Boeing 737-76N

Service difficulty reports · 4,807

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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 = '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 SWAA2022022266574Beam · crackedUPON ACCOMPLISHING INSPECTION OF CCN:5241-I-14079-NG; FOUND 1 INCH CRACK OF #5 BEAM COMMON TO THE FORWARD SERVICE DOOR. / [01] FSD #5 BEAM WAS REMOVED AND REPLACED ON WORK ORDER: 546753 PER SRM 51-40-02-0G-0 PARA 4; 7 AND BOEING DWG: 141A6516.;[02] VERIFIED COFeb 1, 2022 · N7725A · Boeing 73776N · Galley DoorsSDR SWAA2022022266396Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS536 S-25L WL155. EVALUATED CRACK AREA ON STRINGER AT AFT OF FCB BS536 S-25L WL155; AND NO FOUND ALLOWABLE DAMAGE ON SRM 53-00-03-1A-1. REMOVED FCB STINGER CLIP FOR GAIN ACCESS AT BS520 S-25L & SHEAR TIE AT FCB AT BS520 Feb 1, 2022 · N7725A · Boeing 73776N · Fuselage Main, Longeron/StringerSDR SWAA2022022266394Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS536 S-26R WL153. ACCOMPLISHED EWIS PROTECTION WITHIN THE REPAIR AREA AT BS 536 S-26R WL153 IAW AMM 20-60-07-913-801. FABRICATED, LOCATED, AND DRILLED HAT SECTION SPLICE IAW SRM 53-00-03-2R-1 REPAIR 1. LOCATED AND DRILLFeb 1, 2022 · N7725A · Boeing 73776N · Fuselage Main, Longeron/StringerSDR SWAA2022022266404Support · crackedCRACKED PASSENGER CABIN FLOOR SUPPORT AT BS 540; BL 0 - LBL 24.75, WL 208.1. REMOVED PASSENGER CABIN CRACKED FLOOR SUPPORT IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED PASSENGER CABIN FLOOR SUPPORT IAW SRM 51-40-05-0G-0 AND DWG 143A0060. INSTALLED PASSENGERFeb 1, 2022 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2022022266405Support · crackedCRACKED PASSENGER CABIN FLOOR SUPPORT AT B.S. 540; B.L. 0 - R.B.L. 24.75; W.L. 208.1. REMOVED PASSENGER CABIN CRACKED FLOOR SUPPORT IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED PASSENGER CABIN FLOOR SUPPORT IAW SRM 51-40-05-0G-0 AND DWG# 143A0060. INSTALLED PFeb 1, 2022 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2022022266392Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25. MARKED. / [01] REMOVED INTERCOSTAL ATTACH ANGLE FCB AT BS500C FWD SIDE LBL 25 IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW FCB INTERCOSTAL ATTACH ANGLE BS 500C FWD SIDE LBL 25 IAW SFeb 1, 2022 · N7725A · Boeing 73776N · Fuselage Main, Plate/SkinSDR SWAA2022022266400Gusset · crackedFWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. REMOVED FCB AFT BULKHEAD SUPPORT GUSSET CRACKED AT BS500D S-19R WL193 IAW SRM 51-40-02-0G-0, LOCATED AND DRILLED NEW FCB AFT BULKHEAD SUPPORT GUSSET IAW SRM 51-40-05-0G-0 AND DWG 143A9481Feb 1, 2022 · N7725A · Boeing 73776N · Fuselage Main, Plate/SkinSDR SWAA2022022266199Support · corrodedCORROSION ON AFT CARGO AFT BULKHEAD SUPPORT AT STA 947.5; RBL 22.5; WL 178.5. EVALUATED DAMAGE ON AFT CARGO COMPARTMENT AFT BULKHEAD SUPPORT AT STA 947.5;RBL 22.5; WL 178.5 FOUND TO BE OUT LIMITS. REMOVED AFT BULKHEAD SUPPORT AT STA 947.5;RBL 22.5; WL 178.5 Feb 1, 2022 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2022022266196Shield · corrodedAFT CARGO BAY DOOR CUTOUT FWD SHIELD IS CORRODED FROM BS 767 TO 787+6; RBL 23; WL 158. / REMOVED AND EVALUATED SHIELD ON AFT CARGO BAY AT RBL 23 BTW BS 767- BS 787; NO FOUND ALLOWABLE DAMAGE LIMITS; DUE NOT LIMITS IN SRM PART WILL BE REPAIRABLE BY REPLACEMENTFeb 1, 2022 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2022022266197Shield · corrodedAFT CARGO BAY DOOR CUTOUT AFT SHIELD IS CORRODED FROM STA 847 TO STA 867; RBL 23; WL 163. / [01] REMOVED AND EVALUATED SHIELD ON AFT CARGO BAY AT RBL 23 BTW BS 847- BS 867; NO FOUND ALLOWABLE DAMAGE LIMITS; DUE NOT LIMITS IN SRM PART WILL BE REPAIRABLE BY REPLFeb 1, 2022 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2022022266201Floor Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT FROM STA 727 TO STA 767; RBL 22; WL 156. / REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT RBL 22 WL 156 BETWEEN BS727 TO BS767 THE LOWEST REMAINING THICKNESS 0.033' ON BLENDED AREA L=3.5'X W=1.2'XD=0.007 Feb 1, 2022 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2022022266202Support · corrodedCORROSION ON AFT CARGO FLOOR TO SIDEWALL SUPPORT FROM BS 727A+5 TO 767+18; LBL 22; WL 156. / REMOVED CORROSION . THE LOWEST REMAINING THICKNESS 0.032' ON BLENDED AREA L=2.2'X W=1'XD=0.008 ORIG. MAT. THK.=.040' FOUND TO BE OUT OF LIMITS I.A.W SRM 53-00-53-1A-2Feb 1, 2022 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2022022266200Support · corrodedCORROSION ON AFT CARGO BAY AFT BULKHEAD SUPPORT AT STA 947.5; RBL 16 TO LBL 9; WL 179 TO WL 177. EVALUATED DAMAGE ON ACB AFT BULKHEAD SUPPORT AT STA 947.5 RBL16 TO LBL9 WL179 TO WL 177 FOUND TO BE OUT LIMITS. LOCATED AND DRILLED NEW AFT BULKHEAD SUPPORT AT Feb 1, 2022 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2022022266203Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 867 TO 887+16; RBL 22; WL 165 TO WL 189. REMOVED CORROSION. THE LOWEST REMAINING THICKNESS 0.031' ON BLENDED AREA L=3'X W=1'XD=0.009 ORIG. MAT. THK.=.040', FOUND TO BE OUT OF LIMITS I.A.W SRM 53-00-53Feb 1, 2022 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2022022266391Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS 400 - 420 RBL23. EVALUATED FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY LOC BTW BS400 - BS420; RBL 23; BS 400+11. MEASURES= L= 1'; W=700'; D= 0.010'; ORIGINAL MATERIAL THICKNESS=0.040'; MATERIAL LOSS=0.Feb 1, 2022 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2022022266395Shield · corrodedCORROSION ON FWD SHIELD AT FWD CARGO BAY BS420 - BS440 RBL23. EVALUATED FWD SHIELD AT FWD CARGO BAY BTW BS420 - BS440; RBL23; FOUND TO BE OUT LIMITS DUE NOT LIMITS ON SRM; PART WILL BE REPAIRABLE BY REPLACEMENT. IAW. SRM 51-10-02-0G-0.;[02] REMOVED FWD SHIELDFeb 1, 2022 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2022022266397Shield · corrodedCORROSION ON AFT SHIELD AT FWD CARGO BAY BS500 - 500A RBL23. EVALUATED AFT SHIELD AT FWD CARGO BAY BTW BS500 - BS500A; RBL23; FOUND TO BE OUT LIMITS DUE NOT LIMITS ON SRM. REMOVED AFT SHIELD AT FWD CARGO BAY BTW BS 500 - 500A; RBL23. IAW. 51-40-02-0G-0. LOCFeb 1, 2022 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2022022266398Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS 500A - 500D RBL23. EVALUATED FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY MEASURES= L= 1'; W=600'; D= 0.011'; ORIGINAL MATERIAL THICKNESS=0.040'; MATERIAL LOSS=0.011'; REMAINING THICKNESS=0.029'. SIDEFeb 1, 2022 · N7725A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2022022266393Stringer · corrodedCORROSION ON STRINGER AT AREA AFT OF FCB BS536 S-25R WL155. MARKED / ACCOMPLISHED EWIS PROTECTION WITHIN THE REPAIR AREA AT BS BS 536 S-25R WL155 IAW AMM 20-60-07-913-801.;REMOVED CORROSION ON STRINGER AT AREA AFT OF FCB BS 536 S-25R WL155 AREA 3' X 1' X .020'Feb 1, 2022 · N7725A · Boeing 73776N · Fuselage Main, Longeron/StringerSDR SWAA2022022365542Skin · crackedNR 1 SLAT LOWER NOSE SKIN HAD EVIDENCE OF A CRACK FROM ACTUATOR FITTING FASTENER. REMOVED 6 FASTENERS AT NR 1 SLAT LOWER NOSE SKIN FROM ACTUATOR FITTING IAW SRM 51-40-02. FABRICATE 1 DOUBLER AND 2 FILLERS & APPLIED CHEMICAL CONVERSION COATING IAW SRM 57-42Jan 29, 2022 · N7725A · Boeing 73776N · Leading Edge DevicesSDR SWAA2022012062676Light · inoperativeR/H OVERWING EXTERIOR EMERGENCY LIGHT INOP ; / [01] RELAMPED R/H EXTERIOR OVERWING EMERGENCY EXIT LIGHT IAW B737 AMM 33-51-04.Jan 20, 2022 · N7822A · Boeing 73776N · Emergency LightingSDR SWAA2022011761006Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES. ; / [01] REPLACED PANEL 193B PER SRM 51-40-02Jan 13, 2022 · N7822A · Boeing 73776N · Aerodynamic FairingsSDR SWAA2022011360061Panel · looseR/H OWING EMER EXIT ACCESS PANEL LOOSE ; / [01] TIGHTEN PANEL ON R/H OVERWING EMERGENCY EXIT PER AMM 52-22-00.Jan 9, 2022 · N7885A · Boeing 73776N · Emergency ExitsSDR SWAA2022010557974Compensator · faultyFUEL IMBALANCE DEVELOPED RAPIDLY BY THE TIME WE REACHED CRUISE ALTITUDE OF 34;000. OVER 700# LESS IN LEFT MAIN FUEL TANK THAN RIGHT TANK. AND FUEL TOTAL WAS DECREASING MORE RAPIDLY IN LEFT TANK. ; / [01] OK TO CLOSE PNL 532AB PER MPM 56-04-02; [02] PERFORMED FJan 4, 2022 · N7846A · Boeing 73776N · Fuel Indicating SystemSDR SWAA2021122253659Power Supply · inoperativeINOP EMERGENCY LIGHT POWER SUPPLY ASSY ON ROW NUMBER 11 LH SIDE AT PASSENGER CABIN (1 EA) ; 2021-545136 / [01] REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY ASSY ON ROW NUMBER 11 LH SIDE AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-51-06-960-806.<BR>SEE IDec 16, 2021 · N7846A · Boeing 73776N · Emergency LightingSDR SWAA2021122250334Rib · crackedCRACK INSPAR RIB STA 120.30 LOCATED AT UPPER POSITION 1 INCH FROM FRONT SPAR AT LT HORIZONTAL STABILIZER ; 2021-545123 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER: P/N: P3015GOES000Dec 4, 2021 · N7846A · Boeing 73776N · Horizontal Stabilizer, Spar/RibSDR SWAA2021120749830Panel · elongatedWING TO BODY PANEL 193D HAS 1(EA) FASTENER HOLE ELONGATED ; / [01] REPAIRED PANEL PER EA TTG8Q009MJZQDec 3, 2021 · N7811F · Boeing 73776N · Aerodynamic FairingsSDR SWAA2021120249247Sign · brokenEMERGENCY EXIT LIGHT BY FORWARD SERVICE DOOR BROKEN. ; / [01] R&R?D SIGN ASSY IN REF TO A.M.M.33-51-01Dec 1, 2021 · N7729A · Boeing 73776N · Emergency LightingSDR SWAA2021122249095Skin · crackedCRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.250 INCH FROM FRON SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.0 INCH ; 2021-545024 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210138103 DUENov 30, 2021 · N7846A · Boeing 73776N · Horizontal Stabilizer, Plate/SkinSDR SWAA2021122249096Skin · crackedCRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 24.500 INCH FROM FRON SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.300 INCH ; 2021-545025 / [01] REFER TO FAULT TTG8Q009KW5H WHERE EA 21-155-03706 HAS BEEN ATTACHED AS A Nov 30, 2021 · N7846A · Boeing 73776N · Horizontal Stabilizer, Plate/SkinSDR SWAA2021122348550Floor Panel · brokenBROKEN SLEEVE FLOOR PANEL 241DF CENTER SECTION (4 EA) ; 2021-544959 / [01] REPLACED SLEEVE FLOOR PANEL 241DF CENTER SECTION (4 EA) IAW SRM 53-00-50-2R-0.; [02] REPLACED SLEEVE FLOOR PANEL 241DF CENTER SECTION (4 EA) IAW SRM 53-00-50-2R-0.<BR>COMPLETED TASKNov 29, 2021 · N7846A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2021122348551Floor Panel · brokenBROKEN SLEEVE FLOOR PANEL 241FF CENTER SECTION (1 EA) ; 2021-544957 / [01] REPLACED SLEEVE FLOOR PANEL 241FF CENTER SECTION (1 EA) IAW SRM 53-00-50-2R-0.; [02] REPLACED SLEEVE FLOOR PANEL 241FF CENTER SECTION (1 EA) IAW SRM 53-00-50-2R-0.<BR>COMPLETED TASK.Nov 29, 2021 · N7846A · Boeing 73776N · Fuselage Floor PanelSDR SWAA2021122748556Rib · crackedCRACK INSPAR RIB 120.30 LOCATED AT 16.50 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER ; 2021-544963 / [01] TOOL EDDY CURRENT USED P/N: NORTEC 600D S/N: 210138503 AND DUE DATE: 05-MAR-22.; [02] PERFORMED REPAIR ON INSPAR RIB 120.30 AT LT HORIZONTAL STABILNov 29, 2021 · N7846A · Boeing 73776N · Horizontal Stabilizer, Spar/RibSDR SWAA2021122748241Skin · delaminatedCUSTOMER REQUEST - DEBONDED OB AFT FLAP UPPER SURFACE ON IB EDGE AT LT WING ; 2021-544881 / [01] TOOL USED: CALIPER P/N:500-197-30 S/N:A18229508 DUE DATE: 22-SEP-22.; [02] TOOL USED: AUDIBLE BOND TESTER; PN: S-3; SN: 064; DUE DATE: 12-JUL-22; [03] TOOL USED: HNov 28, 2021 · N7846A · Boeing 73776N · Trailing Edge FlapsSDR SWAA2021121347062Track · corrodedCORROSION ON TRACK AT AFT CARGO BAY RBL13 BS807; BS867; BS810; BS817; BS814; BS787; BS795; BS799; BS747. EVALUATED DAMAGE FOUND TO BE OUT LIMIT ON BS799 AND BS 814 VERIFY STEPS 1 TO 9; [02] VERIFIED STEPS 1-9. REMOVED ACB CARGO TRACK BS727-887 RBL 13 IAW SNov 23, 2021 · N7722B · Boeing 73776N · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021121344274Attach Angle · crackedCRACKED BULKHEAD PANEL SUPPORT ATTACH ANGLE AT BS 867, LBL 11, WL 166. FOUND TO BE OUT LIMITS IAW SRM 51-10-02-0G-0. REMOVED THE ATTACH ANGLE IAW SRM 51-40-02-0G-0, DRILLED AND LOCATED BULKHEAD PANEL SUPPORT ANGLE IAW SRM 51-40-05 AND DWG 149A8102. INSTANov 16, 2021 · N7722B · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021121344269Web · corrodedCORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS802 - BS836 RBL26. REMOVED CORROSION ON SUBTHRESHOLD WEB. MAX. MATERIAL LOSS L= 3.' X W=.500' X D=0.008' FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1; PARAG. 4.G.(2) DETAIL G. LOCATED AND DRILLED A NEW SUBTHRESNov 16, 2021 · N7722B · Boeing 73776N · Fuselage Main, StructureSDR SWAA2021121344270Angle · corrodedCORROSION AT AFT CARGO BAY ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS947 RBL17. REMOVED AFT BULKHEAD TO FLOOR SUPPORT ANGLE IAW SRM 51-40-02-0G-0. HAS NO LIMITS IN SRM AND CAN BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0.Nov 16, 2021 · N7722B · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021121344277Stringer Clip · corrodedCORROSION ON STRINGER CLIP BS 887, S22L, LBL 41. FOUND TO BE OUT LIMITS IAW SRM 51-10-02-0G-0. REMOVED STRINGER CLIP IAW SRM 51-40-02-0G-0. PRE-FABRICATED STRINGER CLIP HEAT TREATMENT REQUIRED TO T62 IAW DRAWING 147A3500. LOCATED, DRILLED, AND TREATED THNov 16, 2021 · N7722B · Boeing 73776N · Fuselage Main, Longeron/StringerSDR SWAA2021121344291Support · corrodedCORROSION ON AFT CARGO FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727+8; BS 727+11; BS 727+15; BS 727+18; BS 727A+2; BS 727A+6; BS 727A+10; BS 727A+14; BS 727A+18; BS 727B+2. REMOVED CORROSION, OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA: 4A FIG. 103 DETAIL D. FABNov 16, 2021 · N7722B · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021121344292Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727B+5-727B+12; BS 727B+14-727B+15; BS 727B+18; BS 727C+1-727C+7; BS 727C+8-727C+10; BS 727C+14; BS 727C+18; BS 727D+5; BS 727D+10. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 Nov 16, 2021 · N7722B · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021121344293Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727E-727E+2; BS 727E+5-727E+6; BS 727E+12; BS 727E+14-727E+15; BS 747+2-767. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4A FIG 103 DETAIL D. MANUFACTURED IAW DWG 146ANov 16, 2021 · N7722B · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021121344296Rail · corrodedCORROSION ON AFT CARGO BAY RAIL AT RBL 3 BS 727E; BS 767+5. ; / [01] REMOVED CORROSION ON RAIL ; AFT CARGO BAY AT RBL 3; BS 727E; BS 767+5. MEASURES:BS727E L=2'; W=0.400'; BS767+5 L=2.100'; W=0.350'. IAW; SRM 51-10-02-0G-0.; [06] EVALUATED RAIL ON AFT CARGO BANov 16, 2021 · N7722B · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021121343922Shield · corrodedCORROSION ON FWD CARGO BAY AFT SHIELD. DAMAGE BS 497, 500+9, 500+16, RBL 24, WL 156. LOCATED AND DRILLED A NEW SHIELD IAW SRM 51-40-05, AND DWG 143A8126 REV A.Nov 15, 2021 · N7722B · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021121343925Panel · corrodedCORROSION ON FWD CARGO BAY AFT LOWER BULKHEAD PANEL AT LBL 24-RBL24 BS 500D. ; / [01] REMOVED CORR0SION ON FWD CARGO BAY AFT LOWER BULKHEAD PANEL AT LBL 24 RBL 24 BS 500D L=2' W=1' X 0.020 REMAINING THICKNESS 0.051 ORIGINAL THICKNESS .071' DAMAGE EXCEED 0F 0RINov 15, 2021 · N7722B · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021121343924Support · corrodedCORROSION ON FWD CARGO BAY AFT FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500A+2; BS 500A+6; BS 500A+10; BS 500B+2. DAMAGE REMOVAL TO CLOSE TO FASTENER HOLES, OUT OF LIMITS. SUPPORT IS UNSERVICEABLE IAW SRM 53-00-53-1A-2. FWD CARGO BAY AFT FABRICATED NEW FLOORNov 15, 2021 · N7722B · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021121343921Support · corrodedCORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 419. REMOVED CORROSION, L=.4 X W=.5 X D=0.008 ORIGINAL THICKNESS 0.040 MAT REMAINING 0.032 FOUND TO BE OUT LIMITS PER SRM 53-00-53-1A-2 STEP 4.A.(2)(A) DETAIL D. FABRICATED NEW FLOOR TO SIDEWNov 15, 2021 · N7722B · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021121343916Support · crackedCRACKED FLOOR SUPPORT AT B.S. 540; B.L. 0 - L.B.L. 24.5; W.L. 208.1. ; / [01] FLOOR SUPPORT REMOVED BTW BS540; BL.0; LBL 24.5; WL. 208.1 IAW SRM 51-40-02-0G-0; PART NO HAS ALLOWABLE DAMAGE IN SRM. MUST BE REPAIRED BY REPLACEMENT<BR>IAW. SRM 51-10-02-0G-0 PARAGNov 15, 2021 · N7722B · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021121343917Support · crackedCRACKED FLOOR SUPPORT AT B.S. 540; B.L. 0 - R.B.L. 24.5; W.L. 208.1. ; / [01] FLOOR SUPPORT REMOVED BTW BS540; BL.0; RBL 24.5; WL. 208.1 IAW SRM 51-40-02-0G-0; PART NO HAS ALLOWABLE DAMAGE IN SRM. MUST BE REPAIRED BY REPLACEMENT <BR>IAW. SRM 51-10-02-0G-0 PARANov 15, 2021 · N7722B · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021121343330Floor Panel · deformedPASSENGER CABIN FLOOR PANEL 241BF DEFORMED O/B EDGE. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B(4). REMOVED DAMAGE, AND CLEANED REPAIR AREA IAW SRM 53-00-50-2R-4 PARA 3A-E. INSTALLED REPAIR PLIES, VACUUM BAGGED, AND CHECKED FNov 13, 2021 · N7722B · Boeing 73776N · Fuselage Floor Panel
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