N272WN

Service difficulty reports · 327

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N272WN' AND registry_match = 'registration'
  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 SWAA2024103144342Floor Panel · pulledFLOOR PANEL 231MF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231MF UPPER SKIN WITH MULTIPLE 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 COct 2, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024103144343Floor Panel · pulledFLOOR PANEL 232FF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] OPENED FLOOR PANEL 232FF IAW AMM 53-21-00-000-801;[02] FLOOR PANEL 232FF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-Oct 2, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024103144346Floor Panel · pulledFLOOR PANEL 232DF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232DF UPPER SKIN WITH MULTIPLE 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 COct 2, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024103144349Floor Panel · pulledFWD FLOOR PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 221EF 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] JOB COMPLETE.Oct 2, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024103144350Floor Panel · pulledFWD FLOOR PANEL 221FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 221FF 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] JOB COMPLETE.Oct 2, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024103144354Floor Panel · pulledFWD FLOOR PANEL 231AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 231AF 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 Oct 2, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024110143893Floor Panel · pulledFLOOR PANEL 242DF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242DF; WITH MULTIPLE UPPER SKIN AREAS OF PULLED STRANDS; WAS REPLACED BY FABRICATION IAW SRM 53-00-50-2R-0 AND DRAWING 144A5810 SHEET 123.;[02] CORRECTION TO ITEM 1: FLOOR PANEOct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024110143894Floor Panel · pulledFLOOR PANEL 242CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242CF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.Oct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024110143897Floor Panel · pulledFLOOR PANEL 241VF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241VF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.Oct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024110143898Floor Panel · pulledFLOOR PANEL 241WF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241WF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.Oct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024110143899Floor Panel · pulledFLOOR PANEL 242PF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242PF; WITH MULTIPLE UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-3R-0 AND DRAWING 146A5810 SHEET 163.;[02] ITEM ONE SHOULD READ: FLOOR PANEL 242PF; WITH MUOct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024110143900Floor Panel · pulledFLOOR PANEL 242QF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242QF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTOct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024110143890Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF UPPER SURFACE SKIN DAMAGE A NEW 241AF FLOOR PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Oct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024110143891Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF UPPER SURFACE SKIN DAMAGE A NEW 241BF FLOOR PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Oct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024110143892Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF UPPER SURFACE SKIN DAMAGE A NEW 241DF FLOOR PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Oct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024110143896Floor Panel · pulledFLOOR PANEL 241UF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF UPPER SURFACE SKIN DAMAGE A NEW 241UF FLOOR PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Oct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024110143902Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FABRICATED NEW CABIN FLOOR PANEL 241AAF IAW SRM 53-00-50-2R-0 PARA 1. A. NOTE:;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Oct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024103143901Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN HAS MULTIPLE ARES OF PULLED STRANDS.<[01] 241XF AFT FLOOR PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTAOct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024103143895Floor Panel · debondedAFT FLOOR PANEL 241ABF UPPER SKIN PREVIOUS REPAIR HAS DISBONDED.<[01] 241ABF AFT FLOOR PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHEDOct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024103143905Floor Panel · pulledAFT FLOOR PANEL 241AEF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241AEF UPPER SKIN; WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1Oct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024103143909Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF; UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1Oct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024103143903Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241ACF WITH MULTIPLE AREAS OF UPPER PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1Oct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024103143906Floor Panel · pulledAFT FLOOR PANEL 242SF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242SF; UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1Oct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024103143907Floor Panel · pulledAFT FLOOR PANEL 242TF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242TF WITH UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.Oct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024103143886Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF WITH UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0Oct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024103144059Frame · crackedFWD ENTRY DOOR CUTOUT; BS 312 FRAME IS CRACKED IN RADIUS JUST ABOVE CUT OUT HEADER FRAME<[01] FWD ENTRY DOOR CUTOUT BS 312 FRAME BELOW STR 5L REPAIRED PER EA # M-22-153-01244;[02] VERIFIED CORRECTIVE ACTION; TASK COMPLETE.Oct 1, 2024 · N272WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024103143685Angle · crackedCRACKED ATTACH ANGLE AT MID CABIN BS693 LBL1 WL203. MARKED<[01] REMOVED AND REPLACED ATTACH ANGLE AT MID CABIN BS693 LBL1 WL203 PER REF SRM 51-40-02 AND IPC 32-34-51-05;[02] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED.Sep 30, 2024 · N272WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103143683Angle · crackedCRACKED ATTACH ANGLE AT MID CABIN BS693 RBL23 WL203. MARKED<[01] REMOVED AND REPLACED ATTACH ANGLE (BRACKET) PN#273A9112-45 PER SRM 51-40-02 AND PER DWG#273A9110 REV: -;[02] VERIFIED CORRECTIVE ACTION 1Sep 30, 2024 · N272WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103143686Angle · crackedCRACKED ATTACH ANGLE AT MID CABIN BS691 RBL1 WL205. MARKED<[01] REMOVED AND REPLACED NEW ATTACH ANGLE (BRACKET) PN#273A9112-48 PER SRM 51-40-02 AND PER DWG#273A9111 REV: -;[02] VERIFIED TASK COMPLETESep 30, 2024 · N272WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103143682Angle · corrodedCORROSION ON ANGLE AT MID CABIN BS703 LBL61 WL203. MARKED<[01] CLEANED AREA ON ANGLE AT MID CABIN BS703 LBL61 WL203; NO CORROSION NOTED IAW SOPM 20-30-03;[02] REJECT: AREA OF DAMAGE NEED TO BE VERIFIED BY QC BEFORE PRIMER APPLICATION. [TTG8Q00WET8P];[03] REJECSep 30, 2024 · N272WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024110143311Panel · pulledL/W T/E PANEL 561CB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] L/W T/E PANEL 561CB HAD SEVERAL PULLED FASTENER HOLE ON AFT END REPAIRED IAW SRM 51-70-04-2R-9;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.Sep 29, 2024 · N272WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2024110143006Panel · pulledL/W T/E PANEL 561BB HAS PULLED FASTENER HOLES (MARKED)<[01] L/W T/E PANEL 561BB HAD PULLED FASTENER HOLES REPAIRED IAW SRM 51-70-04-2R-9;[02] VERIFIED JOB COMPLETESep 28, 2024 · N272WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2024110143305Panel · pulledL/W T/E PANEL 561AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] L/W T/E PANEL 561AB HAD SEVERAL PULLED FASTENER HOLE ON AFT END REPAIRED IAW SRM 51-70-04-2R-9;[02] VERIFIED JOB COMPLETESep 28, 2024 · N272WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2024110143306Panel · pulledR/W T/E PANEL 661CB HAS PULLED FASTENER HOLES ON AFT END (MARKED)<[01] R/W T/E PANEL 661CB HAD PULLED FASTENER HOLES ON AFT END REPAIRED IAW SRM 51-70-04-2R-9;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.Sep 28, 2024 · N272WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2024110143307Panel · pulledR/W T/E PANEL 661AB HAS PULLED FASTENER HOLES ON AFT END (MARKED)<[01] R/W T/E PANEL 661AB HAD PULLED FASTENER HOLES ON AFT END REPAIRED IAW SRM 51-70-04-2R-9;[02] VERIFIED JOB COMPLETESep 28, 2024 · N272WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2024110143309Panel · pulledR/W T/E PANEL 661BB HAS PULLED FASTENER HOLES ON AFT END (MARKED)<[01] R/W T/E PANEL 661BB HAD PULLED FASTENER HOLES ON AFT END 51-70-04-2R-9;[02] VERIFIED JOB COMPLETESep 28, 2024 · N272WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2024110151485Support Bracket · crackedGROUND SERVICE HYDRAULIC MODULAR PACKAGE SUPPORT BRACKET CRACKED; STA 663 RBL 57 (MARKED)<[01] REMOVED AND REPLACED GROUND SERVICE HYDRAULIC MODULAR PACKAGE SUPPORT BRACKET STA 663 RBL 57 PN#276A9183-2 IAW SRM 51-40-02 AND PER DWG#111A1001 REV: A;[02] JOB COMPSep 27, 2024 · N272WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103143004Pressure Deck · crackedCRACK FOUND ON RH HORIZONTAL PRESSURE DECK WEB AT BS663+1.5; RBL41; L: 0.5' MARKED<[01] PERFORMED REPAIR AT RH SIDE BS 663 TO BS 675 BETWEEN RBL 30 TO RBL 65 PER SRM 53-40-51-2R-2 REP 2;[02] VERIFIED CORRECTIVE ACTION COMPLETE.Sep 27, 2024 · N272WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2024110142659Skin · pulledNO.1 ENGINE BARREL SKIN FASTENER IS PULLED THROUGH AT ABOUT 1 O'CLOCK POSITION. MARKED<[01] REMOVED INLET FOR MOD S/N: 2245001 INSTALLED S/N: 0736001 SEE TASK CARD TTG8Q00S71JX FOR WORK ACCOMPLISHED (PART REQUIREMENT);[02] VERIFIED ACTION 1.Sep 26, 2024 · N272WN · Boeing 7377H4 · Nacelle/Pylon, Plate/SkinSDR SWAA2024091235890Seal · crackedR/H HORIZONTAL STAB UPPER SLIDING SEAL CRACKED<[01] R&R SLIDER REF AMM 53-31-31Sep 10, 2024 · N272WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024091235889Seal · crackedL/H HORIZONTAL STAB UPPER SLIDING SEAL CRACKED<[01] REMOVED AND REPLACED LH UPPER HORIZONTAL STABILIZER SLIDING SEAL IAW AMM 53-31-31-400-802-NG (STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL INSTALLATION - PERMANENT)<BR>CERTIFY WORK PERFORMEDSep 10, 2024 · N272WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2023121330961Brake Assy · fire#3 BRAKE FIRE AT GATE.MORE THRUST REQUIRED THAN USUAL WHILE TAXING TO GATE. PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-07.Dec 12, 2023 · N272WN · Boeing 7377H4 · Landing Gear Brake SystemSDR SWAA2023090697170Sign · out of adjustL1 DOOR LOWER EXIT SIGN MISSING DIRECTIONAL ARROW.<[01] INSTALLED THE L1 DOOR LOWER EXIT SIGN DIRECTIONAL ARROW ASSY COVER IAW AMM 33-51-01Sep 6, 2023 · N272WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023050946642Light · inoperativeR1 DOOR OUTSIDE EMERGENCY LIGHT INOP.<[01] RELAMPED R1 SLIDE EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECK GOOD.May 7, 2023 · N272WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023012594574Pump · failedLOSS OF HYDRAULIC SYS A. REPLACED NR 1 ENGINE HYDRAULIC PUMP & PRESSURE LINE PER MM29-11-11Jan 23, 2023 · N272WN · Boeing 7377H4 · Hydraulic Pump (Electric/Engine), MainSDR SWAA2023011992284Bolt · looseAFT ENTRY DOOR ASSIST HANDLE WAS LOOSE. ON FURTHER INVESTIGATION FOUND THE ASSIST HANDLE RETAINING BOLTS TO BE LOOSE. TIGHTENED RETAINING BOLTS IAW SRM 51-40-02.Jan 18, 2023 · N272WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2023011989238Support Bracket · crackedAFT CARGO BAY SUPPORT BRACKET CRACKED, BS 867, LBL 15, WL 154. LOCATED AND DRILLED A NEW SUPPORT BRACKET IAW SRM 51-40-05-0G-0, DWG 149A8102, REV-, & DWG 149A8104, REV B. INSTALLED THE NEW SUPPORT BRACKET IAW SRM 51-40-02-0G-0, DWG 149A8102, REV-, & DWG 14Jan 7, 2023 · N272WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023011986803Floor Support · corrodedCORRODED INTERCOSTAL, BS 294.5 - 312, LBL 11, WL 208. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-40-02. LOCATED AND DRILLED A NEW INTERCOSTAL IAW SRM 51-40-05, AND DRAWING 141A5690. 100% OF ALL PERMANENT OR TEMPORARY FASTENERS HAVE BEEN INSTALLED WITH FAYING SDec 31, 2022 · N272WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023011986297Structure · crackedCRACKED BREAK PANEL AT STA 537; RBL 2; WL 208. REMOVED AND REPLACED CRACKED BREAK PANEL AT STA 537; RBL 2; WL 208 IAW SRM 51-40-02-0G-0 AND AMM20-50-11-910-801.Dec 30, 2022 · N272WN · Boeing 7377H4 · Fuselage Structure (General)SDR SWAA2023011986298Floorbeam · crackedCRACKED BREAK PANEL AT STA 537; LBL 2; WL 208.REMOVED AND REPLACED CRACKED BREAK PANEL AT STA 537; LBL 2; WL 208 IAW SRM 51-40-02-0G-0 AND AMM20-50-11-910-801.Dec 30, 2022 · N272WN · Boeing 7377H4 · Fuselage Main, Floor Beam
Back to N272WN