JASC 7110
Service difficulty reports · 2,324
Reports filed under 7110 · Engine Cowling System, newest first.
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 jasc_code = '7110' 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 jasc_code = '7110' 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 DL757953454Panel · heat damageDURING SHOP VISIT AT REPAIR STATION EZ2R812K, ENGINE FAN COWL WAS REPAIRED FOR HEAT DAMAGE ON INTERIOR SKIN AT LOWER FWD END. A 2 SQ FT AREA OF HONEY COMB WAS REMOVED AND REPLACED PER DRAWING 314N3111, SRM 54-21-01 AND 54-21-04.SDR 96ZZZX2554Bracket · missingDURING REMOVAL OF UPPER ENGINE COWLING, FOUND SMALL PORTION OF LT BRACKET MISSING. SUBSEQUENT INSPECTION OF RT BRACKET REVEALED SEVERE EXFOLIATION ALONG UPPER PORTION OF BRACKET. SUSPECT CAUSE AS DISSIMILAR METAL AND GALVANIC CORROSION IN LATENT STAGES.SDR DL72W953365Support Ring · wornDURING HMV, FOUND NR 2 ENG COWL SUPPORT RING WORN. REPAIRED PER M/M 53-11-0 PAGE 801.SDR 95ZZZX5632Flap · departedRIGHT COWL FLAP DEPARTED AIRCRAFT IN-FLIGHT. SUSPECT CORROSION BETWEEN HINGE AND STEEL PIN. SUBMITTER RECOMMENDS IF ANY EXCESSIVE PLAY IS DETECTED IN HINGE AREA, REMOVE AND REPLACE HINGE, ESPECIALLY IF HINGE STILL LOOKS SERVICEABLE. THIS CORROSION IS HIDDENSDR DL72S953223Inlet · crackedTEMP REPAIR OF .8750 INCH CRACK IN NR 2 ENG INLET. REPAIR LOCATED AT 12:20 JUST AFT OF FWD INLET. INSTALLED PERMANENT REPAIR PER MM 54-30-0 PG 801 TO 802.SDR 96ZZZM596Skin · corrodedDURING D-CHECK, NR 2 ENGINE INLET INNER SKIN BULGE AND CRACKED JUST BELOW PRODUCTION JOINT 7 O'CLOCK. REMOVED FASTENERS PER SRM 51-30-2. REMOVED ALL DAMAGED AREA PER SRM 54-10-3. FABRICATED DOUBLER AND FILLER AS 7075-T6 (DOUBLER .050 AND FILLER .040) PER SRSDR P5CA9500670Cowling · crackedCRACK ON FORWARD EDGE NR 3 ENGINE RIGHT COWLING EXTERIOR SURFACE SKIN. REPAIRED PER BOEING SRM 54-30-03.SDR P5CA9500668Cowl Frame · crackedCRACKED FRAME 3RD HOOK NR 4 ENGINE RIGHT MAIN COWL UPPER. REPAIRED PER BOEING SRM 54-30-03.SDR P5CA9500665Cowling · corrodedSURFACE CORROSION ON RIVET HEADS AND SHEARED RIVETS ON THE EXTERIOR SURFACE OF NR 2 LEFT COWLING. REPLACED RIVETS PER BOEING SRM 51-30-02.SDR P5CA9500664Cowling · corrodedSURFACE CORROSION ON INTERIOR SURFACE SKIN OF NR 2 ENGINE RIGHT COWLING. REMOVED CORROSION PER BOEING SRM 51-10-01.SDR P5CA9500663Cowling · corrodedSURFACE CORROSION AND LOOSE RIVETS ON NR 3 ENGINE COWLING, RIGHT EXTERIOR SURFACE SKIN. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS. REPLACED LOOSE RIVETS.SDR P5CA9500662Cowling · corrodedSURFACE CORROSION ON NR 3 ENGINE RIGHT COWLING INTERIOR SURFACE SKIN. REMOVED CORROSION PER BOEING SRM 51-10-01.SDR P5CA9500661Cowling · damagedDAMAGE ON NR 3 ENGINE LEFT FAN COWL EXTERIOR SKIN. REPAIRED PER BOEING SRM 54-30-03.SDR P5CA9500660Bracket · brokenBROKEN HOLDING BRACKET FOR SUPPORT ROD NR 3 ENGINE LEFT COWLING. MANUFACTURED BRACKET PER BOEING SRM 51-20-02, INSTALLED PER 51-30-02.SDR P5CA9500659Cowling · corrodedSURFACE CORROSION ON NR 3 ENGINE LEFT COWLING INTERIOR. REMOVED CORROSION PER BOEING SRM 51-10-01.SDR P5CA9500653Cowl · crackedCRACK WITH STOP HOLE ON EXTERIOR SURFACE O, NR 2 LEFT COWLING, UNDER CSD OIL FILL PANEL. REPAIRED PER BOEING SRM 51-40-02.SDR DLL13953156Nose Cowl · crackedAT HMV, FOUND NOSE COWL CRACKED RT UPPER FWD ACCESS NR 2 INLET. REMOVED FASTENERS FABRICATED REPAIR. DYE CHECKED AND INSTALLED REPAIR PER SRM 54-34-00 FIG 804.SDR DLL13953155Nose Cowl · crackedAT HMV, FOUND NOSE COWL CRACKED AT STA 1705, NR 2 INTAKE. REMOVED OLD ANGLE, AND FABRICATED NEW. INSTALLED PER SRM 54-12-00 PG 806.SDR DLL13953112Nose Cowl · damagedAT HMV, FOUND NOSE COWL HAD TIME LIMITED REPAIR. REMOVED OLD ANGLE. DRILLED NEW ANGLE AND INSTALLED PER SRM 54-12-00, FIG 803.SDR P5CA9500268Stiffener · brokenENGINE NR 3 FAN NOSE COWL AFT BULKHEAD AT 3 O'CLOCK, FOUND BROKEN PIECE IN STIFFNER. TRIMMED AND TREATED PER SRM 51-10-01. MATERIAL IS WITHIN LIMITS PER BOEING SRM 54-12-01.SDR DL757953453Cowl · heat damageDURING SHOP VISIT AT REPAIR STATION EZ2R812K, ENGINE FAN COWL PANEL WAS REPAIRED FOR HEAT DAMAGE AT THE LOWER END INTERIOR SKIN, AFT END LOWER CORNER. DELAMINATION ACROSS PANEL TO WITHIN 10 INCHES OF FWD EDGE AND A PUNCTURE AREA OF 3 BY 1.5 INCHES AT MID PANESDR 95ZZZX3448Truss Mount · crackedDURING C-CHECK, FOUND NR 2 ENGINE TRUSS MOUNT CRACKED AT DIAGONAL BRACE ATTACHMENT CRACKED. REPLACED TRUSS MOUNT.SDR 95ZZZX3428Fasteners · failedDURING INSPECTION FOUND VENTRAL FIN DAMAGED. FOUND UPPER COWLING FASTENER HAD COME LOOSE, STRUCK PROPELLER AND WAS THEN THROWN INTO VENTRAL FIN. FASTENER WAS STILL LODGED IN FIN. PROPELLER WAS REMOVED FOR REPAIRS AND FIN REPAIRED PER STRUCTURAL REPAIR MANUASDR DL72W952946Cowl · wornNR 2 PYLON BS 1352 MATING SURFACE BETWEEN ENG COWLS AND AFT FUSELAGE ARE WORN AT LOWER AREAS. DRILLED, HEAT TREATED, AND INSTALLED REPAIR PER MM 53-11-0.SDR DL757952752Cowl · damagedGROUND DAMAGE TO NOSE COWL PANEL WAS FOUND AT 10 O'CLOCK POSITION, DURING HMV. DAMAGE WAS REPAIRED PER SRM 54-11-01 REF 51-70-17.SDR DL757952680Nose Cowl · damagedGROUND DAMAGE TO NOSE COWL AT 10 O'CLOCK POSITION. REPAIRED PER SRM 54-11-01.SDR UPS203536Engine Ring · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND ENGINE RING CORRODED AT STA 1342. REPLACED IAW SRM 51-10-1, 51-30-2.SDR DL72S952605Nose Cowl · crackedFOUND DURING A-2 LETTER CHECK, NOSE COWL AFT WEB CRACKED 6 INCHES AT 5 O'CLOCK POS/AFT WEB DOUBLER CRACKED 2 INCHES 5:30 POS. REPAIRED PER SRM 54-10-3 FIG 3.SDR DL757952566Cowl · erodedAT HMV, THE NR 1 ENG NOSE COWL WAS FOUND ERODED ON THE COMPOSITE L/E. THIS WAS REPAIRED PER SRM 54-11-01 REF 51-70-03.SDR 95ZZZX4225Strut Assy · misinstalledEND OF STRUT NOT INSTALLED CORRECTLY. CAUSES STRUT TO BIND IN COWLING. END NEEDS TO BE ROTATED IN THE DIRECTION OF THE ARROW PRINTED ON THE TAPES. REMOVED AND REPLACED.SDR P5CA9500011Side Cowl · wornTOP AFT EDGE OF RIGHT SIDE COWL IS WORN AWAY AND BENT DOWN WITH FOOT FORWARD OF AFT END. REPAIRED AS PER SRM 54-14-07.SDR 95ZZZM156Cowl · wornTOP AFT EDGE OF RIGHT SIDE COWL IS WORN AWAY AND BENT DOWN ONE FOOT FORWARD OF AFT END. REPAIRED AS PER SRM 54-14-07.SDR DL72K952200Skin · crackedA 6 INCH BY .25 INCH CRACKS FROM RIVETS ON LT VERT SPAR SKIN, JUST FWD AND BELOW BOTTOM CORNER OF SADDLE PANEL 9501. ALSO, 2 INCH BY .25 INCH CRACKS ON RT SIDE SAME LOCATION AS ITEM 1 ABOVE, AT NR 2 INTAKE STRUCTURE. REPAIRED PER MM 54-30-0.SDR 95ZZZZ239Duct · delaminationTHE NR 1 ENGINE FAN COWL INNER DUCT SKIN DELAMINATED AT 3 O'CLOCK POSITION. REPAIRED PER DALFORT AVIATION XEA NR X2-78-6.SDR DL72L952291Lip · damagedFORWARD COWLING LIP DAMAGED AT 6 O'CLOCK POSITION NR 2 ENG CUTOUT. FOUND DURING CV-2 CHECK. REPAIRED PER M/M 53-11-0 PG 801.SDR DL757952150Skin · damagedFOUND DURING LETTER CHECK, NOSE COWL L/E DAMAGED AT 5 O'CLOCK POS. ALSO, SMALL HOLES IN NOSE COWL 3 O'CLOCK POS. REPAIRED PER SRM 54-11-01.SDR DL76E952109Cowl · crackedFOUND LWR CHANNEL, AFT END OF CORE COWL TO BE CRACKED. REPAIRED PER SRM 54-41-02 PG 217. FOUND AND REPAIRED AT SHOP INSPECTION.SDR DL757952849Nose Cowl · errosionDURING INSPECTION, ENGINE NOSE COWL WAS FOUND WITH EROSION DAMAGE ON T/E COMPOSITE SKIN AT 6 O'CLOCK POSITION, APPROX 5 INCHES LONG. REPAIRED PER SRM 54-11-01 AND 51-70-03.SDR DL72S952506Inlet · crackedNR 2 ENGINE INLET AFT LWR EDGE, BENT AND CRACKING IN SEVERAL PLACES. REPAIRED PER SRM 54-10-3.SDR DL31L952127Cowl · delaminatedNR 1 ENG INLET COWL OUTER BARREL COMPOSITE SKIN DELAMINATED BEHIND LIP ASSY. ALSO, CRACKED AT THE 3 O'CLOCK POS SANDED AREA AROUND DAMAGE AND APPLIED EA 9390 AT 1230. REPAIRED SKIN PER SRM 54-10-00 PG 201.SDR DL757952249Cowl · damagedAT HMV, FOUND NR 1 ENGINE NOSE COWL WITH HOLE IN COMPOSITE PANEL AT 1 O'CLOCK POSITION. REPAIRED PER SRM 54-11-01.SDR DL757952233Cowl · dentedAT HMV, NR 1 ENGINE NOSE COWL WAS FOUND WITH DENT IN L/E LIP ON LOWER EDGE. REPAIRED PER SRM 54-11-01.SDR DL31L952041Nose Cowl · delaminatedNR 2 ENG INLET COWL OUTER BARREL COMPOSITE SKIN DELAMINATED. ACCOMPLISHED REPAIRS PER SRM 54-10-00, PG 201.SDR DL757952766Nose Cowl · dentedDURING AN UNSCHEDULED SHOP O/H DUE TO GROUND DAMAGE, THE LEADING EDGE LIP WAS REPAIRED PER SRM 54-11-01 FIG 203 AT THE 12 O/C POS.SDR DL757952069Cowl · delaminatedFOUND IN LETTER CHECK, OUTBOARD LWR SIDE OF ENG INLET DELAMINATED IN 2 AREAS. REPAIRED COWL PANEL PER DL ERA 301749-14 AND SRM 54-11-01 FIG 201.SDR DLL13952495Inlet · crackedAT HMV, FOUND SKIN CRACKED, AT NR 2 ENG INLET, ANTI-ICE DUCT. TRIMMED OUT DAMAGE, FABRACATED AND DRILLED FILLERS, AND INSTALLED REPAIR PER SRM 54-34-00 FIG 804.SDR DL72S952165Nose Cowl · crackedUPON MAINT INSPECTION, A CRACK WAS FOUND IN OUTER SKIN OF NR 3 ENGINE NOSE COWL. REPAIRED PER SRM 54-30-3.SDR DL757952951Nose Cowl · puncturedCOWL WAS DAMAGED IN STORES, .50 INCH PUNCTURE IN OUTER SKIN AT CENTER OF PANEL AND IN THE 9 O'CLOCK POSITION. THE COWL WAS REPAIRED USING 9390 RESIN. SYSTEM APPROX SIZE OF REPAIR IS 4 INCHES, USING 2 REPAIR PLIES FOR EVERY DAMAGED PLY PER SRM 51-70-17.SDR DL757951881Cowl · damagedFOUND DURING LETTER CHECK INSP, INBD SIDE OF INLET COWL HAS SMALL HOLE. REPAIRED INLET COWL PER SRM 54-11-01.SDR DL767951878Cowl · dentedDENT IN NOSE LIP SKIN AT 7 O/C POSITION. REPAIRED PER SRM 54-11-01 FOR NR 2 ENGINE INTAKE COWL.
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