# Service difficulty reports: N728SW, cancelled Nov 7, 2024

A list on [N728SW, cancelled Nov 7, 2024](https://openairdocs.org/deregistered/N728SW-2024-11-07.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 · 253 reports

- [SDR SWAA2022030379792](https://openairdocs.org/sdr/SWAA2022030379792.md): Seal · torn · Mar 3, 2022 · N728SW · Boeing 737* · Horizontal Stabilizer Miscellaneous Structure
  > RT HORZ LOWER FWD SLIDER TORN / [01] REMOVED AND REPLACED FWD LOWER SLIDER IAW AMM 53-31-31
- [SDR SWAA2022030379793](https://openairdocs.org/sdr/SWAA2022030379793.md): Seal · torn · Mar 3, 2022 · N728SW · Boeing 737* · Horizontal Stabilizer Miscellaneous Structure
  > LT HORZ FWD UPPER SLIDER TORN / [01] REMOVED AND REPLACED FWD UPPER SLIDER IAW AMM 53-31-31
- [SDR SWAA2021111542484](https://openairdocs.org/sdr/SWAA2021111542484.md): Panel · elongated · Nov 10, 2021 · N728SW · Boeing 737* · Aerodynamic Fairings
  > FAIRING PANEL 194E HAS MULTIPLE ELONGATED FASTENER HOLES.; / [01] TSR 2021007285 PNL REPLACEMENT; [02] INSTALLED NEW PANEL REF AMM 53-51-21
- [SDR SWAA2021111542487](https://openairdocs.org/sdr/SWAA2021111542487.md): Panel · elongated · Nov 10, 2021 · N728SW · Boeing 737* · Aerodynamic Fairings
  > FAIRING PANEL 193D HAS MULTIPLE ELONGATED FASTENER HOLES.; / [01] TSR 2021007285 PNL REPLACEMENT; [02] REPLACED PANEL PER AMM53-51-21.
- [SDR SWAA2021102837673](https://openairdocs.org/sdr/SWAA2021102837673.md): Transmitter · out of tolerance · Oct 25, 2021 · N728SW · Boeing 7377H4 · Trailing Flap Position Indicating System
  > FLAPS WOULD NOT EXTEND DURING FLIGHT- USED ALT FLAP EXT AND LANDED FLAP 15; / [01] PERF FIM 27-51-849 WITH NO DEFECTS NOTED; PERF FLAP POSITION VERIFICATION TEST IAW AMM 27-50-00-820 AT FULL DOWN FOUND LH FLAP POSITION OUT OF LIMITS (MEASURED 275.5) R/R LH FL
- [SDR SWAA2021041263185](https://openairdocs.org/sdr/SWAA2021041263185.md): Cover · missing · Apr 10, 2021 · N728SW · Boeing 7377H4 · Emergency Lighting
  > CTR O/W EXIT SIGN MISSING AFT COVER CREW REPORTS / INSTALLED O/W EXIT SIGN LIGHT COVER PER SIP
- [SDR SWAA2021040761842](https://openairdocs.org/sdr/SWAA2021040761842.md): Lens · wrong part · Apr 6, 2021 · N728SW · Boeing 7377H4 · Emergency Lighting
  > FWD ENTRY DOOR LOWER LENS NOT BILINGUAL / REMOVED & REPLACED FWD ENTRY DOOR LOWER EMERGENCIES EENS IAW AMM 33-51-01
- [SDR SWAA2021040761837](https://openairdocs.org/sdr/SWAA2021040761837.md): Lens · wrong part · Apr 6, 2021 · N728SW · Boeing 7377H4 · Emergency Lighting
  > LEFT & RIGHT LOWER EMER EXIT OVERWING LENS MISSING DIRECTIONAL ARROWS / REMOVED AND REPLACED LOWER EMER EXIT OVERWING LENS IAW AMM 33-51-01
- [SDR SWAA2021050535883](https://openairdocs.org/sdr/SWAA2021050535883.md): Seal · cracked · Dec 10, 2020 · N728SW · Boeing 7377H4 · Horizontal Stabilizer Structure
  > RIGHT HORIZONTAL STABILIZER FORWARD LOWER SLIDING SEAL CRACKED / R & R SLIDING SEAL PER AMM 53-31-31.
- [SDR SWAA2021050535882](https://openairdocs.org/sdr/SWAA2021050535882.md): Seal · cracked · Dec 10, 2020 · N728SW · Boeing 7377H4 · Horizontal Stabilizer Structure
  > RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL CRACKED / R&R RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL PER AMM 53-31-31.
- [SDR SWAA2020121435885](https://openairdocs.org/sdr/SWAA2020121435885.md): Clevis · damaged · Dec 10, 2020 · N728SW · Boeing 7377H4 · Horizontal Stabilizer Structure
  > HORIZONTAL STABILIZER FORWARD LOWER SPAR CLEVIS DAMAGED AT AFT RADIUS. DAMAGE MEASURES L=.4 W=.25 D=.2 AT DEEPEST POINT. REPAIRED PER EA 20-155-02462 24647.
- [SDR SWAA2020081107642](https://openairdocs.org/sdr/SWAA2020081107642.md): Bulb · inoperative · Aug 8, 2020 · N728SW · Boeing 7377H4 · Emergency Lighting
  > LT & RT OVERWING EXIT SIGNS HAVE BURNED OUT BULBS. REPLACED THE LAMPS AND PERFORMED A GOOD INSTALLATION TEST IAW AMM 33-51-01-960-801.
- [SDR SWAA2020081107094](https://openairdocs.org/sdr/SWAA2020081107094.md): Bulb · inoperative · Aug 8, 2020 · N728SW · Boeing 7377H4 · Emergency Lighting
  > LEFT & RIGHT OVERWING EXIT SIGNS HAVE BURNED OUT BULBS. REPLACED THE LAMP AND PERFORMED A GOOD INSTALLATION TEST IAW AMM 33-51-01-960-801.
- [SDR SWAA2020081107093](https://openairdocs.org/sdr/SWAA2020081107093.md): Lamp · inoperative · Aug 8, 2020 · N728SW · Boeing 7377H4 · Emergency Lighting
  > LEFT OVERWING SLIDE LIGHT DOES NOT ILLUMINATE. REPLACED THE LAMPS AND PERFORMED A GOOD INSTALLATION TEST IAW AMM 33-51-04-960-801.
- [SDR SWAA2021062407092](https://openairdocs.org/sdr/SWAA2021062407092.md): Scuff Plate · cracked · Aug 7, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / AFT CARGO BAY FWD CORNER SCUFF PLATE WAS REPAIRED PER SRM 53-60-15-2R-1 PAGE 2. PAR. B.(4)(5);(6);(7); & (8). INSTALL WILL BE ACCOMPLISHED ON CUSTOMER CARD: 753-140-00-02Y
- [SDR SWAA2021062406774](https://openairdocs.org/sdr/SWAA2021062406774.md): Scuff Plate · cracked · Aug 6, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / AFT CARGO BAY AFT CORNER SCUFF PLATE WAS REPAIRED PER SRM 53-60-15-2R-1 PAGE 2. PAR B.(4);(5);(6) (7); & (8). INSTALL WILL BE ACCOMPLISHED ON CUSTOMER CARD 753-140-00-02Y.
- [SDR SWAA2020081105334](https://openairdocs.org/sdr/SWAA2020081105334.md): Battery Pack · inoperative · Aug 1, 2020 · N728SW · Boeing 7377H4 · Emergency Lighting
  > AFT EMERGENCY EXITS LIGHT BATTERY M1673 WILL NOT HOLD A CHARGE. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK M1673 AND PERFORMED GOOD TEST IAW AMM 33-51-06-960-805.
- [SDR SWAA2020081707811](https://openairdocs.org/sdr/SWAA2020081707811.md): Skin · gouged · Jul 31, 2020 · N728SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A GOUGE BS 1016+1;.6' BELOW STR 13L / FUSELAGE SKIN GOUGE @ BS 1016+1;.6' BELOW STR 13 LH DAMAGE REPAIRED AND EVALUATED PER EA 20-153-01365 REV IR. (ATS ER 20-03026 REV IR.
- [SDR SWAA2020081707809](https://openairdocs.org/sdr/SWAA2020081707809.md): Skin · gouged · Jul 31, 2020 · N728SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A GOUGE BS 1016+.3; 2' ABOVE STR 13L / FUSELAGE SKIN GOUGE BS 1016+.3; 2' ABOVE STR 13L WAS BLENDED INSPECTED & EVALUATED IAW EA 20-153-01365 REV IR DATED 08/09/2020 & ATS ER 20-03026 REV IR DATED 08/09/2020 DAMAGE IS ALLOWABLE FOR CONTINUED
- [SDR SWAA2020081707808](https://openairdocs.org/sdr/SWAA2020081707808.md): Skin · dented · Jul 26, 2020 · N728SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > DEFT TRANSFERRED FROM CARD 9841860=FUSELAGE EXTERNAL SKIN HAS A DENT LOCATED AT BS 1016+5'; 1' ABOVE STRINGER 14 L/H; DENT MEASURES L=2.7'; W=1.1'; Y=0.026' W/Y=42 / DENT TRANSFERD FROM CARD 9841860; FUSLAGE EXTERNAL SKIN HAS DENT LOCATED @ BS 1016+5'; 1' ABOV
- [SDR SWAA2020081707535](https://openairdocs.org/sdr/SWAA2020081707535.md): Skin · dented · Jul 26, 2020 · N728SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN HAS A DENT LOCATED AT BS 1016+6'; 1' BELOW STRINGER 14 L/H; DENT MEASURES L=0.9'; W=0.7'; Y=0.009' W/Y=77 / FUSELAGE EXTERNAL SKIN DENT @ BS 1016+6'; 1' BELOW STR 14L/H DAMAGE REPAIRED & EVALUATED PER EA 20-153-01365 REV IR DATED 08/09/2
- [SDR SWAA2020081707807](https://openairdocs.org/sdr/SWAA2020081707807.md): Skin · dented · Jul 24, 2020 · N728SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT BS 420+12; 2' BELOW STR 18L. DENT MEASURES L= 1; W= 1; Y=.026'; W/Y= 38 / REPAIRED SKIN DENT AT BS 420+12; 2' BELOW STR18L PER EA 20-153-01372 REV IR AND ER 20-03032 REV.IR.
- [SDR SWAA2021081202720](https://openairdocs.org/sdr/SWAA2021081202720.md): Boot · damaged · Jul 20, 2020 · N728SW · Boeing 7377H4 · Aerodynamic Fairings
  > NOSE RADOME BOOT IS DAMAGED. / REMOVED NOSE RADOME BOOT AND INSTALLED NEW RADOME BOOT IAW AMM 53-52-00-000-802; AMM 53-52-00-400-802
- [SDR SWAA2021081502669](https://openairdocs.org/sdr/SWAA2021081502669.md): Support · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400 - BS500D LBL23 WL157. / REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT FCB BS400-BS500D LBL23 ITEM 7530869 PO #797129 IAW SRM 53-00-53-1A-2; SRM 51-40-02; SRM 51-40-05 AND DWG 143A7501; DWG
- [SDR SWAA2021081502676](https://openairdocs.org/sdr/SWAA2021081502676.md): Shield · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON AFT SHIELD AT FWD CARGO BAY BS494 - BS500A RBL24 WL157. / REMOVED AND REPLACED FCB AFT SHIELD PER SRM S140102; SRM 51-40-05 AND DWG. 143A0080; 91195U 8/1/20
- [SDR SWAA2021081502709](https://openairdocs.org/sdr/SWAA2021081502709.md): Shield · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON FWD SHIELD AT ACB BS767 - BS787 RBL22 WL157. / REMOVED AND REPLACED FWD SHIELD AT ACB BS767 - BS787 RBL22 WL157 PER SRM 51-40-02-0G-0; SRM 51-10-02-0G-0; SRM 51-40-05-0G-0 AND BOEING DRAWING 146A8127 BOEING DRAWING 146A0081. 57006U 03AUG20
- [SDR SWAA2021081502704](https://openairdocs.org/sdr/SWAA2021081502704.md): Cargo Track · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Floor Panel
  > ***CORROSION*** ON TRACK AT ACB BS787 - BS867 RBL13 WL160. / ACB CARGO TRACK AT BS787-BS867 RBL13 WL160 WILL BE REPLACED ON CUSTOMER CARD U194211.
- [SDR SWAA2021081502667](https://openairdocs.org/sdr/SWAA2021081502667.md): Shield · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON FWD SHIELD AT FWD CARGO BAY BS420 - BS440 RBL23 WL157. / REMOVED AND REPLACED FWD SHIELD AT F.C.B. BS420-440 RBL23 WL157 SRM 51-40-02 REF DWG 143A0080 890040 31JUL20
- [SDR SWAA2021052602683](https://openairdocs.org/sdr/SWAA2021052602683.md): Gusset · cracked · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED / REMOVED AND REPLACED FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET BS 500D S-19R WL193. PER SRM 51-40-02 REF DWG 143A7902
- [SDR SWAA2021052602682](https://openairdocs.org/sdr/SWAA2021052602682.md): Gusset · cracked · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / REMOVED AND REPLACED FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET BS 500D S-19L WL193. PER SRM 51-40-02 REF DWG 143A7902
- [SDR SWAA2020081702378](https://openairdocs.org/sdr/SWAA2020081702378.md): Floorbeam · cracked · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACKED FLOORBEAM AT BS 540, BL 0 - LBL 24.5, WL 208.1. REMOVED AND INSTALLED NEW FLOORBEAM IAW SRM 51-40-02-0G-0.
- [SDR SWAA2020081702679](https://openairdocs.org/sdr/SWAA2020081702679.md): Floorbeam · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON AFT BULKHEAD LOWER SUPPORT ANGLE AT FWD CARGO BAY BS500D LBL23 TO RBL23 WL157. CORROSION FOUND ON FCB AFT BULKHEAD LOWER SUPPORT ANGLE BS-500D LBL-23 TO RBL-23 WL-157 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS REPAIRED BY REPLACEMENT
- [SDR SWAA2020081702691](https://openairdocs.org/sdr/SWAA2020081702691.md): Floorbeam · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS947 RBL20 WL181. MARKED / REMOVED AND REPLACED AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS947 RBL20 TO LBL10 WL181 IAW SRM 51-40-02 REF DWG 149A8117.
- [SDR SWAA2020081702698](https://openairdocs.org/sdr/SWAA2020081702698.md): Support Angle · cracked · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS918 RBL11 WL171. REMOVED AND INSTALLED NEW SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS918 RBL11 WL171 ITEM #7531385 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 DWG #147A7221.
- [SDR SWAA2020081702707](https://openairdocs.org/sdr/SWAA2020081702707.md): Support · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS807 LBL21 WL157. / CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727-BS807 LBL21 WL157 FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 20% MATERIAL LOSS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2. REMOVED AND
- [SDR SWAA2020081702708](https://openairdocs.org/sdr/SWAA2020081702708.md): Support · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS767 RBL21 WL157. CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727-BS767 RBL21 WL157 FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 50% MATERIAL LOSS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2. REMOVED AND
- [SDR SWAA2020081702681](https://openairdocs.org/sdr/SWAA2020081702681.md): Stringer · cracked · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS540 S-24L WL165. MARKED / REPAIRED STR AT STA;540 STR 24L WL 165 PER SRM 53-00-03-2R-1; EA 20-153-01391 REV IR AND ER 20-02989 REV IR
- [SDR SWAA2020081702711](https://openairdocs.org/sdr/SWAA2020081702711.md): Track · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON TRACK AT ACB BS766 RBL13 WL156. / REMOVED CORROSION ON ACB TRACK BS 766 RBL 13 WL156 MAX. MAT. LOSS 2.' X.5' X.04' TOP SIDE FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED ACB TRACK BS 727-BS 887 RBL13 WL156 I.A.W SRM 53-00-53-1A-2; SRM 53-00-53
- [SDR SWAA2020081702677](https://openairdocs.org/sdr/SWAA2020081702677.md): Support · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT BS500A - BS500D RBL22 WL157. REMOVED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT BS500A BS400D RBL22 IAW SRM 51-40-02; SRM 51-40-05 SRM 51-20-01; DWG 143A7501 AND DWG 143A7500; SRM 53-00-53-1A-2.
- [SDR SWAA2020081702668](https://openairdocs.org/sdr/SWAA2020081702668.md): Support · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400 - BS420 RBL23 WL157. REMOVED CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS400-BS420 RBL23. REMAINING THICKNESS IS 0.034' OUT OF LIMITS PER SRM 53-00-53-1A-2. FABRICATED NEW FLOOR TO SIDEWALL SUPPO
- [SDR SWAA2020081702690](https://openairdocs.org/sdr/SWAA2020081702690.md): Web · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUBTHRESHOLD WEB AT ACB BS794 - BS847 RBL26 WL157. / REMOVED AND REPLACED ACB SUB THRESHOLD WEB PER SRM 51-40-02; SRM 51-40-05 AND DWG. 146A8340; 91195U 8.2.20
- [SDR SWAA2020081702675](https://openairdocs.org/sdr/SWAA2020081702675.md): Web · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS440 - BS490 RBL27 WL157. / REMOVED CORROSION AT FCB SUB THRESHOLD WEB BS440-490 RBL27 L=3' W=2.4' ORIGINAL THICKNESS 0.045'; MATERIAL LOSS MORE THAN 50% FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1. REMOVED A
- [SDR SWAA2020081702706](https://openairdocs.org/sdr/SWAA2020081702706.md): Floor Support · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL AT ACB BS767 - BS787 RBL6 WL154. / REMOVED AND REPLACED NEW INTERCOATAL AT ACB BS767-BS787 RBL 6 ITEM 7532036 PO#794694 IAW SRM 51-40-02; 51-40-03; SRM 53-60-15-01-1 AND DWG 146A8131; DWG 146A8130. 80641U 03AUG20
- [SDR SWAA2020081702713](https://openairdocs.org/sdr/SWAA2020081702713.md): Attach Angle · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORROSION ON STRINGER ATTACH ANGLE BS767 RBL5 WL150. MARKED / REMOVED AND REPLACED STRINGER ATTACH ANGLE P/N 146A1320-14 PO #799088; BS767 RBL5 WL150 IAW SRM 51-40-02-OG-0 STEP 7.D. REF DWG 146A7810 89004U 04AUG20
- [SDR SWAA2020081702716](https://openairdocs.org/sdr/SWAA2020081702716.md): Stringer Clip · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORROSION ON STRINGER CLIP AT ACB BS747 LBL14 WL153. REMOVED AND REPLACED ON STRINGER CLIP AT ACB BS 747 LBL 14 IAW SRM 51-40-02 AND DWG 146A1260 80641U 03AUG20
- [SDR SWAA2020081702710](https://openairdocs.org/sdr/SWAA2020081702710.md): Web · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB AT ACB BS767+6 RBL20 WL157. / REMOVED AND REPLACED WEB AT ACB BS767 787 RBL 20 WL157 PER SRM 51-40-02-0G-0; SRM 53-60-15-01-01; SRM 53-60-15-1A-1 AND BOEING DRAWING 146A0081. 57006U 03AUG20
- [SDR SWAA2020081702697](https://openairdocs.org/sdr/SWAA2020081702697.md): Angle · corroded · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS914 RBL11 WL171. REMOVED AND INSTALLED NEW SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS914 RBL11 WL171 ITEM #7531385 IAW SRM 51-40-02-0G-0; 51-40-05-0G-0; DWG #147A7221
- [SDR SWAA2020081102381](https://openairdocs.org/sdr/SWAA2020081102381.md): Tab · delaminated · Jul 16, 2020 · N728SW · Boeing 7377H4 · Elevator, Tab Structure
  > RT ELEVATOR TAB HAS SMALL DELAMINATION ON O/B EDGE ON BULLNOSE. REMOVED FINISH FROM DAMAGE AREA IAW AMM 51-21-99-300-802, PARA 3C, (3)(A)-(D). RT ELEVATOR TAB WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G-0 PAR 9 AND WILL BE REINSTALLED.
- [SDR SWAA2020081102680](https://openairdocs.org/sdr/SWAA2020081102680.md): Stringer · cracked · Jul 16, 2020 · N728SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER 25R AFT OF BS 540.
- [SDR SWAA2021081702368](https://openairdocs.org/sdr/SWAA2021081702368.md): Fairing · delaminated · Jul 15, 2020 · N728SW · Boeing 7377H4 · Aerodynamic Fairings
  > FAIRING 193B HAS NUMEROUS AREAS OF DELAMINATION ON OUTER SURFACE (MARKED). / REPLACED FAIRING 193B WITH NEW SERVICEABLE UNIT IAW SRM 51-10-02-0G-0 PAR 9.A.

Next page: https://openairdocs.org/deregistered/N728SW-2024-11-07/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 = 'N728SW' AND deregistration_id = 'N728SW-2024-11-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N728SW-2024-11-07/reports

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