N463WN

Service difficulty reports · 311

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 = 'N463WN' 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 SWAA2024041763196Stringer · crackedFWD CARGO HAS A CRACKED STR AT AFT FASTENER; STR 25R; BS 520+19<[01] DAMAGE WAS REPAIRED PER EA 24-153-00727. THIS IS A CATEGORY A REPAIR AS DEFINED IN 737-700 SRM 51-00-06;[02] VERIFIED TASK COMPLETEDMar 13, 2024 · N463WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024041763198Stringer · crackedFWD CARGO HAS A CRACKED STR AT AFT FASTENER; STR 26L; BS 520+19<[01] REPARED STRINGER 26L; APPLIED CIC ON REPAIR IAW SRM 53-00-03-2R-1Mar 13, 2024 · N463WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024041763197Stringer · crackedFWD CARGO HAS A CRACKED STR AT AFT FASTENER; STR 23R; BS 520+19<[01] 02 - INSPECTED PER [REFERENCE];[02] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 24-153-00709.;[03] VERIFIED CORRECTIVE ACTION #2Mar 13, 2024 · N463WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024041763190Stringer · crackedFWD CARGO HAS A CRACKED STR AT AFT FASTENER; STR 23L; BS 520+19<[01] REPAIRED FCB STR 23L BS 500D-540 IAW SRM 53-00-03-2R-1 REPAIR 1 AND EA # 24-153-00708;[02] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 24-153-00708Mar 13, 2024 · N463WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024041763191Cargo Track · corrodedFWD CARGO TRACK TIE DOWN HAS CORROSION AT BS 420+16; LBL 19; WL 156. ALL PROCESS WILL BE ACCOMPLISHED AND COMPLETED WITH TASK CARD#TTG8Q00S418F.Mar 13, 2024 · N463WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024041763200Sidewall Support · corrodedFWD CARGO FLOOR TO SIDEWALL SUPPORT IS CORRDED AT BS 500A - 500B; LBL 24; WL 156<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT <BR>BS 396 TO BS 500D LBL 24 WL 156 <BR>IAW SRM 51-40-02-0G-0 AND DWG 143A7500.Mar 13, 2024 · N463WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024041763199Threshold · corrodedFWD CARGO CENTER THRESHOLD IS CORRDED AT BS 440+10 - 480+5; RBL 23 - 30; WL 155<[01] REMOVED AND REPLACED FWD CARGO CENTER THRESHOLD BETWEEN BS 440 - 492.4 RBL24 WL 156.5 I.A. W SRM 51-10-02-0G-0; SRM 51-40-02-0G-0 AND DWG 143A8330.;[02] VERIFIED CORRECTIVE ACMar 13, 2024 · N463WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024041763194Support · corrodedFWD CARGO AFT BULKHEAD SUPPORT HAS CORROSION AT BS 500D; LBL 19 - RBL 24; WL 156<[01] REMOVED CORROSION ON FWD CARGO BULKHEAD FOUND TO BE WITHIN LIMITS IAW SRM 53-30-08-1A-1 PARA 4 (2) FIG.103 DET.C.<BR>TOOL USED<BR>ID:ATS2473<BR>DUE:09/2024<BR>S/N UNKNOW;[02]Mar 13, 2024 · N463WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024041763193Shield · corrodedFWD CARGO AFT SHIELD IS CORRODED AT BS 480+14 - 500A; RBL 24; WL 156<[01] REMOVED AND REPLACED FWD. SHIELD ASSY P/N 143A8126-31 LOT: 1553496-2 IAW SRM 51-10-02; SRM 51-40-02; AND DWG 143A0080.;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.Mar 13, 2024 · N463WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024041763192Cargo Track · corrodedFWD CARGO TRACK TIE DOWN HAS CORROSION AT BS 480+17; LBL 19; WL 156<[01] UPDATED PART REQUIREMENTS.;[02] REMOVED AND REPLACED FCB FLOOR TRACK FROM BS 396 TO BS 500D; LBL 19; WL 156 IAW SRM 51-40-02-0G-0 AND DWG# 143A7500;[03] VERIFIEDMar 13, 2024 · N463WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024041763188Attach Angle · crackedMAIN E-BAY O2 BOTTLE FWD SUPPORT BRACKET; LOWER ATTACH ANGLE IS CRACKED AT O/B FASTENER BS 360+2; RBL 14; WL 164<[01] REMOVED AND REPLACED MAIN E-BAY O2 BOTTLE FWD SUPPORT BRACKET BS 360 ; RBL 14; WL 164 IAW SOPM 20-50-01;[02] VERIFIED CORRECTIVE ACTION ITEM 1Mar 13, 2024 · N463WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024041762601Tail Cone · delaminatedTAIL CONE LOWER LOBE RIGHT SIDE WAS FOUND A DELAMINATION SPOT; 9 IN BEHIND STA 1156 L=3 IN W= 2.750 IN. REPAIRED IAW SRM 51-70-05-2R-2.Mar 12, 2024 · N463WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2024041762097Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241DF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0128.;[02] VERIFIEDMar 11, 2024 · N463WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024041762098Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241AF WITH AREAS OF PULLED STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0008;[02] VERIFIED FLOOR PANEL 241AF WAS REPLACED BY FABRICATING A NMar 11, 2024 · N463WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024041762092Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0126.;[02] VERIFIEDMar 11, 2024 · N463WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024041762095Rib · crackedRH HORIZONTAL STAB RIB #4; STAB STA 120.30; CRACKED 2ND AND 4TH VERTICAL STIFFENERS.<[01] NDT HFEC INSPECTED SURFACE; 2ND AND 4TH VERTICAL STIFFENERS PER 737 NDTM PART 6; 51-00-00; PROC 23; CRACKS .500' LONG NOTED AT THE LOWER ENDS. EQUIP ID IS000680 DUE 05/24Mar 11, 2024 · N463WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2024041761525Shelf · corrodedG1 GALLEY HAS CORROSION ON THE SHELF UNDER THE COFFEE MAKEER RAILS<[01] UPDATED PARTS REMOVAL;[02] RECEIVED NEW G1 GALLEY; P/N: 980001-1; S/N: 366.<BR>ORIGINAL G1 GALLEY REMOVED ON TASK CARD TTG8Q001S17C.<BR>INSTALLATION OF NEW G1 GALLEY TO BE ACCOMPLISHED ON Mar 10, 2024 · N463WN · Boeing 7377H4 · Buffet/GalleysSDR SWAA2024041761526Shelf · corrodedG4 GALLEY HAS CORROSION ON THE SHELF UNDER THE COFFEE MAKEER RAILS<[01] UPDATED PARTS REMOVAL;[02] ADDED PART;[03] REMOVED AND REPLACED GALLEY 4 IAW AMM 25-31-45-000-802-004 AND AMM 25-31-45-400-802-004.;[04] REMOVAL AND INSTALLATION OF G-4 GALLEY TO BE ACCOMPMar 10, 2024 · N463WN · Boeing 7377H4 · Buffet/GalleysSDR SWAA2024041761112Skin · debondedPANEL 192AL OUTER SKIN IS DISBONDED. (MARKED)<[01] PANEL 192AL OUTER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 51-70-05-2R-2.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Mar 9, 2024 · N463WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2024041761251Battery Pack · no testEMERGENCY LIGHTING BATTERY PACKS M1668; M1669; M1670; M1672; M1673; M1674 AND M1675 FAIL EMERGENCY LIGHTING CAPACITY CHECK.<[01] REMOVED AND REPLACED M1668; M1669; M1670; M1672; M1673; M1674 AND M1675 EMERGENCY LIGHTING BATTERY PACKS IAW AMM 33-51-06-960-805 SMar 9, 2024 · N463WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024041760661Seal · crackedLT. HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED LT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.Mar 7, 2024 · N463WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024041760660Seal · crackedRT HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED RT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.Mar 7, 2024 · N463WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024030457893Lamp · inoperativeEMERGENCY AREA LIGHT AT SEAT 1 (ABC) INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-03-960-801-NG (AREA LIGHT - LAMP REPLACEMENT - PERMANENT)]Mar 1, 2024 · N463WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023060556065Slide · out of adjustAFT ENTRY DOOR SLIDE FLAP CONTACTING FRAME WHEN CLOSING.<[01] ADJUSTED AFT ENTRY DOOR SLIDE IN CASE. OPS NORMAL. REF AMM25-66-01.Jun 2, 2023 · N463WN · Boeing 7377H4 · Escape SlideSDR SWAA2023011089625Sign · looseFRONT SERVICE DOOR EXIT SIGN LOOSE. REPLACED EMERGENCY LIGHT ASSY IAW AMM 33-51-01.Jan 8, 2023 · N463WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023010989591Cover · missingFWD GALLEY EXIT LIGHT COVER MISSING. INSTALLED MISSING FWD EXIT LIGHT COVER IAW SIPJan 7, 2023 · N463WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022111571110Actuator · inoperativeELECTRIC TRIM INOPERATIVE AFTER TAKEOFF. HORIZONTAL STABILIER TRIM. / [01] -SPEED TRIM FAIL LIGHT ILLUMINATES ON RECALL.<BR>-NO C/B?S POPPED.<BR>-FAULT MESSAGE 22-11182. (DFCS BITE);[02] R&R STAB TRIM CUTOUT RELAY (R384) OPS CHECK AND CLOSE UP REQUIRED.;[03] PNov 12, 2022 · N463WN · Boeing 7377H4 · Stabilizer Control SystemSDR SWAA2022111570393Relay · inoperativeELECTRIC TRIM INOPERATIVE AFTER TAKEOFF. HORIONTAL STABILIER TRIM. / [01] -SPEED TRIM FAIL LIGHT ILLUMINATES ON RECALL.<BR>-NO C/B?S POPPED.<BR>-FAULT MESSAGE 22-11182. (DFCS BITE);[02] R&R STAB TRIM CUTOUT RELAY (R384) OPS CHECK AND CLOSE UP REQUIRED.;[03] PENov 12, 2022 · N463WN · Boeing 7377H4 · Stabilizer Control SystemSDR SWAA2022100551841Panel · looseEMERGENCY EXIT ROW; FO SIDE; DOOR PANEL LOOSE / [01] RESECURED R/H EMERGENCY EXIT DOOR PANEL PER SIPOct 2, 2022 · N463WN · Boeing 7377H4 · Emergency ExitsSDR SWAA2022100351828Cover · detachedEMERGENCY EXIT LIGHT COVER; FO SIDE OVER WING. DETACHED. / [01] COMPLIED WITH EA-GENERAL M-21-133-00720.Oct 1, 2022 · N463WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022042093382Skin · crackedCRACK ON FIXED LEADING EDGE SKIN AT LEVEL KRUEGER FLAP ACTUATOR 1 2022-148404 / [01] TOOL USED PN NORTEC 500D SN N500X1693P030456 DUE DATE 26-JAN-23;[02] REPAIRED INB FIXED LE SKIN BTW KRAS 166.32 TO KRAS 190.52 (KRUEGER FLAP ACTUATOR 1) IAW E/A 22-157-01102 BApr 12, 2022 · N463WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2022042093384Skin · crackedCRACK ON FIXED LEADING EDGE SKIN AT LEVEL KRUEGER FLAP ACTUATOR 4 2022-148405 / [01] TOOL USED PN NORTEC 500D SN N500X1693P030456 DUE DATE 26-JAN-23;[02] REPAIRED ON INB FIXED LE SKIN BTW KRAS 180.52 & KRAS 190.52 (KRUEGER FLAP ACTUATOR 4) RH WING; IAW EA 22-1Apr 12, 2022 · N463WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2022041992884Angle · crackedCRACK ON WEB INTERCOSTAL LOCATED BTW BS 380 TO BS 400 BL 0 FLOOR STRUCTURE OF PASSENGER CABIN 2022-148402 / [01] REPLACED ANGLE LOC BTW BS 380 TO BS 400 BL0 FLOOR STRUCTURE OF PASSENGER CABIN. IAW B737-700 SRM 51-40-02 AND DWG 143A5400; SHEET 38 AND REV A.;[02Apr 10, 2022 · N463WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022042088650Web · crackedCRACK ON WEB FWD POSITION ON ACCESS PANEL 321A AT VERTICAL STABILIZER 2022-148363 / [01] TOOL USED CALIPER P/N 500-197-30 S/N A18135101 DUE DATE 06-AUG-22 <BR>GAGE RADIUS P/N 06457055 S/N AE-28115 DUE DATE 05-JUL-22;[02] TOOL USED: TEMPERATURE CONTROLLER P/N: Mar 27, 2022 · N463WN · Boeing 7377H4 · Vertical Stabilizer Miscellaneous StructureSDR SWAA2022041993175Seat Track · wornWEAR ON SEAT TRACK BS 520 LBL 45.5 AT PASSENGER CABIN 2022-148311 / [01] REPAIRED SEAT TRACK LOC BS 500C TO BS 520 LBL 45.5 AT PASSENGER CABIN I.A.W B737-700 SRM 53-00-52-2R-4 AND REPAIR IS CATEGORY A AND DOES NOT REQUIRED INSPECTIONS SE INDIVIDUAL SING OFF BEMar 24, 2022 · N463WN · Boeing 7377H4 · Fuselage Internal Mounting StructureSDR SWAA2022041987438Lens · brokenBROKEN EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) 2022-148319 / [01] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-01-960-801 PART USED P/N:207377DME1009;[02] REPLACED EMERGENCY EXIT LIGHT Mar 24, 2022 · N463WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022041987433Tie Down · corrodedCORROSION ON TIE DOWN LOC BS 495 BTW STR 18L TO STR 25L FWD CARGO COMPARTMENT 2022-148308 / [01] REPLACED TIE DOWN LOC BS 495 BTW STR 18L TO STR 25L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02;[02] REPLACED TIE DOWN LOC BS 495 BTW STR 18L TO STR 25L FWD CAMar 23, 2022 · N463WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022042087054Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED WS228.25 AND WS253 AFT POSITION RT WING 2022-148189 / [01] REPLACED ANGLE TRAILING EDGE LOCATED WS228.25 AND WS253 AFT POSITION RT WING IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 P/N USED 115A2982-10 PO 2022-102850.Mar 22, 2022 · N463WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022042087061Access Panel · crackedCRACK ACCESS PANEL 561CB TRAILING EDGE AROUND HOLES LT WING 2022-148237 / [01] TOOL USED CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 01-OCT-22.;[02] TOOL USED MULTIMETER P/N: FLUKE 87 ; S/N: 43050123 ; DUE DATE: 03-FEB-23;[03] REPAIRED ACCESS PANEL 561CB LT Mar 22, 2022 · N463WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022042087072Plate · elongatedELONGATED HOLE PLATE ASSY TRAILING EDGE LOCATED WS204.25 TO WS228.25 RT WING 2022-148246 / [01] REPLACED PLATE ASSY TRAILING EDGE LOCATED WS204.25 TO WS228.25 RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001 SHEET 29 REV-.;[02] REPLACED PLATE ASSY TRAILING EMar 22, 2022 · N463WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022041987068Lens · brokenBROKEN EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) 2022-148243 / [01] REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-01-960-801;[02] CORRECTED STEP 1 : REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREMar 22, 2022 · N463WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022042086155Angle · crackedCRACK DORSAL FIN FWD CLOSURE ANGLE RH SIDE AT VERTICAL STABILIZER 2022-148134 / [01] REPLACED CLOSURE ANGLE AND FASTENERS LOCATED RH SIDE AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02. AND DWG 147A0030. REV. ?B?. SEE INDIVIDUAL SIGN OFFS BELOW;[02] JOB COMPMar 21, 2022 · N463WN · Boeing 7377H4 · Vertical Stabilizer Miscellaneous StructureSDR SWAA2022042086156Angle · crackedCRACK LOWER ANGLE LOCATED BS 663 AT LBL 9 REAR LOWER EDGE IN CENTER FUEL TANK 2022-148140 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23.;[02] REPLACED ANGLE AND FASTENERS LOC BS 663 AND BTW LBL 9 TO LBL 46 RMar 21, 2022 · N463WN · Boeing 7377H4 · Wing, Center BoxSDR SWAA2022042086157Support Bracket · crackedCRACK SUPPORT BRACKET BODY STATION 540 AT LBL6 KEEL BEAM 2022-148142 / [01] REPLACED SUPPORT BRACKET BODY STATION 540 RBL6 KEEL BEAM IAW SRM B737-700 51-10-02. TOOL USED DIGITAL CALIPER P/N: 500-197-30N S/N: A21043225; DUE DATE: 10/AUG/22.;[02] CORRECTED STEP Mar 21, 2022 · N463WN · Boeing 7377H4 · Wing, Center BoxSDR SWAA2022042086158Bracket · crackedCRACK SUPPORT BRACKET BODY STATION 540 RBL6 KEEL BEAM 2022-148145 / [01] REPLACED SUPPORT BRACKET BODY STATION 540 RBL6 KEEL BEAM IAW SRM B737-700 51-10-02. TOOL USED DIGITAL CALIPER P/N: 500-197-30N S/N: A21043225; DUE DATE: 10/AUG/22.;[02] REPLACED SUPPORT BMar 21, 2022 · N463WN · Boeing 7377H4 · Fuselage Main, KeelSDR SWAA2022042086142Plate · crackedCRACK PLATE ASSY TRAILING EDGE LOCATED WS204.25 TO WS228.25 LT WING 2022-148117 / [01] REPLACED PLATE ASSY AND FASTENERS ON TRAILING EDGE LOCATED WS204.25 TO WS228.25 LT WING I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG:115A2001 SHEET:30 REV:A;[Mar 21, 2022 · N463WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022042086145Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED WS228.25 TO WS253 FWD POSITION LT WING 2022-148112 / [01] REPLACED ANGLE TRAILING EDGE LOCATED WS228.25 TO WS253 FWD POSITION LT WING IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A2930 ;SHEET 7 ;REV -.;[02] REPLACED ANGMar 21, 2022 · N463WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022042086143Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED WS228.25 TO WS253 AFT POSITION LT WING 2022-148115 / [01] REPLACED ANGLE TRAILING EDGE LOCATED WS228.25 TO WS253 AFT POSITION LT WING IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02; SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CORRECTED STEMar 21, 2022 · N463WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022041986154Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED AT BS 695 BL0 CENTER SECTION 2022-148133 / [01] TOOL USED RADIUS GAUGE SET P/N: S167C S/N: AE-28454 DUE DATE: 17-JUL-22;[02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 02-FEB-23. TEMPERATUREMar 21, 2022 · N463WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2022041986148Web · corrodedCORROSION WEB LOCATED BS 1028 RBL 9 WL 208.1 AT AFT GALLEY AREA 2022-148125 / [01] REPLACED WEB LOCATED BTW BS 1006 BS 1028; BTW BL 0 TO RBL 40 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 STEP 9 AND DWG:147A5730 SHEET:23 REV:C.;[02] Mar 21, 2022 · N463WN · Boeing 7377H4 · Fuselage Main, Structure
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