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.
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
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 2003UALA00964Skin · crackedNR 2 PYLON OUTBOARD WEB CRACKED AT FORWARD ACCESS PANEL INBOARD SKIN LOWER AFT RADIUS. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED REPAIR OF PYLON SKIN PER MM 54-31-99 FIGURE 803.SDR 2003UALA00948Skin · crackedCRACK ON FWD UPPER PYLON SKIN INSIDE ACCESS PNL 432BR, NR 1 ENG. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR B30R20031120Skin · delaminatedDURING 100 HOUR INSPECTION, IT WAS DISCOVERED THAT THE INNER FIBERGLASS SKIN OF THE UPPER AFT SECTION OF THE ENGINE COWLING HAD DISBONDED FROM THE HONEYCOMB STRUCTURE OF THE COWLING. PRYROPEL INSULATION WAS TO BE INSTALLED WHILE THE AIRCRAFT WAS IN INSPECTION SDR ASAA0340355Skin · chafedGYR - DURING SI CHECK, FOUND NR 1 AND 2 PYLON INBOARD AND OUTBOARD STRUT SKINS CHAFING DAMAGE. REPAIRED IAW EA.SDR UPS03441577Skin · crackedINSPECTION TYPE: PFLT CRACK NR 3 ENGINE PYLON OUTBOARD SIDE AT PYLON EMERGENCY DRAIN TUBE. REPAIRED CRACK IAW 54-34-03 FIG 7.SDR AUS20031323Skin · cracked(AUS) RT ENGINE IB NACELLE SKIN CRACKED. STRINGER AND FORMER ALSO CRACKED.SDR USAA030317Skin · crackedPIT - FOUND SKIN CRACKED 1 INCH, NR 2 ENGINE PYLON PANEL 5727R. INSTALLED DOUBLER PER TR 54-30-07. (M)SDR USAA030316Skin · crackedFOUND SKIN CRACKED 1 INCH, NR 1 ENGINE PYLON PANEL 5727L. INSTALLED DOUBLER PER TR 54-30-07. (M)SDR 2003UALA00896Skin · crackedNR 2 PYLON OUTBOARD SIDE, FWD TORQUE BOX, NACELLE STA 240 AND WL 150, EXTERIOR SKIN IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED SIDE SKIN WITH DOUBLER-TRIPLER PER SRM 54-53-01.SDR AWXA200301520Skin · corrodedDURING C-06 CHECK CORROSION WAS FOUND ON INBOARD SKIN OF NR 1 PYLON AFT FIXED FAIRING. MAINTENANCE REMOVED CORRODED SKIN PANEL FROM NAC STA 8370 TO NAC STA 9782, INBOARD; FABRICATED A NEW REPLACEMENT SKIN PANEL PER DWG D54530052; INSTALLED REPAIR PART IAW A32SDR AWXA200301519Skin · corrodedDURING C-06 CHECK, CORROSION WAS FOUND ON OUTBOARD SKIN OF NR 2 PYLON AFT FIXED FAIRING. MAINTENANCE REMOVED CORRODED SKIN PANEL FROM NAC STA 8370 TO NAC STA 9782, OUTBOARD; FABRICATED A NEW REPLACEMENT SKIN PANEL PER DWG D54530052; INSTALLED REPAIR PART IASDR AWXA200301518Skin · corrodedDURING C-06 CHECK CORROSION WAS FOUND ON INBOARD SKIN OF NR 2 PYLON AFT FIXED FAIRING. MAINTENANCE REMOVED CORRODED SKIN PANEL FROM NAC STA 8370 TO NAC STA 9782; FABRICATED A NEW REPLACEMENT SKIN PANEL PER DWG D54530052; INSTALLED REPAIR PART IAW A320 SRM 51-4SDR QXEA200301389Panel · damagedPDX- CREASE IN PANEL 261GT AND HOLE IN NACELLE SKIN JUST ABOVE LEFT HAND COWL DOOR. REPAIRED IAW HORIZON AIR EA 2-54-194 AND RD8-54-1851.SDR AWXA200301469Skin · crackedMCN - MINOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND ON RT PYLON SKIN ON INBOARD SIDE BELOW PANEL 5843R, NAC STA 332.12 - 345.28. MAINTENANCE REMOVED DAMAGED SKIN ON RT PYLON INBOARD SIDE BELOW PANEL 5843R; FABRICATED NEW SKIN PER DWG 313A1355; INSSDR GKZR200479901Panel · crackedNR 4 INBOARD PYLON PLANK CRACKED ABOUT 30 SCREWS AFT FROM L/E BOTTOM ROW. REMOVED NR 4 ENGINE PYLON I/B PLANK PANEL FOR REPAIRS, FABRICATED REPAIR IAW DC-8 SRM 54-2-2, INSTALLED REPAIR IAW DC-8 SRM 54-2-2. REINSTALLED NR 4 ENGINE PYLON PLANK IAW DC-8 SRM 54-SDR AWXA200301400Skin · crackedMCN - MAJOR REPAIR - DURING C-13 CHECK A 1.125 INCH CRACK WAS FOUND IN LT PYLON ACCESS PANEL LANDING (5727L), NAC STA 220. MAINTENANCE PERFORMED HFEC INSPECTION TO IDENTIFY CRACK LENGTH; STOP DRILLED CRACK IN LT PYLON ACCESS PANEL LANDING; FABRICATED A REPAIRSDR EIA2003138Skin · chafedINSIDE LOWER SURFACE OUTBOARD SIDE NR 2 PYLON APPROX. 15 INCHES AFT OF ENGINE REAR MOUNT HAS LARGE CHAFED AREA. OB SIDE OF NR 2 PYLON SKIN REPAIRED IAW ECRA 482-54-177-2.SDR ASAA0380627Skin · crackedFOUND DURING 15K CHECK, LT ENGINE UPPER COWL IS CRACKED. REPAIRED PER EA 7110-01208 AND SRM 54-06. (M)SDR AWXA200301290Skin · corrodedDURING C-03 CHECK FOUND THE NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN PITTED. MAINTENANCE REMOVED PITTED NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN; FABRICATED A NEW SECTION OF SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 8 PG 8-12.SDR AWXA200301296Skin · corrodedMCN - MAJOR REPAIR - DURING C-03 CHECK THE NR 1 PYLON AFT FIXED FAIRING OUTBOARD SKIN WAS FOUND PITTED. MAINTENANCE REMOVED PITTED NR 1 PYLON AFT FIXED FAIRING OUTBOARD SKIN; FABRICATED NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 8-1SDR AWXA200301291Skin · corrodedDURING C-03 CHECK FOUND THE NR 1 PYLON AFT FIXED FAIRING INBOARD SKIN PITTED. MAINTENANCE REMOVED PITTED NR 1 PYLON AFT FIXED FAIRING INBOARD SKIN; FABRICATED A NEW SECTION OF SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 8 PG 8-12.SDR AWXA200301269Skin · corrodedDURING C-03 CHECK THE NR 2 PYLON AFT FIXED FAIRING OUTBOARD SKIN WAS FOUND PITTED. MAINTENANCE REMOVED DAMAGED NR 2 PYLON AFT FIXED FAIRING OUTBOARD SKIN; FABRICATED NEW REPLACEMENT SKIN PER A320 SRM 51-26-71, PG 1-13, FIG 1-5; INSTALLED REPAIR PART IAW A320 SDR 0704017Acoustic Panel · corrodedNR 1 ENG NOSE COWL ACOUSTIC PANEL CORRODED 6 TO 9 O'CLOCK.SDR AWXA200301172Skin Panel · corrodedDURING C-04 CHECK PITTING CORROSION WAS FOUND ON THE NR 2 PYLON AFT FIXED FAIRING OUTBOARD SKIN. MAINTENANCE REMOVED NR 2 PYLON AFT FIXED FAIRING OUTBOARD SKIN; FABRICATED A NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 7-12, & 21-22, FSDR AWXA200301326Skin · crackedDURING C-17 CHECK A .375 INCH CRACK WAS FOUND ON LT PYLON ACCESS LAND (5727L) NAC STA 219. MAINTENANCE STOP DRILLED CRACK LT PYLON ACCESS LAND NAC STA 219 AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A REPAIR DOUBLER AND FILLER WASDR AWXA200301175Skin Panel · corrodedDURING C-04 CHECK PITTING CORROSION WAS FOUND ON THE NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN. MAINTENANCE REMOVED NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN; FABRICATED A NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 7-11, FIG 2, 3.SDR AWXA200301116Skin · corrodedMCN - MAJOR REPAIR - DURING C-07 CHECK CORROSION WAS FOUND ON THE NR 2 PYLON AFT FIXED FAIRING AND PITTED ON THE INBOARD SIDE AT STA. 4067. MAINTENANCE FOUND IT TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE SKIN IAW A320 SRM 54-54-11 PG 2 AND 3 FIGSDR AWXA200301115Skin · corrodedMCN - MAJOR REPAIR - DURING C-07 CHECK CORROSION,PITTING WAS FOUND ON THE NR 2 PYLON OUTBOARD AFT FIXED FAIRING AT STA.4067. MAINTENANCE FOUND IT TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN IAW A320 SRM 54-54-11 PG. 2 AND 3 FIG. 1 SDR AWXA200301166Skin · corrodedDURING C-04 CHECK PITTING CORROSION WAS FOUND ON THE NR 1 PYLON AFT FIXED FAIRING INBOARD SKIN AT LOWER AFT AREA. MAINTENANCE REMOVED NR 1 PYLON AFT FIXED FAIRING INBOARD SKIN; FABRICATED A NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG SDR CALA0300539Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 1 ENGINE PYLON ACCESS PANEL NR 5727L CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230.SDR MALA030431Skin · crackedDURING 4K INSPECTION IN CWA, RT NACELLE OUTBOARD SKIN PANEL NS 203 IS CRACKED. MAINTENANCE ACCOMPLISHED REPAIR IAW SAAB REPAIR STATEMENT 340SDS006007, EO S54068. A/C RELEASE DATE 9/25/03. REFER TO 409 NR 193407 FOR DETAIL.SDR AWXA200301083Skin · erodedDURING C-04 CHECK THE NR 2 ENGINE PYLON AFT FAIRING INBOARD SKIN WAS FOUND ERODED AT THE LOWER SECTION. MAINTENANCE REMOVED ERODED INBOARD SKIN ON THE NR 2 ENGINE PYLON; FABRICATED A NEW SECTION OF REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11,SDR AWXA200301075Skin · erodedDURING C-04 CHECK THE LOWER SECTION OF THE NR 2 PYLON AFT FAIRING OUTBOARD SKIN WAS FOUND ERODED. MAINTENANCE REMOVED ERODED AFT FAIRING SKIN; FABRICATED NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 8-13, & A24-A25 FIG 2-4, & 61.SDR ASOA03432Panel · crackedDURING A GROUND INSPECTION IN DFW, THE LT ENGINE COWL ON THE UNDERSIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LOWER LEFT NOSE COWL PANEL ON THE LEFT ENGINE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)SDR 2003UALA00683Skin · damagedNR 2 NACELLE HAS A LARGE HOLE IN THE UPPER SKIN AT TWELVE O'CLOCK POSITION. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND LIP SPLICE.SDR AWXA200301074Skin · corrodedDURING C-04 CHECK THE NR 1 PYLON AFT FIXED FAIRING SKIN WAS FOUND PITTED. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED CORRODED AFT FIXED FAIRING SKIN; FABRICATED NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SDR SWIA200312489Clip · crackedRIGHT NACELLE FLAP WELL, OUTBOARD SKIN SUPPORT CLIP IS CRACKED OUT OF LIMITS. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SKIN SUPPORT CLIP OUTBOARD IN RIGHT NACELLE FLAP WELL PER SRM 51-40-02.SDR QXEA200301119Skin · crackedDIAPHRAM STRUCTURE AT AFT OUTBOARD SIDE OF LT HAND NACELLE STATION YW191.200 JUST BELOW UPPER WING SKIN TRAILING EDGE IS CRACKED. REPAIRED IAW Q400 SRM 51-40-11.SDR QXEA200301092Panel · crackedL-BRACKET SUPPORTING FILLET SKIN PANEL OF NACELLE FAIRING IS CRACKED AT INBOARD EDGE OF NR 1 NACELLE STATION YW139.00. REPAIRED IAW DHC-8 SRM 51-20-26, 51-40-11, RD 8-54-440 AND HORIZON AIR EA 2-54-182.SDR USAA030173Skin · crackedPIT - FOUND STRUT SKIN PANEL .75 INCH CRACK, PANEL DOUBLER NR 5827R STATION 206.50 TO 215.00. STOP DRILLED CRACK AND INSTALLED DOUBLER PER TR 54-30-07 AND EA 76836 AND SRM 51-20-10. (M)SDR QXEA200301073Skin · crackedRT NACELLE INBOARD INNER SKIN HAS A CRACK AT RIVET JUST AFT OF PANEL 425AL. REPAIRED IAW DHC-8 SRM 51-00-06, RD 8-54-1838 AND HORIZON AIR EA 2-54-179.SDR AWXA200301013Skin · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON NR 1 PYLON AFT FIXED FAIRING INBOARD SKIN. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED CORRODED SECTION OF NR 1 PYLON AFT FIXED FAIRING INBOARD SKIN; FABRICASDR AWXA200300982Panel · crackedDURING C-03 CHECK 2 EACH 1/4 INCHES CRACKS WERE FOUND ON NR 1 ENGINE PYLON PANEL (413DL) ON INBOARD SIDE. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK IS CONTAINED; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW A320 SSDR AWXA200301014Skin · corrodedDURING C-03 CHECK CORROSION WAS FOUND ON NR 1 PYLON TRAILING EDGE FAIRING INBOARD SKIN, PYLON STA 8370 TO 9278. MAINTENANCE REMOVED CORROSION ON NR 1 PYLON TRAILING EDGE FAIRING INBOARD SKIN AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED DAMAGED SKIN PSDR AWXA200301043Skin · crackedDURING C-16 CHECK A 1 INCH CRACK WAS FOUND ON NR 2 ENGINE LT FORWARD COWL INNER SKIN UNDER UPPER FORWARD SAFETY LATCH. MAINTENANCE CUTOUT CRACKED SKIN ON NR 2 ENGINE LT FORWARD COWL INNER SKIN NAC STA 120 RT; FABRICATED A DOUBLER, SHIM AND FILLER; INSTALLED RESDR CALA0300462Skin · crackedINSPECTION FOUND A 0.40 INCH CRACK IN PYLON CUTOUT FOR PANEL NR 5727, NR 1 ENGINE. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5430-01230.SDR AALA20030863Skin · crackedAFW - FOUND NR 2 ENGINE INBOARD SIDE PYLON TORQUE BOX AREA FOUND CRACK EXTENDING FROM ACCESS HOLE AFT. DAMAGED SKIN AREA REMOVED REPAIRED PER SRM REPAIR 54-52-01-2. (M)SDR QXEA200300934Panel · damagedUPPER TRANS COWL HAS FOD DAMAGE AT 12 O'CLOCK POSITION OF NR 1 ENGINE. REPAIRED IAW HORIZON AIR EO R-54-33 AND REO 670-54-23-129.SDR USAA030146Skin · crackedPIT - FOUND SKIN CRACKED 1 INCH, NACELLE STRUT SKIN CRACK AROUND PANEL 57271, LEFT PYLON. DOUBLER INSTALLED PER TR 54-30-07 AND EA 56543B. (M)SDR AWXA200300867Fairing · crackedMCN - MINOR REPAIR - DURING C-01 CHECK A 8.5 INCH CRACK WAS FOUND AT THE AFT END OF THE NR 1 PYLON INBOARD UPPER FAIRING WELDED ASSEMBLY, NAC STA 5369-6077, BETWEEN RIBS 7 & 8. MAINTENANCE REMOVED AND REPLACED WELDED ASSEMBLY INBOARD SIDE OF NR 1 PYLON IAW AMM
Back to JASC 5414