JASC 5730

Service difficulty reports · 27,269

Reports filed under 5730 · Wing, Plate/Skin, 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 = '5730'
  ORDER BY difficulty_date DESC"

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SDR 04FDEA00171Skin · crackedLEFT WING LEADING EDGE 2 CRACKS AT RIVETS STA XOS 630 LEADING EDGE PANEL INTERIOR. LT WING LEADING EDGE : STA XOS 630 LEADING EDGE PANEL INTERIOR, 02 EACH CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25, VOL.I.Jan 16, 2004 · N604FE · Doug MD11SDR 04FDEA00170Skin · crackedLEFT WING LEADING EDGE PANEL INTERIOR MANY CRACKS FROM EOS 560 TO 620 BETWEEN SLAT TRACKS 10 AND 11. LT WING LEADING EDGE SKIN PANEL INTERIOR STA XOS 560 TO XOS 620 BETWEEN SLAT TRACK 10 AND 11, CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25, VOL.I.Jan 16, 2004 · N604FE · Doug MD11SDR 04FDEA00169Skin · crackedLEFT WING - LEADING EDGE PANEL INTERIOR HAS SEVERAL CRACKS AT XOS 550 BETWEEN REFUEL PANEL AND OUTBOARD SLAT TRACK. LT WING LEADING EDGE PANEL INTERIOR AT XOS 550 BETWEEN REFUEL PANEL AND OUTBOARD SLAT TRACK , CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25Jan 16, 2004 · N604FE · Doug MD11SDR 04FDEA00168Skin · crackedLEFT WING - ON LEADING EDGE SKIN PANEL INTERIOR FOUND SEVERAL CRACKS STA XOS 510 UNDER REFUEL ACCESS PANEL. LT WING : LEADING EDGE SKIN PANEL STA XOS 510 UNDER REFUEL ACCESS PANEL INTERIOR , CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG. 25, VOL. I.Jan 16, 2004 · N604FE · Doug MD11SDR COMA0460051Skin · corrodedWHILE PERFORMING TASK 002-57-900-60/601 FOUND CORROSION ON THE LOWER RT WING PLANK ACCESS HOLE CUTOUT (FOR PANEL 640BB) ON THE FORWAD AND AFT CHAMFERS. REMOVED THE CORROSION AND APPLIED SURFACE TREATMENT IAW REO 601R-57-21-030 REV C.Jan 15, 2004 · N952CA · Cndair CL6002B19SDR EWG2004F00000Skin · wrinkledIAW REQUIREMENTS OF FAR 145.63, SUBMITS THIS 8010-4. IN THE PROCESS OF PERFORMING A PHASE 2 AND 3 INSPECTION, DIAGONAL WRINKLES WERE DISCOVERED ON THE TOP LT WING PANEL BETWEEN THE AUX AND AFT SPARS IB OF THE NACELLE. AFTER CONTACT WITH AND REVIEW BY MFG ENGJan 14, 2004 · N6845R · Cessna 425SDR 04FDEA00148Skin · dentedDENT ON LT WING FIXED L/E SKIN AT NR 3 SLAT TAI DUCT. DENT ON L/W FIXED L/E SKIN AT NR 3 SLAT TAI DUCT, FOUND TO BE OUT OF LIMITS IAW SRM 57-20-1. REPAIRED DENT IAW SRM 57-30-4 PG 2Jan 14, 2004 · N236FE · Boeing 727200SDR COMA0460040Skin · crackedLEFT WING LOWER WING PLANK SKIN AT WS 148.00 IS CRACKED. REMOVED DAMAGE, FABRICATED REPAIR DOUBLERS FROM 2024-T3.125 (WVAC PO 21137) AND FILLER FROM 2024-T3.100 (WVAC PO 27013), INSTALLED IAW BOMBARDIER, INC REO 601R-57-21-120 REV D.Jan 14, 2004 · N952CA · Cndair CL6002B19SDR DHL2004806553Skin · corrodedLEFT WING OTBAORD L/E CORRODED AT STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 2H. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. REMOVED EXISTING DOUBLER IAW SRM 51-1-21 PG 1. TRIMMED OUJan 12, 2004 · N806DH · Doug DC873FSDR 04FDEA00099Skin · corrodedCENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK CORRODED. LOCATION AT STA 1235, RIGHT X = 30. CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK AT STA 1235 RH X = 30 CORRODED AREA CARRIED OUT REPAIR IAW EA 1 5710-74294, WINGS - CENTER WING UPPER PJan 12, 2004 · N604FE · Doug MD11SDR SWAA040107Skin · crackedDURING SCHEDULED C1 CHECK, FOUND RT WING FIXED L/E SKIN CRACKED AT WING STATION 213. REPAIRED WING SKIN CRACK PER EA.Jan 10, 2004 · N302SW · Boeing 7373H4SDR GTIA040094Access Panel · corrodedFTW - FOUND LEFT WING ACCESS PANEL HAS SURFACE CORROSION AROUND FASTENERS ON EXTERIOR SIDE. REMOVED CORROSION. FABRICATED REPAIR PART. INSTALLED REPAIR PART. (M)Jan 8, 2004 · N819NK · Doug DC981SDR COMA0460027Skin · corrodedTHE LEFT WING LOWER PLANK ACCESS HOLE CUTOUTS HAVE CORROSION AT 540CB AND 550 AB. REMOVED THE CORROSION AND RESTORED SURFACE FINISH IAW REO 601R-57-21-030 REV C.Jan 8, 2004 · N815CA · Cndair CL6002B19SDR 04FDEA00074Skin · crackedLEFT WING - ON LEADING EDGE SKIN PANEL INTERIOR FOUND SEVERAL CRACKS, STA XOS 510 UNDER REFUEL ACCESS PANEL. LEADING EDGE SKIN PANEL STA XOS 510 UNDER REFUEL ACCESS PANEL INTERIOR, CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG. 25, VOL. I.Jan 8, 2004 · N604FE · Doug MD11SDR GTIA040168Skin · corrodedFTW - FOUND LEFT WING LOWER SKIN PANEL UPPER SURFACE HAS 4 INCH BY 5 INCH DIAMETER EXFOLIATION AT XCW 121 9 INCHES AFT OF WING REAR SPAR AND 9 INCHES MLG TRUNNION FITTING. WING SKIN FSXCW 121 OUTBOARD OF TRUNNION FOUND OUT OF LIMITS. ALT SPAR FS XCW 121 FORWJan 6, 2004 · N819NK · Doug DC981SDR DHL2004752512Panel · dentedDURING C-CHECK, LT WING UPPER T/E PANEL WBL 124 HAS ONE SMOOTH DENT OUTBOARD AND ONE SHARP DENT INBOARD. CUT OUT 2 DENTED AREAS ON LT WING UPPER T/E PANEL, 1 APPROX 1.75 INCH DIA & 2 APPROX 2.25 INCH DIA. FABRICATED FILLERS 1 APPROX 1.75 INCH & 2 APPROX 2.2Jan 6, 2004 · N752DH · Boeing 727223SDR UPS04841822Skin · nickedINSPECTION TYPE: C1, LEFT WING L/E HAS NICKS AT XFS114. REMOVED DAMAGED AREA IAW REO G09663, FABBED NEW DOUBLER FILLER IAW REO G09663, ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED FASTENERS IAW DC8 SRM 51-1-27.Jan 5, 2004 · N814UP · Doug DC873FSDR COMA0460033Skin · crackedREPAIR WING PLANK CRACK AT WS 148.019 LT SIDE. REPAIRED LT HAND LOWER WING PLANK AT WS148.019 IAW EO 601R-57-21-130.Jan 3, 2004 · N924CA · Cndair CL6002B19SDR COMA0460032Skin · crackedREPAIR WING PLANK CRACK AT WS 148.019 RIGHT HAND SIDE. REPAIRED RT HAND LOWER WING PLANK AT WS 148.019 IN ACCORDANCE WITH AEROSPACE REPAIR ENGINEERING ORDER 601R-57-21-130.Jan 3, 2004 · N924CA · Cndair CL6002B19SDR COOSDR030074Panel · corrodedRT WING, LOWER SURFACE FIXED PANEL PN 65-19281-158, OUTER SKIN, CORRODED.Jan 1, 2004 · N79745 · Boeing 727224SDR COOSDR030073Panel · corrodedLT WING, LOWER SURFACE FIXED PANEL PN:65-21656601, OUTER SKIN, CORRODED.Jan 1, 2004 · N79745 · Boeing 727224SDR COOSDR030050Panel · delaminatedRT WING, FIXED PANEL PN 65-50820-142, TMC-284 DELAMINATED.Jan 1, 2004 · N767TW · Boeing 737200SDR COMA0460001Skin · corrodedTHE LEFT AND RIGHT LOWER WING TANK ACCESS PANEL CUTOUTS HAD CORROSION AT PANELS 640AB, 640CB, 640DB, 640FB, 640BB, 540BB, 540FB, 550AB AND 550BB. REMOVED CORROSION AND RESTORED THE FINISH IAW REO 601R-57-21-030 REV C.Dec 31, 2003 · N956CA · Cndair CL6002B19SDR UPS04841686Skin · corrodedINSPECTION TYPE: C3, INTERGRANULAR CORROSION ON RT WING L/E UPPER SKIN AT AFT END AT XFS 347. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW DC8-5720-7767-A.Dec 31, 2003 · N702UP · Doug DC871FSDR UPS04841696Doubler · corrodedINSPECTION TYPE: C3, LT WING L/E INTERNAL DOUBLER IS CORRODED BEYOND LIMITS BETWEEN XFS 622.75 TO XFS 610, LOWER INTERNAL DOUBLER AT PANEL OPENING. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 3641256 AND SRM 51-1-21.Dec 29, 2003 · N702UP · Doug DC871FSDR UPS04M41693Skin · crackedINSPECTION TYPE: 1C, RT WING LOWER FIXED LE SKIN CRACKED AT NR 7 SLAT IB TRACK CUTOUT AT XOS 888. NDT VERIFIES CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-10-00 FIG.21.Dec 29, 2003 · N253UP · Doug MD11FSDR UPS04841689Doubler · crackedINSPECTION TYPE: C3, LT WING LE LOWER INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE AT XFS 597.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG. 5769600 AND SRM. 51-1-21,51-1-20D,57-3-0 FIG. 2D.Dec 29, 2003 · N702UP · Doug DC871FSDR 03FDEA02304Panel · crackedLT WING UPPER TRAILING EDGE PANEL ADJACENT TO NR 3 SPOILER ACTUATOR ATTACHMENT FOUND CRACKED APPROXIMATELY 1.5 INCHES IN LENGTH. C/A: SNRM N0235 LT WING UPPER TRAILING EDGE PANEL ADJACENT TO NR 3 SPOILER ACTUATOR ATTACHMENT CRACKED PANEL REMOVED IAW AMM 20Dec 28, 2003 · N608FE · Doug MD11SDR A6WA200340201Skin · corrodedLT WING LOWER SKIN PLANK HAS CORROSION AT PANEL OPENING 540CB, FORWARD AND AFT OF PANEL OPENING. PERFORMED A MAJOR REPAIR BY BLENDING OUT CORROSION AND TREATING METAL IAW REO 601R-57-21-030. (M)Dec 27, 2003 · N405AW · Cndair CL6002B19SDR COMA0360577Skin · crackedTHE LEFT LOWER WING PLANK FUEL DRAIN FORWARD SCREW HOLE AT WS 85.5 HAD AN INDICATION WHILE PERFORMING EDDY CURRENT INSPECTION (FUEL BOOST PUMP DRAIN VALVE FORWARD SCREW HOLE). DRILLED THE SCREW HOLE TO .3125 INCH TO REMOVE THE INDICATION. FABRICATED AND INSTDec 27, 2003 · N956CA · Cndair CL6002B19SDR DL73S031132Skin · dentedDAMAGE FOUND ON LOWER SKIN PANEL OF RIGHT WING AT STA 525 NEAR OUTBOARD TIP. REPAIRED PER ERA 426849-14.Dec 24, 2003 · N304DL · Boeing 737232SDR 2004F00054Skin · debondedLEFT IB LEADING EDGE WING PANEL WAS REMOVED TO REPLACE THE DE-ICE BOOT AND IT WAS DISCOVERED THAT SUBSTANTIAL DEBONDING OF THE LOWER HALF OF THIS PANEL HAD OCCURRED. THERE WAS NO APPARENT DAMAGE TO THE OUTSIDE SKIN THAT WOULD EXPLAIN THIS AND ITS UNLIKELY THADec 19, 2003 · N904MC · Beech B300SDR COMA0360575Skin · corrodedFRETTING DAMAGE ON LEFT HAND LOWER WING PLANK FUEL ACCESS HOLE CUTOUT AT 550EB. BLENDED DAMAGE OUT AND ROTO-PEENED AFT OUTBAORD HATCHED AREA IN ACCORDANCE WITH REO 601R-57-21-030.Dec 19, 2003 · N712CA · Cndair CL6002B19SDR 2003FA0001277Skin · crackedCRACKS EMANATING FROM THE LT AND RT MLG FORWARD LOWER CUTOUTS IN THE CENTER WING SKIN. CRACKS RUN FORWARD FROM THE IB CORNERS TO THE FIRST AND SECOND RIVETS. CRACKS DO NOT CONTINUE TO THE EDGE OF THE SKIN. LOCATIONS OF THE CUTOUTS ARE JUST INBOARD OF THE NADec 18, 2003 · N139HP · Lkheed P2V7SDR 2003F00653Skin · crackedCRACKS EMANATING FROM THE LT AND RT MLG FORWARD LOWER CUTOUTS IN THE CENTER WING SKIN. CRACKS RUN FORWARD FROM THE IB CORNERS TO THE FIRST AND SECOND RIVETS. CRACKS DO NOT CONTINUE TO THE EDGE OF THE SKIN. LOCATIONS OF THE CUTOUTS ARE JUST INBOARD OF THE NADec 18, 2003 · N140HP · Lkheed P2V7SDR 2003FA0001250Skin · crackedCRACKS EMANATING FROM THE LT AND RT MLG FORWARD LOWER CUT-OUTS IN THE CENTER WING SKIN. CRACKS RUN FORWARD FROM THE INBOARD CORNERS TO THE FIRST AND SECOND RIVETS. CRACKS DO NOT CONTINUE TO THE EDGE OF SKIN. LOCATIONS OF THE CUTOUTS ARE JUST INBOARD OF THE NDec 17, 2003 · N140HP · Lkheed P2V7SDR 2003FA0001249Skin · crackedCRACKS EMANATING FROM THE LT AND RT MLG FORWARD LOWER CUT-OUTS IN THE CENTER WING SKIN. CRACKS RUN FORWARD FROM THE INBOARD CORNERS TO THE FIRST AND SECOND RIVETS. CRACKS DO NOT CONTINUE TO THE EDGE OF SKIN. LOCATIONS OF THE CUTOUTS ARE JUST INBOARD OF THE NDec 17, 2003 · N139HP · Lkheed P2V7SDR 2003UALA00959Skin · damagedLEFT WING INBOARD L/E HAS 4 EACH INTERIM REPAIR DOUBLERS INSTALLED AT L/E STATIONS 330, 415, & 543. MAJOR REPAIR ACCOMPLISHED. PERMANENT FLUSH REPAIRS WERE ACP PER SRM 57-41-01.Dec 15, 2003 · N171UA · Boeing 747422SDR DHL2003802564Skin · delaminatedRIGHT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED STA XW 5.000 - XW 33.000. REMOVED AND REPLACED RIGHT WING T/E UPPER PANEL (STA XW 5.000 - XW 33.000) IAW SRM 51-3-0 PG 1.Dec 13, 2003 · N802DH · Doug DC873SDR AUS20031267Skin · damaged(AUS) FOLLOWING REMOVAL OF THE LT WING THE UPPER SKIN AND INNER RIB FLANGE WAS FOUND TO BE GROUND AWAY TO THE EXTENT THAT THE RIVET EDGE DISTANCE WAS COMPROMISED. SOME RIVETS ALSO EXHIBIT GRINDINGMARKS. THE RT WING WAS THEN REMOVED AND INSPECTED AND FOUND TO BDec 10, 2003 · Beech A36SDR CALA0300707Skin · dentedINSPECTION FOUND A DENT IN RT WING L/E SKIN BETWEEN NR 2 ENGINE AND WING ROOT. A FLUSH REPAIR WAS INSTALLED USING REPAIR PLATE AND FILLER IAW SRM 57-41-01-201.Dec 10, 2003 · N17229 · Boeing 737824SDR COMA0360535Skin · crackedWHILE PERFORMING TASK CARD 002-57-540/640-603 FOUND LEFT WS 85.50 DRAIN HOLE FORWARD SCREW HOLE CRACKED. DRILLED HOLE, PERFORMED EDDY CURRENT INSP, FABRICATED AND INSTALLED FREEZE PLUG IAW BOMBARDIER, INC REO 601R-57-21-383.Dec 8, 2003 · N927CA · Cndair CL6002B19SDR CALA0300706Skin · crackedINSPECTION FOUND A 4.5 INCH CRACK IN RIGHT WING FIXED LEADING EDGE SKIN BETWEEN OSS 397 AND OSS 421. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D, OP 4 AND SRM 57-41-01.Dec 8, 2003 · N33132 · Boeing 757224SDR CALA0300704Skin · crackedINSPECTION FOUND A 6.25 INCH CRACK IN RT WING FIXED L/E SKIN AT STA OSS 421- OSS 471. THE SKIN WAS REPLACED IAW EA 5731-01010, REV D, OP 3.Dec 8, 2003 · N33132 · Boeing 757224SDR AWXA200301624Skin · crackedMCN - MINOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON LT WING LEADING EDGE SKIN AT NR 2 SLAT OUTBOARD AUXILIARY TRACK CUTOUT WS 346 TO WS 349. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-16 PG 27, REPAIR 11.Dec 7, 2003 · N325AW · Boeing 737301SDR DHL2003802553Skin · delaminatedRIGHT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED, STA XW 5.000 - XW 47.000. REMOVED AND REPLACED PANEL ON RIGHT WING T/E STA XW 5.000 - XW 47.000 IAW SRM 51-3-0 PG 1.Dec 4, 2003 · N802DH · Doug DC873SDR TSAA0457017Skin · corrodedREMOVED CORROSION FROM RIGHT FIXED LEADING EDGE AT WBL 375. TRIMMED OUT DAMAGED AREA. FABRICATED A FILLER AND DOUBLER PER TABLE 1. ALODIZED ALL TRIMMED EDGES AND BARE SURFACES. INSTALLED REPAIR PARTS WET WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 57-4Dec 3, 2003 · N820AL · Boeing 737230SDR ABXA040007Skin · corrodedLEFT WING UPPER XRS 519 - 624 CORROSION AROUND FASTENER HEADS (24 EACH). REPAIRED AREA IAW REA D857-48493MR.Dec 3, 2003 · N848AX · Doug DC861SDR DHL2003802571Skin · delaminatedRIGHT WING CENTERWING 723 PANEL LOWER SKIN DELAMINATED STA 742.000. REMOVED AND REPLACED NR 723 PANEL ASSY ON RIGHT WING CENTERWING, STA 742.000 IAW SRM 51-3-0 PG 1.Dec 3, 2003 · N802DH · Doug DC873SDR AWXA200301516Skin · crackedDURING C-12 CHECK A 3 INCH CRACK WAS FOUND ON RT WING UPPER LEADING EDGE SKIN AT NR 8 SLAT INBOARD CORNER. MAINTENANCE REMOVED CRACKED RT WING UPPER LEADING EDGE SKIN PANEL FROM WS 425.50 TO WS 471.30; FABRICATED 3 EACH REPAIR STRAPS & FILLERS; INSTALLED REPADec 2, 2003 · N908AW · Boeing 7572G7
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