N755SA, cancelled Sep 16, 2024

Service difficulty reports · 293

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 = 'N755SA' AND deregistration_id = 'N755SA-2024-09-16'
  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 SWAA2023041426547Cover · missingCAPT SIDE EMERGENCY EXIT LENS COVER MISSING AT LEFT OVER WING<[01] INSTALLED EMERGENCY EXIT LENS COVER AT CAPT SIDE OVER WING IAW S.I.P.Apr 12, 2023 · N755SA · Boeing 7377H4 · Emergency LightingSDR SWAA2023041124557Light · inoperativeINTERIOR EMERGENCY LIGHT AT 17ABC INOP<[01] FOUND CONNECT FOR INTERIOR EMERGENCY LIGHT AT 17ABC NOT CONNECTED. CONNECTED THE CONNECTOR FOR AREA LIGHT AT 17ABC PER SIP AND WDM 33-51-14. OPS CHECK GOOD.Apr 7, 2023 · N755SA · Boeing 7377H4 · Emergency LightingSDR SWAA2023030812872Slide · out of adjustCREW REPORTED R2 SLIDE HANGING TO FAR BELOW SLIDE CASE.<[01] ADJUSTED SLIDE PER MT 725-61-06 AND AMM 25-66-00Mar 5, 2023 · N755SA · Boeing 7377H4 · Escape SlideSDR SWAA2022101359190None · crackedLEFT HORIZONTAL STABILIZER UPPER FORWARD SLIDER CRACKED. / [01] R&R LEFT HORIZONTAL STABILIZER UPPER FORWARD SLIDER PER AMM 53-31-31-401 CONFIG 2-NG.Oct 13, 2022 · N755SA · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2022101157475Sign · inoperativeCUSTOMER REQUEST: ONE BULB INOP EMERGENCY LOWER AT L-1 DOOR / [01] RELAMPED EMERGENCY LOWER EXIT SIGN AT L-1 DOOR PER REF. AMM 33-51-01-960-801. PERFORMED OPS CHECK AND FOUND NORMAL.;[02] VERIFIED STEP 1Oct 8, 2022 · N755SA · Boeing 7377H4 · Emergency LightingSDR SWAA2022101157477Battery Pack · inoperativeCUSTOMER REQUEST: EXTERIOR EMERGENCY LIGHT AFT OF R-1 DOOR INOP / [01] REMOVED AND REPLACED BATTERY PACK M1674 ON TTG8Q00F9CTY. R-1 DOOR EXTERIOR EMERGENCY LIGHT TEST NORMAL PER AMM 33-51-00-710-801.;[02] VERIFIED STEP 1Oct 8, 2022 · N755SA · Boeing 7377H4 · Emergency LightingSDR SWAA2022101157476Battery Pack · inoperativeCUSTOMER REQUEST: RT STOW BIN ROW 3/ROW 6 EMERGENCY LIGHT INOP / [01] REMOVED AND REPLACED M1674 EMERGENCY BATTERY PACK PER AMM 35-51-06-960-805. TEST NORMAL.;[02] VERIFIED STEP 1Oct 8, 2022 · N755SA · Boeing 7377H4 · Emergency LightingSDR SWAA2022101157474Battery Pack · inoperativeCUSTOMER REQUEST: L-1 DOOR UPPER EMERGENCY EXIT SIGN INOPERATIVE / [01] REMOVED AND REPLACED M1674 EMERGENCY BATTERY PACK ON TTG8Q 00F9CTY. L-1 DOOR EMERGENCY EXIT SIGN TEST NORMAL PER AMM33-51-00-710-801.;[02] VERIFIED STEP 1Oct 8, 2022 · N755SA · Boeing 7377H4 · Emergency LightingSDR SWAA2022101157473Battery Pack · inoperativeEMERGENCY LIGHTS INOP AT AFT CABIN AREA LEFT AND RIGHT SIDE / [01] REMOVED AND REPLACED BATTERY PACK M1673 PER AMM 33-51-06-960-805. TEST NORMAL.;[02] VERIFIED STEP 1Oct 7, 2022 · N755SA · Boeing 7377H4 · Emergency LightingSDR SWAA2022101195083Bulkhead · canningOIL CANNING FOUND ON BS1016 AFT PRESSURE BULKHEAD AT STRINGER 2L - 60 IN. FROM APEX. / [01] CUT OUT DAMAGE AREA AT BS1016 AFT PRESSURE BULKHEAD AT STRINGER 2L - 60 IN. FROM APEX. CUT OUT DIMENSION ( 2.0' X 1.5' ); ASPER B737-700 SRM 51-10-02-0G-0.[16] DRILLED Sep 20, 2022 · N755SA · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2022101195081Bulkhead · canningOIL CANNING FOUND ON BS AFT PRESSURE BULKHEAD 5 IN. BELOW STRINGER 11R - 60 IN. FROM APEX. / [01] CUT OUT DAMAGE AREA AT AFT PRESSURE BULKHEAD 5 IN. BELOW STRINGER 11R - 60 INCHES FROM APEX AS PER B737-700 SRM 53-80-08-2R-1 AND SRM 51-10-02-0G-0.;[12] INSTALLESep 20, 2022 · N755SA · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2022100683004None · warpedOIL CANNING FOUND ON BS AFT PRESSURE BULKHEAD 5 IN. BELOW STRINGER 11R - 60 IN. FROM APEX. / [01] TRANSFERRED TO N/R FAULT TTG8Q00EXJBYSep 19, 2022 · N755SA · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022100683005None · warpedOIL CANNING FOUND ON BS1016 AFT PRESSURE BULKHEAD AT STRINGER 2L - 60 IN. FROM APEX. / [01] N/A'D REMAINING MEASUREMENTS; MEASUREMENTS TRANSFERRED TO FAULT TTG8Q00EXJCA;[02] TRANSFERRED TO N/R FAULT TTG8Q00EXJCASep 19, 2022 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022080437783Doubler · crackedEXTERNAL GROUND POWER DOOR CUTOUT INTERNAL SKIN DOUBLER IS CRACKED ON LOWER SIDE OF DOOR. REMOVED DAMAGE SECTION IAW SRM 53-10-15-2R-4.FIG 204. HFEC IAW NDT PART 6; 51-00-00 P23. NO DEFECTS NOTED. PERFORMED VISUAL INSPECTION WITH 10X GLASS OF TRIM OUT AREA Aug 2, 2022 · N755SA · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021112446248Fairing · delaminatedRH MLG AFT W/W FAIRING DENTED & DELAMINATED. PANEL 194GR MEASURES 1.75'H X 4.25'W X 2/32'DREF LOGBOOK#1831149 ; / [01] REF LOG# 178451. COMPLY WITH MPM 3 DAYS METALLIC TAPE REINSPECT WITHIN 3 DAYS. PERMANENT REPAIR REQUIRED WITHIN 20 DAYS. OK TO CONTINUE PER MNov 20, 2021 · N755SA · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2021112346247Tire · failed#3 MAIN TIRE BLOWN ON TAKEOFF. DAMAGE TO WING & FLAPS NOTED AFTER LANDING. ; / [01] C/W TIRE THREADLOSS OR TIRE BURST CONDITIONAL INSPECTION PER AMM 05-51-54.REF LOGBOOK# 1831150 FOR #3&#4 MLG WHEEL ASSY R&R; REF LOGBOOK# 1787451 & LOGBOOK# 1787452 FOR RIGHT INov 20, 2021 · N755SA · Boeing 7377H4 · TireSDR SWAA2021112346766Tire · failed#3 MAIN TIRE BLOWN ON TAKEOFF. DAMAGE TO WING & FLAPS NOTED AFTER LANDING. ; / [01] C/W TIRE THREADLOSS OR TIRE BURST CONDITIONAL INSPECTION PER AMM 05-51-54.REF LOGBOOK# 1831150 FOR #3&#4 MLG WHEEL ASSY R&R; REF LOGBOOK# 1787451 & LOGBOOK# 1787452 FOR RIGHT INov 20, 2021 · N755SA · Boeing 7377H4 · TireSDR SWAA2021102832842None · brokenAFT GALLEY ENTRY DOOR EXIT SIGN MID DOOR BROKEN ; / [01] REPLACED AFT GALLEY SVC DOOR EXIT SIGN LENS RH SIDE REF AMM 33-51-01Oct 25, 2021 · N755SA · Boeing 7377H4 · Emergency LightingSDR SWAA2021090814892Mount · brokenMID CABIN EMERGENCY EXIT LIGHT HANGING FROM CEILING HAS BROKEN MOUNT. ; / [01] ACCOMPLISH EA 21-133-02605 ASSIGNED AS A SUBTASK.; [02] L/P 1686559 INSTALLED INTERIM REPAIR PER EA 21-133-02605. PERMANENT REPAIR REQUIRED WITHIN 2 DAYSSep 3, 2021 · N755SA · Boeing 7377H4 · Emergency LightingSDR SWAA2021090714154Lamp · inoperativeFWD GALLEY EXIT SIGN HAS A BULB OUT / [01] RELAMPED AND PERFORMED GOOD TEST OF FWD GALLEY EXIT SIGN PER AMM 33-25-00-960-801.; [02] CORRECTION FOR REF. S/B 33-51-01-960-801; [03] REF. CORRECTION; [04] VERIFIED CORRECTIVE ACTION 1 AND 2 PER AMM 33-51-01-960-801Sep 1, 2021 · N755SA · Boeing 7377H4 · Emergency LightingSDR SWAA2021090712630Lamp · missingR/H OVERWING EMERGENCY LIGHT MISSING BULBS. ; / [01] RE-LAMPED R/H OVERWING EMERGENCY LIGHT AND PERFORMED A GOOD OP CHECK ALL AS PER AMM 33-51-03-960-801.; [02] VERIFIED CORRECTIVE ACTION 1Aug 27, 2021 · N755SA · Boeing 7377H4 · Emergency LightingSDR SWAA2021090710659Intercostal · corrodedCORROSION; AFT CARGO; BS 807 + 2; RBL 19; WL 156; SUBTHRESHOLD INTERCOSTAL UPPER FLANGE; LWR SURFACE AT NUTPLATE HOLE; MARKED. ; / [01] REMOVED DAMAGE IN ACB BS 807+2 RBL19 WL156 IN AN AREA 1'X1' IAW SRM 53-60-15-1A-1.; [02] VERIFIED CORROSION REMOVED PER SRM Aug 23, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090710661Web · corrodedCORROSION; AFT CARGO BS 789; RBL 20; WL 155; INTERCOSTAL WEB UPPER END; OB SURFACE; MARKED ; / [01] REMOVED CORROSION IN ACB BS789 RBL20 WL 155 IN A 1'X1' AREA IAW SRM 53-60-15-1A-1.; [02] VERIFIED CORROSION REMOVED PER SRM 53-60-15-1A-1.; [03] HFEC INSPECTED Aug 23, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090709346Support · damagedFCB AFT R/H BS500D BULKHEAD SUPPORT HAS OVERSIZE ON LOWER END RBL21 WL 156 ; / [01] EVALUATED OVERSIZE HOLE ON R/H BS 500D BULKHEAD SUPPORT RBL 21 WL 156 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-Aug 21, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090709344Splice · damagedAFT CARGO BAY FLOOR PANEL SPLICE STRAP AT BS 767+4 HAS OVERSIZE HOLES RBL 10 TO LBL10 WL 156 ; / [01] UPDATED MEASUREMENT TABLE; [02] EVALUATED OVERSIZE HOLES ON SPLICE STRAP; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SAug 21, 2021 · N755SA · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021090708356Frame · damagedOVERSIZE HOLE IN FRAME AT BS727A RBL21.5 WL156 COMMON TO UPPER FLOOR TO SIDEWALL SUPPORT FASTENER HOLE ; / [01] REMOVED DAMAGE ON FRAME BS727A RBL21.5 WL156 IAW SRM 53-60-072R-2.; [02] REQUEST DVI OF THE UNDERLYING STRUCTURE AND FUSELAGE SKIN IN REPAIR AREA.; Aug 18, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2021090708355Angle · crackedFORWARD CARGO BAY L/H BAFFLE CLIP BS 400 LBL 23 WL 155 IS CRACKED ; / [01] EVALUATED DAMAGE ON BAFFLE CLIP AND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0. REMOVED OLD BAFFLE CLIP PER SRM 51-40-02-0G-0; Aug 18, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021090708354Gusset · crackedFCB GUSSET BS 500D STRINGER 21 L/H IS CRACKED ; / [01] EVALUATED CRACK; 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 EVALUATED CRACK; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AAug 18, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090708353Gusset · crackedFCB GUSSET BS 500D STRINGER 19 L/H IS CRACKED ; / [01] EVALUATED CRACK; 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 EVALUATED CRACK; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AAug 18, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090708352Gusset · crackedFCB GUSSET BS 500D STRINGER 19 R/H IS CRACKED ; / [01] EVALUATED CRACK; 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 EVALUATED CRACK; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AAug 18, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090707206Panel · chafedPANEL 192F HAS CHAFING DAMAGE TO FWD AND AFT INNER MATING SURFACES ; / [01] IDENTIFIED PANEL 192F IAW SRM 53-40-70-0I-1 FIGURE 2. TABLE 2. ITEM 15.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PARA 4.B.2.(A).<BR><BR>DAMAGE IS Aug 12, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090707209Stiffener · crackedLT HORIZ. STAB RIB ASSY. 4 (STAB STA 120.30) LOWER CHORD AT THE 4TH VERT STIFFENER IS CRACKED. ; / [01] REMOVED CRACK DAMAGE LOWER CHORD AT 4TH VERTICAL STIFFENER L=0.85'X W=0.65' IAW SRM 55-10-09-2R-5 ITEM 4 STEP B.[04] CUT AND REMOVED 1.E.A CRACKED HOLE AFT Aug 12, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2021090707208Stiffener · crackedLT HORIZ. STAB RIB ASSY. 4 (STAB STA 120.30) 2ND VERT STIFFENER IS CRACKED. ; / [01] REMOVED CRACK DAMAGE LOWER RADIUS OF VERTICAL STIFFENER AND WEB L=0.45' X W=0.35' IAW SRM 55-10-09-2R-4 ITEM 4 STEP B.; [02] VERIFIED REMOVAL OF CRACK DAMAGE AND PERFORMED GVIAug 12, 2021 · N755SA · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2021090706323Stringer Clip · crackedCORROSION ON STRINGER CLIP AT AFT CARGO BAY BS827 LBL6 WL156. ; / [01] EVALUATED CORROSION; 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 EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TAug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2021090706310Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT AFT CARGO BAY BS867 LBL6 WL162. ; / [01] EVALUATED CORROSION; 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 EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TAug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2021090706300Shield · corrodedCORROSION ON SHIELD IN FWD CARGO BAY AFT OF DOOR BS500 RBL 21 WL 156 ; / [01] UPDATED MEASUREMENTS TABLE; [02] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] VERIFIED CORROSION OUAug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090706326Shield · corrodedCORROSION ON FWD SHIELD AT AFT CARGO BAY BS767 - BS775 RBL21 WL157. ; / [01] EVALUATED CORROSION; 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 EVALUATED CORROSION; FOUND TO BE OUT OF LIMITSAug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090706332Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS767- BS727C RBL21 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X20' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; [Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090706324Web · corrodedCORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS807- BS827 RBL26 WL159. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X20' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; [02] VERIFIAug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090706304Shield · corrodedCORROSION ON SHIELD IN FWD CARGO BAY FORWARD OF DOOR BS430 RBL 21 WL 156 ; / [01] UPDATED MEASUREMENT TABLE; [02] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] VERIFIED CORROSIONAug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090706328Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727A- BS807 LBL21 WL157. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.040 IN A 1'X160' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090706309Intercostal · corrodedCORROSION ON INTERCOSTAL AT AFT CARGO BAY BS928 RBL3 WL168. ; / [01] EVALUATED CORROSION; 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 EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090706308Intercostal · corrodedCORROSION ON INTERCOSTAL AT AFT CARGO BAY BS928 LBL3 WL168. ; / [01] EVALUATED CORROSION; 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 EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090706327Web · corrodedCORROSION ON WEB AT AFT CARGO BAY BS773 RBL20 WL157 ; / [01] EVALUATED CORROSION; 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 EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITAug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090706336Track · corrodedCORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS727A+19 LBL17 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER ID# 4566A S/N UNKNOWN; [02] EDITAug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2021090706333Angle · corrodedCORROSION ON CLIP AT AFT CARGO BAY BS727D+4 LBL7 WL151. ; / [01] EVALUATED CORROSION; 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 EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LAug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090706329Angle · corrodedCORROSION ON CLIP AT AFT CARGO BAY BS727D+9 RBL7 WL151. ; / [01] EVALUATED CORROSION; 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 EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LAug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021090706335Track · corrodedCORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS727A+17 LBL17 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER ID# 4566A S/N UNKNOWN; ALL WORK Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2021090706334Track · corrodedCORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS727A+10 LBL17 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER ID# 4566A S/N UNKNOWN; ALL WORK Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2021090706331Track · corrodedCORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS727B+3 LBL17 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER ID# 4566A S/N UNKNOWN; ALL WORK TAug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, Structure
Back to N755SA, cancelled Sep 16, 2024