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 UPS04543375Accoustic Liner · delaminatedINSPECTION TYPE: N/A MECHANIC INSPECTION, RT ENG NOSE COWL ACOUSTIC MESH LINER DELAMINATED. REMOVED DEBRIS FROM IGV ACCOMPLISHED BOROS INSPECTION IP AND HP COMPR IAW M/M 72-00-00-6. FOUND SINGLE BLADE IP 2 BENT WITHIN LIMITS IAW M/M 72-00-00 PARA 03.SDR MALA040618Cowl Flap · malfunctionedRT OB COWL OPENED IN FLIGHT. RT ENG COWL FLAP APPEARED TO BE OPEN DURING FLIGHT. AC RETURNED, MAINTENANCE REMOVED AND REPLACED RT ENG FWD COWL, GOOD TO GO.SDR 2005FA0000368Spring · missingON RETURN TO BASE, PILOT REPORTED WHEN CLIMING TO 8000 PT ENGINE SURGED/POWER DROP 2 TIMES. AIRCRAFT WAS DUE A PHASE 1 INSPECTION. WHILE INSPECTING THE ALT AIR DOOR, NOTICED THE DOOR STUCK IN THE OPEN POSITION. FURTHER INSPECTION REVEALED THE SPRING THAT COSDR CA041001014Strut · unsecure(CAN) DURING A FLIGHT AFTER MAINTENANCE, AIRCRAFT WAS IN CLIMB TO FL330 WHEN THROTTLES WERE PULLED BACK. CREW WAS UNABLE TO RETARD LT ENGINE THROTTLE. AIRCRAFT DESCENDED TO FL100 WHERE AN EMERGENCY WAS DECLARED AND THE LT ENGINE FIRE SHUTOFF, PBA WAS PUSHEDSDR CA040814001Camlock · weak(CAN) UPON INSPECTION OF AIRCRAFT DURING ROUTINE MAINTENANCE, THE LT ENGINE FORWARD LOWER COWL WAS FOUND TO HAVE 3 CAMLOCK FASTENERS UNDONE ON THE FORWARD IB SIDE. THE COWL WAS REMOVED, INSPECTED AND THE THREE CAMLOCKS (ONE LONG PN:40S5-11, THE REST SHORT PN:SDR DHL2004745561Skin · dentedDURING A C-CHECK, THE NR 3 ENGINE NOSE COWL HAS 3 EA DENTS (1) NAC STA 88.4 O/B SIDE (2) NAC STA 68.5 O/B SIDE (3) NAC STA 63.5 TO STA 88.4 LWR SIDE. CUT OUT DAMAGED AREAS DIM 2.5625 X 1.4375, .4375 X 1.25, 4.5625 X .5625 AND FABBED DOUBLERS FROM 2024 T3 .040SDR ASMF200407017Cowling · damagedDURING TRANSIT CHECK WAS DETECTED A STRIKE ON LT NOSE COWLING OUT OF LIMITS. IT WAS 2 INCHES WIDE AND 3 INCHES LARGE, 0.335 INCHES DEEP. AIRCRAFT WAS SENT TO THE HANGAR AND NOSE COWLING WAS REPLACED IAW MM 71-10-01, ALL CORRECT.SDR UPS04242774Longeron · crackedINSPECTION TYPE:C, ENGINE NR 2 LT FWD COWL UPPER LONGERON IS CRACKED AT ALIGNMENT PLATE. REMOVED LT FWD COWL UPPER LONGERON IAW SRM 51-30-02. FABRICATED NEW LONGERON PER DRAWING QF7122130-1AND SRM 54-10-06. INSTALLED NEW LONGERON IAW SRM 57-30-02.SDR SWAA041782Cowling · departedON TOUCHDOWN AND REVERSER DEPLOYMENT LOST BOTH SIDES OF NR 1 ENGINE COWLING, WITH DAMAGE TO LT FUSELAGE, LT UPPER WING AND LT HORIZONTAL STAB L/E. ACCOMPLISHED CONDITIONAL INSP OF FUSELAGE, HORIZONTAL STAB, AND PYLON. INSP DUE TO FAN COWLING DEPARTING FROM AISDR QXEA200400454Collar · chafedPDX - CHAFING AROUND OUTSIDE OF HORSE COLLAR. REPAIRED IAW HORIZON AIR EA 6-54-301.SDR COMA0460380Skin · puncturedRIGHT LOWER TRANS COWL HAS PUNCTURE THRU OUTER SKIN. REPAIRED RIGHT HAND LOWER TRANS COWL IAW AERODESIGN REPORT 5170-1.SDR 62227Cowling · separatedPILOT RECEIVED REPORT FROM PASSENGER THAT PART OF THE LT ENG COWL MAY HAVE BLOWN OFF. PILOT CONTINUED TO DESTINATION AND LANDED WITH NO FURTHER INCIDENT. UPON IMMEDIATE WALK AROUND FOUND THAT LT ENG OB COWLING PANEL WAS MISSING AND HAD DEPARTED AIRCRAFT IN FSDR 04FDEA01611Rub Strip · wornNR 2 ENG RIGHT FAN COWL AFT EDGE RUB SEAL WORN. REMOVED AND REPLACED RUB SEAL STRIP IAW SRM 51-31-01 AT MAE.SDR 04FDEA01608Rub Strip · wornNR 3 ENG LT CORE COWL FWD RUB STRIP WORN. REMOVED AND REPLACED RUBSTRIP IAW SRM 51-31-01 AND SRM 51-35-01 AT MAE.SDR C2XA04SH309Cowling · chafedDURING C-CHECK THE NR 1 ENGINE LOWER COWLING WAS FOUND TO BE CHAFED ON THE INNER SKIN. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 04FDEA01339Rub Strip · wornNR 2 ENGINE RIGHT CORE COWL FWD CHAFE STRIP IS WORN. REPLACED RUB STRIP IAW SRM 51-31-01AT MAE.SDR DHL2004754017Cowling · crackedDURING A C-CHECK, NR 2 ENG LT FWD UPPER SUPPORT STRUCTURE HAS (2 EA) HINGE CUTOUT PLATES FOR COWLING ARE BENT OUT & CRACKED AT RADIUS. REMOVED PREVIOUS REPAIRS 2 EA NR 2 ENG L/H FWD UPPER SUPPORT IAW B727 SRM 51-30-2 FABRICATED (2 EA) NEW DOUBLERS 301 1/2 HD SDR C2XA04SH274Rib · chafedSHV-DURING C CHECK THE LEFT UPPER ENGINE COWLING AFT RIB WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RIB IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH258Structure · gougedSHV-DURING C CHECK THE NR 2 ENGINE LOWER COWLING INBOARD EDGE MEMBER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07, FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH257Structure · chafedSHV-DURING C CHECK THE NR 2 ENGINE LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR WRLA200414Cowl Door · missingAIRCRAFT N14075 DEPT. FROM LIRN TO KNGU AT 2100Z WHILE AIRCRAFT CRUISING AFTER 5 HOURS AND 40 MIN.APPROX. 0240Z (ACCORDING TO THE CAPTAIN REPORT) THE ACFT. SHUDDERED AND BOUNCED FOR APPROX. 1/2 SECOND, THEN RETURNED TO STABLE FLIGHT, ACFT. CONTINUE TO KNGU ANSDR AUS20040279Skin · chafed(AUS) ENGINE REAR COWLING SKIN CHAFING IN AREA LOCATED JUST BENEATH THE REAR ATTACHMENT/HINGE POINT. CHAFING EVIDENT ON ALL EIGHT REAR COWLING DOORS.SDR ET72004F00000Heat Shield · delaminatedNOTED HEAT SHIELD HAS DISBONDED FROM RT FIX COWL OUTER SKIN AT APPROX FS 596.0 TO NACELLE STATION 179.0 (OIL CAN). INSPECTION OF FIX COWL INTERIOR (INNER SKIN CORE) AT FS 596.0 TO NACELLE STATION 179.0. NO DEFECTS NOTED. FOUND DELAMINATION ON INNER SKIN CORSDR CA040405007Cowling · cracked(CAN) DURING PHASE 3 INSPECTION THE LT ENGINE LOWER AFT COWL WAS FOUND CRACKED A LONG A SEAM WELD. UNIT WAS REPAIRED IAW COMPANY PROCEDURE ASSY 681-71-10-0093.SDR COMA0460224Cowling · separatedFLIGHT 5892 RT ENGINE COWLING SEPARATED FROM AIRCRAFT AFTER T/O. REPAIRED AND REPLACED ENGINE COWLING.SDR QXEA200400196Fitting · crackedPDX - NR 1 ENGINE FORWARD OUTBOARD SPINE COWL CLEAT CRACKED. REPAIRED IAW DHC-8-400 SRM 51-42-05 AND RD 8/4-71-032.SDR ASAA0480140Nose Cowl · crackedOKC - DURING HV6-CHECK, LEFT ENGINE NOSE COWL IS CRACKED AT AFT FLANGE 7 O'CLOCK POSITION. REMOVED DAMAGED SECTION. REPAIRED WITH DOUBLER AND FILLER PER EA 7110-01221. (M)SDR C2XA04SH127Structure · chafedSHV- DURING C-CHECK THE RIGHT LOWER ENGINE COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH103Skin · chafedSHV- DURING C-CHECK THE RIGHT HAND LOWER COWLING SKIN WAS FOUND TO BE CHAFED IN TWO AREAS BETWEEN STATIONS XN=2180.0 AND XN=2905.0. MAINTENANCE REMOVED THE DAMAGED AREAS AND PERFORMED DOUBLER REPAIRS IAW EMB 135 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RESDR C2XA04SH102Stiffener · chafedSHV- DURING C-CHECK THE RIGHT HAND LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH099Stiffener · chafedSHV- DURING C-CHECK THE RIGHT HAND ENGINE UPPER COWLING AFT INTERNAL STIFFENER WAS FOUND TO BE CHAFED AND EXCEEDED BLEND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICESDR C2XA04SH089Structure · chafedSHV- DURING C-CHECK THE LEFT LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH088Structure · chafedSHV- DURING C-CHECK THE NR 1 ENGINE UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH087Structure · chafedSHV- DURING C-CHECK THE AFT EDGE MEMBER ON THE NR 2 ENGINE UPPER COWLING WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 04FDEA00423Fitting · wornNR 3 ENG NOSE COWL (FAN COWL) GUIDE FITTING LT & RT FOUND WORN. ACCOMPLISHED AS PER EA 1-7110-74316 ENGINES, ENGINE COWLING - INCORPORATION OF P&W SB 71-120.SDR 0354Duct · delaminatedNR 2 ENGINE LT ENGINE COWL TRANSITION DUCT DELAMINATED ON INBOARD SIDE.SDR ABXA040069Nose Cowl · crackedNOSE COWL CRACKED 3 PLACES 6:00 POSITION AT NOSE COWL ANTI-ICE DUCT. INSTALLED ANTI-ICE DUCT IAW DC-9 MM 71-10-01-2-0001, REPLACED DOUBLER IAW DOUGLAS DWG 5959155.SDR RK256001Cowling · missingAFTER TAKEOFF, DEPARTURE INSTRUCTIONS WERE TO CLIMB TO 2000 FEET AND TURN LEFT TO HEADING 120. A LEFT TURN WAS INITIATED A 1000 FEET AND AT APPROXIMATELY 1300 FEET AND HEADING 180 IN LIGHT TURBULENCE, A BUMP WAS FELT BY BOTH PIC AND SIC. PIC VERIFIED FLIGHT SDR CA040129002Accoustic Liner · damaged(CAN) ON TAKEOFF, THRU 100KIAS N1 VIB. BOTH ENGINES 4.0 (RED),VIB. REDUCED AFTER APROX 5 MIN. FOUND ACCOUSTIC LINER DAMAGED. A/C REMOVED FROM SERVICE AND SENT TO HGR FOR REPAIR. (MORE INFO WILL FOLLOW).SDR GTIA040127Nose Cowl · damagedFTW - FOUND TEMP REPAIR INSTALLED NR 2 NOSE COWL ACOUSTIC LINER. REMOVED AND RIGHT NOSE COWL. INSTALLED NOSE COWL. (M)SDR CX2A04SH012Angle · chafedSHV-DURING C CHECK THE NR 2 ENGINE LOWER COWLING AFT OB EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR CA040123002Strut · unsecure(CAN) SHORTLY AFTER TAKEOFF, THE CREW NOTED THAT LT ENGINE THROTTLE COULD NOT BE RETARDED FROM 92 PERCENT. CREW ELECTED TO SHUT ENGINE DOWN WITH FIRE/PUSH PBA. A/C MADE AN UNEVENTFUL LANDING. SUBSEQUENT INSPECTION REVEALED THAT THE CORE COWL SUPPORT STRUT HSDR AWXA200301638Inlet · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK NR 1 ENGINE NOSE COWL WAS FOUND DELAMINATED AT 12:00 POSITION. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-08, FIG 7 & 9, PG 28-29, 47-49.SDR C2XA03SH467Structure · gougedSHV-DURING C-CHECK THE LEFT UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH466Structure · gougedSHV-DURING C-CHECK THE RIGHT UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH449Structure · chafedSHV-DURING C-CHECK THE LEFT LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH446Structure · dentedSHV-DURING C-CHECK THE LEFT UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE DENTED. MAINTENANCE REFORMED THE DENTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH443Structure · dentedSHV- DURING C-CHECK THE LEFT UPPER COWLING INBOARD EDGE MEMBER WAS FOUND TO BE DENTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW EMB 145 SRM 54-10-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH431Stiffener · gougedSHV- DURING C-CHECK THE NR 2 ENGINE UPPER COWLING AFT STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-20-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR AWXA200301476Frame · crackedLCQ - MINOR REPAIR - DURING C-14 CHECK .75 INCH CRACK WAS FOUND IN NR 1 ENGINE FORWARD OUTBOARD COWLING FRAME NR 7 AT PREVIOUS CUTOUT. MAINTENANCE CUTOUT CRACK IN NR 1 ENGINE FORWARD OUTBOARD COWLING FRAME NR 7; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PAR
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