Boeing 737-7CT

Service difficulty reports · 2,413

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 = '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 SWAA2025062383727Cabin Air Sys · odorFORWARD FLIGHT ATTENDANTS REPORTED A EXHAUST SMELL ON A CLIMBOUT. NO ABNORMAL SMELLS OR INDICATION ON THE COCKPIT OR AFT SECTION OF THE AIRPLANE <[01]. C/W CONDITIONAL INSPECTION PER MM 05-51-56. R&R BOTH PACKS COALESCER BAGS PER MM 21-51-05. R&R RECIRCULATJun 19, 2025 · N7828A · Boeing 7377CT · Air Distribution SystemSDR SWAA2025061077148Bulb · inoperativeDURING EMERGENCY LIGHT OPERATIONAL TEST. FOUND AFT EMERGENCY LIGHT BULB IN R/H OVERWING EXIT WINDOW LIGHT ASSEMBLY INOP DURING EMERGENCY LIGHT OPERATIONAL TEST FOUND AFT EMERGENCY LIGHT BULB IN R/H OVERWING EXIT WINDOW LIGHT ASSEMBLY INOP. RELAMPED AND CHECJun 2, 2025 · N7823A · Boeing 7377CT · Emergency LightingSDR SWAA2025061076837Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK (M1672) DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK M1672 IAW AMM 33-51-06-960-805 AND PERFORMED GOOD EMERGENCY LIGHT TEST IAW AMM 33-51-06-960-805.May 31, 2025 · N7823A · Boeing 7377CT · Emergency LightingSDR SWAA2025061076627Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK (M1670) DO NOT ILLUMINATE. REPLACED EMERGENCY BATTERY PACK (M1670); PERFORMED GOOD TEST PER AMM 33-51-06-960-805.May 30, 2025 · N7823A · Boeing 7377CT · Emergency LightingSDR SWAA2025061073449Floorbeam · crackedCRACKED PANEL BREAK AT MID CABIN BS540 RBL1 WL208. MARKED<[01] REMOVED AND REPLACED PANEL BREAK AT MID CABIN BS540 RBL1 WL208 IAW SRM 51-40-02 AND DWG# 143A5240 REV: B;[02] VERIFIED CORRECTIVE ACTION #1May 21, 2025 · N7823A · Boeing 7377CT · Fuselage Main, Floor BeamSDR SWAA2025061073451Floorbeam · crackedCRACKED PANEL BREAK AT MID CABIN BS540 RBL1 WL208<[01] THIS IS DUPLICATED CARD... REMOVED AND REPLACED ON FAULT# TTG8Q010QNP2;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.May 21, 2025 · N7823A · Boeing 7377CT · Fuselage Main, Floor BeamSDR SWAA2025061073450Panel · crackedVERTICAL STAB PANEL 323AL LOWER CLIP CRACKED.<[01] RECEIVED SERVICEABLE PANEL 323AL P/N:654A0004-711; BN 396992. PANEL WILL BE INSTALLED ON TASK CARD TTG8Q00Z3WDY;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.May 21, 2025 · N7823A · Boeing 7377CT · Vertical Stabilizer, Plate/SkinSDR SWAA2025061073097Floorbeam · crackedCRACKED PANEL BREAK AT MID CABIN BS540 LBL1 WL208. MARKED<[01] REMOVED AND REPLACED BS540 LBL1 PANEL BREAK P/N#143A5240-63 IAW SRM 51-40-02 AND PER AIPC# 53-31-00-05;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.May 20, 2025 · N7823A · Boeing 7377CT · Fuselage Main, Floor BeamSDR SWAA2025061072596Attach Angle · crackedLT WING DEFLECTION CONTROL RIB UPPER PANEL ATTACHMENT CRACKED.<[01] REPAIRED LT WING DEFLECTION CONTROL RIB UPPER PANEL ATTACHMENT IAW SRM 57-51-02-2R-3.;[02] CORRECTIVE ACTION COMPLETED.May 19, 2025 · N7823A · Boeing 7377CT · Wing, Attach FittingsSDR SWAA2025060972772Skin · crackedCRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 23. 5' FROM FWD EDGE; .3' IN LENGTH (MARKED)<[01] REMOVED THE DAMAGED PART ON LH HORIZONTAL STABILIZER LOWER SKIN STA 193.90 23.5' FROM FWD EDGE; CUT OUT DIMENSIONS 1.7' X 1.0' AND INSTALLED REPMay 19, 2025 · N7823A · Boeing 7377CT · Horizontal Stabilizer, Plate/SkinSDR SWAA2025061072458Seal · missingR/H LOWER FWD SLIDE SEAL AND HARDWARE MISSING<[01] REPLACED R/H LOWER FWD SLIDE SEAL AND HARDWARE IAW AMM 53-31-31-400-803.;[02] CORRECTIVE ACTION COMPLETED.May 18, 2025 · N7823A · Boeing 7377CT · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2025051268286Lamp · inoperativeEMERGENCY LIGHT AT SEAT ROW 14ABC INOPERATIVE.<[01] REMOVED AND REPLACED EMERGENCY LIGHT LAMP AT SEAT ROW 14ABC. REF AMM 33-51-01. OPERATIONAL CHECK GOOD.May 7, 2025 · N567WN · Boeing 7377CT · Emergency LightingSDR SWAA2025051268285Lamp · inoperativeEMERGENCY LIGHT AT SEAT ROW 6DEF INOPERATIVE.<[01] REMOVED AND REPLACED EMERGENCY LIGHT LAMP AT SEAT ROW 6DEF. REF AMM 33-51-01. OPERATIONAL CHECK GOOD.May 7, 2025 · N567WN · Boeing 7377CT · Emergency LightingSDR SWAA2025042827120Isolator · crackedAFT PASSENGER DOOR'S FORWARD ESCAPE SLIDE ATTACH BRACKET'S UPPER ISOLATOR IS CRACKED.<[01] R&R AFT PASSENGER DOOR'S FORWARD ESCAPE SLIDE ATTACH BRACKET'S UPPER ISOLATOR PER SRM 51-40-02.Apr 22, 2025 · N7831B · Boeing 7377CT · Escape SlideSDR SWAA2025042226090Lamp · inoperativeEMERGENCY AREA LIGHTS AT SEAT ROW 12 LH & 13 RH INOP<[01] RELAMPED EMERGENCY AREA LIGHTS AT SEAT ROW 12 LH & 13 RH IAW AMM 33-51-03 OPS CHECK OKApr 18, 2025 · N7823A · Boeing 7377CT · Emergency LightingSDR SWAA2025042325101Light · inoperativeLEFT HAND OVERWING EMERGENCY EXIT LIGHT ON AFT SIDE INOP <[01]. REMOVED LEFT OVERWING EMERGENCY EXIT SIGN LIGHT ASSEMBLY IAW AMM 33-51-01-960-802; FOUND BROKEN WIRE OF CONNECTOR D12396. REPAIRED WIRE OF CONNECTOR D12396 IAW WDM 33-51-21; SWPM 20-30-12 AND PEApr 15, 2025 · N570WN · Boeing 7377CT · Emergency LightingSDR SWAA2025042124923Handle · looseAFT SERVICE DOOR HANDLE LOOSE; AFT SERVICE DOOR LIGHT ON AT CLIMB. INSPECTED AFT SERVICE DOOR AND FOUND EXCESSIVE PLAY WITH INTERIOR DOOR HANDLE. SECURED HANDLE AS REQUIRED PER AMM 52-41-31. OPS CHECKS GOOD. OK FOR SERVICE.Apr 15, 2025 · N7831B · Boeing 7377CT · Service DoorsSDR SWAA2025042324389Seat · looseSEAT AT ROW 11ABC I/B REAR FOOT WILL NOT TIGHTEN <[01]. REMOVED AND REPLACED THE REAR I/B SEAT FOOT IAW SOPM 20-50-01. INSTALLED SEAT AND TORQUED IAW AMM 25-22-00-400-802. ATS3239; DUE 03/2026; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLApr 13, 2025 · N570WN · Boeing 7377CT · Passenger Compartment EquipmentSDR SWAA2025042323602Scuff Plate · crackedAFT CARGO FWD CORNER SCUFF PLATE CRACKED <[01]. REPAIRED ACB FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1. SCUFF PLATE IS TO BE INSTALLED ON CUSTOMER CARD TTG8Q00ZL13U; [02] VERIFIED CORRECTIVE ACTION.Apr 10, 2025 · N570WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025043021762Stringer Splice · corrodedCORROSION STRINGER SPLICE 28L STA360 AT EQUIPMENT ELECTRONIC COMP 2025-238305<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26. TEMPERATURE CONTROLLER: P/N: P3015GOES00000 S/N: 142811019 DUE DATE: 29-JAN-26.;[02Apr 4, 2025 · N7828A · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2025043021682Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 215 AT LT WING 2025-238300<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 215 AT LT WING IAW B737-700 SRM 51-40-02-0G AND DWG 115A2001 SHEET:30 REV:A. MEASURE CRACK IS 0.322 INCApr 4, 2025 · N7828A · Boeing 7377CT · Wing Miscellaneous StructureSDR SWAA2025043021684Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING 2025-238301<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING IAW. B737-700 SRM 51-40-02-0G AND DWG. 115A2001 SHEET 29 REV - MEASURE CRACK IS L=0.780 Apr 4, 2025 · N7828A · Boeing 7377CT · Wing Miscellaneous StructureSDR SWAA2025043021685Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 272 DEFLECTION CONTROL RIB AREA AT RT WING 2025-238302<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 272 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A930 SHEET 8 REV -Apr 4, 2025 · N7828A · Boeing 7377CT · Wing Miscellaneous StructureSDR SWAA2025043055843Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 215 AT LT WING 2025-238300<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 215 AT LT WING IAW B737-700 SRM 51-40-02-0G AND DWG 115A2001 SHEET:30 REV:A. MEASURE CRACK IS 0.322 INCApr 4, 2025 · N7828A · Boeing 7377CT · Wing Miscellaneous StructureSDR SWAA2025043055845Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING 2025-238301<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING IAW. B737-700 SRM 51-40-02-0G AND DWG. 115A2001 SHEET 29 REV - MEASURE CRACK IS L=0.780 Apr 4, 2025 · N7828A · Boeing 7377CT · Wing Main, Frame StructureSDR SWAA2025043055846Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 272 DEFLECTION CONTROL RIB AREA AT RT WING 2025-238302<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 272 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A930 SHEET 8 REV -Apr 4, 2025 · N7828A · Boeing 7377CT · Wing Miscellaneous StructureSDR SWAA2025042955847Stringer Splice · corrodedCORROSION STRINGER SPLICE 28L STA360 AT EQUIPMENT ELECTRONIC COMP 2025-238305<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26. TEMPERATURE CONTROLLER: P/N: P3015GOES00000 S/N: 142811019 DUE DATE: 29-JAN-26.;[02Apr 4, 2025 · N7828A · Boeing 7377CT · Fuselage Main, Longeron/StringerSDR SWAA2025042321761Skin · crackedCRACK NOTED ON RH HORIZONTAL STABILIZER LOWER SKIN AT STA 193.90 RIB; 17.5' FROM FWD EDGE; L: 0.75' MARKED <[01]. EDITED 13 TO PARTIAL; [02] PERFORMED REPAIR ON RH HORIZONTAL STABILIZER LOWER SKIN AT STA 193.90 RIB; 17.5' FROM FWD EDGE IAW SRM 51-40-02-0G-0 AApr 4, 2025 · N570WN · Boeing 7377CT · Horizontal Stabilizer StructureSDR SWAA2025043055842Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS261 AT LT WING 2025-238292<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS261 AT LT WING IAW. B737-700 SRM 51-40-02-0G AND DWG. 115A2001 SHEET 29 REV - MEASURE CRACK IS L=0.932 INApr 3, 2025 · N7828A · Boeing 7377CT · Wing Miscellaneous StructureSDR SWAA2025042955841Frame · crackedCRACK ON FRAME LOCATED BS 727D BTW STR 8R TO STR 9R AT PASSENGER CABIN 2025-238282<[01] PERFORMED REPAIR ON FRAME LOCATED BS 727D BTW STR 8R TO STR 9R AT PASSENGER CABIN IAW EA 1-A53-12114 SEE INDIVIDUAL SIGNOFF BELOW.;[02] TASK COMPLETED RIIApr 3, 2025 · N7828A · Boeing 7377CT · Fuselage Main, FrameSDR SWAA2025042321205Scuff Plate · crackedFWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE IS CRACKED <[01]. UPON FURTHER INVESTIGATION; SCUFF PLATE WAS DAMAGED BEYOND REPAIR. RECEIVED NEW FCB FWD CORNER SCUFF PLATE FROM STORES. LOCATED AND DRILLED IAW BOEING DWG 143A8331 REV-C AND SRM 51-40-05.; [02] VERApr 2, 2025 · N570WN · Boeing 7377CT · Cargo CompartmentsSDR SWAA2025042320972Floor Panel · delaminatedPASS CABIN FLOOR 241AF DELAMINATED IN SEVERAL AREAS <[01]. FABRICATION OF NEW 241AF FLOOR PANEL HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]; [02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 2, 2025 · N570WN · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025042321200Scuff Plate · crackedAFT CARGO COMPARTMENT; AFT CORNER SCUFF PLATE IS CRACKED. <[01] WELDED THE CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1594362-1 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(4). REFERRED TO BAC5975 EQUIPMENT USED; WELDING MACHINE ID# E10583 CAL DUE DATE 01/2Apr 2, 2025 · N570WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025042321202Structure · corrodedCORROSION ON CREASE BEAM INNER CHORD UPPER SURFACE; STA 687-727; RBL65 WL208. <[01] REMOVED AND REPLACED INNER CREASE BEAM CHORD BS 675-732 RBL 65 WL 208 P/N 144A5910U10 LOT 1601385-1 I.A.W SRM 51-40-02-0G-0 AND DWG 144A5900; [02] REMOVED AND REPLACED INNER CRApr 2, 2025 · N570WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025042321203Panel · crackedCRACKED PANEL BREAK BS 540 BL0-LBL25; WL208 <[01]. INSTALLED NEW PANEL BREAK BS 540 BL0-LBL25; WL208 PER SRM 51-40-02; 51-40-05 AND DWG 143A0060 REV A.; [02] VERIFIED ACTION 1. JOB COMPLETE.Apr 2, 2025 · N570WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025042321204Panel · crackedCRACKED PANEL BREAK BS 540 BL0-RBL25; WL208 <[01]. REMOVED AND REPLACED PANEL BREAK BS 540 BL0-RBL25; WL208 PER SRM 51-40-02; 51-40-05 AND DWG 143A0060 REV A.; [02] VERIFIED ACTION 1. JOB COMPLETE.Apr 2, 2025 · N570WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025040720989Air Data Module · failedIAS DISAGREE ON BOTH PFDS - CAPT SIDE UNRELIABLE. LOST AIRSPEED / ALTITUDE / EECS ON ALTN / SPEED TRIM FAIL.<[01] R&R FO?S AIR DATA MODULE IAW AMM 34-21-04;[02] R&R FO?S AIR DATA MODULE IAW AMM 34-21-04<BR>A/C RECERTIFIED TO CAT III STATUS PER MT 734-00-03<BR>Apr 2, 2025 · N7825A · Boeing 7377CT · Air Data ComputerSDR SWAA2025040220605Seat · loosePASSENGER SEAT LOOSE IN TRACK AT 12DEF.<[01] RESECURED SEAT ROW 12DEF IN FLOOR TRACK REF AMM 25-22-00Apr 2, 2025 · N566WN · Boeing 7377CT · Passenger Compartment EquipmentSDR SWAA2025043020500Pressure Web · crackedCRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT RBL 41 BETWEEN STA 663 TO BS 675 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.375 IN. APPROX 2025-238167<[01] TOOL USED ON STEP 6 AND STEP 7:EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 200048001; DApr 1, 2025 · N7828A · Boeing 7377CT · Fuselage Main, StructureSDR SWAA2025043020347Threshold · crackedCRACK ON THRESHOLD SHEET AFT CARGO COMPARTMENT 2025-238163<[01] REPLACED THRESHOLD SHEET AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A8340 SHEET 16 REV - SEE INDIVIDUAL SIGNOFFS BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED THRESHOLD SHEET AFApr 1, 2025 · N7828A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025043020771Floorbeam · crackedCRACK ON BRAKE PANEL FLOOR STRUCTURE LOCATED STA540 AND LBL 1 AT PASSENGER CABIN 2025-238184<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED STA540 AND BETWEEN LBL 0 AND LBL 24.75 AT CENTER PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DApr 1, 2025 · N7828A · Boeing 7377CT · Fuselage Main, Floor BeamSDR SWAA2025043020501Access Panel · delaminatedDELAMINATED ACCESS PANEL 193B BODY FAIRING AT LOWER FUSELAGE 2025-238170<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189334; DUE DATE: 26/JAN/26.;[02] TOOL USED SCALE PN: SCA-301; SN: AE-41435; DUE DATE: 11/APR/25.;[03] TOOL USED MULTIMETER P/N: FLUKE 1587 FApr 1, 2025 · N7828A · Boeing 7377CT · Aerodynamic FairingsSDR SWAA2025043020348Scuff Plate · crackedCRACK FWD CORNER SCUFF PLATE AFT CARGO COMPARTMENT 2025-238162<[01] TOOL USED DIGITAL CALIPER P/N: 500-193-30; S/N: 0000291; DUE DATE: 01-NOV-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :1753759 ; DUE DATE : 30/JUN/25;[03] REPAIRED THE FWD Apr 1, 2025 · N7828A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025043055801Threshold · crackedCRACK ON THRESHOLD SHEET AFT CARGO COMPARTMENT 2025-238163<[01] REPLACED THRESHOLD SHEET AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A8340 SHEET 16 REV - SEE INDIVIDUAL SIGNOFFS BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED THRESHOLD SHEET AFApr 1, 2025 · N7828A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025043055802Scuff Plate · crackedCRACK FWD CORNER SCUFF PLATE AFT CARGO COMPARTMENT 2025-238162<[01] TOOL USED DIGITAL CALIPER P/N: 500-193-30; S/N: 0000291; DUE DATE: 01-NOV-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :1753759 ; DUE DATE : 30/JUN/25;[03] REPAIRED THE FWD Apr 1, 2025 · N7828A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025043055807Floorbeam · crackedCRACK ON BRAKE PANEL FLOOR STRUCTURE LOCATED STA540 AND LBL 1 AT PASSENGER CABIN 2025-238184<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED STA540 AND BETWEEN LBL 0 AND LBL 24.75 AT CENTER PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DApr 1, 2025 · N7828A · Boeing 7377CT · Fuselage Main, Floor BeamSDR SWAA2025043055804Access Panel · delaminatedDELAMINATED ACCESS PANEL 193B BODY FAIRING AT LOWER FUSELAGE 2025-238170<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189334; DUE DATE: 26/JAN/26.;[02] TOOL USED SCALE PN: SCA-301; SN: AE-41435; DUE DATE: 11/APR/25.;[03] TOOL USED MULTIMETER P/N: FLUKE 1587 FApr 1, 2025 · N7828A · Boeing 7377CT · Aerodynamic FairingsSDR SWAA2025042955803Pressure Web · crackedCRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT RBL 41 BETWEEN STA 663 TO BS 675 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.375 IN. APPROX 2025-238167<[01] TOOL USED ON STEP 6 AND STEP 7:EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 200048001; DApr 1, 2025 · N7828A · Boeing 7377CT · Fuselage Main, StructureSDR SWAA2025043020344Access Panel · crackedCRACK AROUND HOLES ACCESS PANEL 561CB TRAILING EDGE AT LT WING 2025-238153<[01] TOOL USED ON STEP 12:ULTRASONIC EQUIPMENT P/N:EPOCH 650; S/N:190984811; DUE DATE:24-FEB-26;[02] TOOL USED: HUMIDITY/TEMPERATURE CHART RECORDER P/N: TH800; S/N: 08193228; DUE DATE: Mar 31, 2025 · N7828A · Boeing 7377CT · Aerodynamic FairingsSDR SWAA2025043055798Access Panel · crackedCRACK AROUND HOLES ACCESS PANEL 561CB TRAILING EDGE AT LT WING 2025-238153<[01] TOOL USED ON STEP 12:ULTRASONIC EQUIPMENT P/N:EPOCH 650; S/N:190984811; DUE DATE:24-FEB-26;[02] TOOL USED: HUMIDITY/TEMPERATURE CHART RECORDER P/N: TH800; S/N: 08193228; DUE DATE: Mar 31, 2025 · N7828A · Boeing 7377CT · Wing, Plate/Skin
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