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 2003UALA00132Skin · crackedNR 1 PYLON STRUT OUTBOARD SIDE SKIN IS CRACKED AT FORWARD ACCESS HOLE. MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH DOUBLERS.SDR DLM88030109Panel · separatedSECTION OF ACOUSTIC PANEL SEPARATED FROM INLET COWL OF NR 1 ENGINE. MINOR DAMAGE TO FAN BLADES. REPLACED INLET.SDR 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.SDR QXEA0300198Panel · gougedPDX - NR 2 NACELLE PANEL 424AR HAS A GOUGE IN CENTER OF PANEL. REPAIRED IAW HORIZON AIR EA 2-71-193.SDR 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 ADJACENTSDR 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 REPAIRSDR 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 & 5SDR AUS20030026Skin · corroded(AUS) LT NACELLE UPPER INBOARD SKIN CORRODED BETWEEN SKIN AND SUPPORTING STRUCTURE.SDR 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; SSDR 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.SDR 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.SDR 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 INSPESDR 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, ACTUATIOSDR 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.SDR 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 REPAIRSDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR QXEA0202105Panel · chafedPDX - CHAFING ON PANEL 412BT. REPAIRED IAW DHC-8 200 SRM 54-00-16, PAGE 2, TABLE 1.SDR 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; FABRICSDR 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 11/20/02SDR 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 5SDR 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 SDR 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 CRACKSDR 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 PERFORMEDSDR 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)SDR 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 RADISDR 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 B73SDR QXEA0201767Doubler · chafedPDX - PREVIOUS REPAIR PATCH IN FORWARD RT CORNER OF TOP DECK OF LOWER COWL CHAFED. REPAIRED IAW RD 8-54-602.SDR CA021016001Panel · missing(CAN) DURING WALK AROUND FOUND PYLON PANEL MISSING RT ENGINE OUTBOARD SIDE. NEW PANEL INSTALLED.SDR 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.SDR QXEA0201592Skin · crackedPDX- RT COWL DEBRIS DOOR SURROUND STRUCTURE INBOARD AND OUTBOARD ARE CRACKED. REPAIRED IAW DHC-8 400 RD 8/4-71-016.SDR QXEA0201593Skin · crackedPDX- LT COWL DEBRIS DOOR SURROUND STRUCTURE INBOARD AND OUTBOARD CHANNEL ARE CRACKED. REPAIRED IAW DHC-8 400 RD 8/4-71-016.SDR 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)SDR 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)SDR 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 DSDR 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.SDR 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 ARSDR 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.SDR 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-SDR 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.SDR 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 BULLSDR 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.SDR 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 REPAIRE
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