JASC 7220
Service difficulty reports · 1,721
Reports filed under 7220 · Turbine Engine Air Inlet 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 = '7220' 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 = '7220' 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 ASAA2013030494079Panel · crackedWHILE ACCOMPLIMENT OF TC 78472000, NR 2 ENG INLET & FAN INSPECTION FOUND BLEED VALVE LOWER PANEL 530-600 POSN AFT LOOKING FWD CRACKED. REPLACED PANEL IAW AMM 72-23-07-400-801-F00.SDR ASAA2013030294043Panel · wornNR 2 ENG INLET AND FAN BLADES DETAILED INSPECTION. FOUND NR 1 FAN DUCT PANEL HAS FASTENER HEAD WORN THRU PANEL. REF AMM 72-23-07, PG 402. R & R NR1 FAN DUCT PANEL, REF MM 72-23-07.SDR ASAA2013022894042Shim · wornFOUND COATING WORN ON FAN BLADE SHIMS FOR NR 1 ENGINE. R & R FAN BLADE SHIMS IAW T/C 78472002.SDR ASAA2013022694116Seal · tornNR 1 ENGINE TREND DATA SHOWS A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. DATA SCATTER INDICATES HARDWARE INSPECTION AND FAN LUBE REQUIRED. PERFORMED NR 1 ENG FAN BLADE LUBE IAW TC 78472002. DURING FAN BLADE INSPECTION FOUND PLATFORM SEAL POSITISDR UALA2013022401084Nose Cowl · dentedNR 2 ENGINE HAS A THREE INCH DENT ON NOSE COWL AT APPROXIMATELY THE SEVEN O'CLOCK. INLET DENT AT 5:00, IS MAJOR AXIS IS 3.5", MINOR AXIS 1.75" DEPTH 0.25" NO CRACKS NOTED AT LEADING EDGE LIP SKIN, IN ZONE K1 AND J. DENT IS BEYOND LIMITS SRM 54-10-00, PG 105-SDR UALA2013022201061Repair · looseON WALKAROUND CREW FOUND NR 1 ENGINE INLET ATTRITION LINER HAS PREVIOUS REPAIR AT 6 O'CLOCK POSITION POPPED LOOSE. DAMAGE AREA APPROX 2"X 2". AREA IS LESS THAN 20 PERCENT OF ATTRITION LINER. ITEM CARRIED FORWARD FOR 20 CYCLES PER MT-72-17. ACP REPAIR PER 7SDR UALA2013022201077Spinner · damagedENGINE 2 SPINNER HAS MINOR DAMAGE. REMOVED NR 2 ENGINE CONE SPINNER REF AMM 72-38-11-000-010-A 13 & INSTALLED NEW SPINNER CONE.SDR UALA2013022201070Rivet · missingNR 2 ENGINE INLET LIP AT 6 O'CLOCK POSITION HAS ONE MISSING RIVET. RIVET TO BE REPLACED WITH IN NEXT 50 HRS.SDR UALA2013021400879Nose Cowl · damagedDAMAGE TO NR 4 NOSE COWL. PUNCTURE AT 5:00 POSITION, APPROX 4 INCHES LENGTH FORE TO AFT, 2 INCHES IN WIDTH, APPROX 1.25 INCHES DEEP. REPLACED NR 4 NOSE COWL.SDR UALA2013021100800Fastener · shearedNR 1 ENGINE INTAKE LIP HAS ONE SHEARED OR BROKEN RIVET 7 O`CLOCK POSITION FORWARD ROW OF RIVETS. ONE MISSING RIVET.SDR DALA13007050939Skin · crackedCRACKS ON LT ENGINE NOSE COWL INNER BARRIER SKIN AT 12:00, 3:00, 9:00, 10:00, 11:00, AND 11:30 CLOCK POSITIONS. DAMAGE WAS EVALUATED AND WAS FOUND OUT OF LIMITS IAW SRM 54-04 AD AND NOSE COWL WAS REPLACED IAW AMM 71-10-01.SDR UALA2013021100804Bracket · brokenNR 2 ENGINE FAN EXIT LINER SEGMENTS AT 12 THRU 2 O'CLOCK POSITIONS APPEAR TO HAVE DAMAGE. REMOVED TWO LINER'S, AT 1 & 2 O'CLOCK POSITIONS, FOUND FOUR BRACKETS BROKEN. REMOVED FOUR BROKEN BRACKETS & REPLACED. COMPLETED INSTALLATION OF 2 FAN EXIT CASE LINERS.SDR UALA2013020500716Blade · damagedON ARRIVAL WALK AROUND FOUND TWO FAN BLADES DAMAGED BY FOD IN NR 1 ENGINE FAN. REPLACED TWO SETS OF FAN BLADES ON NR 1 ENGINE PER MM 72-31-02. REPLACED BLADE NR 1 AND MATE NR 19 AND REPLACED NR 31 AND MATE NR 13, DIS NR 2189 SENT.SDR CA130207005Sensor · defective(CAN) ON START-UP THE INLET BARRIER FILTER SYS WOULD NOT TEST ON THE LT SIDE. A FAULT WAS INDICATED ON THE CONTROL PANEL FOR IBF. THROUGH TROUBLESHOOTING IT WAS DISCOVERED 1 OF THE 2 DIFFERENTIAL PRESSURE SENSOR WAS DEFECTIVE. THE PART WAS REPLACED WITH NEWSDR ASAA2013020393818Shim · damagedACCOMPLISHING NR 1 NG FAN BLADE LUBE T/C 78472002 FOUND FAN BLADE SHIMS MISSING MORE THAN 25 MOLY DAG COATING. REF MM 72-21-02, PG 615, STEP L (1)(A)(1). INSTALLED NEW FAN BLADE SHIMS REF T/C 78472002, STEP 44.SDR UALA2013020100613Nose Cowl · dentedENGINE 1 NOSE COWL DENT OUTER BARREL 4 O'CLOCK POSITION OUT OF AMM LIMITS. REMOVED & REPLACED NR 1 ENGINE NOSE COWL, OPS CHECKED OKAY.SDR UIEA2013012800034Blade · nickedFAN BLADE NICKED NR 1 ENGINE. BLENDED AREA WITHIN LIMITS IAW AMM 72-31-02, FLORESCENT PARTICLE INSPECTION WITH NO ITEMS INDICATED.SDR R61A201301180061Spinner · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT ENGINE SPINNER CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE SPINNER IAW GE 34-10E MM 72-00-00 AND SB 72-0201. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR ASAA2013011793688Fastener · looseNR 1 ENGINE FAN DUCT PANEL FASTENER FOUND LOOSE AND RETORQUED SCREWS ON ALL PANELS IAW AMM 72-23-07.SDR ASAA2013011093666Panel · wornNR 2 ENGINE FAN DUCT PANEL AT 200 POSITION LOWER MIDDLE BOLT PULLING THROUGH HOLE. R & R NR 2 ENGINE FAN DUCT PANEL IAW AMM 72-23-07-000-801.SDR 7AHR20130107001Duct · damagedNR 2 ENGINE HAS A DAMAGED LOWER TURBINE FAN DUCT SEGMENT. R & R THE LOWER TURBINE FAN DUCT SEGMENT IAW OVERHAUL MANUAL 72-00-00.SDR ASAA2012123093584Panel · damagedNR 2 ENGINE, NR 1 FAN DUCT PANEL HAS CAPTIVE BOLT LOOSE AND PULLED THRU PANEL. REMOVED PANEL IAW AMM 72-23-07-000-801-F00. INSTALLED NEW PANEL IAW AMM 72-23-07-400-801-F00.SDR ASAA2012122693554Screw · wornNR 2 ENGINE, NR 5 FAN DUCT PANEL WITH LPTACC SCOOP HAS 2 LOOSE FASTENERS AND MISSING 2 WASHERS. ON FURTHER INSPECTION, NOTED THAT THERE WERE NO MISSING WASHERS, THE SCREW HEADS HAD WORN LEAVING A GAP BETWEEN THE PANEL AND SCREW HEAD. REPLACED ALL SCREWS ONSDR USAA2012122400002Spinner · misalignedON TAKEOFF ROLL ABOUT 100 KIAS ENGINE NR 1 LP VIB INDICATED 4.6. AFTER TAKEOFF FOLLOWED QRH ENGINE ABNORMAL VIBRATION CHECK LIST AND ENGINE VIB (ENGINE 1 LP). RETURNED TO GREEN AT 60%. MAINTENANCE FOUND SPINNER MISALIGNED RE-INSTALLED SPINNER. PERFORMED ENSDR ASAA2012121493467Shim · wornACCOMPLISHING NR 1 ENGINE FAN BLADE LUBE PER T/C 78472002 FOUND FAN BLADE SHIMS EXHIBIT MORE THAN 25 MOLD AG COATING LOSS ON ALL SHIMS REF MM 72-21-02, PG 615, STEP L (1)(A). INSTALLED ALL NEW SHIMS IAW T/C 78472002 ON NR 1 ENGINE.SDR UALA2012121207199Acoustic Panel · brokenFOUND ACOUSTIC PANEL ON THE 6 O'CLOCK POSITION BROKEN, 1.5 INCH DIAMETER AND 3.75 INCH IN LENGTH. ATTRITION LINER OK TO CF PER 72-01-7 GO FOR 20 CYCLES. REPAIRED ACOUSTIC PANEL AT THE 6 O'CLOCK POSITION ON THE NR 1 ENG PER MT 72-017.SDR UALA2012120406943Acoustic Liner · damagedCRACK IN ACCOUSTICAL LINING REPAIR AREA NR 1 ENGINE 6 O`CLOCK POSITION. REPAIR MATERIAL BOND SECURE, OK TO CONTINUE PER AMM.SDR DALA1256060603Inlet · damagedNR 1 ENGINE INLET COWL RT SIDE 9 OCLOCK POSITION HAS A DENT. DENT OUT OF LIMITS IAW SRM 54-11-01. R & R NR 1 ENGINE INLET COWL IAW AMM 71-11-01.SDR ASAA2012112893382Panel · damagedWHILE ACCOMPLISHING ENGINE FAN BLADE INSPECTION ON NR 2 ENGINE, FOUND NR 6 FAN DUCT PANEL WITH A PULLED THRU FASTENER, REF AMM 72-23-07. ACFT GROUNDED. R & R NR 6 FAN DUCT PANEL REF AMM 72-23-07.SDR ASAA2012112693376Screw · looseNR 2 ENGINE FAN DUCT PANELS AT 2, 5, 7, AND 8 O`CLOCK POSTIONS AFT LOOKING FWD HAVE ONE LOOSE SCREW AT EACH LOCATION. REPLACED PANEL AT 7 O`CLOCK POSITION. TIGHTENED ALL LOOSE SCREWS AS REQUIRED REF 72-23-07.SDR 2012F00243Blades · damagedLEFT ENGINE FAN ROTOR BLADES WERE FOUND DISTORTED. R & R THE LT ENG FAN ROTOR BLADES IAW AMM 72-31-02, PAGES 401 TO 403, 426 TO 429.SDR ASMF201211011Case · damagedDURING TRANSIT CHECK, IT WAS DETECTED SCRATCH ON RT ENGINE FAN INLET CASE. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL PERFORMED AN ENGINE REVISION IAW MM 72-24-01, DETECTING SCRATCH AND GROOVE ON RT ENGINE FAN INLET CASE OUT OF LIMITS; SO THE RT ENGINE WAS SDR ASAA2012112093361Fan · out of balanceNR 2 ENGINE VIBRATION INDICATE BETWEEN 1.9-2.0 AT 84-97 N1 CAUSING AN AUDIBLE AND TACTILE VIBRATION. VARYING THE RPM WILL CAUSE THE AUDIBLE AND TACTILE VIBRATION TO INCREASE FOR A PERIOD AND THEN SETTLE DOWN TO A LESSER VALUE. PERFORMED ONBOARD FAN TRIM BALSDR ASMF201211009Blade · dentedCAPTAIN REPORTED THAT DURING TAKEOFF AT ROTATION SPEED A BIRD STRIKE ON RT ENGINE; FLIGHT CREW CONTINUED TO DESTINATION DUE TO RT ENGINE PARAMETERS WERE NORMAL AND VIBRATION REACHED 2.9 OF N2. . MX PERSONNEL PERFORMED A BIRD STRIKE CONDITIONAL INSPECTION IAW MSDR ASAA2012111993327Blade · lack of lubePILOT REPORTED THAT NR 2 ENGINE VIBRATION 2.4 - 2.6. DURING TAKEOFF AND CRUISE. ACCOMPLISHED WO 187681, FAN BLADE LUBE, BOROSCOPE & MX. ACCOMPLISHED VIBRATION SURVEY AMM 71-00-00-700-814-F00. ALL INDICATION WITHIN SERVICEABLE LIMITS.SDR DALA12013390917Nose Cowl · damagedNR 2 ENG NOSE COWL INNER BARREL AT 9 O'CLOCK POSITION, SMALL AREAS OF WIRE MESH LOOSE. INSTALLED PERMANENT REPAIR IAW SRM 54-04AD.SDR UALA2012111906665Spinner · crackedNR 1 ENGINE NOSE SPINNER FOUND CRACK NEAR BOLT. REPLACED NR 1 ENGINE INLET CONE FAIRING PER AMM.SDR UALA2012111906657Acoustic Panel · crackedDURING WALK AROUND FOUND ACOUSTIC PANEL REPAIR ON 1 ENGINE CRACKED AND LOOSE. DAMAGED AREA MEASURES APP ROX 1.5 SQ IN AT 6 O CLOCK POSITION. CF PER MT-72-017. PARTS: 841-0591 ADH3002-48 AVL SFR RES/17NOV. ACCOUSTICAL PANEL DAMAGED AREA HAS PROGRESSED TO 6"XSDR DXTR20121108001Nut · corrodedNR 2 ENGINE FAN SHAFT NUT IS DAMAGED FROM CORROSION. FOUND SHAFT NUT CORRODED. R & R CORRODED NUT FROM MAIN SHAFT. INSTALL NEW NUT IAW LMM 72-06-03, REV 7, & 72-70-02.SDR ASAA2012102093166Screw · vibrationVIBRATION ANOMALY ON NR 2 ENGINE, ALL PARAMETERS ARE WITHIN LIMITS. ACCOMPLISHED TSR WEIGHTS ON ENGINE. MATCHED THE AAVM LOC. 24-P12 & LOC 26-P12 PERFORMED ONE PLANE BALANCE & CHANGED CONFIG TO NEW SOLUTION - LOC 24 FROM P12 TO P14, 26 FROM P12 TO P14, LOC 2SDR DALA2014121006492Nose Cowl · dentedBIRDSTRIKE, NR 1 ENGINE NOSE COWL DENT AT 3 O`CLOCK POSITION. INSPECTED IAW SRM 54-13-01, PG 104. TIME LIMITED REPAIR IAW PS 900-5-1, NR 04.SDR ASAA2012101793152Panel · damagedNR 2 ENG, NR 1 DUCT PANEL ELONGATED BOLT HOLE INBD REAR HOLE. INSTALLED OVERSIZE COUNTERSUNK WASHER ON PANEL IAW EA 800-72EA-08993. R & R NR 2 ENG, NR 1 FAN DUCT PANEL REF MM 72-23-07.SDR ASAA2012101793151Panel · looseWHILE ACCOMPLISHING NR 2 ENGINE INLET AND FAN BLADE INSPECTION, FOUND FAN DUCT PANELS NR 1, 5, 9, 8, AND 7 WITH LOOSE FASTENERS, REF MM 72-23-07-000-801-F00, FIG 401. TIGHTENED FAN DUCT PANELS ON NR 2 ENG, PANELS 1, 5, 9, 8, AND 7. REPLACED NR 7 PANEL REF MM SDR ASAA2012101393111Panel · looseNR 1 ENG INLET AND FAN BLADES -DETAILED INSPECTION FOUND 1 FAN STRUT DUCT PANEL THAT HAS TWO FASTENERS LOOSE WITH POSSIBLE DAMAGE TO PANEL. R & R 1 FAN STRUT DUCT PANEL REF AMM 72-23-07.SDR IXXA20121011030OSpinner · damagedDURING TAKEOFF ROLL, THE ACFT HAD A VIBRATION ON THE RT ENGINE (BIRD STRIKE) AND THE CREW REJECTED TAKE OFF AT 100 KTS. THE ACFT RETURNED BACK TO THE GATE WHERE MX PERSONNEL PERFORMED A HIGH ENERGY STOP INSPECTION IAW AMM 5-51-14. FURTHER INSP OF THE RT ENGINSDR UALA2012101105779Inlet · dentedNR 1 ENGINE INLET COWL AT 8:00 O'CLOCK POSITION HAS DENT. ACCOMPLISHED HFEC INSPECTION, NO CRACKS NOTED, CHECKED THE DENT PER SRM 54-10-01 PG 104 DETAIL IV, DENT FOUND WITHIN LIMITS A OVER Y RATIO IS 31. NO ACTION NEEDED OK TO ARCHIVE.SDR DALA13008175531Inlet · erodedON PDC FOUND NR 1 ENG INLET COWL PAINT ERRODED AT EDGE OF COMPOSITE AT 4 O`CLOCK POS. PERFORMED INTERM REPAIR IAW SRM 54-11-01. REPAIRED NR 1 ENGINE COWL PAINT EROSION IAW 900-3-6, NR 36. OK FOR SERVICE.SDR ASAA2012100893085Spinner · wornNR 2 ENG FRONT SPINNER CONE HAS MORE THAN 50 MISSING OF BLACK SULFURIC ANODIZED COATING. R & R NR 2 ENG FRONT SPINNER CONE REF MM 72-21-01.SDR UALA2012100805706Acoustic Panel · damagedNR 2 ENGINE HAS MISSING ACOUSTIC MATERIAL IN ENGINE INLET. PERFORMED REPAIR PER MT71 -006 REF CF9044 FOR PERM REPAIR AT 7 O'CLOCK POSITION.SDR USAA2012100900001Acoustic Panel · damagedABORTED TAKEOFF DUE TO LOUD NOISE FROM LEFT SIDE OF AIRCRAFT AT APPROXIMATELY 110 KNOTS. FOUND NR 1 ENGINE MID ACOUSTIC PANELS (3 EACH) DAMAGED AND SEVERAL OUTLET GUIDE VANES (OGV) DAMAGED. REMOVED AND REPLACED 3 MID ACOUSTIC PANELS PER AMM 72-23-00-400-025
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