# N8698B: 2016 Boeing 737-8H4 - Status: Valid registration - Airframe: [Boeing 737-8H4](https://openairdocs.org/model/boeing-737-8h4) (registry code 138440A, 143 seats) - Engine: [CFM International CFM56-7B27E/F series](https://openairdocs.org/engine/cfm-international-cfm56-7b27e-f-series) (registry code 13100) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs) - Serial number: 36977 - Year built: 2016 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 7, 2016 - Certificate issued: October 17, 2016 - Expires: October 31, 2029 - Mode S code: ABF3B8 - Registered owner: [Southwest Airlines Co](https://openairdocs.org/faa-owner/SOUTHWEST%20AIRLINES%20CO) - Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas) - Owner type: Corporation - Owner's area on the map: 32.8326° N, 96.8491° W: Placed by OpenAirDocs at the center of ZIP code 75235, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8698B - Page: https://openairdocs.org/aircraft/N8698B From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every CFM International CFM56-7B27E/F model are included. ## ADs that may apply (OpenAirDocs): 6 in force ### Matched by airframe (Boeing 737-8H4) None in force. ### Matched by engine (CFM International CFM56-7B27E/F series) - [AD 2023-05-05](https://openairdocs.org/ad/2023-05-05): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 98 more. Effective May 10, 2023 - [AD 2018-26-01](https://openairdocs.org/ad/2018-26-01): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jan 10, 2019 - [AD 2018-09-51](https://openairdocs.org/ad/2018-09-51): Engine · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 7, 2018 - [AD 2015-18-04](https://openairdocs.org/ad/2015-18-04): 73-tooth gearshaft located in the engine accessory gearbox (AGB) · CFM International CFM56-3, CFM56-7B20, CFM56-7B20/2 and 47 more. Effective Oct 20, 2015 - [AD 2015-04-02](https://openairdocs.org/ad/2015-04-02): Dual engine thrust instability event · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Mar 31, 2015 - [AD 2009-11-02](https://openairdocs.org/ad/2009-11-02): HPC 4-9 spools · CFM International CFM56-2, CFM56-2A, CFM56-2B and 109 more. Effective Jun 23, 2009 ### Historical (superseded or no longer in force) - [AD 2021-10-09](https://openairdocs.org/ad/2021-10-09) (historical): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 82 more. Effective Jun 24, 2021 - [AD 2018-18-01](https://openairdocs.org/ad/2018-18-01) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Oct 16, 2018 - [AD 2018-10-11](https://openairdocs.org/ad/2018-10-11) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 1, 2018 - [AD 2018-09-10](https://openairdocs.org/ad/2018-09-10) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective May 14, 2018 - [AD 2013-26-01](https://openairdocs.org/ad/2013-26-01) (historical): Oil dynamic seal assembly · CFM International CFM56-3, CFM56-3B, CFM56-3C and 52 more. Effective Feb 3, 2014 ## Information bulletins (advisory) (1 in force) - [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014 - [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011 ## NTSB investigations None matched to N8698B. ## FAA accident and incident reports None matched to N8698B. ## Service difficulty reports (82, newest 50) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA2026090829296](https://openairdocs.org/sdr/SWAA2026090829296), Sep 1, 2026: BULB. INOPERATIVE. EMERGENCY SIGN ON LAV D HAS INOPERATIVE BULBS. REPLACED THE BULBS AND PERFORMED GOOD FUNCTIONAL TEST IAW AMM 33-51-01-960-801. - [SDR SWAA2026090814511](https://openairdocs.org/sdr/SWAA2026090814511), Sep 1, 2026: LAMP. INOPERATIVE. EMERGENCY EXIT R/H GROUND ILLUM LIGHT INOP. REPLACED LAMP AND PERFORMED GOOD FUNCTIONAL TEST IAW AMM 33-51-04-960-801. - [SDR SWAA2026040786320](https://openairdocs.org/sdr/SWAA2026040786320), Apr 3, 2026: COVER. LOOSE. R1 SLIDE COVER APPEARS LOOSE<[01] SECURED R1 DOOR SLIDE COVER IN REFERENCE TO AMM 70-20-02. - [SDR SWAA2026032782691](https://openairdocs.org/sdr/SWAA2026032782691), Mar 24, 2026: CROSSBEAM. CRACKED. FWD CARGO BAY BS 540 AT FLOOR LEVEL AND RIGHT OF BL 0, EXPANSION JOINT BREAK PANEL ASSEMBLY CRACKED. REMOVED AND REPLACED BREAK PANEL ASSEMBLY IAW SRM 51-40-02- - [SDR SWAA2025092416430](https://openairdocs.org/sdr/SWAA2025092416430), Sep 19, 2025: NUT. CRACKED. FWD SERVICE DOOR ASSIST HANDLE NUT IS CRACKED. REMOVED AND REPLACED FWD SERVICE DOOR ASSIST HANDLE NUT IAW AMM 52-41-31. - [SDR SWAA2025092411425](https://openairdocs.org/sdr/SWAA2025092411425), Sep 5, 2025: BATTERY PACK. INOPERATIVE. RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK AT BS 659 FOUND INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW MM 33-51-06. ACCOMPLISHED OPS CHECK IAW AMM 3 - [SDR SWAA2025092411423](https://openairdocs.org/sdr/SWAA2025092411423), Sep 4, 2025: ANGLE. CRACKED. LEFT WING ANGLE ASSY INBD OF MIDFLAP DEFLECTION RIB IS CRACKED. REMOVED THE LT WING ANGLE ASSY IAW SRM 51-40-02. LOCATED AND DRILLED FASTENER HOLES IN THE NEW A - [SDR SWAA2025091609400](https://openairdocs.org/sdr/SWAA2025091609400), Aug 29, 2025: COVER. DAMAGED. LENS ASSY OVER RT AFT WING EXIT SCREW HOLE ELONGATED. REMOVED AND REPLACED LENS ASSY COVER IAW AMM 33-21-00-960-805-NG. - [SDR SWAA2025092409233](https://openairdocs.org/sdr/SWAA2025092409233), Aug 28, 2025: SEAL. CRACKED. LEFT HORIZONTAL STAB UPPER FWD SLIDING SEAL CRACKED. REMOVED AND REPLACED LT HORIZONTAL STAB UPPER FWD SLIDING SEAL IAW AMM 53-31-31. - [SDR SWAA2025092409234](https://openairdocs.org/sdr/SWAA2025092409234), Aug 28, 2025: SEAL. CRACKED. RIGHT HORIZONTAL STAB UPPER FWD SLIDING SEAL CRACKED. REMOVED AND REPLACED RT HORIZONTAL STAB UPPER FWD SLIDING SEAL IAW AMM 53-31-31. - [SDR SWAA2025092408975](https://openairdocs.org/sdr/SWAA2025092408975), Aug 27, 2025: FUEL TANK. CRACKED. BS 663 RIGHT, THE INBD FWD FUEL TANK FASTENER HOLE HAS CRACK INDICATION AT SECOND LAYER. CLEANED HOLE IAW SRM 51-10-02. PERFORMED HOLE PROBE INSPECTION IAW NDT - [SDR SWAA2025092408526](https://openairdocs.org/sdr/SWAA2025092408526), Aug 27, 2025: ANGLE. CRACKED. RIGHT WING ANGLE ASSY, INBD OF MID FLAP DEFLECTION RIB IS CRACKED. REMOVED ANGLE ASSY IAW SRM 51-40-02. LOCATED AND DRILLED FASTENER HOLES IN NEW ANGLE PER SRM - [SDR SWAA2025092408527](https://openairdocs.org/sdr/SWAA2025092408527), Aug 27, 2025: ANGLE. CRACKED. RIGHT WING CLIP BETWEEN MID FLAP DEFLECTION RIB AND ANGLE IS CRACKED. REMOVED CLIP PER SRM 51-40-02. LOCATED AND DRILLED FASTENER HOLES IN NEW CLIP PER SRM 51-4 - [SDR SWAA2025092408976](https://openairdocs.org/sdr/SWAA2025092408976), Aug 27, 2025: WEDGE. DELAMINATED. LEFT INBD T/E MAIN FLAP AFT WEDGE DELAMINATED. LOCATED AND DRILLED FASTENER HOLES IN NEW MAIN FLAP T/E WEDGE REF SRM 51-40-02-0G-0. REPLACED THE WEDGE IAW SRM 5 - [SDR SWAA2025092408973](https://openairdocs.org/sdr/SWAA2025092408973), Aug 27, 2025: WEDGE. DELAMINATED. RIGHT INBD T/E MAIN FLAP AFT WEDGE DELAMINATED. LOCATED AND DRILLED NEW WEDGE IAW SRM 51-40-02. INSTALLED NUTPLATES IAW SRM 51-40-02. INSTALLED THE NEW WEDGE 11 - [SDR SWAA2025092408416](https://openairdocs.org/sdr/SWAA2025092408416), Aug 26, 2025: CHANNEL. CRACKED. RIGHT WING TRAILING EDGE FIXED PANEL SUPPORT CHANNEL ATTACH BRACKET WAS CRACKED. REMOVED SUPPORT CHANNEL WEB IAW SRM 51-40-02. LOCATED & DRILLED FASTENER HOLES - [SDR SWAA2025092408417](https://openairdocs.org/sdr/SWAA2025092408417), Aug 26, 2025: SKIN. DELAMINATED. R WING OTBD TRAILING EDGE AFT FLAP LOWER INBD SURFACE HAS DELAMINATION. - [SDR SWAA2025092408045](https://openairdocs.org/sdr/SWAA2025092408045), Aug 25, 2025: ATTACH ANGLE. CRACKED. BS 663 VAPOR BARRIER ATTACH ANGLE HAS CRACK AT APPROXIMATELY RBL 9. REPLACED THE ATTACH ANGLE IAW SRM 51-40-02 & DWG 111A1000. - [SDR SWAA2025092408046](https://openairdocs.org/sdr/SWAA2025092408046), Aug 25, 2025: ATTACH ANGLE. CRACKED. BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT APPROXIMATELY RBL 34. REMOVED THE ATTACH ANGLE IAW SRM 51-40-02. C/W HOLE PROBE INSP IAW NDT 51-00-00, PART 6, PROC - [SDR SWAA2025092407618](https://openairdocs.org/sdr/SWAA2025092407618), Aug 24, 2025: COVER. CRACKED. OVERWING ESCAPE, LOWER BEZELS BROKEN & CRACKED AT POSITIONS RF, LF, LA. R & R BEZELS COVERS IAW SIP. - [SDR SWAA2025031704092](https://openairdocs.org/sdr/SWAA2025031704092), Mar 11, 2025: HANDLE. BROKEN. AFT SERVICE DOOR ASSIST HANDLE BROKEN<[01] R&R'D AFT SERVICE DOOR ASSIST HANDLE REF AMM 25-21-25-401-NG (AFT ENTRY AND AFT SERVICE DOORWAYS SIDEWALL LINING PANE - [SDR SWAA2024121878895](https://openairdocs.org/sdr/SWAA2024121878895), Dec 18, 2024: BATTERY PACK. INOPERATIVE. LH INTERIOR OVER WING EMERGENCY ESCAPE HATCH LIGHTS INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY M1694 PER AMM 33-51-06. - [SDR SWAA2024082828567](https://openairdocs.org/sdr/SWAA2024082828567), Aug 21, 2024: BATTERY PACK. INOPERATIVE. FWD CABIN EMERGENCY LIGHT BATTERY PACK IS INOP AT STA 500C L/H<[01] REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06;[02] INSPECTED THE WORK PERFORMED ON CORR - [SDR SWAA2024082828568](https://openairdocs.org/sdr/SWAA2024082828568), Aug 21, 2024: BATTERY PACK. INOPERATIVE. FWD CABIN EMERGENCY LIGHT BATTERY PACK INOP AT STA 500C R/H<[01] R&R BATTERY PACK AND OPS CHECK GOOD PER AMM 33-51-06;[02] INSPECTED THE WORK PERFORMED ON CORRE - [SDR SWAA2024082828569](https://openairdocs.org/sdr/SWAA2024082828569), Aug 21, 2024: BATTERY PACK. INOPERATIVE. AFT CABIN EMERGENCY LIGHT BATTERY PACK INOP AT STA 727C R/H<[01] REMOVED AND REPLACED BATTERY PACK. OPS CHK GOOD PER MM.33-51-06;[02] INSPECTED THE WORK PERFORM - [SDR SWAA2024082926891](https://openairdocs.org/sdr/SWAA2024082926891), Aug 16, 2024: FAIRING. DELAMINATED. L/H WING #3 CANOE FAIRING; AFT CONE; OUTBOARD SIDE; HAS SEVERAL AREAS OF DELAMINATION INDICATED BY BULGING FACE SHEET.<[01] REMOVED AND REPLACED THE #3 CANOE FA - [SDR SWAA2024082824241](https://openairdocs.org/sdr/SWAA2024082824241), Aug 9, 2024: ANGLE. CRACKED. FWD CARGO; FOUND CRACK ON AFT FLOOR CLIP AT STA 500H.<[01] REMOVED AND REPLACED CLIP PER SRM 51-40-02.;[02] 02 - INSPECTED PER [SRM 51-40-02-0G-0-B00069 (GENERA - [SDR SWAA2024082824240](https://openairdocs.org/sdr/SWAA2024082824240), Aug 9, 2024: ANGLE. CRACKED. FWD CARGO; FOUND CRACK ON FWD FLOOR CLIP AT STA 500H.<[01] REMOVED AND REPLACED CLIP PER SRM 51-40-02.;[02] 02 - INSPECTED PER [SRM 51-40-02-0G-0-B00069 (GENERA - [SDR SWAA2024082923292](https://openairdocs.org/sdr/SWAA2024082923292), Aug 6, 2024: SKIN. DELAMINATED. L/H O/B TRAILING EDGE FLAP I/B LOWER SURFACE IS DELAMINATED.<[01] OK TO INSTALL NEW L/H O/B AFT FLAP S/N 001118;[02] INSTALLED NEW L/H O/B AFT FLAP PER AMM 27-5 - [SDR SWAA2024082826890](https://openairdocs.org/sdr/SWAA2024082826890), Aug 6, 2024: PANEL. LOOSE. L/H SHELF PANEL LOOSE AT L/H DEFLECTION RIB<[01] REMOVED HARDWARE AND FASTENERS PER SRM 57-51-02-2R-4.;[02] REMOVED DAMAGE FROM UPPER CONTROL RIB TAB PER SRM 57 - [SDR SWAA2024082922314](https://openairdocs.org/sdr/SWAA2024082922314), Aug 3, 2024: PANEL. CRACKED. #1 ENGINE INBD FAN COWL DEFLECTOR WEB PANEL CRACKED JUST INSIDE OF OIL SERVE DOOR (MARKED)<[01] REMOVED AND REPLACED #1 ENG INBD FAN COWL PER AMM 71-11-02
RE - [SDR SWAA2024082822018](https://openairdocs.org/sdr/SWAA2024082822018), Aug 3, 2024: FLOOR SUPPORT. CORRODED. CORROSION FOUND ON INTERCOSTAL BETWEEN STA 947 TO STA 967 AT LBL 50.<[01] REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL IS OUT OF MANUAL LIMITS PER SRM 53- - [SDR SWAA2024082821571](https://openairdocs.org/sdr/SWAA2024082821571), Aug 2, 2024: MOUNT. CORRODED. THE AFT LAVATORY MOUNT STRUCTURE IS CORRODED AT STA 947 RBL 51<[01] REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-5 - [SDR SWAA2024082821572](https://openairdocs.org/sdr/SWAA2024082821572), Aug 2, 2024: MOUNT. CORRODED. THE AFT LAVATORY MOUNT STRUCTURE IS CORRODED AT STA 947 RBL 27<[01] REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-5 - [SDR SWAA2024082821577](https://openairdocs.org/sdr/SWAA2024082821577), Aug 2, 2024: STRUCTURE. CORRODED. LAV MOUNT SHOWS SIGNS OF CORROSION UNDER MOUNT AT STA 947 LBL 25<[01] FURTHER INVESTIGATION REVEALS THAT THERE IS NO CORROSION ON UNDERLYING STRUCTURE BENEATH L - [SDR SWAA2024082821998](https://openairdocs.org/sdr/SWAA2024082821998), Aug 2, 2024: FLOOR SUPPORT. CORRODED. CORROSION FOUND ON INTERCOSTAL BETWEEN STAS 947-967; RBL 50.<[01] REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51- - [SDR SWAA2024082822001](https://openairdocs.org/sdr/SWAA2024082822001), Aug 2, 2024: THRESHOLD. CORRODED. AFT CARGO DOOR THRESHOLD PLATE HAS CORROSION IN MULTIPLE LOCATIONS. REMOVED SURFACE CORROSION ON AFT CARGO DOOR THRESHOLD PLATED. MATERIAL REMOVED .020 AND REMA - [SDR SWAA2024082821578](https://openairdocs.org/sdr/SWAA2024082821578), Aug 2, 2024: MOUNT. CORRODED. THE AFT LAVATORY MOUNT STRUCTURE IS CORRODED AT STA 947 LBL 50<[01] REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL IS OUT OF MANUAL LIMITS PER SRM 53-70-51- - [SDR SWAA2024082821999](https://openairdocs.org/sdr/SWAA2024082821999), Aug 2, 2024: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT ANGLE LOCATED BETWEEN STAS 927-947; RBL 25 CORRODED.<[01] REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53- - [SDR SWAA2024082822008](https://openairdocs.org/sdr/SWAA2024082822008), Aug 2, 2024: FLOOR SUPPORT. CRACKED. FWD PASSENGER COMPARTMENT FLOOR STRUCTURE WET AREA; INTERCOSTAL UPPER ANGLE HAS 2EA CRACKS AT FLOOR PANEL ATTACH HOLES STA. 380+7' AND STA. 380+14' LBL 13.<[01] - [SDR SWAA2024082822012](https://openairdocs.org/sdr/SWAA2024082822012), Aug 2, 2024: FLOORBEAM. CORRODED. FWD PASSENGER COMPARTMENT FLOOR STRUCTURE WET AREA; FLOOR BEAM UPPER SURFACE HAS CORROSION AT FLOOR PANEL ATTACH HOLE STA. 328 RBL 39.<[01] REMOVED CORROSION. O - [SDR SWAA2024082821854](https://openairdocs.org/sdr/SWAA2024082821854), Aug 2, 2024: PANEL. DELAMINATED. WING TO BODY FAIRING 191FR HAS DELAMINATION AT FWD LOWER CORNER<[01] DAMAGE REMOVAL ACCOMPLISHED FOR LAY UP OF REPAIR PLIES IAW SRM 51-70-05-2R-10 REPAIR #10.;[ - [SDR SWAA2024082821324](https://openairdocs.org/sdr/SWAA2024082821324), Aug 1, 2024: PLATE. CORRODED. FWD CARGO R/H SIDEPLATE HAS CORROSION RBL 24; STA. 500B-500C<[01] BLENDED AREAS; REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] T - [SDR SWAA2024082821325](https://openairdocs.org/sdr/SWAA2024082821325), Aug 1, 2024: PLATE. CORRODED. FWD CARGO R/H SIDEPLATE HAS CORROSION RBL 24; STA. 500C-500D<[01] BLENDED AREAS; REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] T - [SDR SWAA2024082821326](https://openairdocs.org/sdr/SWAA2024082821326), Aug 1, 2024: PLATE. CORRODED. FWD CARGO R/H SIDEPLATE HAS CORROSION RBL 24; STA. 500D-500E<[01] BLENDED AREAS; REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] TH - [SDR SWAA2024082821317](https://openairdocs.org/sdr/SWAA2024082821317), Aug 1, 2024: PLATE. CORRODED. FWD CARGO R/H SIDEPLATE HAS CORROSION RBL 24; STA. 500F-500G<[01] BLENDED AREAS; REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] T - [SDR SWAA2024082821328](https://openairdocs.org/sdr/SWAA2024082821328), Aug 1, 2024: PLATE. CORRODED. FWD CARGO R/H SIDEPLATE HAS CORROSION RBL 24; STA. 500H-500I<[01] BLENDED AREAS; REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] T - [SDR SWAA2024082821319](https://openairdocs.org/sdr/SWAA2024082821319), Aug 1, 2024: ANGLE. CORRODED. FWD CARGO L/H SIDEPLATE HAS CORROSION LBL 24; STA. 500C-500D<[01] REMOVED SURFACE CORROSION AT L/H TRANSITION ANGLE FROM STA. 500C-500D PER SRM 51-10-02; FOUND - [SDR SWAA2024082821322](https://openairdocs.org/sdr/SWAA2024082821322), Aug 1, 2024: ANGLE. CORRODED. FWD CARGO L/H SIDEPLATE HAS CORROSION LBL 24; STA. 500B-500C<[01] REMOVED SURFACE CORROSION AT L/H TRANSITION ANGLE FROM STA. 500B-500C PER SRM 51-10-02; FOUND - [SDR SWAA2024082821331](https://openairdocs.org/sdr/SWAA2024082821331), Aug 1, 2024: ANGLE. CORRODED. FWD CARGO L/H SIDEPLATE HAS CORROSION LBL 24; STA. 500A-500B<[01] REMOVED SURFACE CORROSION AT L/H TRANSITION ANGLE FROM STA. 500B-500C PER SRM 51-10-02; FOUND All 82: https://openairdocs.org/aircraft/N8698B/reports.md ## STCs that may be installed (OpenAirDocs) (31) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Boeing 737-8H4) - [STC ST00555AT](https://openairdocs.org/stc/ST00555AT): Installation of Airshow 210 system. AIRCRAFT RECONFIG TECHNOLOGIES, LLC. Lists 737 Series - [STC SA4842SW](https://openairdocs.org/stc/SA4842SW): Modification of air to air heat exchanger (P/N 182820-2 Series 2). Honeywell International Inc. Lists 737 Series - [STC SA270NW](https://openairdocs.org/stc/SA270NW): Installation of modified seat. Aviation Technical Services. Lists 737 Series - [STC ST01162NY](https://openairdocs.org/stc/ST01162NY): Installation of Literature Pockets. Magee Plastics Company. Lists 737 Series - [STC SA2607SO](https://openairdocs.org/stc/SA2607SO): Installation of coffee maker P/N 416-1001-29. B/E Aerospace Inc. Lists 737 Series - [STC SA2608SO](https://openairdocs.org/stc/SA2608SO): Installation of rail assembly, P/N 416-0201-15. B/E Aerospace Inc. Lists 737 Series - [STC SA3058SO](https://openairdocs.org/stc/SA3058SO): Installation of coffee maker 416-0001-23 and rail assembly 416-0201-5. B/E Aerospace Inc. Lists 737 Series - [STC ST01476AT](https://openairdocs.org/stc/ST01476AT): Installation of coffee maker. B/E Aerospace Inc. Lists 737 Series - [STC ST01778AT](https://openairdocs.org/stc/ST01778AT): Installation of espresso maker p/n 3510-0066-01. B/E Aerospace Inc. Lists 737 Series - [STC SA629GL](https://openairdocs.org/stc/SA629GL): Installation of Grimes galley, Model 1545LW unit 2 and unit 4. B/E Aerospace. Lists 737 Series - [STC ST01332AT](https://openairdocs.org/stc/ST01332AT): Installation of Galley Service Carts. Champ International, Inc. Lists 737 Series - [STC ST09870SC](https://openairdocs.org/stc/ST09870SC): Installation of Mechanical Window Shades. Lou Martin & Associates. Lists 737 Series - [STC ST00033AT](https://openairdocs.org/stc/ST00033AT): Installation of a single Mode S system and provisions for a TCAS II system. General Aerospace, Inc. Lists 737 Series - [STC SA4532NM](https://openairdocs.org/stc/SA4532NM): Installation of Coltech, CTD-80 ATSCALL, enabling company calling of selected aircraft via company selected radio. Avtech Corporation. Lists 737 Series - [STC ST4532NM](https://openairdocs.org/stc/ST4532NM): Installation of Coltech CTD-80 ATSCALL, enabling company calling of selected aircraft via company selected radio. Avtech Corporation. Lists 737 Series - [STC ST00774NY](https://openairdocs.org/stc/ST00774NY): Installation of a passenger cabin Liquor/beverage service cart P/N E500170. (757-222) (767-222) (727-222) (737 SERIES 222, 291, 322, 522) (747-100 SERIES 238B). Driessen Aircraft Interior Systems USA, Inc. Lists 737 Series - [STC ST02052AT](https://openairdocs.org/stc/ST02052AT): Installation of a single Collins GNLU910A flight management system, along with global navigation satellite system sensor. General Aerospace, Inc. Lists 737 Series - [STC SA02034AT](https://openairdocs.org/stc/SA02034AT): Manufacture of tray carrier, P/N 2282-506. BFE Services. Lists 737 Series - [STC ST01968AT](https://openairdocs.org/stc/ST01968AT): Manufacture of inserts for galley stowage. JK Aerospace, Inc. Lists 737 Series - [STC SA01916AT](https://openairdocs.org/stc/SA01916AT): Manufacture of Tray Carrier P/N 1839-501. BFE Services. Lists 737 Series - [STC SA2534SO](https://openairdocs.org/stc/SA2534SO): Installation of window shades, acoustic panes and reveals. Magee Plastics Company. Lists 737 Series - [STC ST179CH](https://openairdocs.org/stc/ST179CH): Installation of cargo container curtain. Plastic Composites Corp. Lists 737 Series - [STC SA00056LA](https://openairdocs.org/stc/SA00056LA): Installation of Weber Coffeemaker, P/N 870130-415. Monogram Systems. Lists 737 Series - [STC SA6090NM](https://openairdocs.org/stc/SA6090NM): Installation of emergency vision assurance system (EVAS). VisionSafe Corporation. Lists 737 Series - [STC SA370NW](https://openairdocs.org/stc/SA370NW): Removal of passenger interior, installation of cargo compartment liners and cargo tie down equipment. Western Metal Products. Lists 737 Series - [STC SA2589CE](https://openairdocs.org/stc/SA2589CE): Install Bennetts Seat Converter Stowage Compartment on passenger seat(s). John's Aircraft and Upholstery. Lists 737 Series - [STC SA1029NW](https://openairdocs.org/stc/SA1029NW): Installation of a cargo system. Western Metal Products. Lists 737 Series - [STC SA1258EA](https://openairdocs.org/stc/SA1258EA): Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584). Miller Stuart R. Lists 737 Series - [STC SA1052SO](https://openairdocs.org/stc/SA1052SO): Installation of GE battery P/N43B022RB36 in place of Marathon P/N CA-727-7, CA-727-20, or CA-27-20 batteries or SAFT P/N23180 batteries; or installation of GE battery P/N 43B020RB10 replacing Marathon P/N CA-727-7, CA-727-20 or CA-27-20 or SAFT P/N 23186 or 23180 batteries. General Electric Company. Lists 737 Series - [STC SA1082NW](https://openairdocs.org/stc/SA1082NW) (historical): Installation of auxiliary fuel tanks in the aft cargo compartment. (737 series -2K9A). Rogerson ATS. Lists 737 Series ### Approved for the engine (CFM International CFM56-7B27E/F series) - [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC ## Earlier aircraft with N8698B The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8698B before. - [Cancelled 1975-12-10](https://openairdocs.org/deregistered/N8698B-1975-12-10): Cessna 172, S/N 36398. Exported to Canada. Owner: [Wooden Shoe Aviation Inc](https://openairdocs.org/faa-owner/WOODEN%20SHOE%20AVIATION%20INC) ## Related - Other Boeing 737-8H4 aircraft: https://openairdocs.org/model/boeing-737-8h4/aircraft.md - The CFM International CFM56-7B27E/F series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b27e-f-series.md --- 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.