Boeing 737-7BD

Service difficulty reports · 7,528

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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 = '7377BD'
  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 SWAA2024090315312Floorbeam · crackedFWD PASSENGER COMPARTMENT WET AREA; CRACK ON FLOOR BEAM WL 208 BS 295.5 RBL 52.<[01] REMOVED DAMAGED AREA OF FLOOR BEAM AND REPAIRED AT BS 295.5 RBL 26 TO RBL 64 WL 208 IAW SRM 53-10-51-2R-16.;[02] TASK COMPLETED;[03] VERIFIED STEPS AND CORRECTIVE ACTION ITEMSJul 22, 2024 · N7739A · Boeing 7377BD · Fuselage Main, Floor BeamSDR SWAA2024090315316Floor Support · crackedFWD PASSENGER COMPARTMENT WET AREA; CRACK ON INTERCOSTAL WL 208 BS 344+6 RBL 31.<[01] REMOVED AND INSTALLED REPLACEMENT INTERCOSTAL WL 208; BS 344 TO 360; RBL 31 IAW SRM 51-40-02-0G-0.;[02] REJECTION: FLOOR INTERCOSTAL INSTALATION AT STA 344 RBL 31 HAS 2 MISSIJul 22, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024090315320Floor Support · crackedFWD PASSENGER COMPARTMENT WET AREA; CRACK ON INTERCOSTAL WL 208 BS 344+5 CENTERLINE.<[01] DAMAGE EXCEEDS LIMITATIONS PER SRM 53-10-51-1A-1. REMOVED AND REPLACED INTERCOSTAL AT STA 344-360; LBL 11; PER SRM 51-40-02-0G-0; REF BOEING DWG 141A5400 SHEET 34;[02] VEJul 22, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024082915396Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241AF HAS DELAMINATION<[01] PASSENGER CABIN FLOOR PANEL 241AF WITH DELAMINATION WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.Jul 22, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024082315300Bracket · crackedCRACK ON SUPPORT BRACKET ACCESS PANEL 651FB TRAILING EDGE AT RT WING 2024-443808<[01] REPLACED SUPPORT BRACKET AND FASTENERS ON ACCESS PANEL 651FB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; 51-40-02 AND DWG 115A2710 REV: - .<BR>MESSURE OF CRAJul 22, 2024 · N7732A · Boeing 7377BD · Wing Miscellaneous StructureSDR SWAA2024090314887Bonding Jumper · corrodedLH WING TE; LOWER O/B FIXED TE ACCESS PANEL; AILERON TRANSMITTER BONDING JUMPER SCREW HAS CORROSION.<[01] REMOVED AND INSTALLED LH WING AILERON POSITION TRANSMITTER BONDING JUMPER GROUNDING TERMINAL IAW SWPM 20-20-10;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.Jul 21, 2024 · N7739A · Boeing 7377BD · Wing System WiringSDR SWAA2024090315156Jumper · corrodedCORROSION ON LOWER BONDING JUMPER TO AFT BOOST PUMP TANK #1.<[01] REMOVED AND REPLACED LOWER BONDING JUMPER TO AFT BOOST PUMP TANK #1 IAW AMM 28-22-41-400-801. SEE PREVIOUS STEPS TO VERIFY.;[02] VERIFIED CORRECTIVE ACTION STEP 1.Jul 21, 2024 · N7739A · Boeing 7377BD · Fuel System WiringSDR SWAA2024090314891Balance Weight · corrodedLH WING TE; LOWER O/B FIXED TE ACCESS PANEL; I/B AILERON BALANCE WEIGHT ORSS 514+14 HAS CORROSION.<[01] REMOVED AND REPLACED AILERON BALANCE WEIGHT IAW CMM 57-50-26;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.Jul 21, 2024 · N7739A · Boeing 7377BD · AileronsSDR SWAA2024082315142Access Panel · crackedCRACK ON ACCESS PANEL 334GB ELEVATOR LT HORIZONTAL STABILIZER 2024-443804<[01] TOOL USED; CALIPER PN: 500-197-30; SN: A18229508; DUE DATE: 14/JAN/25.;[02] TOOL USED CALIPER PN: 500-464; SN: B17030933; DUE DATE: 07/NOV/24.;[03] TOOL USED HOT BONDER PN: HCS9200BJul 21, 2024 · N7732A · Boeing 7377BD · Horizontal Stabilizer, Plate/SkinSDR SWAA2024090314873Stub Frame · crackedFWD SERVICE DOOR CUTOUT SURROUND STRUCTURE; AFT FACE TO THE DOOR FRAME WL 208 RBL 55 BS 291.5+4 HAS CRACK.<[01] TRIMED OUT DAMAGE PART OF THE STUB FRAME AND FABRICATED; LOCATED; DRILLED AND ISTALLED NEW CLIP AT BS 291.5+4 RBL 55 WL 208 IAW SRM 53-10-15-2R-7;[0Jul 20, 2024 · N7739A · Boeing 7377BD · Fuselage Main, FrameSDR SWAA2024090314875Intercostal · crackedFWD ENTRY DOOR CUTOUT SURROUND STRUCTURE; INTERCOSTAL BS 303.9+8 S-6L HAS CRACK.<[01] HFEC INSPECTED FRAME AT BS 303.9+8' STR 6L PER 737NDT PART 6 51-00-00 PROCEDURE 23. FOUND CRACK ON EDGE OF EXISTING TRIM OUT. MARKED END OF CRACK WITH BLACK SHARPIE; CRACK MEJul 20, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024083014849Floorbeam · corrodedAFT PASSENGER COMPARTMENT WET AREA; CORROSION ON FLOOR BEAM BS 986.5 LBL 35 TO 45.<[01] REMOVED AND REPAIRED BS986 L/H FLOOR BEAM UPPER CHORD RBL 36 TO RBL 48 I.A.W SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4;[02] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COJul 20, 2024 · N7739A · Boeing 7377BD · Fuselage Main, Floor BeamSDR SWAA2024083014871Strap · corrodedAFT PASSENGER COMPARTMENT WET AREA; CORROSION ON TENSION STRAP WL 208; LBL 5; BS 1016+14.<[01] REMOVED AND REPLACED NEW TENSION STRAP LBL5 BS1006-BS1030 WL208 I.A.W SRM 51-40-02-0G-0.;[02] INSTALLED NEW TENSION STRAP LBL5 BS1006-BS1030 WL208 I.A.W SRM 51-40-02Jul 20, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024090314391Fitting · corrodedAFT PASSENGER COMPARTMENT; VERTICAL FIN FRONT SPAR FITTING; BS 1016 CENTERLINE WL 283 CORROSION ON BOTH ATTACH POINTS GALLEY.<[01] REPLACED BOTH BUSHINGS AND CLIPS ON AFT PASSENGER COMPARTMENT;VERTICAL FIN FRONT SPAR FITTINGS; BS 1016 CENTERLINE WL 208 IAW AMMJul 19, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024090314421Shear Web · corrodedAFT PASSENGER COMPARTMENT WET AREA; CORROSION ON SHEAR WEB SEVERAL AREAS LBL 5; BS 1016+2; 1016+16.<[01] REMOVE AND REPLACE ACCOMPLISHED ON CCN TTG8Q00UQ37R;[02] UPDATED TABLE MEASUREMENT;[03] VERIFIED. CARD COMPLETE.Jul 19, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024090314409Shear Web · corrodedAFT PASSENGER COMPARTMENT WET AREA; CORROSION ON SHEAR WEB SEVERAL AREAS LBL 7 TO 13; BS 1016+10; 1016+16; AND LBL 17; BS 1016+5.<[01] REMOVE AND INSTALL L/H BS1016-BS1030 WL208 SHEAR WEB IAW SRM 51-40-02-0G-0;[02] REMOVED AND INSTALLED L/H BS1016-BS1030 WL208Jul 19, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024090314373Former · crackedR/H FAIRING FORMER BS 500D BETWEEN STRINGER 18 R/H AND 19 R/H IS CRACKED<[01] REMOVED AND REPLACED FAIRING FORMER AT BS 500D BETWEEN STR 18R TO STR 19R; WL 188 PER SRM 51-40-02 AND DWG:116A3010; ID:0029; REV: B.;[02] VERIFIED.Jul 19, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024090314385Attach Angle · crackedR/H UPPER ATTACH ANGLE BS 663 RBL 6 WL 165 CRACKED (MARKED) B.S. 663 R/H LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT RBL 6 W.L. 165.<[01] REMOVED AND REPLACED R/H UPPER ATTACH ANGLE VAPOR BARRIER BS 664 WL 165 IAW SRM 51-40-02 AND DWG 111A1000 REJul 19, 2024 · N7739A · Boeing 7377BD · Fuselage Main, Attach FittingsSDR SWAA2024083014405Floorbeam · corrodedAFT PASSENGER COMPARTMENT WET AREA; CORROSION ON CROSSBEAM SEVERAL AREAS WL 208;BS 986.6; RBL 27 TO RBL 48.<[01] REMOVED AND REPAIRED BS986 R/H FLOOR BEAM UPPER CHORD RBL 34 TO RBL 48 I.A.W SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4;[02] VERIFIED CORRECTIVE ACTIJul 19, 2024 · N7739A · Boeing 7377BD · Fuselage Main, Floor BeamSDR SWAA2024083014415Strap · corrodedAFT PASSENGER COMPARTMENT WET AREA; CORROSION ON TENSION STRAP WL 208; RBL 5; BS 1006+2; 1016; 1016+10 TO 1016+14.<[01] TENSION STRAP TO BE REMOVED AND REPLACED ON CCN TTG8Q00UP776 DUE TO CORROSION DAMAGE AND NOT ALLOWABLE ENTRIES ON SRM I.A.W SRM 51-10-02-0G-Jul 19, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024083014425Strap · corrodedAFT PASSENGER COMPARTMENT WET AREA; CORROSION ON TENSION STRAP LBL 28; BS 1016+1; 1016+14; 1016+8.<[01] REMOVED AND INSTALLED NEW TENSION STRAP BS1006-BS1024 LBL28 WL208 I.A.W SRM 51-40-02-0G-0;[02] REMOVED AND INSTALLED NEW TENSION STRAP BS1006-BS1024 LBL28 WJul 19, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024083014411Strap · corrodedAFT PASSENGER COMPARTMENT WET AREA; CORROSION ON TENSION STRAP LBL 18; BS 1016+9 TO 1016+14.<[01] REMOVED AND INSTALLED NEW TENSION STRAP BS 1006-1028 LBL 18 WL 208 IAW SRM 51-40-02-0G-0;[02] REMOVED AND INSTALLED NEW TENSION STRAP BS 1006-1028 LBL 18 WL 208 IJul 19, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024083014417Strap · corrodedAFT PASSENGER COMPARTMENT WET AREA; CORROSION ON TENSION STRAP WL 208; RBL 18; BS 1016+12.<[01] REMOVED AND REPLACED TENSION STRAP BS 1006-1028 RBL 18 WL 208 IAW SRM 51-40-02-0G-0;[02] REMOVED AND REPLACED TENSION STRAP BS 1006-1028 RBL 18 WL 208 IAW SRM 51-40Jul 19, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024072214639Power Supply · faultyEMERGENCY EXIT LIGHTS ARC HALF ON HALF OFF WITH AIRCRAFT ON GROUND POWER ON APU POWER.<[01] R/R RIGHT AFT POWER SUPPLY AS PER AMM 33-51-06. OPS CK OK. NO FAULTS NOTED AT THIS TIME.Jul 19, 2024 · N7737E · Boeing 7377BD · Emergency LightingSDR SWAA2024090314355Floor Panel · corrodedMAIN CABIN FLOORBOARD AREA AT RBL 6; WL 208 & STA 1008 APPROX; FOUND 1EA MISDRILLED HOLE AT PLATE MARKED<[01] TENSION STRAP TO BE REMOVED AND REPLACED ON CCN TTG8Q00UP776 DUE TO CORROSION DAMAGE AND NOT ALLOWABLE ENTRIES ON SRM I.A.W SRM 51-10-02-0G-0 PAR 9.C;Jul 18, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024090313840Attach Angle · corrodedCORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS767 TO BS787 RBL21 WL156<[01] REMOVED AND REPLACED ANGLE UNDER SHIELD AT ACB BETWEEN BS 767 TO BS 787+6' ;RB 21; WL 156 PER SRM 51-40-02 AND DWG:146A8123;ID:0016;REV:-;[02]Jul 18, 2024 · N7739A · Boeing 7377BD · Fuselage Main, Attach FittingsSDR SWAA2024083014357Strap · corrodedMAIN CABIN FLOORBOARD AREA AT RBL 6; WL 208 & STA 1028 APPROX; FOUND CORROSION AT PLATE MARKED<[01] REMOVED AND INSTALLED NEW TENSION STRAP RBL6 BS1006-BS1028 WL208 I.A.W SRM 51-40-02-0G-0;[02] REMOVED AND INSTALLED NEW TENSION STRAP RBL6 BS1006-BS1028 WL208 IJul 18, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024083013842Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] REMOVED AND REPLACED SHIELD AT ACB BETWEEN BS 767 TO 787+6';RBL 22; WL 156 PER SRM 51-40-02 AND DWG:146A0081;ID:0034;REV:-;[02] VERIFIED CORRECTIJul 18, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024083013844Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS767+6 RBL11.5 WL156<[01] EVALUATED CORROSION ON STRAP BS 767+6 RBL 11.5 WL 156; FOUND TO BE OUT OF LIMITS; RECEIVED NEW STRAP AND APPLIED WHITE ENAMEL; NEW STRAP TO BE INSTALLED ON FAULT TTG8Q0Jul 18, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024083013846Support Plate · 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 SIDEWALL SUPPORT AT ACB BETWEEN BS727+4 TO BS 847 LBL 22 WL 156 PER SRM 51-40-02. AND BOEING DWG 146A7502 IDJul 18, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024083013848Support Plate · corrodedCORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] REMOVE AND REPLACE SIDEWALL SUPPORT AT ACB BETWEEN BS 727+4' TO BS 767 RBL 22 WL 156 PER SRM 51-40-02 AND BOEING DWG 146A7500Jul 18, 2024 · N7739A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024082314333Floor Support · crackedAAI REPORT: PASSENGER CABIN FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540 BL O TO RBL 24.75 2024-443778<[01] REPLACED CABIN FLOOR STRUCTURE SUPPORT LOC. STA 540 BL 0 TO RBL 24.75 IAW B737-700 SRM 51-10-02 ITEM 9 DWG 143A00600 SHEET 46 REV. -<BR>SEE INDIVIDUAL SJul 18, 2024 · N7732A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024082314334Floor Support · crackedAAI REPORT: PASSENGER CABIN FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540 BL 0 TO LBL 24.75. 2024-443779<[01] REPLACED CABIN FLOOR STRUCTURE SUPPORT LOC. STA 540 BL 0 TO LBL 24.75 IAW B737-700 SRM 51-10-02 ITEM9 AND DWG 143A0060 SHEET 46 REV. -;[02] CORRECTED IJul 18, 2024 · N7732A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024083013382Floor Panel · pulledFWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 221BF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Jul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024083013392Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222CF 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] ATTACHED CURE SHEET.Jul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024083013400Floor Panel · pulledFWD FLOOR PANEL 232BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FORWARD FLOOR PANEL 232BF UPPER SKIN; WITH AREAS OF PULLED STRANDS; WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Jul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024083013434Floor Panel · pulledAFT FLOOR PANEL 242SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 241XF AFT UPPER SURFACE DAMAGE HAS BE REPAIRED IAW SRM 53-00-50-2R-1 AND BOEING DWG: 147A5810 ID: 0058.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Jul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024082913386Floor Panel · pulledFWD FLOOR PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221EF 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 Jul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024082913372Floor Panel · pulledFWD FLOOR PANEL 221FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-O PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.Jul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024082913376Floor Panel · pulledFWD FLOOR PANEL 221A UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221A UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-O PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.Jul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024082913388Floor Panel · pulledFWD FLOOR PANEL 222AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222AF 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 Jul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024082913390Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222BF 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] JOB COMPLETE.Jul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024082913394Floor Panel · pulledFWD FLOOR PANEL 222A UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222A 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 ACJul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024082913396Floor Panel · pulledFWD FLOOR PANEL 222B UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222B 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 ACJul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024082913398Floor Panel · pulledFWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-O PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.Jul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024082913406Floor Panel · pulledFLOOR PANEL 231FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-O PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.Jul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024082913410Floor Panel · pulledFLOOR PANEL 232DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232DF 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] JOB COMPLETE.Jul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024082913412Floor Panel · pulledFLOOR PANEL 232FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION 1.Jul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024082913414Floor Panel · pulledAFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241UF 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] JOB COMPLETE.Jul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024082913418Floor Panel · pulledAFT FLOOR PANEL 241VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241VF 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] JOB COMPLETE.Jul 17, 2024 · N7739A · Boeing 7377BD · Fuselage Floor Panel
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