Service difficulty reports

1,771,154 reports of malfunctions and defects, newest first. Air carriers must report; general aviation reporting is voluntary.

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'
  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 DALA2026061603590Floor Support · corrodedFOUND CABIN LONGERON FLOOR SUPPORT CORROSION AT C75- C76, Y-2462. REPLACED FLOOR SUPPORT ASSY PER SRM 51-72-11. (1649193) AIRCRAFT WAS GROUNDED.Jun 16, 2026 · N801NW · Airbus A330323 · Fuselage Miscellaneous StructureSDR DALA2026061603589Fitting · crackedCABIN RIGHT SIDE ROD FITTING FOUND CRACK AT STRINGER 16 FROM FR53.5 TO FR53.6. REPLACED IAW SRM 51-72-11. (1649191) AIRCRAFT WAS GROUNDED.Jun 16, 2026 · N801NW · Airbus A330323 · Fuselage Miscellaneous StructureSDR SCNA20260616249Bracket · looseFWD ENTRY LEFT SIDE GIRT BAR BRACKET IS LOOSE. ADJUSTED FWD PAX DOOR GIRT BAR BRACKETS REF AMM 25-66-01. OK FOR SERVICE.Jun 16, 2026 · N814SY · Boeing 7378BK · Emergency EquipmentSDR 2026F00125Rudder · no discrepancyTHE PILOT DEPARTED RWY 9 ON THE SUNNY TRANSITION TO VQS AND AT APPROXIMATELY 1 MILE NORTH OF PUNTA LAS MARIAS, THE PIC DECIDED TO RETURN TO SIG DUE TO STIFFNESS OF THE RIGHT RUDDER PEDDLE. AN EMERGENCY WAS NOT DECLARED DUE TO THE PIC HAVING FULL CONTROL OF THJun 16, 2026 · N908VL · Bnorm BN2B26 · Rudder Control SystemSDR SWIA2026061577708Angle · gougedFORWARD WATER-WASTE DOOR SURROUND STRUCTURE ANGLE GOUGED FROM DRAIN VALVE ASSY. REMOVED AND INSTALLED NEW FORWARD WATER-WASTE DOOR SURROUND STRUCTURE ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG SH670-32280, REV H COMPLIED WITH TASK CARD 51-900-1002-SKY, LEAK Jun 15, 2026 · N822SK · Cndair CL6002D24 · Fluid Service DoorsSDR SWIA2026061577660Angle · corrodedFS280 BULKHEAD LH LOWER WEB ANGLE IS CORRODED MX32451081 C-CHECK RO 10132026EVALUATED LH LOWER WEB ANGLE AND FOUND OUT OF LIMITS REMOVED AND REPLACED WITH 1 EA OF NEW ANGLE REF CRJ900 SRM 51-42-06-001-001-A01 REV 38 JUL 252020 AND BOMBARDIER DWG CC670-34010 RJun 15, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, BulkheadSDR SWIA2026061577659Stringer · corrodedCORROSION FOUND ON STR22R FS 333 TO FS 349 C-CHECK RO 10132026REMOVED AND REPLACED STRINGER PN SH670-31379-1S WITH NEW AT STGR22R, FS333 TO FS349 PER REF CRJ 900 SRM 51-42-06-001-001-A01, DWG SH670-31350, REV A LEAK CHECK GOOD SEE CONTINAUTION CARD FOR FURTJun 15, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA2026061577636Stringer · corrodedCORROSION FOUND ON STRINGER 24R, BS 349 - 364. REPAIRED THE STRINGER IAW SRM 53-00-03-201-001-A02, SRM 51-42-06-001-001-A01, & DWG SH690-31350, REV M. COMPLIED WITH ALL STEPS OF 51-900-1002-SKY. LEAK CHKD GOOD.Jun 15, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA2026061577542Frame · corrodedEVIDENCE OF CORROSION FORMING IN MULTIPLE SMALL AREAS AT APPROX FS1015-FS1031 STGR 27-STGR 26R BETWEEN THE TAPE C-CHECK RO 10062026REPAIRED CORROSION GOUGE DAMAGE BETWEEN FS1000-1047 STGR27-21R ON THE EXTERNAL SKIN IAW MHIRJ REO 670-53-61-2740 REV-- DATED 2Jun 15, 2026 · N713SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2026061577152Skin · damaged2 SKIN BURN MARKS NEAR STGR 25R AND BETWEEN FS32200-FS37400 2 SKIN BURN MARKS NEAR STGR 25R AND BETWEEN FS32200-FS37400 REF TABLE 1 OF REO 670-53-00-719 REV-, TABLE 1 DAMAGE 23, 26 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN 27769127 FOR ASSOCIATED CPS REO Jun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026061577151Skin · damaged7 SKIN BURN MARKS NEAR STGR 25R AND 26R AND BETWEEN FS28200-FS29600 7 SKIN BURN MARKS NEAR STGR 25R AND 26R AND BETWEEN FS28200-FS29600 REF TABLE 1 OF REO 670-53-00-719 REV-- TABLE 1 DAMAGE 11, 13, 14, 15, 16, 17, 19 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DJun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026061577150Skin · damaged5 SKIN BURN MARKS NEAR STGR 25R AND 26R AND BETWEEN FS24100-FS27900 5 SKIN BURN MARKS NEAR STGR 25R AND 26R AND BETWEEN FS24100-FS27900 REF TABLE 1 OF REO 670-53-00-719 REV- TABLE 1 DAMAGE 2, 4, 7, 9, 10 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN 27769127 Jun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026061577149Skin · damaged5 RIVETS ON STGR 25R BETWEEN FS37000 AND 40200 5 BURNT RIVETS LOCATED ON STGR 25R BETWEEN FS37000-FS40200 REF TABLE 1 OF REO 670-53-00-719 REV- TABLE 1 DAMAGE 24, 25, 27, 28, 29 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN 27769127 FOR ASSOCIATED CPS REO 670-Jun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026061577148Skin · damaged5 RIVETS ON STGR 25R AND 26R BETWEEN FS23350 AND FS27400 5 BURNT RIVETS LOCATED ON STGR 25R AND 26R BETWEEN FS23350-FS27400 REF TABLE 1 OF REO 670-53-00-719 REV-- TABLE 1 DAMAGE 1, 3, 5, 6, 8 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN 27769127 FOR ASSOCIATEJun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026061577145Skin · damaged6 RIVETS ON STGR 24R BETWEEN FS44550 AND FS45700 6 BURNT RIVETS LOCATED ON STGR 24R FS44550-FS45700 REF TABLE 1 OF REO 670-53-00-719 REV-- TABLE 1 DAMAGE 43, 44, 45, 46, 465, 47 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN 27769127 FOR ASSOCIATED CPS REO 670-Jun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026061577144Skin · damaged5 SKIN BURN MARKS NEAR STGR 24R AND 25R AND BETWEEN FS43525-FS44550 5 SKIN BURN MARKS NEAR STGR 24R AND 25R AND BETWEEN FS43525-FS44550 REF TABLE 1 OF REO 670-53-00-719 REV-- TABLE 1 DAMAGE 39, 40, 41, 42, 48 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN 2776Jun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026061577142Skin · damaged9 RIVETS ON STGR 25R BETWEEN FS42200 AND FS43700 9 BURNT RIVETS LOCATED ON STGR 25R BETWEEN FS42200-FS43700 REF TABLE 1 OF REO 670-53-00-719 REV-- DATED 2024-02-15 TABLE 1 DAMAGE 30, 31, 32, 33, 34, 35, 36, 37, 38 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN Jun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026061577140Stringer · damaged6 BURNED RIVETS LOCATED ON STR 25R AND 26R BTWN BS 282 - 319.70, REF TABLE 1 OF REO 670-53-00-719 REV--, TABLE 1, DAMAGE 12, 18, 20, 21, 22, 225. PERFORMED REPAIR OF DAMAGE HOLE 12 ,18,20,21,22,225, IAW SRM 51-42-13 , 51-11-00 , 53-00-00 , AMM 20-30-00 ,21-3Jun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR REXA2026082601714Access Panel · corrodedCORROSION ON ACCESS 542BZ 532DZ, 542AZ AND 642AZ. CORROSION WAS REMOVED ON ACCESS 532DZ PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN OF LIMITS PER CRJ-900 SRM 57-41-01-101-002-A01, DUE TO EXCESIVE DAMAGE ON ACCESS 542BZ, 542AZ AND 642AZ WAS REPLACJun 15, 2026 · N926XJ · Cndair CL6002D24 · Wing, Plate/SkinSDR REXA2026082601713Access Panel · corrodedCORROSION ON ACCESS 542BZ 532DZ, 542AZ AND 642AZ. CORROSION WAS REMOVED ON ACCESS 532DZ PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN OF LIMITS PER CRJ-900 SRM 57-41-01-101-002-A01, DUE TO EXCESIVE DAMAGE ON ACCESS 542BZ, 542AZ AND 642AZ WAS REPLACJun 15, 2026 · N926XJ · Cndair CL6002D24 · Wing, Plate/SkinSDR REXA2026082601712Access Panel · corrodedCORROSION ON ACCESS 542BZ 532DZ, 542AZ AND 642AZ. CORROSION WAS REMOVED ON ACCESS 532DZ PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN OF LIMITS PER CRJ-900 SRM 57-41-01-101-002-A01, DUE TO EXCESIVE DAMAGE ON ACCESS 542BZ, 542AZ AND 642AZ WAS REPLACJun 15, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601711Hinge · crackedCRACK AND WEAR ON LOWER HINGE AND MID HINGE AT ACCESS PANEL 832ET. LOWER HINGE AND MID HINGE AT ACCESS PANEL 832ET WERE REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 AND PER CRJ-900 SRM 51-42-06-001-001-A01.Jun 15, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026082601710Hinge · crackedCRACK AND WEAR ON LOWER HINGE AND MID HINGE AT ACCESS PANEL 832ET. LOWER HINGE AND MID HINGE AT ACCESS PANEL 832ET WERE REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 AND PER CRJ-900 SRM 51-42-06-001-001-A01.Jun 15, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026082601687Frame · crackedCRACK ON FRAME AT INTERNAL FUSELAGE STRUCTURE OVER FS333.00 AND BTW STGR 2L TO 2R. FRAME AT INTERNAL FUSELAGE STRUCTURE FS333.00 AND BTW STGR 2L TO 9R. WAS REPLACE PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01Jun 15, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026082601663Angle · corrodedCORROSION ON STRIKER SILL, ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR. CORROSION ON STRIKER SILL, ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR. WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, MOUNTING ANGLE Jun 15, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601662Striker · corrodedCORROSION ON STRIKER SILL, ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR. CORROSION ON STRIKER SILL, ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR. WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, MOUNTING ANGLE Jun 15, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026082601659Support Angle · corrodedCORROSION AT FS 280.00 FLOOR ACCESS PANEL SUPPORT ANGLE, BTW LBL 12'' TO RBL12'' FS 280.00 FLOOR ACCESS PANEL SUPPORT ANGLE, BTW LBL 12'' TO RBL12'' WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01Jun 15, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601658Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT LEFT WING. MACHINED RIB OF LEADING EDGE SS58.41 AT LEFT WING. WAS REPAIRED PER REO 690-57-41-240 REV --Jun 15, 2026 · N926XJ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR 1SMA20260615001Brake · burnedDURING TAXI FOLLOWING CONSECUTIVE REJECTED TAKEOFFS, THE AIRCRAFT EXPERIENCED A LANDING GEAR BRAKE FIRE. INVESTIGATION REVEALED THAT THE HEAT GENERATED BY THE CONSECUTIVE ABORTS CAUSED THE CALIPER HYDRAULIC SEAL (P/N: MS28775-222 O-RING) TO MELT AND FAIL. THISJun 15, 2026 · N4599X · Piper PA32300 · Landing Gear Brake SystemSDR SWIA2026061576910Angle · crackedFOUND A CRACK ON PAX DOOR INTERCOSTAL DD7 AFT ANGLE. REPLACED PAX DOOR INTERCOSTAL DD7 AFT ANGLE IAW DWG 601R31702, REV-N, &SRM 51-42-06 REV. 39 DATED MAR 10/21.COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.LEAK CHECKED GOOD WITH NO DEFECTS NOTED.Jun 15, 2026 · N936EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026061576909Floor Support · unknownAS PER REO 601R-53-61-8559, REV -, REINCORPORATE REPAIR TO CARGO BAY FLOOR SUPPORT, BS 562.72 - 589 IAW REO 601R-53-61-690, REV -D, FABRICATED AND INSTALLED NEW REPAIR DOUBLERS AND FILLER IAW REO 601R-53-61-690 REV-D. COMPLIED WITH SKYWEST TASK CARD 51-900-10Jun 15, 2026 · N936EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR 2A6R2026061575901Floor Panel · damagedDAMAGE WAS FOUND ON THE COCKPIT FLOOR PANEL IN THE FORM OF IMPACT DAMAGE AND CORROSION. A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2026-24444A DATED 16 JUL 2026, AIR MJun 15, 2026 · N819LF · Urocop EC135P2 · Fuselage Floor PanelSDR UIEA2026061400478Beam · crackedRHW L/E NEAR NO.3 PYLON O/B D-BEAM UPPER CHORD FOUND CRACK(<P>UPPER CHORD REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 FIG 201.</P>)Jun 15, 2026 · N485MC · Boeing 74745EF · Nacelle/Pylon, Attach FittingsSDR 1Q2R2026072950088Fitting · gougedLEFT ELEVATOR PCU 2 FITTING GOUGE DAMAGE. PERFORMED PERMANENT REPAIR IAW REO 670-55-21-113 REV--, AND EA 57-2025-1480, REV C.Jun 15, 2026 · N523AE · Cndair CL6002C10 · Elevator, Spar/RibSDR VNAA202607280012Seat Track · corrodedWEAR AND CORROSION AT SIDE SEAT RAILS (L/H) (6EAS) ON FS 744.15 TO FS 977.00 AT PAX CABIN. SIDE SEAT RAILS (L/H) (6EAS) ON FS 744.15 TO FS 977.00 AT PAX CABIN DUE TO EXCESSIVE DAMAGE WERE REPLACED PER CRJ900 SRM 53-41-49-101-001-A02 AND PER CRJ-900 AMM 53-0Jun 15, 2026 · N552NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202607280011Seat Track · corrodedWEAR AND CORROSION AT SIDE SEAT RAILS (R/H) (6EAS) ON FS 669.40 TO FS 977.00 (EXCEPT SIDE SEAT RAIL LOCATED ON FS 895.00 TO FS 913.00) AT PAX CABIN. SEAT RAILS (R/H) (6EAS) ON FS 669.40 TO FS 977.00 (EXCEPT SIDE SEAT RAIL LOCATED ON FS 895.00 TO FS 913.00) AJun 15, 2026 · N552NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202607280010Seat Track · wornWEAR ON RH SIDE RAIL BTW 379.00 TO FS 661.00+10.00 (3EAS) AT PAX CABIN. DUE EXCESIVE DAMAGE ON RH SIDE RAIL BTW 379.00 TO FS 661.00+10.00 (3EAS) AT PAX CABIN. WAS REPLACED PER CRJ-900 SRM 53-21-49-101-001-A01. AND SRM 53-31-49-101-001-A02. AND PER CRJ-900 AMJun 15, 2026 · N552NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202607280009Seat Track · wornWEAR ON LH SIDE RAIL BTW 379.00 TO FS 669.40 (4EAS) AT PAX CABIN. DUE EXCESIVE DAMAGE ON LH SIDE RAIL BTW 379.00 TO FS 669.40 (4EAS) AT PAX CABIN WERE REPLACED PER SRM 53-21-49-101-001-A01. AND SRM 53-31-49-101-001-A02 PER AMM 53-00-49 (CONFIG A12).Jun 15, 2026 · N552NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202607280008Hinge · wornWEAR IN PASSENGER-DOOR PIANO HINGE ON THE FUSELAGE SIDE, FS343. WEAR IN PASSENGER-DOOR PIANO HINGE ON THE FUSELAGE SIDE, FS343.00 WAS REPAIRED PER REO 690-53-21-2156 REV.--Jun 15, 2026 · N552NN · Cndair CL6002D24 · Fuselage, Door HingeSDR VNAA202607280007Rib · crackedCRACK ON RIB LEADING EDGE SS57.16 AT LEFT WING. CRACK ON RIB LEADING EDGE SS57.16 AT LEFT WING WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-10-001-001-A01 AND CRJ-900 SRM 51-42-21-001-001-A01.Jun 15, 2026 · N552NN · Cndair CL6002D24 · Wing, Rib/BulkheadSDR SWAA2026072434470Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW BS 947 - 967, RBL 51, WL 208.1 IN AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 147A5650, SHEET 71, REV A.Jun 15, 2026 · N8650F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026072493079Bulkhead · delaminatedDELAMINATED BULKHEAD PANEL 121HW AT FWD CARGO BAY. REPAIRED BULKHEAD PANEL 121HW IAW AMM 25-00-00-300-801.Jun 15, 2026 · N8650F · Boeing 7378H4 · Fuselage Main, BulkheadSDR SWAA2026061512466Battery · no testCOCKPIT FLASHFLIGHT WILL NOT TEST. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00.Jun 15, 2026 · N8949Q · Boeing 7378 · Emergency EquipmentSDR SWAA2026061512458Flashlight · inoperativeFWD GALLEY FLASHLIGHT INOPERATIVE. PERFORMED OPS CHECK OF FWD GALLEY FLASHLIGHT IAW AMM 25-64-00.Jun 15, 2026 · N299WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2026061512464Lens · brokenEXIT ROW SIGN BROKEN. INSTALLED A NEW EMERGENCY RT LOWER EXIT SIGN LENS ON INSIDE OVERWING DOOR PER AMM 33-51-01.Jun 15, 2026 · N436WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026072063670Crossbeam · crackedCRACKED PANEL BRAKE AT LBL 1 BS 540 WL 208. REMOVED AND REPLACED BREAK PANEL AT LBL 1 BS 540 WL 208 IAW SRM 51-40-02-OG-0 AND DWG 143A0060 SHEET:46 REV-.Jun 15, 2026 · N257WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026071744137Support · corrodedCORRODED SUPPORT ZEE LBL 22 BTW BS 727D TO BS 767, WL 156 IN THE AFT CARGO BAY. REPLACED SUPPORT ZEE IAW SRM 51-10-02 ITEM 9, SRM 51-40-02-0G-0, AND DWG 146A7500, SHEET 85, REV A.Jun 15, 2026 · N930WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026071713458Support Angle · crackedCRACKED SUPPORT ANGLE BTW BS 907 TO BS 927, STR 25R AND STR 27R IN AFT CARGO BAY. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 147A7221, SHEET 24, REV-.Jun 15, 2026 · N930WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026071733706Support · corrodedCORRODED SUPPORT ANGLE BTW BS 767 - 787, RBL 22, WL 156 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, AND DWG 146A8123, SHEET 16, REV -.Jun 15, 2026 · N930WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026071712141Cargo Track · crackedCRACKED CARGO TRACK RBL 13.84 AND BS 727C AT AFT CARGO BAY. ACCOMPLISHED NDT INSPECTION IAW SRM 53-00-53-2R-3, STEP 4F. STEPS 11 TRHU 14. REPAIRED CARGO TRACK RBL 13.84 AND BS 727B TO 727D AT AFT CARGO BAY IAW SRM 53-00-53-2R-3, REPAIR 3.Jun 15, 2026 · N930WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings