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 MALA050439Stringer · crackedDURING C2 INSPECTION, FOUND 1 CRACKED STRINGER NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL.SDR MALA050346Stringer · crackedDURING C2 INSPECTION, FOUND 1 CRACKED STRINGER, NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL.SDR UPS05444425Frame · crackedNR 2 PYLON AFT BULKHEAD I/B FRAME ADJACENT TO UPPER SPAR FITTING FOUND CRACKED, CRACK LENGTH .375 AND .250. NR 2 PYLON AFT BULKHEAD I/B FRAME REPAIRED AS PER HX RS R54-53-35295 AND UPS EA ENGINEERING FILE NR 747-54-20051.SDR UPS05444421Frame · crackedNR 2 PYLON AFT BULKHEAD O/B FRAME ADJACENT TO UPPER SPAR FITTING FOUND CRACKED, (CRACK LENGTH .25 INCH AND .9375 INCH ). NR 2 PYLON AFT BULKHEAD O/B FRAME REPAIRED AS PER HX RS NR R54-53-35295 AND UPS ENGINERING FILE NUMBER 747-54-20051.SDR 05FDEA00886Spar Cap · crackedNACELLES/PYLONS - PYLON STRUCTURE - CRACK ON NR 2 ENGINE PYLON UPPER SPAR CAP COMPLY WITH EA 1-5450-76453. COMPLIED NR 2 ENG UPPER SPAR REPAIR PER EA 1-5450-81683.SDR AWXA200500444Spar · crackedSAL - MAJOR REPAIR - DURING ACCOMPLISHMENT OF SB 757-54A0039 A 1.375 INCH CRACK WAS FOUND ON NR 2 ENGINE PYLON UPPER SPAR WEB. MAINTENANCE STOP DRILLED CRACK ON NR 2 ENGINE PYLON UPPER SPAR WEB; PERFORMED HFEC INSPECTION TO VERIFY CRACK CONTAINED; FABRICATED SDR DHL2005783513Frame · crackedNR 2 ENGINE STRUT RT COWLING FRAME CRACKED AT 3RD CUTOUT (ENGINE SUPPORT STRUCTURE). ROUTED OUT DAMAGED AREA AND FABBED REPAIR ANGLE FROM 301 1/2HD .050 PO NR 90001233 DIM 7 3/4" BY 3 1/2" IAW 727 SRM 54-10-2 FIG 8 AND 51-40-3 FIG 1. REPAIR ANGLE TREATED, PRSDR UIEA200500027Spar · crackedDURING SCHEDULED MAINTENANCE, NR 3 PYLON INBOARD MIDSPAR CHORD WAS FOUND CRACKED ON THE VERTICAL FLANGE. THE AFFECTED SECTION OF CHORD WAS TRIMMED OUT. NDT INSPECTION WAS PERFORMED AT TRIMMED EDGES AND AT AL AFFECTED FASTENERS LOCATION TO ENDURE A CRACK AND SDR MALA050234Longeron · chafedRIGHT NACELLE, I/B SIDE, INSIDE FWD ELECTRONIC BAY, INBOARD LOWER LONGERON IS CHAFED. THE DAMAGE IS ACCEPTABLE IAW SAAB DOCUMENT 340S0S008258.SDR QXEA200500284Frame · wornYYC - RT ENGINE UPPER FAN COWL INTERNAL OUTBOARD FORWARD FRAME WORN. REPAIRED IAW HORIZON AIE EA R-54-75 AND REO 670-54-14-336.SDR CA050117001Frame · cracked(CAN) DURING A ROUTINE INSPECTION A CRACK WAS FOUND PROPAGATING FROM THE OVAL HOLE IN THE RT FRAME AT STATION 207.125 (HALF WAY BETWEEN THE FLOOR AND THE WINDOW). THE CRACK WAS APPROXIMATELY 1 = INCH LONG AND EXTENDED FROM THE 11 O`CLOCK POSITION OF THE LIGHTSDR UPS05443719Frame · crackedINSPECTION TYPE:C, NR 4 NACELLE STRUT REAR MOUNT BULKHEAD FWD OUTBOARD FRAME WEB FOUND CRACKED (REFER ATTACH SKETCH FOR LOCATION). REAR ENG MOUNT BULKHEAD FRAME REPAIRED PER RS R54-53-35228 AND ENGINEERING FILE NUMBER 747-54-20050.SDR SWIA200414399Rib · crackedRIGHT PYLON RIB FS 605 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED RIB IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00.SDR QXEA200500020Frame · gougedYYC - LEFT HAND ENGINE FORWARD FRAME INTAKE COWL ATTACHMENT LUGS, INBOARD HAS BEEN GOUGED ON INBOARD FACE, ABOVE PIN HOLE. REPAIRED IAW HORIZON AIR EA 6-54-325 AND RD 8/4-54-219.SDR QXEA200500021Frame · gougedYYC - RIGHT HAND ENGINE FORWARD FRAME, INTAKE COWL ATTACHMENT LUG, OUTBOARD HAS BEEN GOUGED ON THE OUTBOARD FACE. REPAIRED IAW HORIZON AIR EA 6-54-325 AND RD 8/4-54-219.SDR SWIA200414187Rib · crackedLEFT PYLON AFT RIB IS CRACKED; FS 605.00, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED RIB IAW SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00.SDR 04FDEA03134Longeron · wornNR 3 INBOARD COWLING UPPER LONGERON CHAFED UNDER RUB STRIP. FABRICATED AND INSTALLED DOUBLER IAW FEDEX EA 8-5410-81527, NACELLES/ PYLONS, NR 3 ENGINE INBOARD CORE COWL UPPER LONGERON, REPAIR. REFERENCE NON-ROUTINE N00471.SDR UIEA200400193Frame · crackedD-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION THE NR 3 PYLON AFT ENGINE MOUNT BULKHEAD UPPER ASSY FRAMES CRACKED. STOPPED DRILLED THE CRACK ENDS IAW SRM 51-10-01. HFEC INSPECTED TO ENSURE CRACK CONTAINMENT. FABRICATED AND INSTALLED REPAIR ANGLES ON THE FSDR 2004UALA00913Spar · crackedNR 2 NACELLE UPPER SPAR WEB IS CRACKED SEVERAL PLACES AS SEEN THROUGH ACCESS 446BL. REPAIRED UPPER SPAR WEB WITH DOUBLER AND FILLER JUST FWD OF PYLON AFT BLKHD PER SRM 54-53-01, FIG 208. PER SB 767-54-0092 R1 PROBABLE CAUSE OF CRACKING IS FLEXING OF PYLON MISDR UPS04443313Spar · crackedINSPECTION TYPE:C, A 3 INCH CRACK WAS FOUND AT LOWER WEB AT NAC 220 OF NR 3 PYLON AT PER O/B SIDE. NR 3 PYLON NAC STA 220 O/B SIDE AFT LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 23.SDR UPS04443314Spar · crackedINSPECTION TYPE:C, NR 3 PYLON NAC STA 222 AFT LOWER SPAR WEB I/B SIDE CRACK IS FOUND AS MARK. NR 3 PYLON NAC STA 222 I/B SIDE AFT LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 23.SDR EIA2004121Spar · crackedCRACK AT NAC STA 210, LOWER SPAR WEB, CENTER AREA, NR 1 PYLON. REPAIR LWR SPAR WEB PER SRM 54-10-03, FIG 2, SPAR WEB FABRICATED IAW SRM 54-10-03, FIG 2.SDR ABXA040342Spar Cap · crackedLEFT PYLON FORWARD UPPER SPAR CAP CRACKED AT SECOND FASTENER INBOARD OF FUSELAGE LOFT LINE. REPAIRED IAW JOB CARD EA 54100011-102 AND EA 54100011-001.SDR UPS04242970Frame · crackedINSPECTION TYPE: C, ENGINE NR 2 NACELLE UPPER FRAME CRACKED BETWEEN MID AND AFT HINGE POINTS. FABRICATED FRAME IAW SRM 54-10-06, FRAME REPLACED IAW SRM 51-30-02.SDR 04FDEA02149Frame · crackedNR 2 ENGINE RIGHT CORE COWL FORTH RIB AFT CRACKED JUST ABOVE ACCESS DOOR. REMOVED DOUBLER IAW SRM 51-31-01. RECEIVED FROM WELD SHOP CORE COWLING FRAME WELDED BY TRAVLER T4/445038 AND DPS10-301. INSTALLED DOUBLER STIFFENER AND CLIP IAW SRM 51-33-01 AND SRM 5SDR UPS04442834Rib · crackedINSPECTION TYPE:C, NR 4 PYLON NAC STA 232 APPROX I/B RIB CRACKED AS MARK (JUST FWD OF PYLON VALVE PANEL CUTOUT). NR 4 PYLON RIB REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 8 AND SRM 51-30-02.SDR C2XA04SH424Rib · chafedSHV - DURING C-CHECK THE NR 2 ENGINE LOWER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH416Rib · chafedSHV - DURING C-CHECK THE NR 2 ENGINE UPPER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGEMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH397Rib · chafedSHV - DURING C-CHECK THE NR 1 UPPER ENGINE COWLING FT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGEMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR AUS20040512Rib · cracked(AUS) NR 1, NR 3 AND NR 4 PYLONS HAD NR 4 RIB CRACKED IN THE LOWER FLANGE RADIUS. PYLON NR 1, CRACK LENGTH 22.86MM (0.9IN) PYLON NR 3, CRACK LENGTH 12.7MM (0.5IN) PYLON NR 4, CRACK LENGTH 20.32 (0.8IN).SDR SWIA200413399Frame · crackedRIGHT OUTBOARD NACELLE INTERNAL FRAME CRACKED. DISCOVERED AT C-CHECK INSPECTION. INSTALLED DOUBLER AT AFFECTED AREA IAW 120 SRM 51-10-02 P2 SEC 2B.SDR C2XA04SH337Rib · chafedSHV - DURING C-CHECK THE LEFT HAND LOWER COWLING RIB AT STATION NX-2180.0 WAS FOUND TO HAVE A HOLE CHAFED IN IT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 54-10-07 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH319Stiffener · chafedDURING C-CHECK THE NR 1 ENGINE LOWER ENGINE COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 04FDEA01400Rib · crackedNUMBER 2 ENGINE INLET STRUCTURE RIB CRACKED AT SPLICE AT 1 O’CLOCK POSITION, ACCESS THROUGH PANEL 362JR. REMOVED SPLICE, INTERCOSTAL AND STIFFENER SECTION IAW DC10 SRM 51-35-01 VOL 2, FORMED STIFFENER AND SPLICE IAW DC10 SRM 51-10-00 VOL 2, INSTALLED REPAIR PSDR C2XA04SH295Stiffener · chafedSHV - DURING C-CHECK THE NUMBER 2 ENGINE LOWER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGEMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SWIA200413405Frame · crackedRIGHT ENGINE FRAME NR 1 IS CRACKED ON OUTBOARD SIDE. DISCOVERED AT C-CHECK. INSTALLED NEW RIGHT ENGINE FRAME NR 1 IAW SB 120-54-0036 AND RII CARD RII54-301.SDR SWIA200413403Frame · crackedLEFT INBOARD NACELLE INTERNAL FRAME CRACKED. DISCOVERED AT C-CHECK INSPECTION. INSTALLED DOUBLER AT AFFECTED AREA IAW EMB120 SRM 51-10-02 PG 2 SEC 2B.SDR SWIA200413402Frame · crackedLEFT OUTBOARD NACELLE INTERNAL FRAME CRACKED. DISCOVERED AT C-CHECK INSPECTION. APPLIED DOUBLER TO LEFT OUTBOARD NACELLE FRAME IAW SRM 120 51-10-02 PG 2 SEC 2B.SDR SWIA200413401Frame · crackedRIGHT INBOARD NACELLE INTERNAL FRAME CRACKED. DISCOVERED AT C-CHECK INSPECTION. APPLIED DOUBLER TO RIGHT INBOARD NACELLE FRAME IAW SRM 120 51-10-02 PG 2 SEC 2B.SDR C2XA04SH278Rib · chafedSHV-DURING C CHECK THE RIGHT ENGINE LOWER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR UIEA200400069Rib · crackedFOUND INTERIOR RIB CRACKED AT NAC STA 318.20 RIGHT SIDE NR 3 PYLON LOWER AREA. DEFECT RECTIFIED AS PER TARNSIT W/O 71181467000001 IAW BOEING DRAWING 65B94117 REV E, 65B89043 REV D, 65B89044 REV B, AND BOEING SEP-SIN-04-00049H. (M)SDR UIEA200400070Rib · crackedFOUND INTERIOR RIB CRACKED AT NAC STA 300 LEFT SIDE NR 3 PYLON LOWER AREA. DEFECT RECTIFIED AS PER TRANSIT W/O 71181467000001 IAW BOEING DRAWING 65B94117 REV E, 65B89043 REV D, 65B89044 REV B, AND BOEING SEP-SIN-04-00049H. (M)SDR UIEA200400065Rib · crackedFOUND INTERIOR RIB CRACKED AT NAC STATION 220 RIGHT SIDE. DEFECT RECTIFIED AS PER TRANSIT W/O 71181467000001 IAW BOEING DRAWING 65B94117 REV E, 65B89043 REV D, 65B89044 REV B, AND BOEING RES SIN-04-00049H. (M)SDR SWIA200413330Frame · crackedRT NACELLE FRAME NR 1 CRACKED INBOARD AND OUTBOARD AT TORSION BAR MOUNTS. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT NACELLE FRAME IAW 120 SB 120-54-0036 AND RII. PART II COMPLIED WITH.SDR UPS04442101Spar · crackedINSPECTION TYPE:C NR 2 PYLON AFTER LOWER SPAR WEB NAC STA 240 AND NAC STA 256 I/B EDGE AREA CRACKS ARE FOUND AT 2 LOCATION AS MARK. NR 2 PYLON LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 2.SDR C2XA04SH181Rib · gougedSHV- DURING C-CHECK THE NR 1 ENGINE UPPER COWLING, AFT OUTBOARD RIB WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR DHL2004363004Rib · crackedDURING A-CHECK, PYLON ENGINE NR 1 AT COWL HINGE FITTING INBOARD SIDE HAS A CRACK BELOW TEE BRACKET AT RIB 4. NR 4 RIGHT RIB HAS APPROXIMATELY A 3 INCH CRACK AT REVERSER HINGE AFT BRACKET (VISUALLY DETECTED). PERFORM EXTERNAL INSPECTION OF SIDE PANEL AND BOLTSDR C2XA04SH156Rib · chafedSHV - DURING C-CHECK, THE AFT EDGE MEMBER OF THE NR 2 ENGINE UPPER COWLING WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH145Rib · gougedSHV - DURING C-CHECK THE LEFT UPPER COWLING OUTBOARD REINFORCEMENT ANGLE WAS FOUND TO BE GOUGED BETWEEN STATION XN 2355 AND XN 3168. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RSDR SWIA200413166Rib · crackedLEFT PYLON LEADING EDGE RIB CRACKED ON LOWER FLANGE AT FS 605.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIB IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, AND RII53-401.
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