JASC 5415
Service difficulty reports · 1,305
Reports filed under 5415 · Nacelle/Pylon, Attach Fittings, 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 = '5415' 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 = '5415' 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 02FDEA00740Fitting · corrodedRT WING PYLON AFT MOUNT FITTING ATTACHMENTS CORRODED. R&R FITTING PER EA 6-5450-66459.SDR SWIA200211426Fitting · crackedFS 718 LT AND RT PYLON FITTING TIE ANGLES CRACKED. FOUND DURING C CHECK INSPECTION. NEW TIE ANGLE FIT AND INSTALLED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21.P/N: 600-36030-31SDR 02FDEA00698Bearing · corrodedRIGHT WING ENGINE PYLON AFT MOUNT FITTING BEARING CORRODED. R&R FITTING PER EA 6-5450-65104.SDR 02FDEA00696Fitting · corrodedCORROSION ON RIGHT WING ENGINE PYLON THRUST AND SIDE LOAD FITTING. R&R FITTING PER EA 6-5450-65103.SDR 02FDEA00642Fitting · corrodedLT PYLON AFT MOUNT FITTING FOUND CORRODED. R&R FITTING PER SB A310-54-2021 ON PYLON STRUCTURE.SDR DL733021065Beam · wornWORN AREAS WERE FOUND IN THE CROWN BEAM LUG BORES ON THE NR 1 AND NR 2 PYLONS. THE WORN AREAS WERE REMOVED BY OVERSIZING THE LUG BORES ON THE NR 1 AND NR 2 PYLON. OVERSIZED BUSHINGS WERE INSTALLED IN THE BORES. THE DAMAGE WAS FOUND AT HMV.SDR SWIA200211333Bracket · crackedFOUND LEFT ENGINE PYLON LEADING EDGE LOWER ATTACH BRACKET CRACKED DURING C CHECK INSPECTION. FITTED AND INSTALLED NEW RIB IAW CRJ SRM 51-40-11, 51-42-06.SDR 2002UALA01334Bracket · bentNR 2 ENGINE CROSS TIE INBOARD LEG UPPER BRACKET IS BENT AND FASTENER CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED UPPER BRACKET FOR CROSS TIE.SDR COMA0260420Pylon · corrodedDURING REMOVAL OF THE LEFT ENIGNE ASSEMBLY, DISCOVERS FRETTING CORROSION ON THE AFT ENGINE PYLON THRUST FITTING MOUNTING RIB 6 TO 2 O'CLOCK POSITION ON FWD SIDE.REPAIRED IN ACCORDANCE WITH 601R-54-50-044.SDR AWXA200200647Angle · crackedMCN - MAJOR REPAIR - DURING C-12 CHECK A 1" CRACK WAS FOUND ON THE #2 PYLON ATTACH ANGLE AT THE FRONT SPAR LOWER CHORD AREA, NACELLE STA 254. MAINTENANCE TRIMMED OUT CRACKED SECTION OF ANGLE, FABRICATED A NEW REPAIR SECTION ANGLE, AND INSTALLED REPAIR IAW AWA SDR 02FDEA00404Fitting · corrodedRT WING PYLON SPIGOT BALL JOINT FOUND WITH BROWN STAIN ALL AROUND THE CIRCUMFERENCE OF FITTING. CLEARED IAW EA 6-5450-59029.SDR COMA0260350Pylon · corrodedDURING REMOVAL OF THE RIGHT ENGINE ASSEMBLY, DISCOVERED FRETTING CORROSION ON THE AFT ENGINE PYLON THRUST FITTING MOUNTING RIB.REPAIRED IN ACCORDANCE WITH REO 601R-54-50-036.SDR AUS20020426Pin · cracked(AUS) NR 1 STRUT, MIDSPAR FUSE PIN CRACKED LONGITUDINALLY INSIDE THE BORE OF THE PIN. CRACK LENGTH APPROXIMATELY 30.48MM (1.2IN). FOUND DURING INSPECTION IAW AD/B767/78.SDR QXEA0200532Truss · damagedSMF- INBOARD AND OUTBOARD AFT DIAGONAL TRUSS SHOWS SIGNS OF HEAT DAMAGE. REPAIRED IAW HORIZON AIR EA 6-54-60.SDR COMA0260187Pylon · corrodedDURING REMOVAL OF THE LEFT ENGINE ASSEMBLY, DISCOVERED FRETTING CORROSION ON THE AFT ENGINE PYLON THRU FITTING MOUNTING RIB W.O. 41725.REPAIRED I/A/W REO 601R-54-50-036.SDR P5CA0200664Bolt · shearedONE BOLT HEAD SHEARED OFF ON RT SIDE OF NR 1 ENGINE AFT MOUNT TO PYLON FITTING. REMOVED AND REPLACED TWO BOLTS ON RT SIDE FOR AFT MOUNT TO FITTING PER MM 54-41-02.SDR DL733020337Attach Fitting · wornA BEARING WAS FOUND MIGRATED FROM THE LUG BORE OF THE AFT FITTING ON THE NR 2 PYLON CROWN BEAM. AFTER REMOVAL OF THE BEARING LIGHT GOUGES WERE FOUND IN THE LUG BORE. THE LUG WAS REAMED TO A LARGER DIAMETER, A STEEL REPAIR BUSHING INSTALLED, AND A NEW BEARINGSDR MWEA020158Stiffener · crackedLEFT ENGINE PYLON AFT VERITCAL STIFFENER IS CRACKED LOCATED BETWEEN UPPER AND LOWER AFT PYLON SPARS. -- FABRICATED AND INSTALLED STIFFENER.SDR MWEA020157Clip · crackedRIGHT PYLON SUPPORT CLIP AT UPPER REAR SPAR CAP IS CRACKED. -- FABRICATED AND INSTALLED CLIP.SDR MWEA020139Clip · crackedRIGHT PYLON SUPPORT CLIP AT LOWER REAR SPAR CAP IS CRACKED. FABRICATED AND INSTALLED CLIP.SDR COMA0260120Pylon · corrodedDURING REMOVAL OF THE RIGHT ENGINE ASSEMBLY, DISCOVERED FRETTING/PITTING CORROSION ON THE AFT ENGINE PYLON THRUST FITTING MOUNTING VIB.REPAIRED IN ACCORDANCE WITH REO 601R-54-50-036.SDR HNAA0200020Fitting · crackedDURING REPAIR OF THE NR 1 NACELLE HORSE COLLAR THE INTERNAL TOP MOUNT FITTING WAS FOUND CRACKED AT THE TOP AFT CORNER FROM THE RADIUS TO THE EDGE OF THE ATTACH FLANGE. THE CRACK ENCIRCLES THE TOP RIVET OF THE AFT ATTACH FLANGE. REMOVED AND REPLACED THE FITTISDR UIEA02003Attach Fitting · scoredDURING CURRENT C-CHECK AT SIAEC WHILE PERFORMING TERMINATING ACTION PER ATLAS AIR EO 4757A082, NR 4 PYLON LOWER WING DIAGONAL BRACE ATTACH FITTING, TAPER LOCATION INSTALLATION ' FOUND THE LAST THREE FASTENER HOLES SCORED. POSITIONS ARE ONE EACH AT INBOARD 2NDSDR P5CA0100619Doubler · torn#2 PYLON INBD SIDE, AFT END, ABOVE AFT MOUNT, HAS A 1" RIP IN DOUBLER. REPAIRED PER SRM 54-12-01 & SRM 51-40-00.SDR COMA0160952Fitting · corrodedDURING REMOVAL OF THE RIGHT ENGINE ASSEMBLY, DISCOVERED PITTING CORROSION ON THE AFT ENGINE PYLON THRUST FITTING MOUNTING RIB. REPAIRED IAW REO 601R-54-50-040.SDR COMA0160854Pylon · corrodedDURING REMOVAL OF THE RIGHT ENGINE ASSEMBLY DISCOVERED CORROSION ON THE AFT ENGINE PYLON THRUST FITTING MOUNTING RIB.REPAIRED I/A/W REO 601R-54-50-032.SDR 0103706642Attach Fitting · frettedDuring "PCK" found fretting corrosion in several areas of number 3 strut aft diagonal brace attach fitting. Repaired per EA 66-186713.SDR QXEA0101680Clip · crackedPDX - LEFT HAND AFT NACELLE AND EXHAUST SHROUD SUPPORT BRACKETS, CLIPS, AND ATTACH POINTS ARE CRACKED AND CHAFED. REPAIRED IAW RD 8/4 54-033, RD 8/4 54-044, RD 8/4 54-019, RD 8/4 54-016, EA 6-54-30, EA 6-54-28, EA 6-54-42, EA 6-54-26, EA 6-54-25.SDR QXEA0101679Bracket · crackedPDX - RIGHT HAND AFT NACELLE DECK AND EXHAUST SHROUD SUPPORT BRACKETS, CLIPS, AND ATTACH POINTS ARE CRACKED AND CHAFED. REPAIRED IAW RD 8/4-54-033, RD 8/54-044, RD 8/54-31, RD 8/54-016, EA 6-54-31, EA 6-54-27, AND EA 6-54-29.SDR COMA0160777Pylon · corrodedDURING REMOVAL OF THE RIGHT ENGINE ASSEMBLY, DISCOVERED PITTING CORROSION ON THE AFT ENGINE PYLON THRUST FITTING MOUNTING RIB.REPAIRED IN ACCORDANCE WITH REO 601R-54-50-026.SDR SWIA200110351Beam · crackedENGINE PYLON BOX BEAM UPPER WEB HAS 2 CRACKS AT LBL 8.0 AND RBL 7.5, RADIATING FWD FROM TRAILING EDGE OF BEAM. CARRY OUT REPAIRS TO LOWER BOX BEAM WEB IAW REO 601R-53-61-345 AND 601R-53-61-368. CARRY OUT REPAIRS TO UPPER BOX BEAM WEB IAW REO 601R-53-61-442. SDR SWIA200110350Beam · crackedENGINE PYLON BOX BEAM LOWER WEB CRACKING FROM ANCHOR NUTS AT STRESS PANEL FS 640 LEFT AND RIGHT SIDES. REPAIRS ACCOMPLISHED IAW REO 601R-53-61-366, LEFT AND RIGHT SIDES OF BOX BEAM. HFEC INSPECTION CARRIED OUT IAW REO 53-61-366. NO CRACKS FOUND.SDR CALA0100892Fitting · tornINSPECTION FOUND #2 PYLON AFT FITTING TORN. THE TORN AREA WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5750-03588.SDR USAA011246Strut · wornPIT - STRUT BEARING BORE REQUIRES RECHAMFERING, MAIN BEARING BORE. MACHINE BORE AND RECHAMFER. (M)SDR AWXA0002254Pin · crackedRIGHT PYLON MIS SPAR O/B FUSE PIN HAS EDDY CURRENT CRACK INDICATION. REMOVED AND REPLACED I/B AND O/B FUSE PINS IAW EO 54-51-03 MM 54-51-02 PG 401-403.SDR QXEA0101348Angle · crackedPDX - CRACK IN ANGLE ATTACHED TO FRAME 2948, ADJACENT TO FIREWALL, AND AT THE TOP OF THE STUB WING. REPAIRED IAW THE F-28 STRUCTURAL REPAIR MANUAL 54-02-02, PAGES 12 AND 13, FIGURE 7.SDR AUS20010714Bolt · corroded(AUS) WING/PYLON BOLTS (3OFF) CORRODED UNDER THE HEAD AND ON THE BOLT SHANK. FOUND DURING INSPECTION IAW ER BA6-54-40-4 REV E.SDR AUS20010712Bolt · corroded(AUS) WING/PYLON BOLT CORRODED UNDER HEAD. FOUND DURING INSPECTION IAWER BA6-54-40-4.SDR UPS01436077Fastener · crackedINSPECTION TYPE:C NR 4 PYLON ATTACH FITTING TAPER LOCK FASTENER FOUND 4EA CRACKED. REF ATTACHED SKETCH. LOCKS REPLACED AS PER EO 747-5740-12227-A.SDR C2XA01BT107Mount · damagedYUL---DURING 2C INSPECTION MAINTENANCE FOUND RT ENGINE LT LOWER NACELLE ATTACHMENT HAS HOLE ELONGATED. RT FORWARD Z-MOUNT REMOVED AND REPLACED IAW ATR42 JIC 54-11-61.SDR MWEA010642Attach Angle · crackedRIGHT HAND PYLON UPPER ATTACH ANGLE IS CRACKED, STATION 980. FABRICATED AND INSTALLED ANGLE AND SPLICE STRAPS.SDR C2XA01TY086Mount · chafedTYS DURING A SCHEDULED INSPECTION THE LEFT ENGINE PYLON FORWARD YOKE MOUNT WAS FOUND CHAFED. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB GST-1365/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR CALA0100308Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 2 ENGINE O/B LOWER PYLON ANGLE AT NAC STA 278. A DOUBLER WAS INSTALLED ON THE ANGLE IAW SRM 51-40-00.SDR 2001UALA00371Beam · crackedNR 2 ENGINE PYLON FAN COWL SUPPORT BEAM NAC STA 102 LT SIDE INNER ANGLE CRACKED AFT SIDE OF WEB NEAR CENTER CHORD. MAJOR REPAIR ACCOMPLISHED.REPLACED ANGLE PER SRM.SDR QXEA0100429Strut · chafedPDX - DURING INSPECTION, FOUND TWO CHAFED AREA''S IN LOWER INBOARD ENGINE NACELLE SUPPORT STRUT. REPAIRED IN ACCORDANCE WITH ENGINEERING APPROVED REPAIR DRAWING RII COMPLIED WITH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR MWEA010368Fitting · corrodedLEFT LOWER PYLON BEAVER TAIL FITTING BOTTOM SURFACE CORRODED. REMOVED DAMAGED FITTING, DRILLED UP NEW FITTING AND INSTALLED.SDR DL757010455Fitting · tool damageNR 1 PYLON / NACELLE ATTACH SUPPORT SIDE LINK FITTING MISDRILLED HOLE AT NR 2 ATTACH HOLE THROUGH SIDE LINK FITTING, WING LOWER SKIN AND WING FRONT SPAR LOWER CHORD.SDR DHL2001701002Support Fitting · crackedDURING A POST-MOD INSPECTION OF PYLON, CRACKS WERE FOUND IN FWD ENGINE SUPPORT FITTING UPPER FLANGE BOLT HOLES E AND F. REPAIRED NR 3 ENGINE PYLON AT BOLT HOLES E AND F, IAW BOEING MESSAGE CPZ-OSC-01-00017H APPROVED AS ALTERNATE MEANS OF COMPLIANCE TO AD 97-0SDR MWEA010148Fitting · crackedFITTING CRACKED AT VERTICAL WEB AT LEFT ENGINE PYLON STRUCTURE, VIEWED THROUGH PANEL 8105A. REMOVED AND REPLACED FITTING.SDR CA010404011Fitting · cracked(CAN) DURING INSPECTION OF NR 2 RT PYLON, THE MIDSPAN FITTING FOUND CRACKED BETWEEN FASTENERS. NR 2 ENGINE REMOVED AS PER WORK CRD 71125-2. NR 2 PYLON REMOVED AS PER WORK CARD 54102-2 FROM AIRCRAFT FOR REPAIR. NR 2 MIDSPAN FITTING RELACED AS PER ENGINEERING VA
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