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 SWAA2025021995295Battery Pack · inoperativeEMERGENCY EXIT BATTERY PACK M1674 WILL NOT CHARGE<[01] REMOVED AND REPLACED M1674 BATTERY PACK IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD<BR>WN49843;[02] VERIFIED ITEM 1<BR>C/WFeb 12, 2025 · N7723E · Boeing 73776N · Emergency LightingSDR SWAA2025021995296Battery Pack · inoperativeEMERGENCY EXIT BATTERY PACK M1675 WILL NOT CHARGE<[01] OPS CHECKED M1675 BATTERY IAW AMM 33-51-06-960-805; NO FAULT FOUND; OPS CHECK GOOD;[02] VERIFIED ITEM 1<BR>C/WFeb 12, 2025 · N7723E · Boeing 73776N · Emergency LightingSDR SWAA2025021995297Battery Pack · inoperativeEMERGENCY EXIT BATTERY PACK M2335 WILL NOT CHARGE<[01] REMOVED AND REPLACED M2335 BATTERY PACK IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD<BR>WN49840;[02] VERIFIED ITEM 1<BR>C/WFeb 12, 2025 · N7723E · Boeing 73776N · Emergency LightingSDR SWAA2025021995298Battery Pack · inoperativeEMERGENCY EXIT BATTERY PACK M1668 WILL NOT CHARGE<[01] REMOVED AND REPLACED M1668 BATTERY PACK IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD<BR>01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] WN4Feb 12, 2025 · N7723E · Boeing 73776N · Emergency LightingSDR SWAA2025021995299Battery Pack · inoperativeEMERGENCY EXIT BATTERY PACK M1670 WILL NOT CHARGE<[01] REMOVED AND REPLACED M1670 BATTERY PACK IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.<BR>WN49839;[02] VERIFIED ITEM 1<BR>C/WFeb 12, 2025 · N7723E · Boeing 73776N · Emergency LightingSDR SWAA2025022092140Support Bracket · cracked(152-02) PASSENGER CABIN STA 867 STR 1R; FEEDER CABLE SUPPORT BRACKET IS CRACKED.<[01] REMOVED BRACKET AT BS867; BETWEEN S-1 AND S-2R; IAW SRM 51-40-02-0G-0. FABRICATED NEW BRACKET IAW BOEING DWG 287A4015 REV. -; BOEING PL 287A4015 REV. K; AND EA 25-153-00335.Feb 1, 2025 · N7723E · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2025020392062Girt Bar · brokenAFT SERVICE DOOR SLIDE BAR HOLDER NUT PLATE BROKEN.<[01] INSTALLED NEW NUT PLATE; @0530 REQUIRES CURE TIME OF 1 HOUR.;[02] NUT PLATE IS FULLY INSTALLED IAW SRM 51-40-10.Feb 1, 2025 · N7822A · Boeing 73776N · Emergency EquipmentSDR SWAA2025020392309Lamp · inoperativeLEFT O/W EXIT SIGN LIGHT INOP<[01] OK TO CONTINUE PER. MEL 33-2-03. SP1B AUTHORIZATION #235312. ALL EMERGENCY LIGHTS AND SIGN ILLIUNNATE ON LH OVERWING DOOR. FOUND SIDEWALL LIGHT UNDERNEATH EXIT SIGN TO BE INOP.; [02] REMOVED AND REPLACED L/H O/W EXIT SIGN LIGFeb 1, 2025 · N7733B · Boeing 73776N · Emergency LightingSDR SWAA2025021991720Stiffener · corrodedCORROSION ON STIFFENER AT MID CABIN BS692 RBL64 WL203. MARKED<[01] THIS CARD WILL BE ACCOMPLISHED ON CARD NBR TTG8Q00YEMTL;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.Jan 30, 2025 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2025022091296Skin · crackedCRACK FOUND ON LH HORIZONTAL STABILIZER LOWER SKIN AT STA193.90; 17.5' FROM FWD EDGE; L: 0.6' MARKED<[01] REPAIRED LH HORIZONTAL STABILIZER LOWER SKIN AT STA193.90; 17.5' IAW SRM 55-10-01-2R-11 REPAIR 11.;[02] VERIFIED RII ITEMS ARE COMPLETEJan 29, 2025 · N7885A · Boeing 73776N · Horizontal Stabilizer, Plate/SkinSDR SWAA2025021991051Floor Panel · pulledFLOOR PANEL 231XF HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 231XF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.Jan 29, 2025 · N7885A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025021991052Floor Panel · pulledFLOOR PANEL 241DF HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241DF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.Jan 29, 2025 · N7885A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025021991053Floor Panel · pulledFLOOR PANEL 241AF HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.Jan 29, 2025 · N7885A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025021991281Web · corrodedCORROSION ON SUBTHRESHOLD WEB AT ACB BS807 - BS847 RBL28 WL160. MARKED<[01] REMOVED AND REPLACED SUBTHRESHOLD WEB IAW SRM 51-40-02 AND DWG 146A8340 ID:0028 REV: -.Jan 29, 2025 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2025021991297Strap · corrodedCORROSION ON STRAP AT MID CABIN BS692 RBL65 WL203. MARKED<[01] REMOVED AND REPLACED NEW INNER CHORD IAW SRM 51-40-02 & DWG 144A5900;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.Jan 29, 2025 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2025021991298Floor Panel · crackedCRACKED PANEL BREAK AT MID CABIN BS540 LBL1 WL208.<[01] REMOVED AND REPLACED NEW PANEL BREAK AT MID CABIN BS540 LBL1 TO LBL24 IAW SRM 51-40-02 AND DWG 143A0060 ID:0002 REV: B.<BR>APPLIED TO CIC ON DISCREPANCY AREA IAW AMM 51-21-91-620-802.<BR>CLOSED FLOOR PANEJan 29, 2025 · N7885A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025021990520Stiffener · crackedLEFT HAND HORIZONTAL STABILIZER #3 INSPAR RIB; AT STABILIZER STATION 111.10; 4TH VERTICAL STIFFENER IS CRACKED.<[01] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 111.10 RIB 4TH VERTICAL STIFFENER AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4;[02Jan 28, 2025 · N7885A · Boeing 73776N · Horizontal Stabilizer StructureSDR SWAA2025021990521Stiffener · crackedRIGHT HAND HORIZONTAL STABILIZER #3 INSPAR RIB; AT STABILIZER STATION 111.10; 4TH VERTICAL STIFFENER IS CRACKED.<[01] REMOVED THE DAMAGED PART AT RH HORIZONTAL STABILIZER STA 111.10 RIB 4TH VERTICAL STIFFENER AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4;[0Jan 28, 2025 · N7885A · Boeing 73776N · Horizontal Stabilizer StructureSDR SWAA2025021990370Connector · brokenBROKEN CONNECTOR AT FSD EXIT INDICATOR LIGHT; WIRE LABEL W4142 D03658 M/W L01186<[01] REPLACED CONNECTOR D03658 PER SWPM 20-30-12 AND WM 33-51-21.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.Jan 28, 2025 · N7885A · Boeing 73776N · Light System WiringSDR SWAA2025021997681Wire · brokenBROKEN CONNECTOR AT FSD EXIT INDICATOR LIGHT; WIRE LABEL W4142 D03658 M/W L01186<[01] REPLACED CONNECTOR D03658 PER SWPM 20-30-12 AND WM 33-51-21.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.Jan 28, 2025 · N7885A · Boeing 73776N · Light System WiringSDR SWAA2025022089840Intercostal · crackedDOT A24-77 FORWARD PIT. VERTICAL INTERCOSTAL AT STATION 480+15 BETWEEN STRINGERS 23L AND 25L CRACKED AT UPPER EDGE. BLENDED DAMAGE IAW SRM 51-10-02-0G-0. FOUND ADJACENT TO BLEND .040'; LOSS .007'; REMAINING .033' USING NDT TO VERIFY IN STEP 5. UPON FURTHER Jan 26, 2025 · N7723E · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2025021989045Floor Panel · pulledDOT#55 A-043 CABIN FLOOR PANEL 241KF HAS PULLED FIBERS ON TOP SIDE OF PANEL<[01] AUDIT C/W;[02] REFER TO FAULT TTG8Q00YBAGR WHERE EA 25-153-00203 WAS ADDED AS A SUBTASK..Jan 24, 2025 · N7723E · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025021989044Floor Panel · pulledDOT#54 A-043 CABIN FLOOR PANEL 242GF HAS PULLED FIBERS ON TOP SIDE OF PANEL<[01] AUDITED;[02] REFER TO FAULT TTG8Q00YBAGR WHERE EA 25-153-00203 WAS ADDED AS A SUBTASK.Jan 24, 2025 · N7723E · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025021989043Floor Panel · pulledDOT#53 A-043 CABIN FLOOR PANEL 231WF HAS PULLED FIBERS ON TOP SIDE OF PANEL<[01] REPAIRED PER EA 25-153-00203.Jan 24, 2025 · N7723E · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025022088437Stringer · crackedFASTENER TAB FOR LEFT WING INBOARD UPPER FIXED LEADING-EDGE STRINGER P/N 116A4531-5 IS BROKED OFF. REMOVED AND REPLACED -5 STRINGER ON LEFT WING INBOARD UPPER FIXED LEADING-EDGE P/N 116A4531-5 ATAG WN49678 IAW BOEING DWG 116A4008 REV - SRM 51-40-02. VERIFIEJan 22, 2025 · N7723E · Boeing 73776N · Wing, Longeron/StringerSDR SWAA2025022086137Stub Frame · crackedFWD GALLEY DOOR CUTOUT; UPPER FWD STUB FRAME HFEC SURFACE INSPECTION; FOUND 1' CRACK IN STUB FRAME AT JOGGLE; .70' ABOVE SEAL DEPRESSOR. MARKED IN BLACK. REF. CARD TTG8Q00TSZ8V INSP - FORWARD GALLEY DOOR (R1) BEAR STRAP BS 290-296 BETWEEN S-8R AND S-9R - GROUPJan 15, 2025 · N7723E · Boeing 73776N · Fuselage Main, FrameSDR SWAA2025021986335Floor Panel · pulledFLOOR PANEL 222DF HAS PULLED FIBERS ON TOP SURFACE<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/WJan 15, 2025 · N7723E · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025021985676Floor Panel · crackedFLOOR PANEL 221BF HAS 5EA PLACES OF PANEL BEING CRACKED/BROKEN ON LOWER SURFACE.<[01] REPLACED FLOOR PANEL 221BF WITH SERVICEABLE FLOOR PANEL ON SHELF I.A.W REFERENCE TO AIPC 53-21-51-75 PG 14 SHEET 01 ITEM A;[02] INFO ONLY: PANEL 221BF WAS REPLACED ON #TTG8Q0Jan 14, 2025 · N7723E · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025021985674Floor Panel · pulledFLOOR PANEL 221BF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] REPLACED FLOOR PANEL 221BF WITH SERVICEABLE FLOOR PANEL ON SHELF I.A.W REFERENCE TO AIPC 53-21-51-75 PG 14 SHEET 01 ITEM A;[02] INFO ONLY: PANEL 221BF WAS REPLACED ON #TTG8Q00Y4M8W & INSTALLED ON #TTJan 14, 2025 · N7723E · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025021985682Floor Panel · corroded(A204 DOT 93) FLOOR PANEL 221BF HAS 8EA FASTNER INSERTS WITH CORROSION; MARKED IN RED.<[01] REPLACED FLOOR PANEL 221BF WITH SERVICEABLE FLOOR PANEL ON SHELF I.A.W REFERENCE TO AIPC 53-21-51-75 PG 14 SHEET 01 ITEM A;[02] INFO ONLY: PANEL 221BF WAS REPLACED ON #Jan 14, 2025 · N7723E · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025021985681Floor Panel · pulledFLOOR PANEL 231UF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.Jan 14, 2025 · N7723E · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025021985671Floor Panel · pulled(A204 DOT 97) FLOOR PANEL 231KF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/WJan 14, 2025 · N7723E · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025021985680Floor Panel · debonded(A204 DOT 98) FLOOR PANEL 231KF; AFT LH CORNER OF FLOOR PANEL IS DISBONDED.<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/WJan 14, 2025 · N7723E · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025021985670Floor Panel · pulled(A204 DOT 99) FLOOR PANEL 231GF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/WJan 14, 2025 · N7723E · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025021985668Floor Panel · pulled(A204 DOT 101) FLOOR PANEL 231DF; UPPER SURFACE FACE SHEET MISSING FIBERS.<[01] C/W EA 25-153-00105. VERIFIED ALL STEPS COMPLETE.;[02] VERIFIED C/W;[03] C/WJan 14, 2025 · N7723E · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025021985679Handle · out of adjust(A204 DOT 86) RH EMERGENCY EXIT DOOR 843 PULL CLOSE HANDLE RECESS HAS 2EA MISSING QUARTER TURN STUDS.<[01] REPLACED MISSING QUARTER TURN STUDS IN HANDLE RECESS ON DOOR 843 I/A/W 52-22-51-400-801 .;[02] VERIFIED STEP 1<BR>AUDIT C/WJan 14, 2025 · N7723E · Boeing 73776N · Emergency ExitsSDR SWAA2025022085662Winglet · corrodedDOT#42 A-043 RH WINGLET HAS CORROSION ON LOWER OTBD T/E 18' FROM BOTTOM EDGE<[01] 04 - REPAIRED PER [SRM 57-30-01-1A-2-APB-AP37.1-0632-A01611 (PERMANENT (NON-DENT DAMAGE TYPES)-WINGLETS)];[02] VERIFIED STEP 1<BR>AUDIT CWJan 13, 2025 · N7723E · Boeing 73776N · Wing Main, Frame StructureSDR SWAA2025022085661Winglet · corrodedDOT#43 A-043 RH WINGLET HAS CORROSION ON UPPER INBD T/E 42' FROM BOTTOM EDGE<[01] 04 - REPAIRED PER [SRM 51-10-02-0G-0-A00248 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)] AND IAW APB 57-30-01 FIGURE 102 (D);[02] 04 - REPAIRED PER [SRM 5Jan 13, 2025 · N7723E · Boeing 73776N · Wing Main, Frame StructureSDR SWAA2025021985451Receiver · crackedDOT#38 A-043 FWD CARGO COMPARTMENT AFT BKHD UPPER STAINTION RAIL CAMLOCK RECIVER CRACKED STA 500D LBL 39 WL 193<[01] REMOVED AND REPLACED CAMLOCK AT AFT BULKHEAD UPPER RAIL IAW SRM 51-40-02-0G-0;[02] VERIFIED ITEM 1<BR>AUDIT C/WJan 13, 2025 · N7723E · Boeing 73776N · Fuselage Main, StructureSDR SWAA2025021985667Sidewall Support · corroded154-86 AFT CARGO COMPARTMENT STA 907 STR 24R+4 SIDEWALL PANEL SUPPORT CORRODED NEAR THE FASTENER HOLE<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]<BR> BOEING DWG 147A9409 ID:Jan 13, 2025 · N7723E · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2025022085126Seal · cracked(DOT 152-1) LEFT HORIZONTAL STABILIZER GAP COVER 333AB; SLIDING SEAL IS CRACKED.<[01] REMOVE AND REPLACED LEFT HORIZONTAL STABILIZER GAP COVER 333AB; SLIDING SEAL I.A.W SRM STEP 4.<BR>ISSUE TAG WN49657;[02] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER GAP CJan 11, 2025 · N7723E · Boeing 73776N · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2025022085127Seal · cracked(DOT 152-2) LEFT HORIZONTAL STABILIZER PANEL 333AB; SLIDING SEAL SUPPORT BRACKET IS CRACKED.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER PANEL 333AB; SLIDING SEAL I.A.W SRM 51-40-02-0G<BR>ISSUE TAG WN49657;[02] VERIFIED TASK COMPLETE<BR><BR>AUDIT C/WJan 11, 2025 · N7723E · Boeing 73776N · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2025021984885Floor Panel · corrodedDOT#27 A-043 FLIGHT COMPARTMENT FLOOR PANEL 211AF HAS CORROSION ON BOTTOM FWD EDGE STA 259.5 BL 0 WL 208<[01] REPLACED IAW SRM 51-40-02-0G-0 & BOEING DWG: 141A631 REV: B<BR>ATAG: WN 49596<BR>P/N: 141A5133U15ATSMR0;[02] FAULT RESOLVED ON OTHER FAULT. SEE FAULT Jan 10, 2025 · N7723E · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025022084619Frame · crackedMAIN CABIN STA 440 FRAME HAS EVIDENCE OF CRACK AROUND FASTENER OF RAIL SUPPORT BRACKET I/B OF STR 8 L/H. REMOVED DAMAGE AND REPAIRED FRAME AT STA 440 S-8L IAW EA 25-153-00218.Jan 9, 2025 · N7723E · Boeing 73776N · Fuselage Main, FrameSDR SWAA2025022084621Frame · crackedMAIN CABIN STA 380 FRAME HAS EVIDENCE OF CRACK AROUND FASTENER OF RAIL SUPPORT BRACKET I/B OF STR 8 L/H. REPAIRED PER EA 25-153-00153 TTG8Q00YDMJL;[02] REPAIRED FRAME AT BS380; BETWEEN S-7L AND S-8L; IAW EA 25-153-00153.Jan 9, 2025 · N7723E · Boeing 73776N · Fuselage Main, FrameSDR SWAA2025022084618Frame · cracked(DOT#147-48) MAIN CABIN STA 400 FRAME HAS EVIDENCE OF CRACK AROUND FASTENER OF RAIL SUPPORT BRACKET I/B OF STR 8 L/H<[01] REPAIRED FRAME AT BS400; BETWEEN S-7L AND S-8L; IAW EA 25-153-00154.;[02] VERIFIED ITEM 1<BR>C/W;[03] C/WJan 9, 2025 · N7723E · Boeing 73776N · Fuselage Main, FrameSDR SWAA2025022084613Crease Beam · corrodedCABIN FWD WET AREA R1 CREASE BEAM CRRODED AT STA 312+15' LBL 60 WL 208<[01] REMOVED DAMAGE FROM CABIN FWD WET AREA R1 CREASE BEAM CORRODED AT STA 312+15' LBL 60 WL 208; FOUND IT OUT OF LIMITS ; ORIG T . ADJACENT TO BLEND .085'; LOSS .017'; REMOVED DAMAGED PARTJan 9, 2025 · N7723E · Boeing 73776N · Fuselage Main, StructureSDR SWAA2025021984610Floor Panel · corrodedDOT L7-010: AFT CARGO COMPARTMENT FLOOR PANEL 140AF IS CORRODED AT FASTENER HOLES<[01] EVALUATED CORROSION ON AFT CARGO COMPARTMENT FLOOR PANEL 140AF; FOUND TOTAL ACCUMULATED CORROSION DAMAGE TO BE MORE THAN THE 20IN ALLOWED; OUT OF LIMITS IAW SRM 53-00-53-1A-Jan 9, 2025 · N7723E · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025021984611Floor Panel · corrodedDOT L7-012: AFT CARGO COMPARTMENT FLOOR PANEL 140CF IS CORRODED AT FASTENER HOLES<[01] VERIFIED LIMITS ON AFT CARGO COMPARTMENT FLOOR PANEL 140CF; DISTANCE BETWEEN DAMAGE IS 2' (MINIMUM ALLOWABLE DISTANCE BETWEEN DAMAGE IS 5') THEREFORE IS FOUND OUT OF THE LIMJan 9, 2025 · N7723E · Boeing 73776N · Fuselage Floor PanelSDR SWAA2025022083950Angle · buckled(A204 DOT 73) FORWARD CARGO STA 500 TO 500A; STR 26L; BAFFLE PLATE UNDER Z-ANGLE IS BUCKLED ON FORWARD SIDE.<[01] REMOVED AND INSTALLED NEW RIVETS AT FORWARD CARGO STA 500 TO 500A STR 26L BAFFLE PLATE UNDER Z ANGLE I/A/W SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;Jan 8, 2025 · N7723E · Boeing 73776N · Fuselage Miscellaneous Structure
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