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 UALA2011071503602Structure · damagedAS REPORTED ON STATUS NR 1 ENG HAS BIRD STRIKE DAMAGE. REPLACED NR 1 ENG INLET COWL PER MM.SDR UALA2011070103230Fairing · crackedLARGE CRACK ON NR 4 ENGINE PYLON AT ATTACHMENT JOINTS. ACCOMPLISHED INSP OF NR 4 PYLON SAILTAIL FAIRING PER MM. ALL NORMAL, NO DEFECTS NOTED.SDR A6WA201140725Seal · chafedLT UPPER NOSE COWL T/E SEAL CHAFED. R & R LT UPPER NOSE COWL SEAL IAW CMM 71-14-01.SDR UALA2011062303099Nose Cowl · damagedNR 1 NOSE COWL DAMAGED AT 8 O'CLOCK POS. REPLACED NOSE COWL.SDR FDEA201106202341Shim · looseEXISTING REPAIR THE LT WING OTBD NACELLE FITTING HAS SHIM MIGRATION BETWEEN THE WING SURFACE. EA F-5740-146462, PART 1. REPAIR CLASSIFIED AS MAJOR.SDR CA110617004Structure · departedUPON LANDING, THE RT ENGINE LOWER FAN COWL, FELL OFF THE ACFT ON THE RUNWAY. THE ACFT TAXIED TO THE GATE UNEVENTFULLY. INVESTIGATION REVEALS THAT THE ACFT HAD AN A1 CHECK THE NIGHT BEFORE AND THE COWLS WERE OPEN. THIS WAS THE SECOND LANDING OF THE DAY WHENSDR CA110617003Plate · damagedDURING "A"-CHECK FOUND DAMAGE ON LT NACELLE FIREWALL INTERFACE PLATE, PN 82454317 AND ON HYD TUBE, PN 82974222-001. THE HYD TUBE IS FIXED ON THE INTERFACE PLATE WITH A WASHER AFT OF THE INTERFACE PLATE AND A WASHER/NUT ON THE FWD SIDE OF THE PLATE. THE AFT WASDR FDEA201106142243Bushing · gougedRIGHT PYLON OTBD WING STRUT BUSHING HAS GOUGES. R & R BUSHING IAW SOPM 20-50-03 AND EA F-5720-146285. MAJOR REPAIRSDR IPXA1567635Fitting · nickedINSPECTION TYPE:MOD, WHILE ACCOMPLISHING HFEC INSP IAW EO B757-5410-17144J FOUND SHARP NICK IN FASTENER HOLE CODE "D" (REF FIG 4) ON NR 1 PYLON UPPER LINK FITTING OTBD HOLE. REPAIRED IAW ER NR11-03082, DATED 06-29-11.SDR IPXA11567591Fitting · nickedINSPECTION TYPE:MOD, WHILE ACCOMPLISHING HFEC INSP IAW EO B757-5410-17144. FOUND SHARP NICK IN FASTENER HOLE CODE "D" (REF FIG 4) ON NR1 PYLON UPPER LINK FITTING OTBD HOLE. REPAIRED IAW ER 11-03082, DATED 06-28-11.SDR FDEA201106052121Fitting · corrodedNR 1 PYLON SPIGOT RECEPTACLE FITTING HAS PITTING CORROSION ON UPPER PLATE. REMOVED NR 1 PYLON IAW AMM 54-50-00-4. REMOVED AND REPLACED UPPER AND LOWER SPIGOT FITTINGS IAW S/B 54-2020 PARA B(6). REINSTALLED NR 1 PYLON IAW AMM 54-50-00-4. COMPLIED WITH EA-5450-SDR UALA2011052702596Inlet · delaminatedNR 1 ENG INBOARD FAN COWL HAS A LARGE AREA OF DELAMINATION LOWER FWD CORNER. FOUND ONE LAYER OF DELAMINATED FIBERGLASS INSTALLED OVER ALUMINUM FOIL REPAIR. ALUMINUM FOIL DELAMINATED FROM COWL APPROX 27" X 18". DELAM BEYOND LIMITS. WILL REQUIRE REPAIR PER SSDR FOTR2104615078Nose Cowl · dentedNR1 ENGINE NOSE COWL 6 OCLOCK POSITION HAS A DENT. REPAIRED ON FASI WO 21046, NR 15078.SDR UIEA2011051700259Inlet · erodedDURING WALK-AROUND INSP, MX FOUND THE NR 3 RT FAN COWL L/E WITH EROSION DAMAGE, MEASURING 0.350 IN. WIDE X 1.5 FT. LONG (REF FIG 1). THE DAMAGE IS BEYOND THE ALLOWABLE DAMAGE LIMITS IAW SRM 54-25-01 (ALLOWABLE DAMAGE 1). (DISPOSITION WAS MADE TO PERFORM A TISDR P5CA2011051000025Door Frame · crackedCRACK ON NR 1 PYLON, RIGHT SIDE, FWD PRESSURE RELIEF DOOR FRAME OF AFT FAIRING. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1110.SDR FDEA201104251619Structure · departedAFTER DEPARTURE, WEST OF THE AIRPORT BY APPROX 20NM OVER THE WATER, FELT A SHARP BUMP THAT FELT LIKE WAKE TURBULENCE CLIMBING THROUGH APPROX 14000 FT AND 320 KTS UPON LANDING, COWLING ON NR 2 ENGINE JUST BEHIND WHERE THE REVERSER SEPARATES IS COMPLETELY MISSSDR 2011FA0000248Duct · chafedDURING ANNUAL INSP FOUND THE LT ENGINE FUEL METERING UNIT BLAST DUCT CHAFING ON ENGINE MOUNT TUBE. FOUND THAT THE METAL WIRE IN THE BLAST DUCT HAD WORN THROUGH THE BLAST DUCT AND WORE INTO THE ENGINE MOUNT TUBE REQUIRING THE ENGINE MOUNT TO BE REMOVED FOR REPASDR A6WA201140293Structure · chafedT/E OF RT LOWER NOSE COWL IS CHAFED. R & R T/E STRIP ON RT LOWER NOSE COWL IAW CMM 71-14-01.SDR 2011FA0000247Duct · chafedDURING ANNUAL INSP, FOUND THE RT ENGINE FUEL METERING UNIT BLAST DUCT CHAFING ON ENGINE MOUNT TUBE. FOUND THAT THE METAL WIRE IN THE BLAST DUCT HAD WORN THROUGH THE BLAST DUCT AND WORE INTO THE ENGINE MOUNT TUBE REQUIRING THE ENGINE MOUNT TO BE REMOVED FOR REPSDR UIEA2011040800244Door · dentedDURING MX WALKAROUND, MX FOUND DENT ON THE NR 1 ENGINE OIL SERVICE DOOR. MX ACCOMPLISHED PART 2, EO 1971A027, AND INSTALLED A BLANKING PLATE. EO 1971A027 ALLOWS THE BLANKING PLATE TO BE INSTALLED FOR UP TO 10FC. DUE TO LACK OF PART AVAILABILITY, DOOR REPLACEMSDR IPXA11566180Angle · damagedINSPECTION TYPE: NR 1 INBD SIDE A, HAD DOOR GUIDE CLIP AFT OF HINGE IS DAMAGED. REPLACED CLIP (ANGLE) IAW SRM 51-40-02-0G, DWG 311N5002, BDW 311N5196, SRM 51-40-05-0G, SRM 51-10-02-0G.SDR A6WA201140370Cowl Door · chafedLT LOWER CURE COWL CHAFED BY FWD LATCHES. BLENDED DAMAGED AREA FABRICATED AND INSTALLED REPAIR DOUBLER.SDR A6WA201140315Latch · wornLT LWR CORE COWL AFT OF FWD DOOR LATCH IS WORN. REPAIR IAW CMM 71-12-01.SDR FDEA201103231161Rub Strip · damagedAFTER REMOVAL OF RUBSTRIP ON NR 2 ENGINE OTBD CORE COWL, UPPER HINGE GOUGE FOUND. POWER PLANT-COWLING CORE COWL SKIN REPAIR COMPLIED WITH ON E. A. F-7111-146400 STEPS 1-23 DATED 03/17/2011,8100-9 DATED 05/03/2011 CAT MAJOR REPAIR.SDR 2011FA0000200Angle · crackedDISCOVERED PURSUANT COMPLIANCE WITH TASK CARD 767-57-594-00, LT WING AFT PYLON FAIRING INBOARD ANGLE T/E IS CRACKED IN RADIUS. NAC STA 408. CAUSE UNKNOWN. INSTALLED REPAIR ANGLES IAW DWG 54-11089-1 AND B767-300 SRM 51-40-02 AND EO RN 767-57-30.SDR LR7A2011032300171Mount · scoredDURING SCHEDULED B-2 CHECK PER JOBCARD HB7251 FOUND NR 2 ENGINE UPPER INBOARD AND OUTBOARD AND LOWER OUTBOARD TRUSS MOUNT BORES WITH SCORING DAMAGE AT CWS178L & 213L. REPAIRED IAW LAC MEA 382-54-11-003 R0.SDR LR7A2011032300170Mount · scoredDURING SCHEDULED B-2 CHECK PER JOB CARD HB7251 FOUND NR 1 ENGINE UPPER INBOARD AND OUTBOARD TRUSS MOUNT BORES WITH SCORING DAMAGE AT OWS 162L & 197L. REPAIRED IAW LAC MEA 382-54-11-003 R0.SDR UIEA2011030700192Structure · chafedCHAFING DAMAGE ON THE NR 1 ENG NACELLE STRUT INBD AFT SIDE OF FR ACCESS DOOR ASSY. (REPAIR IAW EI T2011A54B-536, REV 00)SDR FDEA201103070897Ring · dentedNR 3 ENGINE NOSE COWL LIP RING DENTED AT 6 O'CLOCK POSITION. CUT-OUT DAMAGED AREA AT NR 3 ENGINE NOSE COWL LIP RING AT 6 O'CLOCK POSITION, FABRICATED REPAIR PARTS AND DOUBLER, AND INSTALLED REPAIR PARTS AND DOUBLER IAW SRM 54-30-3 FIG 2, 51-10-2, AND 51-30-2SDR FDEA201103050855Nose Cowl · damagedNR 3 ENGINE NOSE COWL DENTED AT 4:00 POSITION ON EXTERIOR SKIN CUT OUT DAMAGE ON NR 3 ENGINE NOSE COWL EXTERIOR SKIN AT 4:00 POSITION IAW SRM, REV 103, 51-10-1. FABRICATED FILLER AND 4 DOUBLERS IAW IAW SRM 54-30-3, FIG 2. INSTALLED DOUBLERS AND FILLER IAW SRMSDR FDEA201103040846Skin · damagedMISSING MATERIAL NR 3 ENGINE NOSE COWL OTBD AFT T/E 3 O'CLOCK POSITION. CUT OUT DAMAGE IAW SRM REV 103, 54-30-3 FIG 3A. FABRICATED FILLER AND DOUBLER FOR NR 3 ENGINE NOSE COWL IAW SRM 54-30-3 FIG 3A AND 54-30-2 FIG 1. INSTALLED DOUBLER AND FILLER IAW SRM 54-SDR UALA2011022400914Nose Cowl · crackedNR 1 ENGINE NOSE COWL AT 6 O'CLOCK POSITION HAS A CRACK RUNNING BETWEEN 3 BLIND RIVETS AND TERMINATING BETWEEN THE 2 ROWS OF RADIAL RIVETS. CRACK LENGTH 2.75 INCHES LONG. STOP DRILL CRACK IAW SRM IN PREPARATION FOR TYPE 2 MX FERRY. NR 1 ENGINE NOSE COWL AT SDR FOTR2022202146Nose Cowl · puncturedHOLE IN NR 1 ENGINE NOSE COWL AT APPROX 9 O`CLOCK POSITION LOOKING AFT. CUTOUT DAMAGE FROM NR 1 ENGINE COWLING DIM. 5" X 2" IAW SRM 54-30-2 FIG 2. FABRICATED 2 EA STRAPS 5.3" X 1.3" AND 2 EA 3.4" X 1.3" FROM 2024T3 .071 PO 90010564. FABRICATED FILLER FROM 2SDR A6WA201140095Fairing · crackedPANEL 434BT (STANG FAIRING) CRACKED TOP R/B SIDE. REPLACED WITH NEW PART.SDR UIEA2011021400139Access Door · wornWORN ON NR 1 PYLON RT ACCESS DOOR ASSY. REPAIRED DAMAGE AREA IAW T2011A54B-34, REV 00.SDR UALA2011021100724Heat Shield · crackedHEAT SHIELD CHECKED ON OTBD MOUNT HOLE OF MODULE 50G. LOCATED APPROX 9" AFT OF FWD PYLON LIP ABOVE NOSE COWL. INSTALLED HEAT SHIELD AND MODULE CHECKED GOOD, NO LEAKS NOTED.SDR DALA1109780178Fitting · damagedNR 2 PYLON AFT STRUT FITTING FASTENER HOLE FOUND OVERSIZE AND REPAIRED IAW ERA 487050-14.SDR CA110210009Door · missingDURING A SCHEDULED 1A CHECK, THE RT MAGNETIC CHIP DETECTOR ACCESS DOOR 424CR WAS FOUND TO BE MISSING. IT APPEARS TO HAVE COME OFF IN FLIGHT AS THERE WAS DAMAGE TO THE EXTERIOR OF THE FAN COWL JUST ABOVE THE ACCESS DOOR OPENING, CONSISTENT WITH A PANEL ON ITS SDR ASOA201100240Beam · crackedLT UPPER OTBD ANGLE ON ENGINE BEAM CRACKED ON AFT END. REMOVED ANGLE AND REPLACED WITH NEW ANGLE IAW SRM 51-42-21.SDR FDEA201102080508Skin · chafedNR 2 STRUT AFT FAIRING MOST FWD UPPER OTBD FLANGE CHAFED AND WORN AT NUT-PLATE MOUNT SURFACE. CHAFED AND WORN AFT FAIRING ON NR 2 STRUT. R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR.SDR FDEA201102080506Brace · crackedNR 2 STRUT, UPPER SURFACE RT SIDE AFT PANEL SUPPORT BRACKET CRACKED/BROKEN AT PP STA 184.50. CRACKED AFT PANEL SUPPORT ON NR 2 STRUT R & R IAW SRM 51-40-02. REPAIR IS CLASSIFIED AS MINOR.SDR IPXA1564748Fairing · gougedINSPECTION TYPE:MOD, NR1 PYLON AFT FAIRING STRUCTURE FWD INBD UPPER NUTPLATE SUPPORT IS WORN AROUND NUTPLATES. REMOVED, FABRICATED, AND INSTALLED IAW DWG NR313N5033, AND SRM 51-40-02.SDR CWQR201105Manifold · crackedMANIFOLD CLOSE OUT FLANGE THAT ATTACHES TO THE ENGINE INLET BULKHEAD HAS A 3.4 IN LONG CRACK. THIS CRACK WAS FOUND DURING DIASSEMBLY OF ENGINE INLET FOR OTHER CRACKS FOUND DURING A SCHEDULED INSP. ALSO SUBMITTED TO MFG ON (SCR 553324).SDR A6WA201140117Cowling · chafedRT LOWER CORE COWL IS CHAFED AT FWD LATCHES. REPAIRED RT LOWER CORE COWL IAW CMM 228-50142, TASK 71-12-01-300-822-A01.SDR A6WA201140118Cowling · chafedLT LOWER CORE COWL IS CHAFED AT FWD LATCHES. REPAIRED LT LOWER CORE COWL IAW CMM 228-50142 TASK 71-12-01-300-822 AOL.SDR FOTR2021700805Structure · damagedNR 3 PYLON DAMAGED. REMOVED TITANIUM DOUBLER FROM NR 3 PYLON IAW SRM 51-30-2 AND EA 2708-5401 REV 1, LOCATED AND DRILLED NEW TITANIUM DOUBLER PN 69-18227-2, PO 20217102 IAW SRM 51-30-5 AND 51-30-6. FABRICATED 2 EA, FREEZE PLUGS FROM 15-5PH .375 PO 20217121 DISDR IPXA1564707Structure · chafedINSPECTION TYPE:C4, NR2 ENGINE PYLON RT FWD CHORD IS CHAFED, NAC STA 206. R & R IAW SRM 51-40-02.SDR QXEA2011012600069Diaphragm · cracked- DIAPHRAGM AT FS 197.00 IN RT NACELLE IS CRACKED. REMOVED CRACKED DIAPHRAGM RT NACELLE IAW SRM 51-40-07-02-01. DRILLED FASTENERS HOLES IN NEW DIAPHRAGM PN 85414131-102 IAW SRM 51-40-07-02-01. INSTALLED NEW DIAPHRAGM IAW SRM 51-40-15-02-01.SDR DALA1104690178Bushing · migratedNR 1 PYLON STRUT LWR SPAR FITTING ATT BUSHING REPLACED IAW SRM 54-53-90, FIG 201 REPAIR 4.SDR CA110121001Attach Bolt · shortDURING AN N1 CHECK ON THE ACFT, A PYLON INSP FOUND THAT THE AFT FIXED FAIRINGS WERE MISSING SEVERAL ITEMS OF ATTACH HARDWARE. IN THE LT PYLON FIXED FAIRING, BOTH FWD PIP PINS HAD FALLEN OUT, AS HAD ONE OF FOUR MID-POINT ATTACH BOLTS. THE MISSING HARDWARE WAS F
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