# Service difficulty reports: N755SA, cancelled Sep 16, 2024

A list on [N755SA, cancelled Sep 16, 2024](https://openairdocs.org/deregistered/N755SA-2024-09-16.md).

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

Page 1 of 6 · 293 reports

- [SDR SWAA2023041426547](https://openairdocs.org/sdr/SWAA2023041426547.md): Cover · missing · Apr 12, 2023 · N755SA · Boeing 7377H4 · Emergency Lighting
  > CAPT 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.
- [SDR SWAA2023041124557](https://openairdocs.org/sdr/SWAA2023041124557.md): Light · inoperative · Apr 7, 2023 · N755SA · Boeing 7377H4 · Emergency Lighting
  > INTERIOR 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.
- [SDR SWAA2023030812872](https://openairdocs.org/sdr/SWAA2023030812872.md): Slide · out of adjust · Mar 5, 2023 · N755SA · Boeing 7377H4 · Escape Slide
  > CREW REPORTED R2 SLIDE HANGING TO FAR BELOW SLIDE CASE.<[01] ADJUSTED SLIDE PER MT 725-61-06 AND AMM 25-66-00
- [SDR SWAA2022101359190](https://openairdocs.org/sdr/SWAA2022101359190.md): None · cracked · Oct 13, 2022 · N755SA · Boeing 7377H4 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER UPPER FORWARD SLIDER CRACKED. / [01] R&R LEFT HORIZONTAL STABILIZER UPPER FORWARD SLIDER PER AMM 53-31-31-401 CONFIG 2-NG.
- [SDR SWAA2022101157475](https://openairdocs.org/sdr/SWAA2022101157475.md): Sign · inoperative · Oct 8, 2022 · N755SA · Boeing 7377H4 · Emergency Lighting
  > CUSTOMER 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 1
- [SDR SWAA2022101157477](https://openairdocs.org/sdr/SWAA2022101157477.md): Battery Pack · inoperative · Oct 8, 2022 · N755SA · Boeing 7377H4 · Emergency Lighting
  > CUSTOMER 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 1
- [SDR SWAA2022101157476](https://openairdocs.org/sdr/SWAA2022101157476.md): Battery Pack · inoperative · Oct 8, 2022 · N755SA · Boeing 7377H4 · Emergency Lighting
  > CUSTOMER 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 1
- [SDR SWAA2022101157474](https://openairdocs.org/sdr/SWAA2022101157474.md): Battery Pack · inoperative · Oct 8, 2022 · N755SA · Boeing 7377H4 · Emergency Lighting
  > CUSTOMER 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 1
- [SDR SWAA2022101157473](https://openairdocs.org/sdr/SWAA2022101157473.md): Battery Pack · inoperative · Oct 7, 2022 · N755SA · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY 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 1
- [SDR SWAA2022101195083](https://openairdocs.org/sdr/SWAA2022101195083.md): Bulkhead · canning · Sep 20, 2022 · N755SA · Boeing 7377H4 · Fuselage Main, Bulkhead
  > OIL 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
- [SDR SWAA2022101195081](https://openairdocs.org/sdr/SWAA2022101195081.md): Bulkhead · canning · Sep 20, 2022 · N755SA · Boeing 7377H4 · Fuselage Main, Bulkhead
  > OIL 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] INSTALLE
- [SDR SWAA2022100683004](https://openairdocs.org/sdr/SWAA2022100683004.md): None · warped · Sep 19, 2022 · N755SA · Boeing 7377H4 · Fuselage Main, Structure
  > OIL CANNING FOUND ON BS AFT PRESSURE BULKHEAD 5 IN. BELOW STRINGER 11R - 60 IN. FROM APEX. / [01] TRANSFERRED TO N/R FAULT TTG8Q00EXJBY
- [SDR SWAA2022100683005](https://openairdocs.org/sdr/SWAA2022100683005.md): None · warped · Sep 19, 2022 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > OIL 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 TTG8Q00EXJCA
- [SDR SWAA2022080437783](https://openairdocs.org/sdr/SWAA2022080437783.md): Doubler · cracked · Aug 2, 2022 · N755SA · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > EXTERNAL 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
- [SDR SWAA2021112446248](https://openairdocs.org/sdr/SWAA2021112446248.md): Fairing · delaminated · Nov 20, 2021 · N755SA · Boeing 7377H4 · Aerodynamic Fairings
  > RH 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 M
- [SDR SWAA2021112346247](https://openairdocs.org/sdr/SWAA2021112346247.md): Tire · failed · Nov 20, 2021 · N755SA · Boeing 7377H4 · Tire
  > #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 I
- [SDR SWAA2021112346766](https://openairdocs.org/sdr/SWAA2021112346766.md): Tire · failed · Nov 20, 2021 · N755SA · Boeing 7377H4 · Tire
  > #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 I
- [SDR SWAA2021102832842](https://openairdocs.org/sdr/SWAA2021102832842.md): None · broken · Oct 25, 2021 · N755SA · Boeing 7377H4 · Emergency Lighting
  > AFT GALLEY ENTRY DOOR EXIT SIGN MID DOOR BROKEN; / [01] REPLACED AFT GALLEY SVC DOOR EXIT SIGN LENS RH SIDE REF AMM 33-51-01
- [SDR SWAA2021090814892](https://openairdocs.org/sdr/SWAA2021090814892.md): Mount · broken · Sep 3, 2021 · N755SA · Boeing 7377H4 · Emergency Lighting
  > MID 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 DAYS
- [SDR SWAA2021090714154](https://openairdocs.org/sdr/SWAA2021090714154.md): Lamp · inoperative · Sep 1, 2021 · N755SA · Boeing 7377H4 · Emergency Lighting
  > FWD 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 33-51-01-960-801
- [SDR SWAA2021090712630](https://openairdocs.org/sdr/SWAA2021090712630.md): Lamp · missing · Aug 27, 2021 · N755SA · Boeing 7377H4 · Emergency Lighting
  > R/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 1
- [SDR SWAA2021090710659](https://openairdocs.org/sdr/SWAA2021090710659.md): Intercostal · corroded · Aug 23, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION; 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
- [SDR SWAA2021090710661](https://openairdocs.org/sdr/SWAA2021090710661.md): Web · corroded · Aug 23, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION; 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
- [SDR SWAA2021090709346](https://openairdocs.org/sdr/SWAA2021090709346.md): Support · damaged · Aug 21, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB 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-
- [SDR SWAA2021090709344](https://openairdocs.org/sdr/SWAA2021090709344.md): Splice · damaged · Aug 21, 2021 · N755SA · Boeing 7377H4 · Fuselage Floor Panel
  > AFT 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 S
- [SDR SWAA2021090708356](https://openairdocs.org/sdr/SWAA2021090708356.md): Frame · damaged · Aug 18, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, Frame
  > OVERSIZE 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.;
- [SDR SWAA2021090708355](https://openairdocs.org/sdr/SWAA2021090708355.md): Angle · cracked · Aug 18, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FORWARD 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;
- [SDR SWAA2021090708354](https://openairdocs.org/sdr/SWAA2021090708354.md): Gusset · cracked · Aug 18, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB 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 A
- [SDR SWAA2021090708353](https://openairdocs.org/sdr/SWAA2021090708353.md): Gusset · cracked · Aug 18, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB 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 A
- [SDR SWAA2021090708352](https://openairdocs.org/sdr/SWAA2021090708352.md): Gusset · cracked · Aug 18, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB 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 A
- [SDR SWAA2021090707206](https://openairdocs.org/sdr/SWAA2021090707206.md): Panel · chafed · Aug 12, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PANEL 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
- [SDR SWAA2021090707209](https://openairdocs.org/sdr/SWAA2021090707209.md): Stiffener · cracked · Aug 12, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, Structure
  > LT 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
- [SDR SWAA2021090707208](https://openairdocs.org/sdr/SWAA2021090707208.md): Stiffener · cracked · Aug 12, 2021 · N755SA · Boeing 7377H4 · Horizontal Stabilizer Structure
  > LT 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 GVI
- [SDR SWAA2021090706323](https://openairdocs.org/sdr/SWAA2021090706323.md): Stringer Clip · cracked · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORROSION 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 T
- [SDR SWAA2021090706310](https://openairdocs.org/sdr/SWAA2021090706310.md): Stringer Clip · corroded · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORROSION 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 T
- [SDR SWAA2021090706300](https://openairdocs.org/sdr/SWAA2021090706300.md): Shield · corroded · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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 OU
- [SDR SWAA2021090706326](https://openairdocs.org/sdr/SWAA2021090706326.md): Shield · corroded · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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 LIMITS
- [SDR SWAA2021090706332](https://openairdocs.org/sdr/SWAA2021090706332.md): Support · corroded · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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; [
- [SDR SWAA2021090706324](https://openairdocs.org/sdr/SWAA2021090706324.md): Web · corroded · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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] VERIFI
- [SDR SWAA2021090706304](https://openairdocs.org/sdr/SWAA2021090706304.md): Shield · corroded · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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 CORROSION
- [SDR SWAA2021090706328](https://openairdocs.org/sdr/SWAA2021090706328.md): Support · corroded · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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;
- [SDR SWAA2021090706309](https://openairdocs.org/sdr/SWAA2021090706309.md): Intercostal · corroded · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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
- [SDR SWAA2021090706308](https://openairdocs.org/sdr/SWAA2021090706308.md): Intercostal · corroded · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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
- [SDR SWAA2021090706327](https://openairdocs.org/sdr/SWAA2021090706327.md): Web · corroded · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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 LIMIT
- [SDR SWAA2021090706336](https://openairdocs.org/sdr/SWAA2021090706336.md): Track · corroded · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION 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] EDIT
- [SDR SWAA2021090706333](https://openairdocs.org/sdr/SWAA2021090706333.md): Angle · corroded · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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 L
- [SDR SWAA2021090706329](https://openairdocs.org/sdr/SWAA2021090706329.md): Angle · corroded · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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 L
- [SDR SWAA2021090706335](https://openairdocs.org/sdr/SWAA2021090706335.md): Track · corroded · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION 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
- [SDR SWAA2021090706334](https://openairdocs.org/sdr/SWAA2021090706334.md): Track · corroded · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION 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
- [SDR SWAA2021090706331](https://openairdocs.org/sdr/SWAA2021090706331.md): Track · corroded · Aug 11, 2021 · N755SA · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION 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 T

Next page: https://openairdocs.org/deregistered/N755SA-2024-09-16/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N755SA-2024-09-16/reports

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