JASC 5720

Service difficulty reports · 13,638

Reports filed under 5720 · Wing Miscellaneous Structure, newest first.

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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 = '5720'
  ORDER BY difficulty_date DESC"

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SDR MTNA100802Structure · corrodedFOUND CORROSION INSIDE LEFT FUEL FEEDER TANK BETWEEN RIBS 4 AND 5. THERE WERE SEVERAL AREAS FROM STIFFENER 1 TO STIFFENER 10. CORROSION REMOVED AS PER SRM ATR72 CH 51-21-42. APPLIED TREATMENT TO NEUTRALIZE ANY HEDDIN CORROSION. PERFORMED FINAL BLEND OUT IAOct 6, 2008 · N810FX · Aerosp ATR72202SDR 08FDEA04228Splice · corrodedRIGHT WING INBD T/E AT THE MAIN LANDING SUPPORT LOWER FWD AUX SPLICE HAS CORROSION. REPLACED 2 SPLICES P/N ARC 0634-2 & P/N ARB 0636-1 IAW DWG ARC 0621.Oct 6, 2008 · N550FE · Doug MD1010FSDR UPS08853618Structure · misrepairedINSPECTION TYPE:SV RT WING LOWER L/E DOUBLER REPAIR NEEDS VALIDATION FOR REPAIR AT STA XFS 747.600. DOES NOT MEET CRITERIA IN APPENDIX H STEP 1 SURVEY SEQ 89 4-W4-17. PREVIOUSLY REPAIRED IAW DC8 SRM 57-2-1 FIG 2H PG 15.Oct 5, 2008 · N894UP · Doug DC873FSDR UPS08853565Structure · misrepairedINSPECTION TYPE:SV, L/E STATION XFS 88 DOUBLER DOES NOT MEET CRITERIA FOR APPENDIX H. REPAIR PREVIOUSLY ACCOMPLISHED PER DC8 73F SRM 57-2-1 FIG 2H CLASS B.Oct 3, 2008 · N894UP · Doug DC873FSDR UPS08853727Stiffener · crackedINSPECTION TYPE:SV EVALUATE EFN 70220061052 ORIGINAL NR 902713 CRACKED STIFFENER IN 2ND L/E LEADING EDGE ACCESS HOLE OUTBOARD OF NR 3 PYLON. REPAIRED BY 57-02-00.Oct 2, 2008 · N702UP · Doug DC871FSDR UPS08853726Structure · damagedINSPECTION TYPE:SV EVALUATE EFN 7022004 ORIGINAL NRC 750568. REPAIRED PER SRM 57-02-00.Oct 2, 2008 · N702UP · Doug DC871FSDR 08FDEA04143Channel · crackedLEFT WING UPPER L/E PANEL 517 CT HAS A CRACKED CHANNEL. REMOVED CRACKED CHANNEL IAW DC/MD-10 SRM 51-35-01; VOL II. MATERIAL ID 7075-0, 0.063; PO 629531.1 & FABRICATED IAW DAC DWG ARB 2407; REV G. ALODINED & PRIMED IAW DC/MD-10 SRM 51-21-01; VOL II; PG 21 Sep 30, 2008 · N550FE · Doug MD1010FSDR UPS08653429Web · crackedINSPECTION TYPE:C RT WING FRONT SPAR AREA LES 680 D-NOSE WEB FOUND CRACK (CRACK LENGTH .5 INCH). D-NOSE WEB REPAIRED AS PER SRM 57-41-13-2R3 FIG 201 REPAIR 3.Sep 29, 2008 · N330UP · Boeing 76734AFSDR 08FDEA04068Retainer · corrodedLT WING SPAR UNDERWING PANEL SEAL RETAINER HAS CORROSION O/B OF APU FIRE BOTTLE AT WS 182 TO 200. FABRICATED SEAL RETAINER REF DWR 65-21656. TREATED AND PRIMED REF SRM 51-10-2 PG 1- 9. INSTALLED SEAL RETAINER REF 51-30-2 P1-3. THIS IS A CLASSIFIED A MINSep 26, 2008 · N488FE · Boeing 727227SDR 08FDEA04066Retainer · corrodedLT WING REAR SPAR LWR CHORD APPROX STA 182, SEAL RETAINER CORRODED REMOVED SEAL RETAINER REF SRM 51-30-2. FABRICATED NEW RETAINER REF DWG 65-21656. TREATED AND PRIMED REF SRM 51-10-2 PGS 1-3. INSTALLED SEAL RETAINER REF SRM 51-30-2 PG'S 1-3. THIS IS CLASSISep 26, 2008 · N488FE · Boeing 727227SDR 08FDEA04062Skin · chafedRIGHT WING LEADING EDGE TELESCOPIC DUCT CUT OUT INBOARD DOUBLER FOUND CHAFED. DOUBLER REPAIRED AS PER SRM 57-10-00. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 26, 2008 · N613FE · Doug MD11FSDR UPS08M53410Stiffener · brokenINSPECTION TYPE:1C BROKEN STIFFENING RIB INSIDE RT WING I/B LEADING EDGE PANEL 616EB, ON UPPPER PANEL PART NUMBER ARB2386-402PFD PANEL 616ET. REMOVED 2 EACH STIFFENER RIBS, FABRICATED, AND INSTALLED STIFFENER RIBS IAW DWG ARB2440, MD-11 SRM 51-21-01, 51-41-01Sep 19, 2008 · N287UP · Doug MD11FSDR 08FDEA03933Channel · crackedRT WING, I/B AILERON O/B L/E SEAL MOUNT BRACKET/UNDERWING PANEL MOUNT BRACKET CRACKED 10 INCH I/B FROM O/B END OF AILERON REMOVED SEAL MOUNT BRACKET AND ATTACH ANGLE, FABRICATED NEW "U" CHANNEL. FABRICATED NEW ATTACH ANGLE, HEAT TREATED TO T4 CONDITION. U CHSep 18, 2008 · N488FE · Boeing 727227SDR UPS08853658Flange · crackedINSPECTION TYPE:SV RT WING LEADING EDGE AUX TANK AFT INBOARD SIDE VENT TUBE FLANGE CRACKED. REMOVED, REPAIRED, REINSTALLED FLANGE IAW DCI MM 20-12-00-2.Sep 17, 2008 · N894UP · Doug DC873FSDR UPS08M53377Stiffener · brokenINSPECTION TYPE:1C BROKEN STIFFENING RIB ON BOTTOM OF LT WING UPPER I/B LEADING EDGE PANEL 516ET. REMOVED AND REPLACED 2 EACH Z-STIFFENERS IAW SRM 51-33-01, 51-21-1, 51-35-1.Sep 17, 2008 · N287UP · Doug MD11FSDR UPS08M53403Strap · crackedINSPECTION TYPE:2C LT WING SPLICE STRAP AT L/E WING STA 683 IS CRACKED. REMOVED, FABRICATED, AND INSTALLED SPLICE STRAP IAW DWG ARB3954 MD-11 SRM 51-35-01, 51-31-01, 51-33-01.Sep 15, 2008 · N282UP · Doug MD11FSDR UPS08653344Support Bracket · crackedINSPECTION TYPE:C LT WING NR 6 SLAT LWR LIP NR 5, 7 & 8 SUPPORT BRACKET CRACK (CRACK LENGTH .5 INCH). THREE EA SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Sep 14, 2008 · N332UP · Boeing 76734AFSDR HNAA2009021200050Panel · corrodedDURING 'C' CHECK INSPECTIONS, THE LT WING STRESS PANEL, 522AT, WAS FOUND TO HAVE CORROSION IN SOME OF THE SCREW COUNTER SINKS THAT WAS BEYOND ACCEPTABLE LIMITS. THE PANEL WAS REPLACED. THIS IS AN AMENDMENT TO HNAA2009010900383 TO CORRECT ITEM 1C, REGISTRATIOSep 13, 2008 · N982HA · Dhav DHC8102SDR 08FDEA03852Support Beam · crackedLWR SIDE OF I/B SPOILER FITTING HAS MISSING AND LOOSE FASTENERS EVALUATED AND FOUND CRACK ON SPOILER SUPPORT BEAM. REPAIRED I/B SPOILER SUPPORT BEAM CRACK AT SPOILER FITTING AREA IAW FEDEX DRAWING NR: SR27-57-038 REV "C".Sep 12, 2008 · N492FE · Boeing 727227SDR UPS08M53378Strap · crackedINSPECTION TYPE:2C LT WING SPLICE STRAP AT LEADING EDGE WING STA 562 IS CRACKED WHERE MARKED. REMOVED AND REPLACED SPLICE STRAP IAW SRM 51-31-1, 51-21-1, 51-33-1.Sep 9, 2008 · N282UP · Doug MD11FSDR 08FDEA03767Attach Bracket · crackedLEFT WING FUEL TANK FWD MOST FUEL LINE CLAMP ATTACH BEACKET IS CRACKED AT XORS 683; ACCESS 536 AB. REMOVED & INSTALLED THE INTERCOSTAL IN REF TO SRM 51-31-01; VOL II. FABRICATED INTERCOSTAL P/N ARL 0500-21IN REF TO DWG ARL 0500, REV "BU". ALODINED IN Sep 8, 2008 · N550FE · Doug MD1010FSDR 08FDEA03761Channel · crackedRIGHT WING OUTBD UPPER FUEL TANK ACCESS OPENING 634 CT HAS FUEL LINE CLAMP ATTACH BRACKET IS CRACKED XORS 538; FWD AND OUTBD OF ACCESS OPENING. REMOVED & INSTALLED THE INTERCOSTAL IN REF TO SRM 51-31-01; VOL II. FABRICATED INTERCOSTAL P/N ARL 0501-44 IN REFSep 8, 2008 · N550FE · Doug MD1010FSDR 2009FA0000105Attach Fitting · corrodedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE LWR RT WING AFT ATTACH FITTING PN 5011024-2 FAILED NDT INSPECTION. REPLACED WING FITTING.Sep 2, 2008 · N425JH · Cessna 425SDR 08FDEA03687Stiffener · crackedRIGHT WING INBOARD UPPER L/E PANEL 617 CT HAS 2 CRACKED CHANNELS. REMOVED 2 EA STIFFENERS IAW SRM 51-35-01 VOL II. FABRICARED IAW DWG ARB 2407; REV " G " (-13 & -9). ALODINED & PRIMED IAW SRM 51-21-01 VOL II PGS 21-24 AND INSTALLED IAW SRM 51-35-01 VOL IISep 1, 2008 · N550FE · Doug MD1010FSDR 08FDEA03686Angle · brokenLEFT WING INBOARD UPPER L/E PANEL 516 DT HAS A BROKEN ANGLE. ANGLE FABRICATED IAW DWG ARB 1261. HEAT TREATED IAW TPS 1003, REV "A". PRIMED IAW SRM 51-21-01; VOL II. INSTALLED IAW SRM 51-31-01 VOL II.Sep 1, 2008 · N550FE · Doug MD1010FSDR 08FDEA03685Channel · crackedLEFT WING INBOARD UPPER L/E PANEL 517 CT HAS A CRACKED CHANNEL. REMOVED STIFFENER IAW SRM 51-35-01 VOL II. FABRICATED STIFFENER IAW DWG ARB 2407; REV "G". ALODINED & PRIMED IAW SRM 51-21-01 VOL II PGS 21-24. INSTALLED IAW SRM 51-35-01 VOL II.Sep 1, 2008 · N550FE · Doug MD1010FSDR UPS08M53312Structure · crackedINSPECTION TYPE:1C RIGHT WING TELESCOPING DUCT CUTOUT UPPER I/B CORNER AND O/B CORNER CRACKED. REMOVED CRACK, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 43.Aug 31, 2008 · N250UP · Doug MD11FSDR UPS08M53269Stiffener · crackedINSPECTION TYPE:1C LEFT WING L/E STIFFENER XFS 587 CRACKED. REMOVED, FABRICATED, AND INSTALLED STIFFENER IAW DWG ARB2918, MD-11 SRM 51-35-01.Aug 29, 2008 · N250UP · Doug MD11FSDR EIA2008030Structure · crackedLTW L/E DEVICE FAIRING AFT WEB ADJACENT LOWER CHORD AND UPPER CHORD. CRACK AT ILES 1127. REPAIRED PER 51-40-04 AND 57-20-03 SRMAug 28, 2008 · N485EV · Boeing 747212BSDR EIA2008033Structure · crackedRT WING L/E DEVICE FAIRING AFT WEB ADJACENT UPPER CHORD AND LOWER CHORD CRACK AT 1 LES 1127. REPLACED PER SRM 57-20-03.Aug 28, 2008 · N485EV · Boeing 747212BSDR 08FDEA03608Support Bracket · corrodedLT WING, REAR SPAR SURFACE 1, RIB 4, HYD TUBE SUPPORT BRACKET WITH INNER- GRANULAR CORROSION (DELAMINATED). REMOVED THE CORRODED TUBE SUPPORT BRACKET. FABRICATED A NEW BRACKET PER AIRCRAFT DRAWING 25 A935-40675. INSTALLED THE NEW BRACKET AND HYD TUBES PER Aug 28, 2008 · N455FE · Airbus A310222SDR 08FDEA03607Support Bracket · corrodedRT WING, REAR SPAR RIB 1-RIB-4, HYD TUBE SUPPORT BRACKET WITH INNER-GRANULAR CORROSION. REMOVED THE CORRODED TUBE SUPPORT BRACKET. FABRICATED A NEW BRACKET PER AIRCRAFT DRAWING 25 A935-40675. INSTALLED THE NEW BRACKET AND HYD TUBES PER AMM 20-21-12-0 AND AMAug 28, 2008 · N455FE · Airbus A310222SDR U2R2008F00003Support Angle · crackedDURING C-CHECK INSP, FOUND LT WING X RS 71, 5-52 NR 2 MAIN FUEL TANK INTERIOR LOWER SUPPORT ANGLE CRACKED. (K)Aug 25, 2008 · N872SJ · Doug DC871FSDR QXEA200800953Intercostal · crackedPDX - C-CHECK, LT WING VERTICAL INTERCOSTAL, LOCATED UNDER OUTBOARD SPOILER HAS A CRACKED LIGHTENING HOLE. REMOVED INTERCOSTAL AT OUTBOARD SPOILER, MATCH DRILLED NEW FROM STOCK INTERCOSTAL AT YW 357.30. PAINTED AND INSTALLED NEW FROM STOCK INTERCOSTAL IAW 8-Aug 20, 2008 · N410QX · Bombdr DHC8402SDR 08FDEA03515Shroud · corrodedFOUND CORROSION ON TOP SKIN OF OUTER SHROUD BOX, RIB 25-28 RT OUT OF LIMIT. REPAIR PERFORMED BY CUT AWAY THE AFFECTED RIBS, REWORK OF CORROSION AND INSTALLING MANUFACTURED ANGLES TO THE CUT RIB POSITIONS IAW RAS/BAE/1007548/2008 ISS, APPROVED BY EA 6-5751-120Aug 20, 2008 · N743FD · Airbus A300B4622RSDR 08FDEA03513Shroud · corrodedFOUND CORROSION ON TOP SKIN OF OUTER SHROUD BOX, RIB 25-28 LT OUT OF LIMIT. REPAIR PERFORMED BY CUT AWAY THE AFFECTED RIBS, REWORK OF CORROSION AND INSTALLING MANUFATURED ANGLES TO THE CUT RIB POSITIONS IAW RAS/BAE/1007548/2008 ISS A, APPROVED BY EA 6-5751-12Aug 20, 2008 · N743FD · Airbus A300B4622RSDR 08FDEA03510Structure · corrodedFOUND CORROSION UNDER STATIC DISCHARGER ON RT WING TIP. REPAIR PERFORMED BY CORROSION REWORK AND INSTALLING AN EXTERNAL PATCH IAW RAS/FOK/160/2008 ISS A, APPROVED BY EA 6-5730-120085.Aug 20, 2008 · N743FD · Airbus A300B4622RSDR 08FDEA03436Shroud · dentedFOUND DENT ON LEADING EDGE SKIN, RIB 29 RT REPAIR PERFORMED BY NDT FOR CRACK FREE CONDITION AND LET THE DENT AS IT IS IAW RAS/BAE/1007864/2008, APPROVED EA 6-5741-123064.Aug 15, 2008 · N744FD · Airbus A300B4622RSDR UPS08553286Frame · chafedINSPECTION TYPE:C3 RT WING FAIRING 672HB FWD LWR EDGE STIFFENER IS CHAFED AT LOWER O/B SIDE. REMOVED AND REPLACED FRAME PER SRM 51-40-02.Aug 14, 2008 · N416UP · Boeing 75724APFSDR 08FDEA03407Angle · crackedLT WING ROOT TE UPPER PNL IB OF NR 7 SPOILER HAS FRETTED/CRACKED IB SUPPORT ANGLE BS 950A, WBL 70. REPLACED SUPPORT ANGLES REF SRM 51-30-02 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.Aug 13, 2008 · N211FE · Boeing 7272S2FSDR 08FDEA03406Angle · crackedLEFT WING OB LE CAVITY, LE UPPER SKIN FORMED SUPPORT ANGLE CRACKED AT AFT END ABOVE TAI DUCT AT INBD END OF NR 4 SLAT WELL. REMOVED INTERCOSTAL AND DAMAGED SUPPORT ANGLE, FABRICATED NEW SUPPORT ANGLE, HEAT TREAT "T-3". TREAT AND PRIMED SUPPORT ANGLE, INSTALLAug 13, 2008 · N211FE · Boeing 7272S2FSDR 08FDEA03401Support Angle · crackedRIGHT WING OB LE CAVITY, LE UPPER SKIN FORMED SUPPORT ANGLE CRACKED AT AFT END ABOVE TAI DUCT AT INBD END OF NR 5 SLAT WELL. REMOVED INTERCOSTAL AND SUPPORT ANGLE AT SLAT STA 260. FABRICATED NEW SUPPORT ANGLE. VERIFIED MATERIAL 2024 T-3, FAB'D WITH 2024-0, Aug 13, 2008 · N211FE · Boeing 7272S2FSDR CNMA20090028Support · crackedLT OTBD FLAP, INBD HINGE STRUCTURE UNDER PANEL 535JL, SUPPORT CRACKED. REPLACED SUPPORTS CRACKED UNDER PANEL 535JL IAW SRM 51-35-01 VOL II REV 93.Aug 8, 2008 · N108AX · Doug DC1030SDR 2009FA0000106Fitting · damagedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE LOWER RT WING AFT ATTACH FITTING PN 5011024-2 INBD BOLT HOLE ELONGATED AND MARRED. REPLACED WING FITTING.Aug 4, 2008 · N522WD · Cessna 425SDR UPS08853149Fitting · crackedINSPECTION TYPE:C1 NR 4 ALT Z-FITTING CRACKED. REMOVED CRACKED FITTING IAW SRM 51-01-20D. FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 3644046, SRM 51-01-24, AND 51-01-20D.Aug 2, 2008 · N715UP · Doug DC871FSDR UPS08853131Fitting · crackedINSPECTION TYPE:C1 NR 1 ALT Z-FITTING IS CRACKED. REMOVED Z-FITTING IAW SRM 51-01-20D. FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 364046, SRM 51-01-20D.Jul 31, 2008 · N715UP · Doug DC871FSDR UPS08M53095Support Angle · crackedINSPECTION TYPE:2C, LT WING FIXED L/E ANGLE SUPPORT AT STA XORS 346 FOUND CRACKED. REMOVED, FABRICATED AND INSTALLED ANGLE IAW MD-11 SRM 51-33-01 DWG ARB2918 AND SRM 51-21-01.Jul 31, 2008 · N281UP · Doug MD11FSDR USAA920081424Anchor Fitting · corrodedSAL-C6- MAJOR REPAIR - CORROSION ON ANCHORAGE FITTING LT WING. REPAIRED ANCHORAGE FITTING LT WING IAW US AIRWAYS EA 132038. (A)Jul 26, 2008 · N627AW · Airbus A320231SDR USAA920081422Anchor Fitting · corrodedSAL-C6- MAJOR REPAIR- CORROSION ON ANCHORAGE FITTING RT WING. REPAIRED ANCHORAGE FITTING RT WING IAW US AIRWAYS EA 132038. (A)Jul 26, 2008 · N627AW · Airbus A320231SDR 08FDEA02998Duct · crackedRT WING INBD FIXED L/E INLET SCOOP IS CRACKED ON THE FWD END APPROX 2 INCHES LONG. REMOVED PANEL IAW SRM 51-40-21, PG 7; SECT 5. WELDED CRACK IN THE RIGHT WING L/E INLET SCOOP IAW DWG A21040014. INSTALLED IAW SRM 51-40-21; PG 7.Jul 21, 2008 · N728FD · Airbus A300B4622R
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