N906WN

Service difficulty reports · 276

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 = 'N906WN' 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 SWAA2023100600380Baffle · elongatedFCB BAFFLE BETWEEN BS 500 TO BS 500A LBL25 WL 155 HAS AN ELONGATED HOLE<[01] REPLACED FCB BAFFLE BETWEEN BS 500 TO BS 500A LBL25 WL 155 PER REF SRM 51-40-02 AND DWG 143A7505;[02] VERIFIED MEASUREMENT TABLE.;[03] VERIFIED CORRECTIVE ACTION 1.Sep 13, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023100600384Support · corrodedAFT CARGO BAY AFT BULKHEAD SUPPORT HAS CORROSION AT BS 947; RBL 22; WL 178<[01] THIS STRUCTURAL ITEM DO NOT HAVE ENTRIES FOR ALLOWABLE DAMAGE WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 PARA 9.;[02] REMOVED AND INSTALLED NEW AFT CARGO BAY AFT BULKHEAD SUPSep 13, 2023 · N906WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2023100600385Support · corrodedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727E+15; LBL 22; WL 155<[01] REMOVED AND INSTALLED FLOOR TO SIDEWALL SUPPORT FROM BS 727 TO BS 847<BR>PER SRM 51-40-02 AND DWG 146A7500.;[02] UPDATED MEASUREMENTS.;[03] VERIFIED CORRECTIVE ACTION 1 ANSep 13, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023100600386Support · corrodedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 767 - 727D+5; RBL 22; WL 157<[01] THIS FAUL WILL BE ACCOMPLISHED ON CARD # TTG8Q00NEDL9;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.Sep 13, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023100600390Support · corrodedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727A+14; RBL 22; WL 156<[01] REMOVED AND REPLACED AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT FROM BS 727 TO BS 767 RBL 22 WL 156. IAW SRM 51-40-02 AND DWG 146A7500.;[02] VERIFIED CORRECTIVE ACTION COMPLESep 13, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023100600387Support · corrodedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727D+11 - 727D; LBL 22; WL 155<[01] THIS DISCREPANCY WILL BE ACCOMPLISHED ON CARD TTG8Q00NECTH;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.Sep 13, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023100600388Shield · corrodedAFT CARGO BAY FWD SHIELD HAS CORROSION AT BS 767+11; RBL 24; WL 158<[01] THIS STRUCTURAL ITEM DO NOT HAVE ENTRIES FOR ALLOWABLE DAMAGE WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 PARA 9.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] REMOVED AND INSTALLED NEW FWSep 13, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023100699366Floorbeam · corrodedCORROSION ON FLOOR BEAM AT AFT CABIN BS986 RBL43 WL208. MARKED.<[01] ACCOMPLISHED REPAIR PER SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4;[02] VERIFIED MEASUREMENT TABLE.;[03] VERIFIED CORRECTIVE ACTION 1.Sep 11, 2023 · N906WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2023100699367Floorbeam · corrodedCORROSION ON FLOOR BEAM AT AFT CABIN BS986 LBL43 WL208. MARKED.<[01] REPAIRED FLOOR BEAM PER EA 23-153-02817 AND SRM 53-70-51-2R-6;[02] VERIFIED CORRECTIVE ACTION 1;[03] VERIFIED MEASUREMENT TABLESep 11, 2023 · N906WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2023100699105Stiffener · crackedR/H HORIZONTAL STAB RIB AT STA 120.30 #2 VERTICAL STIFFENER CRACKED AT LOWER END.<[01] VERIFIED STEP 1.;[02] MEASUREMENT TABLE UPDATED.;[03] REMOVED THE DAMAGE PART AT RH HORIZONTAL STABILIZER STA 120.30 RIB 2ND VERTICAL STIFFENER AND INSTALLED REPAIR PARTS IASep 11, 2023 · N906WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2023100699106Stiffener · crackedR/H HORIZONTAL STAB RIB AT STA 120.30 #4 VERTICAL STIFFENER CRACKED AT LOWER END<[01] MEASUREMENT TABLE UPDATED.;[02] REMOVED THE DAMAGE PART AT RH HORIZONTAL STABILIZER STA 120.30 RIB 4TH VERTICAL STIFFENER AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4;[03Sep 11, 2023 · N906WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2023100698173Floor Panel · pulledAFT FLOOR PANEL 242SF UPPER SKIN HAS PULLED STRANDS.<[01] VERIFIED STEPS 3 AND 7.;[02] REPAIRED UPPER SKIN ON AFT FLOOR PANEL 242SF IAW SRM 53-00-50-2R-1.;[03] VERIFIED RII REQUIREMENTS ARE MET.;[04] VERIFIED RII REQUIREMENTS ARE MET.;[05] VERIFIED FLOOR PANELSep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023100698174Floor Panel · pulledAFT FLOOR PANEL 242TF UPPER SKIN HAS PULLED STRANDS.<[01] AFT FLOOR PANEL 242TF UPPER SKIN WITH PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTSSep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023100698180Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF UPPER SKIN WITH PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] VERIFIED CORRECTIVE ACTION #1;[03] TASK COMPLETESep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023100698181Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN HAS PULLED STRANDS.<[01] AFT FLOOR PANEL 241XF UPPER SKIN HAS PULLED STRANDS AND WAS REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED FLOOR PANEL 241XF IS REPAIRED PER SRM 53-00-50-2R-1Sep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023100698182Floor Panel · pulledAFT FLOOR PANEL 241YF UPPER SKIN HAS PULLED STRANDS.<[01] VERIFIED STEPS 3 AND 7.;[02] REPAIRED UPPER SKIN ON AFT FLOOR PANEL 241YF IAW SRM 53-00-50-2R-1.;[03] VERIFIED RII REQUIREMENTS ARE MET.;[04] VERIFIED FLOOR PANEL 241YF IS REPAIRED PER SRM 53-00-50-2R-1Sep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023100698176Floor Panel · pulledAFT FLOOR PANEL 241ZF UPPER SKIN HAS PULLED STRANDS.<[01] AFT FLOOR PANEL 241ZF UPPER SKIN PULLED STRANDS WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED FLOOR PANEL 241ZF IS REPAIRED PER SRM 53-00-50-2R-1 AND VERIFIED THE MEASUREMENT TABLE.Sep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023100698177Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL THE DAMAGE; DECIDED TO FABRICATE A NEW FLOOR PANEL. ROUGH-CUT FLOOR PANEL USING BMS4-17 TYPE VI LOT 1531501-1 AND DETERMINED INSERT HOLE LOCATIONS; WORK PERFORMED IAW SRM 53-00Sep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023100698178Floor Panel · pulledAFT FLOOR PANEL 241ABF UPPER SKIN HAS PULLED STRANDS.<[01] AFT FLOOR PANEL 241ABF UPPER SKIN HAS PULLED STRANDS AND WAS REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED RII INSPECTION REQUIREMENTS ARE MET.;[03] VERIFIED FLOOR PANEL 241ABF WAS REPAIRED PER SRM 53-0Sep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023100698183Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS PULLED STRANDS.<[01] VERIFIED STEP 3;[02] REPAIRED UPPER SKIN ON AFT FLOOR PANEL 241ACF IAW SRM 53-00-50-2R-1.;[03] VERIFIED RII REQUIREMENTS ARE MET.;[04] VERIFIED FLOOR PANEL 241ACF IS REPAIRED PER SRM 53-00-50-2R-1.Sep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023100698184Floor Panel · pulledAFT FLOOR PANEL 241ADF UPPER SKIN HAS PULLED STRANDS.<[01] REPAIRED UPPER SKIN OF AFT FLOOR PANEL 241ADF IAW SRM 53-00-50-2R-1.;[02] COMPLETESep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023100698179Floor Panel · pulledAFT FLOOR PANEL 241AEF UPPER SKIN HAS PULLED STRANDS.<[01] REPAIRED UPPER SKIN DAMAGE ON AFT FLOOR PANEL 241AEF IAW SRM 53-00-50-2R-1.;[02] COMPLETESep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023100698185Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SKIN HAS PULLED STRANDS.<[01] REPAIRED DAMAGED UPPER SKIN ON FWD FLOOR PANEL 221CF IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] JOB COMPLETE.Sep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023100698460Stringer · crackedAREA AFT OF FWD CARGO BAY HAS A CRACKED STR AT THE AFT FASTENER; STR 26R; BS 520+19; WL 152<[01] REPAIRED FCB STR 26R BETWEEN BS 500D AND BS 540 IAW SRM 53-00-03-2R-1 REPAIR 1;[02] VERIFIED MEASUREMENTS FIELDS.Sep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023100608401Stringer Splice · crackedAREA AFT OF FWD CARGO BAY HAS A CRACKED STR AT THE AFT FASTENER; STR 26L; BS 520+19; WL 152<[01] VERIFIED APPLICABILITY PER REF SRM 53-00-03-2R-1;[02] VERIFIED NDT HFEC INSPECTION COMPLETED IN SUB-STEP 2; COMPLETES THE REQUIREMENTS OF SRM SRM 53-00-03-2R-1 STESep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023100698461Stringer · crackedAREA AFT OF FWD CARGO BAY HAS A CRACKED STR AT THE AFT FASTENER; STR 26L; BS 520+19; WL 152<[01] VERIFIED APPLICABILITY PER REF SRM 53-00-03-2R-1;[02] VERIFIED NDT HFEC INSPECTION COMPLETED IN SUB-STEP 2; COMPLETES THE REQUIREMENTS OF SRM SRM 53-00-03-2R-1 STESep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023100698175Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS PULLED STRANDS.<[01] AFT FLOOR PANEL 242UF UPPER SKIN WITH PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] VERIFIED ACTION 1 CARD COMPLETE.;[03] VERIFIED ACTION 1. CARD COMSep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023100698466Support · corrodedFWD CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 500C+8; RBL 24; WL 155<[01] THIS JOB CARD WILL BE ACCOMPLISHED ON CUSTOMER CARD [TTG8QNAXX7] .;[02] VERIFIED CORRECTIVE ACTION 1.;[03] VERIFIED MEASUREMENTS.<BR>JOB COMPLETE.Sep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023100698462Support · corrodedFWD CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 500A+3; RBL 24; WL 155<[01] REMOVED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT FROM BS 500A TO BS 500D RBL 24 PER SRM 51-40-02 AND DWG 143A7500;[02] VERIFIED CORRECTIVE ACTION 1.<BR>VERIFIED MEASUREMSep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023100698463Shield · corrodedFWD CARGO BAY SHEILD HAS CORROSION AT BS 500+19; RBL 24; WL 155<[01] VERIFIED STEP 1 AND MEASUREMENT TABLE.;[02] REMOVED AND INSTALLED NEW FWD CARGO BAY SHEILD BETWEEN BS 492 TO BS 500A RBL 24 PER SRM 51-40-02 AND DWG 143A0080;[03] VERIFIED CORRECTIVE ACTION 2Sep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023100698464Support · corrodedFWD CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 500A+6; LBL 25; WL 155<[01] REMOVED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT BETWEEN BS400 TO BS500D LBL25 IAW SRM 51-40-02; SRM 53-00-53-2R-6 REPAIR 6; DWG 143A7501 AND DWG 143A7500;[02] VERIFIED Sep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023100698467Shield · corrodedFWD CARGO BAY SHEILD HAS CORROSION AT BS 420+16; RBL 24; WL 155<[01] VERIFIED STEP 1 AND MEASUREMENT TABLE.;[02] REMOVED AND INSTALLED FWD CARGO BAY SHIELD BS 420 AT BS 440 RBL 24 IAW SRM 51-40-02 AND DWG 143A0080;[03] VERIFIED MEASUREMENTS.<BR>JOB COMPLETE.Sep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023100698468Support · corrodedFWD CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 400+9; RBL 24; WL 155<[01] REMOVED AND REPLACED FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT PER REF SRM 51-40-02 AND DWG NBR 143A7500;[02] VERIFIED CORRECTIVE ACTION COMPLETE. VERIFIED MEASUREMENT TABLE CSep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023100598458Attach Angle · crackedFWD CARGO INTERCOSTAL ATTACH ANGLE IS CRACKED; COMMON TO FLOOR TO SIDEWALL SUPPORT AT BS 480; LBL 25; WL 155; (MARKED)<[01] REMOVED AND REPLACED FWD CARGO INTERCOSTAL ATTACH ANGLE PER REF SRM 51-40-02 AND DWG NBR 143A7502;[02] VERIFIED CORRECTIVE ACTION COMPLESep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2023100598459Sidewall Support · pulledFWD CARGO INTERCOSTAL HAS A PULLED THROUGH RIVET COMMON TO FLOOR TO SIDEWALL SUPPORT AT BS 500C; LBL 25; WL 155 (MARKED)<[01] VERIFIED APPLICABILITY PER SRM 53-30-53-0I-2 IDENTIFICATION. BAFFLE OPEN HOLES DOES NOT MEET HOLE QUALITY SPECIFICATION PER SRM 51-40-Sep 8, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023100997855Bulkhead · crackedRIGHT STATION 663 COMPOSITE BULKHEAD IS CRACKED AT WL 157 RB; 30.<[01] RIGHT STATION 663 COMPOSITE BULKHEAD; WITH CRACK AT WL 157 RB; 30; WAS REPAIRED IAW SRM 51-70-04-2R-10.;[02] VERIFIED CORRECTIVE ACTION #<BR>VERIFIED MEASUREMENTSSep 7, 2023 · N906WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2023100997713Bulkhead · crackedRIGHT STATION 663 COMPOSITE BULKHEAD IS CRACKED AT WL 157; RB; 30.<[01] THE CRACK AT B.S.663 RBL 30 WL 157 WILL BE REPAIRED ON FAULT TTG8Q00NABLL;[02] THE CRACK AT B.S.663 RBL 30 WL 157 WILL BE REPAIRED ON FAULT TTG8Q00NABLL;[03] VERIFIED CORRECTIVE ACTION ITESep 7, 2023 · N906WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2023100698164Intercostal · crackedCABIN FWD WET AREA HAS A CRACKED INTERCOSTAL AT BS 328+14; RBL 19; WL 208 (MARKED) BS 328+14 RBL 19 IS INCORRECT; BS 312-328 RBL 31 IS CORRECT<[01] REMOVED AND INSTALLED NEW INTERCOSTAL P/N 141A5410U12 AT FLOOR STRUCTURE BETWEEN BS 312 TO BS 328 RBL 31 PER SRMSep 7, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023100697711Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS PULLED STRANDS.<[01] FLOOR PANEL 231XF UPPER SKIN WITH PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] REMOVED AND INSTALLED FLOOR PANEL 231XF IAW AMSep 7, 2023 · N906WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023100697709Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS PULLED STRANDS.<[01] FLOOR PANEL 241AF UPPER SKIN WITH PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.Sep 7, 2023 · N906WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023100697712Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 241DF WAS REPLACED WITH A NEW SERVICEABLE UNIT IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION 1.Sep 7, 2023 · N906WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023100997397Attach Angle · crackedWING CENTER SECTION HAS A CRACKED CABLE INTERCOSTAL ATTACH ANGLE AT BS 685+9; WL 203; RBL 24<[01] CORRECTED MEASUREMENT FIELD ITEM 5;[02] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE <BR>AT BS 685+9; WL 203; RBL 24 WING CENTER SECTION<BR>I.A.W SRM 51-40-02-0GSep 6, 2023 · N906WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2023100697238Stiffener · crackedLEFT HORIZONTAL STAB RIB 5 #3 STIFFENER LOWER RADIUS IS CRACKED.<[01] MEASUREMENT TABLE UPDATED.;[02] REMOVED THE DAMAGE PART AT LH HORIZONTAL STABILIZER STA 129.50 RIB 3RD VERTICAL STIFFENER AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4;[03] VERIFIED CORRESep 6, 2023 · N906WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2023100697239Stiffener · crackedR/H HORIZONTAL STAB RIB 4 STIFFENER #3 LOWER RADIUS IS CRACKED.<[01] MEASUREMENT TABLE UPDATED.;[02] REMOVED THE DAMAGE PART AT RH HORIZONTAL STABILIZER STA 120.30 RIB 3RD VERTICAL STIFFENER AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4;[03] VERIFIED CORRECSep 6, 2023 · N906WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2023100697396Angle · crackedWING CENTER SECTION HAS A CRACKED CABLE INTERCOSTAL ATTACH ANGLE AT BS 685+9; WL 203; LBL 24<[01] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE <BR>AT BS 685+9; WL 203; LBL 24 WING CENTER SECTION <BR>I.A.W SRM 51-40-02-0G-0 AND DWG 273A9111.<BR>VERIFIED CUSTOMSep 6, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023061659230Intercostal · crackedFLOOR PANEL BREAK(INTERCOSTAL) RIGHT OF CENTER AT STA 540 IS CRACKED; IN THE A/C DISTRIBUTION BAY<[01] REMOVED AND REPLACED INTERCOSTAL AT B.S.540 JUST RIGHT OF CENTER PER SRM 51-40-02.Jun 15, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023061659227Intercostal · crackedFLOOR PANEL BREAK(INTERCOSTAL) LEFT OF CENTER AT STA 540 IS CRACKED; IN THE A/C DISTRIBUTION BAY<[01] LOCATED AND DRILLED NEW INTERCOSTAL IAW 737 SRM 51-40-05;[02] REMOVED AND REPLACED FLOOR PANEL BREAK INTERCOSTAL LEFT OF CENTER AT STA 540 PER SRM 51-40-02Jun 15, 2023 · N906WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023061559224Battery Pack · failedEMERGENCY LIGHT BATTERIES AT LOCATIONS M1673 (AFT LEFT) AND M1675 (FWD LEFT) FAILED CAPACITY TEST<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AT LOCATIONS M1673 (AFT LEFT) AND M1675 (FWD LEFT); OPS TEST GOOD. PER AMM 33-51-06Jun 15, 2023 · N906WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023061559228Girt Bar · out of adjustFWD GALLEY SERVICE DOOR RH GIRT BAR HANGER LOOSE<[01] REMOVED AND REPLACED FWD GALLEY SERVICE DOOR RH GIRT BAR HANGER RIVET REF SRM 51-40-02.Jun 15, 2023 · N906WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2023050243353Slide · failedAFT ENTRY DOOR SLIDE BOX OPENED WHILE PROVO WAS ENTERING SLIDE DID NOT DEPLOY<[01] REINSTALLED EMER EXIT SLIDE TO AFT ENTRY DOOR AMM 25-66-01Apr 28, 2023 · N906WN · Boeing 7377H4 · Escape Slide
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