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 FDEA202112062991Skin · crackedRIGHT HAND WING FIXED LEADING EDGE SKIN AT APPROXIMATE STATION XOS 990 FOUND CRACK. RIGHT HAND WING FIXED LEADING EDGE SKIN AT APPROXIMATE STATION XOS 990 REPAIR CARRIED OUT AS PER SRM 57-40-01-2R REPAIR 9 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6SDR SWAA2021120850260Panel · delaminatedFOUND R/T WING PANEL 651AT DELAMINATED ON CENTER LOWER SIDE APPROX. 7''X 7.5''. REMOVED AND REPLACED R/T WING PANEL 651AT PER SIPSDR WX0A1900010073983Skin · corrodedNRC 5000-0015: 1237-19. LH WING, UPPER SKIN PANEL, CORROSION FOUND BTW REAR SPAR AND FALSE SPAR AT RIB 6 AREA. / LH WING, UPPER SKIN PANEL CORROSION BETWEEN REAR SPAR AND FALSE SPAR AT RIB 6 AREA REPAIRED AS PER AIRBUS DOSSIER 80990965 AND REPAIR DRAWING R572SDR WX0A1900010073982Skin · corrodedNRC 5000-0013: 1237-17. LH WING, UPPER SKIN PANEL SEVERAL CORROSION SPOTS (3X) FOUND AT REAR SPAR AREA BTW RIB 14-15. / LH WING, UPPER SKIN PANEL CORROSION SPOTS AT REAR SPAR AREA BETWEEN RIB 14-15 REPAIRED AS PER AIRBUS DOSSIER 80990965 AND REPAIR DRAWING R5SDR WX0A1900010073981Skin · corrodedNRC 5000-0012: 1237-16. LH WING, UPPER SKIN PANEL, CORROSION FOUND AT REAR SPAR AND RIB 17 AREA. / LH WING, UPPER SKIN PANEL CORROSION AT REAR SPAR AREA AND RIB 17 REPAIRED AS PER AIRBUS DOSSIER 80990965 AND REPAIR DRAWING R572-58616 ISSUE K PARA. D AND COMPLSDR WX0A1900010073980Skin · corrodedNRC 5000-0010: 1237-14. LH WING, UPPER SKIN PANEL, CORROSION FOUND AROUND BONDING SPIGOT HOLE (FRONT SPAR INBD OF RIB 20 AREA) / LH WING, UPPER SKIN PANEL CORROSION AROUNF BONDING SPIGOT HOLE (FRONT SPAR INBD OF RIB 20 AREA) REPAIRED IAW AIRBUS DOSSIER 80990SDR WX0A1900010073979Skin · corrodedNRC 5000-0011: 1237-15. LH WING, UPPER SKIN PANEL, SEVERAL CORROSION SPOTS (5X) FOUND AT REAR SPAR AREA BTW RIB 18-20. / LH WING, UPPER SKIN PANEL CORROSION SPOTS (5X) AT REAR SPAR AREA BTW RIB 18-20 REPAIRED AS PER AIRBUS DOSSIER 80990965 AND REPAIR DRAWING SDR WX0A1900010073978Skin · corrodedNRC 5000-0014:1237-18. LH WING, UPPER SKIN PANEL, SEVERAL CORROSION SPOTS (7X) FOUND BTW REAR SPAR AND FALSE SPAR AND RIB 7-9. / LH WING, UPPER SKIN PANEL CORROSION SPOTS (7X) BTW REAR SPAR AND FALSE SPAR AND BTW RIB 7-9 REPAIRED AS PER AIRBUS DOSSIER 80990965SDR WX0A1900010073977Skin · corrodedNRC 5000-0008: 1237-12. LH WING, UPPER SKIN PANEL SEVERAL CORROSION SPOTS (4X) FOUND AT REAR SPAR AREA BTW RIB 25-26. / LH WING, UPPER SKIN PANEL CORROSION SPOTS (4X) AT REAR SPAR BTW RIB 25-26 REPAIRED AS PER AIRBUS DOSSIER 80990965 AND REPAIR DRAWING R572-58SDR DALA2021120707560None · noneSHIP 6715 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 583140-14AD REV.C. CORRECTIVE ACTION: REF ERA 583140-14AD REV C. (2039138)SDR SWAA2021120749978Panel · corrodedL/W FUEL PANEL 534BB INNER SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-10-02-0G-0. FOUND WITHIN LIMITS IAW SRM 57-20-01-2R-1, FIG 203, DETAIL B-B. TREATED REWORKED AREA OF PANEL IAW SRM 51-10-02-0G-0.SDR DALA2021121007627None · noneSHIP 6808 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588964-14 REV A. CORRECTIVE ACTION: REF ERA 588964-14. (2037067)SDR SWAA2021120349010Panel · corrodedFUEL PANEL 532JB HAS FRETTING CORROSION AT RING MATTING SURFACE. ; / [01] REMOVED CORROSION IAW B737 ARM 57-20-01-2R 1. REPAIR 1; [02] VERIFIED STEP 1 C/W; [03] EVALUATED MATERIAL LOSS ON PANEL 532JB; LOSS OF .002. MAX ALLOWABLE IS .020. WITHIN LIMITS IAW B737SDR SWAA2021120349008Panel · corrodedFUEL PANEL 532GB HAS FRETTING CORROSION AT RING MATTING SURFACE. ; / [01] REMOVED CORROSION IAW B737 SRM; 57-20-01-2R-1. REPAIR 1; [02] VERIFIED STEP 1 C/W; [03] EVALUATED MATERIAL LOSS ON PANEL 532GB; LOSS OF .009. MAX ALLOWABLE IS .020. WITHIN LIMITS IAW B73SDR SWAA2021120349007Panel · corrodedFUEL PANEL 532CB HAS FRETTING CORROSION AT RING MATTING SURFACE. ; / [01] REMOVED CORROSION IAW B737 SRM; 57-20-01-2R-1. REPAIR 1; [02] VERIFIED STEP 1 C/W; [03] EVALUATED MATERIAL LOSS ON PANEL 532CB; LOSS OF .005. WITHIN LIMITS IAW B737 SRM 57-20-01-2R-1. RESDR SWAA2021120349006Panel · corrodedFUEL PANEL 532BB HAS FRETTING CORROSION AT RING MATTING SURFACE. ; / [01] REMOVED CORROSION IAW B737 SRM; 57-20-01-2R-1. REPAIR 1; [02] VERIFIED STEP 1 C/W; [03] EVALUATED MATERIAL LOSS ON PANEL 532BB;LOSS OF .004; MAX ALLOWABLE IS.020. WITHIN LIMITS IAW B737 SDR SWAA2021120349001Panel · corrodedFUEL PANEL 532HB HAS FRETTING CORROSION AT RING MATTING SURFACE. ; / [01] REMOVED CORROSION IAW B737 SRM; 57-20-01-2R-1. REPAIR 1; [02] VERIFIED STEP 1 C/W; [03] EVALUATED MATERIAL LOSS ON PANEL 532HB; LOSS OF .005; MAX ALLOWABLE IS .020. WITHIN LIMITS IAW B73SDR GTIA2021120236157Skin · corroded"CORROSION FOUND ON TOP SKIN PNL, RIB12+14 & STR11. RAF01 2871822-01 CREATED-REPAIRED CORRODED AREA IAW REO L23533 CAT B REINSPECT 30,000 FC OR 41,900 FH FROM EMBODIMENT AND A INTERVAL OF 25,000 FC OR 34,900 FH METHOD DETAILED EXTERNAL IAW AIRBUS RDAF 8099269SDR SWAA2021122048831Skin · crackedCRACK FOUND AT LW #4 SLAT SKIN AT ACTUATOR FITTING ATTACHMENT 3RD 0/B AFT RIVET. CRACK LENGTH 0.0394' AT 1 O'CLOCK POSITION. ; CRACK FOUND AT LW #4 SLAT SKIN AT ACTUATOR FITTING ATTACHMENT 3RD 0B AFT RIVET. CRACK LENGTH 0.0394' AT 1 O'CLOCK POSITION. REMOVED SDR DALA2021120107387None · noneSHIP 5639 AD // AA - RH ENG DRAG FTG CLAMP UP HOLES NBR 1 TO 10 WERE INSPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #1 SCRATCH ON SKIN BTW 11 - 1 CLOCK POSITION, CORROSION ON SKIN AT 8 CLOCK POSITION, CORROSION ON FITTING 10 CLOCK POSITION ; HOLE #2 SCRATCHESDR DALA2021120107386None · noneSHIP 5639 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #11 CORROSION ON SKIN BTW 7 TO 8 OCLOCK POSITION AND BURRS ON FITTING LOWER EDGE BTW 9 OCLOCK POSITION, HOLE #12 CORROSION ON SKIN AND FITTING BTW 6 SDR DALA2021113007361None · noneSHIP 5639 AD // AA - RH ENG DRAG FTG CLAMP UP HOLES NBR 11 TO 18 WERE INSPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #14 CORROSION ON SKIN BTW 11 - 1 CLOCK POSITION , SCRATCHES ON SKIN 8 - 10 CLOCK POSITION , SCRATCHES ON FITTING 1 - 3 CLOCK POSITION ; HOLE SDR DALA2021113007357None · noneSHIP 5639 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #1 GOUGES ON FITTING LOWER EDGE BTW 4 AND 11 OCLOCK POSITION,HOLE #2 CRACK ON SKIN BTW 1 TO 2 OCLOCK POSITION AND CORROSION ON SKIN AND FITTING BTW 6SDR SWAA2021121347565Skin · delaminatedSUPPLEMENTAL INFORMATION: PANEL 561BB UPPER & LOWER SKINS IS DELAMINATED AT O/B HONEYCOMB BAY. (MARKED) ; / [01] PART/MATERIAL IDENTIFIED PER SRM 57-51-01-0I-1 FIG 3 TABLE 3 ITEM 9.<BR>DELAMINATION EXCEEDS ALLOWABLE LIMITS AS GIVEN IN SRM 57-51-01-1A-1 PARA 4 SDR DALA2021112907326None · noneSHIP 5639 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 595669-14AD. CORRECTIVE ACTION: REF ERA 595669-14AD. (2030791)SDR DALA2021112907327None · noneSHIP 5639 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 595622-14AD. CORRECTIVE ACTION: REF ERA 595622-14AD. (2029031)SDR FDEA202111242931Panel · delaminatedR/W I/B L/E PANEL 611KT HAS COMPOSITE DAMAGE ON THE INNER SURFACE@ CORNER REPAIRED PER FEDEX EA # F-5730-T0365459-P1SDR DALA2021112907314None · noneSHIP 5645 BUBBLING PAINT / SIGNS OF CORROSION ON L/H WING UPPER SURFACE WALKWAY AT REAR SPAR ATTACH FASTENERS. DOT 81-001. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON L/H WING UPPER SURFACE WALKWAY AT REAR SPAR ATTACH FASTENERS IAW ER 595447-14 REV ORIGINAL. C/WSDR WX0A2021112273881Skin Panel · corrodedREF: NRI 6-5 - R/H WING TOP SKIN PANEL 2, OVERHANG LOWER SURFACE, FALSE REAR SPAR AREA, AT RIB 8, SKIN WITH CORROSION. / REPAIRED RH WING TOP SKIN PANEL 2, OVERHANG AREA LOWER SURFACE FALSE REAR SPAR, IJR-RIB T/E, WX.4392, DUE TO CORROSION IAW COOPESA EO N.COOSDR DALA2021112207174None · noneSHIP 6804 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588348-14AD REV.A. CORRECTIVE ACTION: REF ERA 588348-14AD.SDR DALA2021112207173None · noneSHIP 6804 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588314-14AD REV.A. CORRECTIVE ACTION: REF ERA 588314-14AD. (2023615)SDR EE4Y2021111914344Plate · corrodedRH WING, TOP SKIN PANEL NO.2, FALSE REAR SPAR AREA, BETWEEN RIB 7 AND RIB 9 OVERHANG LOWER SURFACE WITH CORROSION. NOTE: THE TOP SKIN PANEL WAS REPAIRED AS PER AIRBUS DOSSIER NO: 80987519 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2021-14279_SDR WX0A1900010073972Skin · corrodedNRC 5000-0042: 33284-34 LH WING, UPPER SURFACE, CORROSION FOUND ON AREA FWD OF SPOILER #3 (BETWEEN RIB 13 AND 14) / LH WING UPPER SURFACE SKIN, FWD OF SPOILER #3 BTW RIB 13-14, UPPER SKIN REPAIRED AND FOUND STRUCTURALLY ACCEPTABLE IAW AIRBUS DOSSIER # 80969544SDR WX0A1900010073971Skin · corrodedNRC 5000-0044: 33284-36 LH WING, AREA FWD OF SPOILER #2 (BETWEEN RIB 10 AND 11) SUSPECTED CORROSION (02 RIVET DAMAGED AND PRC MISSING) / AFTER INVESTIGATION, CORROSION FOUND AT LH WING UPPER SKIN AREA FWD OF SPOILER #2 AND RIB 10 AREA. LH WING UPPER SKIN FWD OSDR WX0A1900010073969Skin · corrodedNRC 6000-0048: 1237-66. RH WING, CORROSION FOUND ON BOTTOM SKIN PANEL #3 UPPER SURFACE, BETWEEN REAR SPAR AND FASLE SPAR AREA, INBD OF RIB #6. / RH WING BOTTOM SKIN PANEL #3 UPPER SURFACE BTW REAR SPAR AND FALSE REAR SPAR AREA INBOARD OF RIB #6, CORROSION REMOSDR FDEA202111172874Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 669 FOUND CRACK. LEFT WING FIXED LEADING EDGE DOUBLER AT STATION XOS 669 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202111172872Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 655 FOUND CRACK. LEFT WING FIXED LEADING EDGE DOUBLER AT STATION XOS 655 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202111172871Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 613 FOUND CRACK. LEFT WING FIXED LEADING EDGE DOUBLER AT STATION XOS 613 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202111162865None · noneAGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 647. EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 647 EVALUATED AND FOUND DOUBLER CRACKED AND NOT REPAIRED PER SRM 57-40-02-SDR FDEA202111162864None · noneAGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 637 . EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 637 EVALUATED AND FOUND DOUBLER CRACKED AND NOT REPAIRED PER SRM 57-40-02SDR FDEA202111162863None · noneAGING AIRCRAFT- EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 631. EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 631 EVALUATED AND FOUND DOUBLER CRACKED AND NOT REPAIRED PER SRM 57-40-02-2SDR AALA202111172303Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN PANEL LOWER SURFACE BETWEEN RIB 15 AND RIB 16. REPAIRED SKIN PANEL PER EA 329846.SDR AALA202111171802Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN PANEL LOWER SURFACE AT WS 5512 AND RIB 10. REPAIRED SKIN PANEL PER EA 329847.SDR UATA2021122242416Skin · corrodedLOWER WING SKIN SECTION @ WING STATION 2800 UNDER FLAP PYLON WAS FOUND TO HAVE SEVERE PITTING CORROSION. FABRICATED NEW SKIN AS PER ORIGINAL, AND REPLACED PER AC43.13-1B, PAR 4-53, 4-55, 4-57 AND CASA 212 SRM SECT. II, FIG 2.26SDR AALA202111178278Plate · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING LOWER SKIN TRAILING EDGE MOUNTING PLATE HYDRAULIC LINE FEED THRU HOLES WORN. REPLACED MOUNTING PLATE PER SRM 57-21-11-300-005.SDR SWAA2021121343322Panel · pulledRT WING T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES. CLEANED PANEL AND REMOVED FINISH AS NEEDED IAW AMM 51-21-11-150-815 PARA. 17. C. AND D. VISUAL INSPECTION FOUND DAMAGE TO GLASS FIBER PLIES TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4. SDR DALA2021111506989None · noneSHIP 689 A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #1 CORROSION ON SKIN BTW 9 TO 11 OCLOCK POSITION, HOLE #2 CORROSION ON SKIN BTW 7 TO 1 OCLOCK POSITION, HOLE #3 CORROSION ON SKIN BTW 5 TO 8 OCLOCK POSITIONSDR DALA2021111506992None · noneSHIP 6716 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 582683-14AD REV.C. CORRECTIVE ACTION: REF ERA 582683-14AD REV C. (2015426)SDR DALA2021111506988None · noneSHIP 678 A.A.- CORROSION ON: HOLE 11 BTW 10-5 HRS SKIN/FITTING, HOLE 12 BTW 7-9 HRS SKIN/FITTING AND HOLE 16 BTW 12-3 HRS FITTING. CORRECTIVE ACTION: SUMMARY OF NRC 00320: HOLE 11 BTW 10-5 HRS SKIN/FITTING, HOLE 12 BTW 7-9 HRS SKIN/FITTING AND HOLE 16 BTW 12-3SDR DALA2021111506983None · noneSHIP 678 A.A.- CORROSION ON: HOLE 1 BTW 4-5 HRS FITTING, HOLE 2 BTW 2-3 HRS & 7-9 HRS SKIN/FITTING, HOLE 4 BTW 2-3 HRS SKIN/FITTING, HOLE 6 BTW 11-12 HRS FITTING, HOLE 7 BTW 1-7 HRS SKIN/FITTING AND HOLE 10 BTW 1-5 HRS SKIN/FITTING AT RH ENG DRAG FITTING. CORR
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