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 UALA2012062903430Inlet · gougedNR 1 ENGINE NACELLE HAS A DENT IN THE INLET COWL LOCATED AT THE 12:00 POSITION, DENT IS IN THE LIP, SKIN PORTION OF THE INLET COWL. DENT DIMENSIONS REPORTED TO BE 3.5 INCHES (LENGTH) BY 0.875 INCHES (WIDTH) BY .0625 INCHES DEEP DOES NOT MEET THE A OVER Y CRITSDR DALA12001775812Fairing · crackedMAINTENANCE DISCOVERED A CRACK IN THE NR 2 ENGINE STRUT FAIRING AT STA 149.5 RT SIDE. REPAIRED CRACKED FRAME, INSPECTED AND TREATED AREA AS PER ER/A 504589-14 REV ORG.SDR UALA2012061403274Latch · unsecureTHIRD FASTENER ABOVE RIGHT ENG OUTBOARD SIDE UNLATCHED. SECURED LATCH.SDR DALA1236070663Fairing · damagedMAINTENANCE DISCOVERED PYLON FAIRING STRUCTURE SPLICE PLATE, DAMAGE ON TOP OF NR 2 PYLON AT STATION 136 RIGHT SIDE. REPLACED SPLICE PLATE PER BAC DRAWING 31343100.SDR DALA1236060663Fairing · departedDURING CLIMB-OUT, FELT A SLIGHT SHUDDER AND DISCOVERED THAT THE FORWARD STRUT FAIRING ON THE RIGHT ENGINE HAD COME OFF. FIRST OFFICER INSPECTED AREA FROM CABIN AND NO OTHER DAMAGE NOTED. CONTINUED TO DESTINATION. REMOVED PANELS 442 AR AND 442 AL AND REPASDR 29GA94754060512Keelbeam · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT NACELLE INBOARD KEEL BEAM UPPER ATTACHMENT HOLE FOR TRUSS APPEARS TO HAVE A CRACK AND HAS CORROSION. REPLACED RIGHT NACELLE UPPER KEEL WEB.SDR 29GA2012060594754Keelbeam · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT NACELLE INBOARD KEELBEAM LOWER ATTACHMENT HOLE FOR TRUSS APPEARS TO HAVE A CRACK AND HAS CORROSION. REPLACED RIGHT INBOARD LOWER KEEL WEB.SDR DALA1236895503Skate Angle · crackedRIGHT PYLON AFT INBD SKATE ANGLE CRACKED. REPAIRED IAW EA 06-075495-03 REV E.SDR C77A20120603019Heat Shield · erodedLT PYLON HEATSHIELD SECTION NR 2 HAS 1 ELONGATED HOLE. REAM THE HOLE TO MATCH SELECTED WASHER, INSTALL COUNTERSUNK WASHER NAS1169 BONDED TO HEAT SHIELD ON WO 553865-404 IAW ETD2012-170-007658 AND EA E170-54-005 REV IR WO 572653.SDR REXA2012052400900Fairing · crackedHINGE LINE FAIRING 422DB CRACKED. DOT A124-003. REMOVED AND REPLACED HINGE LINE FAIRING 422DB IAW ARM 51-42-06.SDR 7AHR201205242306Plate · gougedNR 2 ENGINE CROSSBEAM LOWER INBD ENGINE TO WING FAIRING HAS GOUGES ON CROSSBEAM FACE. REMOVED DAMAGED PLATE FROM CROSSBEAM IAW 51-30-2. FABRICATED NEW PLATE IAW SRM 51-20-1. INSTALLED NEW PLATE ON CROSSBEAM FACE SRM 51-30-2.SDR A6WA201240609Structure · damagedCORE COWLING 435AT INBD L/E CORNER DAMAGED CUTOUT DAMAGED AREA OF 435AT CORE COWLING INBD L/E CORNER IAW CMM 71-12-01. SRS18 SEE FORM 412 FOR INSTALL, FAB OF DOUBLER AND FILLER.SDR A6WA201240610Structure · gougedCORE COWL 435AB DAMAGE ON INNER CENTER STIFFENER. BLENDED GOUGE ON INNER CENTER HOT CHANNEL .050. REMOVED .008 REMAINING, .042 WITHIN LIMITS USING AMM 51-21-400 IAW CMM 71-12-01, SRM 51-21-11, 57-25-06, 51-25-26.SDR A6WA201240608Structure · damagedCORE COWLING 435AB INBD L/E CORNER DAMAGED. CUTOUT DAMAGED CORNER OF 435AB CORE COWL INBD L/E IAW CMM 71-12-01. SEE FORM 412 FOR FAB AND INSTALL OF FILLER AND DOUBLER.SDR CA120505002Cowl Door · detached(CAN) THE RT ENGINE UPPER NOSE ACCESS COWL BECAME DETACHED FROM THE ACFT IN FLIGHT. THE CREW DID OBSERVE SOME BUFFET EFFECT BUT DID NOT KNOW THE CAUSE AT THE TIME. THE MISSING PART WAS DISCOVERED POST LANDING. THE ACFT DID HAVE MAINTENANCE CONDUCTED DURING ANSDR ASOA201201540Cowl Door · missingDURING DESCENT, FELT WHAT WAS LIKE WAKE TURBULANCE. UPON POST FLIGHT FOUND TOP OF RT ENGINE COWL MISSING. PERFORMED INSPECTIONS OF ENGINE, PYLON, AND EMPENNAGE AE, REF L/P'S 667135 AND 667141, NO FAULTS NOTED. INSTALLED NEW COWL IPC 71--14-01 ITEM 5 IAW AMMSDR DALA1239570679Bushing · migratedLT ENGINE UPPER LINK AFT ATTACH OTBD INNER BUSHING MIGRATED. MAINTENANCE REPAIRED BUSHING IAW SRM 54-51-90.SDR DALA1239560679Bushing · migratedRT ENGINE UPPER LINK AFT ATTACH OTBD INNER BUSHING MIGRATED. MAINTENANCE REPAIRED BUSHING IAW SRM 54-51-90.SDR DALA1239550679Bushing · migratedLT ENGINE UPPER LINK FWD ATTACH OTBD INNER BUSHING MIGRATED. MAINTENANCE REPAIRED BUSHING IAW SRM 54-51-90.SDR UALA2012042302428Fairing · peelingNR 1 ENGINE STRUT FAIRING TRAILING EDGE AFT FAIRING INBD SIDE FORWARD EDGE PEELING BACK. REMOVED NR 1 ENG STRUT AFT FAIRING PERFORMED COMPOSITE REPAIR).SDR UALA2012040602137Structure · damagedENG 4 INLET COWL LIP DAMAGED. REMOVED AND REPLACED NR 4 ENGINE NOSE COWL IAW AMM.SDR FDEA201204051267Intercostal · crackedRT NR 2 ENGINE INTAKE DUCT PANEL NR 364RR ON WIRE CUT-OUT INTERCOSTAL FOUND CRACKED. REPAIRED IAW SRM 55-30-02, FIG 201, REV 49, REPAIR 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR EIAA20120403035Access Panel · gougedNR 3 PYLON RT SIDE INSIDE ACCESS PANEL 473AR DEEP GOUGE JUST UNDER CUT OUT. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-020-2.SDR UALA2012040202041Plate · looseNR 2 ENGINE PYLON ELECRICAL FEEDER CABLES W8100 & W8101 RETAINMENT PLATE IS LOOSE & HAS MIGRATED AFT. VIEWED FROM INSIDE OF PYLON DISC BOX ON FWD FACE OTBRD MOST FEED THRU.SDR CA120322008Door · missing(CAN) CLIMBING THROUGH 14,000 FT, THE FLIGHT CREW OBSERVED A MOMENTARY LT ENGINE N1 OVERSPEED. THE REST OF THE ENGINE PARAMETERS APPEARED NORMAL. UPON DESCENT, THE LT ENGINE THRUST LEVER BECAME STUCK AND UNABLE TO REDUCE N1 SPEED BELOW 81 PERCENT. THE FLIGHTSDR A6WA201240356Structure · damagedCLIMBING THRU FL140, LT ENG OBSERVED MOMENTARY OVERSPEED OF N1. NORM ENG INDICATIONS OBSERVED. UPON DECENT LEFT ENGINE THRUST LEVER STUCK AND UNABLE TO REDUCE N1 BELOW 81 PERCENT. COMPLIED WITH QRH, THRUST LEVER JAM PROCEDURE AND SHUTDOWN LEFT ENGINE INFLISDR UIEA2012042000155Structure · crackedNR 3 NACELLE AFT END CAP CRACKED AT CTR PORTION. REPAIRED IAW EO 4471A090.SDR HNAA2012030700664Structure · crackedNR 1 FINGERNAIL DECK WHEEL HUMP HAS CRACK ALONG AFT SIDE (INBD HUMP). REPAIRED DAMAGE IAW RD8-54-1494.SDR EE4Y20120305098Channel · corrodedNR 1 ENGINE CNA FIRE PROOF BULKHEAD LT AND RT CHANNELS CRACKED. REPLACED LT AND RT CHANNELS IAW SRM 51-72-11, PARAG 4 AND 6.SDR EE4Y20120305099Channel · corrodedNR 1 ENGINE CNA FIRE PROOF BULKHEAD LT AND RT CHANNELS CRACKED. REPLACED LT AND RT CHANNELS IAW SRM 51-72-11, PARAG 4 AND 6.SDR EE4Y201203050106Channel · crackedNR 1 ENGINE,PYLON, PRECOOLER CASE, WITH CRACKS IN BOTH CORNERS. REPAIRED PRECOOLER CASE LT AND RT LATERAL CHANNELS AT NR 7 AND NR 8 RIBS IAW SRM 54-12 FIG 209.SDR HALA2012022500084Scupper · missingETOPS SIGNIFICANT SYS - NR 1 ENGINE INBD CORE COWL MISSING SCUPPER ASSY 314T1237-14. REPLACED NR 1 ENGINE SCUPPER ASSY 314T1237-14, OK FOR SERVICE.SDR FDEA201202160589Spar · damagedRT PYLON SPIGOT RECEPTACLE FITTING FOUND A MISDRILLED BOLT HOLE. REPAIRED IAW AMM 54-50-00 AND AMM 20-21-12SDR HNAA2012021600585Shroud · crackedAFT NACELLE FIREWALL JET PIPE SHROUD ABOVE THE JET PIPE IS CRACKED AT THE 1 O'CLOCK POSITION. REPAIRED IAW EO8-54-12-0071 FOR NR 2 NACELLE.SDR HNAA2012021600584Strut · chafedNR 2 NACELLE OTBD LOWER ENGINE SUPPORT STRUT CHAFED AT THE OIL COOLER RETURN LINE, MEASURED AT 0.012". REPAIRED IAW RD8-54-1264. COMPLIED WITH HFEC INSP. NO DEFECTS NOTED.SDR HNAA2012020300552Support · damagedNR 1 INBD LOWER NACELLE SUPPORT TUBE HAS DAMAGE BEYOND LIMITS. 22" IN FROM KNUCKLE END. R & R STRUT.SDR HNAA2012020300550Strut · damagedNR 2 NACELLE LOWER OTBD ENGINE SUPPORT STRUT IS DAMAGED MIDWAY DOWN ON THE TUBE MEARSURING LENGTH 0.0467, WIDTH 0.553, DEPTH 0.029. REMOVED SUPPORT STRUT.SDR A6WA201240256Retainer · debondedLT LOWER CORE COWL HEAT SHIELD HAS AREAS AND DEBONDED. FABRICATED AND INSTALLED RETAINER STRIP ON LT LOWER CORE COWL HEAT SHIELD IAW CMM 71-12-01.SDR FDEA201201180242Door · missingRT ENGINE IDG SERVICING DOOR MISSING. R AND R DOOR IAW SRM 51-40-02.SDR FDEA201201110079Fastener · looseNR 2 ENGINE NOSE COWL HAS NUMEROUS RIVETS LOOSE IN NOSE LIP SKIN. NOSE COWL REPLACED.SDR CA120110005Nose Cone · cut(CAN) DURING A WALK AROUND, NOTICED SOME IMPACT DAMAGE ON THE COMPOSITE NOSE, ON THE LT SIDE AT STA X140 AND Z105.5. A "KNIFE LIKE" CUT THROUGH THE FIBERGLASS SHELL, APPROXIMATELY 1.5" LONG, AND GOING APPROXIMATELY 1 MILLIMETER DEEP INTO THE UNDERLYING HONEYCSDR UALA2012010300065Latch · unsecureON PREFLIGHT F/O FOUND AFT LATCH OF LEFT ENGINE CORE COWL HANGING DOWN FOUND BROKEN KEEPER ASSY FOR LATCH. REPLACED AND ADJUSTED PER AMM.SDR A6WA201240064Transcowl · crackedRT LOWER TRANS COWL UPPER FWD INTERLOCK FITTING IS CRACKED. R & R FITTING PN 228-50242-122 IAW SRM 51-42-14.SDR UALA2011123007166Casting · damagedNR 1 PYLON AFT FAIRING HEAT SHIELD PAN CASTING AND ITS SEAL RETAINER PN 313W3807-4 WERE FOUND WITH ELONGATED FASTENER HOLE.SDR ASMF20111221007Nose Cowl · dentedDURING TRANSIT CHECK, DETECTED A BIRD IN RT ENGINE, SO BIRD STRIKE CONDITIONAL INSP WAS PERFORMED IAW MM 05-51-18, DETECTING A DENT OF 8.0" LONG, 5.0" WIDE AND 0.375" DEPTH IN THE NOSE COWLING AT 12 HRS POSITION, THIS DENT WAS FOUND OUT OF LIMITS IAW SRM 54-10SDR QXEA2011121901404Structure · brokenPANEL 414AR AFT LOWER ATTACH POINT NUTPLATE STRUCTURE BROKE OFF. ACFT DOWN FOR C-CHECK. REMOVED BROKEN FLANGE IAW SRM 51-40-10-02-01. MATCH DRILLED NEW FLANGE TO ACFT IAW SRM 51-40-07-02-01. INSTALLED NEW FLANGE IAW SRM 51-42-05-02-01 AND 51-40-15-02-01. SDR A6WA201240215Structure · chafedRT UPPER NOSE COWL AFT EDGE STRIP IS CHAFED. R & R RT UPPOER NOSE COWL AFT EDGE STRIP IAW CMM 71-14-01-300-814-A01.SDR A6WA201240086Heat Shield · dentedRT LOWER CORE COWL FIRE SHIELD DENTED. REPAIRED RT LOWER CORE COWL FIRE SHIELD IAW CMM 71-12-01, SRS 095.SDR UIEA2011121200713Door · damagedDURING WALKAROUND INSPECTION, MX FOUND THE NR 4 RT ENGINE CORE COWL DOOR SKIRT (MID) FAIRING BENT INWARD, CURLED AND CRACKED IN RADIUS OF BEND. THE LENGTH OF THE DAMAGE EXCEEDS THE SRM LIMITS. PERFORMED A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTSDR ASOA201102333Fitting · brokenCLIP BROKEN TOP OF LT PYLON. R & R CLIP ON TOP LT PYLON IAW SRM 51-40-11-001-001-A01 & SRM 51-42-06-001-001-A01 & SRM 51-21-11-001-001-A01 & SRM 51-25-06-001-001-A01.
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