# N952WN: 2010 Boeing 737-7H4

- Status: Valid registration
- Airframe: [Boeing 737-7H4](https://openairdocs.org/model/boeing-737-7h4) (registry code 1384404, 143 seats)
- Engine: [CFM International CFM56-7B24/3 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-3-series) (registry code 13074)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 36667
- Year built: 2010
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 23, 2010
- Certificate issued: December 27, 2010
- Expires: December 31, 2029
- Mode S code: AD3E16
- 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=952WN
- Page: https://openairdocs.org/aircraft/N952WN

From the FAA registry file of October 22, 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 CFM56-7B24/3 model are included.

## ADs that may apply (OpenAirDocs): 10 in force

### Matched by airframe (Boeing 737-7H4)

None in force.

### Matched by engine (CFM International CFM56-7B24/3 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 2022-02-03](https://openairdocs.org/ad/2022-02-03): Turbine Engine Accessory Drive · CFM International CFM56-3, CFM56-3B, CFM56-3C and 34 more. Effective Mar 22, 2022
- [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 2010-13-09](https://openairdocs.org/ad/2010-13-09): Stage 3 low-pressure turbine (LPT) · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 88 more. Effective Jul 26, 2010
- [AD 2010-01-05](https://openairdocs.org/ad/2010-01-05): LP turbine rear frames · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 25 more. Effective Feb 18, 2010
- [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
- [AD 2006-26-01](https://openairdocs.org/ad/2006-26-01): Fuel filters · CFM International CFM56-2, CFM56-2A, CFM56-2B and 93 more. Effective Jan 3, 2007

### 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
- [SAIB NE-08-17R1](https://openairdocs.org/saib/NE-08-17R1) (historical): Propulsion Technology LLC Unapproved Repair. Issued May 22, 2008
- [SAIB NE-08-17](https://openairdocs.org/saib/NE-08-17) (historical): Propulsion Technologies International Unapproved Repair. Issued May 14, 2008

## NTSB investigations

None matched to N952WN.

## FAA accident and incident reports

None matched to N952WN.

## Service difficulty reports (222, 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 SWAA2026082178201](https://openairdocs.org/sdr/SWAA2026082178201), Aug 16, 2026: HANDLE. LOOSE. PAX CABIN FWD ENTRY DOOR LOWER ASSIST HANDLE LOOSE. INSTALLED THE ASSIST HANDLE CORRECTLY IAW AMM 52-11-31-400-802 STEP 3.G.(2).
- [SDR SWAA2026082179287](https://openairdocs.org/sdr/SWAA2026082179287), Jul 31, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON LEADING EDGE TIP STRUCTURE ACCESS PANEL 341B AT RT HORIZONTAL STAB. REPLACED LEADING EDGE TIP STRUCTURE LOCATED ON ACCESS PANEL 341B AT RT HO
- [SDR SWAA2026082160911](https://openairdocs.org/sdr/SWAA2026082160911), Jul 30, 2026: FRAME. CRACKED. CRACKED FRAME, OTBD FAN COWL AFT POSITION, NR 1 ENGINE. REPLACED THE FRAME & FASTENERS IAW SRM 51-40-02, AND 71-13-30, REV 34.
- [SDR SWAA2026081749181](https://openairdocs.org/sdr/SWAA2026081749181), Jul 30, 2026: STRINGER. CRACKED. CRACKED ON STRINGER 8. INTERNAL AREA FUEL TANK, RIB 19 - 20, UPPER SKIN, LOWER SURFACE AFT AREA, LT WING. IAW EA 26-157-02068, THE CONFIGURATION IS ACCEPTABLE. 
- [SDR SWAA2026081772706](https://openairdocs.org/sdr/SWAA2026081772706), Jul 24, 2026: RIB. CRACKED. CRACKED LEADING EDGE RIB ACCESS PANEL 331B, HSS 95.96, LT HORIZONTAL STAB. REPLACED RIB IAW SRM 51-10-02, ITEM 9, DWG 186A1303, SHEET 1, REV A, AND DWG 186A1001
- [SDR SWAA2026082160196](https://openairdocs.org/sdr/SWAA2026082160196), Jul 23, 2026: SUPPORT. CORRODED. CORRODED SUPPORT ZEE, BS 727 - 847, LBL 21, WL 156 (10 POINTS) IN THE AFT CARGO BAY. REPLACED SUPPORT AND FASTENERS IAW SRM 51-40-02-0G-0, DWG 146A7500, SHEET 1
- [SDR SWAA2026082174260](https://openairdocs.org/sdr/SWAA2026082174260), Jul 23, 2026: WEB. CORRODED. CORRODED WEB, BS 747 - 767, RBL 22, WL 156, IN THE AFT CARGO BAY. REPLACED THE WEB AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & DWG 146A750
- [SDR SWAA2026082196517](https://openairdocs.org/sdr/SWAA2026082196517), Jul 23, 2026: WEB. CORRODED. CORRODED SHIELD WEB BTWN BS 767 & 794.3, WL 156, & RBL 22 IN THE AFT CARGO BAY, REPLACED THE SHIELD WEB IAW SRM 51-40-02-0G, AND DWG 146A0081, SHEET 43, REV-.
- [SDR SWAA2026082142009](https://openairdocs.org/sdr/SWAA2026082142009), Jul 23, 2026: SUPPORT. CORRODED. CORRODED SUPPORT ZEE BTWN BS 727 & 767, RBL 21, WL 156. (7 POINTS) IN THE AFT CARGO BAY. REPLACED SUPPORT ZEE AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 53-00-53-
- [SDR SWAA2026082198560](https://openairdocs.org/sdr/SWAA2026082198560), Jul 23, 2026: WEB. CRACKED. CRACKED WEB, BS 927 - 947.5, STR 25R IN THE AFT CARGO BAY. REPLACED THE WEB, NUTPLATES 5(E/A) AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & 
- [SDR SWAA2026082152321](https://openairdocs.org/sdr/SWAA2026082152321), Jul 23, 2026: FITTING. CRACKED. CRACKED FITTING, BS 947.5, STR 26L. REPLACED THE FITTING IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, & DRAWING 149A8103, SHEET 8, REV -.
- [SDR SWAA2026081761813](https://openairdocs.org/sdr/SWAA2026081761813), Jul 23, 2026: SUPPORT ANGLE. CRACKED. CRACKED CARGO LINER SUPPORT ANGLE, BS 727E, LBL 51, IN THE AFT CARGO BAY. REPLACED LINER SUPPORT ANGLE IAW SRM 51-40-02-0G-0, DWG 149A9490, SHEET 21, REV-, AND 
- [SDR SWAA2026081741374](https://openairdocs.org/sdr/SWAA2026081741374), Jul 23, 2026: ANGLE. CRACKED. CRACKED ANGLE BS 867, STR 26L - 27L. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, & DWG 149A8102, SHEET 19, REV A.
- [SDR SWAA2026081734883](https://openairdocs.org/sdr/SWAA2026081734883), Jul 23, 2026: SUPPORT ANGLE. CRACKED. CRACKED CARGO LINER SUPPORT ANGLE, BS 887, RBL 53, AFT CARGO BAY. PERFORMED REPAIR ON CARGO LINER SUPPORT ANGLE IAW SRM 51-70-11-2R-0, SRM 51-10-02-0G, PARAGRAP
- [SDR SWAA2026081786862](https://openairdocs.org/sdr/SWAA2026081786862), Jul 23, 2026: SUPPORT ANGLE. CRACKED. CRACK CARGO LINER SUPPORT ANGLE, BS 727D, LBL 51 IN THE AFT CARGO BAY. FAULT RESOLVED ON OTHER FAULT DOCUMENTED ON TTG8Q01DC1BT.
- [SDR SWAA2026081787560](https://openairdocs.org/sdr/SWAA2026081787560), Jul 23, 2026: RIB. CRACKED. CRACK ACCESS PANEL 321A LEADING EDGE RIB 8 VERTICAL STABILIZER 2026-443094 REPLACED RIB ASSY 8 AND FASTENERS OF THE ACCESS PANEL 321A AT VERTICAL STABILIZER FIN
- [SDR SWAA2026081791006](https://openairdocs.org/sdr/SWAA2026081791006), Jul 23, 2026: SUPPORT ANGLE. CRACKED. CRACKED CARGO LINER SUPPORT ANGLE, BS 727B, LBL 51 IN THE AFT CARGO BAY. REPLACED THE LINER SUPPORT ANGLE IAW SRM 51-40-02-0G-0, DWG 149A9490, SHEET 21, REV-, &
- [SDR SWAA2026081769287](https://openairdocs.org/sdr/SWAA2026081769287), Jul 23, 2026: SEAL. CRACKED. CRACKED SEAL BLADE ACCESS PANEL 333AT, LT HORIZONTAL STAB. REPLACED THE SEAL BLADE ACCESS PANEL 333AT IAW SRM 51-40-02, & DWG 186A3101, SHT 19, REV -.
- [SDR SWAA2026081760834](https://openairdocs.org/sdr/SWAA2026081760834), Jul 22, 2026: LIGHT. INOPERATIVE. INOPERATIVE EMERGENCY LIGHT ON LAVATORY B. REPLACED EMERGENCY LIGHT IAW AMM 33-51-01-960-802. TESTED OK.
- [SDR SWAA2026081771897](https://openairdocs.org/sdr/SWAA2026081771897), Jul 22, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500D, STR 28L, FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A7902, SHEET 126, REV A.
- [SDR SWAA2026082134945](https://openairdocs.org/sdr/SWAA2026082134945), Jul 21, 2026: GUSSET. CRACKED. CRACKED GUSSET ANGLE, BS 500D, STR 19L IN THE FWD CARGO BAY. REPLACED THE GUSSET ANGLE AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND 
- [SDR SWAA2026081700759](https://openairdocs.org/sdr/SWAA2026081700759), Jul 21, 2026: TIE CLIP. CRACKED. CRACKED TIE CLIP, BS 500C, STR 19L IN THE FWD CARGO BAY. REPLACED THE TIE CLIP IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, & DWG 143A1224, SHT 49, RE
- [SDR SWAA2026081782335](https://openairdocs.org/sdr/SWAA2026081782335), Jul 21, 2026: GUSSET. CRACKED. CRACK GUSSET ANGLE, BS 500D, STRINGER 19R IN THE FWD CARGO BAY. REPLACED THE GUSSET ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, & D
- [SDR SWAA2026081755543](https://openairdocs.org/sdr/SWAA2026081755543), Jul 21, 2026: CROSSBEAM. CRACKED. CRACKED FLOOR BRAKE PANEL, BS 540, LBL 1 IN PAX CABIN. REPLACED THE FLOOR BRAKE PANEL IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A0060, SHEET 58, REV A.
- [SDR SWAA2026081784126](https://openairdocs.org/sdr/SWAA2026081784126), Jul 21, 2026: THRESHOLD. CRACKED. CRACKED SCUFF PLATE AFT CORNER, AFT CARGO BAY. REPAIRED AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4. B, STEPS 2 - 7, FIGURE 203.
- [SDR SWAA2026081786778](https://openairdocs.org/sdr/SWAA2026081786778), Jul 21, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 400, LBL 25 IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM-51-10-02, ITEM (9), SRM-51-40-02, & DWG:143A7505, SHEET 117, REV-.
- [SDR SWAA2026081716148](https://openairdocs.org/sdr/SWAA2026081716148), Jul 21, 2026: TIE CLIP. CRACKED. CRACK TIE-CLIP LOCATED BS500D, STR 26R IN THE FWD CARGO BAY. PERFORMED DETAIL VISUAL INSPECTION ON TIE-CLIP AND DID NOT FIND A CRACK IAW SRM 51-00-06-0G-0, & AP
- [SDR SWAA2026081769113](https://openairdocs.org/sdr/SWAA2026081769113), Jul 21, 2026: CROSSBEAM. CRACKED. CRACKED FLOOR STRUCTURE BRAKE PANEL BS 540 AND RBL 1. REPLACED FLOOR STRUCTURE BRAKE PANEL BS 540 AND RBL 1 TO RBL 24.75 IAW SRM 51-40-02, SRM 51-10-02, ITEM 9,
- [SDR SWAA2026081784221](https://openairdocs.org/sdr/SWAA2026081784221), Jul 21, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 440, LBL 21 IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A7505, SHT 118, REV-.
- [SDR SWAA2026081763623](https://openairdocs.org/sdr/SWAA2026081763623), Jul 21, 2026: WEB. CRACKED. CRACKED WEB BTW BS 500B - 500C, LBL 21 FWD CARGO BAY. REPLACED WEB BS 500B - 500C, LBL 21 IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHT 117, REV-.
- [SDR SWAA2026082131133](https://openairdocs.org/sdr/SWAA2026082131133), Jul 20, 2026: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT STRIP (5EA) LT & RT SIDES, ALONG PAX CABIN. REPLACED PHOTOLUMINESCENT STRIP (5EA) IAW AMM-33-51-15-400-802.
- [SDR SWAA2026081786772](https://openairdocs.org/sdr/SWAA2026081786772), Jul 20, 2026: GIRT BAR. WORN. DETERIORATED GIRT BAR FITTINGS HARDWARE AND PLATE ON ENTRY AND SERVICE DOORS. REPLACED THE GIRT BAR FITTINGS HARDWARE AND PLATE IAW AMM 25-66-02-000-801, AND AM
- [SDR SWAA2026081746157](https://openairdocs.org/sdr/SWAA2026081746157), Jul 20, 2026: FLOOR PANEL. ELONGATED. ELONGATED HOLES ON FLOOR PANEL 120CF IN THE FWD CARGO BAY. FABRICATED A NEW FLOOR PANEL 120CF IAW AMM 25-52-01-201-801, & DWG 453A1610, SHEET 2, REV D.
- [SDR SWAA2026081716175](https://openairdocs.org/sdr/SWAA2026081716175), Jul 20, 2026: FITTING. DETERIORATED. DETERIORATED GIRT BAR FITTINGS HARDWARE AND PLATE ON ENTRY AND SERVICE DOOR AT FWD GALLEY. REPLACED GIRT BAR FITTINGS HARDWARE AND PLATE ON ENTRY AND SERVICE DO
- [SDR SWAA2026081717544](https://openairdocs.org/sdr/SWAA2026081717544), Jul 19, 2026: PRESSURE DECK. CRACKED. CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB, LBL 31 BTWN BS 663 - 675 IN THE MAIN WHEEL WELL. PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB IAW SR
- [SDR SWAA2026081735919](https://openairdocs.org/sdr/SWAA2026081735919), Jul 19, 2026: ACCESS PANEL. CRACKED. ELONGATED HOLES ON ACCESS PANEL 561BB ON THE LT WING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2026081757257](https://openairdocs.org/sdr/SWAA2026081757257), Jul 19, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON RT WING ACCESS PANEL 661BB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2026082179296](https://openairdocs.org/sdr/SWAA2026082179296), Jul 18, 2026: LIGHT. INOPERATIVE. INOPERATIVE BULLNOSE EMERGENCY LIGHT, OVERHEAD BIN 8R IN THE PAX CABIN. REPLACED THE BULB IN THE EMERGENCY LIGHT IAW AMM 33-51-03-960-801, AND TESTED OK .
- [SDR SWAA2026081747166](https://openairdocs.org/sdr/SWAA2026081747166), Jul 18, 2026: ACCESS DOOR. DAMAGED. ELONGATED HOLE ON ACCESS PANEL 571BB TRAILING EDGE ON LT WING. REPAIRED THE ACCESS PANEL 571BB IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2025102928662](https://openairdocs.org/sdr/SWAA2025102928662), Oct 26, 2025: FASTENER. MISSING. R1 GIRT BAR FASTENER TLD. INSTALLED FASTENER IN GIRT BAR ATTACHMENT PER AMM 25-66-01 AND SRM 51-40-02
- [SDR SWAA2025102326056](https://openairdocs.org/sdr/SWAA2025102326056), Oct 20, 2025: GIRT BAR. OUT OF ADJUST. R1 DOOR SLIDE COMPARTMENT GIRT BAR HOOK MISSING 1 RIVET. COMPLIED WITH EA M-23-125-01839 FOR INTERIM REPAIR. TLD ISSUED.
- [SDR SWAA2025063085335](https://openairdocs.org/sdr/SWAA2025063085335), Jun 25, 2025: LIGHT. INOPERATIVE. CABIN EMERGENCY LIGHT INOP AT OVERHEAD BIN ROW 9ABC AND 13DEF. <[01] RELAMPED AND OPS CHECKED GOOD IAW MM 33-51-03.
- [SDR SWAA2024101547477](https://openairdocs.org/sdr/SWAA2024101547477), Oct 11, 2024: HANDLE. LOOSE. AFT ENTRY DOOR FWD HANDLE IS LOOSE<[01] TIGHTENED AFT ENTRY DOOR FWD ASSIST HANDLE PER AMM 25-21-25-420-801 STEP 3.B.(5);[02] VERIFIED ITEM 1
- [SDR SWAA2024101545987](https://openairdocs.org/sdr/SWAA2024101545987), Oct 8, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1669 INOP<[01] REPLACED EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1669; PERFORMED GOOD TEST PER AMM 33-51-06
- [SDR SWAA2024101542425](https://openairdocs.org/sdr/SWAA2024101542425), Sep 27, 2024: LENS. BROKEN. SEAT ROW 14ABC EMERGENCY LIGHT LENS BROKEN<[01] REMOVED AND REPLACED BROKEN EMERGENCY LIGHT LENS AT SEAT ROW 14ABC IAW AMM 33-51-03-960-801 STEP 2. D. (1)(2)(3)
- [SDR SWAA2024101542248](https://openairdocs.org/sdr/SWAA2024101542248), Sep 26, 2024: SKIN. DELAMINATED. LEFT OUTBOARD AFT FLAP HAS AREA OF DELAMINATION AT LOWER O/B END<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22-000-801 AND AMM 27-51-22-400-801.;[
- [SDR SWAA2024101540875](https://openairdocs.org/sdr/SWAA2024101540875), Sep 24, 2024: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK AT LBL 45; IN THE WELL AT STA STA 500D+6 TO STA 500D+9; AND ON THE CROWN AT STA 500D+6.<[01] CORRECTION TO FAULT DESCRIPTION: WATER LINE
- [SDR SWAA2024101441223](https://openairdocs.org/sdr/SWAA2024101441223), Sep 24, 2024: STUB FRAME. CRACKED. CRACK FOUND ON R1 DOOR STUB FRAME BS 291.5 + 7.5; WL266.5; L: 0.6' MARKED<[01] VERIFIED RII ITEMS COMPLETE;[02] REMOVED DAMAGED STUB FRAME AND INSTALLED NEW STU
- [SDR SWAA2024101540712](https://openairdocs.org/sdr/SWAA2024101540712), Sep 23, 2024: WEB. CRACKED. RIGHT WING TRANSVERSE WEB UPPER O/B LEG IS CRACKED AT O/B ATTACH RIVET<[01] RIGHT WING TRANSVERSE WEB CRACK L = 0.900' AND IS FOUND OUT OF LIMITS PER SRM 57-51-
- [SDR SWAA2024101440847](https://openairdocs.org/sdr/SWAA2024101440847), Sep 23, 2024: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 241AF TOP SURFACE IS DELAMINATED.<[01] UPDATED MEASUREMENTS.;[02] UPDATED STEP 1;[03] REMOVED PANEL 241AF PER AMM 53-21-00-000-801. IDENTIFIED

All 222: https://openairdocs.org/aircraft/N952WN/reports.md

## STCs that may be installed (OpenAirDocs) (32)

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 737-7H4)

- [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 CFM56-7B24/3 series)

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC
- [STC SE03036CH](https://openairdocs.org/stc/SE03036CH): Application of a deep compressive stress layer using a Low Plasticity Burnishing (LPB) process on CFM56-7 Series Engines Stage 1 High Pressure Compressor (HPC) Blade Dovetails in accordance with Delta Air Lines Inc. Drawing No. 72-0396, Revision B, dated November 3, 2011, or later FAA Approved revision. Delta Air Lines Inc

## Related

- Other Boeing 737-7H4 aircraft: https://openairdocs.org/model/boeing-737-7h4/aircraft.md
- The CFM International CFM56-7B24/3 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-3-series.md

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