JASC 7220
Service difficulty reports · 1,721
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 UALA2012090605042Acoustic Liner · damagedNR 2 ACOUSTIC LINER SEGMENT 6 O'CLOCK POSITION PREVIOUS REPAIR CHIPPING OFF. ACOUSTIC LINER TO BE REPAIRED WITHIN 50 FLT HRS PER AMM. ACCOMPLISHED NEW REPAIR OF PREVIOUS REPAIRED AREA BY REMOVING AND REPLACING ADHESIVE.SDR ASAA2012092192931Shim · damagedFAN BLADE LUBE NR 2 ENG FOUND 24 FAN BLADE SHIMS WITH DAMAGED COATING. ACFT GROUNDED. R & R 24 FAN BLADE SHIMS ON NR 2 ENGINE REF T/C 78472002, PN 340-252-307-0.SDR ASAA2012092192930Panel · looseWHILE ACCOMPLISHING ENG INLET & FAN BLADE INSPECTION ON NR 1 ENG, T/C 78472000, FOUND FAN DUCT PANEL NR 3 WITH LOOSE FASTENER. R & R FAN DUCT PANEL NR 3 IAW MM 72-23-07-400-801.SDR ASAA2012091292875Screw · looseWHILE ACCOMPLISHING TC 78472000 INLET INSP NR 1 ENG ESN 896511 FOUND LOUVER PANEL OTB 60 POSN HAD LOOSE FASTENERS. TIGHTENED LOUVER PANEL AT OTB 60 POSN REF AMM 72-23-07, STEP D (2) (A) 2.SDR ASAA2012091092862Screw · looseNR 2 ENG FAN DUCT PANELS AT 500 AND 700 POSITIONS HAVE 1 EA LOOSE BOLT IAW PANEL. ACFT GROUNDED. SECURED LOOSE FASTENERS AS REQUIRED REF MM 72-23-07. NO DISCREPENCIES NOTED.SDR IPXA2675096Blade · damagedINSPECTION TYPE: ETOP ATB - NR 1 ENGINE BIRD STRIKE, EMERGENCY DECLARED. ACFT IS OOS. REPLACED 14 DAMAGED FAN BLADES ON NR 1 ENGINE; REPAIRED DAMAGE TO ACCOUSTIC LINER AFT OF FAN BLADES; BOROSCOPED ENGINE CORE AND UN-SHINGLED 12 TO 16 HPC 1ST STAGE BLADES.SDR UALA2012080804305Liner · delaminatedFAN EXIT LINER OUTER SKIN DELAMINATING 11:00 O'CLOCK POSITION. AREA IS APPROX 14 INCH BY 5 INCH PICS ON RVI. REPLACED.SDR ASAA2012080392662Panel · damagedNR 1 ENGINE INLET AND FAN BLADES DETAILED INSPECTION FOUND ONE SCREW MISSING AND NUTPLATE MISSING AT 6 O`CLOCK POS ENGINE NOSE COWL LWR VENT PANEL (M). APPLICABLE HOLE IS OVERSIZED & PULLED THRU. R & R WITH NEW PANEL IAW SRM 51-40-02 AND SEALED IAW SRM 51-20-SDR UALA2012080604214Liner · damagedNR 2 ENGINE FAN SOUND ABSORBING LINER HAS A HOLE IN IT AT THE 4 O'CLOCK POSITION IT IS .750 INCH BY .750 INCH, THE HOLE IS ALSO .825 INCH DEEP. SUPPLEMENTAL DATA UPDATE, LARGE AMOUNT OF SOFT AND HARD POTTING MATERIAL IN HOLE FROM EARLIER ATTEMPS TO REPAIR. WSDR ASAA2012082792767Seal · tornDIAGNOSTICS REPORTS, NR 2 ENGINE TREND DATA SHOWS A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. DATA INDICATES HARDWARE INSPECTION AND FAN RELUBE REQUIRED. ACFT GROUNDED. FOUND EXCESSIVE LUBE ON FAN BLADE. FOUND ALL PLATFORMS HAD TORN SEALS. R SDR CA120723021Scoop · cracked(CAN) NR 2 L/E RAM AIR SCOOP DUCT ASSY CRACKED AND PIECE BLOWN OUT. LANDING LIGHTS, LEADING EDGE REPLACEDSDR ASAA2012072192573Seal · tornNR 2 ENG FAN BLADE LUBE FOUND 10 PLATFORMS WITH TORN RUBBER SEALS. ACFT GROUNDED. INSTALLED 10 NEW FAN BLADE PLATFORMS IAW TC 78472002. ACCOMPLISHED VIBRATION SURVEY TEST 7 IAW AMM 71-00-00, NR 2 ENG VIB WITHIN LIMITS.SDR ASAA2012071992574Panel · looseNR 2 ENGINE, FAN DUCT PANEL AT 400 O`CLOCK POSITION, UPPER ROW FWD BOLT LOOSE. ACFT GROUNDED. SECURED NR 2 ENGINE FAN DUCT PANEL BOLT AT THE 400 O`CLOCK POSITION IAW AMM 72-23-02-400-801-F00.SDR UALA2012062903441Rub Strip · damagedNR 2 ENGINE ACCOUSTICAL PANEL MISSING POTTING COMPOUND AT PREVIOUS REPAIR, APPROX 1 1 BY- 69647 :ITEM SHOULD READ FAN BLADE RUBSTRIP MISSING POTTING COMPOUND CF 605. SEE MM72-33-01-801 FOR REPAIR AND MM 72-33-01-601 FOR INSPECTION CHECK. NEED PCN840-0440, 84SDR UALA2012062903431Rub Strip · damagedNR 2 ENGINE ACCOUSTICAL PANEL MISSING POTTING COMPOUND AT PREVIOUS REPAIR, APPROX 11. ITEM SHOULD READ FAN BLADE RUBSTRIP MISSING POTTING COMPOUND CF 605 ^24JUN ORD RCF-P :SEE MM72-33-01-801 FOR REPAIR AND MM 72-33-01-601 FOR INSPECTION CHECK. NEED PCN840-04SDR ASAA2012062092390Blade · wornREF WO 168524, WHILE PERFORMING TASK CARD 7847220, FOUND THE FOLLOWING FAN BLADES WORN ON NR 2 ENGINE, WORN AREAS ABOVE .004 AREA J. REF AMM 72-21-02-801-F00, PARA U. ACFT GROUNDED. REMOVED BLADES.SDR ASAA2012062092389Shim · wornALL BLADE SHIMS NR 2 ENGINE WORN. ACFT GROUNDED. R & R ALL FAN BLADE SHIMS ON NR 2 ENGINE, PN OFF 340-252-307-0, PN ON 340-252-307-0.SDR ASAA2012061792358Seal · unbondedNR 1 ENGINE, PLATFORM AT BLADE NR 4 HAS ELASTOMER SEAL UNBONDED. ACFT GROUNDED. R & R NR 4 & NR 16 BLADE PLATFORM IAW T/C 78472002, STEP 46. C/W ENG NR 1, TEST 7, VIBRATION SURVEY IAW T/C 78472002, STEP 53. VIBRATION SURVEY WITHIN LIMITS.SDR ASAA2012061792357Shim · wornNR 1 ENGINE FAN BLADE SHIMS WORN, ACFT GROUNDED. R & R NR 1 ENG FAN BLADE SHIMS, REF T/C 78472002, STEP 44.SDR ASAA2012061692352Shim · wornCOATING WORN ON ALL 24 FAN BLADE SHIMS ON NR 2 ENGINE. ACFT GROUNDED. R & R ALL 24 FAN BLADE SHIMS ON NR 2 ENGINE IAW AMM 72-21-02.SDR ASAA12511614Seal · missingWHILE PERFORMING FAN BLADE LUBE TASK CARD 78472002. FOUND NR 16 PLATFORM MISSING RUBBER SEALS. ACFT GROUNDED. R & R NR 16 PLATFORM IAW TASK CARD NR 7847002. NR 2 ENG REQUIRES TEST 7. VIBRATION SUEVEY REF AMM 71-00-00, PB 501. COMPLETED NR 2 ENG ENGINE RUNSDR ASAA12511610Shim · wornNR1 ENG FAN LUBE ALL 24 EA FAN BLADE SHIMS WORN. ACFT GROUNDED. REPLACED ALL 24 FAN BLADE SHIMS ON NR 1 ENG REF MM 72-21-02-400-801-F00 & T/C 78472002.SDR ASAA12511600Shim · wornNR 1 ENGINE FAN BLADE SHIMS WORN TO LIMITS (24 EA). ACFT GROUNDED. REMOVED 24 WORN SHIMS FOR NR 1 ENGINE FAN BLADE AND INSTALLED 24 SERVICABLE FAN BLADE SHIMS REF TASK CARD 78472002SDR ASAA12511579Panel · wornNR 2 ENG, NR 3 &NR 4 FAN DUCT PANELS ARE WORN THRU AT ATTACH POINT. ACFT GROUNDED. REPLACED NR 3 & NR 4 FAN DUCT PANELS IAW AMM 72-23-07-400-801-F00.SDR ASAA12511461Cone · gougedDURING NR 1 ENGINE FAN LUBE FOUND DEEP GOUGE ON MATING SURFACE OF FRONT SPINNER CONE. ACFT GROUNDED. R & R FRONT SPINNER CONE ON NR 1 ENG REF MM 72-21-01-400-801-F00.SDR ASAA12511460Shim · wornDURING NR 1 ENGINE FAN LUBE FOUND ALL BLADE SHIMS MISSING MOLYDAG COATING. ACFT GROUNDED. R & R NR 1 ENGINE 24 FAN BLADE SHIMS. REF MM 72-21-02-400-801-F00.SDR ASAA1251459Seal · tornDURING NR1 ENGINE FAN LUBE FOUND 18 OF THE 24 BLADE PLATFORMS WITH TORN OR MISSING SEALS. ACFT GROUNDED. R & R COMPLETE SET OF 24 EA BLADE PLATFORMS ON NR 1 ENG, REF MM 72-21-02-400-801-F00.SDR AALA20120419006Bullet · inoperativeDFW - CREW REPORTED SIGNFICANT ENGINE PRESSURE RATIO SPLIT THAT BECAME WORSE AS ALTITUDE INCREASED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 1 ENGINE PT2 BULLET. SYSTEM GROUND CHECK NORMSDR CALA2012041300260Blades · damagedTAKE OFF ROLL NR 2 ENGINE BIRD STRIKE & VIBRATION 4.5 IN CLIMB. NR 2 ENGINE BSI, FAN BLADES & ACOUSTIC PANELS R & R IAW AMM 72-21-02-000-801.SDR ASAA12511387Shim · damagedWHILE ACCOMPLISHING FAN BLADE LUBE ON NR 2 ENGINE REF T/C 78472002 FOUND FAN BLADE SHIMS MISSING COATING ON ALL 24 SHIMS. REPLACED FAN BLADE SHIMS IN THE PROCESS OF T/C 78472002.SDR MYWA201204130044Cable · out of rigNR 1 ENGINE SLOW TO START & EGT FLASHING CHECK VSV FEEDBACK CABLE STATIC RIG CHECK. ON INITIAL CHECK, FOUND THAT THE NOTCH ON VARIABLE RIG PLATE WAS NOT ALIGNED. ADJUSTED STATICLY VSV FEED BACK CABLE AS PER AMM 75-31-02 PART I & J. ENGINE STARTED FROM FUELSDR ASAA12511383Shim · wornPROTECTIVE COATING ON ALL 24 SHIMS WORN OFF ON NR 1 ENGINE REF T/C 78472002. REMOVED AND REPLACED ALL 24 SHIMS REF T/C 78472002.SDR ASAA12511364Spinner · wornNR 2 ENGINE INTAKE FAN SPINNER CONE IS MISSING MAJORITY OF PAINT. REMOVED SPINNER CONE & INSTALLED NEW REF: AMM 72-21- 01.SDR REXA2012040300475Blade · lack of lubeNR 1 ENGINE FAN VIBRATION, 1.8 IN CAUTION RANGE AT FLT LVL 320. PERFORMED FAN BLADE TANG LUBRICATION IAW AMM 72-21-02. PERFORMED HIGH POWER ENGINE RUN. OPS CHECKED GOOD. OK FOR SERVICE.SDR ASAA12511293Spinner · out of limitsNR 1 ENG INLET SPINNER CONE OUT OF LIMITS PER T/C 78472002 (FAN BLADE LUBE). REMOVED AND REPLACED SPINNER CONE PER AMM 72 21 01. T/C 78472002.SDR ASAA12511292Panel · damagedREF T/C 78472000 NR 1 ENG INLET AND FAN BLADES DETAILED INSP FOUND NR 5 FANDUCT PANEL HAS SEVERAL FASTENERS LOOSE AND DAMAGE W/ DAMAGE TO PANEL. REPLACED NR 5 FANDUCT PANEL AS REQ.SDR ASAA12511291Panel · damagedREF T/C #78472000 NR 1 ENG INLET AND FAN BLADES DETAILED INSPT FOUND NR 1 FAN DUCT PANEL HAS ONE FWD RT FASTENER AND COUNTERSINK DAMAGED. REPLACED NR 1 FAN DUCT PANEL AS REQ.SDR UALA2012032001801Rivet · looseBIRD STRIKE. BIRD STRIKE INSPECTION ACP. NO AIRFRAME DAMAGE NOTED. NEC TO ADDRESS LOOSE RIVETS AT UPPER 2.5 SCREENS ON RT ENG.SDR ASAA12511267Screw · looseNR 1 ENG SEVERAL FASTENERS LOOSE ON FAN FRAME ACOUSTICAL PNLS LEFT SIDE. SECURED FASTENERS NR 1 ENG ON FAN FRAME ACOUSTICAL PNL LEFT SIDE REF AMM 72 23 07.SDR ASAA12511259Fastener · looseNR 1 ENG FAN DUCT PNL LOOSE FASTENERS AT 7 O'CLOCK POSITION VEIW AFT LOOKING FWD. SECURED FASTENERS NR 1 ENG FAN DUCT PNL AT 7 O'CLOCK POS VEIW AFT LOOKING FWD REF AMM 72 23 07.SDR ASAA12511257Fastener · looseNR 1 ENG INLET COWL HAS FASTENER LOOSE AT 6 O'CLOCK POSITION LOOKING INTO FAN. ON DEFERRAL.SDR ASAA12511192Spinner · damagedNR 1 ENG REAR SPINNER CONE AFT EDGE (AT FAN BLADE NR 11) HAS DAMAGE ALONG INTERFACE WITH BLADE PLATFORM (MARKED). REMOVED AND REPLACED NR 1 ENGINE REAR SPINNER CONE REF B737NG AMM 71 21 01.SDR UALA2012030701494Nose Cowl · corrodedNR 2 ENGINE NOSE HAS CORROSION AT 6 O"CLOCK POSITION. REMOVED NR 2 ENGINE NOSE COWL PER MM. INSTALLED NEW NOSE COWL PER MM. ACCOMPLISHED OPS CHECK PER MM. NO FAULTS FOUND.SDR ASAA12511180Panel · looseNR 1 ENG FAN DUCT PANELS HAVE LOOSE FASTENERS & WORN HOLES AT RT SIDE STRUT AT 12:00 LT & RT SIDE OF 6:00 STRUT & BELOW THE 9:00 STRUT. REMOVED & REPLACED THE 12:00 FAN DUCT PANEL THE 9:00 FAN PANEL NR 2 AT THE 6:00 POSITION WITH SERVICEABLE PANELS.SDR ASAA12511140Bolt · looseNR 1 ENG FAN DUCT PANEL AT 4:00 POS (UPPER CTR BOLT) AND 10:00 POS (LWR AFT BOLT) FASTENERS LOOSE. (FINDING DURING C/W T/C 78472000) RE-TORQUED BOLT AT 4:00 POS (UPPER CTR BOLT) RE-TORQUED BOLT AT 10:00 POS (LWR AFT BOLT) REF M/M 72 23 07, OK FOR SVC.SDR ASAA12511094Panel · damagedNR 2 ENGINE FAN DUCT PANEL AT LT SIDE OF 6 O`CLOCK LLDLK STRUT AFT LOOKING FWD HAS TWO LOOSE FASTENERS ONE PULLED THRU PANEL. INSTALLED NEW PANEL PER AMM 72 23 07 000 801 F00 AND 400 801 F00.SDR AALA20120208TUL01Bullet · looseOMA - CREW REPORTED RIGHT ENGINE COMPRESSOR STALL. RIGHT ENGINE REDUCED TO IDLE. EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. INSPECTION FOUND RIGHT ENGINE NOSE BULLET CAME LOOSE. REPLACED FRONT ACCESSORY DRIVE GROUP. SYSTESDR ASAA12511006Panel · damagedWHILE ACCOMPLISHING ASA T/C 78472000 ON NR 1 ENG FOUND FASTENER ON NR 2 FAN DUCT PANEL BETWEEN NR 2 & NR 3 STRUTS PULLING THRU PANEL. UPPER CENTER FASTENER REF MM 72 23 07 000 801 F00 FIG 401. REPLACED FAN DUCT PANEL REF MM 72 23 07.SDR ASAA12510980Fastener · looseREF T/C #78472000 NR 2 ENGINE INLET AND FAN BLADES DETAILED INSPECTION STEP J. FOUND FAN DUCT PANEL 5 HAS 3 LOOSE FASTENERS & POSSIBLE DAMAGE TO FASTENERS INSERTS. OPENED PANEL & INSPECTED FASTENER INSERTS. NO DAMAGE NOTED. RE-INSTALLED PANEL & SECURED PERSDR ASAA12510979Panel · damagedREF T/C #78472000 NR 2 ENGINE INLET AND FAN BLADES DETAILED INSPECTION STEP J. FOUND FAN DUCT PANEL NR 7 HAS DAMAGE FASTENER HOLE & FASTENER LOOSE. REPLACED PANEL PER AMM 72 23 07 400 801 F00. OK FOR SERVICE.
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