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 ASAA2019082643483Shroud · damagedREFERENCE LOG 12179648 - FILLER MISSING OR FAILED TO POLYMERIZE ON SEVERAL REPAIRED AREAS OF #1 ENGINE ABRADABLE SHROUD BETWEEN THE 10 AND 2 OCLOCK POSITION. GROUNDED - YES. REMOVED NO# 1,2,3,4, FAN BLADES ON ENG# 1 TO FOM. PREPPED AND CLEARED AREAS WITH MISSISDR ASAA2019082230452Panel · wornWHILE ACCOMPLISHING #1 ENG INLET INSP T/C # 78472000NL APPEARS WORN BY LOOSE FASTENER. GROUNDED - YES. REMOVED AND REPLACED #2 FAN DUCT PNL REF B737-800 AMM 72-23-07.SDR ASAA2019081930429Panel · delaminatedNR 2 ENGINE INLET AND FAN BLADE- DETAILED INSP. FOUND #5 GAS STRUT PANEL HAS BOTH AFT FASTENER INSERTS DELAMINATED FROM PANEL, 5 O'CLOCK POS. {M} ALF. GROUNDED - YES. REMOVED & REPLACED #5 STRUT PANEL REF B737-800 AMM 72-23-07.SDR ASAA2019081930430Spacer · debondedDURING ACCOMPLISHMENT FO TC 78472010, FOUND NR 2 ENG FAN BLADE SPACERS #3 AND #21 DISBONDED BOTH SIDES TO ELASTOMERS. GROUNDED - YES. REPLACED SPACERS 3 AND 21 ON T/C 78472010.SDR ASAA2019081730419Spacer · wornALL 24 SPACERS ON #2 ENGINE ARE LOOSE AND WORN. GROUNDED - YES. REPLACED ALL 24 SPACERS ON #2 ENGINE DURING T/C 78472010 ACCOMPLISHMENT.SDR ASAA2019081730418Blade · wornALL 24 PLATFORMS ON #2 ENGINE ARE WORN AND MISSING ELASTOMERS. GROUNDED - YES. REPLACED ALL 24 PLATFORMS ON #2 ENGINE DURING T/C 78472010 ACCOMPLISHMENT.SDR ASAA2019081730415Blade · worn#2 ENGINE ESN TREND DATA SHOWS A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. GROUNDED - YES. DURING #2 ENGINE FAN LUBE FOUND PLATFORMS AND SPACERS WORN CAUSING FAN BLADES TO BE LOOSE. NO EXCESS LUBE FOUND. REPLACED ALL 24 PLATFORMS AND SPACERS. VIBSDR ASAA2019081330392Spinner · worn#2 ENG FRONT SPINNER CONE WORN TO LIMITS. GROUNDED - YES. REMOVED AND REPLACED FRONT SPINNER CONE ON #2 ENG REF. B737-800 AMM 72-21-01-401.SDR ASAA2019081330391Spacer · debondedWHILE ACCOMPLISHING T/C 78472002 FOUND SPACERS #'S 3, 7, 18 AND 20 DISBONDED ON #2 ENG. GROUNDED - YES. REMOVED AND REPLACED SPACERS #'S 3, 7, 18 AND 20 REF.SDR ASAA2019081330390Blade · wornWHILE ACCOMPLISHING T/C 78472002 FOUND PLATFORM #3 ON ENGINE #2. MISSING ELASTOMER. GROUNDED - YES. REMOVED AND REPLACED #3 PLATFORM ON ENGINE #2.SDR ASAA2019081330389Blade · incorrectWHILE ACCOMPLISHING T/C 78472002 FOUND PLATFORM #1,16,17 AND 24 WITH P/N 340-001-807-0 INTERMIXED WITH P/N 340-001-816-0 AND NOT PROPERLY SPACED 180 DEGREES OUT ON #2 ENGINE. GROUNDED - YES. REMOVED AND REPLACED PLATFORMS #1, 16,17 AND 24 WITH P/N 340-001-816-SDR UIEA2019081305047Inlet · scratchedSCRATCHES ON THE INLET, NR 1 ENG NOSE COWL, FROM 5 TO 7 O'CLOCK. REMOVED SCRATCH AND MEASURED THE REWORKED AREA; DEPTH = 0.003", LENGTH = 2.8", WIDTH = 1.2". IT IS WITHIN ALLOWABLE LIMIT IAW SRM 54-12-01-1A-1 DETAIL III REV. 110 AND JOB CARD ATTACHING SHEET COSDR ASAA2019080330302Strut · damagedWORKING ON TC 78472000 #1 ENG ESN 661176 FOUND STRUT PANEL FASTENER PULLED THRU LOCATED AT 8 OCLOCK POSITION ALF. GROUNDED - YES. REPLACED #1 ENG FAN DUCT PANEL 8 OCLOCK POSITION REF B737-900 AMM 72-23-07.SDR HNAA20190806Blade · damagedNR 2 ENGINE FAN BYPASS VANES DAMAGED. REPLACED ALL 15 FAN BLADES IAW ENG MANUAL 72-25-10-400-801.SDR UIEA2019072204820Cone · erodedL ENG CONE FOUND WITH EROSION PEELING ALL OVER THE CONE. (<P>REMOVED AND REPLACED CONE SEGMENT PER AMM 72-31-01.</P>)SDR ASAA2019071630089Spinner · wornWHILE ACCOMP T/C 78472010 FOUND #1 ENG. SPINNER FRONT CONE ANODIZED COATING WORN BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE SPINNER FRONT CONE REF T/C 78472010 ENG FAN BLADE LUBRICATION.SDR ASAA2019071630087Spinner · scratched#1 ENG FRONT SPINNER CONE HAS PAINT MISSING, LOOKS LIKE SCRATCH. GROUNDED - YES. REMOVED & REPLACED OUTER NOSE CONE ASSY. REF AMM 72-21-01.SDR ASMF20190816004Blade · missingDURING TRANSIT CHECK, IT WAS DETECTED MISSING MATERIAL ON FAN BLADE OF ENGINE NO. 1S/N: 956321; AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL ISSUED THE WO 5544667 TO PERFORM A CONDITIONAL INSPECTION; IT WAS FOUND FAN BLADE WITH MISSING MATERIAL WISDR ASAA2019071430046Elastomer · debondedPER T/C 78472010 #1 ENGINE #1, 2, 4, 10, 11, 13, 16, 22, 23, AND 7,5,12, AND 24 SPACERS ELASTOMERS ARE DISBONDED. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE #1, 2,4,10,11,13,16,22,23 AND 7,5,12 AND 24 SPACERS ELASTOMERS WITH NEW PER T/C 78472010.SDR ASAA2019071230050Spacer · debondedWHILE ACCOMPLISHING T/C 78472010 #1 ENGINE FOUND SPACER WITH DISBONDED ELASTIC MATERIAL. GROUNDED - YES. REPLACED 1 EA SPACER REF T/C 78472010 @ #1 ENG.SDR ASAA2019071230049Spinner · wornWHILE ACCOMPLISHING #1 ENG FAN LUBE T/C 78472010 FOUND NOSE SPINNER WITH WORN PAINT. GROUNDED - YES. REPLACED NOSE SPINNER REF T/C 78472010 @ #1 ENG.SDR ASAA2019070629956Elastomer · debondedWHILE ACCOMPLISHING T/C 78472010 #1 ENGINE FOUND 3 SPACERS WITH ELASTOMETER STRIPS DEBONDING REQUIRES REPLACEMENT. GROUNDED - YES. THREE SPACERS REMOVED AND REPLACED PER T/C # 78472010.SDR ASAA2019070629955Platform · scratchedWHILE ACCOMPLISHING T/C 78472010 #1 ENGINE FOUND 1 PLATFORM WITH SCRATCH ON AREA F REQUIRES REPLACEMENT. GROUNDED - YES. PLATFORM REMOVED AND REPLACED PER T/C 78472010.SDR ASAA2019070629954Retaining Ring · damagedWHILE ACCOMPLISHING T/C 78472010 #1 ENGINE FOUND HUB RETAINING RING FRETTING ON MATING SURFACE REQUIRES REPLACEMENT. GROUNDED - YES. RETAINING RING REMOVED AN REPLACED PER T/C 78472010.SDR ASAA2019070529953Platform · damagedWHILE ACCOMPLISHING T/C 78472010 #2 ENGINE FOUND #1, #16 PLATFORMS DAMAGE ON AREA F AND REQUIRE REPLACEMENT. GROUNDED - YES. REMOVED & REPLACED #1 & #16 PLATFORMS ON #2 ENGINE REF TC 78472010.SDR ASAA2019070529952Nut Plate · damagedDURING FAN LUBE ON #1 ENG, IT WAS FOUND THAT AFT SPINNER CONE HAS A BAD NUT-PLATE. GROUNDED - YES. REMOVED AND REPLACED #1 ENG AFT SPINNER CONE AND SWAPPED ALL 36 BALANCE SCREWS IAW AMM 71-00-00-750-802-F00, 14.F.(12)(C)1). ALL BALANCE SCREWS ARE P07 OR P14. ASDR ASAA2019070529951Spacer · unbondedWHILE ACCOMPLISHING TC 78472010 #2 ENGINE FOUND 12 SPACERS WITH UNBONDED MATERIAL AND REQUIRES REPLACEMENT. GROUNDED - YES. REMOVED AND REPLACED 12 SPACERS AS REQUIRED ON #2 ENGINE REF TC 78472010.SDR ASAA2019070429914Fastener · looseREF T/C #78472000 #2 ENG INLET AND FANBLADES- DETAILED INSP. FOUND #1 1'O'CLOCK POS STRUT DAMAGED BY LOOSE FASTENER #1 RT MIDDLE FASTENER (M) ALF. GROUNDED - YES. REPLACED #2 ENG #1 O'CLOCK POS AFT ACOUSTICAL PANEL REF AMM 72-23-02/601.SDR ASAA2019070129890Spinner · damagedWHILE ACCOMPLISHING T/C # 78472010 FOUND #1 ENGINE SPINNER CONE DAMAGE. GROUNDED - YES. REPLACED #1 ENGINE SPINNER CONE REF. T/C # 78472010.SDR ASAA2019062499763Nut Plate · corroded#2 ENG INLET AND FANBLADES - DETAILED INSPT. S/N 862264. FOUND 5 EACH NUT PLATES THAT HAVE CORROSION UNDER THEM ON R/H SIDE AFT END OF FAN FRAME. 1 EACH #3 ACOUSTICAL PANEL FWD MIDDLE NUT PLATE, 1 EACH #4 FWD R/H NUT PLATE ON #4 ACOUSTICAL PANEL, 2 EACH #5 ACOSDR ASAA2019061829743Panel · damagedNR 2 ENG INLET AND FAN BLADES - DETAILED INSPT. FOUND NR 3 STRUT PANEL AT 3 O'CLOCK POS. HAD 2 LOOSE FASTENER UPPER MIDDLE POS. THAT HAS DAMAGE TO FASTENER AND PANEL. GROUNDED - YES. REMOVED AND REPLACED NR 3 STRUT PANEL AT 3 O'CLOCK POSITION WITH NEW REF IAW SDR UIEA2019061904527Spinner · crackedFOUND THE NR 1 ENGINE FAN BLADE SPINNER CRACKED. R & R THE NR 1 ENG SPINNER DOME IAW AMM 72-31-01.SDR IPXA2019062443665Bulkhead Web · crackedNR 2 ENG INLET COWL AFT BULKHEAD WEB CRACKED 3 O'CLOCK POSITION AT SENSE LINE FITTINGREPAIR PER PW SRM 54-10-00 REPAIR #14SDR IPXA2019062443664Bulkhead Web · crackedNR 2 ENG INLET COWL AFT BULKHEAD WEB CRACKED 9 O'CLOCK POSITION AT SENSE LINE FITTINGREPAIR PER PW SRM 54-10-00 REPAIR #14SDR ASAA2019061229682Blade · damagedWHILE ACCOMPLISHING T/C #78472010, RE-MAPPING THE #2 ENGINE REQUIRED REPLACEMENT OF 5 PAIRS. GROUNDED - YES. REPLACED ALL 5 PAIRS OF BLADES. REF T/C #78472010.SDR CA190809017Bushing · worn(CAN) FLIGHT CREW ADVISED MTCE THE THE #1 ENGINE WAS PERSISTENTLY APPROACHING (BUT NOT EXCEEDING) ITT LIMITS DURING STARTS. MOC REQUESTED AN INSPECTION OF THE VGV SYSTEM. AN UNUSUAL AMOUNT OF PLAY WAS FOUND IN ONE OF THE ACTUATORS (MASTER) ON REMOVAL THE ATTASDR ASAA2019061029665Spinner · erodedWHILE ACCOMPLISHING INLET INSP ON #1 ENGINE (REF T/C 78472000) FOUND FRONT SPINNER CONE EROSION BEYOND LIMITS. GROUNDED - YES. REMOVE AND REPLACE SPINNER CONE ON #1 ENGINE REF B737-800 AMM 72-21-01-000-801-F00 AND 72-21-01-400-801-F00.SDR HALA2019061000286Eec · malfunctionedATB - ENG L SYS FAIL ENROUTE FOLLOWED BY REV L FAULT. PERFORMED EEC1 RTS TEST. TEST FAILED. EEC BOX FAULT. REMOVED & REPLACED EEC1 PER AMM 73-21-01. RTS TEST PASSED. PERFORMED FUNCTIONAL CHECK OK L REV PER AMM 78-30-00-720-801. OPS NORMAL. OK FOR SVC.SDR ASAA2019060769608Platform · damagedWHILE ACCOMP TC 78472010 FOUND PLATFORM ELASTOMER DAMAGE BEYOND 40" #1 ENG POSN. GROUNDED - YES. REPLACED ALL 24 PLATFORMS REF T/C 78472010 SUBTASK 839-095.SDR ASAA2019060629607Spacer · debondedWHILE ACCOMP TC 78472010 FOUND 4 SPACERS WITH DISBOND ON 2 AREAS. GROUNDED - YES. REPLACED THE 4 SPACERS REF T/C 78472010 SUBTASK 839-046.SDR ASAA2019060659600Stop Pin · wornREF TASK CARD # 78472010, #2 ENG S/N 896760 DURING FAN BLADE LUBRICATION THE RETAINING FLANGE AXIAL STOP PINS WERE FOUND WORN. GROUNDED - YES. INSTALLED NEW AXIAL STOP PINS IN THE AFT FACE OF THE RETAINING FLANGE REF B737-800 AMM 72-21-01-900-801-F00 STEP 2E(5SDR ASAA2019060529599Shim · wornREF T/C 78472010, #2 ENG S/N 896760 DURING FAN BLADE LUBRICATION THE FAN BLADE SHIMS MOLYDAG COATING WAS FOUND WORN. GROUNDED - YES. INSTALLED NEW FAN BLADE SHIMS FOR #2 ENG REF T/C 78472010.SDR ASAA2019060659598Spacer · debondedREF T/C 78472010, #2 ENG S/N 896760 DURING FAN BLADE LUBRICATION THE #10 FAN BLADE SPACER ELASTOMER STRIP WAS FOUND DISBONDED. GROUNDED - YES. INSTALLED NEW #10 FAN BLADE SPACER FOR #2 ENG REF T/C 78472010.SDR ASAA2019060229558Spacer · debondedREF TASK CARD 78472010 #1 ENGINE, ALL SPACERS DISBONDED. GROUNDED - YES. REMOVED & REPLACED #1 ENGINE SPACERS W/ NEW PER TASK CARD 78472010.SDR ASAA2019052129430Shroud · erodedWHILE ACCOMPLISHING TASK CARD 78472000 FOUND ABRADABLE SHROUD ON #1 ENG ERODED AND SHOWING PARENT MATERIAL AT THE 6 O CLOCK TO 7 O CLOCK POSITION ALF. GROUNDED - YES. ACCOMPLISHED ABRADABLE SHROUD REPAIR ON #1 ENGINE PER AMM 72-24-02-200-802-F00.SDR ASAA2019052129429Screw · wornREF T/C #78472000, #2 ENGINE, 8-9 OCLOCK A.L.F., LOWER FORWARD FASTENER FOR ACOUSTIC PANEL IS LOOSE/WORN (MARKED). GROUNDED - YES. REMOVED WORN WASHER AND SCREW FASTENER, REPLACE WITH NEW HARDWARE IAW AMM 72-23-02.SDR ASAA2019051829387Platform · gougedFOUND #14 AND #24 PLATFORM GOUGE ON #2 ENGINE. GROUNDED - YES. REPLACED #14 AND #24 PLATFORM ON #2 ENG PER T/C 78472010.SDR ASAA2019051729389Paint · peelingSPINNER FRONT CONE PAINT WORN AND PEELED. GROUNDED - YES. REMOVED AND REPLACED SPINNER FRONT CONE IAW T/C#78472010.SDR AC2R2019051540701Filter · crackedFILTER MAINTENANCE AID (FMA) IS CRACKED. THIS REPORT IS FOR TWO FMA'S WHICH WERE FOUND CRACKED.SDR AC2R2019051513901Filter · crackedFILTER MAINTENANCE AID OF INLET BARRIER FILTER (IBF) IS CRACKED. SUPPLEMENTAL INFORMATION: THERE HAVE BEEN FIVE OF THESE FILTER MAINTENANCE AIDS REMOVED FROM SERVICE FOR CRACKS.
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