMITS IAW SRM 53-00-01, FIG101, TREATED, PRIMED AND APPLIED TEFLON COATING IAW AA5331-01190-02. ERA 489979-SDR DALA1111366316Skin · wornVERTICAL STABILIZER SEAL INTERFACE INSP CARD LT SIDE FOUND WEAR BETWEEN STA 2360-2380. BLENDED AREA, MAX MATERIAL REMOVED IS .010" HFEC NO CRACKS. WITHIN LIMITS IAW SRM 53-00-01, FIG 101, TREATED PRIMED AND APPLIED TEFLON COATING IAW AA 5331-01190-02, ERA 489SDR DALA1111356316Skin · wornVERTICAL STABILIZER SEAL INTERFACE INSP LT SIDE. FOUND LIGHT WEAR BETWEEN STA 2520-2560 BLENDED AREA MAX MATERIAL REMOVED IS .002" HFEC NO CRACKS. WITHIN LIMITS IAW SRM 53-00-01, FIG 101 TREATED, PRIMED AND APPLIED TEFLON COATING IAW AA 5331-01190-02, ERA 489
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