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 AMWA0828013ASkin · damagedRT UPPER WING SKIN BETWEEN WS117.5 AND WS133 HAD NUMEROUS ELONGATED HOLES FROM OVERSIZED RIVETS. REPAIRED IAW REPORT NR 6878-1 REV IR.SDR 07FDEA04453Skin Panel · corrodedFOUND CORROSION AT CENTER TANK TOP SKIN C 44-48, TRACK 3-5, LT/RT REPAIR PERFORMED BY REMOVAL OF CORROSION AND INSTALLING OF TWO DOUBLERS IAW DRAWING R573-10011 AT BEAM 4 AND 6, C 44-2 AND C 44 LT/RT IAW EA 6-5710-81129 AND RAS/AS/0036/2005 ISS A.SDR 07FDEA04450Skin · wornFOUND ON RT WING ON PYLON NR 2 ELONGATED HOLE AT WING TO PYLON BOTTOM SKIN ON AREA OF HYDRAULIC LINES. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW DRAWING R572-49184, APPROVED BY EA 6-5720-81128 AND RAS/BAE/100457/2005 ISS A.SDR 07FDEA04449Skin · wornFOUND ON LT WING ON PYLON NR 1 ELONGATED HOLE AT WING TO PYLON BOTTOM SKIN ON AREA OF HYDRAULIC LINES. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW DRAWING R572-49184, APPROVED BY EA 6-5720-81128 AND RAS/BAE/100457/2005 ISS A.SDR 07FDEA04436Skin · corrodedFOUND CORROSION ON LT WING BOTTOM SKIN AT RIB 7-8, CENTER SPAR STRINGER 13 REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW EA 6-5720-112460 AND RAS/BAE/1005212/2007 ISS A.SDR 07FDEA04435Skin · corrodedFOUND CORROSION ON RT WING BOTTOM SKIN RIB 1-2 IN FRONT OF FRONT SPAR NEAR TRACK NR 1 REPAIR PERFORMED BY REWORK OF CORROSION IAW EA 6-5720-112461 AND RAS/BAE/1005290/2007 ISS A.SDR FDEA200710014425Skin · looseDURING INSPECTION ON RT WING OTBD FLAP LWR SKIN FOUND 50 LOOSE FASTENERS. REPAIRED AREA IAW SRM 57-00-01 VOL I FIG 4 SHT 5.SDR TRAX200701452Skin · corrodedFLANGE (ON WING) OF FWD PANEL 622CT CORRODED. 10-11-07 RT WING FLANGE, 622 CT AREA, CORROSION REMOVED IAW SRM 57-14-12 FIG 401. FLANGE WITHIN LIMITS (MATERIAL REMAINING 0.746") IAW SRM 57-14-12 FIG 301, HFEC PERFORMED IAW NTM, NO CRACKS FOUND. REPAIR DETSDR TRAX200701450Skin · corrodedLEFT WING FLANGE OF ACCESS 521DT CORRODED. 10-11-07 LT WING FLANGE, 521 DT AREA, CORROSION REMOVED IAW SRM 57-14-12 FIG 401 FLANGE WITHIN LIMITS (MATERIAL REMAINING 0.762") IAW SRM 57-14-12 FIG 302 HFEC PERFORMED IAW NTM. NO CRACKS FOUND, REPAIR DESDR TRAX200701449Skin · corrodedLEFT WING FLANGE OF ACCESS 522CT CORRODED. 10-11-07 LT WING FLANGE 522 CT AREA, CORROSION REMOVED IAW SRM 57-14-12 FIG 401. FLANGE WITHING LIMITS (MATERIAL REMAINING), 0748 IAW SRM 57-14-12. HFEC PERFORMED BY HEATHAIR AMO 46-90 W/O 37536 IAW NTM NO CRACKSDR DLM90071289Skin · puncturedLT FIXED WING L/E SKIN STA XRS 105.000 HAS A PUNCTURE. REPAIRED L/E SKIN IAW MD-90 SRM 57-20-01 FIG 11 VOL 1 ON N/R 5200-0043 ON HMV-2 IN OKC.SDR UIEA200700418Panel · delaminatedLT WING UPPER L/E FIXED PANEL AT WS 490.00 HAS AN AREA OF 2.0 INCH LONG BY 2.0 INCH WIDE OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18, SHEETS 1 THRU 5 AND SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A393.SDR UIEA200700417Panel · delaminatedRT WING UPPER L/E FIXED PANEL AT WS 317.32 HAS AN AREA OF 2.0 INCH LONG BY 2.0 INCH WIDE OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18, SHEETS 1 THRU 5 AND SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A393.SDR 07FDEA04379Doubler · crackedRIGHT WING FIXED LEADING EDGE LOWER ANGLE DOUBLER AT XOS 546 FOUND CRACKED. 10-16-07 RT WING FIXED LEADING EDGE LOWER ANGLE CRACKED DOUBLER AT XOS 546 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100.SDR 07FDEA04378Access Panel · crackedRIGHT WING LEADING EDGE ACCESS PANEL 618GB INBOARD SUPPORT FOUND CRACKED. 10-16-07 RIGHT HAND WING LEADING EDGE ACCESS PANEL 618GB CRACKED INBOARD SUPPORT STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER FEDEX SDR 07FDEA04365Skin · chafedFOUND CHAFING MARKS BETWEEN SLAT TRACK 6 AND JACK 4, LEADING EDGE SKIN, RT WING. REPAIR PERFORMED BY INSTALLATION OF NEW SKIN INSERT IAW SRM 57-41-12/FIG 203, 204.SDR 07FDEA04364Skin · chafedFOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 203, 204, CHAFING MARKS BETWEEN SLAT TRACK 5 AND SLAT TRACK 6, LEADING EDGE SKIN, RT WING. NEW REPAIR SKIN INSERT INSTALLED IAW SRM 57-41-12/FIG 203, 204.SDR 07FDEA04363Skin · chafedFOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 204, CHAFING MARKS BETWEEN JACK 3 AND SLAT TRACK 5, LEADING EDGE SKIN, RT WING. NEW REPAIR SKIN INSERT INSTALLED IAW SRM 57-41-12/FIG 203, 204.SDR 07FDEA04360Skin · chafedFOUND CHAFING MARKS BETWEEN JACK 3 AND SLAT TRACK 5, LEADING EDGE SKIN, LT WING. NOSE SKIN REPAIR PERFORMED SRM 57-41-12/FIG 203, 204.SDR 07FDEA04359Skin · chafedFOUND CHAFING MARKS BETWEEN SLAT TRACK 5 AND SLAT TRACK 6, LEADING EDGE SKIN, LT WING. REPLACEMENT OF CHAFED NOSE SKIN IAW SRM 51-72-10.SDR 07FDEA04354Skin · corrodedOLD DOUBLER REPAIR AT RT WING-LET TO STATIC DISCHARGER NO. V, FINAL REPAIR IS NECESSARY. AFTER REMOVAL OF DOUBLER FOUND ADDITIONAL CORROSION AND A MISDRILLED HOLE ON THE SKIN OF INBOARD PANEL OF RT FENCE. REPAIR PERFORMED BY SKIN CUTOUT AND INSTALLING FABRICSDR CALA0700543Skin · crackedINSPECTION FOUND A .75 INCH CRACK IN RIGHT WING LEADING EDGE SKIN AT NR 5 SLAT ACTUATOR. THE SKIN WAS REPAIRED IAW SRM 57-41-01, PAGE 202, FIGURE 201.SDR 07FDEA04346Skin Panel · wornELONGATED HYDRAULIC FITTING HOLE NR 1 ON RT WING LOWER SKIN, PYLON SUPPORT BRACKET, RIB 8. REPAIR OF HOLE NR 1 PERFORMED BY OVERSIZING AND BUSHING IAW EA 6-5720-82851 AND RAS/BAE/1000639/2005 ISSUE A.SDR A6WA200740568Skin · corrodedLT LOWER WING PLANK AT ACCESS PANEL 540 CB HAS MINOR PITTING DAMAGE IN NON-CRITICAL AREA, .001-.002 INCH DEEP. MAINTENANCE REPAIRED LT LOWER WING PLANK PER BOMBARDIER REO 601R-57-21-030 REV F. (M)SDR A6WA200740571Skin · corrodedMINOR PITTING ON RIGHT LOWER WING PLANK WS 54.897 ACCESS PANEL 640BB IN NON-CRITICAL AREA. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030. (M)SDR A6WA200740570Skin · corrodedMINOR PITTING DAMAGE LT LOWER WING PLANK WS 188.040 FUEL ACCESS PANEL 550BB IN NON-CRITICAL AREA .001 INCH -.002 INCH DEEP. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030. (M)SDR A6WA200740572Skin · corrodedMINOR PITTING DAMAGE RT LOWER WING PLANK WAS 12.245 ACCESS PANEL 610AB, .001 INCH-.002 INCH DEEP IN CRITICAL AND NON-CRITICAL AREAS. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)SDR A6WA200740569Skin · corrodedLT LOWER WING PLANK HAS MINOR PITTING DAMAGE IN A NON-CRITICAL AREA .001-.002 DEEP AT WING ACCESS PANEL 540BB. MAINTENANCE REPAIRED LT LOWER WING PLANK IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)SDR EIA2007183Skin · corrodedLEFT WING LOWER SKIN AT FSSI 1050-1070 SKIN UPPER FOWARD SIDE OF FRONT SPAR FOUND CORROSION. BLENDED OUT SKIN CORROSION PER B747 SRM 51-10-01. PERFORMED DVI OF BLEND AREA AND HFEC OF HOLES AND SURFACE. FLAP PEEN AREA PER SOPM 20-10-03. FABRICATED REPAIR PESDR UIEA200700403Skin · corrodedLEFT WING UPPER SURFACE WS 807 TO STR 516 SURFACE CORROSION EVIDENT. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.
SDR UIEA200700402Skin · corrodedLEFT WING UPPER SURFACE WS 353 TO WS 586 REAR SPAR HAS MINOR SURFACE CORROSION EVIDENT. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.
SDR UIEA200700400Skin · corrodedRIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 724.5 TO WS 917 BETWEEN MID SPAR AND FRONT SPAR. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700399Skin · corrodedRIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 724.5 TO WS 917 BETWEEN MID SPAR AND REAR SPAR. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700398Skin · corrodedRIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 528 TO WS 724.5 BETWEEN MID SPAR AND REAR SPAR. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700397Skin · corrodedRIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM SIDE OF BODY TO WS 528 BETWEEN MID SPAR AND FRONT SPAR. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700396Skin · corrodedRIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM SIDE OF BODY TO WS 528 BETWEEN MID SPAR AND FRONT SPAR. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.
SDR UIEA200700395Skin · corrodedRIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 528 TO WS 724.5 BETWEEN MID SPAR AND FRONT SPAR. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700394Skin · corrodedRIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM SIDE OF BODY TO WS 528 BETWEEN MID SPAR AND REAR SPAR. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR 07FDEA04306Skin Panel · failedFOUND OLD REPAIR ON BOTTOM SKIN FLANGE SUPPORT STRAP AFT FROM REAR SPAR, INBOARD OF RIB NR 9, LT WING CRACK (20MM) IN SUPPORT FLANGE. REPAIR PERFORMED BY MOD SB A300-57-6064 (FINAL REPAIR).SDR A6WA200740576Skin · corrodedRIGHT LOWER WING PLANK FOR FUEL PANEL 650AB CUT OUT HOLE NR 9 HAS MINOR CORROSION IN NON-CRITICAL AREA APPROX .003 INCH DEEP. MAINTENANCE REPAIRED RT LOWER WING PLANK FOR FUEL PANEL 650AB CUT OUT HOLE NR 9 IAW AIR WISCONSIN E06/021/457 AND BOMBARDIER REO 601RSDR A6WA200740575Skin · corrodedLT LOWER WING PLANK FUEL PANEL CUTOUT FOR PANEL 510AB HOLE NR 2 HAS MINOR CORROSION IN NON-CRITICAL AREA APPROX .003 INCH DEEP. MAINTENANCE REPAIRED LT LOWER WING PLANK FUEL PANEL CUT OUT FOR PANEL 510AB HOLE NR 2 IAW AIR WISCONSIN E06/021/457 AND BOMBARDIER SDR A6WA200740577Skin · corrodedRIGHT LOWER WING PLANK FUEL PANEL CUT OUT FOR PANEL 640BB HOLE NR 1 HAS MINOR CORROSION IN NON-CRITICAL AREA APPROX .003 INCH DEEP. MX REPAIRED RIGHT LOWER WING PLANK FUEL PANEL CUT OUT FOR PANEL 640BB HOLE NR 1 IAW AIR WISCONSIN E06/021/457 AND BOMBARDIER RESDR UIEA200700393Skin · corrodedRIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700371Skin · corrodedSURFACE CORROSION EVIDENT AROUND HEAD FROM WS 724.50 TO WS 917.00 BETWEEN REAR SPAR AND MID SPAR. SURF, CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700382Skin · corrodedLHW UPPER SURFACE MID SPAR WS 1112 WS 1280 WS 1330 WS 1392 CORROSION EVIDENT. SURF CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700383Skin · corrodedSURF CORROSION EVIDENT AROUND HEAD FROM WS 528 TO WS 724.5 BETWEEN REAR SPAR AND MID SPAR. SURF CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR UIEA200700380Skin · corrodedLHW UPPER SURFACE WS 807 STR S16 CORROSION EVIDENT. SURF CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR 07FDEA04258Skin · delaminatedCORROSION AND DELAMINATION FOUND AT RT WING TE PANEL ASSY TO PREVIOUS REPAIRS REPAIR PERFORMED BY DAMAGE REMOVAL, BONDING REPAIR AND INSTALLING OF NEW ANGLES AND DOUBLERS IAW EA 6-5720-112455 AND RAS/BAE/1003755/2006 ISS A.SDR 07FDEA04255Skin Panel · corrodedCORROSION FOUND UNDER LT WING TIP STATIC DISCHARGER NR 1. REPAIR PERFORMED BYBLEND OUT CORROSION AND INSTALLING A PATCH IAW EA 6-5730-112474 AND RAS/FOK/178/2007 ISS A.SDR 07FDEA04254Skin Panel · corrodedCORROSION FOUND UNDER RT WING TIP STATIC DISCHARGER NR 1 AND NR 2 REPAIR PERFORMED BY BLEND OUT CORROSION AND INSTALLING A PATCH IAW EA 6-5730-112504 AND RAS/FOK/179/2007 ISS A.
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