JASC 5420
Service difficulty reports · 3,949
Reports filed under 5420 · Nacelle/Pylon Miscellaneous Structure, 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 = '5420' 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 = '5420' 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 IPXA2M75206Fairing · crackedINSPECTION TYPE: 4C, NR 3 PYLON LOWER AFT FAIRING FOUND WITH A CRACK PROPAGATING FROM PREVIOUS STOP-DRILL REPAIR NEAR YPN297. REPAIRED NR 3 PYLON LOWER AFT FAIRING IAW EA 011-5450-01-A4215 REV IR AND UPS EO MD11-5450-48454-A.SDR UALA2012081604566Latch · damagedLEFT INBD PYLON ACCESS PANEL AFT LATCH IS UNHOOKED. FOUND LATCH DAMAGED REPLACED LT INBOARD PYLON LATCH.SDR FDEA201208132963Web · crackedNR 3 PYLON ON UPPER WEB STATION YN = 224 MISREPAIRED. REPAIRED IAW EA 8-5450-159884. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.SDR EIAA20120813059Structure · chafedNR 4 PYLON STRUT FORWARD ENGINE MOUNT BULKHEAD O/B CHORD CHAFED. PERFORMED BLEND OUT OF DAMAGE LAW B747 SRM 54-10-01. PERFORMED UT THICKNESS CHECK OF BLENDED AREA LAW B747 NDT MANUAL PART 4/51-00-00, OUT OF LIMITS AS PER B747 SRM 54-10-01 FIG 1. REMOVED ANSDR EIAA20120813058Structure · chafedNR 3 PYLON STRUT FORWARD ENGINE MOUNT BULKHEAD O/B CHORD CHAFED. PERFORMED BLEND OUT OF DAMAGE LAW B747 SRM 54-10-01. PERFORMED UT THICKNESS CHECK OF BLENDED AREA LAW B747 NDT MANUAL PART 4/51-00-00, OUT OF LIMITS AS PER B747 SRM 54-10-01 FIG 1. REMOVED ANDSDR AALA20120810007Web · crackedRIGHT PYLON UPPER WEB AT GENERATOR FEEDER CABLES, PASS THROUGH. INSTALLED REPAIR DOUBLER AND FILLER SHIM ON RIGHT PYLON UPPER WEB AT GENERATOR FEEDER CABLES PASS THROUGH PER 767 AARD 54-52-01-1.SDR DALA1244950684Structure · delaminatedMAINTENANCE DISCOVERED DELAMINATION ON THE NR 2 ENGINE NOSE COWL AT THE 7 O`CLOCK POSITION WHERE INLET LIP MEETS COMPOSITE. INSTALLED PERMANENT REPAIR TO NR 2 INLET COWL IAW SRM 54-11-01.SDR KCSA201208071144Stiffener · chafedNR 2 PYLON LEFT SIDE IS CHAFED AT STIFFENER FOR COMPENSATOR VALVE.SDR AALA20120806001Web · crackedLEFT PYLON UPPER TORQUE BOX FEEDER CABLE THRU HOLE CRACKED. INSTALLED DOUBLER REPAIR PER AARD 54-52-01-1.SDR C77A20120805031Washer · looseRT PYLON OTBD AFT ATTACHMENT WASHER, IS LOOSE. REMOVE CASTELLATED NUT, CHECK RUN-ON TORQUE AND REINSTALL AND TORQUED NUT TO SPECIFIED TORQUE VALUE LISTED IN ETD AND RESAFTIED IAW ETD 2012-170-010558 AND EA E175-54-104 REV IR.SDR C77A20120805030Washer · looseLT PYLON OTBD AFT ATTACHMENT WASHER IS LOOSE. REMOVE CASTELLATED NUT, PN PE22072L14, CHECK RUN-ON TORQUE AND REINSTALL AND TORQUED NUT TO SPECIFIED TORQUE VALUE LISTED IN ETD AND RESAFTIED ON WO 526397-427 IAW ETD 2012-170-010558 AND EA E175-54-104, REV IR ONSDR UALA2012080604212Strip · looseRUBBER STRIP LEFT ENGINE INBD SIDE COMING APART, PER SRM SECURED RUBBER STRIP IN PLACE.SDR FDEA201208022816Web · crackedNR 1 PYLON, INTERNAL WEB BETWEEN RIB A 11 AND RIB J 08 HAS A 2 INCH CRACK, AREA IS FORWARD OF PRE-COOLER. STOP DRILLED CRACK IAW SRM 54-52-11 PG 202. NDT VERIFIED STOP DRILL AT THE END OF CRACK IAW NTM 51-10-08. REPAIRED IAW SRM 54-52-11, FIG 201 (SHEET 1 SDR QXEA2012073000766Intercostal · crackedCRACKED INTERCOSTAL ON LT NACELLE, VIEWED THRU BOAT TAIL ACCESS INTERCOSTAL IS FOR FINGERNAIL MOUNTING. REMOVED CRACKED INTERCOSTAL ON LT NACELLE IAW SRM 51-42-05-02-01. RECEIVED NEW INTERCOSTAL AND MATCH DRILLED TO EXISTING STRUCTURE IAW SRM 51-40-07-02-01.SDR USAA2012073000004Support · crackedC6 PHASE CHECK - CRACK ON RIGHT WING PYLON INBOARD TOP SIDE AT LOUVERED PANEL LANDS SUPPORT AT RIB 7. REPAIRED RIGHT WING PYLON INBOARD TOP SIDE AT LOUVERED PANEL LANDS SUPPORT AT RIB 7 IAW A320 SRM 54-50-00, 51-42-11.SDR USAA2012073000032Structure · damagedC3 CHECK - LEFT PYLON INBOARD LOWER CHORD UPPER BOLT HOLE ELONGATED. REPAIRED CHORD IAW EA 104119.SDR SWAA2013012111611Strip · crackedUPPER PYLON PHENOLIC NUT PLATE STRIP CRACKED (3 LOCATIONS) ALONG AFT EDGE OF PANEL 57710L. REPAIRED UPPER PYLON PHENOLIC NUT PLATE STRIPS PER EA 1-354-1468.SDR AALA20120715003Angle · crackedMID SPAR FITTING CLOSE OUT ANGLE CRACKED. REMOVED AND REPLACED ANGLE.SDR AALA20120713004Web · crackedLEFT PYLON UPPER WEB CRACKED AT INTEGRATED DRIVE GENERATOR FEEDER CABLE THRU HOLE. INSTALLED DOUBLER REPAIR PER AARD 54-52-01-1.SDR FDEA201207122557Web · crackedNR 2 ENGINE PYLON OTBD LATERAL PANEL BETWEEN RIB 6 -7 HAS TWO CRACKS BOTH MEASURE .75 OF AN INCH. STOP DRILLED CRACKS IAW SRM 54-52-31, PG 212, 213, 214 CONFIG 1 INSTALLED. REPAIR DOUBLER IAW A310-200, 54-52-31, PG 215.SDR UALA2012071203781Support Beam · wornNR 2 ENGINE INBD FAN COWL SUPPORT BEAM INSTALLATION WEB WORN. REPAIRED NR 2 ENG INBD ENG COWL SUPPORT WEB IAW ECRA 5450-01968. MINOR REPAIR.SDR QXEA2012062800563Angle · crackedLEFT ENGINE SPLINE COWL HAS A CRACKED ANGLE BY THE FORWARD HINGE FOR PANEL 412AL AND A POSSIBLE CRACK ON THE ANGLE BY THE FORWARD HINGE FOR PANEL 412AR. REPLACED ANGLES IAW SRM 51-41-00-00-01, AND 51-42-05-02-01.SDR AALA20120628004Web · crackedLEFT PYLON FORWARD TORQUE BOX FEEDER CABLE THRU HOLE CRACKED. REPAIRED PER AARD 54-52-01.SDR A6WA201240700Panel · damagedPANEL NR422 DB DIVIDER PANEL KNIFE EDGED. REMOVED UNSERVICEABLE DIVIDERS AND REPLACED WITH SERVICEABLE IAW SRM 51-42-06.SDR USAA2012070900039Channel · crackedQ1 CHECK - VERTICAL CRACK ON NR 2 ENGINE PYLON LOWER FRAME CHANNEL AT NAC STA 319, WL 119.0. REPLACED NR 2 ENGINE PYLON LOWER FRAME CHANNEL AT NAC STA 319, WL 119.0 IAW B737 SRM 51-40-02-0G, FIG 9 & 12.SDR UALA2012062903436Cowling · dentedCREW REPORT: DENT ON RT ENGINE COWLING BEHIND OIL SERVICE DOOR SAMC TEXT: LCL MAINT REPORTS: NR 2 ENGINE LEFT FAN COWL HAS A SMOOTH DENT APPROX 9.0\L X 6.0\W X 0.03125\DEEP, LOCATED AFT OF OIL SERVICE ACCESS PANEL, NO DELAMINATION, CRACKS OR CREASE. BEYOND ASDR U2RA201206210001Beam · crackedNR 2 PYLON OTBD SKIRT FAIRING BEAM L/E CRACKED. 4 CRACKS EXTEND FROM FASTENER HOLE. CRACK LENGTHS .8"SDR AALA20120612006Torque Box · crackedCRACKS IN THE LEFT PYLON FORWARD TORQUE BOX AT FASTENER HOLES. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 54-52-01-1.SDR USAA2012062100022Fitting · corroded3S CHECK - CORROSION ON RIGHT PYLON SPIGOT FITTING BETWEEN PYLON STA 4697 TO STA 4954, & BETWEEN RIB 5 TO RIB 4. REPLACED RIGHT PYLON SPIGOT FITTING IAW A320 SRM 54-51-12.SDR ABXA20120604359Angle · crackedANGLE BRACKET CRACKED ON I/B SIDE & O/B SIDE BROKEN BELOW HYD BAY DOORS 1ST LATCH, ABOVE EXHAUST NOZZLE. REPLACED CRACKED ANGLE BRACKET P/N 313T1380-31 IAW B767 SRM 51-40-02, ACFT WAS GROUNDED.SDR USAA2012062500031Hinge Fitting · damaged2S CHECK - ELONGATED HOLE ON NR 1 ENGINE PYLON OUTBOARD FAN COWL AT NR 1 HINGE AT PYLON NACELLE STA 409. REPLACED NR 1 ENGINE PYLON OUTBOARD FAN COWL AT NR 1 HINGE IAW A319 SRM 51-42-11.SDR UALA2012060103044Seal · damagedNR 2 ENGINE PYLON GAP STRIP 2ND FROM FWD BLENDED BEYOND LIMITS. REPAIRS TO GATORBACKS COMPLETE. DAMAGE TO GAP SEAL. GAP COVER STRIPS REPLACED AND FWD SEAL.SDR QXEA2012053100446Stiffener · crackedPANEL 424AL AFT STIFFENER IS CRACKED. REMOVED STIFFENER AND INSTALLER NEW IAW SRM 51-42-05-02-01. TREATED AND PAINTED IAW SRM 51-25-05-02-01.SDR QXEA2012053100445Stiffener · crackedPANEL 424AR, AFT STIFFENER IS CRACKED. REMOVED STIFFENER AND INSTALLER NEW IAW SRM 51-42-05-02-01. TREATED AND PAINTED IAW SRM 51-25-05-02-01.SDR QXEA2012053100444Stiffener · crackedNACELLE PANEL 414AR AFT STIFFENER IS CRACKED. REMOVED STIFFENER AND INSTALLED NEW IAW SRM 51-42-05-02-01. TREATED AND PAINTED IAW SRM 51-25-05-02-01.SDR UALA2012052903014Rub Strip · wornNR 2 ENGINE PYLON IS WORN WHERE CNA SPRING SEAL MEETS PYLON. WEAR IS 0.012" DEEP. MAJOR REPAIR ACCOMPLISHED. REMOVED WORN WEAR STRIP & DOUBLER. FABRICATED & INSTALLED NEW WEAR STRIP & DOUBLER REF SRM 54-51-12 FIG 202. SRI RE-INSPECTION CAPTURED ON BY CF90SDR UALA2012052702984Angle · crackedNR 2 ENGINE PYLON LT SIDE ANGLE CRACKED AT NACELLE STA 156.00 AND STA 161.00. MAJOR REPAIR ACCOMPLISHED: REMOVED AND FABRICATED NEW ANGLE. INSTALLED NEW ANGLE PER SRM 51-40-02.SDR UIEA2012052700252Barrel · crackedENGINE 4 INLET COWL OUTER BARREL CRACKED AT 9 O'CLOCK. TIME LIMITED REPAIR ACCOMPLISHED IAW EO4471A094.SDR REXA2012052400917Fairing · crackedHINGE LINE FAIRING 422DB CRACKED. REMOVED AND REPLACED HINGE LINE FAIRING 422DB IAW ARM 51-42-06.SDR R61A201205230296Stiffener · crackedWHILE A/C WAS IN FOR HEAVY CHECK FOUND RT PYLON OUTBOARD PNL 429YR NUT PLATE HOLE AREA HAS A CRACK. MX CUT OUT DAMAGED AREA AND FABRICATED FILLER AND DOUBLER AS A PERMANENT REPAIR IAW EMB ETD 2012-170-007462. PN 170-38356-002. A/C REMAINS IN CMH FOR HEAVY CHSDR SWIA201231075Support · crackedRIB SUPPORT CRACKED NEAR RIGHT NACELLE AFT OUTBOARD EXHAUST MOUNT UNDER CRADLE BLANKET. (C-CHECK) REPLACED RIGHT OUTBOARD AFT HALF FRAME AT EXHAUST MOUNT POINT IN REFERENCE TO 120 SRM.SDR UALA2012111906649Mount Fitting · wornNR 2 PYLON TO ENGINE LT AND RT SIDE MOUNT FITTING WEAR WAS BLENDED REF ECRA:5451-01086. PERFORMED HFEC INSPECTION WITH NO DEFECTS FOUND.SDR FDEA201205151814Structure · crackedNR 2 PYLON, HORIZ FLANGE FASTENER HOLE CRACKED IN TITANIUM RT THIRD HOLE FROM AFT BULKHEAD. REAMED HOLE TO .405 IAW EA F-5450-157204 STEP1, AND 2ND HOLE TO .437 IAW EA F-5450-157204, STEP 3, NDT CHECK FOR CRACK, NO CRACK NOTED. INSTALLED FASTNER IAW-SRM-51-40SDR QXEA2012051300383Angle · crackedLEFT NACELLE AT UPPER DECK BOTH STIFFENING ANGLES ARE CRACKED. REMOVED LT STIFFNER IAW SRM 51-42-05. REMOVED RT STIFFNER AND DRILLED UP NEW LT AND RT STIFFNERS IAW SRM 51-42-05.SDR UALA2012051102733Fastener · looseFOUND EIGHT LOOSE FASTENERS ON RT NACELLE STRUT AFT FAIRING HEAT SHIELD FWD SEAL, REMOVED & REPLACED FASTENERS.SDR UALA2012051002692Web · crackedFWD END OF NR 2 PYLON, INTERNAL WEB IS CRACKED. STOP DRILLED CRACK, REF S RM54-52-12. ACCOMPLISHED WELD REPAIR PER SRM 54-50-00. INSTALLED DOUBLER REPAIR OVER WELD PER SRM 54-52-12 FIG 207, SHEET 2. N-R F1834T.SDR A6WA201240534Bracket · brokenT2 SENSE LINE BRACKET BROKEN, SUPPORT BRACKET FOR THE T2 SENSE LINE ON TOP OF THE ENGINE. REMOVED ENG INLET AND INSTALLED A NEW SERVICEABLE BRACKET.SDR ABXA20120504341Beam · crackedRIGHT PYLON LOWER FWD INBD ANGLE CRACKED AND HAS PULLED THROUGH RIVETS, INBD SIDE OF PYLON AT LOWER FWD CORNER OF HYDRAULIC COMPARTMENTS. REMOVED AND REPLACED NR 2 INBD PYLON BEAM IAW B767 SRM 51-40-02, ACFT WAS GROUNDED.SDR AALA20120505010Web · crackedNUMBER 1 ENGINE LEFT PYLON UPPER TORQUE BOX SKIN HAS POSSIBLE CRACK AT AFT OUTBOARD AND FORWARD INBOARD NUT PLATE LOCATIONS FOR GENERATOR FEEDER CABLE PASS THRU. INSTALLED DOUBLE REPAIR PER AARD 54-52-01-1.SDR ASOA201201558Support Bracket · crackedTWO SUPPORT BRACKETS CRACKED ON NOSE INLET COWLING OTBD SIDE. R & R SUPPORT BRACKETS IAW SRM 51-21-06 AND CMM 71-61-01-400-001-A01.
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