JASC 5420
Service difficulty reports · 3,949
Reports filed under 5420 · Nacelle/Pylon Miscellaneous Structure, 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 = '5420' 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 = '5420' 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 IPXA09555597Fairing · chafedINSPECTION TYPE:C4 NACELLE STRUT AFT FAIRING NR 443FR IS CHAFED ON INNER SURFACE ACCESS PANEL WAS REPLACED IAW SRM 51-40-02.SDR IPXA09555596Swivel · looseINSPECTION TYPE:C4 NR 1 ENGINE LEFT NACELLE STRUT PANEL NR 434AL HOLD OPEN ROD SWIVEL IS LOOSE AND WORN. REMOVED AND REPLACED BASE AND SWIVEL PER SRM 51-40-02.SDR ABXA201004130055Stiffener · crackedSTIFFENER ON OUTBOARD MID INTERNAL PYLON ABOVE PNL 426BR, VIEWED LOOKING THROUGH PNL 442AL LOOKING OUTBOARD BY HYD SUPPORT IS CRACKED AND WORN. REMOVED AND REPLACED STIFFENER IAW B767 SRM 51-40-02 AND 51-10-02.SDR FDEA200904061204Support Bracket · chafedNR 1 ENGINE OUTBD FAN COWL; FORWARD EDGE ALIGNMENT PIN SUPPORT BRACKET IS CHAFED AT THE BOTTOM SURFACE. REMOVED DAMAGE IAW EA 6-7110-127946. FOUND TO BE WITHIN LIMITS IAW EA 6-7110-127946; VIEW A-A. PRIMED IAW SRM 51-23-10.SDR WRLA2009089Web · crackedDURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON NR 1 ENG PYLON INTERNAL WEB CRACK AT STA 300 (REF GET N/R U05024). REPAIRED THIS CRACKED AREA PER MD-11 SRM 57-00-01 VOL 1 FIG 10 REV 40 AND JOB CARD ATTACH SHEET 079586. JOB COMPLETED AND CONDITION CHECK NOSDR WRLA2009088Angle · crackedDURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON NR 3 ENG PYLON INTERNAL ANGLE AT STA 180 (REF GET N/R U05032). REPLACED THE INTERNAL ANGLE PER MD-11 SRM 51-35-01 VOL 2 REV 40. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR FDEA200903261076Web · crackedNR 1 NOSE COWL INTERIOR WEB IS CRACKED, 2 PLACES AT LIGHTNING HOLE, NAC STA 77.5 REMOVED AFT LOWER PANEL AT NR 1 ENG NOSE COWL FOR FOM IAW SRM 51-30-2. CUT OUT DAMAGED AREA IAW SRM 51-10-1. HFEC INSPECTION PERFORMED IAW NDTM 51-00-00 FIG 23, PT 6. NO DEFECTSDR FDEA200903241442Track · corrodedNR 1 PYLON, RIB 18, LUG ATTACHMENT WING TO PYLON WITH CORROSION AT ATTACHMENT ROLLER TRACK OF BEARING. REPAIR ACCOMPLISHED AS PER FEDEX EA 6-5450-127411.SDR IPXA09555297Support Angle · chafedINSPECTION TYPE:C2 ENGINE NR 1 NACELLE STRUT, I/B SIDE FWD LOWER STRUCTURE, NUT PLATE IS DETACHED AND CHAFED INTO THE SUPPORT ANGLE, AT PANEL 435AR ATTACH POINT. REMOVED AND REPLACED CHORD COMMON TO PANEL 435AR IAW SRM 51-40-02-0G AND AMM 51-21-10-7.SDR IPXA09555212Bracket · crackedINSPECTION TYPE:C3 ENGINE NR 2 NACELLE STRUT HAS CRACKED BRACKET, OUTBOARD FWD LWR CORNER JUST UNDER PNL 445AR. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02-06, 51-40-05-06, AND 51-40-06-0G.SDR C2XA09TY049Stiffener · crackedAIRCRAFT CURRENTLY IN A C-CHECK STATUS. INSPECTION FOUND A CRACK IN THE AFT PYLON STIFFENER/STRINGER INSIDE PANEL 414DB. MAINTENANCE REMOVED AND REPLACED THE PYLON STRINGER STIFFENER. ALL WORK WAS ACCOMPLISHED IAW EMB 145 SRM 51-40-02. AIRCRAFT WILL BE RELSDR FDEA200903160930Support Bracket · crackedNR 2 PYLON PNEUMATIC BLEED DUCT, LT SIDE LOWER END, CRACKED SUPPORT BRACKET ATTACHED TO HEAT SHIELD. WELDED CRACKED SUPPORT BRACKET IAW AEROSPATIALE DWG A36115020 AND APA 01-04- 21. REMOVED AND INSTALLED IAW A300-600 AMM 36-11-00-01.SDR IPXA09555024Support Beam · damagedINSPECTION TYPE:C3 UPON REMOVAL, FOUND NR 2 PYLON FAN COWL SUPPORT BEAM O/B RAIL EDGE DAMAGE APPROXIMATELY INCHES FROM AFT END. REPAIRED FAN COWL SUPPORT BEAM O/B RAIL IAW ER 09-1804.SDR IPXA09555023Support Beam · crackedINSPECTION TYPE:C3 NR 2 PYLON FWD RT FAN COWL SUPPORT BEAM O/B RAIL CRACKED 8 INCHES FROM FRONT END. REPAIRED FAN COWL SUPPORT BEAM RAIL IAW ER 09-1804.SDR FDEA200903120912Fitting · corrodedNR 2 PYLON SPIGOT BEARING RECEPTACLE CORRODED REMOVED AND REPLACED NR 2 PYLON SPIGOT FITTING PER EA NR 6-5450-124230.SDR FDEA200903120911Fitting · corrodedNR 1 PYLON SPIGOT RECEPTACLE FITTING HAS CORROSION ON INSIDE THE HOLE. REMOVED AND REPLACED NR 1 PYLON SPIGOT FITTING PER EA NR 6-5450-124229.SDR DL757090338Support Angle · crackedNR 1 PYLON SUPPORT BEAM INBD SUPPORT ANGLE CRACKED AT NACELLE STA 105. REPLACED ANGLE PER SRM 51-70-11 PAGE 1 STEPS 3-7 AND 10-11 ON ATS CARD 00713.SDR DL757090337Support Angle · crackedNR 1 PYLON SUPPORT BEAM OUTBOARD SUPPORT ANGLE CRACKED AT NACELLE STA 105. REPLACED ANGLE PER SRM 51-70-11 PAGE 1 STEPS 3-11 AND 10-11 ON ATS CARD 00714.SDR DU4R2009308Web · corrodedS/O 318002 N/R 35473 DURING SCHEDULED INSPECTION, FOUND NR 2 PYLON LT AFT SIDE WEB HAS NUMEROUS AREAS OF CORROSION ON INNER AND OUTER SURFACES INCLUDING AROUND FASTENER HOLES.SDR IPXA09555008Angle · crackedINSPECTION TYPE:C1 L-ANGLE CRACKED ON OUTBOARD SIDE OF THE NR 2 ENGINE PYLON, NAS 246, COMMON TO THE AFT LOWER CORNER OF PANEL 445AR CUTOUT. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02-06 AND SRM 51-40-05-0G.SDR IPXA09554979Angle · crackedINSPECTION TYPE:C1 L-ANGLE CRACKED RT SIDE NR 2 PYLON NAS 209. REMOVED AND REPLACED ANGLE PER SRM 51-40-02.SDR UIEA200900019Brace · chafedPYLON NR 1 DIAGONAL BRACE IS CHAFED ON OTBD SIDE 11 O'CLOCK POSITION, ZONE 5, 29.5 INCHES FROM FORWARD END. CHAFE IS 2.0 INCH LONG BY 0.125 INCH WIDE. INTERIM REPAIR WAS ACCOMPLISHED AS PER 747-200 SRM 54-41-01, FIG 3 SHEETS 1 THRU 4. REFERENCE ATLAS AIR EOSDR MCC2009F00000Latch · failedACFT ON FINAL APPROACH, WHEN PILOT HEARD A THUD. STATED HE THOUGHT HE HAD HIT A BIRD. UNEVENTFUL LANDING WAS MADE. PILOT DEPARTED AC AND FOUND LT ENGINE TOP COWLING HAD COME OPEN. MX FOUND OUT, BAD LATCHING MECHANISM BROKE. SUSPECT LATCH BROKE AND THE COWSDR UALA2009022300606Structure · crackedNR 2 ENG STRUT FWD TORQUE BOX ZONE 442, UPPER SURFACE AT LWR POINT DRAIN HOLES, LT AND RT HAVE POSSIBLE EDGE CRACKS. MAJOR REPAIR ACCOMPLISHED. STOP DRILLED CRACKS, FABRICATED DOUBLERS AND INSTALLED.SDR UALA2009022300605Structure · damagedNR 2 PYLON DRAIN HOLES REQUIRE REPAIR. MAJOR REPAIR ACCOMPLISHED. STOP DRILLED CRACK, FAB 2 EA DOUBLERS AND INSTALLED.SDR QXEA2009021900134Diaphragm · crackedPDX - C1 - LT NACELLE OUTBOARD DIAPHRAGM AT ST XN 197.810 IS CRACKED. REMOVED CRACKED ANGLE AND DIAPHRAGM, LOCATED AND DRILLED UP NEW ANGLE AND INSTALLED ANGLE AND DIAPHRAGM REF RD 8/4-54-155 ALL EXCEPT ONE FASTENER. INSTALLED REMAINING FASTENER AND PAINTED SDR DL757090215Web · gougedNR 2 PYLON UPPER WEB DAMAGED BEYOND LIMITS PER 5440. REPAIRED PER 51-70-13 FIGURE 1 ON ATS NR 00749. WEB WAS GOUGED.SDR UPS09554767Angle · crackedINSPECTION TYPE:C3 LOWER FWD CORNER OF PANEL 435AR ANGLE IS CRACKED. REMOVED & REPLACED ANGLE IAW SRM 51-40-02.SDR SWIA200921260Riser · corrodedLEFT PYLON PRODUCTION RISER FRETTING CORROSION (C CHECK). REPAIRED PER REO.SDR ASAA0944268Rub Strip · chafedRUBSTRIP MISSING AND STRUCTURE CHAFED AT PANEL 5729 IB AFT LATCH AREA. ACCOMPLISHED RUBSTRIP REPLACEMENT PER ER09 1229.SDR UPS09554434Angle · crackedINSPECTION TYPE:C3 NR 2 ENGINE PYLON OUTBOARD SIDE OF STRUT FOUND CRACKED ANGLE, LOCATED 24 INCHES DOWN FROM LWR WING AND NAC STA 206.00. REPLACED ANGLE PER SRM 51-40-02.SDR UPS09554660Fitting · damagedINSPECTION TYPE:C "04" ITEM, NR 2 PYLON 1EA COMMON TO THE OUTBOARD BATHTUB FITTING AND THE OUTBOARD LOWER CHORD WAS REAMED OVERSIZE (MECH REQ). REAMED UP ELONGATED HOLE COMMON TO BATHTUB FITTING AND O/B LWR CHORD UNTIL TRUE AND ROUND IAW EA 757-5450-27-A1829.SDR ASAA0944198Bushing · migratedRT PYLON DIAGONAL BRACE AFT OB FUSE PIN BUSHING MIGRATED. R&R DIAGONAL BRACE.SDR UPS09554353Bracket · crackedINSPECTION TYPE: C2 THE UPPER AFT SUPPORT ANGLE IS CRACKED ON THE NR 2 ENG LWR FUEL DRAIN LINE 6 O'CLOCK POSITION, PPS200 REMOVED, FABRICATED, LOCATED, DRILLED, AND INSTALLED REPLACEMENT DRAIN LINE BRACKET IAW RR RB211-EM 78-11-04 (RENEW FUEL DRAIN BRACKET ).SDR KCSA091001Stiffener · crackedNR 3 PYLON HAS CRACKED OTBD STIFFENER AT APPROX NAC STA 132.00, JUST AFT OF THE FWD ENGINE MOUNT BULKHEAD.SDR UPS09554332Bracket · crackedINSPECTION TYPE: C2 SUPPORT BRACKET IS CRACKED ON THE NR 2 ENGINE INBD TURBINE COOLING INLET RING, 9 O'CLOCK PPS 156. REMOVED AND REPLACED BRACKET IAW EM 72-52-03-300-003.SDR USAA2009020290256Stiffener · crackedMCN - C12 - MAJOR REPAIR - RIGHT PYLON STIFFENER CRACKED AT PP STA 153.90 AT INBOARD END. REPLACED RIGHT PYLON STIFFENER AT PP STA 153.90 AT INBOARD END IAW B757 SRM 51-40-02.SDR UPS09554363Bracket · crackedINSPECTION TYPE:C1 NR 1 ENGINE NACELLE FWD SUPPORT ANGLE FOR ACCESS PANEL 435 AT LWR BRACKET CRACKED. REPLACED BRACKET PER SRM 51-40-02-0G.SDR UALA2009010500039Angle · crackedCRACKS FOUND ON NR1 PYLON CLOSEOUT ANGLE, 2ND FASTENER FROM INBD EDGE AT 0:00 POS AND 0900 POS. MAJOR REPAIR ACCOMPLISHED: STOPPED DRILLED CRACKS AND INSTALLED FILLER AND STRAP DOUBLER REPAIR.SDR UPS09554375Strut · corrodedINSPECTION TYPE:C2 CORROSION ON THE NR 2 ENGINE CNA LWR STRUT 6 O'CLOCK POSITION PPS205. REPAIRED PER ATS ER 09-1052 DATED 12JAN09 AND UPS EO 757-7810-31855A.SDR FDEA200812295316Support · crackedNR 1 PRECOOLER SUPPORT IS CRACKED. MATERIAL ID PER ASTME-1476-01 & WELD PER P.S. 01-04-21.SDR MASA2008122100751Door · chafedLT & RT UPPER AND LOWER CORE COWL DOORS CHAFE DAMAGE AT AFT EDGE. REPAIRED WORN AFT SEAL.SDR DL757081719Fitting · wornTHE NR 2 PYLON INBOARD SIDE LOAD FITTING WAS FOUND WORN AT THREE LOCATIONS ALONG THE INBOARD EDGE. LOCALLY BLENDED, ROTO PEENED, AND REFINISHED EACH DAMAGE LOCATION.SDR UALA2008121206860Structure · crackedNR 2 PYLON INBOARD SIDE IS CRACKED AT PNL LANDING. MAJOR REPAIR ACCOMPLISHED. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR.SDR UALA2008120406749Bushing · looseON NR 2 ENGINE, UPPER LINK, FWD BUSHING HAS MOVEMENT-ROTATED. EVIDENCED BY BROKEN SEALANT AROUND THE BUSHING PERIMETER. REPLACED BUSHINGS.SDR UALA2008120406748Bushing · out of positionNR 2 ENGINE, FWD SECTION OF DIAGONAL BRACE, OUTBOARD LUG BUSHING HAS MIGRATED OUT. REPLACED INNER AND OUTER BUSHINGS.SDR UALA2008120406747Web · crackedNR 2 PYLON UPPER WEB, OUTBOARD DRAIN HOLE CRACKED. MAJOR REPAIR ACCOMPLISHED. STOP DRILL CRACK. INSTALLED REPAIR DOUBLER AND FILLER REPAIR.SDR FDEA200812020105Fitting · corrodedPYLONS, PYLON STRUCTURE, NR 1 AND NR 2 PYLON AFT FITTING BORES AND BOLTS HOLES CORROSION REPAIR.SDR 2008UALA06476Angle · damagedNR 1 PYLON MIDSPAR FITTING CLOSE-OUT ANGLE, 2 EACH INBOARD FASTENER HOLES ARE ELONGATED IN PREVIOUS REPAIR AREA. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING REPAIR ANGLES AND FABRICATED A NEW REPAIR DOUBLER AND TRIPLER ANGLE. BOTH HOLES MEASURE .531 INCH ANSDR ASAA0893704Bracket · crackedAT RSS 261 RIGHT JUST AFT OF NR 2 PYLON AFT BRACKET CRACKED AT FIXED TRAILING EDGE. REMOVED CRACKED BRACKET AND REPLACED WITH SERVICEABLE PER SRM 51 40 02 ITEM 9.
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