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 C2XA99IA160Frame · crackedDURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT NACELLE FRAME CRACKED ON COWL FLANGE FOR PANEL 414. WELDED CRACKED AREA IAW MIL-STD-2219, NDT PENETRANT REVEALS NO CRACK EXISTS AFTER REPAIR. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99IA158Frame · crackedDURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT NACELLE FORWARD FRAME CRACKED AT INBOARD COWL STAY FITTING. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW SRM 51-70-05 AND 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR ASOA99023Frame · crackedDURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (M)SDR COMA9910026Frame · crackedLEFT NACELLE, FRAME WEB NR 10 CRACKED AT INBOARD RADIUS OF THE FLANGE. REPAIRED BY SPLICING IN A NEW FLANGE PER AERODESIGN REPORT NR 1076-2 AND EMB120 SRM 51-40-02.SDR ASOA99010Frame · crackedDURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (M)SDR EIAA990001Frame · crackedHKG - DURING B-CHECK, NR 2 PYLON NACELLE STATION 162 LEFT AND RIGHT FRAMES FOUND CRACKED ADJACENT TO FIRE BOTTLE ATTACHMENTS. REPAIRED PER SRM 54-10-03 FIG 1. (M)SDR UPS99228417Rib · crackedINSPECTION TYPE-C, SUSPECT CRACK ON CENTER ENGINE AFT MOUNT SUPPORT RIB RIGHT CHORD APP ROX 17 INCHES FROM TOP OF CHORD. RIB CHORD REPLACED IAW DRAWING 65-22913, 65-17553, 65-17551.SDR 99ZZZX204Frame · crackedDURING ROUTINE MAINTENANCE CHECK, CRACKS WERE FOUND ON BOTH ENGINE NACELLE NR 1 FRAMES. ON THE LT FRAME, THE CRACK IS LOCATED ON THE LOWER SIDE OF THE STIFFENING WEB BETWEEN THE TOP OUTBOARD MOUNTING BOLT HOLE AND THE OUTBOARD EDGE OF THE FRAME. ON THE RT FRSDR 99ZZZX200Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN RIGHT FORWARD NACELLE NR 1 FRAME. REPETITIVE DISCREPANCY AS PREVIOUSLY DETAILED AND REPORTED. SUBMITTER STATED POSSIBLE CAUSE REMAINS UNKNOWN, WOULD SUSPECT ENGINE TORQUE AND VIBRATION AS CONTRIBUTING FACTSDR 99ZZZX199Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN LEFT FORWARD NACELLE NR 1 FRAME. REPETITIVE DISCREPANCY AS PREVIOUSLY DETAILED AND REPORTED. SUBMITTER STATED POSSIBLE CAUSE REMAINS UNDETERMINED, WOULD SUSPECT ENGINE TORQUE AND VIBRATION AS CONTRIBUTING SDR HNAA9893786Frame · crackedSBY - NR 2 NACELLE OUTBOARD MAIN OUTBOARD MAIN FRAME 'Z' MEMBER CRACKED AT UPPER END. STOP DRILLED CRACK AND INSTALLED RIVETS THROUGH 'Z' MEMBER, LANDING GEAR MAIN FRAME AND SKIN. (M)SDR 99ZZZX201Frame · crackedDURING ROUTINE MAINTENANCE CHECKS, CRACKS WERE FOUND ON BOTH ENGINE NACELLE NR 1 FRAMES. ON THE LT FRAME, THE CRACK IS LOCATED ON THE LOWER SIDE OF THE STIFFENING WEB BETWEEN THE TOP OUTBOARD MOUNTING BOLT HOLE AND THE OUTBOARD EDGE OF THE FRAME. THE CRACK ISDR 98ZZZX4703Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN RT ENGINE FORWARD NACELLE NR 1 FRAME. SEEMS TO BE A REPETITIVE DISCREPANCY AS PREVIOUSLY DETAILED AND REPORTED. SUBMITTER STATED POSSIBLE CAUSE IS STILL UNDETERMINED. WOULD SUSPECT ENGINE TORQUE AND VIBRASDR 98ZZZX4702Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN LEFT ENGINE FORWARD NACELLE NR 1 FRAME. SEEMS TO BE A REPETITIVE DISPREPANCY AS PREVIOUSLY DETAILED AND REPORTED. SUBMITTER STATED CAUSE REMAINS UNDETERMINED. WOULD SUSPECT ENGINE TORQUE AND VIBRATION TO SDR ASOA98102Frame · crackedDURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS INBOARD AND OUTBOARD OF MOUNT HOLES FOR LEFT AND RIGHT SIDE OF ENGINE FORWARD TORQUE MOUNT. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (SDR ASOA98101Frame · crackedDURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS INBOARD AND OUTBOARD OF MOUNT HOLES FOR LEFT AND RIGHT SIDE OF ENGINE FORWARD TORQUE MOUNT. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (SDR 98ZZZX4708Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN RT ENGINE FORWARD NACELLE NR 1 FRAME. SUBMITTER STATED SEEMED TO BE A REPETITIVE DISCREPANCY AS PREVIOUSLY DETAILED AND REPORTED AND POSSIBLE CAUSE IS STILL UNDETERMINED. WOULD SUSPECT ENGINE TORQUE AND VISDR 98ZZZX4704Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN LT ENGINE FORWARD NACELLE NR 1 FRAME. SEEMS TO BE A REPETITIVE DISCREPANCY AS PREVIOUSLY DETAILED AND REPORTED. SUBMITTER STATED CAUSE IS STILL UNDETERMINED. WOULD SUSPECT ENGINE TORQUE AND VIBRATION TO BSDR DL76L982300Spar Web · crackedTWO CRACKS WERE FOUND ON 8/20/97 EMANATING FROM A DRAIN HOLE ON THE NR 1 ENGINE STRUT FWD UPPER SPAR WEB AT NAC STA 158. THE CRACKS WERE TRIMMED OUT ON A TIME-LIMITED BASIS. AT 11/98 OVERHAUL, A PERMANENT DOUBLER REPAIR WAS INSTALLED. CRACKS WERE DUE TO FATSDR CALA9802027Frame · crackedINSPECTION FOUND THREE .75 INCH CRACKS IN VERTICAL FIN FRAME ON TOP OF S-DUCT AT FRAME 1303. A REPAIR WAS INSTALLED IAW SRM 51-40-2 PAGE 1 AND 51-30-2 PAGE 4.SDR ABXA9800936Rib · crackedDURING C-CHECK, FOUND FORWARD UPPER EDGE OF NR 1 PYLON RIB CRACKED INSIDE ACCESS PANEL AREA 8111. REPAIRED RIB IAW ABX DC9 SSRM DWG K05159.SDR C2XA98IA327Frame · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE OUTBOARD AFT MAIN LANDING GEAR DOOR, AFT HINGE POINT FORWARD FRAME CRACKED. MAINTENANCE REMOVED AND REPLACED THE HALF FRAME IAW EMB-120 SRM 54-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERIVCE. TT: 1SDR C2XA98IA325Frame · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT NACELLE INBOARD AFT MAIN LANDING DOOR, FORWARD HINGE POINT FRAME CRACKED. MAINTENANCE STOP-DRILLED THE CRACK AND INSTALLED REPAIR DOUBLER IAW EMB-120 SRM 54-20-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR AU981085Keelson · cracked(AUS) LEFT NACELLE STRUCTURE INBOARD KEELSON CRACKED. PART TC: 29,623.SDR 98ZZZX3228Frame · crackedDURING PERFORMANCE OF C-CHECK INSPECTION TASK ON NR 1 FRAME OF ENGINE NACELLE. CRACKS WERE VISUALLY DETECTED IN THE VICINITY OF THE MOUNT HOLES FOR THE TORQUE MOUNT. THE LEFT MOUNT CRACKS WERE FOUND ON THE INBOARD AND OUTBOARD (LEFT) FRAME INBOARD SIDE HAS SDR C2XA98IA233Frame · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE FRAME 9 CRACKED ON THE OUTBOARD UPPER AFT SIDE. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR 98ZZZX2498Frame · crackedDURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT ENGINE NACELLE WAS FOUND CRACKS IN WEB APPROXIMATELY 5 INCHES OUTBOARD OF MOUNT HOLES FOR LEFT AND RT SIDE OF ENGINE FORWARD TORQUE MOUNT. RIGHT NACELLE WAS ALSO FOUND TO HAVE A CRACK IN THE SAME AREA ON THE OTBD SDR P5CA9800792Frame · crackedNR 1 PYLON RIGHT FRAME AT NAC STN 168 CRACKED AND LEFT FRAME AT NAC STN 193 FOUND CHAFED. REPLACED FRAMES PER BOEING SRM 51-10-01.SDR CALA9800806Rib · crackedFIRST RIB AFT OF AFT ENG MOUNT IS CHAFED TWO SPOTS NUMBER ONE ENGINE PYLON. REMOVED DAMAGED AREA NR 1 ENGINE PYLON MOUNT RIB. FABRICATED NEW REPAIR, INSTALLED PER SRM 51-40-2 AND 51-30-2.SDR P5CA9800850Frame · crackedNR 1 ENG LT SIDE COWL FOURTH FRAME FROM FRONT IS CRACKED ABOVE THE LATCH. REPAIRED PER SRM 51-10-01 P 18.SDR C2XA98IA114Rib · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE RIB CRACKED ON LEFT SIDE AT FRAME NR 13. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED REPAIR DOUBLER IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR 98FDEA00272Rib · crackedNR 2 ENG INLET INTERNAL 7TH RIB AFT OF FWD WEB CRACKED, UPPER CAP APPROX 7 LONG, 5:00 POSITION. * S/D* REPAIRED RIB CAP WITH ANGLE DOUBLER IN REF TO SRM 54-10-00. INSTALLED REPAIRED RIB CAP REF SRM 54-10-00. 4-16-98.SDR 98FDEA00232Rib · crackedRIB CRACKED AT BS 1283 AT 7 O'CLOCK POSITION ON S-DUCT. *S/D* REPAIRED RIB AT BS 1283 AT 7 O'CLOCK POSITION ON 5 DUCT IAW FED-EX SRM 54-10-3.SDR DL72E980709Rib · wornHOLE WORN THROUGH LIP OF NR 2 ENGINE CUTOUT AT 9 O'CLOCK POSITION. FOUND ON LETTER CHECK F-1. INSTALLED DOUBLER PER M/M 53-11-0 PG 801.SDR TWAA9809306Frame · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND NR 1 PYLON LOWER END CHORD ANGLE CRACKED, 60 INCHES AFT OF LEADING EDGE, 4 INCHES INBOARD AT OUTBOARD END. INSTALLED DOUBLER PER SRM 54-01, FIG 2, PAGE 7. (X)SDR EIAA980160Frame · holeMZJ - DURING 'C4' CHECK INSPECTION, NR 4 PYLON HAS A HOLE IN FRAME THAT IS BEHIND THE LEFT DOUBLER AT STATION 180. FABRICATED AND INSTALLED THREE ANGLES IAW SRM 54-10-03 AND SRM 51-30-02. (M)SDR RAIA980310Frame · crackedSTL - DURING INSPECTION, FOUND RIGHT ENGINE INTERMEDIATE FRAME CRACKED AT INBOARD VERTICAL MEMBER ABOVE ENGINE ISOLATOR MOUNT. MAINTENANCE REPLACED RIGHT ENGINE INTERMEDIATE FRAME. (M)SDR CALA9800385Frame · crackedINSPECTION FOUND A 4 AND 2 INCH CRACK ON CENTER FRAME ON LT SIDE OF NR 2 ENGINE INLET INSIDE PANEL NR 363EL. THE CRACKS WERE STOP DRILLED IAW SRM 51-90-00. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 54-00-01 AND 51-21-01.SDR EIAA980127Frame · crackedHKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON FRAME CRACKED AT NAC 163. REPAIRED IAW SRM 51-10-01. (X)SDR EIAA98041Frame · crackedHKG - DURING 'C5/D' CHECK INSPECTION, NR 3 PYLON INTERIOR O/B VERTICAL FRAME AT STATION 180 IS CRACKED AT THE UPPER CORNER. REPAIRED IAW SRM 54-10-03 FIG 1. (M)SDR ABXA9800148Frame · crackedNR 3 PYLON 2ND FROM AFT LOWER APRON FRAME CRACKED AT LEFT END. REPAIRED ANGLE IAW DC8 SRM 53-2-0.SDR 98ZZZX2760Frame · crackedATW - NR 4 PYLON BOX STRUCTURE AT RIB NR 4 BOTTOM OTBD FLANGE HAS CRACK APPROXIMATELY .3750 INCH LONG. NR 4 PYLON CRACKING RIB 4 LOWER FLANGE .3750 INCH LONG IS ACCEPTABLE AND MAY CONTINUE IN SERVICE. 1,000 CYCLE REPEAT INSPECTION. DETAILS REPORTED TO BAE RSDR 98ZZZX2756Rib · crackedATW - NR 3 PYLON BOX STRUCTURE AT RIB 4 OTBD BOTTOM FLANGE HAS A CRACK DEVELOPING THAT IS APPROXIMATELY .3750 INCH LONG. NR 3 PYLON CRACKING RIB 4 LOWER FLANGE .3750 INCH LONG IS ACCEPTABLE AND MAY CONTINUE IN SERVICE. 1,000 CYCLE REPEAT INSPECTION. DETAILSSDR 98ZZZX2765Rib · crackedATW - NR 2 PYLON RIB 4 LOWER FLANGE HAS .125 INCH LONG CRACK ON INBOARD SIDE OF CUT-OUT. CRACK MAY CONTINUE IN SERVICE WITH REPETITIVE INSPECTIONS IAW RIL HC546H9018. REPORTED DETAILS TO BAE RDO. GEN W/C FOR REINSPECT.SDR COMA9710497Frame · crackedDURING 1C INSPECTION, TASK 419-012 REVEALED A CRACK IN LEFT NACELLE UPPER HALF-FRAME. REPLACED HALF-FRAME USING AERODESIGN REPORT 2524-2.SDR COMA9710496Frame · crackedDURING 1C INSPECTION, TASK 419-012 REVEALED A CRACK IN LEFT NACELLE UPPER HALF FRAME. THE CRACK WAS .52 LONG AND STARTED AT A NUTPLATE FASTENER. THE NUTPLATE IS ONE OF FOUR INSTALLED TO ATTACH THE EXHAUST DUCT MOUNT BRACKET. REPAIRED HALF-FRAME USING AERODESDR DL72S972348Frame · crackedFRAME CRACKED NR 2 INLET S-DUCT HOUSING FRAME CRACKED ON LT SIDE FS 1233 AT INTERSECTION WITH HORSE COLLAR. REMOVED DAMAGE AND FABRICATED DOUBLERS PER SRM 51-400-3, INSTALLED DOUBLERS PER SRM 51-40-3.SDR UPS97425028Frame · crackedINSPECTION TYPE-C, PYLON 1, FOUND CRACK IN FRAME AT NS 165 LT (NEAR FIRE BOTTLE ATT BRACKET). REPLACED FRAME PER SRM 51-30-02.SDR UPS97425027Frame · crackedINSPECTION TYPE-C, PYLON NR 1, FOUND CRACK IN LT FRAME AT NS 235, BETWEEN MIDSPAR AND LWR SPAR. REPLACED FRAME PER SRM 51-30-02.SDR C2XA97IA312Half Frame · crackedIAH - DURING 2,000 CYCLE STRUCTURAL INSPECTION, FOUND LEFT NACELLE OUTBOARD AFT MAIN LANDING GEAR DOOR AFT HINGE POINT, AFT NACELLE HALF FRAME CRACKED. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW EMB120 SRM 51-10-02. THE AIRCRAFT WAS APPR
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