JASC 5730

Service difficulty reports · 27,262

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.

SDR FDEA202409041236Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 764 FOUND CRACK ABOUT 0.3". REPAIR CARRIED OUT AT LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 654 AS PER MD - 11 SRM 57 - 40 - 02 - 2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED ASSep 4, 2024 · N596FE · Doug MD11FSDR FDEA202409041235Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 676 FOUND CRACK ABOUT 0.3". REPAIR CARRIED OUT AT RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 676 AS PER MD - 11 SRM 57 - 40 - 02 - 2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED ASep 4, 2024 · N596FE · Doug MD11FSDR FDEA202409041234Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 619 FOUND CRACK ABOUT 0.2". REPAIR CARRIED OUT AT RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 619 AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR Sep 4, 2024 · N596FE · Doug MD11FSDR FDEA202409041233Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 749 FOUND CRACK ABOUT 0.3 INCH. REPAIR CARRIED OUT AT LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 794 AS PER MD - 11 SRM 57 - 40 - 02 - 2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIEDSep 4, 2024 · N596FE · Doug MD11FSDR FDEA202409041232Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 688 FOUND CRACK ABOUT 0.2 INCH. REPAIR CARRIED OUT AT LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 688 AS PER MD - 11 SRM 57 - 40 - 02 - 2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIEDSep 4, 2024 · N596FE · Doug MD11FSDR FDEA202409041231Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 654 FOUND CRACK ABOUT 0.3 INCH. REPAIR CARRIED OUT AT LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 654 AS PER MD - 11 SRM 57 - 40 - 02 - 2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIEDSep 4, 2024 · N596FE · Doug MD11FSDR FDEA202409041230Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 618 FOUND CRACK ABOUT O.2 INCH. REPAIR CARRIED OUT AT LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 618 AS PER MD - 11 SRM 57 - 40 - 02 - 2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIEDSep 4, 2024 · N596FE · Doug MD11FSDR SIMA20240903004Skin · chafedRIGHT WING SKIN PANEL ABOVE PYLON CHAFFED. (MAJOR REPAIR) BLENDED AREA OF RH WING SKIN PANEL ABOVE PYLON FOUND TO BE BEYOND LIMITS IAW SRM 57-49-01 AD01 TABLE 101 AND FIGURE 102 SHEET 2. REMOVED AND REPLACED RH WING SKIN PANEL ABOVE PYLON IAW EMB 175 SRM 51-41Sep 3, 2024 · N321JS · Emb ERJ170200LRSDR LR7A2024090303565Skin · crackedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH OUTER WING FS597 SPAR CAP FASTENER HOLES CRACKED AT OWS4-9R. / REPAIRED IAW LAC MEA 382-57-24-118 DRC# 0141.Sep 3, 2024 · N402LC · Lkheed 382GSDR LR7A2024090303564Skin · crackedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH OUTER WING PLANK CORRODED FASTENER HOLES AT FS517, OWS5-7R. / REPAIRED IAW LAC MEA 382-57-24-119. DRC# 0140.Sep 3, 2024 · N402LC · Lkheed 382GSDR LR7A2024090303562Skin · crackedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND OUTER WING PLANK RAINBOW FITTING MULTIPLE HOLES CRACKED AT OWS5L, FS529-578. / REPAIRED IAW LAC MEA 382-57-24-099. DRC# 0135. / PSE# 57-50-01, AD 2012-06-09Sep 3, 2024 · N402LC · Lkheed 382GSDR LR7A2024090303513Skin · misrepairedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND INCORRECT REPAIR ON RH OUTER WING LOWER PLANK AT OWS425R, FS532. / REPAIRED IAW LAC MEA 382-57-24-076. DRC# 0902.Sep 3, 2024 · N402LC · Lkheed 382GSDR YENA2024090301212Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TOP SKIN UPPER SURFACE RIB 20 LEADING EDGE RH WING; REF AEROMAN NR 2024-448430 WO 2024 262/1 ACCOMPLISHED THE REPAIR OF THE CORROSION ON THE RH WING TOP SKIN PANEL 2 UPPER SURFACE, FRONT SPAR LEVEL AND BETWEEN RIBS 19-20 BONSep 1, 2024 · N589JB · Airbus A320232SDR YENA2024090301211Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TOP SKIN UPPER SURFACE OVERHAND LOC RIB 17 RH WING; REF AEROMAN NR 2024-448504 WO 2024 262/1 ACCOMPLISH THE REPAIR OF THE CORROSION ON THE RH WING TOP SKIN PANEL 2 UPPER SURFACE, FRONT SPAR LEVEL AND BETWEEN RIBS 19-20 BONDISep 1, 2024 · N589JB · Airbus A320232SDR YENA2024090301209Skin · corrodedDURING HEAVY MAINTENANCE: WINGS / RH WING / TOP SKIN PANEL 2 / UPPER SURFACE / FRONT SPAR & RIBS 19-20 / BONDING SPIGOT /CORROSION DAMAGE – PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 57-9051-24 REV. 0 (COVER + PARTS 1-2) /2/ AIRBUS MESSAGE 81443224/008 /3/ ASep 1, 2024 · N589JB · Airbus A320232SDR DALA2024090208630Skin · corrodedSHIP 3143 CORROSION UPPER SURFACE EXTERNAL SKIN LOCATED BTW RIB 11 TO RIB 12 AT LEVEL STR 11 ON LH WING. CORRECTIVE ACTION: PERFORMED BLEND OUT LOC. UPPER SURFACE EXTERNAL SKIN LOCATED ON RIB 11 PLUS 13 IN AT LEVEL STR 11 ON LH WING AS PER A319 SRM 51-74-00. (Sep 1, 2024 · N343NB · Airbus A319114SDR UIEA2024083000883Access Panel · leakingRH WING LOWER SURFACE. FUEL LEAK ON FUEL ACCESS PANEL BTWN RIB 11 AND 12.(<P> FUEL STICK WAS REPLACED IAW AMM 28-44-01-404-033. NO FURTHER DEFECTS NOTED</P>)Aug 30, 2024 · N1709A · Boeing 767375SDR UIEA2024082800858Skin · corrodedRH WING LOWER SKIN, CORROSION ON SKIN AT REAR SPAR LOWER CHORD BTWN W. STA 879.2 AND 906.2.(<P>RH WING LOWER SKIN, CORROSION ON SKIN AT REAR SPAR LOWER CHORD BT WN W. STA 879.2 AND 906.2. REPAIR BY LOWER SKIN CORROSION BETWEEN REAR SPAR AND WSTA 906 AT RH WINGAug 30, 2024 · N1709A · Boeing 767375SDR ABXA20240830162Skin · corrodedWHILE 762CK WAS UNDERGOING C-CHECK IN OSC. MAINTENANCE DISCOVERED CORROSION ON THE L/H WING UPPER SKIN AT WING STA 1066, BETWEEN RIB 33 & 34, AT THE FWD SPAR. AFTER CORROSION REMOVAL, THE REMAINING MATERIAL THICKNESS WAS LESS THAN THE ALLOWABLE LIMITS OF SRM 5Aug 30, 2024 · N762CK · Boeing 7673P6SDR ABXA20240830161Skin · corrodedWHILE 762CK WAS UNDERGOING C-CHECK IN OSC. MAINTENANCE DISCOVERED CORROSION ON THE L/H WING UPPER SKIN AT WING STA 1066, BETWEEN RIB 33 & 34, AT THE FWD SPAR. AFTER CORROSION REMOVAL, THE REMAINING MATERIAL THICKNESS WAS LESS THAN THE ALLOWABLE LIMITS OF SRM 5Aug 30, 2024 · N762CK · Boeing 7673P6SDR SWAA2024100840138Panel · debondedDEBONDED PLATE ACCESS PANEL 532BB FUEL TANK AT LT WING 2024-533603<[01] REPLACED PLATE ACCESS PANEL 532BB FUEL TANK AT LT WING IAW B737-700 SRM 51-10-02-0G AND DWG 110A0113-67; DWG 110A0113-67PL; DWG 110A0113-65 AND DWG110A0113-65PL SEE INDIVIDUAL SIGN OFF BELAug 29, 2024 · N266WN · Boeing 7377H4SDR CALA2024090300537Landing · damagedLEFT WING FUEL TANK LANDING 540PB OUTB OF RIB 19 HAS DAMAGE AT HOLE "N" AND AT HOLE "F".REAMED BOTH HOLES TO 0.297"IAW SRM 57-21-11 PGS 201-220, FIG.202.FABRICATED NEW BUSHINGS & INSTALLED IN HOLES N & F IAW SRM 51-72-12 PGS 1-8,FIG 2. IAW SRI 57-21-11-2- 002-Aug 29, 2024 · N485UA · Airbus A320232SDR ABXA20240829166Skin · corrodedDURING MAINTENANCE CHECK DURING INSPECTION CORROSION BEYOND ALLOWABLE LIMITS PER THE BOEING SRM (57-20- 01) AT RH UPPER WING SKIN AT WING STRINGER U-2 TO U-4 AND RUNS UNDER THE RIB CHORD TO SKIN EDGE AT BL 97.95. CORROSION BETWEEN THE SKIN IN THE FASTENER HOLEAug 29, 2024 · N364CM · Boeing 767338SDR ABXA20240829165Skin · corroded"DURING MAINTENANCE CHECK AT PEMCO (TPA) AND DURING INSPECTION CORROSION BEYOND ALLOWABLE LIMITS PER THE BOEING SRM (57-20-01) AT RH UPPER WING SKIN AT WINGS STRINGER S-15 AND RUNS UNDER THE PLUS CHORD TO SKIN EDGE AT BL 97.95. CORROSION BETWEEN THE SKIN IN THAug 29, 2024 · N364CM · Boeing 767338SDR 2024FA0000670Skin · corrodedREPAIRED THE LH UPPER WING SKINS BY BLENDING CORRODED AREAS, PERFORMING NDT, AND REPORTING FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS FOUND ACCEPTABLE, AND FABRICATED & INSTALLED TWO REPAIR DOUBLERS AS REQUIRED IN ACCORDANCE WITH TEXTRON FIELD Aug 29, 2024 · N648QS · Cessna 560XLSDR SWAA2024100731478Access Panel · crackedCRACK ACCESS PANEL 661BB TRAILING EDGE AROUND HOLES RT WING 2024-533518<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 14-JAN-25;[02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18175478 DUE DATE 25/JAN/25;[03] TOOL USED: SCALE P/N: CR5200 S/N: Aug 28, 2024 · N266WN · Boeing 7377H4SDR UIEA2024083000865Skin · damagedRHW - L/E ANTI-ICING DUCT SEPERATED AT NO.16 K/FLAP FWD L/E D-BEAM AREA AS MARKED.(<P>RHW L/E ANTI-ICING DUCT SEPERATED AT NO.16 K/FLAP FWD L/E D-BEAM SKIN PANEL CLOSE UP AS PER RI-57-41-17056 REV.A AND SRM 51-40-02 REV.43. NO FURTHER DEFECTS NOTED.</P>)Aug 27, 2024 · N852GT · Boeing 74787UFSDR DALA2024082808512Skin · corrodedSHIP 3143 CORROSION UPPER SURFACE EXTERNAL SKIN LOCATED BTW RIB 8 TO RIB 9 REAR SPAR ON LH WING. CORRECTIVE ACTION: PERFORMED BLEND OUT ON AFFECTED AREA (5 POINTS) LOC. ON UPPER SURFACE EXTERNAL SKIN LOCATED BTW RIB 8 TO RIB 9 REARSPAR ON LH WING. AS PER A319 Aug 27, 2024 · N343NB · Airbus A319114SDR DALA2024082808511Skin · corrodedSHIP 3143 CORROSION UPPER SURFACE EXTERNAL SKIN LOCATED BTW RIB 4 TO RIB 5 FRONT SPAR (2 POINTS). CORRECTIVE ACTION: PERFORMED BLEND OUT LOC. ON UPPER SURFACE EXTERNAL SKIN BTW RIB 4 TO RIB 5 FROM SPART LH WING (2 POINTS) AS PER A319 SRM51-74-00. (0525058)Aug 27, 2024 · N343NB · Airbus A319114SDR DALA2024082808510Skin · corrodedSHIP 3143 CORROSION UPPER SURFACE EXTERNAL SKIN LOCATED BTW RIB 3 TO RIB 4 AT LE VEL STR 11 ON LH WING. CORRECTIVE ACTION: PERFORMED BLEND OUT LOC. UPPER SURFACE EXTERNAL SKIN LOCATED ON RIB 3 PLUS 7 IN. AT LEVEL STR 11 AS PER A319 SRM 51-74-00. (0525036)Aug 27, 2024 · N343NB · Airbus A319114SDR SWAA2024100930945Access Panel · crackedCRACK ON OPEN HOLE ACCESS PANEL 561BB AT LT WING 2024-528510<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:A18229508 DUE DATE:14-JAN-25.;[02] TOOL USED SCALE P/N: CR5200 S/N: 8343110774 DUE DATE: 28-FEB-25.;[03] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N: 18196127 Aug 26, 2024 · N256WN · Boeing 7377H4SDR SWAA2024100430609Panel · delaminatedL/W LEADING EDGE PNL 521KB FWD EDGE DELAMINATED<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #521KB AS PER B737 SRM 51-70-04-2R-13; TOOL USED: TEMPERATURE CONTROL ID 172858 DUE DATE 5-13-25; MATERIAL USED: PO#2061896; PO#1690463. APPLIED TOPAug 26, 2024 · N497WN · Boeing 7377H4SDR SWAA2024100430940Panel · delaminatedRIGHT WING LEADING EDGE PNL 621JB DELAM AT FWD EDGE<[01] REPAIRED DAMAGE AREA AT RIGHT WING LEADING EDGE PANEL 621JB AS PER SRM 51-70-04-2R-13 .MATERIAL USED EA9390 PO2061896 PLUS BMS9-3-120TYD CL7.;[02] VERIFIED CORRECTIVE ACTION.Aug 26, 2024 · N497WN · Boeing 7377H4SDR CALA2024092602497Skin · crackedDURING L/H WING LOWER PANEL (DET) INSP. W/C# 29-5720-1-2811, DISCOVERED WHAT APPEARS TO BE A CRACK EMITTING FROM BOTH SIDES OF A SINGLE FASTNER. FASTNER LOCATION IS IN WING SPLICE S-9 NEAR RIB 19-20. (LAST FASTNER OF ROW) PERFORMED HFEC PER NDTM PART 6 51-00-0Aug 26, 2024 · N14237 · Boeing 737824SDR AALA202408287444Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE CORROSION ON RIGHT WING FUEL TANK ACCESS PANEL 640JB BOLT HOLES. REPLACED ACCESS PANEL PER TASK CARD 26C64057020.Aug 24, 2024 · N189UW · Airbus A321211SDR AALA202408289038Access Panel · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING FUEL TANK ACCESS PANEL 540JB BOLT HOLES WORN. REPLACED ACCESS PANEL PER TASK CARD 26C54057020.Aug 24, 2024 · N189UW · Airbus A321211SDR SWI2024F01179Panel · corrodedPANEL 541DB HAS FRETTING CORROSION AT MULTIPLE POINTS ON THE PANEL (MARKED) MX#28736038 (C-CHECK RO 11-6/2024) REMOVED CORROSION ON INNER MATTING SURFACE AT PANEL 541DB REF CRJ700 SRM 51-21-06-001-001-A01 AND FOUND TO BE OUT OF LIMITS AND REPAIR REF REOAug 23, 2024 · N755EV · Cndair CL6002C10SDR SWAA2024091229527Doubler · looseLEFT WING TRAILING EDGE: DEFLECTION RIB SUPPORT BEAM ATTACHMENT. THE 2 HORIZONTAL ATTACHMENT FASTENERS ARE LOOSE, BEAM & BRACKET HOLES ARE ELONGATED. CUT OUT DAMAGE IN CONTROL RIB UPPER TAB IAW SRM 57-51-02-2R-4. CUT OUT DAMAGE IN SUPPORT BEAM IAW SRM 57-51-02Aug 23, 2024 · N8648A · Boeing 7378H4SDR HNAA2024100100896Nut Plate · corrodedE051650 CORROSION AROUND NUT PLATE HOLES ON LH WING AT AFT BELLY PANEL LH LOWER ATTACHMENT FLANGES. RAR LH WING AFT BELLY PANEL LOWER ATTACHMENT FLANGE IAW EMB-145 SRM 51-40-02Aug 22, 2024 · N696AE · Emb EMB145LRSDR SWIA2024090300822Winglet · chafedTHE RH WINGLET TIP FAIRING HAS EXCESSIVE PLAY WITH EVIDENCE OF FRETTING PRESENT ON ATTACHING FASTENERS. (FILED CLOSED) EVALUATED RH WINGLET TIP FAIRING ATTACHING FASTENERS AND FOUND MULTIPLE OVERSIZED HOLES AFFECTING RH WINGLET INBOARD AND OUTBOARD SKINS,Aug 22, 2024 · N800SK · Cndair CL6002D24SDR SWAA2024092328549Access Panel · crackedCRACK ACCESS PANEL 561BB TRAILING EDGE AROUND HOLES LT WING 2024-504380<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 14-JAN-25.;[02] TOOL USED STEP 12: ULTRASONIC EQUIPMENT; P/N: GEIT1480179; S/N: GOPLS15100171; DUE DATE: 07 DEC 24.;[03] REAug 21, 2024 · N7880D · Boeing 7377K5SDR YENA2024082601150Skin · corrodedDURING HEAVY MAINTENANCE: DENT UPPER EXTERNAL SKIN OB FLAP ON LH WING; (RESOLVED ON W/O: 1310500 TASKCARD: NR-00021 ) REF AE W/O# 2024-131/1. N/R# 2024-336623. REPAIRED UPPER EXTERNAL SKIN OB FLAP ON LH WING AS PER EC NO. A24-882-01, AEROMAN EA# 57-9017-24 CAug 20, 2024 · N648JB · Airbus A320232SDR YENA2024082601149Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE RIB 17 TO RIB 18 CPCP F INDING ON RH WING; (RESOLVED ON W/O: 1310500 TASKCARD: NR-00022 ) REF AEROMNAN NR 2024-336699 WO 2024 131/1 ACCOMPLISHED REPAIR OF THE CORROSION ON THE RH WING TOAug 20, 2024 · N648JB · Airbus A320232SDR YENA2024082201148Access Panel · corrodedDURING HEAVY MAINTENANCE: CORROSION ACCESS PANEL 674BB INTERNAL AREA RIB 6 LOWER SKIN ON RH WING (CPCP FINDING);WORK ACCOMPLISHED ON AEROMAN NR 2024-336762 WO: 2024 131/1. ACCOMPLISHED REPAIR OF CORROSION SPOT AT RH WING BOTTOM SKIN PANEL 3 UPPER SURFACE AT RIAug 20, 2024 · N648JB · Airbus A320232SDR YENA2024082201147Access Panel · corrodedDURING HEAVY MAINTENANCE: CORROSION ACCESS PANEL 674BB INTERNAL AREA RIB 6 LOWER SKIN ON RH WIN G (CPCP FINDING); WORK ACCOMPLISHED ON AEROMAN NR 2024-336762 WO:2024 131/1 ACCOMPLISHED REPAIR OF CORROSION SPOT AT RH WING BOTTOM SKIN PANEL 3 UPPER SURFACE AT RAug 20, 2024 · N648JB · Airbus A320232SDR YENA2024082201145Skin · damagedDURING HEAVY MAINTENANCE, WINGS / RH WING / BOTTOM SKIN PANEL 3 / UPPER SURFACE AT RIB 6-6A BTWN FALSE REAR SPAR AND REAR SPAR / CORROSION - PERMANENT REPAIR (PENDING DTA); REFERENCE: /1/ AEROMAN EA 57-9011-24 REV. 00 (COVER + PART 1 -5) - RH WING REPAIR /2/ AAug 20, 2024 · N648JB · Airbus A320232SDR YENA2024082201144Skin · damagedDURING HEAVY MAINTENANCE, RT WING BOTTOM SKIN PANEL 3, UPPER SURFACE AT RIB 6-6A BTWN FALSE REAR SPAR & REAR SPAR CORROSION. DAMAGE WAS EVALUATED AGAINST SRM 57-21-11-283-005, BUT FOUND TO BE OUT OF LIMIT DUE SINCE DAMAGE CORRODED THROUGH SKIN. MANUFACTURER Aug 20, 2024 · N648JB · Airbus A320232SDR CALA2024082002245Skin · crackedSUSPECTED CRACK NOTED ON THE LEFT LOWER WING AT THE O/B MOST FASTENER OF STRINGER 9. (MARKED) SEE PIC. 5725-01139 ON OR BEFORE 18 FEBRUARY 2026. ON THE LH WING LOWER SKIN BETWEEN WSTA 564 AND WSTA591, ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF EC/RA ALL Aug 20, 2024 · N17244 · Boeing 737824SDR SWIA202411120819Skin · bentLH LEADING EDGE 530JL HAS SLIGHT BEND NEAR TRAILING EDGE INBOARD SIDE. APPROX 1.25" FROM TRAILING EDGE, AND 5.75" LONG STARTING FROM INBOARD EDGE. (FILED CLOSED) REMOVED LEADING EDGE 530JL INBOARD RIB AND REWORKED DENT NEAR TRAILING EDGE INBOARD SIDE. APAug 19, 2024 · N453SW · Cndair CL6002B19SDR AALA202411142627Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE UPPER SKIN PANEL LOWER SURFACE AT RIB 14. REPAIRED SKIN PANEL PER EA 357758.Aug 17, 2024 · N162UW · Airbus A321211
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