JASC 5730
Service difficulty reports · 27,262
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 EE4Y2024032219719Plate · corrodedDURING ACCOMPLISHMENT OF ALLEGIANT WORK CARD ZL-471-01-1-002, RH WING LOWER SURFACE PYLON REINFORCING PLATE WITH CORROSION BETWEEN WING RIB 8 AND RIB 9 STRINGER 5 AND 6. AIRBUS WAS CONTATCED ASKING REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND DSDR JR2R20240322336Skin · chafedLH WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKS. REPAIREDSDR AALA202404018230Skin Panel · debondedAIRCRAFT WAS NOT GROUNDED: UPPER SURFACE OF LEFT WING FIXED TRAILING EDGE SKIN PANEL 551ET IS DISBONDED. REPAIRED PANEL PER EA 352845A AND SRM 57-51-01-1A-1.SDR CALA2024032500855Skin · crackedLEFT WING FIXED LEADING EDDGE ABOVE THE PYLON IS CRACKED. PART IS CURRENTLY RMOVED FROM THE AIRCRAFT.SDR AALA202403228230Skin Panel · debondedAIRCRAFT WAS NOT GROUNDED: UPPER SURFACE OF LEFT WING FIXED TRAILING EDGE SKIN PANEL 551ET IS DISBONDED.**SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)SDR EE4Y2024032119626Skin Panel · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT WORK CARD 572179-01-1-001 LH WING TRAILING EDGE BETWEEN RIB 21 AND RIB 22 OVERHANG AREA WITH CORROSION WAS FOUND.DAMAGE WAS REPORTED TO AIRBUS ASKING REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND OVERHANG ASDR VNAA20240513001Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-459 REV. - -SDR VNAA20240426003Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-458 REV - -.SDR VNAA20240426002Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN. SDR AALA202405303660Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR SPAR TOP SKIN PANEL LOWER SURFACE BETWEEN RIB 7 AND RIB 8. REPAIRED SKIN PANEL PER EA 352824.SDR IXXA2024041503Skin · corrodedRIGHT WING UPPER SKIN IS CORRODED AT WING ROOT JUST AFT OF AFT OVERWING EXIT DOOR STEPSDR AALA202403266633Panel · damagedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD T/E LOWER PANEL 661 GB HAS FIBERGLASS EXPOSURE. ACCOMPLISHED PERMANENT SURFACE FINISH REPAIR AT RIGHT HAND WING T/E LOWER PANEL 661 GB. PER DMC AMM B787-A-51-21-13-01A-257A-A.SDR AALA202403260058Panel · damagedAIRCRAFT IN BASE MAINTENANCE: LEFT WING FIX LEADING EDGE OUTBOARD OF NAC STRUT PANEL 521KB HAS FIBERGLASS EXPOSURE THROUGHOUT PANEL. ACCOMPLISHED PERMANENT SURFACE FINISH REPAIR AT LEFT WING LEADING EDGE PANEL 521KB. PER DMC AMM B787-A-51-21-13-01A-257A-A.SDR DALA2024031903470Skin · damagedSHIP 3102 LIGHTNING STRIKE FOUND ON RH WING TIP AND STATIC WICK. CORRECTIVE ACTION: BLENDED AFFECTED AREA REF. A319 SRM 57-31-22, NO DAMAGE NOTED ON STATIC WICK, PRIMED AND PAINTED AREA REF. A319 SRM 51-21-11. (0250715)SDR DALA2024032003523Skin · corrodedCORROSION TRAILING EDGE UPPER SKIN LOWER SURFACE OVERHANG LOCATED FROM RIB7 TO RIB9 ON LH WING. COMPLIED WITH ER/A 589793-14AD REV. B MATCHES WITH ALL STEPS ON ER/A 589793-14AD REV B PRI REV 0 AND REV. 1 IT IS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS TRASDR CALA2024031900786Access Panel · missingFOA LEADING EDGE SLAT 1 UNDER WING ACCESS PANEL MISSING. CONFIRMED 521AJB LEADING EDGE SLAT MECHANISM LUBRICATION ACCESS LEADING EDGE SLAT LINKAGE FAIRING PANELS INSTALLED. PARTS CDL FOLLOWED, INOP. DOORS MISSING. INSPECTED AREA NO DAMAGES FOUND. CHKD ALL WISDR SWAA2024042564243Skin · crackedCRACK LEADING EDGE LOCATED SLAT STATION 322.71 AT RT WING. PERFORMED PERMANENT REPAIR ON SLAT 7 AT RT WING. IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8.SDR R61A2024041200179Skin · crackedRH WING LOWER SKIN NEAR SPAR 1 AND RIB 17 FOUND CRACK. MX REPAIRED SKIN CRACK IAW ETD 2024-170-007952 REV D. MAJORSDR FDEA202403150316Skin · crackedRT WING: FIXED WING L/E - LOOKING THROUGH LIGHTENING HOLE APPROX 8-12 INCHES OUTBD OF OUTBD SLAT TRACK FOR SLAT #8 BRACKET/ANGLE IS CRACKED. HFEC VERIFIED. (MARKED AND DOT 33) REMOVED FORMER P/N 114T2511-14, AND ANGLE P/N 114T2511-12 AND REPLACED WITH NEWSDR SWAA2024041162873Access Panel · crackedCRACK ACCESS COVER 642CL AT RT WING. REPLACED ACCESS COVER 642CL AT RT WING IAW SRM 51-10-02-0G-0 ITEM 9.A.(1). AND SRM 51-40-02-0G-0 ITEM 9. INSTALLATION IS DOCUMENTED ON TTG8Q00RKXQX.SDR SWAA2024041162874Access Panel · crackedCRACK ACCESS COVER 643CL AT RT WING. REPLACED ACCESS COVER 643CL AT RT WING IAW SRM 51-10-02-0G-0 ITEM 9.A.(1). AND SRM 51-40-02-0G-0 ITEM 9. INSTALLATION WILL BE ACCOMPLISHED ON TTG8Q00RKXQL;[02] CORRECTED STEP 1. REPLACED ACCESS COVER 643CL AT RT WING IAW SDR CALA2024032700884Skin · dentedBIRD STRIKE DAMAGE AT L/H WING, LEADING EDGE #2.SDR QXE2024F00000Skin · gougedRH WING FIXED LEADING EDGE GOUGE OUTBOARD OF RIB 41. COMPLIED WITH EC ETD2024-170-007081 PERMANENT REPAIR RH WING FIXED LEADING EDGE GOUGE OUTBOARD OF RIB 41.SDR QXEA2024031800065Skin · gougedRH WING FIXED LEADING EDGE UPPER SURFACE IS GOUGED BETWEEN RIBS 41-42. INSTALLED FILLER AND DOUBLER REPAIR ON RH WING FIXED LEADING EDGE UPPER SURFACE BETWEEN RIBS 41-42 IAW ETD2024-170-007081 AND HORIZON EC ETD2024-170-007081SDR 2DYA202403130068Skin · corrodedBLEND REPAIR LH WING LOWER SKIN AT WS 1040.0SDR 2DYA202403130067Skin · corrodedBLEND REPAIR TO RH INSPAR WING PANEL NO.1 LOWER SURFACE AT THE REAR OF SPAR AND WS 635.0SDR 2DYA2024F00066Skin · corrodedCORROSION ON TE SKIN AT STA. WS 839.00SDR AWKA202404187191Skin · corrodedREPAIRED THE RH UPPER IB WING SKIN BY R&R OF THE RH AFT DRAG ANGLE (WING-TO-FUSELAGE FAIRING) BLENDING CORRODED AREAS, PERFORMING NDT, REPLACING BLENDED FASTENERS, ROTO-PEENING BLENDED AREAS, TREATING AND PRIMING, AND REPLACING AN EXISTING SKIN PANEL WITH NEW SDR SWAA2024041162308Access Panel · elongatedELONGATED HOLE PLATE ACCESS PANEL 644BB FLAP SUPPORT FAIRING 8 AT RT WING 2024-165916<[01] REPLACED PLATE ACCESS PANEL 644BB FLAP SUPPORT FAIRING 8 AT RT WING I.A.W. B737-800 SRM 51-40-02-0G-0;[02] CERTIFIED WORK PERFORMEDSDR SWAA2024041667969Panel · delaminatedLEFT WING LOWER LEADING-EDGE PANEL#521DB HAS DELAMINATION AT ONE CORNER. APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #521DB IAW SRM 51-70-04-2R-13 PARAG 4-D-G.SDR DALA2024031103218Skin · crackedLOWER WING SKIN AND DOUBLER PER PRI 615647-14AD, REV 1, STEP 23, SHOWS CRACK INDICATIONS (3 EA) COMMON TO LOWER WING SKIN DOUBLER BELOW XRS164, ALONG INBOARD EDGE. MARKED. COMPLIED WITH LH WING / REAR SPAR LOWER CAP / XRS=159 / CRACK ERA 615647-14AD REV ORIG SSDR DALA2024031103217Skin · crackedINSPECTION OF LOWER WING SKIN AND DOUBLER PER PRI 615647-14AD, REV 1, STEP 23, SHOWS CRACK INDICATIONS (4 EA) COMMON TO LOWER WING SKIN DOUBLER AT XRS 164. 1 EACH IS OUTBOARD OF XRS 164, 3 EACH ARE INBOARD OF XRS 164. MARKED. COMPLIED WITH LH WING / REAR SPAR SDR SWAA2024040961300Access Panel · damagedELONGATED HOLE ACCESS PANEL 661CB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2024040961299Access Panel · damagedELONGATED HOLE ACCESS PANEL 661BB TRAILING EDGE AT RT WING. REPAIRED THE ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2024041660522Skin · crackedR/W MOVEABLE SLAT NO-7 L/E NOSE SKIN ACTUATOR ATTACHED RIB APPEAR CRACKED @ FASTENER HEADS MKD DOT<[01] ACCOMPLISHED PERMANENT REPAIR OF DAMAGE FOUND AT RT WING SLAT #7 NOSE SKIN AT ACTUATOR ATTACHING AREA PER REF B737 SRM 57-42-01-2R-8;[02] VERIFIED STEP 1; RSDR A6WA202403088723Skin · dentedDENTS ON R/H WING OUTBOARD LEADING EDGE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED R/H WING OUTBOARD LEADING EDGE ASSY REF AMM 57-41-01 REV 66. REMOVED AND REPLACED LEADING EDGE SKIN REF CRJ200 SRM 51-40-11 REV 39.SDR GTIA2024030837975Skin · corrodedCORROSION FOUND ON LH WING TOP SKIN AT RIBS 1-2 BOLT HOLES 433-441 AND RIB 7A FALSE REAR SPAR. RAF 01 CREATED. SDR SUBMITTED-ACCOMPLISHED PERMANENT REPAIR LF LH TOP SKIN PANEL #2 RIBS 1-2 AND RIB 7A WX 4392.633 PER REO L24919 , EA 5721-2416 INSTRUCTIONS CAT B SDR DALA2024030803173Skin · unknownREPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 583471-14AD REV C . REF ERA 583471-14AD. (0234122)SDR DALA2024030803172Skin · corrodedSHIP 5657 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 584851-14AD REV D. CORRECTIVE ACTION: REF ERA 584851-14AD. (0234396)SDR SWAA2024040559584Panel · crackedLT WING T/E PANEL 561BB AFT ROW OF FASTENER HOLES HAVE CRACKS AT HOLES<[01] LEFT WING TRAILING-EDGE PANEL 561BB AFT ROW OF FASTENER HOLES WITH CRACKS AT HOLES WAS REPAIRED IAW SRM 51-70-04-2R-9.;[02] VERIFIED CORRECTIVE ACTION #1SDR IPXA2024032525309Panel · crackedR/H WING ROOT UNDER PANEL 613AB, SKIN IS CRACKED BY NUTPLATE. INSTALLED DOUBLER AT R/H WING ROOT UNDER PANEL 613AB, IAW SRM 53-15-53 AND SRM 51-40-21. APPLIED TOP COAT AT EXTERNAL DOUBLER AT R/H WING ROOT UNDER PANEL 613AB. IAW SRM 51-23-10.SDR CALA2024030800667Panel · missingPDA 2 LEFTWING LEADING EDGE PANEL MISSING. ON ARRIVAL FROM SJD, TECH FOUND PANEL 522WB (L/H WING) MISSING WHEN PERFORMING EXTERIOR GVI INSTALLED NEW COVER ASSY ON BLOWOFF PANEL REF IPC 57-41-37.SDR SWAA2024040559033Panel · crackedRT WING T/E PANEL 661BB AFT ROW OF FASTENER HOLES HAVE CRACKS AROUND HOLE<[01] RIGHT WING TRAILING-EDGE PANEL 661BB AFT ROW OF FASTENER HOLES WITH CRACKS AROUND HOLES WERE REPAIRED IAW SRM 51-70-04-2R-9.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024040559031Web · crackedRIGHT WING; TRANSVERSE WEB IS CRACKED; UPPER LEG; O/B END ABOVE #2 PYLON AFT TIP<[01] REMOVED AND REPLACED RIGHT WING; TRANSVERSE WEB AT UPPER LEG; O/B END ABOVE #2 PYLON AFT TIP IAW SRM 51-40-02; AIPC 57-50-00-36A AND DWG 115A2512;[02] VERIFIED CORRECTIVE ACTSDR CALA2024030700651Skin · corrodedRIGHT WING UPPER SKIN AT OVER WING FUEL FILL PORT IS CORRODED. FOUND R/W UPPER SKIN FILL PORT TO BE OUT OF LIMITS PER B767-300 ACCOMPLISHED ON BACK OF NR AND PWS #27 PAGES 1 AND 2. REF AMES SRM 57-20-01, ALLOWABLE DAMAGE 1, TABLE 1. MIN REMAINING (ILN) NRC 167SDR CALA2024030500636Skin · gougedR/H WING L/E AT #1 SLAT ABOVE #3 TRACK SKIN IS GOUGED APPROX. 1. 5 INCH LONG. REMOVED AND REPLACED SKIN AT RH WING #1 SLAT ABOVE #3 TRACK A320 SRM 51-72-11.SDR EE4Y2024030419559Skin Panel · misrepairedLH WING, MAIN BOX T/E LOWER SKIN, AT RIB 10 WITH EXISTING REPAIR WITHOUT RECORDS. NOTE: THE WING SKIN WAS REPAIRED AS PER SRM PART II, 57-10-01 PARAGRAPH 7 (FREEZE PLUG REPAIR 2) AREA 2 FIGURE 201 SHEET 2 REPAIR 54 REPAIR INSTRUCTIONS. ( FOR ADDITIONAL DETAILSSDR VNAA202404080014Skin · damagedSPEED TAPE APPLIED - LH #2 SLAT AFT SKIN AT SS329.00 THE SUBJECT REWORKED CONDITION IS STRUCTURALLY ACCEPTABLE FOR 650 FH FROM THE EXPIRY OF THE E.A. 23-C9-57-1049 REVISION IR TIME VALIDITY (800 FH, REF) LH #2 SLAT AFT SKIN AT SS329.00 WAS REPAIRED PER REO 69SDR VNAA202404080003Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB AND 697AB) AT RH WING LOWER SKIN. SETTLEMENT AREA OF FAIRINGS (683AB, 686AB, 692AB, 695AB AND 697AB) AT RH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-452 REV - -.SDR VNAA202404080002Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB AND 597AB) AT LH WING LOWER SKIN. SETTLEMENT AREA OF FAIRINGS (583AB, 586AB, 592AB, 595AB AND 597AB) AT LH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-453 REV - -.
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