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 DALA2022062304402Drag Brace · crackedSHIP 6713 AWR A.D.// A.A. CRACK WAS FOUND ON RH ENG DRAG FTG CLAMP-UP, HOLE #16 (FITTING LAYER) AT 3 O CLOCK POSITION; IN REF. CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00226: HOLE #16 (FITTING LAYER) AT 3 O CLOCK POSITION WAS REPAIRED PER PRI 600069-14 REV 2 ANSDR DALA2022062204367Skin · corrodedSHIP 6713 CORROSION WAS FOUND ON COUNTERSINK OF OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP AS FOLLOWS: HOLE #11 BTW 10 TO 12 O CLOCK POSITION; HOLE #15 AT 12 O CLOCK POSITION; HOLE #16 AT 9 O CLOCK POSITION & HOLE #17 AT 7 O CLOCK POSITION IN REF. CARD. CORRECTIVESDR DALA2022062204366Skin · corrodedSHIP 6713 A.D.// A.A. CORROSION WERE FOUND ON COUNTERSINK OF OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP AS FOLLOWS: HOLE #1 CORROSION BTW 12 AND 2 O CLOCK POSITION; HOLE #2 CORROSION AT 10 O CLOCK POSITION ; HOLE #3 CORROSION BTW 9 TO 3 O CLOCK POSITION; HOLE #4 CSDR DALA2022062204365Skin · corrodedSHIP 6713 A.D.// A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP AS FOLLOWS: HOLE #11 PITTING CORROSION ON SKIN AND FITTING ALL AROUND; HOLE #12 PITTING CORROSION ON SKIN ALL AROUND AND FITTING AT 3 O CLOCK POSITION; HOLE #13 CORROSION ON SKISDR DALA2022062204364Skin · corrodedSHIP 6713 AWR A.D.// A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP AS FOLLOWS: HOLE #2 PITTING CORROSION ON SKIN AND FITTING BTW 2 AND 8 O CLOCK POSITION; ; HOLE #5 CORROSION ON SKIN AT 1 O CLOCK POSITION; IN REF. CARD. CORRECTIVE ACTION: SSDR DALA2022121408118Skin · damagedDURING H CHECK, THREE ELONGATED HOLES WERE FOUND ON RH WING BOTTOM SKIN AT FUEL TANK ACCESS CUT-OUT BETWEEN RIB 37- 38. HOLES 11 THRU 15 AND 17 WERE FOUND WITHIN THE ALLOWABLE DAMAGE LIMITS OF A330 SRM TASK 57- 21-11-300-001; THEREFORE, THIS ER/A PROVIDES REPASDR DALA2024071507151Skin · damagedSHIP 684 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589971-14AD REV.A. CORRECTIVE ACTION: SUMMARY: REPETITIVE BHEC WAS PERFORMED PER ER/A 589971-14AD REV.A SECTION IV AND DISCREPANCIES WERE FOUND INSDR FDEA202206151943Skin · corrodedL/H WING UPPER SKIN DRAG FITTING BOLTS HOLES HAVE CORROSION HOLES #1, #2 , #4 , #7 , #9 , #10 #12, #14, #15 , #16 , #17, AND #18 ACCOMPLISHED PER E.A :F-5730-T0369693SDR COEA2022080403921Panel · corrodedWO 238451 NR 600006 HEAVY CHECK COE/MAJOR REPAIR: UPPER CENTER WING CUTOUT BETWEEN RIBS 4R AND 5R FLANGE FOR PANEL 622CT AND FOIL HAVE FRETTING. CORRECTIVE ACTION: REPAIR PER SRAS DO/TS-3860/04...2939 ISSUE F, DATED 7/18/2022.SDR COEA2022080402921Panel · corrodedWO 238451 NR 500006 HEAVY CHECK COE/MAJOR REPAIR: UPPER CENTER WING CUTOUT BETWEEN RIBS 4L AND 5L FLANGE FOR PANEL 522CT AND FOIL HAVE FRETTING. CORRECTIVE ACTION: REPAIR PER SRAS DO/TS-3860/04...2939 ISSUE F, DATED 7/18/2022.SDR COEA2022080401921Panel · dentedWO 238451 NR 500005 HEAVY CHECK COE/MAJOR REPAIR: UPPER CENTER WING CUT OUT BETWEEN RIBS 1L & 2L FLANGE FOR PANEL 521DT & FOIL HAVE FRETTING. CORRECTIVE ACTION: REPAIR PER SRAS DO/TS-3860/04...2939 ISSUE F, DATED 7/18/2022.SDR FDEA202206151432Skin · crackedL/W #3 SLAT I/B TRACK COVE PANEL IS CRACKED ON I/B SIDE REMOVED AND REPLACED PER BOEING DWG # 114N4077 REV FSDR IXXA2022061203Skin · damagedCRACK DAMAGE RIGHT WING FIXED LEADING EDGE SKINSDR SWAA2022071417506Skin · crackedSLAT #8 CRACKED ON LOWER L/E SKIN AT ACTUATOR RIB O/B 2ND FROM L/E FASTENER HOLE. / [01] NDI HFEC VERIFY CRACK ON #8 SLAT LOWER SKIN AT ACTUATOR FITTING IAW SRM 51-10-02-0G-2; STEP 5.C.;[10] FABRICATED REPAIR PARTS (1) DOUBLER 7075 T6 CLAD 0.071' LOT# 1478276-SDR SIMA20220611003Spar · crackedLH WING TIP REQUIRES REPLACEMENT DUE TO SPAR CRACK-C/A-REMOVED LH WING TIP AND INSTALLED SERVICEABLE WING TIP IAW AMM 57-30-00-400-801SDR SIMA20220611002Spar · crackedRH WING TIP REQUIRES REPLACEMENT DUE TO SPAR CRACK.-C/A-INSTALLED RH WING TIP IAW AMM 57-30-00.SDR IXXA2022112901Skin · corrodedLEFT WING LOWER WING PNL STA. 822-829 IS CORRODED AT FUEL PNLSDR SIMA20220610003Spar · crackedLH WINGTIP FWD SPAR CRACKED. REPLACE PER EO-EJ-57AD-017 IAW AMM.-C/A-REMOVED AND INSTALLED SERVICEABLE LH WING TIP IAW ERJ175 AMM 57-30-00.SDR DALA2022061304134Drag Fitting · corrodedSHIP 675 A.D.// A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #12 CORROSION BTW SKIN BTW 2 TO 4 AND 6 OCLOCK POSITION ; HOLE #16 CORROSION BTW SKIN BTW 11 TO 12 OCLOCK POSITION. IN REF. CARD 5720-01100-05B JOB#0SDR DALA2022061304133Drag Fitting · corrodedSHIP 675 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #1 CORROSION ON SKIN AND FITTING BTW 2 AND 6 OCLOCK POSITION; HOLE #2, CORROSION BTW 2 TO 3 O?CLOCK POSITION ON BUSHING INSTALLED AT SKIN AND CORROSIOSDR DALA2022061304132Drag Fitting · corrodedSHIP 675 [AD / AA] LH ENG DRAG FTG HOLES NBR 11 TO 18 WERE INPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #16, CORROSION ON SKIN AND FITTING BTW 7-8 CLOCK POS. IN REF TASK CARD 5720-01100-05A JOB #105-0001 STEP 14.B. CORRECTIVE ACTION: SUMMARY OF NRC 00101: HSDR DALA2022061304131Drag Fitting · corrodedSHIP 675 [AD / AA] LH ENG DRAG FTG HOLES NBR 1 TO 10 WERE INPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #1, CORROSION ON SKIN AND FITTING BTW 2-3 CLOCK POS ; HOLE #4, CORROSION ON SKIN 9 CLOCK POS ; IN REF TASK CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00100: SDR DALA2022060904033Skin · corrodedSHIP 3228 CORROSION UPPER SURFACE TOP SKIN LOC.TRAILING EDGE AREA BTW RIB 24 AND RIB 25 ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 599241-14AD REV.ORIGINAL. (2269511)SDR COEA2022080911917Panel · corrodedWO 238445 NR 600016 HEAVY CHECK COE/MAJOR REPAIR: UPPER CENTER WING CUTOUT BETWEEN RIBS 4R AND 5R PANEL 622CT FLANE AND FOIL HAVE FRETTING DAMAGE. CORRECTIVE ACTION: REPAIR PER SRAS DO/TS- 4504/08...4888 ISSUE F, DATED 8/3/2022.SDR COEA2022080910917Panel · corrodedWO 238445 NR 500016 HEAVY CHECK COE/MAJOR REPAIR: UPPER CENTER WING CUTOUT BETWEEN RIBS 4L AND 5L PANEL 522CT FLANGE AND FOIL HAVE FRETTING DAMAGE. CORRECTIVE ACTION: REPAIR PER SRAS DO/TS-4504/08...4888 ISSUE F, DATED 8/3/2022.SDR COEA2022080909917Panel · corrodedWO 238445 NR 500015 HEAVY CHECK COE/MAJOR REPAIR: UPPER CENTER WING CUTOUT BETWEEN RIBS 1L AND 2L PANEL 521DT FLANGE AND FOIL HAVE FRETTING DAMAGE. CORRECTION ACTION: REPAIR PER SRAS DO/TS...4504/08...4888 ISSUE F.SDR IPXA2022062483450Skin · corrodedINSPECTION TYPE:3CRT WING UPPER SURFACE AFT SKIN REAR SPAR HAS CORROSION AT STA.XORS=693-XORS=696.REPAIRED CORRODED SKIN AT UPPER REAR SPAR IAW VT-SAA EA 011-5730-01-A9610 REV I/R AND UPS EO MD11-5730-84039-A (MINOR).SDR AALA202206143613Skin · damagedAIRCRAFT IN BASE MAINTENANCE: DAMAGE ON WING FIXED LEADING EDGE SKIN BEHIND THE NUMBER 4 SLAT TEMPORARY REPAIR INSTALLED FOR MAINTENANCE FERRY FROM GSO TO TUL PER EA 336732. **SUPPLEMENTAL REPORT FOR AALA202206103613: LEFT WING LEADING EDGE REPAIRED PER SRM 51SDR DALA2022061004093Drag Fitting · corrodedSHIP 666 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #2 CORROSION ON SKIN AND FITTING BTW 2 TO 3 AND 9 TO 11 OCLOCK POSITION; HOLE #3 CRACK ON FITTING BTW 9 OCLOCK POSITION, CORROSION ON SKIN AND FITTINGSDR AALA202206103613Skin · damagedAIRCRAFT IN BASE MAINTENANCE: DAMAGE ON WING FIXED LEADING EDGE SKIN BEHIND THE NUMBER 4 SLAT TEMPERARY REPAIR INSTALLED FOR MAINTENANCE FERRY FROM GSO TO TUL PER EA 336732. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)SDR AALA202206289048None · wornAIRCRAFT WAS GROUNDED: LEFT HAND ENGINE AFT PYLON AREA LOWER WING SKIN BETWEEN RIB 7 AND 8 HAS DOUBLER DAMAGE FROM ELONGATED FASTENER HOLE AROUND FITTING. REPAIRED DOUBLE / MOUNTING PLATE PER AARD 57-21-11-1 NOTE: THIS EVENT WAS PREVIOUSLY REPORTED ON AALA202SDR IXXA2023080501Skin · corrodedCORROSION ON THE LOWER EXTERIOR SURFACE OF THE CENTER WING SKIN, JUST ABOVE AND AFT OF THE LEFT ECS AIR CONDITIONER REHEATER, AT THE BUTT SEAM FOR THE WING STRINGER.SDR DALA2022060804015Drag Fitting · corrodedSHIP 666 [AD / AA] LH ENG DRAG FITTING HOLES NBR 1 TO 10 WERE INSPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #2 CORROSION ON SKIN AND FITTING BTW 2-4 CLOCK POS ; HOLE #3 CORROSION ON SKIN AND FITTING AT 10 CLOCK POS AND BTW 3 - 5 CLOCK POS ; HOLE #4 CORROSIOSDR DALA2022060804014Drag Fitting · corrodedSHIP 666 [AD/ AA] LH ENG DRAG FITTING HOLES 11 TO 18 WERE INSPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #13 CORROSION BTW SKIN AND FITTING BTW 2 - 4 CLOCK POS ; HOLE #17 CORROSION BTW SKIN AND FITTING AT 5 CLOCK POS. IN REF TASK CARD. CORRECTIVE ACTION: SUMSDR DALA2022060703973Drag Fitting · damagedSHIP 5644 R/H ENG DRAG FTG CLAMP-UP HOLE #2 HAS 2 EACH INDICATIONS IN THE BOTTOM OF THE SKIN LAYER AT THE 3 & 9 O'CLOCK POSITIONS LOOKING AFT. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON R/H ENG PYLON INBD FITTING HOLE #2 ON RH UPPER DRAG FITTING, IAW ER/A 58974SDR DALA2022060703972Drag Fitting · damagedSHIP 5644 R/H ENG DRAG FTG CLAMP-UP HOLE #4 HAS 2 EACH INDICATIONS ONE IN THE TOP & ONE IN THE BOTTOM OF THE FITTING LAYER AT THE 3 O'CLOCK POSITION LOOKING AFT. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON R/H ENG PYLON OTBD FITTING HOLE #4 ON RH UPPER DRAG FITTSDR DALA2022060703971Drag Fitting · damagedSHIP 5644 R/H ENG DRAG FTG CLAMP-UP HOLE #10 HAS 1 EACH INDICATION IN THE TOP OF THE FITTING LAYER AT THE 6 O'CLOCK POSITION LOOKING AFT. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON R/H FITTING HOLE #10 ON RH UPPER SKIN & DRAG FITTING OUTER WING BY REAMING HOLE SDR SIMA20220603003Spar · crackedRH WING TIP SPAR 1 CRACKED. REPLACE PER EO EJ-57AD-017 IAW AMM.-C/A-REPLACE PER EO EJ-57AD-017 IAW AMM.SDR SIMA20220603002Spar · crackedLH WING TIP SPAR 1 CRACKED. REPLACE PER EO EJ-57AD-017 IAW AMM.-C/A- REPLACE PER EO EJ-57AD-017 IAW AMM.SDR WX0A1900010074119Skin · corrodedNRC 6000-0030: (744-1) CORROSION FOUND ON RH WING, TOP SKIN UPPER SURFACE AT REAR SPAR AREA, 5 INCHES INBD FROM RIB 13./RH WING TOP SKIN TRAILING EDGE OVERHANG AT RIB 13 DATUM (AREA #6) PERMANENTLY REPAIRED AS PER AIRBUS DOSSIER #80871570 AND ERO #R5721-0105 RSDR DALA2022060603942Skin Panel · corrodedSHIP 5644 LH WING UPPER SKIN HAS AREA OF CORROSION ABOVE FRONT SPAR 11" OB OF FUSELAGE. DOT 009. CORRECTIVE ACTION: ACCOMPLISHED BLEND REPAIR ON LH WING UPPER SKIN PANEL 2 AT FRONT SPAR WBL 95, 11" O/B OF FUSELAGE IAW ER/A 599512-14 REV A SECTION I. (2261135)SDR AALA202206227648Access Panel · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING FUEL TANK ACCESS PANEL 540LB HAS ELONGATED / WORN COUNTERSUNK FASTENER HOLE. REPLACED ACCESS PANEL PER TASK CARD 26C54057020.SDR FDEA202206011353Finger Doubler · delaminatedLEFT HAND WING - FINGER DOUBLERS AT TRAILING EDGE COMPARTMENT BETWEEN STATION XW 375 AND XW 387 FOUND DISBONDED. LEFT HAND WING FINGER DOUBLER AT TRAILING EDGE COMPARTMENT BETWEEN STATION XW 375 AND XW 387 REPAIR CARRIED OUT AS PER SRM 57-50-01-2R REPAIR 6SDR FDEA202206011352Finger Doubler · delaminatedRIGHT HAND WING - FINGER DOUBLERS AT TRAILING EDGE COMPARTMENT BETWEEN STATION XW 375 AND XW 387 FOUND DISBONDED. RIGHT HAND WING FINGER DOUBLERS AT TARILING EDGE COMPARTMENT BETWEEN STATION XW 375 AND XW 387 REPAIR CARRIED OUT AS PER SRM 57-50-01-2R REPAISDR DALA2022060303888None · noneSHIP 178 ER/A 574133-14AD SECT I REPAIR WAS ACCOMPLISHED ON A/C 178 , CORRECTIVE ACTION: ACCOMPLISH ER/A 574133-14AD REV. A SECTION III PRIOR TO 6,000 CYCLES OR 18,000 FLIGHT HOURS AFTER SECTION I REPAIR. (2260159)SDR WX0A2022062274124Skin · corrodedNRC 6000-0024: AT R/H WING TOP SKIN, CORROSION FOUND AT TRAILING EDGE OVERHANG AT RIB 12 DATUM, STATION WMRX 3355.516. / RH WING TOP SKIN TRAILING EDGE OVERHANG AT RIB 12 DATUM, APPROX STA WMRX 3355.516 (AREAS #4 - #5) PERMANENTLY REPAIRED AS PER AIRBUS DOSSIESDR WX0A2022062274123Skin · corrodedNRC 6000-0027: AT R/H WING TOP SKIN, CORROSION FOUND AT TRAILING EDGE OVERHANG BTW STATION WMRX 5626.98 AND WMRX 6173.91 (APPROX. RIB 16 TO 17). / RH WING TOP SKIN TRAILING EDGE OVERHANG BETWEEN STA WMRX 5626.98 AND WMRX 6173.91 (AREAS #10 - #11) PERMANENTLY RSDR WX0A2022062274122Skin · corrodedNRC 6000-0025: AT R/H WING TOP SKIN, CORROSION FOUND AT TRAILING EDGE OVERHANG BTW STATION WMRX 4037.38 AND WMRX 5261.977 (APPROX. RIB 13 TO 15). / RH WING TOP SKIN TRAILING EDGE OVERHANG BETWEEN WMRX 4037.38 AND WMRX 5261.977 (AREAS #7, #8, #9), PERMANENTLY RSDR WX0A2022062274121Skin · corrodedNRC 6000-0023: AT R/H WING TOP SKIN, CORROSION FOUND AT TRAILING EDGE OVERHANG BTW STATION WX 3494.5 AND WX 4490.52 (APPROX. RIB 7 TO 8). / RH WING TOP SKIN TRAILING EDGE OVERHANG BETWEEN WX 3494.5 AND WX 4490.52 (AREAS #1, #2, #3), PERMANENTLY REPAIRED AS PERSDR WX0A2022062274120Skin · corrodedNRC 5000-0019: AT L/H WING TOP SKIN, CORROSION FOUND AT TRAILING EDGE OVERHANG BTW STATION WX 3494.5 AND WX 4490.52 (APPROX. RIB 7 TO 8). / LH WING TOP SKIN TRAILING EDGE OVERHANG BETWEEN STA WX 3494.5 AND WX 4490.52 (AREAS #1, #2, #3) PERMANENTLY REPAIRED AS
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