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 EIA2006018Skin · corrodedCORROSION FOUND ON THE RT WING BETWEEN WS 1026 - 1057 (LES 1046 - 1078). ECRA 478-57-176-2 INSTRUCTS TO REMOVE CORROSION, ACCOMPLISH NDI INSPECTION, CUT OUT THE DAMAGED WING SKIN MATERIAL AND FABRICATE REPAIR. THIS REPAIR IS LIMITED TO 135000 HOURS OR 38788 SDR EIA2006021Skin · corrodedDURING "B-CHECK", CORROSION FOUND ON THE RT WING AT WS 1280 (LES 1302) OUTBOARD OF JACKPAD LOCATION. INSTRUCTS TO REMOVE CORROSION, ACCOMPLISH NDI INSPECTION, FABRICATE AND INSTALL FORM FIT FILLERS AND THE SUBSTITUTION OF BACB30PT RADIUS LEAD IN BOLTS AND BACSDR UPS06846359Skin · crackedRT UPPER WING SKIN CRACKED 1/2" LONG, AT XCW69.500 REAR SPAR AREA. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED 2 DOUBLERS AND 1 FILLER IAW SRM 57-2-1 FIG 20.SDR QXEA200600442Panel · damagedPDX - RIGHT WING ACCESS PANELS 621BT, 622AT, 622BT, 622CT AND 623AT, SCREW COUNTERSINKS DIRTY, POSSIBLE CORROSION/PITTING. ALODINE WORN OFF. MAINTENANCE REPAIRED IAW RD 8/4-57-432, NDTM PART 1, 51-00-06 AND HORIZON EO 6-57-317.SDR AUCR200600001Panel · crackedLT WING, STA. 82, 2.9 IN. FRACTURE IN NR 7 PLANK FORWARD TANG. FRACTURE WAS LOCATED BY ULTRASONIC INSPECTION DURING EVALUATION OF FUEL STAIN AT ANNUAL INSPECTION. THERE EXISTS AN APPROVED REPAIR FOR THIS DAMAGE IN THE SRM.SDR QXEA200600441Flange · damagedPDX - RIGHT WING FUEL TANK ACCESS AFT FLANGE HAS PITTING AROUND A SCREW HOLE AT APPROX YW50. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NDTM PART 6, 51-00-02 AND RD 8/4-57-317.SDR QXEA200600440Flange · damagedPDX - LT WING FUEL TANK ACCESS AFT FLANGE HAS PITTING AROUND SCREW HOLES, 5 LOCATIONS AT YW79. MAINTENANCE REPAIRED IAW RD 8/4-57-441 AND NDTM PART 6, 51-00-02.SDR QXEA200600439Flange · damagedPDX - LT WING FUEL TANK ACCESS AFT FLANGE HAS PITTING AROUND SCREW HOLE AT APPROX YW126. MAINTENANCE REPAIRED IAW RD 8/4-52-441, NDTM PART 6, 51-00-02 AND RD 8/4-57-317.SDR QXEA200600413Skin · corrodedPDX: LT WING FUEL TANK ACCESS AFT FLANGE HAS PITTING AROUND SCREW HOLE AT APPROX YW 50. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NDTM PART 6, 51-00-02 AND RD 8/4-24-317.SDR QXEA200600412Skin · corrodedPDX: LT WING FUEL TANK ACCESS AFT FLANGE HAS PITTING AROUND SCREW HOLE AT APPROX YW 126. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NDTM PART 6, 51-00-02 AND RD 8/4-24-317.SDR QXEA200600411Skin · corrodedPDX: LT WING FUEL TANK ACCESS AFT FLANGE HAS PITTING AROUND SCREW HOLES (5 LOCATIONS) AT YW 79. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NDTM PART 6, 51-00-02 AND RD 8/4-24-317.SDR 06FDEA0445Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 534. REPAIR CARRIED OUT AT CRACK FOUND AT RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT XORS 534 AS PER FEDEX EA 1-5730-90735, TITLE: WING - LEADING EDGE BEADED DSDR 06FDEA0438Skin · crackedLOWER SURFACE OF LT WING TE AT THE I/B MOST OF OUTBD FLAP THERE IS A CRACK EMMINATING REPAIRED IAW AIRBUS REPAIR DRAWING R572.SDR AMTA200600051Access Panel · corrodedRIGHT WING OWS 151 AND OWS 175 AREA BOTTOM WING FUEL TANK ACCESS CUTOUT WITH PITTING CORROSION. CORROSION REMOVED IAW L1011 SRM 51-21-01, BLENDED AREA FOUND WITHIN LIMITS IAW L1011 SRM 57-32-00 FIG 810. (M)SDR AMTA200600050Access Panel · corrodedRIGHT WING OWS 00 AND OWS 26 AREA BOTTOM WING FUEL TAN ACCESS CUTOUT WITH PITTING CORROSION. CORROSION REMOVED IAW L1011 SRM 51-21-01. BLENDED AREA FOUND WITHIN LIMITS IAW L1011 SRM 57-32-00 FIG 810. (M)SDR 06FDEA0342Skin · misdrilledDOUBLE DRILLED HOLE AT NUT PLATE IN LOWER SKIN OF LEFT WING BULLNOSE 9 INCHES I/B OF NR 3 SLAT O/B SLAT TRACK. *S/D* REPAIRED LOWER SKIN OF LEFT WING BULLNOSE IAW EA 7-5710-91433.SDR 06FDEA0344Skin · chafedRT WING FIXED TRAILING EDGE HAS CHAFE MARK AND SPOTS OF GOUGES FROM WS 224.5 TO WS 625.0 (SKIN UNDER FWD END OF SPOILER.) FABRICATED AND INSTALLED NEW STRAPS IAW SRM 57-30-2 REPLACEMENT PARTS FABRICATED ON TRAVELERS T5/564670,T5/564665,T5/564668,T5/564644,SDR AMTA200600060Access Panel · corrodedRIGHT WING OWS 52 AND OWS 72 AREA BOTTOM WING FUEL DIPSTICK CUTOUT WITH PITTING CORROSION. CORROSION REMOVED IAW L1011 SRM 51-21-01. BLENDED AREA FOUND WITHIN LIMITS IAW L1011 SRM 57-32-00 FIG 810. (M)SDR AMTA200600059Access Panel · corrodedRT WING BETWEEN OWS 296 AND OWS 320 BOTTOM WING FUEL TANK ACCESS CUTOUT WITH PITTING CORROSION. CORROSION REMOVED IAW L1011 SRM 51-21-01. BLENDED AREA AND FOUND WITHIN LIMITS IAW L1011 SRM 57-32-00 FIG 810. (M)SDR AMTA200600058Access Panel · corrodedRIGHT WING BETWEEN OWS 320 AND OWS 344 BOTTOM WING TANK ACCESS CUTOUT WITH PITTING CORROSION. CORROSION REMOVED IAW L1011 SRM 51-21-01. BLENDED AREA FOUND WITHIN LIMITS IAW L1011 SRM 57-32-00 FIG 810. (M)SDR AMTA200600057Access Panel · corrodedRIGHT WING BETWEEN OWS 344 AND OWS 368 AREA BOTTOM FUEL TANK ACCESS PANEL CUTOUT WITH PITTING CORROSION. CORROSION REMOVED IAW L1011 51-21-01. BLENDED AREA FOUND WITHIN LIMITS IAW L1011 SRM 57-32-00 FIG 810. (M)SDR AMTA200600056Access Panel · corrodedRIGHT WING BETWEEN IWS 399 AND IWS 425 AREA OVERWING TANK ACCESS PANEL CUTOUT WITH PITTING CORROSION. CORROSION REMOVED IAW L1011 SRM 51-21-01. BLENDED AREA FOUND WITHIN LIMITS IAW L1011 SRM 57-32-00 FIG 802. (M)SDR AMTA200600055Access Panel · corrodedRIGHT WING BETWEEN OWS 52 AND OWS 78 AREA OVERWING FUEL TANK ACCESS CUTOUT WITH PITTING CORROSION. CORROSION REMOVED IAW L1011 SRM 51-21-01. BLENDED AREA FOUND WITHIN LIMITS IAW L100 SRM 57-32-00 FIG 802. (M)SDR AMTA200600054Access Panel · corrodedRIGHT WING BETWEEN OWS 272 AND 296 BOTTOM WING FUEL TANK ACCESS PANEL CUTOUT WITH PITTING CORROSION. CORROSION REMOVED IAW L1011 SRM 51-21-01. BLENDED AREA WITHIN LIMITS IAW L1011 SRM 57-32-00 FIG 810. (M)SDR AMTA200600053Access Panel · corrodedRIGHT WING OWS 248 AND OWS 272 AREA BOTTOM WING FUEL TANK ACCESS CUTOUT WITH PITTING CORROSION. CORROSION REMOVED IAW L1011 SRM 51-21-01. BLENDED AREA FOUND WITHIN LIMITS IAW L1011 SRM 57-32-00 FIG 810. (M)SDR AMTA200600052Access Panel · corrodedRIGHT WING BETWEEN OWS 199 AND OWS 233 BOTTOM WING FUEL TANK ACCESS CUTOUT WITH PITTING CORROSION. CORROSION REMOVED IAW L1011 SRM 51-21-01. BLENDED AREA FOUND WITHIN LIMITS IAW L1011 SRM 57-32-00 FIG 810. (M)SDR AMTA200600049Access Panel · corrodedLT UNDER WING SURFACE FUEL TANK 2L ACCESS CUTOUT HOLES FOUND WITH SURFACE CORROSION ON THE FOLLOWING PANELS, 532BB, 532DB, 532FB, 533BB, 533DB, 533FB, 533HB, 533KB, 532CB, 532EB, 533AB, 533CB, 533EB, 533GB, 533JB, 534AB. FUEL ACCESS PANEL CUTOUT AREA MINOR SUSDR AMTA200600048Access Panel · corrodedLT OVERWING FUEL TANK ACCESS PANEL CUTOUT IS PITTED AND CORRODED AT OWS 452. LT WING UPPER SURFACE AT OWS 452 FUEL TANK ACCESS CUTOUT FLANGE SURFACE CORROSION CLEANED IAW SRM 51-21-01. NDT AND FOUND NO CRACKS. UT THICKNESS 134 MM. (M)SDR AMTA200600047Access Panel · corrodedLEFT OVERWING FUEL TANK ACCESS CUTOUT FLANGE PITTED AND CORRODED AT OWS 70. LEFT WING UPPER SURFACE AT OWS 70 CORROSION CLEANED FROM FUEL TANK ACCESS CUTOUT IAW SRM 51-21-01. FOUND NO CRACKS. UT THICKNESS REMAINING .291 MM. (M)SDR AMTA200600046Access Panel · corrodedLT OVERWING IWS 412 FUEL TANK ACCESS CUTOUT FLANGES PITTING AND CORRODED. LEFT WING UPPER SURFACE AT IWS 412 CORROSION CLEANED FROM FUEL TANK ACCESS CUTOUT IAW SRM 51-21-01. NDT FOUND NO CRACK. UT THICKNESS TEST SHOWED MATERIAL THICKNESS .310 MM. (M)SDR WRNA200600022Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND AT RIGHT HAND WING SKIN UPPER SURFACE PANEL NR 2 AT THREE FASTENER LOCATION JUST INBOARD OF RIB NR 5, APPROXIMATELY 17 INCHES AFT OF REAR SPAR. REPAIRED PER AVBORNE REPAIR REFERENCE 25599-6-10-18-06. REMOVED FASTENERS ASDR I5HA0258001Wing · gougedA BAGGAGE CART DISCONNECTED FROM ITS TOW VEHICLE AND IMPACTED THE AIRCRAFT IN THE AREA OF THE LOWER LT WING LEAVING GOUGES AT WING STATIONS 51.5 AND 52.5 RANGING FROM .078 TO .380 WIDE AND .016 TO .038 DEEP. THE DAMAGE WAS ACCESSED. THE DAMAGED AREA DOES NOTSDR 06FDEA0246Skin · crackedLEFT WING EXTERNAL SKIN OF L/E SLAT TRACK NR 10 XOS 660 FOUND CRACK .5 INCH LONG ON THE SLAT TRACK HOLE ANGLE. INSTALLED EXTERNAL DOUBLER IAW SRM 57-10-00 FIG 68 VOL 1, FABRICATED PART IAW DETAIL PART TRAVELER F163379/N00379 AND IAW SRM 57-10-00 FIG 68 VOL 1.SDR 06FDEA0245Doubler · unknownRIGHT WING L/E SKIN EXTERNAL DOUBLER AT STA XOS 900 TO STA XOS 916. REWORKED REPAIR IAW SRM 57-10-00 FIG 28 VOL 1, REPAIRED IAW SRM 57-10-00 FIG 28 VOL 1, FABRICATED PART IAW DETAIL PART TRAVELER 1214 AND SRM 57-10-00 FIG 28 VOL 1.SDR QXEA200600184Skin · corrodedPDX: ON LEFT WING APERTURE FOR PANEL 522BT THE 2ND HOLE ON AFT SIDE FROM OUTBOARD END IS BLENDED OUT OF LIMITS FOR RD 8/4-57-441. MINIMUM REMAINING MATERIAL IS .062". MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02-250-801, HORIZON EA 5-57-424 AND RDD 8/4-57-SDR QXEA200600180Skin · corrodedPDX: ON LEFT WING APERTURE FOR PANEL 522BT THE 4TH HOLE ON FWD SIDE FROM THE INBOARD END IS BLENDED OUT OF LIMITS FOR RD 8/4-57-441. MINIMUM REMAINING MATERIAL IS .162". MAINTENANCE REPAIRED IAW NDTM PART 6, 51-11-02-250-801, HORIZON EA 6-57-424 AND RD 8/4-5SDR QXEA200600157Skin · corrodedPDX: RT WING ON APERTURE FOR FUEL PANEL 622BT HAS FRETTING CORROSION AROUND BOLT HOLES. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NDTM PART 6, 51-00-02 AND HORIZON EO 6-57-317.SDR QXEA200600155Skin · corrodedPDX: RT WING ON APERTURE FOR FUEL PANEL 622CT HAS FRETTING CORROSION AROUND BOLT HOLES. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NDTM PART 6, 51-00-02 AND HORIZON EO 6-57-317.SDR QXEA200600147Skin · corrodedPDX: LT WING LANDING FOR PANEL 522CT HAS 1 HOLE ON FWD SIDE AND 6 HOLES ON AFT EDGE WITH FRETTING CORROSION ON EDGES OF HOLES. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NDTM PART 6, 51-00-02 AND HORIZON EO 6-57-317.SDR QXEA200600140Skin · corrodedPDX: FOUND RT WING APERTURE LANDING FOR PANEL (621BT) HAS FRETTING CORROSION AROUND NUMEROUS BOLT HOLES. MAINTENANCE REPAIRED IAW RD 8/4-57-441, RD 8/4-57-526, NDTM PART 6, 1-84-7A AND HORIZON EA 6-57-427.SDR 06FDEA0234Skin · chafedLEFT HAND WING - LEADING EDGE SKIN BETWEEN SLAT TRACK NR 6 AND NR 7. FOUND WITH CHAFING MARK. DOUBLER FABRICATED AND INSTALLED AT LEFT HAND WING LEADING EDGE SKIN BETWEEN SLAT TRACK #6 AND #7 AS PER SRM 57-10-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED ASDR USAA060069Skin · damagedABOVE RSS 140, 6" OUTBD OF FUSELAGE, UPPER WING SKIN, BLENDED DAMAGE OUT SHOT PEENED AND TREATED SKIN PER SRM 51-20-06 FIG 1, DEFECT SIZE: 7.0" BY 2.25" AREA, CHAFFED SKIN.SDR QXEA200600179Skin · corrodedPDX: ON RIGHT WING APERTURE FOR PANEL 622CT THE 7TH HOLE ON FWD SIDE OF APERTURE FROM INBOARD END HAS A NICK ON EDGE OF HOLE APPROX .012 INCH DEEP. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02-250-801, HORIZON EA 6-57-424 AND RD 8/4-57-604.SDR QXEA200600178Skin · damagedPDX: ON RIGHT WING APERTURE FOR PANEL 622BT, THE 8TH HOLE ON AFT SIDE OF APERTURE FROM INBOARD END IS BLENDED OUT OF LIMITS FOR RD 8/4-57-441. REMAINING MATERIAL MINIMUM .163 INCH. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02-250-801, HORIZON EA 6-57-424 ASDR QXEA200600177Skin · damagedPDX: ON RT WING 4 INCHES FROM INBOARD END OF PANEL 622CT ON FWD EDGE OF FUEL TANK OPENING HAS A NICK ON EDGE OF APERTURE APPROX .010 DEEP. MAINTENANCE REPAIRED IAW NDTM PART 6, 51--00-02-250-301, HORIZON EA 6-57-424 AND RD 8/4-57-604.SDR IXXA06SMN051SDoubler · wornDURING ROUTINE C-CHECK INSPECTION, NR 1 STUB WING DOUBLER LWR PART WORN STA XOLDO 67.750. PERFORMED MAJOR REPAIR IAW SRM 57-2-1A FIG 1. REMOVED WORN DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED STOP DRILL. FABRICATED EXTERNAL REPAIR DOUBLER IAW SRM 57-2-1SDR IXXA06SMN044SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING UPPER SKIN SCRATCHED AND DENTED ON INBD FLAP BETWEEN XW 104.000 AND XW 122.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 PAGE 2. REMOVED DAMAGED PLATING IAW DC-8 SRM 57-1-0, DC-8 SRM 51-1-21. FABRICATED NEW PLATINSDR 06FDEA0192Skin · corrodedLEFT HAND WING UPPER SURFACE TRAILING EDGE FOUND CORROSION AT XORS 697. REMOVED AS PER SRM 51-21-01. FOUND EXCEEDED LIMIT PER SRM 57-10-00. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-90729.SDR QXEA200600315Fastener · looseYYC - C3 RIGHT WING UPPER SKIN TRAILING EDGE (INBOARD OF MULTI FUNCTION SPOILER) HAS LOOSE FASTENER. REPAIRED IAW CRJ700/900 SRM 51-42-06-001-001-A01.SDR A6WA200640047Skin · corrodedRT WING PLANK HOLE NR 15 HAS CORRODION AT IB AFT SIDE 4 INCHES L X .002 INCH-.003 INCH D AND IB FWD SIDE 1.5 INCH L X .001 INCH - .002 INCH D AND AT OB SIDE 1 INCH L X .002 INCH-.003 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RT WING PLANK ACCESS HOLE
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