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 UIEA200400043Frame · crackedD CHECK, DURING SCHEDULE MAINTENANCE INSPECTION OF NR 3 PYLON, THE BULKHEAD UPPER ASSEMBLY RHS FORWARD ANGLE FRAME FLANGE WAS FOUND CRACKED AT THE END FASTENER HOLE COMMON TO THE FRONT SPAR FITTING AND STRUT CAP SKIN ASSY. FABRICATED A REPAIR ANGLE TO RESTORESDR QXEA200400259Truss · chafedPDX - NR 1 ENGINE INBOARD UPPER TRUSS IS CHAFED. REPAIRED IAW DHC-8 RD 8-54-036, STEP 3.SDR KBM2004F00136Strap · wornEXHAUST HEAT SHIELD STRAP. HEAT SHRINK WORN REGS REPLACEMENT. REMOVED AND REPLACED.SDR MALA040276Door · openRIGHT COWLING POPPED OPEN INFLIGHT. AIR RETURN TO MEM. REPLACED LEFT AND RIGHT FWD COWLINGS ON RIGHT ENGINE WITH SERVICEABLE UNITS. RIGHT P/N 7271110-271, LEFT P/N 7271110-269. GOOD FOR SERVICE.SDR EIA2004011Shield · tornNR 4 ENGINE LOWER I/B PYLON SKIRT FIRE SHEILD WORN THROUGH FROM NAC STA. 180.00 TO NAC STA. 265.94. NR 4 ENG LWR I/B SKIN REPAIRED PER SRM 54-30-03 FIG 35 & 36 PG 111-118.SDR BROWN2004001Pylon · vibrationAIRCRAFT CONTINUES TO EXPERIENCE A RUMBLE IN FLIGHT AT SPEEDS BETWEEN 430 AND 460 KTAS (NORMAL CRUISE SPEEDS). MFG HAS MADE NUMEROUS ATTEMPS TO CORRECT THE PROBLEM BUT THEY HAVE NOT BEEN SUCCESSFUL. THE RUMBLE CAN BE HEARD AND FELT IN THE COCKPIT AND CABIN. SDR UIEA200400020Strut · crackedDURING ZONAL INSPECTION IT WAS DISCOVERED THE NR 4 ENGINE PYLON STRUT PRECOOLER EXHAUST VENT WITH CRACKS ON THE RIGHT SIDE OF THE STRUT. THE REPAIRS WERE MADE ON THE RIGHT SIDE OF THE STRUCT STRUCTURE ASSEMBLY. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOSDR UIEA200400019Strut · crackedDURING D-CHECK AT SIN, DURING ZONAL INSPECTION IT WAS DISCOVERED THAT NR 3 ENGINE PYLON STRUT PRECOOLER EXHAUST VETN WITH CRACKS ON THE RIGHT SIDE OF THE STRUT. THE REPAIRS WERE MADE ON THE RIGHT SIDE OF THE STRUT STRUCTURE ASSEMBLY. THE NR 3 STIFFENER WAS RSDR UIEA200400017Strut · crackedDURING D-CHECK AT SIN, DURING ZONAL INSPECTION IT WAS DISCOVERED THAT NR 1 ENGINE PYLON STRUT PRECOOLER EXHAUST VENT HAD CRACKS ON THE RIGHT SIDE OF THE STRUT. THE REPAIRS WERE MADE ON THE RIGHT SIDE OF THE STRUT STRUCTURE ASSEMBLY. THE NR 3 STIFFENER WAS RESDR UIEA200400018Strut · crackedDURING D-CHECK AT SIN, DURING ZONAL INSPECTION IT WAS DISCOVERED THAT NR 2 ENGINE PYLON STRUT PRECOOLER EXHAUST VENT WITH CRACKS ON THE RIGHT SIDE OF THE STRUT. THE REPAIRS WERE MADE ON THE RIGHT SIDE OF THE STRUT STRUCTURE ASSEMBLY. THE NR 3 STIFFENER WAS RSDR 04FDEA00377Bracket · crackedNR 3 ENGINE I/B TRAILING EDGE LOWER BALL SCREW G/B SUPPORT BRACKET IS CRACKED. REMOVED DAMAGED BRACKET IAW SRM 51-35-01. RECEVIED NEW BRACKET P/N 311OM24POO1A. LOCATED AND DRILLED IAW SRM 51-31-01. INSTALLED BRACKET ACTUATOR IAW SRM 51-31-01 AND 51-31-01.SDR DLM88040122Nose Cowl · missingNUMBER 2 ENGINE COWLING LOOSE. PORTION MISSING. FOUND ON POST FLIGHT WALKAROUND. REMOVED AND REPLACED RIGHT NOSE COWL ASSY PER MM. ASSOC PARTS REPLACED AS FOLLOWS, THERMOSTATIC REGUALTOR VLV 759702239 S/N 5969C. NOSE COWL A/I SHUTOFF VLV 754001305 S/N 232SDR DL76S040114Cap · missingDURING FLIGHT, NR ENGINE PYLON DEPARTED AIRCRAFT. UNDER INVESTIGATION.SDR M7K2004F00004Fastener · shearedON THE ENGINE FAIRING 1 OF 4) LATCHING HOOK OF THE FASTENER SHEARED AT HOOK BASE AND CRYSTALIZATION OF THE METAL AT THE BREAK SEEMED APPARENT. NO SIGNIFICANT WEAR NOTED BEFORE THE BREAK OCCURRED THIS IS A TITAIUM MATERIAL. SUGGEST USING STAINLESS STEEL.SDR UPS04441810Spar · crackedINSPECTION TYPE:C NR 2 PYLON - LWR WEB CRACKED THRU FASTENERS AFT OF PNEU DUCT CUTOUT APPROX 15 INCHES FWD OF AFT MOUNT, CRACK RUNS LONGITUDINALLY. LWR SPAR 5 LOCATIONS CRACK END BY STOP DRILLED HOLES PER SRM 54-10-03 FIG 2 NDT CONFIRMED NIL CRACKS AND PERFORSDR CA040202012Spar · cracked(CAN) NACELLE OB WEB TO SPAR ATTACHMENT CHANNEL CRACKED IN BEND RADIUS ON LOWER END OF CHANNEL. THIS CONDITION EXISTED IN THE SAME AREA ON BOTH NACELLES. CRACKS ARE COMMON IN THESE AREAS ON HIGH CYCLE AIRPLANES. LATER SN AIRCRAFT COME FROM THE FACTORY WITH DOSDR QXEA200301605Mount · chafedPDX- LOWER INNER TRUSS MOUNTS TUBE HAS FIVE CHAFE SPOTS IN A FOUR INCH AREA NEAR FUEL FLOW TRANSMITTER. REPAIRED IAW HORIZON AIR EA 2-54-198.SDR QXEA200301556Angle · crackedLT LOWER COWL HAS Z-ANGLE CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-16 AND SRM 51-42-05 AND SRM 51-40-15.SDR QXEA200301546Frame · crackedPDX- LEFT HAND NACELLE AFT FINGERNAIL DECK FRAME IS CRACKED. REPAIRED IAW Q400 RD 8/4-54-033.SDR QXEA200301545Structure · crackedPDX- LEFT HAND NACELLE AFT FINGERNAIL DECK IS CRACKED AT FINGERNAIL MOUNT HOLES. REPAIRED IAW Q400 RD 8/4-54-044.SDR QXEA200301489Panel · chafedPDX- LT SIDE OF LT NACELLE OUTBOARD GRAVEL GUARD MOUNT ON TOP PANEL OF WHEEL WELL IS CHAFED. REPAIRED IAW DHC-8 SRM 51-20-11 AND 51-40-11.SDR 2004F00015Rivet · looseAIRCRAFT WAS EN ROUTE FROM BUFFALO, NY TO PONTIAC, MI AND GOT AN INDICATION OF A FIRE ON THE NR 2 ENGINE. PILOT DECLARED AN EMERGENCY AND LANDED AT MTC SELFRIDGE AFB. UPON RECOVERY INSPECTION IT WAS FOUND THAT A FIRE LOOP CLIP HAD CAME LOOSE AND GROUNDED THESDR SWIA200312675Bracket · crackedRT HYD LOWER PACK BRACKET CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIGHT HYD LOWER PACK BRACKET WITH A SERVICEABLE UNIT IAW SRM 51-10-02, 51-40-00.SDR SWIA200312672Structure · crackedRIGHT ENGINE INBOARD SIDE NACELLE DECK CHAFED AND CRACKED AT HYDRAULIC PRESSURE HOSE NIPPLE CONNECTION (REF: S/B 120-29-0049 PAGE 2, FIG 1, DET B). DISCOVERED DURING C-CHECK INSPECTION. DOUBLER ADDED TO AREA, INBOARD NACELLE DECK IAW SRM120 51-10-02 PG 2 SESDR QXEA200301451Strut · chafedPDX- UPPER OUTBOARD ENGINE STRUT IS CHAFED AT TWO LOCATIONS AT INBOARD AFT END OF NR 2 NACELLE. REPAIRED IAW DHC-8 RD 8-54-036.SDR CA031031010Duct · cracked(CAN) DISCOVERED COWL DUCT CRACKING DURING ROUTINE MAINTENANCE INSPECTION. MFG HAS PREVIOUSLY IDENTIFIED THIS PROBLEM AND DESIGNED A FIELD REPAIR TO RECTIFY IT. INCORPORATED FIELD REPAIR FR-KA-00038 TO BOTH ENGINE COWLS. DUCT PN 101-910049-12 ALSO AFFECTEDSDR GTIA030918Isolator · corrodedFOUND RIGHT ENGINE FORWARD LOWER ISOLATOR CORRODED. REMOVED ISOLATOR. INSTALLED NEW ISOLATOR. (M)SDR GTIA030919Isolator · corrodedLT ENGINE PYLON AFT ISOLATOR RUSTY. REMOVED LT ENGINE PYLON AFT ISOLATOR ASSEMBLY. INSTALLED NEW LT ENGINE PYLON AFT ISOLATOR. (M)SDR 2004F00035Door · departedLEFT ENGINE COWLING SIDE DOOR DEPARTED FROM AIRCRAFT DURING FLIGHT. INSPECTION REVEALED THAT THE CAUSE WAS MOST LIKELY, FAILURE TO SECURE DOOR PANEL PRIOR TO FLIGHT NM-SLC-FSDO. (M)SDR 03FDEA01793Structure · chafedCOMPLY WITH EA 6-5410-73845 PYLONS/NACELLES - NR 1 AND NR 2 ENGINE CORE COWL CHAFING REPAIR. COMPLIED WITH EA 6-5410-73845 PYLONS/NACELLES NR 1 AND NR 2 ENGINE CORE COWL CHAFING REPAIR.SDR F3LA200300151Channel · crackedDURING C-5 CHECK, INSPECTION REPORTED NR 1 ENGINE CHANNEL CRACKED OUTBOARD LOWER AFT END LT PYLON AT STA 320. REPLACED CHANNEL PER SRM 51-40-02.SDR CA031014007Door · missing(CAN) A/C TAXIED TO GATE AFTER LANDING. THE LOWER LEFT FIXED COWL DOOR WAS MISSING FROM AIRCRAFT. SEVERAL MOMENTS LATER THE COWL WAS FOUND OUT ON TAXI WAY AND RECOVERED BY AIRPORT AUTHORITIES.A NUMBER OF CAMLOC FASTENERS WERE FOUND IN COWL.THE REMAINDER OF FASDR UPS03441458Frame · crackedINSPECTION TYPE: C, NR 2 PYLON - LT AND RT NAC STA 286.5 FRAME FOUND CRACKED. DURING DIAG BRACE STEEL FITTING MOD ACCOMPLISHMENT. LT AND RT NAC STA 286.5 FRAME REPLACE AS PER SRM 51-10-01 PG 8.SDR QXEA200301229Spar · crackedPDX- BRACKET CRACKED AT YW128.0R, RIGHT HAND FWD SPAR NEXT TO NR 2 ENGINE NACELLE. REPAIRED IAW DHC-8 SRM 51-40-00.SDR QXEA200301232Structure · damagedPDX- REPLACE EXISTING LOWER RIGHT COWL PARTS WITH THICKER ONES. REPAIRED IAW HORIZON AIR EO 6-71-103.SDR C2XA03SH366Structure · chafedDURING C-CHECK THE LT LOWER ENGINE COWLING AFT EDGE MEMBER WAS FOUND TO CHAFED THRU. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR QXEA200301234Truss · chafedPDX- THREE CHAFE MARKS ON BOTTOM SIDE OF UPPER NR 1 ENGINE TRUSS 26 INCHES AFT OF FORWARD ATTACH POINT. REPAIRED IAW DHC-8 RD 8-54-036.SDR QXEA200301146Structure · crackedPDX- AFT END OF RT HAND NACELLE FINGERNAIL DECK IS CRACKED AROUND BOLT HOLES. REPAIRED IAW Q400 SRM 51-00-02, TASK 51-00-02-250-801 AND RD 8/4-54-044.SDR QXEA200301153Support Angle · crackedNR 1 ENGINE LOWER COWL BYPASS DOOR APERTURE RIGHT SIDE SUPPORT ANGLE IS CRACKED. REPAIRED IAW HORIZON AIR EO 6-71-103.SDR ARWA20030910Structure · brokenDURING AN A-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 1 PYLON EDGE BROKEN, AFT OF LT FORWARD MOUNT.SDR ARWA20030909Structure · crackedDURING AN A-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 1 PYLON WITH CRACK, AFT OF RT FORWARD MOUNT.SDR QXEA200301149Shroud · crackedPDX- NR 2 NACELLE RT HAND SIDE, NACELLE TO FLAP SHROUD DIAPHRAGM IS CRACKED AT STATION XN200.06. REPAIRED IAW Q400 SRM 51-40-10, 51-42-05.SDR QXEA200301166Support Bracket · crackedLEFT LOWER COWL AFT CONE SUPPORT BRACKET IS CRACKED. REPAIRED IAW HORIZON AIR EO 6-71-103.SDR QXEA200301154Support Angle · crackedNR 1 ENGINE LOWER COWL BYPASS DOOR APERTURE LEFT SIDE SUPPORT ANGLE IS CRACKED. REPAIRED IAW HORIZON AIR EO 6-71-103.SDR KBM2004F00141Strap · wornENGINE MO 5 HEAT SHIELD STRAP BRACKET HEAT SHRINK IS WORN. REMOVED AND REPLACED.SDR AWXA200301045Gusset · crackedDURING C-16 CHECK A .1250 INCH CRACK WAS FOUND AT FASTENER HOLE ON NR 1 ENGINE FIXED FAIRING COVER PLATE (GUSSET) AT AFT END, 1ST RIB. MAINTENANCE REMOVED CRACKED GUSSET ON NR 1 ENGINE FIXED FAIRING AFT END, 1ST RIB; FABRICATED A NEW REPLACEMENT GUSSET IAW DWSDR 2003FA0000883Panel · crackedDURING INSPECTION FOUND RT WING, INBOARD LEADING EDGE BLEED AIR TUBE HEATSHIELD PANEL LOWER MOUNT FLANGE CRACKED APPROXIMATELY HALF WAY LENGTHWISE. THIS IS THE THIRD C-560XL THAT WE HAVE FOUND THIS CONDITION ON. REPLACED THE PANEL WITH NEW.SDR UPS03441318Web · crackedINSPECTION TYPE: C, SEVERAL CRACKS WERE FOUND AT NR 3 PYLON REAR MOUNT BULKHEAD FORWARD AND AFT FRAME WEB, DETAILS PLEASE REER ATTACHED FIGURE. FRAME WEBS REPLACED AND REPAIRED AS PER RS R54-53-35063 INSPECTIONS TO CONTINUE PER UPS EO B747-5410-13908 AND UPSSDR 03FDEA01407Stiffener · chafedAFT STIFFNER IS CHAFED AT NR 6 LT NACELLE, ATTACH POSITION ABOVE NR 2 ENGINE BS 1456. REMOVED AFT STIFFENER, FABRICATED, DRILLED, ALODINED, PRIMED AND RE-INSTALLED RIBS AND STIFFENER AT BS 1456 AND 1459 AT NR 6 LT COWL ATTACH POSITION ABOVE NR 2 ENGINE.SDR CALA0300509Angle · crackedINSPECTION FOUND A 4 INCH CRACK IN NR 1 ENGINE PYLON ANGLE FOR AFT LOWER O/B ACCESS PANEL. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02.
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