# Service difficulty reports: N8513F A list on [N8513F](https://openairdocs.org/aircraft/N8513F.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 3 · 118 reports - [SDR SWAA2026083140674](https://openairdocs.org/sdr/SWAA2026083140674.md): Nut · loose · Aug 26, 2026 · N8513F · Boeing 7378H4 · Passenger/Crew Doors > FORWARD ENTRY DOOR LINER ASSIST HANDLE IS LOOSE TIGHTENED FOWARD ENTRY DOOR ASSIST HANDLE NUTS IAW AMM 52-11-31-400-802 STEP 3. G. (2) (D). - [SDR SWAA2026051196766](https://openairdocs.org/sdr/SWAA2026051196766.md): Unknown · odor · May 8, 2026 · N8513F · Boeing 7378H4 · Air Distribution System > STRONG CHEMICAL /FUME/NAUSEATING SMELL DURING T/O DISSIPATED DURING CLIMB ABOVE 10000 STARTED AGAIN DURING APPROACH AND LANDING<[01] PERF CONDITIONAL INSP IAW AMM 05-51-56; NO SMELLS OR DEFECTS NOTED; OK FOR SERVICE - [SDR SWAA2026022774330](https://openairdocs.org/sdr/SWAA2026022774330.md): Lens · damaged · Feb 25, 2026 · N8513F · Boeing 7378H4 · Emergency Lighting > R & R SMALL RECTANGLE OVERWING EXIT LIGHT LENS ASSY PER 33-51-01. REMOVED AND REPLACED EMERGENCY EXIT LIGHT AT FWD LEFT EMERGENCY EXIT ROW FLOOR IAW AMM33-51-01. OPS CHECKED GOOD. - [SDR SWAA2026022674322](https://openairdocs.org/sdr/SWAA2026022674322.md): Lens · detached · Feb 25, 2026 · N8513F · Boeing 7378H4 · Emergency Lighting > EMERGENCY EXIT LIGHT LENS FELL OFF AT ROW 14ABC. REINSTALLED LIGHT LENS AT ROW 14ABC PER AMM 33-51-01. - [SDR SWAA2026022473468](https://openairdocs.org/sdr/SWAA2026022473468.md): Megaphone · inoperative · Feb 23, 2026 · N8513F · Boeing 7378H4 · Emergency Equipment > FORWARD MEGAPHONE INOPERATIVE. REMOVED AND REPLACED FORWARD MEGAPHONE IAW AMM 25-64-00. OPS CHECKED GOOD. - [SDR SWAA2026011460904](https://openairdocs.org/sdr/SWAA2026011460904.md): Flashlight · inoperative · Jan 12, 2026 · N8513F · Boeing 7378H4 · Emergency Equipment > FWD GALLEY EMERGENCY FLASHLIGHT SEAL IS BROKEN AND FLASHLIGHT IS DEAD. R & R FWD GALLEY EMERGENCY FLASHLIGHT SEAL AND SECURED THE FLASHLIGHT IAW AMM 25-64-00; OPS CHECKED GOOD. - [SDR SWAA2026010758066](https://openairdocs.org/sdr/SWAA2026010758066.md): Battery Pack · inoperative · Jan 4, 2026 · N8513F · Boeing 7378H4 · Emergency Lighting > AFT LT EMERGENCY EXIT LIGHTS INOPERATIVE. R & R AFT LT EMERGENCY EXIT POWER SUPPLY CHARGER ASSY AND BATTERY PACK IAW AMM 33-51-06. - [SDR SWAA2026010759156](https://openairdocs.org/sdr/SWAA2026010759156.md): Power Supply · inoperative · Jan 4, 2026 · N8513F · Boeing 7378H4 · Emergency Lighting > AFT LT EMERGENCY EXIT LIGHTS INOPERATIVE. R & R AFT LT EMERGENCY EXIT POWER SUPPLY CHARGER ASSY AND BATTERY PACK IAW AMM 33-51-06. - [SDR SWAA2026010557554](https://openairdocs.org/sdr/SWAA2026010557554.md): Battery Pack · faulted · Jan 2, 2026 · N8513F · Boeing 7378H4 · Emergency Lighting > LEFT EMERGENCY LIGHTING CHARGER C/B POPPED. P18-3 (A10). R & R LEFT EMERGENCY LIGHTING BATTERY PACK AND CHARGER PER 33-51-06. - [SDR SWAA2026010558360](https://openairdocs.org/sdr/SWAA2026010558360.md): Charger · faulted · Jan 2, 2026 · N8513F · Boeing 7378H4 · Emergency Lighting > LEFT EMERGENCY LIGHTING CHARGER C/B POPPED. P18-3 (A10). R & R LEFT EMERGENCY LIGHTING BATTERY PACK AND CHARGER PER 33-51-06. - [SDR SWAA2025120140303](https://openairdocs.org/sdr/SWAA2025120140303.md): Proximity Sensor · faulted · Nov 27, 2025 · N8513F · Boeing 7378H4 · Leading Edge Slat Position Indicating System > LEADING EDGE DEVICE EXTENDED ON ITS OWN AT FL 370 MACH.79. PERFORMED LEADING EDGE FLAP/SLAT OPS TEST IAW 27-88-00-700-801; ALSO TASK 27-81-00-803 FLAP/SLAT TEST NOTE NR 1 KRUGER RETRACT SENSOR R & R. - [SDR SWAA2025102225760](https://openairdocs.org/sdr/SWAA2025102225760.md): Battery · no test · Oct 19, 2025 · N8513F · Boeing 7378H4 · Emergency Equipment > AFT CAPTAIN SIDE FLIGHT ATTENDANT FLASHLIGHT TEST FAILED. REMOVED AND REPLACED AFT LT OTBD FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECK GOOD AT THIS TIME. - [SDR SWAA2025102021958](https://openairdocs.org/sdr/SWAA2025102021958.md): Battery · inoperative · Oct 6, 2025 · N8513F · Boeing 7378H4 · Emergency Lighting > LEFT OVERWING DOOR; EMERGENCY LIGHT FWD AND AFT ARE INOP LEFT OVERWING DOOR EMERGENCY LIGHT FWD AND AFT ARE INOP. REPLACED M1670 EMERGENCY BATTERY AND TESTED IAW AMM 33-51-06-960-805, NO DEFECTS NOTED. DADO PANEL SPRING CLIP HOLDER AT THIS LOCATION DAMAGED - [SDR SWAA2025101621957](https://openairdocs.org/sdr/SWAA2025101621957.md): Battery Pack · inoperative · Oct 6, 2025 · N8513F · Boeing 7378H4 · Emergency Lighting > ONLY ONE AISLE LIGHT ON THE LEFT SIDE IS OPERATIVE. REPLACED M2335 EMERGENCY BATTERY AND TESTED PER AMM 33-51-06-960-805; NO DEFECTS NOTED. DADO PANEL SPRING CLIP HOLDER AT THIS LOCATION DAMAGED; PREVENTING REINSTALLATION OF PANEL. DEFECT TTG8Q015M2AE GENERAT - [SDR SWAA2025101621956](https://openairdocs.org/sdr/SWAA2025101621956.md): Lamp · inoperative · Oct 6, 2025 · N8513F · Boeing 7378H4 · Emergency Lighting > LEFT SIDE AFT ESCAPE EMERGENCY LIGHT (L732) IS INOPERATIVE. REPLACED THE LAMP LT AFT ESCAPE EMERGENCY LIGHT IAW AMM 33-51-04-960-801 AND PERFORMED GOOD EMERGENCY LIGHT TEST IAW AMM 33-51-00-710-801. - [SDR SWAA2025102020310](https://openairdocs.org/sdr/SWAA2025102020310.md): Attach Angle · cracked · Oct 1, 2025 · N8513F · Boeing 7378H4 · Fuselage Main, Attach Fittings > BS 663 VAPOR BARRIER FOUND ATTACH ANGLE CRACKED AT LBL9. REPAIRED PER SRM 53-10-10-2R-5 REPAIR-5. - [SDR SWAA2025102020308](https://openairdocs.org/sdr/SWAA2025102020308.md): Attach Angle · cracked · Oct 1, 2025 · N8513F · Boeing 7378H4 · Fuselage Main, Attach Fittings > BS 663 VAPOR BARRIER FOUND ATTACH ANGLE CRACKED AT RBL 34 APPROX. ATTACH ANGLE CRACKED AT RBL 34 APPROX. WAS REPAIRED BY REPLACEMENT ON TASK CARD TTG8Q015GJUC; IAW SRM 51-10-02-0G-0; PAR 9. - [SDR SWAA2025102020309](https://openairdocs.org/sdr/SWAA2025102020309.md): Attach Angle · cracked · Oct 1, 2025 · N8513F · Boeing 7378H4 · Fuselage Main, Attach Fittings > BS 663 VAPOR BARRIER FOUND ATTACH ANGLE CRACKED AT RBL9 APPROX. MARKED<[01] REMOVED AND REPLACED VAPOR BARRIER UPPER ATTACH ANGLE AT BS 663 IAW SRM 51-40-02; DGW: 111A100 ID:0359 REV: - AND DWG:111A1000 ID: 0361 REV: B;[02] VERIFIED COMPLETION CORRECTIVE ACTIO - [SDR SWAA2025102019449](https://openairdocs.org/sdr/SWAA2025102019449.md): Handle · loose · Sep 29, 2025 · N8513F · Boeing 7378H4 · Passenger/Crew Doors > FORWARD ENTRY DOOR LINING UPPER AND LOWER ASSIST HANDLE ARE LOOSE. TIGHTENED FORWARD ENTRY DOOR LINING UPPER AND LOWER ASSIST HANDLES IAW AMM 52-11-31-400-802 STEP G. (2). - [SDR SWAA2025102019450](https://openairdocs.org/sdr/SWAA2025102019450.md): Floorbeam · cracked · Sep 29, 2025 · N8513F · Boeing 7378H4 · Fuselage Main, Floor Beam > FLOORBEAM AT BS540 FROM BL0-LBL24; WL208 IS CRACKED. REMOVED AND REPLACED IAW SRM 51-40-02-0G-0 AND DWG 143A0060 REV: -. - [SDR SWAA2025102019451](https://openairdocs.org/sdr/SWAA2025102019451.md): Floorbeam · cracked · Sep 29, 2025 · N8513F · Boeing 7378H4 · Fuselage Main, Floor Beam > FLOORBEAM AT BS540 FROM BL0-RBL24; WL208 IS CRACKED<[01] REMOVED AND REPLACED IAW SRM 51-40-02-0G-0 AND DWG 143A0060 REV: -. - [SDR SWAA2025102019291](https://openairdocs.org/sdr/SWAA2025102019291.md): Skin · delaminated · Sep 29, 2025 · N8513F · Boeing 7378H4 · Trailing Edge Flaps > RT WING OTBD AFT FLAP HAS DELAMINATION ON THE UPPER SURFACE 4' FROM THE INBOARD END NEAR THE TRAILING EDGE. RT OTBD AFT FLAP WAS REMOVED ALONG WITH FLAP ASSY AND SERVICABLE RT OTBD AFT FLAP WITH FLAP ASSY WAS INSTALLED ON FAULT TTG8Q015LVFW. - [SDR SWAA2025102019084](https://openairdocs.org/sdr/SWAA2025102019084.md): Skin · pulled · Sep 28, 2025 · N8513F · Boeing 7378H4 · Nacelle/Pylon, Plate/Skin > LEFT INLET COWL OUTER LIP SKIN HAS 3 PULLED THROUGH RIVETS AT 10 O'CLOCK. REMOVED AND REPLACED FASTENERS ON LEFT INLET COWL OUTER LIP SKIN PER REF SRM 54-10-01-1A-2. - [SDR SWAA2025082607769](https://openairdocs.org/sdr/SWAA2025082607769.md): Flashlight · inoperative · Aug 23, 2025 · N8513F · Boeing 7378H4 · Emergency Equipment > AFT LEFT FLASHLIGHT INOPERATIVE. PERFORMED FLASHLIGHT CHECK PER AMM 25-64-00. PROPERLY INSTALLED FLASHLIGHT IN HOLDER. OPS CK NORMAL. - [SDR SWAA2025081300209](https://openairdocs.org/sdr/SWAA2025081300209.md): Flashlight · failed · Aug 10, 2025 · N8513F · Boeing 7378H4 · Emergency Equipment > AFT CABIN FLASHLIGHT WON'T TEST. SECURED AFT FLASHLIGHT AS PER AMM 25-64-00.OPS CK OK. - [SDR SWAA2025052775039](https://openairdocs.org/sdr/SWAA2025052775039.md): Lens · missing · May 24, 2025 · N8513F · Boeing 7378H4 · Emergency Lighting > L/H EXIT ROW SIGH/LIGHT LENS MISSING. REPLACED LENS IAW AMM 33-51-03. - [SDR SWAA2025051972738](https://openairdocs.org/sdr/SWAA2025051972738.md): Compressor · stalled · May 15, 2025 · N8513F · Boeing 7378H4 · Turbine Engine Compressor Section > AT 800 ON TAKEOFF # 1 ENGINE COMPRESSOR STALLED EGT GAUGE MOMENTARILY FLASHED RED THEN IMMEDIATELY RETURNED TO NORMAL.<[01] PERFORMED #1 ENG HPT AND STAGE 1 LPT BORESCOPE INSPECTION PER AMM 72-00-00. REF NON ROUTINE TTG8Q010JFTL FOR LPT GUIDE VANE DAMAGE;[02] - [SDR SWAA2024112671062](https://openairdocs.org/sdr/SWAA2024112671062.md): Flashlight · inoperative · Nov 23, 2024 · N8513F · Boeing 7378H4 · Emergency Equipment > FWD FA FLASHLIGHT INOPL<[01] R+R FWD INBD FA FLASHLIGHT ASSY PER AMM SIP. CKS OK. - [SDR SWAA2024111258028](https://openairdocs.org/sdr/SWAA2024111258028.md): Flashlight · no test · Nov 8, 2024 · N8513F · Boeing 7378H4 · Emergency Equipment > AFT FLASHLIGHT DOES NOT TEST<[01] RESECURED FLASHLIGHT IN MOUNT TEST GOOD REF MM 25-64-00 - [SDR SWAA2024102952303](https://openairdocs.org/sdr/SWAA2024102952303.md): Battery Pack · inoperative · Oct 24, 2024 · N8513F · Boeing 7378H4 · Emergency Lighting > EMERGENCY EXIT LIGHTS ASSOCIATED TO BATTERY PACK M1671 INOP<[01] REMOVED; REPLACED AND PERFORMED GOOD INSTALLATION TEST OF M1671 EMERGENCY BATTERY PACK AS DOCUMENTED ON ATTACHED STEPS.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE. - [SDR SWAA2024102952304](https://openairdocs.org/sdr/SWAA2024102952304.md): Battery Pack · inoperative · Oct 24, 2024 · N8513F · Boeing 7378H4 · Emergency Lighting > EMERGENCY EXIT LIGHTS ASSOCIATED TO BATTERY PACK M1676 INOP<[01] REMOVED; REPLACED AND PERFORMED GOOD INSTALLATION TEST OF M1676 EMERGENCY BATTERY PACK AS DOCUMENTED ON ATTACHED STEPS.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE. - [SDR SWAA2024102951765](https://openairdocs.org/sdr/SWAA2024102951765.md): Battery Pack · no test · Oct 22, 2024 · N8513F · Boeing 7378H4 · Emergency Lighting > EMERGENCY LIGHTS RELATED TO BATTERY PACK M1695 FAIL TEST<[01] REMOVED; REPLACED AND PERFORMED GOOD INSTALLATION TEST OF M1695 EMERGENCY BATTERY PACK AND RELAMPED INOP BULBS IN LOCATOR L1188 AS DOCUMENTED ON ATTACHED STEPS.;[02] VERIFIED COMPLETION CORRECTIVE A - [SDR SWAA2024102954526](https://openairdocs.org/sdr/SWAA2024102954526.md): Bulb · no test · Oct 22, 2024 · N8513F · Boeing 7378H4 · Emergency Lighting > EMERGENCY LIGHTS RELATED TO BATTERY PACK M1695 FAIL TEST<[01] REMOVED; REPLACED AND PERFORMED GOOD INSTALLATION TEST OF M1695 EMERGENCY BATTERY PACK AND RELAMPED INOP BULBS IN LOCATOR L1188 AS DOCUMENTED ON ATTACHED STEPS.;[02] VERIFIED COMPLETION CORRECTIVE A - [SDR SWAA2024102951767](https://openairdocs.org/sdr/SWAA2024102951767.md): Battery Pack · no test · Oct 22, 2024 · N8513F · Boeing 7378H4 · Emergency Lighting > EMERGENCY LIGHTS RELATED TO BATTERY PACK M1672 FAIL TEST<[01] REMOVED; REPLACED AND PERFORMED GOOD INSTALLATION TEST OF M1672 EMERGENCY BATTERY PACK IAW AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. - [SDR SWAA2024102947282](https://openairdocs.org/sdr/SWAA2024102947282.md): Scuff Plate · cracked · Oct 11, 2024 · N8513F · Boeing 7378H4 · Fuselage Miscellaneous Structure > AFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED<[01] AFT CARGO BAY AFT CORNER SCUFF PLATE REPAIRED PER SRM 53-60-15-2R-1.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. - [SDR SWAA2024102951470](https://openairdocs.org/sdr/SWAA2024102951470.md): Panel · cracked · Oct 9, 2024 · N8513F · Boeing 7378H4 · Emergency Exits > ASD PANEL 844DZ IS CRACKED<[01] REMOVED ASD PANEL 844DZ IAW SRM 51-40-02-0G-0. INSTALLATION WILL BE PERFORMED ON WC TTG8Q00VH6SY.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE. - [SDR SWAA2024102946071](https://openairdocs.org/sdr/SWAA2024102946071.md): Floor Panel · cracked · Oct 8, 2024 · N8513F · Boeing 7378H4 · Fuselage Floor Panel > FWD FLOOR PANEL 221BF O/B AFT CORNER TANG IS CRACKED ON LOWER SKIN.<[01] FWD FLOOR PANEL 221BF O/B AFT CORNER TANG WAS CRACKED ON LOWER SKIN AND REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2024102946113](https://openairdocs.org/sdr/SWAA2024102946113.md): Floorbeam · corroded · Oct 8, 2024 · N8513F · Boeing 7378H4 · Fuselage Main, Floor Beam > CORROSION ON PASSENGER CABIN FLOOR BEAM AT BS 947 RBL 24 AND RBL 50 WL 208<[01] REMOVED AND REPAIRED DAMAGE PART OF THE BS947 UPPER CHORD FLANGE LBL60-RBL60 WL208 INCLUDED DISCREPANCY RECORD ON TTG8Q00WATV5 ALL I.A.W SRM 53-70-51-2R-5 REPAIR 5 ALTERNATIVE 1;[0 - [SDR SWAA2024102946089](https://openairdocs.org/sdr/SWAA2024102946089.md): Floor Panel · pulled · Oct 8, 2024 · N8513F · Boeing 7378H4 · Fuselage Floor Panel > FWD FLOOR PANEL 232AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 232AF 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] JOB COMPLETE. - [SDR SWAA2024102946097](https://openairdocs.org/sdr/SWAA2024102946097.md): Shield · corroded · Oct 8, 2024 · N8513F · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION FWD CARGO BAY AFT SHIELD BS500+1 TO BS500+19 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] DAMAGED SHIELD REPLACED DUE NO DATA FOUND ON SRM NEW SHIELD LOCATED; DRILLED AND INSTALLED IAW SRM 51-40-02-0G-0; 51-40-05-0G-0 AND DWG 143A0080. - [SDR SWAA2024102946101](https://openairdocs.org/sdr/SWAA2024102946101.md): Shield · corroded · Oct 8, 2024 · N8513F · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] EVALUATED; REMOVED DAMAGED PART; AND LOCATED; DRILLED AND INSTALLED NEW PART AFT CARGO BAY SHIELD PER SRM 51-10-02; SRM 51-40-02-0G; SRM 51-40-05 - [SDR SWAA2024102946102](https://openairdocs.org/sdr/SWAA2024102946102.md): Support Plate · corroded · Oct 8, 2024 · N8513F · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS787 LBL22 WL156<[01] CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE FOUND TO BE OUT OF LIMITS. REMOVED; REPLACED AND INSTALLED NEW L/H - [SDR SWAA2024102946108](https://openairdocs.org/sdr/SWAA2024102946108.md): Floor Support · corroded · Oct 8, 2024 · N8513F · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTAL AT 949 LBL 25 WL 208.<[01] LOCATED AND DRILLED NEW INTERCOSTAL BS 948-BS967 LBL 25 WL208 I.A.W BOEING DWG 147A5650 REV- AND SRM 51-40-05-0G-0;REMOVED AND TO BE INSTALLED ON CCN TTG8Q00WATYP STEP 7;[02] VERIFIED ACTION ITEM 1; CARD COMP - [SDR SWAA2024102946109](https://openairdocs.org/sdr/SWAA2024102946109.md): Floor Support · corroded · Oct 8, 2024 · N8513F · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTAL AT BS 949 LBL 52 WL 208.<[01] LOCATED AND DRILLED NEW INTERCOSTAL BS 948-BS967 LBL 52 WL208 I.A.W BOEING DWG 147A5650 REV- AND SRM 51-40-05-0G-0;REMOVED AND TO BE INSTALLED ON CCN TTG8Q00WATYP STEP 7;[02] VERIFIED ACTION ITEM 1; CARD C - [SDR SWAA2024102946104](https://openairdocs.org/sdr/SWAA2024102946104.md): Floor Support · corroded · Oct 8, 2024 · N8513F · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTAL AT BS 948 RBL 24 WL208<[01] LOCATED AND DRILLED NEW INTERCOSTAL BS 948-BS967 RBL 24 WL208 I.A.W BOEING DWG 147A5650 REV- AND SRM 51-40-05-0G-0;REMOVED AND TO BE INSTALLED ON CCN TTG8Q00WATYP STEP 7;[02] VERIFIED ACTION ITEM 1; CARD COM - [SDR SWAA2024102946114](https://openairdocs.org/sdr/SWAA2024102946114.md): Web · corroded · Oct 8, 2024 · N8513F · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS794 TO BS847 RBL 26 WL156<[01] CORROSION ON AFT CARGO BAY SUB THRESHOLD WEB FOUND TO BE OUT LIMITS. REMOVED; REPLACED AND INSTALLED NEW AFT CARGO BAY SUB THRESHOLD WEB PER SRM 53 - [SDR SWAA2024102946111](https://openairdocs.org/sdr/SWAA2024102946111.md): Floor Support · corroded · Oct 8, 2024 · N8513F · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTAL AT BS 960 RBL49 WL208<[01] LOCATED AND DRILLED NEW INTERCOSTAL BS 948-BS967 RBL 49 WL208 I.A.W BOEING DWG 147A5650 REV- AND SRM 51-40-05-0G-0;REMOVED AND TO BE INSTALLED ON CCN TTG8Q00WATYP STEP 7;[02] ADDED PART;[03] VERIFIED CORRECTI - [SDR SWAA2024102946510](https://openairdocs.org/sdr/SWAA2024102946510.md): Floor Support · cracked · Oct 8, 2024 · N8513F · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED INTERCOSTAL AT FWD WET AREA BS391 BL0 WL208.<[01] ALL STEPS COMPLETED REMOVED INTERCOSTAL AT BS380-BS400 BL0 WL208 PER SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW INTERCOSTAL AT FWD WET AREA BS391 BL0 WL208. PER SRM 51-40-05 AND BOE DWG 143A5400 SHEET 52 - [SDR SWAA2024102946107](https://openairdocs.org/sdr/SWAA2024102946107.md): Floorbeam · corroded · Oct 8, 2024 · N8513F · Boeing 7378H4 · Fuselage Main, Floor Beam > CORROSION ON FLOOR BEAM AT BS 947 LBL 26 AND LBL 50 WL 208.<[01] EVALUATED CORROSION ON BS947 FLOOR BEAM LBL 26 AND LBL 50 WL 208 LOWEST REMAINING THICKNESS IS 0.145' ON LBL50 DAMAGE EXCEED LIMITS GIVEN ON SRM SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1 PAR.4.D (2)(A - [SDR SWAA2024102946507](https://openairdocs.org/sdr/SWAA2024102946507.md): Floor Support · cracked · Oct 8, 2024 · N8513F · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACKED FLOOR SUPPORT AT BS 394 LBL14 WL208<[01] REMOVED CRACKED FLOOR SUPPORT @ BS380 - BS400 LBL14 WL208 PER SRM 51-40-02-0G-0 AND LOCATED AND DRILLED NEW FLOOR SUPPORT PER DWG: 143A5400 ID: 0182 REV: - AND SRM 51-40-05 AND INSTALLED NEW FLOOR SUPPORT @ BS38 Next page: https://openairdocs.org/aircraft/N8513F/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 = 'N8513F' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N8513F/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.