JASC 7220
Service difficulty reports · 1,718
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 SWAA2026101996044Engine · bird ingestionBIRD STRIKE NR 2 ENGINE, ODOR, NO ABNORMAL INDICATIONS. ODOR WENT AWAY AFTER 30 SECONDS. REMOVED & REPLACED NR 2 ENGINE SURFACE AIR / OIL COOLER IAW AMM 79-21-02. REMOVED AND REPLACED OGV PLATFORMS UPPER RIGHT SIDE IAW AMM 72-21-09.SDR SWAA2026101659349Acoustic Panel · delaminatedNR 1 ENGINE FAN, AFT ACOUSTIC PANEL DELAMINATED BTWN NR 4 & 5. R & R IAW AMM 72-23-02-401.SDR SWAA2026101656194Acoustic Panel · delaminatedNR 1 ENGINE FAN, FRAME AFT ACOUSTIC PANEL DELAMINATED BTWN NR 5 AND 6 FAN FRAME STRUTS. REMOVED AND REPLACED IAW AMM 72-23-02-401.SDR SWAA2026101659487Acoustic Panel · delaminatedNR 1 ENGINE FAN, FRAME AFT ACOUSTIC PANEL DELAMINATED BTWN NR 7 & 8 FAN FRAME STRUTS. REMOVED AND REPLACED IAW AMM 72-23-02-401.SDR HNAA2026100200942Seal · leakingBURNING ODOR IN FLIGHT DECK. NO EICAS MSG. REMOVED FAN SPINNER IAW 72-21-20-000-801, REMOVED FWD RETAINER IAW 72-21-30-000-801, REMOVED FAN BLADES IAW 72-21-15-000-801, REMOVED FAN SPINNER LOCK NUT PLUG IAW 72-21-05-000-801. INSTALLED TEFLON LIP SEAL IAW EMM SDR AALA202609258964Check Valve · crackedAIRCRAFT WAS GROUNDED: ENGINE 1 STALL MESSAGE ON ECAM AT BEGINNING OF DESCENT FROM FL360 - THE ENGINE RECOVERED ITSELF WITHIN A FEW SECONDS AND THE ENGINE OPERATED NORMALLY FOR REMAINDER OF THE FLIGHT - MAINTENANCE THE INLET PRESSURE CHECK VALVE HAD 2 CRACKED SDR DALA2026092405335Blades · dentedFOUND TWO BLADES DENTED ON NR 2 ENG. FOUND BLADES 29 AND 30 DENTS TO BE OUT OF LIMITS IAW AMM 72 -21-00-320-001-Q, DAMAGE EXCEEDS A DEPTH OF 1 INCH IN SECTION D INTO SECTION C. REROMVED SPINNER FRONT & REAR CONE IAW AMM 72-21 REMOVED AND REPLACED THE FAN BSDR YENA2026091400799Guide Vane · damagedFLT # 324, LAX-JFK. (ETOPS) NR 1 ENG SGV INNER LINER MISSING SMALL PIECE @ BETWEEN 7 - 9 O'CLOCK POSITION.SDR AALA202608272328Blade · contaminatedAIRCRAFT WAS GROUNDED: FUMES REPORTED IN CABIN. ONCE ON CLIMB OUT BUT DISAPPEARED QUICKLY. NO FUMES DURING CRUISE. FUMES RETURNED ON DESCENT AND WERE STRONG. ACCOMPLISHED QRH AND TURNED #2 PACK SWITCH OFF AND FUMES DISSIPATED. NOTE: BOTH FUMES EVENT WERE SDR AALA202608134744Engine · damagedAIRCRAFT WAS GROUNDED: BIRD STRIKE ON TAKEOFF RESULTING IN ENGINE FAILURE DUE TO SEVERE DAMAGE ON ENGINE #1. ENGINE SHUT DOWN AND PLANE RETURNED AND LANDED AT MYR. MULTIPLE FAN BLADES DAMAGED. SEVERE VIBRATIONS. OIL ON OUTSIDE OF ENGINE. BIRD STUCK IN LEFT MAISDR CALA2026081318568Blades · damagedACFT DIVERTED TO CUN FROM RTB DUE ENG 1 BIRD STRIKE. ENG 1 PRELIMINARY INSPECT 2 AFT ACOUSTIC PANELS REPLACED IAW AMM 72-21-08/401 AND 5 OGV PLATFORMS REPLACED IAW AMM 72-21-09/401, ALL OK. FAN BLADE 9. R & R IAW AMM 72-22-02-960-802-G00, OPS CHKD IAW AMM 71-SDR SIMA20260808003Engine · vibrationNR 2 ENG HIGH VIBRATION AT 4.0. NOTICED AFTER 80KTS. STAYED AT 4.0 IN AMBER. LEVELED AT 12000FT TO RUN QRH. AFTER RUNNING QRH STEPS ENG REMAINED 4.O - 4.2 AS WELL AS BEING ABLE TO FEEL A VIBRATION FROM THE ENG2 SIDE. ENG 2 DID RETURN TO GREEN WITH REDUCED THRUSDR YENA2026080700656Seal · leakingFLT 220, SAN-BOS. (ETOPS) FOUND OIL IN SPINNER OF # 2 ENG; REMOVED & REPLACED FAN SHAFT COVER SEAL IAW AMM 72-15-01, SEE DEFECT 4556649 FOR LEAK AND OPS TEST.SDR AALA202608039467Blade · bentAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INTO PHL DUE TO THE FLIGHT CREW REPORTING HIGH ENGINE VIBRATION DURING TAKEOFF ROLL FOLLOWED BY ENGINE 1 HIGH VIBRATION ECAM - SLOWLY REDUCED OVER TIME FROM 8 TO 3.3 BUT WOULD INCREASE WITH REDUCTION IN THRUST -SDR DALA2026073004423Seal · damagedDURING CLIMBOUT, NR 2 ENGINE REACHED V.I. 4.4 WITH IN AT 95. COMPLIED WITH QRH DISCONNECTED AUTO THROTTLE REDUCED NR 2 ENG TO BELOW 4.0VUB AND OPERATED REST OF FLIGHT AT REDUCED POWER. PERFORMED NR 2 ENG FAN LUBE IAW W/C7221-6127 FOUND PLATFORMS 18, 8, & 7 SESDR CALA2026071717847Spinner · missingPDA 1 PDA 1 ON ARRIVAL FOR #2 ENG SPINNER CONE DEPARTED PIECE IS TRAPEZOIDAL MEASURING 13 INCHES ON THE TRAILING EDGE 8 INCHES ON THE LEADING EDGE AND 11 INCHES ON THE SIDES SEE PICTURE REF LOG PAGE 9567803 FOR ENGINE VIBE SOURCE OF DIVERSION/ ENGINE REPLACEMSDR DALA2026070603927Engine · bird ingestionATB- RETURNED TO DUB DUE TO LEFT ENGINE BIRD STRIKE. C/W BIRD STRIKE INSPECTION PER AMM. REPAIRED FAN EXIT GUIDE VANE PER AMM 72-33. C/W LEFT ENGINE BORESCOPE INSPECTION, NO DAMAGE FOUND. C/W POWER ASSURANCE RUN, NO ISSUES NOTED. (LP 8776550 - AIRCRAFT WAS GRSDR CALA2026063017473Acoustic Liner · damagedDURING ENGINE NR 1 WASH, NOTED ON ACOUSTIC OUTER PANEL DAMAGED. AT 3 O'CLOCK POSITION. CONFIRMED DAMAGE AT ACOUSTIC OUTER PANEL DAMAGED ABOUT 3 O'CLOCK, MEASURING 18.5"LENGTH X 4.5"WIDE X 1" DEEP. DAMAGE NOT COVERED BY SRM LIMITS. REF AMM DMC-B787-A-G72-21-01SDR CALA2026063017468Guide Vane · damagedDURING NR 1 ENGINE WASH, NOTED A 10TH OGV DAMAGED. CONFIRMED 10TH OGV DAMAGED WITH A CRACK MEASSURING 2 INCH. REPLACED AS REQUIRED, AS REFERENCE AMM DMC-B787-A-G72-21-03-01A-520A-A FOR REMOVAL AND AMM DMC-B787-A-G72-21-03-01A-720A-A FOR INSTALLATION. NO FURTHSDR REXA2026062400975Engine · bird ingestionBIRD INGESTED ON CLIMB OUT R ENG DEGRADED FAN VIB 9.9 FOLLOWED QRH VIB CONTINUED EVENTUALLY R ENG FLAME OUT RAN EMER CHECK FOR SEVERE ENGINE DAMAGE. REMOVED AND REPLACED RT ENG ASSY IAW JOBCARD 900-72-430-902 OPS CHECK GOODSDR CALA2026060816880Guide Vane · missingNR 1 ENGINE OTBD APPROXIMATELY 7 O ,CLOCK POSITION NEXT TO ENGINE OIL COOLER HAVE 2EA OUTLET GUIDE VANE OUTER PLATFORM MISSING.. INSTALLED 2EA OGV PLATFORM ON NR 1 ENG OTBD APPROX 7 O' CLOCK NEXT TO ENGINE OIL COOLER. IAW AMM 72-21-09-400-801-G00.SDR DALA2026052903275Engine · failedSHIP 3833 -ATB/IFSD/DE- DUE TO RIGHT ENGINE FAILED DURING CLIMB. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT ENGINE ON LOG PAGE 1612033 IAW AMDS W/C 7100-4423 RH. (LOG 8288268 - AIRCRAFT WAS GROUNDED).SDR CALA2026042815809Panel · missingFOUND MISSING ONE FAN STATOR BLANK OFF PLATE AND THREE (3) CAPTIVE BOLTS ON ENGINE NR 1, RT SIDE, APPROXIMATELY AT 3?4 O`CLOCK POSITION PERFORMED GVI ON THE ENG IAW AMM DMC-B787-A-G72-00-00-14A-311A-A, NOTHING ABNORMAL WAS FOUND AT THE ENGINE, TEST FROM THE NUSDR DALA2026042302606Acoustic Liner · damagedDURING SERVICE CHECK FOUND DAMAGE IN #1 ENG INLET COWEL ACOUSTIC LINER. REPAIRED DAMAGE IN #1 ENG INLET COWEL ACOUSTIC LINER PER B717 SRM 54-10-01 (7985278) (AIRCRAFT GROUNDED)SDR AALA202604218663Blade · damagedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING CLIMB AROUND FL270 NUMBER 1 ENGINE STARTED TO EXPERIENCE HIGH VIBRATION (5 UNITS) AND SURGING. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MCO. DURING POST FLIGHT FOUND PIECE MISSING BETSDR UIEA2026040500127Fan · vibrationDURING CLIMB, RIGHT ENGINE FAN VIBRATION REACHED 4.3. DURING CRUISE, VIB 0.8. PERFORMED BLADE LUBE PER AMM 72-31-02. SPINNER RE-TORQUED PER AMM 72-31-01. TRIM BALANCE AND VIBRATION SURVEY PER AMM 72-31-00. #1 BEARING CHECKS GOOD. N2 VIBE AT POWER 2.0, FAN VISDR QEMY20260316001Spool · corrodedBOOSTER SPOOL ASSY, THE SUBJECT BOOSTER SPOOL ASSY HAS FRETTING ON SURFACE B 0.005” IN DEPTH. THERE IS NO INSPECTION CRITERIA TO ACCEPT THIS IN 72-21-04. DR 02369450 STATES THERE IS NO REPAIR SOLUTION FOR THIS FINDING AND IS BEYOND ACCEPTABLE LIMITS FOR CFM TSDR SWAA2026030275464Scupper · fireGROUND CREW OBSERVED FLAME COMING FROM SCUPPER VENT ON NR 1 ENG. USED RAMP FIRE EXTINGUISHER TO EXTINGUISH. PERFORMED CLEANING AFTER DRY CHEMICAL FIRE EXTINGUISHER USED ON #1 ENG SCUPPER VENT AND NO DAMAGE FOUND AT THIS TIME PER AMM 05-51-95 AND EA M-23-172-0SDR VNAA2026021412201Pin · damagedLEFT ENG VIBRATION, 1.8 AT 87 N1, FL 330. RAN QRH VIBRATION INCREASED 2.1 DIVERTED TO ATL. REMOVED AND REPLACED THE FAN BLADE PINS IAW AMM 72-21-02-400-801-A01-PSA.SDR R61A2026020500034Blade · damagedBIRD STRIKE ON TAKEOFF – BLOOD IN ENGINE – ENGINE 1 LP HIGH VIBRATION – MULTIPLE BENT FAN BLADES. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. C/W BIRD STRIKE INSPECTION. REMOVED AND REPLACED #1, #2, #3, #14, #15, AND #16 FAN BLADES. LH RVSM AREA PLACED ON DESDR 2026FA0000029Mesh · deterioratedLEFT ENGINE INLET MESH DETERIORATIONSDR 2026FA0000028Mesh · deterioratedRIGHT ENGINE INLET MESH DETERIORATIONSDR 2026FA0000027Mesh · deterioratedRIGHT ENGINE INLET MESH DETERIORATION.SDR YENA2026011300029Actuator · failedFLT 839 JFK- JFK, (TAKE OFF ABORTED). ON TAKEOFF AT ABOUT 50 KNOTS RECEIVED ENG 1 COMPRESSOR VANE MESSAGE. TAKEOFF REJECTED. REF L/PG 4454616 TEM 1 ON TAKE OFF AT ABOUT 50 KNOTS RECEIVED ENG 1 COMPRESSOR VANE MESSAGE TAKE OFF REJECTED. REMOVED AND REPLACED VSDR NACA202601060001Blades · damagedNR 2 ENGINE, SIX FAN BLADES WERE DAMAGED DURING INSTALLATION OF INLET COWL AT 12 O'CLOCK POSITION. THE ENGINE WAS R & R FOR REPAIR. RECEIVED SERVICEABLE ENGINE. ENGINE WILL BE REINSTALLED ON W/O 4677 NR 21605SDR DALA2025122909471Engine · failedATO- REJECTED TAKEOFF AT 110 KNOTS DUE TO LEFT ENGINE FAIL. MAINTENANCE REPLACED THE NUMBER 1 ENGINE PER AMDSWC 7100-4423-LH.SDR NACA2025122200001Blades · mechanic errorNUMBER 2 ENG. SIX FAN BLADES WERE DAMAGED DURING INSTALLATION OF INLET COWL AT 12 O'CLOCK POSITION. ENGINE R & R FOR REPAIR. RECEIVED SERVICEABLE ENGINE. ENGINE WILL BE REINSTALLED ON W/O 4677 NR 21605SDR HNAA2026012100036Inlet · corrodedRIGHT ENGINE INLET HAS CORROSION ON THE INTERNAL LWR SIDE WHERE THE GENERATOR INLETS ARE LOCATED. RAR RH ENGINE INLET IAW EMB 145 AMM 71-60-01,SDR SWAA2025122253197Rib · cracked#1 ENG OUTER LINER HAS ONE CRACK THAT GOES ACROSS 3 AND A HALF PANELS AT S10 (RIGHT IGNITOR). COLD SIDE INSPECTION SHOWS RIBS 4;5 AND 6 ARE CRACKED. OKAY TO CONTINUE; CIS FOR 25 CYCLES FOR ENGINE REPLACEMENT PER AMM 72-00-00-200-805-F00. REF TSR-20250010142.SDR 2025FA0000826Inlet · deterioratedRIGHT ENGINE INLET MESH DETERIORATIONSDR 2025FA0000825Inlet · deterioratedLEFT ENGINE INLET MESH DETERIORATIONSDR 2025FA0000824Inlet · deterioratedLEFT ENGINE INLET MESH DETERIORATION.SDR CALA2025121012009Blade · damagedACFT AIR TURN BACK DUE TO BIRD STRIKE, FOUND FAN BLADE DAMAGE ON RT ENG & MULTIPLE DAMAGE ON RT & LT TE FLAPS. BIRD STRIKE CONDITIONAL INSPECTION ACCOMPLISHED IAW AMM 5-51-18. FOUND DAMAGED. NO OTHER DAMAGE WAS FOUND, INCLUDING TO NR 1 ENGINE. DAMAGE WAS DUESDR SIMA20251130001Engine · vibrationENG 1 LP VIBRATION REOCCURRING THROUGHOUT FLIGHT IN EXCESS OF 10 SECS, MAX REACHED 5.1 OCCURRED AT ALTITUDE AND IN DESCENT INTO PHX, COMPLIED WITH PROCEDURES AND VIBRATIONS DID NOT GO AWAY EMERGENCY DECLARED. SPOKE WITH PILOTS. PILOTS DECLARED AN EMERGENCY COMSDR CALA2025112711506Blade · damagedNUMBER 1 ENGINE FAN BLADE FAIRING N6 HAD PART OF THE TRAILING EDGE OF THE FAIRING THAT DEPART THE AIRPLANE. THE PART MISSING IS 8 BY 6 INCHES, (24 SQ INCHES) PERFORMED FOD INSPECTION IAW AMM 72-00-00-210-808-N02, THERE IS NO EVIDENCE OF BIRD STRIKE OR CORE INGSDR DALA2025111808411Seal · bypassingCABIN REPORTED " DIRTY SOCKS" FWD CABIN AND BURNED RUBBER SMELL AFT CABIN BRIEFLY ON BASE / FINAL TURN BEFORE LANDINGS. SMELL CLEARED AFTER A MINUTE OR TWO. FOUND NBR 2 FAN SHAFT SEAL BYPASSING OIL. REPLACED FAN SHAFT SEAL NBR 2 ENGINE PER A321 AMM 72-11-01.SDR NACA2025110100011Blade · damagedNUMBER 2 ENG FAN BLADE HAS A NICK WITH A BURR ON L/E AT FAN BLADE TIP. REPAIRED NICK AT NR 2 ENG FAN BLADE ON L/E IAW AMM 72-31-02-308-003-N00. PERFORMED HFEC, NO CRACKS IAW AMM 72-31-02-206-100-N00. BLADE NR 23.SDR NACA2025110100010Blade · damagedNUMBER 2 ENGINE FAN BLADE HAS 2 DINGS APPROX 3.5" APART FROM EACH OTHER 1ST DING APPROX 2.5" FROM FAN BLADE TIP ON L/E OF FAN BLADE. REPAIRED THE 2 DINGS AT NR 2 ENG FAN BLADE 2.5" AND 6" FROM FAN BLADE TIP IAW AMM 72-31-02-308-N00. PERFORMED HFEC, NO CRACKSDR NACA2025110100009Blade · damagedNUMBER 2 ENGINE FAN BLADE HAS A DING APPROX .5" ON L/E FROM FAN BLADE TIP. REPAIRED THE DING AT NR 2 ENG FAN BLADE 5" ON L/E FROM FAN BLADE TIP IAW AMM 72-31-02-308-003-N00. PERFORMED HFEC, NO FOUND CRACKS IAW AMM 72-31-02-206-100-N00. BLADE NR 2.SDR NACA2025110100008Blade · nickedNUMBER 2 ENG FAN BLADE HAS A NICK APPROX 2.5" ON L/E FROM FAN BLADE TIP. REPAIRED THE NICK AT NR 2 ENG FAN BLADE 2.5" ON L/E FROM FAN BLADE TIP IAW 72-31-02-308003-N00. PERFORMED HFEC, NO CRACKS FOUND IAW AMM 72-31-02-206-100-N00. BLADE NR 3.
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