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 FDKA200705230Frame · chafedLEFT LOWER COWL AFT FRAME IS CHAFED OUT OF LIMITS. REPLACED AFT FRAME WITH NEW ONE.SDR SWIA200718444Rib · crackedRIGHT NACELLE FLAP INNER RIB IS CRACKED, DISCOVERED AT C-CHECK. REPAIRED NACELLE FLAP INNER RIB IAW SRM 51-70-05.SDR DL76L070501Spar · crackedTHE NR 2 PYLON UPPER SPAR WEB WAS FOUND CRACKED AT THE FUEL LINE PASS THROUGH. THE CRACKED WEB WAS CUT OUT AND A REPAIR DOULBER WAS INSTALLED.SDR NWAA071509884Frame · crackedDURING ENGINE CHANGE, FOUND CRACKS IN NR 1 PYLON HORIZONTAL WEB FRAME AT XN 39.250. REPAIRED PER EA 98-209044.SDR 07FDEA01486Spar · crackedA 16MM LONG CRACK WERE FOUND IN THE END OF THE STIFFENER RIB 10 ON PYLON NR 2 LOWER SPAR. REPAIR PERFORMED IAW SB A310-54-2016, APPROVED BY EO 6-5450-7-3302 PT 6.SDR 07FDEA01405Spar · corrodedCORROSION ON UPPER SPAR OF RT PYLON AT RIB 14. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5451-101244 ISSUE "A" AND RAS 044734/013/2006 ISSUE "A".SDR UIEA200700194Spar · damagedNR 4 ENG LT LOWER SPAR CHORDS (SIDE COWL HINGE AREA) AFT AREA FOUND DAMAGED. DAMAGED WEB REPAIRED AS PER BOEING MSG 1-308420578-2.SDR NWAA071706744Frame · crackedDURING "M" CHECK, FOUND CRACKS IN NR 3 PYLON FRAME AND STIFFENER AT NAC STA 210 AND CUT OUT SKIN AT ACCESS PANEL 473 CL. REPAIRED PER EA 67-209239.SDR FDKA200704167Frame · chafedTHE AFT FORMER ON THE LT LOWER ENGINE COWLING IS CHAFED BEYOND ALLOWABLE LIMITS. THE DAMAGED FORMER WAS REMOVED AND REPLACED.SDR KCSA071107Rib · damagedNR 2 PYLON RIB AT NAC STA 209 HAS ELONGATED FASTENER HOLE.SDR DJFA2007036Frame · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE FOUND A CRACK IN THE NR 1 ENGINE AFT NACELLE SUPPORT FRAME. THE CRACK WAS ABOUT .25 INCH, LOCATED ON THE IB SIDE JUST FWD OF THE TR AND JUST ABOVE THE PYLON AT ABOUT THE 0930 POSITION LOOKING AFT. CRACK WAS REPAIREDSDR 07FDEA01133Rib · crackedPYLON NR 2 AT AFT SPAR SECTION PYLON TORQUE BOX INNER SURFACE HAS SEVERAL WORKING RIVETS. VISIBLE THRU OPEN ACCESS DOOR NR 484CR. UPON FURTHER INVESTIGATION CRACKS CONTINUING PAST STOP DRILLED ON RIB 20. REMOVED RIB ASSY IAW SRM 51-40-21. FABBED AND RECESDR SWIA200718067Frame · crackedLEFT MLG OUTBOARD AFT DOOR AFT ATTACH ARM UPPER ATTACH POINT NACELLE FRAME CRACKED, DISCOVERED DURING A-CHECK INSPECTION. INSTALLED SERVICEABLE HALF-FRAME ON LEFT OUTBOARD AFT NACELLE IAW SRM 51-40-02. OPERATIONAL CHECKS GOOD.SDR 07FDEA00896Spar · crackedCRACKED HOLE ON PYLON NR 2 AT RIB 8 UPPER SPAR. REPAIR WAS PERFORMED IAW SRM 54-51-31/FIG 201 AND APPROVED BY EA 6-5451-103400.SDR QXEA200700407Frame · chafedC4 PDX - RIGHT NACELLE INBOARD FRAME INSIDE WHEELWELL HAS CHAFE LEFT FORWARD CORNER AT STATION ZN 15.00 AND XN 130.06. REPAIRED IAW SRM 51-20-16, 51-20-36, AND 51-20-51, RD8-54-2370.SDR CA070313009Frame · cracked(CAN) DURING ANNUAL INSPECTION, THE LOWER LONGITUDINAL FRAME OF THE STAINLESS STEEL FIREGATE P/N 80450-1 WAS NOTED TO BE CRACKED AT THE FWD END AND BULGED AT THE AFT END. (2) OTHER AC HAVE SIMILAR DAMAGE. WATER WAS FOUND IN THE TUBE AND THE DAMAGE APPEARS TO SDR UIEA200700121Frame · crackedNR 1 PYLON AFT UPPER BULKHEAD "T" FRAME HAS A CRACK AT AFT FLANGE AND A SECOND CRACK AT FORWARD FLANGE, OUTBOARD OF NR 1 PYLON FRONT SPAR CHORD ASSEMBLY. AFT FLANGE CRACK IS 0.750 INCH LONG. FORWARD FLANGE CRACK IS 0.375 INCH LONG AT NACELLE STATION 270.00. ASDR NWAA070796305Frame · crackedDURING "M" CHECK, FOUND CRACK IN AFT LOWER SIDE OF PYLON FRAME OUTBOARD CUTOUT FOR PANEL 484ER. REPAIRED PER EA 63-208900.SDR USAA070135Frame · crackedTHE U-SHAPE FRAME IN NR 1 PYLON BELOW AFT SPAR CRACKED. REPLACED U-SHAPE FRAME PER EA 98483, DEFECT SIZE: 1 INCH.SDR SWIA200718005Rib · crackedLEFT MLG MID COWL FIRST RIB AFT OF DOOR FRAME CRACKED AT STRINGER CUT OUT, DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIB IAW SRM 51-70-05 AND RII 54-900-1000.SDR 07FDEA00349Rib · gougedNR 3 ENGINE UPPER COWL 2ND FROM FWD END RIB IS GOUGED ACCOMPLISHED TYPICAL FORMED REPAIR ON NR 3 ENG UPPER COWL REB REF SRM 51-43-3, PG 1-3 FIG 1. REINSTALLED NR 3 ENG UPPER COWL REF MM 71-10-011-4.SDR KCSA071050Frame · gougedNR 1 PYLON INTERNAL FRAME IS GOUGED AT NAC STA 194, WL 150, ABOVE MID SPAR AREA.SDR KCSA071048Frame · crackedNR 4 PYLON ENGINE MOUNT BULKHEAD FRAME IS CRACKED 1 INCH FORWARD SIDE, INBOARD OF PYLON UPPER SPAR CHORD AT NAC STA 221.9SDR KCSA071047Frame · crackedNR 2 PYLON REAR ENGINE MOUNT BULKHEAD FRAME IS CRACKED 1 INCH FORWARD SIDE, INBOARD & OUTBOARD OF PYLON UPPER SPAR CHORD AT NAC STA 221.9.SDR KCSA071046Frame · crackedNR 1 PYLON REAR ENGINE MOUNT BULKHEAD FRAME IS CRACKED 1 INCH, FORWARD SIDE, INBOARD & OUTBOARD OF PYLON UPPER SPAR CHORD AT NAC STA 221.9.SDR SWIA200718019Rib · crackedLT IB NACELLE RIB CRACKED BENEATH WING. (DISCOVERED DURING C-CHECK INSPECTION) DOUBLER INSTALLED IAW SRM 120 51-10-02 PG 2 SEC. 2B.SDR SWIA200718017Frame · crackedLT NACELLE FRAME NR 1 CRACKED AT WEBBING. (DISCOVERED DURING C-CHECK INSPECTION) COMPLIED WITH SB 120-54-0036 REV. 02 09 JUN 99 TO LT ENGINE NACELLE FRAME NR 1.SDR SWIA200718012Frame · crackedLEFT NACELLE FRAME CRACKED AT AFT OUTBOARD DOOR AFT HINGE ATTACH POINT FORWARD BOSS, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT NACELLE FRAME AFT DOOR FORWARD HINGE ATTACH POINT IAW SRM 120 51-10-02 PG 2 SEC 2B.SDR KCSA071026Spar · crackedNR 1 PYLON MID SPAR WEB CRACKED BY REAR ENGINE MOUNT, NAC STA 221.9, WL 138.5.SDR UPS07448988Frame · crackedINSPECTION TYPE:C NR 2 PYLON UPPER WING CAVITY O/B FRAME AT NAC STA 237 TOP CORNER AREA CRACKED AS RED MARKED. NR 2 PYLON AT NAC STA 237 O/B FRAME REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND SRM 51-30-02.SDR WRNA200700006Frame · crackedDURING B-CHECK, FOUND NR 1 PYLON FRAME STA 250 CRACKED AT INSIDE BOTTOM AFT PIGEON HOLE. REPAIRED IAW BOEING 747 SRM 54-14-03 FIG 1.SDR SWIA200717832Frame · crackedFOUND LEFT NACELLE FRAME 1 CRACKED AT INBOARD WEB, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW LEFT FRAME NR 1 IAW EMB 120 SRM 51-40-02, SB 120-54-0036 PART II AND RII 54-900-1000.SDR 06FDEA04246Rib · crackedNR 1 ENGINE PYLON UPPER LEADING EDGE NR 8 RIB IS CRACKED. STOPPED DRILLED IAW SRM 54-50-1. REMOVED WEB IAW SRM 51-40-21 WELDING REPAIR IAW MAE T6/650912 INSTALLED WEB IAW 51-40-21.SDR DL76G070545Rib · gougedNR 1 ENGINE I/B CORE COWL AFT RIB IS GOUGED. REPAIRED PER ERA 458864-14 AND SRM 54-45-01 REPAIR 4.SDR DL76G070544Frame · crackedNR 2 ENGINE I/B CORE COWL AFT HAT FRAME IS CRACKED. FAB`D REPAIR DOUBLER PER ERA 458865-14. INSTALLED REPAIR PER SRM 51-40-02 PAGE 2 AND 3 SRM 54-45-01 REPAIR 4 PARA 4G AND 4H.SDR F3LA200600163Rib · failedDURING C-1 CHECK, INSPECTION REPORTED RT PYLON RIB 9 FAILED HEAT TREATMENT TEST. READINGS BELOW 200. ACCOMPLISHED MODIFICATION (INSTALLATION OF RIB REINFORCEMENT KIT) PER EA A9-54R-11704.SDR QXEA200603471Frame · chafedC3 PDX - LEFT ENGINE LOWER FAN COWL TORQUE BOX FRAME IS CHAFED AT 9:00 O'CLOCK POSITION. REPAIRED IAW SRM 51-12-00 AND REO670-54-21-735.SDR QXEA200603468Frame · chafedC3 PDX - LEFT ENGINE UPPER FAN COWL TORQUE BOX FRAME IS CHAFED AT 9:00 O'CLOCK POSITION. REPAIRED IAW SRM 51-12-00 AND REO670-54-21-735.SDR QXEA200603467Frame · chafedC3 PDX - LEFT ENGINE UPPER FAN COWL TORQUE BOX FRAME HAS CHAFE AT 11:00 O'CLOCK POSITION. REPAIRED IAW SRM 51-12-00 AND REO670-78-34-378.SDR QXEA200603474Frame · gougedC2 PDX - NACELLE FORWARD FRAME ASSEMBLY GOUGED/GALLED NEAR LOWER COWL ATTACH POINT, LEFT SIDE, NR 1 ENGINE. REPAIRED IAW SRM 51-14-00 AND RD8/4-54-388.SDR KCSA061525Frame · wornNR 2 PYLON FWD OB FRAME WORN THROUGH FROM BOTTOM AT NAC STA 190.SDR KCSA061480Frame · crackedNR 3 PYLON O/B FRAME CRACKED NAC STA 269, NAC WL 176.SDR DL76S060873Spar · crackedTHE NUMBER 1 PYLON UPPER SPAR FITTING, RHS AT ATTACH FITTING HOLE SHOWED A CRACK INDICATION. THE SUBJECT HOLE WAS OVERSIZED, AND THE BOEING APPROVED REPAIR INVOLVED INSTALLATION OF A STRAIGHT SHANK FREEZE PLUG PER ERA 456634-14.SDR DL76S060870Spar · damagedDURING ACCOMPLISHMENT OF EO 01-074906-03 THE NUMBER 2 PYLON SPLICE PLATE UPPER OUTBOARD HOLE WAS FOUND TO ALREADY BE OVERSIZED TO BEYOND MAX EO LIMIT. THE BOEING APPROVED REPAIR INVOLVED INSTALLATION OF AN OVERSIZED FASTENER PER ERA 456537-14.SDR 9SBA00706Frame · corrodedCORROSION FOUND ON LT NACELLE HOOP FRAME (ANGLE FIREWALL) REMOVED AND REPLACE HOOP FRAME IAW AC 43.13-1B PARA 4.23 AND 4-6.SDR S9BA00406Angle · corrodedRIGHT HAD ENGINE NACELLE HOOP (ANGLE FIREWALL) FRAME HAS CORROSION. REMOVED AND REPLACED HOOP FRAME.SDR HALA0600822Frame · crackedNR 1 ENG PYLON AFT SECTION OB LOWER FRAME IS CRACKED. REMOVED CRACKED FRAME FROM NR 1 PYLON AFT SECTION. DRILLED EXTENSION IAW SRM 51-40-02. ALODINED AND PRIMED EXTENSION IAW SRM 51-24-04 AND 51-20-00. INSTALLED OB LOWER CORD ON NR 1 PYLON AFT SECTION IAW SDR KCSA061550Frame · crackedNR 2 PYLON INTERNAL FRAME IS CRACKED AT NAC STA 190, OUTBOARD SIDE.SDR SWIA200617286Frame · crackedRIGHT INBOARD NACELLE FRAME CRACKED BENEATH WING B-BRACKET, DISCOVERED DURING C-CHECK INSPECTION. APPLIED DOUBLER AT RIGHT INBOARD NACELLE FRAME IAW SRM 120 51-10-02, PG 2 SEC 2B.SDR SWIA200617282Frame · crackedRIGHT OUTBOARD NACELLE FRAME CRACKED, BENEATH WING B-BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER ON RIGHT OUTBOARD NACELLE FRAME HYDRAULIC LINE STANDOFF (B-BRACKET) IAW EMB 120 SRM 51-10-02 PG 2 SECT 2B.
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