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 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.SDR NACA2025110100007Blade · nickedNUMBER 2 ENG FAN BLADE AT L/E TO FAN BLADE TIP HAS A NICK AND TIP IS SLIGHTLY BENT OUT. REPAIRED THE NICK AT NR 2 ENG FAN BLADE L/E CORNER IAW AMM 72-31-02-208-003-N00. PERFORMED HFEC NO CRACKS FOUND IAW AMM 72-31-02-206-100-N00. BLADE NR 14.SDR NACA2025110100006Case · damagedNR 1 ENG. FAN CASE HAS GOUGES ON THE V-GROOVE FROM 8 O'CLOCK TO 9 O'CLOCK POSITION. REMOVED DAMAGED ON NR 1 ENG FAN CASE V-GROOVE FROM 8 O'CLOCK TO 9 O'CLOCK POSITION WAS FOUND WITHIN LIMITS IAW AMM 72-34-07, STEP 2.E, TABLE 801. REMOVED .030" DEPTH, MAXIMUMSDR NACA2025110100005Case · damagedNUMBER 1 ENG. FAN CASE HAS A GOUGE ON THE V-GROOVE AT 3 O'CLOCK POSITION. REMOVED DAMAGE ON NR 1 ENG FAN CASE V-GROOVE AT 3 O'CLOCK POSITION WAS FOUND WITHIN LIMITS IAW AMM 72-34-07 STEP 2. E, TABLE 801. REMOVED 0.090 DEPTH, MAXIMUM ALLOWED 0.125".SDR NACA2025110100004Blade · damagedNUMBER 1 ENG. FAN BLADE NR 12 HAS A DING APPROX. 1" ON L/E FROM BLADE TIP. THIS AREA WAS PREVIOUSLY BLENDED. REPAIRED DING AT NR 1 ENG FAN BLADE NR 12 1" ON L/E FROM BADE TIP AREA -A- IAW AMM 72-31-02-308-003-N00. PERFORMED HFEC, NO FOUND CRACKS AT THE AREA SDR NACA2025110100003Blade · damagedNUMBER 1 ENG. FAN BLADE NR 12 HAS A DING APPROX. 1" ON L/E FROM BLADE TIP. THIS AREA WAS PREVIOUSLY BLENDED. REPAIRED DING AT NR 1 ENG FAN BLADE NR 12 1" ON L/E FROM BADE TIP AREA -A- IAW AMM 72-31-02-308-003-N00. PERFORMED HFEC, NO FOUND CRACKS AT THE ARESDR NACA2025110100002Bladder · damagedNUMBER 1 ENG. FAN BLADE NR 27 HAS A DING APPROX. 1.75" ON L/E FROM BLADE TIP. EVALUATED DENT AT NR 1 ENG FAN BLADE NR 27 1.75" ON L/E FROM BLADE TIP FOUND TO BE IN LIMITS IAW AMM 72-31-02. PERFORMED HFEC, NO CRACKS FOUND IAW AMM 72-31-02-206-100-N00.SDR NACA2025112100001Blade · damagedNUMBER 1 ENG FAN BLADE NR 37 HAS A DING APPROX. 1.75" ON L/E FROM BLADE TIP. REPAIRED DING AT NR 1 ENG, FAN BLADE NR 37 1.75" ON L/E FROM BLADE TIP IAW AMM 72-31-02-308-003-N00. PERFORMED HFEC, NO FOUND CRACKS IAW AMM 72-31-02-206-100-N00.SDR CALA2025102910715Blade · bird ingestionBIRD STRIKE ON T/O AIRFRAME AND ENG VIB RIGHT ENG APPEARS TO H AVE BLADE DAMAGE. PERFORMED AIRFRAME AND ENGINE BIRD STRIKE INSPECTIONS IAW AMM 05-51-14-200-803-A AND AMM 72-00-00-200-010-A. NO AIRFRAME DAMAGE WAS NOTED. NOTED ENGINE DAMAGE LIMITED TO A SISDR QXEA2025102000325Blade · damagedFLIGHT 2399. BIRD STRIKE #1 ENGINE ON INITIAL CLIMB OUT. RETURNED TO FIELD. ACCOMPLISHED UNEVENTFUL LANDING. REMOVED FROM SERVICE. FOUND BIRD INGESTED ON #1 ENGINE FAN BLADE PERFORMED BIRD STRIKE INSPECTION PER E175 AMM 05-50-02-200-801-A. REF MTC E175-720001 SDR SWIA20251018Blades · damagedBIRD STRIKE ON TAKEOFF AT 600-800 FEET AGL, CAUSING HIGHER THAN NORMAL VIBRATION IN THE RIGHT ENGINE. BOTH ENGINES WERE OPERATING; RIGHT ENGINE LP VIBE PEAKED AT 2.0. DECLARED AN EMERGENCY AND RETURNED TO SBP. POSTFLIGHT INSPECTION SHOWN SEVERAL BENT FAN BLSDR NACA2025101000002Valve · crackedIP VALVE ON #1 ENGINE HAS SIGNS OF CRACKING AND CORROSION ON FUSELAGE. INSTALLED SERVICEABLE IP VALVE ON # 1 ENG IAW AMM 36-11-06-404-033-002. NO LEAK NOTED.SDR NACA2025101000001Vane · brokenONE EA FAN EXIT VANE OF THE NR 2 ENGINE HAS A BROKEN PLATFORM AT THE INNER BASE OF PART. PERFORMED EVALUATION IF 1 EACH FAN EXIT VALVE OF #2 ENG BROKEN PLATFORM NO ADITIONAL DEFECTS NOTED. REPAIRED FAN EXIT VALVE IAW 72-33-02-308-003-N00 .SDR AALA202510109652Guide Vane · contaminatedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: ON TAKEOFF HIT A BIRD WITH THE NUMBER 1 ENGINE THEN ENCOUNTERED A STRONG BURNING ODOR IN THE FLIGHT DECK. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MIA. DURING INSPECTION FOUND DAMAGE TO NUMBSDR AALA202510107492Guide Vane · contaminatedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: ON TAKEOFF HIT A BIRD WITH THE NUMBER 1 ENGINE THEN ENCOUNTERED A STRONG BURNING ODOR IN THE FLIGHT DECK. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MIA. DURING INSPECTION FOUND DAMAGE TO NUMBSDR AALA202510100725Guide Vane · contaminatedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: ON TAKEOFF HIT A BIRD WITH THE NUMBER 1 ENGINE THEN ENCOUNTERED A STRONG BURNING ODOR IN THE FLIGHT DECK. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MIA. DURING INSPECTION FOUND DAMAGE TO NUMBSDR AALA202510104139Guide Vane · contaminatedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: ON TAKEOFF HIT A BIRD WITH THE NUMBER 1 ENGINE THEN ENCOUNTERED A STRONG BURNING ODOR IN THE FLIGHT DECK. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MIA. DURING INSPECTION FOUND DAMAGE TO NUMBSDR AALA202510107507Guide Vane · contaminatedAIRCRAFT WAS GROUNDED: AN EMERGENCY DECLARED DUE TO ON TAKEOFF HIT A BIRD WITH NR 1 ENG THEN ENCOUNTERED A STRONG BURNING ODOR IN FLT DECK. ACFT AIR INTERRUPTED BACK TO & LANDED SAFELY AT MIA. DURING INSPECTION FOUND DAMAGE TO NR 1 ENG BLADE PLATFORM & BIRD SDR AALA202510103742Guide Vane · contaminatedAIRCRAFT WAS GROUNDED: AN EMERGENCY DECLARED DUE TO: ON TAKEOFF HIT A BIRD WITH THE NR 1 ENGINE, ENCOUNTERED A STRONG BURNING ODOR IN FLT DECK. ACFT AIR INTERRUPTED BACK TO & LANDED SAFELY AT MIA. DURING INSPECTION FOUND DAMAGE TO NR 1 ENG BLADE PLATFORM & BSDR AALA202510108748Guide Vane · contaminatedAIRCRAFT WAS GROUNDED: AN EMERGENCY DECLARED DUE TO ON TAKEOFF HIT A BIRD WITH NR 1 ENG, THEN ENCOUNTERED A STRONG BURNING ODOR IN FLT DECK. ACFT AIR INTERRUPTED BACK TO & LANDED SAFELY AT MIA. DURING INSPECTION FOUND DAMAGE TO NR 1 ENGINE BLADE PLATFORM & BISDR AALA202510100112Guide Vane · contaminatedAIRCRAFT WAS GROUNDED: AN EMERGENCY DECLARED DUE TO ON TAKEOFF HIT A BIRD WITH THE NR 1 ENGINE THEN ENCOUNTERED A STRONG BURNING ODOR IN FLT DECK. ACFT AIR INTERRUPTED BACK TO & LANDED SAFELY AT MIA. DURING INSPECTION FOUND DAMAGE TO NR 1 ENG BLADE PLATFORM & SDR AALA202510103573Guide Vane · contaminatedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: ON TAKEOFF HIT A BIRD WITH THE NR 1 ENG THEN ENCOUNTERED A STRONG BURNING ODOR IN THE FLT DECK. ACFT AIR INTERRUPTED BACK TO & LANDED SAFELY AT MIA. DURING INSPECT FOUND DAMAGE TO NR 1 ENGINE BLADE PLATSDR CALA2025100909840Blade · out of limitsDURING WALK AROUND, FOUND FAN BLADE TIP OF NR 2 ENG BENT. ON FURTHER INSPECTION IAW AMM 72-21-02-200-801-F00, FOUND ORIGINAL BLADE NR 8 TO BE OUT OF LIMITS. IN ADDITION, FOUND ADJACENT BLADE NR 9 TO HAVE A TIP CURL OUT OF LIMITS. FOUND SEVERAL OTHER BLADESSDR HALA20251008309Cooling Duct · crackedETOPS - ON WALK AROUND, FOUND #2 ENG EEC COOLING INLET DUCT CRACKED. REMOVED AND REPLACED #2 ENG EEC COOLING DUCT INLET PER CMM 71-60-00. SEC CHK GOOD. OK FOR SVCSDR QXEA2025100700316Blade · damagedBIRDSTRIKE ON TO AT V1 #2 ENGINE AND RH MLG. ENGINE INDICATIONS NORMAL ON CLIMB WITH LP 1.4 MAX & HP 2.6 MAX. ALL OTHER INDICATIONS NORMAL. SNARGE AND BENT FAN BLADES FOUND DURING POST FLIGHT INSPECTION. REMOVED FROM SERVICE. PERFORMED BIRDSTRIKE INSP, FOUND 3SDR HALA20251001296Filler · brokenETOPS - ON PDSC WALK AROUND HEARD LOOSE OBJECT IN NR 2 ENGINE SPINNER. FOUND NR 2 ANNULUS FILLER FRIONT ARM & LOCATION PIN BROKEN OFF. REMOVED NR 2 ANNULUS FILLER & BROKEN PART. INSTALLED NEW ANNULUS FILLER IN NR 2 POSITION PER AMM 72-31-41. OK FOR SVC. (NOTESDR DALA2025091806864Case · bird ingestionRETURNED TO MIA DUE TO RIGHT ENGINE BIRD STRIKE AFTER TAKEOFF. MAINTENANCE FOUND MULTIPLE FAN BLADES AND FAN CASE DAMAGED. FAN CASE DAMAGE EXCEEDS B737AMM LIMIT. ENGINE CHANGE ON LOG PAGE 1199194.SDR DALA2025091506764Fan · failedDIV DE- DUE TO RIGHT ENGINE COMPRESSOR STALL AND FAILURE TO ADVANCE BEYOND 50% N2 DURING CRUISE. ENGINE WAS NOT SHUT DOWN AND DIVERTED TO BZE. CONTRACT MAINTENANCE FOUND FAN VERY HARD TO TURN AND METAL ON AFT SUMP CHIP DETECTOR. REPLACED RIGHT ENGINE ON LOG SDR QEMY20250905001Hub · crackedDURING INCOMING INSPECTION AT GE WALES, DEFECTS ON THE FAN FRAME HAVE BEEN NOTED. INNER HUB OF FAN FRAME FOUND CRACKED ON SURFACE L FLANGE IN 2 OFF LOCATIONS. IN BOTH LOCATIONS THE CRACK HAS FULL PENETRATION THROUGH THE FLANGE. DR #02238550 WAS REJECTED BY THESDR NACA2025082600006Case · gouged21422 #1 ENG FAN CASE HAS A GOUGE ON THE V-GROOVE AT 8 O'CLOCK TO 9 O'CLOCK POISTION DOT 012002. REMOVED DAMAGE ON #1 ENG FAN CASE V-GROOVE AT 8 O'CLOCK AND 9 O'CLOCK POSITION WAS FOUND WITHIN LIMITS PER B767 AMM 72-34-07 STEP 2 E TABLE 801 REMOVED 0.090 DEOSDR NACA2025082600005Case · gouged21421 #1 ENG FAN CASE HAS A GOUGE ON THE V-GROOVR AT 3 O'CLOCK POISTION DOT 012001. REMOVED DAMAGE ON #1 ENG FAN CASE V-GROOVE AT 3 O'CLOCK POSITION WAS FOUND WITHIN LIMITS PER B767 AMM 72-34-07 STEP 2 E TABLE 801 REMOVED 0.090 DEPTH MAX ALLOWED 0.125".SDR NACA2025082600004Blade · damaged21420 #1 ENG FAN BLADE # 3 HAS A DING APPROX 1.5" ON L/E FROM BLADE TIP DOT 063631. REPAIRED DING AT #1 ENG FAN BLADE #37 1.5 ON L/E FROM BLADE TIP IAW B767 AMM 72-31-02-308-003-MOD PERFORMED HFEC NO CRACK FOUND IAW AMM 72-31-02-206-100 MOD.SDR NACA2025082600003Blade · damaged#1 ENG FAN BLADE # 27 HAS A DING APPROX 1.75" ON L/E FROM BLADE TIP DOT 063629 . REPAIRED DING AT #1 ENG FAN BLADE #12 1" ON L/E FROM BLADE TIP AREA A IAW B767 AMM 72-31-02-308-MOD PERFORMED HFEC NO CRACK FOUND AT THE AREA IAW AMM 72-31-02-206-100 MOD. NO ENSDR NACA2025082600002Blade · damaged21418 #1 ENG FAN BLADE # 27 HAS A DING APPROX 1.75" ON L/E FROM BLADE TIP DOT 063629. EVLAUATED DING AT #1 ENG FAN BLADE #37 1.75 ON L/E FROM BLADE TIP FOUND TO BE IN LIMITS IAW B767 AMM 72-31-02 PERFORMAED HFEC NO CRACKS FOUND IAW B767 AMM 72-31-02-206-100.SDR NACA2025082600001Blade · damaged#1 ENGINE FAN BLADE #37 HAS A DING APPROX 1.75" REPAIRED DING AT #1 ENG FAN BLADE #37 ON LE BLADE TIP IAW B767 AMM 72-31-308. ENGINE INFORMATION UNAVAILABLE.SDR DALA2025082006222Seal · leakingDIVERSION TO MCI DUE TO DIRTY SOCK SMELL IN THE AFT CABIN. FOUND OIL BEHIND #2 ENGINE SPINNER. REPLACED #2 ENGINE FAN SHAFT COVER SEAL AND PERFORMED LEVEL B ECS DECONTAMINATION. RAN ENGINES NO LEAKS OR ODORS PRESENT. (LP 7859728)SDR AALA202508043666Blades · dirtyAIRCRAFT WAS GROUNDED: ON TAKE OFF ROLL & CLIMB STRONG SMELL OF A MUSKY ODOR (DIRTY SOCK) CONFIRMED BY FA'S. LASTED ABOUT 10 MINUTES. MAINTENANCE FOUND EXCESSIVR GREASE ON #1 ENGINE FAN BLADES, CLEANED FAN BLADES AND GUIDE VANES IAW AMM 70-00-00.SDR DALA2025080205800Spinner · leakingFUME EVENT ON TAKE OFF FROM SDQ - TOGA T/O APU ON OFF RWY 18. AT ABOUT LIFT OFF A STRONG FUEL FUME/OIL SMELL WAS EVIDENT. CLEAN A/C CONFIGURATION AND SHUT DOWN APU. ONCE APU BLEED WAS SWITCHED OFF FUMES DIMINISHED CREW OXYGEN (O2) MASK USE. FUMES DID NOT RETURSDR 2025F00166Fan · misconfiguredNEW PS3/P3B RIGID AIR TUBES (PSS DRAINAGE) AND BRACKET WERE INTRODUCED IN 2019 ON LEAP-1B (CAD MOD312504 / SB72-0280). THIS CHANGE WAS CERTIFIED FOR AN INSTALLATION ON THE NG FFOS (NEW GENERATION FAN FRAME OUTER SHROUD) BUT NOT ON THE INITIAL EIS FFOS CONFIGURSDR DALA2025072405575Seal · leakingAIRCRAFT 5048, ON DESCENT NOTICED INTERMITTENT SMELL SIMILAR TO BURNING RUBBER. CORRECTIVE ACTION: FOUND NOSE SPINNER SEAL LEAKING. REPLACED SEAL PER PW1500G EMM 72-11. (LP 7561494)SDR CALA2025072506910Blade · damagedREF L/P 5642792, DUE TO BLADE DAMAGE ON #1 ENGINE, PLEASE COMPLETE FOD INGESTION INSPECTION PER AMM 72-00-00-210-807-N02 ACP'D INSPECTION OF #1 ENG DUE TO #7 FAN BLADE BEING FOUND BENT. REF AMM INLET, EXHAUST, AND EXTERNALS INSPECTION REFERENCE: TASK 72-00-00-SDR CNMA2025090001Case · corrodedDURING C CHECK, CORROSION WAS FOUND ON THE NR 2 ENGINE FWD AND AFT CASE AROUND THE EXTERIOR AND INTERIOR SKIN. IT WAS FOUND TO BE OUT OF REPAIRABLE LIMITS FOR THE FWD FAN CASE PER AMM 72-32-00 AND OUT OF FLYABLE LIMITS PER AMM 72-00-00. THE ENGINE WAS REMOVED SDR CALA2025071806713Fairing · crackedDUE TO VIBRATION TRENDS ON THE NR 2 ENGINE. WHILE PERFORMING INSPECTION OF INLET & FAN BLADES FOUND SPINNER FAIRING CRACKED. R & R SPINNER FAIRING PER AMM TASK. 72-35-01-404-010-R04 PERFORMED FIM TASK ON NR 2 ENG BVCU 75-32-00/101 (FIG 103), NO FAULTS NOTED. SDR MASA2025052800043Blade · damagedENG 2 BIRDSTRIKE (EMER DECLARED) REMOVED AND REPLACED FAN BLADE PINS AND BUMPERS. APPLIED RTV TO ENG #2 CONTAINMENT CASE TO COMPY WITH PRP.SDR DALA2025051903803Oil System · leakingSHIP 5024 UPON DESCENT JFK FA'S REPORTED DIRTY SOCK BURNT RUBBER SMELL IN CABIN. NO PERCEPTABLE SMELL IN COCKPIT, APU OFF. CORRECTIVE ACTION: FOUND OIL PUDDLE BEHIND SPINNER OF #2 ENGINE. R/R FAN SHAFT COVER SEAL PER A321 AMM 72-15 (6862980)SDR DALA2025050903591Blade · fodSHIP 3273 DISC: POSSIBLE BIRD INJESTION IN ENGINE #2 ON TAKEOFF FROM KBWI POSSIBLE BIRD STRIKE. BIRD FLEW BY WINDSCREEN THEN N1 VIB IMMEDIATELY CLIMBED TO 8.0 BUT QUICKLY DECREASED TO 4.1. ALL OTHER ENGINE PARAMETERS NORMAL ENG #2. C/A: PERFORMED BIRD STRIKE ISDR CALA2025041804020Blade · chippedE2 BLADE 14. ON-WING- FAN BLADE ULTRASONIC INSPECTION AND BROACHED DISK LUBRICATION - DURING BLADE LUBE, FOUND CHIPPED CU-NI-IN COATING GREATER THAN AREA X. PER AMM 72-21-02-200-801-F00, PARAGRAPH K.(1) (C) 2) C) (2) CONTINUE IN SERVICE LIMIT OF 50 FLIGHT CSDR 9WGA2025042954622Inlet · corroded#3 INLET HAS PITTING CORROSION AT 11 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET AT 11 O'CLOCK POSITION. FOUND WITHIN LIMITS IAW MD-11 SRM 54-12-02-1A-0, FIGURE 103 DETAIL IV AND SRM 51-21-01. NO MATERIAL LOSS ATSDR 9WGA2025042954621Inlet · corroded#3 INLET HAS PITTING CORROSION BETWEEN 8 & 9 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET BETWEEN 8 AND 9 O'CLOCK POSITION. FOUND WITHIN LIMITS IAW MD-11 SRM 54-12-02-1A-0, FIGURE 103 DETAIL Q AND SRM 51-21-01. NOSDR 9WGA2025042954620Inlet · corroded3# INLET HAS PITTING CORROSION AT 3 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET AT 3 O'CLOCK POSITION. FOUND WITHIN LIMITS IAW MD-11 SRM 54-12-02-1A-0, FIGURE 103, DETAIL IV AND SRM 51-21-01. NO MATERIAL LOSS AT
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