Boeing 737-79P

Service difficulty reports · 2,376

Newest first. 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'
  WHERE aircraft_model_key = '73779P'
  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 SWAA2023102099581Strap · corrodedCORROSION ON STRAP LOCATED BS 1006 TO BS 1040 RBL 3 AND WL 208.1 AT AFT GALLEY AREA 2023-577885<[01] REPLACED STRAP AND FASTENERS LOCATED BETWEEN BS 1006 TO BS 1040 RBL 3 AND WL 208.1 AT AFT GALLEY AREA I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG# 147A5730; SHEETSep 12, 2023 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023092199509Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] WELDED AFT CARGO BAY AFT CORNER SCUFF PLATE PER SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2); (4); (5) USING ER4043 FILLER ROD LOT NUMBER 1131216<BR>EQUIPMENT USED ; WELDING MACHINE E10583 CALIBRATION DUE DATE 01/20Sep 12, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023092199508Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<Sep 12, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023101798941Slide · out of adjustFWD ENTRY DOOR. L1. SLIDE PRESSURE VISOR IS TORN.<[01] RECEIVED PART AND INSTALLATION WILL BE ACCOMPLISHED ON T/C MT 725-61-06;<BR>SLIDE REM/INSTL TTG8Q00NC3V2;[02] VERIFIED STEP 1Sep 11, 2023 · N7833A · Boeing 73779P · Escape SlideSDR SWAA2023101799116Sidewall Support · elongatedFWD CABIN WET AREA L/H SIDE WALL SUPPORT CLIP HOLE ELONGATED @ S-10L STA 270 MKD DOT<[01] REMOVED AND REPLACED SUPPORT CLIP AT FWD CABIN WET AREA L/H SIDE WALL; STA 270; S-10L AS PER B737-700 SRM 51-40-02-0G-0; DWG# 141A9502.;[02] VERIFIED STEP 1 REMOVAL AND RSep 11, 2023 · N7833A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023101799112Floor Support · crackedMAIN CABIN CENTER WING BOX FLOOR SUPPORT BREAK CRACKED AT FASTENER'S TAIL RBL 1 STA 540<[01] REMOVED AND REPLACED SUPPORT BREAK ASSY AT MAIN CABIN STA 540 BETWEEN BL 0 TO RBL 24 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 143A0060.;[02] VERIFIED STEP 1 COMPLETE.Sep 11, 2023 · N7833A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023101799114Angle · corrodedCORROSION AT RIVETS TAILS 4EA ATTACHED ANGLE ABOVE L-1 DOOR STA 328<[01] REMOVED AND REPLACED 4EA RIVETS AT UPPER FUSELAGE SKIN ATTACHED ANGLE ABOVE L-1 DOOR STA 328 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 141A8240.;[02] VERIFIED STEP 1 COMPLETE.Sep 11, 2023 · N7833A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023101799115Angle · corrodedCORROSION AT SEVERAL RIVETS TAILS ATTACHED ANGLE ABOVE L-1 DOOR STA 328+ 10' MKD DOT<[01] REMOVED AND REPLACED RIVETS AT UPPER FUSELAGE SKIN ATTACHED ANGLE ABOVE L-1 DOOR STA 328+10' REF B737-700 SRM 51-40-02-0G-0 AND DWG # 141A8240.;[02] VERIFIED S5EP 1 COMPLSep 11, 2023 · N7833A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023092899197Scuff Plate · crackedAFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] REPAIRED THE CORNER SCUFF PLATE PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(4) AND BAC 5975 APPLIED A CHEMICAL CONVERSION COATING TO BARE ALUMINUM SURFACES PER SOPM 20-43-03; TYPE 2; CLASS A OR C AND SRM 53-60Sep 11, 2023 · N7861J · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023102098919Bracket · crackedCRACK SUPPORT BRACKET ON TRAILING EDGE LOCATED ORSS273 AT LT WING 2023-577831<[01] REPLACED SUPPORT BRACKET ON TRAILING EDGE LOCATED ORSS273 AT LT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. DWG: 115A2900 SHEET: 1 REV: E<BR><BR>CRACK LENGTH IS: Sep 10, 2023 · N7862A · Boeing 73779P · Wing Miscellaneous StructureSDR SWAA2023102098920Bracket · crackedCRACK TRAILING EDGE SUPPORT BRACKET LOCATED ORSS273 INTERNAL AREA AT RT WING 2023-577836<[01] REPLACED SUPPORT BRACKET LOCATED ORSS273 INTERNAL AREA AT RT WING IAW B737-700 SRM 51-10-02 Ï¿½TEM 9.;[02] CORRECTED STEP 1.<BR>REPLACED SUPPORT BRACKET LOCATED ORSS2Sep 10, 2023 · N7862A · Boeing 73779P · Wing Miscellaneous StructureSDR SWAA2023102098918Web · crackedCRACK WEB TRAILING EDGE ON AREA OF DEFLECTION CONTROL RIB BEAM ATTACHMENT ORSS278 LT WING 2023-577830<[01] REPLACED WEB LOCATED TRAILING EDGE ON AREA OF DEFLECTION CONTROL RIB BEAM ATTACHMENT ORSS278 LT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02Sep 10, 2023 · N7862A · Boeing 73779P · Wing Miscellaneous StructureSDR SWAA2023102098923Floorbeam · crackedCRACK FLOOR BEAM LOCATED STA 294.5 AND RBL 54 AT FWD GALLEY AREA 2023-577850<[01] TOOL USED EDDY CURRENT P/N: NORTEC 600D; S/N: 210138203; DUE DATE: 09-JUN-24.;[02] TOOL USED: RADIOMETER PHOTOMETER P/N: XRP-3000; S/N: 1753759; CAL DUE DATE: 14-OCT-23;[03] TOOLSep 10, 2023 · N7862A · Boeing 73779P · Fuselage Main, Floor BeamSDR SWAA2023101998922Frame · crackedCRACK FRAME ON BS 312 LOCATED BTW STR 5L TO STR 6L FWD GALLEY AND LAV 2023-577847<[01] PERFORMED PERMANENT REPAIR ON INNER CHORD OF FRAME BS312 BTW STR5L TO STR6L AT FWD GALLEY I.A.W. EA M-22-153-01244<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] CERTIFIED WORK PSep 10, 2023 · N7862A · Boeing 73779P · Fuselage Main, FrameSDR SWAA2023101798929Floor Support · crackedBELOW CABIN FLOOR SUPPORT BREAK CRACKED AT CENTER WING BOX LBL 2 STA 540<[01] REMOVED AND REPLACED SUPPORT BREAK ASSY AT MAIN CABIN STA 540 BETWEEN BL 0 TO LBL 24 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 143A0060.;[02] VERIFIED STEP 1 REMOVAL AND REPLACEMENT OFSep 10, 2023 · N7833A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023102098453Panel · crackedCRACK ACCESS PANEL 661AB TRAILING EDGE AT RT WING 2023-577757<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: A18135081; DUE DATE: 21-JUL-24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 24/JAN/24.;[03] TOOL USED HOTBONDER P/N: HCS9200B-AV Sep 9, 2023 · N7862A · Boeing 73779P · Wing, Plate/SkinSDR SWAA2023102098439Panel · crackedCRACK ACCESS PANEL 661CB TRAILING EDGE AT RT WING 2023-577763<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: A18135081; DUE DATE: 21-JUL-24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 24/JAN/24.;[03] TOOL USED HOTBONDER P/N: HCS9200B-AV Sep 9, 2023 · N7862A · Boeing 73779P · Wing, Plate/SkinSDR SWAA2023102098455Panel · crackedCRACK ACCESS PANEL 561BB TRAILING EDGE AT LT WING 2023-577759<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: A18135081; DUE DATE: 21-JUL-24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 24/JAN/24.;[03] TOOL USED HOTBONDER P/N: HCS9200B-AV Sep 9, 2023 · N7862A · Boeing 73779P · Wing, Plate/SkinSDR SWAA2023102098720Floor Panel · crackedCRACK INNER CHORD LOCATED BTW STA 294.5 TO STA 312 LBL 54 AT FWD GALLEY AREA 2023-577781<[01] TOOL USED: CALIPER 0-6? P/N: 700-113-10 S/N: 0033174 AND DUE DATE: 12-MAR-24;[02] REPLACED INNER CHORD LOCATED BS270 TO BS360 WL208.1 AND LBL56 AT FWD GALLEY AREA ANDSep 9, 2023 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2023102098717Web · crackedCRACK WEB LOCATED BTW STA 312 TO STA 328 LBL 48 AT FWD GALLEY AREA 2023-577779<[01] REPLACED WEB LOCATED BTW BS312 TO BS328 LBL48 AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV. -<BR><BR>SEE INDIVIDUAL SIGSep 9, 2023 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023102098723Web · crackedCRACK WEB LOCATED BTW STA 312 TO STA 328 AND RBL 34 AT FWD GALLEY AREA 2023-577777 CORRECTED LOCATION IS : RBL 31.6<[01] REPLACED WEB LOCATED BTW BS312 TO BS328 RBL31.6 AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A5400 SHSep 9, 2023 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023102098721Web · crackedCRACK WEB LOCATED BTW STA 328 TO STA 344 LBL 48 AT FWD GALLEY AREA 2023-577780<[01] REPLACED WEB LOCATED BTW STA 328 TO STA 344 LBL 48 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK COMPLETED; RII Sep 9, 2023 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023102098722Web · crackedCRACK WEB LOCATED BTW STA 277 TO STA 294.5 AND BL 0 AT FWD GALLEY AREA 2023-577778<[01] REPLACED WEB LOCATED BTW STA 277 TO STA 294.5 AND BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND 141A5400 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK COMPLETED; Sep 9, 2023 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023102098423Angle · crackedCRACK ON SUPPORT ANGLE LOCATED FLOOR STRUCTURE FWD FACE BS 695 RBL 1 WL 208.1 AT CENTER SECTION 2023-577693<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142Sep 8, 2023 · N7862A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023101998436Light · brokenBROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2023-577723<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN IAW B737-700 AMM 33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSSep 8, 2023 · N7862A · Boeing 73779P · Emergency LightingSDR SWAA2023101798488Access Panel · corroded***CORROSSION*** FWD CARGO COMPARTMENT FLOOR ACCESS PANEL # 120BF HAS LIGHT CORROSSION<[01] REMOVED CORROSION AT FWD CARGO COMPARTMENT FLOOR ACCESS PANEL #120BF PER SRM 51-10-02-0G-0<BR>EVALUATED REWORKED AREA. ORIGINAL MATERIAL THICKNESS: 0.071'; MATERIAL LOSSep 8, 2023 · N7833A · Boeing 73779P · Fuselage Structure (General)SDR SWAA2023101798489Access Panel · corroded***CORROSSION*** FWD CARGO COMPARTMENT FLOOR ACCESS PANEL # 120AF HAS LIGHT CORROSSION<[01] REMOVED CORROSION AT FWD CARGO COMPARTMENT FLOOR ACCESS PANEL #120AF PER SRM 51-10-02-0G-0<BR>EVALUATED REWORKED AREA. ORIGINAL MATERIAL THICKNESS: 0.071'; MATERIAL LOSSep 8, 2023 · N7833A · Boeing 73779P · Fuselage Structure (General)SDR SWAA2023101798490Access Panel · corroded***CORROSSION*** FWD CARGO COMPARTMENT FLOOR ACCESS PANEL # 120CF HAS LIGHT CORROSSION<[01] REMOVED CORROSION AT FWD CARGO COMPARTMENT FLOOR ACCESS PANEL #120CF PER SRM 51-10-02-0G-0<BR>EVALUATED REWORKED AREA. ORIGINAL MATERIAL THICKNESS: 0.071'; MATERIAL LOSSep 8, 2023 · N7833A · Boeing 73779P · Fuselage Structure (General)SDR SWAA2023101997900Handle · brokenBROKEN LINING ENTRY DOOR HANDLE AT FWD GALLEY AREA 2023-577613<[01] REPLACED LINING ENTRY DOOR HANDLE AT FWD GALLEY AREA I.A.W. B737-700 AMM 52-11-31-400-802 STEP 3.G.(2) ITEM (C) AND (D);[02] REPLACED LINING ENTRY DOOR HANDLE AT FWD GALLEY AREA I.A.W. B737-70Sep 7, 2023 · N7862A · Boeing 73779P · Passenger/Crew DoorsSDR SWAA2023101997851Handle · deterioratedDETERIORATED ENTRY DOOR HANDLE AT FWD GALLEY AREA (1 EA) 2023-577606<[01] REPLACED ENTRY DOOR HANDLE AT FWD GALLEY AREA (1 EA) I.A.W B737-700 SOPM 20-50-01 REV 38 AND DWG 411A2203 REV E.;[02] CORRECTED STEP 1. REPLACED ENTRY DOOR HANDLE AT FWD GALLEY AREA (1 ESep 7, 2023 · N7862A · Boeing 73779P · Passenger/Crew DoorsSDR SWAA2023101699598Support Angle · crackedRIGHT VAPOR BARRIER UPPER SUPPORT ANGLE STA 663 FOUND CRACK AT RBL 7.<[01] REPAIRED AREA AT VAPOR BARRIER UPPER SUPPORT ANGLE STA 663 AS PER B 737-700 SRM 57-10-10-2R-5 FIG 202 SHEET 4;[02] VERIFIED; STEP # 1.Sep 7, 2023 · N7833A · Boeing 73779P · Fuselage Main, BulkheadSDR SWAA2023092697887Skin · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN BS887 STR25R TO STR25L<[01] CORRECTION TO TASK DETAIL SHOULD STATE ' CORROSION ON EXTERNAL FUSELAGE SKIN BS887 STR25R TO STR25L FWD OF BUTT JOINT ';[02] REMOVED CORROSION IN AN AREA OF 7.80' X 0.5 0' REMOVED 0.004' ORIGINAL Sep 7, 2023 · N7861J · Boeing 73779P · Fuselage Main, Plate/SkinSDR SWAA2023101797257Skin · crackedCRACK FOUND ON LOWER SKIN OF R/H HORIZONTAL STABILIZER AT STAB STA 193.90; 8.5' FROM FRONT SPAR; I/B ROW. CRACK LENGTH : 1'. CRACK FOUND ON LOWER SKIN OF R/H HORIZONTAL STABILIZER AT STAB STA 193.90 8.5' FROM FRONT SPAR I/B ROW. CRACK LENGTH : 1'.<[01] STEP 12Sep 6, 2023 · N7833A · Boeing 73779P · Horizontal Stabilizer, Plate/SkinSDR SWAA2023101797421Slat · pulledLEFT WING # 3 SLAT ACTUATOR LOWER SURFACE OF L/E HAS SIX FASTENERS PULLED IN.<[01] CUT DAMAGED AND FABRICATE REPAIR PARTS DOUBLER AND FILLER. EVALAUTED SURFACE ROUGHNESS ON CUT EDGES FOUND SMOOTHER THAN 63 MICROINCHES RA. AND FOUND SMOOTHER THAN 125 MICROINCHESep 6, 2023 · N7833A · Boeing 73779P · Leading Edge DevicesSDR SWAA2023101797427Slat · pulledLEFT WING # 2 SLAT ACTUATOR LOWER SURFACE OF L/E HAS SEVEN FASTENERS PULLED IN.<[01] CRACK FOUND ON #2 SLAT ACTUATOR FITTING. SLAT REPLACEMENT TO BE ACCOMPLISHED ON NR #TTG8Q00NSYZE.;[02] VERIFIED STEP 1.Sep 6, 2023 · N7833A · Boeing 73779P · Leading Edge DevicesSDR SWAA2023101697418Floor Panel · delaminatedPASSENGER CABIN CENTER SECTION FLOOR PANEL #242AF; UPPER SURFACE DELAMINATED DOT 223-242AFC1.<[01] RECEIVED NEW CABIN FLOOR PANEL #242AF FROM STOCK. PANEL WILL BE INSTALLED ON ROUTINE CARD TTG8Q00MVXR8.;[02] VERIFIED STEP #1Sep 6, 2023 · N7833A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2023101697419Floor Panel · delaminatedPASSENGER CABIN CENTER SECTION FLOOR PANEL #231XF; UPPER SURFACE DELAMINATED DOT 223-231XFC1.<[01] FABRICATED NEW PASSENGER CABIN CENTER SECTION FLOOR PANEL# 231XF; PO # 1792296 AS PER B737-700 IPC 53-21-00-42A; DWG# 144A5810. INSTALLATION WILL BE ACCOMPLISHEDSep 6, 2023 · N7833A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2023101697420Floor Panel · delaminatedPASSENGER CABIN CENTER SECTION FLOOR PANEL #241DF; UPPER SURFACE DELAMINATED DOT 223-241DFC1.<[01] RECEIVED NEW CABIN FLOOR PANEL #241DF FROM STOCK. PANEL WILL BE INSTALLED ON ROUTINE CARD TTG8Q00MVWH0.;[02] VERIFIED STEP #1Sep 6, 2023 · N7833A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2023101697423Floor Panel · delaminatedPASSENGER CABIN CENTER SECTION FLOOR PANEL #241AF; UPPER SURFACE DELAMINATED DOT 223-241AFC1.<[01] RECEIVED NEW CABIN FLOOR PANEL #241AF FROM STOCK. PANEL WILL BE INSTALLED ON ROUTINE CARD TTG8Q00MVWH6.;[02] VERIFIED STEP #1Sep 6, 2023 · N7833A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2023092697507Strap · elongatedAAI: REF: NRC: T684603: FWD CARGO COMPARTMENT: FRAME STRAP HAS AN ELONGATED FASTENER HOLE AT STA 492.4; STR 23R.<[01] OVERSIZED HOLE TO ROUND CONDITION PER EA 23-153-02732Sep 6, 2023 · N7861J · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023092697508Angle · misinstalledAAI: REF: NRC: TTG8Q00A1SR1: FWD CARGO COMPARTMENT: REPAIR ANGLE HAS IMPROPERLY INSTALLED FASTENER AND HOLE ELONGATED AT STA 500A; STR 25R.<[01] REMOVED; REPLACED AND INSTALLED NEW CLIP AT BS 500A STR 25R WL 156 PER SRM 51-40-02-0G-0 AND DWG 143A7505;[02] VERISep 6, 2023 · N7861J · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023092695959Rib · crackedR/H HORIZONTAL STABILIZER HAS A CRACKED RIB AT STA.129.50; 2ND VERTICAL STIFFENER FROM L/E<[01] VERIFIED APPLICABILITY OF SRM 55-10-09-2R-4 REPAIR 4.;[02] VERIFIED CORRECTIVE ACTION 1;[03] REMOVED CRACK DAMAGE RIGHT HAND HORIZONTAL STABILIZER INPSAR RIB AT STASep 1, 2023 · N7861J · Boeing 73779P · Horizontal Stabilizer, Spar/RibSDR SWAA2023092695960Rib · crackedL/H HORIZONTAL STABILIZER 4TH VERTICAL STIFFENER FROM L/E IS CRACKED AT BS 129.5; INSPAR RIB 5<[01] REMOVED CRACK DAMAGE LEFT HAND HORIZONTAL STABILIZER 4TH VERTICAL STIFFENER FROM LEADING EDGE AT STAB STA 129.50 INSPAR RIB 5 AND INSTALLED REPAIR IAW SRM 55-10Sep 1, 2023 · N7861J · Boeing 73779P · Horizontal Stabilizer, Spar/RibSDR SWAA2023092195952Baffle · crackedFCB BAFFLE IS CRACKED BETWEEN BS 400 TO BS 420 LBL 24 WL 156<[01] REMOVED AND REPLACED FCB BAFFLE BETWEEN BS400 TO BS420;LBL24;WL156.IAW SRM 51-40-02 AND DWG#143A7505 REV B.;[02] TASK CARD COMPLETESep 1, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023092195951Baffle · crackedFCB BAFFLE IS CRACKED BETWEEN BS 400 TO BS 420 LBL 24 WL 156<Sep 1, 2023 · N7826B · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023090595915Nut · deterioratedDETERIORATED SERVICE DOORWAY ASSIST HANDLE NUT AT AFT GALLEY AREA (2 EA) 2023-469812<[01] REPLACED SERVICE DOORWAY ASSIST HANDLE NUT AT AFT GALLEY AREA (2 EA) IAW B737-700 AMM-52-41-31-400-802 STEP 3.F.(2);[02] COMPLETEDSep 1, 2023 · N7832A · Boeing 73779P · Service DoorsSDR SWAA2023092695772Floor Panel · delaminatedPANEL 222BF FWD O/B CORNER IS DELAMINATED<[01] DELAMINATION AT FWD O/B CORNER ON FLOOR PANEL 222BF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] JOB COMPLETE.Aug 31, 2023 · N7861J · Boeing 73779P · Fuselage Floor PanelSDR SWAA2023092695330Sidewall Support · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] REMOVED AND REPLACED ACB L/H FLOOR TO SIDEWALL SUPPORT PLATE BS 727+4 TO BS 847; LBL 22; WL 156 IAW SRM 51-40-02-0G-0; DWG#146A75Aug 30, 2023 · N7861J · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023092695328Sidewall Support · corrodedCORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727C TO BS767 RBL22 WL156<[01] REMOVED AND REPLACED ACB R/H FLOOR TO SIDEWALL SUPPORT PLATE BS 727+4 TO BS 767; RBL 22; WL 156 IAW SRM 51-40-02-0G-0; DWG#14Aug 30, 2023 · N7861J · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2023092695464Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727D+6 RBL11.5 WL156<[01] CORROSION ON STRAP FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED AS PER SRM 51-10-02.;[02] VERIFIED CORRECTIVE ACTION 1;[0Aug 30, 2023 · N7861J · Boeing 73779P · Fuselage Miscellaneous Structure
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