N245WN

Service difficulty reports · 314

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N245WN' AND registry_match = 'registration'
  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 SWAA2024041563789Floorboard · delaminatedDELAMINATION ON 241YF FLOORBOARD AFT WET AREA.<[01] IDENTIFIED FLOOR PANEL 241YF IAW SRM 53-00-50-01-1 FIG. 6 TABLE 6 AND FOUND DELAMINATION TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A PARA 4.F. <BR>REPAIR TO BE ACCOMPLISHED PER SRM 53-00-50-2R-1;[02] FLMar 15, 2024 · N245WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024041563788Floor Panel · delaminatedDELAMINATION ON 242RF FLOORBOARD AFT WET AREA.<[01] FLOOR PANEL 242RF WET AREA DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION #1Mar 15, 2024 · N245WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024041563787Floorboard · delaminatedDELAMINATION ON 241XF FLOORBOARD AFT WET AREA.<[01] 241XF FLOORBOARD AT AFT WET AREA WITH DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.Mar 15, 2024 · N245WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024041563786Door Frame · crackedSTA 312 FRAME INNER RADIUS IS CRACKED ABOVE L1 DOOR CUT-OUT.<[01] REPAIRED CRACK ON BS 312 FRAME STR 6 L ON FAULT ATTACHED TTG8Q00S70JT PER EA M-21-153-01244;[02] CORRECT EA NUMBER IS M-22-153-01244.;[03] VERIFIED TASK COMPLETEMar 15, 2024 · N245WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2024041563783Support · corrodedCORROSION ON R1 DOOR THRESHOLD SUPPORT FROM STA 294+9 TO 312+13; RBL 58-60; WL 209.<[01] UPDATED P/N;[02] CERTIFY;[03] REMOVED CORROSION ALONG FSD R1 DOOR THRESHOLD SUPPORT AT RBL55; WL208; BS58-60 + 5'; L:1' X W:1' D: 0.013' FROM ORIGINAL THICKNESS IS 0.090' Mar 15, 2024 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024041563780Channel · corrodedCORROSION ON R1 MOP SILL FROM STA 294.5 TO STA 328; RBL 55-61; WL 208 TO 209.<[01] UPDATE TO P/N;[02] CERTIFY;[03] REMOVED AND REPLACED MOP SILL BETWEEN BS 259 TO BS 360; RBL 53;WL 208 PER SRM 51-40-02 AND DWG 141A8310 REV.-.Mar 15, 2024 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024041563779Floor Support · crackedCRACKED INTERCOSTAL AT STA 312+5; RBL 30; STA 208.<[01] UPDATED TABLE;[02] UPDATED STEPS 1-4;[03] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02-0G-0 AND DWG: 141A5400.;[04] UPDATED MEASUREMENTS TABLE.Mar 15, 2024 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024041563777Channel · corrodedCORROSION ON L1 DOOR MOP SILL FROM STA 294.5+16 TO STA 344; LBL 55-61; WL 208.2<[01] UPDATED MEASUREMENT TABLE;[02] UPDATE STEPS 1;2;[03] PARTIAL UPDATE STEP 3;[04] STEP 3 COMPLETE;[05] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.Mar 15, 2024 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024041563784Floorbeam · corrodedCORROSION ON STA 328 FLOOR BEAM AT RBL 20; WL 208.1<[01] BS 328 FLOOR BEAM TO BE REPAIRED ON CARD# TTG8Q00S6FCK.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.Mar 15, 2024 · N245WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024041563800Shear Web · corrodedCORROSION ON SHEAR WEB AFT WET AREA STA-1016 LBL-3 WL 208.<[01] UPDATED MEASUREMENTS TABLE;[02] UPON FURTHER INVESTIGATION FOUND CORROSION TO BE IN THE STRAP INSTEAD OF SHEAR WEB; PART WILL BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARA 9.C.;[03] UPON FMar 15, 2024 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024041563801Shear Web · corrodedCORROSION ON SHEAR WEB AFT WET AREA STA-1016 RBL-3 WL 208<[01] UPON FURTHER INVESTIGATION FOUND CORROSION TO BE IN THE STRAP INSTEAD OF SHEAR WEB; PART WILL BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARA 9.C.;[02] UPDATED MEASUREMENTS TABLE.;[03] VERIFIMar 15, 2024 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024041563804Shear Web · corrodedCORROSION ON SHEAR WEB AFT WET AREA STA-1016 LBL-40 APPROX. WL 208<[01] UPON FURTHER INVESTIGATION FOUND PRIMER CHIPPED AND RIVETS DAMAGED AT BS 1006+3 AND 1006+4 AND 1016. CLEANED AREA AROUND THE FASTENERS AT BS 1006+3 AND 1006+4 AND WEB AT BS 1006 PER SRM 51Mar 15, 2024 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024041564063Stiffener · crackedLH HORIZONTAL STAB RIB 4 STIFFENER #4 (AFT) HAS A CRACK.<[01] L/H HORIZONTAL STAB RIB #4 ( STA. 120.3 ) WILL BE REPLACED ON FAULT #TTG8Q00S5BZ7. NO FURTHER ACTION REQUIRED;[02] VERIFIED CORRECTIVE ACTION 1.Mar 15, 2024 · N245WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024041564262Doubler · crackedDURING REMOVAL R/H VAPOR BARRIER BS 663 FOUND DOUBLER P/N 111A1511-24 CRACKED<[01] REMOVED AND REPLACED IAW SRM 51-40-02 AND DWG 111A1001 REV.- AND DWG 111A1000 REV;;[02] VERIFIED CORRECTIVE ACTION & MEASUREMENTS FIELDS. CARD COMPLETE.Mar 15, 2024 · N245WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2024041564260Plate · crackedR/W T/E WIGGLE PLATE LOCATED JUST O/B OF PANEL 651DB IS CRACKED<[01] REMOVED AND REPLACED R/W T/E WIGGLE PLATE LOCATED JUST O/B OF PANEL 651DB IAW SRM 51-40-02-0G-0 PARA. 4.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.Mar 15, 2024 · N245WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2024041563491Floorbeam · corrodedCORROSION ON BS 986.5 FLOOR BEAM LBL 43 WL 208<[01] REMOVED CORROSION FROM AFT WET AREA FLOOR BEAM BS 986 LBL 43 WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. ACCOMPLISHED REPAIR OF 986 FLOOR BEAM PER SRM 53-70-51-2R-6;[02] VERIFIED ITEM 1Mar 14, 2024 · N245WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024041563493Floorbeam · corrodedCORROSION ON BS 986.5 FLOOR BEAM RBL 43 WL 208<[01] UPDATED MEASUREMENT TABLE.;[02] REMOVED CORROSION NO BS 986-05 FLOR BAEM AT RBL 43; WL 208 AND FOUND TO BE OUT LIMIT'S AND REPAIRED PER SRM 53-70-51-2R.;[03] VERIFIED.Mar 14, 2024 · N245WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024041563756Plate · crackedL/W T/E WIGGLE PLATE CRACKED O/B OF SWING DOWN PANEL 551DB.<[01] TASK COMPLETE:<BR>REMOVED CRACKED WIGGLE PLATE IAW SRM 51-40-02-0G-0. RECEIVED NEW WIGGLE PLATE (PN: 7570723) AND INSTALLED IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION. COMPLETEMar 14, 2024 · N245WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2024031261153Floor Panel · crackedAFT CARGO COMPARTMENT FLOOR PANEL IS CRACKED OR TURN ABOUT 30INCH LONG ( PANEL 140BF)<[01] REMOVED PANEL PER AMM 25-52-10;[02] 01 - REMOVED AND REPLACED PER [AMM 25-52-10-000-801-NG (CARGO FLOOR PANEL REMOVAL - PERMANENT)]Mar 8, 2024 · N245WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024020246826Latch · out of adjustEXIT DOOR ROWS ; TRAY TABLE LOCK LATCHES SWING BOTH DIRECTION @ 11 CB ; 12 FED EXIT DOOR ROWS TRAY TABLE LOCK LATCHES SWING BOTH DIRECTION @ 11 CB 12 FED<[01] REPLACED TRAY TABLE LATCHES @ SEAT ROWS 11B & 12FED IAW CMM 25-21-42.Jan 31, 2024 · N245WN · Boeing 7377H4 · Passenger Compartment EquipmentSDR SWAA2023101710942Beam · crackedINNER SKIN CRACKED AFT SIDE 20.5 INCHES FROM BOTTOM. REMOVED FRAME PER SRM 51-40-02 2.P/N 141A6120-6 AND IT SHOULD BE P/N 141A6121-7. LOCATED NEW BEAM PER SRM 51-40-05. 3. INSTALLED NEW BEAM P/N 141A6121-7 PER SRM 51-40-02. 4. INSPECTED WORK ABOVE 5.C/WOct 14, 2023 · N245WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2023100306641Door · crackedL1 DOOR HAS A VISIBLE .4' CRACK ON THE LOWER FORMED INTERCOSTAL; LOCATED 12' FROM FORWARD EDGE OF DOOR AND 32.5' FROM BOTTOM EDGE. EXTENDS FROM THE UPPER INBOARD CORNER TO THE TOOLING HOLE. PERFORMED NDT PART 6 51-00-00 PROCEDURE 23 TO VERIFY CRACK. REMOVED Oct 3, 2023 · N245WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2023050544163Handle · looseDOOR ASSIST HANDLE AFT OF DOOR 1L IS LOOSE<[01] SECURED ASSIST HANDLE AFT OF L1 DOOR IAW AMM 25-21-31-420-802 STEP 3B(6);[02] VERIFIED STEP 1. AUDIT C/W.May 1, 2023 · N245WN · Boeing 7377H4 · Emergency ExitsSDR SWAA2023050544161Handle · looseR1 DOOR ASSIST HANDLE LOOSE<[01] SECURED R1 ASSIST HANDLE IAW AMM 52-41-31-400-802 STEP 3F(2);[02] VERIFIED STEP 1. AUDIT C/W.May 1, 2023 · N245WN · Boeing 7377H4 · Galley DoorsSDR SWAA2023050444162Handle · looseL1 DOOR ASSIST HANDLE LOOSE<[01] SECURED L1 DOOR ASSIST HANDLE IAW AMM 52-11-31-400-802 STEP 3G(2);[02] VERIFIED STEP 1. AUDIT C/W.May 1, 2023 · N245WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2023050541685Angle · crackedCENTER TANK LEFT HAND LOWER ATTACH ANGLE HAVE CRACK IN OPEN HOLE AT STA 663; LBL 31.83 ; W/L 168.54 CENTER TANK LEFT HAND LOWER ATTACH ANGLE HAVE CRACK IN OPEN HOLE AT STA 663 LBL 31.83 W/L 168.54<[01] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 16. NO DEFECTS NOTApr 26, 2023 · N245WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2023050530844Floor Panel · delaminatedDOT #A114-007. CABIN FLOOROARD PANEL 242AF HAS AREAS OF PULLED FIBERS ALNOG EDGES AND CENTER ON UPPER SURGACE.<[01] WORK ACCOMPLISHED ON NON-ROUTINE TTG8Q00KMD1G;[02] VERIFIED STEP 1Apr 24, 2023 · N245WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023050530847Floorboard · pulledDOT #114-012. CABIN FLOORBOARD PANEL 231ZF HAS AREAS OF PULLED FIBERS ON UPPER SURFACE.<[01] EVALUATED DAMAGE; TOP SIDE OF PANEL IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1; TAP TEST GOOD NO DELAMINATION NOTED. <BR><BR>VERIFIED REPAIR MATERIALS IAW B737 Apr 24, 2023 · N245WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023050530859Floorboard · pulledDOT #114-016. CABIN FLOORBOARD 232SF HAS AREAS OF PULLED FIBERS ALONG THE CENTER ON UPPER SURFACE.<[01] EVALUATED DAMAGE; TOP SIDE OF PANEL IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1; TAP TEST GOOD NO DELAMINATION NOTED. <BR><BR>VERIFIED REPAIR MATERIALApr 24, 2023 · N245WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023050530860Floorboard · pulledDOT A114-017. CABIN FLOORBOARD 231XF HAS AREAS WITH PULLED FIBERS ON UPPER SURFACE.<[01] EVALUATED PANEL 231XF AND FOUND PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW B737-700 SRM 53-00-50-2RApr 24, 2023 · N245WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023050531147Web · crackedRIGHT HAND 663 VAPOR BARRIER WEB IS CRACKED AT RBL 50<[01] EVALUATED R/H 663 VAPOR BARRIER AND FOUND A CRACK 4.5' AT RBL 50. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 57-10-10-2R-2 PAR 1A & NOTE. CLEAN AND PREP. IAW B737-700 SRM 51-70-04-2R-10 PAR 4A-C. VERIFY Apr 24, 2023 · N245WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2023050530386Angle · crackedCENTER TANK RIGHT HAND LOWER ATTACH ANGLE IS CRACKED AT STA 663; RBL 8; W/L 168.54<[01] ANGLE BEEN REPAIRED ON N/R TTG8Q00KKYZ9 I.A.W SRM 57-10-10-2R-5;[02] VERIFIED ITEM 1<BR>AUDIT C/WApr 23, 2023 · N245WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2023050830375Attach Angle · crackedCENTER TANK LEFT HAND LOWER ATTACH ANGLE IS CRACKED AT STA 663; LBL 48; W/L 168.54<[01] REMOVED TWO BRACKETS AT OUTBD OF STA 663 LBL 48 I/A/W SRM 51-40-02-0G-0;[02] STARTED REMOVING CENTER TANK LEFT HAND LOWER ATTACH ANGLE AT STA 663; LBL 48 W/L 168.54 I/A/W SApr 21, 2023 · N245WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2023050830383Angle · crackedDOT A24-6 LH WING I/B L/E / WTB FAIRING SUPPORT ANGLE FOR PANEL 195AL CRACKED. MARKED<[01] REMOVED L/H WING I/B L/E WTB FAIRING SUPPORT ANGLE FOR PANEL 195AL I/A/W SRM 51-40-02-0G-0;[02] DRILLED UP NEW SUPPORT ANGLE FOR PNL 195AL I/A/W SRM 51-40-02-0G-0 AND BOApr 21, 2023 · N245WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2023050530376Angle · crackedCENTER TANK RIGHT HAND LOWER ATTACH ANGLE IS CRACKED AT STA 663; RBL 48; W/L 168.54<[01] STARTED REMOVEING STA 663 CENTER TANK RIGHT HAND LOWER ATTACH ANGLE IAW SRM 51-40-02-0G-0 SRM 57-10-10-2R-5 FIG 202;[02] VERIFIED ITEM 1 OF STEPS 1 AND 2;[03] COMPLETED REApr 21, 2023 · N245WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2023021000642Bracket · crackedLEFT WING; T/E UPPER SHELF PANEL JUST AFT OF PYLON; MID SEAL RETAINER ON FWD SIDE CRACKED.<[01] REMOVED AND REPLACED SEAL RETAINER BRACKET ON LEFT WING T/E UPPER SHELF PANEL JUST AFT OF PYLON IN REF TO SRM 51-40-02Feb 9, 2023 · N245WN · Boeing 7377H4 · Wing, Control SurfacesSDR SWAA2022112172578Slide · detachedFWD CREW ENTRANCE DOOR WAS OPENED WITH THE SLIDE STILL ARMED. THE SLIDE DID NOT DEPLOY OR INFLATE; BUT THE SLIDE DID DISCONNECT FROM THE DOOR / [01] REMOVED AND REPLACED FWD ENTRY EMERGENCY ESCAPE SLIDE REF MT 725-61-06Nov 16, 2022 · N245WN · Boeing 7377H4 · Escape SlideSDR SWAA2022102060248Panel · delaminated193B PANEL FWD R/H I/B CORNER HAS EDGE DAMAGE OF 0.100 IN AND DELAMINATION MEASURES 0.300 FROM CORNER. / [01] REPLACED PANEL 193B IAW AMM 20-50-11Oct 16, 2022 · N245WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2022082947186None · stuckGIRT BAR AT FWD SERVICE DOOR IS STUCK IN RETAINING CLIP / [01] REMOVED AND INSTALLED ORIGINAL GIRT BAR FROM RETAINING CLIP IAW AMM 25-66-00. OP CHECK GOOD.Aug 28, 2022 · N245WN · Boeing 7377H4 · Escape SlideSDR SWAA2022061719661Cover · missingOVERWING EMERGENCY EXIT LIGHT COVER MISSING LH EXIT / [01] REPLACED EXIT LIGHT COVER PER SIPJun 16, 2022 · N245WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022050293229Megaphone · deterioratedMEGAPHONE LOCATED AT AFT L/H WINDSCREEN IS BROKEN AND PLACARD DETERIORATED / [01] REMOVED AND REPLACED MEGAPHONE LOCATED AT AFT L/H WINDSCREEN AND EMER. EQUIP. PLACARD AS PER DWG: 25600001 AND BOING AMM 20-10-14-400-801.;[02] VERIFIED STEP 1Apr 11, 2022 · N245WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2022050292822Rib · crackedR/H HORIZONTAL STAB L/E PANEL - RIB #3 (I/B) - POSSIBLE CRACK / [01] PERFORMED HFEC AT SUSPECTED CRACK IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK CONFIRMED. CRACK LENGTH:0.218';[02] REMOVED RIB #3 AT RH HORIZONTAL STABILIZER L/E PANEL IAW B737-700 SRM 51-40Apr 10, 2022 · N245WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2022050292535Doubler · crackedELECTRICAL GROUND POWER RECEPTACLE(EGPR) SURROUND DOUBLER IS CRACKED AT AFT VERT. MID. FLANGE BS 235.8; WL 190-170. / [01] REMOVED THE INITIAL RUBBING BLOCK & LAMINATED SHIM AS PER B737-7 SRM 51-40-02-0G-0.;[02] TRIMMED OUT DAMAGE AREA OF EGPR SURROUNDING DOUBApr 8, 2022 · N245WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022042992544Bracket · crackedFWD CARGO COMP STA 500D STR 25L BRACKET CRACKED / [01] REMOVED & REPLACED CLIP BRACKET AT FWD CARGO COMP STA 500D STR 25L AS PER B737-7 SRM 51-40-02-0G-0 & DWG 143A0102.;[02] VERIFIED STEP 1Apr 8, 2022 · N245WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022042992545Gusset · crackedFWD CARGO COMP STA 500D STR 18L GUSSET CRACKED / [01] REMOVED AT FWD CARG0 COMP. STA 500D STR.18L GUSSET PER B 737-700 IN REF. SRM 51-40-02-0G-0;[02] VERIFIED STEP 1. OK TO INSTALL NEW GUSSET;[03] INSTALLED NEW GUSSET AT FWD CARGO COMPT. STA 500D; STRG. 18L ASApr 8, 2022 · N245WN · Boeing 737 · Fuselage Main, Plate/SkinSDR SWAA2022050292224Scuff Plate · corrodedAFT CARGO DOOR CUTOUT AFT PLATE-ASSY SCUFF CORRODED P/N 453A2611-2 / [01] REMOVED CORROSION AT AFT CARGO CAP STRIP FOUND TO BE OUT OF LIMIT (EXFOLIATION) REF B737-700 SRM 51-10-02 REPLACED CAP STRIP INSTALLATION WILL BE ACCOMPLISHED ON TTG8Q004CNRU;[02] VERIFIApr 7, 2022 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022050292232Shield · corrodedFWD CARGO DOOR CUTOUT AFT SHIELD BETWEEN STA 500 AND STA 500A RBL 21' UPPER SURFACE CORROSION / [01] REMOVED AT FWD CARGO DOOR CUTOUT AFT SHIELD BETWEEN STA 500 AND 500A RBL 21' (EXFOLIATION) FOUND TO BE OUT OF LIMIT REF B737-700 SRM 51-10-02 AND 53-00-53;[02]Apr 7, 2022 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022050292222Shield · corrodedAFT CARGO COMP STA 767+3 RBL 21' DOOR CUTOUT FWD SHIELD SURFACE CORROSION / [01] FOUND CORROSION ON AFT CARGO COMPARTMENT FWD SHIELD SUPPORT LOWER ANGLE BETWEEN STA 767 AND STA 787 RBL 22'TO BE EXFOLIATING CORROSION OUT OF LIMITS PER SRM 53-60-15-1A-1;[02] RECApr 7, 2022 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022042992219None · crackedFWD CARGO COMP STA 500C STR 25L CLIP UNDER ZEE CHANNEL CRACKED / [01] REMOVED CLIP AT FWD CARGO CONP STA 500C STR 25L AS PER B-737-7-SRM-51-40-02-0G-0;[02] VERIFIED STEP 1 OK TO INSTALL NEW CLIP;[03] INSTALLED NEW CLIP AT FWD CARGO COMP STA 500 C STR 25L IAW BApr 7, 2022 · N245WN · Boeing 737 · Fuselage Main, Plate/SkinSDR SWAA2022042992220Gusset · crackedFWD CARGO COMP STA 500D STR 18R GUSSET CRACKED / [01] REMOVED GUSSET AT FWD CARGO COMP STA 500 D ST 18 R IAW B737 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1. OK TO INSTALL NEW GUSSET;[03] INSTALLED NEW GUSSET AT FWD. CARGO COMPT. STA. 500D; S-18R; AS PER B737-7 SRApr 7, 2022 · N245WN · Boeing 737 · Fuselage Main, Plate/Skin
Back to N245WN