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 FDEA202201270150Former · crackedRIGHT HAND WING OUTBOARD LEADING EDGE COMPOARTMENT AT APPROXIMATELY STATION XOS 559 01 EACH FORMER FOUND CRACK . RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 559 CRACKED FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG .SDR DALA2022013100602None · noneSHIP 5657 [AD.AA] LH ENG DRAG FTG CLAMP-UP HOLES #1 TO #10 INSPECTION WAS ACCOMPLISHED AND FOLLOWING DAMAGES WERE FOUND: HOLE #3 CORROSION ON SKIN BTW 11 TO 1 CLOCK POS ; HOLE #4 CORROSION ON SKIN AT 3 CLOCK POS , SCRATCHES ON FITTING AT 12, 6, 5, AND 9 CLOCK SDR DALA2022013100600None · noneSHIP 5657 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW;HOLE #14 SCRATCH ON FITTING BTW 5 OCLOCK POSITION, HOLE #17 CORROSION ON SKIN BTW 8 OCLOCK POSITION AND SCRATCHES ON SKIN AND FITTING BTW 11 TO 1 OCLOCK POSDR DALA2022013100599None · noneSHIP 5657 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #7 SCRATCH ON SKIN AND FITTING BTW 11 OCLOCK POSITION IN REF. CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00205. AREA WAS REPAIRED PER ETI-57-22-005 REV SDR 2024FA0000117Skin · crackedR/H WING AFT WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEWSDR IPXA2022021478950None · noneINSPECTION TYPE:1CRT WING T/E LOWER ACCESS DOOR SILL CRACK AT I/B STA. XORS 480.REMOVED AND REPLACED CRACKED SILL IAW SRM 51-33-01 (MINOR).SDR FDEA202201250131Angle · crackedLH WING FIXED LEADING EDGE NOSE FORMED ANGLE BROKEN AT WS 433. NOSE FORMED ANGLE WAS REPLACED FOR NEW ONE, AT LH WING FIXED LEADING EDGE AT WS 433 IAW EA #: H-5720-T0366557 AND SRM 51-10-02-0G PARAGRAPH 9(A) REV. 82 DEC15, 2021SDR FDEA202201250130Angle · crackedRH WING, FIXED LEADING EDGE WITH (2EA) NOSE FORMER ANGLES CRACKED AT L.E.S. 446.10, L.E.S. 500.10. RH WING, FIXED LEADING EDGE (2EA) NOSE FORMER ANGLES AT L.E.S. 446.10, L.E.S. 500.10 WERE REPLACED IAW E.A. #: H-5720-T0366557 AND SRM 51-10-02-0G PARAGRAPH SDR FDEA202201250129Angle · crackedLH WING FIXED LEADING EDGE NOSE FORMED ANGLE BROKEN AT WS 486. ANGLE WAS REPLACED AT LH WING FIXED LEADING EDGE NOSE AT WS 486 IAW E.A. #: H-5720- T0366557 AND SRM 51-10-02-0G PARAGRAPH 9(A) REV.82 DEC 15, 2021SDR DALA2022012600541None · noneSHIP 175 ER/A 584203-14AD SECT. I REPAIR WAS ACCOMPLISHED ON A/C 175 IN THE RH WING SKIN AT STR L-6.5. FOLLOW ON ACTION IS REQUIRED FOR SECT. III INSPECTION. CORRECTIVE ACTION: ACCOMPLISH ER/A 584203-14AD REV. A SECTION III PRIOR TO 6,000 CYCLES OR 18,000 FLIGSDR AALA202201246292Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING UPPER SKIN PANEL #2 LOWER SURFACE BETWEEN WMRX4390 AND WMRX6415, BETWEEN RIB 13 NAD RIB 14. REPAIRED SKIN PANEL PER EA 332921.SDR CALA2022012400209Skin · wornSUPPORT TASK RIGHT WING OB FWD FLAP IB END LE AREA SKIN WORN AS MARK, TRANSCRIBED FROM HAECO GSO NR LP 9280465 REPAIRED TRAILING EDGE FLAP NOSE SKIN IAW 57-53-01-2R-3 REPAIR 3 . HAECO GSO MECH V890956 INSP QC302SDR FDEA202201220117Skin · damagedINDY LINE FOUND ON NRC6053-509 TOP SKIN OF WEDGE ARC1953-503 (ARC1953-4, 2024-T3 0.025 TH, AND THE ARC1953-7 DOUBLER 0.016 TH ) PULLING BACK FROM IB EDGE (XOF 511.260 TO XOF 522.276), DAMAGED SKIN MEASURES 12" X 35" APPROX. REPAIRED FLAP WEDGE USING EA 8-5SDR YENA2022022500101Skin · failedDURING HEAVY MAINTENANCE, EXISTING REPAIR SLAT 1 EXTERNAL SKIN LEADING EDGE AREA ON LH WING (FOR AIGING AIRCRAFT PROGRAM - FCBS); PERFORMED PERMANENT REPAIR ON LEADING-EDGE SLAT 1 LH WING BETWEEN WFX957 AND TRACK 2 IAW EA 57-0010-22, AIRBUS RDAF 81010777/003/2SDR DALA2022012400460None · noneSHIP 5648 R/H WING UPPER SURFACE AFT I/B LARGE T/E PANEL IS BULGING UP ALONG FRONT EDGE IN 2 AREAS ABOVE WING REAR SPAR. CORRECTIVE ACTION: REPAIRED R/H WING UPPER SURFACE ON WING SKIN REAR SPAR AREA 160.00 - 170.00 IAW DELTA ERA 596513-14 REV ORIGINAL. (20938SDR DALA2022012400458None · noneSHIP 5648 LH ENG DRAG FTG CLAMP UP # 9 FASTENER HOLE HAS CRACK LIKE INDICATIONS IN THE FTG AT APPROX 6 & 9 OCLOCK POSITIONS. CORRECTIVE ACTION: REPAIRED L/H ENGINE DRAG FITTING # 9 FASTENER HOLE IN FITTING IAW ERA 585688-14AD REV C. (2094221)SDR DALA2022012400457None · noneSHIP 5648 LH ENG DRAG FTG CLAMP UP # 4 FASTENER HOLE HAS CRACK LIKE INDICATION IN THE FTG AT APPROX 6 OCLOCK POSITION. CORRECTIVE ACTION: REPAIRED L/H ENGINE DRAG FITTING # 4 FASTENER HOLE IN FITTING IAW ERA 585688-14AD REV C. (2094212)SDR DALA2022012400456None · noneSHIP 5648 LH ENG DRAG FTG CLAMP UP # 15 FASTENER HOLE HAS CRACK LIKE INDICATIONS IN THE FTG AT APPROX 12 OCLOCK POSITION. CORRECTIVE ACTION: REPAIRED L/H ENGINE DRAG FITTING # 15 FASTENER HOLE IN THE FITTING IAW ERA 585688-14AD REV C. (2094208)SDR DALA2022012400455None · noneSHIP 5648 LH ENG DRAG FTG CLAMP UP # 17 FASTENER HOLE HAS CRACK LIKE INDICATIONS IN THE SKIN AT APPROX 6 & 7 OCLOCK POSITION. CORRECTIVE ACTION: REPAIRED L/H ENGINE DRAG FITTING # 17 FASTENER HOLE IN WING SKIN IAW ERA 588688-14AD REV C. (2094198)SDR DALA2022012400454None · noneSHIP 5648 LH ENG DRAG FTG CLAMP UP 3 3 FASTENER HOLE HAS CRACK LIKE INDICATION IN THE FTG AT APPROX 5 OCLOCK POSITION. CORRECTIVE ACTION: REPAIRED L/H ENGINE DRAG FITTING 33 FASTENER HOLE IN FITTING IAW ERA 585688-14AD REV C. (2094192)SDR DALA2022012400453None · noneSHIP 5648 LH ENG DRAG FTG CLAMP UP # 10 FASTENER HOLE HAS CRACK LIKE INDICATIONS IN THE SKIN AT APPROX 6 & 7 OCLOCK POSITIONS. CORRECTIVE ACTION: REPAIRED L/H ENGINE DRAG FITTING # 10 HOLE IN THE WING SKIN IAW ERA 585688-14AD REV C. (2094187)SDR DALA2022012400452None · noneSHIP 5648 LH ENG DRAG FTG CLAMP UP # 2 FASTENER HOLE HAS CRACK LIKE INDICATIONS IN THE SKIN & FTG AT APPROX 8 OCLOCK POSITION. CORRECTIVE ACTION: REPAIRED # 2 FASTENER HOLE ON THE L/H ENGINE DRAG FITTING AND SKIN IAW ERA 585688-14AD REV C. (2094178)SDR DALA2022012400450None · noneSHIP 5648 RH ENGINE DRAG FITTING # 11 HOLE HAS 2 EA CRACK INDICATIONS OF CORROSION IN THE SKIN AND FITTING LAYER AT 3 AND 9 O CLOCK LOOKING AFT. CORRECTIVE ACTION: REPAIRED R/H ENGINE DRAG FITTING # 11 HOLE WING SKIN AND FITTING IAW ERA 585683-14AD REV C. (209SDR DALA2022012400449None · noneSHIP 5648 RH ENGINE DRAG FITTING # 13 HOLE HAS AN INDICATION OF CORROSION IN THE SKIN LAYER AT THE 9 OCLOCK POSITION LOOKING AFT. CORRECTIVE ACTION: REPAIRED R/H ENGINE DRAG FITTING # 13 HOLE IN WING SKIN IAW ERA 585683-14AD REV C. (2093981)SDR DALA2022012400448None · noneSHIP 5648 RH ENGINE DRAG FITTING # 4 HOLE HAS 2 EA CRACK INDICATIONS IN THE SKIN AT THE 3 AND 9 OCLOCK POSITIONS LOOKING AFT. CORRECTIVE ACTION: REPAIRED R/H ENGINE DRAG FITTING # 4 HOLE IN THE WING SKIN IAW ERA 585683-14AD REV C. (2093969)SDR DALA2022012400447None · noneSHIP 5648 RIGHT HAND ENGINE OUTBOARD DRAG FITTING VERTICAL SIDE FLANGE BOTTOM AFT HOLE IS SCORED. CORRECTIVE ACTION: REPAIRED R/H ENGINE O/B DRAG FITTING VERTICAL SIDE FLANGE BOTTOM AFT HOLE IAW ERA 585683-14AD REV C. (2093951)SDR DALA2022012400446None · noneSHIP 5648 DISCOVERED SHIM MIGRATION ON RH ENG INBD SHIM ID# 1A DURING CLAMP UP INSPECTION. CORRECTIVE ACTION: R/H ENGINE I/B SHIM REMOVED AND REPLACED IAW ERA 585683-14AD REV C ( DRAG FITTING TO WING SKIN).SDR DALA2022012400445None · noneSHIP 5648 #2 ENGINE PYLON OUTBOARD DRAG FITTING RADIUS BETWEEN HOLE 17 AND BUSHING HAS SCORE MARKS. CORRECTIVE ACTION: REPAIRED #2 ENGINE PYLON O/B DRAG FITTING RADIUS BETWEEN HOLE 17 AND BUSHING IAW ERA 585683-14AD REV C. (2093936)SDR DALA2022012100435None · noneSHIP 5648 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 585688-14AD REV.C. CORRECTIVE ACTION: REF ERA 585688-14AD REV C. (2093343)SDR DALA2022012100433None · noneSHIP 5648 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 585683-14AD REV.C. CORRECTIVE ACTION: REF ERA 585683-14AD REV C. (2091666)SDR DALA2022011900364None · noneSHIP 6822 A.A. / AD (VT)(GVI) WAS PERFORMED AND DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP, SECTION 2, AS FOLLOW: HOLE #1 CORROSION ON SKIN, BTW 6 AND 9 OCLOCK POSITION, HOLE #2 CORROSION ON FITTING AND SKIN, BTW 4 AND 7 OCLOCK POSITION, HOLESDR DALA2022011900363None · noneSHIP 6822 A.A./ A.D. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #15 SCRATCHES BTW 11-12 OCLOCK POSITION ON SKIN AND FITTING, HOLE #11 SCRATCHES AT 9 OCLOCK POSITION ON FITTING, HOLE #18 CORROSION BTW 2-3 OCLOCK POSDR IPXA2022012878391Stiffener · noneINSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N:111T2005-7) ON STA 785.9 , LBL 11.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.82.01, UPS EO B767-5740-58151-C AND UPS EO E767-5720-76672-A.SDR IPXA2022012878392Stiffener · noneINSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER(P/N:111T2008-12) ON STA 785.9, RBL 33.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV. 82.01, UPS EO B767-5730-58151-C AND UPS EO B767-5720-76672-ASDR FDEA202201110044None · noneAGING AIRCRAFT - EXISTING DOUBLER REPAIR FOUND AT LEFT HAND WING LEADING EDGE LOWER SURFACE SLAT TRACK NUMBER 10 CUTOUT STATION XOS =659. EXISTING DOUBLER REPAIR AT LEFT HAND WING LEADING EDGE LOWER SURFACE SLAT TRACK NUMBER 10 CUTOUT STATION XOS =659 EVALSDR FDEA202201110043None · noneAGING AIRCRAFT - EXISTING BEADED DOUBLER REPAIR FOUND AT LEFT HAND WING LEADING EDGE CAVITY STATION XOS =759 TO XOS =763. EXISTING BEADED DOUBLER REPAIR AT LEFT HAND WING LEADING EDGE CAVITY STATION XOS =759 TO XOS =763 EVALUATED AND FOUND REPAIRED IN ACCOSDR FDEA202201110042None · noneAGING AIRCRAFT - EXISTING BEADED DOUBLER REPAIR FOUND AT LEFT HAND WING LEADING EDGE CAVITY STATION XOS 636 TO XOS 643. EXISTING BEADED DOUBLER REPAIR AT LEFT HAND WING LEADING EDGE CAVITY STATION XOS =636 TO XOS=643 EVALUATED AND FOUND REPAIRED IN ACCORDASDR FDEA202201110041None · noneAGING AIRCRAFT - EXISTING BEADED DOUBLER REPAIR FOUND AT LEFT HAND WING LEADING EDGE CAVITY STATION XOS=629 TO XOS=633. EXISTING BEADED DOUBLER REPAIR AT LEFT HAND WING LEADING EDGE CAVITY STATION XOS=629 TO XOS=633 EVALUATED AND FOUND REPAIRED IN ACCORDANSDR SIMA20220108006Winglet · crackedRH WINGLET FWD ATTACH LUG IS CRACKED TWORDS BOTTOM AFT SIDE-C/A-COMPLETE:RAR'D RH WINGLET IAW EMB 175 AMM 57-30-00-400-801-A.SDR SIMA20220108007Winglet · crackedLH WINGLET FWD ATTACH POINT IS CRACKED-C/A-COMPLETE:RAR'D LH WINGLET IAW AMM 57-30-00.SDR IPXA2022020378605Skin · damagedINSPECTION TYPE:3CR/H WING FIXED L/E SKIN HAS IMPACT DAMAGE AT STA. XOS. 1063.REPAIRED DAMAGED R/H WING FIXED L/E SKIN AT STA. XOS. 1063 IAW VT-SAA EA 011-5730-01-A9455 REV. I/R AND UPS EO MD11-5730-82770-A. (MAJOR) REF. FAA FORM 8100-9SDR FDEA202201060016Doubler · crackedRIGHT HAND WING - LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 796 FOUND CRACK. RIGHT HAND WING LEADING EDGE CAVITY DOUBLER AT STATION XOS 796 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 1SDR FDEA202201060017Doubler · crackedLEFT HAND WING - LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 654 FOUND CRACK. LEFT HAND WING LEADING EDGE CAVITY DOUBLER AT STATION XOS 654 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100SDR FDEA202201060015Skin · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO ACCESS DOOR CORNER NUMBER 5 FOUND CRACK APPROXIMATE 0.2 " AT APPROXIMATE STATION XOS 491. LEFT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO ACCESS DOOR CORNER NUMSDR IPXA2022012078074Slat · crackedINSPECTION TYPE:1CLT WING #2 SLAT INNER SKIN CRACK AT UPPER O/B END.REMOVED AND REPLACED LT WING #2 SLAT ASSY. IAW AMM 27-80-20.SDR IPXA2022012078066None · corrodedINSPECTION TYPE:1CLT WING T/E REAR SPAR UPPER CAP HAS CORROSION BETWEEN XORS.729 AND XORS. 752 .REPAIRED CORRODED UPPER CAP AT LT WING IAW MD-11 SRM 57-00-10 AND 51-21-01 (MINOR)SDR IPXA2022011877987Doubler · crackedINSPECTION TYPE:1CRT WING FIXED L/E BEADED DOUBLER CRACK BETWEEN STA.XOS=753-0-XOS=759.1REPAIRED RT WING CRACKED BEADED DOUBLER BETWEEN STA.XOS 753.0-XOS=759.1 IAW SRM 57-40-02 REPAIR 15,FIG 205 REV.68.01.(MAJOR).SDR FDEA202201050007None · noneAGING AIRCRAFT - EXISTING BEADED DOUBLER REPAIR FOUND AT RIGHT HAND WING LEADING EDGE CAVITY STATION XOS 999. EXISTING BEADED DOUBLER REPAIR AT RIGHT HAND WING LEADING EDGE CAVITY STATION XOS 999 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 57-4SDR HNAA2022021000073Not Reported · not reportedE894799 - LH INBD FLAP SHROUD HINGE HAS 2 FASTENERS THAT ARE PULLING THRU AT INBD END .... REMOVED LH INBOARD FLAP SHROUD HINGE
SECTION WITH 2 FASTENERS PULLING THROUGH AT INBOARD END, PREPPED AND INSTALLED SERVICEABLE HINGE SECTION IAW EMB 145 SRM 51-20-03, SDR COEA2022020105819Skin · corrodedWO 232464 NR 500008 HEAVY CHECK COE/MAJOR REPAIR: L/H UPPER WING CUT-OUT LANDING FOR PANEL 521DT HAS FRETTING. LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS DO/TS-531/06...3474 ISSUE H, DATED 1/27/2022.
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