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 JGVR20181210002Access Panel · corrodedFUEL PANEL LANDS 511AB, 511BB, 511DB, AND 511EB HAVE AREAS OF CORROSION. BLENDED AREAS OF CORROSION ON FUEL PANEL LANDS 511AB, 511BB, 511DB, AND 511EB IAW CITATION 560XL SPM: 51-10-00. PERFORMED REPAIR TO BLENDED AREAS PER TEXTRON LETTER REF. DQ16664M1 RRL DATSDR JGVR20181210001Panel · corrodedUNDER-WING PANELS 510DB AND 610DB HAVE SMALL AREAS OF CORROSION. FOUND DURING COMPLIANCE OF TASK A570000. REPLACED CORRODED FUEL ACCESS PANELS 510DB AND 610DB WITH NEW FUEL ACCESS PANELS PN:9912514-22 AND 9912514-21.SDR SWAA2022022822978Seal · crackedLEFT HAND HORIZONTAL STAB; FORWARD LOWER SLIDER SEAL TEFLON RUNNER CRACKED / REPLACED L/H HORIZONTAL STAB; FORWARD LOWER SLIDER SEAL IAW AMM 53-31-31-000-803 AND AMM 53-31-31-400-803 AND IPC 53-31-31-02A ATAG #UK1490; AA9777SDR DALA2018121187148Access Panel · missingACCESS PANELS 522MB, 522PB, 622MB, 622PB MISSING ON LEFT AND RIGHT WING. COVERED AREAS WITH SPEED TAPE AND DEFERRED. LP 5263059SDR SWAA2022022815387Panel · elongatedR/W T/E PANEL 671BB HAS A ELONGATED HOLE. ( MARKED ) / REPAIRED ELONGATED HOLE ON R/W T/E PANEL 671BB IAW SRM 51-70-05-2R-6 59278U 12/17/18SDR DALA2018121067124Skin · damagedDAMAGE ON LWR AFT TRAILING EDGE OF WING TIP L/H SIDE. C/W PERMAMENT REPAIR PER SRM 57-31-01. (LP 5263140)SDR AALA201812269004Skin · corrodedCORROSION FOUND ON THE SKIN BETWEEN RIBS 5 - 6 ON THE LEFT WING. REPAIRED THE SKIN IAW EA 105103A.SDR AALA201812075003Skin · crackedDURING ACCOMPLISHMENT OF ECO F2326AA-001, AND HFEC ROTARY HOLE PROBE INSPECTION, ON THE LEFT WING DIAGONAL BRACE, FASTENER HOLE NR 9, FOUND A CRACK INDICATION IN THE SKIN LAYER ONLY AT THE AFT INBOARD SIDE OF HOLE. REPAIRED IAW EA 287209.SDR DALA2018120407032Skin · damagedRT LOWER WING SKIN STRINGER L-6.5. BETWEEN WSTA990.2 AND WSTA1018.2. DIAMETER:0.625" HOLE REPAIRED PER ER/A 572984-14.SDR DALA2018120407031Skin · crackedLT WING LOWER SKIN, STRINGER L-9.5 WSTA906.20 TO WSTA934.20. ONE CRACKED HOLE REPAIRED PER ER/A 572983-14.SDR DALA2023011300272Doubler · not reportedSHIP 183 RH LOWER WING SKIN EXTERNAL DOUBLER REPAIR AT STR 6.5 AND STA 990. CORRECTIVE ACTION: ER/A 572984-14AD REVISED TO REV. A. ACCOMPLISH ER/A 572984-14AD REV A SECTION II INSPECTIONS. (0850550)SDR SWAA2022022858659Panel · delaminatedFWD OUTB'D CORNER OF PANEL 621SB DELAMINATED. / REPAIRED PANEL PER SRM 57-41-01SDR FDEA201812030123Skin · corrodedRT WING, CORROSION ON UPPER SURFACE, 22" AFT OF FRONT SPAR AT WS 204.5 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND SDR FDEA201812030122Skin · corrodedRT WING, CORROSION ON UPPER SURFACE, ABOVE REAR SPAR AT WS 269 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TOSDR FDEA201812030121Skin · corrodedRT WING, CORROSION ON UPPR SURFACE, ABOVE REAR SPAR AT WS 361 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TO SDR FDEA201812030120Skin · corrodedRT WING, CORROSION ON UPPER SURFACE, ABOVE FRONT SPAR, WS 642 TO WS 654 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 ANSDR FDEA201812030119Skin · corrodedRT WING, CORROSION ON UPPER SURFACE, AS OF REAR SPAR WS 289-293 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TSDR FDEA201812030118Skin · corrodedRT WING CORROSION ON UPPR SURFACE AFT OF REAR SPAR, WS312 TO WS316 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUNSDR FDEA201812030112Skin · corrodedLT WING, CORROSION ON UPPER SURFACE, ABOVE REAR SPAR AT WS 215 REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUTS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 TABLE 1 REV 125, AND FSDR FDEA201812030111Skin · corrodedLT WING, CORROSION ON UPPER SURFACE, ABOVE REAR SPAR AT WS 300 REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUT IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 TABLE 1 REV 125, AND FOSDR FDEA201812030110Skin · corrodedLT WING UPPER TE, EVIDENCE OF CORROSION ADJACENT TO FASTENER HEADS AT AREA 5 INCHES AFT OF REAR SPAR AND 67 INCHES OUTBOARD OF WING ROOT FAIRING 195AL REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUT IAW SRM 57-20-01-1A ALLOWABLE DASDR ASOA2018121935345Skin · crackedREF: CO# 7496618 JOB# 7749665 OP# 35: LOWER WING PLANK CUTOUT FOR R/H BOOST PUMP HAS AN INDICATION NOTED ON THE LOWER SURFACE OF THE WNG PLANK ON THE AFT SIDE OF CUT OUT. INDICATION IS .150" LONG BY 100% FSH. FAILED NDT INSPECTION.C/A: REPAIRED DAMAGE I.A.W. SDR YENA2018120730817Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN LOCATED UPPER SURFACE BTWN RIB 4-5 ON LH WING; PERFORMED PERMANENT REPAIR LOC EXTERNAL SKIN BTWN RIB 4-5 UPPER SURFACE ON LH WING IAW EA 57-0384-18 REV.0 PART 1 & 2 / EC A18-990-01. THIS JOB MSDR YENA2018120730816Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN LOCATED UPPER SURFACE BTWN RIB1-2 ON LH WING; PERFORMED PERMANENT REPAIR LOC EXTERNAL SKIN BTWN RIB 1-2 UPPER SURFACE ON LH WING IAW EA 57-0384-18 REV.0 PART 1 & 2 / EC A18-990-01. THIS JOB MUSDR YENA2018120730815Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN LOCATED UPPER SURFACE AT LEVEL RIB 7 ON LH WING; PERFORMED PERMANENT REPAIR LOC EXTERNAL SKIN BETWEEN RIB 7 UPPER SURFACE ON LH WING IAW EA 57-0384-18 REV.0 PART 1 & 2 / EC A18-990-01. REF. AESDR YENA2018120730814Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN LOCATED BTWN RIB 8-9 UPPER SURFACE ON LH WING; PERFORMED PERMANENT REPAIR LOC EXTERNAL SKIN BTWN RIB 8-9 UPPER SURFACE ON LH WING IAW EA 57-0384-18 REV.0 PART 1 & 2 / EC A18-990-01. REF. AEROMSDR FDEA201812033418Finger Doubler · detachedRIGHT WING TRAILING EDGE INBOARD ISLAND UPPER SKIN FINGER DOUBLER AT XORS 449 FOUND DETACHED. RIGHT WING - TRAILING EDGE INBOARD ISLAND UPPER AT XORS 449 DAMAGED SKIN AREA REPAIRED AS PER SRM 57-50-01-2R FIGURE 202 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER SDR FDEA201811300155Skin · corrodedLT WING, UPPER SURFACE RSS 170 TO RSS 200 AT WING SKIN AND TRAILING EDGE PANEL JOING SUSPECT CORROSION. COROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE OF LIMITS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 1 REV 125. REPAIR CARRIED OUT IAW EA #F-573SDR FDEA201811300109Skin · corrodedPLEASE EVALUATE EXISTING BLENDS ON LT WING UPPER SURFACE AT WS.748 TO WS761, 2 INCHES FWD OF REAR SPAR AND TRILING EDGE PANEL JOINT REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUTS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 ANSDR FDEA201811300108Skin · corrodedPLEASE EVALUATE EXISTING BLENDS ON LT WING UPPER SURFACE AT WS 791 TO WS 806, 7 INCHES AFT OF FRONT SPAR AND LEADING EDGE JOINT REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUTS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101 TABLE SDR FDEA201811300107Skin · corrodedPLEASE EVALUATE EXISTING BLENDS ON LT WING UPPER SURFACE AT WS 791 TO WS 806, 7 INCHES AFT OF FRONT SPAR AND LEADING EDGE JOINT REMOVED CORROSION IAW SRM 51-10-02 REV 125 EVALUATED BLEND OUT AND FOUND AREA TO BE OUT OF LIMITS IAW DUE TO LOCATION OF DAMAGE IAW SDR ASOA2018121435341Skin · corrodedREF: CO# 7476718 JOB# 7747675 OP# 57 LOWER WING PLANK CUTOUT FOR RH BOOST PUMP HAS MULTIPLE INDICATIONS NOTED AROUND ENTIRE CIRCUMFERENCE ON HORZ AND VERTICAL SURFACE 50% FSH. FAILED NDT INSP. C/A: PERFORMED MAJOR REPAIR CARD NO: REO 601R-57-21-2908 BLENDED TOSDR AALA201812039001Skin · crackedA CRACK WAS FOUND ON THE LOWER SKIN, OTBD FIXED LEADING EDGE RIB 15 ON THE RT WING. REPAIRED THE SKIN IAW SRM 57-41-11-300-013, AND DRAWING D574-59073.SDR JGVR20181130001Access Panel · corrodedCENTER WING FUEL QUANTITY DIPSTICK PANEL 172BZ HAS LEVEL 2 CORROSION AROUND SEVERAL SCREWS REQUIRING REPLACEMENT OF OUTER PANEL. FOUND WHILE PERFORMING C750 BASE CHECKLIST.SDR FDEA201811290068Skin · corrodedLT OVERWING FILL PORT HAS EVIDENCE OF CORROSION CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01-1A FIG 102 DETAIL 1. REV 125 ALLOWABLE MINIMUM REMAINING THICKNESS = 0.240" ACTUAL REMAINING THICKNESS = 0.145" REPAIRSDR FDEA201811290066Skin · corrodedRT OVERWING FILL PORT HAS EVIDENCE OF CORROSION CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01-1A FIG 102 DETAIL 1. ALLOWABLE MINIMUN REMAINING THICKNESS = 0.240" ACTUAL REMAINING THICKNESS = 0.148 REPAIR CARRIED OUSDR SWIA2018121245310Skin · dentedDENT ON RH WING LEADING EDGE. (FLT#3110) FO: 11/30/2018. CLOSED C/W REO.SDR SWIA2018113045310Skin · dentedDENT ON RT WING LEADING EDGE. FLIGHT 3110. FO: 11/30/2018. CARRIED FORWARD FOR RESCHEDULING, TIME REMAINING UNTIL NEXT RE-INSPECTION IS DUE OR UNTIL PERMANENT REPAIR IS REQUIRED.SDR R61A201812181242Skin · cracked*** WHILE THE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** MAJOR... A 0.465 INCH CRACK WAS FOUND ON LH WING LOWER SKIN @ RIB 17 AND STR 19. CRACK WAS REPAIRED IAW ETD2018-170-125321 REV A. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECKSDR ASOA2018121475339Skin · crackedREF: CO#7476718 JOB# 7747675 OP#43 R/H LOWER WING PLANK AND STRAP JOINT CRACKED AT RWS 148.00. C/A REPAIRED DAMAGE IAW EXPRESSJET ECTC REO 601R-57-21-130 01.SDR DALA2018112766842Skin · corrodedLEFT WING LOWER SKIN WSTA 962.2-900.2 HAS A CRACKED FASTENER HOLE AT L-9.5. C/W ERA 573238-14. (LP 5141061)SDR FDEA201811233355Finger Doubler · detachedRIGHT WING FINGER DOUBLER FOUND DETACHED AT ISLAND UPPER SKIN OUTBOARD OF INBOARD AILERON AT STATION XW 375 AND E 65.00. REPAIR CARRIED OUT ON STATION XW 375, E 65.00 TO E 70.00 AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-SDR FDEA201811233354Finger Doubler · detachedLEFT WING FINGER DOUBLER FOUND DETACHED AT ISLAND UPPER SKIN OUTBOARD OF INBOARD AILERON AT STATION XW 375 AND E 65.00. REPAIR CARRIED OUT AT STATION XW 375, E 65.00 TO E 70.00 AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-SDR DALA2018112626781Skin · damagedSKIN FOUND THE NO.66 HOLE DIAMETER :0.624" REPAIRED PER ERA 573161-14. (LP 0836480)SDR DALA2018112626780Skin · crackedHFEC SURFACE INSPECTION FOUND 01 EA CRACK APPROX 0.080"IN LENGTH AT THE FWD DIRECTION OF THE MOST O/B HOLE AND REPAIRED. (LP 0836471)SDR ASOA201811185325Skin · damagedREF: CO# 7654518 JOB# 7765456 OP# 6: WHILE PERFORMING SB 601R-57-046, FOUND (1EA) FASTENER TO BE OVERSIZE IN R/H LOWER BUTTSTRAP AND WINGPLANK.C/A: REPAIRED DAMAGE I.A.W. BOMBARDIER REO 601R-57-21-2900 REV.--, DATED 2018-11-12 AND EXPRESSJET EC/TC REO 601R-57-SDR FDEA201811183273Doubler · crackedRIGHT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 667 FOUND CRACK. DOUBLER REMOVED AS PER SRM 51-31-01-0G AND REPLACED WITH NEW RIB DOUBLER AS PER SRM 51-33-01-0G. FABRICATED RIB DOUBLER AS PER DWG ARB3954 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10SDR K11A2020010302Skin · corrodedLEFT WING UPPER SURFACE WBL 72 APPROX S-19C HAS CORROSIONSDR AALA2018121989019Skin · wornWEAR FOUND ON THE INBOARD SKIN ON THE FIXED LEADING EDGE RIB UNDER THE ROOT FILLER FAIRING BETWEEN STATION 0 - 700, RIB 1 TO 2, LT WING. REPAIRED THE SKIN IAW EA 287405.SDR DALA2018121307165Skin · crackedRIGHT WINGS UPPER SKIN PANEL OUTBOARD UPPER LINK PITCH LOAD FITTING AREA CRACKED FASTENER LOCATIONS C/W ERA 507538-14 (LP 0829134)
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