Boeing 737-76N

Service difficulty reports · 4,807

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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 aircraft_model_key = '73776N'
  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 SWAA2024040559584Panel · crackedLT WING T/E PANEL 561BB AFT ROW OF FASTENER HOLES HAVE CRACKS AT HOLES<[01] LEFT WING TRAILING-EDGE PANEL 561BB AFT ROW OF FASTENER HOLES WITH CRACKS AT HOLES WAS REPAIRED IAW SRM 51-70-04-2R-9.;[02] VERIFIED CORRECTIVE ACTION #1Mar 6, 2024 · N7731A · Boeing 73776N · Wing, Plate/SkinSDR SWAA2024040459578Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ACF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1Mar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459580Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED FLOOR PANEL 242VF UPPER SKIN DAMAGE HAS BEEN REPAIRED IMar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459588Floor Panel · pulledFWD FLOOR PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PULLED STRANDS ON UPPER SKIN OF PANEL 221EF HAVE BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED PANEL 221EF HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[03] WORKSCOPE IS COMPLETE.Mar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459589Floor Panel · pulledFWD FLOOR PANEL 222AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222AF HAVE BEEN REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED UPPER SKIN OF FLOOR PANEL 222AF HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1;[03Mar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459596Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222BF UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED FLOOR PANEL 222BF UPPER SKIN DAMAGE HAS BEEN REPAIRED IMar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459597Floor Panel · pulledCABIN FLOOR PANEL 231FF HAS PULLED STRANDS.<[01] CABIN FLOOR PANEL 231FF WITH PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1Mar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459991Floorbeam · corrodedBS 986 FLOOR BEAM HAS CORROSION AROUND OUTBOARD R/H FASTENER HOLE; RBL 43; WL 208<[01] VERIFIED STEPS 2;7 COMPLETED.;[02] VERIFIED DVI; STEP 8 COMPLETE.;[03] 'REFER TO FAULT TTG8Q00S04MW FOR REPAIR RESOLUTION' PER EA# 24-153-00653-WIP1 STEP 1;[04] ' EA-GENERALMar 6, 2024 · N7731A · Boeing 73776N · Fuselage Main, Floor BeamSDR SWAA2024040459571Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE; FABRICATED NEW 231XF FLOOR PANEL FROM BMS4-17 TYPE 6 LOT#1555604-2; INSERTS INSTALLED USING BMS5-107 LOT#AK3BA2380A-A THEN CURED USING HEAT LAMP AND THERMOMETER ATS2209Mar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459572Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE; FABRICATED NEW 241AF FLOOR PANEL FROM BMS4-17 TYPE 6 LOT#1555604-2; INSERTS INSTALLED USING BMS5-107 LOT#AK3BA2380A-A THEN CURED USING HEAT LAMP AND THERMOMETER ATS2209Mar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459574Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241DF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS RELACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0128.;[02] VERIFIED Mar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459573Floor Panel · pulledFLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242CF 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:0153.;[02] VERIFIEDMar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459577Floor Panel · pulledAFT FLOOR PANEL 241ABF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ABF UPPER SKIN WITH AREAS OF 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] VERIFIED CORRECTIVMar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459579Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242UF UPPER SKIN WITH AREAS OF 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] VERIFIED CORRECTIVE Mar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459585Floor Panel · pulledFWD FLOOR PANEL 221AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED FWD FLOOR PANEL 221AF IAW SRM 51-10-02-0G-0 PARA 9; AIPC 53-21-51-75 ITEM 65 AND MODIFIED PER DWG D1040M002.;[02] VERIFIED CORRECTIVE ACTION 1.Mar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459586Floor Panel · pulledFWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF UPPER SKIN WITH AREAS OF 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] VERIFIED CORRECTIVE Mar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459594Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221CF UPPER SKIN WITH AREAS OF 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] VERIFIED CORRECTIVE Mar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459587Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221DF UPPER SKIN WITH AREAS OF 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] VERIFIED CORRECTIVE Mar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459591Floor Panel · pulledCABIN FLOOR PANEL 241UF HAS PULLED STRANDS.<[01] FABRICATED 241UF FLOORBOARD PANEL IAW SRM 53-00-50-2R-0 ALONG WITH DWG:146A5810 SHEET: 54;[02] VERIFIED FABRICATION OF FLOOR PANEL 241UF PER SRM 53-00-50-2R-0 ALONG WITH DWG:146A5810 SHEET: 54Mar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459592Floor Panel · pulledCABIN FLOOR PANEL 241WF HAS PULLED STRANDS.<[01] CABIN FLOOR PANEL 241WF WITH PULLED STRANDS WAS REPLACED BY FABRICATION IAW SRM 53-00-50-2R-0 AND DRAWING 146A5810 SHEET 28.;[02] VERIFIED CORRECTIVE ACTION #1Mar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459593Floor Panel · pulledCABIN FLOOR PANEL 231JF HAS PULLED STRANDS.<[01] FLOOR PANEL 231JF WITH PULLED STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 143A5810 ID:0138;[02] VERIFIED FLOOR PANEL 231JF WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-Mar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040459598Floor Panel · pulledCABIN FLOOR PANEL 231MF HAS PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED CABIN FLOOR PANEL 231MF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-09A ITEM 277.;[02] VERIFIED CORRECTIVE ACTION 1.Mar 6, 2024 · N7731A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024040559033Panel · crackedRT WING T/E PANEL 661BB AFT ROW OF FASTENER HOLES HAVE CRACKS AROUND HOLE<[01] RIGHT WING TRAILING-EDGE PANEL 661BB AFT ROW OF FASTENER HOLES WITH CRACKS AROUND HOLES WERE REPAIRED IAW SRM 51-70-04-2R-9.;[02] VERIFIED CORRECTIVE ACTION #1Mar 5, 2024 · N7731A · Boeing 73776N · Wing, Plate/SkinSDR SWAA2024040462290Vapor Barrier · crackedR/H B/S 663 VAPOR BARRIER IS CRACKED AT RBL 34 WL 157<[01] R/H B/S 663 VAPOR BARRIER IS CRACKED AT RBL 34 WL 157 WAS REPAIRED IAW SRM 51-70-04-2R-10.;[02] VERIFIED REPAIR OF THE R/H B/S 663 VAPOR BARRIER IAW SRM 51-70-04-2R-10.Mar 5, 2024 · N7731A · Boeing 73776N · Fuselage Main, BulkheadSDR SWAA2024040459306Vapor Barrier · crackedL/H B/S 663 VAPOR BARRIER IS CRACKED AT LBL 33 WL 166<[01] L/H VAPOR BARRIER CRACKS AT BS 663 LBL 33 WL 166 WERE REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED L/H VAPOR BARRIER CRACKS AT BS 663 LBL 33 WL 166 WERE REPAIRED IAW SRM 51-70-04-2R-10;[03] WORKSCOPE Mar 5, 2024 · N7731A · Boeing 73776N · Fuselage Main, BulkheadSDR SWAA2024040459310Web · corrodedCORROSION; FCB SUBTHRESHOLD BS480+1; RBL28; WL156<[01] VERIFIED STEP 1 COMPLETE.;[02] VERIFIED STEP 5 COMPLETE; STEP 6 IN PARTIAL.;[03] REMOVED AND REPLACED FCB SUBTHRESHOLD WEB WL156 I.A.W SRM 51-10-02-0G-0 AND SRM 51-40-02-0G-0 AND DWG 143A8330.Mar 5, 2024 · N7731A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024040559031Web · crackedRIGHT WING; TRANSVERSE WEB IS CRACKED; UPPER LEG; O/B END ABOVE #2 PYLON AFT TIP<[01] REMOVED AND REPLACED RIGHT WING; TRANSVERSE WEB AT UPPER LEG; O/B END ABOVE #2 PYLON AFT TIP IAW SRM 51-40-02; AIPC 57-50-00-36A AND DWG 115A2512;[02] VERIFIED CORRECTIVE ACTMar 4, 2024 · N7731A · Boeing 73776N · Wing, Plate/SkinSDR SWAA2024022856245Sign · detachedOVERWING EMERGENCY EXIT SIGN FOUND DETACHED<[01] CELING PANEL OVERWING AIRCRAFT LEFT LOWERED TO FOM REF AMM 25-21-45;[02] REMOVED AND REPLACED CEILING OVERWING EXIT SIGN ASSY. AMM 33-51-01. OPS CHECK GOOD. REINSTALLED CEILING PANEL OVER THE L/H OVERWING EXIT IFeb 26, 2024 · N7725A · Boeing 73776N · Emergency LightingSDR SWAA2024022053651Slide · unsecureFWD ENTRY EMER SLIDE CASING CAME LOOSE WHEN OPENING DOOR<[01] ACCOMPLISHED MT 725-61-06 REM/INSTL PER M/M 25-66-01Feb 18, 2024 · N7822A · Boeing 73776N · Escape SlideSDR SWAA2024020648255Girt Bar · looseFORWARD L1 DOOR GIRT BAR LOOSE<[01] ADJUSTED L1 DOOR GIRT BAR PER SIPFeb 3, 2024 · N7812G · Boeing 73776N · Emergency EquipmentSDR SWAA2024020247472Lens · missingFWD OVHD EMERGENCY LIGHT LENS MISSING/ FIXTURE BROKEN IN RECESSED CEILING PANEL @ ROW 2 SEE ATTACHED PHOTOS<[01] R&R FWD OVHD EMERGENCY LIGHT ASSY PER C.M.M. 33-30-41 OPS CHECK NORMALFeb 1, 2024 · N7725A · Boeing 73776N · Emergency LightingSDR SWAA2024020247449Battery Pack · inoperativeR1 SLIDE EMERGENCY LIGHT INOP<[01] R/R M1674 BATTERY PACK PER AMM 33-51-06Feb 1, 2024 · N7884G · Boeing 73776N · Emergency LightingSDR SWAA2024020547052Girt Bar · chafedAFT ENTRY DOOR (L-2) GIRT BAR SKIRT RUBBING AGAINST THRESHOLD WHEN OPENING AND CLOSING DOOR.<[01] JOB ACCOMPLISHED ON TTG8Q00R9LS3;[02] VERIFIED CORRECTIVE ACTION.Jan 31, 2024 · N7727A · Boeing 73776N · Emergency EquipmentSDR SWAA2024020547053Girt Bar · chafedAFT SERVICE DOOR (R-2) GIRT BAR SKIRT RUBBING AGAINST THRESHOLD WHEN OPENING AND CLOSING DOOR.<[01] JOB ACCOMPLISHED ON TTG8Q00R9LWJ.;[02] VERIFIED CORRECTIVE ACTION.Jan 31, 2024 · N7727A · Boeing 73776N · Emergency EquipmentSDR SWAA2024021346663Scuff Plate · crackedCORNER FWD CARGO FWD SCUFF PLATE CRACKED REF TTG8Q00R6V17 CORRECTION NOTE REF TO TTG8Q00R7WMD<[01] RECEIVED REPAIRED FORWARD CORNER SCUFF PLATE PN 143A8331-3 FROM JL WELDING REF WO 16523 & OREDER# 414492.;[02] VERIFIED RECEIVEDJan 30, 2024 · N7811F · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024021346664Scuff Plate · crackedCORNER FWD CARGO AFT SCUFF PLATE HAS CRACK REF TTG8Q00R7WMD<[01] RECEIVED REPAIRED FORWARD CARGO DOOR AFT SCUFF PLATE PN 143A8331-4 FROM JL WELDING WO# 16524 AND ORDER # 414493.;[02] VERIFIED RECEIVEDJan 30, 2024 · N7811F · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024020246219Connector · disconnectedL2 EXTERIOR EMERGENCY LIGHT INOP<[01] PERFORMED TROUBLESHOOTING AS PER B737 WDM 33-51-14. FOUND CONNECTOR D11086 DISCONNECTED. CONNECTOR D11086 WAS CONNECTED PROPERLY AS PER B737 AMM 33-51-04-960-802; SUBTASK 33-51-04-420-002. TEST PASSED AS PER B737 AMM TASK Jan 30, 2024 · N7727A · Boeing 73776N · Light System WiringSDR SWAA2024020545213Tee Angle · crackedLT W/W APPROX. STA 727 LBL 20 W/W STRUCTURE LOWER T CLIP IS CRACKED AT LOWER END.<[01] REMOVED AND REPLACED LOWER T CLIP AT LT W/W APPROX. STA 727 LBL 20 SRM 51-40-02-0G-0 AND DWG149A7601;[02] VERIFIED LOWER T CLIP REPLACEMENTJan 27, 2024 · N7727A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024020545212Support Angle · crackedLT W/W APPROX. STA 727 LBL 20 W/W STRUCTURE SUPPORT VERTICAL ANGLE IS CRACKED AT LOWER END. 124-010<[01] REMOVED CRACK ANGLE AT L/H W/W APPROX. STA. 727 AND LBL 20 PER REF SRM 51-40-02-0G-0; FABRICATED NEW ANGLE AT L/H W/W APPROX. STA 727 LBL 20; PER. DRAWING Jan 26, 2024 · N7727A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024020244789Battery Pack · inoperativeSEVERAL EMERGENCIES LIGHT INOP AT MAIN CABIN. SEVERAL EMERGENCY LIGHTS INOP AT MAIN CABIN.<[01] PERFORMED T/S OF THE EMERGENCY LIGHTS; FOUND M1672 AND M1673 DEFECTS. REF. TO FIM 33-50- TASK 801. (J. (2)).;[02] VERIFIED STEP 1;[03] REMOVED AND REPLACED EMERGENCJan 26, 2024 · N7727A · Boeing 73776N · Emergency LightingSDR SWAA2024020244046Pin · out of positionG1 GALLEY EMERGENCY EXIT LIGHT WIRE BROKEN AT CONNECTOR G1 GALLEY LOWER EMERGENCY EXIT SIGN INOP<[01] REMOVED AND REINSTALLED G1 GALLEY EMERGENCY EXIT LIGHT L1186; FOUND CONNECTOR PIN PUSHED BACK; RESECURED PIN CONNECTOR D3658 PER REF SWPM 20-60-01 WDM 33-51-2Jan 24, 2024 · N7727A · Boeing 73776N · Light System WiringSDR SWAA2024020543680Panel · crackedCRACK - AT UPPER AFT CORNER (PANEL 192BR FAIRING- UNDERWING RIGHT FAIRING ABOVE A/C DOOR)<[01] REPAIRED PANEL #192BR AT DAMAGD AREA PER B737 SRM 51-70-04-2R-2; SRM 51-70-04-2R-0 PARA 4.L.7. MATERIALS USED RESIN P/O#1791128; CLOTH P/O#1690463; GRAPHI P/O#204306Jan 22, 2024 · N7727A · Boeing 73776N · Aerodynamic FairingsSDR SWAA2024020542629Access Panel · crackedL/H WING UPPER I/B ACCESS PANEL 551 DT CRACK AT T/E<[01] APPLIED REPAIR AT PANEL#551DT PER B737 SRM 51-70-04-2R-0 PARAGRAPH 4.N MATERIAL USED RESIN EY 3804 PO#20400614 FIBERGLASS PO#1690463.;[02] VERIFIED STEP 1Jan 19, 2024 · N7727A · Boeing 73776N · Wing, Plate/SkinSDR SWAA2024012442542Connector · disconnectedR2 DOOR EMERGENCY UPPER EXIT SIGN LIGHT INOPERATIVE.<[01] RECONNECT CONNECTOR D12448 AS PER REF B737 WDM 33-51-13. PERFORMED EXIT SIGN LIGHT OPERATIONAL TEST FOUND NORMAL AS PER REF AMM 33-51-01-960-802.;[02] VERIFIED STEP 1Jan 19, 2024 · N7725A · Boeing 73776N · Light System WiringSDR SWAA2024012442543Lamp · inoperativePASSENGER EMERGENCY OVERHEAD BIN LIGHT AT ROW 9L/H INOPERATIVE.<[01] RELAMPED PASSENGER EMERGENCY OVERHEAD BIN LIGHT AT ROW 9L/H AS PER AMM 33-51-03-960-801. TEST OK.;[02] VERIFIED STEP 1.Jan 19, 2024 · N7725A · Boeing 73776N · Emergency LightingSDR SWAA2024012442544Lamp · inoperativeR1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] RELAMPED R1 DOOR EXTERIOR EMERGENCY LIGHT AS PER AMM 33-51-04-960-801. TEST OK;[02] VERIFIED STEP 1.Jan 19, 2024 · N7725A · Boeing 73776N · Emergency LightingSDR SWAA2024012442541Battery Pack · inoperativePASSENGER EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACKS M1668 AND M1669 INOPERATIVE.<[01] REMOVED AND INSTALLED A NEW EMERGENCY BATTERY PACK AT POSITION M1669 AS PER AMM 33-51-06-960-805. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT POSITION M1668 AS PER REJan 19, 2024 · N7725A · Boeing 73776N · Emergency LightingSDR SWAA2024020241577Strap · corroded*CORROSION* AFT CARGO FLOOR SUPPORT STRAP AT STA 767 BETWEEN LBL 21 AND RBL 21 WL 156.3<[01] FOUND EXFOLIATED CORROSION OUT OF LIMITS AT AFT CARGO FLOOR SUPPORT STRAP AT STA 767 BETWEEN LBL 21 AND RBL 21 WL 156.3 PER SRM 53-00-53-1A-2.<BR>RECEIVED NEW AFT CARGJan 16, 2024 · N7727A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024020241576Strap · corroded*CORROSION* AFT CARGO FLOOR SUPPORT STRAP AT STA 727D BETWEEN LBL 21 AND RBL 21 WL 156.3<[01] FOUND EXFOLIATED OUT OF LIMITS CORROSION AT AFT CARGO FLOOR SUPP STRAP AT 727D BETWEEN LBL 21 AND RBL 21 WL 156.3 PER SRM 53-00-53-1A-2.<BR>RECEIVED NEW FLOOR STRAP PJan 16, 2024 · N7727A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024020540175Stringer · debondedAFT CABIN CEILING AT STA 787 STR16L STRINGER COVERS DISBONDED. AFT CABIN L/H SIDE AT STA 787 STR16L STRINGER COVERS DISBOMDED<[01] REBONDED STRINGER COVERS AT AFT CABIN CEILING AT STA 787 STR 16L REF SOPM 20-50-12;[02] CORRECTION TO STEP 1: REBONDED STRINGER CJan 11, 2024 · N7727A · Boeing 73776N · Fuselage Main, Longeron/Stringer
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