JASC 7220
Service difficulty reports · 1,719
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 9WGA2025042954619Inlet · corroded#3 INLET HAS PITTING CORROSION BETWEEN 5 & 6 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET BETWEEN 5 & 6 O'CLOCK POSITION. FOUND WITHIN LIMITS IAW MD-11 SRM 54-12-02. NO MATERIAL LOSS AT THIS TIME. O. ARILA D0011. SDR CALA2025041603886Blade · damagedCREW DEBRIEF - ON ROTATION. FELT THUMP. ON CLIMB #2 ENGINE STALLED 3 TIMES. REDUCED POWER, ENGINE QUIT STALLING. ONCE LEVELED OUT.ACCOMPLISHED CHECKLIST. SHUT ENGINE DOWN. NO SEVER VIBRATION. AT ROTATION FLT CREW OBSERVED A RABBIT INGESTED #2 ENGINE, ENGINE STSDR HALA20250404100Seal · brokenETOPS - #2 ENG ANNULUS FILLER AT POS 2, POS 10, POS 5 BROKEN SEAL . REPLACED ANNULUS FILLER AT POS 2, POS 10, POS 5 PER AMM 72-31-41-400-802-ASDR UIEA2025031200279Case · corrodedENG 2, FAN CASE, AT 6' O CLOCK, UNDER STRUT AREA, BASE WITH CORROSION L=2.100" W=1"(<P>ENG 2, FAN CASE, AT 6' O CLOCK, UNDER STRUT AREA, BASE, CORROSION LEVEL 1 WAS REWORKED, EVALUATED, INSPECTED AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW AMM 72-33-00-206-001SDR UIEA2025031200278Case · corrodedENG 1, AFT FAN CASE, AT 5 TO 6 O'CLOCK APROX, WITH SEVERAL POINTS OF CORROSION (3EA).(<P>ENG 1, AFT FAN CASE, AT 5 TO 6 O'CLOCK APROX, CORROSIONS LEVEL 1 WAS REWORKED, EVALUATED, INSPECTED AND FOUND TO BE WITHIN ALLOWABLE LIMITS. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025030600215Bolt · corrodedENG 2, FAN CASE, OGVS BOLTS AREA, 113 BOLTS, BETWEEN 7 - 11 WITH CORROSION.(<P>ENG 2, FAN CASE, OGVS BOLTS AREA, 113 BOLTS, BETWEEN 7 - 11, CORROSION WAS EVALUATED, REMOVED, AND PERFORMED DVI, FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS IAW. AMM 72-33-00-206-00SDR UIEA2025030194202Case · corrodedENG 1, FWD FAN CASE, AT 6 O'CLOCK APPROX, FWD MATING FLANGE WITH SEVERAL POINTS OF CORROSION (2EA).(<P>ENG 1, FWD FAN CASE, AT 6 O'CLOCK APPROX, FWD MATING FLANGE CORROSION LEVEL 1 WERE REWORKED, EVALUATED, INSPECTED AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAWSDR UIEA2025022500162Case · corrodedENG 2, FAN CASE AREA AT 6 O´CLOCK POSITION, AROUND THE ANCHORED NUT WITH CORROSION.(<P>ENG 2, FAN CASE AREA AT 6 O´CLOCK POSITION, AROUND THE ANCHORED NUT WAS REMOVED, CORROSION LEVEL 1 WAS REWORKED, INSPECTED, EVALUATED AND ALLOWABLE LIMITS FOUND IAW AMM 72SDR SWAA2025031805856Blade · worn#1 ENGINE FAN BLADE #18 HAS CU-NI-IN COATING FLAKED/WORN BEYOND AREA X ON THE CONCAVE SIDE. #1 ENGINE FAN BLADE #18 HAS CU-NI-IN COATING FLAKED/WORN BEYOND AREA X ON THE CONCAVE SIDE. <[01] R AND R #1 ENGINE FAN BLADE #18 IAW MT 772-21-20; [02] C/W PARTS TRANSSDR VNAA2025031411103Pin · faultedEXCESSIVE N1 VIBRATION ON RH ENG. RAN QRH PROCEDURE. DID NOT CORRECT ISSUE AT NORMAL POWER SETTINGS. HAD TO REDUCE RH THRUST TO 72-73% TO KEEP VIB BELOW 1.7. / REMOVED AND REPLACED RH ENGINE FAN BLADE PINS IAW CRJ900 AMM 72-21-02-400-801-A01-PSA. PERFORMED VIBSDR YENA2025031200246Spinner · damagedFLT#2288, JFK-AMS. (ETOPS)' ON ENG # 2 SPINNER CONE SHOWS LITTLE COATING MISSING; REMOVED AND REPLACED ENG #2 SPINNER INLET CONE IAW AMM 72-11-01-400-801-A. NO DEFECT NOTED ON SPINNER, MX-4 UPDATED, PLACARD REMOVED, THIS CLEARS MDDR #576332.'SDR 2025FA0000184Case · damagedDURING ROOT CAUSE ANALYSIS WHILE PROCESSING OF A CUSTOMER COMPLAINT (202502-1029217) MTU MAINTENANCE CHECKED PREVIOUSLY REPAIRED GE90 FAN STATOR MODULES INCLUDING MODULES REPAIRED BY OTHER REPAIR STATIONS AND FOUND A DIFFERENCE IN THE APPLIED POLYSULFIDE MATESDR DALA2025021101086Seal · leakingAIRCRAFT 5027, ON DESCENT BELOW 10000 FEET, FAS NOTICED "DIRT SOCK" SMELL AND REPORTED BURNING EYES AND THROAT. CORRECTIVE ACTION: FOUND OIL IN THE RT ENG NOSE CONE. REPLACED MAIN CAP SEAL PER A321 72-11 LEAK CK GOOD. PERFORMED LEVEL B DECONTAMINATION OF THE ESDR 9WGA2025021234405Case · corrodedENG #2 FAN CASE FOUND CORROSION UNDER MID OUTER LINER SEGMENT #3. REMOVED CORROSION AT ENG #2 FAN CASE, UNDER MID OUTER LINER SEGMENT #3. FOUND WITHIN LIMITS IAW B747-400 CF6-80C2 EM GEK 92451 REV 99, 12/01/2024, ESM 72-22-01, MAT. REMOVED 0.002. AIRCRAFT APSDR 9WGA2025021234404Case · corrodedENGINE #3 FAN CASE FOUND SLIGHTLY CORROSION BETWEEN 04:00TO 06:00 O'CLOCK. REMOVED CORRSOION AT ENGINE #3 FAN CASE BTW 0400 TO 0600 O'CLOCK, MATERIAL REMOVED 0.003, IAW CF6-30C2 W/M GEK 924 51 REV. 99, 12/01/2024 CFM 72-22-01. ALODINED AND PRIMED AREA IAW B7SDR 9WGA2025021234403Case · corrodedENGINE #4 FAN CASE FOUND SLIGHTLY CORROSION AT 04:00 TO 06:00 O'CLOCK UNDER OGV #40 TO #44. REMOVED LIGHT CORROSION AT ENG #4 FAN CASE AT 04:00 06:00 O'CLOCK MAT. REMOVED 0.002, FOUND WITHIN LIMITS IAW B747-400. CFA-80C2 E/M GEK 92451 REV. 99 12/01/2024, ESMSDR HALA20250127035Blade · damagedETOPS - ENGINE #2 FAN BLADE #5 LEADING EDGE DAMAGE FOUND. REMOVED AND REPLACED ENG #2 FAN BLADE #5 PER AMM: 72-11-03. FUNCTIONAL TES (FAN BLADE BALANCE) GOOD PER AMM: 71-00-00-710-807-A. OKAY FOR SERVICE.SDR UIEA2025012100100Frame · corrodedENG 1, FAN FRAME, BTWN 4-8 O'CLOCK SURFACE WITH SEVERAL POINTS OF CORROSION.(<P>ENG 1, FLOWPATH EXTENSION BETWEEN 4 TO 8 O'CLOCK WERE REPLACED IAW AMM 72-33-00-308-104-H00 REV 144. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025011300041Case · corrodedENG 1, BTW 10-3 O'CLOCK, V-GROOVE WITH CORROSION.(<P>ENG 1, BTW 10-3 O'CLOCK, V-GROOVE WITH CORROSION. AREA WAS CLEANED. INITIALS MEASURES WERE PERFORMED. DAMAGES WERE BLEND OUT AND REWORKS WERE FOUND WITHIN ALLOWABLE LIMITS I.A.W. AMM TASK 72-33-00-206-001 RESDR UIEA2025011300040Case · corrodedENG1, FAN CASE, BTW 12-6 O'CLOCK, WITH SEVERAL POINTS OF CORROSION.(<P>ENG 1, FAN CASE, BTW 12-6 O'CLOCK, WITH SEVERAL POINTS OF CORROSION. CORROSION WAS EVALUATED IAW AMM 72-33-00-206-OOI-HOO REV 143 22AUG22, SUBTASK 72-33-00-216-011-HOO REV 143 22AUG24. CORRSDR HALA20241220375Packing · leakingETOPS - FOUND OIL STAINING @ BOTH ENG'S INLET CONE WEEP HOLES WHILE ACCOMPLISHING HAL CARD E1128-321-21-008-1. REPLACED BOTH ENGS FAN SHAFT COVERS PACKING PER AMM 72-15-00-960-801-A.LEAK CHK OK.SDR NACA2024121700001Blade · nickedLH ENGINE BLADE #9 NICK FOUND. REMOVED NICK AT LH ENG BLADE 9 AT AREA A PER AMM 72-31-02. NDT HFEC AND FPI DEFERRED.SDR QXEA2024121600315Blades · damagedON TAKEOFF ABOVE 1000' WE HAD A BIRDSTRIKE ON THE #1 ENGINE. LP VIBRATION WAS NOTED AT 4.1 OR HIGHER. NOTICABLE VIBRATION AND SOUND. FOUND DAMAGE TO MULTIPLE #1 FAN BLADES WITH EVIDENCE OF A BIRD STRIKE IN THE NACELLE & ON THE FLAP BEHIND MLG #1 SIDE. VIBRATIOSDR IPXA2024121872254Inlet · cracked*SUPPLEMENTAL SDR* R/H ENGINE INLET, INNER LIP, AT APPROXIMATE 12 O€™CLOCK POSITION, HAS 6 INCH CRACK SPANNING SEVERAL FASTENERS. REMOVED AND REPLACED R/H INLET COWL REF 767 M/M CHAP 71-11-01-404-005-H00.SDR QXEA2024120200286Blades · damagedFLIGHT 2052. REJECTED TAKEOFF ABOVE 80 KIAS AND BELOW V1. AN OBJECT ON THE RUNWAY HIT THE RIGHT SIDE OF THE AIRCRAFT, POTENTIALLY THE RIGHT MAIN LANDING GEAR. REMOVED FROM SERVICE. C/W GVI OF MLG REF AMM TASK 05-50-12-200-801. C/W BIRD STRIKE INSPECTION IAW AMSDR DALA2024112011100Seal · leakingAIRCRAFT 5035, CABIN REPORTS FUMES IN MID CABIN AND AFT. PRIOR TO TOP. SMOKE / FUMES AND REMOVAL OF FUMES COMPLETED. SMELL WAS BURNT RUBBER. CORRECTIVE ACTION: SOURCE WAS THE RT ENGINE. FOUND OIL WETTING UNDER RIGHT SPINNER. REPLACED FAN DRIVE COVER SEAL IAW PSDR HALA20241118326Packing · leakingETOPS - STRONG DIRTY SOCK SMELL AT TOD IN MAIN CABIN. NO VISIBLE SMOKE. CONCENTRATION FROM ROW 46 TO COCKPIT. LASTED INTERMITTENTLY. ODOR WAS NOTICED AFT FIRST AT TOD, THEN MOVED FORWARD TO THE FORWARD FLIGHT ATTENDENT SEATS. DID NOT NOTICE SMELL IN THE FLIGHTSDR GTIA2024111838526Cone · leakingFA REPORTED A "DIRTY SOCK" SMELL IN THE REAR OF THE A/C ( PACKS - A320 WITH MOD. 30626/MP K6443 (ENHANCED ECS) OR A321 WITH MOD. 157080/MP K17996 (PACK FLOW SELECTOR) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) )-PER TSM 05-50-00-810-831A & AMM 72-11-01-220-8SDR QXEA2024110500257Blades · damagedFLIGHT 2248. DURING TAKE OFF ROLL HIT A BIRD ON THE LEFT ENGINE. DECLARED EMERGENCY WITH ATC AND RETURNED TO THE FIELD. LANDING UNEVENTFUL. FIRE DEPARTMENT MET AIRCRAFT AS PRECAUTION. FOUND EVIDENCE ABOUT BIRD STRIKE ON ENG #1. SEVERAL FAN BLADES DAMAGED. REMOSDR DALA2024102410390Seal · leakingSHIP 5005 - SMOKE/ODOR EVENT - ON APPROACH, FLIGHT CREW REPORTED DIRTY SOCK SMELL IN COCKPIT. O2 MASKS DONNED AND EMERGENCY DECLARED. CORRECTIVE ACTION: WORKING THROUGH NOGO ODI WORK CARD. OIL LEVELS CHECKED NORMAL, NO OIL WETTING FROM APU. FOUND WETTING UNDERSDR DXTA2024102100894Blades · lack of lubeRIGHT ENGINE ENGINE VIBRATION: VIBRATION FELT AND HEARD DURING CLIMBOUT. RIGHT ENGINE FAN VIB WAS 3.0, AMBER COLOR. QRH RAN. FELT NO VIBRATION IN FLIGHT CONTROLS. FLIGHT ATTENDANT HEARD LOUD NOISES AND VIBRATION FROM THE CABIN. CORRECTIVE ACTION; REMOVED & CLSDR DALA2024100909868Shim · damagedSHIP 1817 -DIV- CREW REPORTED #2-ENGINE HIGH N1 VIBES IN FLIGHT. CORRECTIVE ACTION: FOUND #32 FAN BLADE SHIM DAMAGED. REPLACED SHIM AND LUBED FAN BLADES. ALL CHECK NORMAL. (6629804)SDR FDEA202409111297Intercostal · crackedEMPENNAGE: FROM #2 ENG INTAKE DUCT ACCESS PANEL FOUND RIGHT HAND INTERCOSTAL AFT EDGE CRACKED (LENGTH :1 INCH) BETWEEN STATION 2161 REAR CENTER SPAR TO REAR SPAR. EMPENNAGE RIGHT HAND INTERCOSTAL AFT EDGE BETWEEN STATION 2161 REAR CENTER SPAR TO REAR SPAR SDR VNAA2024090911101Pin · unserviceableENGINE FAN "LEFT" VIB 2.9 AT FL330 RAN QRH VIB DID NOT DECREASE BELOW 1.8 UNTIL AT FL250 WITH REDUCED THRUST / REMOVED BLADE PINS IN LH ENG DUE TO HIGH VIBES. REPLACED LH ENG BLADE RETAINING PINS IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA. PERFORMED LH ENGINSDR DALA2024090308652Packing · leakingAIRCRAFT 5003, DIRTY SOCK SMELL FROM VENTS ON DESCENT INTO LAX THROUGH LANDING. CORRECTIVE ACTION: FOUND #1 AND #2 ENGINE OIL WETTING FROM BACK OF SPINNER. DUE TO TYPE 2 AND 3 CORRECTIVE ACTIONS PERFORMED ECS DECONTAMINATION PER WC 2100-2003 AND A321 AMM 21-00SDR CALA2024090302366Fairing · missingRIGHT WING EXTERNAL INSPECTIONS {B777-06-3-7157} - NO. 2 ENG NO. 6 FAN BLADE FAIRING HAS APPROX 12" OF SEAL MISSING. SEE PIC. HOURS OR LESS. REQUEST DIP. REF AMM 72-31-07-200-801-N00 MATERIAL MISSING FOR MORE THAN 0.400 INCH (10.160 MM) IN LENGTH.REPLACE THE FSDR DXTA2024071612363Blade · damagedAIRCRAFT WAS SALAMMED BY CRICKETS AND GRASSHOPPERS. FUNNY SMELL AIRBORNE WITH A BURNT INSECT SMELL, LIKE POPCORN. CHIPS APPEAR IN THE FAN BLADE.SDR DALA2024070706830Blades · damagedSHIP 1810 - DIV FLIGHT 0131 MUC-ATL DIVERTED TO CDG DUE TO RIGHT ENGINE HIGH VIBRATIONS AFTER TAKE OFF. CORRECTIVE ACTION: REMOVE AND REPLACED DAMAGED FAN ROTOR BLADE (PAIRS) #13 AND #32, #14 AND #33, #15 AND #34, #16 AND #35. (6194101)SDR SWI2024F00491Spinner · dentedRAMPER FOUND DENT ON LEFT SIDE JUST AFT OF NOSE CONE INSPECTED DENT FOUND TO BE 2.5" LONG BY 1" WIDE BY .048" DEEP AT THE DEEPEST POINT WITH NO CREASES. NO DAMAGE FOUND IN HYDRAULIC COMPARTMENT OR BEHIND RADOME. DAMAGE IS OUT OF LIMITS PER CRJ 900 SRM 53-00-01SDR HALA20240610156Blade · damagedETOPS - WHILE REMOVING # 1 ENGINE # 19 BLADE, FOUND # 18 FAN BLADE S/N: LAEDAS9430 DAMAGED/CRACKED AT ROOT. REMOVED AND REPLACED DAMAGED FAN BLADE S/N LAEDA59430 PER AMM 72-11-03. FAN TRIM BALANCE OKAY. OK FOR SVC.SDR NACA2024061200001Blade · damagedDURING CLIMB, LEFT ENGINE N1 VIBE REACHED 3.0. AT TOP OF CLIMB, ENG N1 REACHED 5.0. LASTED 6-7 MINUTES UNTIL TOP OF DESCENT. VIBRATION FELT IN COCKPIT. PERFORMED FIM 71-05FT 806 STEPS 1-4 NO DEFECTS NOTED. BORESCOPE REQUIRED. BORESCOPE FOUND HPC # 5-7 DAMAGED SDR QEMY20240624001Spool · corrodedINCOMING CONDITION HIGHLIGHTED DURING THE INSPECTION PROCESS. THE BOOSTER SPOOL HAS FRETTING ON SURFACE A (MORE THAN AMM & ESM LIMITS). KNOWN CONDITION. DR#01983965 WAS NOT APPROVED. FIRST TIME EXPOSURE OF THIS AREA FROM NEW MAKE. SERVICE RUN CONDITION, NOT A SDR VNAA2024053111101Blade · unserviceableLEFT ENGINE HIGH VIBES ON TAKEOFF. 2.0 MAX. COULDNT ADVANCE THRUST ABOVE IDLE WITHOUIT HIGH VIBES RETURN TO FIELD / REMOVED AND REPLACED FAN BLADE PINS FOR LH ENG IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA. OPS CHECK GOODSDR AALA202405295728Panel · missingAIRCRAFT WAS GROUNDED: AFTER ARRIVAL AT LAX THE FLIGHT CREW FOUND THE INBOARD LOWER VBV LOUVERED PANEL AT THE 5 O'CLOCK POSITION MISSING ON THE LEFT HAND ENGINE BYPASS DUCT / FAN CASE. MAINTENANCE NOTED DAMAGE TO THE INBOARD C DUCT AND INBOARD FLAP WHICH WAS RSDR 2DYA202405080128Engine · failedFAILED BSI IAW ASB RB211-72-AL 102, EO 767-72-0015 AD 2024-07-04 EASA 2024-0069.SDR IPXA2024070855351Nose Cowl · crackedENGINE #2 NOSE COWL FRON SIDE, LIP WITH CRACK IN POSITION 10 HRS, APROX 0,5 INCH DOT 108-110. INSTALLED DOUBLER AND FILLER ON AREA OF #2 NOSE COWL FRONT SIDE, I.A.W. PWA SRM 54-10-00, FIGURE 204.SDR 2024FA0000340Blade · damagedSAE GENNEVILLIERS REPAIR SHOP HAS IDENTIFIED A POTENTIAL NON CONFORMANCE ON 2 REPAIRED FAN BLADES DELIVERED TO SAESM. THE NON CONFORMANCE IS A POTENTIAL MISS OF PERFORMING A LOCAL ETCHING ON A PRESSURE FACE OF THE BLADES ACCORDING TO SUBTASK ESM 72-21-01-220-0SDR 2024FA0000339Blade · damagedSAE GENNEVILLIERS REPAIR SHOP HAS IDENTIFIED A POTENTIAL NON CONFORMANCE ON 2 REPAIRED FAN BLADES DELIVERED TO SAESM. THE NON CONFORMANCE IS A POTENTIAL MISS OF PERFORMING A LOCAL ETCHING ON A PRESSURE FACE OF THE BLADES ACCORDING TO SUBTASK ESM 72-21-01-220-0SDR DALA2024041304393Seal · leakingAIRCRAFT 5014, DIRTY SOCK SMELL ON TAXI IN. CORRECTIVE ACTION: REPLACED FAN SHAFT COVER SEAL. COMPLIED WITH ECS CLEAN AND BURN OUT, NOT SMELLS NOTED. (LP 4179769)SDR YENA2024041600554Blade · unknownDURING HEAVY MAINTENANCE: ENGINE - PW1133GA-JM - ESN P771638 - LOW EGTM / HPT BLADE FINDINGS - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
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