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"

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SDR DHL2005741553Skin · dentedDENT ON RT WING L/E AT WING STA 131-198. DENT FOUND TO BE OUT OF LIMITS IAW 727 SRM 57-20-1 FIG 1. REMOVED AND REPLACED RT WING FIXED L/E ASSY AT L/E STA 130 TO L/E STA 349 P/N 65-16209-6 PO 5096106 IAW 727 SRM 51-30-2 PER CUSTOMER REQUEST.Apr 18, 2005 · N741DH · Boeing 7272Q9SDR DHL2005741500Skin · crackedRT WING T/E SKIN CRACKED AT NR 11 SPOILER 32 HINGE CUTOUT. STOP DRILLED CRACK RT WING T/E SKIN AT NR 11 SPOILER IAW B727 SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM MATERIAL USE 7075T6 .071 PO NR 900573 IAW B727 SRM 57-30-4 FIG 11. DIMENSIONS 6 INCHES BY 4 Apr 18, 2005 · N741DH · Boeing 7272Q9SDR A6WA200540160Skin · chafedRIGHT LOWER WING PLANK UNDER PANEL 650HB IS CHAFED IN TWO AREAS. INBOARD AREA CHAFED .050 INCH WIDE 6 INCHES LONG APPROX .002 INCH DEEP. OUTBOARD AREA CHAFED .050 INCH WIDE 4 INCHES LONG APPROX .001 INCH DEEP. FORWARD CENTER IS AT STARTING STAGES OF CORROSIApr 18, 2005 · N417AW · Cndair CL6002B19SDR A6WA200540211Panel · damagedATTACHMENT HOLE ENLARGED ON OUTBOARD SIDE OF PANEL 684BB, DAMAGED WHILE REMOVING SCREW HOLE DIA WAS .193 NOW .265. INSTALLED FABRICATED 100 COUNTERSINK FREEZE PLUG IAW BRAS EO NR 601-57-6666. (M)Apr 17, 2005 · N460AW · Cndair CL6002B19SDR DHL2005741550Skin · crackedLT WING L/E CRACKED AT NR 4 SLAT O/B TRACK CUTOUT. STOP DRILLED CRACK AT CUTOUT. FABRICATED REPAIR PARTS PLATE 301 1/2 HARD, 0.020 (6.8 X 5.2 INCH) PO 509613, BACKING STRAPS 2 EA 2024-T3, 0.063 (.80 X 3.0 INCH) PO 9001978, FILLER 301 1/2 HARD, .032 (2.2 X 6.Apr 14, 2005 · N741DH · Boeing 7272Q9SDR ASOA05333Skin Panel · crackedDURING A C-CHECK, THE LOWER WING PLANK AT WS 148.019 LT/RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANK AT WS 148.019 LT/RT IAW EO. (K)Apr 13, 2005 · N821AS · Cndair CL6002B19SDR QXEA200500790Skin · chafedYYC - RIGHT AILERON UPPER SKIN LEADING EDGE HAS CHAFE MARKS. REPAIRED IAW CRJ700 SRM 57-52-32-400-808-A01, 57-52-32-400-809-A01, 57-52-32-400-810-A01 AND SRM 57-52-32-400-811-A01.Apr 12, 2005 · N614QX · Cndair CL6002C10SDR QXEA200500769Skin · chafedYYC-LEFT WING BOTTOM SKIN HAS CHAFE MARK UNDER FAIRING 586AB. REPAIRED IAW CRJ700 SRM 57-00-01-101-001-A01, 51-12-00-04-001-A01, AND 51-25-16-001-001-A01.Apr 12, 2005 · N614QX · Cndair CL6002C10SDR 2005FA0000600Skin · corrodedDURING SCHEDULED INSPECTION FOUND SEVERAL SMALL SPOTS OF CORROSION ON BOTH LEFT AND RIGHT LOWER WING SKINS. PN OF THESE WING SKINS ARE: 67221463, 4 , 67221663,4 AND 67221723. SOME OF THESE AREAS EXCEEDED .007 INCH DEPTH. CONTACTED MFG ENGINEERING FOR REPAIR DIApr 12, 2005 · N906QS · Cessna 750SDR A6WA200540146Skin Panel · corrodedLT LOWER WING PLANK IS CORRODED UNDER PANEL 550FB, INBOARD SIDE 3 INCH LONG BY .100 WIDE BY .002 INCH DEEP, FORWARD SIDE .200 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP. S/D - REPAIRED LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT FOR PANEL 550 FB IAWApr 9, 2005 · N417AW · Cndair CL6002B19SDR A6WA200540145Skin Panel · corrodedLEFT LOWER WING PLANK IS CORRODED UNDER PANEL 550HB AT FORWARD CENTER EDGE .600 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP, INBOARD EDGE 4 INCHES LONG BY .050 INCH WIDE BY .003 INCH DEEP, OUTBOARD SIDE 4.5 INCH LONG BY .025 INCH WIDE BY .003 INCH DEEP. S/DApr 9, 2005 · N417AW · Cndair CL6002B19SDR A6WA200540151Skin · corrodedLEFT LOWER WING PLANK IS CORRODED UNDER PANEL 550AB, OUTBOARD EDGE 1 INCH LONG BY .100 WIDE BY .002 DEEP. (M)Apr 9, 2005 · N417AW · Cndair CL6002B19SDR A6WA200540149Skin · corrodedLEFT LOWER WING PLANK IS CORRODED UNDER PANEL 660CB, AFT INBOARD EDGE .400 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP. (M)Apr 9, 2005 · N417AW · Cndair CL6002B19SDR A6WA200540152Skin · corrodedLEFT LOWER WING PLANK IS CORRODED UNDER PANEL 540BB, FORWARD INBOARD EDGE 4 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP, AFT EDGE .050 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP. (M)Apr 9, 2005 · N417AW · Cndair CL6002B19SDR A6WA200540153Skin · corrodedLEFT LOWER WING PLANK IS CORRODED AROUND ENTIRE CIRCUMFERENCE UNDER PANEL 510AB, .100 INCH S BY .002 INCH DEEP. (M)Apr 9, 2005 · N417AW · Cndair CL6002B19SDR MWEA050030Skin · crackedRIGHT WING LEADING EDGE SKIN CRACKED AT STATION X15 = 136.421 AT SLAT TRACK. INSTALLED DOUBLER AND TRIPLER.Apr 7, 2005 · N808ME · Doug DC982SDR 05FDEA00868Skin · damagedWHILE WORKING EO 6-5710-7-5004 PT 4, RT WING FOR LANDING ASSY FOR PANEL 675CB, 2 EA HOLES NOTED ARE LARGER THAN DRAWING SIZE. THIS IS AN INCOMING CONDITION. HOLE NR 10 .390", EDGE MARGIN RIB .610", PLANK .760", NR 17 .390", EDGE MARGIN RIB .570", PLANK .840"Apr 6, 2005 · N402FE · Airbus A310SDR DHL2005783519Skin · dentedRT WING INBD AILERON UPPER SKIN IS DENTED, WING STA 436. CUT OUT DAMAGED AREA DIM 3" BY 1 1/4" IAW B727 SRM 57-50-5 FIG 2. FABRICATED DOUBLER FROM 2024T3 .032 PO NR 9002034 DIM. 5 1/8" BY 6 1/4" IAW B727 SRM 57-50-5 FIG 2. TREATED AND PRIMED IAW B727 SRM 51Apr 4, 2005 · N783DH · Boeing 727227SDR ASOA05279Skin · crackedDURING A C-CHECK IN MCN, THE LOWER WING PLANK AT WS 148.019 LEFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANK AT WS 148.019 LEFT IAW ASA EO 600-57-0134A. (M)Apr 1, 2005 · N820AS · Cndair CL6002B19SDR UPS05844364Skin · damagedINSPECTION TYPE: C1, LT WING LEADING EDGE UPPER SURFACE 10 FT O/B OF NR 1 ENG STUB WING HAS FASTENER BULGING & PULLED THROUGHT SKIN. INSTALLED DOUBLER AND CONICAL WASHERS IAW SRM 51-1-26 & 57-2-1.Mar 30, 2005 · N810UP · Doug DC873FSDR 05FDEA00669Skin Panel · crackedLEFT WING, LEADING EDGE PANEL LAND, JUST FWD OF FLAP TRACK NR 5 PANEL LAND AND REPAIR CRACKED (MARKED). REMOVED LANDING PLATE IAW A310 SRM 51-40-2, FABBED NEW PLATE IAW DRAWING A572443982, TREATED, PRIMED AND TOPCOATED IAW A310 SRM 51-75-10. REINSTALLED LANDMar 28, 2005 · N419FE · Airbus A310222SDR QXEA200500558Panel · corrodedYYC - RIGHT HAND WING FUEL LID PANEL 641BB HAS FRETTING CORROSION. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-57-12-002, ISSUE 1.Mar 26, 2005 · N612QX · Cndair CL6002C10SDR QXEA200500559Panel · corrodedYYC - RIGHTHAND WING FUEL LID REBATE PANEL 641BB HAS MINOR FRETTING CORROSION. REPAIRED IAW CRJ700 SRM 51-21-16-001-001-A01 AND TASK 51-80-00-760-802-A01.Mar 26, 2005 · N612QX · Cndair CL6002C10SDR DHL2005740006Skin Panel · delaminatedRT WING LOWER TE PANEL AT WING STA 190 WBL 90 IS DELAMINATED ON UPPER SURFACE, BELOW APU EXHAUST DUCT. REMOVED RT WING LOWER TE PANEL AT WING STA 190 RBL 90 IAW B727 SRM 51-30-2. CUT OUT DELAMINATED AREA OF UPPER SURFACE APPROX 6" BY 8". REMOVED INSERTS ANMar 25, 2005 · N740DH · Boeing 7272Q9SDR DHL2005805575Seal · crackedRT WING T/E UPPER SKIN STEEL SEAL CRACKED XRS 9.000 - XRS 15.000. REMOVED CRACKED SEAL FITTING IAW SRM 57-1-0 PAGE 1, SRM 51-1-21 PAGE 1. FABRICATED NEW SEAL FITTING (STEEL SHEET 301CRES 0.500 HARD 0.012) IAW FAA FORM 8110-3 DATE 03-23-05 EO NR AST050227 DATMar 25, 2005 · N805DH · Doug DC873FSDR 05FDEA00640Skin · damagedPANEL LAND AT 550 GB HAS 5 EA ELONGATED HOLES. REPAIRED 3 EA HOLES IAW A310-200 SRM 51-40-44 FIG 1. COMPLIED WITH EA 6-5710-87184 BY INSTALLING 1 EA REPAIR BUSHING FOR REMAINING HOLE.Mar 25, 2005 · N401FE · Airbus A310203SDR 05FDEA00639Skin · damagedPANEL LAND AT 550 HB HAS 4 EA ELONGATED HOLES. REPAIRED 1 EA HOLE IAW A310-200 51-40-44 FIG 1. COMPLIED WITH EA 6-5710-87184 BY INSTALLING 3 EA REPAIR BUSHINGS FOR REMAINING 3 HOLES.Mar 25, 2005 · N401FE · Airbus A310203SDR 05FDEA00638Skin · damagedPANEL LAND AT 650GB HAS 12 EA ELONGATED HOLES. REPAIRED 8 EA HOLES IAW A310-200 SRM 51-40-44 FIG 1. COMPLIED WITH EA 6-5710-87184 BY INSTALLING 4 EA REPAIR BUSHINGS FOR REMAINING 4 HOLES.Mar 25, 2005 · N401FE · Airbus A310203SDR 05FDEA00637Skin · damagedPANEL LAND AT 650HB HAS 9 EA ELONGATED HOLES. REPAIRED 5 EA HOLES IAW A310-200 SRM 51-40-44 FIG 1. COMPLIED WITH EA 6-5710-87184 BY INSTALLING 4 EA REPAIR BUSHINGS FOR REMAINING 4 HOLES.Mar 25, 2005 · N401FE · Airbus A310203SDR 05FDEA00636Skin · damagedPANEL LAND AT 650MB HAS 8 EA ELONGATED HOLES. REPAIRED 5 HOLES IAW A310-200 SRM 51-40-44 FIG 1, AND COMPLIED WITH EA 6-5710-87184 BY INSTALLING 3 EA REPAIR BUSHINGS FOR REMAINING 3 HOLES.Mar 25, 2005 · N401FE · Airbus A310203SDR DHL2005740562Skin · crackedL/WING T/E UPPER SURFACE CRACKED AT NR 4 SPOILER HINGE CUTOUT (NR3). REMOVED FASTENER AT L/WING T/E UPPER AT NR 4 SPOILER HINGE CUTOUT NR 3 IAW B727 SRM 51-30-2, STOP DRILL CRACK .250 TERMINATED AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIRMar 24, 2005 · N740DH · Boeing 7272Q9SDR QXEA200500538Skin · chafedPDX - RIGHT WING LOWER SKIN IS CHAFED BY WING TO FUSELAGE FAIRING STRUCTURE, AFT OF LEADING EDGE SPAR. REPAIRED IAW SRM 57-10-30 AND SRM 51-21-10.Mar 21, 2005 · N416QX · Bombdr DHC8401SDR DHL2005805636Skin · damagedLT OUTER WING INBD L/E HOLE ELONGATED AT STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-16-05 DWG X83-R02 REV IR DATE 02-23-05. REMOVED FASTENERS FROM AREA (REPAIRED) IAW SRM 51-1-21 PAGE 1, SRM 51-3-0 PAGE 1, SRM 51-1-20DMar 21, 2005 · N805DH · Doug DC873FSDR DHL2005805677Skin · damagedRT WING OUTBD L/E UPPER SKIN HOLES ELONGATED STA XFS 560.000.(MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-16-05 DWG X83-R01 REV IR DATED 02-21-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW DWG X83-R01. PERFOMar 21, 2005 · N805DH · Doug DC873FSDR DHL2005805672Doubler · damagedRT WING CTR L/E OUTBOARD SLOT VANE EXISTING DOUBLER EDGE DISTANCE AND FASTENERS HOLES SPACE NOT ALLOWABLE, STA XOLDO 67.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-16-05 DWG X83-R03 REV IR DATED 02-24-05. REMOVED FASTENERS IAW SRMMar 21, 2005 · N805DH · Doug DC873FSDR AWXA200500374Skin · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A .375 INCH CRACK WAS FOUND IN PREVIOUS REPAIR OF RT WING SKIN AT INBOARD MID FLAP LEADING EDGE CUTOUT FOR FORE FLAP CONTROL ROD RS 176.0. MAINTENANCE REMOVED PREVIOUS REPAIR OF RT WING SKIN AT RS 176.0; FABRICATED A NEWMar 21, 2005 · N305AW · Boeing 7373G7SDR UPS05844300Skin · crackedINSPECTION TYPE: C2, RT WING UPPER SURFACE CRACKED 2 INCH LONG AROUND FASTENER HEAD AT STA XRS 76 STRINGER 16. REPAIRED RT WING UPPER SURFACE IAW DC-8 SRM 57-2-1 FIG 10.Mar 18, 2005 · N819UP · Doug DC873FSDR UPS05844292Skin · crackedINSPECTION TYPE:C2 LEFT WING L/E LWR DRAIN HOLE HAS 2 INCH CRACK AT STA XFS 585. REMOVED DAMAGE, FABRICATED DOUBLER & FILLER, AND INSTALLED IAW DC-8 SRM 57-3-0, 57-2-0 FIG 6, 51-1-21, AND 51-1-20D.Mar 18, 2005 · N819UP · Doug DC873FSDR UPS05844288Skin · corrodedINSPECTION TYPE: C2, LT LWR WING L/E HAS HEAVY CORROSION AT STA XFS 566. REMOVED CORROSION AND FOUND OUT OF LIMITS PER SRM 57-2-0 FIG 7. CUT OUT DAMAGED AREA AND REPAIRED IAW DC-8 SRM 57-2-1, 57-3-0, & 57-2-1.Mar 18, 2005 · N819UP · Doug DC873FSDR DHL2005782557Skin · crackedL/WING T/E SURFACE CRACKED AT NR 4 SPOILER HINGE CUTOUT (3RD). STOP DRILLED CRACK SIZE .250 IAW B727 SRM 51-10-1. REMOVED NR 4 SPOILER IAW B727 MM 27-61-0. NDT AREA IAW B727 NDTM PART 6 51-00-00 FIG 23 CRACK TERMINATES AT STOP DRILL HOLE, FABRICATE DOUBLER Mar 18, 2005 · N782DH · Boeing 727227SDR 05FDEA00602Skin · crackedLEFT WING T/E BOTTOM SKIN HAS INDICATION OF CRACK ON I/B CORNER SIDE CUTOUT PANEL 581AB AS MARKED. COMPLIED WITH EA 6-5710-86028.Mar 18, 2005 · N446FE · Airbus A310222SDR A6WA200540107Access Panel · corrodedRT LOWER WING PLANK FUEL TANK ACCESS PANEL CUT-OUT BETWEEN SS 50.54 AND WS 66.2 HAS MINOR FRETTING AND FAYING SURFACE LESS THAT .006 INCH DEEP. (K) BLEED MINOR FRETTING ON RT LOWER WING PLANK BETWEEN WS 50-54 AND 66.2 IAW REO. (K)Mar 17, 2005 · N415AW · Cndair CL6002B19SDR A6WA200540106Access Panel · corrodedLT LOWER WING PLANK FUEL TANK ACCESS PANEL CUT-OUT BETWEEN SS 0.00 AND WS 29.42 HAS MINOR FRETTING ON FAYING SURFACE LESS THAN .006 INCH DEEP. C/A PENDING (K)Mar 17, 2005 · N415AW · Cndair CL6002B19SDR 05FDEA00587Panel · crackedRIGHT WING T/E PANEL LANDING FOR ACCESS PANEL 675CB HAS 1.0 INCH CRACK. REMOVED AND REPLACED LANDING PLATE IAW SRM 51-72-10.Mar 17, 2005 · N419FE · Airbus A310222SDR 05FDEA00540Skin · misrepairedCOMPLY WITH AGING 9 - AGING INSPECTION, RT WING - REPAIR ON UPPER SKIN SURFACE BETWEEN TRAILING EDGE AND REAR SPAR AND BETWEEN RIB 2 AND TRACK 3. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED IN ACCORDANCE WITH Mar 15, 2005 · N451FE · Airbus A310222SDR 05FDEA00539Skin · misrepairedCOMPLY WITH AGING 9 - AGING INSPECTION, RT WING - REPAIR ON LWR SKIN SURFACE BETWEEN FRONT SPAR AND MAIN, AND BETWEEN RIB 3 AND RIB 4. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-53-12.Mar 15, 2005 · N451FE · Airbus A310222SDR 05FDEA00530Skin · misrepairedCOMPLY WITH AGING 9 - AGING INSPECTION, LT WING - REPAIRS (2) AT LT WING LWR SURFACE (ALL SPEED AILERON) PLEASE EVALUATE. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-61-12.Mar 15, 2005 · N451FE · Airbus A310222SDR DHL2005782539Skin · dentedDENT ON RT WING L/E ABOVE NR 5 KFLAP (MARKED). CUT OUT DAMAGED AREA DIMENSIONS 1 1/2" BY 1/2" AND FABRICATED REPAIR DOUBLER MATERIAL USE 2024 T3 0.080 PO NR 9002012 DIMENSIONS 5 1/4" BY 5 1/4" IAW B727 SRM=57-30-4 FIG NR 1, PARTS TREATED AND PRIMED IAW B727 SMar 14, 2005 · N782DH · Boeing 727227SDR UPS05444200Panel · crackedRT WING L/E CAVITY AT FSSI 998 L/E MOST FWD D-SECTION ATT PANEL AND UPPER EDGE CHORD FOUND CRACKED, AFT OF NR 20 VC FLAP, CRACK LENGTH 1 INCH. PANELS AND CHORD REPAIRED AS PER SRM 57-20-03 FIG 7.Mar 12, 2005 · N682UP · Boeing 747121SDR AWXA200500447Skin · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON TOP LT WING IN SPAR SKIN AT BS 575, WBL 81.5. MAINTENANCE CUT OUT DAMAGED AREA OF LT WING IN SPAR SKIN AT BS 575, WBL 81.5; FABRICATED A -5 FILLER AND 4 EACH REPAIR PLATES (DOUBLERS); IMar 11, 2005 · N336AW · Boeing 737375
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