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 QXEA2013021900404Skin · corrodedCORROSION ON LT WING LANDING INBD SIDE FOR PANEL 524ET. REMOVED CORROSION IAW SRM 57-20-35-02-05, REV 12 MIN THICKNESS NOTED .085" CONFIRMED CRACK FREE IN AFFECTED AREA REF NTM 51-00-04-910-801, PT 1 AND 51-00-06-910-801 PT 1, REV 7. FOUND BLENDS TO BE WITHISDR FDEA201302180363Skin · damagedLT WING L/E COMMON TO THE OTBD SIDE OF PYLON DAMAGED. REPAIRED IAW EA 1-5730- 163589. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116. .SDR 7AHR20130218001Skin · crackedCRACK IN WING SKIN AT NR 8 SLAT TRACK HINGED DOOR ACCESS PANEL 1289C AT WING STATION 286.6. REPAIR REQUIRED WAS OUTSIDE OF THE STANDARD SRM REPAIR SCHEME. ENGINEERING FIRM, FLIGHT VEHICLES CONSULTING PROVIDED A REPAIR SCHEME. FABRICATED, LAYED OUT NEW FASTESDR ASAA2013021794098Skin · chafedLEFT WING INBD EXHAUST GATE IS CHAFED ON UPPER OTBD SURFACE. REPAIRED LT WING INBD EXHAUST GATE IAW SRM 57-53-01, REPAIR 10.SDR QXEA2013021700419Access Panel · corrodedCORROSION ON PANEL 624CT MATING SURFACE. REMOVED CORROSION FROM PANEL 624CT IAW SRM 57-20-35-02-02, REV 12. MINIMUM REMAINING ON PAD IS .1195 IS WITHIN LIMITS IAW SRM 57-20-35-02-02, REV 12. CONFIRMED AFFECTED AREAS CRACK FREE REF NTM 51-00-06-910-801, PT 1SDR QXEA2013021700413Skin · corrodedCORROSION ON PANEL 524ET MATING SURFACE. REMOVED CORROSION FROM PANEL 524ET IAW SRM 57-20-35-02-02, REV 12. MINIMUM REMAINING ON PAD IS .119 IS WITHIN LIMITS IAW SRM 57-20-35-02-01, REV 12. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801, PT 1, SDR SWAA2013032614165Plate · crackedLEFT WING UPPER SURFACE PLATE CRACKED BETWEEN WBL 254 TO 279.25. REMOVED AND REPLACED PLATE IAW DWG AND SRM.SDR QXEA2013021600410Skin · corrodedCORROSION ON PANEL 524BT MATING SURFACE. REMOVED CORROSION AND BLENDED IAW SRM REV 12 57-20-35-02-02. MIN REMAINING THICKNESS .118 WITHIN LIMITS IAW SRM REV 12 57-20-35-02-02. ALODINED, PAINTED AND RE-IDENTIFIED IAW SRM, REV 12 57-20-35-02-02. CONFIRMED AFFSDR QXEA2013021600409Skin · corrodedCORROSION ON PANEL 524AT MATING SURFACE. REMOVED AND BLENDED CORROSION IAW SRM R12 57-20-02-02 MIN REMAINING THICKNESS .115 WITHIN LIMITS IAW SRM REV 12 57-20-35-02-02. ALODINED, PAINTED AND RE-IDENTIFIED IAW SRM 57-20-35-02-02, REV 12. CONFIRMED CRACK FREE SDR DALA13009115650Access Panel · corrodedLEFT WING FUEL CUTOUTS DISCOVERED CORROSION AND PITTING AT PANEL CUTOUTS 541EB AND 541 FB LWR LIP. REMOVED CORROSION AND PITTING FROM RT WING PANEL 541EB AND 541FB LWR LIP CUTOUT IAW SRM 57-20-01, PG 203. ORIG MATERIAL THICKNESS IS .210 IAW DWG 69-35321 MATSDR SWAA2013031113522Skin · crackedRIGHT WING LEFT SKIN CRACKED AT STA 208. REPAIRED SKIN PER EA.SDR ASAA2013021493977Panel · damagedLEFT WING PIE PANEL AFT LANDING HAS TWO MISDRILLED HOLES. REPAIRED PIE PANEL LANDING IAW ASA EA 400-57EA-09832, REV.SDR ASAA2013021493926Skin · wornLT WING INBD L/E EXTERNAL, UPPER SURFACE SKIN CHAFED. CHECKED LIMITS ORIG .063 MATERIAL LOSS .010 REMAINING .053 FOUND TO BE OUT OF LIMITS IAW SRM 57-41-01, FIG 107, DETAIL C. R & R CLOSEOUT SKIN IAW SRM 51-40-02 ALODINED IAW SRM 51-20-01.SDR CA130218010Skin · damaged(CAN) OPERATOR REPORTED CORROSION DAMAGE TO THE LOWER WING SKIN AND STRINGER AT STN 89.15. REO6-57-V114 TO REPAIR THE DAMAGE.SDR SWAA2013021512725Fairing · crackedRIGHT WING INBOARD "ELEPHANT EAR" FAIRING WORN/EDGE CRACKED. REPAIRED PER SRM.SDR USAA2013030700006Access Panel · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING LOWER FUEL DOOR 540HB BETWEEN WS 7316 TO WS 7792 BETWEEN RIB 13 TO RIB 14. REPLACED LEFT WING LOWER FUEL DOOR 540HB IAW A321 SRM 51-72-11.SDR SBAA2013021400002Panel · deformedDURING VISUAL INSPECTION NOTICED THAT LEFT WING INBOARD AND MIDWING TKS PANELS WERE SLIGHTLY DEFORMED ALONG LEADING EDGE. DURING VISUAL INSPECTION OF BACKSIDE OF LEADING EDGE IT WAS NOTED THAT LEADING EDGE WAS PUSHED IN APPROX .25 INCHES DEEP AND .50 INCHES WSDR FDEA201302120328Skin · damagedLT WING LOWER SURFACE INBD PYLON PANEL 484BR HAS CHAFED WING APPROX 11" X 50" X .040". COMPLIED WITH EA 6-5710-T0300089 AND WRI 57105072.SDR IPXA13M77399Doubler · crackedINSPECTION TYPE:4C, CRACKED BEADED DOUBLER IN LT WING FIXED L/E XOS 665. REPAIRED BEADED DOUBLER IAW EO MD 11-5730-48222-A.SDR IPXA13M77398Doubler · crackedINSPECTION TYPE:4C, CRACKED BEADED DOUBLER IN LT WING L/E XOS 770. REPAIRED BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 203.SDR USAA2013030500002Access Door · damaged2S CHECK - ELONGATED HOLE ON LEFT WING FUEL DOOR 540LB BETWEEN WS 8744 TO WS 9235 & BETWEEN RIB 16 TO RIB 17. REPLACED LEFT WING FUEL DOOR 540LB IAW A321 SRM 51-72-11.SDR IPXA13M77226Doubler · crackedINSPECTION TYPE:4C, CRACKED BEADED DOUBLER IN LT WING L/E COMPARTMENT AT XOS 645. REPAIRED LT WING FIXED L/E BEADED DOUBLER AT STA XOS 645 REF SRM 5 7-40-02, REPAIR 15, FIG 203.SDR SWAA2013022012926Nonskid · missingRIGHT WING EMERGENCY EXIT PATH MISSING SMALL AREA OF NOSKID. REPAINTED OVERWING ESCAPE WALKWAY ARROW IAW B717 AMM 11-21-05.SDR SWAA2013022012925Skin · corrodedRIGHT MLG W/W UPPER WING SKIN CORRODED 24" OUT APPROX .750 WIDE, TOP SIDE (FROM I/B KEEL BEAM WEB) 004. REMOVED CORROSION ON CENTER WING SKIN RBL 19"-29". CORROSION HAS BEEN BLENDED ON THE AFT EDGE OF THE 5940741-6 SKIN WITH REMAINING THICKNESS OF .089"-.16SDR REXA20130200100Skin Panel · corrodedRIGHT WING PLANK ACCESS HOLE FOR PANEL 640BB CORRODED. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.SDR FDEA201302090311Skin · crackedLT WING UPPER FIXED T/E AT AILERON ACTUATOR CUTOUT PANEL LANDING FOR PANEL 575 BT IS CRACKED .4 IN LENGTH. REMOVED LANDING AT LT WING UPPER FIXED T/E AT AILERON ACTUATOR CUT-OUT IAW SRM 51-40-21, PARA 5, 7, AND 16. LOCATED AND DRILLED NEW LANDING IAW SRM 5SDR SWAA2013022112945Skin Panel · corrodedRIGHT WING , UPPER SURFACE, CUTOUT FOR FUEL ACCESS PANEL 620 AT CORRODED. REMOVED CORROSION AT RUB STRIP IAW B717 SRM 51-40-4.SDR ERAA20130014Access Panel · corrodedCORROSION FOUND ON FUEL PANEL 524AT AND BT. REMOVED CORROSION REF BOMBARDIER RD 8-57-320.SDR UALA2013021100798Access Panel · leakingRIGHT WING HAS EVIDENCE OF FUEL LEAKS PANEL 640JB OUTBOARD. FOUND FUEL LEAKING FROM ACCESS PANELS. ALL PANELS SCREWS TORQUED. LEAK CHECKED OKAY.SDR DXTA2013022705299Skin · corrodedRT WING UPPER SKINS HAS CORROSION. STRIPPED WING IAW MM 20-10-228. PREPPED, ALODINED, APPLIED CARBO ZINC 11 TO VISULOK FASTENERS AND APPLIED CA 7660TG TO DHS FASTENER HEADS IAW SRM 57-10-14 AND 57-10-13 . APPLIED 10P8-11 PRIMER IAW MM 20-110-228. APPLIED EXTSDR QXEA2013020700329Skin · corrodedRT WING SKIN PANEL LANDING FOR PANEL 621BT HAS SURFACE CORROSION ON INBD AND OTBD AREAS OF CUTOUT. REMOVED CORROSION IAW RD 8/4-57-441. INSPECTED THE RT WING SKIN PANEL LANDING IAW RD 8/4-57-441, REPAIR ITEM 3 AND HORIZON NDT MANUAL 8.2.1.2. PANEL 621BT FOUNSDR QXEA2013020700328Skin · damagedLT WING SKIN PANEL LANDING FOR PNL 524AT HAS DAMAGE TO UPPER SURFACE AT OTBD AND INBD SIDES OF CUT OUT. BLENDED OUT DAMAGE IAW RD 8/4-57-445. INSPECTED SKIN PANEL LANDING IAW RD 8/4-57-445 REPAIR 4 AND NDT MANUAL 8.2.1.2. MIN THICKNESS NOTED .066 REF NTM 51-SDR UIEA2013020700075Skin · damagedON WALK AROUND FOUND LIGHTNING STRIKE BURN MARK ON RT WINGLET T/E AT STA 121.637; WLT BL 62.836, MEASURING 2.5" X 1.0". (THE DAMAGE EXCEEDS THE SRM 57-30-01-1A-2 ALLOWABLE DAMAGE 2 - WINGLET SKIN LIMITS. DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR SDR SBAA2013021100001Panel · deformedDURING VISUAL INSPECTION NOTICED THAT RIGHT WING INBOARD TKS PANEL WAS DEFORMED ALONG LEADING EDGE FROM WS.37.00 TO WS 51.00. UPON INSPECTION OF BACKSIDE OF LEADING EDGE FOUND THAT LEADING EDGE WAS PUSHED IN APPROX .50 INCHES DEEP AND .50 INCHES WIDE BETWEEN NSDR DXTA2013021105281Access Panel · corrodedLT WING FUEL PANEL CORRODED.SDR ASOA2013022603079Access Panel · crackedFOUND RT BOOST PUMP ACCESS HOLE CUTOUT LANDING HAS MULTIPLE INDICATIONS NOTED AROUND ENTIRE LANDING 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE FROM RT BOOST PUMP CUT-OUT LANDING. MAX MATERIAL REMOVED 0.010". REPAIRED IAW REO 601R-57-21-1865.SDR ASOA2013021803036Skin · crackedFOUND RT FUEL ACCESS HOLE 650AB HAS MULTIPLE INDICATIONS NOTED ON LANDING INBD SIDE APPROX 6.0" IN LENGTH 80 PERCENT FSH, FAILED NDT INSPECTION. REPAIRED IAW REO 601R-57-21-030.SDR ASOA2013021803035Skin · crackedFOUND RT FUEL ACCESS HOLE 640BB HAS MULTIPLE INDICATIONS NOTED ON LANDING OTBD SIDE APPROX 2.0" IN LENGTH 50 PERCENT FSH, FAILED NDT INSPECTION. REPAIRED IAW REO 601R-57-21-030.SDR IPXA13M77175Doubler · crackedINSPECTION TYPE: 1C, RT WING INNER BEADED DOUBLER CRACKED NEAR XOS 665. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 661-667 IAW SRM 57-40-02, REPAIR 15, FIG 203. (MAJOR)SDR IPXA13M77136Doubler · crackedINSPECTION TYPE:1C, RT WING INNER BEADED DOUBLER CRACKED NEAR XOS787. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS783-789 IAW SRM 57-40-02, REPAIR 15 FIG, 203 (MAJOR).SDR ERAA20130008Skin Panel · dentedLEFT WING LOWER SKIN DENT FOUND AT SAT YW290. HFEC AND UT INSP NO DISBONDS OR CRACKS. DENT ALLOWABLE WITHIN LIMITS REF BOMBARDIER RD 8-57-5779. LOCATION UW290 - YW297 BETWEEN STR 15 - 16.SDR ABXA20130223400Skin · corrodedRIGHT WING UPPER SKIN HAS AREA OF CORROSION AT FWD SPAR ATTACH POINT WS 490 APROX FWD OF VORTEX GENERATORS. REMOVED CORROSION IAW B767 SRM 51-10-02 & 57-20-01. C/W REA 657-60480-MR, ACFT WAS GROUNDED.SDR REXA2013020400089Skin Panel · chafedLEFT WING FORWARD LOWER WING PLANK PANEL AT WS 54.897 ON FUEL DOOR LANDING IS PITTED AND CHAFED IN THE NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.SDR FDEA201302020257Access Panel · cracked12 EA FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STA=700. REPAIRED AS PER SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 51. INITIAL REPEATSDR FDEA201302020256Access Panel · cracked11 EA FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS =690 AND STA=700. REPAIRED AS PER SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 51. INITIAL REPEAT INSPSDR IPXA13M77184Doubler · crackedINSPECTION TYPE:1C, LT WING INNER BEADED DOUBLER CRACKED NEAR XOS627. FOUND PREVIOUS REPAIRS IN AREAS ADJACENT TO XOS627 CRACK. REMOVED OLD DOUBLERS AND INSTALLED LARGE SINGLE REPAIR BETWEEN XOS 621-648 IAW STASA EA 011-5730-01-A4457 REV IR AND EO MD11-5730-SDR IPXA13M77178Skin · chafedINSPECTION TYPE:1C, LT WING FIXED L/E EXTERIOR REPAIR DOUBLER AT ANTI-ICE DUCT SLOT XOS 464-470 IS CHAFED. R & R DOUBLER AT LT WING FIXED L/E EXTERIOR STA XOS 464 -470 IAW SRM 57-40-01, REPAIR 10, FIG 201 AND EO MD11-5730-43061-A. (MAJOR)SDR FDEA201302020260Skin · corrodedRT WING UPPER SKIN, WS 435 ALONG THE FWD EDGE CORRODED. REPAIRED IAW EA F-5710-165127. CORROSION DETERMINED TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 101, SHT 4, PAGE 104 DET A. THIS REPAIR IS CLASSIFIED AS A CATAGORY A MAJOR REPAIR.SDR IPXA13M77043Doubler · crackedINSPECTION TYPE:1C, LT WING BEADED DOUBLER CRACKED NEAR XOS854. REPAIRED LT WING FIXED L/E INNER BEADED DOUBLER BEWTEEN XOS 850-856 IAW EO MD11-5730-48222-A. (MAJOR)SDR IPXA13M77042Doubler · crackedINSPECTION TYPE:1C, LT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XOS613. REPAIRED LT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 610-616 IAW EO MD11-5730-48222-A. (MAJOR)
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