# Service difficulty reports: N8318F A list on [N8318F](https://openairdocs.org/aircraft/N8318F.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 4 · 154 reports - [SDR SWAA2026100925581](https://openairdocs.org/sdr/SWAA2026100925581.md): Sign · broken · Oct 5, 2026 · N8318F · Boeing 7378H4 · Emergency Lighting > EMERGENCY EXIT SIGN BROKEN. SECURED EMERGENCY EXIT SIGN COVER IAW AMM 20-50-11. - [SDR SWAA2026091064500](https://openairdocs.org/sdr/SWAA2026091064500.md): Pump · faulty · Sep 6, 2026 · N8318F · Boeing 7378H4 · Fuel Boost Pump > WITH FUEL IN CTR TANKS AND ALL PUMPS OPERATING, RIGHT MAIN FUEL QUANTITY DECREASES. WITH X FEED, L MAIN PUMPS ON AND CENTER ON AND R MAIN OFF, R MAIN QUANTITY STABLE. SUSPECT LOW OUTPUT FROM R CTR WITH FUEL IN CTR TANKS AND ALL PUMPS OPERATING RIGHT MAIN FUE - [SDR SWAA2026050595132](https://openairdocs.org/sdr/SWAA2026050595132.md): Window · cracked · May 4, 2026 · N8318F · Boeing 7378H4 · Flight Compartment Windows > L1 WINDSHIELD CRACKED. R & R (CAPTS) L1 FLIGHT COMPARTMENT WINDOW IAW AMM 56-11-11. - [SDR SWAA2026032681084](https://openairdocs.org/sdr/SWAA2026032681084.md): Elec Connector · damaged · Mar 18, 2026 · N8318F · Boeing 7378H4 · Light System Wiring > EMERGENCY AISLE LIGHT WIRE CLOSE TO CONNETOR D14714 IS DAMAGE (STA 727D+8) MID CEILING PANEL<[01] RETERMINATED WIRES FOR EMERGENCY LIGHT CONNECTOR D14714 APOX (STA 727D+8) MID CEILING PANEL RIGHT SIDE; PER SWPM 20-63-02; WDM 33-51-14.
FUNCTIONAL TEST WILL B - [SDR SWAA2026010557035](https://openairdocs.org/sdr/SWAA2026010557035.md): Circuit Breaker · broken · Dec 30, 2025 · N8318F · Boeing 7378H4 · Light System Wiring > CIRCUIT BREAKER P6-11 A9 BROKEN. CABIN EMER LIGHTS. REMOVED AND REPLACED CIRCUIT BREAKER P6-11 A9 IAW AMM 20-60-05. - [SDR SWAA2025120943186](https://openairdocs.org/sdr/SWAA2025120943186.md): Handle · broken · Dec 5, 2025 · N8318F · Boeing 7378H4 · Service Doors > R1 DOOR CLOSING ASSIST HANDLE BROKEN., REPLACED HANDLE NUT IN REF W/ MM 52-41-31. - [SDR SWAA2025092918595](https://openairdocs.org/sdr/SWAA2025092918595.md): Ground Wire · loose · Sep 27, 2025 · N8318F · Boeing 7378H4 · Light System Wiring > AFT ENTRY DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. FOUND SHORT IN EMERGENCY LIGHT ASSY. BEGIN REMOVAL PROCCESS IAW AMM 33-51-04-960-802. COMPLIED UP TO STEP F, 2. FOUND GROUND LOOSE AT HOUSING FIXTURE. SECURED GROUND AND REASSEMBLED IAW AMM 33-51-04. OPS CHEC - [SDR SWAA2025082203763](https://openairdocs.org/sdr/SWAA2025082203763.md): Light · missing · Aug 13, 2025 · N8318F · Boeing 7378H4 · Emergency Lighting > MID CABIN OVERHEAD CEILING EXIT LIGHT ASSY IS MISSING 2X CLOSE OUT COVERS<[01] INSTALLED CLOSE OUT COVERS ON MID CABIN OVERHEAD EXIT LIGHT ASSEMBLY PER AMM 33-51-01-960-802 STEP 3.C.(10);[02] VERIFIED CORRECTIVE ACTION STEP 1. - [SDR SWAA2025061681193](https://openairdocs.org/sdr/SWAA2025061681193.md): Handle · loose · Jun 13, 2025 · N8318F · Boeing 7378H4 · Passenger/Crew Doors > FWD ENTRY DOOR L1 UPPER ASSIST HANDLE IS LOOSE. RESECURED FWD ENTRY DOOR UPPER ASSIST HANDLE REF AMM 20-50-11. - [SDR SWAA2024080621519](https://openairdocs.org/sdr/SWAA2024080621519.md): Skin · delaminated · Aug 2, 2024 · N8318F · Boeing 7378H4 · Trailing Edge Flaps > LH WING; OUTBOARD AFT FLAP; LOWER SKIN DELAMINATED. 7 1/2 INCH X 7 1/2 INCH; 5 INCHES FROM TRAILING EDGE; 6 INCHES FROM INBOARD EDGE.<[01] REPLACED LH WING; O/B AFT FLAP PER AMM 27-51-22. OPS CHECK GOOD;[02] 02 - INSPECTED PER [AMM 27-51-22-401-NG (OUTBOARD AF - [SDR SWAA2024061098184](https://openairdocs.org/sdr/SWAA2024061098184.md): Battery Pack · defective · Jun 4, 2024 · N8318F · Boeing 7378H4 · Emergency Lighting > EMERGENCY LIGHTS AT L1 DOOR DO NOT STAY 'ON' FOR MORE THAN TEN SECONDS WHEN SWITCH IS SELECTED TO ON POSITION.<[01] PERFORMED TROUBLESHOOTING OF EMERGENCY LIGHTS L1 AS PER B737 SSM 33-51-12; FOUND BATTERY PACK M1675 DEFECTIVE. REMOVED AND REPLACED EMERGENCY LI - [SDR SWAA2024061190717](https://openairdocs.org/sdr/SWAA2024061190717.md): Web · damaged · May 28, 2024 · N8318F · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure > HORIZONTAL LOWER BEAM STA 1088 HAS THE -1 REPAIR REPLACEMENT WEB WITH MULTIPLES RIVET HOLES ELONGATED. (FABRICATE NEW PART AS PER WIP)<[01] REMOVED -1 REPLACEMENT WEB AND FABRICATED NEW PER EA 24-153-01328; INSTALLATION WILL BE ACCOMPLISHED ON EA 24-153-01328 - [SDR SWAA2024061190146](https://openairdocs.org/sdr/SWAA2024061190146.md): Doubler · damaged · May 26, 2024 · N8318F · Boeing 7378H4 · Horizontal Stabilizer, Plate/Skin > HORIZONTAL LOWER BEAM STA 1088 HAS THE -2 REPAIR DOUBLER WITH FEW RIVET HOLES ELONGATED. CORRECTION TO DESCRIPTION....HORIZONTAL LOWER BEAM STA 1088 HAS THE [1] REPAIR DOUBLER WITH FEW RIVET HOLES ELONGATED.<[01] COMPLETED FABRICATION OF NEW REPAIR DOUBLER; C - [SDR SWAA2024061190147](https://openairdocs.org/sdr/SWAA2024061190147.md): Shim · damaged · May 26, 2024 · N8318F · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure > HORIZONTAL LOWER BEAM STA 1088 HAS THE -3 SHIM WITH FEW RIVET HOLES ELONGATED.<[01] COMPLETED FABRICATION OF REPAIR SHIM; MATERIAL: 0.010-INCH 2024-T3 CLAD SHEET PO#1685376 PER EA24-153-01328 WIP 2 STEP 5.
SURFACE ROUGHNESS GUAGE B/C 171854 NO CAL DUE AND T - [SDR SWAA2024060786908](https://openairdocs.org/sdr/SWAA2024060786908.md): Battery Pack · inoperative · May 17, 2024 · N8318F · Boeing 7378H4 · Emergency Lighting > SEVERAL EXTERIOR AND INTERIOR EMERGENCY LIGHTS INOPERATIVE.<[01] PERFORMED TROUBLESHOOTING EMERGENCY LIGHT AS PER REF AMM 33-50 TASK 801 FOUND BATTERY PACK M2335 AND M1673 DEFECTIVE; REPLACE BATTERY PACK M2335 AND M1673 AS PER REF AMM 33-51-06-960-805; TEST PA - [SDR SWAA2024061186485](https://openairdocs.org/sdr/SWAA2024061186485.md): Angle · cracked · May 16, 2024 · N8318F · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure > TAIL COMPT AT LOWER HORIZONTAL BEAM WEB HAS FWD END OF LWR WEB ANGLE CRACKED STA 1090 RBL 31. 8-5<[01] ACCOMPLISHED EA 24-153-01328. REF FAULT TTG8Q00TCRJG.;[02] ACCOMPLISHED EA 24-153-01328. REF FAULT TTG8Q00TCRJG. - [SDR SWAA2024061086486](https://openairdocs.org/sdr/SWAA2024061086486.md): Bracket · cracked · May 16, 2024 · N8318F · Boeing 7378H4 · Flight Compartment Equipment > SECOND OBSERVER'S SEAT ASSEMBLY STOPPER BRACKET FOR FIRST OBSERVER'S SEAT MOUNTING BRACKET IS CRACKED.<[01] REMOVED AND REPLACED SECOND OBSERVER'S SEAT ASSEMBLY STOPPER BRACKET FOR FIRST OBSERVER'S SEAT MOUNTING BRACKET AS PER B737;
SRM 51-40-02-0G-0;[02] R - [SDR SWAA2024061185895](https://openairdocs.org/sdr/SWAA2024061185895.md): Web · cracked · May 15, 2024 · N8318F · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure > ACCOMPLISH HIDDEN DAMAGE INSPECTION IN TAIL COMPARTMENT AT LWR HORIZ BEAM IN AREA AFFECTED BY BENT AND CRACKED HORIZONTAL WEB BS 1088 TO 1112 BL 0 TO RIGHT SIDE FUSELAGE SKIN INCLUDING 1088 BULKHEAD. ACCOMPLISHED A PRELIMINARY DETAIL VISUAL INSPECTION OF EXP - [SDR SWAA2024061085889](https://openairdocs.org/sdr/SWAA2024061085889.md): Beam · cracked · May 15, 2024 · N8318F · Boeing 7378H4 · Fuselage Main, Structure > LOWER HORIZONTAL BEAM WEB AT STA 1088+1' RBL 20 CRACKED<[01] SUMMARY EA 24-153-01328 HAS BEEN ISSUED. - [SDR SWAA2024061185255](https://openairdocs.org/sdr/SWAA2024061185255.md): Plate · cracked · May 13, 2024 · N8318F · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure > #1 ENGINE IB FAN COWL WITH SIDE PLATE (BETWEEN ENGINE OIL ACCESS DOOR AND AFT HOLD OPEN ROD) CRACKED. REMOVED AND REPLACED SHIELD PLATE AT #1 ENGINE IB FAN COWL AS PER SRM 51-40-02-0G.;[02] VERIFIED STEP #1 - [SDR SWAA2024060784386](https://openairdocs.org/sdr/SWAA2024060784386.md): Scuff Plate · cracked · May 10, 2024 · N8318F · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO COMPT SCUFF PLATE FWD CORNER IS CRACKED. RECEIVED AND INSTALLED SERVICEABLE FWD CORNER SCUFF PLATE IN REF WITH AMM 53-11-02/401. - [SDR SWAA2024060778429](https://openairdocs.org/sdr/SWAA2024060778429.md): Winglet · corroded · Apr 24, 2024 · N8318F · Boeing 7378H4 · Wing Main, Frame Structure > CORROSION AT RIGHT WINGLET UPPER TIP AFT EDGE.<[01] CUT OUT DAMAGED AREA WITH CORROSSION AT RIGHT WINGLET UPPER TIP AFT EDGE AS-PER SRM 57-30-01 REPAIR 6 FIG 201 DETAIL 2.TREATED PRIMED AND TOP COATED WORKED AREAS AT RIGHT WINGLET UPPER TIP AFT EDGE. AS-PER SO - [SDR SWAA2024052377743](https://openairdocs.org/sdr/SWAA2024052377743.md): Door · corroded · Apr 21, 2024 · N8318F · Boeing 7378H4 · Fluid Service Doors > CORROSION AT TOILET SERVICE DOOR 145AL BONDING FASTENER ATTACH AREA SURFACE.<[01] CORROSION FOUND OUT OF LIMITS PER SRM 52-40-01-1A-4; REPLACED AND INSTALLED NEW TOILET SERVICE DOOR PER AMM 52-49-07-000-801 AND SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1. - [SDR SWAA2024052377741](https://openairdocs.org/sdr/SWAA2024052377741.md): Hinge Fitting · corroded · Apr 21, 2024 · N8318F · Boeing 7378H4 · Fuselage, Door Hinge > TOILET SERVICE DOOR 145AL WITH CORRODED FWD AND AFT HINGE FITTINGS.<[01] ACQUIRED NEW TOILET SERVICE DOOR 145AL ON CUSTOMER TASK CARD TTG8Q00SWM0Z; FWD AND AFT HINGE FITTINGS ATTACHED ON NEW ASSEMBLY OF TOILET SERVICE DOOR. THIS TASK WILL BE ACCOMPLISHED ON TT - [SDR SWAA2024061177087](https://openairdocs.org/sdr/SWAA2024061177087.md): Floor Panel · damaged · Apr 19, 2024 · N8318F · Boeing 7378H4 · Fuselage Floor Panel > CABIN FLOOR PANEL241XF UPPER SKIN FIRST PLY TORN MISSING MATERIALIN SEVERAL AREA<[01] ACQUIRED FLOOR PANEL 241XF (PN#147A5810-18) AS PER DWG #147A5810; INSTALLATION OF FLOORBOARD 241XF WILL BE ACCOMPLISHED ON CUSTOMER TASK CARD (TTG8Q00SBRC7);[02] VERIFIED STE - [SDR SWAA2024061176250](https://openairdocs.org/sdr/SWAA2024061176250.md): Floor Panel · corroded · Apr 18, 2024 · N8318F · Boeing 7378H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 221DF WITH MULTIPLE LE INSERTS CORRODED.<[01] FAULT RESOLVED ON OTHER FAULT TTG8Q00STT09;[02] VERIFIED STEP 1 - [SDR SWAA2024060775641](https://openairdocs.org/sdr/SWAA2024060775641.md): Floor Support · cracked · Apr 17, 2024 · N8318F · Boeing 7378H4 · Fuselage Miscellaneous Structure > CABIN FLOOR STRUCTURE INTERCOASTAL CRACKED AT FASTENER HOLES BETWEEN STA 380-400 LBL 13.<[01] REMOVED AND REPLACED CRACKED INTERCOSTAL AT CABIN FLOOR STRUCTURE BETWEEN STA 380-400 LBL 13 AS PER SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1 - [SDR SWAA2024060775976](https://openairdocs.org/sdr/SWAA2024060775976.md): Attach Bracket · cracked · Apr 17, 2024 · N8318F · Boeing 7378H4 · Fuselage Main, Attach Fittings > FWD CARGO COMPT STA 500H ATTACHMENT BRACKET FROM SL 25 TO FRAME IS CRACKED.<[01] REMOVED AND REPLACED FWD CARGO COMPT STA 500H ATTACHMENT BRACKET FROM SL 25 TO FRAME IN REF WITH SRM 51-40-02-0G-0;[02] VERIFIED STEP 1. - [SDR SWAA2024060775977](https://openairdocs.org/sdr/SWAA2024060775977.md): Attach Bracket · cracked · Apr 17, 2024 · N8318F · Boeing 7378H4 · Fuselage Main, Attach Fittings > FWD CARGO COMPT STA 500G ATTACHMENT BRACKET FROM SL25 TO FRAME IS CRACKED.<[01] REMOVE AND REPLACE FWD CARGO COMPT STA 500G ATTACHMENT BRACKET FROM SL25 TO FRAME IN REF TO SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.;[03] CORRECTION: UPDATED MEASUREMENT TABLE.;[04] - [SDR SWAA2024060775978](https://openairdocs.org/sdr/SWAA2024060775978.md): Attach Bracket · cracked · Apr 17, 2024 · N8318F · Boeing 7378H4 · Fuselage Main, Attach Fittings > FWD CARGO COMPT STA 500H ATTACHMENT BRACKET FROM SR25 TO FRAME IS CRACKED.<[01] REMOVED AND REPLACED FWD CARGO COMPT STA 500H ATTACHMENT BRACKET FROM SR25 TO FRAME IN REF WITH SRM 51-40-02-0G-0;[02] VERIFIED STEP 1. - [SDR SWAA2024060775979](https://openairdocs.org/sdr/SWAA2024060775979.md): Attach Bracket · cracked · Apr 17, 2024 · N8318F · Boeing 7378H4 · Fuselage Main, Attach Fittings > FWD CARGO COMPT STA 500G ATTACHMENT BRACKET FROM SR25 TO FRAME IS CRACKED.<[01] REMOVE AND REPLACED FWD CARGO COMPT STA 500G ATTACHMENT BRACKET FROM SR25 TO FRAME REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1. - [SDR SWAA2024060775986](https://openairdocs.org/sdr/SWAA2024060775986.md): Cam · out of adjust · Apr 17, 2024 · N8318F · Boeing 7378H4 · Service Doors > R1 DOOR HANDLE BOX CAM RUBBING AGAINST INNER SKIN BOTTOM RIVET HEADS. REMOVED AND REPLACED BLIND RIVETS AT R-1 DOOR INNER SKIN IN REF B737-800 SRM 51-40-02-0G-0; BOEING DWG# 141A6516.;[02] VERIFIED STEP 1 - [SDR SWAA2024052375981](https://openairdocs.org/sdr/SWAA2024052375981.md): Cam · chafed · Apr 17, 2024 · N8318F · Boeing 7378H4 · Service Doors > R1 DOOR HANDLE BOX CAM HAS CHAFFING MARKS AT BOTTOM FACE.<[01] REMOVED AND REPLACED HANDLE BOX CAM R1 DOOR AS PER B737 AMM 52-41-11-400-801;[02] VERIFIED STEP 1 - [SDR SWAA2024061075494](https://openairdocs.org/sdr/SWAA2024061075494.md): Frame · cracked · Apr 16, 2024 · N8318F · Boeing 7378H4 · Fuselage Main, Frame > PASSENGER CABIN STA 312 WL282 LBL 33 CRACKED (ABOVE L-1 DOOR CUTOUT).<[01] ACCOMPLISHED EA M-22-153-01244(737-NG-SWA-BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33BETWEEN S-5L AND S-6L;[02] VERIFIED STEP 1 - [SDR SWAA2024061075636](https://openairdocs.org/sdr/SWAA2024061075636.md): Floor Support · cracked · Apr 16, 2024 · N8318F · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD WET AREA FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 344-360 BL 0 CRACKED AT FASTENER HOLE.<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD WET AREA BETWEEN STA 344-360 BL 0 AS-PER SRM 51-40-02-0G-0;[02] VERIFIED STEP 2 - [SDR SWAA2024061075637](https://openairdocs.org/sdr/SWAA2024061075637.md): Floor Support · cracked · Apr 16, 2024 · N8318F · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD WET AREA FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 312-328 RBL 30 CRACKED.<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD WET AREA FLOOR STRUCTURE BETWEEN STA 312-328 RBL 30 AS PER SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1 - [SDR SWAA2024060775635](https://openairdocs.org/sdr/SWAA2024060775635.md): Floor Support · cracked · Apr 16, 2024 · N8318F · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD WET AREA FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 312-328 LBL 46 CRACKED AT FASTENER HOLE.<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD WET AREA FLOOR STRUCTURE BETWEEN STA 312-328 LBL 46 AS PER SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1 - [SDR SWAA2024061174943](https://openairdocs.org/sdr/SWAA2024061174943.md): Floorbeam · corroded · Apr 15, 2024 · N8318F · Boeing 7378H4 · Fuselage Main, Floor Beam > CABIN FLOORBEAM IS CORRODED AT BS 947.15 NEXT TO LEFT AFT LAVATORY, INBOARD MOUNT. DAMAGE EVALUATION AND REPAIR OF FLOORBEAM CORROSION AT BS 947, LEFT AFT LAVATORY I/B MOUNT WILL BE ACCOMPLISHED ON CUSTOMER TASK CARD TTG8Q00SRRMT STEP 4 AND STEP 6. - [SDR SWAA2024061174940](https://openairdocs.org/sdr/SWAA2024061174940.md): Floorbeam · corroded · Apr 15, 2024 · N8318F · Boeing 7378H4 · Fuselage Main, Floor Beam > CABIN FLOORBEAM IS CORRODED AT 947.15 NEXT TO RIGHT AFT LAVATORY, INBOARD MOUNT. DAMAGE EVALUATION AND REPAIR OF FLOOR BEAM CORROSION AT STA 947; RIGHT AFT LAVATORY I/B MOUNT WILL BE ACCOMPLISHED ON CUSTOMER TASK CARD TTG8Q00SRRMT STEP 4 AND STEP 6. - [SDR SWAA2024061175114](https://openairdocs.org/sdr/SWAA2024061175114.md): Floorbeam · corroded · Apr 15, 2024 · N8318F · Boeing 7378H4 · Fuselage Main, Floor Beam > AFT PASSENGER CABIN FLOOR BEAM 947.5 CORRODED IN MULTIPLE AREAS ALONG THE FULL LENGTH OF THE BEAM<[01] ACCOMPLISHED REPAIR AT AFT PASSENGER CABIN CENTER OF FLOOR BEAM 947.5 REF SRM 53-70-51-2R-5. - [SDR SWAA2024061074942](https://openairdocs.org/sdr/SWAA2024061074942.md): Floorbeam · corroded · Apr 15, 2024 · N8318F · Boeing 7378H4 · Fuselage Main, Floor Beam > CABIN FLOOR BEAM IS CORRODED AT 947.15 NEXT TO RIGHT AFT LAVATORY; OUTBOARD MOUNT.<[01] AFTER FURTHER INSPECTION NO CORROSION WAS FOUND AT CABIN FLOOR BEAM STA 947.5 AT RIGHT AFT LAVATORY O/B MOUNT. CORROSION WAS ONLY FOUND ON ADJACENT ATTACHED INTERCOASTAL AT - [SDR SWAA2024060774693](https://openairdocs.org/sdr/SWAA2024060774693.md): Floor Support · cracked · Apr 15, 2024 · N8318F · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CABIN FLOOR SUPPORT IS CRACKED BETWEEN 276-294.5; 1 INCH RIGHT OF CENTER LINE. REMOVED AND REPLACED NEW FLOOR SUPPORT AT FWD CABIN BETWEEN STA 276-294.5 1 INCH RIGHT OF CENTER LINE AS-PER SRM 51-40-02-0G-0. - [SDR SWAA2024060774939](https://openairdocs.org/sdr/SWAA2024060774939.md): Floor Support · corroded · Apr 15, 2024 · N8318F · Boeing 7378H4 · Fuselage Miscellaneous Structure > AFT CABIN FLOOR SUPPORT BETWEEN 947.15-967 LEFT OF CENTER LINE 24 INCHES IS CORRODED. CORROSION EVALUATION AND REPLACEMENT OF FLOOR SUPPORT AT STA 947.5-967 LBL 24 WILL BE ACCOMPLISHED ON CURRENT CUSTOMER CARD TTG8Q00SRQT9; REMOVED INTERCOSTAL AT AFT CABIN BS - [SDR SWAA2024060774169](https://openairdocs.org/sdr/SWAA2024060774169.md): Skin · delaminated · Apr 12, 2024 · N8318F · Boeing 7378H4 · Leading Edge Devices > LEFT WING SLAT # 2 UPPER SURFACE O/B T/E COMPOSITE MAY BE DELAMINATED.MARKED DOT 251-002<[01] REMOVED AND INSTALLED SERVICEABLE LEFT WING SLAT #2 AS PER AMM 27-81-21-000-801 AND AMM 27-81-21-400-801.;[02] CORRECTION TO STEP 1: REMOVED AND INSTALLED SERVICEABLE - [SDR SWAA2024061073696](https://openairdocs.org/sdr/SWAA2024061073696.md): Panel · corroded · Apr 11, 2024 · N8318F · Boeing 7378H4 · Wing Main, Frame Structure > REFUEL PANEL (P15) FACE PLATE HAS SIGN OF CORROSION AROUND FUEL QTY GAUGES.<[01] REMOVED REFUEL PANEL (P15) AS PER B737 AMM TASK 28-21-00-000-801. REMOVED REFUEL QUANTITY INDICATOR AS PER B737 AMM TASK 28-41-61-000-801
REINSTALLED REFUEL QUANTITY INDICATOR - [SDR SWAA2024020749432](https://openairdocs.org/sdr/SWAA2024020749432.md): Unknown · odor · Feb 6, 2024 · N8318F · Boeing 7378H4 · Air Distribution System > CREW REPORTS BURNING PLASTIC SMELL FROM FORWARD CABIN AREA. ALL ENGINE INDICATIONS NORMAL. RETURNED TO DAL- NORMAL LANDING<[01] ACCOMPLISHED TASK 05-51-56 AND FIM 21-00 TASK 806. NO UNUSUAL ODORS NOTED. OPS AND CKS OK. - [SDR SWAA2024012544153](https://openairdocs.org/sdr/SWAA2024012544153.md): Mount · cracked · Jan 24, 2024 · N8318F · Boeing 7378H4 · Galley Doors > AFT GALLEY SERVICE DOOR LOWER LINING SUPPORT 2 EA. ISOLATOR MOUNTS DOORSIDE CRACKED.<[01] R&R AS DOOR LOWER LINING SUPPORT ISOLATOR MOUNTS PER SRM 51-40-02 - [SDR SWAA2024012444137](https://openairdocs.org/sdr/SWAA2024012444137.md): Light · cracked · Jan 24, 2024 · N8318F · Boeing 7378H4 · Emergency Lighting > PAX CABIN AISLE O/H CENTER EMERGENCY EXIT LIGHT ASSY CRACKED.<[01] R&R'D PAX CABIN AISLE O/H CENTER EMERGENCY EXIT LIGHT ASSY PER CMM 33-24-03 - [SDR SWAA2023083094460](https://openairdocs.org/sdr/SWAA2023083094460.md): Lens · loose · Aug 28, 2023 · N8318F · Boeing 7378H4 · Emergency Lighting > L-1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF.<[01] INSTALLED EXIT LENS IAW AMM 33-51-01. OPS CK GOOD - [SDR SWAA2023030712000](https://openairdocs.org/sdr/SWAA2023030712000.md): Lamp · inoperative · Mar 3, 2023 · N8318F · Boeing 7378H4 · Emergency Lighting > EMERGENCY SLIDE LIGHT AFT OF L2 DOOR INOP<[01] PERFORMED LAMP REPLACEMENT FOR EMERGENCY SLIDE LIGHT AFT OF L2 DOOR IAW AMM 33-51-04 Next page: https://openairdocs.org/aircraft/N8318F/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 = 'N8318F' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N8318F/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.