# Service difficulty reports: N8510E A list on [N8510E](https://openairdocs.org/aircraft/N8510E.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 SWAA2026070718413](https://openairdocs.org/sdr/SWAA2026070718413.md): Handle · loose · Jul 4, 2026 · N8510E · Boeing 7378H4 · Passenger/Crew Doors > FWD ENTRY DOOR L1 BOTTOM DOOR HANDLE IS LOOSE, TIGHTENED FWD ENTRY DOOR BOTTOM DOOR ASSIST HANDLE IAW AMM 52-11-31-400-802 SECTION 3.G.(2). - [SDR SWAA2026070718410](https://openairdocs.org/sdr/SWAA2026070718410.md): Sign · damaged · Jul 3, 2026 · N8510E · Boeing 7378H4 · Emergency Lighting > CEILING EXIT SIGN HOUSING COMMON TO OWE ROWS FOUND DAMAGED. REMOVED AND REPLACED CEILING EXIT SIGN HOUSING COMMON TO OWE ROWS IAW AMM 33-51-01-960-802. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00-720-801 AND AMM 33-51-00-710-801. OPS CHECK AND T - [SDR SWAA2025122955539](https://openairdocs.org/sdr/SWAA2025122955539.md): Flashlight · inoperative · Dec 24, 2025 · N8510E · Boeing 7378H4 · Emergency Equipment > FWD FLIGHT ATT FLASH LIGHT INOPERATIVE. REPLACED FWD INB EMERGENCY FLASHLIGHT AND BATTERY REF 25-64-00. OPS TEST GOOD. - [SDR SWAA2025122956411](https://openairdocs.org/sdr/SWAA2025122956411.md): Battery · inoperative · Dec 24, 2025 · N8510E · Boeing 7378H4 · Emergency Equipment > FWD FLIGHT ATT FLASH LIGHT INOPERATIVE. REPLACED FWD INB EMERGENCY FLASHLIGHT AND BATTERY REF 25-64-00. OPS TEST GOOD. - [SDR SWAA2025121652148](https://openairdocs.org/sdr/SWAA2025121652148.md): Flashlight · inoperative · Dec 13, 2025 · N8510E · Boeing 7378H4 · Emergency Equipment > FLASHLIGHT AFT GALLEY F/O SIDE INOPERATIVE. OPS TESTED THE FLASHLIGHT IAW AMM 25-64-00. OPS CHECKED GOOD. COULD NOT DUPLICATE. - [SDR SWAA2025112036063](https://openairdocs.org/sdr/SWAA2025112036063.md): Support · delaminated · Nov 18, 2025 · N8510E · Boeing 7378H4 · Trailing Edge Flaps > RIGHT WING OTBD FLAP NR 7 FWD SUPPORT FAIRING HAS MULTIPLE FASTENER HOLES FIBER GLASS DELAMINATED. REPLACED RT WING OTBD FLAP NR 7 FWD SUPPORT FAIRING IAW MM 27-51-28. - [SDR SWAA2025112036061](https://openairdocs.org/sdr/SWAA2025112036061.md): Fitting · cracked · Nov 17, 2025 · N8510E · Boeing 7378H4 · Nacelle/Pylon, Main Frame > NR 2 AFT PYLON STRUT FAIRING HAS A CRACKED FITTING. REMOVED CRACKED PYLON BRACKET FITTING IAW SRM 51-40-02. LOCATED AND DRILLED NEW END FITTING ASSY IAW SRM 51-40-02. C/W INSPECTION OF CA NR 2. INSTALLED NEW END FITTING ASSY IAW SRM 51-40-02. - [SDR SWAA2025112033729](https://openairdocs.org/sdr/SWAA2025112033729.md): Girt Bar · out of adjust · Nov 11, 2025 · N8510E · Boeing 7378H4 · Emergency Equipment > AFT ENTRY DOOR SLIDE GIRT BAR CURTAIN CATCHES LOWER THRESHOLD DURING CLOSE. REPOSITIONED GIRT BAR CURTAIN IAW AMM 25-66-01. - [SDR SWAA2025112033199](https://openairdocs.org/sdr/SWAA2025112033199.md): Battery Pack · inoperative · Nov 9, 2025 · N8510E · Boeing 7378H4 · Emergency Lighting > RIGHT OVERWING EXITS INTERIOR EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACK FOR RIGHT OVER WING EXIT EMERGENCY LIGHTS IAW AMM 33-51-06. OPS CHECKED GOOD IAW AMM 33-51-06. - [SDR SWAA2025112033197](https://openairdocs.org/sdr/SWAA2025112033197.md): Battery Pack · inoperative · Nov 9, 2025 · N8510E · Boeing 7378H4 · Emergency Lighting > LEFT OVERWING EXITS INTERIOR EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACK FOR LEFT HAND OVER WING EXITS PER AMM 33-51-06. OPS CHECKS GOOD PER AMM 33-51-06. - [SDR SWAA2025112032160](https://openairdocs.org/sdr/SWAA2025112032160.md): Angle · cracked · Nov 6, 2025 · N8510E · Boeing 7378H4 · Trailing Edge Flaps > LEFT WING UPPER TRAILING EDGE ANGLE CRACKED INBD OF MID SPAN DEFLECTION RIB. REMOVED AND REPLACED IAW SRM 51-40-02-0G-0-B00069. INSPECTION COMPLETED ON CORRECTIVE ACTION NR 1 FOR REPLACEMENT OF ANGLE. - [SDR SWAA2025111130181](https://openairdocs.org/sdr/SWAA2025111130181.md): Attach Angle · cracked · Oct 30, 2025 · N8510E · Boeing 7378H4 · Fuselage Main, Attach Fittings > BS 663 RT VAPOR BARRIER UPPER ATTACH ANGLE AT RBL 13 COMMON TO FUEL TANK SHOWS A CRACK INDICATION. - [SDR SWAA2025112029184](https://openairdocs.org/sdr/SWAA2025112029184.md): Floor Panel · corroded · Oct 28, 2025 · N8510E · Boeing 7378H4 · Fuselage Floor Panel > FWD CARGO FLOOR PANEL 120DF HAS SURFACE CORROSION ON RT EDGE. REMOVED PANEL 120DF IAW AMM 25-52-10. INSTALLED FWD CARGO PANEL 120DF IAW AMM 25-52-10. INSTALLED FWD CARGO PANEL 120DF PER AMM 25-52-10. - [SDR SWAA2025112028595](https://openairdocs.org/sdr/SWAA2025112028595.md): Paint · degraded · Oct 25, 2025 · N8510E · Boeing 7378H4 · Wing Structure > THE LEFT WING UPPER INBD SURFACE EMERGENCY ESCAPE PATHWAY HAS HEAVILY DEGRADED PAINT. RESTORED FINISH PER AMM 51-21-97-370-802.;[02] INSPECTION C/W - [SDR SWAA2025111828605](https://openairdocs.org/sdr/SWAA2025111828605.md): Paint · degraded · Oct 25, 2025 · N8510E · Boeing 7378H4 · Placards and Markings > THE RIGHT WING UPPER INBD SURFACE EMERGENCY ESCAPE PATHWAY HAS DEGRADED PAINT. RESTORED OVERWING EMERGENCY WALKWAY COATING AS REQUIRED PER AMM 51-21-97. - [SDR SWAA2025112027488](https://openairdocs.org/sdr/SWAA2025112027488.md): Floor Panel · pulled · Oct 23, 2025 · N8510E · Boeing 7378H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 231XF HAS FIBERS PEELING ON UPPER SURFACE. REPLACED CABIN FLOOR PANEL 231XF WITH NEW FLOOR PANEL PER AMM 53-21-00. - [SDR SWAA2025112027688](https://openairdocs.org/sdr/SWAA2025112027688.md): Seat Track · cracked · Oct 23, 2025 · N8510E · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings > FLOORBOARD SUPPORT STRUCTURE FOR PANEL 231UF LOCATED BETWEEN 0BL AND NR 3 SEAT TRACK IS CRACKED AT INBD ATTACH FASTENER. REMOVED FLOORBOARD SUPPORT STRUCTURE FOR PANEL 231UF LOCATED BETWEEN 0BL AND NR 3 SEAT TRACK PER SRM 51-40-02. INSTALLED NEW FLOORBOARD S - [SDR SWAA2025112027687](https://openairdocs.org/sdr/SWAA2025112027687.md): Seat Track · cracked · Oct 23, 2025 · N8510E · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings > FLOORBOARD SUPPORT STRUCTURE FOR PANEL 231UF LOCATED BETWEEN BL 0 AND NR 2 SEAT TRACK IS CRACKED AT INBD ATTACH FASTENER. REMOVED FLOORBOARD SUPPORT STRUCTURE FOR PANEL 231UF LOCATED BETWEEN 0BL AND NR 2 SEAT TRACK PER SRM 51-40-02. INSTALLED NEW FLOORBOARD - [SDR SWAA2025112027218](https://openairdocs.org/sdr/SWAA2025112027218.md): Attach Bracket · cracked · Oct 23, 2025 · N8510E · Boeing 7378H4 · Fuselage Main, Attach Fittings > SEAT TRACK NR 4 ATTACH BRACKET CRACKED ON BOTH INBD AND OTBD RADIUS'S AT BS 727B, UNDER FLOORBOARD 242DF. VERIFIED CRACKS IAW NDT MANUAL, PART 6, 51-00-00, PROC.23. REMOVED FASTENERS AND DISPLACED CRACKED GUSSET IAW SRM 51-40-02. REMOVED GUSSET, LOCATED, A - [SDR SWAA2025112027219](https://openairdocs.org/sdr/SWAA2025112027219.md): Attach Bracket · cracked · Oct 23, 2025 · N8510E · Boeing 7378H4 · Fuselage Main, Attach Fittings > SEAT TRACK NR 1 ATTACH BRACKET CRACKED ON BOTH INBD & OTBD. RADIUS'S AT BS 727B UNDER FLOORBOARD 241FF. VERIFIED CRACKS PER 737 NDT MANUAL PART 6; 51-00-00 PROC.23. REMOVED CRACKED GUSSET PER SRM 51-40-02. LOCATED AND DRILLED NEW GUSSET PER SRM 51-40-02. - [SDR SWAA2025111127487](https://openairdocs.org/sdr/SWAA2025111127487.md): Floor Panel · pulled · Oct 23, 2025 · N8510E · Boeing 7378H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 241AF HAS FIBERS PEELING UP ON UPPER SURFACE. - [SDR SWAA2025112027210](https://openairdocs.org/sdr/SWAA2025112027210.md): Attach Angle · cracked · Oct 22, 2025 · N8510E · Boeing 7378H4 · Fuselage Main, Attach Fittings > BS 663 RT VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT RBL 34. REMOVED FASTENERS IN THE ATTACH ANGLE AND BULKHEAD IAW SRM 51-40-02. MATCH DRILLED NEW REPLACEMENT ANGLE IAW SRM 51-40-02. INSTALLED FASTENERS IN ATTACH ANGLE IAW SRM 51-40-02 & DWG 111A1000. - [SDR SWAA2025112027211](https://openairdocs.org/sdr/SWAA2025112027211.md): Attach Angle · cracked · Oct 22, 2025 · N8510E · Boeing 7378H4 · Fuselage Main, Attach Fittings > BS 663 LT VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT LBL 34. REMOVED THE LT VAPOR BARRIER UPPER ATTACH ANGLE IAW SRM 51-40-02. C/W HFEC OF OPEN HOLES IN REPAIR AREA PER NDT PART 6 51-00-00 PROD. 16, NO DEFECTS NOTED. MATCH DRILLED NEW ANGLE IAW SRM 51-4 - [SDR SWAA2025081905322](https://openairdocs.org/sdr/SWAA2025081905322.md): Hmu · dirty · Aug 16, 2025 · N8510E · Boeing 7378H4 · Fuel Controlling System > #2 ENG NEVER REACHED TAKEOFF THRUST OF 91.2 ON TAKEOFF ROLL. DIRECTIONAL CONTROL (YAW) NOTICED ON TAKEOFF. #2 ENG LAGGED THRUST RESPONSE ON SINGLE ENGINE APPROACH.<[01] FOUND DEBRIS IN FUEL FILTER PHOTOS SENT TO POWERPLANT ENGINEERING. HMU AND FUEL PUMP ASSY R - [SDR SWAA2025081905943](https://openairdocs.org/sdr/SWAA2025081905943.md): Pump · dirty · Aug 16, 2025 · N8510E · Boeing 7378H4 · Engine Fuel Pump > #2 ENG NEVER REACHED TAKEOFF THRUST OF 91.2 ON TAKEOFF ROLL. DIRECTIONAL CONTROL (YAW) NOTICED ON TAKEOFF. #2 ENG LAGGED THRUST RESPONSE ON SINGLE ENGINE APPROACH.<[01] FOUND DEBRIS IN FUEL FILTER. HMU AND FUEL PUMP ASSY REPLACED ON TTG8Q014LMX2 - [SDR SWAA2025051971750](https://openairdocs.org/sdr/SWAA2025051971750.md): Fairing · delaminated · May 16, 2025 · N8510E · Boeing 7378H4 · Aerodynamic Fairings > LH WING TO BODY FAIRING PANEL 192CL HAS EDGE DELAMINATION LH WING TO BODY FAIRING PANEL 192CL HAS EDGE DELAMINATION AT FWD OB CORNER 2IN.X 2IN.<[01] REPAIRED PANEL PER SRM 51-70-08. - [SDR SWAA2025042326527](https://openairdocs.org/sdr/SWAA2025042326527.md): Flashlight · failed · Apr 19, 2025 · N8510E · Boeing 7378H4 · Emergency Equipment > FWD FA INBOARD FLASHLIGHT DOES NOT TEST <[01]. REPLACED FLASHLIGHT ASSY PER AMM 25-64-00 OP'S CK NORMAL. - [SDR SWAA2025031805603](https://openairdocs.org/sdr/SWAA2025031805603.md): Girt Bar · loose · Mar 15, 2025 · N8510E · Boeing 7378H4 · Emergency Equipment > FWD SERVICE DOOR GIRT BARS LOOSE <[01]. TIGHTENED AS NEEDED PER M/M SIP. - [SDR SWAA2025022097348](https://openairdocs.org/sdr/SWAA2025022097348.md): Girt Bar · out of adjust · Feb 18, 2025 · N8510E · Boeing 7378H4 · Emergency Equipment > L1 DOOR GIRT BAR RETAINER REPLACEMENT DUE TO REPORTS OF L1 DOOR GIRT BAR RETAINERS NEEDING ADJUSTMENT REPLACE BOTH RETAINERS AT NEXT OPPORTUNITY. REQUIRES P/N:65C16820-10 OR -12. ADJUSTED FWD ENTRY DOOR GIRT BAR RETAINERS IAW AMM 25-66-01. OPS CHECK GOOD. - [SDR SWAA2024112170221](https://openairdocs.org/sdr/SWAA2024112170221.md): Bracket · out of position · Nov 21, 2024 · N8510E · Boeing 7378H4 · Emergency Equipment > FWD GALLEY DOOR 2-04 DOES NOT OPEN WHEN R1 GIRT BAR IN STOWED POSITION<[01] ADJUSTED R1 GIRT BAR BRACKET PER S.I.P - [SDR SWAA2024111456624](https://openairdocs.org/sdr/SWAA2024111456624.md): Light · inoperative · Nov 5, 2024 · N8510E · Boeing 7378H4 · Emergency Lighting > LOWER EMERGENCY EXIT PROXIMITY LIGHTS AT R/H OVERWING EXIT DOORS INOP<[01] UPON FURTHER INVESTIGATION; FOUND LOWER EMERGENCY EXIT PROXIMITY LIGHTS AT R/H OVERWING EXIT DOORS CONNECTED TO WIRING FOR R/H OVERWING EXIT DOOR HEATERS. RECONNECTED CONNECTORS TO CORR - [SDR SWAA2024111456623](https://openairdocs.org/sdr/SWAA2024111456623.md): Battery Pack · inoperative · Nov 5, 2024 · N8510E · Boeing 7378H4 · Emergency Lighting > MULTIPLE EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1672 INOP<[01] DOCUMENTATION OF TROUBLESHOOTING FOR EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1672; FOUND R/H AFT SLIDE LIGHT (L733) AND R/H AFT GALLEY EXIT INDICATOR LIGHT (L1191) TO BE INOP.

ALL EMERGENCY LIGHT ASSOCIATED WITH BATTERY PACK M1671 INOP<[01] REMOVED EMERGENCY LIGHT BATTERY PACK M1671 AND INSTALLED SERVICEABLE BATTERY PACK AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. - [SDR SWAA2024111356619](https://openairdocs.org/sdr/SWAA2024111356619.md): Battery Pack · inoperative · Nov 5, 2024 · N8510E · Boeing 7378H4 · Emergency Lighting > ALL EMERGENCY LIGHT ASSOCIATED WITH BATTERY PACK M1676 INOP<[01] REMOVED EMERGENCY LIGHT BATTERY PACK M1676 AND INSTALLED SERVICEABLE BATTERY PACK AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. - [SDR SWAA2024111354286](https://openairdocs.org/sdr/SWAA2024111354286.md): Battery Pack · inoperative · Oct 28, 2024 · N8510E · Boeing 7378H4 · Emergency Lighting > PERFORM OUTBOUND EMERGENCY LIGHTS CHECK<[01] PERFORMED EMERGENCY LIGHT TEST PER AMM 33-51-00-710-801.
GENERATED CARD ID FOR DISCREPANCIES FOUND.
ALL EMERGENCY LIGHT ASSOCIATED WITH BATTERY PACK M1671 INOP TTG8Q00WV8HP
ALL EMERGENCY LIGHT ASS - [SDR SWAA2024111353604](https://openairdocs.org/sdr/SWAA2024111353604.md): Baffle · cracked · Oct 26, 2024 · N8510E · Boeing 7378H4 · Cargo Compartments > FCB BS 400 - BS 420 LBL 25. WL 155 BAFFLE CRACKED AT FWD ATTACH ANGLE<[01] REMOVED AND REPLACED BAFFLE BS 400- BS 420; LBL 25; WL 155 MADE FROM 7075-T6 X 0.020' CLAD SHEET LOT # 1540102-1 PER DWG#143A7505; DWG#143A7510 AND SRM 51-10-02-0G-0 PARAGRAPH 9.C.;[02] - [SDR SWAA2024111453080](https://openairdocs.org/sdr/SWAA2024111453080.md): Handle · out of adjust · Oct 24, 2024 · N8510E · Boeing 7378H4 · Galley Doors > FORWARD GALLEY SERVICE DOOR HANDLE HAS EXCESSIVE PLAY (MARKED.)<[01] RETORQUE HANDLE SHAFT ASSEMBLY AND SAFETIED; NO MORE PLAY NOT.
IAW AMM 52-41-11-400-801
ID: ATS2609 CAL DUE: 02/25;[02] CORRECTIVE ACTION COMPLETED. NO MORE PLAY NOTED. - [SDR SWAA2024111452734](https://openairdocs.org/sdr/SWAA2024111452734.md): Floorbeam · corroded · Oct 24, 2024 · N8510E · Boeing 7378H4 · Fuselage Main, Floor Beam > CORROSION ON FLOOR BEAM AT BS 947.5 RBL 51; WL208.1<[01] REPAIRED BS 947 FLOOR BEAM IAW SRM 53-70-51-2R-5 REPAIR-5; EA# 24-153-02977 WIP-1&2 REV-A;[02] 'REFER TO FAULT TTG8Q00WLNXF WHERE EA 24-153-02977 WAS ADDED AS A SUBTASK.';[03] VERIFIED ACTION 1;2.
JOB - [SDR SWAA2024111352870](https://openairdocs.org/sdr/SWAA2024111352870.md): Handle · out of adjust · Oct 24, 2024 · N8510E · Boeing 7378H4 · Passenger/Crew Doors > AFT ENTRY DOOR HANDLE HAS EXCESSIVE PLAY (MARKED.)< - [SDR SWAA2024111353084](https://openairdocs.org/sdr/SWAA2024111353084.md): Handle · out of adjust · Oct 24, 2024 · N8510E · Boeing 7378H4 · Passenger/Crew Doors > AFT ENTRY DOOR HANDLE HAS EXCESSIVE PLAY (MARKED.)<[01] IT WAS ADJUSTED AFT ENTRY DOOR HANDLE EXCESSIVE PLAY
IAW AMM 52-13-11-400-802;[02] CORRECTIVE ACTION STEP NO.1
UPON FURTHER EVALUATION FOUND COTTER PIN LOOSE; DISASSEMBLED AND REASSEMBLED; AFT ENTR - [SDR SWAA2024111452255](https://openairdocs.org/sdr/SWAA2024111452255.md): Attach Angle · cracked · Oct 23, 2024 · N8510E · Boeing 7378H4 · Cargo Compartments > ATTACH ANGLE CRACKED IN FCB BS400 LBL24 WL156.<[01] REMOVED AND REPLACED ATTACH CLIP P/N 143A7502-155. LOT # 1573245-1 AT STA 400; LBL 24; WL 156 PER SRM 51-40-02 AND DWG# 143A7505.;[02] CORRECTION CORRECTIVE ACTION 1.
REMOVED AND REPLACED ATTACH CLIP P/N 1 - [SDR SWAA2024111452348](https://openairdocs.org/sdr/SWAA2024111452348.md): Attach Angle · cracked · Oct 23, 2024 · N8510E · Boeing 7378H4 · Cargo Compartments > ATTACH ANGLE CRACKED IN FCB BS500G+18 RBL26 WL156.<[01] REMOVED AND REPLACED ANGLE AT FCB BS500G+18 RBL26 WL156 IAW SRM 51-40-02 AND DWG 143A7505 ID:0152 REV: -;[02] VERIFIED STEP 4 COMPLETE; CORRECTION ACTION ITEM 1; MEASUREMENT FIELD COMPLETE; CARD COMPLETE. - [SDR SWAA2024111452351](https://openairdocs.org/sdr/SWAA2024111452351.md): Attach Angle · cracked · Oct 23, 2024 · N8510E · Boeing 7378H4 · Cargo Compartments > ATTACH ANGLE CRACKED IN FCB BS500H RBL26 WL156.<[01] REMOVED AND ANGLE AT FCB BS500H RBL26 WL156 IAW SRM 51-40-02 AND DWG 143A7505 ID:0152 REV: -;[02] VERIFIED STEP 4 COMPLETE; MEASUREMENT FIELD CARD COMPLETE. - [SDR SWAA2024111452352](https://openairdocs.org/sdr/SWAA2024111452352.md): Attach Angle · cracked · Oct 23, 2024 · N8510E · Boeing 7378H4 · Cargo Compartments > ATTACH ANGLE CRACKED IN FCB BS500F+18 RBL26 WL156.<[01] REMOVED AND REPLACED ANGLE AT FCB BS500F+18 RBL26 WL156 IAW SRM 51-40-02 AND DWG 143A7505 ID:0152 REV: -;[02] VERIFIED STEP 4 CORRECTION ACTION ITEM 1; MEASUREMENT FIELD COMPLETE; CARD COMPLETE. - [SDR SWAA2024111451915](https://openairdocs.org/sdr/SWAA2024111451915.md): Sill Drain · corroded · Oct 23, 2024 · N8510E · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION ON MOP SILL (AFT SERVICE DOOR; R2) FROM BS 946 TO BS 986+5; RBL 52; WL 208.<[01] REMOVED AND REPLACED MOP SILL AT AFT SERVICE DOOR R2 PER WL 208 RBL 52 PER SRM 51-40-02 AND DWG 147A8501 REV A; DWG 147A0000 REV -;[02] VERIFIED ITEM 1 AND TASK CARD COM - [SDR SWAA2024111451916](https://openairdocs.org/sdr/SWAA2024111451916.md): Intercostal · corroded · Oct 23, 2024 · N8510E · Boeing 7378H4 · Fuselage Main, Structure > CORROSION ON INTERCOSTAL AT BS 927+19; LBL24; WL208. (MARKED)<[01] REMOVED AND REPLACED INTERCOSTAL ANGLE IAW SRM 51-40-02 &
DWG 147A5400; BS927-BS947 LBL24; WL208;[02] VERIFIED CORRECTIVE ACTION. JOB COMPLETE. - [SDR SWAA2024111452254](https://openairdocs.org/sdr/SWAA2024111452254.md): Web · corroded · Oct 23, 2024 · N8510E · Boeing 7378H4 · Fuselage Main, Structure > CORROSION ON FCB DOOR CUTOUT SURROUND SUBTHRESHOLD BS440+8 AND 480+4 RBL28;WL156<[01] REMOVED AND REPLACED FCB DOOR SUBTHRESHOLD WEB P/N 654A0003-58; LOT# 1575932-1 BS440 TO BS492 RH WL156 IAW SRM 51-40-02 AND DWG 143A8330 REV B;[02] VERIFIED ACTION ITEMS AND - [SDR SWAA2024111452361](https://openairdocs.org/sdr/SWAA2024111452361.md): Threshold · corroded · Oct 23, 2024 · N8510E · Boeing 7378H4 · Fuselage Miscellaneous Structure > MULTIPLE SPOTS OF CORROSION ON ACB DOOR CUTOUT SURROUND SUBTHRESHOLD BS787+8 TO 807+5 RBL25 WL156<[01] CORRECTED MEASUREMENT TABLE;[02] REMOVED AND REPLACED ACB DOOR SUBTHRESHOLD WEB P/N 146A8123-25; LOT# 1579502-1 BS 787+8 TO BS 847 RBL25 WL156 IAW SRM 51-40- - [SDR SWAA2024111451918](https://openairdocs.org/sdr/SWAA2024111451918.md): Floorbeam · corroded · Oct 23, 2024 · N8510E · Boeing 7378H4 · Fuselage Main, Floor Beam > CORROSION ON HARD POINT ATTACHED TO FLOOR BEAM; AT BS 947.5; RBL51; WL208.<[01] AFTER FURTHER INVESTIGATION FOUND CORROSION LOCATED ON THE UPPER FLANGE OF BS947 RBL51 FLOOR BEAM ONLY. NO CORROSION HAS BEEN FOUND ON HARDPOINT ATTACH FITTING. CORROSION ON FLOOR - [SDR SWAA2024111451917](https://openairdocs.org/sdr/SWAA2024111451917.md): Floorbeam · corroded · Oct 23, 2024 · N8510E · Boeing 7378H4 · Fuselage Main, Floor Beam > CORROSION ON FLOOR BEAM; AT BS 947.5; LBL24; WL208. (MARKED)<[01] 'REFER TO FAULT TTG8Q00WLNXF WHERE EA 24-153-02977 WAS ADDED AS A SUBTASK.' AND 'FAULT RESOLVED ON OTHER FAULT' REPAIR REFERENCE IS SELECTED.;[02] VERIFIED ACTION 1.
JOB COMPLETE. Next page: https://openairdocs.org/aircraft/N8510E/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 = 'N8510E' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N8510E/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.