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 MASA2012031634583O-Ring · damagedBURNING RUBBER ODOR IN CABIN AND SMOKE FROM RT ENGINE. R & R C SUMP O-RINGS AND CLEANED COKING FROM AREA LEAK CK GOOD AND NO FURTHER SMOKE PRESENT.SDR UALA2012031201586Fireshield · wornNR 4 ENG OUTBOARD CORE COWL TRAILING EDGE IS WORN. NR 4 ENGINE, RT CORE COWL FIRESHIELD WORN. REPLACED CORE COWL.SDR CA120223003Fastener · loose(CAN) THIS ACFT WAS IN FOR A 400/800 HR INSPECTION. WHEN ENGINE COWLS OPENED, 1 OF THE BOLTS SECURING THE OUTER FAN DUCT PANEL WAS FOUND BACKED OUT TO THE POINT OF HANGING & READY TO FALL OUT. GIVEN THE TIME ON THIS ACFT, THESE PANELS, BOTH ENGINES, HAD NEVESDR ZZDA2012190Frame · chafedLT ENGINE LOWER COWL FRAME, CHAFED. OPEN DEFECT. SEE NR 24565.SDR VNAA2012021500010Cowling · damagedCREW REPORTED HEARING LOUD BANG AND AIRCRAFT YAWED TO LEFT DURING FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND DAMAGE TO LEFT ENGINE LOWER TRANSCOWL AND DENTS IN FUSELAGE. PAINTED LT LOWER TRANSITION CSDR 29GA93871021012AAttach Bracket · crackedDURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS COWLING ATTACH BRACKET WELD AREA CRACKS AND ENGINE MOUNT ATTACH POINTS WELD AREA CRACKS AND TRUSS TUBE CHAFE. PERFORMED WELD REPAIRS TO ENGINE TRUSS IN ACCORDANCE WITH FAA APPROVED DATA.SDR UALA2012020200659Rub Strip · looseNR 2 ENG RUB STRIP LOOSE LEADING EDGE OF REV COWL. INTERIM REPAIR ACCOMPLISHED PER ECRA 7111-01296. CLEANED AREA WITH SOLVENT PER GPM. APPLIED 3 LAYERS OF ALUMINUM TAPE 2524-2-0200 TO DISCREPANT AREAS. TAPE TO BE RE-INSPECTED EVERY 25 HOURS BEGINNING PTT 8SDR VNAA2012020600018Rod · disconnectedCREW REPORTED LEFT THRUST LEVER WAS JAMMED IN POSITION DURING FLIGHT. CREW FOLLOWED QRH (QUICK REFERENCE HANDBOOK), SHUT DOWN LEFT ENGINE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND LEFT ENGINE AFT CORE UPPER COWL UPPER SUPPORT ROD DSDR REXA201200113Transcowl · damagedRT TRANS COWL HIT BY SNOW PLOW. DAMAGE NOTED TO BE AS: DENT 7 1/2 IN LONG BY 3/8 WIDE WITH A CRACK IN THE OUTER SHELL 6" LONG BY 1/4 " DEEP. OVERALL PAINT SCRATCH 12 1/2 LONG AND 3 1/4 WIDE AT WIDEST POINT. CRACK DID NOT PUNCTURE INNER LINING. REMOVED AND RSDR NSVA2011384Structure · damagedFWD RT FWD O/B ATTACH HOLE ELONGATED. CONTROL# 202-67 REFERENCE TD. 340-54-11-37 DATED 12/13/.SDR NSVA2011371Structure · damagedFWD RT FWD O/B ATTACH HOLE ELONGATED. CONTROL #202-67 REFERENCE TD. 340-54-11-37 DATED 12/13/2011 AND 409#407311.SDR 9JLA2011122800001Structure · crackedDURING THE POST FLIGHT INSPECTION WALK AROUND IT WAS NOTED THAT THE NR 2 ENGINE GREEN SHEET ON THE LT SIDE WAS FOUND CRACKED AND TORN LOOSE FROM ITS ATTACHMENT. THE DAMAGED GREEN SHEET WAS FOUND VIEWED FROM THE EXHAUST END OF ENGINE. THE ATTACHMENT POINTS FOSDR UALA2011121506901Nose Cowl · dentedNR 2 ENGINE NOSE COWL HAS A DENT ON LEADING EDGE AT 5:00 POSITION. MAJOR REPAIR ACCOMPLISHED. EVALUATED DENT LIMITS AND FOUND OUT OF LIMITS PER SRM. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLERS AND INSTALLED PER SRM ON NON ROUTINE 29135.SDR UALA2011121506900Nose Cowl · dentedRAMP REPORTED DENT IN NR 2 ENG NOSE COWL 6 O'CLOCK POSITION. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE SKIN PER SRM. FABRICATED REPAIR DOUBLERS AND INSTALLED PER SRM.SDR TX9Y20111207007Longeron · crackedDURING INSPECTION OF NR 3 ENGINE RT SIDE COWL, ONE CRACK AND ONE DEEP CHAFING DAMAGE WERE FOUND AT LOWER LONGERON (P/N:65B94280-199). THE REPAIR WAS PERFORMED AS PER BOEING MESSAGE NUMBER TEC-SOF-11-0102.SDR ABXA20111107135Frame · crackedOUTBD CORE COWL DOUBLER CRACKED ON INSIDE NEAR EXHAUST DUCT. INSTALLED REPAIR DOUBLER IAW SRM 51-40-02 AND DRAWING 314T1210, WELDED REPAIRED DOUBLER IAW ABX PROCESS STANDARDS MANUAL CHAPTER 900-7 REV 49, AWG.SDR UALA2011110706006Fairing · missingNR 2 ENGINE MID SPAN SHROUD PANEL MISSING AT THE 8 O'CLOCK POSITION. INSTALLED MISSING INTERMEDIATE CASE FAIRING AT THE 8 O'CLOCK POSITION AS REQUIRED.SDR ZZDA2011912Cowling · crackedRIGHT ENGINE LOWER COWLING SECOND FROM FWD HINGE CUTOUT, CRACKED. OPEN DEFECT.SDR ZZDA2011911Cowling · crackedRIGHT ENGINE UPPER COWLING SECOND FROM FWD HINGE CUTOUT, CRACKED. OPEN DEFECT.SDR A6WA201140866Cowling · missingLT LOWER FORWARD COWL MISSING, (FOUND COWL ON RUNWAY). INSTALL LEFT LWR NOSE COWL W/SERV COWL. INSTALL LEFT LOWER NOSE COWL WITH SERV COWL. S/N OFF C0360 S/N ON SB/RJNAC/C0791.SDR P5CA2011100700483Fairing · wornNR 2 ENGINE LEFT CORE COWL'S TITANIUM FAIRING HAS WEAR DAMAGE THAT IS OUT OF SRM LIMITS. ACCOMPLISHED REPAIR AS PER EO 4478A192.SDR UALA2011091905029Cowling · damagedUNDERSIDE OF NR 4 ENGINE NACELLE IS DAMAGED. REPLACED INLET COWL NR 4 ENGINE REF MM & CHECKS REF JRH 2-86-1, ALL SATISFACTORY, NO FURTHER DEFECTS.SDR UALA2011091604993Nose Cowl · damagedNOSE COWL DAMAGED BY GROUND EQUIP. UNDERSIDE OF NUMBER 4ENGINE NACELLE IS DAMAGED. CARRIED OUT INSPECTION. WILL REQ RPL OF NOSE COWL. PCN 185-9199 COWL AND SLING 056-0097 ON ORDER. RPLC'D INLET COWL NR 4 ENGINE AND CHECKS ALL SATISFACTORY, NO FURTHER DEFECTSSDR P5CA2011090900465Skin · crackedNR 4 ENGINE RT CORE COWL OUTER SKIN HAS A 1 INCH CRACK UNDER PRE-COOLER EXHAUST DUCT. RT CORE COWL OUTER SKIN STOP DRILLED AS PER EO 4471A007 (FAA FORM 8110-3 DATED 08 SEPTEMBER 2011 ISSUED) WITH DVI AT EVERY CYCLE. PERMANENT REPAIR TO BE ACCOMPLISHED WITHSDR ZZDA2011713Structure · crackedNR 2 ENGINE UPPER COWLING NR 2 HINGE CUTOUT AREA, CRACKED. ACCOMPLISHED NR 2 HINGE CUTOUT AREA REPAIR PER B717 MM 71-12-02, SRM 54-50-02 AND 51-10-04.SDR CA110815001Cowling · missing(CAN) ON LANDING ROLLOUT, THE LT ENGINE (UPPER) COWLING SEPARATED FROM THE AC. THE RAMP NOTICED IT MISSING WHILE MARSHALLING IN THE ACFT AT THE GATE. THE ATC TOWER WAS NOTIFIED, THEY HAD A SWEEP DONE ON RWY WHICH THEY LANDED ON, AND FOUND THE COWL.SDR PIYRS261101462Cowling · separatedWHILE IN DECENT AT ALTITUDE BETWEEN 25K AND 20K A FAINT BANG WAS DETECTED AND SMALL JOLT WAS FELT THROUGHOUT THE AIRFRAME. THE FLIGHT CONTINUED WITHOUT DIFFICULTY TO THE SCHEDULED DESTINATION WHERE LANDING OCCURRED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVESDR UALA2011071903661Cowling · damagedNR 1 ENGINE LT FAN COWL DAMAGED DUE TO CONTACT WITH OXYGEN CART. REMOVED NR 1 ENGINE OUTBD FAN COWL FOR REPAIR. REPLACED FAN COWL NR 1 ENG.SDR NSVA2011158Cowling · crackedFLIGHT 9542 IAH CLL HAD A BIRD STRIKE DURING DEPARTURE. THE CREW WAS NOT AWARE THAT THERE WAS DAMAGE UNTIL ACFT LANDED IN CLL. THE BIRD HAD STRUCK THE LEFT SIDE OF THE LEFT ENGINE COWLING. IT LEFT A CRACK THAT EXTENDS FROM THE FIGURE EIGHT PART OF THE COWLISDR CA110706009Latch · strippedTHE FWD LOWER LATCH ASSY FAILED DUE TO THE INTERNAL THREADS IN THE ALUMINUN FITTING PULLING OUT. THE METAL THREADS ON THE STUD HAVE NO APPARENT WEAR, HOWEVER THE THREADS IN THE FITTING ARE BEYOND LIMITS. IT IS ONLY UNDER LOAD THRU THE CAM ACTION OF LOCKING SDR ABXR2011070100039Cowling · wornNR 2 ENGINE O/B CORE COWL EXHAUST DUCT THAT MATES TO THE PRECOOLER HAS HOLE WORN THROUGH. WELDED CORE COWL IAW ROHR CMM.SDR NSVA2011146Panel · openON ROTATION THE RT TOP COWLING PANEL ON THE ENGINE OPENED AND BEGAN FLAPPING/BENT. CREW REQUESTED TO RETURN TO AIRPORT / REDUCED SPEED TO 160 KTS AND RETURNED WITHOUT INCIDENT. MX IS INSPECTING AND REPLACING PANEL. SWAPPED FWD COWLING OFF OF 309CE. STILL WSDR UALA2011061302905Cowling · dentedNR 2 ENGINE HAS A DENT ON FAN COWL BELOW OIL SERVICE PANEL HAS A DENT. REPAIRED PER MT-71-012 INSTRUCTIONS.SDR WRLA20110601490Nose Cowl · crackedENGINE NR 2 FRONT SPAR OF NOSE COWL INSIDE CRACKED 0400 POS. LIP SKIN ON POSITION 12/3/6/9 CLOCK POS. FOUND SEVERAL NEW CRACKS NEXT TO EXISTING DOUBLER.SDR UALA2011052302530Nose Cowl · damagedNR 1 ENGINE CONTACTED LOADING BRIDGE ON ARRIVAL TO GATE. REPLACED NOSE COWL.SDR JR2R2011052400220Panel · damagedPANEL 443BT NR 2 ENGINE UPPER AFT IS CRACKED AND BENT. FABBED NEW PANEL 443BT IAW CRJ 900 SRM 51-24-16 AND 51-24-36.SDR UALA2011051602414Skin · delaminatedNR 1 ENG INBD-RT FAN COWL HAS OUTER SKIN AREA OF FROST 9" BY 8" DUE TO FROZEN WATER IN CORE AND INNER SKIN DELAMINATION 14" BY 13" 14 INCH ALONG FORWARD TAPER OF HONEY COMB CORE AND AFT UP TO 13 INCHES FROM L/E OF CORE TAPER AREA OUT OF LIMITS PER SRM. NOTE FSDR NSVA2011111Cowling · defectiveRETURNED TO GATE DUE TO RT TAIL PIPE HOT LIGHT ILLUMINATED, REPEAT. REMOVED AND REPLACED AFT RT NACELLE COWL ASSY, OPS CHECKED GOOD. PBG RECORDED PRECIPITATION 1.10 INCH FOR THE DAY. SPOT DETECTORS 4320.8 HOURS SINCE REPLACEMENT.SDR P5CA2011051000017Frame · crackedCRACK FOUND ON THE AFT HAT FRAME OF NR 2 ENGINE, LEFT CORE COWL. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A71B-990.SDR QMLDMG2192Cowling · delaminatedFOUND DELAMINATION ON OUTER STRUCTURE OF COWLING, APPROX 1 INCH IN DIAMETER, WHILE PERFORMING A STANDARD TAP TEST INSP.SDR REXA201100240Cowling · openTHE CORE COWLS OF THE NR 2 ENGINE CAME OPEN DURING FLIGHT AND THE TRANSLATING COWLS WERE SUBSEQUENTLY ALSO DAMAGED WHEN THE THRUST REVERSERS WERE DEPLOYED UPON LANDING. BOMBARDIER REO 601R-71-12-4046 WAS ISSUED TO INSPECT THE COWLS FOR FERRY FLIGHT FOR PERMANSDR VNAA2011042100012Access Panel · departedLEFT UPPER ENGINE COWL DEPARTED AIRCRAFT DURING LANDING ROLL AT DCA. MAINTENANCE INSPECTED AIRCRAFT, REPLACED UPPER NOSE COWL ACCESS PANEL ON LEFT ENGINE, REMOVED AND REPLACED LOWER NOSE COWL ACCESS PANEL ON LEFT ENGINE AND PERFORMED CHECKS USING AIRCRAFT MAISDR UALA2011041301793Cowling · damagedNR 1 ENGINE LT SUPPORT COWLING, FWD SEAL WORN AND LOOSE. REMOVED OLD RUB STRIP AND CUT TO FIT NEW RUB STRIP. REPLACED NR 1 ENGINE LT CORE COWL PER AMM.SDR A6WA201140291Strip · chafedT/E STRIP ON RT UPPER NOSE COWL IS CHAFED. R & R T/E STRIP ON RT UPPER NOSE COWL IAW CMM 71-14-01.SDR ABXA2011051049Bracket · crackedINBOARD CORE COWL T-BRACKET CRACKED AT FIRST RIB O/B OF 2ND FROM AFT END HINGE. REMOVED AND REPLACED T-BRACKET ON I/B COWL AT FIRST R.B O/B OF 2ND FROM AFT HINGE IAW 767 DRAWING 314T1210.SDR NOCA03511Angle · crackedANGLE CRACKED NR 2 ENGINE SAILBOAT FAIRING A-FRAME. REPLACED CRACKED ANGLES AS PER SRM 51-10-02.SDR UALA2011032901505Brace · damagedNR 2 ENG CORE COWL STRUCTURAL BRACE IS CONTACTING OIL TUBE SUPPORT BRACKET ON BOTH LEFT AND RIGHT SIDES. AREA OF DAMAGE IS BELOW AFT HOLD OPEN ROD MOUNT BRACKET. REMOVED DOUBLER AT COWL HOLD OPEN ROD AT I/B AND O/B COWLS AND DUPLICATED PER BOEING DRAWING. NSDR JR2R2011032700104Structure · crackedLT ENGINE UPPER TRANS COWL COAMING IS CRACKED. REMOVED AND REPLACED TRANS COWL COAMING IAW CRJ 900 SRM 51-42-13.SDR MASA2011032402231Acoustic Liner · damagedDAMAGE TO LEFT ENG FWD CORE COWL. HOLE IN INBOARD UPPER ACOUSTIC LINER. MX C/W REPAIR. MX REMOVED DAMAGE AND FILLED W/STRUCTURAL ADHESIVE IAW CRJ900 SRM 54-10-00.SDR JR2R2011031500089Fairing · crackedHINGE LINE FAIRING PNL 433BB CRACKED. FABRICATED NEW HINGE FAIRING PNL IAW CRJ 900 SRM 51-40-11.
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