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 AUCR200600004Skin Panel · damagedBOTTOM LT WING WS68.5, 4 FUEL BOOST PUMP SCREEN ATTACHING HOLES ELONGATED IN NR 17 AND NR 18 RISER.SDR AUCR200600003Panel · crackedCRACKED RISER, NR 4 FUEL TANK LOWER PLANK NR 4 AT NR 27 RISER WS397R.SDR 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.SDR 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)SDR 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.SDR 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 INTERNASDR 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.SDR 06FDEA1591Skin · dentedMULTIPLE DENTS FOUND AT RT WING INBOARD FLAP ASSY LOWER SURFACE OUTBOARD SEGMENT. DENT REPAIRED AS PER SRM 57-10-00 FIG2 VOL1.SDR 06FDEA1590Skin · dentedMULTIPLE DENTS FOUND AT RT WING INBOARD FLAP ASSY LOWER SURFACE INBOARD SEGMENT. DENT REPAIRED AS PER SRM 57-10-00 FIG2 VOL1.SDR 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).SDR 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)SDR 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.SDR 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.SDR 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.SDR DHL2006743007Acoustic Panel · delaminatedRIGHT WING PANEL AFT OF APU EXH LARGE DELAMINATION, 10 X 18 WBL 70 TO 90.SDR DHL2006743005Acoustic Panel · delaminatedRIGHT WING PANEL AFT OF APU EXH LARGE DELAMINATION, 10 X 18 WBL 70 TO 90.SDR 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)SDR 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.SDR 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)SDR CALA0600123Skin · crackedLEFT WING LEADING EDGE CRACKED APPROXIMATELY 4 INCHES, FSS 376, APPROXIMATELY 66 INCHES OUTBOARD OF PYLON. REPAIRED PER EA 5731-01010.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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, SDR 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 INSTALLESDR 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 TEMPORARSDR 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.SDR 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)SDR 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 PEENEDSDR 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 OUSDR 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.SDR 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.SDR 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.SDR KCSA061105Skin · corrodedFOUND LT WING UPPER SKIN BULGING AND RIVETS PULLED ABOVE FRONT SPAR AT WS 360.SDR 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 THISSDR 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 20-1SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 57-2-1SDR 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.SDR 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.SDR 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.SDR ASAA0610331Skin · crackedFOUND RT WING LE SKIN CRACKED AT NUMBER 4 SLAT ACTUATOR CUTOUT. REPAIRED PER SRM 57 30 4 FIG 5.SDR ASAA0610330Skin · crackedRT WING LE SKIN CRACKED AT NR 5 SLAT CENTER STOP. REPAIRED PER SRM 57 30 4 FIG 5.
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