JASC 5420

Service difficulty reports · 3,949

Reports filed under 5420 · Nacelle/Pylon Miscellaneous Structure, newest first.

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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"

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SDR 08FDEA01781Channel · crackedNR 1 PYLON PANEL NR 438 CL, INNER CHANNEL IS CRACKED. REMOVED CRACKED CHANNEL AND INSTALLED A NEW CHANNEL REF DC/MD-10 SRM 51-31-01, VOL II.May 6, 2008 · N567FE · Doug MD1010FSDR 08FDEA01779Seal · bentNR 3 PYLON ACCESS PANEL NR 488 DR, SPRING SEAL IS BENT. REMOVED 2 SEALS IAW SRM 51-35-01; VOL II. FABBED 2 SEALS IAW SRM 51-10-00; VOL II; FIG 1 & 51-31-01; VOL II; FIG 2. PART MARKED PER GMM 7-0-1001. INSTALLED SEALS IAW SRM 51-35-01; VOL II.May 6, 2008 · N567FE · Doug MD1010FSDR 08FDEA01726Fairing · crackedRIGHT SIDE NR 1 PYLON LOWER AFT FAIRING HAS A CRACK APPROX 2 INCHES LONG. REMOVED & INSTALLED FAIRING IN REF TO SRM 51-31-01 VOL II. REMOVED DAMAGE; FABRICATED REPAIR AND INSTALLED REPAIR IN REF TO SRM 54-00-01 FIG 26 VOL I & SRM 51-33-01 VOL II.May 2, 2008 · N567FE · Doug MD1010FSDR DL76L080651Angle · crackedWHILE ACCOMPLISHING OPN 5281AD MTC, FOUND THE CLOSE OUT ANGLE CRACKED. CLOSE OUT ANGLE WAS REPLACED. MTC ALSO FOUND THEY NEEDED AN ADDITIONAL WASHER UNDER THE HEAD OF THE FASTENER FOR PROPER GRIPPING. THIS WAS AUTHORIZED. ADDITIONAL INSPECTIONS WERE ACCOMPApr 30, 2008 · N176DN · Boeing 767332SDR 08FDEA01674Rub Strip · wornNR 1 ENGINE OUTBD CORE COWL UPPER T/E CHAFE STRIP IS WORN. BLENDED AREA; ALODINED; PRIMED AND PAINTED IN REF TO EA 8-7110-118486.Apr 29, 2008 · N567FE · Doug MD1010FSDR 08FDEA01675Rub Strip · wornNR 1 ENGINE INBD CORE COWL FWD CHAFE STRIP IS WORN IN SEVERAL PLACES. REMOVED THE ASL 0040-2N ADAPTER IAW SRM 51-35-01; VOL II. DRILLED AND LOCATED NEW ASL 0040-2N ADAPTER IAW SRM 51-35-01; VOL II AND DWG ASL 0040 REV J. INSTALLED NEW ASL 0040-2N ADAPApr 29, 2008 · N567FE · Doug MD1010FSDR DL757080641Structure · damagedDURING HMV AT SAA, THE NR 1 PYLON INBOARD SIDE HAD AN ELONGATED HOLE IN THE UPPER CHORD AT N STA 128. THE ELONGATED HOLE WAS REPAIRED PER BOEING INSTRUCTIONS.Apr 25, 2008 · N646DL · Boeing 757232SDR DL757080640Structure · crackedHMV AT SAA, A CRACK WAS FOUND IN THE UPPER CHORD OF THE NR 1 PYLON, RT SIDE, AT NACELLE STA 136. THE CRACK WAS REPAIRED PER BOEING INSTRUCTIONS.Apr 25, 2008 · N646DL · Boeing 757232SDR 08FDEA01600Panel · wornNR 2 PYLON PANEL NR 424 CR IS WORN FROM FRETTING AROUND THE EXTERIOR FASTENER HOLES. REMOVED DAMAGE REF A300-600 SRM 51-73-10. ORIGINAL THICKNESS .078. REMAINING THICKNESS .032. REMOVED .046. BEYOND LIMITS REF A300-600 SRM 54-52-51. FABRICATED DOUBLER ANApr 25, 2008 · N661FE · Airbus A300F4605RSDR 08FDEA01597Panel · wornNR 2 PYLON PANEL NR 423 CL IS WORN FROM FRETTING AT TWO LOCATIONS FRONT AND BACK. REMOVED DAMAGE REF A300-600 SRM 51-73-10. ORIGINAL THICKNESS .078. REMAINING THICKNESS .052. REMOVED .026. BEYOND LIMITS REF A300-600 SRM 54-52-51. FABRICATED DOUBLER AND FApr 25, 2008 · N661FE · Airbus A300F4605RSDR 08FDEA01540Bushing · corrodedFOUND CORROSION ON PYLON NR 2, RIB 12 OUTBOARD WING LUGS. REPAIR PERFORMED BY REPLACEMENT OF BUSHINGS IAW SRM 57-20-34 PB 200, APPROVED BY EA 6-5451-117148.Apr 25, 2008 · N745FD · Airbus A300B4622RSDR 08FDEA01491Panel · chafedNR 2 PYLON; RIGHT FWD LOWER FAIRING; PANEL 486R IS CHAFED AT THE ATTACHMENT POINTS. REMOVED PANEL AND CHECKED LIMITS. STIFFENER WAS OUT OF LIMITS. FABBED A NEW STIFFENER ON N/R N01140. INSTALLED STIFFENER IAW SRM 51-40-21; PG 7 AND REINSTALLED PANEL IAW SApr 23, 2008 · N661FE · Airbus A300F4605RSDR 08FDEA01490Panel · chafedNR 2 PYLON LEFT FWD LOWER FAIRING; PANEL 485BL IS CHAFED AT THE ATTACHMENT POINTS. REMOVED PANEL AND CHECKED THE LIMITE. THE STIFFENER WAS OUT OF LIMITS. FABBED A NEW STIFFENER ON N/R N01141 & INSTALLED THE STIFFENER IAW SRM 51-40-21. INSTALLED THE PANApr 23, 2008 · N661FE · Airbus A300F4605RSDR CALA0800348Angle · crackedRIGHT ENGINE PYLON VERTICAL ANGLE AFT SIDE OF PANEL OPENING NR 5858R CRACKED. INSTALLED SUPPORT ASSY 313A1380-214 AND PYLON PANEL 15852R IAW B737 SRM 51-40-02.Apr 21, 2008 · N19638 · Boeing 737524SDR 08FDEA01444Bracket · bentNR 3 ENGINE INBD AND OUTBD CENTER T/R ALIGNMENT PADS ARE BENT. REMOVED AND REPLACED IAW SRM 51-35-02; VOL II AND EM-78-32-03; REPAIR 17. VERIFIED GAP AND LATCH CHECKS GOOD AT THE NR 3 T/R IAW AMM 78-32-11-2.Apr 17, 2008 · N365FE · Doug MD1010FSDR 08FDEA01447Stiffener · corrodedPYLON NR 1 STIFFENER AT RIB 9 WITH CORROSION. THE STIFFENER WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21.Apr 1, 2008 · N724FD · Airbus A300B4622RSDR HALA0800469Bracket · crackedRT ENGINE RT COWL SKIRT PANEL, BRACKET CRACKED. SPLICED PLATE FABRICATE IAW BOEING DRAWING 311T1570-94, INSTALLED IAW SRM 51-40-02.Mar 27, 2008 · N596HA · Boeing 767332SDR HALA0800467Bracket · crackedRT ENGINE RT COWL SKIRT PANEL, BRACKET CRACKED. SPLICED PLATE FABRICATED IAW BOEING DRAWING 311T1570-94, INSTALLED IAW SRM 51-40-02.Mar 27, 2008 · N596HA · Boeing 767332SDR CALA0800266Fitting · corrodedNR 2 ENGINE PYLON RIGHT FITTING HAS CORROSION INSIDE BUSHING HOLE. REPAIRED NR 2 ENGINE PYLON RIGHT FITTING IAW EC/RA 5450-01735 AND PACE EA350-54-001.Mar 26, 2008 · N18350 · Boeing 7373T0SDR 08FDEA01127Seal · crackedNR 2 ENGINE LEFT CORE COWL SKIRT FAIRING SPRING SEALS ARE CRACKED. REMOVED & REPLACED THE SPRING SEAL IAW SRM 51-35-01; VOL II.Mar 24, 2008 · N365FE · Doug MD1010FSDR NWAA081149875Web · crackedDURING ENGINE CHANGE, FOUND CRACKS IN LT PYLON CLOSURE WEB AT STA YN 135. REPAIRED PER EA 98-211617.Mar 22, 2008 · N784NC · Doug DC951SDR A6WA200840231Retainer · crackedRIGHT ENGINE, PYLON PANEL 422 DB SEAL RETAINER IS CRACKED. REPLACED IAW CRJ 200 SRM 51-42-06. (M)Mar 21, 2008 · N440AW · Cndair CL6002B19SDR UPS08M52150Fairing · damagedINSPECTION TYPE:C PYLON NR 2 EXHAUST FAIRING LT FWD SEAL MOUNT 3RD HOLE FROM BOTTOM FOUND ELONGATED AFTER REMOVAL OF SEAL AND RETAINER. DAMAGED AREA TRIMMED OUT PER EN1131-08. HFEC INSP C/OUT PER DAC NDTSPM R.13 06-10-01.001 FOUND NO CRACK EVIDENT. EXTERNALMar 20, 2008 · N294UP · Doug MD11SDR UPS08M52149Fairing · damagedINSPECTION TYPE:C PYLON NR 2 EXHAUST FAIRING RT FWD SEAL 2ND MOUNT HOLE FROM BOTTOM FOUND ELONGATED AFTER REMOVAL OF SEAL AND RETAINER. DAMAGED AREA TRIMMED OUT PER EN1131-08 AND MD11-54-20174. HFEC INSP C/OUT PER DAC NDT SPM R.13 06-10-01.001 FOUND NO CRACKMar 20, 2008 · N294UP · Doug MD11SDR 08FDEA01064Channel · crackedNR 1 PYLON PANEL NR 437 DR HAS A CRACKED CHANNEL. REMOVED CHANNEL IAW AMM 51-31-01 VOL II. FABRICATED CHANNEL IAW SRM 51-10-00 FIG 2 VOL II & DWG 7054, REV J. HEAT TREATED CHANNEL IAW TPS 1003. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. PART MARKED CHANMar 19, 2008 · N365FE · Doug MD1010FSDR 08FDEA01049Panel · corrodedNR 2 PYLON PANEL NR 423 EL IS CORRODED ON THE MATING SURFACES. RECEIVED NEW PANEL. INSTALLED NEW EDGE STRIPS TO THE PANEL REF SRM 51-40-21 PARA 6.Mar 19, 2008 · N425FE · Airbus A310203SDR DL76G080387Shim · migratedMIGRATED SHIM BETWEEN NR 2 PYLON AFT PITCH LOAD FITTING AND WING SKIN. PITCH LOAD FITTING AND DAMAGED SHIM WAS REMOVED, SHIM WAS REPLACED AND PITCH LOAD FITTING WAS REINSTALLED.Mar 18, 2008 · N1603 · Boeing 767332SDR 08FDEA01015Fitting · corrodedFOUND ON PYLON NR 1 SPIGOT FITTING WITH CORROSION AROUND BEARING SEAT. REPAIR PERFORMED BY REPLACEMENT OF SPIGOT FITTING IAW SB 54-6017, APPROVED BY EA 6-5451-114936.Mar 18, 2008 · N745FD · Airbus A300B4622RSDR 08FDEA01014Fitting · corrodedFOUND ON PYLON NR 2 SPIGOT FITTING WITH CORROSION AROUND BEARING SEAT. REPAIR PERFORMED BY REPLACEMENT OF SPIGOT FITTING IAW SB 54-6017, APPROVED BY EA 6-5451-114936.Mar 18, 2008 · N745FD · Airbus A300B4622RSDR HALA0800427Structure · damagedNR 1 ENGINE I/B CORE COWL HAS VARIOUS DEFECTS ALONG THE BOTTOM STRUCTURE. BLENDED THE DAMAGE AREA IAW SRM 54-41-02, FIG 101.Mar 17, 2008 · N596HA · Boeing 767332SDR 08FDEA01002Panel · crackedNR 1 ENGINE PYLON PANEL NR 438CR IS CRACKED. WELD REPAIRED CRACKS IAW DAC DRWG AUB 7120; DPS 4.801 AND DPS 10.225.Mar 17, 2008 · N384FE · Doug MD1010FSDR 08FDEA00952Drain Line · crackedNR 1 PYLON HYD/FUEL DRAIN PAN HAS A 3/4 INCH CRACK ON THE DRAIN TUBE AT 837. REMOVED DRAIN PAN REF A310-300 SRM 51-40-21; PG 7. WELD REPAIRED REF AEROSPATIALE DWG IA-546-10805 AND INSTALLED DRAIN PAN REF A310-300 SRM 51-40-21; PG 7.Mar 14, 2008 · N803FD · Airbus A310203SDR HALA0800409Channel · crackedLT STRUT AFT FAIRING CHANNEL, INBD CRACKED AT FWD END. I/B AFT FAIRING CHANNEL PT NR 313T1380-243. REPLACED IAW SRM 51-40-02, REV 76.Mar 13, 2008 · N594HA · Boeing 767332SDR 08FDEA00867Fairing · brokenNR 2 ENGINE AFT FAIRING (BEAVER TAIL), LOWER AFT CORNER, (INNER PAN) IS BROKEN OUT.Mar 11, 2008 · N384FE · Doug MD1010FSDR 08FDEA00823Drain · chafedNR 1 ENGINE PYLON AFT FAIRING LOWER PANEL 438EL HAS A CHAFED DRAIN TUBE. WELDED CHAFED AREA IAW DPS 10.225. MINOR REPAIR.Mar 10, 2008 · N384FE · Doug MD1010FSDR HALA0800395Bracket · crackedAPPROX 1/2" CRACK TO LIGHT STRUCTURE BRACKET RT ENGINE STRUT NAC STA 298.93 - 297, INBD SIDE ATOP AND FWD OF PANEL 447 ELX. BRACKET MEASURES APPROX 3 INCHES BY 1 INCH AND ATTACHES STRUT AFT TORQUE BOX TO SIDE PANELS, FWD AND ABOVE HYDRAULIC SHUTOFF VALVE. REMar 9, 2008 · N594HA · Boeing 767332SDR HALA0800371Acoustic Liner · damagedACOUSTIC LINER DAMAGE OK TO CONTINUE PER M105 FILE NR 478112. REPAIR PER AMM 72-34-01, NO LATER THAN 3/31/08. OK TO CONTINUE PER GMM4-3.1Mar 9, 2008 · N478HA · Boeing 717200SDR SWIA200819373Nacelle · damagedLEFT LOWER NACELLE AT OIL COOLER AREA DAMAGED FROM BIRD STRIKE. REPAIRED THE LOWER NACELLE BIRD STRIKE DAMAGE AREA IAW EMB SRM 51-40-22, 51-40-06, 51-22-00 AND 51-25-00. Mar 7, 2008 · N581SW · Emb EMB120ERSDR 08FDEA00774Bracket · damagedFOUND ON PYLON NR 3 ON STA YN=240 THE BRACKET WITH DAMAGED AND DO NOT INSTALLED FOR DWG REPLACE WEB FOR SRM 51-33-01 VOL II AND DWG AUB7027.Mar 7, 2008 · N68059 · Doug DC1010FSDR HALA0800373Attach Bracket · gougedNR 2 ENGINE NOSE INLET COWL TO FAN CASE ATTACHMENT BRACKET AT 3 O'CLOCK POSITION GOUGED. DAMAGE AT 3 O'CLOCK ON NOSE COWL AFT BULKHEAD INNER RING BLENDED IAW SRM 54-11-02/1A01, FIG 101, DETAIL 111, WITHIN SRM LIMITS.Mar 6, 2008 · N594HA · Boeing 767332SDR 08FDEA00761Fairing · crackedNR 1 ENGINE AFT PYLON FAIRING; AFT WELDED SKIN IS CRACKED. STOP DRILLED THE CRACK IAW SRM 54-55-51 FIG 201.FABRICATED REPAIR IAW SRM 54-55-51 FIG 201 & EA 06-5480-118441. INSTALLED REPAIR IAW SRM 54-55-51 FIG 201 & EA 06-5480-118441. MINOR REPAIR.Mar 6, 2008 · N803FD · Airbus A310324SDR 08FDEA00750Support Bracket · crackedNR 2 PYLON FIRE EXTINGUISHER NR 2 SUPPORT BRACKET IS CRACKED. CLEANED MARKED AREA PER AMM 12-21-11-0. ACCOMPLISHED HFEC IAW NTM 51-10-01 PT 6 USING T8257A. NO CRACKS NOTED. PRIMED CLEANED AREA PER SRM 51-23-10.Mar 6, 2008 · N425FE · Airbus A310203SDR 08FDEA00720Drain Pan · crackedNR 2 ENGINE PYLON HYDRAULIC/FUEL DRAIN PAN IS CRACKED IN 4 PLACES ON THE BOTTOM SIDE OF THE PAN. REMOVED DRIP PAN IAW AIRBUS A310 SRM 51-40-21; PG 7, WELD REPAIRED CRACKS IAW AEROSPATIALE DWG 41A54610805. REINSTALLED DRIP PAN IAW AIRBUS A310 SRM 51-40-21; PGMar 5, 2008 · N803FD · Airbus A310324SDR KCSA081140Stiffener · damagedNR 2 PYLON AT NAC STA-248 O/B LOWER STIFFENER DAMAGED.Mar 5, 2008 · N715CK · Boeing 747209BSDR ABXA080090Attach Angle · crackedINBOARD ATTACH ANGLE FOR PANEL 437DB HAD APPROXIMATELY 3 INCH CRACK NEAR BOTTOM. REMOVED AND REPLACED CRACKED ATTACH PART IAW B767 SRM 51-40-2.Mar 4, 2008 · N788AX · Boeing 767281SDR 2008UALA01191Structure · chafedNR 2 PYLON RIGHT SIDE IS CHAFED IN 5 SPOTS AT NAC 195. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA, FABRICATED & INSTALLED DOUBLER REPAIR.Mar 3, 2008 · N651UA · Boeing 767322SDR ABXR080106Fitting · crackedPYLON UPPER REAR SPAR STRAP CLIP JUST INSIDE PYLON CRACKED. REMOVED, FABRICATED, AND INSTALLED NEW CLIP IAW DC9 SRM 51-30-1 AND 51-30-5.Mar 3, 2008 · N205US · Doug DC932FSDR UPS08551740Angle · damagedINSPECTION TYPE:4 DAMAGED I/B SIDE OF FORWARD FAIRING "L" ANGLE ON NR 1 ENGINE PYLON. REPAIRED PER ER 08-1337 AND SRM 51-40-02.Feb 29, 2008 · N435UP · Boeing 75724APFSDR DL76L080296Angle · crackedNR 1 ENGINE PYLON MIDSPAR CLOSE OUT ANGLE FOUND CRACKED. REMOVED AND REPLACED CLOSE OUT ANGLE.Feb 29, 2008 · N177DN · Boeing 767332SDR 08FDEA00665Channel · fracturedNR 2 PYLON AFT POWER FAIRING 485 AL AFT SUPPORT CHANNEL HAS A FRACTURE AT THE OUTBD EDGE. REMOVED CHANNEL & FABRICATE WEB & CHANNEL ON OPS 00748 & 00749. ASSEMBLED & INSTALLED TO NR 2 PYLON IAW SRM 51-40-01 PG 7.Feb 29, 2008 · N803FD · Airbus A310324
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