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 BIGA20171205001Latch · wornTHE RIGHT ENGINE INBOARD ACCESS COWLING (PN: 212-53105-1) DISENGAGED ALLOWING THE COWLING TO OPEN IN FLIGHT. THE COWLING DID NOT DEPART THE AIRCRAFT. THE LATCHES WERE CLOSED AND LOCKED, BUT THE FORWARD LATCH SHOWED SIGNS WEAR TO THE HOOK AND MOST LIKELY DISESDR SWIA201743996Gusset · damagedRIGHT ENGINE UPPER FAN COWL DOOR INNER SKIN HAS DAMAGE. (C-CHECK) RO: 11/17/2017 NEW OUTBOARD GUSSET P/N: CN622-0430-205,INSTALLED NEW IAW SRM.SDR A6WA201745369Louver · crackedLT LWR NOSE COWL 432AB LOUVERED VENT IS CRACKED.SDR UIEA2017073101389Rivet · shearedNR 1 ENGINE LT CORE COWL INTERIOR SURFACE UPPER AFT EDGE WEAR STRIP ATTACH RIVETS FOUND SHEARED. NR 1 ENGINE LT CORE COWL INTERIOR SURFACE UPPER AFT EDGE WEAR STRIP ATTACH SHEARED RIVETS REMOVED AND REPLACED AS PER SRM 51-40-02 REV 104.SDR UIEA2017080101407Rivet · shearedNR 1 ENGINE LT CORE COWL INTERIOR SURFACE UPPER DATA PLATE SUPPORT ATTACH RIVETS FOUND SHEARED. NR 1 ENGINE LT CORE COWL INTERIOR SURFACE UPPER DATA PLATE SUPPORT ATTACH SHEARED RIVETS REMOVED AND REPLACED AS PER SRM 51-40-02 REV 104.SDR UIEA2017080101408Fastener · damagedNR 2 ENGINE RT CORE COWL FWD HINGE ATTACH FASTENER FOUND DAMAGED AS MARKED. NR 2 ENGINE RT CORE COWL FWD HINGE ATTACH DAMAGED FASTENER REMOVED AND REPLACED AS PER SRM 51-40-02 REV 104.SDR UIEA2017080301412Rivet · shearedNR 2 ENGINE RT CORE COWL INTERIOR SURFACE UPPER DATA PLATE SUPPORT ATTACH RIVETS FOUND SHEARED. NR 2 ENGINE RT CORE COWL INTERIOR SURFACE UPPER DATA PLATE SUPPORT ATTACH SHEARED RIVETS REMOVED AND REPLACED AS PER SRM 51-40-02 REV 104.SDR UIEA2017081101457Doubler · wornNR 2 ENGINE LT CORE COWL ZEE FRAME FOUND EXISTING REPAIR DOUBLER WORN, LOCATED 2ND FROM FWD. NR 2 ENGINE LT CORE COWL ZEE& FRAME LOCATED 2ND FROM FWD EXISTING WORN REPAIR FILLER AND DOUBLER REMOVED AND NEW FILLER AND DOUBLER FABRICATED AND INSTALLED AS PER SRMSDR UIEA2017081101458Frame · wornNR 1 ENGINE RT CORE COWL ZEE FRAME FOUND WORN LOCATED 5TH FROM FWD LOWER SECTION ADJACENT TO SUPPORT PLATE. NR 1 ENGINE RT CORE COWL ZEE FRAME LOCATED 5TH FROM FWD WORN AREA PATCH REPAIR CARRIED OUT AS PER SRM 54-42-02-2R-2 REPAIR 2 REV 104.SDR UIEA2017081101460Seal · damagedNR 1 ENGINE LT CORE COWL FAIRING UPPER EDGE FLIPPER DOOR SEAL FOUND DAMAGED. NR 1 ENGINE LT CORE COWL FAIRING UPPER EDGE FLIPPER DOOR DAMAGED SEAL REMOVED AND REPLACED AS PER SRM 51-40-02 REV 104.SDR UIEA2017081101461Seal · damagedNR 1 ENGINE RT CORE COWL FAIRING UPPER EDGE FLIPPER DOOR SEAL FOUND DAMAGED. NR 1 ENGINE RT CORE COWL FAIRING UPPER EDGE FLIPPER DOOR DAMAGED SEAL REMOVED AND REPLACED AS PER SRM 51-40-02 REV 104.SDR UIEA2017081101462Seal · damagedNR 2 ENGINE LT CORE COWL FAIRING UPPER EDGE FLIPPER DOOR SEAL FOUND DAMAGED. NR 2 ENGINE LT CORE COWL FAIRING UPPER EDGE FLIPPER DOOR DAMAGED SEAL REMOVED AND REPLACED AS PER SRM 51-40-02 REV 104.SDR UIEA2017081101463Seal · damagedNR 2 ENGINE RT CORE COWL FAIRING UPPER EDGE FLIPPER DOOR SEAL FOUND DAMAGED. NR 2 ENGINE RT CORE COWL FAIRING UPPER EDGE FLIPPER DOOR DAMAGED SEAL REMOVED AND REPLACED AS PER SRM 51-40-02 REV 104.SDR UIEA2017081101464Rivet · shearedNR 1 ENGINE NOSE COWL EXTERIOR SURFACE AFT EDGE RUB STRIP ATTACH RIVETS FOUND SHEARED LOCATED 10 TO 11 O'CLOCK POSITION. NR 1 ENGINE NOSE COWL EXTERIOR SURFACE AFT EDGE RUB STRIP ATTACH SHEARED RIVETS REMOVED AND REPLACED AS PER SRM 51-40-02 REV 104.SDR DALA2017120608453Cowling · erodedNR 2 ENG OUTBD FAN COWL HAS LEADING EDGE EROSION, 15" LONG FROM BOTTOM CENTER. ACCOMPLISHED A PERMANENT REPAIR TO NR 2 ENGINE OUTBD FAN COWL L/E IAW SRM.SDR DALA2017120608451Cowling · erodedNR 2 ENG INBD FAN COWL HAS LEADING EDGE EROSION, 20" FROM BOTTOM CENTER. ACCOMPLISHED A PERMANENT REPAIR TO NR 2 ENGINE INBD FAN COWL L/E IAW SRM.SDR FDEA201709252733Cowling · delaminatedNR 2 ENGINE RIGHT FAN COWL INNER LOWER FWD SURFACE IS DAMAGED. DAMAGE IS FROM CONTINUED OIL CONTAMINATION FROM EITHER SERVICING OR OIL LEAK AT IDG SERVICE DOOR ON INNER SKIN FORWARD LOWER CORNER OF FAN COWL. HOT BOND COMPOSITE REPAIR REF SRM 51-70-04.SDR FDEA201709052457Cowling · damagedNR 1 ENGINE INLET COWL WIRE MESH DELAMINATED AT 12 O'CLOCK POSITION. DAMAGED AREA EVALUATED AND FOUND OUTSIDE REPAIRABLE LIMITS IAW AMM 71-11-01 AND SRM 54-10-01. TRIMMED AND RESEALED LOOSE EDGES OF DAMAGED WIRE MESH IAW AMM SRM 71-11-01 AND SRM 54-10-01. REPSDR UIEA2017081501487Frame · gougedNR 2 ENGINE OUTBD CORE COWL FRAME GOUGED. FABRICATED AND INSTALLED REPAIR DOUBLER AND REPAIR ANGLE PER SRM 56-41-02-2R-2 FIG 201.SDR DALA201907203986Cowling · damagedPD: UPPER AFT AND FWD RUB STRIPS AND RUB PADS WORN;LOWER LONGERON DAMAGED; SURGE BLEED SEAL WORN;AFT ALIGMENT PIN BUSHING MISSING. CA: REPLACED ALL WORN PARTS PER CMM 71-11-73 DAL REV48; REPLACED BUSHING PE RERA 401967-14 MA REV B REPLACED ALL WORN PARTS PER CSDR UIEA2017072001245Rub Strip · damagedNR 1 ENGINE, LT CORE COWL EXTERIOR FWD SURFACE WEAR STRIP FOUND DAMAGED. WEAR STRIP REMOVED AND REPLACED AS PER SRM 51-40-02 REV 104.SDR UIEA2017070101081Bracket · wornNR 2 ENGINE LT CORE COWL ATTACH 5TH HAT FROM LOWER FOUND WORN. MOST AFT FRAME ATTACH WORN HAT (5TH FROM LOWER) REMOVED AND REPLACED AS PER SRM 51-40-02 REV 104.SDR DALA2017071805547Door · crackedNR 1 ENG NOSE COWL 6 OCLOCK POS PRESSURE RELIEF DOOR CRACKED. REPLACED THE DOOR ASSY IAW AMM 71-11.SDR DALA2017071105332Cowling · crackedCRACK ON FIXED COWL APRON HINGE, LATCH ASSEMBLY AFT OF LOWER FAN COWL DOOR ENGINE LT. CRACK ON FIXED COWL WAS REPAIRED PER SRM 54-00-00 REP 1 HINGE, GUSSET, AND CLIP WERE REMOVED AND REINSTALLED PER SRM 51-41-02-0G AND 51-41-05-0G.SDR UIEA2017071201183Cowling · damagedNR 1 ENGINE I/B CORE COWL HAS DAMAGED TRAILING EDGE CORNER. REMOVED AND REPLACED NR 1 ENG I/B CORE COWL PER AMM.SDR UIEA2017071201184Plate · brokenNR 1 ENGINE I/B CORE COWL HAS BROKEN CHAFE PLATE AT TRAILING EDGE. REMOVED AND REPLACED I/B CORE COWL PER AMM 71-11-06.SDR UIEA2017071201185Seal · damagedNR 2 ENGINE O/B FAN COWL HAS A DAMAGED SEAL AT TRAILING EDGE. REMOVED AND REPLACED DAMAGED SEAL AT NR 2 ENGINE O/B FAN COWL T/E SRM 51-40-02.SDR UIEA2017071201186Seal · tornNR 2 ENGINE I/B FAN COWL HAS TORN SEAL BOTTOM OF TRAILING EDGE. NR 2 ENGINE I/B FAN COWL SEAL BOTTOM ON TRAILING EDGE WAS REMOVED AND REPLACED IAW AMM 20-11-00.SDR UIEA2017052300844Bracket · wornNR 2 ENGINE RT CORE COWL HOLD OPEN ROD STOW PIN BRACKET AND ADAPTER FOUND WORN AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121.SDR UIEA2017052300845Support Bracket · wornNR 2 ENGINE RT CORE COWL HOLD OPEN ROD SUPPORT BRACKET AT BASE SIDE FOUND WORN AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121.SDR UIEA2017052500860Skin · crackedNR 1 ENGINE RT CORE COWL EXTERIOR AREA PRECOOLER EXIT DUCT CUT-OUT AREA FOUND CRACK AS MARKED. NR 1 ENG RT CORE COWL SKIN PRECOOLER EXIT DUCT ASSY CUT-OUT BELOW NAC STA.281.12 LOWER SECTION CRACK AREA. EXTERNAL PATCH REPAIR CARRIED OUT AS PER SRM 54-42-01-2R-3SDR UIEA2017052300836Frame · damagedNR 1 ENGINE LT CORE COWL 2ND ZEE FRAME COUNT FROM FWD FOUND EXISTING REPAIR WORN AS MARKED. NR 1 ENG LT CORE COWL 2ND FROM FWD DAMAGED ZEE FRAME REMOVED AND REPLACED AS PER SRM 51-40-02, REV 104.SDR UIEA2017052300837Cowling · wornNR 2 ENGINE RT CORE COWL PRECOOLER EXIT DUCT LIP FOUND WORN AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121.SDR UIEA2017052300839Skin · crackedNR 2 ENGINE RT CORE COWL SKIN FOUND CRACK LOCATED AT AFT UPPER CUTOUT AREA AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121. REFER TO NRC 0688 FOR CORE COWL REPLACEMENT DETAILS.SDR UIEA2017052300841Seal · crackedNR 2 ENGINE RT CORE COWL FLIPPER DOOR FOUND SEAL CRACK AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121.SDR UIEA2017052300842Strip · wornNR 2 ENGINE RT CORE COWL FWD UPPER EXTERIOR AREA WEAR STRIP FOUND WORN AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121.SDR UIEA2017051800815Adapter · wornNR 1 ENGINE RT CORE COWL HOLD OPEN ROD STOW ADAPTER FOUND WORN AS MARKED. NR 1 ENGINE RT CORE COWL HOLD OPEN ROD STOW ADAPTER REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.SDR UIEA2017041000532Rivet · looseNR 1 ENGINE RT CORE COWL UPPER SUPPORT PLATE FOUND RIVET LOOSE AS MARKED. NR 1 ENG RT CORE COWL UPPER SUPPORT PLATE ATTACH LOOSE RIVET REMOVED AND REPLACED AS PER SRM 51-40-02, REV 103.SDR DALA2017052004114Fitting · gougedRIGHT NR 2 ENGINE O/B CORE COWLING LWR AFT LATCH BLOCK FITTING AND ATTACH STRUCTURE IS GOUGED. FITTING BLOCK IS LOOSE AND FASTENERS LOOSE. BLENDED GOUGE ON RT ENGINE O/B CORE COWL LOWER AFT LATCH BLOCK FITTING AND STRUCTURE. BEYOND LIMITS OF SRM 54-41-02 DETASDR DXTR2017051705Cowling · delaminatedTHE LT ENGINE UPPER COWLING HAS AN AREA OF DELAMINATION ON THE INNER SURFACE. THE DAMAGE
MEASURES APPROXIMATELY 18.0 INCHES BY 12.0 INCHES. AQRD ERO-895901 PROVIDED ENGINEERING FOR A ONE-TIME FLIGHT TO MOVE THE AIRCRAFT TO KADS WHERE A PERMANENT REPAIR WILL BSDR IPXA2017051517139Support Rib · damagedWHILE PERFORMING TC545028-01-1-435 FOUND DAMAGE TO NR 1 ENG RT FAN COWL AFT HINGE CONSISTING OF CHAFING ON FWD SUPPORT RIB MEASURING .750 LONG X .062 DEEP. AFT SUPPORT RIB MEASURING .250 LONG X .0625 DEEP. ACCOMPLISHED INTERIM REPAIR IAW EO -7110-64275-A.SDR YENA201704280318Engine · failedFROM CLIMB TO CRUISE, ALTITUDE FL 350, THERE WAS CONTINUOUS ENG OIL SCENT IN THE COCKPIT FROM THE BLEED AIR SUPPLY SYSTEMS. THE NR 1 ENGINE WAS R & R, ALL OP CHECKS NORMAL.SDR CALA2017041400969Support Beam · gougedNR 1 ENG I/B FAN COWL SUPPORT BEAM WEB HAS DEEP GOUGES. ACCOMPLISHED NR 1 ENGINE I/B FAN COWL SUPPORT BEAM WEB REPAIR IAW EC/RA 5410-01844 PER 75-7100- 1-2907.SDR 2017F00056Cowling · wornLEFT ENGINE HARD COWL DAMAGE REPAIR. ENGINEERING MEMO REF: DQ7684M1 DATED APRIL 5, 2017.SDR ASOA201704031426Skin · chafedRT ENGINE CORE COWL INTERNAL SKIN CHAFED DAMAGED IN MULTIPLE AREAS. COMPLIED WITH EC/TC REO 670-54-23-959,REO 670-54-23-959, EC/TC REO 690-54-23-208,REO 690-54-23-208, FUR-71-10-00289, EC/TC FUR-71-10-00289,EC/TC 25-2014-387, EA 25-2014-387.SDR IPXA2017041916290Fastener · missingINSPECTION TYPE: 3C, NR 1 ENGINE INLET COWL HAS ONE MISSING FASTENER AT THE 12 O'CLOCK POSITION. REPAIRED THE INLET COWL IAW EA 0117110-01-A6742 REV I/R AND EO MD11-7110-63982-A.SDR DALA201907203982Cowling · damagedPD: H/O ROD PARTS DAMAGED AND-OR WORN; FWD RUB STRIPS WORN; ENGINE OIL ACCESS DOOR LATCHES AND BUSHINGS WORN; 2ND AND 3RD FRAMES WORN; SHIELD IS CRACKED. CA: REPLACED ALL WORN AND DAMAGED PARTS PER CMM 71-13-30 REV 24 REPLACED ALL WORN AND DAMAGED PARTS PER SDR DALA2017020701024Cowling · crackedFOUND NR 4 ENG LT FAN COWL UPPER TRAILING SIDE HAS CRACKS 2 IN SURFACE AND 7 IN BACK. REPLACED NR 4 ENG LT FAN COWL PER AMM 71-11.SDR U2RA201706110001Longeron · damagedDURING ACCOMPLISHMENT D CHECK INSPECTION FOUND NUMBER 4 ENGINE INBOARD CORE COWL RIVET PULLED THROUGH LOWER EDGE. REMOVED AND REPLACED LOWER AFT SECTION AND DAMAGED FASTENERS IN ACCORDANCE WITH ENGINEERING DISPOSITION EO MAS-J217-N919CA-008 REV IR AND SRM 51-4SDR P5CA2017011200023Strip · chafedCHAFING NR 2 ENG RT CORE COWL INNER AFT WEAR STRIP CHAFING. REMOVED DAMAGED STRIP IAW SRM 51-40-02-0G-0 REV 67. INSTALLED NEW STRIP IAW SRM 51-40-02-0G-0 REV 67 AND CMM 71-13-24 REV43. JOB COMPLETED AND CONDITION CHECK NORMAL.
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