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 FDEA201007052349Rib · crackedNR 1 ENGINE INLET COWL INNER SUPPORT BRACKETS ARE CRACKED AT 6 OCLOCK POSITION CUT OUT DAMAGED AREA. FABRICATED FRAME SECTION USING 2024T-3 .063 DIMS 6 5/8" X 2 1/4" AND STRAP REPAIR USING 2024T-3 .071 DIMS 13 1/4" X 1 1/4" AND INSTALLED ALL REPAIR PARTS IAWSDR IPXA10561446Frame · damagedINSPECTION TYPE:C2, NR 2 PYLON, STA 205 UNDER PANEL 445AR RT FWD FRAME CHORD HAS OVERSIZED HOLES FROM WORKING FASTENERS, NO EDGE DISTANCE. R & R CHORD IAW SRM 51-40-05-OG AND SRM 51-40-02.SDR IPXA0561364Frame · crackedINSPECTION TYPE:C2, NR 2 PYLON UPPER FRAME IS CRACKED ON LT FWD LOWER SIDE AT NAC STA 159 UNDER PANEL NR 442AL. REMOVED, FABRICATED REPLACEMENT, AND INSTALLED FRAME SRM 51-40-02-0G.SDR IPXA10561258Frame · gougedINSPECTION TYPE:C2, NR 2 PYLON UPPER FRAME OTBD SIDE IS GOUGED AT NAC STA 137 UNDER PANEL NR 441AT. R & R SPLICE PLATE IAW SRM 51-40-02-0G.SDR DALA1019980662Frame · damagedAFTER SKIN REMOVAL ON NR2 PYLON OTBD SIDE RT FOUND 1 EA OVERSIZE HOLE FWD FRAME LWR HOLE AT STA 108. COMPLIED WITH ER/A 483519-14 REV ORIG AT SAA. DURING HMV ON N/R CARD 169569.SDR USAA2010062591286Spar · crackedSAL - S4 - MAJOR REPAIR - CRACK ON INBOARD SIDE OF SPAR ON RIGHT WING UPPER FORWARD PYLON AT RIB NR 7. REPLACED INBOARD SIDE OF SPAR ON RIGHT WING UPPER FORWARD PYLON AT RIB NR 7 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D54630485.SDR FDEA201006182061Frame · corrodedNR 2 ENG STRUT FAIRING PANEL 443AR FRAME HAS CORROSION. COMPLIED WITH EA F-5450-141157 PART 1, STEPS 1-7. A MINOR REPAIR.SDR USAA2010062591285Spar · crackedSAL - S4 - MAJOR REPAIR - CRACK ON INBOARD SIDE OF SPAR ON LEFT WING UPPER FORWARD PYLON AT RIB NR 7. REPLACED INBOARD SIDE OF SPAR ON LEFT WING UPPER FORWARD PYLON AT RIB NR 7 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D54630485.SDR FDEA201006121971Rib · damagedUPON REMOVAL OF AFT MOUNT NR 1 PYLON FOUND FWD OTBD FASTENER TO BE DAMAGED. REPAIRED AFT MOUNT NR 1 PYLON IAW EA 6-5450-135200 BY THE FOLLOWING REPAIR INSTRUCTION. R & R TAPERED SHIM BY NEW ONE AND BY TECHNICAL DISPOSITION REF 70534938/007/2010 ISSUE B DATSDR ABXA201006110091Frame · crackedCUT OUT LOWER FRAME IS CRACKED AT FWD END UNDER PANEL 437 ELX. REPLACED FRAME UNDER PANEL 437 ELX IAW B767 SRM 51-40-02SDR FDEA201006081868Spar · damagedDURING REMOVAL OF NR2 PYLON OTBD SKIN 1EA NUTPLATE HOLE IN LOWER SPAR IN THE PRECOOLER CUTOUT AREA FOUND ELONGATED COMPLIED WITH EA F-5450-139153 "NACELLES/PYLONS - ELONGATED HOLE IN PYLON LOWER SPAR" DATED 05/21/10. CONSIDERED "MAJOR REPAIR" IAW EA MAJOR REPASDR KCSA101072Frame · damagedNR 2 ENGINE PYLON AFT I/B FRAME DAMAGED AT NAC STA 221.9SDR WRLA20100607379Rib · crackedCRACK - FOUND NR 1 PYLON 437 CENTER PANEL INSIDE FWD LT SIDE RIB ANGLE CRACK, NRC U05018 ISSUED.SDR ABXA201006070092Frame · crackedCUTOUT FRAME IS CRACKED AT FWD END UNDER PANEL 437 ERX. REPLACED FRAME UNDER PANEL 437 ERX IAW B767 SRM 51-40-2.SDR AALA20100513TUL02Shim · migratedRIGHT ENGINE PYLON FORWARD OUTBOARD LOWER MID SPAR SHIM MIGRATED. REPAIRED IAW AARD 54-50-07-1.SDR DL76L101202Spar · crackedNR1 SPAR WEB REPLACED IAW VA 73089AD AND DWG 311T3130 FOR SB 767-54-0080 AND EA 01-074916-3AD.SDR SWIA201024365Rib · crackedRIB UNDER LEFT EXHAUST AFT INBOARD MOUNT CRACKED. (C CHECK) REPAIRED PER EMB APPROVED REPAIR AND SRM.SDR IPXA10M60134Rib · chafedINSPECTION TYPE:2C, NR3 ENGINE PYLON AT AFT LOWER FAIRING V-RIB IS DAMAGED AT INBD FASTENER HOLE. REMOVED FABRICATED AND INSTALLED REPLACEMENT V-RIB REF DAC DWG AUB7536 AND SRM 51-31-01.SDR KCSA101053Frame · damagedNR 2 PYLON FWD I/B FRAME DAMAGED AT NAC STA 221.9.SDR KCSA101052Frame · damagedNR 3 PYLON O/B FRAME DAMAGED AT NAC STA 221.9.SDR KCSA101050Frame · damagedNR 3 PYLON FWD I/B FRAME, NAC STA 221.9 DAMAGED.SDR AALA20100503TUL10Frame · crackedNUMBER 1 PYLON MID FRAME BULKHEAD INBOARD LOWER FORWARD ATTACH TO LOWER SPAR HAD SHIM MIGRATION. INSTALLED NEW SHIM. ALSO EDDY CURRENT INSPECTION SHOWED CRACK INDICATION AT INBOARD FORWARD LOWER HOLE. REAMED FORWARD OUTBOARD HOLE TO .498 NO CRACK INDICATED.SDR KCSA101033Frame · damagedNR 3 PYLON O/B FRAME AT NAC STA 221 DAMAGED.SDR KCSA101032Frame · damagedNR 2 PYLON FWD O/B FRAME AT NAC STA 221 DAMAGED.SDR KCSA101031Frame · crackedNR 1 PYLON I/B BULKHEAD FRAME AT NAC 221 CRACKED .5 INCH.SDR UALA2010042201342Spar · crackedNR 1 PYLON UPPER SPAR WEB LOWER SURFACE CLOSE- OUT TEE FITTING PN 311T3157-1 AT MID-SPAR FITTING NAC STA 237 HAS 1.5 INCH CRACK VERIFIED BY NDT. HFEC VERIFIED STOP DRILL, ROTO PROBE INSP BOLT HOLES REF NDT PT6. INSTALLED REPAIR SPLICE AND FILLER REF EA AND MASDR AALA20100420TUL07Frame · crackedNUMBER 4 FRAME CRACKED 2 PLACES. STOP DRILLED CRACKS AND INSTALLED FILLER AND STRAP PER AARD54-52-01-1.SDR KCSA101020Frame · crackedA 7 INCH CRACK IN NR 4 PYLON O/B FRAME AT NAC STA 236 AND STR 4R.SDR KCSA101019Frame · crackedA .5 INCH CRACK IN NR 3 PYLON NAC STA 225 FRAME AT STR 3R.SDR ABXA201004200065Frame · crackedNR 1 STRUT PANEL 437BL CUTOUT LOWER FRAME IS CRACKED AT FWD END. REMOVED AND REPLACED NR 1 STRUT LOWER FRAME OUTBOARD IN HYD ACCESS BAY IAW B767 SRM 51-40-02.SDR USAA2010041590800Rib · chafedPHX - C6 - MAJOR REPAIR - NR 2 PYLON, NR 7 RIB IS DAMAGED AT CLAMP ATTACHMENT. REPLACED NR 2 PYLON NR 7 RIB IAW SRM 51-42-11.SDR KCSA101018Spar · crackedA 1.5 INCH CRACK IN NR 4 PYLON LOWER SPAR WEB, 5 INCHES I/B OF PYLON CENTER LINE, NAC STA 195.SDR KCSA101017Spar · crackedA 1.5 INCH CRACK IN NR 4 PYLON LOWER SPAR WEB, 3 INCHES I/B OF PYLON CENTER LINE, NAC STA 195.SDR ABXA201004130054Frame · crackedNR 1 STRUT PANEL 437BR CUTOUT LOWER FRAME IS CRACKED AT FWD END. REMOVED AND REPLACED FRAME IAW B767 SRM 51-40-02.SDR DALA1011890661Spar · damagedNR 1 PYLON FWD UPPER SPAR CHORD, N STA 138, LT SIDE FOUND EXTRA HOLES IN WEB NOT SHOWN IN DWG 313N3100, SHT 5, ZONE 4D. ACCOMPLISHED ER/A 481534-14 REV ORIGINAL, REF NON ROUTINE 160616 (DL757101365).SDR SWIA201024112Frame · crackedRIGHT ENGINE FRAME OUTBOARD SIDE CRACKED. (C CHECK) REPLACED RIGHT ENGINE FRAME PER SRM.SDR AALA20100317AFW01Bushing · damagedRIGHT PYLON ONLY THE INBOARD MOST AND OUTBOARD MOST MIDSPAR BUSHINGS WERE FOUND TO MOVE BY USING LIGHT PRESSURE. ACCOMPLISHED BORE/FASTENER HOLE REWORK PER EA B767-54-009486.SDR EE4Y1003026Rib · crackedDURING INSPECTION NR 2 ENGINE PYLON T/E STRUCTURE AT STA Y 900 O/B RIB UPPER SECTION CRACKED.SDR EE4Y1003016Support · crackedDURING INSPECTION NR 2 ENGINE PYLON AT STA 817 CLOSING RIB HOSES SUPPORT CRACKED.SDR DHLA201000042Frame · wornNR3 ENG LT T/R FIXED STRUCTURE FRAME WORN STA YN 203.000 AT 7 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW FORM 8110-3, DATED 04-16-10, EVA D878-00307 REV IR DATED 03-30-10. REMOVED FASTENERS IAW SRM 51-1-221, SRM 51-3-0. CUT OUT DAMAGED AREA AND FABRICATED NEW FRSDR DHLA201000041Frame · wornNR3 ENG T/R FIXED STRUCTURE FRAME WORN STA YN 203.000 AT 5 O'CLOCK POS. RT PERFORMED MAJOR REPAIR IAW FORM 8110-3, DATED 04-16-10, EVA D878-00308 REV IR DATED 03-31-10. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED AREA AND FABRICATED NEW FRAMSDR Q2S2010F00033Frame · crackedWS NR 0924, WC-SAI EAO NR 4754020R1. NR 4 PLYON INBD REAR EANGINE MOUNT BULKHEAD INBD LOWER CHORD FWD CRACKED. REPAIR CARRIED OUT IAW EN:1014-10, FORM 8100-9, DATED 19 MARCH 2009 ISSUED FOR THE REPAIRED.SDR FDEA201003010575Spar · damagedNR 1 PYLON UPPER SPAR WEB AT THE AFT BULKHEAD; AFT ROW OF FASTENERS; 1 IS BROKEN AND 11 ARE LOOSE. COMPLIED WITH EA 8-5450-136627.SDR FDEA201003010571Spar · damagedNR 3 PYLON UPPER SPAR WEB AT THE AFT BULKHEAD; THE AFT ROW OF FASTENERS; 12 EA IS LOOSE. COMPLIED WITH EA 8-5450-136627.SDR DL757100810Spar · mismanufacturedNR 1 PYLON LT SIDE FWD UPPER SPAR CHORD AT STA 138 HAS 3 ADDITIONAL FASTENERS INSTALLED NOT IAW DWG IN COMING CONDITION. C/W ER/A 480026-14 REV ORIGINAL AT SAA DURING HMV ON N/R CARD 159257.SDR 22AA201000061Rib · crackedDURING "C" CHECK, NR 2 ENGINE RT CORE COWL AFT RIB LOWER SIDE FOUND WITH CRACK. NON-ROUTINE NR 0297, CRACK AREA AT NR 2 ENGINE RT CORE COWL AFT RIB LOWER SIDE AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.SDR 22AA201000060Rib · crackedDURING "C" CHECK, NR 2 ENGINE LT CORE COWL AFT RIB LOWER SIDE FOUND WITH CRACK. NON-ROUTINE NR 0296, CRACK AREA AT NR 2 ENGINE LT CORE COWL AFT RIB LOWER SIDE AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.SDR 22AA201000058Rib · wornDURING "C" CHECK, NR 2 ENG RT CORE COWL AFT MOST RIB FOUND WITH WEAR MARK. NON-ROUTINE NR 0201, WORN AREA AT NR 2 ENGINE RT CORE COWL AFT MOST RIB AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.SDR 22AA201000054Rib · wornDURING "C" CHECK, NR 2 ENGINE LT CORE COWL AFT MOST RIB FOUND WITH WEAR MARK. NON-ROUTINE NR 0195, WORN AREA AT NR 2 ENGINE LT CORE COWL AFT MOST RIB AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.SDR DL76L100674Spar · crackedNR1 PYLON MID SPAR CRACKED AT INBD MID SPAR FITTING OTBD ROW NR2 FASTENER HOLE (COUNT FRON REAR) RUNNING AFT OTBD APPROX .4375" IN LENGTH. REPAIRED IAW ERA 479969-14AD REV 0.
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