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 U2RA2022072800031Cowling · wornWEAR DAMAGE WAS FOUND ON NO.3 ENG RH CORE COWL (P/N:224M4761-539, S/N: 1099) FWD FRAME EXISTING REPAIR. THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, LNC'S ENGINEERING ORDER 22089-7, REV LR, WHICH WAS APPROVED BY FASDR U2RA2022072800027Cowling · dentedIT WAS DISCOVERED (3 EA.) ELONGATED FASTENER HOLES IN THE OUTER SKIN OF THE RIGHT CORE COWL (P/N 224-2302-545, S/N 0619) CURRENTLY INSTALLED ON AIRCRAFT N919CA LOCATED AT APPROXIMATE NAS STA. 307.00, THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLISDR SWAA2022072222991Web · crackedCRACK ON WEB INBOARD FAN COWL LOC.INTERNAL AREA ACCESS DOOR 414AR ON ENGINE 1 2022-382902. / [01] INSTALLED WEB AND FASTENERS LOC INBOARD FAN COWL LOC.INTERNAL AREA ACCESS DOOR 414AR ON ENGINE 1 IAW B737-700 SRM 51-40-02 . SEE INDIVIDUAL SIGN OFFS BELOW.;[02] SDR SWAA2022071222206Bracket · cracked#2 ENGINE O/B FAN COWL OIL ACCESS DOOR CLOSE-OUT FRAME BRACKET IS CRACKED / [01] REMOVED #2 ENGINE O/B FAN COWL OIL ACCESS DOOR CLOSE-OUT FRAME BRACKET. POSITIONED NEW BRACKET - DRILLED UP PILOT HOELES TO FINAL SIZE; AND INSTALLED FASTENERS IAW CMM 71-13-30; SSDR U2RA2022061700020None · noneGROUND EQUIPMENT DAMAGE TO NUMBER 1 ENGINE INLET COWLING - ACCOMPLISHED TIME LIMITED MAJOR REPAIR OF COWLING PER FLIGHT VEHICLES CONSULTING, INC ENGINEERING ORDER 220092-1 REVISION IR DATED 6/14/2022.SDR VNAA202208279999Cowling · wornWEAR (2 EAS) ON LOWER COWLING OF LH ENGINE. (MOT1)SDR REXA2022070501463Latch · chafedRH UPPER TRANSCOWL LATCH COAMING HAS CHAFING WITH 100% MATERIAL LOSS. REMOVED AND REPLACED RH UPPER TRANSCOWL LATCH COAMINGSDR REXA2022070501462Latch · chafedRH LOWER TRANSCOWL LATCH COAMING HAS CHAFED AREA WITH 100% MATERIAL LOSS REPLACED RH LOWER TRANSCOWL LATCH COAMING.SDR REXA2022070501461Latch · chafedLH UPPER TRANSCOWL LATCH COAMING HAS CHAFED AREA WITH 100% MATERIAL LOSS REPLACED LH UPPER TRANSCOWL LATCH COAMING.SDR UIEA2022052200496Skin · cracked#4 ENG R/H CORE COWL LWR AREA OF AIR EXHAUST FOUND 2EA BOLT HOLE CRACKED SKIN 2EA BOLT HOLE CRACK AREA REPAIRED AS PER SRM 54-45-01-2R-4 REPAIR 4 FIG 201</P>)SDR REXA2022060201044Fairing · crackedRH ENGINE UPPER COWL HINGE LINE FAIRING 443BT CRACKED PERFORMED REPAIR ON RH ENGINE UPPER COWL HINGE LINE FAIRING PER EA CRJ954-12492 REV D DATED 05/24/2022SDR AALA202205266736Cowling · damagedAIRCRAFT WAS GROUNDED: BIRD STRIKE IN NUMBER 2 ENGINE. EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO BZN. PERFORMED BIRD STRIKE INSPECTION AS PER AMM 05-51-18-201 ONLY NOTED DAMAGE WAS NUMBER 2 ENGINE FAN BLADES. **SUPPLEMENTAL REPORT FOR AALA202205193421: RSDR MK1Y20220515006None · usedDURING MAINTENENCE INSPECTION FOUND DAMAGEON #1 ENGINE RIGHT CORE COL PRECOOLER EXIT DUCT UPPER SIDE (DEEP GROOVES, HOLE AND WORNAREA)SDR MK1Y20220515005Duct · damagedDURING MAINTENENCE INSPECTION FOUND DAMAGE ON #2 ENGINE RIGHT CORE COWL PRECOOLER EXIT DUCT UPPER SIDE (DEEP GROOVES, HOLE AND WORNAREA)SDR UIEA2022051400468Rod · unserviceable#2 ENGINE I/B CORE COWL HOLD OPEN STRUT DOES NOT LOCK IN OPEN POSITION. REMOVED AND REPLACED #2 ENG I/B CORE COWL HOLD OPEN ROD STRUT IAW B763 AMM 20-11-00SDR UIEA2022051400469Cowling · installedENGINE #1 REINSTALL ALL ENGINE COWLS DUE TO ENGINE CHANGE CANCELATION. INSTALL INLET COWL ON ENGINE #1 AS PER B767-300 AMM 71-11-01. INSTALLED FAN COWL ( LEFT RIGHT ) ON ENGINE # AS PER B767-300 AMM 71-11-04. INSTALLED LEFT AND RIGHT CORE COWLS ON ENGINSDR REXA2022070501430Transcowl · crackedRH ENGINE LOWER TRANSCOWL HAS 2 EA. CRACKS ON THE INNER SKIN, WITH A MAX LENGTH OF .75". REPAIRED RH LOWER TRANSCOWL PER EA CRJ954-13806.SDR REXA2022070501429Latch · crackedLH LOWER TRANSCOWL LATCH COAMING CHAFED. 3.0" X .40" X 100% REPLACED LH LOWER TRANSCOWL LATCH COAMING.SDR SWAA2022052306715Web · cracked#1 ENGINE I/B FAN COWL OIL SERVIDE DOOR SPLASH WEB CRACKED / [01] INFO: PROBABLY A DUPLICATE DISCREPANCY. SEE ALSO FAULT TTG8Q00C79ZG;[02] REMOVED AND REPLACED PER SRM 51-40-02.<BR> DUPLICATE WRITE UP ON #1 ENG. I/B FAN COWL SUPPORT ANGLE IS CRACK AT UPPER EDGSDR SWAA2022053110250Bracket · brokenBROKEN SUPPORT BRACKET LOC. FAN CASE AT 6 OCLOCK ON ENGINE 2 2022-228510 / [01] REPLACED SUPPORT BRACKET LOC. FAN CASE AT 6 OCLOCK ON ENGINE 2 I.A.W B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPPORT BRACKET LOC. FAN CASE AT 6 OCLOCK ONSDR IXXA2022050302Cowling · chafedLOWER CLOSE OUT CHANNEL CHAFED IN MULTI AREAS WHERE STOP PADS MATE UP ON #1 ENGINE O/B CORE COWL LOWER ENDSDR IXXA2022050301None · cracked#1 ENGINE I/B CORE COWL UPPER LOUVER EXHAUST ON AFT FLANGE CRACKEDSDR SWAA2022053107246Angle · crackedCRACK ANGLE INBOARD FAN COWL LOC. INTERNAL AREA IDG SERVICE DOOR ON ENGINE 2 (1 EA) 2022-228463. / [01] REPLACED NEW ANGLE INBOARD FAN COWL LOC. INTERNAL AREA IDG SERVICE DOOR ON ENGINE 2 IAW B737-700 SRM 51-10-02 ITEM 9 AND CMM <BR>71-13-30;[02] TASK COMPLETESDR SWAA2022052306714Support Angle · cracked#1 ENG. I/B FAN COWL SUPPORT ANGLE IS CRACK AT UPPER EDGE; ANGLE IS ON AFT SIDE OF OIL ACCESS DOOR OPENING. MRKD / [01] INFO: PROBABLY A DUPLICATE DISCREPANCY. SEE ALSO FAULT TTG8Q00C9UGE;[02] REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-40-02.;[03] REMOVED ASDR MK1Y20220429005None · noneENGINE # 1 LH CORE COWL HAT FRAME NAC STA 303.75, MID LOWER AREA: DURING THE MAINTENANCE INSPECTION AT IAI, A 1.2 INCH CRACK WAS FOUND ON THE ENG # 1 L/H CORE COWL AFT HAT FRAME P/N 224-2318. THE AFT HAT FRAME FALLS UNDER ZONE CC2 AS PER TABLE 101 B767-300 SRMSDR REXA2022062801408Latch · wornRH LOWER FWD CORE COWL BLOW OFF DOOR 444CB LATCH PLATE WORN WITH 100% MATERIAL LOSS. REPLACED RH LOWER FWD CORE COWL LATCH LATESDR REXA2022062801407Latch · wornRH UPPER FWD CORE COWL BLOW OFF DOOR 444CT LATCH PLATE WORN WITH 100% MATERIAL LOSS. REPLACED RH UPPER FWD CORE COWL LATCH PLATESDR 4DPA2022041900001Service Panel · bentCREW FELT A SUDDEN YAW LEFT MOTION AT CRUISE FL310. THE AMOUNT OF DRAG WAS TOO MUCH TO MAINTAIN CRUISE SPEED. CREW DECLARED AN EMERGENCY AND ELECTED TO DIVERT TO LAX. UPON INSPECTION AFTER LANDING PANEL 414CB HAD SEPARATED HALFWAY CAUSING THE DRAG AND YAWING. SDR DALA2022042002760Access Door · missingSHIP 3219 ON ARRIVAL FOUND RT ENG STARTER VALVE ACCESS DOOR MISSING. CORRECTIVE ACTION: REPLACED DOOR PER A320 AMM 71-13. OK FOR SERVICE. (6183530)SDR IXXA2022060306Web · cracked#2 OB CORE COWL INNER WEB CRACKEDSDR 2022F00188Cowling · missingR/H UPPER COWLING AFT INBOARD LATCH PIN BROKEN. ACCOMPLISHED NJA RFTS-106244 REV. 0 DATE: 14APR2022; N801QS (700-0023) COWL LATCH PIN MISSING. PERMANENT REPAIR REQUIRED WITHIN 30 CALENDAR DAYS, ON OR BEFORE 14MAY2022.SDR SWAA2022051800587Rod · looseLOOSE HOLD OPEN ROD OUTBOARD FAN COWL SUPPORT BRACKET AFT POSITION LT ENGINE 2022-204200 / [01] REPLACED HOLD OPEN ROD OUTBOARD FAN COWL SUPPORT BRACKET AFT POSITION LT ENGINE IAW SRM 51-40-02-0G-0;[02] TASK COMPLETEDSDR REXA2022050900820None · wornRH ENGINE LOWER CORE COWL RUB STRIP HAS HEAVY WEAR REMOVED WORN RH ENG. LOWER CORE COWL RUB STRIP AND REPLACED WITH NEW RUB STRIP PER EA CRJ954-13184 REV A DATED: 4/5/2022.SDR SWAA2022050293431Plate · crackedCRACK INBOARD FAN COWL PLATE ON INTERNAL AREA ON ENGINE 1 2022-192554 / [01] REPLACED PLATE LOC. INBOARD FAN COWL INTERNAL AREA ON ENGINE 1. IAW B737-700 SRM 51-40-02-0G-0 AND 51-10-02 ITEM (9. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] CORRECTED STEP 1: REPLACED PLASDR IPXA2022033180702None · noneINSPECTION TYPE:NA#2 ENG RIGHT FAN COWL HAS PUNCTURE ON INNER SKIN FWD EDGE 46" FROM LWR EDGEA NEW #2 OUTBD FAN COWL WAS INSTALLED ON LOGPAGE 140560 ITEM 2, P/N 221-0302-521 S/N 1024001. THIS CLEARS DEFERRAL D768680SDR DALA2022040102220None · noneSHIP 5810 INSPECTION REQUIRED ON THE DRAGGED ENGINE NACELLE/ENGINE SEIZURE AND STRUT DAMAGE CONDITION. AND HARD LANDING ON HIGH DRAG 1 SIDE LANDING CONDITION. CORRECTIVE ACTION: PERFORMED INSPECTION PER B757 AMM 05-51 AND 05-51. NO DISCREPANCY FOUND ON PYLON, SDR 2022F00169Cowling · erodedLH ENGINE LOWER COWL HAS AN AREA DELAMINATED ALONG THE LEADING EDGE. THE REPAIR WAS DEEMED MINOR IN SCOPE. REPAIRED PER TEXTRON AVIATION ENGINEERING MEMO DQ34060M1 DATED MAR 21, 2022.SDR VNAA202203269913Channel · chafedRH ENGINE LOWER FAN COWL FORWARD EDGE HAS TWO CHAFES.SDR 2022F00157None · gougedR/H UPPER COWL GOUGED BY O/B BLEED AIR CLAMP AT AFT BLEED AIR COUPLING. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ34079M1. DATED. MARCH 22, 2022. 680A-0138 (N582QS) ENGINE UPPER COWL (LEFT AND RIGHT) DAMAGE (GOUGE).SDR 2022F00151None · gougedL/H UPPER COWL GOUGED BY O/B BLEED AIR CLAMP AT AFT BLEED AIR COUPLING. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ34079M1, DATED. MARCH 22,2022. 680A-0138 (N582QS) ENGINE UPPER COWL (LEFT AND RIGHT) DAMAGE (GOUGE).SDR YENA2022032100293None · noneFLT#890, SJU-EWR. 'AFTER DESENT AND LEVEL AT 10000FT STRONG ODOR/FUMES SMELL IN COCKPIT AND CABIN SMELL CHARACTERIZED AS BURNING ALCOHOL AND WAS RECOGNIZED BY ENTIRE CREW. APPEARS TO DISSAPATE AFTER 30 MINUTES. BETTER WITH PACK ONE OFF; PERFORMED ENG 1 AND 2 LSDR SWAA2022041183643Cowling · corroded#2 ENGINE I/B FAN COWL HAS HEAVY CORROSION LOWER FWD AREA. / [01] REPLACED #2 ENGINE I/B FAN COWL WITH SERVICEABLE FAN COWL FOR COMPANY CONVENIENCE DUE TO CORROSION. FAN COWL TO BE INSTALLED ON CARD #TTG8Q00B99TS LINE #1322.;[02] MY NAME INTERRED IN STEPS 2;3 SDR A6WA202203138129Cowling · damagedREF 334833/1 DAMAGE FOUND ON RH ENG INLET COWL. AIRCRAFT REQUIRES INSPECTION FOR FURTHER DAMAGE. *** AIRCRAFT REMOVED FROM SERVICE *** PERV GVI OF NOSE AREA FOR BIRD STRIKE DAMAGE NO DEFECTS NOTED NO EVDIENCE OF ENG INJSETION IAW AMM 05-51-25-210-801. AC OK SDR DALA2022031401626Cowling · missing(LOG 6822888) AFTER LANDING AND DEPLOYMENT OF THE THRUST REVERSERS. TOWER REPORTED AN PART OF THE LEFT ENGINE COWLING DEPARTED THE AIRCRAFT. R/R ENG COWLS. INSTALLED OUTBOARD INLET FAN COWL PER B737 AMM71-11. INSTALLED INBOARD FAN COWL PER B737 AMM 71-11.SDR SWAA2022032382681Stiffener · cracked#1 ENGINE I/B FAN COWL INNER WEB STIFFINER AT OIL ACCESS DOOR IS CRACKED / [01] REMOVED AND REPLACED #1 ENGINE I/B FAN COWL INNER WEB STIFFENER AT OIL ACCESS DOOR PER SRM 51-40-02-0G-0-B00069 AND CMM 71-13-30;[02] ADDED MESURMENTS;[03] CERTIFIED;[04] INSPECTIOSDR IPXA2022032280382Plate · brokenINSPECTION TYPE:A300ENGINE #2 T/R DOOR R/H UPPER INTERNAL ZONE HAS PLATE BROKEN.FABRICTED NEW PLATE AND INSTALLED IAW SRM 51-40-21.SDR REXA2022031000373Coaming · crackedR-H-S UPPER TRANSCOWL LATCH SEAL FOUND BROKEN. - REPLACED PLACARD IAW CRJ900 AMM 20-60-04-400-801(A0)SDR IXXA2022061314Cowling · dentedN0 1 ENGINE INBD TR UPPER SECTION AROUND BLOCKER DOOR HAS PUNCTURES AND DENTSSDR IXXA2022060811Cowling · cracked#1 ENGINE OB CORE COWL CRACKED AT LOWER CORNER OF VENT PANELSDR NACA2022022600001Cpu · crackedRH COWLING HAS A CRACK ON LOWER AREA 10" LONG FROM THE EDGE. REMOVED AND REPLACED CORE COWLING IAW B767 AMM 71-11-06 OPS CHECKED GOOD. NO TIME DATA IN SYSTEM.
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