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 DALA1118630136Spar · crackedNR 1 PYLON MID SPAR FWD WEB FOUND CRACKED DURING ACCOMP OF SB 767-54-0081 REV 1. NR 1 PYLON MID SPAR CRACKED WEB REPAIRED IAW ER/A 488781-14.SDR AALA20110211AFW01Spar · crackedFOUND 1.5 INCH CRACK IN THE LEFT PYLON STRUT FORWARD UPPER SPAR WEB AROUND THE POWER FEEDER CABLE CUTOUT. TRIMMED IT OUT (1.0€ RADIUS) PER BOEING SB 767-54-0090 REV 2 DATED JAN 28, 2010 AND EA B767-54-015200.SDR EIAA2011010Frame · crackedNR 3 PYLON REAR ENGINE MOUNT BULKHEAD HAS ALL 4 FRAMES CRACK DAMAGE BEYOND LIMITS OF S/B 747-54A2202 FIG 12. REPLACED ALL 4 FRAMES PER B747 SRM 51-30-05 PG 6-9 AND 51-30-02 PG 8-9 ITEM 7D AND SB 747-54A2202 FIG 12.SDR UALA2011013100500Frame · crackedFRAME CRACKED AT NAC STA 149.5. ENSURE THE ADJACENT HYD LINE IS SECURE AND SHOWS NO SIGNS OF WEAR IN THE AREA. DETAILED INSP OF ABOVE ITEM ACCOMPLISHED. HYD LINE IS SECURE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED REPAIR DOUBLER ON FWD FRAME, ACCOMPLISHEDSDR UIEA2011012000034Frame · wornWORN NR 4 ENG LT CORE COWL INNER FRAME WORN AT 7:00 POS. (REPAIR IAW 747-400 SRM 54-45-02. REPAIR 1. REV 58)SDR UIEA2011011900033Frame · wornWORN NR 4 ENG LT CORE COWL INNER FRAME WORN AT 7:00 POS. (REPAIR IAW 747-400 SRM 54-45-02. REPAIR 1. REV 58)SDR KCSA111034Frame · crackedNR 2 PYLON NAC STA 221.9 BULKHEAD UPPER AFT FRAME CRACKED, LBL 2.SDR KCSA111033Frame · crackedNR 2 PYLON NAC STA 221.9 BULKHEAD UPPER AFT FRAME CRACKED.SDR KCSA111019Frame · crackedNR 2 PYLON RT FWD FRAME CRACKED .5 INCH ON NAC STA 221 BULKHEAD UPPER SECTION.SDR KCSA111018Frame · crackedNR 2 PYLON LT FWD FRAME CRACKED .5 INCH ON NAC STA 221 BULKHEAD UPPER SECTION.SDR KCSA111017Frame · crackedNR 3 PYLON RT REAR ENGINE MOUNT BULKHEAD FRAME CRACKED .25 INCH AT NAC STA 221, RBL 2.SDR KCSA111016Frame · crackedNR 1 PYLON LT REAR ENGINE MOUNT BULKHEAD UPPER FRAME CRACKED AT NAC STA 221, LBL 2.SDR USAA2011021090680Rib · crackedCWF - S2 - MAJOR REPAIR - CRACK ON NR 2 PYLON INBOARD RIB 8A. REPLACED WEB ON NR 2 PYLON INBOARD RIB 8A IAW A330 SRM 51-42-11 & PMS 01-04-21.SDR USAA2011021090679Rib · crackedCWF - S2 - MAJOR REPAIR - CRACK ON NR 2 PYLON OUTBOARD RIB 8A. REPAIRED WEB ON NR 2 PYLON OUTBOARD RIB 8A IAW A330 SRM 51-42-11 & PMS 01-04-21.SDR IPXA1564234Frame · damagedINSPECTION TYPE:C2, NR 1 ENG NACELLE STRUT AFT FAIRING AREA, NUTPLATE ATTACH ANGLE IS DAMAGED AT SEVERAL NUTPLATE LOCATIONS LOCATED AT FWD SIDE OF CUTOUT FOR PANEL 435AR (MARKED). REMOVED, FABRICATED AND REPLACED NUTPLATE ATTACH ANGLE FRAME CORD. IAW SRM 51-4SDR IPXA1564180Frame · damagedINSPECTION TYPE:C2, NR2 ENG NACELLE STRUT AFT FAIRING AREA 1 EA NUTPLATE HAS ATTACH FASTENERS PULLED THRU. R & R WITH SERVICABLE IAW SRM 51-40-02-0G, SRM 51-40-05-0G.SDR COMA2011010350265Spar · chafedLEFT PYLON FRONT SPAR CHAFED. REPAIRED IAW REO601R-54-50-006 AND REO 601R-54-50-077.SDR COMA2011010350264Spar · chafedRIGHT PYLON FRONT SPAR CHAFED. REPAIRED IAW REO601R-54-50-006 AND REO 601R-54-50-077.SDR DALA1107370175Spar · damagedDURING ACCOMPLISHMENT OF EA01-074965-03, AD OPN 0306 WITH REF SB767-54-0080, FIG 10, FOUND NR 1 STRUT UPPER SPAR WEB, PN 311T4100-55, HAS EXISTING REPAIR DOUBLER INTERFERE WITH NEW STIFFENER 311T3040-11 AND RING DOUBLER 311T3040-13. IN ADDITION FOUND WEB HAS SDR DALA1101860659Frame · misrepairedAFTER GAINING ACCESS FOR EA 06-075079-3 (UPPER STRUT FTG) FOUND FRAME STA 161 FOR FAIRING LOWER OTBD SIDE HOLES FOR DOME NUTS DOUBLE DRILLED. COMPLIED WITH ERA 488005-14 REV ORIGINAL DURING HMV ON NON ROUTINE CARD 183087.SDR DALA1032563357Rib · crackedDURING H-CHECK FOUND NR 2 PYLON AFT LWR FAIRING (LAPF) INTERIOR RT FWD BULKHEAD FIRST RIB FROM FWD FOUND WEB CRACKED AS MARKED. PYLON NR 2 LOWER AFT PYLON FAIRING (LAPF) INTERIOR RT FWD BULKHEAD FIRST RIB FROM FWD WEB CRACK AREA REPAIR CARRIED OUT AS PER PRI SDR DALA1032553357Rib · crackedDURING H-CHECK FOUND NR 1 PYLON/ AFT FAIRING (454AL) LT FWD RIB FOUND LOWER LT CORNER WITH 01EA CRACKS AS MARKED PYLON NR 1 AFT FAIRING (454AL) LT FWD RIB CRACK AREA REPAIR CARRIED OUT AS PER PRI 486995-14 REVISION O.SDR DALA1032160176Spar · crackedNR 2 PYLON I/B SIDE MID SPAR FITTING HOLES COMMON TO STRUT HORZ CHORD FOUND FIVE FASTENER HOLES CRACKED AT WEB AND REPAIR ACCOMPLISHED PER ERA 485491-14AD REV ORIG. (DL76L103081)SDR DALA1032150176Spar · damagedNR 1 PYLON MID SPAR WEB O/B WEB TEN HOLES LARGER THAN SB CALL OUT AND REPAIR ACCOMPLISHED PER ERA 485492-14AD REV ORIG (DL76L103080)SDR SWIA201025588Frame · crackedLEFT ENGINE FRAME NR 1 CRACKED AT OUTBOARD TORSION MOUNT ATTACH POINT. (C-CHECK) REPLACED LEFT ENGINE FRAME NR 1.SDR ZZDA2010540Rib · gougedLEFT LOWER ENGINE COWLING RIB, GOUGED. ACCOMPLISHED ENGINE COWLING RIB ANGLE AND FILLER REPAIR PER B717 SRM 54-20-05 FIG 201 REPAIR 3.SDR AALA20101029AFW02Spar · crackedCRACK WAS FOUND ON LEFT PYLON FORWARD UPPPER SPAR WEB COMMON TO THE INTEGRATED DRIVE GENERATOR POWER FEEDER CABLES PASS THROUGH, THIS AREA IS PRONE TO CRACKING. EXTENDED THE UPPER WEB TRIM LINE, FABRICATED FILLERS, DOUBLERS AND HEAT TREATED ALSO TREATED ALL ASDR KCSA101151Stiffener · gougedNR 3 PYLON UPPER SPAR STIFFENER GOUGED AT NAC STA 202.SDR USAA2010102192338Rib · crackedBFM - MAJOR REPAIR - S2 CHECK - CRACKED RIB FRAME AT FR 7264. REPLACED RIB FRAME AT FR 7264 AW A330 SRM 51-42-11.SDR CA101015012Longeron · damaged2 INDICATING HOLES FOUND AT THE NR 4 QEC LONGERON AT THE OTBD LONGERON AT THE INBD AFT HOLE AND THE INBD LONGERON AT THE INBD AFT HOLE. REPAIRED IAW SUPPLIED ERO.SDR QXEA2010101800642Bolt · corrodedNR2 INBD FITTING UPPER SPAR ATTACHMENT PIN BOLT IS CORRODED. REPLACED BOLT IAW AMM 20-10-01 TABLE 3.SDR AALA20101011AFW01Fitting · damagedABNORMALITIES NOTED ON LEFT PYLON MID SPAR FITTING INBOARD AND OUTBOARD EDGE OF UPPER TANG. PYLON WAS REMOVED AND AREAS WERE POLISHED PER 767-300 SRM CHAPTER 51, HIGH FREQUENCY EDDY CURRENT INSPECTION SHOWED NO CRACKS. AREAS WERE CAD PLATED PER SOPM 20-42-10.SDR DALA1026130177Spar · crackedNR 2 PYLON UPPER SPAR WEB LT AND RT DRAIN AREA CRACKED. REPAIR ACCOMPLISHED IAW ERA 485462-14.SDR DALA1026200177Spar · damagedNR 2 PYLON AFT STRUT MID SPAR FITTING AREA. FASTENER HOLE LARGER THAN SB REQUIREMENT. ACCOMPLISHED IAW ERA 485460-14AD.SDR DALA1026100177Spar · damagedNR 2 STRUT MID SPAR WEB EXISTING FASTENER PATTERN FOUND DEVIATED WITH SB 767-54-0080. ACCOMPLISHED IAW ERA 485461-14AD.SDR KCSA101120Frame · crackedNR 4 PYLON I/B FRAME CRACKED AT NAC STA 221 BULKHEAD.SDR TRBA2010110Frame · crackedDURING HEAVY CHECK, A CRACK WAS FOUND AT LT ENG, NACELLE LOWER COWL FWD FRAME AT STA X=1065. FABRICATED & INSTALLED DOUBLER IAW DWG EO
81958110527.SDR ABXA201008200110Frame · crackedINBOARD PYLON NR 1 BELOW 437 BR FRAME CRACKED. REMOVED STRIKER PLATES AND FRAME. RE-INSTALLED STRIKER PLATES AND NEW FRAME PER SRM 51-40-02.SDR AALA20100823AFW01Doubler · crackedNUMBER 1 PYLON FORWARD UPPER SPAR WEB REPAIR DOUBLER CRACKED. ACCOMPLISHED REPAIRED PER EA B767-54-011251.SDR VGQY2010081000076Frame · crackedNR 3 PYLON INTERIOR AFT SIDE UPPER AFT ENGINE MOUNT BULKHEAD FRAME ATTACHING CHORD FOUND CRACK MARKS AT NAC STA 286 (NEXT TO I-BEAM). NDT METHOD OF EDDY CURRENT INSP REQ'D TO VERIFY AND LOCATE SUBJECT CRACK MARKS FOR STRUCTURE REPAIR. COMPLIED WITH EN 1188-1SDR VGQY2010081000066Frame · crackedNR 4 PYLON INTERIOR - DET FOUND CRACKS ON BOTH I/B AND O/B SIDE OF AFT MOUNT BULKHEAD FWD AREA UPPER CHORD AT NAC STA 270. COMPLIED WITH EN 1185-10.SDR FDEA201008062863Spar · damagedNR 3 PYLON UPPER SPAR AT THE AFT BULKHEAD HAS (4 EA) BOLTS SPINNING (NR 5,6,7 & 9) GOING INBD TO OTBD. R & R 1 EA FASTENER AT ACCESSIBLE LOCATION IAW DWG AUB 7025, REV "AZ". R & R NUTS AT 3 EA TRAPPED FASTENERS IAW EA 8-5450-136697.SDR FDEA201007292722Rib · damagedDURING EO 6-5450-7-5003A P2 COMPLIANCE A .375" CRACK WAS FOUND PROPAGATING FROM A SCREW HOLE AT RIB NR 8 ON THE OTBD SIDE OF THE NR 2 PYLON. REPAIRED SRM 54-51-31 AND EO 6-5450-7-5003A P2 INSTRUCTIONS.SDR WGFY2010FA0751011Former · crackedPYLON NR 1 INTERNAL NS 270.00 UPPER RT SIDE FORMER CRACKED.SDR WGFY2010FA0751010Former · crackedPYLON NR 1INTERNAL NS 270.00 UPPER LT SIDE FORMER CRACKED.SDR WGFY2010FA0751009Former · crackedSTRUT NR 4 NAC 270.00 RT SIDE UPPER FORMER WAS CRACK.SDR WGFY2010FA0751008Former · crackedSTRUT NR 4 NS270.00 LT SIDE UPPER FORMER WAS CRACK.SDR QXEA2010072600441Rib · crackedC5 CHECK - RT NACELLE PANEL 424AR SFT END RIB CRACKED. R & R END RIB WITH NEW IAW SRM 51-42-05.SDR IPXA10561435Frame · gougedINSPECTION TYPE:C2, NR 1 ENGINE PYLON: CUTOUT FOR PANEL 435AR FWD EDGE ATTACH FITTING UPPER NUT PLATE IS GOUGING INTO FITTING MATERIAL. REPLACED NR 1 ENGINE PYLON FRAME CHORD (313N5056-5) IAW SRM 50-40-02 AND 51-40-08.SDR IPXA10661192Frame · crackedINSPECTION TYPE:C, NR 1 PYLON INTERNAL LT SIDE BS 285.45 VERTICAL FRAME CRACK NR1 PYLON INTERNAL LT SIDE BS285.45 VERTICAL FRAME REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02.
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