Boeing 737-7BD

Service difficulty reports · 7,528

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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 = '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 SWAA2024010326169Floor 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] PANEL REPLACED. JOB CONov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024010326170Floor 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] PANEL REPLACED. JOB CONov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024010326163Floor 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] PANEL REPLACED. JOB Nov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024010326173Floor Panel · pulledFWD FLOOR PANEL 231CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 231CF 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] PANEL REPLACED. JOB Nov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024010326164Floor Panel · pulledFWD FLOOR PANEL 232AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 232AF 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] PANEL REPLACED. JOB Nov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024010326491Channel · corrodedAFT SERVICE DOOR MOPSILL HAS CORROSION ON UPPER FLANGE; BS 978; RBL 50; WL 209<[01] ASD MOPSILL WILL BE REMOVED AND REPLACED ON FAULT#TTG8Q00PYVBU;[02] VERIFIED ITEM 1.;[03] CARD COMPLETENov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024010326492Skin · crackedDURING INSPECTION ON TTG8Q00AGQLW; FOUND 1EA CRACK ON L/H HORIZONTAL STABILIZER LOWER SKIN AT STATION 193.90 ; 18' FROM FWD EDGE L: 1' MARKED<[01] REMOVED THE DAMAGED PART ON LH HORIZONTAL STABILIZER LOWER SKIN STA 193.90 18' FROM FWD EDGE; CUT OUT DIMENSIONS Nov 30, 2023 · N7730A · Boeing 7377BD · Horizontal Stabilizer, Plate/SkinSDR SWAA2023122926410Scuff Plate · crackedCRACK AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2023-750317<[01] TOOL USED DIGITAL CALIPER P/N:500-193-30;S/N:0000291;DUE DATE:01-NOV-24.;[02] TOOL USED: RADIOMETER KIT; P/N: XRP-3000; S/N: 1753759; DUE DATE: 12-APR-24.;[03] REPAIRED AFT CORNER SCUFF PLANov 30, 2023 · N7752B · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2023122926411Floorbeam · corrodedCORROSION ON FLOOR BEAM BS986.5 LBL43.5 WL208.1 AT AFT GALLEY AREA 2023-750328<[01] TOOL USED: ULTRASONIC THICKNESS GAGE: PN : 45MG SN: 130060401 DUE DATE: 20-MAR-24;[02] PRECISION GAUGE P/N: 2204A65 S/N: AE-411311 DUE DATE: 02/MAY/24;[03] TOOL USED: EDDY CURRNov 30, 2023 · N7752B · Boeing 7377BD · Fuselage Main, Floor BeamSDR SWAA2023122926412Floorbeam · corrodedCORROSION ON FLOOR BEAM BS986.5 RBL43.5 WL208.1 AT AFT GALLEY AREA 2023-750327<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 00D; S/N: 190023010; DUE DATE: 24-JUL-24;[02] REPAIRED FLOOR BEAM BS986.5 RBL43.5 WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM Nov 30, 2023 · N7752B · Boeing 7377BD · Fuselage Main, Floor BeamSDR SWAA2023122128505Tee Angle · crackedT-CLIP P/N 149A7627-5 COMMON TO BS 663 VAPOR BARRIER WL 150 LBL 25 IS CRACKED<[01] REMOVED AND REPLACED PER REF SRM 51-40-02 AND DWG 111A7000;[02] VERIFIED CORRECTIVE ACTIONS STEP 1 AND MEASUREMENTS TABLE.Nov 30, 2023 · N7750A · Boeing 7377BD · Fuselage Main, Attach FittingsSDR SWAA2023122126408Angle · crackedANGLE P/N 149A7218-7 BS 649-663; WL 142-150; LBL 25 IS CRACKED<[01] REMOVED AND REPLACED PER REF SRM 51-40-02 AND DWG 111A7000;[02] VERIFIED CORRECTIVE ACTIONS STEP 1 AND MEASUREMENTS TABLE.Nov 30, 2023 · N7750A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2023113026222Light · inoperativeRIGHT AFT ESCAPE SLIDE EMERGENCY LIGHT INOP<[01] RELAMPED RIGHT AFT ESCAPE SLIDE EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECK NORMAL.Nov 30, 2023 · N7728D · Boeing 7377BD · Emergency LightingSDR SWAA2024010325975Pressure Deck · cracked.5' CRACK FOUND ON HORIZONTAL PRESSURE DECK WEB STA 663 LBL 41. CORRECTION ==.5' CRACK FOUND ON HORIZONTAL PRESSURE DECK WEB STA 663 RBL 41<[01] CORRECTION TO TITLE:<BR>INCORRECTLY PUT 'LBL 41'<BR>CORRECT LOCATION IS RBL 41.;[02] REPAIRED HORIZONTAL PRESSURE DNov 29, 2023 · N7730A · Boeing 7377BD · Fuselage Main, StructureSDR SWAA2024010325978Frame · corrodedAFT PASSENGER COMPARTMENT FLOOR FRAME HAS CORROSION AT FASTENER; BS 986.5; RBL 44; WL 208<[01] ACCOMPLISHED CORROSION REPAIR PER SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE.Nov 29, 2023 · N7730A · Boeing 7377BD · Fuselage Main, FrameSDR SWAA2024010325977Web · corrodedAFT PASSENGER COMPARTMENT 1016 WEB FLOOR STRUCTURE HAS CORROSION AT BS 1016+13; LBL 5; WL 208<[01] AFT PASSENGER COMPARTMENT 1016 WEB FLOOR STRUCTURE HAS CORROSION AT BS 1016+13; LBL 5; WL 208 WAS REPAIRED IAW EA 23-153-03550;[02] VERIFIED CORRECTIVE ACTION ENNov 29, 2023 · N7730A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024010325979Channel · corrodedAFT PASSENGER COMPARTMENT MOPSILL AT THE AFT SERVICE DOOR HAS CORROSION AT BS 967+14; RBL 47; WL 208<[01] REMOVED AND REPLACED MOPSILL AT BS 907 - 1006 RBL 47; WL 208;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE.Nov 29, 2023 · N7730A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024010325976Strap · corrodedAFT PASSENGER COMPARTMENT 1016 TENSION STRAP HAS CORROSION AT BS 1016+11; LBL 3; WL 208<[01] VERIFIED MEASUREMENTS TABLE.;[02] VERIFIED FAULT IS COMPLETEDNov 29, 2023 · N7730A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2023122926072Skin · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.90 RIB AND 8 INCH. FROM REAR SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 1.00 INCH. APPROX. 2023-750170<[01] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE: 15-FEB-24 Nov 29, 2023 · N7752B · Boeing 7377BD · Horizontal Stabilizer, Plate/SkinSDR SWAA2023122925970Vapor Barrier · crackedCRACK ON VAPOR BARRIER LOCATED ON BS663 BTW RBL 40 AND RBL 54.21 AND BTW WL171.5 AND WL160 AT MAIN WHEEL WELL COMPARTMENT 2023-750124<[01] TOOL USED: CALIPER: PN: 600-464;SN: B17030933; DUE DATE: 07-NOV-24;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 1818Nov 29, 2023 · N7752B · Boeing 7377BD · Fuselage Main, BulkheadSDR SWAA2023122125969Floor Panel · pulledAFT FLOOR PANEL 241ACF HAS PULLED THROUGH INSERT<[01] FLOORBOARD 241ACF THROUGH INSERT REPAIR HAS BEEN FINISHED IAW SRM 53-00-50-2R-6.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED FLOOR PANEL 241ACF REPAIR HAS BEEN PERFORMED SRM 53-00-50-2R-6.Nov 29, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023120427045Cylinder · corrodedUPON REMOVAL OF THE INNER CYLINDER; IT WAS FOUND THAT THE OUTER CYLINDER HAS CORROSION ON THE INNER SURFACE. UPON REMOVAL OF THE INNER CYLINDER IT WAS FOUND THAT THE OUTER CYLINDER HAS CORROSION ON THE INNER SURFACE.<[01] TRANSFERRED DISCREPANCY TO TTG8Q00Q1BGNov 29, 2023 · N7736A · Boeing 7377BD · Main Landing Gear Strut/Axle/TruckSDR SWAA2023122125362Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOORBOARD 222BF UPPER SKIN HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED FLOOR PANEL 222BF HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[03] WORNov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125365Floor 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-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125366Floor Panel · pulledFWD FLOOR PANEL 232BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXCESSIVE DAMAGE FWD FLOOR PANEL 232BF WAS REPLACED WITH A NEW SERVICEABLE PART IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125351Floor Panel · pulledPANEL 241WF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241WF 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] PANEL REPLACED. JOB COMPLETE.Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125352Floor Panel · pulledPANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242AF WAS REPLACED WITH NEW SERVICEABLE PANEL IAW SRM 51-10-01-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125355Floor Panel · pulledPANEL 242QF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 242QF 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] PANEL REPLACED. JOB COMPLETE.Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125357Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FWD FLOOR PANEL 221CF WAS REPLACED WITH A NEW SERVICEABLE PANEL IAW SRM 51-10-02-0G-0 PAR 9.A.(1).;[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125360Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221DF UPPER SKIN HAD AREAS OF PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED FLOOR PANEL 221DF PER IS REPAIRED PER SRM 53-00-50-2R-1.;[03] WORKSCOPE COMPLETE.Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125346Floor Panel · pulledPANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 231ZF 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] PANEL REPLACED. JOB COMPLETE.Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125347Floor Panel · pulledPANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 232SF 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 ACTION #1<BR>VERIFIENov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125348Floor Panel · pulledPANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID:0127.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE.Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125349Floor Panel · pulledPANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 241BF WAS REPLACED WITH NEW SERVICEABLE PANEL IAW SRM 51-10-01-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125350Floor Panel · pulledPANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241UF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF DAMAGE IAW SRM 53-00-50-2R-0; DWG 146A5810 ID:0470.;[02] ATTACHED CURE SHEET.<BR>Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125354Floor Panel · pulledPANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241EF 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] PANEL REPLACED. JOB COMPLETE.Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125340Floor Panel · crackedAFT FLOOR PANEL 242WF O/B AFT CORNER IS CRACKED.<[01] REPAIRED DAMAGED O/B AFT CORNER ON AFT FLOOR PANEL 242WF IAW SRM 53-00-50-2R-6.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE.Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125343Floor Panel · pulledAFT FLOOR PANEL 242SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242SF 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 DAMAGE.;[02] PANEL REPLACED. JOB COMPNov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125344Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] VERIFIED COMPLETION OF REPAIR TO AFT FLOOR PANEL 242UF IAW SRM 53-00-50-2R-1;[02] VERIFIED REPAIR OF AFT FLOOR PANEL 242UF IAW SRM 53-00-50-2R-1;[03] WORKSCOPE IS COMPLETE.Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125345Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS.;[02] AL STEPS COMPLETENov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125353Floor Panel · pulledPANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 231YF 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] PANEL REPLACED. JOB COMPLETE.Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125337Floor Panel · pulledAFT FLOOR PANEL 241ABF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXCESSIVE DAMAGE AFT FLOOR PANEL 241ABF WAS REPLACED WITH A NEW SERVICEABLE PART IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125338Floor Panel · pulledAFT FLOOR PANEL 241ADFF UPPER SKIN HAS AREAS OF PULLED STRANDS. CORRECT PANEL IS 241ADF.<[01] AFT FLOOR PANEL 241ADF 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 DAMAGNov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125339Floor Panel · pulledAFT FLOOR PANEL 242RF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242RF 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] PANEL REPLACED. JOB Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125342Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOORBOARD 241ACF UPPER SKIN HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED FLOOR PANEL 241ACF UPPER SKIN HAS BEEN REPAIRED PER SRM 53-00-50-Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125335Floor Panel · pulledAFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ZF UPPER SKIN HAD AREAS OF PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED FLOOR PANEL 241ZF IS REPAIRED PER SRM 53-00-50-2R-1.;[03] WORKSCOPE COMPLETE.Nov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125341Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN PREVIOUS REPAIR HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241XF UPPER SKIN PREVIOUS REPAIR AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS.;[02] ALL STEPS COMPLETENov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2023122125722Panel · delaminatedPANEL 191D OUTER SURFACE HAS AREA OF DELAMINATION.<[01] PANEL 191D OUTER SURFACE HAD AREA OF DELAMINATION REPAIRED 51-70-05-2R-2;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTSNov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Structure (General)SDR SWAA2023122125713Sidewall Support · corrodedAFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727A+2 - 767; RBL 20-22; WL 155<[01] REMOVED AND INSTALLED AFT CARGO COMPARTMENT NEW FLOOR TO SIDEWALL SUPPORT FROM BS 727 TO BS 767 IAW SRM 51-40-02 AND DWG 146A7500.;[02] VERIFIED CORRECTIVENov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2023122125714Sidewall Support · corrodedAFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727E+10 - 787+8; LBL 20-22; WL 155<[01] REMOVED AND INSTALLED AFT CARGO COMPARTMENT NEW FLOOR TO SIDEWALL SUPPORT FROM BS 727 TO BS 847 IAW SRM 51-40-02 AND DWG 146A7500.;[02] VERIFIED CORRECTNov 28, 2023 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
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