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 FDEA2020041000629Skin · crackedRIGHT HAND WING FIXED LEADING EDGE SKIN #14 SLAT TRACK CUTOUT FOUND CRACKED AT XOS 891. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE SKIN #14 SLAT TRACK CUTOUT AT XOS 891 AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR SDR FDEA2020040100640Skin · corrodedMAIN CARGO DECK, STA 1241 102LBL TO 110LBL, CENTER WING UPPER SKIN CORROSION CENTRE WING TOP SKIN AT STRINGER 13, BETWEEN XCW 102 TO XCW110, CORROSION REWORK PERFORMED IAW EA 8-5710-T0353142 PART 1.SDR DALA2020040102112Skin · crackedFOUND HOLE #1 AND #2 CRACKED REAMED #1 AND #2 HOLES TO .7660IN SKIN ONLY. LEFT WING LOWER SKIN. REPAIRED CRACKED HOLES PER ERA 5853240-14 (LP 1541345)SDR DALA2020033102097Skin · puncturedLHW FUELING STATION PANEL INNER SKIN FOUND PUNCTURE. REPAIRED PER ERA 586230-14 (LP 1540332)SDR FDEA2020032760608Skin · corrodedSMIS 303 57-30 6345 25MAR20 MEM OPEN U MOD TYPE T MOD NO. 8-5730-T0353169 REV NO. PS P1 WING, SKIN AND PLATES: CENTER WING UPPER, CENTER SKIN PANEL, STR 14 TO STR 15, COMPLY WITH E..A. 8-5730-T0353169 REV NO. POS. P1 INFO 25MAR20 14:44 **SDR FDEA2020032760607Skin · corrodedSMIS 303 57-30 6346 25MAR20 MEM OPEN U MOD TYPE T MOD NO. 8-5730-T0353174 REV NO. PS P1 WING, SKIN AND PLATES: CENTER WING UPPER, FWD AND CENTER SKIN PANELS, STR 15, X COMPLY WITH E..A. 8-5730-T0353174 REV NO. POS. P1 INFO 26MAR20 11:54 *SDR DALA2020033002072Fastener · looseSHIP 5803 AWR: AD: LOOSE FASTENERS NBR 1,2,3,4,5,6,7,8,9 AND 10 OF LH DRAG FITTING REF AMDS. CORRECTIVE ACTION: SUMMARY 1,2,3,4,5,6,7,8,9 AND 10 AT LHS UPPER SKIN & DRAG FITTINGS WAS PERFORMED PER ETI-57-20-052 REV. 4 AND ER/A 586129-14AD REV. ORG. SECTION I. SDR DALA2020033002071Fastener · looseSHIP 5803 AWR: AD: LOOSE FASTENERS NBR 11,12,13,15,16 AND 17 OF LH DRAG FITTING REF AMDS. CORRECTIVE ACTION: SUMMARY OF NRC 00428: TEMPORARY REPAIR FOR LOOSE FASTENERS NBR 11, 12, 13, 15, 16, AND 17 AT LHS UPPER SKIN & DRAG FITTINGS WAS PERFORMED PER ETI-57-20SDR 2020F00141Skin Panel · corrodedAIRBORNE/PEMCOAIR NON-ROUTINE 2387N3320 DISCREPANCY: LEFT WING LOWER AFT SKIN APPROX 950 HAS FLAKING PAINT. (REQIURES EVALUATION) REPAIRED AREA IAW E.O. #200665.SDR 2020F00139Skin · corrodedAIRBORNE/PEMCO NON-ROUTINE 2387N1310 DISCREPANCY: R/H WING UPPER FLANGE ,LOWER SURFACE, CORRODED AT WS 455 TO 496. CORRECTIVE ACTION: REMOVED CORROSION AND REPAIRED RH WING REAR SPAR,UPPER FLANGE WS 431.97 TO WS 532.46. EVALUATED AREA MAT.THICKNESS .200 MAT. SDR 2020F00135Skin Panel · corrodedAIRBORNE/PEMCO NON-ROUTINE 2387N3319 DISCREPANCY: LEFT WING LOWER AFT SKIN APPROX. WS 642 HAS FLAKING PAINT.(REQUIRES EVALUATION) CORRECTIVE ACTION: REPAIRED PANEL IAW B767-200 E.O.# 20064.SDR 2020F00134Skin Panel · corrodedAIRBORNE/PEMCO NON-ROUTINE 238N3321 DISCREPANCY: LEFT LOWER AFT SKIN AT WS 1075 HAS FLAKING PAINT.(REQUIRES EVALIUATION)CORRECTIVE ACTION: INSTALLED REPAIR ON LEFT WING LWR SKIN WS 1075 IAW B767 E.O.# 20066 REV.IRSDR DALA2020033002069Fastener · looseSHIP 5803 AWR, AD, A.A.: LOOSE FASTENER NBR 12, 13, 14, 15, 16 AND 18 BY CRACKED PAINT ALL THE WAY AROUND THE FASTENER HEAD AT RH WING UPPER SKIN DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NRC 00466 PERMANENT REPAIR ON LOOSE FASTENER NBR 12, 13, 14, 15, 16 ANSDR DALA2020033002067Fastener · looseSHIP 5803 AWR, AD, A.A.: LOOSE FASTENER NBR 1, 2, 3, 4, 5, 6, 8, 9 AND 10 BY CRACKED PAINT ALL THE WAY AROUND THE FASTENER HEAD AT RH WING UPPER SKIN DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NRC 00465: PERMANENT REPAIR ON LOOSE FASTENER NBR 1, 2, 3, 4, 5, 6SDR DALA2020032702046Fastener · looseSHIP 5802 BROKEN PAINT AROUND THE FASTENER HEAD #3 AT RH WING DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NRC 00488: TIME LIMITED REPAIR SECTION I WAS PERFORMED. IN ACCORDANCE AMDS FASTENER #3 WAS REMOVED, HOLE NBR 3 AT RH WING DRAG FITTING WAS INSPECTED NO DISDR SWIA202005210862Skin · chafedRH AND LH LOWER WING PLANK AT RBL45 AND LBL45 HAVE CHAFE DAMAGE IN PREVIOUSLY REPAIRED AREAS (C-CHECK) RO 5/16/2020 REPAIRED RH AND LH LOWER WING PLANK AT RBL45 AND LBL 45 IAW REO.SDR DALA2022030901540None · noneSHIP 5802 SECTION I TEMPORARY REPAIR TO LH WING UPPER SKIN AT DRAG FITTING ATTACHMENTS REQUIRES SECTION II PERMANENT REPAIR WITHIN 3,000 FLIGHT CYCLES OR 24 MONTHS (WHICHEVER OCCURS FIRST) PER ERA 586294-14. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED PESDR ABXA202006250077Skin · corrodedRIGHT WING UPPER SURFACE, EXFOLIATION ON SKIN APPROX. 20 FEET OUTBD OF FUSELAGE AND 5.2 FEET AFT OF FRONT SPAR. THE AIRPLANE WAS GROUNDED.SDR HALA2020032500075Skin · corrodedUPPER WING SKIN IN LEFT HAND WHEEL AREA CORROSION, BLENDED XRS 37 OUT OF LIMITS, PER DRAWING # SG9557001. REPAIRED PER E105-487297- PERM.SDR YENA2020032300258Skin · corrodedDURING HMV, WING / LH TRAILING EDGE / TOP SKIN OVERHANG RIBS 15-17 / CORROSION / WV 017 UPGRADE - PERMANENT REPAIR ; THIS REPAIR IS CLASSIFIED AS MAJOR. THIS REPAIR HAS APPROVED DATA VIA REFERENCE /1/ AND WAS ACCOMPLISH VIA AEROMAN EA REFERENCE /2/. A20-245-SDR DALA2023019200422Skin · not reportedSHIP 171 ERA 585240-14AD SECTION I ISSUED FOR REPAIRS TO LH WING LOWER WI NG SKIN AT STRINGERS L-9.5 AND L-6.5. FOLLOW ON ACTION IS REQUIR ED. CORRECTIVE ACTION: ER/A 585240-14AD REVISED TO REV. A. ACCOMPLISH ER/A 585240-14AD REV A SECTION II INSPECTIONS. STATSDR SWIA2020041750165Skin · worn* R/H WING FUEL ACCESS PANEL LOCATION 650CB HAS PITTING ON EDGE (MARKED) (C-CHECK) RO 4/16/2020 BLENDED OUT DAMAGED AREAS AS REQUIRED ON RH WING FUEL ACCESS PANEL LOCATION 650CB PER REO. GAP CHECK AND LEAK CHECK ARE GOOD. SEE CONTINUATION FOR DETAILS.SDR SWIA2020041750164Skin · worn* L/H WING FUEL ACCESS PANEL LOCATION 510AB INBOARD EDGE HAS PITTING (MARKED) (C-CHECK) RO 4/16/2020 BLENDED OUT DAMAGE AREAS OF LH WING FUEL ACCESS PANEL 510AB PER REO. BLEND OUT IS OUT OF LIMITS. RECEIVED REO. ROTO PEENED AND RESTORED REWORKED AREA. SEESDR SWIA2020041750163Skin · worn* FUEL ACCESS PANEL LOCATION WING PLANK PERIMETER.550HB HAS PITTING AND DEEP WEAR GROOVE MARKING .(MARKED) (C-CHECK) RO 4/16/2020 BLENDED OUT DAMAGE AREAS OF LH WING FUEL ACCESS PANEL 550HB PER REO. BLEND OUT IS OUT OF LIMITS. RECEIVED REO. ROTO PEENED ANDSDR 2020F00112Panel · damagedREPAIR TO LEFT AND RIGHT WING INBOARD LEADING EDGE PANELS DAMAGED (OVERSIZED ATTACH FASTENER HOLES). TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ25190M1 REV A DATED 03/19/2020. P/N 6922590-1, 6922590-2, 6922530-45, AND 6922530-46.SDR DALA2022033002141None · noneSHIP 5803 SECTION I TEMPORARY REPAIR TO LH WING UPPER SKIN AT DRAG FITTING ATTACHMENTS REQUIRES SECTION II PERMANENT REPAIR. CORRECTIVE ACTION: REF ERA 586129-14AD REV A. (1533796)SDR DALA2022030901541None · noneSHIP 5803 REF ERA 586153-14, ACCOMPLISH SECTION II REPETITIVE INSPECTIONS EVERY 2100 CYCLES AFTER ACCOMPLISHMENT OF SECTION I PERMANENT REPAIR. CORRECTIVE ACTION: ERA 586153-14 UPDATED TO REV. A. (1533903)SDR FXTA202000520001Panel · deformedDURING PREFLIGHT INSPECTION, NOTICED TKS WING PANEL TOP SEALANT SEPARATED FROM SKIN ON INBOARD SECTION OF PANEL. UPON INVESTIGATION IT WAS DETERMINED THAT PANEL TANK HAD DEFORMED FROM OVER PRESSURIZATION.SDR SWIA2020032449346Skin Panel · crackedTRANSFER FROM EAML 402910 : TRANSFERRED FROM CAMP 20675068. DURING WALKAROUND FOUND CRACK IN LEADING-EDGE SKIN PANEL FROM SS144.94 TO SS249.04, 622BR. FLIGHT 4602 - FILED CLOSED PERFORMED REPAIR TO RH WING FIXED LEADING EDGE SKIN BETWEEN SS201.55 - SS210.69SDR T17A202003198009Skin · corrodedMINOR SURFACE CORROSION ON RIGHT WING UPPER SURFACE FORWARD OF SPOILER. MX REMOVED SURFACE CORROSION AS REQUIRED. NO PITS FOUND ON THE BASE MATERIAL. TREATED ALUMINUM IAW BEECHCRAFT 400XP SRM 50-20-31,50-20-32,51-20-22 CORROSION SPOT MEASURES .250X.165. NO REISDR A6WA2020032647244Skin · dentedPERFORM PERMANENT REPAIR TO R/H L/E BETWEEN WS 226 TO WS 242 THAT MEASURES 2.0"L X 2.5" W X .037"D. "AIRCRAFT REMOVED FROM SERVICE" DENT AT WS 242 REFORMED TO ORIGINAL CONTOUR AND HFEC WITH NO CRACK INDICATIONS. REF ASAP EA# AWAC-CRJ257-01476 REV IR DTD 03/SDR R61A202003230445Winglet · cracked***WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY MAINTENANCE*** RH WINGLET CRACKED AT FWD SPAR. REMOVED AND REPLACED LH WINGTIP IAW 170EO-57-30-0001-1. AIRCRAFT REMAINS OUT OF SERVICE FOR THE REMAINDER OF HEAVY CHECK.SDR R61A2020032330444Winglet · cracked***WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY MAINTENANCE***LH WINGLET CRACKED AT FWD SPAR. REMOVED AND REPLACED LH WINGTIP IAW 170EO-57-30-0000-1. AIRCRAFT REMAINS OUT OF SERVICE FOR THE REMAINDER OF HEAVY CHECK.SDR KO0R202003130004Skin · corrodedLEFT WING UPPER SKIN AT XRS 80 (PANEL # 1307C CUTOUT) IS CORRODED.SDR KO0R202003130003Skin · corrodedLEFT WING UPPER SKIN AT XRS 125 (PANEL # 1303C CUTOUT) IS CORRODED.SDR KO0R202003130002Skin · corrodedRIGHT WING UPPER SKIN AT XRS 80 (PANEL # 1409C CUTOUT) IS CORRODED.SDR KO0R202003130001Skin · corrodedRIGHT WING UPPER SKIN AT XRS 125 (PANEL # 1410C CUTOUT) IS CORRODED.SDR C77A2020031200030Winglet · crackedTHIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH SB 170-57-0072 PART I, WHICH ACCOMPLISHES A STRUCTURAL MODIFICATION THAT CONSISTS OF REPLACING THE CURRENT LH WING TIP SPAR 1 (P/N 171-16231-001 OR 171-16231-003) WITH A NEW, REDESIGNED SPAR 1 (P/N 171-22480-401), WSDR C77A2020031200029Winglet · crackedTHIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH SB 170-57-0072 PART II, WHICH ACCOMPLISHES A STRUCTURAL MODIFICATION THAT CONSISTS OF REPLACING THE CURRENT RH WING TIP SPAR 1 (P/N 171-16231-002 OR 171-16231-004) WITH A NEW, REDESIGNED SPAR 1 (P/N 171-171-22480-40SDR SWIA2020031649264Skin Panel · crackedTRANSFER FROM EAML 397420 : TRANSFERRED FROM CAMP 20630046. CRACK FOUND ON LH WING FIXED LEADING-EDGE SKIN PANEL 522BL AT APPROXIMATELY SS181.00. FLIGHT 4732 - FILED CLOSED COMPLIED WITH TEMPORARY REO FOR REPAIR OF LEFT WING L/E BETWEEN SLAT TRACK 1-3 AND SDR SWIA2020041750135Skin · corrodedRH WING UPPER PLANK OPENING FOR 640CT HAS CORROSION AROUND NUT PLATE (C-CHECK) RO 4/16/2020 BLENDED OUT CORROSION AROUND THE OPENING AT PANEL 640CT REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. RECEIVED NEW REO. COMPLIED WITH ALL STEPS OF REO. BOND CHECK GOOSDR SWIA2020041750133Skin · corrodedLH WING UPPER PLANK OPENING FOR 540CT HAS CORROSION AROUND NUT PLATE (C-CHECK) RO 4/16/2020 BLENDED OUT CORROSION AROUND THE OPENING AT PANEL 540CT REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. RECEIVED NEW REO. COMPLIED WITH ALL STEPS OF REO. BOND CHECK GOOSDR SWIA2020041750130Skin · chafed*CENTER WING PLANK AFT RH BOTTOM EDGE APPROXIMATELY RBL45.0 IS CHAFFED (MARKED) (C-CHECK) RO 4/16/2020 PERFORMED REPAIR CENTER WING PLANK AFT RH BOTTOM EDGE APPROXIMATELY RBL45.0 REF BOMBARDIER REO, DWG. PRESSURIZATION LEAK WAS GOOD .SDR SWIA2020041750129Skin · chafed*CENTER WING PLANK AFT LH BOTTOM EDGE APPROXIMATELY LBL45.0 IS CHAFFED (MARKED) (C-CHECK) RO 4/16/2020 PERFORMED REPAIR CENTER WING PLANK AFT LH BOTTOM EDGE APPROXIMATELY LBL45.0 REF BOMBARDIER REO, DWG. PRESSURIZATION LEAK WAS GOOD.SDR SWIA2020033149779Nut Plate · brokenPANEL 571LL ON L/H WING HAS ONE BROKEN NUTPLATE. (C CHECK) RO 3/27/2020 REMOVED BROKEN NUTPLATE AND INSTALLED NEW P/N NAS1789-3 NUTPLATE IAW CRJ 200 SRM.SDR ABXA2020062620093Skin Panel · corrodedLT WING T/E LOWER SKIN PANEL HAS CORROSION NUMEROUS PLACES BETWEEN WS 815 AND WS 900. THE AIRPLANE WAS GROUNDED.SDR ABXA2020062620092Skin · corrodedLT WING UPPER SURFACE HAS CORROSION AT FASTENER HOLES 3 EA 258-262 INCHES OUTBD. THE AIRPLANE WAS GROUNDED.SDR ABXA2020062620091Skin · corrodedLT WING UPPER SURFACE HAS CORROSION AT FASTENER HOLE 170 INCHES OUTBD AT 86 INCHES INBD OF LEADING EDGE. THE AIRPLANE WAS GROUNDED.SDR ABXA20200320090Skin · corrodedLH WING UPPER SURFACE HAS CORROSION AT FASTENER HOLE 196 INCHES OUTBD AT 86 INCHES INBD OF LEADING EDGE. THE AIRPLANE WAS GROUNDED.SDR ABXA20200320089Skin · corrodedLH WING UPPER SURFACE HAS CORROSION AT FASTENER HOLE 25 INCHES OUTBD AT LEADING EDGE. THE AIRPLANE WAS GROUNDED.
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