JASC 5414

Service difficulty reports · 4,360

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 REXA2014060400568Panel · chafedTASK CARD 900-71-430-103 TOP SIDE OF NR 1 ENG PYLON PANEL 433BT IS CHAFED OTBD AFT. LOCATED & DRILLED NEW PANEL FASTENER HOLES. REMOVED STIFFENERS FROM OLD PANEL & INSTALLED ON NEW PNL IAW SRM 51-42-00-001-001-A01. PAINTED NEW PNL IAW SRM 51-25-01-001-001-AJun 4, 2014 · N928XJ · Cndair CL6002D24SDR R61A201407290932Skin · dentedLEFT NACELLE INBD DENTED. MAINTENANCE REPAIRED IAW RD 8/4-54-1325.May 31, 2014 · N203WQ · Bombdr DHC8402SDR SWIA201437779Skin · crackedLT ENGINE NACELLE OTBD SIDE FWD OF FWD COWL DOOR SKIN CRACKED. REPAIRED DAMAGED SKIN ON LT ENGINE NACELLE OTBD SIDE FWD OF FWD COWL DOOR SKIN BY MEANS OF A DOUBLER REPAIR IAW ETD.May 24, 2014 · N584SW · Emb EMB120ERSDR AALA20140522008Skin · crackedNUMBER 1 PYLON OTBD SKIN AT LT PPS 156 CRACKED. REPAIR DOUBLER INSTALLED IAW EA B757-54-034667.May 22, 2014 · N652AA · Boeing 757223SDR AALA20140521019Skin · crackedNUMBER 1 PYLON OTBD SKIN & DOUBLER WERE FOUND CRACKED AT STATION 156. INSTALLED DOUBLER AT STATION 156.May 21, 2014 · N652AA · Boeing 757223SDR SWIA201438122Skin · crackedLEFT ENGINE NACELLE HAS A THREE INCH CRACK ON OUTBOARD AFT SKIN AT FLAP HINGE AREA. REPAIRED LT ENGINE NACELLE SKIN.May 19, 2014 · N223SW · Emb EMB120ERSDR ERAA20140030Skin · crackedCRACK ON RT NACELLE OTBD SKIN AT TOP CORNER OF COWLING PANEL 426AR CUT OUT. REPAIRED IAW RD8-54-3511.May 14, 2014 · N889EA · Dhav DHC8106SDR ASOA2014052110545Skin · dentedRT FAN COWL UPPER FWD CORNER, SKIN DENT. FABRICATED AND INSTALLED REPAIR DOUBLER ANGLE IAW SRM 51-14-00-201-004-A01. PERMANENT & MAJOR REPAIR.May 4, 2014 · N608QX · Cndair CL6002C10SDR ASOA2014060210609Skin · chafedRT LOWER CORE COWL INTERIOR AT 6:00 O'CLOCK POSITION IS CHAFED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLIED WITH ALL STEPS OF REO 670-54-23-959 REV 8. COMPLIED WITH EC/TC REO 670-54-23-959 COMPLIED WITH REPAIR OF THE FWD CORE COWL IAWMay 2, 2014 · N707EV · Cndair CL6002C10SDR SWIA201437572Skin · corrodedLT PYLON AFT UPPER SKIN CORROSION ON SPLICE PLATE. C-CHECK REPLACED SPLICE PLATE IAW SRM.May 2, 2014 · N779CA · Cndair CL6002B19SDR ASOA2014052110519Skin · chafedRIGHT ENGINE LOWER CORE COWL INNER SKIN IS CHAFED. RECEIVED EC/TC REO 670-54-23-959: COMPLIED WITH REPAIR OF THE FWD CORE COWL IAW REO 670-54-23-959. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED ACDC FIRESHIELD. INSTALLED NEW ACOC FIREApr 23, 2014 · N608QX · Cndair CL6002C10SDR ASOA2014052110552Skin · dentedRT FAN COWL UPPER FWD CORNER, SKIN DENT. COMPLIED WITH PERMANENT REPAIR OF RT FAN COWL UPPER FWD CORNER SKIN IAW SRM 54-14-00. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REPAIR IAW SRM 54-14-00-201-001-A01. COMPLIED WITH SRM 54-14-00-201-004Apr 21, 2014 · N608QX · Cndair CL6002C10SDR SWAA2014061729123Access Panel · crackedNUMBER 2 PYLON RT NACELLE STRUT ACCESS PANEL 5864R CRACKED. REPAIRED PANEL IAW EA.Apr 15, 2014 · N387SW · Boeing 7373H4SDR AALA20140414003Skin · crackedNUMBER 2 ENG PYLON HAS A CRACK INDICATION AT INBD UPPER AFT THRUST REVERSER HINGE MOUNT FASTENER HOLE, ALUMINUM SKIN LAYER ONLY. REMOVED CRACK BY ENLARGING HOLE TO .831 INCHES IN ALUMINUM SKIN LAYERS ONLY & INSTALLED FREEZE PLUG. INSTALLED DOUBLER IAW B757-Apr 14, 2014 · N660AM · Boeing 757223SDR SWIA201437103Skin · crackedRIGHT ENGINE TOP COWL, WHERE THE FORWARD INBD DOOR HOLD OPEN ROD ATTACHES HAS A CRACK APPROXIMATELY 1.5" LONG. REPAIRED 1.5" LONG CRACK ON HALF FRAME. LOCATED ON RT ENGINE TOP COWL BY FWD INBD DOOR HOLD OPEN ROD ATTACHES IAW ETD.Apr 11, 2014 · N224SW · Emb EMB120ERSDR SWIA201437051Skin · crackedLEFT WING NACELLE FLAP BOTTOM SKIN IS CRACKED NEXT TO ACCESS PANEL. C-CHECK, R & R LT WING NACELLE FLAP IAW AMM.Apr 10, 2014 · N563SW · Emb EMB120ERSDR KCSA201404101040Skin · damagedNR 2 PYLON OTBD LOWER SKIN DAMAGED AT NAC STA 226.5.Apr 10, 2014 · N746CK · Boeing 747246FSDR KCSA201404081039Skin · damagedNR 2 PYLON INBD SKIN LOWER SKIRT DAMAGED FROM NAC STA 214-227.Apr 8, 2014 · N746CK · Boeing 747246FSDR SWIA201441064Skin · dentedDENTS ON THE LT ENGINE LOWER FAN COWL ASSY. REPAIRED IAW REO AND SRM.Apr 3, 2014 · N785SK · Cndair CL6002C10SDR SPUY201403310033Skin · corrodedNR 3 ENGINE, LT UPPER COWLING SKIN SHOWS CORROSION FROM NAC STA. 185.20-194.8.Mar 31, 2014 · N199AJ · Boeing 7272F9SDR FDEA201403290598Skin · corrodedNR 1 PYLON RT AFT SKIN INTERNAL SURFACE BETWEEN STATIONS 144 & 153, LOWER AREA HAS CORROSION & MISSING PRIMER. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01, FIG. 102, DETAIL III. ACCOMPLISHED EA F-5450-T0305710, PT 1. MAMar 29, 2014 · N975FD · Boeing 7572B7SDR SWIA201436860Skin · damagedLEFT NACELLE OTBD SKIN DAMAGED ABOVE OTBD FWD MLG GEAR DOOR. C-CHECK, INSTALLED DOUBLER REPAIR IAW ETD.Mar 25, 2014 · N301YV · Emb EMB120ERSDR C77A20140323011Panel · wornPYLON PANEL 429NR HAS FOUR OVERSIZED FASTENER HOLES. REAMED FASTENER HOLE BACK TO ROUND & INSTALL NAS 1169C REPAIR WASHER IAW STANDARD PROCEDURES IN SRM 51-40-02 ON WORK ORDER 740147-446 IAW ETD 2014-170-023806 & EA E175-54-166 2 REV IR WORK ORDER 1418103.Mar 23, 2014 · N625CZ · Emb ERJ170200LRSDR C77A20140323010Panel · wornPYLON PANEL 429ML HAS ONE OVERSIZED FASTENER HOLE. REAMED FASTENER HOLE BACK TO ROUND & INSTALL NAS 1169C REPAIR WASHER IAW STANDARD PROCEDURES IN SRM 51-40-02 ON WORK ORDER 740147-445 IAW ETD 2014-170-023806 & EA E175-54-166 2 REV IR WORK ORDER 1418103.Mar 23, 2014 · N625CZ · Emb ERJ170200LRSDR C77A20140323009Panel · wornPYLON PANEL NR 429LR HAS ONE OVERSIZED FASTENER HOLE. REAMED FASTENER HOLE BACK TO ROUND & INSTALL NAS 1169C REPAIR WASHER IAW STANDARD PROCEDURES IN SRM 51-40-02 ON WORK ORDER 740147-444 IAW ETD 2014-170-023806 & EA E175-54-166 2 REV IR WORK ORDER 1418103.Mar 23, 2014 · N625CZ · Emb ERJ170200LRSDR C77A20140323008Panel · wornPYLON PANEL 419YL HAS ONE OVERSIZED FASTENER HOLE. REAMED FASTENER HOLE BACK TO ROUND & INSTALL NAS 1169C REPAIR WASHER IAW STANDARD PROCEDURES IN SRM 51-40-02 ON WORK ORDER 740147-459 IAW ETD 2014-170-023806 & EA E175-54-166 1 REV IR WORK ORDER 1418102.Mar 23, 2014 · N625CZ · Emb ERJ170200LRSDR C77A20140323007Panel · wornPYLON PANEL 419KL HAS ONE OVERSIZED FASTENER HOLE. REAMED FASTENER HOLE BACK TO ROUND & INSTALL NAS 1169C REPAIR WASHER IAW STANDARD PROCEDURES IN SRM 51-40-02 ON WORK ORDER 740147-443 IAW ETD 2014-170-023806 & EA E175-54-166 1 REV IR WORK ORDER 1418102.Mar 23, 2014 · N625CZ · Emb ERJ170200LRSDR C77A20140323006Panel · wornPYLON PANEL 419ML HAS TWO OVERSIZED FASTENER HOLES. REAMED FASTENER HOLE BACK TO ROUND & INSTALL NAS 1169C REPAIR WASHER IAW STANDARD PROCEDURES IN SRM 51-40-02 ON WORK ORDER 740147-442 IAW ETD 2014-170-023806 & EA E175-54-166 1 REV IR WORK ORDER 1418102.Mar 23, 2014 · N625CZ · Emb ERJ170200LRSDR C77A20140323005Panel · wornPYLON PANEL 419NR HAS TWO OVERSIZED FASTENER HOLES. REAMED FASTENER HOLE BACK TO ROUND & INSTALL NAS 1169C REPAIR WASHER IAW STANDARD PROCEDURES IN SRM 51-40-02 ON WORK ORDER 740147-441 IAW ETD 2014-170-023806 & EA E175-54-166 1 REV IR WORK ORDER 1418102.Mar 23, 2014 · N625CZ · Emb ERJ170200LRSDR SWIA201436954Skin · chafedRIGHT ENGINE NACELLE ZONE 433, INNER SKIN IS CHAFED. C-CHECK, REPAIRED SKIN IAW REO.Mar 19, 2014 · N770SK · Cndair CL6002C10SDR C77A20140313009Panel · wornRT PYLON PANEL 429NR HAS FIVE EACH ELONGATED FASTENER HOLES. REAMED FASTENER HOLES BACK TO ROUND & INSTALL NAS 1169C REPAIR WASHER IAW SRM 51-40-02 ON WORK ORDER 736922-450 IAW ETD 2014-170-019606 & EA E175-54-164.1 REV IR WORK ORDER 1412994.Mar 13, 2014 · N624CZ · Emb ERJ170200LRSDR C77A20140313008Panel · wornRT PYLON PANEL 429ML HAS THREE EACH ELONGATED FASTENER HOLES. REAMED FASTENER HOLES BACK TO ROUND & INSTALL NAS 1169C REPAIR WASHER IAW SRM 51-40-02 ON WORK ORDER 736922-448 IAW ETD 2014-170-019606 & COMPASS EA E175-54-164.1 REV IR WORK ORDER 1412994.Mar 13, 2014 · N624CZ · Emb ERJ170200LRSDR C77A20140313007Panel · wornATTACH FASTENER HOLES IS WORN OVERSIZE ON LT PYLON PANEL 419ML. REAMED FASTENER HOLE BACK TO ROUND & INSTALL NAS 1169C REPAIR WASHER IAW SRM 51-40-02 ON WORK ORDER 736922-441 IAW ETD 2014-170-019606 & EA E175-54-164.1 REV IR WORK ORDER 1412993.Mar 13, 2014 · N624CZ · Emb ERJ170200LRSDR C77A20140313006Panel · wornATTACH FASTENER HOLES IS WORN OVERSIZE ON LT PYLON PANEL 419NR. REAMED FASTENER HOLE BACK TO ROUND & INSTALL NAS 1169C REPAIR WASHER IAW SRM 51-40-02 ON WORK ORDER 736922-440 IAW ETD 2014-170-019606 & EA E175-54-164.1 REV IR WORK ORDER 1412993.Mar 13, 2014 · N624CZ · Emb ERJ170200LRSDR C77A20140313005Panel · wornATTACH FASTENER HOLES IS WORN OVERSIZE ON LT PYLON PANEL 419KL. REAMED FASTENER HOLE BACK TO ROUND & INSTALL NAS 1169C REPAIR WASHER IAW SRM 51-40-02 ON WORK ORDER 736922-439 IAW ETD 2014-170-019606 & EA E175-54-164 1 REV IR WORK ORDER 1412993.Mar 13, 2014 · N624CZ · Emb ERJ170200LRSDR CALA2014030790538Skin · wornNR 1 PYLON LOWER SURFACE WORN AT RIB FROM CNA SEAL. AREA WAS BLENDED IAW SRM51-73-00 WITH MAX WEAR OF .007 & WITHIN SRM54-51-12 FIGURE 103 LIMIT. INSTALLED ANTI CHAFING PLATE REPAIR IAW SRM 54-51-12 FIGURE 202.Mar 5, 2014 · N480UA · Airbus A320232SDR C77A20140301006Panel · wornPYLON PANEL 429ML HAS AN OVERSIZE FASTENER HOLE. REAMED FASTENER HOLE BACK TO ROUND & INSTALLED NAS 1169C REPAIR WASHER IAW SRM 51-40-02 ON WORK ORDER 784497-422 IAW ETD 2014-170-014371-A & EA E170-54-021 REV IR WORK ORDER 1408043.Mar 1, 2014 · N751CZ · Emb ERJ170100LRSDR C77A20140301005Panel · wornPYLON PANEL 429NR HAS 2 OVERSIZE FASTENER HOLES. REAMED FASTENER HOLE BACK TO ROUND & INSTALLED NAS 1169C REPAIR WASHER IAW SRM 51-40-02 ON WORK ORDER 784497-419 IAW ETD 2014-170-014371-A & EA E170-54-021 REV IR WORK ORDER 1408043.Mar 1, 2014 · N751CZ · Emb ERJ170100LRSDR C77A20140301004Panel · wornPYLON PANEL 419NR HAS AN OVERSIZE FASTENER HOLE. REAMED FASTENER HOLE BACK TO ROUND & INSTALLED NAS 1169C REPAIR WASHER IAW SRM 51-40-02 ON WORK ORDER 784497-414 IAW ETD 2014-170-015217 & EA E170-54-022 REV IR WORK ORDER 1408383.Mar 1, 2014 · N751CZ · Emb ERJ170100LRSDR CALA2014030390530Skin · crackedNR 1 PYLON RT SIDE SKIN AT NACELLE STATION 244, ACCESS PANEL 482ER CUTOUT AFT LOWER CORNER CRACKED. REPAIRED IAW ECRA 5450-02150.Feb 28, 2014 · N116UA · Boeing 747422SDR CALA2014030390529Skin · crackedNR 1 PYLON RT SIDE SKIN AT NACELLE STATION 244, ACCESS PANEL 452ER CUTOUT AFT LOWER CORNER CRACKED. REPAIRED IAW ECRA 5450-02149.Feb 28, 2014 · N116UA · Boeing 747422SDR COEA2014032506911Skin Panel · debondedWORK ORDER 132789 NR 400004 HEAVY CHECK COE MAJOR REPAIR. PANEL 476AR INNER SKIN SEPARATED FROM CORE. LT NACELLE INBD LATERAL PANEL. REPAIR IAW SRAS DT S-1417/14 8311 DATED 3/21/2014.Feb 22, 2014 · N911FX · Aerosp ATR42300SDR SWIA201436632Skin · chafedLT ENG PANEL 433AB HAS INNER SKIN CHAFE JUST FWD OF THE MOST FWD LATCH. C CHECK LT ENG PANEL 433AB INNER SKIN CHAFE REPAIRED IAW REO.Feb 20, 2014 · N773SK · Cndair CL6002C10SDR DALA14011505639Panel · damagedNR 1 ENG PYLON INBOARD SIDE, AN APPROXIMATE TWO INCH DENT WITH A ONE INCH CRACK IN SIDE ON L/E OF EXISTING REPAIR. REMOVED PANEL AND REPAIRED IAW ER/A 523411-14. INSTALLED PANEL IAW RI 532411-14 AND C/W ERA 523411-14.Feb 20, 2014 · N539US · Boeing 757251SDR AALA20140303006Skin · crackedNR 1 PYLON, THE INBD UPPER AFT HOLE THROUGH THE PYLON SKIN AT THE THRUST REVERSER AFT HINGE FITTING WAS FOUND TO HAVE A CRACK INDICATION DURING HFEC INSPECTION. REMOVED CRACK BY REAMING THE OUTER SKIN ONLY TO .640 & INSTALLED A FREEZE PLUG IAW EA B757-54-03384Feb 19, 2014 · N659AA · Boeing 757223SDR DALA2017041102912Panel · corrodedCORROSION LVL 2, NR 2 PYLON AFT STRUT FAIRING I/B AFT PANEL CORRODED AND REPLACED PER ERA 521585-14.Feb 18, 2014 · N189DN · Boeing 767332SDR DALA14014730189Panel · damagedNR 2 PYLON PANEL 447AL SCREW HOLE FOUND ELONGATED. REPLACED IAW ERA 521576-14.Feb 15, 2014 · N189DN · Boeing 767332SDR DALA14014720189Panel · damagedNR 2 PYLON PANEL 447AR SCREW HOLE FOUND ELONGATE REPLACED IAW ERA 521576-14.Feb 15, 2014 · N189DN · Boeing 767332SDR DALA2017041102917Skin Panel · corrodedNR 2 PYLON, AFT STRUT FAIRING I/B S/W PANEL EXTERNAL SURFACE FOUND CORRODED AND REPLACED.Feb 14, 2014 · N189DN · Boeing 767332SDR C77A20140214005Panel · damagedLEFT PYLON PANEL 419KL HAS 2 OVERSIZED FASTENER HOLES. REAMED FASTENER HOLE BACK TO ROUND & INSTALLED NAS 1169C REPAIR WASHER IAW SRM 51-40-02 ON WORK ORDER 746718-464 IAW ETD 2014-170-011172 & EA E170-54-020 REV IR WORK ORDER 1405981.Feb 14, 2014 · N749CZ · Emb ERJ170100LR
Back to JASC 5414