# N938WN: 2009 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: 36645
- Year built: 2009
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 7, 2009
- Certificate issued: June 23, 2009
- Expires: August 31, 2027
- Mode S code: AD0562
- 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=938WN
- Page: https://openairdocs.org/aircraft/N938WN

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 N938WN.

## FAA accident and incident reports

None matched to N938WN.

## Service difficulty reports (203, 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 SWAA2026040183992](https://openairdocs.org/sdr/SWAA2026040183992), Mar 28, 2026: LIGHT. DAMAGED. 1 DEF EMERGENCY ESCAPE PATH LUMINESCENCE STRIP DAMAGED. R & R PHOTOLUMINESCENT STRIP IAW AMM 33-51-15.
- [SDR SWAA2026040183989](https://openairdocs.org/sdr/SWAA2026040183989), Mar 28, 2026: LENS. WRONG PART. RIGHT EMERGENCY EXIT DOOR FWD LOWER EMERGENCY EXIT LIGHT LENS MISSING DIRECTIONAL ARROW PLACARD. REPLACED RIGHT HAND EMERGENCY EXIT SIGN. REF AMM 33-51-0123478.
- [SDR SWAA2025061281091](https://openairdocs.org/sdr/SWAA2025061281091), Jun 11, 2025: UNKNOWN. ODOR. PLASTIC BURNING SMELL DETECTED BY FA AND PASSENGERS AROUND ROW 5-6 DURING PUSHBACK. COULD NOT FIND SOURCE. RETURNED TO GATE<[01] INSPECTED CABIN AREA FWD CARGO 
- [SDR SWAA2025050868690](https://openairdocs.org/sdr/SWAA2025050868690), May 7, 2025: SWITCH. FAULTY. NR 2 ENG FUEL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT<[01] REMOVED AND REPLACED DIFFERENTIAL PSI SWITCH PER AMM 73-34-01 AND REPLACED FUEL FILTER PER AMM 73-1
- [SDR SWAA2025050868723](https://openairdocs.org/sdr/SWAA2025050868723), May 7, 2025: FILTER. FAULTY. NR 2 ENG FUEL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED DIFFERENTIAL PSI SWITCH PER AMM 73-34-01 AND REPLACED FUEL FILTER PER AMM 73-11-02
- [SDR SWAA2025042926244](https://openairdocs.org/sdr/SWAA2025042926244), Apr 19, 2025: LAMP. INOPERATIVE. EMERGENCY EXIT LOCATOR SIGN FORWARD OF THE L/H OWE HAS 1 EA LAMP INOP<[01] RELAMPED AND PERFORMED GOOD TEST OF EMERGENCY EXIT LOCATOR SIGN AT L/H OWE IAW AMM 33
- [SDR SWAA2025042923872](https://openairdocs.org/sdr/SWAA2025042923872), Apr 11, 2025: RIB. CRACKED. L/H HORIZONTAL STABILIZER INSPAR RIB AT STAB STA. 111.10 UPPER O/B FLANGE CRACKED AT FWD END<[01] REPAIRED L/H HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 111.
- [SDR SWAA2025042922877](https://openairdocs.org/sdr/SWAA2025042922877), Apr 8, 2025: FLOORBEAM. CRACKED. CRACKED BREAK PANEL BS 540 BL 0-LBL 25 WL 208.<[01] REMOVED AND REPLACED BREAK PANEL BS 540 BL 0-LBL 25 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 143A0060
- [SDR SWAA2025042922878](https://openairdocs.org/sdr/SWAA2025042922878), Apr 8, 2025: FLOORBEAM. CRACKED. CRACKED BREAK PANEL BS 540 RBL 25 -RBL 45 WL 208.<[01] REMOVED AND REPLACED BREAK PANEL BS 540 RBL 25 -RBL 45 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 143A0060
- [SDR SWAA2025042922528](https://openairdocs.org/sdr/SWAA2025042922528), Apr 8, 2025: STRAP. CORRODED. AFT CARGO BAY FLOOR T STRAP HAS CORROSION BS 767+5 RBL 8 WL 156<[01] EVALUATED CORROSION ON FLOOR STRAP; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM A
- [SDR SWAA2025042922529](https://openairdocs.org/sdr/SWAA2025042922529), Apr 8, 2025: STRAP. CORRODED. AFT CARGO BAY FLOOR T STRAP HAS CORROSION BS 727D+5 LBL 5 TO RBL 11 WL 156<[01] EVALUATED CORROSION ON FLOOR STRAP; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS I
- [SDR SWAA2025042922354](https://openairdocs.org/sdr/SWAA2025042922354), Apr 7, 2025: SHIELD. CORRODED. CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] CORROSION WAS FOUND TO BE OUT OF LIMITS. REMO
- [SDR SWAA2025042922342](https://openairdocs.org/sdr/SWAA2025042922342), Apr 7, 2025: SUPPORT PLATE. CORRODED. CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] CORROSION WAS FOUND TO BE
- [SDR SWAA2025042922355](https://openairdocs.org/sdr/SWAA2025042922355), Apr 7, 2025: SUPPORT PLATE. CORRODED. CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] CORROSION WAS FOUND TO BE OUT
- [SDR SWAA2025042922349](https://openairdocs.org/sdr/SWAA2025042922349), Apr 7, 2025: SEAT TRACK. CORRODED. CORROSION ON PAX CABIN SEAT TRACK LBL25 BS380; BS434; BS434 CROWN WL208. MARKED<[01] UPDATED STEPS 1 AND 2;[02] STEP 3 COMPLETE;[03] REMOVED AND REPLACED NEW SE
- [SDR SWAA2025042921495](https://openairdocs.org/sdr/SWAA2025042921495), Apr 3, 2025: SKIN. CRACKED. CRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 26'' FROM FWD EDGE; 0.8' IN LENGTH (MARKED)<[01] REMOVED THE DAMAGED PART ON LH HORIZONTAL STA
- [SDR SWAA2025042921485](https://openairdocs.org/sdr/SWAA2025042921485), Apr 3, 2025: STIFFENER. CRACKED. RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 92.70; 3RD VERTICAL STIFFENER IS CRACKED.<[01] REPAIRED RIGHT HAND HORIZONTAL STABILIZER INSP
- [SDR SWAA2025042921484](https://openairdocs.org/sdr/SWAA2025042921484), Apr 3, 2025: STIFFENER. CRACKED. LH HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 111.10; 3RD VERTICAL STIFFENER IS CRACKED.<[01] REPAIRED LH STAB INSPAR RIB 3RD VERTICAL STIFFENER AT
- [SDR SWAA2025042921482](https://openairdocs.org/sdr/SWAA2025042921482), Apr 3, 2025: WEB. CORRODED. CORROSION ON LOWER SILL WEB UPPER SURFACE FROM BS 624 TO BS 632; RBL68; WL208<[01] 'THE DAMAGE WAS REWORKED PER 737-700 SRM 53-40-15-1A-1 (ALLOWABLE DAMAGE 1) A
- [SDR SWAA2025042920767](https://openairdocs.org/sdr/SWAA2025042920767), Apr 2, 2025: SKIN. DEBONDED. PANEL 191HL OUTER SKIN HAS A DISBOND. (MARKED)<[01] 191HL PANEL OUTER SKIN SURFACE DAMAGE HAS BEEN REPAIRED PER [SRM 51-70-05-2R-2-A00733 (REPAIR 2 - REPAIR OF 
- [SDR SWAA2025043020746](https://openairdocs.org/sdr/SWAA2025043020746), Apr 1, 2025: LIGHT. DEBONDED. FWD ENTRY CLOSE OUT PANEL ANNUNCIATOR LIGHT BAR IS DISBONDED<[01] REMOVED AND REINSTALLED THE FWD ENTRY CLOSE OUT PANEL ANNUNCIATOR LIGHT BAR PER AMM 33-51-01-9
- [SDR SWAA2025031001963](https://openairdocs.org/sdr/SWAA2025031001963), Mar 4, 2025: LIGHT. INOPERATIVE. LEFT OVERWING EXIT HATCH SIDEWALL LIGHT INOP<[01] R&R LEFT OVERWING EXIT HATCH SIDEWALL LIGHT REF AMM 33-51-01
- [SDR SWAA2024111157941](https://openairdocs.org/sdr/SWAA2024111157941), Nov 7, 2024: SLIDE. OUT OF POSITION. FWD ENTRY DOOR SLIDE NEEDS REPOSITIONED<[01] REPOSITIONED FWD ENTRY SLIDE PER MM 25-66-00 AND MT 725-61-06
- [SDR SWAA2024090634237](https://openairdocs.org/sdr/SWAA2024090634237), Sep 5, 2024: LIGHT. LOOSE. 11 DEF EMERGENCY LIGHT LOOSE IN O/H BIN BULLNOSE<[01] SECURED 11DEF EMERGENCY LIGHT IN O/H BULLNOSE PER CMM 25-24-02.
- [SDR SWAA2024080521198](https://openairdocs.org/sdr/SWAA2024080521198), Jul 31, 2024: SIGN. DETACHED. OVERWING EXIT ROW EMERGENCY EXIT SIGN KNOCKED DOWN.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-960-802-NG (EXIT SIGN - LIGHT ASSEMBLY REPLACEMENT - PERMAN
- [SDR SWAA2024041773613](https://openairdocs.org/sdr/SWAA2024041773613), Apr 11, 2024: POST. CORRODED. CORROSION; EVIDENCE OF CORROSION AFT OF FWD LAV AFT I/B POST AT APPROX FUSE STATION 307 TO 331; LBL 12 TO 38 WL 208<[01] NO STRUCTURE CORROSION FOUND. CORROSION
- [SDR SWAA2024041773611](https://openairdocs.org/sdr/SWAA2024041773611), Apr 11, 2024: ACCESS PANEL. LOOSE. ACCESS PANEL 192DR LATCHES LOOSE<[01] 01 - REMOVED AND REPLACED PER [AMM 52-48-42-400-802-NG (ENVIRONMENTAL CONTROL SYSTEMS (ECS) HIGH PRESSURE DOOR - INSTALLAT
- [SDR SWAA2024041173356](https://openairdocs.org/sdr/SWAA2024041173356), Apr 11, 2024: DOOR FRAME. CRACKED. FWD SERVICE DOOR LOWER AFT STOP FITTING CRACKED. REMOVED AND REPLACED PER [AMM 52-41-00-401-NG (GALLEY SERVICE DOOR - REMOVAL/INSTALLATION - PERMANENT. FWD GALL
- [SDR SWAA2024022957100](https://openairdocs.org/sdr/SWAA2024022957100), Feb 27, 2024: SLIDE. EXPOSED. FRONT PROVISIONING DOOR SLIDE PARTIALLY EXPOSED<[01] ADJUST/CHECK FWD SLIDE SERVICE DOOR ESCAPE SLIDE PER AMM 25-66-01-200-802
- [SDR SWAA2024013045631](https://openairdocs.org/sdr/SWAA2024013045631), Jan 28, 2024: LIGHT. INOPERATIVE. FOUND RH OVER-WING EMERGENCY LIGHT INOP<[01] RELAMP SLIDE/OVERWING LIGHT. OPS CHECK GOOD. PER AMM 33-51-04.
- [SDR SWAA2024012343276](https://openairdocs.org/sdr/SWAA2024012343276), Jan 21, 2024: LIGHT. INOPERATIVE. ROW 11 AND 13 RIGHT SIDE EMERGENCY LIGHTS INOP<[01] R&R POWER SUPPLY AT THE RIGHT CABIN EMERGENCY EXIT. OP CHECK GOOD.
- [SDR SWAA2023122835687](https://openairdocs.org/sdr/SWAA2023122835687), Dec 28, 2023: NUT. BROKEN. FWD SERVICE DOOR ASSIST HANDLE BROKEN<[01] R&R NUT THAT ATTACHES FWD SERVICE DOOR ASSIST HANDLE PER AMM 52-41-31.
- [SDR SWAA2023100608232](https://openairdocs.org/sdr/SWAA2023100608232), Oct 5, 2023: SLIDE. LOW PRESSURE. L2 DOOR SLIDE PRESS LOW<[01] REMOVED AFT ENTRY SLIDE IAW AMM 25-66-01;[02] INSTALLED AFT ENTRY SLIDE IAW AMM 25-66-01
- [SDR SWAA2023100206285](https://openairdocs.org/sdr/SWAA2023100206285), Oct 1, 2023: TRANSMITTER. LOCKED. FLAP LOCKOUT WITH FLAPS BETWEEN 1 AND 5<[01] REMOVED AND REPLACED L/H T/E FLAP POSITION TRANSMITTER IAW AMM 27-58-01
- [SDR SWAA2023083195658](https://openairdocs.org/sdr/SWAA2023083195658), Aug 31, 2023: BRACKET. CRACKED. PASSENGER CABIN: FORWARD SERVICE DOOR: (R1) AFT SLIDE ATTACH BOLT MOUNT ISOLATOR BRACKET CRACKED.<[01] R&R FORWARD SERVICE DOOR: (R1) AFT SLIDE ATTACH BOLT MOUN
- [SDR SWAA2023072581448](https://openairdocs.org/sdr/SWAA2023072581448), Jul 23, 2023: BATTERY PACK. INOPERATIVE. DURING EMERGENCY LIGHTS OPS TEST; L/H OVERWING EXIT LIGHT TOP AND BOTTOM INOP<[01] REMOVED AND REPLACED L/H MID BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD
- [SDR SWAA2023060254544](https://openairdocs.org/sdr/SWAA2023060254544), May 31, 2023: STRAP. BROKEN. AFT FA FLASHLIGHT STRAP BROKEN<[01] R & R STRAP REF AMM 25-64-00
- [SDR SWAA2023060254412](https://openairdocs.org/sdr/SWAA2023060254412), May 31, 2023: LENS. MISSING. RIGHT SIDE EMERGENCY EXIT PLASTIC COVER MISSING<[01] INSTALLED NEW EMERGENCY EXIT INDICATOR LENS PER AMM 33-51-01.
- [SDR SWAA2023052350326](https://openairdocs.org/sdr/SWAA2023052350326), May 20, 2023: FUSE. INOPERATIVE. CUSTOMER REQUEST. EMERGENCY EXIT LIGHT INOPERATIVE @ SEAT ROW 14ABC AND ROW 22DEF AND ROW 24ABC.<[01] REMOVED AND REPLACED FUSES AT EMERGENCY POWER SUPPLIES M16
- [SDR SWAA2023052349986](https://openairdocs.org/sdr/SWAA2023052349986), May 18, 2023: WEB. DAMAGED. REJECT : QC SME FOUND FLIGHT DECK FLOOR WEB REPAIR WITH 5 EA. BAD RIVET TAILS AT B.S. 252 RBL 7' - LBL 18' W.L. 208.<[01] REMOVED AND REPLACED FASTENERS (5 EA.)
- [SDR SWAA2023052349535](https://openairdocs.org/sdr/SWAA2023052349535), May 17, 2023: LIGHT. INOPERATIVE. CABIN EMERGENCY LIGHTS ARE INOP AT 6CBA AND 9CBA AND LEFT SIDE AT OVER WING EXIT<[01] RELAMP CABIN EMERGENCY AREA LIGHT AT ROW 6CBA AND 9CBA IN REF. B737 AMM 33
- [SDR SWAA2023052348923](https://openairdocs.org/sdr/SWAA2023052348923), May 15, 2023: BRACKET. BROKEN. PANEL #651EB SUPPORT STRUCTURE HAS A BROKEN BRACKET.<[01] INSTALLATION OF BRACKET WILL BE ACCOMPLISH ON CARD #TTG8Q00L0V6J;[02] VERIFIED STEP1.
- [SDR SWAA2023052248534](https://openairdocs.org/sdr/SWAA2023052248534), May 14, 2023: BRACKET. CRACKED. RIGTH WING LOWER I/B FIXED TRAILING EDGE BRACKET CRACKED<[01] INSTALLED NEW BRACKET AT RIGTH WING LOWER I/B FIXED TRAILING EDGE PER SRM 51-40-02-0G-0;[02] VERIF
- [SDR SWAA2023052348142](https://openairdocs.org/sdr/SWAA2023052348142), May 13, 2023: LIGHT. INOPERATIVE. R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP 1
- [SDR SWAA2023052348441](https://openairdocs.org/sdr/SWAA2023052348441), May 13, 2023: BATTERY PACK. INOPERATIVE. PAX EMERGENCY LIGHT POWER SUPPLY M1670 INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY (M1670) IN REF WITH B737 AMM 33-51-06-960-80
- [SDR SWAA2023052351339](https://openairdocs.org/sdr/SWAA2023052351339), May 13, 2023: POWER SUPPLY. INOPERATIVE. PAX EMERGENCY LIGHT POWER SUPPLY M1670 INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY (M1670) IN REF WITH B737 AMM 33-51-06-960-80
- [SDR SWAA2023052347454](https://openairdocs.org/sdr/SWAA2023052347454), May 11, 2023: WEB. ELONGATED. FOUND TWO EXISTING HOLES AT LH WEB ENLONGATED<[01] FAULT RESOLVED ON ANOTHER FAULTS: TTG8Q00KYXWT AND TTG8Q00KYXWZ;[02] VOID STEP 1. THE CORRECT STATEMENT IS: F
- [SDR SWAA2023052347455](https://openairdocs.org/sdr/SWAA2023052347455), May 11, 2023: WEB. ELONGATED. FOUND ONE EXISTING HOLES AT LH WEB ELONGATED ( I/B THE ANOTHER ELONGATED HOLE) STA 258 LBL22 WL 208.1<[01] FINAL HOLE SIZE .215 DIAMETER ; AND INSTALLATION OF F
- [SDR SWAA2023052247665](https://openairdocs.org/sdr/SWAA2023052247665), May 11, 2023: DOOR. OUT OF ADJUST. R1 DOOR NEEDS ADJUSTMENT<[01] ADJUSTED R1 DOOR IN REF. B737 52-41-00-820-801;[02] VERIFIED R1 DOOR ADJUSTMENT.
- [SDR SWAA2023052247457](https://openairdocs.org/sdr/SWAA2023052247457), May 11, 2023: WEB. DAMAGED. FOUND ONE EXISTING HOLES AT LH WEB ELONGATED ( FWD THE ANOTHER ELONGATED HOLE<[01] FINAL HOLE SIZE .250 DIAMETER ; INSTALLATION OF FASTENER WAS ACCOMPLISHED ON 

All 203: https://openairdocs.org/aircraft/N938WN/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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