JASC 7120
Service difficulty reports · 3,029
Reports filed under 7120 · Engine Mount 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 = '7120' 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 = '7120' 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 ICRR202408060002Pin · crackedCRACK INDICATION DISCOVERED IN THREADS DURING LIQUID PENETRANT INSPECTION (SOPM 20-20-2)SDR ICRR202408060001Thrust Link · indicationSURFACE INDICATION DISCOVERED DURING MAGNETIC PARTICLE CHECK (SOPM 20-20-01)SDR 2024FA0000555Isolation Mount · crackedDURING THE REPLACEMENT OF THE ENGINE MOUNTS, WE FOUND THAT THE TORQUE CALLED OUT IN THE MAINTENANCE MANUAL (CESSNA 100- SERIES SERVICE MANUAL 1962 AND PRIOR PARA 12-10(B) AND PAGE 1-8 FOR 3/8-24 AN310 SELF LOCKING NUT NOTE 2 (160-190 IN. LBS)) APPEARS TO BE ESDR SWIA20240722Bolt · wornRIGHT ENGINE BACKUP THRUST LINK MOUNT BOLT IS WORN BEYOND SERVICABLE LIMITS (FILED - CLOSED)REMOVED AND REPLACED RIGHT ENGINE BACKUP THRUST LINK MOUNT BOLT IN REFERENCE TO GE CF34-8C ESM 71-20-00- ASSEMBLYTORQUE WRENCH SN 5060772342 DUE 12/2024SDR DALA2024071507150Drag Fitting · corrodedDAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DRAG BRACE AS FOLLOW: HOLE # 6 CORROSION ON SKIN AND FITTING BTW 5-7 O CLOCK POSITION & HOLE # 9 CORROSION ON SKIN AND FITTING BTW 9 TO 11 O CLOCK POSITION IN REF. CARD 5720-01100 -04A JOB # 121-00SDR DALA2024070806912Mount · damagedSHIP 3153 #1 ENG FWD MOUNT BOTH ALIGNMENT PIN HOLES DAMAGE. CORRECTIVE ACTION: BLENDED ALIGNMENT PINN HOLES ON FWD IAW A319 SRM 54-51-18-283- 001. (0431700)SDR ICRR202407050001Thrust Link · indicationSURFACE INDICATION FOUND DURING MAGNETIC PARTICLE CHECK (SOPM 20-20-01)SDR AALA202407031672Thrust Link · defectiveAIRCRAFT WAS GROUNDED: DURING AN UNSCHEDULED LEFT ENGINE CHANGE MAINTENANCE FOUND FORWARD ENGINE MOUNT THRUST LINK WAS MISSING A BUSHING ON THE REPLACEMENT ENGINE. MAINTENANCE REPLACED THE THRUST LINK PER AMM 71-21-12 AND EA 355869.SDR ICRR202406210001Yoke · damagedABNORMAL INDICATION WAS DISCOVERED DURING ULTRASONIC TEST NDT 71-21-101 PART 4SDR DALA2024061906233Drag Fitting · corrodedDAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #1 CORROSION ON FITTING AT 8 O CLOCK POSITION, HOLE #2 CORROSION ON FITTING-SKIN AND BTW TO 1-2 O CLOCK POSITION,AND GOUGE ON FITTING-SKIN BTW TO 1-2 O CLOCK POSITION ANDSDR 2024FA0000451Mount · crackedAD 80-19-12R1 REQUIRES THAT DYE PENETRANT INSPENTION TO BE DONE ON THE ENGINE MOUNT LOWER TUBES. ON 5TH-NOV 2023, DYE PENETRANT INSPECTION WAS CONDUCTED BUT NO CRACK WAS FOUND, BUT AFTER CONFIRMING THE RESULT WITH MPI, A CRACK OF 12MM WAS IDENTIFIED. KINDLY NSDR AALA202405295691Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON #1 ENGINE AFT MOUNT LINK ASSEMBLY INNER PINS (2 EACH). REPLACED INNER PINS PER AMM 71-22-11.SDR DALA2024052805584Drag Fitting · damagedSHIP 6700 DAMAGE WAS FOUND IN HOLES AT LH ENG DRAG FTG CLAMP-UP AND DRAG BRACE AS FOLLOWS: HOLE #11 SCRATCHES ON FTG BTW 7 TO 10 O CLOCK POSITION, HOLE #12 CORROSION ON SKIN AT 5 O CLOCK POSITION, HOLE #13 SCRATCHES ON SKIN & FTG BTW 4 TO 12 O CLOCK POSITION, SDR DALA2024052805583Drag Fitting · damagedSHIP 6700 DAMAGE WAS FOUND IN HOLES AT RH ENG DRAG FTG CLAMP-UP AND DRAG BRACE AS FOLLOWS: HOLE #11 CORROSION ON SKIN/FTG AT 10 O CLOCK POSITION, HOLE #12 CORROSION ON SKIN/ FTG ALL BORE, HOLE #13 CORROSION ON FTG BTW 1-3 O'CLOCK POSITION, HOLE #14 CORROSION OSDR DALA2024052805582Drag Fitting · damagedSHIP 6700 CORROSION WAS FOUND ON COUNTERSINK AT HOLES #1 TO #18 AT RH ENG DRAG FTG CLAMP-UP AND DRAG BRACE AIN REF CARD 5720-01100-04B STEP 14.C. CORRECTIVE ACTION: SUMMARY OF NRC 00370: COUNTERSINK AT HOLES #1 TO #18 AT RH ENG DRAG FTG CLAMP-UP WERE REPAIRED SDR DALA2024052805581Drag Fitting · damagedSHIP 6700 DAMAGE WAS FOUND IN HOLES AT LH ENG DRAG FTG CLAMP-UP AND DRAG BRACE AS FOLLOWS: HOLE #1 CORROSION ON SKIN & FTG BTW 6 TO 8 O CLOCK POSITION, HOLE #2 CORROSION ON SKIN BTW 6 TO 1 O CLOCK POSITION AND CORROSION ON FTG AT 12 O CLOCK POSITION, HOLE #3 CSDR DALA2024052805580Drag Fitting · damagedSHIP 6700 DAMAGE WAS FOUND IN HOLES AT RH ENG DRAG FTG CLAMP-UP AND DRAG BRACE AS FOLLOWS: HOLE #2 CORROSION ON SKIN/FTG BTW 3-9 O CLOCK POSITION, HOLE #3 CORROSION ON SKIN/FTG BTW 7-9 & 3-4 O CLOCK POSITION, HOLE #4 CORROSION ON SKIN/FTG ALL BORE, HOLE #5 CORSDR DALA2024052805579Drag Fitting · damagedSHIP 6700 DAMAGE WAS FOUND IN HOLES AT RH ENG DRAG FTG CLAMP-UP AND DRAG BRACE AS FOLLOWS: HOLE #2 CORROSION ON SKIN/FTG BTW 3-9 O CLOCK POSITION, HOLE #3 CORROSION ON SKIN/FTG BTW 7-9 & 3-4 O CLOCK POSITION, HOLE #4 CORROSION ON SKIN/FTG ALL BORE, HOLE #5 CORSDR F3LA2024052400075Pin · missingDISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 15346.0301 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. #2 ENGINE FWD MOUNT FAIL SAFE PIN REQUIRES INSTALL.
CORRECTIVE ACTION: INSTALLED #2 ENGINE FWD MOUNT FAILSAFE PIN IAW A320 AMM 71-21-11-400-802-A.SDR SWI2024F00522Yoke · chafedRH ENGINE YOKE CHAFED ON UPPER AND LOWER SIDE OF MOUNTING POINT ON SIDE THAT CONNECTS TO THE AIRCRAFT FROM CONTACT WITH THE STAYING FAIRINGS (FLAGGED). (C-CHECK RO 6/19/2024) COMPLIED WITH REPAIR TO RH ENGINE YOKE UPPER AND LOWER SIDE REF REO 670-71-21-SDR 2024FA0000311Thrust Link · crackedSUB-SURFACE INDICATION DISCOVERED DURING MAGNETIC PARTICLE INSPECTION (SOPM 20-20-01)SDR HNAA2024051400373Yoke · corrodedE031858 R/H ENG. FWD. ENGINE YOKE, FWD. FITTING HAS POSSIBLE CRACK. : REMOVED AND INSTALLED NEW R/H ENG. YOKE UPPER AND LOWER FWD. AND AFT LINKAGE IAW FCD1-54-21-0017DSDR 2024F00104Yoke · damagedABNORMAL INDICATION WAS DISCOVERED DURING ULTRASONIC TEST NDT 71-21-101 PART 4.SDR 2024FA0000255Mount · chafedDURING ANNUAL TYPE INSPECTION, CHAFFING (FIG A) WAS NOTED ON THE RH AFT ENGINE MOUNT FITTING P/N 35-910027-3 SERVICE BULLETIN SB71-3638 ADDRESSES DAMAGE TO THE 35-910027-3 FITTING CAUSED BY CHAFFING FROM THE OPTIONAL 35-910003-85 HEAT SHIELD AND PROVIDES APPROSDR FDEA202403210424Mount · corroded#1 ENG FWD MOUNT FWD RH MOUNT HOLE PITTED, APPEARS TO HAVE CORROSION. COMPLIED WITH EA 1-5450-T0378566 P1 AND P2 TITLE: NACELLES/PYLON- WING PYLON/STRUT - FWD ENGINE MOUNT, FWD IB TRUSS BOLT HOLE CORROSION PERMANENT REPAIR.SDR ICRR202403150072Mount · failed inspFAILED EDDY CURRENT PER NDT MANUAL PART 6, CRJ 700 71-21-101-250.SDR DALA2024031103206Clamp · crackedSHIP 5657 CUSTOMER CARD: 5720-01100-04A. LH ENG DRAG FTG CLAMP; FOUND 1EA FASTENER HOLE CRACKED AT THE #9 LOCATION, 6 O'CLOCK DIRECTION, AND APPROX .030 LONG IN THE FITTING. CORRECTIVE ACTION: COMPLIED WITH ER/A 584851-14AD REV D. (0236582)SDR AALA202404157786Mount · corrodedAIRCRAFT IN BASE MAINTENANCE: #2 ENGINE AFT MOUNT 2EA LONG INNER PINS HAS PITTING CORROSION. ENGINE 2 AFT MOUNT INNER PIN REPLACED.SDR DALA2024030503044Drag Fitting · damagedSHIP 698 DAMAGES WERE FOUND ON RH ENG DRAG FTG HOLES AS FOLLOW: HOLE #11 CORROSION ON FITTING BETWEEN 7 AND 8 CLOCK POSITIONS, HOLE #14 CORROSION ON SKIN AND FITTING BETWEEN 8 AND 9 CLOCK POSITIONS. CORRECTIVE ACTION: ACCOMPLISH SECTION II, III, IV, IAW ER/A 5SDR DALA2024030102894Shear Pin · corrodedSHIP 3128 CORROSION ON SHEAR PIN ON UPPER POSITION RH HAND LINK ON AFT ENGINE MOUNT ENGINE 2. CORRECTIVE ACTION: REPLACED NEW SHEAR PIN ON UPPER POSITION RH HAND LINK ON AFT ENGINE MOUNT ENGINE 2 AS PER A320 FAM AMM 71-22-11-000-042-A AND AS PER A320 FAM AMM 7SDR DALA2024030102893Mount · crackedSHIP 3128 CRACK ON RETAINER FWD MOUNT LOC. LH FWD HAND LINK ON ENGINE 1. CORRECTIVE ACTION: REPLACED RETAINER FWD MOUNT LOC. LH FWD HAND LINK ON ENG 1 AS PER A320 FAM AMM 71-21-11-000-043-A AND A320 FAM AMM 71-21-11-400-043-A. (0224303)SDR DALA2024030102887Nose Cowl · damagedSHIP 3220 DISC: BIRD STRIKE. C/A: FOUND BIRD STRIKE DAMAGE ON ENG #1 NOSE COWL LIP APPROX. 2 0' CLOCK POSITION LOOKING FWD. PERFORMED INSPECTION OF AIRCRAFT AFTER A BIRD STRIKE PER A320 AMM 05-51-14-200-803-A FOUND NO OTHER DAMAGE ON AIRCRAFT OTHER THAN ENG #1SDR DALA2024022302550Bushing · damagedSHIP 5641 DURING INTERFACE INSP OF THE REMOVAL OF UPPER LINK # 2 ENG FOUND FWD SPAR FITTING BUSHING DAMAGED. CORRECTIVE ACTION: COMPLIED WITH ERA 584011-14 REV A AT #2 ENG UPPER LINK. (0213440)SDR AALA202402235744Mount · looseAIRCRAFT WAS GROUNDED: #2 ENGINE REAR OUTBOARD MOUNT FOUND TO BE LOOSE WITH COTTER PIN OFF. #2 ENGINE AFT MOUNT BEAM ASSEMBLY REPLACED.SDR DALA2024022002352Drag Brace · damagedSHIP 6819 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DRAG BRACE AS FOLLOW: HOLE #13 CORROSION ON SKIN AND FITTING BTW 4 TO 9 O CLOCK POSITION. HOLE #14 CORROSION ON SKIN AND FITTING BTW 7 TO 11 O CLOCK POSITION AND SCRATCHES ALL SDR ICRR202402020001Mount · crackedA CRACK INDICATION WAS DISCOVERED DURING A VISUAL INSPECTION PER CRJ 700 DOCUMENT# CSP-B-010, MANUAL ID: NDTM PART 4 AND PART 6 REV 36 2/8/2022.SDR AALA202401249005Mount · excess playAIRCRAFT IN BASE MAINTENANCE: #2 ENGINE AFT MOUNT OUTBOARD LINK BEARING IN CENTER BEAM HAS AXIAL PLAY. MAINTENANCE REPLACED #2 ENGINE AFT MOUNT PPER AMM 71-22-11.SDR IPXA2024032081123Mount · crackedLARGE CRACK OUTBOARD SIDE ENGINE 1 AT MOUNT POINT ON WING. INSTALL NO.1 ENG PYLON TO WING FARING I.A.W SRM 51-40-02-0G REV.100 AND DWG NO.65B13507 SH1 TRV.G AND DWG NO.65B13639 SH2 REV.D.SDR 2024FA0000000Thrust Link · making metalSURFACE INDICATION DISCOVERED DURING MAGNETIC PARTICLE CHECK (SOPM 20-20-01)SDR ICRR202312210001Bolt · abnormalFAILED LINEAR INDICATION WAS FOUND IN THREADS DURING DYE PENETRANT INSPECTION (NDT 51-20-08 PART 1).SDR SWIA202402201212Mount · damagedDURING AUDIT OF 1C TASK CARD 54-440-301 (INTERNAL ZONAL INSPECTION OF THE RIGHT NACELLE), FOUND RH ENGINE FWD. ENGINE MOUNT HAS RUB MARKS ON LOWER SURFACES FROM HINGE LINE FAIRING PANELS. (C-CHECK RO 2/19/2024) COMPLIED WITH OF REO 670-71-21-094 REV.-- DATSDR SWI2024031200219Striker · looseRIGHT ENGINE THRUST TORQUE BOX AFT SIDE UPPER OUTBOARD LATCH STRIKER LOOSE (C-CHECK RO 3/9/2024) REMOVED R/H ENGINE THRUST REVERSER UPPER OUTBOARD LATCH STRIKER AND INSTALLED NEW LATCH STRIKER REF. MHIRJ REO 601R-78-30-4353 REV. €“ DATED 2024-01-26 AND SKSDR HNAA2024011700018Unknown · unknownTHE RH PYLON FWD ENGINE YOKE AT SPAR II UPPER FLANGE WHERE THE FASTENER WAS REMOVED FOR INSPECTION SHOWS A RELEVANT INDICATION WHEN PERFORMING THE HFEC ROTOSCOPE INSPECTION. ACCOMPLISHED REPAIR BY REAMING, BUSHING INSTALL, COLD WORKING IAW SB145-54-0008 AND EOSDR HNAA2024011700017Unknown · unknownE012280 : THE LH PYLON FWD ENGINE YOKE AT SPAR II UPPER FLANGE WHERE THE FASTENER WAS REMOVED FOR INSPECTION SHOWS A RELEVANT INDICATION WHEN PERFORMING THE HFEC ROTOSCOPE INSPECTION. ACCOMPLISHED REPAIR BY REAMING, BUSHING INSTALL, COLD WORKING IAW SB145-54-0SDR 2023FA0000701Unknown · unknownMAGNETIC MRO AS, PERFORMING MAINTENANCE UNDER CAYMAN ISLANDS APPROVAL RECEIVED PART 740-2040-503 WITH 8130-3 (TRACKING A239896) FROM FAA REPAIR STATION 3S7R970B (SET AERO). DURING INSPECTION IT WAS FOUND THAT INCORRECT PN WAS USED FOR MOUNT ASSEMBLING DURING WSDR 2023FA0000579Nut · backed outNOTICED A LOSS OF FUEL PRESSURE EN ROUTE. ELECTED TO LAND AT NEAREST SUITABLE AIRPORT. FOUND THAT THE MIXTURE CABLE SUPPORT NUT HAD BACKED OFF AND ALLOWED THE CABLE TO PULL THE MIXTURE ARM TOWARDS LEAN, RESULTING IN PARTIAL LOSS OF POWER.SDR DU4R202309280294Mount Fitting · damagedDURING SCHEDULED INSPECTION, FOUND #2 PYLON ATTACH ENGINE TO PYLON I/B AND O/B HOLES AT RIB 1 HAS DAMAGED HOLES.S/O 339001 N/R #28498SDR DALA2023092507882Unknown · unknownSHIP 3171 THE #2 ENGINE PYLON FORWARD ENGINE MOUNT PYRAMID FITTING MIDDLE AND AFT ALIGNMENT PIN HOLES ARE NICKED/DAMAGED. CORRECTIVE ACTION: EVALUATED AND REWORKED PER A319 SRM 54-51-18-283-001. (2985786)SDR YENA2023092201120Unknown · unknownFLT#8008, CDG-JFK. (ETOPS) '#1 EGN NO.3 BEARING CARBON SEAL FAILED BSI AND PER PRATT ENGIE REQUIRES REMOVAL AS UNSERVICEABLE; INSTALLED #1 ENG IAW TASK CARD A320-71-00-51-400-802-A REF WO # 1282086.'SDR IPXA2023091894189Bracket · crackedINSPECTION TYPE:1CENG 1 PYLON FWD BRACKET UNDERNEATH BUTTERFLY PANEL HAS A CRACKREMOVED, FABRICATED AND INSTALLED IAW SRM 51-40-21
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