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 2003UALA00132Skin · crackedNR 1 PYLON STRUT OUTBOARD SIDE SKIN IS CRACKED AT FORWARD ACCESS HOLE. MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH DOUBLERS.Jan 30, 2003 · N582UA · Boeing 757222SDR DLM88030109Panel · separatedSECTION OF ACOUSTIC PANEL SEPARATED FROM INLET COWL OF NR 1 ENGINE. MINOR DAMAGE TO FAN BLADES. REPLACED INLET.Jan 29, 2003 · N960DL · Doug MD88SDR P5CA0300746Cap · crackedNR 4 PYLON WING KNEE-PAD (NU-CAP) PANEL TRAILING EDGE FASTENER HOLE BROKEN OUT. REPAIRED AND FILLED AREA, RE-DRILLED HOLE AND PROTECTED IAW SRM 51-40-00.Jan 26, 2003 · N524UP · Boeing 747200SDR QXEA0300198Panel · gougedPDX - NR 2 NACELLE PANEL 424AR HAS A GOUGE IN CENTER OF PANEL. REPAIRED IAW HORIZON AIR EA 2-71-193.Jan 24, 2003 · N346PH · Dhav DHC8202SDR UIEA200300003Skin · wrinkledDURING CURRENT C-CHECK AT SIA, FOUND NR 2 PYLON R/S SKIN WRINKLED TWO PLACES FROM 1) NAC 286 TO 300 AT STR 5, 2) NAC 300 TO 316 AT STRINGER6. REPAIR AREA (1) CUTOUT EXISTING DAMAGE IN FLAT BAY AREAS ONLY. HFEC INSPECTED ALL OPEN HOLES, CUT EDGES AND ADJACENTJan 22, 2003 · N516MC · Boeing 747243BSDR SROM200300016Skin · dentedDURING C CHECK INSPECTION FOUND NR 1 ENGINE IB NACELLE NR 2 LATCH CUTOUT DAMAGED. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 54-30-1, 51-40-2 & 51-10-2. MINOR REPAIRJan 16, 2003 · N733PA · Boeing 737205SDR SROM200300014Skin · crackedDURING C CHECK INSPECTION FOUND NR 2 ENGINE IB NACELLE SKIN CRACKED BETWEEN NR 3 & 4 RIBS, 27 INCHES FROM LOWER EDGE. CUT OUT DAMAGE 1.3 X 1.5 INCHES, FABRICATED REPAIR DOUBLER, ALODINED & PRIMED PART AND INSTALLED REPAIR DOUBLER PER SRM 51-40-2, 51-10-3 & 5Jan 16, 2003 · N733PA · Boeing 737205SDR AUS20030026Skin · corroded(AUS) LT NACELLE UPPER INBOARD SKIN CORRODED BETWEEN SKIN AND SUPPORTING STRUCTURE.Jan 14, 2003 · Doug C54ESDR AWXA200300090Doubler · crackedMCN - MAJOR REPAIR - DURING C-14 CHECK 2 EACH 5/8 INCHES CRACKS WERE FOUND ON NR 1 PYLON SKIN AND DOUBLER AT THE AFT LOWER CORNER OF PANEL 5724L, NAC STA 254. MAINTENANCE REMOVED EXISTING EXTERNAL DOUBLER AND PERFORMED HFEC INSPECTION VERIFYING CRACK LENGTH; SJan 10, 2003 · N331AW · Boeing 737300SDR CALA0300004Skin · crackedINSPECTION FOUND A 2" CRACK IN L/H ENGINE PYLON SKIN AT PANEL #5727L. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230, REV. B.Jan 6, 2003 · N76355 · Boeing 7373T0SDR SROM200300011Skin · dentedDURING C CHECK INSPECTION FOUND NR 2 ENGINE IB NACELLE SKIN DENTED. REPAIRED NR 2 ENGINE IB NACELLE SKIN BY FABRICATING REPAIR PARTS FOR SKIN AND INSTALLING ON NACELLE AFTER REMOVING DAMAGE PER SRM 54-10-3. MINOR REPAIR.Jan 5, 2003 · N733PA · Boeing 737205SDR AWXA200300061Skin · crackedDURING C-14 CHECK A 7/8 INCH CRACK WAS FOUND ON SKIN OF NR 1 ENGINE PYLON AT INBOARD SIDE, FORWARD ACCESS PANEL, FORWARD EDGE. MAINTENANCE STOP DRILLED CRACK ON SKIN OF NR 1 ENGINE PYLON AT INBOARD SIDE, FORWARD ACCESS PANEL, FORWARD EDGE; PERFORMED HFEC INSPEJan 2, 2003 · N334AW · Boeing 737300SDR 2003FA0000032Cowling · wornIT IS POSSIBLE THAT DUE TO NORMAL WEAR OF THE ENGINE COWL CAUSED CONTACT WITH THE NLG DOOR EDGE PREVENTING THE NLG FROM FULLY EXTENDING. IN ADDITION IT IS POSSIBLE THAT DUE TO THE INCORPORATION OF STC SA 5934SW, REMOVING HYDRAULIC POWER FROM THE NLG, ACTUATIODec 31, 2002 · N11KR · Cessna T210LSDR AUS20021479Panel · missing(AUS) NR 1 ENGINE ACOUSTIC PANEL LOCATED ON THE OUTBOARD SIDE IMMEDIATELY BEHIND FAN IS MISSING. PANEL WAS NOT FROM THE ICE IMPACT AREA.Dec 21, 2002 · Boeing 767330SDR SROM200200030Skin · gougedDURING C CHECK FOUND NR 1 ENGINE OUTBOARD COWL INNER SKIN GOUGED 24 INCHES FROM FWD END. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS PER SRM 54-30-1 & 53-30-3 MINOR REPAIRDec 19, 2002 · N736BP · Boeing 737205SDR ASAA0210370Skin · gougedPAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL AT NACELLE STATION 150.25 GOUGED. REMOVED AND REPAIRED DAMAGED AREA PER SRM. (M)Dec 7, 2002 · N741AS · Boeing 7372Q8CSDR ASAA0210371Channel · chafedPAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL U-CHANNEL AT NACELLE STATION 122.25-149.25 CHAFED. REMOVED AND REPAIRED DAMAGED AREA PER SRM. (M)Dec 7, 2002 · N741AS · Boeing 7372Q8CSDR ASAA0210368Skin · damagedPAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL AT NACELLE STATION 192.65 WITH AN ELONGATED HOLE. REMOVED AND REPAIRED DAMAGED AREA PER SRM. (M)Dec 5, 2002 · N741AS · Boeing 7372Q8CSDR ASAA0210365Skin · dentedPAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL SKIN AT NACELLE STATION 109.25 DENTED. REMOVED DAMAGED AREA AND REPAIRED LEADING EDGE PER SRM. (M)Dec 5, 2002 · N741AS · Boeing 7372Q8CSDR ASAA0210349Skin · gougedDURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL AT NACELLE STATION 205 GOUGED. REMOVED DAMAGE AND REPAIRED NR 1 ENGINE COWL PER SRM. (M)Dec 4, 2002 · N741AS · Boeing 7372Q8CSDR ASAA0210356Skin · gougedPAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL AT NACELLE STATION 222.25 GOUGED. REMOVED DAMAGED AREA AND REPAIRED PER SRM. (M)Dec 4, 2002 · N741AS · Boeing 7372Q8CSDR ASAA0210358Skin · gougedPAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL SKIN AT NACELLE STATION 165.25 GOUGED. REMOVED DAMAGED SKIN AND REPAIRED PER SRM. (M)Dec 4, 2002 · N741AS · Boeing 7372Q8CSDR ASAA0210359Skin · gougedPAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL RIB AT NACELLE STATION 207.67 GOUGED. REMOVED DAMAGED AREA AND REPAIRED PER SRM. (M)Dec 4, 2002 · N741AS · Boeing 7372Q8CSDR ASAA0210354Skin · gougedPAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL FRAME AT NACELLE STATION 188.64 GOUGED. REMOVED DAMAGED FRAME SECTION AND REPAIRED PER SRM. (M)Dec 4, 2002 · N741AS · Boeing 7372Q8CSDR QXEA0202105Panel · chafedPDX - CHAFING ON PANEL 412BT. REPAIRED IAW DHC-8 200 SRM 54-00-16, PAGE 2, TABLE 1.Dec 3, 2002 · N365PH · Dhav DHC8202SDR AWXA200201190Doubler · crackedMAJOR REPAIR - DURING C-14 CHECK, A 1/2 INCH CRACK WAS FOUND ON INTERNAL DOUBLER FOR PANEL 5727 LT, NR 1 PYLON. MAINTENANCE STOP DRILLED CRACK ON INTERNAL DOUBLER FOR PANEL 5727 LT, NR 1 PYLON; PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICNov 25, 2002 · N155AW · Boeing 7373G7SDR MALA020657Skin · chafedDURING 6Y/4Y INSPECTION IN CWA, CHAFING DAMAGE TO LT INBOARD NACELLE SKIN CAUSED BY WING LEADING EDGE FAIRING SEAL. MAINTENANCE COMPLETED REPAIR IAW EO S54053. A/C RELEASE DATE 11/20/02Nov 18, 2002 · N370PX · Saab 340BSDR SWIA200211652Skin · crackedLEFT NACELLE OUTBOARD SIDE JUST AFT OF FRAME 3 FORWARD HOOK FOR FORWARD COWL DOOR LATCH NACELLE IS CRACKED WHERE AFT PART OF THE LATCH HOOK GOES INTO THE NACELLE. FOUND DURING C-CHECK INSPECTION. FABRICATED AND INSTALLED REINFORCEMENT PLATE IAW EMB120 SRM 5Nov 12, 2002 · N209SW · Emb EMB120ERSDR USAABB02190Fairing · detachedPHL - FLT 43 - UPON LANDING, THE FORWARD PORTION OF THE LEFT ENGINE STRUT FAIRING PARTIALLY DETACHED. THE NR 5 SPOILER AND THE A30 MAIN LANDING GEAR TIRE WERE DAMAGED. MAINTENANCE REPLACED THE STRUT FAIRING AND THE WHEEL ASSEMBLY, AND PROGRAMMED THE SPOILER Nov 10, 2002 · N655US · Boeing 7672B7SDR UPS02439902Skin · crackedINSPECTION TYPE: ASV NR 3 PYLON INBD SIDE AFT AND BELOW "TEXAS" DOUBLER PREVIUOS REPAIR SHO WS EVIDENCE OF CRACK EXTENDING UPWARD FROM REPAIR.(MARKED). VERIFIED END OF CRACK WITH HFEC G. BUCHERT QC 10445. REMOVED DOUBLER . HS 86801 11 10 02. STOPDRILLED CRACKNov 10, 2002 · N520UP · Boeing 747200SDR AALA20021601Fairing · departedSFO - FLT 1994 - EN ROUTE SFO-DFW - ON TAKEOFF, LEFT PYLON DOGHOUSE FAIRING DEPARTED THE AIRCRAFT. RETURNED TO SFO WITHOUT INCIDENT. INSPECTED AIRCRAFT AND LEFT PYLON FOR OTHER DAMAGES. NO OTHER DAMAGED NOTED, PER SRM 54-5170-01 INTERIM REPAIR WAS PERFORMEDNov 5, 2002 · N320AA · Boeing 767223SDR EIA2002104Skin · chafedMZJ - AFT EDGE INNER SKIN WORN/CHAFED IN NUMEROUS AREAS ESPECIALLY BOTH LOWER CORNERS ON NR 4 ENGINE NOSE COWL TO FORWARD FAIRING. REPAIRED AFT AND UPPER SKINS AND INNER SKIN PER B747 SRM 51-40-02 FIG 1. (M)Oct 28, 2002 · N480EV · Boeing 747121SDR AWXA200201115Fairing · crackedLCQ - MAJOR REPAIR - DURING C-04 CHECK A 1" CRACK WAS FOUND AT THE FORWARD UPPER CORNER RADIUS OF THE INBOARD FLAP, OUTBOARD TRACK FAIRING ASSEMBLY, INBOARD SIDE OF EXTERNAL SHELL, L/H ENG PYLON. MAINTENANCE CUTOUT CRACKED AREA AT THE FORWARD UPPER CORNER RADIOct 23, 2002 · N335AW · Boeing 7373U3SDR AWXA200201114Fairing · crackedDURING C-04 CHECK A 1 INCH CRACK WAS FOUND AT THE INBOARD FORWARD UPPER CORNER OF THE AFT CANOE FAIRING, RT ENGINE PYLON. MAINTENANCE CUTOUT CRACKED AREA OF AFT CANOE FAIRING, RT ENGINE PYLON; FABRICATED A FILLER AND DOUBLER; AND INSTALLED REPAIR PARTS IAW B73Oct 23, 2002 · N335AW · Boeing 7373U3SDR QXEA0201767Doubler · chafedPDX - PREVIOUS REPAIR PATCH IN FORWARD RT CORNER OF TOP DECK OF LOWER COWL CHAFED. REPAIRED IAW RD 8-54-602.Oct 16, 2002 · N364PH · Dhav DHC8202SDR CA021016001Panel · missing(CAN) DURING WALK AROUND FOUND PYLON PANEL MISSING RT ENGINE OUTBOARD SIDE. NEW PANEL INSTALLED.Oct 11, 2002 · Boeing 7673Y0SDR QXEA0201649Skin · chafedPDX - NR 2 ENGINE LOWER NACELLE OUTBOARD SIDE IS CHAFED ON PREVIOUS REPAIR. REMOVED AND REPLACED CHAFED REPAIR PATCH AS PER D8 RD 8-54-602.Oct 8, 2002 · N345PH · Dhav DHC8202SDR QXEA0201592Skin · crackedPDX- RT COWL DEBRIS DOOR SURROUND STRUCTURE INBOARD AND OUTBOARD ARE CRACKED. REPAIRED IAW DHC-8 400 RD 8/4-71-016.Oct 2, 2002 · N409QX · Bombdr DHC8401SDR QXEA0201593Skin · crackedPDX- LT COWL DEBRIS DOOR SURROUND STRUCTURE INBOARD AND OUTBOARD CHANNEL ARE CRACKED. REPAIRED IAW DHC-8 400 RD 8/4-71-016.Oct 2, 2002 · N409QX · Bombdr DHC8401SDR ASAA0210204Fairing · chafedPAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE OUTBOARD FIXED FAIRING AT NACELLE STATION 155, WING STATION 255R CHAFED. REPAIRED FAIRING PER SRM. (M)Oct 1, 2002 · N747AS · Boeing 7372X6CSDR USAA020372Skin · crackedPIT - FOUND PYLON BONDED SKIN CRACKED 1.687, LEFT ENGINE PYLON STATION 196, PANEL NR 572 LEFT OPENING. REPAIRED PER TYPICAL REPAIR 54-30-07. (M)Sep 28, 2002 · N350US · Boeing 737301SDR UIEA200200047Skin · crackedDURING CURRENT C CHECK, FOUND NR4 PYLON RIGHT HAND FORWARD ACCESS PLATE CUTOUT, BETWEEN NAC 211 AND 220, CRACKED. CRACKS INITIATED FROM THE CLIP NUT HOLES OF THE INNER LIP DOUBLER (4 PLACES). TRIMMED AWAY INNER DOUBLER AROUND THE ENTIRE CUTOUT. FABRICATED DSep 20, 2002 · N505MC · Boeing 7472D3BSDR UIEA200200042Skin · damagedDURING CURRENT C CHECK AT SIAEC FOUND NR 3 PYLON OUTBOARD SIDE LOWER AFT ACCESS PLATE CUTOUT DAMAGED ON RETAINING LIP, NAC 286 ABOVE WL 136. SKIN AND DOUBLER WERE TRIMMED TO REMOVE DAMAGE. HFEC INSPECTED AREA OF REMOVED DAMAGE. NO ADDITIONAL CRACKING FOUND.Sep 20, 2002 · N508MC · Boeing 747230BSDR UIEA200200037Skin · crackedDURING CURRENT C-CHECK AT SIAEC, FOUND NR 2 PYLON LEFT ACCESS PLATE CUTOUT (463CL) AT NAC STATION 332 TO 350 CRACKED AT LOWER FORWARD CORNER APPROX .5 INCH. TRIMMED OUT CRACKED AREA. HFEC INSPECTED THE TRIMMED OUT AREA AND ALL FASTENER HOLES IN THE REPAIR ARSep 19, 2002 · N512MC · Boeing 747230BSDR QXEA0201584Hinge · wornCKB-RT LOWER NACELLE FOD DOOR HINGE POINTS ARE WORN. REPAIRED IAW HORIZON AIR EA. 6-71-58A AND WVAC EO. DH8S-71-0579A.Sep 17, 2002 · N406QX · Bombdr DHC8401SDR AWXA200200978Panel · crackedDURING C-06 CHECK A 1 INCH CRACK WAS FOUND ON NR 2 ENGINE PYLON LOWER TRAILING EDGE PANEL, AT THE INBOARD FORWARD END. MAINTENANCE REMOVED THE LOWER TRAILING EDGE PANEL. FABRICATED A NEW LOWER TRAILING EDGE PANEL, AND INSTALLED REPAIR PART IAW B757-200 SRM 51-Sep 15, 2002 · N907AW · Boeing 757225SDR ZW0A0209604Skin · crackedDURING CHECK-C MAINT FOUND CRACKS IN PYLON DURING REPAIR. FWD ACCESS HOLE NACELLE STA 116.5 EMITTING FWD APPROX 1.5 INCHES, INBD AND OTBD SIDES. ACCOMPLISHED REPAIR PER EMLR 73252 AND SB 757-54-0037.Sep 13, 2002 · N702TW · Boeing 7572Q8SDR ZW0A0209603Skin · crackedDURING CHECK-C MAINT CRACKS FOUND ON NUMBER 2 PYLON THE FWD ACCESS HOLE AT NACELLE STA 116.5, OTBD AND INBD OF PYLON, CRACKS 1.625 INCHES LONG AT TOP FWD SECTION OF ACCESS HOLE. CRACK IS VISIBLE ON OTBD AND INBD SIDE OF SKIN. ACCOMPLISHED BOEING SERVICE BULLSep 12, 2002 · N702TW · Boeing 7572Q8SDR ZW0A0209602Skin · crackedDURING CHECK-C MAINT IN THE NUMBER 2 PYLON, THE FWD ACCESS HOLE TO INTERIOR AT APPROX NAC STA 116.5, THE OTBD SIDE OF PYLON HAD CRACK 1.625 INCHES LONG. CRACK LOCATED TOP FWD SECTION OF ACCESS HOLE. CRACK IS VISIBLE ON OTBD AND INBD SIDE OF SKIN.Sep 12, 2002 · N702TW · Boeing 7572Q8SDR CA020913011Panel · delaminated(CAN) NR 1 ENGINE SUFFERED DAMAGE TO THE FRONT ANTI ICE IMPACT PANEL IN THE LOWER HALF OF THE FAN CASE. AFTER A FERRY FLIGHT TO A MAIN BASE THE DAMAGE WAS REPAIRED. A NUMBER OF DAYS LATER, THE SAME REPAIRED PANELS WERE FOUND DELAMINATED. ONE PANEL WAS REPAIRESep 9, 2002 · Airbus A320231
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