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 SWIA200922909Rod · out of positionLEFT THRUST LEVER JAMMED AFTER TAKEOFF. (FLT 6005) RESTOWED LEFT CORE COWL HOLD OPEN ROD.SDR VNAA2009101900006Nose Cowl · dentedAFTER ARRIVAL IN GNV, THE CREW REPORTED A DENT ON THE RT ENGINE COWL LIP AT APPROXIMATELY THE 11:30 POSITION DUE TO A POSSIBLE BIRD STRIKE. MAINTENANCE INSPECTED THE DENT AND REMOVED AND REPLACED THE RT ENGINE NOSE COWL ASSEMBLY USING THE AIRCRAFT MAINTENANCESDR IPXA09557598Support Angle · crackedINSPECTION TYPE:C2 NR 2 ENGINE I/B TURBINE CASE COOLING AIR INLET SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED CRACKED NR 2 ENGINE I/B TURBINE CASE COOLING AIR INLET SUPPORT ANGLE IAW SRM 51-40-02-0G.SDR CA091006005Bracket · cracked(CAN) ON INSPECTION ACFT, FOUND CRACKED ATTACH BRACKETS, ANGLES AND HINGE HALFS ON THE COWLING INLET AIR BYPASS DOORS. THE SECOND AND THIRD AFT HAD DAMAGE FOUND DUE TO INCREASED INSP BASED ON THE DAMAGE BEING FOUND ON THE FIRST. ALL PARTS WERE OR WILL BE REPLSDR UALA2009090302770Nose Cowl · damagedNR 1 ENG STRUCK JETWAY WHILE PARKING AT GATE B17. NOSE COWL OUTER SKIN AND CORE DAMAGED. NO DAMAGE TO INNER SKIN. ACCMP'D INTERIM REPAIR TO L-NOSE COWL. INSTALLED METAL PATCH INNER AND OUTER FAN COWL SEAL EDGES AND TAPE. ACFT FERRIED TO SFO FOR REPAIR. NSDR IPXA09M57370Skin · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQUENCE 253-P3-01, NR 3 ENG RT CORE STA NAC 290 AND STA NAC 300, AND NAC WL 70.0, NOT CORRELATED WITH MD-11 SRM WRONG FASTENERS AND CORNER RADIUS AND SKIN STILL CRACKED (UNDER REPAIR). REMOVED DOUBLERS, CUTOUT DAMAGE, FABRICASDR IPXA09557221Cowling · damagedINSPECTION TYPE:C1 NR 2 ENGINE I/B FAN COWL HAS DAMAGE ON THE LOWER EDGE JUST AFT OF THE AFT LATCH. REPAIRED IAW ER09-4299.SDR IPXA09M57074Skin · damagedINSPECTION TYPE:N/A DAMAGE TO NR 2 ENG RT FAN COWL DOOR JAMB 4 INCH CRACK. REPAIRED PER EO MD11-7110-34619.SDR QXEA2009081400612Bracket · brokenPDX - MODIFICATION - PANEL 413DR FWD ATTACH ANGLE BRACKET IS BROKEN. REMOVED ANGLE BRACKET, DRILLED NEW BRACKET AND INSTALLED REF Q400 SRM 51-42-05.SDR IPXA09556959Bracket · corrodedINSPECTION TYPE:C1 NR 2 ENGINE O/B CORE COWL UNDER SIDE BOTTOM OF THIRD FRAME CORROSION. REMOVED AND REPLACED BRACKET AT DEFECT LOCATION (CORROSION CONFINED TO -82 BRACKET ONLY).SDR IPXA09556681Rub Strip · chafedINSPECTION TYPE:C1 NR 2 ENG I/B CORE COWL UPPER AFT RUB STRIP IS CHAFING ON INNER SKIN. REMOVED & REPLACED RUB STRIP.SDR IPXA09556664Channel · chafedINSPECTION TYPE:C1 NR 2 ENGINE O/B CORE COWL HAS CHAFED CHANNEL L/E SURFACE 13 INCHES FROM BOTTOM 1 INCH FROM T/E. REMOVED AND REPLACED CATCH PER SRM 51-40-02.SDR IPXA09556663Rub Strip · chafedINSPECTION TYPE:C1 NR 2 ENGINE O/B CORE COWL UPPER AFT RUB STRIP IS CHAFED ON INNER SURFACE. REMOVED AND REPLACED PLATE PER SRM 51-40-02.SDR A6WA200940305Bracket · crackedRT ENG NOSE COWL ALIGNMENT STOP BRACKET FOUND CRACKED. RT ENG NOSE COWL ALIGNMENT BRACKET REMOVED FOR NUT PLATE INSTALLATION IAW SRM 51-42-06. (K)SDR IPXA09556332Cowling · wornINSPECTION TYPE:C2 NR 2 ENGINE I/B CORE COWL JUST AFT OF THE AFT HINGE WORN THROUGH. REMOVED AND REPLACED PER SRM 51-40-02.SDR DL757090866Acoustic Panel · delaminatedDURING SHOP VISIT, LARGE DELAMINATIONS WERE FOUND ON (PN 314N3011-4)ENGINE INLET ACOUSTIC PANEL, REQUIRING REPLACEMENT OF THE DELAMINATED SKINS. REPAIRED IAW ERA 474813-14.SDR DL757090865Acoustic Panel · delaminatedDURING SHOP VISIT, LARGE DELAMINATIONS WERE FOUND ON THE PN 314N3011-170, ENGINE INLET ACOUSTIC PANEL, REQUIRING REPLACEMENT OF THE DELAMINATED SKINS. REPAIRED IAW ERA 474812-14.SDR IPXA09555680Plate · chafedINSPECTION TYPE:C2 NR 2 ENGINE I/B CORE COWL HAS CHAFED DEFLECTOR PLATE AT UPPER AFT INNER SURFACE. REPLACED DEFLECTOR PLATE IAW SRM 51-40-05-0G, 51-40-02-0G.SDR DL76G090570Nose Cowl · damagedBIRD STRIKE AFTER TAKEOFF CAN DETECT ODOR IN CABIN RETURNING TO JFK FOR REPAIRS. NR 1 ENG BIRDSTRIKE. PERFORMED BOROSCOPE, ALL NORMAL. REPLACED ENGINE NOSE COWL.SDR IPXA09M55257Cowling · tornINSPECTION TYPE:3C NR 1 ENG OUTBOARD FAN COWL COMPOSITE MATERIAL TORN AT FWD LATCH. REMOVED DAMAGE, BONDED REPAIR PLYS IAW MD-11 SRM 54-20-00 PARA 7 REPAIR 4.SDR CA090219019Cowling · departedAFTER GEAR UP SELECTION, AND ALREADY IN A RIGHT TURN, TO FOLLOW THE DEPARTURE ROUTE, WE EXPERIENCED AN ABNORMAL YAW TO THE RIGHT FOR 1 SECOND AND THEN BACK TO NORMAL. WE EXPECTED A BIRDSTRIKE. NORMAL FLIGHT AND NORMAL LANDING. AFTER LANDING I PERFORMED AN ISDR MASA2009011100017Cowl Door · chafedMAJOR REPAIR. LT AND RT UPPER AND LWR CORE COWL DOORS, CHAFE DAMAGE AT AFT EDGE.SDR UPS09554365Support Bracket · crackedINSPECTION TYPE:C2 INBOARD SUPPORT BRACKET IS CRACKED AT AFT COMPRESSION ROD ON THE NR 2 ENGINE, 12 O'CLOCK POSITION PPS195. REMOVED AND REPLACED NR 2 ENG I/B AFT COMPRESSION ROD SUPPORT BRACKET IAW SRM 51-40-02.SDR UPS09M54405Skin · delaminatedINSPECTION TYPE:1C NR 1 ENG OUTBOARD FAN COWL HAS DELAMINATED SKIN AT TOP SIDE CENTER SECTION UNDER CENTER HINGE. REPAIRED NR 1 OUTBOARD FAN COWL UPPER CENTER AREA REF MD11 VOL IV SRM 54-20-00 PARA 11 REPAIR 8.SDR 2008F00028Cowling · crackedPOSTFLIGHT RAMP INSP DISCLOSED THAT EACH ENG COWLING HAD SMALL CRACK FWD OF AND CONNECTING TO OTBD AFT LATCHING MECHANISM. CRACKS REPAIRED AND ACFT RETUNED TO SERVICE.SDR UPS08154007Nose Cowl · crackedINSPECTION TYPE:N/A NR 2 ENGINE NOSE COWL AT 6 O`CLOCK POS CRACKED. REPAIRED PER EO A300-7110-30481-B.SDR UALA2008112106613Nose Cowl · dentedBIRD STRIKE NR 2 ENGINE INLET COWL AT 1 O'CLOCK POSITION. BAD COWL REMOVED.SDR MASA2008110600765Cowling · missingASH FLT 2743 PHX-RON. NR 1 ENGINE LOWER TRANSLATING COWL FOUND MISSING ON POST FLIGHT WALK AROUND. MX INSPECTED DAMAGE AND INSTALLED NR 1 LOWER FAN COWL.SDR HDNA200811030001Cowling · departedDURING CRUISE FLIGHT, THE AIRCRAFT SHUDDERED LIGHTLY AND THE PILOT SAW A FLASH OF WHITE. THE NR 1 ENGINE TOP FORWARD COWLING DISENGAGED FROM THE AIRPLANE. INITIAL THOUGHT WAS A BIRD STRIKE, BUT THERE WAS NO VISIBLE EVIDENCE. THE ENGINE INSTRUMENTS WERE MONISDR DALA1149659017Latch · defectiveENGINE UPPER COWL DOOR LATCH REPLACED IAW EA 09-056907-12, ME06.SDR WRAL2008082Frame · crackedDURING BRIDGE CHECK, MX FOUND NR 3 ENGINE LT CORE COWL AFT FRAME CRACK AT 9 O’CLOCK POSITION. OPENSDR DALA1169230923Cowl Door · damagedREPAIR MARK UPPER COWL DOOR ASSEMBLY. LEFT SIDE REPAIRED IAW EA 09-056907-12 ME05.SDR CA080806006Cowling · departed(CAN) AS INDICATED BY MAINT CONTROL, ACFT DEPARTED. MISSING COWLING FROM NR2 ENGINE WAS DISCOVERED DURING WALKAROUND INSP BY GROUND MAINT. IT WAS ALSO APPARENT THAT PORTIONS OF THE COWLING THAT DEPARTED ENGINE, STRUCK THE LEADING EDGES OF THE LT AND RT HORIZONSDR 2010FA0000333Cowling · delaminated(KADY) DELAMINATION ON THE NR 2 ENG NOSE COWL. MINOR REPAIR ACCOMPLISHED BY FABRICATE REPAIR DOUBLER, STRAP AND CURE AFTER BOND.SDR 08FDEA02764Adapter · wornNR 1 ENGINE LEFT CORE COWL LEADING EDGE IS WORN. ADAPTER REMOVED AND REPLACED PER DC/MD-10 SRM 51-31-01.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 A6WA200840488Bracket · crackedON RT ENGINE INLET BRACKET FOUND CRACKED AT STATION XN155.845 NEAR 5 O`CLOCK POSITION (LOOKING FWD). RT ENGINE BRACKET AT STATION XN 138.845 NEAR 5 O’CLOCK POSITION (LOOKING FWD) REPLACED IAW CRJ 200 SRM 51-42-06 & SRM 51-42-13. (A)SDR 08FDEA01941Doubler · crackedNR 3 ENG LOWER COWL, I/B SIDE EDGE, 3RD LATCH CUTOUT FROM FWD END, LOWER CUTOUT AREA, DOUBLER CRACKED OUT. REMOVED AND REPLACED DOUBLER, REF SRM 51-30-2 PG 2, THIS IS CLASSIFIED AS A MINOR REPAIR.SDR ARWA20080501Cowling · dentedNR 3 ENGINE NOSE COWL LIP HAS A DENT AT 5 O'CLOCK POSITION. TRANSFERRED TO CARRY-OVER ITEM NR 7584 IN ACCORDANCE WITH ARROW CARGO GMM 5-08-1 AND EO NR AS11722 FOR TRACKING OF DENT.SDR A6WA200840396Ring · wornCORE COWL 445 CLOSURE RING WORN BEYOND LIMITS. CORE COWL 445AB CLOSURE RING REPLACES IAW 71-12-01-300-820-A01 REPAIR. (A)SDR 08FDEA01725Nose Cowl · dentedNR 1 ENGINE NOSE COWL L/E HAS A DENT AT THE 6-7 O'CLOCK POSITION. NR 1 ENGINE NOSE COWL DENTS FOUND TO BE OUT OF LIMITS DUE TO DREASE IAW SRM 54-11-00; VOL I. REMOVAL AND REPLACEMENT ACCOMPLISHED ON N/R N00284.SDR Q2SA751004Cowling · inflt separationINFLIGHT ON CLIMB-OUT AT ABOUT 10,000 FT, LOUD NOISE HEARD WITH SLIGHT YAW TO THE LEFT. INFLIGHT INSPECTION REVEALED PANELS MISSING ABOVE THE NR 2 ENGINE PYLON AND DAMAGE TO THE LEADING EDGE OF THE WING JUST ABOVE THE NR 2 ENGINE PYLON. NO ABNORMAL FLIGHT INSDR 08FDEA01646Skin · dentedNR 3 ENGINE NOSE COWL HAS DENTS ON THE EXTERNAL SKIN AT APPROX 5 O'CLOCK POSITION. REWORKED SKIN IN REF TO EA 8-5410-116980.SDR 08FDEA01617Cowling · wornNR 3 ENG LT CORE COWL INNER SURFACE OF LEADING EDGE WORN. REMOVED ASL 0040-0 ADAPTER. LOCATED & DRILLED HOLES IAW SRM 51-35-01 & ASL 0040. INSTALLED ASL 0040 ADAPTER IAW SRM 51-35-01 & ASL 0040. PAINTED IAW SRM 51-23-01.SDR DHL2008807500Skin · wornNR 1 ENG NACELLE INLET COWL UPPER SKIN WORN STA YN 147.534 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8-70 SRM 71-5-2 FIG 2 (SHEET 1-2). REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED SKIN (AL2024T3 0.080") AND SPLICE (SHEET CRESSDR DHL2008807503Skin · wornNR 3 ENG NACELLE INLET COWL UPPER SURFACE WORN AT 12 O'CLOCK POS STA YN 147.534 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8-70 SRM 71-5-2 FIG 2 (SHEET 1-2). REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED SKIN (AL2024T3 0.080"SDR DHL2008807504Skin · wornNR 2 ENG NACELLE INLET COWL UPPER SKIN WORN STA YN 147.534 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 70 SRM 71-5-2 FIG. 2 (SHEET 1-2). REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED SKIN (AL2024T3 0.080") AND SPLICE (SHEET CRSDR 08FDEA01211Skin · chafedNR 2 ENGINE LEFT FAN COWL INNER SKIN CHAFED. REMOVED DAMAGED AREA, FABRICATED REPAIR DETAILS, PREPPED DETAILS & REPAIR AREA, LAYED UP REPAIR, VACUUM BAGGED REPAIR, CURED REPAIR, PERFORMED POST CURE INSPECTION, INSTALLED RIVETS & SEALED IAW SRM 54-00-01 VOL I.SDR 08FDEA01210Skin · chafedNR 2 ENGINE RIGHT FAN COWL INNER SKIN IS CHAFED. REMOVED DAMAGED AREA, FABRICATED REPAIR DETAILS, PREPPED DETAILS FOR BONDING, BONDED REPAIR; INSTALLED RIVETS & SEALED IAW SRM 54-00-01 VOL I. PRIMED IAW SRM 51-21-01 VOL II.
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