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 04FDEA02637Skin · damagedLEFT WING TRAILING EDGE SKIN AFT OF MAIN LANDING GEAR LOWER SURFACE REQUIRES FABRICATION. FABRICATED DOUBLER AND SKIN IAW DAC DWG ARC0468, BONDED SKIN AND DOUBLER IAW TPS 1001 REV E AND DAC DWG ARC0468 AND EA 9-5710-81448. ALODINED AND PRIMED CONTACT UPPER SSDR 04FDEA02647Panel · debondedFINGER DOUBLERS DISBONDED INSIDE LEFT WING TRAILING EDGE FAIRING BETWEEN XW 373 AND XORS 486, ACCESS THROUGH 641 MB. REMOVED ARC0584-1 SKIN FOR REPLACEMENT IAW DC10 SRM 51-35-01, 51-33-01 VOL II. FABRICATED NEW ARC0584-1 SKIN ASSEMBLY IAW DAC DWG 0584. INSTSDR 04FDEA02642Panel · delaminatedPANEL 636 DL HAS SEVERAL AREA OF DELAMINATION. REPAIRED PANEL P/N ARC0566-2 BY FABRICATING AND BONDING NEW SKIN, DOUBLERS AND CORE IAW FEDEX EA 8-5710-77513, DAC DWG ARC0566 AND TPS 1001 REV E, REFERENCE N/R N00321.SDR 04FDEA02646Panel · delaminatedRIGHT WING PANEL 635 GL DELAMINATED AND ONE GOUGE. REPAIRED PANEL 635 GL BY FABRICATING AND BONDING NEW SKINS, DOUBLERS AND CORE IAW TPS 1001 REV E, DAC DWG ARC2008 AND FEDEX EA 8-5750-81442. REFERENCE N/R N00239.SDR 04FDFEA02637Skin · damagedLEFT WING TRAILING EDGE SKIN AFT OF MAIN LANDING GEAR LOWER SURFACE REQUIRES FABRICATION. FABRICATED DOUBLER AND SKIN IAW DAC DWG ARC0468, BONDED SKIN AND DOUBLER IAW TPS 1001 REV E AND DAC DWG ARC0468 AND EA 9-5710-81448. ALODINED AND PRIMED CONTACT UPPER SSDR 04FDEA02641Doubler · tornLEFT WING LEADING EDGE CAVITY, CORRUGATED SKIN TORN ABOVE ANTI-ICE TELESCOPE DUCT, STA XORS 372. REMOVED AND INSTALLED TELESCOPING DUCT IAW DC10 MM 30-11-01-2. REPAIRED DAMAGED SKIN IAW FEDEX EA 8-5710-81456 STEP 1-10, REFERENCE N/R N00730.SDR 04FDEA02640Panel · delaminatedLEFT WING LOWER TRAILING EDGE PANE 541KB DELAMINATED INTERIOR SURFACE. REMOVED INNER SKIN, OUTER SKIN, DOUBLER AND CORE IAW FEDEX EA 8-5750-81445. BONDED NEW INNER SKIN, OUTER SKIN DOUBLER AND CORE IAW FEDEX EA 8-5750-81445 AND TPS 1001 REV E, REFERENCE N/R SDR 04FDEA02638Panel · delaminatedRIGHT WING TRAILING EDGE PANEL 641 EB HAS MANY AREA OF DELAMINATION. REPAIRED RIGHT WING TRAILING EDGE PANE 641EB BY FABRICATING AND BONDING INNER AND OUTER SKIN, HONEYCOMB CORE AND INNER DOUBLER IAW EA 8-5710-7763, DAC DWG ARC0264 AND TPS 1001 REV E, REFERENSDR UPS04843263Skin · crackedINSPECTION TYPE: C3, POSSIBLE CRACK IN UPPER WING SKIN (LT) AT FASTENER ON AFT SIDE OF STRINGER 15, JUST O/B OF RIB AT XRS 74. NDT VERIFIED CRACK 1 INCH IN LENGTH. CUT OUT DAMAGED AREA 1.375 INCH DIAMETER. NDT VERIFIED NO CRACKS NOTED AT CUT OUT. FABRICATESDR 04FDEA02632Panel · corrodedLEFT WING UPPER SURFACE XIS=247 FWD SIDE FOUND CORROSION. LEFT WING UPPER SURFACE XIS=247 FWD SIDE REPAIRED AS PER EA NR 1-5710- 81539, TITLE: WINGS LT WING UPPER SURFACE, CORROSION BLEND OUT AT XORS 144.25.SDR 2005FA0000268Panel · corrodedDURING WIG (LT) NDT INSPECTION EXFOLIATION CORROSION NOTED ON WING UPPER PLANK AND FRONT BEAM BETWEEN RBS 284 THRU 375. REMOVED EXFOLIATION CORROSION IAW SRM. REPAIRS COMPLETED.SDR 2005FA0000103Skin · corrodedDURING WING (RIGHT) NOT INSPECTION, EXFOLIATION CORROSION NOTED ON WING UPPER PLANK AND FRONT BEAM BETWEEN RBS 284 THRU 375. EXFOLIATION CORROSION REMOVED IAW SRM. REPAIRS COMPLETED.SDR COOSDR040038Skin · delaminatedLT WING, OB AFT FLAP LOWER AND UPPER SKIN DELAMINATED AT WBL 240.SDR UPS04243181Panel · delaminatedINSPECTION TYPE: C, LEFT WING UPPER SURFACE T/E PANEL FWD OD MLG BEAM HAS DELAMINATION ON AFT END, ALSO HAS UPPER SURFACE DENTS. REPAIRED AND INSTALLED PANEL AS PER DRAWING 65-21655 IAW SRM 51-30-02.SDR DHL2004801505Doubler · crackedLEFT INNER WING OUTBOARD L/E SECTION INTERNAL DOUBLER CRACKED 0.250, STA XW 485.000. REMOVED CRACKED INTERNAL DOUBLER IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW INTERNAL DOUBLER (ALCLAD 7075-T6 0.050) IAW DC8 SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED IAW DSDR USAA040587Skin · crackedPIT - FOUND SKIN CRACKED 1 INCH, LOWER LEADING EDGE SKIN FORWARD OF OUTBOARD ALT SLAT TRACK. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PE SRM 57-43-01, FIG 206. (M)SDR IXXA0500023SSkin · crackedDURING A ROUTINE C CHECK INSPECTION, RT WING TOP PANEL PLATING HAS CRACK DAMAGE STA XRS 74.000, S-9. MAJOR REPAIR ACCOMPLISHED IAW DC8 SRM 57-2-1 FIG 17 PG 87, 88 1. REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21. REMOVED DAMAGED AREA IAW DC8 SRM 57-2-1 PAGESSDR QXEA200400651Access Panel · corrodedRT WING FUEL PANEL 624AT HAS CORROSION ON BOTTOM IB END IN TWO PLACES. BLENDED DAMAGED AREA IAW HDC 8400 SRM 57-20-35-350-801, PARAGRAPPH 1, 2, 3. 4. 5, ;A B1-4. REMOVED PANEL TOP SURGACE PAINT FOR MEASUREMENTS. PERFORMED THICKNESS CHECK OF PANEL AT BLENDED SDR QXEA200400652Access Panel · corrodedFUEL PANEL 622CT HAS CORROSION ON BOTTOM SURFACE AROUND SCREW HOLES. BLENDED CORROSION AREA IAW SRM 57-10-35-350-802, PARAGRAPH 1-6B(4). FOUND BLENDED AREA TO BE OUT OF LIMITS. REPLACED FUEL PANEL 622CT WITH NEW FROM STOCK.SDR QXEA200400654Access Panel · corrodedPDX - LEFT HAND WING CUTOUT FLANGE FOR ACCESS PANEL 524BT HAS FRETTING DAMAGE AT BOTH ENDS OF MATING SURFACE. BLENDED OUT FRETTING CORROSION. DAMAGE FOUND TO BE BEYOND LIMITS. MAPPED AND SENT TO ENGINEERING. REPAIRED IAW HORIZON AIR EA 6-57-232 AND RD 8/4 SDR CALA0400617Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING L/E SKIN AT STA XF 251 JUST FORWARD OF FUELING DOOR. THE SKIN WAS REPAIRED IAW SRM 57-06B, FIGURE 4.SDR COOSDR040022Skin · corrodedRT WING LEADING EDGE SLOT SKIN CORRODED, BETWEEN XW 329.25 AND XW 359.0.SDR UIEA200400152Panel · delaminatedFOUND LER LEFT WING PANEL AT ILES 173.6 HAD DELAMINATION HEAT DAMAGE WHILE ON GROUND. THE PANELS WERE REPLACED IAW SRM 51-30-02 AND AMM 51-24-11. (M)SDR UPS04443026Plate · crackedINSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE PLATE (BS 1241)FOUND CRACK AT HOLE NR 5 APPROX 0.060 INCH. RT WING REAR SPAR UPR SPLICE PLATE HOLE NR 5 CRACK FREE AT 1.00 INCH WAS REPAIRED IAW EO B747-5740-17032.SDR SWAA042405Skin · corrodedDURING SCHEDULED C4 CHECK, FOUND LT WING SKIN AT WING STATION 132, STRINGER 3, CORRODED. REPAIRED SKIN PER EA.SDR QXEA200400646Panel · corrodedCOUNTERSINKS IN PANEL 522CT HAVE FRETTING. REMOVED CORROSION FROM COUNTERSINKS ON PANEL 522CT WITH SCOTCH BRITE. MAPPED FOR ENGINEERING. OK TO INSTALL NEW FROM STOCK 522CT PANEL IAW D-84 AMM 57-11-01-400-801, PARAGRAPH 1-4, A-D (1-8).SDR QXEA200400640Panel · corrodedPDX - PANEL 622CT COUNTER SINKS HAVE FRETTING. REMOVED CORROSION FROM COUNTER SKINS ON FUEL PANEL 622CT USING SCOTCH BRITE. COMPLETED CLEANING FRETTING CORROSION USING SCOTH BRITE. MAPPED FOR ENGINEERING. REPLACED PANEL WITH NEW FROM STOCK.SDR IXXA0500030SPanel · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND RT INNER WING EXTENDED LEADING EDGE SLANT PANEL UPPER CAP INTERIM REPAIRS BETWEEN STATIONS XFS. 32.500 AND XFS. 182.500. REPAIR ACCOMPLISHED. REMOVED DAMAGED SLANT PANEL UPPER CAP IAW EC8 SRM 51-1-20D PG 21, DC8 SRMSDR COOSDR040023Skin · corrodedWING CENTER SECTION LOWER SKIN AFT SECTION BETWEEN LBL 30 AND RBL 30 SKIN OUTER FACE CORRODED.SDR COOSDR040012Skin · corrodedWING CENTER SECTION FROM STA 740 TO STA 745 BETWEEN LBL 67.000 INCHES AND LBL 61.000 INCHES, UPPER SKIN PANEL WITH CORROSION ON OUTER SURFACE.SDR 04FDEA02485Skin · corrodedCENTER WING TANK, STA 1219 - STA 1239, LBL 27 - LBL 47 HORIZONTAL PRESSURE PANEL TOP SURFACE CORRODED. CORROSION REMOVED, MATERIAL ORIGINAL THICKNESS = 0.175 INCH, MATERIAL REMOVED = 0.017 INCH, REMAINING MATERIAL = 0.158 INCH AND FOUND WITHIN LIMITS AS PERSDR QXEA200400645Panel · corrodedCOUNTERSINKS IN PANEL 522BT HAVE FRETTING. BLENDED AND CLEANED FRETTING CORROSION ON 12 COUNTERSINKS WITH SCOTCH BRITE. MAPPED PANEL 522BT FOR ENGINEERING. HFEC INSPECTION BLENDED AREAS FOR CRACKS IAW D8-400 NDTM, PART 1, 51-00-06. NO CRACKS NOTED. INSTALSDR QXEA200400644Panel · corrodedPDX - COUNTERSINKS IN PANEL 522AT HAVE FRETTING. REMOVED CORROSION AND DAMAGE. NO MEASUREMENTS MADE. MAPPED COUNTERSINKS FOR ENGINEERING. HFEC INSPECTED BLENDED PANEL FOR CRACKS IAW D8/400 NDTM PART 1, 51-00-06/ NO CRACKS NOTED. INSTALLED NEW PANEL 522AT SDR QXEA200400643Panel · corrodedPDX - COUNTERSINKS FOR 523AT HAVE FRETTING. REMOVED CORROSION FROM 2 COUNTERSINK HOLES ON FORWARD EDGE OF PANEL USING SCOTCH BRITE. REMOVED CORROSION FROM REMAINING COUNTERSINK HOLES, BLENDED DAMAGE. MEASURED ALL HOLES, 4 HOLES OVERSIZED. MAPPED AND ROUTEDSDR COOSDR040035Panel · corrodedLT WING, FIXED PANEL NR 571, PN 5648891-1, WITH CORROSION AND DELAMINATED AT SEVERAL PLACES.SDR QXEA200400639Panel · corrodedPDX - LITE FRETTING CORROSION FROM 14 COUNTER SINKS AT FORWARD EDGE OF PANEL USING SCOTCH BRITE ON AFT EDGE OF PANEL. NO MEASUREMENTS TAKEN, FRETTING DAMAGE AND REMOVED CORROSION FROM REMAINING 42 COUNTER SKINS USING SCOTCH BRITE. NO MEASUREMENTS TAKEN. MEASDR QXEA200400637Panel · corrodedLITE FRETTING IN COUNTER SINKS OF PANEL 622AT. REPAIRED IAW DHC-8-400 SRM 51-26-10 AND AMM 57-11-01-400-801, PAGE 408-409, PARAGRAPH 4 A, C, D (1-2).SDR QXEA200400638Panel · corrodedLIGHT FRETTING IN COUNTER SINKS OF PANEL 622BT. REPAIRED IAW DHC-8-400 SRM 51-26-10 AND AMM 57-11-01-400-801, PAGE 408-409, PARAGRAPH 4 A, C, D (1-2).SDR USAA040465Skin · delaminatedPIT - FOUND SKIN TO CORE BOND DELAMINATION 11.25 INCH BY 7.25 INCH, RIGHT WING OUTBOARD AFT FLAP TOP SKIN TO CORE BOND, CENTER. REMOVED TOP SKIN AND CORE, INSTALLED NEW CORE SECTION AND DOUBLER ASSY PER T/R 57-50-39A AND 51-70-10. (M)SDR USAA040533Skin · wornCLT - FOUND SKIN AND SPAR WEB WORN .360 INCH, .500 INCH, .225 INCH HOLES, FASTENER HOLES AT OUTBOARD FLAP TRACK FITTING. OVERSIZED HOLES AND INSTALLED FREEZE PLUGS PER EA 95714. (M)SDR ABXA040330Skin · gougedRIGHT WHEEL INBOARD AILERON, 3 RIVETS MISSING HEADS OR PART OF HEAD AND OPEN HOLE AT APPROXIMATELY XA 562, LOWER LEADING EDGE. REMOVED AND REPLACED DAMAGED SKIN SECTION AND DOUBLER IAW REA D857-49983MR.SDR IXXA0500044SSkin · damagedDURING A ROUTINE C-CHECK INSPECTION, RT WING OUTBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIR AROUND STA XF. 226.000. REPAIR ACCOMPLISHED. REMOVED ALL FASTENERS WITHIN REPAIR AREA. REMOVED THE DAMAGED AREA. PERFORMED NDT INSPECTION, CLEANED, TREATED AND SDR ABXA040315Skin · corrodedMAIN CABIN FS 759, RIGHT BUTT LINE 8, WING CENTER SECTION, CORRODED. FABRICATED REPAIR DOUBLER AND REPAIRED AREA IAW REA D857-49995-MR.SDR UPS04242997Panel · erodedINSPECTION TYPE: C, LT WING LOWER FIXED L/E PANEL FSS 262 TO FSS 312 ERRODED ALONG L/E AT O/B END. PANEL REMOVED IAW 51-30-2. PANEL DERIVETED FROM BRACKET IAW 51-30-2. FUEL DRAIN PIPES DISCONNECTED IAW MM 29-00-00. PANEL FABRICATED IAW DRG 65-21653. PANELSDR 04FDEA02413Skin · corrodedRT WING, WING UNDER SURFACE JUST ABOVE NR 3 PYLON FWD INBOARD OF THRUST LINK CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME I. COMPLIED WITH FEDEX EA 1-5750-76815, WINGS RT WING - LOWER FORWARD PANEL ASSEMBLY - CORRODED.SDR COMA0460443Skin · crackedCRACK FOUND ON LEFT WING PLANK, IAW CRJ REO 601R-57-21-130.SDR COMA0460442Skin · crackedCRACK FOUND ON RIGHT WING PLANK, I/A/W CRJ REO 601R-57-21-130.SDR P5CA0401164Panel · delaminatedDELAMINATION UNDER SPEED TAPE REPAIR LT WING, LOWER SERVICE WBL 175 FWD SPAR. REMOVED DAMAGE AREA RE-BONDED PER SRM 51-40-15.SDR P5CA0401163Panel · delaminatedDELAMINATION ON PANEL LT WING LANDING LIGHT ENTRY DOOR SPLIT & DELAMINATION 4 X 8 INCHES UNDERSPEED TAPE. REMOVED DAMAGE & REPAIRED PER SRM 51-40-13.SDR P5CA0401160Access Panel · crackedRIGHT WING ACCESS PANEL 672 DB HAS CRACK & DELAMINATION. REMOVED DAMAGE AREA & BONDED PER SRM 51-40-15.
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