JASC 5730
Service difficulty reports · 27,254
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 IPXA2026050544404Skin · crackedRIGHT WING ROOT, MLG DOOR CUTOUT AFT INNER SKIN PANEL HAS (1EA) CRACK. REMOVED SKIN FROM RH WING ROOT, MLG DOOR CUTOUT AFT INNER SKIN PANEL IAW SRM 51-40-21-001. INSTALLED NEW SKIN PANEL IAW A300-600 SRM 51-40-21-001.SDR IPXA2026041811914Skin · crackedRIGHT WING INBOARD T/E UPPER FIXED PANEL SKIN CRACK, WBL 235.2. I.A.W. 747-400F SRM 57-51-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV. 106 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 26SDR CALA2026041015262Skin Panel · crackedRIGHT LOWER WING SKIN CRACKED AT ACCESS PANEL 643BB. STARTED TO REMOVE FASTENERS INSIDE FUEL CELL AREA AS REQUIRED. REMOVE DAMAGED PANEL P/N757-3401-2 IAW SRM 51-40-02 AND DRAWINGS LISTED ON AVO16784. CONTINUED REMOVING FASTENERS. REMOVED DOUBLER REPAIR. SDR VNAA20262687185Access Panel · damagedLEADING EDGE PRIMARY STRUCTURE 5771.25FH PERM REPAIR, PANEL 522CBSDR IPXA2026053005015Skin · gougedLEFT INBD FLAP, LEADING EDGE, AT RIB 13, 2 GOUGES WITH SEPARATION OF 1.5 INCH EACH OTHER. SKIN INSERT (1EA) AND BUTTSTRAP (2EA) WAS INSTALLED IAW SRM 51-40-21-001 AND SRM 57-50-00-200.SDR IPXA2026052106050Panel · damagedLH WING, PANEL 513AT WITH A SCREW HOLE ELONGATED DOT 53-090. RECEIVED NEW PANEL IAW AIPC 53-15-63-01 ITEM 50. VERIFIED RECEIVED NEW PANEL , AND VERIFIED EFFECTIVITY IAW AIPC 53-15-63-01 ITEM 50. INSTALLATION IS CONTROLLED ON TASKCARD T3F18E007EFYB.SDR YENA2026040900385Skin · damagedDURING HEAVY MAINTENANCE, RT WING BOTTOM SKIN PANEL NR 2 ACCESS PANEL 640JB FASTENER HOLE OUT OF ROUND E EA, AT RIB BAY 14-15. REFERENCE CAS WO 531-1485203 SASK 33 AND 34 AND WO 1485203- NR 13 AND 14. TWO EACH BUSING REPAIRS PERFORMED AT RIB BAY 14-15 AT PANSDR IPXA2026041685731Skin · crackedRIGHT WING UPPER SURFACE, TRAILING EDGE RIB 17-18 SKIN PANEL HAS (1EA) CRACK. DOT 28-18. NEW REPLACEMENT SKIN, REINFORCING PLATE, BUTTSTRAP, PACKING STRIP AND REINFORCING PLATE INSTALLED IAW SRM57-51-12-201 PAGE 203 TABLE 202.SDR 2026FA0000455Skin · crackedR/H WING AFT WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEW.SDR 2026FA0000449Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITHNEWSDR IPXA2026041685299Skin · crackedLH WING UPPER SURFACE, TRAILING EDGE RIB 15-16 SKIN PNEL HAS (1EA) CRACK. DOT 28-08. UPPER SURFACE RIB 15-16 SKIN PARTIALLY CUTTED IAW A300-600F SRM57-51-12-201, TABLE 202. INSTALLED LH WING SPOILER #5 I.A.W. A300 AMM 27-61-53/401. PERFORMED ADJUSTMENT AND OPSSDR IPXA2026050883072Skin · crackedRH WING BETWEEN SLAT# 8 AND #9 ON FIXED LEADING EDGE SKIN IN CRACKED. COMPLIED WITH STEP FOR EO-97223-REQ1 AND VT-MAE EA 757-5741-27-A4443, REV-, PRIOR TO FURTHER FLIGHT IS DOCUMENTED ON T3F18E008PRFYSDR R61A2026042600111Skin · crackedWHILE IN HEAVY CHECK - RT WING FIXED LEADING EDGE SKIN AT SLAT NR 2 OTBS TRACK CUTOUT CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IN RT WING FIXED LEADING EDGE SKIN AT SLAT NR 2 OTBD TRACK CUTOUT. REF: ETD2026-170-006454.SDR R61A2026050300116Skin · crackedDURING HEAVY CHECK RT WING FLE SLAT TRACK CUT OUT NR 4 FOUND CRACKED. REPAIRED SLAT TRACK NR 4 CUTOUT IAW ETD 2026-170-006571.SDR DALA2026040702219Access Door · missingLEFT INBD FLAP MAIN TRACK DOOR MISSING. REPAIRED PER LOG PAGE 8893486. (LOG PAGE 8493062 - AIRCRAFT WAS GROUNDED).SDR VNAA202606120044Access Panel · corrodedCORROSION ON SEVERAL LOCATIONS OF THE ACCESS PANEL SEATING SURFACE (621AT, 621AB & 621BR) (521AT, 521AB & 521BR) BOTH WINGS. CORROSION ON SEVERAL LOCATIONS OF THE ACCESS PANEL SEATING SURFACE (621AT, 621AB & 621BR) (521AT, 521AB & 521BR) BOTH WINGS. WERE REPASDR SWAA2026051185578Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 661CB AT RT WING. REPAIRED ACCESS PANEL 661CB AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2026051185579Access Panel · elongatedELONGATED HOLE ACCESS PANEL 561CB AT LT WING. REPAIRED ACCESS PANEL 561CBAT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.SDR CALA2026040115004Access Door · missingLEFT WING LEADING EDGE SLAT MECHANISM ACCESS DOOR MISSING. PANEL 521WB. PANEL 521WB REPLACED I.A.W AMM TASK 57-41-01-400-801. LOOSE ARTICAL CHECK CARRIED OUT BEFORE PANEL FITTMENT. PARTS DEPARTING LOGPAGE CREATED.PARTS USED: 76-5741-3-0002,QTY :1SDR 2026F00056Access Panel · corrodedFOUND 39 AREAS OF CORROSION AROUND NUTPLATES FOR PANEL 523AB AND 2 AREAS ON PANEL LAND. MECHANICALLY REMOVED 39 AREAS AROUND NUTPLATES WHICH WERE REMOVED PLUS 2 AREAS OF CORROSION ON PANEL LAND OF CORROSION IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TSDR K11A2026033100375Door · missingDURING WALKAROUND FOUND RH FUEL BOOST PUMP DOOR MISSING. TRANSFERRED TO DMI #73300134, CAT D, DUE 7/29/26 IAW B737 KC2 MEL CDL REF 57-30-4, SPECIAL PROCEDURES DCL 57-30-04 COMPLIED WITH PLACARDS INSTALLED. PERFORMED GROUND HANDLING HITS AIRPLANE OR PART DEPARSDR HNAA2026042300355Skin · crackedRIGHT WING TOP SURFACE, ANGLE NR 4 FROM FWD AND AT RIB 1A CRACKED AT AFT SIDE. REPAIRED IAW SRM 57-20-01SDR JR2R20260330621Skin · chafedRIGHT WING FIXED LEADING EDGE OVER PYLON CHAFED.SDR JR2R20260330558Skin · chafedLEFT WING FIXED LEADING EDGE OVER PYLON CHAFED .SDR SWAA2026043084387Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10. REFER TO INDIVIDUAL SIGNOFFS BELOW. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.SDR CALA2026033014919Skin · damagedTHE REPAIR INCORPERATED VIA ECRA 5720-03636 FOR THE R/H WING INT ERSPAR LWR SKIN APB PANEL P/N 757-3401-2 REPLACEMENT BETWEEN WS 711.50 & 743.50 IS APPROVED AS TIME LIMITED FOR 18 MONTHS UNTIL PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA).SDR CALA2026033014917Skin · damagedTHE REPAIR INCORPERATED VIA ECRA 5720-03636 FOR THE RT WING APB SPLICE & ADJACENT LWR SKIN PANEL HOLES CRACKED INBD OF WS 711.5 0 & THE LWR SKIN PANEL L-8 STRINGER AT APPROX. WSTA 700 IS APPROVED AS TIME LIMITED.SDR CALA2026033014912Skin Splice · crackedRIGHT WING OTBD MAIN SKIN SPLICE WAS CRACKED. REMOVED AND REPLACED SKIN SPLICE IAW DWG 757-3400, SRM 51-40-02, ECRA 5720-03636 REV-, & REO G25831, REV IR.SDR CALA2026033014910Skin · crackedRIGHT WING OTBD FWD SKIN SPLICE WAS CRACKED. R & R THE SKIN SPLICE IAW DWG 757-3400, REV E, SRM 51-40-02, EC/RA 5720-03636 REV-, & REO G25831, REV IR.SDR SWAA2026050483699Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561CB AT LT WING. REPAIRED ACCESS PANEL 561CB AT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2026041683358Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 661BB TRAILING EDGE AT RT WINGREPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2026041683359Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 661CB TRAILING EDGE, RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.SDR N6WA2025032705Skin · gougedRIGHT WING SKIN PANEL 632AR HAS A GOUGED. REPAIRED THE RT LEADING EDGE PANEL 632AR IAW GOJET EO C550-57MR-020-O.SDR SWAA2026042282591Access Door · crackedCRACK ON ACCESS PANEL 551GB AT TRAILING EDGE LT WING. REPAIRED ACCESS PANEL 551GB AT TRAILING EDGE LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.SDR DALA2026032602015Plate · corrodedCORROSION LOWER SURFACE EXTERNAL SKIN REINFORCING PLATE LOCATED AT LEVEL RIB 8 ON RH WING. C/A: COMPLIED WITH ER/A 632291-14AD REV ORIGINAL MATCHES WITH ALL STEPS OF PRI 632291-14AD REV 0 AND REV 1 IT IS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON BOTTOM SDR DALA2026032602012Skin · corrodedRIGHT WING, TOP SKIN, PANEL 2, LOWER SURFACE, T/E OVERHANG AREA WITH CORROSION AT RIB 11+520MM. C/A: PERFORMED REPAIR AT RH WING TOP SKIN PANEL 2/0 WER SURFACE T/E OVERHANG AREA AT RIB 11 + 520MM (AREA2) IAW ER/A NO. 632748-14AD REV ORIGINAL DATED 21 MAR 26. TSDR DALA2026032602010Skin · corrodedRIGHT WING, TOP SKIN, PANEL 2, LOWER SURFACE, T/E OVERHANG WITH CORROSION AT RIB 10 AREA. C/A: PERFORMED REPAIR AT RH WING TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 10 (AREA1) I.A.W ER/A NO. 632748-14AD REV ORIGINAL DATED 21-MAR-26. THIS IS A MASDR CALA2026032514824Skin · crackedDURING ROTO INSP OF LT UPPER WING SKIN. CRACK INDICATION WAS NOTED IN FASTENER HOLE #3 ON THE SKIN LAYER AT 12 O' CLOCK. NR 3 HOLE TAKEN TO SECOND OVER, NO CRACK INDICATION DETECTED WITH NDT OPEN HOLE INSPECTION. NEW FASTENER INSTALLED. WORK PER EC/RA:5720-036SDR DALA2026032401961Skin · corrodedSHIP 3164 DISC: RH WING TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 11+140MM SKIN WITH CORROSION. NOTE: WAS FOUND DURING THE PROCESS OF ORNRC 600-126. C/A: PERFORMED REPAIR AT RH WING TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 11+140SDR DALA2026032401960Skin · corrodedR/H WING, TOP SKIN, PANEL 2, LOWER SURFACE, T/E OVERHANG WITH CORROSION AT RIB 15 AREA. C/A: PERFORMED REPAIR AT RH WING TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 15 (AREA 4) I.A.W ER/A NO. 632748-14AD REV ORIGINAL DATED 21-MAR-26. THIS IS A MAJSDR JR2R20260323878Panel · chafed516ET HAS CHAFING FROM RIVET HEAD. REPAIRSDR DALA2026032602018Skin · corrodedER/A 632748-14AD ISSUED FOR REPAIR AND REWORK TO RH WING TRAILIN G EDGE SKIN CORROSION. FOLLOW ON ACTION REQUIRED. C/A: PERFORM SECTION IV EVERY SOONER OF 12200FC OR 24500FH AFTER SECT ION I. ASSOCIATED ER/A 14-632748 ADDED FOR AC 3164. (LP: 1505733)SDR DALA2026032602019Skin · corrodedER/A 632748-14AD ISSUED FOR REPAIR AND REWORK TO RH WING TRAILIN G EDGE SKIN CORROSION. FOLLOW ON ACTION REQUIRED. C/A: PERFORM SECTION III EVERY SOONER OF 15000FC OR 30000FH AFTER SEC TION I. ASSOCIATED ER/A 14-632748 ADDED FOR AC 3164. (LP: 1505729)SDR DALA2026032401959Skin · corrodedER/A 632748-14AD ISSUED FOR REPAIR OF CORROSION TO RH WING TRAIL ING EDGE SKIN. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION V EVERY SOONER OF 15000FC OR 30000FH AFTER SECTI ON I.SDR DALA2026032401958Skin · corrodedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR OF RH WI NG TRAILING EDGE SKIN CORROSION PER ER/A 632748-14AD. C/A: SECTION I IS LIMITED TO SOONER OF 60000FC / 120000FH. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE.SDR DALA2026032401957Skin · damagedER/A 632748-14AD ISSUED FOR RH WING TRAILING EDGE SKIN CORROSION REWORK. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II EVERY SOONER OF 10000FC OR 20000FH AFTER SECTION I.SDR SWIA2026032076329Skin · corrodedRBL45 RT WING LOWER PLANK TRAILING EDGE AREA, CORRODED & CHAFFED FROM THE WING TO BODY FAIRING. REPAIRED RBL45 RT WING LOWER PLANK TRAILING EDGE IAW REO 601R-57-21-4071 REV -. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR IPXA2026033175660Plate · chafedCHAFED PLATE, FWD EDGE LOWER FACE OF LT WING INBD L/E LOWER PLATE, ISS 250.625 - ISS 256.145. INSTALLED NEW SKIN PLATE IAW SRM 51-40-02-0G, REV 94, DWG 114T1000 ,SH 4, REV -, DWG 114T1225, SH 6, REV -, SH 7, REV -, DWG 114T1220, SH 6, REV -, SH 7, REV -, & DSDR UATA202603275702Skin · crackedRIGHT WING HAS CRACK ON TRAILING EDGE UNDERSIDE ABOVE OUTBOARD FLAP ASSEMBLY AT WS5000 AS MARKED. REPAIRED CRACKED SECTION OF RH FLAP COVE SKIN. SEE 337 DATED 3/20/2026. REMOVED 75MM X 25MM SECTION FROM INBOARD CRACKED AREA AND 90MM X 25MM SECTION FROM OUTBOARSDR UATA1740327265701Skin · crackedRH WING HAS CRACK ON TRAILING EDGE UNDERSIDE ABOVE OUTBOARD FLAP ASSEMBLY AT WS4800 AS MARKED. REPAIRED CRACKED SECTION OF RT FLAP COVE SKIN. REMOVED 75MM X 25MM SECTION FROM INBOARD CRACKED AREA AND 90MM X 25MM SECTION FROM OUTBOARD CRACKED AREA. REMOVED RIV
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