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"

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SDR SWAA2021071280230Shield · corrodedCORROSION ON AFT SHIELD AT AFT CARGO BAY BS857 - BS864 RBL21 WL165. ; / [01] EVALUATED CORROSION ON SHIELD; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED - CORROSION ON SHIELD; FOUND TO BE OJun 3, 2021 · N7823A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021070781189Frame · dentedDENT ON FRAME AT AFT CARGO BAY BS747 3' BELOW S-23L WL163. ; / [01] UPDATED DAMAGE TABLE; [02] FRAME IS FOUND OUT OF LIMITS DUE TO NO DENT DAMAGE ALLOWED ON FRAMES PER SRM 51-00-07-1A-1; [03] CUT AND REMOVED DAMAGE FRAME BS 747 3' BELOW STR 23L MEASURING 1.1'XJun 3, 2021 · N7823A · Boeing 7377CT · Fuselage Main, FrameSDR SWAA2021071279712Retainer · crackedRT WING UPPER T/E PANEL JUST AFT OF #2 PYLON; VERT SEAL RETAINER IS CRACKED. ; / [01] REMOVED AND REPLACED RIGHT WING UPPER T/E PANEL JUST AFT OF #2 PYLON VERT. SEAL RETAINER IAW SRM 51-40-02-0G-0 AND AIPC 57-50-00-25.; [02] VERIFIED REMOVED AND REPLACED RIGHTJun 2, 2021 · N7823A · Boeing 7377CT · Wing Main, Frame StructureSDR SWAA2021070879710Floor Support · crackedCRACKED FLOOR SUPPORT BS 277-294.5 BL0 WL208 ; / [01] REMOVED CRACKED FLOOR SUPPORT BS 277-294.5 BL 0 WL 208 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW FLOOR SUPPORT BS 277 - 294.5 PER SRM 51-40-02-0G-0; BOEING DWG 141A5400; SRM 51-40-05-0G-0; [03] OK TO Jun 2, 2021 · N7823A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021070879711Floor Support · crackedCRACKED FLOOR SUPPORT BS 312-328 LBL45 WL208 ; / [01] REMOVED CRACKED FLOOR SUPPORT BS312-328 LBL45 WL208 PER SRM 51-40-02-OG-0.; [02] LOCATED AND DRILED NEW FLOOR SUPPORT AT BS312-328 LBL45 WL208 PER SRM51-40-05-0G-0. OK TO INSTALL; [03] VERIFIED LOCATED AND Jun 2, 2021 · N7823A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021070779707Floor Support · crackedFLOOR SUPPORT CRACKED AT BS 294.5-312 RBL16 WL208 ; / [01] REMOVED INTERCOSTAL FROM BS 294.5-312 RBL 16 WL208 PER SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW INTERCOSTAL FOR BS 294.5-312 RBL16 WL 208 PER SRM 51-40-05-0G-0. OK TO INSTALL; [03] VERIFIED LOCJun 2, 2021 · N7823A · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2021070779709Channel · crackedCRACKED FWD ENTRY DOOR MOPSILL INNER CHORD BS 303.9 LBL50 WL 208 ; / [01] REMOVED CRACKED FWD ENTRY DOOR MOPSILL INNER CHORD IAW SRM 51-40-02; [02] LOCATED AND DRILLED NEW FWD ENTRY DOOR MOPSILL PER SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG 141A8112.; [03]Jun 2, 2021 · N7823A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021070779705Floor Support · crackedCRACKED FLOOR SUPPORT BS 344-360 BL 0 WL 208 ; / [01] REMOVED CRACKED FLOOR SUPPORT INTERCOSTAL AT IAW SRM 51-40-02 AND DWG 141A5400.; [02] LOCATED AND DRILLED NEW INTERCOSTAL PER SRM 51-40-05 AND DWG 141A5400 SHEET 32 AND 16.REQUEST OK TO INSTALL.; [03] VERIFJun 2, 2021 · N7823A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021062179725Scuff Plate · brokenFWD CARGO COMPARTMENT;SHOWS DOOR SILL FWD SCUFF PLATE BROKEN ; / RECEIVED NEW SCUFF PLATE AT FWD CARGO COMPARTMENT LOWER FWD CORNER ISSUE TAG WN5158 P.O 1684224;SCUFF PLATE WILL BE INSTALL ON ROUTINE CARD TTG8Q004CNJV; VERIFIED 1Jun 2, 2021 · N7828A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021060779715Angle · corrodedCORROSION ON THRESHOLD SUPPORT ANGLE BS 312+10 LBL50 WL 209 ; / REPAIR ACCOMPLISHED PER SRM 53-10-15-1A-1; REINSTALLED ONE NUTPLATE ON THRESHOLD SUPPORT ANGLE BS 321 LBL 50 WL 209 PER SRM 51-40-02-0G-0.; VERIFIED COMPLETEJun 2, 2021 · N7823A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021060779706Retainer · crackedRT WING UPPER T/E PANEL JUST AFT OF #2 PYLON; HORIZ SEAL RETAINER IS CRACKED. ; / REMOVED AND REPLACED RIGHT WING UPPER T/E PANEL JUST AFT OF #2 PYLON HORIZ. SEAL RETAINER IAW SRM 51-40-02-0G-0 AND AIPC 57-50-00-25.; VERIFIED REMOVED AND REPLACED RIGHT WING UPJun 2, 2021 · N7823A · Boeing 7377CT · Wing Main, Frame StructureSDR SWAA2021071279268Fairing · chafedCHAFE DAMAGE ON INNER SURFACE OF WING TO BODY FAIRING 193AL ; CHAFE DAMAGE ON INNER SURFACE OF WING TO BODY FAIRING 193AL / [01] IDENTIFIED PANEL 193AL IAW SRM 53-40-70-0I-1.FIG 2; ITEM[7]. FOUND DAMAGE ALONG EDGEBAND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-7Jun 1, 2021 · N7823A · Boeing 7377CT · Aerodynamic FairingsSDR SWAA2021071279279Fairing · chafedCHAFE DAMAGE ON INNER SURFACE OF 192E FAIRING / [01] IDENTIFIED PANEL192E / MATERIAL IAW SRM 53-40-70-0I-1 FIGURE 2. TABLE 2. ITEM (3). FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PAR 4.B.(6)(A). REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-05-Jun 1, 2021 · N7823A · Boeing 7377CT · Aerodynamic FairingsSDR SWAA2021071279284Strap · corrodedCORROSION ON SHEAR WEB TENSION STRAP AT B.S. 1023-1024; L.B.L. 3; W.L. 208.1. ; / [01] REMOVED CORROSION ON STRAP BS1023-1024 LBL3 WL 208 IAW SRM 51-10-02. AREA OF REMOVAL 1'X6' REMOVED .020' MATERIAL. ORIGINAL THICKNESS .071'. NO ALLOWABLE LIMITS IN SRM. PARTJun 1, 2021 · N7823A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021071279277Stiffener · crackedRT HORIZ. STAB RID ASSY. 4 (STAB STA 120.30) 2ND VERT STIFFENER IS CRACKED. ; / REMOVED RT HORIZONTAL STABILIZER INSPAR RIB LOCATED AT STAB STATION 120.30 IAW SRM 51-40-02-0G-0; [03] -SRM 55-10-09-2R-4 REMOVED DAMAGED SECTION ON RIB 3RD STIFFENER IAW SRM 55-10Jun 1, 2021 · N7823A · Boeing 7377CT · Horizontal Stabilizer StructureSDR SWAA2021071279278Floorbeam · corrodedCORROSION ON FLOOR BEAM; ON UPPER SURFACE; AT B.S. 947; R.B.L. 43-49; W.L. 208.1. ; / [01] REMOVED CORROSION ON FLOOR BEAM ON UPPER SURFACE AT B.S. 947 R.B.L. 43-49 W.L. 208.1 IN AREA OF 2.2' BY 6.0' PER SRM 53-70-51-1A-1 AND SRM 51-10-02-0G-0; [02] VERIFIED CJun 1, 2021 · N7823A · Boeing 7377CT · Fuselage Main, Floor BeamSDR SWAA2021071279271Channel · corrodedCORROSION ON AFT ENTRY DOOR MOP SILL AT B.S. 950-986; L.B.L. 52; W.L. 208.1. ; / [01] REMOVED CORROSION ON AFT ENTRY DOOR MOPSILL AT B.S. 950-986 L.B.L. 52 W.L. 208.1 IN AREA OF 2.3' BY 36' BY 0.010' PER SRM 53-70-15-1A-1 AND SRM 51-10-02-0G-0. OUT OF LIMITS PJun 1, 2021 · N7823A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021071278896Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER SUPPORT ANGLE IS CRACKED AT R.B.L. 8; W.L. 164. ; / [01] INSTALLED EWIS PROCTECTION AT REPAIR AREA PER AMM 20-60-07; AND REMOVED FASTENERS PER SRM 51-40-02-0G-0; [02] VERIFIED ITEM 1.; [03] CONFORMED -1 REPLACEMENT ANGLEMay 31, 2021 · N7823A · Boeing 7377CT · Fuselage Main, BulkheadSDR SWAA2021071278890Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER SUPPORT ANGLE IS CRACKED AT L.B.L. 8; W.L. 164. ; / [01] INSTALLED EWIS PROCTECTION AT REPAIR AREA PER AMM 20-60-07; AND REMOVED FASTENERS PER SRM 51-40-02-0G-0; [02] VERIFIED ITEM 1; [03] CONFORMED -1 REPLACEMENT ANGLE May 31, 2021 · N7823A · Boeing 7377CT · Fuselage Main, BulkheadSDR SWAA2021060478898Fairing · chafedWING TO BODY FAIRING PANEL 194CL INNER SURFACE AREAS ARE CHAFED. CHAFING ALONG THE INNER EDGE BAND EXCEEDS THE ALLOWABLE LIMITS OF SRM 53-60-70-1A-1 PARA 4 B 3 A. REMOVED CHAFING DAMAGE FROM ALONG THE INNER EDGE BAND; CLEANED REPAIR AREA. FABRICATED REPAIRMay 31, 2021 · N7823A · Boeing 7377CT · Aerodynamic FairingsSDR SWAA2021060378650Lens · detachedRT. OVERWING EXIT COVER FELL OFF. ; / REINSTALLED RT. OVERWING EXIT LIGHT COVER. REFERENCE AMM 33-51-01. OPS CHECK GOOD.May 30, 2021 · N569WN · Boeing 7377CT · Emergency LightingSDR SWAA2021070779266Pressure Deck · dentedFLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. ; / [01] EVALUATED DENTS ON FLIGHT DECK FLOOR AT BS 255; RBL 4-LBL 14; WL 207.54. DENTS FOUND TO BE GOUGED THEREFORE DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1; FIGURE 105;May 28, 2021 · N7823A · Boeing 7377CT · Fuselage Main, StructureSDR SWAA2021063078363Floor Panel · corrodedAFT CARGO COMPARTMENT FLOOR PANEL 140AF HAS MULTIPLE SPOTS OF CORROSION. ; / [01] PARTIALLY LOCATED AND TRIMMED NEW FLOOR MATERIAL FOR REPLACEMENT OF AFT CARGO FLOOR PANEL 140AF AS PER B737-7 AMM 25-52-01-201-801.; [02] VERIFIED PARTIAL WORK ON 140AF FABRICATIMay 28, 2021 · N7825A · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2021063078362Floor Panel · corrodedAFT CARGO COMPARTMENT FLOOR PANEL 140CF HAS MULTIPLE SPOTS OF CORROSION ; / [01] LOCATED AND DRILLED NEW FLOOR PANEL IAW B737-7 SRM 51-40-05-0G-0; [02] VERIFIED LOCATED AND DRILLED COMPLETED. OK TO TREAT AND PRIME.; [03] TREATED AND PRIMED UNDER SIDE OF NEW AFMay 28, 2021 · N7825A · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2021063078359Floor Panel · delaminatedAFT WET AREA FLOOR PANEL #241ABF TOP SURFACE LAYERS DELAMINATED ; / [01] REPAIRED FLOOR PANEL 241ABF; [02] LATE ENTRY OK TO INSTALL REPAIR; [03] REMOVED DAMAGED FACE SHEET; PREPARED DAMAGED AREA TO APPLY REPAIR PLIES AND APPLIED REPAIR PLIES AT FLOOR PANEL #24May 28, 2021 · N7825A · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2021063078351Floor Panel · delaminatedFORWARD WET AREA FLOOR PANEL # 222AF TOP LAYER DELAMINATED ; / [01] CLEANED AT PANEL 222AF ;AS PER B737-7 SRM 53-00-50-2R-0; [02] VERIFIED CLEANING OF PNL. 222AF ; STEP ONE.; [03] MEASURE; [04] REPAIRED DAMAGE AREA AT FLOOR PANEL #222AF AS PER BOEING SRM 53-00May 28, 2021 · N7825A · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2021063078347Seat Track · corroded**CORROSION**PASSENGER CABIN L/H I/B SEAT TRACK BETWEEN STA # 767 AND STA # 787; WITH SPOT OF SURFACE CORROSION. DOT # 208-15 ; / [01] REMOVED CORROSION AT MAIN CABIN L/H I/B SEAT TRACK BETWEEN STA 767 AND STA 787 AS PER SRM 51-10-02-0G-0; [02] VERIFIED STEP 1May 28, 2021 · N7825A · Boeing 7377CT · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021063078327Seat Track · corroded**CORROSION**PASSENGER CABIN R/H O/B SEAT TRACK AT STA # 807; SPOT OF CORROSION. DOT # 208-45. DOT # 208-45 ; / [01] BLENDED OUT CORROSION AT PASSENGER CABIN R/H O/B SEAT TRACK STA 807 IRW B737-700 SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1; [02] VERIFIED CORROSION May 28, 2021 · N7825A · Boeing 7377CT · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021063078297Strap · corrodedCORROSION. ** AFT WET AREA GALLERY FLOOR SUPPORT. WEB STRAP BETWEEN STA 1006 & 1016 LBL 3 ; / [01] REMOVED CORROSION AT AFT WET AREA GALLEY SUPPORT WEB STRAP BETWEEN STA 1006-1016 LBL 3 AS PER B737-700 SRM 51-10-02-0G-0; NO SRM ALLOWABLE DAMAGE EXIST.; [02] VEMay 27, 2021 · N7825A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021063078296Web · corrodedCORROSION ** AT AFT WET GALLERY SUPPORT FLOOR. WEB FORWARD OF AFT PRESSURE BULKHEAD STA 1016 LBL 4 TO LBL15 ; / [01] REMOVED CORROSION AT WEB STA 1016 AND LBL 4-16 AS PER B737-700 SRM 51-10-02-0G-0; NO SRM ALOWABLE DAMAGE EXIST; [02] REMOVED FASTENER (75%) AS May 27, 2021 · N7825A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021063078291Retainer · crackedLT WING T/E STRUCTURE;SHOWS FIXED PANEL;BETWEEN #5 AND #6 SPOILER PANELS WITH INBFWD SEAL RETAINER CRACKED ATUPPER FWD ATTACHMENT. ; / [01] REMOVED AND REPLACED AT LT WING T/E STRUCTURE FIXED PNL BETWEEN #5 AND #6 SPOILER PANEL I/B FWD SEAL RETAINER IN IAW SRMMay 27, 2021 · N7825A · Boeing 7377CT · Trailing Edge FlapsSDR SWAA2021063078290Floor Support · crackedAFT WET AREA FLOOR. SUPPORT INTERCOSTAL APPEAR CRACK AND HAS ELONGATED HOLES BETWEEN STA 927 & 947 BL -0 ; / [01] PERFORMED HFEC INSP ON AFT WET AREA FLOOR SUPPORT INTERCOSTAL B/W STA 927 & 947 BL-0; IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL UMay 27, 2021 · N7825A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021062178376Skin · delaminatedSPOILER #1 UPPER SURFACE WITH DELAMINATED DENT LOCATED 47' FROM I/B EDGE & 10' FROM AFT EDGE. CLEANED SURFACE; SEALED EDGES OF THE DOUBLER AND APPLIED FINISHED. REF B737-700 SRM 51-20-05 AND AMM 51-21-99.;CUT OUT DAMAGED AREA SIZE 4' DIAMETER AT SPOILER #1 UMay 27, 2021 · N7828A · Boeing 7377CT · SpoilersSDR SWAA2021060778298Web · corrodedCORROSION ON AFT WET AREA FLOOR SUPPORT WEB STRAP STA 1016 RBL 20. REMOVED CORROSION. NO LIMITS FOUND IN SRM. REMOVED PART IAW SRM 51-40-02-0G-0, LOCATED & DRILLED HOLES AT NEW STRAP IAW SRM 51-40-05-0G-0. REMOVED AND INSTALLED THE NEW STRAP IAW SRM 51-40May 27, 2021 · N7825A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021063077767Floorbeam · corrodedAFT CARGO FLOOR SUPPORT AT B/S 771 AT STRINGER 25L TO 25R IS WORN AND CORRODED. ; / [01] REMOVED AND REPLACED AFT CARGO STRAP IAW SRM-51-40-02-0G-0; [02] INSPECTION IS CAPTURED ON CUSTOMER CARD<BR>TTG8Q005JCRMMay 26, 2021 · N7825A · Boeing 7377CT · Fuselage Main, Floor BeamSDR SWAA2021063077766Floor Support · corrodedAFT CARGO FLOOR SUPPORT AT STRINGER 25L 'Z' CHANEL IS CORRODED B/S 700-847 ; / [01] REMOVED AND REPLACED Z-CHANNEL IAW B737-7 SRM 51-40-02-0GH-0; [02] VERIFIED INSTALLATION OF Z-CHANNEL.May 26, 2021 · N7825A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021063077764Floor Support · corrodedAFT CARGO RIGHT FLOOR SUPPORT 'Z' CHANNEL AT STRINGER 25R IS CORRODED AT 700-767 ; / [01] REMOVED CORROSION AT AFT CARGO R/H ZEE CHANNEL FROM 727 TO767 AS PER B737-700 SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS DUE TO EXFOLIATION CORROSION AS PER B737-700 SRMay 26, 2021 · N7825A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021063077763Floor Support · crackedFWD PASSENGER COMPARTMENT FLOOR STRUCTURE;SHOWS INTERCOSTAL UPPER MID SURFACE CRACKED;BETWEEN B.S.312 AND B.S.328 RBL 32.0 W/L 207.54 ; / [01] INSTALLED EWIS PROTECTION IN AREA AT EAT 312 TO 328 RBL 32.0 REF B-737 700 AMM 20-60-07-913-801; [02] VERIFIED. EWIS May 26, 2021 · N7825A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021063077758Door Frame · crackedL1 DOOR ABOVE CUTOUT STA 312 CIRCUNFERENTIAL CRACKED ; / [01] REMOVED FASTENERS IN REF B-737 SRM 51-40-02; [02] TRIMMED OUT DAMAGED AREA IN REFERENCE B-737 SRM 57-10-07-2R-1; [03] PERFORMED HFEC INSP ON REWORKED CUTOUT AREA AT L1 DOOR ABOVE STA 312. IAW B 737 May 26, 2021 · N7825A · Boeing 7377CT · Fuselage Main, StructureSDR SWAA2021062177041Skin · delaminatedSPOILE #8 UPPER SURFACE DENT DELAMINATED 7.2' FROM AFT EDGE AND 38' FROM I/B EDGE. SPOILER #8 TO BE REPLACED ON CARD TTG8Q0058MCG. REMOVED R/H WING # 8 SPOILER ASSY AS PER 737-700 AMM 27-61-11-000-801.May 25, 2021 · N7828A · Boeing 7377CT · SpoilersSDR SWAA2021061875032Channel · corrodedCORROSION AT FWD CARGO RH SIDE PLATE STA 500-500D; WL 156 ; / FABRICATED SIDE PLATE (Z-CHANNEL) IN REF B737-700 DRAWING NUMBER 243A7501 AT FWD CARGO COMPARTMENT FS 500-500D R/H RBL 24 WL 156;INSPECTED FABRICATED SIDE PLATE (Z-CHANNEL;OK TO TREAT AND PRIME SIDEMay 19, 2021 · N7828A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021052474543Hook And Loop · looseFWD SERVICE DOOR ESCAPE SLIDE VELCRO STRIPS ON THE GIRT ARE NOT ATTACHED TO VELCRO STRIPS ON THE BACKING PAN SHELF. ; / REATTACHED FWD SERVICE DOOR ESCAPE SLIDE VELCRO STRIP ON THE GIRT TO VELCRO STRIP ON THE BACKING PAN SHELF PER AMM 25-66-01.May 19, 2021 · N7829B · Boeing 7377CT · Escape SlideSDR SWAA2021052474542Hook And Loop · looseAFT ENTRY DOOR ESCAPE SLIDE VELCRO STRIPS ON THE GIRT ARE NOT ATTACHED TO VELCRO STRIPS ON THE BACKING PAN SHELF. ; / REATTACHED AFT ENTRY DOOR ESCAPE SLIDE VELCRO STRIP ON THE GIRT TO VELCRO STRIP ON THE BACKING PAN SHELF PER AMM 25-66-01.May 19, 2021 · N7829B · Boeing 7377CT · Escape SlideSDR SWAA2021052474541Hook And Loop · looseAFT SERVICE DOOR ESCAPE SLIDE VELCRO STRIPS ON THE GIRT ARE NOT ATTACHED TO VELCRO STRIPS ON THE BACKING PAN SHELF. ; / RE-ATTACHED AFT SERVICE DOOR ESCAPE SLIDE VELCRO STRIP ON THE GIRT TO VELCRO STRIP ON THE BACKING PAN SHELF PER AMM 25-66-01.May 19, 2021 · N7829B · Boeing 7377CT · Escape SlideSDR SWAA2021062173422Scuff Plate · crackedAFT CARGO COMPARTMENT AFT CORNER SCUFF PLATE CRACKED (18-061) ; / RECEIVED SERVICEABLE AFT CORNET SCUFF PLATE P/N 146A8341-9. WELDED SCUFF PLATE CORNER TO INSTALLED ON CUSTOMER BARCODE TTG8Q004CDCK; VERIFIED WORK ACCOMPLISHED.May 15, 2021 · N7828A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021062173421Scuff Plate · crackedAFT CARGO COMPARTMENT FWD CORNER SCUFF PLATE CRACKED (18-060) ; / RECEIVED SERVICEABLE SCUFF PLATE CORNER PN 146A8341-7. SCUFF PLATE TO BE INSTALLED ON CUSTOMER BARCODE TTG8Q004CDCK; VERIFIED WORK ACCOMPLISHED.May 15, 2021 · N7828A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021061673418Floor Support · crackedFWD WET AREA BETWEEN STA 312 TO 328 RBL 30 INTERCOSTAL HOLE HAS CRACK ; / IAW B737-7 SRM;INSPECTED INTERCOSTAL INSTALLATION;INSTALLED NEW INTERCOSTAL FWD AREA BETWEEN STA 312 TO328 IN REFB737-700 SRM 51-40-02-0G-0 DOCUMENT 141A5400;LOCATED AND DRILLED NEW INTEMay 15, 2021 · N7828A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021062175498Skin · delaminatedMULTIPLE DENTS ON #1 SPOILER AT UPPER SURFACE ; / PERFORMED TAP TEST ON DENT IAW NDTM PART 1;51-01-02. DENT HAS EVIDENCE OF DELAMINATION.; PERFORMED TAP TEST ON DENT IAW NDTM PART 1;51-01-02. DENT HAS EVIDENCE OF DELAMINATION.; PERFORMED TAP TEST ON DENT IAW NMay 14, 2021 · N7828A · Boeing 7377CT · SpoilersSDR SWAA2021062173415Strap · corrodedCORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT LATERAL STRAP ON UPPER SURFACE AT B.S. 727D+5 L.BL. 20' -R.BL. 20'.(51-004) ; / REMOVED CORROSION ON T STRAP STA. 727 D+5 PER B 737 SRM 51-10-02-0G-0 FOUND EXFOLIATION CORROSION OUT OF LIMITS PER B737 SRM 53-00-May 14, 2021 · N7828A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2021062173413Channel · missingAFT CARGO COMPARTMENT FLOOR SUPPORT 'Z' CHANNEL TO FRAME MISSING 1/4' ATTACH BOLT B.S. 727+5 R.BL. 21'(51-001) ; / INSTALLED BOLT AT STA. 727 PLUS 5 RBL 21 ON FLOOR SUPPORT Z CHANNEL PER REF. B 737 SRM 51-40-02-0G AND DRAWING # 146A0061; VERIFIEDMay 14, 2021 · N7828A · Boeing 7377CT · Fuselage Miscellaneous Structure
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