JASC 5411
Service difficulty reports · 1,454
Reports filed under 5411 · Nacelle/Pylon, Frame/Spar/Rib, 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 = '5411' 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 = '5411' 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 SWIA200312286Rib · crackedRT PYLON RIB FS 605 CRACKED. DISCOVERED DURING C-CHECK, REPLACED RIB IAW CRJ SRM 51-40-11.SDR SWIA200312285Rib · crackedLT PYLON HAS CRACK IN RIB AT FS 605.00. DISCOVERED DURING C-CHECK, REPLACED RIB IAW CRJ SRM 51-40-11.SDR SWIA200312169Frame · crackedRT ENGINE FRAME 1 CRACKED. DISCOVERED DURING C-CHECK. REMOVED & REPLACED FRAME 1 PER SB 120-54-0036 WITH NEW P/N 120-0351-004.SDR SWIA200312168Frame · crackedLT ENGINE FRAME 1 CRACKED. DISCOVERED DURING C-CHECK. REMOVED & REPLACED FRAME 1 PER SB 120-54-0036 WITH NEW P/N 120-0351-003.SDR AWXA200300806Profile · crackedDURING C-03 CHECK A .5 INCH CRACK WAS FOUND ON INBOARD UPPER ANGLE (PROFILE) AT ATTACH SCREW HOLE JUST AFT OF RIB 7 ON THE NR 2 PYLON. MAINTENANCE CUT OUT CRACKED AREA OF ANGLE JUST AFT OF RIB 7 ON THE NR 2 PYLON; FABRICATED A REPAIR SPLICE AND FILLER; INSTALSDR AWXA200300790Rib · crackedDURING C-03 CHECK A .125 INCH CRACK WAS FOUND ON NR 1 PYLON RIB, 4TH LOWER RIB FROM UPPER DRAIN LINE CLEARANCE HOLE, OUTBOARD EDGE IN AFT FIXED FAIRING. MAINTENANCE REMOVED CRACKED RIB; FABRICATED A NEW REPLACEMENT RIB; INSTALLED REPAIR PART IAW A320 SRM 51-4SDR C2XA03SH198Rib · gougedDURING C-CHECK NUMBER TWO UPPER COWLING WAS FOUND TO HAVE A GOUGE AT THE AFT RIB. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED RIB IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR UPS03440972Frame · crackedINSPECTION TYPE: C, NR 2 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD, CRACK REVEALED AT O/B SIDE FWD FRAME WEB LOWER O/B EDGE AS MARKED. NR 2 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD FRAME WEB REPAIRED AS PER RS R54-53-35039 AND UPS ENGINEERING FILE NR 747-54-2SDR SWIA200312157Frame · crackedREINFORCEMENT FRAME FOR LT HYD PACK FWD FIREWALL, LT SIDE CRACKED AT HYD PRESS LINE FITTING POINT. (DISCOVERED DURING C-CHECK) INSTALLED REPAIR DOUBLER IAW IC 2003-12012138. SEE RII 54-301 & M337. P/N: 120-18896-001SDR ABXA030191Frame · damagedNR 2 ENGINE RIGHT CORE COWL FRAME NAS STA. 304.60 AND NAC WL 73, DAMAGE WAS FOUND ON FRAME P/N 314T1210-333. REPAIRED AREA IAW REA B671-46254MR.SDR SWIA200312091Rib · crackedFS 605 LT PYLON RIB CRACKED. (DISCOVERED DURING C-CHECK) REPLACED RIB IAW CRJ SRM 51-40-11 P/N: 601-37004-85SDR DHL2003366514Frame · wornNR 1 O/B CORE NACELLE L/E FRAME, EXISTING REPAIR WORN THROUGH. REMOVED WORN FRAME AND INSTALLED NEW FRAME IAW BAC DWG NSL6361.SDR DHL2003366513Rib · damagedNR 1 ENG O/B CORE NACELLE INTERIOR AFT RIB IS DAMAGED. ROUTED OUT DAMAGE AREA AN INSTALLED REPAIR DOUBLER IAW TIMCO REO G09306.SDR DHL2003366511Longeron · crackedNR 1 ENGINE O/B CORE NACELLE DOOR UPPER HINGE, CRACK ACCESS LONGITUDNAL SUPPORT ANGLE DOT C3158. REMOVED DAMAGED LONGERON ASSY & INSTALLED NEW LONGERON ASSY IAW DAC WSL6361.SDR SWIA200312118Support · crackedRT WHEEL WELL INBOARD SIDE VERTICAL SUPPORT CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED RIGHT WHEEL WELL BRACKET IAW 120 SRM 51-10-02. P/N: 120-22916-001SDR SWIA200312116Frame · crackedRIGHT ENGINE FRAME 1 CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED RIGHT NACELLE FRAME 1 IAW SERVICE BULLETIN 120-54-0036.SDR AWXA200300595Structure · crackedDURING C-03 CHECK A 1/2 INCH CRACK WAS FOUND ON RT PYLON ATTACH ANGLE (EXTRUSION PROFILE) AT THE INBOARD FORWARD CORNER OF PANEL 4230 LT. MAINTENANCE CUTOUT DAMAGED SECTION OF ATTACH ANGLE; FABRICATED A FILLER AND REPAIR SPLICE; INSTALLED REPAIR PARTS IAW A320SDR 03FDEA00486Frame · crackedNR 1 ENGINE UPPER NACELLE SKIN HAS CRACK FORWARD OF PIN LATCH CUTOUT AREA. REMOVED, FABRICATED AND INSTALLED ANGLE IAW BOEING 727 SRM 51-30-2.SDR 03FDEA00482Frame · gougedNR 3 ENGINE NACELLE HAS A GOUGE AT FRAME NR 7. REPAIRED COWLING FRAME IAW BOEING 727 SRM 54-10-2 FIGURE 5.SDR 03FDEA00478Frame · chafedNR 3 ENGINE UPPER COWLING NR 5 UPPER LATCH FRAME STIFFENER HAS CHAFING CONDITION.SDR 03FDEA00474Frame · chafedNR 3 ENGINE COWLING FRAME NR 5 HAS A HOLE AND CHAFING CONDITION.SDR 030035164Frame · crackedLEFT HAND PYLON FRAME (WEB) AT FS 556 HAS 2 HORIZONTAL CRACKS RUNNING BETWEEN 2 HYDRAULIC LINE CONNECTIONS. SHEAR WEB PART NUMBER 1159P20502-511. CRACKS ARE WHERE THE FOLLOWING HYDRAULIC LINES ARE ATTACHED TO WEB WITH BULKHEAD FITTING: AE700755-1 (FLEX LINE), SDR SWIA200311945Rib · crackedLEFT PYLON RIB AT FS 605.00 CRACKED LOWER OUTBOARD FLANGE. FOUND DURING C-CHECK INSPECTION. REPLACED RIB IAW CRJ SRM 51-40-11, 51-42-21, AND 51-23-00.SDR ASAA0310188Frame · chafedOKC - DURING D-CHECK, FOUND NR 1 ENGINE COWL FRAME AT NACELLE STATION 116.25 CHAFED. FABRICATED AND INSTALLED REPAIR TO FRAME PER SRM. (M)SDR ASAA0310175Longeron · gougedOKC - DURING D-CHECK, FOUND NR 2 ENGINE COWL LONGERON AT NACELLE STATION 170.50 - 221 GOUGED. REMOVED AND REPLACED LONGERON IAW SRM. (M)SDR ASAA0310176Frame · chafedDURING D-CHECK, FOUND NR 2 ENGINE COWL FRAME AT NACELLE STATION 124.25 CHAFED. REMOVED AND REPLACED FRAME IAW SRM. (M)SDR ASAA0310179Frame · crackedOKC - DURING D-CHECK, FOUND NR 1 ENGINE COWL FRAME AT NACELLE STATION 100.60 CRACKED. REMOVED DAMAGED SECTION AND REPAIRED PER SRM. (M)SDR 2003UALA00304Frame · crackedNR 2 PYLON AFT LOWER INBOARD FRAME CRACKED BELOW PANEL 444 DL. MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME.SDR ASAA0310074Rib · gougedPAE - DURING C-CHECK, FOUND NR 2 ENGINE COWL RIB AT NACELLE STATION 152.25, GOUGED. REMOVED DAMAGED AREA AND REPAIRED RIB PER SRM. (M)SDR SWIA200311907Rib · crackedRIGHT PYLON RIB AT FS 605 IS CRACKED AT LOWER FLANGE NEAR OUTBOARD END. FOUND DURING C-CHECK INSPECTION. REPLACED RIB IAW CRJ SRM 51-40-11, 51-42-06, AND 51-42-20. P/N 601-37004-86.SDR 030011849Frame · crackedLEFT HAND PYLON FRAME (WEB) AT FS 556 HAS 2 HORIZONTAL CRACKS RUNNING BETWEEN 2 HYDRAULIC LINE CONNECTIONS. SHEAR WEB PART NUMBER 1159P20502-511. CRACKS ARE WHERE THE FOLLOWING HYDRAULICS LINES ARE ATTACHED TO WEB WITH BULKHEAD FITTINGS: AE700755-1 (FLEX LINE)SDR AMWA12Spar Cap · chafedUPON A MAINTENANCE CHECK IT WAS DISCOVERED THAT BOTH THE RIGHT AND LEFT LOWER SPAR CAP WAS CHAFFING. BLENDED OUT THE CHAFED AREA IN ACCORDANCE TO RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT WILL BE REQUIRED.SDR AMWA11Spar Cap · chafedUPON A MAINTENANCE CHECK IT WAS DISCOVERED THAT BOTH THE RIGHT AND LEFT LOWER SPAR CAP BEHIND INNER FENDER WAS CHAFED BY FUEL PRESSURE SWITCH LINE. THE CORRECTIVE ACTION WAS THAT THEY BLENDED , ALODINED AND PRIMED THE CHAFFED AREA IN ACCORDANCE TO RAYTHEON FIESDR AMWA10Spar Cap · chafedUPON A DETAILED INSPECTION MAINTENANCE FOUND THAT THE LEFT AND RIGHT LOWER SPAR CAP BEHIND NACELLE INNER WAS CHAFED. BLENDED BOTH OF THE LOWER SPAR CAPS IN ACCORDANCE WITH RAYTHEON FIELD REPAIR. REFERENCE NUMBER JMP/0209-03. NO TEARDOWN REPORT WILL BE REQUIRESDR QXEA0300269Frame · crackedPDX - AFT NACELLE FRAME CRACKED AT STATION XN210.00, ON OUTBOARD SIDE OF NACELLE, NEXT TO TRAILING EDGE OF WING. REPAIRED IAW HORIZON AIR EA 6-54-193.SDR QXEA0300233Frame · crackedPDX-LOWER COWL NR 2 MID FRAME IS CRACKED. REPAIRED IAW RD8/4-71-016.SDR 2003UALA00134Spar · crackedNR 2 PYLON UPPER SPAR WEB AT STA 180 IS CRACKED AT RADIUS OF CUTOUT. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER SPAR WEB WITH DOUBLER AND ANGLE REPAIR.SDR 2003UALA00107Spar · crackedNR 1 PYLON UPPER SPAR WEB CRACKED AT AFT CUTOUT, AFT OUTBOARD RADIUS. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB W/DOUBLER.SDR P5CA0300738Frame · crackedCRACK, APPROX. 1", FOUND #4 PYLON REAR ENG. MOUNT BULKHEAD TOP MOST L/H FRAME ON HORIZONTAL FLANGE, STARTING FROM TOP EDGE. FRAME REPAIR CARRIED OUT PER SRM 54-10-03 & FAA FORM 8110-3.SDR P5CA0300737Frame · crackedCRACK 1-1/2" FOUND #3 PYLON REAR ENG. MOUNT BULKHEAD TOP MOST L/H FWD FRAME REAPIR ANGLE, STARTING FROM TOP EDGE RADIUS. FRAME REPAIR ANGLE REPLACED PER SRM 54-10-03 & FAA FORM 8110-3.SDR P5CA0300736Frame · cracked5 CRACKS TOTAL FOUND #2 PYLON REAR ENG. MOUNT BULKHEAD TOP MOST FWD FRAME. L/H: (1) 2" CRACK ON L/H SIDE FRAME, STARTING FROM TOP EDGE ON VERTICAL FLANGE. R/H: (3) 1/2" EA. CRACKS ON R/H SIDE, STARTING ON 1ST AFT FASTENER HOLE FROM TOP ON HORIZONTAL FLANGESDR P5CA0300735Frame · crackedCRACK FOUND #1 PYLON REAR ENG. MOUNT BULKHEAD L/H FWD FRAME APPROX. 1/2" FROM TOP RADIUS. FRAME REPAIR CARRIED OUT PER SRM 54-10-03 & FAA FORM 8110-3.SDR 2003UALA00091Frame · crackedNR 2 PYLON SAILTAIL FRAME WAS CRACKED AT C-CHECK. MAJOR REPAIR ACCOMPLISHED. FRAME REPLACED.SDR 2003UALA00077Spar · crackedRT PYLON, STA 180 JUST FORWARD OF WING FRONT SPAR, UPPER SPAR WEB IS CRACKED IN WEB RADIUS. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB WITH DOUBLER ANGLE.SDR 2003F00284Frame · crackedAT C-CHECK, FOUND NR 2 ENGINE BULKHEAD AT FUSELAGE STATION 1342 ENGINE COWL LIP SEAL IS CRACKED AT 10 O'CLOCK TO 11 O'CLOCK POSITION. INSTALLED NEW COWL SEAL LIP RETAINER NR 2 ENGINE AT STATION 1342 FROM STRINGER 6L TO STRINGER 6R. (M)SDR P5CA0300729Frame · crackedCRACK FOUND #4 PYLON REAR ENG. MOUNT BULKHEAD FRAME ASSY BELOW NAC WL 167.0 ON L/H FWD, R/H FWD & AFT AT FASTENER HOLE. REPLACEMENT OF CRACKED FRAME ASSY CARRIED OUT AS PER SRM 51-10-01SDR 2003UALA00069Spar · crackedNR 1 PYLON, AFT UPPER SPAR WEB, IS CRACKED AT CORNER OF FEED THROUGH CUT-OUT. MAJOR REPAIR ACCOMPLISHED W/DOUBLER AND STIFFENERS.SDR SROM200300013Rib · chafedDURING C CHECK INSPECTION FOUND NR 2 ENGINE OB NACELLE NR 10 RIB CHAFED 8 INCHES FROM LOWER EDGE. CUT OUT DAMAGE 1 X 3 INCHES, FABRICATED REPAIR DOUBLER, ALODINED, PRIMED PART AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3 AND 54-30-1. MINOR REPAIR.SDR SWIA200311692Frame · crackedFOUND CRACKS IN FRAME NR 1 ON RIGHT NACELLE. FOUND DURING ENGINE CHANGE. COMPLIED WITH S/B 120-54-0036, INSTALLED NEW FRAME NR 1.SDR AMWA113Rib · crackedDURING INSPECTION THE LEFT I/B WING OF ENG NACELLE RIB THAT SUPPORTS LANDING GEAR POWER PACK WAS FOUND TO BE CRACKED ON TOP SIDE IN RADIOUS OF RIB APPROX 3 INCHES LONG. REPAIRED BY REPLACING RIB ASSY.
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