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 IPXA2019092747310Cowling · damagedINSPECTION TYPE:4C#2 ENG. INLET COWL HAS NUMEROUS LOOSE RIVETS.REPAIRED #2 ENG. INLET COWL IAW VT-SAA EA 011-7110-01-A7896 REV. I/R AND UPS EO MD--17110-55725-C. (MINOR)SDR UIEA2019081905226Skin · worn#1 ENG LT CORE COWL EXTERIOR AREA, AFT EDGE RIVET FOUND WORN. #1 ENG LT CORE COWL EXTERIOR SKIN REPAIRED IAW RI 71-11-13699 REV A.SDR IPXA2019091846952Hinge Fitting · chafedINSPECTION TYPE:12YR #2 ENGINE RT FAN COWL AFT HINGE FITTING IS CHAFED. REPAIRED CHAFED #2 ENGINE RT FAN COWL AFT HINGE FITTING IAW EA 300-7110-01-A7891 REV IR AND EO A300-7110-73917-A. (MINOR) LP 181477/2.SDR IPXA2019091446751Hinge Fitting · chafedINSPECTION TYPE:12YR #1 ENGINE I/B FAN COWL AFT HINGE FITTING IS CHAFED. REPAIRED CHAFED #1 ENGINE I/B FAN COWL AFT HINGE FITTING IAW EA 300-7110-01-A7889 REV IR AND EO A300-7110-73916-A. (MINOR)SDR CA190812009Inlet · cracked(CAN) DESCRIPTION: DURING AN HMV INSPECTION (737-345-70-842-01-01) A CRACK WAS FOUND AT THE 6 O`CLOCK POSITION OF THE @2 INLET COWL. REPLACING PART (TC# 20190812009)SDR UIEA2019072504850Rod · damaged#1 ENGINE INBD FAN COWLING FWD HOLD OPEN ROD DAMAGED. (<P>REMOVED AND REPLACED ENGINE #1 INBD FAN COWLING HOLD OPEN ROD AS PER AMM 70-10-00.</P>)SDR JGVR20190725001Acoustic Panel · debondedFOUND AREA OF ACOUSTIC PANEL AT THE 7 O'CLOCK POSITION ON THE #1 ENGINE INLET DISBONDED. REBONDED ARE PER ENGINEERING WORD ORDER.SDR REXA2019071701140Fairing · corrodedLATE FINDING: WORN OUT LT ENGINE LOWER HNGE-LINE FAIRING 433BB. SUMMARY: SKIN OF LT ENGINE LOWER HINGE-LINE FAIRING 433BB. WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR. 6. C. AND SRM 51-42-10-001-001-A01 PAR. 8. C.SDR IPXA2019071944621Fastener · looseINSPECTION TYPE:4C #2 ENG. INLET ASSY HAS 2 LOOSE FASTENERS AT THE 9:30 O'CLOCK POS. REPAIRED #2 ENG. INLET ASSY IAW EA 011-7110-01-A7840 REV. I/R AND EO MD11-7110-73270-A. (MINOR)SDR SWAA2022031107763Support Bracket · crackedLEFT ENGINE I/B FAN COWL; SUPPORT BRACKET AFT OF OIL SERVICE DOOR IS CRACKED. / REMOVED SUPPORT BRACKET AFT OF OIL SERVICE DOOR ON L/H ENGINE I/B FAN COWL. VERIFIED PART AS P/N 314-2259-4; LOCATE AND DRILLED NEW PART; INSTALLED SUPPORT BRACKET AFT OF OIL SERVISDR IPXA2019072544879Hinge · chafedINSPECTION TYPE:4C #3 O/B FAN COWL AFT HINGE AIRCRAFT SIDE IS CHAFED. REPAIRED CHAFED #3 O/B FAN COWL HINGE AIRCRAFT SIDE IAW EA 011-5440-01-A7839 REV. IR AND EO MD11-5440-73276-A. (MINOR).SDR IPXA2019070243991Skin · puncturedINSPECTION TYPE:N/A **SUPPLEMENTAL SDR** #2 ENG FAN COWL INBD HAS 3 PUNCTURES TO THE INNER SKIN. ACCOMPLISHED TEMP REPAIR PER EO A300-7110-73121-A. REPEAT INSP EVERY 30 DAYS, PERM REPAIR IN 90 DAYS. D-675419 CREATED. REPLACED #2 ENGINE UI/B FAN COWL IAW AMM 7SDR UIEA2019070104643Fairing · delaminated#2 ENG STRUT FAIRING I/B SIDE PERMANENT REPAIR IS DELAMINATED ON INTERIOR SURFACE, VIEWED THRU ACCESS DOOR #447BL AREAS MARKED.(<P>REPAIRED #2 ENGINE STRUT FAIRING I/B SIDE, P.N. 313T3381-1 IAW SRM 51-70-10-2R-0.<BR /></P>)SDR 2019F00228Cowling · chafedLH ENGINE UPPER COWL CHAFE. REFERENCE MANUFACTURER DOCUMENT S-750-ATA51/01RD REV. A. AND ENGINEERING MEMO DQW21934M1SDR IPXA2019071044289Rivet · looseINSPECTION TYPE:4C #2 ENG. INLET ASSY HAS 1 LOOSE RIVET AT 8:30 POS. REPAIRED #2 ENG. INLET ASSY IAW EA 011-7110-01-A7829 REV. I/R AND EO MD11-7110-73153-A. (MINOR)SDR REXA2019061601002Access Panel · crackedLT ENGINE LOWER PCU ACCESS PANEL 432AC IS SUSPECTED TO BE CRACKED. REMOVED AND REPLACED LOUVERS ON PANEL 432AC IAW CMM 20-42-10. APPLIED FINISH COAT IAW CMM 20-25-16.SDR SWAA2022031066706Angle · cracked#1 ENG O/B T/R LARGE ANGLE NEAR TOP AFT SIDE CRACKED. / :REPLACED BRACKET REF SRM 51-40-02SDR REXA2019060701020Cowling · crackedLT ENG UPPER CORE COWL INBD LE IS CRACKED. REPAIRED LT UPPER CORE COWL INBD LE IAW CMM 71-12-01.SDR DALA201907804074Skin · erodedPD: UPPER V-GROOVE WORN; LOWER SKIN L/E EROSION; BLOW OUT DOOR HINGES WORN; ACOUSTIC PANEL DENTED; TAI TUBE SEAL WORN AT FWD BULKHEAD; PROBE BONDING STRAP IN POOR CONDITION. CA: REPAIRED PER ERA 417433-14MA, REV B; C/W SRM 51-70-03 PARA. 5.0 FIG. 23; REPLACEDSDR IPXA2019063043919Latch · corrodedINSPECTION TYPE:12YR #2 ENG O/B AND I/B FAN COWLS LATCHING PLATES HAS FRETTING CORROSION. REMOVED AND REPLACED PER PW CMM 71-13-07.SDR REXA201906120861Skin · gouged445AB OUTER SKIN GOUGED AT LATTCHES. REMOVED GOUGED DOUBLER AND REPLACED WITH NEW FABRICATED DOUBLER I.A.W. CRJ-200 CMM 71-12-01.SDR DALA2019053103331Nose Cowl · dentedON WAKEUP CK FOUND #2 ENG LARGE DENT APPOX 3" LONG AND .250" DEEP IN NOSE COWLING AT 4 O'CLOCK POS. REMOVED #2 ENG NOSE COWL PER AMM 71-10-01 INSTALLED #2 ENG NOSE COWL PER AMM 71-10-01. COWL, NOSE, LT OFF 88-7110-9-0001 02236 ON 88-7110-9-0001 49422. (LP62537SDR SWIA2019070246015Cowling · dentedDENT LOCATED ON LEFT ENGINE LOWER FAN COWL AT 5 OCLOCK. (C-CHECK) RO: 06/28/2019 DRESSED BACK DENT ON LT ENGINE LOWER FAN COWL AT 5 OCLOCK POSITION IAW REO.SDR FXGA201905211975Nose Cowl · crackedRIGHT ENGINE NOSE COWL INLET LE RING HAS CRACK @ THE 9 O'CLOCK POSITION. TO CUT OUT AND REPAIR DAMAGED RT ENGINE NOSE COWL INLET LE RING. TO CUT OUT AND REPAIR DMAMAGED RT ENGINE NOSE COWL INLET LE RING IAW SRM 54-04A FIGURE 5.SDR UIEA2019052204268Cowling · cracked#3 ENGINE LT CORE COWL, INNER WALL AFT FRAME, FOUND CRACK AT 7:30 O' CLOCK POSITION. (<P>#3 ENG LT CORE COWL, INNER WALL AFT FRAME, CRACK AREAS REPAIRED IAW EO:1971A210 REV. 0.</P>)SDR DALA2019052103112Access Panel · missingFOUND ON ARRIVAL #1 ENG UPPER COWLING MISSING ACCESS PANEL. I/B SIDE JUST AFT OF NOSE COWL. INSTALLED #1 ENG INBD PANEL. (LP5564856)SDR DALA2019051503017Cowling · dentedNR 1 ENG. NOSE COWL LIP HAS DENT AT APPROX. 2 O'CLOCK POSITION. REPLACED NR 1 ENGINE NOSE COWL, REF AMM 71-10-01. COWL, NOSE, LT OFF 88-7110-9-0001 99491 ON 88-7110-9-0001 00084. (LP1074461)SDR CALA2019051300762Cowling · peelingPIECE OF ENGINE COWLING NR 1 ENGINE IS PEELED BACK INTO AIR STREAM. ON RIGHT OF PYLON ADDED PARTS NEEDED INFO TAPED SECURED PANEL STOPPED DRILL CRACK. INSPECT AFTER EACH FLIGHT FOR TAPE BEING SECURED. MUST BE REPLACED WITHIN 50 HOURS. INTERIM REPAIR ACCOMPLISHSDR REXA2019050500710Ring · chafedPANEL RACK. LEFT ENGINE CORE COWL PANEL TRAILING EDGE RUB STRIP WORN. REMOVED AND REPLACED CLOSER RING AND RUB STRIP IAW CMM 71-12-01 TASK 71-12-01-300-820-A01.SDR REXA2019042800707Panel · damagedPANEL RACK. LEFT ENGINE COWL PANEL 432-AT TRAILING EDGE KNIFE EDGED. REMOVED AND REPLACED TRAILING EDGE ON PANEL 432AT IAW CMM 71-14-01.SDR IPXA2019051942249Frame · crackedINSPECTION TYPE:4C NR 3 O/B T/R CORE COWL INNER HOUSING IS CRACKED AT THE 12 O'CLOCK POS. ON AFT RIB (FRAME). REMOVED AND REPLACED CRACKED AFT RIB (FRAME) ON NR 3 O/B T/R CORE COWL AT 12 O'CLOCK POS. IAW SRM 54-05-41. (MINOR)SDR IPXA2019051542157Cowling · chafedINSPECTION TYPE:4C NR 1 ENG. RT FAN COWL HAS CHAFE DAMAGE ON THE UPPER FWD. DOOR HINGE FITTING.REPAIRED CHAFED RT FAN COWL FWD. HINGE IAW EA 011-7110-01-A7766 REV. I/R AND EO MD11-7110-72596-A. (MINOR)SDR 2019F00192Cowl Door · crackedREPAIR OF RH LOWER COWL DOOR CRACK. AVIATION REPAIR LETTER DQ19319M1.SDR REXA2019042400676Rub Strip · chafedLT LOWER CORE COWL LIP IS CHAFED. REMOVED AND REPLACED GWI LIP AND RUBSTRIP IAW CMM 71-12-01.SDR REXA2019042200668Rub Strip · chafedRT UPPER NOSE ACCESS COWL TRAILING EDGE HAS CHAFING DAMAGE. REMOVED AND REPLACED NOSE ACCESS COWL T/E (RUB-STRIP) IAWCMM 71-14-01.SDR CALA2019042200637Seal · damagedPDA 3 RIGHT ENG INBD FAN COWL STRAKE SEAL LEADING EDGE ERODED AND HAS OPEN GAP INTO THE AIRSTREAM. REMOVED AND REPLACED NR 2 ENG VORTEX CONTROL DEVICE PER AMM 71-11-08.SDR SWAA2022030827311None · elongated# 1 ENGINE; INLET COWL; ACCESS PANEL AT 6 O'CLOCK; FASTENER HOLES ELONGATED (2 EA) / OBTAINED; LOCATED; DRILLED; ALODINED; PRIMED; AND TOP COATED NEW PANEL FOR #1 ENGINE INLET COWL 6 O'CLOCK POS REF B737 SRM 561-40-05 TABLE B; 51-20-01 PARA 5.A.(6).; SOPM 20-4SDR IPXA2019032440417Hinge · chafedINSPECTION TYPE:2C NR 1 ENG OTBD FAN COWL FWD HINGE IS CHAFED. ACCOMPLISHED REPAIR ON NR 1 ENG OTBD FAN COWL FWD HINGE PER EA# 011-7110-01-A7658 I/R AND EO MD-11-7110-72001-A.SDR UIEA2019032203648Nose Cowl · dentedNR 2 NOSE COWL HAS INTERNAL DENTS 5-7 O'CLOCK (<P>REPAIRED NR 2 NOSE COWL (6 DENST) AT INTERNAL POSITION 5-7 IAW AMM SRM 54-15-01-2R REP 3 PAR 3</P>)SDR UIEA2019032203641Latch · brokenNR 2 ENG OB CORE COWL PRESS RELIEF DOOR LWR BROKEN. (<P>R/R LATCH ON THE NR 2 ENG O/B CORE COWL PRESS RELIEF DOOR IAW SRM 51-40-02</P>)SDR UIEA2019032203640Bearing · wornNR 2 ENG LT CORE COWL HOLD OPEN ROD ATTACH BEARING WORN. (<P>REPLACED NR 2 ENG LT CORE COWL HOLD OPEN ROD END BEARING IAW SRM 51-40-02. NO ADJUSTMENT DISTURBED.</P>)SDR UIEA2019032203639Bearing · wornNR 2 ENG BEARING RT CORE COWL HOLD OPEN ROD ATTACH BEARING WORN. (<P>REPLACED NR 2 ENG CORE COWL HOLD OPEN ROD END BEARING IAW AMM 51-40-02. NO ADJUSTMENTS DISTURBED.</P>)SDR UIEA2019032203637Latch · crackedNR 1 ENG I/B CORE COWL FWD LATCH HAS A CRACK (<P>REPAIRE FWD LATCH ON THE NR 1 ENG CORE COWL IAW SRM 54-42-01-2R-7</P>)SDR UIEA2019032203630Hinge · looseNR 2 ENG RT CORE COWL PRESS RELIEF DOOR FITS LOOSE WHEN FULLY CLOSED (<P>REPLACED UPPER AND LOWER HINGES ON PREE RELIEF DOOR IAW SRM 51-40-02</P>)SDR UIEA2019032203627Seal · tornNR 1 ENG I/B FAN COWL, LOWER SEAL TORN. (<P>R/R AND REPLACED SEAL IAW AMM 20-10-23.</P>)SDR UIEA2019031503546Skin · crackedNR 2 ENG RT CORE COWL HAS AN EXTERNAL SKIN CRACK WHICH WAS FOUND JUST BELOW THE EXHAUST GRILL AREA.(<P>REPAIRED NR 2 ENG RT CORE COWL EXTERNAL SKIN CRACK AREAS IAW CV19-02154 AND RI-54-45-13424.</P>)SDR UIEA2019031403541Cowling · damagedACOUSTIC LINER RT ENGINE 5 O'CLOCK ABRADEABLE MATERIAL MISSING 1/8 INCH DIAM(<P>REMOVED & REPLACED NR 2 ENG NOSE COWLING ASSY IAW AMM 71-11-01-404-005-H00, OPS CK GOOD</P>)SDR A8ZR20190301001Cowling · separatedTHE AIRCRAFT NR 1 POWERPLANT OUTBOARD CORE COWL SEPARATED UPON THE TAKEOFF PHASE OF FLIGHT. THE PILOTS NOTICED A ABNORMAL VIBRATION AFTER V1 SPEED AND RETURNED TO THE DEPARTURE AIRPORT. DAMAGE WAS SUSTAINED TO THE NACELLE COWL AREA, THE POWERPLANT AND FLAP SYSSDR REXA2019022600268Seal · wornRT ENG LWR NOSE COWL TE IS KNIFE EDGED. REMOVED/REPLACED NOSE COWL T/E IAW CMM 71-14-01.SDR DALA201905302786Fastener · loosePD: PCW LIPSKIN REPAIR HAS MULTIPLE LOOSE FASTENERS. CA: REPLACED LOOSE RIVETS ON LIPSKIN REPAIR REF SRM 54-10-00 REPAIR 5 REV 59. THE WORK SPECIFIED IN BLOCK(S) 11/12 ACCOMPLISHED REF OEM CMM 71-11-07 REV 68 W/APPLICABLE SUP. INFO DAL REV 43 PUB # 04018. REP
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