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.

SDR AUCR200600004Skin Panel · damagedBOTTOM LT WING WS68.5, 4 FUEL BOOST PUMP SCREEN ATTACHING HOLES ELONGATED IN NR 17 AND NR 18 RISER.Apr 27, 2006 · N925AU · Lkheed P3ASDR AUCR200600003Panel · crackedCRACKED RISER, NR 4 FUEL TANK LOWER PLANK NR 4 AT NR 27 RISER WS397R.Apr 27, 2006 · N925AU · Lkheed P3ASDR IXXA06RNG047SPanel · misalignedDURING ROUTINE C CHECK, FOUND SLOT PANEL AFT HOLES DO NOT ALIGN UP WITH THE HOLES IN THE WING ON CENTER EXTENDED LEADING EDGE AROUND LOWER SKIN RIGHT HAND. DAMAGED AREA WAS CLEANED, REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW EWO ATI 57-085.Apr 26, 2006 · N823BX · Doug DC871FSDR CA060511008Doubler · cracked(CAN) DOUBLER P/N 114-120048-54 FOUND CRACKED AT FWD OB CORNER. CAN NOT SEE CRACK UNLESS COLLECTOR FUEL TANK IS REMOVED. (TC NR 20060511008)Apr 26, 2006 · Beech 1900CSDR QXEA200601296Plate · damagedYYC - C4 LEFT HAND CENTER WING, LADDER PLATE UNDER PANEL 522AT HAS FRETTING DAMAGE BETWEEN YW 62 - YW 77. REPAIRED IAW RD8-57-1471 AND SRM 51-20-36.Apr 26, 2006 · N355PH · Dhav DHC8202SDR UPS06846846Skin · crackedFOUND CRACK ON LWR SURFACE BETWEEN F/S AND C/S JUST INBD OF XRS 463 NR 4 ALT TANK. CUT OUT SKIN DAMAGE AT WING STA XWS 467 IAW UPS EO DC8-5730-24293-A SAA EA NR 008-5710-01-A0156. FABRICATED AND INSTALLED -1 FILLER, -2 DOUBLER, -3 EXTERNAL TRIPLER,-4 INTERNAApr 25, 2006 · N752UP · Doug DC871FSDR CA060502000Skin · cracked(CAN) SKIN CRACKED AT HILOC FASTENERS ATTACHING SKIN TO AFT FLANGE OF WING ATTACH FITTING. CONDITION EVIDENT ON BOTH LT AND RT SKINS OF WING CENTER SECTION. MFG HAS A FIELD REPAIR TO DEAL WITH THESE CRACKS. CRACKS FOUND VISUALLY WITH WING BOLT COVERS REMOVED.Apr 24, 2006 · Beech 100BEECHSDR 06FDEA1591Skin · dentedMULTIPLE DENTS FOUND AT RT WING INBOARD FLAP ASSY LOWER SURFACE OUTBOARD SEGMENT. DENT REPAIRED AS PER SRM 57-10-00 FIG2 VOL1.Apr 24, 2006 · N526FE · Doug MD11SDR 06FDEA1590Skin · dentedMULTIPLE DENTS FOUND AT RT WING INBOARD FLAP ASSY LOWER SURFACE INBOARD SEGMENT. DENT REPAIRED AS PER SRM 57-10-00 FIG2 VOL1.Apr 24, 2006 · N526FE · Doug MD11SDR 06FDEA1588Skin · dentedEXISTING DENT FOUND AT LT WING INBOARD FLAP LOWER SURFACE LOCATED 69 INCHES FROM OUTBOARD AND 6 INCHES FROM AFT. DENT REPAIRED AS PER SRM 57-10-00 FIG2 VOL1 (MAJOR REPAIR).Apr 24, 2006 · N526FE · Doug MD11SDR CA060421012Skin · chafed(CAN) LT WING UPPER SKIN, WBL 76.75 FROM AFT EDGE OF SKIN FWD FOR 9.5 INCH SKIN CHAFED AND REPAIRED IAW CUSTOMER EA. (TC NR 20060421012)Apr 20, 2006 · Boeing 737290CSDR QXEA200601535Panel · corrodedYYC C3 CENTER WING DRY BAY ACCESS LIDS HAVE CORROSION IN SCREW HOLE COUNTERSINKS AT 521BT, 521AT,AND 621BT. REPAIRED IAW RD 8/4-57-432, ISSUE 1.Apr 19, 2006 · N425QX · Bombdr DHC8402SDR QXEA200601534Panel · corrodedYYC C3 RIGHT HAND FUEL TANKS ACCESS LIDS HAVE CORROSION IN SCREW HOLE COUNTERSINKS AT 623AT, 622CT, 622BT AND 622AT. REPAIRED IAW RD 8/4-57-432, ISSUE 1.Apr 19, 2006 · N425QX · Bombdr DHC8402SDR QXEA200601533Panel · corrodedYYC C3 LEFT HAND WING FUEL TANKS ACCESS LIDS HAVE CORROSION IN SCREW HOLE COUNTERSINKS AT 523AT, 522CT, 522BT AND 522AT. REPAIRED IAW RD 8/4-57-432, ISSUE 1.Apr 19, 2006 · N425QX · Bombdr DHC8402SDR DHL2006743007Acoustic Panel · delaminatedRIGHT WING PANEL AFT OF APU EXH LARGE DELAMINATION, 10 X 18 WBL 70 TO 90.Apr 19, 2006 · N743DH · Boeing 727225SDR DHL2006743005Acoustic Panel · delaminatedRIGHT WING PANEL AFT OF APU EXH LARGE DELAMINATION, 10 X 18 WBL 70 TO 90.Apr 19, 2006 · N743DH · Boeing 727225SDR CA060511006Skin · cracked(CAN) OB FWD CORNER OF COLLECTOR TANK OPENING. SKINS P/N 114-120048-73 AND 74 FOUND CRACKED. HEAVY SKIN .071 (TC NR 20060511006)Apr 18, 2006 · Beech 1900CSDR QXEA200601652Panel · damagedYYC C3 LEFT HAND WING, CENTER FUSELAGE SECTION 521, ALL REBATES FOR PANELS IN SECTION 521 HAVE CUT MARKS FROM BOX CUTTERS. REPAIRED IAW DHC-8-400 SRM 51-14-00-350-803, 51-25-10-370-801 ADN R5D 8/4-53-451, ISSUE 1.Apr 17, 2006 · N425QX · Bombdr DHC8402SDR RU32006F00001Wing · scratchedUPON POST FLT, DISCOVERED STRATCHES ON RT WINGLET. APPARENTLY WHILE POSITIONING OVER GCP AT RKTP, SCRAPED GCP SIGN. NO INDICATION OF CONTACT WHILE AT RTKP. RETURNED TO RKSO WHERE DAMAGE WAS NOTED. PERFORMED TEMP REPAIR REFERENCE REO. (K)Apr 17, 2006 · N87 · Cndair CL6002B16SDR CALA0600123Skin · crackedLEFT WING LEADING EDGE CRACKED APPROXIMATELY 4 INCHES, FSS 376, APPROXIMATELY 66 INCHES OUTBOARD OF PYLON. REPAIRED PER EA 5731-01010.Apr 17, 2006 · N12116 · Boeing 757224SDR QXEA200601125Panel · chafedPDX - C4 RIGHT INBOARD WING LOWER INBOARD FLANGE FOR LEADING EDGE PANEL 611AR CHAFED. REPAIRED IAW RD 8-57-811, ISSUE 3, PAGE 4 STEPS 4-7.Apr 16, 2006 · N356PH · Dhav DHC8202SDR UIEA200600081Skin Panel · corrodedLT WING LE O/B OF O/B LANDING LT AT AREA OF LOOSE RIVETS THERE IS TWO SPOTS OF INNERGRANULAR CORROSION (MARKED). INTERIM REPAIR TO LEADING EDGE LT WING PER SRM 57-30-04 AND XEO57-041306 AND 8110-3. REPEAT INSP EVERY A CK AND PERMANENT REPAIR AT C-CK.Apr 15, 2006 · N505MC · Boeing 7472D3BSDR QXEA200601651Skin · damagedYYC C3 LEFT HAND WING, CENTER FUSELAGE SECTION 521, FORWARD REBATE FOR PANEL 262AT, HAS CHAFING DAMAGE. REPAIRED IAW DHC-8-400 SRM 51-14-00-350-803 AND 51-25-10-370-801.Apr 13, 2006 · N425QX · Bombdr DHC8402SDR QXEA200601650Panel · damagedYYC C3 LEFT HAND WING STATION YW42, AFT REBATE FOR PANEL 261CT HAS CHAFING DAMAGE. REPAIRED IAW DHC-8-400 SRM 51-14-00-380-803 AND 51-25-10-320-801.Apr 13, 2006 · N425QX · Bombdr DHC8402SDR QXEA200601128Access Panel · corrodedPDX - C4 FUEL ACCESS PANEL 624AT HAS CORROSION AROUND INBOARD FASTENER HOLES. REPAIRED IAW RD 8-57-30 AND DHC-8-200 SRM 51-20-16.Apr 13, 2006 · N356PH · Dhav DHC8202SDR QXEA200601653Panel · damagedYYC C3 LEFT HAND WING, FUEL TANK LID REBATES FROM STATION YW191 TO STATION YW425 HAVE CUT MARKS FROM BOX CUTTERS. REPAIRED IAW DHC-8-400 SRM TASK 57-20-30-320-82, 57-20-30-992-802 AND 51-21-10-380-801.Apr 11, 2006 · N425QX · Bombdr DHC8402SDR QXEA200601536Panel · corrodedYYC C3 RIGHT HAND FUEL TANK STATION YW353.019 TO YW389-019 FUEL TANK LID ATTACH REBATE HAS LIGHT SURFACE CORROSION AROUND 12 SCREW HOLES. REPAIRED IAW DHC-8 Q400 SRM 57-20-30-320-802 AND SRM 51-21-10-380-801.Apr 11, 2006 · N425QX · Bombdr DHC8402SDR UIEA200600080Skin · delaminatedLEFT WING UPPER LEADING EDGE PANEL AT NR 2 ENGINE PYLON DELAMINATED AT PREVIOUS REPAIR JUST I/B OF L/E GAP PANEL. REMOVED DAMAGE LEADING EDGE PANEL IAW B-747-200 SRM 51-30-02.SENT TO OUTSIDE SERVICE AIRCRAFT CONNECTION INC. REPAIRED PER SRM 51-40-08 PAGE 1, Apr 10, 2006 · N527MC · Boeing 7472D7BSDR A6WA200640144Skin · dentedRT IB FLAP HAS A SMALL DENT ON BOTTOM OF FLAP AT WS 65.75 .5 INCH LONG X .2500 INCH WIDE X .006 DEEP. (K) MAINTENANCE REPAIRED DENT ON BOTTOM OF FLAP AT WS 65.75 BY CUTTING OUT DAMAGE, FABRICATED REPAIR DOUBLER, PERFORMED EDDY CURRENT INSPECTION AND INSTALLEApr 9, 2006 · N404AW · Cndair CL6002B19SDR IXXA060455SSkin · crackedDURING PREFLIGHT INSPECTION, FOUND RUNNING FUEL LEAK INBOARD OF NR 1 PYLON COMING FROM NUMBER ONE ALTERNATE FUEL TANK. THE DAMAGE WAS REMOVED AND REPAIRED PER BOEING ROD SKETCH 06-04-18-001 REF TIMCO GOODYEAR S/O 216006. OPS 27846 REPAIR APPROVED AS TEMPORARApr 7, 2006 · N821BX · Doug DC871FSDR QXEA200601171Skin · damagedPDX: LT AFT FUSELAGE SKIN HAS IMPACT DAMAGE JUST FORWARD OF CENTER SPAR X920.618 BETWEEN STR 22-29. MAINTENANCE REPAIRED IAW NDTM PART 6, TASK 51-00-01-250-801, HORIZON EA 6-55-135 AND RD 8/4-55-255.Apr 7, 2006 · N405QX · Bombdr DHC8402SDR A6WA200640143Access Panel · corrodedLT WING LOWER PLANK FUEL TANK ACCESS PANEL 110AB CUT-OUT HAS MINOR CORROSION AT IB RADIUS. NOT IN CRITICAL REGION. (K) REPAIRED FUEL TANK ACCESS PANEL 510AB CUTOUT IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)Apr 6, 2006 · N404AW · Cndair CL6002B19SDR A6WA200640142Access Panel · corrodedLT WING PLANK LOWER FUEL ACCESS PANEL 540BB CUT-OUT HAS MINOR CORROSION AT C/B RADIUS NOT IN CRITICAL REGION. (K) MAINTENANCE REPAIRED MINOR CORROSION ON FUEL ACCESS PANEL (540BB) CUTOUT BY BLENDING OUT DAMAGE, PERFORMING EDDY CURRENT INSPECTION, SHOT PEENEDApr 6, 2006 · N404AW · Cndair CL6002B19SDR A6WA200640141Skin · corrodedRT WING LOWER PLANK FUEL ACCESS PANEL 640BB CUT-OUT HAS MINOR CORROSION AT THE IB RADIUS AND THE FWD MID EDGE WHICH IS IN THE CRITICAL REGION. (K) MAINTENANCE REPAIRED MINOR CORROSION ON FUEL TANK ACCESS PANEL (640BB) CUTOUT (IN CRITICAL AREA) BY BLENDING OUApr 6, 2006 · N404AW · Cndair CL6002B19SDR ABXA060217Skin · crackedCRACK IN RIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN 8" FROM INBOARD EDGE, STA. XFS 304. STOP DRILLED CRACK AND INSTALLED REPAIR IAW REA D857-53580, REV. IR.Apr 5, 2006 · N812AX · Doug DC863FSDR ABXA060218Skin · crackedRIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN HAD 3 EACH CRACKS AT APPROX. XFS 410 - 423. REPAIRED CRACKS IAW REA D857-53581, REV. IR.Apr 5, 2006 · N812AX · Doug DC863FSDR ABXA060194Skin · crackedCRACK IN RIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN 8 INCHES FROM INBOARD EDGE STA XFS 304. STOP DRILLED CRACK AND INSTALLED REPAIR IAW REA D857-53580, REV IR.Apr 5, 2006 · N812AX · Doug DC863FSDR KCSA061105Skin · corrodedFOUND LT WING UPPER SKIN BULGING AND RIVETS PULLED ABOVE FRONT SPAR AT WS 360.Apr 5, 2006 · N716CK · Boeing 747122SDR IXXA06RNG021SPlate · corrodedDURING ROUTINE C CHECK FOUND CORROSION ON THE INBOARD EXTENDED LEADING EDGE NOSE PLATING AROUND STATION XFS 5000 LEFT HAND. CORRODED AREA WAS REMOVED AND INTERNAL DOUBLER WAS FABRICATED & INSTALLED IAW EWO ATI 57-074. FAA FORM 8110-3 WAS ISSUED APPROVING THISApr 4, 2006 · N823BX · Doug DC871FSDR EIA2006069Skin · corrodedDURING C CHECK, CORROSION WAS FOUND ON WING CENTER SECTION NR 2 UPPER WING SURFACE AT STA 1140 RBL11 AND RBL74. DAMAGE TRIMMED OUT AND REPAIRED DOUBLER, INSTALLED CHORD SECTION REPLACEMENT PER BOEING SR1D 1-177601899, SRM 51-10-02, SRM 57-30-01, AND SCPM 20-1Apr 3, 2006 · N477EV · Boeing 747SR46SDR IXXA06RNG004SSkin · crackedDURING A C-CHECK INSPECTION FOUND A CRACK ON CENTER EXTENDED LEADING EDGE AROUND LOWER SKIN XFS 341.000 RT. REPAIR DOUBLER AND ALUMINUM FILLER WERE FABRICATED AND INSTALLED IAW EWO ATI 57-068. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.Apr 3, 2006 · N823BX · Doug DC871FSDR IXXA06RNG003SSkin · crackedDURING A CHECK INSPECTION FOUND TWO CRACKS ON CENTER EXTENDED LEADING EDGE AROUNG LOWER SKIN A STA XFS 304.000 RT. REPAIR DOUBLER AND ALUMINUM FILLER WER FABRICATED AND INSTALLED IAW EWO ATI 57-067. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.Apr 3, 2006 · N823BX · Doug DC871FSDR 06FDEA1295Skin · corrodedFOUND RIGHT WING T/E LOWER SKIN AT T/E OF NR 2 PYLON HAS 3 AREAS OF EXFOLIATED CORROSION. COMPLIED WITH EA 6-5730-99016 PART 1.Apr 3, 2006 · N455FE · Airbus A310322SDR SROM200600004Skin · crackedRT WING LEADING EDGE CRACKED AT NR 5 SLAT UPSTOP CUTOUT JUST OB OF THE ACTUATOR. REPAIRED BY INSTALLING INTERNAL STAINLESS DOUBLER IAW DER APPROVED 8110, REPORT NR SCS-5740-001SR.Apr 3, 2006 · N736BP · Boeing 737205SDR IXXA06RNG015SSkin · corrodedDURING ROUTINE C CHECK, FOUND TWO AREAS OF CORROSION OUT OF LIMITS ON OUTER OUTBOARD EXTENDED LEADING EDGE UPPER SKIN, STATION XFS 722 - 835, LEFT HAND. DAMAGED AREA WAS REMOVED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 57-071 AND SRM 57-2-1Apr 2, 2006 · N823BX · Doug DC871FSDR QXEA200601064Access Panel · corrodedYYC - C4 RIGHT HAND WING ACCESS PANEL 622AT COUNTER SINK SCREW HOLES HAVE FRETTING CORROSION. REPAIRED IAW RD 8-57-1715, ISSUE 3, DHC-8-200 SRM 51-20-16, PARAGRAPH D AND DHC-8-200 MM 20-32, PAGES 1-3.Apr 2, 2006 · N353PH · Dhav DHC8202SDR P5CA0601465Skin · corrodedEXFOLIATION CORROSION ON LEFT WING LOWER SKIN AT AFT SPAR AREA WS 1376. REPAIRED PER BOEING 8100-9. FABRICATED AND INSTALLED 1-2-3-4 PLATES FILLER PER ECRA 921FT-57-747-004.Mar 31, 2006 · N921FT · Boeing 747283BSDR P5CA0601464Skin · crackedLEFT WING LOWER SKIN BETWEEN DRY BAY PANELS AT WS 1516 HAS SKIN CRACKED. REPAIRED PER BOEING 8100-9. REPAIRED CRACKED LEFT WING LOWER SKIN PER ECRA 921FT-57-747-001.Mar 31, 2006 · N921FT · Boeing 747283BSDR ASAA0610331Skin · crackedFOUND RT WING LE SKIN CRACKED AT NUMBER 4 SLAT ACTUATOR CUTOUT. REPAIRED PER SRM 57 30 4 FIG 5.Mar 31, 2006 · N742AS · Boeing 737290CSDR ASAA0610330Skin · crackedRT WING LE SKIN CRACKED AT NR 5 SLAT CENTER STOP. REPAIRED PER SRM 57 30 4 FIG 5.Mar 31, 2006 · N742AS · Boeing 737290C
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