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 6001LENGAttach Angle · corrodedENGINE NACELLE ATTACHING FITTING ANGLE REMOVED FOR CORROSION. PARTS ARE CADMIUM PLATED, BUT NOT PAINTED. ALSO DISCOVERY IMPROPER DRILL HOLES AND RIVET SET DAMAGE AROUND SEVERAL HOLES.SDR HALA0800375Attach Bracket · gougedAT 2 ENG NOSE INLET COWL TO FAN CASE ATTACHMENT BRACKETS AT 7 O'CLOCK POSITION GOUGED. DAMAGE ON NOSE COWL AFT BULKHEAD INNER RING, 7 O'CLOCK POSITION BLENDED IAW SRM 54-11-02/1A01, FIG 101, DETAIL 111, WITHIN SRM LIMITS.SDR HALA0800374Attach Bracket · gougedNR 2 ENGINE NOSE INLET COWL TO FAN CASE ATTACHMENT BRACKETS AT 5 O'CLOCK POSITION GOUGED. DAMAGE AT 5 O'CLOCK POSITION ON NOSE COWL AFT BULKHEAD INNER RING BLENDED IAW SRM 54-11-02/1A01, FIGURE 101, DETAIL 111, WITHIN SRM LIMITS.SDR 08FDEA00664Attach Angle · crackedPYLON NR 1 LEFT SIDE, FWD ATTACH ANGLE FOR PANEL 413 CL IS CRACKED. REMOVED AND REPLACED BRACKET PER A310-300 SRM 51-40-21, PG 7.SDR TRAX200800355Attach Angle · crackedRT PYLON INBD ATTACH ANGLE CRACKED FS 1108.0. C/W REPAIR ON RT PYLON INBOARD ATTACH ANGLE AT FS 1108.0.SDR DHL2008753509Attach Angle · cracked"C" CHECK 1 ENG PYLON OB UPPER ATTACH ANGLE CRACKED AT SECOND HOLE, VERIFIED BY NDT. REMOVED DAMAGED ANGLE AT NR 1 ENGINE (PYLON) OB UPPER IAW B727 SRM 51-30-2. LOCATED HOLE, DRILLED AND DEBURRED ANGLE WITH P/N 69-16977-1 PO NR 738094 IAW B727 SRM 51-30-5 ANSDR UIEA200800031Fitting · chafedDURING SCHEDULED MAINTENANCE, FOUND NR 4 PYLON WEAR DAMAGE ON THE LUG FACE OF THE UNDERWING MIDSPAR FITTINGS. THE DAMAGE WAS REMOVED FROM THE LUG SURFACES BY BLENDING SMOOTH. THE FITTINGS WERE CONFIRMED FREE OF CRACKS AND OTHER DAMAGE BY DETAIL VISUAL AND NDSDR UIEA200800030Lug · chafedDURING SCHEDULED MAINTENANCE FOUND NR 1 PYLON WEAR DAMAGE ON THE LUG FACE OF THE UNDERWING MIDSPAR FITTINGS. THE DAMAGE WAS REMOVED FROM THE LUG SURFACES BY BLENDING SMOOTH. THE FITTINGS WERE CONFIRMED FREE OF CRACKS AND OTHER DAMAGE BY DETAIL VISUAL AND NDTSDR G60A200800027Attach Angle · crackedLT PYLON UPPER OUTBOARD SIDE STA YN214 ATTACH ANGLE CRACKED.SDR 08FDEA00363Fitting · corrodedAFTER INSP FOR FINAL REAM FOUND NR 2 PYLON MID BULKHEAD FWD AND AFT LUG HOLES FOR SLEEVE BOLTS ACTUALLY REAMED TO .772", FOUND CORROSION ON EO NR F-5450-7-5005 PE STEP 10. HFEC INSPECTION FWD AND AFT SLEEVE BOLT HOLES IN THE NR 2 PYLON MID BULKHEAD FITTING PESDR 2007UALA05080Fitting · crackedNR 2 PYLON CROSS TIE FITTING HAS A CRACK ON THE OUTBOARD ATTACH FASTENER LOCATION AT NAC STA 107.7. ACCOMPLISHED MAJOR REPAIR.SDR F3LA200700366Hinge Fitting · corrodedDURING C-5 CHECK, INSPECTION REPORTED NR 2 PYLON T/R COWL FITTINGS AT RIB 1 AND RIB 2 CORRODED. REMOVED AND REPLACED NR 2 PYLON OTBD T/R COWL FITTINGS AT RIBS 1 AND 2 IAW AMM 54-57-17-000-003 AND 54-57-17-420-053.SDR QXEA200801862Attach Fitting · crackedPDX - C4 CHECK - LEFT OUTBOARD FORWARD SPINE COWL CLEAT IS CRACKED AT THE INBOARD BOLT HOLE. REMOVED CRACKED CLIP AND INSTALLED FABRICATED CLIP IAW RD AND SRM.SDR KCSA071523Attach Angle · crackedNR 4 PYLON STA - 221 UPPER ATTACH ANGLE ON I/B SIDE IS CRACKED .5 INCH LONG.SDR QXEA200701703Attach Fitting · crackedC2 PDX - LEFT ENGINE NACELLE INBOARD FORWARD SPINE COWL CLIP HAS A CRACK. REPAIRED IAW RD8/4-71-032.SDR NWAA073679855Attach Angle · crackedDURING "H" CHECK, FOUND CRACK IN LOWER PYLON ATTACH ANGLE AT BS 1167. REPAIRED PER EA 98-210188.SDR ABXA070407Attach Angle · crackedLOWER PYLON LEADING EDGE ATTACH ANGLE CRACKED. REMOVED AND REPLACED FORWARD SECTION OF PYLON LOWER ATTACH ANGLE IN ACCORDANCE WITH DC9 SRM 54-04.SDR 07FDEA04406Fitting · chafedFOUND CHAFING MARKS AT PYLON TO WING FITTING RIB 18, PYLON NR 2 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR UIEA200700450Brace · looseNR 1 PYLON DIAGONAL BRACE UNDERWING FITTING TENSION FASTENER HEAD SHEARED. REMOVED AND INSTALLED FASTENER AS PER 51-30-02.SDR UIEA200700443Brace · chafedNR 4 STRUT DIAGONAL BRACE FORWARD END CHAFED. CHAFING AREA DAMAGE BLENDED AS PER BOEING MESSAGE 1-636565614-4.SDR 07FDEA04249Panel · wornWEARED HOLES IN LATERAL PANELS (INBOARD AND OUTBOARD), RIB 8 UPPER SPAR OF PYLON NR 2 RT. REPAIR PERFORMED BY INSTALLATION OF BUTTERFLY DOUBLERS ON BOTH PANELS IAW SRM 54-51-31/CONFIG 2/PB201.SDR 07FDEA04035Panel · dentedDURING ACCOMPLISHMENT OF EO 6-5450-7-3304 (SB 54-2026 EMBODIMENT) FOUND AT PYLON NR 2 AN OLD CRACK REPAIR AND LOWER SKIN WAVINESS. REPAIR PERFORMED BY STRAIGHTEN OUT THE DENTED AREA AND INSTALLING REPAIR PARTS AND DOUBLER IAW DRAWING R546-10305, APPROVED BY ESDR FDKA200709500Bracket · crackedPRECOOLER MOUNT BRACKET CRACKED ON THE NR 2 ENGINE. REMOVED AND REPLACED MOUNT BRACKET.SDR 07FDEA03893Fitting · damagedFOUND IMPACT DAMAGE ON PYLON THRUST AND SIDE LOAD FITTING, LT WING REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5720-114892 AND RAS/BAE/1005535/2007 ISS A.SDR 07FDEA03892Fitting · damagedFOUND IMPACT DAMAGE ON PYLON THRUST AND SIDE LOAD FITTING, RT WING REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5720-114892 AND RAS/BAE/1005535/2007 ISS A.SDR DL757071212Support Fitting · migratedBUSHINGS MIGRATED IN NR 1 PYLON WING AND STRUT SUPPORT FITTINGS FOR UPPER LINK. BUSHINGS REPLACED PER EA 06-075079-03 AND ERA 464036-14.SDR 07FDEA03763Fitting · corrodedCORROSION ON THE WHOLE LOWER SURFACE OF THE LT PYLON PYRAMID, FWD PYLON TO ENGINE ATTACH FITTING. REPAIR PERFORMED AS PER SRM 54-51-81 BY BLENDING OUT CORROSION, REPROTECTION BY CADMIUM PLATING AND HIGH TEMPERATURE PAINT IAW EA 6-5451-92174 AND RAS 039464/014SDR 07FDEA03755Fitting · gougedGOUGE AT AFT PYLON TO ENGINE FITTING, RT PYLON. REPAIR PERFORMED BY SMOOTH BLEND OUT TO ELIMINATE SHARP EDGES AND REPROTECTION AS PER SRM WITH CADMIUM PLATING AND HIGH TEMPERATURE PAINT IAW EA 6-5451-92173 AND RAS 039403/010/2005.SDR 07FDEA03672Panel · corrodedFOUND CRACK ON PYLON NR 2 AT RIB 8 INBOARD AND OUTBOARD SIDE AT PANEL (ABOUT 8MM) DOUBLER REPAIR ON SIDEWALL PANELS PERFORMED IAW SRM 5451-31 FIG 201.SDR 07FDEA03671Attach Fitting · chafedFOUND CHAFING MARKS, ENLARGED HOLES AND NOT CORRECT INSTALLED BUSHINGS AT PYLON NR 2 PYLON TO WING ATTACH FITTING LUGS AT RIB 12. REPAIR PERFORMED BY OVERSIZING THE BORES AND INSTALLING NEW REPAIR BUSHS IAW DRAWING R571-40283, APPROVED BY EA 6-5450-81064 AND SDR ABXA070312Attach Angle · crackedLEFT PYLON LOWER ATTACH ANGLE WAS CRACKED FS 990. REPAIRED LOWER PYLON ATTACH ANGLE IAW DC9 SRM.SDR CALA0700479Fitting · corrodedINSPECTION FOUND NR 2 ENGINE LT MIDSPAR ATTACH FITTING CORRODED. REPAIRED IAW ECRA 5410-01629.SDR CALA0700478Fitting · corrodedINSPECTION FOUND NR 2 ENGINE RT MIDSPAR ATTACH FITTING CORRODED. REPAIRED IAW ECRA 5410-01629.SDR 07FDEA02841Fitting · corrodedPYLON NR 1 LOWER FITTING WITH CORROSION IN BEARING HOLE REPAIR PERFORMED BY SB A300-54-6018, APPROVED BY EA 6-5451-106504SDR 07FDEA02840Fitting · corrodedPYLON NR 2 LOWER FITTING CORROSION IN BEARING HOLE REPAIR PERFORMED BY SB A300-54-6018, APPROVED BY EA 6-5451-106505.SDR 07FDEA02837Fitting · damagedPYLON NR 1 FWD PYLON-WING ATTACH FITTING LUG WITH LITTLE WAVE DAMAGE REPAIR PERFORMED BY BLEND OUT IAW SRM 51-74-10, APPROVED BY EA 6-5451-106518 AND RAS /BAE/1005084/2007 ISS A.SDR CWQR200709Mount · crackedDURING AN INSPECTION FOUND THE ENGINE NACELLE ATTACH FLANGE EARS CRACKED IN (2) LOCATIONS. SENT TO MFG FOR EVALUATION AND REPAIR. SUBMITTED SCR TO MFG UNDER NR 308174.SDR 07FDEA02767Mount · corrodedENG NR 3: AFTER ENGINE REMOVAL FOUND PYLON FWD MOUNT LT MOUNT LT AFT BORE HOLE, SUSPECT PITTING CORROSION. [08-20-07] REPAIR CARRIED OUT AT ENG NR 3 PYLON FWD MOUNT LH AFT BORE HOLE AS PER FEDEX EA 1-5410-112377, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-SDR DL757071004Attach Fitting · misalignedINSTALLATION OF NEW NR 1 AND NR 2 PYLON WING ATTACH TENSION CLIPS WOULD HAVE REQUIRED SPOTFACE GREATER THAN THE 0.005" ALLOWABLE PER EO 6-070332-03 WHICH PERTAINED TO S/B 757-54-0034 REV 1 FOR THE SIP MODIFICATION. TAPERED RADIUS FILLERS WERE FABRICATED AND ISDR DL757071003Attach Fitting · misalignedNUMBER 2 PYLON SIDE LINK ATTACH FITTING HOLE NR 3 WAS FOUND MISALIGNED WHILE ACCOMPLISHING DELTAS EO 6-70332-3 COVERING SB 757-54-0034. A TAPERED RADIUS FILLER WAS INSTALLED PER ANAMOC TO AD 2003-18-05.SDR 2007UALA02729Structure · corrodedCORROSION FOUND ON NR 4 PYLON DSB OUTBOARD WING FITTING, 4 EACH ECCENTRIC BUSHINGS AROUND SURFACE, & 4 EACH DSB BEARINGS. [08-14-07] CORROSION FOUND ON NR 4 PYLON DUAL SIDE BRACE OTBD WING FTNG, 4 EACH ECCENTRIC BUSHINGS AROUND SURFACE, & 4 EACH DSB BEARINSDR DL76S070828Fitting · crackedDURING INSPECTION PER SIP EO MOD, NR 1 PYLON BULKHEAD FITTING WAS FOUND CRACKED AT BOLT HOLE COMMON TO UPPER SPAR FITTING. THE DISCREPANT HOLE ON BULKHEAD FITTING WAS OVERSIZED TO A FINAL DIAMETER OF 1.125" UNTIL THE CRACK INDICATION WAS REMOVED. BOEING APPRSDR DL76S070777Fitting · damagedDURING INSPECTION OF THE AFT PITCH LOAD FITTING PER EA 01-074906-03AD, SEVERAL HOLES WERE FOUND TO BE OVERSIZED BEYOND THE ALLOWABLE LIMITS. BOEING WAS CONTACTED AND THEY ALLOWED THE OVERSIZED HOLES WITH CORRESPONDING MATCHING FASTENERS AS REFERENCED IN ERA 4SDR 07FDEA02126Fitting · corrodedPYLON NR 2 FWD ENGINE FITTING, CORROSION ON TENSILE BOLT HOLES REPAIR PERFORMED BY REMOVAL OF CORROSION THRU OVERSIZING AND BUSH INSTALLATION IAW EA 6-5442-106473 AND RAS/052121/005/2007 ISS. A.SDR DL76L070563Angle · crackedTHE NR 1 ENGINE PYLON CLOSEOUT ANGLE WAS FOUND CRACKED. THE CLOSEOUT ANGLE WAS REMOVED AND REPLACED.SDR DLM88070513Fitting · corrodedCORROSION FOUND ON THE BORE AND SURROUNDING AREA OF THE EXISTING LOWER HOLE (FRONT FACE) OF THE RT PYLON FRONT SPAR ENGINE MOUNT FITTING, P/N 5935711-2 SATATION 1307.00. TIME LIMITED REPAIR PERFORMED IAW ERA 461312-12REV O. AFFECTED HOLE OF FITTING P/N 59357SDR UIEA200700229Attach Angle · crackedNR 1 PYLON AFT MOUNT BULKHEAD FITTING CAP SKIN ATTACH ANGLE STATION 286 BOTH SIDES CRACKED. THE CHORDS CRACKED FLANGES WERE REMOVED BY TRIMMING PER SRM 51-10-01. ALL FASTENERS HOLES WERE NDT INSPECTED. REPAIR FILLERS AND ANGLES WERE INSTALLED ON FORWARD ANDSDR UIEA200700223Attach Angle · crackedNR 4 PYLON AFT MOUNT BULKHEAD FITTING CAP SKIN ATTACH ANGLE BOTH SIDES FOUND CRACKED. THE CHORD CRACKED FLANGES WERE REMOVED BY TRIMMING PER SRM 51-10-01. THE EDGES AND FASTENER HOLES WERE NDT INSPECTED. FILLERS AND REPAIR ANGLES WERE INSTALLED ON FORWARD ASDR UIEA200700222Attach Angle · crackedNR 3 PYLON AFT MOUNT BULKHEAD FITTING CAP SKIN ATTACH ANGLE BOTH SIDES FOUND CRACKED. THE CHORD CRACKED FLANGES WERE REMOVED BY TRIMMING PER SRM 51-10-01. THE EDGES AND FASTENER HOLES WERE NDT INSPECTED. FILLERS AND REPAIR ANGLES WERE INSTALLED ON FORWARD ASDR UIEA200700221Attach Angle · crackedNR 1 PYLON AFT MOUNT BULKHEAD FITTING CAP SKIN ATTACH ANGLE BOTH SIDES FOUND CRACKED. THE CHORD CRACKED FLANGES WERE REMOVED BY TRIMMING PER SRM 51-10-01. THE EDGES AND FASTENER HOLE WERE NDT INSPECTED. FILLERS AND REPAIR ANGLES WERE INSTALLED ON FORWARD AN
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