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 DL72S000644Panel · missingFWD BLOW OUT PANEL ON RT SIDE OF NR 2 ENG COWL MISSING. REPLACED BLOW OUT PANEL, NO DUCT LEAKS NOTED ON ENG RUN.SDR 20000420AP001Cowling · damagedJFK - FLT 570 - DURING TAXIING GATE, ENG NR 2 INTAKE COWL BARREL AND RT ENG FAN COWL RE HIT BY A BELT LOADER. STAYED AT JFK FOR MX. PERFORMED INSPECTION THE FOLLOWING DAMAGE WAS FOUND: TWO CRACKS ON THE EXTERIOR LOWER SKIN OF THE ENG INTAKE COWL BARREL, AFT SDR CA000329024Cowl Door · separated(CAN) SHORTLY AFTER ROTATION LEFT ENGINE OUTBOARD FAN COWL DOOR ASSY DEPARTED. COWL APPEARS TO HAVE COME UNLATCHED AT THE LOWER EDGE CAUSING IT TO ROTATE UPWARDS AND BREAK OFF APPROX 24 INCHES FROM THE UPPER EDGE. INCIDENT UNDER INVESTIGATION BY SAFTEY BOARD.SDR QXEA0000781Structure · wornYYC- WEAR MARKS IN TOP AFT SURFACE AREA OF LEFT HAND ENGINE BOTTOM COWL AT FIREWALL LOCATION. REPAIRED IAW DHC-8 SRM 8-71-189.SDR CALA0000240Angle · crackedINSPECTION FOUND ANGLE CRACKED THROUGH LOWER ACCESS PANEL NR 7406 OF NR 2 ENGINE NOSE COWL. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5, AND 51-30-2.SDR DHL200072443CTube · crackedAT C CHECK, FOUND NR 2 ENGINE RT FWD COWL, END OF DRAIN TUBE AREA SHOW SKIN CRACKED. INSTALLED EXTERNAL DOUBLER REPAIR AT NR 2 ENGINE RT FWD COWL END OF DRAIN TUBE AREA PER SRM 54-10-3 FIG6. ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200072442CSkin · erodedFOUND DURING C CHECK, NR 2 ENGINE RT COWL, LOWER SKIN AFT MIDDLE SECTION IS ERODED. INSTALLED EXTERNAL DOUBLER REPAIR AT NR 2 ENGINE RT FWD COWL PER SRM 54-10-3 FIG 6. ALODINED AND PRIMED PER SRM 51-10-2SDR P2EA00040Cowling · damagedMSP - FLT 707 - NR 2 ENGINE RIGHT TAILPIPE COWLING DAMAGED BY FUEL TRUCK. REPLACED NR 2 ENGINE RIGHT TAILPIPE COWLING PER MM 71-11-11. (M)SDR 20000329SH043Latch · crackedCRACKS FORM AT THE BEND RADIUS OF THE LATCH ASSEMBLY WITHIN A FEW HOURS OF NORMAL OPERATION. SEVERAL ASSEMBLIES (6) HAVE FAILED IN THE SAME MANNER. THIS ASSY IS FORMED WITH A MUCH SMALLER BEND RADIUS AS COMPARED TO AN OLDER STYLE PIPER OEM LATCH ASSY.SDR HEEA065896Fitting · galledFITTING HAD GALLED THREADS.SDR MALA000130Cowling · failedDTW - FLT 3016 - COWLING ON RIGHT ENGINE APPEARS LOOSE IN FLIGHT, RETURNED TO DTW. MAINTENANCE REPLACED RIGHT FORWARD AND LEFT FORWARD ENGINE COWLINGS IAW AMM CH54A11 CHECKS GOOD AT THIS TIME. (M)SDR P2EA00021Angle · crackedSJO - DURING Q-CHECK, FOUND NR 2 ENGINE NOSE COWL AFT SECTION WALL ANGLE CRACKED A 7 O'CLOCK POSITION. FABRICATED ANGLE IAW SRM 51-20-01. REMOVED AND REPLACED IAW SRM 51-30-2. (M)SDR CALA0000082Cowl · crackedINSPECTION FOUND A 1 INCH CRACK IN INTERNAL DOUBLER STRAP OF NR 2 ENGINE NOSE COWL THROUGH ACCESS PANEL NR 7403 UPPER RT SIDE. THE NR 2 ENGINE NOSE COWL WAS REMOVED AND REPLACED IAW MM 71-10-01.SDR CA000209047Panel · missing(CAN) ON ARRIVAL FOUND RT ENG UPPER COWL OVERPRESSURE RELIEF PANEL MISSING. INSTALLED.SDR ASAA0010012Rib · wornSEA - DURING SCHEDULED C-CHECK, THE NR 2 ENGINE INBOARD COWL, 4TH RIB AFT, WAS FOUND WORN IN TWO PLACES. REPAIRED PER EA 5410-01044. (M)SDR DHL200071760DSkin · crackedAT D CK, NR 1 ENGINE AFT FIXED COWL HAS APROX 4 INCH CRACK AT FWD FRAME I/B FLANGE AT UPPER EDGE OF COWL. CUTOUT DAMAGED AREA PER B727 SRM 54-10-3 FIG 5. ACCOMPLISHED HFEC INSPECTION OF CUTOUT, VERIFIED CRACK REMOVED. INSTALLED REPAIR PER B727 SRM 54-10-3 FSDR DHL200071785DRib · chafedAT D-CK, NR 1 ENG, LOWER COWL HAS NR 5 RIB CHAFFING OIL FILTER HOUSING NUTS. REMOVED OLD REPAIR PER B727 SRM 54-10-3. INSTALLED DOUBLER REPAIR PER B727 SRM 54-10-3. REF: N/R 6543.SDR DHL200071778DRib · crackedAT D-CK, NR 3 ENG LWR COWL HAS NR 13 RIB RADIUS CRACKED AT 6:00 O'CLOCK POS. STOP DRILLED CRACK AT NR 13 RIB RADIUS PER B727 SRM 51-10-1. INSTALLED REPAIR ON NR 13 RIB OF NR 3 ENG COWL PER B727 SRM 54-10-3. REF: N/R 6560.SDR DHL200071761DSkin · crackedAT D-CK, NR 3 ENG UPPER COWL, HAS IMPROPER S/M REPAIR AT OUTBD NR 5 LATCH. REMOVED AND REPLACED REPAIR OUTBD OF NR 5 LATCH PER B727 SRM 54-10-3 FIG 6. REF: N/R 6566.SDR HEED065793Screen · crackedSCREEN CRACKED. REPLACED UNIT.SDR 20000420AP005Intake Duct · damagedSAL - FLT 390 - DURING TAKEOFF (SAL-TGU-SAP-MIA) A LARGE BIRD IMPACTED THE ENGINE NR 1, HOWEVER THE ENGINE PARAMETERS REMAINED NORMAL, DUE TO THIS SITUATION THE AIRCRAFT RETURNED TO EL SALVADOR STATION FOR MAINTENANCE. AT EL SALVADOR, MAINTENANCE TECHNICANS PSDR 2000ZZZX21Mount · tornDURING PHASE 2 INSPECTION, FOUND 4 LOWER COWL ATTACH SHOCK MOUNTS TORN AT THE BASE. LOCATED AT THE 2, 3, AND 4 O'CLOCK POSITIONS AND THE LOWER L. REPLACED SHOCK MOUNTS.SDR 2000ZZZX109Cover · crackedTHE LEFT NOSE COWL AIRLINE COVER (POCKET) FOR THE 14TH STAGE T/R PDU LINE SHOWS SIGNS OF HEAT DAMAGE AND IS BUCKLED AND CRACKED.SDR 2000ZZZX105Cover · crackedTHE LEFT AND RIGHT NOSE INLET COWL AIRLINE COVER (POCKET) FOR THE 14TH STAGE T/R PDV LINE SHOW SIGNS OF EXCESSIVE HEAT DAMAGE AND IS BUCKLED AND CRACKED.SDR 2000ZZZX104Cover · crackedTHE LEFT AND RIGHT NOSE INLET COWL AIRLINE COVER (POCKET) FOR THE 14TH STAGE T/R PDV LINE SHOW SIGNS OF EXCESSIVE HEAT DAMAGE AND IS BUCKLED AND CRACKED.SDR 2000ZZZX60Slip Joint · crackedPART WAS FOUND CRACKED 330 DEGREES AROUND WELD AND WAS VISIBLE BY OPENING THE OUTBOARD COWLING DOOR.SDR VNAA9912001Door · unlatchedDURING CLIMB, THE FLIGHT CREW FELT A VIBRATION ON THE LEFT SIDE. THE CREW TURNED ON THE WING LIGHT AND NOTICED THE LEFT ENGINE OUTBOARD COWLING FLAPPING IN FLIGHT. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE AT PIT INSPECTED ANDSDR CA991229073Latch · worn(CAN) COWL LATCH FOUND WEARING A HOLE IN THE LT ENGINE NR 1 CYLINDER VALVE COVER.SDR UPS99431161Cowl · damagedNR 3 ENGINE COWL DAMAGED ON INBOARD SIDE PUNCTURED. PERFORMED TEMP REPAIR PER EO AND DEFERRED INCIDENT RS99-409 DEFFERAL D182831.SDR UPS99831148Cowl · damagedINSPECTION TYPE:N/A, UPON LANDING NUMBER 3 AND 4 ENGINE COWLS CONTACTED RUNWAY. *S/D* REMOVED AND REPLACED NUMBER 3 AND 4 ENGINE AND DAMAGED FAN COWLS PER MM 71-10-02 AND TC 9071-1, 9071-2. PERFORMED ENGINE RUNS PER TC 9071-2 AND 9071- 3. REFER TO LOG PAGESDR CA991209050Bracket · broken(CAN) AIRCRAFT WAS ON FLIGHT FROM DAYTON TO OSHAWA. IN THE CLIMB THROUGH 6,500 FEET, THE LEFT COWL CAME FORWARD AT THE TOP 304 INCHES. THE CREW DECIDED TO RETURN TO DAYTON AND LANDED UNEVENTFULLY. TWO BRACKETS ON THE UPPER PART OF THE COWL WERE FOUND BROKENSDR CALA9901505Cowl · corrodedINSPECTION FOUND CORROSION ON INLET SKIN OF NR 2 NOSE COWL INSIDE FRONT ACCESS. THE NOSE COWL WAS REMOVED AND REPLACED IAW MM 71-10-01.SDR CALA9901480Angle · crackedINSPECTION FOUND NR 1 ENGINE INTAKE EXTERNAL SIDE AFT SUPPORT ANGLES(2) CRACKED. THE CRACKS WERE 1 LONG. THE SUPPORT ANGLES WERE REPLACED IAW SRM 51-30-00.SDR 20000622SH004Mount · tornFOUND, OF ELEVEN SHOCK MOUNTS ON THE AIRCRAFT, THREE TO BE DETERIORATED, ONE TORN 50 PERCENT THROUGH. SUBMITTER HAS WITNESSED AT LEAST 20 OF THESE J7444-36 MOUNTS TORN, ALL WITH LESS THAN 500 HOURS TT. ON THE NEW SERIES 172R AIRCRAFT, THE DASH 36 MOUNT IS MASDR 99T64R512EWACowl · damagedFOUND DURING D-CHECK. HOLE ON INSIDE OF LT FORWARD OF LT FORWARD COWL NR 1 ENGINE. CUT OUT DAMAGED AREA, FILLED WITH LY5052 02 RESIN AND HY5052 02 RESIN CATALYST AND MIRCO BALLONS. FABRICATED DOUBLER AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 10SDR 20000622SH006Pan · crackedDURING AN ANNUAL INSPECTION, THE PN 002-410014-3 ''PAN'', LOCATED AT THE FORWARD NOSE COWLING AREA, BELOW THE ENGINE CRANKSHAFT FLANGE, AND ABOVE THE AIR FILTER, HAD LARGE CRACKS WITH A PIECE MISSING APPROXIMATELY 2 INCH BY 4 INCH. SUBMITTER SUSPECTED SOME TYSDR RRXA991522Cowl · separatedON POST FLIGHT, NOTED NR 1 ENGINE COWLINGS MISSING AND DAMAGE TO UNDERSIDE OF WING. REPAIRED PYLON IAW COTNEY EA NR EAJ47-1, REPAIRED WING IAW EAJ47-1.SDR DHL9974223CCowl · misrepairedAT C-CHECK, NR 1 ENGINE NOSE COWL HAS IMPROPER REPAIR TO SKIN EDGE AT FRAME APPROX NAC STA99. REMOVED OLD REPAIR. INSTALLED DOUBLER PER SRM 51-40-2, 4 BY 7.5, N/R 6680.SDR DHL9974222CCowl · puncturedAT C CHECK, NR 1 NOSE COWL HAS SMALL PUNCTURES IN SKIN AT FRAME APPROX NAC STA 92. CUT OUT DAMAGED AREA. INSTALLED DOUBLER 4 BY 8 PER SRM 54-30-3. N/R 6679.SDR DHL9974217CCowl · crackedAT C CHECK, NR 3 ENG NOSE COWL AFT WEB CRACKED OUT. INSTALLED WEB REPAIR PER SRM 51-40-2, 27 BY 6, N/R 6671.SDR DHL9974216CCowl · crackedAT C CHECK, NR 1 ENGINE UPPER COWL PANEL REPAIR DOUBLER AT FWD INBD CORNER IS CRACKED. REPLACED DOUBLER AT CORNER PER SRM 54-30-3, 14 BY 6, N/R 6668.SDR DHL9974213CCowl · crackedAT C-CHECK, NR 1 ENGINE NOSE COWL AFT EDGE OF COWL SKIN IS BENT AND PULLED LOOSE FROM RIVET HEAD AND SKIN FLUSH REPAIR NOT FITTED PROPERLY. REMOVED FLUSH REPAIR, CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 51-30-2 11.5 BY 5, N/R 6641.SDR DHL9974211CFrame · damagedAT C CHECK, NR 3 ENGINE LOWER COWL, HORIZONTAL FRAME DAMAGED INBD SIDE 27 AFT FOF FWD EDGE. REMOVED AND REPLACED DAMAGED FRAME PER SRM 1-10-2, N/R 6634.SDR DHL9974214CCowl · crackedAT C CHECK, NR 3 ENGINE INLET COWL OUTER SKIN CRACKED AT FASTENER AT 1 O'CLOCK APPROX 6 AFT OF LEADING EDGE. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 54-30-3, 10 BY 2, N/R 6624.SDR DHL9974204CCowl · damagedAT C CHECK, NR 4 ENGINE INLET COWL OUTER SKIN DAMAGED ALONG TRAILING EDGE AT 4 O' CLOCK. CUT OUT DAMAGED AREA. INSTALLED DOUBLER REPAIR PER SRM 54-30-3, 8.25 BY 4.75, N/R 6625.SDR PLGA990921ACowl · damagedBOS - FLT 4859 - SHORTLY AFTER TAKEOFF, CREW NOTED THE LEFT INBOARD ENGINE COWLING OPENED IN-FLIGHT. CREW RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE COWLING ASSEMBLY AND CHECKED FIT AND SECURITY, ALL CHECKS GOOD. AIRCRAFT RETURNEDSDR DL72S992079Skin · cracked5 INCH CRACK NR 2 ENG INLET OUTER SKIN BELOW DOUBLER AT 3:00 POSITION. REPAIRED PER MM 54-30-0 P 801.SDR CALA9901245Cowl · crackedINSPECTION FOUND A 12 CRACK IN NR 2 ENGINE INLET HOUSING INTERNAL LOWER AFT WALL. THE NR 2 ENGINE NOSE COWL WAS REMOVED AND REPLACED IAW MM 71-10-01.SDR AU991005Panel · separated(AUS) LEFT ENGINE NOSE COWL ANTI-ICE PANEL LOCATED AT THE 12 O'CLOCK POSITION SEPARATED FROM THE ENGINE. THE AIRCRAFT HAD JUST COMPLETED A C-CHECK.SDR 99ZZZM681Skin · damagedNR 3 ENGINE COWL UPPER HALF INBOARD SECTION BY NR 1, NR 2, AND NR 3 LATCH RECEPTICALS DAMGED SKIN. REPAIRED DAMAGED SKIN IAW SRM 51-10-1. FABRICATED DOUBLER IAW RM 53-10-4. INSTALLED DOUBLER IAW SRM 53-10-4. (M)
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