# N945WN: 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: 36660
- Year built: 2010
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 31, 2010
- Certificate issued: April 6, 2010
- Expires: March 31, 2030
- Mode S code: AD21BC
- 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=945WN
- Page: https://openairdocs.org/aircraft/N945WN

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 CFM56-7B24/3 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 N945WN.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20130316003521I](https://openairdocs.org/incident/20130316003521I), Mar 16, 2013: Boeing 737-7H4 (N945WN), Romulus, MI, Minor damage. After push back from gate D23, aircraft N945WN started to taxi under its own power. It moved forward about 10 feet and started a right turn. At about 10…

## Service difficulty reports (201, 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 SWAA2026101491322](https://openairdocs.org/sdr/SWAA2026101491322), Oct 10, 2026: GIRT BAR. OUT OF POSITION. AFT ENTRY DOOR GIRT BAY FLAP, OBSTRUCTING DOOR CLOSURE. ADJUSTED THE GIRT BAR Z-FOLD TO LIFT GIRT ABOVE DOOR FRAME AND PREVENT INTERFERENCE IAW AMM 25-66-01.
- [SDR SWAA2026020666170](https://openairdocs.org/sdr/SWAA2026020666170), Jan 30, 2026: BATTERY PACK. INOPERATIVE. ALL EMERGENCY LIGHTS COMMON TO M1674 EMERGENCY BATTERY INOPERATIVE. REMOVED & REPLACED AND PERFORMED GOOD TEST OF EMERGENCY BATTERY PACK M1674.IAW AMM 33-51-06-
- [SDR SWAA2026020965484](https://openairdocs.org/sdr/SWAA2026020965484), Jan 28, 2026: ELEC CONNECTOR. BROKEN. G1 GALLEY EMERGENCY EXIT LIGHT, BLUE PLUG IS BROKEN ON ACFT WIRE SIDE. SPLICED G1 GALLY EMERGENCY LIGHT IAW SWPM 20-30-12. OPS CHECK TO BE PERFORMED ON CC TTG8Q
- [SDR SWAA2026020663254](https://openairdocs.org/sdr/SWAA2026020663254), Jan 20, 2026: SIDEWALL SUPPORT. CORRODED. CORROSION ON THE FLOOR TO SIDEWALL SUPPORT IN THE AFT CARGO BAY BS 727+4 - 727E, RBL 22, WL 156. R & R THE RT FLOOR TO SIDEWALL SUPPORT BS 727 - 767, RBL 22, WL
- [SDR SWAA2026020663256](https://openairdocs.org/sdr/SWAA2026020663256), Jan 20, 2026: STUB FRAME. CRACKED. CRACK FOUND ON FSD STUB FRAME .15' ABOVE SEAL DEPRESSOR, BS 291.5+8, L: .6'. REMOVED AND REPLACED FSD STUB FRAME IAW SRM 51-40-02-0G-0, DWG 141A8370, REV D.
- [SDR SWAA2026020662922](https://openairdocs.org/sdr/SWAA2026020662922), Jan 19, 2026: SCUFF PLATE. CRACKED. FWD CARGO BAY AFT CORNER SCUFF PLATE CRACKED. REPAIRED THE AFT CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, STEP 4.B.(2). RESTORED PROTECTIVE FINISHES IAW SRM 51-2
- [SDR SWAA2026020662920](https://openairdocs.org/sdr/SWAA2026020662920), Jan 19, 2026: SIDEWALL SUPPORT. CORRODED. CORRODED FLOOR TO SIDEWALL SUPPORT BS 500A - 500D, RBL 25, WL 156. REMOVED AND REPLACED THE FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 143A7500, R
- [SDR SWAA2026020662523](https://openairdocs.org/sdr/SWAA2026020662523), Jan 18, 2026: FLOOR SUPPORT. CORRODED. CORROSION ON FWD CARBO BAY AFT BULKHEAD TO FLOOR SUPPORT BS 500D, LBL 24 - RBL 24, WL 156. REMOVED AND REPLACED AFT BULKHEAD TO FLOOR SUPPORT IAW SRM 51-40-02-0
- [SDR SWAA2026020662522](https://openairdocs.org/sdr/SWAA2026020662522), Jan 18, 2026: SIDEWALL SUPPORT. CORRODED. CORROSION ON FWD CARGO BAY, LT AFT BODY TO SIDEWALL SUPPORT BS 492 - 500D, LBL 25, WL 156. DAMAGED FLOOR TO SIDEWALL SUPPORT FOUND OUT OF LIMITS. REMOVED AND IN
- [SDR SWAA2026020662525](https://openairdocs.org/sdr/SWAA2026020662525), Jan 18, 2026: SIDEWALL SUPPORT. CORRODED. CORROSION ON FWD CARGO BAY, RT AFT BODY TO SIDE WALL SUPPORT BS 492 - 500A, RBL 25, WL 156. REMOVED AND REPLACED THE SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, AND
- [SDR SWAA2026020662526](https://openairdocs.org/sdr/SWAA2026020662526), Jan 18, 2026: THRESHOLD WEB. CORRODED. CORROSION ON FWD CARGO BAY SUB THRESHOLD WEB, BS 447 - 478, RBL 28.5, WL 156. REMOVED AND REPLACED THE THRESHOLD WEB IAW SRM 51-40-02-0G-0, AND DWG:143A8330, RE
- [SDR SWAA2026020662524](https://openairdocs.org/sdr/SWAA2026020662524), Jan 18, 2026: ATTACH ANGLE. CRACKED. CRACKED FWD CARGO BAY AFT INTERCOSTAL ATTACH ANGLE AT AFT SIDE BS 500C, LBL 25, WL 154. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143
- [SDR SWAA2026020662528](https://openairdocs.org/sdr/SWAA2026020662528), Jan 18, 2026: BAFFLE. CRACKED. CRACK ON FCB UNDER LT AFT BODY TO SIDE WALL SUPPORT, BS 500C, LBL 25, WL 154. REMOVED AND REPLACED BAFFLE BS 500B - 500C, LBL 25, WL 154 IAW SRM 51-40-02-0G-0, 
- [SDR SWAA2026020662529](https://openairdocs.org/sdr/SWAA2026020662529), Jan 18, 2026: THRESHOLD WEB. CORRODED. CORROSION ON ACB SUB THRESHOLD WEB AT BS 795 - 846, RBL 18 - 28, WL 160. REMOVED AND REPLACED THE SUB THRESHOLD WEB IAW SRM 51-40-02-0G-0, AND DWG 146A8340, REV
- [SDR SWAA2026020662530](https://openairdocs.org/sdr/SWAA2026020662530), Jan 18, 2026: SIDEWALL SUPPORT. CORRODED. CORROSION ON ACB RT BODY TO SIDE WALL SUPPORT AT BS 752 - 787, RBL 22, WL 156. REMOVED AND REPLACED THE RT SHIELD FWD OF ACB BS 767 - 794, RBL 22, WL 156 IAW SR
- [SDR SWAA2026020662531](https://openairdocs.org/sdr/SWAA2026020662531), Jan 18, 2026: SIDEWALL SUPPORT. CORRODED. CORROSION ON ACB LT BODY TO SIDE WALL SUPPORT, BS 732 - 798, LBL 22, WL 158. REMOVED AND REPLACED ACB LT FLOOR TO SIDEWALL SUPPORT, BS 727 - 847, LBL22, WL 158 
- [SDR SWAA2026020662533](https://openairdocs.org/sdr/SWAA2026020662533), Jan 18, 2026: SUPPORT ANGLE. CORRODED. CORROSION ON AFT CARGO BAY BODY TO AFT BULKHEAD SUPPORT ANGLE, BS 947, LBL 9 - RBL 9, WL 179. REMOVED AND REPLACED ACB AFT BULKHEAD LOWER SUPPORT ANGLE BS 947, 
- [SDR SWAA2026020662535](https://openairdocs.org/sdr/SWAA2026020662535), Jan 18, 2026: FLOORBEAM. CORRODED. CORRODED CABIN FLOORBEAM AT BS 986.5, RBL 47, WL 208. REPAIRED IAW SRM 53-70-51-2R-6-A00995,REPAIR 6, SECTION 47.
- [SDR SWAA2026020962230](https://openairdocs.org/sdr/SWAA2026020962230), Jan 16, 2026: SEAT TRACK. CORRODED. CORROSION ON PASSENGER CABIN SEAT TRACK ON TOP OF CROWN BS 480 - 484, LBL 25, WL 208. THE SEAT TRACK REPLACED ON CC TTG8Q019XDP9.
- [SDR SWAA2026020962232](https://openairdocs.org/sdr/SWAA2026020962232), Jan 16, 2026: SEAT TRACK. CORRODED. CORROSION ON PASSENGER CABIN SEAT TRACK ON TOP OF CROWN BS 500C+8, LBL 25, WL 208. THE SEAT TRACK BS 480 - 520 REPLACED ON CC TTG8Q019XDP9.
- [SDR SWAA2026020662223](https://openairdocs.org/sdr/SWAA2026020662223), Jan 16, 2026: CROSSBEAM. CRACKED. CRACKED CROSSBEAM, BS 540 BL 0 - RBL 25, WL 207. REMOVED AND REPLACED THE CROSSBEAM IAW SRM 51-40-02-0G.
- [SDR SWAA2026020662234](https://openairdocs.org/sdr/SWAA2026020662234), Jan 16, 2026: SCUFF PLATE. CRACKED. FWD CARGO BAY, FWD DOOR SURROUND SCUFFPLATE IS CRACKED. REPAIRED FWD DOOR SURROUND SCUFFPLATE IAW AMM SRM 53-30-15-2R-1, STEP 4.B.(2), SOPM 20-30-02, SRM 51-20-
- [SDR SWAA2026020662233](https://openairdocs.org/sdr/SWAA2026020662233), Jan 16, 2026: WEB. CORRODED. CORROSION ON AFT CARGO BAY LOWER SILL SUB THRESHOLD WEB BTWN BS 807 - 847, WL 156. RESOLVED ON CUSTOMER CARD TTG8Q019Y4AA.
- [SDR SWAA2026020961567](https://openairdocs.org/sdr/SWAA2026020961567), Jan 14, 2026: SEAL. CRACKED. RIGHT HORIZONTAL STAB UPPER SLIDE SEAL IS CRACKED. REMOVED AND REPLACED THE RIGHT STABILIZER TO BODY UPPER FRONT SPAR SLIDING SEAL PLATE IAW AMM 53-31-31-000-80
- [SDR SWAA2026011360118](https://openairdocs.org/sdr/SWAA2026011360118), Jan 10, 2026: SKIN. DELAMINATED. DORSAL FIN, PN: 174A0103-7; SN: WN0346, FAILED TAP TEST. DAMAGED AREA SHOWS SIGNS OF DELAMINATION & DEBONDING IAW SRM 51-10-06. ESTIMATED AREA OF DELAMINATION &
- [SDR SWAA2025071089979](https://openairdocs.org/sdr/SWAA2025071089979), Jul 10, 2025: UNKNOWN. SMOKE. ON DECENT, NOTICED POSSIBLE SMOKE COMING FROM CAPTAINS SIDE VENT, SMELL DISSIPATED ONCE LT PACK TURNED OFF. FA DID NOT NOTICE ANY ODORS. PERFORMED CONDITIONAL I
- [SDR SWAA2025041423449](https://openairdocs.org/sdr/SWAA2025041423449), Apr 10, 2025: SEAT BACK. OUT OF ADJUST. EXIT ROW SEAT 11C DOES NOT STAY IN THE UPRIGHT POSITION; <[01]. ADJUSTED RETRACTACTUATOR ON SEAT 11C PER AMM25-22-00.
- [SDR SWAA2025021094098](https://openairdocs.org/sdr/SWAA2025021094098), Feb 7, 2025: LAMP. INOPERATIVE. CR - RR - LT OVERWING EXIT LIGHT INOP<[01] RELAMPED LEFT OVERWING EMERGENCY EXIT EMERGENCY LIGHT AND OPS CHECK GOOD IAW SWA B737-800 AMM 33-51-01-960-801. <BR>P
- [SDR SWAA2024101648041](https://openairdocs.org/sdr/SWAA2024101648041), Oct 12, 2024: HANGER ASSY. LOOSE. L1 EMERGENCY EXIT SLIDE GIRT BAR LEFT HANGER LOOSE.<[01] REMOVED DAMAGED FASTENER FROM ENTRY DOOR SLIDE COVER LEFT GIRT BAR HANGER AND SUBSTITUTED SAFETY WIRE P
- [SDR SWAA2024091236029](https://openairdocs.org/sdr/SWAA2024091236029), Sep 10, 2024: LENS. LOOSE. EMERGENCY EXIT SIGN COVER NEXT TO AFT SERVICE DOOR FELL OFF. REPLACED LENSE IAW AMM 33-51-03.
- [SDR SWAA2024072918290](https://openairdocs.org/sdr/SWAA2024072918290), Jul 27, 2024: SLIDE. OUT OF ADJUST. L2 DOOR OPENED WITH GIRT BAR ATTACHED. SLIDE FELL NOT DEPLOYED<[01] REINSTALLED L2 DOOR SLIDE IAW AMM 25-66-01; MT 725-61-06.
- [SDR SWAA2024072314746](https://openairdocs.org/sdr/SWAA2024072314746), Jul 21, 2024: SEAT BACK. OUT OF ADJUST. SEAT 11F RECLINE INTO EMERGENCY EXIT ROW<[01] ADJUSTED LOCK TO PROPER EXIT ROW CONFIGURATION PER AMM 25-22-00.
- [SDR SWAA2024062505051](https://openairdocs.org/sdr/SWAA2024062505051), Jun 24, 2024: ACTUATOR. OUT OF ADJUST. FLIGHT ATTENDANT REPORTS THAT SEAT 11F RECLINES TO THE POINT OF INPEDING THE EXIT ROW<[01] ADUSTED SEAT 11F SEAT ULTRALOCK ACTUATOR LOCKING NUT PER CMM 25-23-67
- [SDR SWAA2024042376976](https://openairdocs.org/sdr/SWAA2024042376976), Apr 19, 2024: TAILPIPE. FIRE. ENTERING THE RUNWAY AN A/C BEHIND US REPORTED A TAILPIPE FIRE IN #1 ENGINE- ENGINE INDICATIONS IN THE COCKPIT WERE NORMAL WITH NO FIRE INDICATION-<[01] UPON FUR
- [SDR SWAA2024022956477](https://openairdocs.org/sdr/SWAA2024022956477), Feb 27, 2024: BATTERY PACK. NO TEST. EMERGENCY BATTERY PACK M01669 FAILED A CAPACITANCE CHECK. REMOVED AND REPLACED THE BATTERY PACK M01668 PER AMM 33-51-06.
- [SDR SWAA2024022956476](https://openairdocs.org/sdr/SWAA2024022956476), Feb 27, 2024: BATTERY PACK. NO TEST. EMERGENCY BATTERY PACK M01668 FAILED A CAPACITANCE CHECK. REMOVED AND REPLACED BATTERY PACK M01668 PER AMM 33-51-06.
- [SDR SWAA2024022956475](https://openairdocs.org/sdr/SWAA2024022956475), Feb 27, 2024: BATTERY PACK. NO TEST. EMERGENCY BATTERY PACK M01672 FAILED A CAPACITANCE CHECK. REMOVED AND REPLACED THE BATTERY PACK M01672 IAW AMM 33-51-06.
- [SDR SWAA2024022754529](https://openairdocs.org/sdr/SWAA2024022754529), Feb 22, 2024: BATTERY PACK. INOPERATIVE. EXTERIOR AFT OVERWING EMERGENCY SLIDE LIGHTS LH AND RH INOP.<[01] REMOVED; REPLACED; AND PERFORMED INSTALLATION TEST FOR BATTERY PACK AT M1673 AS PER B737 AMM 3
- [SDR SWAA2024022754530](https://openairdocs.org/sdr/SWAA2024022754530), Feb 22, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY AREA AISLE LIGHTS AT ROWS 9 AND 11 ABC IINOP.<[01] REMOVED; REPLACED; AND PERFORMED INSTALLATION TEST FOR BATTERY PACK AT M1670 AS PER B737 AMM 33-51-
- [SDR SWAA2024022954834](https://openairdocs.org/sdr/SWAA2024022954834), Feb 21, 2024: REPAIR. UNKNOWN. CUSTOMER REQUEST - ACCOMPLISH HFEC INSPECTION OF PREVIOUS CUTOUT ON FLIGHT DECK FLOOR REPAIR CALLED OUT ON STEP 9 OF EA 1-A53-33179 REV IR<[01] REMOVED AND REIN
- [SDR SWAA2024022754399](https://openairdocs.org/sdr/SWAA2024022754399), Feb 21, 2024: HINGE FITTING. CORRODED. ECS DOOR 192CL; SECOND FROM FWD HINGE FITTING AT BONDIN STUD HAS CORROSION.<[01] REMOVED AND REPLACED FWD HINGE FITTING AT ECS COMP. PER SRM 51-40-02-0G-0;[02] 
- [SDR SWAA2024022953811](https://openairdocs.org/sdr/SWAA2024022953811), Feb 15, 2024: SUPPORT BRACKET. CRACKED. PNEUMATIC MANIFOLD SUPPORT BRKT CRKED. LOCATED IN L/H A/C BAY JUST AFT OF BS 540 (P/N 212A1116-1)<[01] RECEIVED NEU PART PO#2043476] REMOVED AND REPLACED DAMAGE
- [SDR SWAA2024022752346](https://openairdocs.org/sdr/SWAA2024022752346), Feb 14, 2024: FLOORBEAM. CRACKED. CABIN FLOOR SUPPORT AT STA 537.45 BETWEEN BL0 AND LBL24 CRACKED.<[01] REMOVED AND REPLACED FLOOR SUPPORT P/N 143A5240-63 AT STA. 537.45 BETWEEN BL 0 TO LBL 24 P
- [SDR SWAA2024022751131](https://openairdocs.org/sdr/SWAA2024022751131), Feb 11, 2024: PLATE. CRACKED. UPPER PLATE CRACK AT STA. 537.45 BETWEEN BL0 AND LBL 24<[01] REMOVED CRACKED UPPER PLATE AT STA. 537.45; BETWEEN BL0 AND LBL24; WL 208.1 PER REF. SRM 51-40-02-0
- [SDR SWAA2024022751132](https://openairdocs.org/sdr/SWAA2024022751132), Feb 11, 2024: FLOOR PANEL. PEELING. CABIN FLOOR PANEL 231UF UPPER SKIN SURFACE PEELING.<[01] RECEIVED NEW FLOOR PANEL 231UF; WILL BE INSTALLED ON <BR>TTG8Q00RGQPH.;[02] VERIFIED STEP 1
- [SDR SWAA2024022751309](https://openairdocs.org/sdr/SWAA2024022751309), Feb 11, 2024: FAIRING. DELAMINATED. #1 FWD FLAP FAIRING (PNL 544AB) ERRODED/DELAMINATED<[01] WILL BE C/W ON TTG8Q00RAXXR;[02] VERIFIED STEP 1
- [SDR SWAA2024022951129](https://openairdocs.org/sdr/SWAA2024022951129), Feb 10, 2024: ANGLE. CRACKED. FOUND ANGLE SUPPORT CRACKED AT RT. WING T/E I/B OF DEFLECTION RIB<[01] REMOVED AND REPLACED ANGLE CLIP AT RIGHT WING T/E I/B OF DEFLECTION CONTROL RIB IN REF B7
- [SDR SWAA2024022750823](https://openairdocs.org/sdr/SWAA2024022750823), Feb 10, 2024: FLOOR PANEL. PEELING. CABIN FLOOR PANEL 241AF UPPER SKIN SURFACE PEELING.<[01] RECEIVED NEW FLOOR PANEL 241AF; WILL BE INSTALLED ON TTG8Q00QKJS4.;[02] VERIFIED STEP 1
- [SDR SWAA2024022751012](https://openairdocs.org/sdr/SWAA2024022751012), Feb 10, 2024: SUPPORT. CRACKED. R/WING TRAILING EDGE PANEL 661AB O/B LOWER 'T' SUPPORT STRUCTURE HAS A CRACK AT FWD EDGE MKD 107-011<[01] RECEIVED NEW PART PO#2043476] REMOVED AND REPLACED FIT
- [SDR SWAA2024022751013](https://openairdocs.org/sdr/SWAA2024022751013), Feb 10, 2024: SUPPORT. CRACKED. R/WING TRAILING EDGE ACCESS PANEL 661AB MUST O/B FWD SUPPORT STRUCTURE HAS A CRACK AT O/B EDGE MKD 107-010<[01] REMOVED AND REPLACE DAMAGED WIGGLE PLATE AT R/WI

All 201: https://openairdocs.org/aircraft/N945WN/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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