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.

SDR SWIA200820457Riser · corrodedC-CHECK, FRETTING CORROSION AT RIGHT PRODUCTION RISER. REPAIRED PER REO.Aug 10, 2008 · N959SW · Cndair CL6002B19SDR A6WA200840572Channel · crackedRT ENGINE UPPER CORE COWL AFT U CHANNEL IB SIDE CRACKED. RT ENGINE UPPER CORE COWL AFT U CHANNEL IB SIDE REPAIRED IAW SHORTS CMM 20-12-00. (K)Aug 8, 2008 · N445AW · Cndair CL6002B19SDR UPS08553114Support · crackedINSPECTION TYPE:MOD NR 1 PYLON UNDERWING FAIRING STRUCTURE LT FWD SUPPORT BRACE IS CRACKED AT PPS 185.0. REMOVED AND REPLACED PER SRM 51-40-02.Aug 8, 2008 · N453UP · Boeing 75724APFSDR 08FDEA03296Fairing · chafedFOUND CHAFING MARKS ON PYLON NR 2 UPPER AFT FAIRING RIB 19 REPAIR PERFORMED BY REWORK OF CHAFING MARK, NDT FOR CRACK FREE CONDITION AND INSTALLING A STRIP TO LIMIT NEW CHAFING IAW RAS /70511364/010/2008 ISS A , APPROVED BY EA 6-5454-120084.Aug 7, 2008 · N743FD · Airbus A300B4622RSDR 08FDEA03210Angle · looseTHE NR 3 PYLON AFT BULKHEAD TO SPAR ANGLE, INBD AND OUTBD SIDES HAS 1 EA BOLT PER SIDE LOOSE AT PYLON STA YN 417. REMOVED AND REPLACED 2 EA FASTENER IAW DC/MD-10 SRM 51-31-01; VOL II AND TORQUED IAW DC/MD-10 AMM 20-30-02-2. PERFORMED HFEC EDDY CURRENT INSPECAug 1, 2008 · N564FE · Doug MD1010FSDR 08FDEA03205Fairing · crackedNR 1 PYLON STRUT AFT FAIRING LOWER PAN SKIN, AFT FOUND WITH A CRACK ABOUT 1/2 INCHES LONG. CRACKED SKIN REMOVED AND REPLACED IAW B757-200 SRM 54-50-70 REV 93 AND AMM 20-11-00 REV 2. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.Aug 1, 2008 · N919FD · Boeing 75723ASDR 08FDEA03204Fairing · crackedNR 2 PYLON STRUT AFT FAIRING LOWER PAN SKIN, AFT HAS ABOUT 1/3 INCH LONG CRACK NEAR PPSTA 276. CRACKED SKIN REMOVED AND REPLACED IAW B757-200 SSRM 54-50-70 REV 93 AND AMM 20-11-00 REV 2. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.Aug 1, 2008 · N919FD · Boeing 75723ASDR UPS08553012Bracket · crackedINSPECTION TYPE-C2, BRACKET IS CRACKED IN THE NR 2 ENG PYLON HYD BAY, OB SIDE AT FWD LWR CORNER OF PANEL 445AR CUTOUT, NAS STA 208. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02-0G.Jul 30, 2008 · N423UP · Boeing 75724APFSDR 08FDEA03166Support Bracket · gougedNR 1 ENGINE PYLON, THROTTLE INTERLOCK ACTUATOR AFT SUPPORT BRACKET IS GOUGED. REMOVED DIRECTIONAL PILOT VALVE PUSH ROD IAW MD-10-10 AMM 76-10-03-02. REMOVED, FABRICATED AND INSTALLED AUL 7047-7 SUPPORT IN REF TO DAC DWG AUL 7047, REF "F". ALODINED AND PRIMJul 30, 2008 · N372FE · Doug MD1010FSDR 08FDEA03071Rub Strip · wornNR 3 PYLON PANEL 487 CL HAS BOTH FLANGES WORN. BLENDED RUB STRIPS. ORIGINAL MATERIAL 0.063. MATERIAL REMOVED 0.040. MATERIAL REMAINING 0.023. FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01; VOL I AND 54-31-01; VOL II. PRIMED RUB STRIPE IAW SRM 51-21-01; VJul 25, 2008 · N372FE · Doug MD1010FSDR UPS08852995Stiffener · crackedINSPECTION TYPE:C1, NR 4 PYLON RT INTERIOR STRUCTURE AREA HAS A CRACKED STIFFENER AT STA. YN 326. FABRICATED AND REPLACED STIFFENER IAW DWG 5756791, AND 51-01-24,51-01- 21D.Jul 24, 2008 · N715UP · Doug DC871FSDR KCSA081339Stiffener · severedLOWER SIDE OF HORIZ FIREWALL WEB. CENTER LONGERON STIFFENER SEVERED NR 3 PYLON NAC STA 160. (A)Jul 23, 2008 · N715CK · Boeing 747209BSDR 08FDEA03032Fairing · wornNR 3 PYLON PANEL 488 CR IS WORN AT THE FASTENER HOLES. BLENDED WORN AREA OUT OF LIMITS. ORIGINAL MATERIAL 0.050. MATERIAL REMOVED IS 0.011. MATERIAL REMAINING IS 0.039 REF DC/MD-10 SRM 54-00-01, VOL I. FABBED REPAIR DOUBLER AND INSTALLED DOUBLER REF DC/MDJul 23, 2008 · N372FE · Doug MD1010FSDR KCSA081333Stiffener · damaged#2 PYLON NAC STA 180 BULKHEAD STIFFENER DAMAGED ON AFT CENTER SIDE OF BULKHEAD. (A)Jul 21, 2008 · N712CK · Boeing 747122SDR 08FDEA03000Bracket · wornNR 1 ENGINE INBD FAN COWL INTERIOR SURFACE BRACKET IS WORN AT APPROX THE 3 O'CLOCK POSITION. REMOVED BRACKET IAW SRM 51-31-01, VOL II. FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01, VOL I AND DAC DWG PLWSPO959, REV H. MATERIAL ID 2024-T3, 0.032 IAW DAC DWG PLWJul 21, 2008 · N372FE · Doug MD1010FSDR 08FDEA02985Bracket · crackedNR 1 ENG UPPER COWL, BRACKET CRACKED AT FWD O/B LOWER CORNER REMOVED AND REPLACED CRACKED SEGMENT, PAINTED AFFECTED AREA OF COWLING. REF SRM 51-30-2 PG 2, MM 51-20-151-7 PG1-5. THIS IS CLASSIFIED AS A MINOR REPAIR.Jul 19, 2008 · N273FE · Boeing 727233SDR 08FDEA02836Web · crackedAFTER REMOVAL ACCESS PANEL ON PYLON NR 3 WITH OAN J/C 0600B430-1JR FOUND HORIZ WEB WITH CRACKS. REPAIRED CRACKS IAW SRM 54-00-01 FIG 2B SHT 2 & FIG 13 SHT 6 VOL I.Jul 12, 2008 · N40061 · Doug DC1010SDR 08FDEA02728Fairing · crackedNR 2 PYLON AFT FAIRING LT FWD OF 483 CL CUTOUT; METAL PLATING IS CRACKED AT THE LOWER END. REMOVED METAL PLATE REINFORCEMENT IAW A300-600 SRM 51-40-00. FABBED REPAIR DOUBLER IAW A300-600 SRM 54-50-10; PG 214. STOP DRILLED THE CRACK IAW A300-600 SRM 54-50-00Jul 7, 2008 · N674FE · Airbus A300F4605RSDR 08FDEA02694Strap · unknownFOUND OLD REPAIR ON RT AFT PYLON BOX NOT PERFORMED IAW DRAWING R546-10314. REPAIR RENEWED IAW DRAWING R546-10314 AND RAS 034632/010/2004 ISS A, APPROVED BY EA 6-5451-120101.Jul 4, 2008 · N742FD · Airbus A300B4622RSDR 2008UALA03660Web · chafedNR 2 ENG FWD PYLON HYDRAULIC PRESSURE LINE FEED THROUGH ELBOW IS LOOSE AND WEARING INTO FIRE WALL. *S/D* ACCOMPLISHED MAJOR REPAIR IN SFO. REPAIRED PYLON WEB PER MM 54-51-95.Jul 1, 2008 · N517UA · Boeing 757222SDR 08FDEA02491Web · crackedWEB CRACKED OUTBOARD OF PRECOOLER NR 1 PYLON. DRILLED CRACK STOP HOLES PER SRM 54-52-31. REMOVED THE RELATED FASTENERS PER SRM 51-40-21. MANUFACTURED THE DOUBLER AND BROKE SHARP EDGES PER SRM 51-26-20. DRILLED FASTENER HOLES TO THE WEB AND THE DOUBLER PER Jun 26, 2008 · N456FE · Airbus A310222SDR 2008UALA03614Bushing · out of positionNR 1 PYLON INBOARD MID SPAR FITTING BUSHING MIGRATED .035 NO CORROSION OR ROTATION.Jun 26, 2008 · N657UA · Boeing 767322SDR 2008UALA03613Bushing · out of positionNR 2 PYLON INBOARD MID SPAR FITTING BUSHING MIGRATED .030 NO CORROSION OR ROTATION.Jun 26, 2008 · N657UA · Boeing 767322SDR 2008UALA03553Web · crackedNR 2 PYLON UPPER WEB CRACKED, NAC STA 182 AT FWD OUTBD CORNER OF FEED THROUGH CUTOUT. FOUND CRACKED WEB SUSPECT NORMAL AC OPERATION. REPAIRED CRACK IAW SB 767-54-0091 FIG 10. AC OK FOR SERVICE.Jun 23, 2008 · N657UA · Boeing 767322SDR 08FDEA02222Shim · crackedNR 1 PYLON RIB 3-A STA 615 INBD SIDE SHIM HAS A .75 INCH CRACK.Jun 11, 2008 · N665FE · Airbus A300F4605RSDR 08FDEA02221Shim · crackedNR 1 PYLON RIB 3-A; STA 615, THE OUTBD SIDE SHIM HAS A 3/4 INCH CRACK.Jun 11, 2008 · N665FE · Airbus A300F4605RSDR 08FDEA02186Stiffener · crackedNR 3 PYLON PANEL NR 487 EL HAS A CRACKED STIFFENER. REMOVED AND REPLACED THE CRACKED STIFFENER IAW DC/MD-10 SRM 51-31-01; VOL II ON PANEL 487 EL ON THE NR 3 PYLON.Jun 6, 2008 · N357FE · Doug MD1010FSDR HALA0800617Channel · crackedTHE VERTICAL U-CHANNEL IS CRACKED AT AFT INBOARD EDGE OF NR 2 ENG PYLON, 7: INBOARD OF THE DIAGONAL BRACE AFT MOUNT FITTING. REMOVED AND REPLACED VERTICAL U-CHANNEL AT AFT INBOARD EDGE OF NR 2 ENG PYLON PER SRM 54-53-70/ 101 AND SRM 51-70-11-06-0 FIG 1. (S)Jun 3, 2008 · N589HA · Boeing 76733ASDR A6WA200840464Angle · crackedANGLE CRACKED ON RT PYLON ACCESS PANEL 422 BT. ANGLE REPLACED IAW SRM 51-42-06. (A)May 30, 2008 · N402AW · Cndair CL6002B19SDR DL757080780Brace · damagedDURING ACCOMPLISHMENT OF THE SIP MOD, S/B 757-54-0034 REV 1, THE DIAGONAL BRACE LOWER/FWD I/B LUG WAS INADVERTENTLY OVERSIZED TO 2.003" INSTEAD OF THE REQUIRED 2.000" MAXIMUM. AN OVERSIZED BUSHING WAS INSTALLED. AD 2003-18-05 APPLIES.May 27, 2008 · N641DL · Boeing 757232SDR USAA920081108Strap · crackedBFM - MAJOR REPAIR - C3 CHECK - CRACKED CHORD STRAP ON NR 2 PYLON. REPLACED CHORD STRAP ON NR 2 PYLON IAW USAIRWAYS EA 100416.May 21, 2008 · N250AY · Boeing 767201SDR DU4R2008208Support · gougedS/O NR312001 NR 24376, NR1 ENGINE PYLON FAN COWL SUPPORT UPPER CHORD FWD HORIZ END FLANGE NAC 166-175 APPROX IS GOUGED.May 21, 2008 · N742VA · Boeing 737448SDR A6WA200840432Plate · corrodedRT PYLON TRAILING EDGE, INBOARD UPPER BONDING PLATE CORRODED. CORROSION REMOVED IAW CRJ 200 SRM 51-21-06 AND WITHIN LIMITS IAW SRM 54-00-00. (A)May 20, 2008 · N406AW · Cndair CL6002B19SDR A6WA200840436Plate · corrodedLEFT PYLON TRAILING EDGE, OUTBOARD UPPER BONDING PLATE CORRODED. REPLACED BECAUSE OF MATERIAL OUT OF LIMITS TOLERANCE IAW ARM 54-00-00. FORMED AND INSTALLED NEW BONDING PLATE IAW SRM 51-24-21 AND SRM 51-42-10. (A)May 20, 2008 · N406AW · Cndair CL6002B19SDR A6WA200840433Plate · corrodedLEFT PYLON TRAINING EDGE, INBOARD UPPER BONDING PLATE CORRODED. REMOVED CORROSION ON UPPER BONDING PLATE LT PYLON TRAILING EDGE INBOARD SIDE IAW CRJ 200 SRM 51-21-06 AND WITHIN LIMITS IAW SRM 54-00-00. (A)May 20, 2008 · N406AW · Cndair CL6002B19SDR 08FDEA01903Angle · crackedNR 3 ENGINE LOWER COWL, O/B SIDE EDGE, COWL STRUCTURE AREA CRACKED OUT, JUST AFT OF THE 4TH LATCH CUT OUT FROM FWD END REMOVED AND REPLACED ANGLE REF DWG 65- 19507. THIS IS CLASSIFIED AS A MINOR REPAIR.May 20, 2008 · N220FE · Boeing 727233SDR NOCA03908Fitting · crackedFAN COWL SUPPORT BEAM FITTING ASSY IS CRACKED IN TWO PLACES LT SIDE. REPLACED COWL SUPPORT BEAM FITTING AND SHIMMED AS PER SRM 51-10-02.May 19, 2008 · N760NA · Boeing 76739HSDR 08FDEA01865Fairing · delaminatedNR 3 PYLON STRINGER FAIRING NR 489 A, LOWER SECTION OF THE FAIRING IS DELAMINATED AND COMING APART. FAIRING 489 AL WAS REPLACED ON FEDEX N/R N00610.May 16, 2008 · N567FE · Doug MD1010FSDR 08FDEA01864Fairing · damagedNR 3 PYLON STRINGER FAIRING NR 489 AL LOWER FRAME HAS MULTIPLE DRILLED HOLES ON BOTH SIDES. REPLACED FAIRING NR AUB 7107-46, PO 619490.1 IAW DAC DWG 6 NR AUB 7107, REV "P".May 16, 2008 · N567FE · Doug MD1010FSDR Q2SA758002Access Panel · crackedPOST FLIGHT WALK-AROUND, FOUND HYDRAULIC ACCESS PANEL ON NR 1 ENGINE SAIL BOAT FAIRING OPEN. FOUND CRACK AT NR 1 ENGINE INBOARD SAIL BOAT DOOR, AT THE FORWARD HINGE. HYDRAULIC ACCESS PANEL OPENED IN FLIGHT.May 15, 2008 · N758SA · Boeing 747281FSDR TRAX200800622Support Beam · crackedUPPER SURFACE OF ENGINE SUPPORT BEAM APPEARS CRACKED AT B.L. 0 AND FS 640. POSSIBLE CRACK NEEDS VERIFIED. PERFORMED EDDY CURRENT INSPECTION OF ENGINE SUPPORT BEAM AT BL 0.00, FS 640.00, ENGINE SUPPORT BEAM VERIFIED CRACKED AT RIGHT HAND FASTENER HOLE FORWARD May 13, 2008 · N978EV · Cndair CL6002B19SDR A6WA200840419Bracket · crackedCRACKED BRACKET ON RT NOSE INLET COWL APPROX 4 O`CLOCK POSITION. BRACKET FABRICATED IAW SRM 51-24-16 AND REPLACED IAW SRM 51-42-13.May 13, 2008 · N442AW · Cndair CL6002B19SDR 08FDEA01842Rub Strip · gougedNR 3 ENGINE INBD CORE COWL UPPER RUB STRIP IS WORN (GOUGED). REMOVED THE DAMAGED RUB STRIP IAW SRM 51-35-01 VOL II. FABRICATED PER DWG NSL 6061, REV "BC". PRIMED & PAINTED IAW SRM 51-21-01; PG 21; 51-23-01; VOL II. INSTALLED IAW 51-23-01; VOL II.May 13, 2008 · N567FE · Doug MD1010FSDR LR7A08051Mount · crackedDURING SCHEDULED C-8 CHECK, FOUND NR 3 ENGINE INBD TRUSS MOUNT DIAGONAL BRACE ATTACHMENT LUG CRACK. REPAIR ACCOMPLISHED BY REPLACING NR 3 ENGINE INBD TRUSS MOUNT IAW RELEVANT PARAGRAPHS OF SMP583 CHAP 54-30 AND FIG 54-30-06 SHEET 1, 2, 3, AND 5.May 13, 2008 · N403LC · Lkheed 382GSDR 08FDEA01824Attach Angle · chafedNR 2 PYLON LOWER FAIRING PANEL NR 485 AL, RT UPPER ATTACH ANGLE IS CHAFED IN SEVERAL PLACES. REMOVED THE NR 2 PYLON LOWER FAIRING UPPER ATTACH ANGLE PER FEDEX SRM 51-40-21. LOCATED & DRILLED NEW UPPER ATTACH ANGLE IAW SRM 51-40-44. ALODINED & PRIMED NEW ATTMay 12, 2008 · N815FD · Airbus A310324SDR A6WA200840413Bracket · crackedLEFT TAIL PIPE STANDOFF BRACKET FOR FIRE DETECTION LOOP CRACKED. REPLACED IAW SRM 51-42-06. (S)May 10, 2008 · N442AW · Cndair CL6002B19SDR QXEA200800460Support · crackedPDX - C4 CHECK, RT FINGERNAIL DECK LOWER AFT SUPPORT IS CRACKED AT ALL 4 BOLT HOLES. FABRICATED NEW SUPPORT CHANNEL FROM 2024T3 .032 INCH REFERENCE Q400 SRM 54-35-20 REPAIR 2. INSTALLED.May 9, 2008 · N425QX · Bombdr DHC8402SDR A6WA200840473Support · brokenRT ENGINE NOSE INLET HAS A SUPPORT ASSY BROKEN FOR THE T2 LINE AT 12 O`CLOCK POSTIOIN. RT ENGINE NOSE INLET SUPPORT ASSY FOR T2 LINE AT 12 O`CLOCK POSITION REPLACES IAW SRM 51-42-06. (A)May 7, 2008 · N438AW · Cndair CL6002B19SDR A6WA200840383Strip · gougedLT ENGINE UPPER NOSE ACCESS COWL AFT EDGE STRIP GOUGE. LT UPPER ENGINE COWL, AFT EDGE STRIP REPLACED IAW CMM 71-14-01-300-814-A01.May 6, 2008 · N437AW · Cndair CL6002B19SDR A6WA200840382Strip · chafedRT ENGINE NOSE ACCESS COWL (LOWER) TRAILING EDGE STRIP CHAFED BEYOND LIMIT. RT ENGINE NOSE ACCESS COWL (LOWER), NEW TRAILING EDGE STRIP INSTALLED IAW CMM 71-14-01-300-815-A01.May 6, 2008 · N437AW · Cndair CL6002B19
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