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 A6WA201040967Separator · wornLT PYLON PANEL 412DB SEPARATORS ARE KNIFE EDGE. R & R SEPARATORS IAW SRM 51-42-06.Dec 21, 2010 · N454AW · Cndair CL6002B19SDR KCSA101197Skin · damagedNR4 PYLON INBD SKIN DAMAGED ALONG BOTTOM EDGE, NAC STA 200.Dec 19, 2010 · N701CK · Boeing 747236BSDR KCSA101196Skin · damagedNR3 PYLON INBD SKIN DAMAGED ALONG BOTTOM EDGE, NAC STA 215 TO 222.Dec 19, 2010 · N701CK · Boeing 747259BSDR A6WA201140014Plate · corrodedLT PYLON T/E UPPER BONDING PLATES (2 EA) CORRODED. R & R LT PYLON T/E UPPER BONDING PLATES PN 601-37012-33 IAW SRM.Dec 15, 2010 · N457AW · Cndair CL6002B19SDR GTIA1000180Skin · corrodedENGINE NR 2, PYLON AFT FIXED FAIRING, OTBD/RT LATERAL SKIN PANEL WITH CORROSION PANEL (P/N: D5453005220300) THE CORROSION REQUIRES A MAJOR REPAIR.Dec 14, 2010 · N526NK · Airbus A319132SDR GTIA1000179Skin · corrodedENGINE NR 2, PYLON AFT FIXED FAIRING, INBD/LT LATERAL SKIN PANEL WITH CORROSION PANEL (PN: D5453005220200) NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.Dec 14, 2010 · N526NK · Airbus A319132SDR GTIA1000178Skin · corrodedENGINE NR 1, PYLON AFT FIXED FAIRING, INBD/RT LATERAL SKIN PANEL WITH CORROSION PANEL (PN: D5453005220300) THE CORROSION REQUIRES A MAJOR REPAIR.Dec 14, 2010 · N526NK · Airbus A319132SDR GTIA1000177Skin · corrodedENGINE NR 1, PYLON FIXED FAIRING, OTBD/LT LATERAL SKIN PANEL WITH CORROSION (PANEL PN: D5453005220200) THE CORROSION REQUIRES A MAJOR REPAIR.Dec 14, 2010 · N526NK · Airbus A319132SDR EE4Y100557Skin · corroded(EE4Y) ENGINE NR 2, PYLON AFT FIXED FAIRING, OTBD/RT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.Dec 14, 2010 · N526NK · Airbus A319132SDR EE4Y100556Skin · corroded(EE4Y) ENGINE NR2, PYLON AFT FIXED FAIRING, INBD/LT LATERAL SKIN PANEL WITH CORROSION (PANEL PN: D5453005220200) NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.Dec 14, 2010 · N526NK · Airbus A319132SDR EE4Y100555Skin · corroded(EE4Y) ENGINE NR1, PYLON AFT FIXED FAIRING, INBD/RT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.Dec 14, 2010 · N526NK · Airbus A319132SDR EE4Y100554Skin · corroded(EE4Y) ENGINE NR 1, PYLON AFT FIXED FAIRING, OTBD/LT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.Dec 14, 2010 · N526NK · Airbus A319132SDR DALA1035585533Skin · crackedDURING M-CHECK FOUND NR2 PYLON OTBD AFT OF CTR T/R INSOLATOR ACCESS PANEL CUT OUT CRACKED. REMOVED OTBD T/R HINGE AND 1EA DOUBLER FROM NR2 PYLON OTBD IAW SRM 51-40-02, PAGE 240, CUT OUT THE CRACK DAMAGE IAW ERA 487267-14, REV 0, STEPS 5 FAB REPAIR DOUBLER IAWDec 13, 2010 · N533US · Boeing 757251SDR ABXA201012150172Skin · chafedNR 2 STRUT RT SIDE, THE SURFACE OF THE STRUT IS CHAFED (6 INCHES LONG) AND DENTED JUST BELOW AN ANGLE WHERE THE UPPER SECTION OF THE REVERSERS AFT LOWER CORNER MEETS THE STRUT. REPAIRED CHAFED AND DENTED AREA IAW REA B654-59111-MR.Dec 12, 2010 · N786AX · Boeing 767281SDR GTIA1000159Panel · corrodedENG NR 2, PYLON AFT FIXED FAIRING, OTBD/RT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.Dec 7, 2010 · N525NK · Airbus A319132SDR GTIA1000158Panel · corrodedENGINE NR 2, PYLON AFT FIXED FAIRING, INBD/LT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.Dec 7, 2010 · N525NK · Airbus A319132SDR GTIA1000157Panel · corrodedENGINE NR1, PYLON AFT FIXED FAIRING, INBD/RT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.Dec 7, 2010 · N525NK · Airbus A319132SDR GTIA1000156Fairing · corrodedENGINE NR1, PYLON AFT FIXED FAIRING, OTBD/LT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.Dec 7, 2010 · N525NK · Airbus A319132SDR EE4Y100524Panel · corrodedNR 2 PYLON AFT FIXED FAIRING, OTBD/RT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.Dec 7, 2010 · N525NK · Airbus A319132SDR EE4Y100523Panel · corrodedNR 2 PYLON AFT FIXED FAIRING, INBD/LT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.Dec 7, 2010 · N525NK · Airbus A319132SDR EE4Y100522Panel · corrodedNR 1 PYLON AF FIXED FAIRING, INBD/RT LATERAL SKIN PANEL WITH CORROSION. CORROSION REQUIRES A MAJOR REPAIR.Dec 7, 2010 · N525NK · Airbus A319132SDR EE4Y100521Panel · corrodedNR 1 PYLON AFT FIXED FAIRING, OTBD/LT LATERAL SKIN PANEL WITH CORROSION. THE CORROSION REQUIRES A MAJOR REPAIR.Dec 7, 2010 · N525NK · Airbus A319132SDR CA101206015Panel · missingON ARRIVAL AFTER A FLIGHT, IT WAS NOTICED THAT INSP PANEL 443BR ON THE OTBD SIDE OF THE NR 2 ENGINE PYLON WAS MISSING. PANEL PN 311N5049-139, IPC 54-53-01-05, ITEM 175. THE PANEL WAS REPLACED. ACFT TSN 46089, CSN 14630. THIS IS THE SECOND PANEL TO GO MISSINGDec 5, 2010 · Boeing 75728ASDR EE4Y100518Panel · corrodedENGINE NR 1, PYLON AFT FIXED FAIRING, INBD/RH LATERAL SKIN PANEL WITH CORROSION (PANEL PN: D5453005220300) NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.Dec 2, 2010 · N524NK · Airbus A319132SDR EE4Y100512Panel · corrodedENGINE NR1, PYLON AFT FIXED FAIRING, OTBD/LT LATERAL SKIN PANEL WITH CORROSION (PANEL PN: D5453005220300) THE CORROSION REQUIRES A MAJOR REPAIR.Dec 2, 2010 · N524NK · Airbus A319132SDR A6WA201040896Access Panel · crackedLT JETPIPE FAIRING CRACKED NEXT TO LOWER BOLT ACCESS PANEL CRACKED. REPAIRED LT JETPIPE FAIRING CRACK NEXT TO LOWER BOLT ACCESS PANEL BY CALLING OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW CMM 78-11-50 REPAIR.Dec 1, 2010 · N414ZW · Cndair CL6002B19SDR EE4Y100519Panel · corrodedENGINE NR 2, PYLON AFT FIXED FAIRING, OTBD/RT LATERAL SKIN PANEL WITH CORROSION, (PANEL PN: D54530052220300) THE CORROSION REQUIRES A MAJOR REPAIR.Dec 1, 2010 · N524NK · Airbus A319132SDR EE4Y100513Panel · corrodedENGINE NR 2, PYLON AFT FIXED FAIRING, INBD/LT LATERAL SKIN PANEL WITH CORROSION (PANEL PN: D5453005220200) THE CORROSION REQUIRES A MAJOR REPAIR.Dec 1, 2010 · N524NK · Airbus A319132SDR CA101202003Panel · missingON ARRIVAL AFTER A POSITIONING FLIGHT FROM MANCHESTER, UK, IT WAS NOTICED THAT INSPECTION PANEL 443HL ON THE INBOARD SIDE OF THE NR 2 ENGINE PYLON WAS MISSING. PANEL P/N 311N5049-155, IPC 54-53-01-05, ITEM 208. THE PANEL WAS REPLACED. AIRCRAFT TSN 46050, CSNov 30, 2010 · Boeing 75728ASDR A6WA201040895Skin · chafedRT UPPER NOSE COWL AFT EDGE STRIP IS CHAFED. R & R RT UPPER NOSE COWL AFT EDGE STRIP IAW AMM 51-42-06.Nov 28, 2010 · N414ZW · Cndair CL6002B19SDR UALA2010112904368Skin · damagedLARGE FASTENER MISSING FROM INBD SIDE NR 2 ENGINE PYLON, HOLE IS JUST IN FRONT OF PANEL 447ELX. BOLT IS THE FILLER FOR THE BOOTSTRAP SLING. NOT STRUCTURAL. TEMPORARY REPAIR WITH TAPE. REPLACED IN 5 CYCLES. SEE SERVICE TIP 54-52-01. IPC REF 54-51-57 ITEM 8Nov 27, 2010 · N660UA · Boeing 767322SDR DALA1034745646Skin · crackedDURING L-CHECK FOUND NR 2 PYLON STRUT LT SKIN PANEL, CRACKED AT FWD UPPER CORNER INNER AND OUTER SKIN APPROX .5" IN LENGTH. NR 2 PYLON STRUT LT SKIN PANEL REPAIRED IAW EM 5451-01010-02C.Nov 26, 2010 · N546US · Boeing 757251SDR DALA1034735646Skin · crackedDURING L-CHECK FOUND NR 2 PYLON STRUT RT SKIN PANEL CRACKED FOUND AT FWD UPPER CORNER OUTER SKIN APPROX .3750" IN LENGTH. NR 2 PYLON STRUT RT SKIN PANEL REPAIRED IAW EM 5451-01010-02D.Nov 26, 2010 · N546US · Boeing 757251SDR A6WA201040873Skin · chafedLT LOWER CORE COWL CHAFED FROM BLOCKER DOOR NEXT TO FWD LATCHES BLENDED DAMAGE IAW REO 601R-71-12-232, REV D AND WAS FOUND TO BE WITHIN ALLOWABLE LIMITS. DAMAGE MEASURES 4.00 LONG, 0.25 WIDE AND .007 DEEP. TREATED AREA IAW CMM 20-01-11 AND SRM 51-25-06.Nov 23, 2010 · N414ZW · Cndair CL6002B19SDR F3LA2010113000555Access Panel · crackedC-CHECK: NON ROUTINE N0565; LT PYLON ACCESS PANEL NR413DL CRACKED. IAW SRM 54-50-80 AND PMS 01-04-21, STOP DRILLED CRACK ENDS AND WELDED.Nov 22, 2010 · N922FR · Airbus A319111SDR F3LA2010113000554Skin · crackedC-CHECK: NON ROUTINE N0179; RT PYLON UPPER PANEL NR 423DL HAS A 4.0" CRACK AROUND LOUVERS AND ABOUT 1.0" IN LENGHT. IAW SRM 54-52-11 AND PMS 01-04-21, STOP DRILLED CRACK AND WELDED.Nov 22, 2010 · N922FR · Airbus A319111SDR F3LA2010113000553Skin · crackedC-CHECK: NON ROUTINE N0178; NR2 ENGINE PYLON UPPER PANEL NR423DL HAS A 1 EACH CRACK ON THE INTERIOR SIDE AT THE CUT OUT ABOUT .25" IN LENGHT. IAW SRM 54-52-11, STOP DRILL CRACK ENDS AND WELDED IAW PMS 01-04-21.Nov 22, 2010 · N922FR · Airbus A319111SDR A6WA201040868Plate · corrodedRT UPPER PYLON T/E HAS 2 EA BONDING PLATES (PN 601-37012-33) CORRODED. R & R RT UPPER PYLON T/E BONDING PLATES PN 601-37012-33 IAW SRM 51-22-00.Nov 18, 2010 · N421ZW · Cndair CL6002B19SDR GTIA1000117Panel · corrodedDURING INSPECTION, DISCOVERED THAT THE NR1 ENGINE PYLON AFT FIXED FAIRING, OTBD PANEL, TO BE CORRODED BEYOND SRM ALLOWABLE LIMITS. A NEW PANEL WAS FABRICATED AND REPLACED.Nov 18, 2010 · N523NK · Airbus A319132SDR GTIA1000116Panel · corrodedDURING INSPECTION, DISCOVERED THAT THE NR1 ENGINE PYLON AFT FIXED FAIRING, INBD PANEL, TO BE CORRODED BEYOND SRM ALLOWABLE LIMITS. A NEW PANEL WAS FABRICATED AND REPLACED.Nov 18, 2010 · N523NK · Airbus A319132SDR GTIA1000113Panel · corrodedDURING INSPECTION, DISCOVERED THAT THE NR2 ENGINE PYLON AFT FIXED FAIRING, OTBD PANEL, TO BE CORRODED BEYOND SRM ALLOWABLE LIMITS. A NEW PANEL WAS FABRICATED AND REPLACED.Nov 18, 2010 · N523NK · Airbus A319132SDR GTIA1000112Panel · corrodedDURING INSPECTION, DISCOVERED THAT THE NR2 ENGINE PYLON AFT FIXED FAIRING, INBD PANEL, TO BE CORRODED BEYOND SRM ALLOWABLE LIMITS. A NEW PANEL WAS FABRICATED AND REPLACED.Nov 18, 2010 · N523NK · Airbus A319132SDR UALA2010111704258Skin · crackedNR 1 ENGINE INLET COWL LIP SKIN HAS 7 INCH CRACK IN AREA K1. REPLACED NOSE COWL ASSY PER MM, OP CHECKS NORMAL ON ENGINE RUN.Nov 17, 2010 · N466UA · Airbus A320232SDR USAA2010121793150Skin Panel · crackedMCN - MAJOR REPAIR - C20 CHECK - NR 2 PYLON SKIN PANEL CRACKED AT NAC STATION 224. REPAIRED NR 2 PYLON SKIN PANEL AT NAC STATION 224 IAW ER 03-5433-01037-DL1.Nov 16, 2010 · N302AW · Boeing 7373G7SDR A6WA201040915Panel · chafedPYLON PANEL 422DB SEPARATORS ARE KNIFE EDGE. R & INSTALLED PN 601R37138-26 AND PN 601R37138-28 IAW SRM 51-42-06.Nov 15, 2010 · N421ZW · Cndair CL6002B19SDR GTIA1000153Skin · unknownFABRICATE (1 EA) RT PYLON SKIN PANEL LOCATION, INBD SECTION. FABRICATED NR2 ENGINE PYLON INBD SKIN PANEL IAW APPROVED SPECIFICATIONS DOCUMENTED ON FORM MX FR 039.Nov 15, 2010 · N522NK · Airbus A319132SDR FDEA201011154365Skin · crackedNR1 ENG STRUT AFT FAIRING DRAIN TUBE EXIT COVER HAS VERY SMALL CRACK ON LWR EDGE. NR 1 ENGINE STRUT AFT FAIRING DRAIN TUBE EXIT COVER T/E SKIN. R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Nov 15, 2010 · N944FD · Boeing 7572G5SDR EE4Y100493Skin · erodedENGINE NR 1, PYLON AFT FIXED FAIRING, OTBD/ LT LATERAL SKIN PANEL WITH EROSION FROM STA867/ RIB AND STA928/ RIB15. (SKIN PANEL PN: D54530052202) NOTE: THE SKIN EROSION REQUIRES A MAJOR REPAIR.Nov 12, 2010 · N522NK · Airbus A319132SDR EE4Y100492Skin · erodedENGINE NR 1, PYLON AFT FIXED FAIRING, LT LATERAL SKIN PANEL WITH EROSION FROM STA867/ RIB12 TO STA928/ RIB15. (SKIN PANEL PN: D54530052203) NOTE: THE SKIN EROSION REQUIRES A MAJOR REPAIR.Nov 12, 2010 · N522NK · Airbus A319132SDR EE4Y100491Skin · erodedENGINE NR 2, PYLON AFT FIXED FAIRING, LT LATERAL SKIN PANEL WITH EROSION FROM STA 867/ RIB12 TO STA 928/ RIB15. (SKIN PANEL PN: D54530052202) NOTE: THE SKIN EROSION REQUIRES A MAJOR REPAIR.Nov 12, 2010 · N522NK · Airbus A319132
Back to JASC 5414