# Service difficulty reports: N8503A

A list on [N8503A](https://openairdocs.org/aircraft/N8503A.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 2 · 96 reports

- [SDR SWAA2026061712366](https://openairdocs.org/sdr/SWAA2026061712366.md): Lamp · inoperative · Jun 15, 2026 · N8503A · Boeing 7378H4 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT AFT OF L2 DOOR (DOOR SLIDE LIGHT) WILL NOT ILLUMINATE. RELAMPED L2 DOOR EMERGENCY SLIDE LIGHT IAW AMM 33-51-04.
- [SDR SWAA2026021169121](https://openairdocs.org/sdr/SWAA2026021169121.md): Bulb · inoperative · Feb 9, 2026 · N8503A · Boeing 7378H4 · Emergency Lighting
  > DURING WALK AROUND FOUND FWD SERVICE DOOR EXTERIOR EMERGENCY LIGHT OUT. REMOVED & REPLACED THE FWD SERVICE EXTERIOR EMERGENCY LIGHT BULB IAW AMM 33-29-00; OPS CHECKED GOOD
- [SDR SWAA2026011359850](https://openairdocs.org/sdr/SWAA2026011359850.md): Flashlight · failed · Jan 9, 2026 · N8503A · Boeing 7378H4 · Emergency Equipment
  > AFT FA FLASHLIGHT WILL NOT TEST. REINSTALLED AFT FA FLASHLIGHT IN MOUNTING BRACKET AND OP CHECKED IAW AMM 25-64-00. OPS CHECKED GOOD.
- [SDR SWAA2025120441101](https://openairdocs.org/sdr/SWAA2025120441101.md): Flashlight · no test · Dec 1, 2025 · N8503A · Boeing 7378H4 · Emergency Equipment
  > TWO FLASHLIGHTS AFT GALLEY RIGHT SIDE WILL NOT TEST. R & R BOTH AFT GALLEY RT FLASHLIGHTS IAW AMM 25-64-00. OPS CHECKED GOOD.
- [SDR SWAA2025120442746](https://openairdocs.org/sdr/SWAA2025120442746.md): Flashlight · no test · Dec 1, 2025 · N8503A · Boeing 7378H4 · Emergency Equipment
  > TWO FLASHLIGHTS AFT GALLEY RIGHT SIDE WILL NOT TEST.
- [SDR SWAA2025102928510](https://openairdocs.org/sdr/SWAA2025102928510.md): Flashlight · no test · Oct 25, 2025 · N8503A · Boeing 7378H4 · Emergency Equipment
  > EMERGENCY FLASHLIGHT IN FORWARD GALLEY, TEST FAILED. REMOVED AND REPLACED FWD GALLEY EMERGENCY FLASHLIGHT BATTERY IN REFERENCE TO AMM 25-64-00 OPERATIONAL TEST GOOD
- [SDR SWAA2025090307346](https://openairdocs.org/sdr/SWAA2025090307346.md): Battery Pack · inoperative · Aug 23, 2025 · N8503A · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1694 ARE INOPERATIVE. REPLACED AND PERFORMED GOOD FUNCTIONAL TEST OF EMERGENCY LIGHTS BATTERY PACK M1694 PER AMM 33-51-06-960-805.
- [SDR SWAA2025090307347](https://openairdocs.org/sdr/SWAA2025090307347.md): Battery Pack · inoperative · Aug 23, 2025 · N8503A · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1695 ARE INOPERATIVE. REPLACED AND PERFORMED GOOD FUNCTIONAL TEST OF EMERGENCY LIGHTS BATTERY PACK M1695 PER AMM 33-51-06-960-805.
- [SDR SWAA2025090305624](https://openairdocs.org/sdr/SWAA2025090305624.md): Attach Angle · cracked · Aug 18, 2025 · N8503A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > LEFT BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL 8 AND LBL 34, WL167.68. REMOVED, REPLACED, AND INSTALLED NEW ATTACH ANGLE IAW SRM 51-40-02-0G-0 AND DWG 11A1000 REV: -, DWG 11A7000 REV: -.
- [SDR SWAA2025090308052](https://openairdocs.org/sdr/SWAA2025090308052.md): Cap · cracked · Aug 18, 2025 · N8503A · Boeing 7378H4 · Passenger Compartment Equipment
  > PASSENGER SEAT IN ARM FOOD TRAY ARMCAP CRACKED ON SEAT 1EF; 16F. REPLACED CRACKED PASSENGER SEAT IN ARM FOOD TRAY ARMCAP WITH NEW ON SEATS 1EF; 16F IAW CMM 25-23-67-4275 PAGE 3008; PARA. N(4) AND PAGE 7011 PARA. M(8). OPS CHECK GOOD
- [SDR SWAA2025090305368](https://openairdocs.org/sdr/SWAA2025090305368.md): Handle · loose · Aug 17, 2025 · N8503A · Boeing 7378H4 · Passenger/Crew Doors
  > L1 FWD ENTRY DOOR ASSIST HANDLE LOOSE. THIGHTNED L1 FWD ENTRY DOOR ASSIST HANDLE IAW AMM 52-11-31-400-802.
- [SDR SWAA2025090305461](https://openairdocs.org/sdr/SWAA2025090305461.md): Support Beam · out of limits · Aug 17, 2025 · N8503A · Boeing 7378H4 · Wing Main, Frame Structure
  > INBOARD FWD SUPPORT ROD ATTACH POINT ON I/B SUPPORT BEAM ASSY COMMON TO FWD BEARING WALLOWED OUT BEYOND LIMITS ON COMMON TO LT WING T/E PANEL 551GB. REMOVED I/B FWD SUPPORT ROD ATTACH POINT ON I/B SUPPORT BEAM ASSY COMMON TO FWD BEARING IAW 51-40-02-0G-0. IN
- [SDR SWAA2025081803425](https://openairdocs.org/sdr/SWAA2025081803425.md): Fairing · pulled · Aug 12, 2025 · N8503A · Boeing 7378H4 · Trailing Edge Flaps
  > FLAP SUPPORT FAIRING NO. 3 AFT TAIL CONE HAS FASTENER PULLING THROUGH FAIRING.
- [SDR SWAA2025081403416](https://openairdocs.org/sdr/SWAA2025081403416.md): Elec Connector · disconnected · Aug 12, 2025 · N8503A · Boeing 737824 · Light System Wiring
  > RIGHT FWD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RECONNECTED OVERWING EXIT LIGHT ASSEMBLY CONNECTOR AT ROW 14DEF (RH FWD SIDE) OPS CK GOOD FOR EMERGENCY EXIT LIGHT PER AMM 33-21-00.
- [SDR SWAA2025072494543](https://openairdocs.org/sdr/SWAA2025072494543.md): Flashlight · inoperative · Jul 23, 2025 · N8503A · Boeing 7378H4 · Emergency Equipment
  > AFT LEFT EMERGENCY FLASHLIGHT INOP. R & R THE LT REAR EMERGENCY FLASHLIGHT IAW MM 25-64-00.
- [SDR SWAA2025063086288](https://openairdocs.org/sdr/SWAA2025063086288.md): Flashlight · intermittent · Jun 28, 2025 · N8503A · Boeing 7378H4 · Emergency Equipment
  > CAPT SIDE AFT I/B EMERGENCY FLASHLIGHT PUSH TO TEST INTERMITTENT.<[01] REMOVED AND REPLACED CAPTAINS SIDE AFT FA I/B EMERGENCY FLASHLIGHT IAW AMM 25-64-00.
- [SDR SWAA2025043064952](https://openairdocs.org/sdr/SWAA2025043064952.md): Battery · no test · Apr 27, 2025 · N8503A · Boeing 7378H4 · Emergency Equipment
  > AT FA JUMPSEAT FLASHLIGHT DOSE NOT TEST<[01] R AND R FLASH LIGHT BATTERY PER AMM 25-64-00
- [SDR SWAA2024123080906](https://openairdocs.org/sdr/SWAA2024123080906.md): Battery · no test · Dec 26, 2024 · N8503A · Boeing 7378H4 · Emergency Equipment
  > LH AFT GALLEY INBOARD FLASHLIGHT HOLDER WILL NOT TEST<[01] OK TO CONTINUE PER MEL 25-12-01. R\R LH AFT INBD FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD.
- [SDR SWAA2024120574011](https://openairdocs.org/sdr/SWAA2024120574011.md): Flashlight · inoperative · Dec 4, 2024 · N8503A · Boeing 7378H4 · Emergency Equipment
  > L/H AFT FLIGHT ATTENDANT FLASHLIGHT INOP. ADJUSTED FLASHLIGHT AND PERFORMED PUSH TO TEST IN ACCORDANCE WITH AMM 25-64-00. OPERATIONAL TEST IS SATISFACTORY AND NO DEFECTS NOTED AND INSTALLED NEW TAMPER SEAL. NO FURTHER ACTION IS REQUIRED. THIS CLEARS MEL 25-12
- [SDR SWAA2024082625304](https://openairdocs.org/sdr/SWAA2024082625304.md): Plate · cracked · Aug 13, 2024 · N8503A · Boeing 7378H4 · Emergency Exits
  > R/H AFT EMERGENCY EXIT DOOR LOWER STRAP COVER PLATE IS CRACKED<[01] REPLACED R/H AFT EMERGENCY EXIT DOOR LOWER STRAP COVER PLATE IAW IPC 52-22-51-05; DWG 411A6880 SH 6;1 REV B; AND SRM 51-40-02.;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2024082625694](https://openairdocs.org/sdr/SWAA2024082625694.md): Scuff Plate · cracked · Aug 13, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED<[01] REPAIRED AFT CARGO BAY; FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARA 4.B.(4); REFERRED TO BAC 5975;[02] VERIFIED CORRECTIVE ACTION STEP 1.
- [SDR SWAA2024082625695](https://openairdocs.org/sdr/SWAA2024082625695.md): Scuff Plate · cracked · Aug 13, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED<[01] REPAIRED THE AFT CARGO BAY; AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARA 4.B(4). REFERRED TO BAC5975;[02] VERIFIED CORRECTIVE ACTION STEP 1.
- [SDR SWAA2024082624165](https://openairdocs.org/sdr/SWAA2024082624165.md): Frame · cracked · Aug 8, 2024 · N8503A · Boeing 7378H4 · Fuselage Main, Frame
  > DOCUMENTATION FOR MEASUREMENT FIELDS ON FAULT 'FED CUTOUT UPPER STIFFER CRACK IN FRAME IB RADIUS AT BS312; STR5L [TTG8Q00UWBHF]'<[01] REPAIR ACCOMPLISHED AT M-22-153-01244 (737-NG - SWA - BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L);[
- [SDR SWAA2024082619945](https://openairdocs.org/sdr/SWAA2024082619945.md): Floorbeam · corroded · Jul 30, 2024 · N8503A · Boeing 7378H4 · Fuselage Main, Floor Beam
  > FLOOR BEAM CORRODED; BS947; LBL25; WL208<[01] ACCOPLISHED BS947 LBL25 WL208 FLOOR BEAM REPAIR PARTS IAW SRM 53-70-51-2R-5 REPAIR 5 AND IAW EA#24-153-02157-WIP1;[02] REPAIRED PER 737-800 SRM 53-70-51 REPAIR 5 WITH MINOR DEVIATIONS DOCUMENTED IN EA 24-153-02157.
- [SDR SWAA2024082620153](https://openairdocs.org/sdr/SWAA2024082620153.md): Shield · corroded · Jul 30, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOT WITH CORROSION ON FCB SHIELD NUTPLATES ON BS480+14; BS500+14 WL 156.<[01] REMOVED AND REPLACED SHIELD <BR>IAW SRM 51-40-05 AND DWG 143A0080<BR>CARD COMPLETED;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2024082619437](https://openairdocs.org/sdr/SWAA2024082619437.md): Bracket · damaged · Jul 29, 2024 · N8503A · Boeing 7378H4 · Emergency Equipment
  > FED LOWER CUTOUT; FWD. GIRT BAR SUPPORT BRACKET DAMAGED; BS 312; WL 208; LBL55<[01] REMOVED AND REPLACED SUPPORT BRACKET ITEM:141A5220-2 LOT:1571933-1. IAW SRM 51-40-02 AND SOPM 53-42-00-29;[02] REMOVED AND REPLACED SUPPORT BRACKET ITEM:141A5220-2 LOT:1571933-
- [SDR SWAA2024082619441](https://openairdocs.org/sdr/SWAA2024082619441.md): Frame · cracked · Jul 29, 2024 · N8503A · Boeing 7378H4 · Fuselage Main, Frame
  > FED CUTOUT UPPER STIFFER CRACK IN FRAME IB RADIUS AT BS312; STR5L<[01] REPAIR ACCOMPLISHED AT M-22-153-01244 (737-NG - SWA - BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L);[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TAB
- [SDR SWAA2024082619440](https://openairdocs.org/sdr/SWAA2024082619440.md): Attach Angle · corroded · Jul 29, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FED MOP SILL ATTACH ANGLE HAS CORROSION ON CORROSION ON MULTIPLE AREAS BS312 TO BS322+14; WL208; LBL60<[01] REMOVED AND REPLACED FED MOP SILL ATTACH ANGLE WL208; LBL60 I.A.W SRM 51-40-02-0G-0 AND DWG 141A8110.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024082619447](https://openairdocs.org/sdr/SWAA2024082619447.md): Floor Support · cracked · Jul 29, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR INTERCOSTAL HAS A CRACK; BS342+9 WL208 RBL12<[01] REMOVED AND REPLACED INTERCOSTAL BS360 TO BS 344 WL208 RBL12. IAW SRM 51-40-02-0G-0 AND DWG 1541A5400 REV:-;[02] REMOVED AND REPLACED INTERCOSTAL BS360 TO BS 344 WL208 RBL12. IAW SRM 51-40-02-0
- [SDR SWAA2024082619444](https://openairdocs.org/sdr/SWAA2024082619444.md): Angle · corroded · Jul 29, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FED LOWER SILL ANGLE HAS CORROSION; BS 312+6 AND BS 322+11; WL 208; LBL 63<[01] REMOVED AND REPLACED FED LOWER SILL ANGLE BS 312+6 AND BS 322+11; WL 208; LBL 63 IAW SRM 51-40-02-0G-0 AND DWG 141A8110.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024082618420](https://openairdocs.org/sdr/SWAA2024082618420.md): Support · corroded · Jul 28, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD. CARGO COMPARTMENT LH FLOOR TO SIDEWALL SUPPORT FRAME HAS CORROSION ON SEVERAL AREAS FROM BS 396 TO BS500I; WL 156; LBL 25.<[01] UPDATED P/N.;[02] REMOVED AND REPLACED LH FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02 AND DWG 143A7500 ID:0095 REV: -;[03] RII C
- [SDR SWAA2024082618427](https://openairdocs.org/sdr/SWAA2024082618427.md): Channel · corroded · Jul 28, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT RH FLOOR TO SIDEWALL SUPPORT FRAME HAS MULTIPLE AREAS WITH CORROSION FROM BS727F+14 TO BS767; WL156; RBL 22.<[01] REMOVED AND REPLACED ZEE CHANNEL (FLOOR TO SIDEWALL SUPPORT) LOCATED BETWEEN BS.727+4 - BS.767 RBL 20 WL.156 IAW B-737-800 S
- [SDR SWAA2024082618426](https://openairdocs.org/sdr/SWAA2024082618426.md): Support · corroded · Jul 28, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT; RH FLOOR TO SIDEWALL SUPPORT FRAME HAS CORROSION ON SEVERAL AREAS; FROM BS 727C+11 TO BS727F+14; WL 156; RBL 25.<[01] THIS TASK CARD WILL BE ACCOMPLISHED WITH THE CUSTOMER CARD # TTG8Q00UVWPF;[02] VERIFIED
- [SDR SWAA2024082618428](https://openairdocs.org/sdr/SWAA2024082618428.md): Support · corroded · Jul 28, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT LH FLOOR TO SIDEWALL SUPPORT FRAME HAS MULTIPLE AREAS WITH CORROSION FROM BS727D+10 TO BS727J+9; WL156; LBL 22.<[01] REMOVED AND REPLACED ON AFT CARGO COMPARTMENT L/H FLOOR TO SIDEWALL SUPPORT BS 727 BS 847 LBL 22 IAW SRM 51-40-02 AND DWG
- [SDR SWAA2024082618429](https://openairdocs.org/sdr/SWAA2024082618429.md): Sidewall Support · corroded · Jul 28, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT LH FLOOR TO SIDEWALL SUPPORT FRAME HAS SEVERAL AREAS WITH CORROSION FROM BS727J+9 TO BS817; WL156; LBL 22.<[01] THIS TASK CARD WILL BE ACCOMPLISHED WITH THE CUSTOMER CARD TTG8Q00UVWPP;[02] FLOOR TO SIDEWALL SUPPORT WILL BE REPLACED ON TTG
- [SDR SWAA2024082618430](https://openairdocs.org/sdr/SWAA2024082618430.md): Sidewall Support · corroded · Jul 28, 2024 · N8503A · Boeing 7378H4 · Cargo Compartments
  > AFT CARGO COMPARTMENT LH FLOOR TO SIDEWALL SUPPORT FRAME HAS CORROSION AT BS 822; WL 156; RBL 22 CORRECTION. AFT CARGO COMPARTMENT LH FLOOR TO SIDEWALL SUPPORT FRAME HAS CORROSION AT BS 822 WL 156 LBL 22.<[01] THIS TASK CARD WILL BE ACCOMPLISHED WITH THE CUSTO
- [SDR SWAA2024082618418](https://openairdocs.org/sdr/SWAA2024082618418.md): Sidewall Support · corroded · Jul 28, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD. CARGO RH FLOOR TO SIDEWALL SUPPORT FRAME HAS EVIDENCE OF CORROSION ON 3 AREAS FROM BS 396 TO BS 420; WL 156; RBL 25<[01] REMOVED AND REPLACED FWD. CARGO RH FLOOR TO SIDEWALL SUPPORT FRAME FROM BS 396 TO BS 420 IAW SRM 51-40-02 AND DWG 143A7500 REV. -;[02]
- [SDR SWAA2024082618421](https://openairdocs.org/sdr/SWAA2024082618421.md): Sidewall Support · corroded · Jul 28, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD. CARGO COMPARTMENT RH FLOOR TO SIDEWALL SUPPORT FRAME HAS CORROSION ON SEVERAL AREAS FROM BS500A TO BS500I; WL 156; RBL 25.<[01] 01 - REMOVED AND REPLACED RH FLOOR TO SIDEWALL SUPPORT BS500A TO BS500I; WL 156; RBL 25; P/N 143A7501U188 LOT: 1572559-3 IAW SR
- [SDR SWAA2024082618435](https://openairdocs.org/sdr/SWAA2024082618435.md): Sidewall Support · corroded · Jul 28, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT; RH FLOOR TO SIDEWALL SUPPORT FRAME HAS CORROSION AT BS 867+2 AND BS 867+6; WL164; RBL 21. UPDATED RIGHT LOCATION BS767+2 & BS767+6 RBL21 WL164.<[01] REMOVED AND REPLACED AT ACB FWD. SHIELD LOCATED BS.767 - BS.794.25 RBL 21 WL 160 IAW B-7
- [SDR SWAA2024082618422](https://openairdocs.org/sdr/SWAA2024082618422.md): Angle · corroded · Jul 28, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD. CARGO COMPARTMENT AFT BULKHEAD LOWER ANGLE FRAME HAS CORROSION ON SEVERAL AREAS AT BS500I; RBL24 TO LBL24; WL 156<[01] REMOVED AND REPLACED ON FWD CARGO COMPARTMENT OF AFT BULKHEAD LOWER ANGLE BS 500I RBL 24 TO LBL 24 IAW SRM 51-40-02 AND DWG 143A7902 ID:
- [SDR SWAA2024082618425](https://openairdocs.org/sdr/SWAA2024082618425.md): Door Sill · corroded · Jul 28, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT DOOR CUTOUT; LOWER MAIN SILL WEB HAS CORROSION ON MULTIPLE AREAS<[01] REMOVED AND REPLACED SUB-THRESHOLD WEB LOCATED BETWEEN BS.794.37 - BS.847 RBL 25 WL 160 IAW B-737-800 SRM 51-40-02 & DWG# 146A8340 REV: -;[02] VERIFIED CORRECTIVE ACTIO
- [SDR SWAA2024082617984](https://openairdocs.org/sdr/SWAA2024082617984.md): Shield · corroded · Jul 27, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOT WITH CORROSION ON FCB SHIELD NUTPLATES ON BS420+18; BS480+14; BS500+14 WL 156. MULTIPLE SPOT WITH CORROSION ON FCB SHIELD NUTPLATES ON BS420+18.<[01] REMOVED AND REPLACED FCB SHIELD BS420 TO BS440 IAW SRM 51-40-02 AND DWG 143A0080.;[02] VERIFIED
- [SDR SWAA2024082617983](https://openairdocs.org/sdr/SWAA2024082617983.md): Threshold Web · corroded · Jul 27, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOT WITH CORROSION ON FCB DOOR CUTOUT SURROUND SUB-THRESHOLD WEB ON BS440+9; 440+20;440+5; 460+16;460+4; RBL28; WL156.<[01] REMOVED AND INSTALL NEW THRESOLD WEB IAW SRM 51-40-02 AND DWG # 143A8330 REV: A;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 A
- [SDR SWAA2024082617272](https://openairdocs.org/sdr/SWAA2024082617272.md): Floor Panel · pulled · Jul 26, 2024 · N8503A · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE; FABRICATED NEW 231XF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.
- [SDR SWAA2024082617261](https://openairdocs.org/sdr/SWAA2024082617261.md): Floor Panel · pulled · Jul 26, 2024 · N8503A · Boeing 7378H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241E UPPER SKIN HAS AN AREA OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241E UPPER SKIN STRAND DAMAGE WAS REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024082617269](https://openairdocs.org/sdr/SWAA2024082617269.md): Floor Panel · pulled · Jul 26, 2024 · N8503A · Boeing 7378H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 222BF UPPER SKIN HAS AN AREA OF PULLED STRANDS. (MARKED)<[01] FORWARD FLOOR PANEL 222BF; UPPER SKIN AREAS OF PULLED; STRANDS WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.
- [SDR SWAA2024082617265](https://openairdocs.org/sdr/SWAA2024082617265.md): Floor Panel · broken · Jul 26, 2024 · N8503A · Boeing 7378H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221GF FWD O/B CORNER TANG IS BROKEN.<[01] FWD O/B CORNER TANG ON FWD FLOOR PANEL 221GF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.
- [SDR SWAA2024082617263](https://openairdocs.org/sdr/SWAA2024082617263.md): Floor Panel · pulled · Jul 26, 2024 · N8503A · Boeing 7378H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF 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
- [SDR SWAA2024082617273](https://openairdocs.org/sdr/SWAA2024082617273.md): Floor Panel · pulled · Jul 26, 2024 · N8503A · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241AF WAS REPLACED BY FABRICATION IAW SRM 53-00-50-2R-0 AND DRAWING 144A5810-127.;[02] JOB COMPLETE.
- [SDR SWAA2024082616738](https://openairdocs.org/sdr/SWAA2024082616738.md): Angle · cracked · Jul 25, 2024 · N8503A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > R/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED<[01] REMOVED AND REPLACED 663 VAPOR BARRIER UPPER ATTACH ANGLE IAW SRM 51-40-02; DWG 111A1000; AND DWG 111A1001.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPS 1-11

Next page: https://openairdocs.org/aircraft/N8503A/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 = 'N8503A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8503A/reports

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