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 QXEA2010051000298Strip · looseCHAFE STRIP UNDER NR 2 ENGINE HORSE COLLAR PANEL (LT SIDE) IS PULLING UP AND LOOSE. UNINSTALLED CHAFE STRIP UNDER NR 2 ENGINE HORSE COLLAR PANEL LT SIDE BY REMOVING 3 BOLTS, 8 RIVETS AND 4 NUTPLATES IAW SRM 51-40-07. INSTALLED NEW CHAFE STRIP UNDER NR 2 ENGIMay 8, 2010 · N432QX · Bombdr DHC8402SDR IPXA10559828Bracket · crackedINSPECTION TYPE:C2, NR1 NACELLE STRUT AFT FAIRING, RT SIDE CHANNEL ATTACH BRACKET IS CRACKED, AT THE FWD LWR CORNER, JUST AFT OF FWD VERTICAL CHORD R & R BRACKET IAW SRM 51-40-02.May 7, 2010 · N411UP · Boeing 75724APFSDR KCSA101044Strap · damagedNR 3 PYLON INTERNAL STRAP IS DAMAGED AT NAC STA 221.9, WL 190.52.May 6, 2010 · N715CK · Boeing 747209BSDR KCSA101043Strap · damagedNR 2 PYLON INTERNAL STRAP IS DAMAGED AT NAC STA 221.9, WL 190.52.May 6, 2010 · N715CK · Boeing 747209BSDR AALA20100505TUL11Skate Angle · crackedFUSELAGE HAS A CRACK IN LOWER SKATE ANGLE BETWEEN LEFT PYLON AND FUSELAGE AT CANT FRAME AT STATION 1463. INSTALLED REPAIR DOUBLER PER AARD 54-20-00-1.May 5, 2010 · N594AA · Doug DC983SDR USAA2010051790979Hinge Fitting · crackedMCN - C11 - MAJOR REPAIR - NR 4369912 - CRACK AT NR 2 ENGINE PYLON CENTER HINGE FITTING FOR AFT MOVEABLE FAIRING. REPAIRED NR 2 ENGINE PYLON CENTER HINGE FITTING FOR AFT MOVEABLE FAIRING IAW A321 SRM 54-55-12.May 4, 2010 · N192UW · Airbus A321211SDR DHLA201000064Angle · crackedNR 1 ENG PYLON LT UPPER ANGLE CRACKED .7500" STA YN 202.6. PERFORMED MAJOR REPAIR IAW FORM 8110-3 DATED 06-10-10, EVA D854-00335 REV IR DATED 05-13-10. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED AREA IAW SMN DWG ED-5130 REV 01 DATED 05-07May 3, 2010 · N806DH · Doug DC873FSDR FDEA201005031429Web · crackedNR 2 ENG /PYLON---PYLON WEB STRUCTURE IS CRACKED IN 2 PLACES AS SEEN THROUGH NACELLE ACCESS PANEL 421 CL. STOP DRILLED CRACKS IAW SRM 54-52-11. INSTALLED REPAIR IAW SRM 54-21-11, FIG 201, PGS 205 / 206, CONFIG 2 AND SRM 51-40-30. DISPLACED AND REINSTALLED WMay 3, 2010 · N658FE · Airbus A300F4605RSDR HALA2010050200225Angle · brokenNR 1 STRUT AFT FAIRING, AFT "V" ANGLE, INBD ANGLE BROKEN WERE FAIRING ATTACHES TO STRUT. FABRICATION OF REPLACEMENT PARTS IAW DWG 313T3380. MATCH DRILL REPLACEMENT FRAME DWG 313T3380-303, IAW SRMS -40-02, REV 82. ASSY FRAME AND FABRICATED PARTS IAW SRM 51-40-May 2, 2010 · N584HA · Boeing 7673G5SDR IPXA10559827Channel · gougedINSPECTION TYPE:C2, NR1 ENGINE NACELLE STRUT AFT FAIRING, RT SIDE CHANNEL IS GOUGED AT FWD LWR END. NAC STA206 COMMON TO ACCESS PANEL NR 435AR FWD LWR CORNER. REMOVED DAMAGE FROM CHORD IAW UPS EO B757-5450-37704-A.Apr 30, 2010 · N411UP · Boeing 75724APFSDR CALA2010043000182Stiffener · crackedSUPPORT TASK FCD 5420-01488 NR 2 PYLON NAC STA 285 I/B STIFFENER FOUND CRACKED. NR 2 PYLON NAC STA 285 I/B STIFFENER REPLACED AND INSTALLED AS PER FCD5420-01488 STEP 6 AND BOEING DWG 311T2400.Apr 29, 2010 · N59053 · Boeing 767424ERSDR CALA2010043000181Stiffener · crackedSUPPORT TASK FCD 5420-01488 NR 2 PYLON NAC STA 285 O/B STIFFENER FOUND CRACKED. NR 2 PYLON NAC STA 285 O/B STIFFENER REPLACED AS PER FCD5420- 01488 STEP 6 AND BOEING DWG 311T2400, AND INSTALLED AS PER FCD 5420-01488 STEP 6 AND BOEING DWG 311T2400.Apr 29, 2010 · N59053 · Boeing 767424ERSDR CALA2010043000180Stiffener · crackedSUPPORT TASK FCD5420-01487 NR 1 PYLON NAC STA 285 O/B STIFFENER FOUND CRACKED NR 1 PYLON NAC STA 285 O/B STIFFENER. REPLACED AND INSTALLED AS PER FCD5420-01487 STEP 6 AND BOEING DWG 311T2400.Apr 29, 2010 · N59053 · Boeing 767424ERSDR ASOA201000666Support Angle · crackedNR 2 ENG FAIRING SUPPORT ANGLE CRACKED AFT OF FWD YOKE AT 2 O'CLOCK POSITION. REMOVED AND REINSTALLED NR 2 ENG FAIRING SUPPORT ANGLE IAW CRJ 200 SRM 51-42-20. (SDR CLOSED)Apr 25, 2010 · N928EV · Cndair CL6002B19SDR C2XA10SH147Inlet · corrodedSHV - DURING C-CHECK RT INLET HAS SEVERAL NUT PLATE HOLES THAT ARE CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR OF RT INLET NUT PLATE HOLES IAW EC5420-01158. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EPSDR C2XA10TY059Support · corrodedA COUPLE OF BOLT HOLES OUTBOARD OF THE NR 2 GENERATOR SUPPORT ON THE NR 2 ENG INLET FLANGE HAS CORROSION. REMOVED CORROSION AND INSTALLED BUSHINGS IAW EC5420-01158.Apr 21, 2010 · N14920 · Emb EMB145LRSDR FDEA201004201261Fairing · crackedNR 3 PYLON PANEL 488 CL IS CRACKED AT THE EDGE OF THE HINGE CUTOUT. FABRICATED REPAIR DOUBLER IAW SRM 54-00- 01, FIG 2-B, SHEET 2, VOL I. INSTALLED REPAIR DOUBLER IAW SRM 54-00-01, FIG 2-B, SHEET 2, VOL I.Apr 20, 2010 · N361FE · Doug MD1010FSDR SWIA201024238Stiffener · crackedRIGHT NACELLE HYDRAULIC RESERVOIR ATTACH FRAME LOWER STIFFENER CRACKED. (C CHECK) REPLACED STIFFENER PER SRM.Apr 17, 2010 · N297SW · Emb EMB120ERSDR 2010FA0000345Stiffener · crackedPYLON NR 2 INBD NR 3 STIFFENER CRACK 0.67 INCH BETWEEN NAC STA 248 AND NAC STA 259 ON THE RT SIDE.Apr 15, 2010 · N758SA · Boeing 747281FSDR Q2SA758009Stiffener · crackedPYLON NR 1 INBOARD NR 3 STIFFENER CRACK.Apr 12, 2010 · N758SA · Boeing 747281FSDR AALA20100409AFW01Fastener · missingTHE DRAIN MAST OF THE NUMBER 2 PYLON HAS THREE MISSING FASTENERS ON THE INBOARD LEFT SIDE. THE FASTENERS ARE AT THE BOTTOM OF PANEL 313W3560, ON THE CORNER AND TRAILING EDGE, AND COMMON TO THE DRAIN MAST WEDGE (313W3530-1). ACCOMPLISHED REPAIR PER 777 AARD 5Apr 9, 2010 · N795AN · Boeing 777223SDR DLM88101144Web · crackedHMV3 AFT ACCY COMP STA 1380 L5L ENGINE PYLON WEB HAS A CRACK AT HOLE. TRIM OUT DAMAGE AREA, FAB DOUBLER AND FILLER AND INSTALLED PER MD88 SRM 51-30-5 AND 53-11D.Apr 8, 2010 · N993DL · Doug MD88SDR ABXA201004130057Support Beam · crackedHYD BAY LOWER SUPPORT BEAM ON OUTBOARD SIDE CRACKED AND WORN AT FWD END. REPAIRED IAW REA B654-58745MR.Apr 8, 2010 · N742AX · Boeing 767232SDR ABXA201004130056Support Beam · crackedHYD BAY LWR SUPPORT BEAM ON INBOARD SIDE CRACKED AT FWD END. REPAIRED AREA IAW B767 REA B654-58745MR.Apr 8, 2010 · N742AX · Boeing 767232SDR ASOA201000497Fairing · crackedSTANG FAIRING 444BT IS CRACKED AND FASTENER HOLES ARE ENLARGED. RECEIVED SERVICEABLE STANG FAIRING FROM STORES. LOCATED AND INSTALLED FAIRING BRACKETS IAW SRM 51-42-06. REQUIRES PAINT ON FAIRING ASSY. REF MASTER PANEL BOOK FOR INSTALLATION OF STANG FAIRING. Apr 6, 2010 · N920EV · Cndair CL6002B19SDR SIMA201009804Profile · crackedDURING MAINTENANCE BASE VISIT FOUND THE LEFT PYLON PROFILE TO HAVE CRACKS. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR ON THE LEFT PYLON PROFILE IAW EO EM-54MR-312. THE AIRCRAFT WAS RETURNED TO SERVICE.Apr 6, 2010 · N620AE · Emb EMB145LRSDR C2XA10TY050Flange · corrodedRIGHT ENG INLET FLANGE BOLT HOLE HAS CORROSION. REMOVED AND REPLACED BUSHING IAW EC5420-01158.Apr 6, 2010 · N14177 · Emb EMB145XRSDR 2010FA0000433Stiffener · crackedCRACK WAS FOUND ON THE STIFFENER OF THE NR 3 PYLON. INSTALLATION SPLICE REPAIR ANGLES.Apr 5, 2010 · N708SA · Boeing 7472B5FSDR ABXA201004120047Beam · crackedRIGHT ENGINE PYLON OUTBOARD BEAM THAT RUNS ACROSS LOWER PART OF HYD BAY ACCESS DOOR IS CRACKED AT 3RD NUT PLATE HOLE FROM FWD END. REMOVED DAMAGED SECTION OF RIGHT ENGINE OUTBOARD PYLON BEAM IN LOWER PART OF HYD BAY ACCESS DOOR AND SPLICED. REPAIRED PER REA Mar 27, 2010 · N769AX · Boeing 737281SDR ZZDA2010213Structure · crackedRIGHT PYLON APRON NR 2 HINGE CUT OUT AREA, CRACKED. ACCOMPLISHED NR 2 HINGE CUTOUT AREA DOUBLER REPAIR PER TRA 17-54-TR00129.Mar 21, 2010 · N998AT · Boeing 717200SDR ZZDA2010210Structure · crackedLEFT PYLON APRON NR 4 HINGE CUTOUT AREA, CRACKED. ACCOMPLISHED NR 4 HINGE CUTOUT AREA, DOUBLER REPAIR PER TRA 17-54-TR00129.Mar 20, 2010 · N998AT · Boeing 717200SDR EE4Y1003025Angle · crackedDURING INSPECTION NR 2 ENGINE PYLON T/E STRUCTURE AT STA Y 900 O/B RIB LOWER ANGLE CRACKED.Mar 13, 2010 · N784TW · Doug DC915FSDR EE4Y1003024Angle · crackedDURING INSPECTION NR 2 ENGINE PYLON T/E STRUCTURE AT STA Y 917 O/B ANGLE CRACKED.Mar 13, 2010 · N784TW · Doug DC915FSDR EE4Y1003023Angle · crackedDURING INSPECTION NR 2 PYLON STRUCTURE AT STA Y 875 O/B AREA SEAL RETAINER ANGLE CRACKED.Mar 13, 2010 · N784TW · Doug DC915FSDR GUUA93971031110ABracket · crackedDURING MAGNETIC PATICLE INSP, DISCOVERED ENGINE TRUSS COWL BRACKET WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENGINE TRUSS COWL BRACKET WELD AREA CRACKS. NOTE: FOUND DURING MAGNETIC PARTICLE INSP.Mar 11, 2010 · N82539 · Beech 1900DSDR FDEA201003090789Support · crackedRT PYLON AFT COMMON NOZZLE UPPER FAIRING LOWER PANEL SUPPORT FWD ANGLES (BOTH) FOUND FWD CORNER CRACK. CRACKED ANGLES ON RT PYLON AFT COMMON NOZZLE UPPER FAIRIING LOWER PANEL. R & R IAW EA F-7110-137437 (COMMON NOZZLE TO STRUT FAIRING -PARTS ANGLE FABRICATIIMar 9, 2010 · N936FD · Boeing 7572T7SDR FDEA201003090788Angle · crackedLT PYLON AFT COMMON NOZZLE UPPER FAIRING LWR PANEL SUPPORT FWD ANGLES (BOTH) FOUND FWD CORNER CRACK. CRACKED SUPPORT ANGLES LT & RT REPLACED IAW EA F-7110-137437 (COMMON NOZZLE TO STRUT FAIRING - PARTS ANGLE FABRICATION FOR PN LJ34907 & LJ34909). REPAIR IS Mar 9, 2010 · N936FD · Boeing 7572T7SDR DHLA201000039Angle · crackedNR3 ENG TO PYLON ANGLE CRACKED 10" AT 12 O'CLOCK POS STA YN 183.000-202.500. PERFORMED MAJOR REPAIR IAW FORM 8110-3 DATED 04-21-10 EVA D854-00305 REV IR DATED 03-23-10. CUT OUT DAMAGED AREA IAW SMN DWG ED-5104 REV 01 DATED 03-18-10. VISUALLY INSPECTED CUT OUT Mar 4, 2010 · N802DH · Doug DC873SDR FDEA201003010569Strip · wornNR 3 ENG LT CORE COWL FWD CHAFE STRIP IS CHAFED. R & R ADAPTER, PN ASL040-1 SRM 51-35-01, VOL II. APPLIED TEFLON PAINT AMM 71-13-01-2.Mar 1, 2010 · N570FE · Doug MD1010FSDR FDEA201003010567Strip · wornNR 3 ENG RT CORE COWL FWD CHAFE STRIP IS WORN. FOUND TO BE OUT OF LIMITS IAW SRM 51-00-01, FIG 117, SHEET 3; VOL II. REMOVED OLD ADAPTER AND REPLACED WITH NEW ADAPTER IAW SRM 51-35-01, VOL II. APPLIED TEFLON PAINT AS REQUIRED IAW AMM 71-13-01-2.Mar 1, 2010 · N570FE · Doug MD1010FSDR ASAA1047681Beam · damagedNR 1 ENGINE AFT PYLON FAIRING HORIZONTAL I BEAM AT APPROX NAC STA 314 CENTER ATTACH FITTING HAS 2 FASTENERS PULLING THROUGH BEAM AND FITTING. FABRICATED HORIZONTAL BEAM AND FITTING AND INSTALLED.Feb 24, 2010 · N768AS · Boeing 737490SDR IPXA10558684Channel · damagedINSPECTION TYPE:MOD RIGHT PYLON LEFT UNDERWING FAIRING SUPPORT STRUCTURE BULLNOSE ATTACH BRACKET HAS ELONGATED FASTENER HOLES AT PPS 170. REPLACED CHANNEL IAW SRM 51-40-02-0G, SRM 51-40-05, DWG313N5004 AMM 51-21-10.Feb 22, 2010 · N456UP · Boeing 75724APFSDR IPXA10558679Angle · chafedINSPECTION TYPE:MOD NR 2 PYLON AFT FAIRING STRUCTURE RT FWD VERTICAL ANGLE IS CHAFED ON THE OUTER RADIUS. PPS 208.47 P/N 313N5033-100. REPLACED ANGLE IAW SRM 51-40-02-0G, SRM 51-40-05-0G, BOEING DWG 313N5033, SRM 51-40-08-0G, AMM 51-21-04-07, AMM 51-21-10-7.Feb 20, 2010 · N456UP · Boeing 75724APFSDR IPXA10558683Brace · brokenINSPECTION TYPE:MOD RIGHT PYLON RT UNDERWING FAIRING SUPPORT STRUCTURE FWD BRACE HAS UPPER TAB BROKEN OFF AT PPS 185.35. REPLACED BRACE IAW SRM 51-40-02, SRM 51-40-05, SRM 54-50-71-1A 1.Feb 18, 2010 · N456UP · Boeing 75724APFSDR IPXA10558682Angle · crackedINSPECTION TYPE:MOD RT PYLON RT UNDER WING FAIRING SUPPORT STRUCTURE AFT BRACE HAS A CRACK IN THE UPPER RADIUS AT PPS 185.35. REPLACED RT PYLON RT UNDERWING FAIRING SUPPORT STRUCTURE AFT BRACE PER SRM 51-40-05-0G, SRM 51-40-08-0G, SRM 51-40-02, SRM 54-50-71-1Feb 18, 2010 · N456UP · Boeing 75724APFSDR NSVA201048Structure · misrepairedAIRCRAFT REQUIRES MAJOR REPAIR FOR PERMANENT REPAIR OF MISC RIVET DEVIATION ON RT INBOARD NACELLE IAW TD 340-54-09-55.Feb 17, 2010 · N249CJ · Saab 340BSDR NSVA201047Structure · misrepairedAIRCRAFT REQUIRES MAJOR REPAIR FOR PERMANENT REPAIR OF MISC RIVET DEVIATION ON RT OUTBOARD NACELLE IAW TD 340-54-09-56.Feb 17, 2010 · N249CJ · Saab 340BSDR NSVA201046Structure · misrepairedAIRCRAFT REQUIRES MAJOR REPAIR FOR PERMANENT REPAIR OF PULLED RIVETS ON RT INBOARD NACELLE AT STA 203 IAW TD 340-54-09-15.Feb 17, 2010 · N346CJ · Saab 340BSDR NSVA201045Structure · misrepairedAIRCRAFT REQUIRES MAJOR REPAIR FOR PERMANENT REPAIR OF MISC RIVET DEVIATION ON RT INBOARD NACELLE IAW TD 340-54-09-28.Feb 17, 2010 · N277MJ · Saab 340BSDR NSVA201044Structure · misrepairedAIRCRAFT REQUIRES MAJOR REPAIR FOR PERMANENT REPAIR OF MISC RIVET DEVIATION ON LT OUTBOARD NACELLE IAW TD 340-54-09-29.Feb 17, 2010 · N277MJ · Saab 340B
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