JASC 5410
Service difficulty reports · 4,119
Reports filed under 5410 · Nacelle/Pylon, Main Frame, 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 = '5410' 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 = '5410' 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 IPXA09M56931Pylon · damagedCREW REPORTED SEVERE TURBULENCE GOING INTO BNA. DAMAGE TO PYLONS. CONTINUING TURBULENCE INSPECTION FOR FURTHER DAMAGED. REMOVED DAMAGED AREAS AND COLD WORKED DENTED AREA REF EO MD11-5460-34504 B. ACCOMPLISHED HFEC PER NDT SSM 06-10-01-001. NO DEFECTS NOTSDR F3LA2009072700110Cowling · damagedDURING C4 C-CHECK, INSP NOTED THAT THE NR 2 ENGINE OTBD FAN COWL HAS DAMAGE ON THE INSIDE OF COWL, 2 FEET FROM THE TOP AND 1 FOOT FROM THE T/E. MX PERFORMED MAJOR REPAIR TO FAN COWL IAW SRM 54-02-00 AND 54-20-00.SDR FDEA200906302392Fitting · corrodedFOUND CORROSION ON PYLON NR 2 SPIGOT FITTING. REPAIR PERFORMED BY REPLACEMENT OF FITING IAW SB 54-6017, APPROVED BY EA 6-5440-120196.SDR A6WA200940407Structure · crackedRT ENG NOSE INLET COWL BRIDGING PIECE FOUND CRACKED. RT ENG NOSE COWL BRIDGING PIECE REPLACED IAW CMM 20-41-04. (K)SDR FDEA200906202191Fitting · crackedINSIDE THE NR 1 PYLON RT SIDE HAS CRACKED ON THE TOP CORNER OF FITTING P/N 311N5220-56 AT PP STA 186. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96 AND DWG 311N5044 SHEET 5 REV. C. REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.SDR FDEA200906172129Structure · corrodedNR 2 PYLON PLATES AND RIVETS CORRODED ON LT AND RT SIDE OF THE PYLON FOR PANEL NR 441AL. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96 REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.SDR HALA2009061500250Seal · damaged1 INCH CRACK ON THE NR 2 ENGINE LOWER APRON FIRE SEAL L/E 2ND FASTENER HOLE. REPAIRED PER HAL-M-105. FILE NR B10196.SDR OZCA060809001Latch · defectiveON DEPARTURE FROM MIA THE PILOT NOTED THE LT ENGINE COWLING HAD POPPED OPEN AND WAS COLLAPSED AGAINST THE ENGINE. POWER TO THE AFFECTED ENGINE WAS REDUCED AND A UNEVENTFUL LANDING IN MIA WAS PERFORMED. MX INSPECTED THE AIRFRAME , ENGINE AND COWLING AND SUSPESDR 2009FA0000518Support · crackedDURING A SPOT CHECK OF INVENTORY OF SPARE PARTS. FOUND A CRACK ON AN NEW DRIVE END FRAME FOR A STARTER GENERATOR. SUSPECT THAT THE DAMAGE WAS CAUSED WHEN THE FOD SCREEN WAS RIVETED TO THE SUPPORT ASSY. (TOO MUCH FORCE MAY HAVE BEEN APPLIED).SDR DXTA2009052803667Structure · dentedDURING POSTFLIGHT, DISCOVERED DENT IN LT ENGINE PYLON. EVALUATED DAMAGE. REMOVED PYLON LEADING EDGE. INSTALLED NEW LEADING EDGE WITH SEALANT AND RIVETS. PRIMED & PAINTED LEADING EDGE. PER MM 20-33-00. REINSTALLED THE FIRE SEAL REATINERS. IAW SRM 51-30-03.SDR FDEA200905131640Cap · crackedHFEC INSPECTION CARRIED OUT, CRACK APPROXIMATELY 1.5 INCHES LONG FOUND ON THE LT SIDE PYLON UPPER CAP ON RADIUS BETWEEN YID=408 TO YID=410. COMPLIED WITH EA 1-5410-127853, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR UALA2010051901690Fairing · damagedNR 1 ENG PYLON TOP FWD FAIRING (SLIPPER COWL) DAMAGED DURING UNCONTROLLED REVERSER DEPLOYMENT WITH BOTH REVERSER COWLS OPEN FOR MX. ACCOMPLISHED REPAIRS IAW SRM AND UA-EVA-72462. NEEDS TO BE EXAMINED AT THE NEXT 4 CONSECUTIVE C-CKS FOR DAMAGE. REINSPECTED NRSDR GUUA93854041209AKeel · damagedLT NACELLE KEEL DAMAGED PREVIOUS REPAIR. AMENDED REPAIR BY BONDING REPAIR DOUBLERS IAW FAA APPROVED DATA.SDR 2009FA0000445Door · missingRT INBD HINGED COWLING DOOR (PN 109-910027-31) DEPARTED AIRCRAFT. SPINE ASSY (PN 109-910060-1) HINGE ATTACHMENT DAMAGED. NO OTHER DAMAGE TO ACFT NOTED. DOOR AND SPINE ASSY REPLACED WITH SERVICEABLE PARTS. (K)SDR FDEA200904081228Hinge · chafedNR 2 ENGINE INBD FAN COWL DOOR AFT HINGE FITTING, FORWARD LUG HAS A CHAFING AREA. REMOVED DAMAGE IAW EA 6-7110-127945. FOUND TO BE WITHIN LIMITS IAW EA 6-7110-127945; ORIG THICKNESS 0.800. MATERIAL LOSS 0.100. MATERIAL REMAINING 0.700. PRIMED IAW A300-600SDR SWIA200921558Support Beam · crackedENGINE SUPPORT BEAM CRACKED, SB COMPLIANCE. REPLACED CRACKED ANGLE PER SRM.SDR MALA090039Inlet · chafedDURING 30K AND 6Y INSPECTIONS, LT NACELLE LOWER DECK BELOW INLET ASSY IS CHAFED THRU. REPAIREDSDR CA090525006Cowling · departed(CAN) OPERATOR REPORTED THE FOLLOWING TO MFG: DURING A PASSENGER FLIGHT THE LT UPPER ENGINE COWL ACCESS PANEL (PN 228-50080-801) DEPARTED THE ACFT DURING FLIGHT. THE INCIDENT PANEL WAS REMOVED FOR MX ON THE THRUST REVERSER THE NIGHT PRIOR TO THE INCIDENT FLIGHSDR FDEA200902260737Bushing · migratedNR 2 PYLON TO WING ATTACHMENT FITTING LINK HAS A MIGRATED BUSHING AND IS GOUGED. REMOVED AND REPLACED THE BUSHING IAW A310-200 AMM 54-51-75-8. THE GOUGE IS WITHIN LIMITS IAW AIRBUS DWG A54611761 ON THE NR 2 PYLON TO WING ATTACHMENT FITTING.SDR HYIA258PBBeam · crackedLEFT ENGINE OUTBOARD SIDE OF CROSSOVER BEAM IS CRACKED. MAINTENANCE TO REMOVE AND REPLACE CROSSOVER BEAM ASSY.SDR ULXR2009021080900Tube · wornTHIS TUBE WAS WORN AROUND THE CIRCUMFERENCE AT THE POINT WHERE IT PASSES THROUGH THE FIREWALL BOOT. DISCOVERED DURING A 300 HOUR INSP AND REPLACED.SDR ULXR2009021080901Tube · wornTHIS TUBE WAS WORN AROUND THE CIRCUMFERENCE AT THE POINT WHERE IT PASSES THROUGH THE FIREWALL BOOT. DISCOVERED DURING A 300 HOUR INSP AND REPLACED.SDR ULXR2009021080903Tube · wornTHIS TUBE WAS WORN AROUND THE CIRCUMFERENCE AT THE POINT WHERE IT PASSES THROUGH THE FIREWALL BOOT. DISCOVERED DURING A 300 HOUR INSP AND REPLACED.SDR GLBA2009020503Cowling · looseAT 1000FT WITH TORQUE AT 1000'S PROP AT 1550 THE LT ENGINE JUMPED SEVERAL TIMES FROM 50 TO 2000 POUNDS OF TORQUE. MAINTENANCE PERFORMED ENGINE RUNS AND FOUND NO TORQUE SURGE PER BEECH MM 76-10-00. UPON FURTHER INVESTIGATION MAINTENANCE DISCOVERED THE COWLINGSDR FDEA200901280347Frame · crackedNR 1 ENGINE NOSE COWL AFT EDGE IS CRACKED AND SECTION TORN AT 4 O'CLOCK POSITION BS 1200 CUT OUT DAMAGED AREA IAW SRM 51-10-1. FABRICATED REPAIR PARTS AND 1 FILLER IAW SRM 54-10-2 FIG 1 AND 54-10-3 FIG 3. INSTALLED REPAIR PARTS IAW SRM 51-30-2.SDR QXEA2009012700046Diaphragm · crackedPDX - C1 - LT NACELLE DIAPHRAM IS CRACKED JUST ABOVE THE NR 3 FLAP TRACK. DRILLED OFF CRACKED DIAPHRAM AND WEB, STARTED FABRICATION OF MODSUM ANGLES. REF TASK CARD 6-54-441. FINISHED THE FABRICATION OF THE MODSUM ANGLES, LOCATED AND DRILLED UP THE NEW DIAPHSDR HALA2009012400034Strut · brokenETOPS SIGNIFICANT SYSTEM, NR 1 ENG INBOARD EXHAUST COWL HOLD OPEN STRUT JOINT BROKEN. REMOVED AND REPLACED HOLD OPEN STRUT. OPS/SECURITY CHK OK.SDR UPS09554684Structure · crackedINSPECTION TYPE:C NR 1 PYLON FWD AND AFT SLEEVE BOLT HOLE SHOW CRACK INDICATIONS. REMOVED BTH FWD/AFT SLEEVE BLT HOLES TO REMOVE CRACK, HOLE DIA AFTER REAM PER EO757-5410-17144 0.7815" HFEC IAW 757NTM51-00-16 PT6. NO CRACK FOUND (ROTO PROBE) REMOVED FWD/AFT SDR UPS09554683Strut · crackedINSPECTION TYPE:C NR 2 PYLON STRUT TO UPPER LINK FITTING, 2 UPPER VERTICAL HOLES HAVE CRACK INDICATIONS (HFEC). HFEC UPPER LINK FITTING NDT51-00-16 PT6 IND CRACK IN HOLES. HFEC UP LNK STRUT HOLES IAW NDT51-00-17 PT6 IND NO CRACK. REMOVED 2 DISCREP HOLES TO SDR UPS09554333Fitting · wornINSPECTION TYPE: C2 NR1 T/R INBD T/R AFT LWR CORNER FITTING IS WORN AND CHAFED. REMOVED AND REPLACED FITTING IAW EM 70-42-28-300-005.SDR CA090121007Beam · chafedDURING ANNUAL INSPECTION, FRETTING RESIDUE WAS NOTED ON BOTTOM OF LEFT HAND PYLON BEAM ASSEMBLY 427-010-201-107. FURTHER INVESTIGATION AND SUBSEQUENT REMOVAL OF THE BEAM REVEALED CHAFING DAMAGE TO PYLON BEAM 427-010-201-107, ADAPTER 427-010-206-101 AND HOSE 4SDR HYIA3292MBeam · crackedRIGHT ENGINE'S INBOARD ENGINE BEAM IS CRACKED AT THE AFT UPPER WEB 0NE HALF OF AN INCH. REMOVAL AND REPLACEMENT OF THE ENGINE BEAM.SDR HYIA660CABeam · crackedRIGHT ENGINE'S INBOARD ENGINE BEAM CRACKED AT AFT UPPER WEB . REMOVAL AND REPLACEMENT OF ENGINE BEAM.SDR GUUA93854112308AKeelbeam · crackedAT SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT NACELLE KEEL HAS A .75 INCH CRACK. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLERS.SDR DL757081485Strut · damagedDURING THE PYLON MOD, THE NR 2 PYLON LT SIDE STRUT WAS FOUND WITH SEVEN OVERSIZE HOLES. SIX OF THE HOLES WERE CLEANED UP FOR OVERSIZE FASTENERS AND ONE HOLE WAS BUSHED TO THE ORIGINAL HOLE SIZE PER BOEING INSTRUCTIONS.SDR GUUA93654102008AKeel · chafedDURING SCHEDULED ROUTINE MX DISCOVERED LT NACELLE KEEL CHAFING AT THE INBD SIDE FENDER ATTACHMENT FLANGE. REMOVED DAMAGED AREA AND INSTALLED FILLER AND CAP REPAIR DOUBLER.SDR 08FDEA04392Cowling · gouged1 ENGINE INBD FAN COWL IS GOUGED ABOVE THE MID LATCH. CLEANED UP DAMAGE, CHECKED LIMITS, REQUIRES REPAIR. REMOVED SURFACE FINISH, FABBED DOUBLER, ALODINED & PRIMED AREA IAW SRM 51-71-00. SEALED DOUBLER EDGES BOND LINE IAW SRM 51-71-00.SDR 08FDEA04374Bearing · migratedNR 1 PYLON AFT MOUNT FOUND WITH BEARING MIGRATION. REMOVED AND REPLACED WITH NEW HIGHER FITTING ASSEMBLY AS PER SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR DL757081543Structure · damagedNR 2 ENG PYLON INBD LOWER CHORD STA 128 6 FASTENERS AT 5/16 STANDARD SIZE AND 1 AT 3/8 STANDARD SIZE. NOT PER DRAWING, INCOMING DEFECT. FABRICATED FREEZE PLUG REFERENCE ERA 471169-14, STEP 4. INSTALLED FREEZE PLUGS AND FASTENERS IAW ERA 471169-14 STEPS 1, 2SDR WRLA2008082Structure · crackedCORROSION - DURING BRIDGE CHECK, EGAT MECHANIC FOUND NR 3 ENG LT CORE COWL AFT FRAME CRACK AT 9 O’CLOCK POSITION. (REFER TO EGAT NRC U05049). REPAIRED IAW EI W2008A54B-1056 REV 00, AND EI 2008A54B-1056 REV 01.SDR WRLA2008083Frame · crackedDURING BRIDGE CHECK, MX FOUND NR 3 ENGINE LT CORE COWL AFT FRAME CRACK AT 7 O’CLOCK POSITION. REPAIRED CRACK IAW ENGINEERING INSTRUCTION W2008A54B-1082 REV 00.SDR DALA1220369019Latch · wrong partLEFT ENGINE COWL LATCH HOOK ASSEMBLIES (4) WERE ACTUALLY HAD THE WRONG PART NUMBER AND REPLACED IAW 09-056907-12.SDR RYN2008F00022Nose Cowl · dentedNR 3 ENGINE NOSE COWL HAS DENT AT 5 OCLOCK POSITION, LEADING EDGE. REMOVED DENTED AREA AND ACCOMPLISHED NOSE COWL LEADING EDGE LIP SKIN REPAIR IAW SRM 54-30-1, 54-30-3, AND 51-30-2, 51-20-00, 51-31-00. (K)SDR GUUA09300802Keelbeam · crackedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT NACELLE INBOARD KEEL HAS .75 INCH CRACK FORWARD AND ABOVE LANDING GEAR BOLT. REMOVED AND REPLACED INBOARD KEEL.SDR 08FDEA03905Heat Shield · wornNR 2 ENGINE LEFT FAN COWL LOWER FWD INSIDE CORNER CHAFFING PLATE IS WORN AND TORN. REMOVED LOWER FWD HEAT SHIELD. FABRICATED REPAIR FOR HEAT SHIELD AND INSTALLED DC/MD-10 DAC DWG ATL OO55 AND SRM 51-31-01; VOL II.SDR QXEA200801006Frame · chafedC4-CHECK - LT NACELLE TAIL PANEL, 414AR THE THIRD FRAME AFT FROM THE FWD EDGE IS CHAFED SEVERELY AT THE UPPER END. BLENDED OUT MINOR CHAFE IAW D8 Q400 SRM 51-14-00, PG 201, PARA 1-5B, STEP 2. MEASURED, BLEND MATERIAL REMOVED. ALODINED AND PRIMED IAW D8 Q400 SRSDR DL76P081162Door · missingFOUND NR 2 ENG INBD AFT NACELLE STRUT ACCESS DOOR MISSING. FORWARD TO MCO PER CDL 54-53-02.SDR AALA200802260Bushing · corrodedAFW RT UPPER SPAR FITTING HAD PITTING ON BUSHINGS. REPAIRED PER SRM 54 52 90 2R WITH THE FOLLOWING DEVATION. AFTER PERFORMING STEP 5 IT IS ACCEPTABLE TO SKIP TO STEP 16.SDR 08FDEA03682Support · brokenNR 2 ENGINE NOSE COWL ANTI-ICE PICCOLO TUBE SUPPORT LINK AT THE 12 O'CLOCK POSITION IS BROKEN & DISCONNECTED. REMOVED & REPLACED THE NR 2 NOSE COWL IAW AMM 71-11-00-04.SDR 08FDEA03681Support · brokenNR 1 ENGINE NOSE COWL ANTI-ICE PICCOLO TUBE SUPPORT LINKS AT THE 7; 12 & 2 O'CLOCK POSITIONS ARE BROKEN & DISCONNECTED. (TOTAL 8 LINKS) REMOVED & REPLACED THE NR 1 ENGINE NOSE COWL IAW AMM 71-11-00-4.
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