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 DL733021347Beam · wornWORN AREAS WERE FOUND ON THE CROWN BEAM LUG BORES OF THE #1 AND #2 PYLONS. THE BORES WERE OVERSIZED TO 3.100" AND 3.102 RESPECTIVELY. REPAIR BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV.SDR ASAA0210303Pylon · crackedPAE - DURING SCHEDULED C-CHECK, FOUND RIGHT PYLON AT FAIRING STATION 80, WING STATION 166.5 CRACKED. REMOVED DAMAGE AND FABRICATED REPAIRS PER SRM. (M)SDR ABXA030049Skin · gougedNR 1 ENGINE STRUT UNDER WING FAIRING FOUND DEEP GOUGE ON SKIN AT NAC STATION 258 RT SIDE. REPAIRED AREA IAW REA B654-45455MR.SDR SWIA200211532Bracket · crackedRT NACELLE HYDRAULIC RESERVOIR AREA, CRACKED BRACKET JUST AFT OF HYDRAULIC RETURN FILLER PORT. FOUND DURING "C" CHECK INSPECTION. REPLACED BRACKET IAW 120 SRM 51-10-02.SDR AUS20021270Tie Rod · broken(AUS) NR 3 ENGINE EXPERIENCED HIGH VIBRATION LEVELS. INSPECTION FOUND A NACELLE TIE ROD BROKEN AND FOULING ON A PIPE LOCATED ADJACENT TO THE AVM PICKUP. FAN BLADES CLEANED AND LUBRICATED AND AN ENGINE RUN CARRIED OUT.SDR CA021031019Splice Plate · cracked(CAN) THE RT NACELLE I/B SPLICE PLATE CRACKED DUE TO HOLE'S ON UPPER SPAR BEING ELONGATED, THUS CAUSING PLATE TO WORK IN THAT AREA. PARENT STRUCTURE FAILED DUE TO SPLICE PLATE BEING CRACKED AND NACELLE LOADING TRANSFURED TO THAT AREA.SDR Q9P2003F00000Web · crackedCOMPLIED WITH SB 31-51-1 AND SP 31-51-2 FOUND LT AND RT SHEAR WEBS CRACKED ON BOTH FORWARD AND AFT AREAS.SDR QXEA0201814Frame · crackedPDX - LT NACELLE FRAME CRACKED. REPAIRED IAW RD 8/4-71-016.SDR QXEA0201813Frame · crackedPDX - RT NACELLE FRAME CRACKED. REPAIRED IAW RD 8/4-71-016.SDR QXEA0201812Channel · crackedPDX - LT NACELLE INBOARD ZEE CHANNEL CRACKED. REPAIRED IAW RD 8/4-71-016.SDR QXEA0201811Channel · crackedPDX - LT NACELLE OUTBOARD CHANNEL PART NUMBER 87144114 CRACKED. REPAIRED IAW RD 8/4-71-016.SDR C2XA02SH110Structure · gougedDURING C CHECK NR 1 ENG LOWER NACELLE WAS FOUND TO HAVE A GOUGE AT FORWARD OUTBOARD ATTACHEMENT. MAITENANCE REMOVED DAMAGE AREA AND REPAIRED AFFECTED EDGE MEMBER IAW EMB 145 SRM54-10-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH108Stiffener · wornDURING C CHECK NR 2 LOWER ENGINE NACELLE HAD WEAR MARKS 12 INCHES INBOARD OF CENTER. MAITENANCE REMOVED DAMAGE AREA AND PEFORMED AN ANGLE REPAIR IAW EMB SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH106Structure · gougedDURING C CHECK NR 2 ENGINE LOWER NACELLE DISH AROUND INTERIOR OF ENGINE DRAIN WAS FOUND TO HAVE A GOUGE. MAINTENANCE REMOVED AND REPLACED DISH IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURNED TO SERVICESDR QXEA0201768Bracket · chafedPDX - BRACKET ON TOP RT SIDE, 15 INCES FROM AFT END OF LOWER COWL CHAFED. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 51-40-00.SDR QXEA0201689Channel · crackedPDX- NR 2 LOWER COWL DEBRIS DOOR PIVOT POINT CHANNELS, INBOARD AND OUTBOARD CRACKED. REPAIRED IAW RD8-4-71-016.SDR QXEA0201688Channel · crackedPDX- NR 2 LOWER COWL CHANNELS INBOARD AND OUTBOARD OF DEBRIS DOOR CRACKED. REPAIRED IAW RD8-4-71-016.SDR QXEA0201687Attach Angle · crackedPDX- NR 2 LOWER COWL AFT COWL SUPPORT WEB HAS CRACKED UPPER AND LOWER ATTACH ANGLE. REPAIRED IAW RD8-4-71-016.SDR ASAA0210242Attach Angle · brokenDURING SCHEDULED C CHECK FOUND NR 2 ENGINE OUTBOARD FIXED FAIRING ATTACH ANGLE AT NACELLE STATION 139 BROKEN. REMOVED, FABRICATED AND INSTALLED NEW ATTACH ANGLE PER SRM.SDR C2XA02SH097Rib · gougedDURING C CHECK, NR 2 ENGINE NACELLE WAS FOUND TO HAVE A GOUGE ON THIRD RIB PLATE FROM THE END. MAINTENANCE REMOVED DAMAGE AND REPAIRED RIB PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH096Stiffener · gougedDURING C CHECK, NR 1 ENGINE TOP NACELLE AFT STIFFENER 10 INCHES INBOARD OF CENTER WAS FOUND TO HAVE A GOUGED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH094Stiffener · gougedDURING C CHECK INSPECTION, NR 2 LOWER ENGINE NACELLE WAS FOUND TO HAVE A GOUGE ON AFT STIFFENER NEAR CENTER. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR QXEA0201680Angle · crackedPDX - NR 1 ENGINE LOWER NACELLE AFT CONE SUPPORT UPPER ANGLE CRACKED. REPAIRED IAW RD 8/4-71-016.SDR QXEA0201679Support · crackedPDX - NR 1 ENGINE LOWER NACELLE AFT CONE SUPPORT LOWER ANGLE CRACKED. REPAIRED IAW RD 8/4-71-016.SDR C2XA02SH099Skin · gougedSHV-DURING C CHECK #1 ENGINE LOWER COWLING WAS FOUND TO HAVE A GOUGE ON INERIOR SKIN 24 INCHES AFT CENTER OF COWLING. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED A DOUBLER REPAIR IAW EMB SRM 54-10-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR QXEA0201708Frame · crackedCKB - RT ENGINE NACELLE LOWER FRAME IN CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-59 AND WVAC EO DH8S-71-0590.SDR QXEA0201707Frame · crackedCKB - LT ENGINE NACELLE LOWER FRAME IS CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-59 AND WVAC EO DH8S-71-0590.SDR QXEA0201706Angle · crackedCKB - LT ENGINE NACELLE LOWER ANGLE IS CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-59 AND WVAC DH8S-71-0590SDR QXEA0201705Channel · crackedCKB - RT ENGINE NACELLE LOWER CHANNEL IS CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-59 AND WVAC EO DH8S-71-0590.SDR QXEA0201704Angle · crackedCKB - RT ENGINE NACELLE STRUCTURE LOWER ANGLE IS CRACKED. REPAIRED IAW WVAC EO DHC85-71-0590 AND HORIZON AIR EA 6-71-59.SDR QXEA0201669Structure · chafedPDX - TWO CHAFED AREAS IN THE LEFT FORWARD CORNER OF THE NR 1 NACELLE. REPAIRED IAW HORIZON AIR EA 2-54-156.SDR QXEA0201660Drag Strut · chafedPDX - THERE ARE TWO CHAFE MARKS ON HEAVY STRUCTURE IN NR 2 WHEEL WELL FORWARD SECTION ABOVE INBOARD V LOBE OF DRAG STRUT. REPAIRED IAW DHC-8 SRM 51-20-51 AND HORIZON AIR EA 2-54-156.SDR CA021115004Door · separated(CAN) RT ENGINE ANTI-ICE VALVE REPLACED, INVESTIGATION SHOWS THAT INNER HALF OF LOWER COWLING FASTENERS NOT SECURED. AIRCRAFT DEPARTED YVR, CREW NOTICED A 'BANG' AND THEN A CONSTANT VIBRATION, GOING THROUGH 8,000 FT, CLIMBING OUT. CREW CONTINUED TO CLIMB THROSDR QXEA0201713Channel · damagedCKB - LT NACELLE INBOARD CHANNEL HAS ONE HOLE WITH NO RIVET PITCH. REPAIRED IAW HORIZON AIR EA 6-54-132 AND WVAC EO DH8S-54-0598, STEPS 1-4.SDR QXEA0201711Frame · damagedCKB - RT NACELLE FRAME INBOARD AND OUTBOARD CHANNELS HAVE ONE HOLE EACH WITH NO RIVET PITCH FROM ANOTHER EXISTING HOLE. REPAIRED IAW HORIZON AIR EA 6-54-132 AND WVAC EO DH8S-54-0598.SDR AWXA200201021Clip · crackedDURING C-17 CHECK A 1/2 INCH CRACK WAS FOUND ON RIB BRACKET (SPRING CLIP) AT THE OUTBOARD SIDE OF THE RT PYLON NAC STA 282.67, NAC WL 117. MAINTENANCE REMOVED THE DAMAGED SPRING CLIP AT THE OUTBOARD SIDE OF RT PYLON NAC STA 282.67, NAC WL 117; FABRICATED A NEWSDR AWXA200201020Clip · crackedDURING C-17 CHECK 2 EACH 3/4 INCH CRACKS WERE FOUND ON RIB BRACKETS (SPRING CLIPS) AT THE INBOARD SIDE OF THE LT PYLON NAC STA 282.67, NAC WL 117. MAINTENANCE REMOVED 2 EACH DAMAGED SPRING CLIPS AT INBOARD SIDE OF THE LT PYLON NAC STA 282.67, NAC WL 117; FABRISDR C2XA02SH088Angle · gougedSHV DURING C CHECK INSPECTION GOUGE WAS FOUND ON NR 1 ENGINE LOWER COWLING AFT OF ENGINE DRAIN. MAINTENANCE REMOVED DAMAGED SETION AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH087Angle · gougedSHV DURING C CHECK INSPECTION SUPPORT ANGLE WAS FOUND GOUGED ON NR 1 ENGINE LOWER COWLING JUST AFT OF MOST FOWARD PIVOT POINT. MAINTENACE REMOVED DAMAGED AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVISDR QXEA0201633Structure · chafedPDX - NACELLE STRUCTURE HAS BEEN CHAFED BY DOOR HINGE ARM AND BONDING BOLT IN NR 2 WHEEL WELL FORWARD COOR AREA. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11.SDR C2XA02SH070Stringer · damagedSHV DURING C CHECK INDENTATION WAS FOUND ON LT ENGINE LOWER NACELLE SKIN OUTBOARD STRINGER 8 INCHES FROM AFT END. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICESDR UPS02439622Web · crackedINSPECTION TYPE:C #2 PYLON MID SPAR WEB HAS CRACK AT PREVIOUS REPAIR NAC STA 205 APPROX. #2 PYLON MID SPAR WEB CRACK AT NAC STA 205 REPAIRED REF SRM 54-10-03 FTG.12 / SRM 51-30-02.SDR QXEA0201583Frame · crackedCKB-103 FRAME IS SEVERELY CRACKED. REPAIRED IAW DHC-8 SRM 54-10-16, HORIZON AIR EA. 6-71-57 AND WVAC EO. DH8S-71-0562.SDR QXEA0201582Channel · crackedCKB-101 AND 103 CHANNELS ARE SEVERELY CRACKED. REPAIRED IAW DHC-8 SRM 54-10-16, HORIZON AIR EA. 6-71-57 AND WVAC EO. DH8S-71-0562.SDR QXEA0201581Channel · crackedCKB-102 AND 104 CHANNELS ARE SEVERELY CRACKED. REPAIRED IAW DHC-8 SRM 54-10-16, HORIZON AIR EA. 6-71-57 AND WVAC EO. DH8S-71-0562.SDR QXEA0201580Frame · crackedCKB-103 AND 104 Z FRAMES ARE SEVERELY CRACKED. REPAIRED IAW DHC-8 SRM 54-10-16, HORIZON AIR EA. 6-71-57 AND WVAC EO. DH8S-71-0562.SDR USAASA02080Door · unsecureEN ROUTE DURING CLIMB, AT 6,000 FEET AGL, FLIGHT CREW NOTICED SOME VIBRATION. AT FL100, A FLIGHT ATTENDANT NOTIFIED COCKPIT CREW THAT A LARGE PIECE OF DEBRIS WAS LAYING OVER THE LEADING EDGE OF THE RGHT WING. THE FIRST OFFICER WENT BACK TO CABIN AND VERIFIEDSDR CA021007014Rib · damaged(CAN) PILOT ON A RETURN FLIGHT HOME EXPERIENCED A SLOWER THAN NORMAL LANDING GEAR RETRACTION. A VISUAL INSPECTION WAS CARRIED OUT. INSPECTION OF THE LEFT MAIN GEAR AREA REVEALED TWO RIB ASSEMBLIES DAMAGED. THEY WERE LOCATED ADJACENT TO EACH SIDE OF THE GEARSDR AWXA200200926Angle · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1" CRACK WAS FOUND ON THE #2 PYLON AFT PANEL ATTACH ANGLE RADIATING FROM THE LOWER AFT NUTPLATE HOLE. MAINTENANCE REMOVED AND REPLACED THE 32 PYLON AFT PANEL ATTACH ANGLE IAW B737-300 SRM 51-40-02, PG. 38, 44-45, & 63, SDR QXEA021447Strut · chafedPDX- NR 2 ENGINE LOWER OUTBOARD STRUT IS CHAFED ON INNER SURFACE. REPAIRED IAW DHC-8 RD 8-54-036.
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