JASC 5730
Service difficulty reports · 27,269
Reports filed under 5730 · Wing, 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 = '5730' 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 = '5730' 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 A6WA201240114Panel · chafedPANEL 599BB CHAFED, BLENDED OUT DAMAGE, FOUND DAMAGE TO BE WITHIN SERVICEABLE LIMITS IAW REO 601R-57-60-020.SDR CALA2011121500811Skin · crackedSUPPORT TASK - LEFT WING TOP SKIN AND RISER CRACKED AT WS 211.59 STRINGER U12. LEFT WING TOP SKIN AND RISER CRACKED AT WS 211.5 BW STR U12 REPLACED AS PER SRM 51-10-02 AND NEW PANEL INSTALLED AS PER APB DWG 7574-3500 REV B AND FORM 44.0008 ATTACHED ITEM 1 - 4SDR A6WA201240123Skin · chafedLOWER WING SKIN BELOW PANEL 193AB LT & RT CORNER CHAFED. REPAIRED IAW REO 601R-57-21-880.SDR FXGA20111210006Skin · corrodedDURING HEAVY MX, DISCOVERED CORRODED WING SKIN JUST OTBD OF NR 3 NACELLE BETWEEN CENTER AND REAR SPARS.SDR A6WA201240115Skin · chafedLEFT WING INBD L/E INNER SKIN AT INBD END CHAFED PG 79-3. REMOVED, FABRICATED, AND REINSTALL IAW FORM 412 SRM 51-42-06, 51-42-13, 51-22-00, 51-40-11, 51-42-15, 51-21-11, 51-25-06.SDR A6WA201240126Panel · chafedWING PANEL 699B CHAFED. REMOVED CHAFE IAW REO 601R-57-60-020.SDR CA111214008Skin · cracked(CAN) DURING A ROUTINE INSPECTION, A CRACK WAS FOUND AT APPROX WS 61.0 ON THE UNDERSIDE OF THE WING. THE CRACK IS 0.75 INCHES LONG. THE CRACK STARTS AT THE EDGE OF A SMALL RIVETED PANEL & PROCEEDS INTO THE THICKER SKIN. WING PLANK 601R10046.SDR DALA1200710929Skin · damagedHIDDEN DAMAGE ELONGATED HOLES ON ACCESS DOOR CUTOUT NR 1355C AND 1357C AT LT WING LOWER SURFACE (LW). REPAIRS WHERE COMPLETED PER ERA 498175-14 AD REV ORIG.SDR LR7A2011121500244Skin · damagedDURING POST FLIGHT INSPECTION, MX FOUND A SMALL HOLE UNDERSIDE THE T/E OF LT WING INBD OF THE EXTERNAL TANK OWS72, FS617, WL256.5. REPAIR ACCOMPLISHED IAW SMP583, FIGURE 51-140-12, ITEM M2.SDR FXGA2012018002Skin · crackedDURING "A" CHECK DISCOVERED CRACKS ON LOWER WING SKIN AROUND ACCESS PANELS, 143FB AT WING STATION Y-657, 143BB LT WING STATION Y-657, AND 521AB LT WING STATION YA1359.SDR FDEA201112075192Skin · crackedWHILE PERFORMING E F-5450-7-5003 C2 PT3 STEP 41 PANEL 10, APPROX 0.010" CRACK STILL FOUND ON LT WING INBD HOLE FWD SIDE AFTER 2ND EDDY CURRENT INSPECTION. REPAIR CARRIED OUT IAW EA F-5450-157110 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201112045142Skin · crackedRIGHT WING L/E PANEL NR 613AB CUT-OUT FOUND CRACKED. CARRIED OUT REPAIR IAW SRM 53-15-63, FIG 201, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.SDR USAA2011121200040Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING LOWER FUEL DOOR 640KB BETWEEN WS 8268 TO WS 8744 & BETWEEN WING RIB 15 TO RIB 16. REPLACED RIGHT WING LOWER FUEL DOOR 640KB IAW A320 SRM 57-27-11.SDR USAA2011121200039Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING LOWER FUEL DOOR 640PB BETWEEN WS 10204 TO WS 10729 & BETWEEN WING RIB 19 TO RIB 20. REPLACED RIGHT WING LOWER FUEL DOOR 640PB IAW A320 SRM 57-27-11.SDR USAA2011121200038Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING LOWER FUEL DOOR 640JB BETWEEN WS 7792 TO WS 8268 & BETWEEN WING RIB 14 TO RIB 15. REPLACED RIGHT WING LOWER FUEL DOOR 640JB IAW A320 SRM 57-27-11.SDR USAA2011121200037Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING LOWER FUEL DOOR 540KB AT WS 8268, WING RIB 15. REPLACED LEFT WING LOWER FUEL DOOR 540KB IAW A320 SRM 57-27-11.SDR FXGA2011120200005Skin · corrodedDURING HEAVY MX DISCOVERED CORRODED WING SKIN JUST OTBD OF NR 3 NACELLE BETWEEN CENTER AND REAR SPARS.SDR REXA201100821Skin · corrodedFUEL PANEL CUTOUT ON WING LOWER PLANK AT WS 54.897 CORRODED 0.006" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-21-030 REV H.SDR FDEA201112025118Skin · damagedRT WING UPPER SURFACE FIXED T/E SKIN PANEL (SRM 57-51-01, PG 2, ITEM 3) L/E ROW OF RIVETS FOUND SUNKEN IN AT WBL 79.02 OTBD 28" TO 38". REPAIRED IAW EA F-5730-15300 PART 1. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201112025117Skin · corrodedLT WING REAR SPAR UPPER SKIN CORROSION FOUND ADJACENT TO WBL 105. REPAIR CARRIED OUT IAW EA F-5730-153499, PART 1. REPAIR IS CLASSIFIED AS MINOR.SDR VNAA2011120600001Skin · damagedAT TYS, CREW REPORTED BIRD STRIKE TO RIGHT WING, ABOUT HALFWAY ON LEADING EDGE. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION, FOUND DAMAGE ON RIGHT WING MIDDLE LEADING EDGE TO BE WITHIN ALLOWABLE LIMITS PER SRM, FILLED DAMAGE AND PERFORMED CHECKS USING AIRCRASDR REXA201100827Structure · corrodedLT WING FUEL TANK ACCESS HOLE NR 1 AT WS 54.897 HAS PITTING CORROSION APPROX .001"D ON I/B AND O/B ENDS IN NON-CRITICAL REGION AND CHAFING ON THE I/B END APPROX 0.003"D. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.SDR REXA201100826Skin · corrodedLT WING FUEL TANK ACCESS HOLE NR 2 AT WS 12.245 HAS PITTING CORROSION ON I/B AND O/B ENDS IN NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.SDR REXA201100825Structure · corrodedRT WING FUEL TANK ACCESS HOLE NR 1 AT WS 54.897 HAS PITTING CORROSION APPROX .001"D ON I/B AND O/B ENDS IN NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.SDR COEA2011112826801Skin Panel · damagedHEAVY CK COE / MAJOR REPAIR: RT LOWER WING SKIN MAG STICK CUTOUT HAS PRIOR TOOLING DAMAGE BETWEEN RIB 22-23. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.SDR COEA2011112825801Skin Panel · damagedHEAVY CK COE / MAJOR REPAIR: LT LOWER WING SKIN MAG STICK CUT OUT HAS PRIOR TOOLING DAMAGE BETWEEN RIB 22-23. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.SDR HNAA2011112800399Access Panel · corrodedLT AND RT AUXILIARY FUEL PUMP LOWER ACCESS PANEL FOUND CORRODED. HFEC & BOND TEST CARRIED OUT ON REWORKED AREAS IAW RD8-57-1907 NO CRACK INDICATION & NO DISBOND FOUND. LT AND RT AUXILIARY FUEL PUMP LOWER ACCESS PANEL BLEND WITHIN LIMITS IAW RD8-57-1907. RT SSDR UIEA2011112800699Skin · crackedDURING FUELING OPERATIONS AT SYD; MX REPORTED DAMAGE FOUND TO LT WING LOWER L/E PANEL - ILES817.0 FWD OF FUELING ACCESS DOORS, CONSISTING OF A CRACK MEASURING 2.250 INCHES LONG. PERFORMED A TIME LIMITED REPAIR. OPENSDR A6WA201240046Access Panel · corrodedINDICATION OF CORROSION INBD END OF C/O 650AB. REPAIRED IAW REO 601R-57-21-030.SDR FDEA201111265051Doubler · crackedLT WING BEADED DOUBLER FOUND CRACKED. REPAIRED IAW EA 1-5730-154256. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 113.SDR UALA2011112706490Skin · dentedON INSPECTION OF FIXED LEADING EDGE, UNDER RT INBOARD SLAT NR 6 FOUND DAMAGED. TWO, SIX INCH OVAL DENTS MEASURING 1-4 INCH DEEP IN COMPOSITE STRUCTURE. REPAIRED PER SRM.SDR FDEA201111235004Skin · crackedLEFT WING L/E AT XOS 928 SKIN FOUND CRACKED UPON REMOVAL OF FORMER. REPAIRED IAW EA 1-5730-154256. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 113.SDR FDEA201111235014Skin · corrodedEXFOLIATION CORROSION FOUND ON UPPER WING SKIN BENEATH STUB BEAM AT BS940, LBL65. REPAIR CARRIED OUT IAW EA F-5710-154331.SDR COEA2011111722801Structure · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: 521DT PANEL CUTOUT IS CORRODED.(LENGTH 7.625 X 6.62, WIDTH .394", DEPTH .031"). SUBMITTED TO ATR. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS FROM ATR.SDR COEA2011111721801Structure · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: 522CT ACCESS DOOR CUTOUT HAS CORROSION (LENGTH 7.437 X 10.75, WIDTH .394", DEPTH .066"). SUBMITTED TO ATR. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS FROM ATR.SDR COEA2011111720801Structure · corrodedHEAVY CK COE / LEVEL 2 CORROSION: 622CT ACCESS DOOR CUTOUT HAS CORROSION (LENGTH 7.43 X 10.75, WIDTH .394", DEPTH .067"). SUBMITTED TO ATR / REPAIR PER SRI AND SRAS FROM ATR.SDR DALA1164245653Skin · damagedER/A 497012-14 FOR LT LOWER WING SKIN DAMAGE, WSTA 205 AND S-L10. THE LARGEST AREA OF DAMAGE RESULTED IN DEEP GOUGING & DENTING OF THE SKIN AND STRINGER L-11 CENTERED AROUND WSTA 205. STRINGER L-11 WAS ALSO BADLY DEFORMED. DAMAGE TOLERANCE ANALYSIS IS REQUSDR SWIA201131065Skin Panel · corrodedLEFT LOWER WING PLANK AREA PANEL 540BB HAS CORROSION (C-CHECK). REPAIRED IAW REO.SDR SWIA201131064Skin Panel · corrodedRIGHT WING LOWER PLANK AREA PANEL 650GB HAS CORROSION. (C-CHECK) REPAIRED IAW REO.SDR SWIA201131063Skin Panel · corrodedRIGHT WING LOWER PLANK AREA PANEL 650DB HAS CORROSION (C-CHECK). REPAIRED IAW REO.SDR UALA2011111506268Fence · damagedCREW REPORT: LIGHTNING STRIKE. NOT SURE OF ACTUAL LOCATION. SAMC TEXT: CONTACT SAMC, INSPECT PER MM 05-51-18 (FAXED) LEFT WINGTIP FENCE, DAMAGED BY LIGHTNING IN "NO DAMAGE" AREA, REMOVE PER AMM AND CDL PER 57BA. COMPLETED LIGHTNING STRIKE INSPECTION PER AMSDR 29GA95557111411ASkin · corrodedREPORT: DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT WING OUTBOARD TRAILING EDGE UPPER SKIN HAS CORROSION DAMAGE. REMOVED DAMAGED AREA OF SKIN AND INSTALLED REPAIR FILLER AND AN EXTERNAL DOUBLER.SDR 29GA95527111411ASkin · damagedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT WING OUTBOARD TRAILING EDGE UPPER SKIN HAS CORROSION DAMAGE. REMOVED DAMAGED AREA OF SKIN AND INSTALLED REPAIR FILLER AND AN EXTERNAL DOUBLER.SDR REXA201100715Skin · corrodedLT LOWER PLANK FUEL ACCESS HOLE AT WS 54.897 HOLE NR 1 HAS PITTING CORROSION ON I/B EDGE OF CUTOUT MEASURING APPROXIMATELY .002 DEEP IN CRITICAL AND NON-CRITICAL REGION. REF DI 54304. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.SDR REXA201100714Skin · corrodedRT LOWER PLANK FUEL ACCESS HOLE AT WS 54.897 HOLE NR 1 HAS PITTING CORROSION ON I/B EDGE OF CUTOUT MEASURING APPROXIMATELY .002 DEEP IN A NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.SDR FXGAN251CE1145Skin · corrodedFOUND CORROSION ON LT LEADING EDGE AT WING STATION 176.5 TO 184.0 WHICH REQUIRED A MAJOR REPAIR.SDR P5CA2011111100487Panel · crackedTHE LEFT WING, LOWER, LEADING EDGE PANEL FORWARD OF THE INBOARD FUEL ACCESS DOOR HAS A CRACK MEASURING 3 INCHES LONG. A TIME LIMTED REPAIR WAS ACCOMPLISHED IAW PART 1 OF EO 4457A388 8110-3 DATED 11NOV11 AND SRM 51-10-02.SDR JR2R2011111100587Skin · gougedRT WING L/E SKIN GOUGED AT WS 312. COMPLIED WITH MESA RO CRJ9-57-0348 ON RIGHT L/E SKIN GOUGE AS ON AAR WO 1007307-6200-0011 AND MESA WO 711014235.SDR ABXR2012F00008Exhaust Gate · corrodedLOWER SKIN OF EXHAUST GATE CORRODED AT OTBD EDGE. REPAIRED IAW SRM 51-40-02 AND AMES PROCESS STANDARDS MANUAL.SDR ABXR2012F00007Exhaust Gate · corrodedLOWER SKIN OF EXHAUST GATE CORRODED AT OTBD EDGE. REPAIRED IAW SRM 51-40-02 AND PROCESS STANDARDS MANUAL.
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