JASC 7112
Service difficulty reports · 27
Reports filed under 7112 · Engine Air Baffle Section, 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 = '7112' 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 = '7112' 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 YENA2024111101449Bleed Valve · abnormalFLT#290, SAN-JFK. (ETOPS) 'HP BLEED VALVE #2 ENG NOT EFFECTIVE FOR AIRCRAFT ENG S/N P800111 REF IPC 36-11-15-51-50 ITEM 10B P/N 70645A030001 REQUIRED; REMOVED AND REPLACED # 2 ENG HP BLEED VALVE IAW AMM 36-11-51 OPS CHECK GOOD.'SDR UIEA2021102002262None · none#2 ENG O/B FAN COWL IS DELAMINATED(<P>ACCOMPLISHED HOT BONDED PERMANENT REPAIR ON #2 ENG O/B FAN COWL PER 54-22-00-0G-0</P> / <P>54-21-01-0I-1, 54-21-01-01A-1; 54-21-01-2R-1 REPAIR 1</P> / <P>51-70-04-0G-0, WORK ACCOMPLISHED PER SDR SWIA202162724None · crackedWHILE COMPLETING REPAIR ON R/H UPPER TRANSCOWL COAMING, FOUND CRACK IN METAL PERFORATE INNER SKIN UNDER ZED STIFFENER. (C-CHECK RO 11-20-2021) REPAIRED R/H UPPER TRANSCOWL INNER SKIN UNDER "Z" STIFFENER REF REO 670-54-21-1472 REV (--) 2021-10-18 STEPS 1-16SDR SWIA202162171None · worn*LEFT ENGINE FAN COWL TIE BAR BUSHINGS ARE WORN AND MIGRATING. (C-CHECK RO 10/30/2021) REMOVED AND INSTALLED NEW L/H ENGINE FAN COWL TIE BAR REF CRJ 700 AMM 71-11-11-000-801-A01 & 71-11-11-400-801-A01SDR SWIA202162170None · worn*RIGHT ENGINE FAN COWL TIE BAR BUSHINGS ARE WORN AND MIGRATING. (C-CHECK RO 10/30/2021) REMOVED AND REPLACED RH PYLON-MOUNT-FAIRING BRACKET ASSEMBLY. OPERATION CHECK WAS GOOD. REF - CRJ 700 AMM 71-11-11-000-801 A01 AND REF - CRJ 700 AMM 71-11-11-400-801 A0SDR SWIA202162319None · bent*RIGHT ENGINE LOWER FAN COWL €“ AT THE OUTBOARD EDGE FROM THE FRONT GOING AFT IS DAMAGE OF GOUGING, BENT STRUCTURE AND CHAFING. (FLAGGED) (C-CHECK RO 11/5/2021) REMOVED AND REPLACED NEW RH ENGINE LOWER FAN COWL OUTBOARD EDGE MEMBER REF CRJ700 SRM 51-42SDR A6WA202108157938Cowl Door · gougedRH ENGINE LOWER CORE COWL HAS A GOUGE DAMAGE ON INNER SKIN BETWEEN XN166.00 AND XN168.00. PERFORMED DOUBLER REPAIR TO RH ENGINE LOWER CORE COWL HAS A GOUGE DAMAGE ON INNER SKIN BETWEEN XN166.00 AND XN168.00. P/N 228-50162-418. DAMAGE MEASUREMENTS ARE L = 0SDR A6WA201441202Fitting · crackedLEFT JET PIPE LOWER MOUNT FITTING OTBD SUPPORT RIB CRACKED. REMOVED CRACKED FITTING & INSTALLED NEW FITTING IAW CMM20-42-06,20-42-21.SDR AUS20030770Bracket · cracked(AUS) ENGINE COOLING SCROLL BRACKET CRACKED FROM NOTCH ON RT SIDE OF THE BRACKET TO THE BOLT HOLE THEN CONTINUING FOR APPROXIMATELY 12.7MM (0.5IN) PAST THE BOLT HOLE TOWARDS THE CENTER OF THE BRACKET. FOUND DURING INSPECTION IAW AD/R22/24 AMDT1.SDR 2001FA0000191Shroud · chafedNOTED: DURING ANNUAL INSPECTION ON NUMEROUS AIRCRAFT, SCREEN INSIDE OF CARB HEAT SHROUD VIBRATING AND CHAFING ITSELF TO PIECES BE ALLOWED TO BE SUCK INTO THE CARB INLET. (SHROUD LOCATED ON CYLINDER STACK ASSEMBLY WITH CLAMPS).SDR AUS20010769Shroud · misinstalled(AUS) ENGINE TO OIL COOLER WORN AND HOLED BY RUBBING ON CARBURETTOR HEAT SHROUD.SDR 2001FA0000074Air Box · crackedRIGHT ENGINE AIRBOX DISPLAYS MORE THAN NORMAL WEAR DUE TO VIBRATION INDUCED CRACKING OF AIRBOX COMPONENTS.SDR AUS20010830Baffle · missing(AUS) LOWER ENGINE BAFFLE MISSING.SDR AU010141Baffle · damaged(AUS) ENGINE BAFFLES DAMAGED. FOUND DURING INSPECTION IAW AD/PA31/96REQ1.SDR CA010301005Adapter · cracked(CAN) DURING SCHEDULED INSPECTION OF THE R/H ENGINE, THE ENGINE BLEED AIR VENTURI ADAPTER WAS FOUND TO HAVE A V SHAPED CRACKED ON THE OUTSIDE OF THE 90 DEGREE BEND OF THE VENTURI. THE VEE HAD OPENED UP, ALLOWING BLEED AIR TO BE DUMPED INTO THE ENGINE COMPARTMESDR 20001120SH027Baffle · crackedBAFFLE ABOVE OIL COOLER CRACKED OUT FROM PRESS FILTER HOLE. (X)SDR SWIA971558Tq Prob · failedLEFT TORQUE GAUGE INOP TO INTERMITTENT AT 13,000 MSL ON CLIMB-OUT. RETURNED TO SFO. REMOVED AND REPLACED LEFT TORQUE PROBE SENSOR. RAN LEFT ENGINE THROUGH PARAMETERS. NO INTERMITTENT FLUCTUATION OR FAILURE. OPS CHECKS GOOD.SDR SWIA971271Tq Sensor · malfunctionedAFTER TAKEOFF RIGHT TORQUE GAUGE OSCILLATED BETWEEN 40 PERCENT AND 100 PERCENT AND THEN FEATHERED INADVERTENTLY. RETURNED TO FIELD, REMOVED AND REPLACED TORQUE SENSOR ON RIGHT ENGINE, IAW EMB MM 76-11-02. REMOVED AND REPLACED RIGHT ENGINE HMU IAW MM 73-21-00SDR CA980608005Bracket · cracked(CAN) BOTH LEFT AND RIGHT CATCH PAN ASSY SUPPORT BRACKETS CRACKED ACROSS THE SUPPORTING SCREW HOLES. IN ONE CASE, THE SUPPORTING SCREW HOLE NO LONGER ATTACHED TO THE AIR BOX ASSY.SDR AU971480Scroll · failed(AUS) ENGINE SCROLL ASSEMBLY LOWER MOUNT SEPARATED. UPPER RH BRACKET PNO 269A8597 WAS ALSO FOUND TO BE UNSERVICEABLE. THE SCROLL WAS FOULING ON THE IMPELLER.SDR 97ZZZX3074Baffle · chafedDURING ANNUAL INSPECTION, FOUND PROPELLER CONTROL ATTACH BOLT AT GOVERNOR RUBBING ON ENGINE BAFFLE. IF LEFT ALONE, BAFFLE COULD WEAR THROUGH CAUSING PROPELLER CONTROL TO JAM AT A SELECTION OTHER THAN FULL RPM. A BRACKET WAS MANUFACTURED TO KEEP BAFFLE CLEAR.SDR CA970605007Baffle · worn(CAN) GOVERNOR ROD END BOLT RUBBING AGAINST FORWARD ENGINE BAFFLE CAUSING GROOVE GREATER THAN 50 PERCENT OF THE THICKNESS OF THE BAFFLE. STATICALLY THE BAFFLE IS OK, BUT IN-FLIGHT UNDER AIR LOADS THE BAFFLE MOVES AGAINST THE BOLT CAUSING RUBBING AGAINST THE BSDR AU960160Baffle · incorrect fit(AUS) ENGINE FRONT BAFFLE LOWER SIDE SEALING STRIPS INCORRECTLY FITTED - BAFFLE LOWER SIDE MATES WITH LOWER COWL - RAM AIR ENTEREDUNDERSIDE OF ENGINE PREVENTING CORRECT COOLING - PERSONNEL/MAINTENANCE ERRORSDR 96ZZZX196Support Bracket · brokenDURING ANNUAL INSPECTION, NOTED THE BAFFLE SUPPORT BRACKET UNDER THE FRONT CENTER SECTION OF ENGINE WAS BROKEN. OBTAINED NEW BRACKET AND INSTALLED. SUBMITTER STATED FURTHER WORK ON THIS AND ANOTHER MOONEY M20R SHOW THIS BRACKET IS BREAKING WITH REGULARITY, LSDR 95ZZZX5600Clamp · looseTHE CLAMPS ON THE FLEX DUCT THAT CONNECTS THE INTERCOOLER TO THE NR 1 AND NR 2 CYLINDERS ARE TOO LARGE AND BOTTOM OUT BEFORE THEY REACH THE REQUIRED TORQUE OF 30-35 PSI. THE PARTS CATALOG CALLS OUT FOR A U84-270SH CLAMP OF THE CYLINDER AND A U84-260SH CLAMP ASDR 95ZZZX3521Baffling · misinstalledBAFFLING WAS IMPROPERLY INSTALLED, JAMMING PROPELLER CONTROL INTERMITTENTLY. MAINTENANCE SHOULD DOUBLE CHECK THEIR WORK ESPECIALLY SINCE THIS AIRPLANE JUST CAME OUT OF AN INSPECTION.SDR HEEA954490Bracket · failedSTARTER GENERATOR AIR DUCT SUPPORT BRACKET BROKE. INSTALLED NEW SUPPORT.
Back to JASC 7112