JASC 5414

Service difficulty reports · 4,361

Reports filed under 5414 · Nacelle/Pylon, Plate/Skin, 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 = '5414'
  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 2000UALA00294Fillet · looseRETURNED TO SFO AFTER NR 1 ENG COWL FILLET AT TOP PYLON TO COWL SECTION CAME LOOSE.May 31, 2000 · N818UA · Airbus A319131SDR 0002206739Skin · crackedDURING LINE MAINTENANCE INSPECTION FOUND CRACK ON NR 1 PYLON INBOARD SKIN AT SLOT SEAL CUTOUT, NACELLE STATION 180. REPAIRED PER EA 67-170461.May 30, 2000 · N639US · Boeing 747251FSDR AT0000313Skin · corrodedFOUND LEFT PYLON, BOTTOM SIDE CORRODED. CUT OUT CORRODED AREA, FABRICATED FILLER AND DOUBLER ON TRAVELER. TREATED, PRIMED AND INSTALLED FILLER AND DOUBLER IAW DC9 SRM 54-01 FIGURE 4, 51-30-2 AND 51-10-3.May 19, 2000 · N818AT · Doug DC932SDR COMA0010123Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.May 19, 2000 · N263CA · Emb EMB120RTSDR COMA0010122Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.May 19, 2000 · N263CA · Emb EMB120RTSDR COMA0010121Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.May 19, 2000 · N263CA · Emb EMB120RTSDR COMA0010120Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.May 19, 2000 · N263CA · Emb EMB120RTSDR TWAA0008308Skin · crackedDURING CC, FOUND RT PYLON, UPPER SKIN CRACKED AT THE TOP OF THE PYLON ON THE WEDGE APPROXIMATELY 11 INCHES FROM THE FIXED COWL AFT EDGE, OUTBOARD EDGE OF THE SKIN. STOP DRILLED CRACKS, MADE DOUBLER SAME GUAGE THICKNESS AS SKIN AND INSTALLED WITH .125 INCH MS2May 17, 2000 · N978Z · Doug DC931SDR DL757000973Skin · crackedA .75 INCH CRACK WAS FOUND IN THE I/B STRUT SIDE SKIN ON THE NR 2 PYLON UNDER AN EXISTING REPAIR DOUBLER COMMON TO THE FWD ACCESS HOLE. REPAIRED PER ERA 368149-14, REV B.May 17, 2000 · N631DL · Boeing 757232SDR COMA0010103Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5400-432-01I, THE LT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.May 11, 2000 · N258CA · Emb EMB120RTSDR COMA0010102Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-01I, THE RT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGE PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.May 11, 2000 · N258CA · Emb EMB120RTSDR COMA0010101Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.May 11, 2000 · N258CA · Emb EMB120RTSDR COMA0010098Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3364-1, REV IR, 7-25-99.May 11, 2000 · N258CA · Emb EMB120RTSDR L1GA200000087Panel · crackedA CRACK WAS FOUND ON THE NUMBER 1 ENGINE PYLON PANEL 8210A FROM THE EDGE TO THE FASTENER HOLE.May 10, 2000 · N27509 · Doug DC932SDR MALA000323Skin · chafedFOUND DURING C-CHECK, RT NACELLE INBOARD SIDE IS CHAFED WHERE THE WING LEADING EDGE SEATS CONTACT, REFER CELSIUS TASK CARD 4529.May 9, 2000 · N407XJ · Saab 340BSDR RRXA003172Skin · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE NR 2 ENGINE PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED PART IAW DC-8 SRM 51-1-20D.May 8, 2000 · N990CF · Doug DC862SDR RRXA003167Skin · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE NR 2 ENGINE PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D.May 8, 2000 · N990CF · Doug DC862SDR P2EA00193Skin · wornSJO - DURING C-CHECK, FOUND THE NR 1 ENGINE NOSE COWL UPPER SECTION SKIN WITH WEAR LENGTH 10 INCH, WIDTH .25 INCH, DEPTH .025 INCH. REPAIRED THE NR 1 ENGINE NOSE COWL UPPER SECTION SKIN IAW COOPESA EO NR COO-3-54-317-00 DATED MAY 12, 2000. (M)May 8, 2000 · N209US · Boeing 737222SDR P2EA00187Panel · delaminatedSJO - DURING C-CHECK, FOUND THE NR 1 ENGINE PYLON UPPER PANEL WITH DELAMINATED, 14 INCHES IN LENGTH, AND 8 INCHES WIDE. REPAIRED THE NR 1 ENGINE PYON UPPER PANEL IAW COOPESA EO NR COO-CMP-3-57-308-00. (M)May 4, 2000 · N209US · Boeing 737222SDR 0001536718Skin · crackedDURING LINE MAINTENANCE INSPECTION FOUND CRACK IN NR 4 PYLON INBOARD SKIN, SLOT SEAL CUTOUT, NAS STATION 180. REPAIRED PER EA 67-175573.May 2, 2000 · N618US · Boeing 747251FSDR USAA000660Doubler · crackedCLT - FOUND DOUBLER CRACKED 1 INCH, INSIDE ACCESS 4336R, NR 1 PYLON CUTOUT. INSTALLED DOUBLER PER EA 67093. (M)May 1, 2000 · N604AU · Boeing 757225SDR USAA000661Doubler · crackedCLT - FOUND DOUBLER CRACKED 1 INCH, NR 1 PYLON INSIDE ACCESS PANEL 433AL CUTOUT. INSTALLED DOUBLER PER EA 67094. (M)May 1, 2000 · N604AU · Boeing 757225SDR L1GA200000063Web · crackedCRACK CTR WEB OF TOP RT PYLON.Apr 28, 2000 · N14534 · Doug DC932SDR DL767000859Brace · mismanufacturedNR 1 ENGINE DIAGIONAL BRACE REPLACED WITH NEW THREE PIECE DIAGONAL BRACE ASSY TO MEET AD 200-07-05 REQUIREMENTS. NEW DIAG BRACE ASSY 0.033 INCH TOO SHORT WITH MAXIMUM SHIMMING ALLOWANCES. FABRICATED THICKER SHIMS WITH FAA APPROVAL. CORRECTIVE ACTION: 33432Apr 28, 2000 · N101DA · Boeing 767232SDR 0001866304Skin · crackedDURING ''''H'''' CHECK, FOUND CRACK ON NR 1 PYLON INBOARD SKIN AT PANEL 452ER CUTOUT, NACELLE STATION 293. REPAIRED PER EA 63-175731.Apr 27, 2000 · N664US · Boeing 747451SDR DL757000820Skin · crackedNR 1 PYLON CRACKED AT PREVIOUS REPAIR, N/R 610, UPPER FWD CORNER / CRACK LOWER AFT N/R 611 / PREVIOUS REPAIR SURFACE AND FASTENER DAMAGE, N/R 612. REPAIRED PER SRM 54-51-01-2-203.Apr 26, 2000 · N629DL · Boeing 757232SDR CALA0000551Skin · crackedNR 1 PYLON CRACK IN CUT-OUT FOR PANEL 5724 (1). REPAIRED PER EC/RA 5430-01204.Apr 25, 2000 · N16339 · Boeing 7373T0SDR CALA0000511Skin · crackedCRACK ON O/B SIDE OF ACCESS PANEL CUTOUT FOR PANEL 5727L NR 1 (1 INCH). STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER EC/RA 5430-01230.Apr 23, 2000 · N16339 · Boeing 7373T0SDR EIAA2000098Doubler · crackedHAECO-HKG - C6/D-CHECK - PYLON NR 1 RT, NR 3 LT, AND NR 4 LT AT NAC STA 180 DOUBLERS FOUND CRACKED. TRIMMED OFF CRACKED SKIN, NDT INSPECTED, FILLER REPAIRED, AND DOUBLERS INSTALLED PER BOEING MESSAGE EVR-HKG-00-00036H/-00037H/-00044H AND HAECO REPAIR SCHEMES Apr 21, 2000 · N482EV · Boeing 747212BSDR QXEA0001120Skin · bentPDX - NR 2 ENGINE NACELLE SKIN BENT AND RIVET PULLED THROUGH, BELOW STUBWING, AT FORWARD CORNER BY NOSE COWL. REPAIRED IAW FOKKER SRM 51-11-8 AND SRM 54-02-02, PAGE 2, FIGURE 1.Apr 12, 2000 · N494US · Fokker F28MK4000SDR L1GA200000018Panel · crackedCRACK FOUND ON NR 2 PYLON PANEL NR 8210A WITH ELONGATED SCREW HOLE.Apr 10, 2000 · N12508 · Doug DC932SDR L1GA200000010Skin · crackedCRACK FOUND ON RIGHT HAND PYLON SKIN AT STATION 1084.Apr 10, 2000 · N12508 · Doug DC932SDR MALA000263Skin · chafedRT NACELLE INBOARD SKIN IS CHAFED. DISCOVERED DURING HEAVY CHECK AND REPAIRED IAW EO554033.Apr 7, 2000 · N107XJ · Saab SF340ASDR 0001526634Skin · crackedDURING M CHECK, FOUND CRACK IN 3 INCH LONG CRACK ON NR 4 PYLON SKIN INBOARD SIDE, FORWARD OF SLOT SEAL AT APPROX NAS STATION 173. REPAIRED PER EA66-175083.Apr 6, 2000 · N634US · Boeing 747227BSDR CALA0000342Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN RT PYLON SIDEWALL INNER SKIN AT ACCESS NR 5824R. A DOUBLER WAS INSTALLED IAW ECRA 5430-01204.Mar 26, 2000 · N14336 · Boeing 7373T0SDR CA000330004Skin · cracked(CAN) DURING SCHEDULED MAINTENANCE, A CRACK WAS FOUND ON THE LOWER PYLON SKIN. THE CRACKS WERE FOUND ON TWO RIVET ROWS PARALLEL TO THE C/L OF THE AIRCRAFT. THE CRACKS WERE APPROXIMATELY SIX INCHES LONG.Mar 23, 2000 · Cessna 525SDR AU000210Panel · missing(AUS) RIGHT NACELLE FUEL DRAIN PANEL NOT REINSTALLED FOLLOWING MAINTENANCE. SAFETY PLUG AND LOCKWIRE ALSO MISSING.Mar 17, 2000 · Beech B200CSDR UIEA0017Skin · damagedDURING INTERNAL INSPECTION OF PYLON NR 1, NR 2, NR 3 STRUCTURE SURROUNDING THE PRECOOLER EXHAUST EXIT AREA FOUND METAL DISCOLORED AND EXTERNAL SKIN CREASED. OVER TEMPERATURE ANALYSIS INDICATED TEMPER LOSS AND HEAT RELATED DAMAGE. AFFECTED STRUCTURE AND SKIN Mar 17, 2000 · N516MC · Boeing 747243BSDR 0000976730Skin · crackedDURING A NON ROUTINE FLIGHT CHECK, A CRACK WAS FOUND ON THE NUMBER 3 INBOARD SKIN AT THE SLOT SEAL CUTOUT, FORWARD OF NACELLE STATION 180. THE REPAIR WAS ACCOMPLISHED DURING THE HEAVY CHECK ON EA67-170848.Mar 16, 2000 · N630US · Boeing 7472J9FSDR MALA000178Skin · chafedDURING HEAVY CHECK, LT INBD NACELLE SKIN WAS CHAFED. MX REPAIRED IAW EOS54028Mar 15, 2000 · N89XJ · Saab SF340ASDR 0000986730Skin · crackedDURING FLIGHT LINE CHECK, TWO CRACKS WERE FOUND AT NACELLE STATION 226. THE FWD CRACK WAS 1.875 INCH UP FROM BOTTOM EDGE OF PYLON, AND AFT CRACK IS .25 INCH FROM RIVET ON BOTTOM EDGE. REPAIRED DURING HEAVY CHECK USING EA67-173156.Mar 12, 2000 · N630US · Boeing 7472J9FSDR UIEA01024Skin · wornDURING ROUTINE INSPECTION, FOUND NR 3 PYLON SKIN WORN AT NAC STATION 290 WL 145 R/S ACCESS PANEL. TRIMMED OUT WORN AREA. FABRICATED FILLER FROM CRES STEEL 301.5 HARD AND ALUMINUM DOUBLER. INSTALLED PER STANDARD PRACTICES. (M)Mar 9, 2000 · N808MC · Boeing 747212BSDR DHL200072441CAccess Panel · delaminatedFOUND AT C CHECK, NR 1 ENGINE PYLON ACCESS PANEL 5402 HAS DELAMINATION. INSTALLED BONDING REPAIR AT NR 1 ENGINE PYLON ACCSESS PANEL 5402 AS PER SRM 51-40-6 FIG 1.Mar 7, 2000 · N724DH · Boeing 727228SDR 0001146743Skin · crackedDURING COMMISSIONING CHECK, FOUND TWO SKIN CRACKS ON THE OUTER SKIN LAYER OF THE NR 1 PYLON. REPAIRED PER EA67-164988.Mar 7, 2000 · N643NW · Boeing 747249FSDR 0001136743Skin · crackedDURING COMMISSIONING CHECK, FOUND A CRACK ON THE OUTER SKIN LAYER OF THE NR 3 PYLON LT SIDE. REPAIRED PER EA67-164989.Mar 7, 2000 · N643NW · Boeing 747249FSDR 0001126743Skin · crackedDURING COMMISSIONING CHECK, FOUND CRACK ON RIGHT HAND SIDE OF OUTER SKIN LAYER ON THE NR 2 PYLON. REPAIRED PER EA67-164987.Mar 7, 2000 · N643NW · Boeing 747249FSDR TWAA0003811Thrust Reverser · chafedDURING CHECK-C MAINT, UNDER THE RT ENG THRUST REVERSER COWL, AREA ABOVE PYLON, ACCESS 426-BR HAD WEAR SPOTS FROM CHAFING SCREW CONTACT. INSTALLED DOUBLER PER SRM 54-50-01, FIG 206 PAGE 217.Mar 4, 2000 · N603TW · Boeing 767231SDR RRXA000358Skin · crackedDURING A MAINTENANCE VISIT FOUND SKIN CRACK NEAR TOP EXCITER RT FAN REV (1.5 INCH CRACK AND RIVET MISSING). REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK IAW DC-8 SRM 51-1-21 AND DER APPROVED EO 00-016.Feb 25, 2000 · N792FT · Doug DC873FSDR QXEA0000564Skin · delaminatedYYC - NR 2 ENGINE LOWER COWL ASSEMBLY HAS MULTIPLE COMPOSITE DELAMINATIONS AND PAINT CHIPS EXPOSING THE COMPOSITE STRUCTURE. REPAIRED IAW HORIZON AIR EA 9-71-162, DHC8 SRM 51-20-51.Feb 19, 2000 · N358PH · Dhav DHC8202SDR QXEA0000563Skin · delaminatedYYC - NR 1 ENGINE LOWER COWL ASSEMBLY HAS MULTIPLE COMPOSITE DELAMINATIONS AND PAINT CHIPS EXPOSING THE COMPOSITE STRUCTURE. REPAIRED IAW DHC8 SRM 54-70-21 AND SRM 54-70-26, PAGE 101 AND 102.Feb 19, 2000 · N358PH · Dhav DHC8202
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