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 ASAA2023060543469Spacer · worn#2 ENGINE SPACERS WORN BEYOND LIMITS 14. GROUNDED - YES. REPLACED 14 ENGINE SPACERS IAW ASA TC 78472010.SDR ASAA2023060543468Spinner · worn#2 ENGINE CONE PAINT WORN TO LIMITS. GROUNDED - YES. REPLACED #2 ENGINE CONE IAW ASA TC 78472010.SDR ASAA2023060443688Unknown · unknownON ENGINE #1 CRACK FOUND IN ABRADABLE SHROUD AT 9 O'CLOCK POSTION. GROUNDED - YES. ON DEFERRAL. CRACK FOUND TO BE WITHIN DEFERRABLE LIMITS A/C RELEASED FOR SERVICE WITHIN 100 CYCLES PERFORM TAP TEST INSPECTION AT CRACKS LOCATION REF: AMM 72-21-00-200-802-G00 (SDR ASAA2023052943388Guide Vane · nickedFOUND #2 ENG OGV AT 12 O'CLOCK HAS A NICK ON THE LEADING EDGE. GROUNDED - YES. REPLACED #2 ENG OGV AT 12 O'CLOCK POSITION IAW B737-900 AMM 72-23-01.SDR ASAA2023052543361Spinner · wornFRONT SPINNER CONE PAINT WORN. GROUNDED - YES. REMOVED AND REPLACED FRONT SPINNER CONE IAW ASA TC 78472010.SDR ASAA2023052443343Spinner · wornENGINE #2 SPINNER CONE WORN. GROUNDED - YES. REPLACED ENGINE SPINNER REF ASA TASK CARD 78472010.SDR ASAA2023052243328Blade · out of limitsREF ASA TASK CARD 78472010 #2 ENGINE FAN LUBE DUE TO WEAR OUT OF LIMITS ON 20 FAN BLADES IN AREA W, REQUIRES REPLACEMENT OF ALL FAN BLADES , ALL PLATFORMS AND ALL SPACERS. GROUNDED - YES. REF ASA TASK CARD 78472010 #2 ENGINE FAN LUBE REMOVED AND REPLACED ALL PSDR ASAA2023052143329Platform · damaged1 PLATFORM ON #1 ENGINE DAMAGED. GROUNDED - YES. PLATFORM REPLACED PER ASA T/C 78472010 TEST 7 VIBE SURVEY B737-800 AMM 71-00-00 PB SO1 ACCOMPLISHED.SDR VNAA202305171111Blade · unserviceableDURING CLIMBOUT, THE AIRCRAFT WAS EXPERIENCING AN ENGINE VIBE THAT WAS HIGH BUT WITHIN INTOLERANCE. THEY DECLARED AN EMERGENCY FOR LANDING OVERWEIGHT BY 1900 LBS. / COMPLIED WITH FAN BLADE LUBRICATION. REMOVED AND REPLACED RH ENGINE FAN BLADE PINS IAW CRJ900 ASDR ASAA2023051543258Panel · crackedREF ASA T/C # 78472000 #1 ENGINE INLET AND FAN BLADES - DETAILED INSP FOUND 12 O'CLOCK STRUT PROFILE PANEL CRACK ON R/H SIDE, AFT END, AT FWD FASTENER HOLE CRACKED, NEXT TO 1 O'CLOCK AFT ACOUSTICAL PANEL. GROUNDED - YES. REPLACED #1 ENG 12 O'CLOCK STRUT PROFILSDR ASAA2023051543240Panel · delaminatedREF ASA T/C #78472000 #1 ENG. INLET AND FAN BLADES-DETAILED INSPT. FOUND #5 STRUT PANEL AT 5 O'CLOCK POS. HAS 1 EACH FASTENER INSERT DELAMINATED FROM PANEL, AFT I/B FASTENER. GROUNDED - YES. REMOVED AND REPLACED #5 STRUT PANEL. REF B737-800 AMM 72-23-07.SDR HALA2023051500108Blade · faultyETOPS - LEFT ENGINE FAN BLADE #15 HAS DAMAGE ON CONCAVE SIDE 135MM FROM L/E AND 215 MM FROM TIP. 142% DEFELCTION. REF T/C A2020-06-16-PART01. REPLACED #15 FAN BLADE ON #1 ENG PER TASK CARD 330-723100R7-1-1.SDR ASAA2023050743195Spinner · damagedWHILE ACCOMPLISHING ASA T/C 78472000 ON ENGINE 2 FOUND SPINNER CONE MISSING 50 PERCENT OF COATING. GROUNDED - YES. SPINNER CONE REPLACED IAW B737-900 AMM 72-21-00.SDR ASAA2023050543157Blade · damagedREF T/C 78472010 #1 ENG FAN LUBE. #2 BLADE HAS OUT OF LIMITS DAMAGE IN AREA H IN THE PLATFORM SEAL AREA ON THE CONCAVE SIDE. GROUNDED - YES. REPLACED #2 FAN BLADE AND OPPOSITE PAIR, #14 BLADE ON #1 ENG REF T/C 78472010.SDR ASAA2023050343103Blade · out of limitsREF ASA T/C 78472010 #2 ENG FAN LUBE. FOUND OUT OF LIMITS MISSING CU-N1 COATING IN THE PRESSURE FACE AREA ON THE CONCAVE SIDE BLADE #19. GROUNDED - YES. REPLACED BLADE PAIR PER ASA T.C. 78472010.SDR ASAA2023042743056Panel · delaminatedREF ASA T/C #78472000 #1 ENG. INLET AND FAN BLADES - DETAILED INSPT. FOUND #5 I/B AT 5 O'CLOCK POS. STRUT PANEL HAS 1 EACH FASTENER INSERT DELAMINATED FROM PANEL. (M) ALF AFT UPPER INSERT. GROUNDED - YES. REMOVED AND REPLACED #5 FAN DUCT PANEL REF B737-800 AMMSDR ASAA2023042142974Blade · damagedPER T/C 78472010 #2 ENG FAN BLADE LUBE #24 FAN BLADE CU- NI-IN COATING MISSING BEYOND LIMITS ON C.C SIDE. GROUNDED - YES. REMOVED AND REPLACED #24 AND #12 FAN BLADE IAW TASKCARD 78472010.SDR ASAA2023042142973Spinner · damagedPER T/C 78472010 #2 ENG FAN BLADE LUBE FRONT SPINNER CONE ANTI EROSION PAINT MISSING BEYOND LIMITS. GROUNDED - YES. REPLACED FRONT SPINNER CONE REF T/C #78472010.SDR ASAA2023041242826Spacer · wornDURING BLADE LUBE PER ASA TC 7840708 DETERMINED 6 BLADE SPACERS PN 440-001-262-0 ARE WORN TO LIMIT. GROUNDED - YES. REMOVED AND REPLACED BLADE SPACERS PER ASA TC 7840708.SDR ASAA2023041142811Spinner · damagedPER ASA T/C 78472010 #1 ENG. FAN BLADE LUBE FRONT SPINNER CONE WHITE ANTI EROSION PAINT MISSING BEYOND LIMIT. GROUNDED - YES. REMOVED AND REPLACED #1 ENG FRONT SPINNER CONE REF AMM 72-21-01.SDR HALA2023041300087Unknown · unknownETOPS - #1 ENGINE FAN BLADE NICK. BLEND #1 ENG #17 BLADE. ALSO INSPECT AND CLEAN WITHIN LIMITS. PRATT AND WITHNEY 72-11-03. OK FOR SVC.SDR ASAA2023041042792Spacer · delaminatedDURING #1 ENGINE FAN LUBE ASA TASK CARD 78472010 FOUND FRONT SPINNER CONE EROSION REQUIRES REPLACEMENT, AND # 7 FAN BLADE SPACER RUBBER IS DELAMINATING. GROUNDED - YES. REPLACED SPACER FOR #7 FAN BLADE, AND REPLACED FRONT SPINNER CONE #1 ENGINE REF ASA TASK CASDR ASAA2023040742779Blade · faultyDUE TO ONGOING VIBRATION ISSUES ON #2 ENGINE. REQUEST FAN SET REPLACEMENT. TASK CARD 78472010 FAN BLADE ULTRA INSP REQUIRED. GROUNDED - YES. REMOVED AND REPLACED FAN SET PER B737-800 AMM 72-21-02. ACCOMPLISHED VIBRATION SURVEY AND FAN TRIM BALANCE PROCEDURE. VSDR ASAA2023040642844Spinner · damagedREF ASA T/C 78472000 #1 ENG S/N 862434 FRONT SPINNER CONE MISSING OVER 50% OF WHITE SPIRAL SHAPED MARK. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE FRONT SPINNER CONE REF B737-900 AMM 72-21-01.SDR HALA2023040500080Blade · damagedETOPS - DMI 206748 - #2 ENG FAN BLADE POLY COAT PEELING. 0.25"X0.25" AREA - A. DEFERED PER AMM 72-11-03-220-805-A. REPAIR OR REPLACE IN 2600FC. TRANSCRIBED TO E1128-321-72-065 CLEARED MIC SHEET. ORIGINAL SUBMISSION DATE: 4/5/2023.SDR ASAA2023040442718Unknown · unknownWHILE PERFORMING LL1 INSPECTION FOUND NICK ON #2 ENG BLADE #5 LEADING EDGE APPROXIMATLEY 5.5 INCHES FROM END OF BLADE. GROUNDED - YES. NICK ON #5 BLADE MEASURES 0.2 INCHES LENGTH BY 0.032 INCHES DEEP NICK IS BEYOND SERVICABLE LIMIT OF 0.0137 INCHES PER B737-9 SDR UIEA2023040200301Unknown · unknownENGINE #1 INDICATED HIGH VIBE OF 4.9 CLIMBING THROUGH 15,000' UP TO FL 240.(<P>ACCOMPLISHED FIM TASK ON 71-00 FIGURE 118 STEPS 1 &2, NO DEFECTS FOUND. INSTALLED ACCELEROMETER IAW 77-31-01. PENDING OPS CHECK. ACCOMPLISHED VIBRATION SURVEY PER AMM 71-00-00.</P> SDR ASAA2023040242677Shim · warpedFOUND 1 SHIM WARPED WHILE ACCOMPLISHING #2 ENG FAN LUBE. GROUNDED - YES. REPLACED "1" SHIM ON #2 ENG REF ASA T/C 78472010.SDR ASAA2023040242676Blade · wornFOUND 5 PLATFORMS WITH SHIM WEAR WHILE ACCOMPLISHING #2 ENG FAN LUBE. GROUNDED - YES. REPLACED "5" PLATFORMS ON ENGINE #2 REF ASA T/C 78472010.SDR ASAA2023032842635Blade · unknownREF ASA T/C 78472010 #2 ENG FAN LUBE FOUND BLADE PLATFORMS 340-001-816-0 IN LOCATION 2,3,4,5,6,7 REST OF ENG PLATFORMS ARE -817-O REF SUBTASK 839-033. GROUNDED - YES. REMOVED AND REPLACED BLADE PLATFORMS REF T/C 78472010 TASK 839-033.SDR ASAA2023032842634Blade · damagedREF ASA T/C 78472010 FAN BLADE LUBE, #2 ENG #6 BLADE HAS A NICK / SCRATCH ON THE CONVEX SIDE IN THE PLATFORM SEAL AREA APPROX 3 1/2 FROM LEADING EDGE. GROUNDED - YES. DAMAGE FOUND TO BE OUT OF LIMITS REF B737-800 AMM 72-21-02-200-801-F00. REPLACED #2 ENG BLADESDR ASAA2023032342589Spinner · eroded#1 ENGINE FRONT SPINNER CONE SHOWS EROSION. GROUNDED - YES. REMOVED AND REPLACED #1 ENG FRONT SPINNER CONE IAW B737-900 AMM 72-21-01-000-801/72-21-01-400-801.SDR ASAA2023032342583Blade · unknownWHILE PERFORMING #2 ENGINE BLADE LUBE, FOUND SEAL TORN ON BLADE PLATFORM #21. GROUNDED - YES. REPLACED #2 ENGINE BLADE PLATFORM #21 REF ASA T/C 78472010 SUB TASK 839-033.SDR ASAA2023032342582Blade · unknownWHILE PERFORMING #2 ENGINE BLADE LUBE FOUND #1 SEAL MISSING ON BLACK PLATFORM. GROUNDED - YES. REPLACED BLADE PLATFORM REF. ASA T.C 78472010 SUBTASK 839-033.SDR ASAA2023031742419Unknown · unknown#6 BLADE ON THE #1 ENGINE HAS A KNICK. GROUNDED - YES. ACCOMPLISHED FOD INSPECTION #1 ENGINE REF B737-900 AMM 05-52-00/601 AND ACCOMPLISHED GVI OF THE #1 ENGINE FAN BLADE #6 FOUND NICK OUT OF LIMITS REF B737-900 AMM 72-21-02-200-801-F00 IN AREA "I" OF THE BLADSDR HALA2023031400042Blade · damagedETOPS - DMI# 206651 ENG #1 BLADE TIP 17 MISSING POLYURETHANE COATING. ENG CHANGED REF CARD 321-72-HWI-02 MIC UPDATED PLACARD REMOVED. ORIGINAL SUBMISSION DATE: 3/15/2023.SDR ASAA2023031342325Shim · damagedDURING #2 ENG FAN LUBE, FOUND BLADE 3 SHIM DAMAGED. NO ABNORMAL WEAR OR DAMAGE NOTED TO FAN BLADE OR BLADE SLOT. GROUNDED - YES. REMOVED & REPLACED BLADE 3 SHIM ON #2 ENG PER ASA T/C 78472010.SDR SWAA2023031516752Platform · bird ingestionBIRDSTRIKE #1 ENGINE WITH ADVERSE ODDOR ASSOCIATE WITH STRIKE. NO ABNORMAL ENG. INDICATIONS<[01] C/W INSPECTION STEPS UP TO MXI STEP 23 PER MT 872-PRD-01-01 (INSP - LEAP-1B BIRD STRIKE BORESCOPE) SEE 872-PRD-01-01 (INSP - LEAP-1B BIRD STRIKE BORESCOPE) FOR INDSDR SWAA2023031514892Acoustic Panel · bird ingestionBIRDSTRIKE #1 ENGINE WITH ADVERSE ODDOR ASSOCIATE WITH STRIKE. NO ABNORMAL ENG. INDICATIONS<[01] C/W INSPECTION STEPS UP TO MXI STEP 23 PER MT 872-PRD-01-01 (INSP - LEAP-1B BIRD STRIKE BORESCOPE) SEE 872-PRD-01-01 (INSP - LEAP-1B BIRD STRIKE BORESCOPE) FOR INDSDR ASAA2023030142142None · none#1 ENGINE FRONT SPINNER HAS EXCESSIVE PAINT MISSING REF ASA T/C 78472010. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE FRONT SPINNER CONE REF ASA T/C 78472010.SDR ASAA2023030142141Blade · none#1 FAN BLADE FAILED INSPECTION DUE TO SHIM WEAR REF ASA T/C 78472010. GROUNDED - YES. REMOVED AND REPLACED BOTH #1 & #13 FAN BLADES REF ASA T/C 78472010.SDR ASAA2023022442109Engine · wornWHILE ACCOMPLISHING T/C 78472010 FOUND 18 FAN BLADES WITH BLADE SHANK WEAR BEYOND AMM PUBLISHED LIMITS REF B737-900 AMM 72-21-02-200-801-F00 STEP F.1 (E)3)B)<1>. GROUNDED - YES. REMOVED #1 ENGINE ESN 874470. REF ASA SHOP W/O # 1944222.SDR ASAA2023022442108Engine · wornWHILE ACCOMPLISHING ASA T/C 78472010 IT WAS NOTED THAT ALL FAN BLADE SHIMS FOR THE #1 ENGINE TO BE WORN. GROUNDED - YES. REMOVED #1 ENGINE ESN 874470. REF ASA SHOP W/O # 1944222.SDR CALA2023022400532Blade · crackedON ENGINE #1 FOUND #7 FAN BLADE DOVETAIL KEY CRACKED/BROKEN AT ROOT. ATTATCHED PHOTO. ADDED PICTURE RPL''D #1 ENG, DOVETAIL KEY AT #7 FAN BLADE REF AMM''S 72-21-02-020-803-G00 AND 72-21-02-400-803-G00. RAN ENG AT IDLE ALL PARAMETERS NORMAL.SDR ASAA2023021341930Unknown · unknownAMBER "MAINT "LIGHT. GROUNDED - YES. PERFORMED FAULT INTEGRATION IAW B737-9 AMM 31-69-00-750-801 FOUND INACTIVE MAINTENANCE MESSAGE 73-45001 AND 73-45031 PERFORMED B737-9 IFIM G73-00-00-810-A78 CONFIRMED FAULTS WERE INTERMITTENT . ERASED LATCHED MESSAGES AS RESDR ASAA2023021041929Spinner · damagedREF ASA T/C 78472000 ENG INLET & FAN DETAILED INSP FOUND #2 ENG S/N 854343 FRONT SPINNER CONE WHITE ANTI EROSION PAINT MISSING BY 50%. GROUNDED - YES. REMOVED & REPLACED #2 ENGINE SPINNER CONE REF B737-900 AMM 72-21-01.SDR ASAA2023020841876Blade · wornWHILE ACCOMPLISHING ASA T/C 78472010 FOUND BLADES 21, AND 22 HAVE CU-NI-IN COATING MISSING UPON MEASURING IT IS NOT WITHIN LIMITS BLADES NEED TO REPLACED. GROUNDED - YES. REMOVED AND REPLACED BLADES 22 & 10 AS A PAIR IN REF WITH ASA T/C 78472010.SDR ASAA2023020841875Blade · wornWHILE ACCOMPLISHING ASA T/C 78472010 FOUND BLADES 21, AND 22 HAVE CU-NI-IN COATING MISSING APRON MEASURING IT IS NOT WITHIN LIMITS BLADES NEED TO REPLACED. GROUNDED - YES. REMOVED & REPLACED BLADES 21 & 9 AS A PAIR IN REF WITH ASA T/C 78472010.SDR ASAA2023020741874Spinner · damagedWHILE ACCOMPLISHING ASA T/C 78472010 FOUND POSSIBLE GOUGE, SCRATCH, OR CRACK AT ONE OF THE HOLE (MARKED) FOR THE FRONT SPINNER. GROUNDED - YES. REMOVED & REPLACED FRONT SPINNER CONE ON #1 ENGINE REF ASA T/C 78472010.SDR MASA2023020600024Blades · bindingENG 2 LP HIGH VIB OVER LIMITS 4.0-- EMER DECLARED/DIVERTED FLT
R/R 9 FAN BLADES ON ENG 2, REMAPPED BLADES, PERFORMED ON WING TESTING, ENG VIB WITHIN TOLERANCE
Back to JASC 7220