Boeing 737-76N

Service difficulty reports · 4,807

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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 = '73776N'
  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 SWAA2024020539669Support Angle · crackedFWD CABIN FLOOR STRUCTURE BETWEEN STA 380 AND 400 LBL 13 WL 208.1 INTERCOSTAL UPPER FLOOR SUPPORT ANGLE IS CRACKED. 124-053<[01] REMOVED AND INSTALLED NEW ANGLE SUPPORT UPPER INTERCOSTAL AT FWD CABIN FLOOR STRUCTURE BETWEEN STA. 380 TO 400 LBL. 13' WL 208.1 REJan 10, 2024 · N7727A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024020539812Support Angle · crackedFWD CABIN FLOOR STRUCTURE BETWEEN STA 380 AND 400 RBL 8.5 WL 208.1 INTERCOSTAL UPPER FLOOR SUPPORT ANGLE IS CRACKED. 124-054<[01] REMOVED AND REPLACED NEW INTERCOSTAL UPPER ANGLE AT MAIN CABIN BETWEEN STA 380 TO 400 RBL 8.5 WL 208.1 MIXED TIME SEALANT 10:00AM Jan 10, 2024 · N7727A · Boeing 73776N · Fuselage Main, StructureSDR SWAA2024012339784Sign · brokenMAIN CABIN AFT LOWERED CEILING PANEL EXIT LIGHT SINGS BROKEN.<[01] REMOVED AND REPLACED MAIN CABIN AFT LOWERED CEILING PANEL EXIT LIGHT SIGN AS PER AMM 33-51-01-960-802.;[02] REMOVED AND REPLACED MAIN CABIN AFT LOWERED CEILING PANEL EXIT LIGHT SIGN AS PER AMM Jan 10, 2024 · N7725A · Boeing 73776N · Emergency LightingSDR SWAA2024012439148Seat Track · corrodedMAIN CABIN SEAT TRACK AT STA 380 TO STA 390 LBL 48 DIRTY MAIN CABIN SEAT TRACK AT STA 380 TO STA 390 LBL 45.5 DIRTY AND CORRODED.<[01] REMOVED AND INSTALLED NEW SEAT TRACK AT MAIN CABIN FROM STA 360 TO STA 480 LBL 45.50 PER SRM 51-40-02-0G-0 AND DWG 143A5300;[Jan 9, 2024 · N7725A · Boeing 73776N · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024020538521Floor Panel · peelingMAIN CABIN AFT WET AREA FLOOR PNL 241ABF UPPER SURFACE DELAMINATED<[01] RECEIVED NEW AFT WET AREA FLOOR PANEL 241ABF; PANEL WILL BE INSTALLED ON TTG8Q00PGLTN.;[02] VERIFIED STEP 1Jan 7, 2024 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020537081Door Sill · crackedFOUND CRACK AT LH INNER CHORD L-1 DOOR SILL AREA STA 303.9<[01] REMOVED AND REPLACED INNER CHORD AT L1 DOOR BETWEEN STA 277 TO 360 SRM 51-40-02-0G-0 AND DWG 141A8110;[02] VERIFIED STEP 1Jan 2, 2024 · N7727A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024013136056Floor Panel · delaminatedCABIN FLOOR PANEL 232QF UPPER SKIN AFT EDGE DENTED/DELAMINATED 1' SQUARE APPROX.<[01] INSTALLED FLOOR PANEL 232QF AS PER B737 AMM 53-21-00-400-801.;[02] CORRECTION: RECEIVED AND INSTALLED NEW PANEL 232QF.<BR>P/N: 143A5810-110. PO#2051706 AS PER B737 AMM 53-21-Dec 28, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2023122735613Transmitter · incorrectTRAILING EDGE FLAPS DISAGREE ON APPROACH. TRAILING EDGE FLAPS INDICATE 13 DEGREES WITH FLAP HANDLE AT 30 DEGREES.<[01] R&R'D L/H FLAP POSITION X-MITTER PER AMM 27-58-01. OPS CHK NORMALDec 27, 2023 · N7733B · Boeing 73776N · Trailing Flap Position Indicating SystemSDR SWAA2024020535400Seal · damagedR/H HORIZONTAL STAB. UPPER ACCESS PANEL # 343AT HAS 2 EA RUBBER SEAL WITH ELONGATED HOLES<[01] REMOVED AND REPLACED R/H HORIZONTAL STAB. UPPER ACCESS PANEL # 343AT BOTH RUBBER SEAL AS BER 51-40-02-0G-0;[02] CORRECTION TO STEP ONE SHOULD READ;<BR>REMOVED AND REDec 26, 2023 · N7727A · Boeing 73776N · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024020535396Floor Support · corrodedAFT CARGO FLOOR SUPPORT AT B/S 887 22' RIGHT TO 8' LEFT IS CORRODED.<[01] REMOVED AND REPLACED TEE ASSY (PN: 146A9401U39 PO: 1728471) AT AFT CARGO COMPT STA 887; LBL 8 TO RBL 22; PER REF SRM 51-40-02-0G-0 AND DWG #146A7500;[02] VERIFIED STEP 1Dec 26, 2023 · N7727A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024020535398Web · corrodedAFT CARGO THRESHOLD WEB HAS LIGHT CORROSION<[01] REMOVED CORROSION AT AFT CARGO COMPT THRESHOLD WEB FROM STA 794.37 TO STA 847; RBL 23 TO RBL 28; PER REF SRM 51-10-02-0G-0.EVALUATED REWORKED AREA. ORIGINAL MATERIAL THICKNESS: 0.050'; MATERIAL LOST: 0.007; REMADec 26, 2023 · N7727A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024020535466Door · corroded***CORROSION*** AT LH INNER CORE FROM STA 312 TO 344; SEVERAL SPOTS OF CORROSION. DOT 82-010.<[01] THE DISCREPANCY WAS COMPLETED IN THE [TTG8Q00QNCTV] SRM 51-40-02-0G-0 AND DWG 141A8110;[02] CORRECTIVE ACTION WAS RESOLVED ON TTG8Q00QNCTVDec 26, 2023 · N7727A · Boeing 73776N · Service DoorsSDR SWAA2024020535110Frame · corrodedCORROSION....R/H CABIN FLOOR FRAME @ STA 1016 RBL 34 WL 208.1 FASTENER HOLE HAS CORROSION. (18-021)<[01] ACCOMPLISHED REPAIR AT RT. CABIN FLOOR FRAME STA 1016 RBL 34 WL 208.1; PER EA24-153-00155-WIP1; EA24-153-00155-WIP2; AND EA24-153-00155-WIP3;[02] VERIFIED Dec 24, 2023 · N7727A · Boeing 73776N · Fuselage Main, FrameSDR SWAA2024020535104Skin · crackedCRACK FOUND AT LT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90; CRACK LENGTH 0.750'; I/B OF I/B FASTENER ROW; 16.5' FROM L/E. CRACK FOUND AT LT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90 CRACK LENGTH 0.750' I/B OF I/B FASTENER ROW 16.5' FROM L/E.<[01Dec 23, 2023 · N7727A · Boeing 73776N · Horizontal Stabilizer, Plate/SkinSDR SWAA2024020239482Support Bracket · crackedPNEUMATIC CROSSOVER DUCT R/H SUPPORT BRACKET CRACKED<[01] REMOVED AND REPLACED PNEUMATIC CROSSOVER DUCT R/H SUPPORT BRACKET IN REF TO B737 SRM 51-40-02-0G-0.;[02] VERIFIED REPLACEMENT OF BRACKET.Dec 23, 2023 · N7727A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024013135042Support Bracket · crackedPNEUMATIC CROSSOVER DUCT L/H SUPPORT BRACKET CRACKED<[01] REMOVED AND REPLACED PNEUMATIC CROSSOVER DUCT L/H SUPPORT BRACKET IN REF TO B737 SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION.Dec 23, 2023 · N7727A · Boeing 73776N · Wing Miscellaneous StructureSDR SWAA2024020534834Floor Panel · peelingMAIN CABIN FLOOR PANEL 241UF UPPER SURFACE HAS PEELED FIBERS (017)<[01] FLOOR PANEL 241UF WILL BE ACCOMPLISHED ON TTG8Q00QKN94.;[02] STEP 1: ENTER IN ERROR.<BR>FLOOR PANEL 241UF WILL BE ACCOMPLISHED ON TTG8Q00QGLV7.;[03] VERIFIED CORRECTIVE ACTION; STEP 2.Dec 22, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534825Floor Panel · peelingMAIN CABIN FLOOR PANEL 241ACF UPPER SURFACE HAS PEELED FIBERS (014)<[01] RECEIVED NEW FLOOR PANEL 241ACF; P/N D104MM0003-311.<BR>PO# 2052116.<BR>PANEL 241ACF WILL BE INSTALLED ON TTG8Q00PGLTL.;[02] VERIFIED STEP 1Dec 22, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534838Floor Panel · peelingMAIN CABIN FLOOR PANEL 242UF UPPER SURFACE HAS PEELED FIBERS (015)<[01] RECEIVED AFT WET AREA FLOOR PANEL 242UF; PANEL WILL BE INSTALLED ON TTG8Q00PGM33.;[02] VERIFIED STEP 1Dec 22, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534832Floor Panel · peelingMAIN CABIN FLOOR PANEL 241AAF UPPER SURFACE HAS PEELED FIBERS (016)<[01] RECEIVED AFT WET AREA FLOOR PANEL 241AAF; PANEL WILL BE INSTALLED ON TTG8Q00PGLTQ.;[02] VERIFIED STEP 1Dec 22, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534835Floor Panel · corrodedMAIN CABIN FLOOR PANEL 241C HAS CORRODED INSERTS (011)<[01] REMOVED AND REPLACED BROKEN INSERTS AT MAIN CABIN FLOOR PANEL 241C REF. SRM. 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION.Dec 22, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534823Floor Panel · corrodedMAIN CABIN FLOOR PANEL 242VF HAS CORRODED INSERTS (004)<[01] REMOVED AND REPLACED. INSERTS BROKEN AT MAIN CABIN FLOOR PANEL 242VF. REF. SRM. 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION.Dec 22, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534824Floor Panel · corrodedMAIN CABIN FLOOR PANEL 241ACF HAS CORRODED INSERTS (005)<[01] THIS ITEM WILL BE ACCOMPLISHED ON TTG8Q00QGLT3; RECEIVED NEW FLOOR PANEL 241ACF.;[02] VERIFIED STEP 1Dec 22, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534837Floor Panel · corrodedMAIN CABIN FLOOR PANEL 241ADF HAS CORRODED INSERTS (006)<[01] REMOVED AND REPLACED BROKEN INSERTS AT MAIN CABIN FLOOR PANEL 241ADF REF.SRM. 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION.Dec 22, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534827Floor Panel · corrodedMAIN CABIN FLOOR PANEL 242UF HAS CORRODED INSERTS (003)<[01] PANEL 242UF WILL BE REPLACED ON TTG8Q00QGN40;[02] VERIFIED STEP 1Dec 22, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534829Floor Panel · corrodedMAIN CABIN FLOOR PANEL 242B HAS CORRODED INSERTS (001)<[01] REMOVED AND REPLACED INSERTS BROKEN AT MAIN CABIN FLOOR PANEL 242B. REF. SRM. 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION.Dec 22, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534830Floor Panel · corrodedMAIN CABIN FLOOR PANEL 241ABF HAS CORRODED INSERTS (009)<[01] PANNEL ASSY 241ABF WILL BE RE PLACED ON ITEM TTG8Q00QSA0K;[02] VERIFIED STEP 1Dec 22, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534839Floor Panel · corrodedMAIN CABIN FLOOR PANEL 241AAF HAS CORRODED INSERTS (008)<[01] THIS ITEM WILL BE ACCOMPLISHED ON TTG8Q00QGLV0.;[02] VERIFIED STEP 1Dec 22, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534392Support Frame · crackedFWD CABIN WET AREA FUSELAGE SUPPORT FRAME CRACKED @ CUTOUT ABOVE L-1 DOOR FWD STA 312 MKD DOT<[01] ACCOMPLISHED REPAIR FOR EA NO:M-22-153-01244;[02] VERIFIED REPAIR ACCOMPLISHED PER EA NO: M-22-153-01244;[03] VERIFIED REPAIR ACCOMPLISHED PER EA NO: M-22-153-01Dec 21, 2023 · N7727A · Boeing 73776N · Fuselage Main, StructureSDR SWAA2024020534397Floor Panel · peelingCABIN FLOOR PANEL 231BF HAS PEELED UPPER SURFACE FIBERS. 124-028<[01] RECEIVED FLOOR PANEL #231BF WITH P/N: 141A5810-168. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00PGM3P;[02] VERIFIED STEP 1.Dec 21, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534626Floor Panel · peelingCABIN FLOOR PANEL 231AF HAS PEELED UPPER SURFACE FIBERS. 124-030<[01] RECEIVED CABIN FLOOR PANEL 231AF WILL BE INSTALLATION WILL BE ACCOMPLISHED ON TTG8Q00PGM3R;[02] RECEIVED CABIN FLOOR PANEL 231AF WILL BE INSTALLED ON TTG8Q00PGM3R;[03] VERIFIED STEP 2 (CORREDec 21, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534627Floor Panel · peelingCABIN FLOOR PANEL 222BF HAS PEELED UPPER SURFACE FIBERS. 124-024<[01] RECEIVED FLOOR PANEL #222BF; WITH P/N:141A5810-507. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00PGLLD.;[02] VERIFIED STEP 1.Dec 21, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534618Floor Panel · peelingCABIN FLOOR PANEL 221EF HAS PEELED UPPER SURFACE FIBERS. 124-027<[01] RECEIVED PANEL: 221EF P/N: 141A5810-526 INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD: 'TTG8Q00PGM44';[02] VERIFIED STEP 1.Dec 21, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534628Floor Panel · peelingCABIN FLOOR PANEL 221BF HAS PEELED UPPER SURFACE FIBERS. 124-032<[01] RECEIVED FLOOR PANEL #221BF WITH P/N: 141A5810-56. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00PGM4B;[02] VERIFIED STEP 1.Dec 21, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534625Floor Panel · peelingCABIN FLOOR PANEL 222A HAS PEELED UPPER SURFACE FIBERS. 124-031 CABIN FLOOR PANEL 222AF HAS PEELED UPPER SURFACE FIBERS. 124-031<[01] RECEIVED CABIN FLOOR PANEL 222A WILL BE INSTALLATION WILL BE ACCOMPLISHED ON TTG8Q00PGLLF;[02] RECEIVED CABIN FLOOR PANEL 222ADec 21, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534633Floor Panel · peelingCABIN FLOOR PANEL 222CF HAS PEELED UPPER SURFACE FIBERS. 124-025<[01] RECEIVED CABIN FLOOR PANEL 222DF WILL BE INSTALLED ON TTG8Q00PGM3W;[02] RECEIVED CABIN FLOOR PANEL 222CF WILL BE INSTALLED ON TTG8Q00PGM3W;[03] VERIFIED STEP 2 (CORRECTION FOR STEP 1)Dec 21, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534395Support Angle · corrodedCORROSION AT AFT CABIN GALLEY DOOR R-2 CUTOUT LOWER SILL SCUFF PLATES SUPPORT ANGLE MKD DOT<[01] REF TASK CARD TTG8Q00QHCG5 FOR REMOVAL OF CORROSION AT R/H MAIN CABIN INNER CHORD.;[02] MEASUREMENTS WILL BE RECORDED ON TTG8Q00QHCG5;[03] VERIFIED STEPS 1 AND 2;[Dec 21, 2023 · N7727A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024020534617Floor Panel · corrodedCABIN FLOOR PANEL 221DF HAS CORRODED INSERTS. 124-023<[01] RECEIVED NEW FLOOR PANEL 221DF; PANEL WILL BE INSTALLED ON <BR>TTG8Q00PGM47.;[02] VERIFIED STEP 1Dec 21, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534619Floor Panel · corrodedCABIN FLOOR PANEL 221CF HAS CORRODED INSERTS. 124-022<[01] RECEIVED NEW FLOOR PANEL 221CF; PANEL WILL BE INSTALLED ON TTG8Q00PGM49.;[02] VERIFIED CORRECTIVE ACTION.Dec 21, 2023 · N7727A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2024020534383Fitting · damagedR/W REAR SPAR T/E LOWER WIGGLE FITTING HAS SHEARED RIVETS AND ELONGATED HOLE O/B OF FLAP TRACK # 6 MKD DOT<[01] REMOVED AND REPLACED WIGGLE FITTING AT R/W REAR SPAR T/E LOWER SRM 51-40-92-0G-0 AND DWM 115A2781;[02] VERIFIED CORRECTIVE ACTION.Dec 21, 2023 · N7727A · Boeing 73776N · Trailing Edge FlapsSDR SWAA2024020534218Support Angle · crackedLH DEFLECTION CONTROL RIB AND SUPPORT BEAM HAS UPPER MIDDLE SUPPORT BULB SEAL CRACKED.<[01] REMOVED AND REAPLACED SUPPORT ANGLE AT L/H DEFLECTION CONTROL RIB PER REF SRM 51-40-02-0G-0 SRM 51-40-05-0G-0;[02] CW;[03] VERIFIED CORRECTIVE ACTION.Dec 20, 2023 · N7727A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024012433390Frame · crackedSTA. 312 FRAME CRACKED ABOVE L1 DOOR FWD CORNER.<[01] ACCOMPLISHED REPAIR AT STA 312 ABOVE L1 DOOR PER M-22-153-01244;[02] VERIFIED REPAIR PER M-22-153-01244Dec 18, 2023 · N7725A · Boeing 73776N · Fuselage Main, FrameSDR SWAA2024012433202Floor Support · corrodedAFT CARGO FLOOR SUPPORT AT B/S 767-787 IS CORRODED 23' RIGHT OF CENTER LINE.<[01] REMOVED AND REPLACE AFT CARGO FLOOR SUPPORT STRAP AT B/S 767-787 (P/N:146A9401U21) REF. SRM 51-40-02-0G-0;[02] VERIFIED STEP 1Dec 18, 2023 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024012932494Rib · crackedRH WING T/E RIGHT ABOVE #2 ENGINE AFT FAIRING TIP THERE IS A RIB CRACKED AT THE BOTTOM BOLT ATTACHMENT HOLE. DOT 82-002.<[01] THIS N/R WAS ACCOMPLISHED ON N/R: TTG8Q00Q7JM0.;[02] VERIFIED STEP 1Dec 15, 2023 · N7725A · Boeing 73776N · Wing, Rib/BulkheadSDR SWAA2024012632192Stiffener · crackedRH HORIZ. STAB RIB 4 STIFFNER 4 SUSPECT CRACK RH HORIZ. STAB RIB 4 STIFFNER 4 CRACKED<[01] ACCOMPLISHED REPAIR AT RH HORIZ. STAB RIB 4 STIFFNER 4 AS PER SRM 55-10-09-2R-5 REPAIR 5.;[02] VERIFIED REPAIR INSTALLATION AT RH HORIZ. STAB RIB 4 STIFFNER 4.Dec 15, 2023 · N7725A · Boeing 73776N · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024012532386Strap · corroded***CORROSION*** AFT WET AREA AT STA 1016+8' RBL20 WL 208.1. DOT 82-012.<[01] REMOVED AND INSTALLED NEW STRAP AT AFT WET AREA STA.1016+8 RBL20 ASPER REF. B737-SRM 51-40-02-0G-0 AND DWG# 147A5700;[02] RII -- VERIFIED 1.Dec 15, 2023 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024012532387Strap · corroded***CORROSION*** AFT WET AREA AT STA 1016 RBL3 WL 208.1. DOT 82-013.<[01] REMOVED AND REPLACE STRAP AT AFT WET AREA AT STA 1016 RBL3 WL 208.1<BR>AS PER REF. B737.700- SRM-51-40-02-0G-0 AND DWG- 147A5600.;[02] VERIFIED STRAP REPLACEDDec 15, 2023 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024012432376Floor Support · crackedFWD CABIN BETWEEN STA 277 AND STA 294.5 AT BL-0 WL 208.1 INTRCOSTAL CRACKED. DOT 124-001<[01] REMOVED AND INSTALLED NEW INTERCOSTAL P/N 141A5410-3 PO# 2028887 AT FWD CABIN BETWEEN STA 277 AND STA 294.5 AT BL-0 WL 208.1 AS PER SRM-51-40-02-0G-0 AND DWG #141A541Dec 15, 2023 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024012432377Floor Support · crackedFWD CABIN BETWEEN STA 312 AND STA 328 RBL 31 WL 208.1 INTERCOSTAL CRACKED 124-003<[01] REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 312 AND STA 328 RBL 31 WL 208.1 AS PER SRM 51-40-02-0G-0 DWG 141A5400;[02] VERIFIED NEW INTERCOSTAL INSTALLEDDec 15, 2023 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2024012432380Floor Support · crackedFWD CABIN BETWEEN STA 380 AND STA 400 BL-0 WL 208.1 INTERCOSTAL CRACKED 124-009<[01] INSTALLED NEW INTEWRCOSTAL AT ABIN BETWEEN STA 380 AND STA 400 BL-0 WL 208.1 PER SRM 51-40-02-0G-0 DWG 143A5400;[02] CORRECTING STEP 1: INSTALLED NEW INTERCOSTAL AT FWD CABIN Dec 15, 2023 · N7725A · Boeing 73776N · Fuselage Miscellaneous Structure
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