Boeing 737-7CT

Service difficulty reports · 2,414

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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 = '7377CT'
  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 SWAA2023031699660Stringer · crackedCRACK STRINGER 25R AT LEVEL BS540 AT FWD CARGO COMPARTMEN 2023-106199<[01] UT TOOL USED PN: 45MG ; SN: 221859911. DUE DATE: 07-NOV-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/NFeb 7, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2023032099652Web · corrodedCORROSION WEB LOCATED BETWEEN BS420 TO BS440 RBL21.80 AND WL156 AT FWD CARGO COMPARTMENT 2023-106257<[01] TOOL USED PN ULTRASONIC EQUIPMENT PN:45MG; SN: 130066701; DUE DATE: 08-APR-23;[02] REPLACED WEB LOCATED BETWEEN BS420 TO BS440 RBL21.80 AND WL156 AT FWD CFeb 6, 2023 · N566WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2023032099650Plate · brokenBROKEN INBOARD FAN COWL SPRINT PLATE ACCESS DOOR 423BL ON ENGINE 2 2023-106243<[01] REPLACED SPRINT PLATE LOC. INBOARD FAN COWL ACCESS DOOR 423BL ON ENGINE 2 IAW B737-700 SRM 51-10-02 ITEM 9 AND CMM 71-13-30;[02] REPLACED SPRING PLATE LOC. INBOARD FAN COWL ACCFeb 6, 2023 · N566WN · Boeing 7377CT · Nacelle/Pylon StructureSDR SWAA2023031699651Scuff Plate · crackedCRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2023-106247<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189511;DUE DATE:12-OCT-23.;[02] TOOL USED RADIOMETER P/N: XRP-3000; S/N: 1998072; DUE DATE: 03-MAY-23.;[03] REPAIRED AFT CORNER SCUFF PLATE AFeb 6, 2023 · N566WN · Boeing 7377CT · Cargo CompartmentsSDR SWAA2023032099285Stringer · crackedCRACK STRINGER 23L AT LEVEL BS540 FWD CARGO COMPARTMENT. 2023-106192<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[02] TOOL Feb 5, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2023032099274Angle · crackedCRACK ANGLE LOCATED BS500D AFT FACE AND STR 27R AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT 2023-106213<[01] INSTALLED ANGLE LOCATED BS500D AFT FACE AND STR 27R AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT;[02] JOB RII COMPLETEFeb 5, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Plate/SkinSDR SWAA2023032099287Stringer · crackedCRACK STRINGER 23R AT LEVEL BS540 AT FWD CARGO COMPARTMENT 2023-106193<[01] UT TOOL USED PN: 45MG ; SN: 221859911. DUE DATE: 07-NOV-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/Feb 5, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2023032099286Stringer · corrodedCORROSION STRINGER 25L AT LEVEL BS540 FWD CARGO COMPARTMENT. 2023-106194<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[02] TFeb 5, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2023031799279Stringer · crackedCRACK STRINGER 26L AT LEVEL BS540 FWD CARGO COMPARTMENT. 2023-106196<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[02] REPAIFeb 5, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2023031799280Stringer · crackedCRACK STRINGER 27L AT LEVEL BS540 FWD CARGO COMPARTMENT. 2023-106198<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[02] REPAIFeb 5, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2023031699275Angle · crackedCRACK ANGLE LOCATED BS500B AND STR25 FWD CARGO COMPARTMENT 2023-106219<[01] REPLACED ANGLE LOCATED BS500B AND STR25L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED IAW SRM 51-40-02 AND DWG 143A7505 SHEET5 REV B. DUE TO NOT FOUND ALLOWABLEFeb 5, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Plate/SkinSDR SWAA2023031699282Stringer · crackedCRACK STRINGER 26R AT LEVEL BS540 FWD CARGO COMPARTMENT. 2023-106201<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[02] TOOL Feb 5, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2023031699283Stringer · corrodedCORROSION STRINGER 27R AT LEVEL BS540 FWD CARGO COMPARTMENT. 2023-106200<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[02] TFeb 5, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2023032098933Stringer · crackedCRACK STRINGER 26L AT LEVEL BS540 FWD CARGO COMPARTMENT. 2023-106227<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N 130066401 DUE DATE 21-SEP-23;[02] FAULT RAISED IN ERROR DUE TO WRONG LOCATION OF DAMAGE; IS STR 28L. SEE TTG8Q00HNP0P.;[03] CORRECTIVE Feb 4, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2023032098929Stringer · crackedCRACK STRINGER 22L AT LEVEL BS540 FWD CARGO COMPARTMENT. 2023-106224<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N 130066401 DUE DATE 21-SEP-23;[02] FAULT RAISED IN ERROR DUE TO WRONG LOCATION OF DAMAGE; IS STR 23L. SEE TTG8Q00HNPFW.;[03] FAULT RAISEFeb 4, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2023032098930Stringer · corrodedCORROSION STRINGER 24L AT LEVEL BS540 FWD CARGO COMPARTMENT. 2023-106225<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N 130066401 DUE DATE 21-SEP-23;[02] FAULT RAISED IN ERROR DUE TO WRONG LOCATION OF DAMAGE; IS STR 25L. SEE TTG8Q00HNPH3;[03] CORRECTIFeb 4, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2023032098931Stringer · corrodedCORROSION STRINGER 25L AT LEVEL BS540 FWD CARGO COMPARTMENT. 2023-106226<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N 130066401 DUE DATE 21-SEP-23;[02] FAULT RAISED IN ERROR DUE TO WRONG LOCATION OF DAMAGE; IS STR 26L. SEE TTG8Q00HNP0K;[03] FAULT RAFeb 4, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2023032098922Balance Weight · corrodedCORROSION AILERON BALANCE ADJUST WEIGHTS LOCATED BALANCE BAY 5 UPPER AND LOWER POSITION AT LT WING 2023-106179<[01] REPLACED AILERON BALANCE ADJUST WEIGHT FIXED UPPER AND LOWER LOCATED BALANCE BAY 5 AT LT WING I.A.W B737-700 SRM 51-60-01-0G-0 STEP 5.A.(5)(D). Feb 4, 2023 · N566WN · Boeing 7377CT · Wing Miscellaneous StructureSDR SWAA2023032098923Balance Weight · corrodedCORROSION AILERON BALANCE ADJUST WEIGHTS LOCATED BALANCE BAY 5 UPPER AND LOWER POSITION AT RT WING (4 EA) 2023-106182<[01] REPLACED AILERON BALANCE ADJUST WEIGHT FIXED UPPER AND LOWER LOCATED BALANCE BAY 5 AT RT WING I.A.W B737-700 SRM 51-60-01-0G-0 STEP 5.A.(Feb 4, 2023 · N566WN · Boeing 7377CT · Wing Miscellaneous StructureSDR SWAA2023031798932Stringer · crackedCRACK STRINGER 22R AT LEVEL BS540 AT FWD CARGO COMPARTMENT 2023-106228<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N 130066401 DUE DATE 21-SEP-23;[02] RAISED IN ERROR DUE TO WRONG LOCATION OF DAMAGE; IS STR 23R. TTG8Q00HNPJF.;[03] RAISED IN ERROR DUEFeb 4, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2023031698622Panel · elongatedELONGATED HOLE ACCESS PANEL 123YBC AT FWD CARGO COMPARTMENT 2023-106134<[01] FABRICATED ACCESS PANEL 123YBC AT FWD CARGO COMPARTMENT IAW AMM TASK 25-52-01-201-801 STEP 1 E (F) AND DWG 453A1210 REV A MATERIAL USED CONOLITE 0.30?P/N 6100T.030-48132 PO 2022 22908Feb 4, 2023 · N566WN · Boeing 7377CT · Passenger Compartment EquipmentSDR SWAA2023031698928Flashlight Assy · brokenBROKEN WINDSCREEN LT SIDE EMERGENCY FLASHLIGHT ASSY AT AFT GALLEY AREA (1 EA) 2023-106191<[01] REPLACED WINDSCREEN LT SIDE EMERGENCY FLASHLIGHT ASSY AT AFT GALLEY AREA (1 EA) I.A.W CMM ASTRONICS 25-60-02 REV.10 DISASSEMBLY: STEP 2.A PAGE 3001 ASSEMBLY: STEP STFeb 4, 2023 · N566WN · Boeing 7377CT · Emergency EquipmentSDR SWAA2023020799159Battery Pack · inoperativeVARIOUS EMERGENCY LIGHTS DO NOT ILLUMINATE IN THE CABIN.<[01] REPLACED 8 EMERGENCY LIGHT BATTERY PACKS IN POWER SUPPLIES W/ SERVICEABLE OF SAME. OPS CK NORMAL AT THIS TIME. WORK IAW AMM 33-51-06Feb 4, 2023 · N7829B · Boeing 7377CT · Emergency LightingSDR SWAA2023032098036Structure · cracked(CUSTOMER REQUEST) CRACK ON CUT OUT EXTERNAL SERVICE GROUND LOWER FUSELAGE 2023-106020<[01] TOOL USED PN NORTEC 600D SN 220272712 DUE DATE 17-DEC-23;[02] REPAIRED ON CUT OUT EXTERNAL SERVICE GROUND LOWER FUSELAGE IAW B737-700 SRM 53-10-15-2R-4 REPAIR 4 AND SRMFeb 3, 2023 · N566WN · Boeing 7377CT · Service DoorsSDR SWAA2023032098617Panel · corrodedCORROSION ACCESS PANEL 191CR PLATE CUT OUT OF DRAIN MAST AT LOWER FUSELAGE 2023-106128<[01] REPLACED ACCESS PANEL 191CR PLATE CUT OUT OF DRAIN MAST AT LOWER FUSELAGE I.A.W B737-700 SRM 51-40-02;[02] REPLACED ACCESS PANEL 191CR PLATE CUT OUT OF DRAIN MAST AT LOFeb 3, 2023 · N566WN · Boeing 7377CT · Aerodynamic FairingsSDR SWAA2023032098620Panel · corrodedCORROSION ACCESS PANEL 191CR DRAIN MAST AT LOWER FUSELAGE 2023-106130<[01] REPLACED FWD DRAIN MAST IAW AMM 38-31-01-401-NG <BR>TEST IS OK <BR>TOOL USED P/N: 2278-20; S/N: AE-410983; DD: 06-JAN-24<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1:REPLACED Feb 3, 2023 · N566WN · Boeing 7377CT · Aerodynamic FairingsSDR SWAA2023032098614Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL 0 AND RBL 24.5 WL 208.1 CENTER SECTION 2023-106058<[01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL 0 TO RBL 24.5 WL 208.1 CENTER SECTION IAW B737-700 #DWG-143A0060 SHEET= 36 REV= A ANDFeb 3, 2023 · N566WN · Boeing 7377CT · Wing, Center BoxSDR SWAA2023031698623Light · brokenBROKEN SIDEWALL PANEL EMERGENCY LIGHT ASSY ON POSITION 232YHW AT PASSENGER CABIN (1 EA) 2023-106033<[01] REPLACED SIDEWALL PANEL EMERGENCY LIGHT ASSY ON POSITION 232YHW AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 33-51-01-960-802 TEST IS OK.;[02] REPLACED SIDFeb 3, 2023 · N566WN · Boeing 7377CT · Emergency LightingSDR SWAA2023032098035Skin · crackedCRACK EXTERNAL SKIN LOWER AT STAB STA 193.90 AT RT HORIZONTAL STABILIZER 2023-105972<[01] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X12101V022237 DUE DATE 26-JAN-24.;[02] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN 200048001; DUE DATE 3Feb 2, 2023 · N566WN · Boeing 7377CT · Horizontal Stabilizer StructureSDR SWAA2023031798032Vapor Barrier · cracked(CUSTOMER REQUESTS) CRACK VAPOR BARRIER LOCATED BS663 RBL50 AND WL160 AT MAIN WHEEL WELL COMPARTMENT 2023-105960<[01] TOOL USED CALIPER P/N. 500-197-30. S/N. A21043202 DUE DATE. 12-OCT-23;[02] TOOL USED:HOT BONDER P/N:HCS9200B-AV S/N:18196126 DUE DATE:24-FEB-2Feb 2, 2023 · N566WN · Boeing 7377CT · Fuselage Main, KeelSDR SWAA2023031698034Light · brokenBROKEN BASE EMERGENCY EXIT LIGHT ON CEILING PANEL 241YAC AT PASSENGER CABIN 2023-105965<[01] REPLACED BASE EMERGENCY EXIT LIGHT ON CEILING PANEL 241YAC AT PASSENGER CABIN IAW B737-700 AMM 33-51-01-960-801;[02] REPLACED BASE EMERGENCY EXIT LIGHT ON CEILING PANEFeb 2, 2023 · N566WN · Boeing 7377CT · Emergency LightingSDR SWAA2023030897911Seat Track · corrodedLEFT OB CABIN SEAT TRACK HAS EXFOLIATING CORROSION BS 375. 8-26<[01] REMOVED FASTENERS FOR ACCESS TO REMOVE SEAT TRACK CORROSION PER B737-700 SRM 51-40-02-0G-0.;[16] VERIFIED STEP NO15. (FINAL) REMOVED CORROSION AT LEFT O/B CABIN SEAT TRACK BS 375 PER B737-700Feb 2, 2023 · N567WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2023032097614Skin · crackedCRACK EXTERNAL SKIN SLAT 8 AROUND THE FASTENERS THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 451.97 AT RT WING 2023-105954<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N210138203; DUE DATE: 11-APR-23;[02] EVALUATED SLAT 8 OUT LIMITS; CRACFeb 1, 2023 · N566WN · Boeing 7377CT · Leading Edge DevicesSDR SWAA2023032097616Web · corrodedCORROSION FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APPROX AND WBL 94.24 AT RT WING 2023-105956<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N:NORTEC 600D S/N:220273012; CAL DUE DATE: 17-DEC-23;[02] TOOL USED: ULTRASONIC EQUIPMENT; P/N: 45MG; S/N: 130066701Feb 1, 2023 · N566WN · Boeing 7377CT · Wing Miscellaneous StructureSDR SWAA2023030897542Stiffener · crackedRIGHT HORIZONTAL STILIZER RIB 4 CRACKED AT STIFFENER 2 LOWER RADIUS.<[01] REMOVED THE DAMAGE PART OF THE RIB 4 STIFFENER 2 LOWER RADIUS AS SHOW IN FIG. 202 PARA.4 LETTER B REF. SRM 55-10-09-2R-4 REPAIR 4;[02] PERFORMED HFEC INSP ON REWORKED; IAW B 737 NDT PARTFeb 1, 2023 · N567WN · Boeing 7377CT · Horizontal Stabilizer, Plate/SkinSDR SWAA2023030897785Barrier · crackedRT BS 663 VAPOR BARRIER CRACK RBL 45.<[01] MEASUREMENTS;[02] PERFORMED VISUAL INSPECTION ON R/H VAPOR BARRIER AND FOUND CRACK OF 9' PER B737 NDTM 51-05-01;[03] PERFORMED STOP DRILL SIZE 0.25 DIAMETER AT THE END OF THE CRACK PER B737 SRM 57-10-10-2R-2 STEP 6.B;Feb 1, 2023 · N567WN · Boeing 7377CT · Wing Main, Frame StructureSDR SWAA2023030897321Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL #241XF; UPPER SURFACE DELAMINATED DOT 223-PCF241XF.<[01] RECEIVED NEW PANEL 241XF; PO#2005897. PANEL WILL BE INSTALLED ON TTG8Q00H2SLP.;[02] VERIFIED AND INSPECTED STEP #1.Jan 31, 2023 · N567WN · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2023030896999Bracket · crackedLH VAPOR BARRIER SUPPORT BRACKET FOUND CRACKED AROUND FASTENER HOLE<[01] RECEIVED NEW BRACKET P/N 276A9183-5 AND LOCATED AND DRILL PER REF SRM 51-40-05-0G-0;[02] TREATED AND PRIME NEW FASTENER HOLES; PER REF AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[03] OJan 31, 2023 · N567WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2023030897329Channel · brokenRIGHT 'Z' CHANNEL AT FWD END B/S 727 ATTACHMENT IS BROKEN<[01] AFT CARGO R/H Z CHANNEL WILL BE REPLACED FROM STA 727-767 FOR WORK ACCOMPLISHED REFERENCE TASK CARD # TTG8Q00HKAET;[02] FINAL INSPECTION; AFT CARGO R/H Z CHANNEL WILL BE REPLACED FROM STA 727-767 FJan 31, 2023 · N567WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2023030897333Floor Panel · crackedFLOOR PNL 242SF HAS CRACK ON UPPER SURFACE. 8-25<[01] RECEIVED NEW PANEL 242SF PO#2005895. PANEL WILL BE INSTALLED ON TTG8Q00H2URQ.;[02] VERIFIED AND INSPECTED STEP #1.Jan 31, 2023 · N567WN · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2023030897332Channel · corrodedAFT CARGO FLOOR SUPPORT 22' RIGHT 'Z' CHANNEL IS CORRODED AT B/S 727C-727E<[01] AFT CARGO R/H Z CHANNEL WILL BE REPLACED FROM STA 727-767 FOR WORK ACCOMPLISHED REFERENCE TASK CARD #TTG8Q00HKAET;[02] VERIFIED STEP #1.Jan 31, 2023 · N567WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2023030897328Channel · corrodedAFT CARGO FLOOR SUPPORT 22' RIGHT 'Z' CHANNEL IS CORRODED AT B/S 727E-767<[01] FOUND EXFOLIATED CRACKED CORROSION AT AFT CARGO FLOOR SUPPORT Z-CHANNEL PER REF SRM 51-10-02-0G-0;[02] LOCATED AND DRILLED NEW R/H Z-CHANNEL FROM STA 727 TO 767 PER REF SRM 51-40-05Jan 31, 2023 · N567WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2023030897326Channel · corrodedAFT CARGO FLOOR SUPPORT 22' LEFT 'Z' CHANNEL IS CORRODED AT B/S 77B-727E<[01] AFT CARGO L/H Z CHANNEL WILL BE REPLACED FROM STA 727-847 FOR WORK ACCOMPLISHED REFERENCE TASK CARD # TTG8Q00HKADG;[02] VERIFIED STEP #1.Jan 31, 2023 · N567WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2023030897325Channel · corrodedAFT CARGO FLOOR SUPPORT 22' LEFT 'Z' CHANNEL IS CORRODED AT B/S 727-727B<[01] FOUND EXFOLIATED CRACKED CORROSION AT AFT CARGO FLOOR SUPPORT L/H Z CHANNEL STA 727-727B PER SRM 51-10-02-0G-0;[02] LOCATED AND DRILLED NEW L/H Z CHANNEL FROM STA 727- 847 PER REF SRJan 31, 2023 · N567WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2023030897330Channel · corrodedAFT CARGO FLOOR SUPPORT 22' LEFT 'Z' CHANNEL IS CORRODED AT B/S 767-807<[01] AFT CARGO L/H Z CHANNEL WILL BE REPLACED FROM STA 727-847 FOR WORK ACCOMPLISHED REFERENCE TASK CARD # TTG8Q00HKADG;[02] VERIFIED STEP #1.Jan 31, 2023 · N567WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2023030897000Retainer · crackedLH VAPOR BARRIER SEAL RETAINER FOUND CRACKED<[01] RECIEVED; LOCATED AND DRILLED NEW L/H VAPOR BARRIER SEAL RETAINER PN: 111A1512U1 PO:1792296 PER REF SRM 51-40-05-0G-0.;[02] TREATED AND PRIMED NEW HOLES PER REF AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[03Jan 31, 2023 · N567WN · Boeing 7377CT · Fuselage Main, Attach FittingsSDR SWAA2023030897320Fitting · crackedRT WING TRAIL EDGE RIB WBL 201.90 HAS AFT UPPER FITTING CRACKED THRU. 8-24<[01] REMOVED AND REPLACED AFT UPPER FITTING AT RT WING TRAIL EDGE RIB WBL 201.90 PER REF SRM-51-40-02-0G-0.;[02] FINAL INSPECTION; T/E RIB REPLACED.Jan 31, 2023 · N567WN · Boeing 7377CT · Trailing Edge FlapsSDR SWAA2023030896756Vapor Barrier · crackedCOMP- REPAIR LH VAPOR BARRIER CRACK<[01] MEASUREMENTS.;[02] REMOVED THE DAMAGED PLIES AND PREPARED DAMAGED AREA TO APPLY THE GLASS FABRIC REPAIR PLIES; DRILLED 0.25 INHC DIAMETER STOP HOLES AT THE CRACK END. REF B737 SRM 51-70-04-2R-10 PARAGRAP 4 AND SRM 57-10Jan 30, 2023 · N567WN · Boeing 7377CT · Fuselage Main, KeelSDR SWAA2023030896442Doubler · crackedEGPR INTERNAL DOUBLER CRACKED AT FWD LOWER CORNER.<[01] REMOVED PAINT BY STRIPPING AT FUSELAGE SKIN R/H SIDE EGPR AREA REF B737-700 AMM 51-21-11-150-810.; LOCATED AND DRILLED NEW EGPR INTERNAL DOUBLER REF B737-700 SRM 51-40-05-0G-0.;[07] TREATED AND PRIMED DRIJan 28, 2023 · N567WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2023030896443Stiffener · crackedRIGHT HORIZONTAL STABILIZER RIB 4 CRACKED AT STIFFENER 3 LOWER RADIUS.(51-025)<[01] REMOVED THE DAMAGE PART OF THE RIB 4 AT STIFFENER 3 LOWER RADIUS AS SHOW IN FIG. 202 PARA.4 LETTER B REF. SRM 55-10-09-2R-4 REPAIR 4;[02] VERIFIED 1. ACCOMPLISHED GVI OF REPAIRJan 28, 2023 · N567WN · Boeing 7377CT · Horizontal Stabilizer Structure
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