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 DALA2024041304396Cover · leakingAIRCRAFT 8139, AFTER TAKEOFF FROM SFO REAR FLIGHT ATTENDANTS REPORT BAD MOLDY FLOOR SMELL. ZERO EVIDENCE IN FLIGHT DECK. SOURCE UNDETERMINED MULTIPLE FLIGHT ATTENDANTS SMELLED IT CONCENTRATED IN BACK OF THE PLANE - NOTICED SMELL IN FLIGHT DECK AFTER BIG POWER SDR HALA20240401017Blade · damaged#5 FAN BLADE #2 ENGINE MAJOR DAMAGE. REMOVED #2 ENG BLADE SET PER AMM72-38-15. 17601 3-29-24 PERFORMED INSPECTION OF #2 ENGINE FOR FOD PER AMM 72-00-00--200-809. INSTALLLED #2 ENGINE BLADE ASSEMBLY PER AMM 72-38-15.SDR I5PA2024030968802Blade · out of limitsFLT: N/A (MX INSP). ESI - L ENG #8 FAN BLADE NICK OUT OF LIMITS, REQ'S REPLACEMENT. R/R #8 FAN BLADE PER AMM 72-31-02.SDR I5PA2024030968801Blade · out of limitsFLT: N/A (MX INSP). ESI - L ENG #26 FAN BLADE NICK OUT OF LIMITS, REQ'S REPLACEMENT. R/R #26 FAN BLADE PER AMM 72-31-02.SDR NACA2024021500001Blade · cracked#1 ENG #28TH BLADE HAS A 3.968 MM CRACK ON THE LEADING EDGE AREA F SURFACE, 8" FROM THE PLATFORM BASE. PERFORMED 1ST STAGE FAN BLADE REPAIR ON #1 ENG #28 BLADE PER AMM 72-31-02, PERFORMED FLUORESCENT PENETRANT INSPECTION, OK FOR SERVICE FINAL DEPTH 4.783 MMSDR NACA2024021000003Blade · damagedRIGHT ENGINE #25 BLADE SHOWS DAMAGE . BLENDED DAMAGE ON RIGHT ENGINE #25 BLADE IAW CF6-80. BLEND IS WITHIN LIMITS IAW AMM 72-31-02SDR VNAA2024021211101Pin · unserviceableINSPECTED LH FAN BLADES FOR STIFFNESS, NO DEFECTS FOUND, VIBE CHECK GOOD IAW CRJ 900 AMM 72-21-02-200-803-A01. HIGH TORQUE PIN T/S DUE WITHIN 15 CYCLES. / REMOVED AND REPLACED LH ENGINE FAN BLADE PINS IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA. PERFORMED VIBSDR NACA2024012100002Spinner · crackedRIGHT ENGINE SPINNER FOUND WITH CRACKS AROUND MOUNTING BOLT HOLES. REMOVED AND REPLACED RIGHT ENG CONE SEGMENT INLET IAW AMM 72-31-04SDR HALA20240116018Unknown · unknownETOPS - DURING WALK-AROUND INSPECTION FOUND DAMAGE ON #1 ENGINE FAN BLADE (LABELED #1). REMOVED AND REPLACED #1 ENGINE #1 FAN BLADE PER A330 AMM 72-31-41-400-801-A OPS CHECKS OK PERFORMED #1 ENGINE IDLE RUN, NO DEFECTS NOTED A/C OK FOR SERVICESDR 2DYA202405080130Engine · failedFAILED BSI IAW ASB RB211-72-AL 102, EO 767-72-0015 AD 2024-07-04 EASA 2024-0069.SDR 2DYA202405080129Engine · failedFAILED BSI IAW ASB RB211-72-AL 102, EO 767-72-0015 AD 2024-07-04 EASA 2024-0069.SDR FDEA202312201949Blade · damagedAFTER AIRBORNE PASSING APPROXIMATELY 2500 FEET DURING THE CLIMB OUT, WE NOTICED VIBRATION BEGIN ON THE AIRCRAFT. IT CONTINUED TO WORSEN AND STABILIZED WITH THE RIGHT ENGINE EVM SHOWING 4.8 AT CLIMB THRUST WHICH WAS ABOUT 85%. REFERENCING THE APPROPRIATE SDR SWAA2023120526670Blade · damagedBIRD STRIKE ON TAKEOFF ROTATION ABNORMAL SMELL THROUGH AIR COND SYSTEM FOR 2-3 MIN NO ABNORMAL ENG INDICATION.<[01] COMPLIED WITH CFM56-7 BIRD STRIKE VISUAL INSPECTION REF MT 772-00-00. REMOVED AND REPLACED #1 #2 AND #24 FAN BLADES ON #1 ENG REF AMM 72-21-02. SDR VNAA2023111311101Pin · unserviceableREMOVED AND REPLACED PINS ON #2 ENGINE IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA/GE LMM 72-21-00 SPECIAL PROCEDURE 97 / REMOVED AND REPLACED PINS ON #2 ENGINE IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA/GE LMM 72-21-00 SPECIAL PROCEDURE 97.SDR ASAA2023110846080Spacer · debondedWHILE ACCOMPLISHING FAN LUBE #1 ENGINE, FOUND SPACERS AT POSITION 5, 7, 19, AND 22 ELASTOMERS STRIPS UNBONDED. GROUNDED - YES. REMOVED AND REPLACED ENG #1 SPACERS # 5, 7, 19, 22. REF T/C CFM56-7 FAN BLADE LUBRICATION.SDR SWIA2023112404Unknown · dentedBIRD STRIKE ON RIGHT SIDE OR NOSE CONE.INSPECTED IMPACT AREA AND FOUND DENT MEASURING 3.75"L X 2"W X 0.123"D 0.50" AFT OF FR02 BETWEEN STRG 04R AND STRG 06R RT FWD FUSELAGE AFT OF RADOME. DENT IS CREASED, NO OTHER DAMAGE NOTED. REF EAML 1241358 FOR BIRD STRIKESDR ASAA2023110145971Blade · wornFOUND EXCESSIVE WEAR / DAMAGE ON MULTIPLE FAN BLADE PLATFORMS ON #1 ENGINE. GROUNDED - YES. REF W/O 1969863REF T/C SBCFM56-7B-72-1033-1. REMOVED AND REPLACED ALL FRAN BLADE PLATFORMS DURING FAN LUBE T/C ON #1 ENGINE. PERFORMED ENGINE POWER RUN TEST #7 REF AMM SDR ASAA2023103145959Blade · damagedWHILE ACCOMPLISHING FAN LUBE FOUND 8 PLATFORMS WORN/DAMAGED. GROUNDED - YES. REPLACED 8 PLATFORMS WHILE PERFORMING TASK CARD 78472010.SDR 2023FA0000680Unknown · unknownFOUND GOUGE AND DEEP NICKDAMAGE ON ENGINE #1 INLET COWL ACOUSTIC PANEL LOWER SEGMENT.SDR NACA2023101700001Spinner · crackedDURING WALKAROUND FOUND EVIDENCE OF A CRACK, #2 ENGINE SPINNER. REMOVED AND REPLACED #2 ENGINE FAN ROTOR SPINNER IAW B767 AMM 72-31-01. PART UNKNOWN TO TRAX.SDR ASAA2023101245590Platform · damagedPER T/C 78472010 #1 ENG FAN BLADE LUBE . PLATFORMS #8,11 AND 24 SEALS ARE TORN. GROUNDED - YES. REPLACED PLATFORMS 8,11 AND 24 DURING COMPETION OF T/C 78472010.SDR SWAA2023101309856Skin · cracked#2 ENG INLET COWL LOWER LIP SKIN HAS A CRACK AT 6 OCLOCK POSITION.<[01] REMOVED AND REPLACED #2 ENG NOSE COWL PER AMM 71-11-01SDR U2RA2023101400045Liner · missingDURING A SCHEDULED A-CHECK VISIT, DAMAGE WAS FOUND TO THE #4 ENGINE OUTBOARD THRUST REVERSER. FURTHER INSPECTION REVEALED THE #4 OUTER FAN EXIT LINER SEGMENT HAD DETACHED FROM THE FAN CASE RING AND DEPARTED THE AIRCRAFT. SUBSEQUENT C-DUCT DAMAGE WAS REPAIRED ASDR 15DA2023100973501Unknown · unknownENGINE START AND TAXI WERE BOTH NORMAL IN GROUND IDLE. UPON ACCELERATION AND ROTATION IN FLIGHT IDLE, A DISTINCT SMELL OF "BURNING RUBBER" WAS NOTICED THAT PROGRESSIVELY GOT WORSE OVER THE NEXT 10 SECONDS. AT APPROXIMATELY 500 FEET, THE PILOT ELECTED TO DECLARSDR ASAA2023100845483Spacer · debondedPER T/C 78742010 #2 ENGINE FAN BLADE LUBE. #7 AND #10 SPACERS ARE DISBONDED. GROUNDED - YES. REMOVED AND REPLACED #2 ENG FAN BLADE #7 AND #10 SPACERS REF T/C 78472010.SDR ASAA2023100845482Spinner · wornPER T/C 78472010 #2 ENGINE FAN BLADE LUBE. REAR SPINNER CONE WASHERS ARE WORN. 12 WASHERS. GROUNDED - YES. REMOVED AND REPLACED REAR SPINNER CONE WASHERS REF T/C 78472010.SDR ASAA2023100845481Spinner · wornPER T/C 78472010 #2 ENGINE FAN BLADE LUBE. CONE FRONT SPINNER WASHERS ARE WORN. SIX WASHERS. GROUNDED - YES. REMOVED AND REPLACED FRONT CONE SPINNER WASHERS REF T/C 78472010.SDR ASAA2023100345439Unknown · unknownNICK ON THE #2 ENG FAN BLADE #10. GROUNDED - YES. FOUND #2 ENG BLADE #10 IN AREA K TO HAVE A BLADE TEAR REF B737-800 AMM 72-21-02-200-801-F00 SECTION K(1)(H), REQUIRES BLENDING REPAIR PER AMM TASK 72-21-02-300-801-F00. BLENDED #2 ENG BLADE #10 IN REF TO AMM 72SDR ASAA2023093045379Blade · damagedPER TC # 78472010, FAN LUBE FOUND FAN BLADES DAMAGED BEYOND LIMITS ALONG CONTACT POINTS WITH PLATFORM SEALS #2 ENGINE. GROUNDED - YES. DURING #2 ENGINE FAN LUBE REPLACED 6 PLATFORMS, AND REPLACED BLADES WITH SERVICEABLE.SDR SWAA2023092905412Skin · corrodedRIGHT ENGINE INLET HAS CORROSION ON BARREL SKIN AFT CHORD AND FORWARD OF FAN COWL LANDINGS. SEE ATTACHED PHOTOS.<[01] MEASUREMENTS ONLY;[02] INSTALLED INLET COWL PER AMM 71-11-01.;[03] INSTALLED INLET COWL PER AMM 71-11-01;[04] C/W STEP 3.SDR CALA2023092002829Spinner · unknownR ENG VIBRA 3.3 CLIMBING TO 380 MOD TURB AND ICE.KEPT ENG AT REDUCE SETTING DIVERTDEN ATTACHED PIC OF WHAT CREW REPORTED. ALSO FLAGGED FOR SDR AUTO AND MAN EVENT PICTURES ADDED. SEE ATTACHED PHOTO FOR VIB REF ADDITIONAL LOG PAGES 5788441 AND 5787996. ACP VIBRASDR J6B202406100002Case · gougedEVAL GOUGED RT ENG FAN CASE AT 12 OCLOCK POSITION JUST FWD OF FAN CASE BOLTS (C-CHECK RO 11/16/2023) PERFORMED REPAIR OF GOUGED RT ENG. FAN CASE AT 12 OCLOCK POSITION IAW CRJ-200 REO 601R-71-61-4364. REV. -- DATE: 2023-10-12. PERFORMED NDT ET/UT INSPECTSDR SWI2024F00441Case · gougedEVAL GOUGED RT ENG FAN CASE AT 12 OCLOCK POSITION JUST FWD OF FAN CASE BOLTS (C-CHECK RO 11/16/2023) PERFORMED REPAIR OF GOUGED RT ENG. FAN CASE AT 12 OCLOCK POSITION IAW CRJ-200 REO 601R-71-61-4364. REV. -- DATE: 2023-10-12. PERFORMED NDT ET/UT INSPECTSDR ASAA2023091645180Spinner · worn#2 ENGINE FWD SPINNER CONE MORE THAN 50% WORN. GROUNDED - YES. REPLACED AS REQUIRED PER TC 78472010#2 ENGINE FWD SPINNER CONE.SDR ASAA2023083044859Blade · degradedBLADE MAPPING SOULTION REQ'D BLADES: #3, #6, #11, & #15 TO BE CHANGED OUT WITH NEW FOR WORKABLE WEIGHT MOMENTS. ( ALSO SEE LOG'S: 60645296 & 60645297 ). GROUNDED - YES. SWAPPED OUT BLADES WITH NEW: #3, #6, #11, & #15 AS REQUIRED. REF AMM 72-21-02.SDR ASAA2023083044858Blade · degradedWHILE ACCOMP T/C'S: SBCFM56-7B-72-1033 & 78472010; REQ CHANGE OF: BLADES #1, #11, #13, & #23 + 14 PLATFORMS + 14 SPACERS. GROUNDED - YES. REPLACED BLADES: #1, #11, #13, & #23 + 14 PLATFORMS + 14 SPACERS WITH NEW. REF AMM 72-21-02.SDR ASAA2023082944857Blade · failed insp#2 ENGINE #22 FAN BLADE FAILED ULTRASONIC INSP. GROUNDED - YES. INSTALLED NEW FAN BLADES AT 2 POSITIONS 22 AND 10 IAW T/C 78472010.SDR ASAA2023082844817Spacer · degradedDURING NO.2 ENGINE FAN LUBE TASK CARD 78472010; 2 PLATFORMS, AND 14 SPACERS REQUIRE REPLACEMENT. GROUNDED - YES. REPLACED 2 PLATFORMS, AND 14 SPACERS REF NO.2 ENGINE FAN LUBE TASK CARD 78472010.SDR ASAA2023082744791Spinner · eroded#2 ENGINE SPINNER WHITE PAINT ERODED. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE SPINNER CONE PER TC 78472010.SDR ASAA2023081844815Blade · degraded#2 ENGINE TREND DATA STILL SHOWS A RISE IN LOW PRESSURE ROTOR VIBRATION LEVELS WITH FAN SCATTER. (#PRI2/ETOPS)CNR 20230817065. TASK CARD 78472010. GROUNDED - YES. C/W TSR VIBES WITHIN LIMITS REPLACED 5 PLATFORMS.SDR 2023FA0000412Screen · debondedPROTRUDING WIRE MESH AND PARTIAL DAMAGE TO THE FWD AND AFT EDGES OF THE ACOUSTING MESH ON INNER BARREL OF RH INLET ASSEMBLY. REPAIR WAS ACCOMPLISHED WITH GKN TECHNICAL VARIANCE TV00122895 REV H, ISSUE 2 DATED 07/12/2021.SDR ASAA2023080344402Blade · corroded#19 BLADE #1 ENG IS PITTED IN AREA H, PLATFORM SEAL RUB AREA, OUT OF LIMITS. GROUNDED - YES. REPLACED #7 AND 19 FAN BLADES REF AMM 72-21-02 AND T/C 78472010.SDR ASAA2023072944318Platform · damaged#1 ENGINE TREND DATA SHOWS A RISE IN LOW PRESSURE ROTOR VIBRATION LEVELS. TASK CARD 78472010. GROUNDED - YES. WHILE ACCOMPLISHING T/C CFM 56-7 FAN BLADE LUBE FOUND NO IRREGULARITIES IN THE FAN. FOUND EXCESSIVE LUBE, FOUND MULTIPLE DAMAGED PLATFORMS, FOUND MULTSDR SIMA20230726001Unknown · unknownON CLIMB OUT APX FL230, HIGH LP VIBRATION 4.0. WENT BACK TO GREEN ON DESCENT BUT STILL ELEVATED ON LANDING IN REVERSE THRUST, WENT BACK TO AMBER DECLARED EMERGENCY-C/A-RAR # 2 ENGINE FAN BLADE PINS IAW EA72-00-00-013 W/C. OPS CHECK GOOD. NO FURTHER DEFECTS NOTSDR ASAA2023071043965Spinner · damagedFRONT SPINNER CONE PAINT MISSING OVER 50%. GROUNDED - YES. REPLACED FRONT SPINNER CONE REF AMM 72-21-01.SDR ASAA2023070343880Spinner · damaged#2 ENGINE FORWARD SPINNER MISSING MORE THAN 50% ANODIZED COATING. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE FORWARD SPINNER CONE REF AMM 72-21-01.SDR ASAA2023062443729Unknown · unknownPERFORMED ENG RUN VIB SURVEY AS REQUESTED BY TSR14495, #2 ENG WAS FOUND TO BE OUT OF VIB LIMITS AT 64% N1 IN REF TO AMM 71-00-00 TEST 7. GROUNDED - YES. SPINNER WEIGHTS MOVED AFTER COMPLETION OF TEST 7 AND AC ENG RUN TEST 7 PERFORMED AGAIN. HIGHEST VIB WAS 1.4SDR ASAA2023062443716Spinner · wornFOUND #2 ENG SPINNER RQD RPLCMNT. GROUNDED - YES. RMVD REPLACED #2 ENG SPINNER REF T/C 78472010.SDR ASAA2023061943636Spinner · erodedDURING #2 ENGINE FAN LUBE ASA TASK CARD 78472010 FRONT SPINNER CONE EROSION BEYOND LIMIT. GROUNDED - YES. REPLACED FRONT SPINNER CONE #2 ENGINE REF ASA TASK CARD 78472010.SDR ASAA2023060543686Blade · damagedPILOT REPORTS PAINT MISSING ON AFT SIDE OF #2 ENGINE FAN BLADE, BLADE #3. GROUNDED - YES. FOUND MISSING PAINT OF #2 ENGINE, BLADE #3, TO BE WITHIN LIMITS. DEFERRED PER AMM 72-22-02 STEP S(8), FOR A ONE-TIME CONTINUE-IN-SERVICE APPLICATION OF 100 FLIGHT CYCLES.
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