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 BQVA200721071Wedge · damagedDURING THE SCHEDULED 72 MONTH LT WING WEDGE INSPECTION CMP 575030, ONE WING WEDGE HOLD DOWN RIVNUT WAS FOUND TO BE IN AN OVERSIZED HOLE.SDR IXXA07SMN086SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LEADING EDGE HAS A NON STANDARD REPAIR FROM STATION XFS422.000 TO STATION XOLDI6.220. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND, AFTSDR IXXA07SMN085SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LEADING EDGE HAS A NON STANDARD REPAIR FROM STATION XFS416.000 TO STATION XOLDI6.220. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTESDR IXXA07SMN084SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LEADING EDGE HAS A NON STANDARD REPAIR FROM STATION XFS304.000 TO STATION XFS310.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND, AFTSDR IXXA07SMN081SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING LOWER CENTRAL LEADING EDGE HAS A NON STANDARD REPAIR FROM STATION XFS304.000 TO XFS316.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUNDSDR IXXA07SMN053SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER LEADING EDGE CORRODED, BETWEEN STATIONS XFS341.500 AND XFS304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARSDR IXXA07SMN082SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER FORWARD SKIN CORRODED AT STATION XFS410.250. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND DAMAGE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER AND FILLERSDR CALA0700044Skin · crackedINSPECTION FOUND A 6" CRACK IN RT WING FIXED LEADING EDGE SKIN PANEL UPPER SURFACE AT WS 418. PERFORMED OPERATION 04 OF EA 5731-01010 AND REPAIRED THE CRACKED AREA IAW SRM 51-70-17 AND ATTACHED LAYUP PROCEDURE WORK CARD, COMPOSITE REPAIR WITHOUT CORE REPLACEMSDR CALA0700043Skin · crackedINSPECTION FOUND AN 8" CRACK IN LT WING FIXED LEADING EDGE SKIN PANEL UPPER SURFACE AT WS 425.5. PERFORMED OPERATION 04 OF EA 5731-01010 AND REPAIRED CRACKED AREA IAW SRM 51-70-17 AND ATTACHED LAYUP PROCEDURE WORK CARD (COMPOSITE REPAIR WITHOUT CORE REPLACEMESDR 200600073Skin · cracked2EA CRACKS WERE DETECTED WHILE PERFORMING AD 2002-19-14, 1 CRACK EMANATING FROM A FASTENER HOLE LOCATED AT FS 543 RT CW STA 70 LOWER WING AND 1 CRACK EMANATING FROM A FASTENER HOLE AT FS 569, LT CW STA 57, LOWER WING. BOTH CRACKS ARE .1250 INCH LONG.SDR HALA0700039Panel · damagedFOUND RT WING PANEL 611CB LEADING EDGE AND RIGHT WING SLAT LOWER INBOARD CLOSEOUT PANELS DAMAGED. REMOVED AND REPLACED RT WING PANEL 611CB AND RT WING SLAT LWR CLOSEOUT PANEL SECURITY CHECK OKAY.SDR UIEA200700026Panel · crackedLT WING PYLON GAP PANEL AT ILES 640.47 HAS A 3.0 INCH CRACK. ACCOMPLISHED PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 18 SHEET 5 AND SRM 51-40-12, ALSO REFERENCE ATLAS AIR EO 4757A342.SDR UIEA200700027Panel · crackedLT WING UPPER FIXED PANEL, 12 INCHES FROM FORWARD EDGE OF NR 5 SPOILER, WBL 421.00 HAS A 6.0 INCH CRACK. ACCOMPLISHED PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 2 SHEET 5 AND SRM 51-40-12 AND ATLAS AIR EO 4757A342.SDR UPS07M49355Skin · chafedINSPECTION TYPE:C RIGHT WING TOPSIDE FIXED L/E XORS 1093.629 CANTED AREA FOUND CHAFE MARK. AREA SMOOTHEN MATL REMAIN 0.083 EXCEED LIMIT PER SRM 57-00-01 FIG 3 VIR38. L/E SKIN REMOVED PER SRM 51-33-01VIIR38. TRIMMED OUT PER EN1085-07. HFEC C/O PER NDTSPMR12SDR DHL2007802514Skin · misrepairedNR 4 RT STUB WING LWR SURFACE HAS A NON STANDARD REPAIR AT STA XFS 562.500. PERFORMED MAJOR REPAIR IAW SRM 57-2-1A FIG 1 PG 3. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED EXT REPAIR DOUBLER (AL7075T6 0.080") AND INTERNAL DOUBLER (ASDR 07FDEA00186Skin · dentedLT WING INBD FLAP: DENTS ON LOWER SKIN AFT PANEL AT STA XIFH 171, XIFH 177 AND XIFH 201 WITH DEFORMATION OF BACK-UP STRUCTURE. PERFORMED REPAIR SKIN IAW SRM 57-10-00 FIG 3 VOL 1 IAW SRM 51-41-01 FIG 1 VOL 2. REPLACED TEE IAW SRM 51-35-01 PAG 1/13 VOL 2. FABSDR DHL2007802509Skin · crackedRT WING UPPER SKIN 0.750" CRACKED STA XRS 74.000 S-14R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 10 SHEET 1. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG 10 SHEET 1. PERFORMED NDT INSP IAW DC8 NDT SPM PART SDR A6WA200740047Skin · corrodedRT WING LOWER PLANK FUEL TANK ACCESS DOOR CUT OUT HOLE NR 8 (PNL 640FB) HAS MINOR CORROSION AT IB AND OB ENDS APPROX 3 INCH LONG BY .003 INCH DEEP AT IB END AND 1.25 INCH LONG BY .002 INCH DEEP AT OB END. BOTH IN NON-CRITICAL AREA. (M)MAINTENANCE REPAIRED WISDR A6WA200740046Skin · corrodedRT WING LOWER PLANK FUEL TANK ACCESS DOOR CUT OUT HOLE NR 2 (610AB) HAS MINOR PITTING AT IB END IN AN AREA APPROX 1.5 INCH LONG BY .005 INCH DEEP IN NON-CRITICAL AREA. (M) MAINTENANCE REPAIRED WING PLANK HOLE NR 2 (610 AB) IAW REO 601R-57-21-030 REV F AND EOSDR A6WA200740045Skin · corrodedFOUND LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT HOLE NR 2 (PNL 510AB, HAS MINOR PITTING AT INBOARD END IN AN AREA APPROX 3 INCHES LONG BY .005 INCH DEEP IN NON-CRITICAL AREA. (M) MAINTENANCE REPAIRED WING PLANK HOLE NR 2 (510AB) IAW REO 601R-57-21-0SDR A6WA200740044Skin · corrodedFOUND LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT HOLE NR 16 PN. 550HB, HAS MINOR PITTING AT IB END IN AN AREA APPROX 3.25 INCH LONG BY .003 INCH DEEP IN NON-CRITICAL AREA. (M) MAINTENANCE REPAIRED WING PLANK HOLE NR 16 (550 HB) IAW REO 601R-57-21-030 SDR 07FDEA00159Access Panel · corrodedLEFT WING FUEL ACCESS PANEL 534 CT GOUGED ON BOTTOM SIDE. FABRICATED NEW FUEL PANEL IAW DAC DRAWING 0872 REV AP. INSTALLED ON 28C1701-01, MECH 4678 QC 231.SDR 07FDEA00158Access Panel · corrodedLEFT WING FUEL ACCESS PANEL 535AT PITTED ON BOTTOM SIDE. FABRICATED NEW FUEL PANEL IAW DAC DRAWING ARB0872 REV AP. INSTALLED ON CARD, 28C1701-01. MECH 4678 QC 231.SDR 07FDEA00157Access Panel · corrodedRIGHT WING FUEL ACCESS PANEL 634CT IS PITTED ON BOTTOM. FABRICATED NEW FUEL ACCESS PANEL 634CT IAW DAC DRAWING ARB0872 REVISION AP. INSTALLED ON CARD 28C1506-01.SDR UPS07M49237Doubler · crackedINSPECTION TYPE:C LEFT WING L/E LWR COMPT STA XORS 558 FOUND UPPER DOUBLER PANEL CRACKED AS MARKED. LEFT WING L/E LWR COMPT STA XORS 558 UPPER DOUBLER REMOVED PER SRM 51-31-01, V2R 2, R38. REPAIR DOUBLER FILLER ANGLES FAB & HOLES DRILLED PER SRM 57-10-00 -00SDR 07FDEA00152Panel · maint errorWHILE DRILLING HEAD FROM STRIPPED SCREW A HOLE WAS ELONGATED IN WING PLANK COMMON TO PANEL 550 JB COMPLIED WITH EA6-5700-106331 PT1 BY PERFORMING REPAIR IAW AIB TD /J1/S1/04141/2007 ISSUE A.SDR UIEA200700012Panel · dentedRT WING INBOARD LEADING EDGE PANEL AT WBL 158.0 HAS A 2.0 INCH LONG BY 1.5 INCH WIDE BY .073 INCH DEEP DENT. ACCOMPLISHED PERMANENT REPAIR AS PER B747-200 SRM 51-40-09 FIG 18 SHEET 1 THRU 5. ALSO, REFERENCE ATLAS AIR EO NO. 4757A314.SDR UIEA200700011Skin · crackedLT WING, UPPER SURFACE, TRAILING EDGE PANEL, AFT OF REAR SPAR, WBL 445 IS CRACKED AROUND FASTENER HOLE. ACCOMPLISHED PERMANENT REPAIR AS PER B747-200 SRM 51-40-09 FIG 2, SHEETS 1 THRU 5. REPAIR AREA IS 4.0 INCH BY 4.0 INCH ALSO, REFERENCE ATLAS AIR EO NR 475SDR UPS07849118Skin · crackedWHILE GETTING OK TO INSTALL LT AUX TANK. FOUND CRACK ON LT STUB WING LE UPPER IB SIDE. REPAIRED LT LE IB SLOT SUPPORT STRUCTURE SKIN STA XFS-195 IAW RAA DC8-57-20205 A.SDR UPS07849110Skin · crackedINSPECTION TYPE:C3 LT STUB WING L/E ABOVE NR 2 HAS A CRACK ON UPPER O/B SIDE. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SAA EA 008-5710-01-A0615.SDR DHL2007802510Skin · crackedLT WING UPPER SKIN CRACKED 1" S-9 AT STA XRS 74.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR ON LT WING UPPER SKIN STA XRS 74.000 S-9 IAW SRM 57-2-1 FIG 17 PG 87-88. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG 17 PG 87-88. SDR IXXA07SMN043SSkin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HAND WING OUTBOARD SLOT VANE HOLES ELONGATED AT STATION XOLDI6.225. REMOVED EXISTING INTERNAL DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICSDR IXXA07SMN046SSkin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD LEADING EDGE HOLES ELONGATED AT STATION XFS 710.000. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED REPSDR IXXA07SMN044SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING-UPPER LEADING EDGE CORRODED AT STATION 472.099. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERNAL SURFACE. APPLIESDR IXXA07SMN045SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER LEADING EDGE CORRODED AT STATION XFS304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED SDR IXXA07SMN036SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER SKIN HAS A NON STANDARD REPAIR FROM STATION XW104.000 TO STATION XW110.000. REMOVED EXISTING SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN ASDR UPS07M49541Panel · crackedINSPECTION TYPE:C RIGHT L/E LWR COMPT FOUND CRACK AT UPPER DOUBLER PANEL AND STRAP AS MARKED APPROX STA XORS 562. OPEN UP FOR ACCESS, PER DEFECT STATED ABOVE AREA PER SRM 51-31-01 V2 R38. RIGHT WING L/E LWR, STA XORS 562 BEADED DOUBLER TRIMMED PER 57-10-00.FSDR UPS07M49238Doubler · crackedINSPECTION TYPE:C LEFT L/E COMPT UPPER DOUBLER PANEL CRACKED AS MARKED APPROX STA XORS 562. LEFT L/E COMPT UPPER DOUBLER PNL FASTENERS REMOVED PER SRM 51-31-01 VOL II R.38. REPAIR DOUBLER FABRICATED & HOLES DRILLED PER SRM 57-10-00 FIG 258 TEMP R.57-5. VISUSDR QXEA200700708Panel · chafedC4 OKC - FOUND PANEL 584AB CHAFED AT CUTOUT. REPAIRED IAW 51-12-00, 57-51-01.SDR ASAA0741392Skin · dentedTHE LEFT WING TRAILING EDGE I/B FORE FLAP LWR SURFACE HAS AN EXISTING REPAIR WITH MULTIPLE DENTS AND DINGS AT WBL 90. REMOVED THE EXISTING REPAIR DOUBLER AND DAMAGED AREA OF LOWER SKIN FABRICATED AND INSTALLED A SKIN FILLER AND REPAIR DOUBLER IAW SRM 51-70-10SDR 07FDEA00112Skin · damagedRT WING TIP WING LOWER SKIN TWO DOUBLERS REPAIR O/B OF ACCESS DOOR XFS 1191. REMOVED AND REPLACED STIFFENER IAW DWG ARB2204 ARB1044. INSTALLED DOUBLER REPAIR IAW SRM 57-00-01 FIG 4 SHEET 2 VOL 1. FABRICATED PART IAW DETAIL PARTS TRAVELER N01124 AND SRM 57-0SDR 07FDEA00105Skin · misrepairedLT WING L/E UPPER SIDE AT STA XIS240 EXISTING SKIN REPAIR. PERFORMED INSPECTION OF REPAIR AND NOT FOUND INCOMPLIANCE WITH CRITERIA REQ BY EO NR 8-5100-7-5001 BECAUSE FOUND WEAR ON SURFACE OF DOUBLER. REMOVED AND REPLACED REPAIR IAW SRM 57-10-00 FIG 15A SHTSDR AWXA200700109Skin · crackedMCN - MAJOR REPAIR - C-19 CHECK, CRACKS FOUND ON NR 6 SLAT BOTTOM SKIN AT SLAT STA 300 - 351. REPAIRED CRACKS ON NR 6 SLAT BOTTOM SKIN AT SLAT STA 300 - 351 IAW B737-300 SRM 57-43-01-2R6, FIG 201. INSTALLED COVE PANEL IAW B737 AMM 20-50-11-2, FIG 202. INSTASDR IXXA07SMN028SSkin · crackedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND WING UPPER SKIN CRACKED AT STATION XRS105.000, STRINGER 14.REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND, AFTER DAMAGE REMOVED. SDR IXXA07SMN029SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING-EXTERNAL UPPER SKIN CRACKED AT STATION XRS74.000 STRINGER 11. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVESDR UPS07M49239Doubler · crackedINSPECTION TYPE:C LEFT WING FIXED L/E COMPT CRACKED FOUND ON UPPER DOUBLER PANEL AS MARKED (REFUEL ACCESS 519CB COMPT AREA). LEFT WING FIXED L/E COMPT UPPER DOUBLER FASTENER REMOVED PER SRM 51-31-01 VOL 2 R.38. REPAIR DOUBLER FILLERS & ANGLES FABRICATED & HOSDR ABXA070021Skin · corrodedRIGHT WING UPPER SKIN BULGED AT REMOVEABLE TRAILING EDGE AND PANEL NR 1252. REPAIRED RIGHT WING UPPER SKIN BULGE ON TRAILING EDGE PANEL IAW DC9 SRM 51-10-4.SDR AMW107001001Skin Panel · crackedDURING THE INSPECTION PHASE OF A NR 4 DETAILED INSPECTION, A 2.5 INCH SPANWISE CRACK WAS FOUND ON THE UNDERSIDE OF THE RT WING AT WING STATION B.L. 29.06. NO SB OR AD'S APPLY TO THIS AREA OF THE AIRCRAFT. UPON FURTHER INSPECTION OF THIS AIRCRAFT, A REPAIR WASSDR 07FDEA00074Skin · crackedRIGHT WING TELESCOPIC DUCT CUTOUT FOUND CRACKED. CRACK AREA ON THE RIGHT WING TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57-10-00 FIGURE 42 VOLUME I AND FEDEX EA NR 1-5710-107767, TITLE: WINGS, RIGHT WING ANTI-ICING TELESCOPIC DUCT DOOR CUTOUT REPAIR. REPAIRSDR WRLA2007011Skin · corrodedDURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND LEFT WING UPPER SURFACE BULGE CORRODED UNDER FIXED PANEL NEAR XORS=1042 REAR SPAR. REPAIR THE DAMAGE AREA PER EGAT E1 NT W2007A57B-060 REV.00 AND APPROVE DOCUMENT BOEING MESSAGE NR 1-276023171-2. CONDITION CHECK N
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