# N951WN: 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: 36665
- Year built: 2010
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 28, 2010
- Certificate issued: September 10, 2010
- Expires: May 31, 2028
- Mode S code: AD3A5F
- 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=951WN
- Page: https://openairdocs.org/aircraft/N951WN

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 N951WN.

## FAA accident and incident reports

None matched to N951WN.

## Service difficulty reports (178, 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 SWAA2026061712911](https://openairdocs.org/sdr/SWAA2026061712911), Jun 17, 2026: LIGHT. INOPERATIVE. INOP EXTERIOR EMERGENCY EXIT LIGHT AT LT SIDE WING TO BODY FAIRING AREA BS 767. REMOVED AND REPLACED EXTERIOR EMERGENCY EXIT LIGHT AT LT SIDE WING TO BODY FAIRI
- [SDR SWAA2026062212552](https://openairdocs.org/sdr/SWAA2026062212552), Jun 16, 2026: BATTERY PACK. INOPERATIVE. INOPERATIVE EMERGENCY LIGHT ON STOWAGE BIN 2 AND 3 RT. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805, TESTED OK.
- [SDR SWAA2026062212550](https://openairdocs.org/sdr/SWAA2026062212550), Jun 16, 2026: BATTERY PACK. INOPERATIVE. INOPERATIVE EMERGENCY LIGHT IN FWD GALLEY 1. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805, TESTED OK.
- [SDR SWAA2026062208737](https://openairdocs.org/sdr/SWAA2026062208737), Jun 3, 2026: WEB. CRACKED. CRACKED DOUBLER WEB LOCATED ON BS 663.75 VAPOR BARRIER AREA BTW RBL 6.15 AND RBL 31.83. REPLACED WEB LOCATED ON BS 663.75 VAPOR BARRIER AREA BTW RBL 6.15 AND RB
- [SDR SWAA2026062208736](https://openairdocs.org/sdr/SWAA2026062208736), Jun 3, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 193B (LEFT SIDE) BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193B (LEFT SIDE) BODY FAIRING AT FUSELAGE EXTERIOR IAW
- [SDR SWAA2026062208128](https://openairdocs.org/sdr/SWAA2026062208128), May 31, 2026: STRINGER. CRACKED. CRACKED STRINGER 23L, BS 540 IN THE FWD CARGO BAY. PERFORMED A PERMANENT REPAIR CATEGORY A ON STRINGER 23L BETWEEN BS 500D - 540 AT FWD CARGO BAY IAW SRM 53-00-
- [SDR SWAA2026062208039](https://openairdocs.org/sdr/SWAA2026062208039), May 31, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 947.5, S26L IN THE AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, AND DWG 149A8103, SHEET 8, REV -.
- [SDR SWAA2026062208044](https://openairdocs.org/sdr/SWAA2026062208044), May 31, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 867, S26L IN THE AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DRAWING 149A8102, REV A.
- [SDR SWAA2026062207959](https://openairdocs.org/sdr/SWAA2026062207959), May 31, 2026: BRACKET. DAMAGED. ELONGATED HOLE ON FWD BRACKET FRONT SPAR HORIZONTAL STAB RT SIDE. REPLACED FWD BRACKET FRONT SPAR HORIZONTAL STABILIZER RT SIDE IAW SRM 51-40-02. REPLACED FWD B
- [SDR SWAA2026062207958](https://openairdocs.org/sdr/SWAA2026062207958), May 30, 2026: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE, BS 867, STR 3R IN THE PASSENGER CABIN. REPLACED SUPPORT ANGLE IAW SRM 51-10-02, SRM 51-40-02, AND DWG 146A7901, SHEET 66, REV A.
- [SDR SWAA2026062207613](https://openairdocs.org/sdr/SWAA2026062207613), May 29, 2026: ANGLE. CRACKED. CRACKED UPPER ANGLE BS 694, BL 0. REPLACED THE UPPER ANGLE & FASTENERS IAW SRM 51-40-02, SRM 51-10-02, & DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026062207731](https://openairdocs.org/sdr/SWAA2026062207731), May 29, 2026: CROSSBEAM. CRACKED. CRACK ON BREAK PANEL LOCATED BS 540, BL 0 - LBL 24.75. REPLACED THE BREAK PANEL IAW SRM 51-40-02, SRM 51-10-02, ITEM 9.
- [SDR SWAA2026062207612](https://openairdocs.org/sdr/SWAA2026062207612), May 29, 2026: ANGLE. CRACKED. CRACKED LOWER ANGLE, BS 694, BL 0. REPLACED LOWER ANGLE IAW SRM 51-10-02, SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026062207730](https://openairdocs.org/sdr/SWAA2026062207730), May 29, 2026: CROSSBEAM. CRACKED. CRACKED BREAK PANEL, BS 540, BL 0 - RBL 24.75. REPLACED BREAK PANEL IAW SRM 51-40-02.
- [SDR SWAA2026062207295](https://openairdocs.org/sdr/SWAA2026062207295), May 28, 2026: VAPOR BARRIER. CRACKED. CRACK ON VAPOR BARRIER RT SIDE BS 663.75 AT MAIN WHELL WELL. EVALUATED CRACK LOC. ON VAPOR BARRIER RT SIDE BS663.75 AT MAIN WHEEL WELL AND FOUND OUT LIMIT DUE T
- [SDR SWAA2026062207301](https://openairdocs.org/sdr/SWAA2026062207301), May 28, 2026: WEB. CRACKED. CRACKED WEB INBD FAN COWL INTERNAL AREA ON ENGINE 1. REPLACED WEB INBOARD FAN COWL INTERNAL AREA ON ENGINE 1 IAW 71-13-30, PAGE 10092 AND SRM 51-10-02, ITEM 9.
- [SDR SWAA2026062207276](https://openairdocs.org/sdr/SWAA2026062207276), May 27, 2026: PRESSURE DECK. CRACKED. CRACK INDICATION ON HORIZONTAL PRESSURE DECK BETWEEN BS 663 TO 675, RBL 42. PERFORMED A PERMANENT REPAIR ON THEHORIZONTAL PRESSURE DECK BTW RBL30 TO RBL60 AND B
- [SDR SWAA2026062207275](https://openairdocs.org/sdr/SWAA2026062207275), May 27, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-10, REP
- [SDR SWAA2026062206713](https://openairdocs.org/sdr/SWAA2026062206713), May 26, 2026: SCUFF PLATE. CRACKED. CRACKED FWD CORNER SCUFF PLATE IN THE FWD CARGO BAY. REPAIRED FWD CORNER SCUFF PLATE OF FWD CARGO BAY IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975.
- [SDR SWAA2026062206397](https://openairdocs.org/sdr/SWAA2026062206397), May 26, 2026: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ALONG PASSENGER CABIN (1KT). REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING IAW AMM-33-51-15-400-802.
- [SDR SWAA2026062206541](https://openairdocs.org/sdr/SWAA2026062206541), May 26, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLE ON ACCESS PANEL 194E BODY FAIRING AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 194E BODY FAIRING AT LOWER FUSELAGE IAW SRM 51-70-05-2R-8 REPAIR 8.
- [SDR SWAA2026062206215](https://openairdocs.org/sdr/SWAA2026062206215), May 24, 2026: FITTING. CRACKED. CRACKED LOWER SURFACE AROUND FASTENER ON LEFT WING ACTUATOR FITTING SLAT 4. PERFORMED A PERMANENT REPAIR ON THE NOSE SKIN SLAT 4, LT WING IAW SRM 57-42-01-2R-8,
- [SDR SWAA2026051803287](https://openairdocs.org/sdr/SWAA2026051803287), May 15, 2026: BATTERY PACK. NO TEST. M1670 FAILED CAPACITY CHECK. R/R M1670 BATTERY PACK PER AMM 33-51-06
- [SDR SWAA2025121143796](https://openairdocs.org/sdr/SWAA2025121143796), Dec 7, 2025: TRAY. OUT OF ADJUST. TRAY TABLE EXIT ROW (FO SIDE) WONT STAY LOCKED UPRIGHT. OK TO CONTINUE PER MEL 25-10-01. SP-1B. FOUND MISSING SET SCREW INSTALLED NEW SET SCREW ADJUSTED, OPS CH
- [SDR SWAA2025091213608](https://openairdocs.org/sdr/SWAA2025091213608), Sep 11, 2025: BATTERY PACK. FAILED. L/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2025080697911](https://openairdocs.org/sdr/SWAA2025080697911), Aug 3, 2025: LAMP. INOPERATIVE. SIDEWALL LIGHTS INOP AT ROWS 2DEF ;6DEF 16ABC 22DEF;24DEF;23 ABC SIDEWALL LIGHTS INOP AT ROWS 2DEF 6DEF 16ABC 22DEF24DEF23 ABC. RELAMPED CABIN SIDEWALL LIGHTS I
- [SDR SWAA2024120974494](https://openairdocs.org/sdr/SWAA2024120974494), Dec 6, 2024: SKIN. DELAMINATED. LEFT WING OUTBOARD TRAILING EDGE FLAP DELAMINATED(MARKED).<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22.;[02] C/W INSPECTION
- [SDR SWAA2024111157199](https://openairdocs.org/sdr/SWAA2024111157199), Nov 6, 2024: INLET. DAMAGED. #1 ENGINE INLET COWL LIPSKIN HAS A APPROX. 9IN. CREASE AT THE 11 O'CLOCK POSITION.<[01] R & R?D #1 ENGINE INLET PER AMM 71-11-01.
- [SDR SWAA2024072913774](https://openairdocs.org/sdr/SWAA2024072913774), Jul 17, 2024: ACCESS PANEL. DETERIORATED. LEFT WING LOWER I/B FIXED T/E ACCESS PANEL #551GB; SEAL DETERIORATED/BROKEN<[01] REMOVED AND REPLACED L/W LOWER I/B FIXED T/E ACCESS PANEL 551GB SEAL IN REF TO 
- [SDR SWAA2024072612065](https://openairdocs.org/sdr/SWAA2024072612065), Jul 13, 2024: CHANNEL. CORRODED. AFT CARGO R/H 'Z' CHANNEL FROM STA 727C TO 727D HAS 1 SPOT WITH CORROSION. (MARKED)<[01] REMOVED CORROSION; PERFORMED UT THICKNESS INSPECTION; CHECKED LIMITS OF
- [SDR SWAA2024072910521](https://openairdocs.org/sdr/SWAA2024072910521), Jul 8, 2024: CEILING PANEL. CRACKED. AFT CARGO CEILING 141YBC WITH FRAYED/CRACKED EDGES.<[01] FABRICATED AFT CARGO CEILING PANEL 141YBC AS PER AMM 25-52-01-201-801;[02] VERIFIED STEP 1.
- [SDR SWAA2024072910220](https://openairdocs.org/sdr/SWAA2024072910220), Jul 7, 2024: DUCT. CORRODED. #2 ENGINE IB TR C-DUCT AFT EXHAUST AREA INNER SURFACE WITH PITTING CORROSION.<[01] REMOVED PITTING CORROSION AT #2 ENGINE IB TR C-DUCT AFT EXHAUST INNER SURFACE
- [SDR SWAA2024072909595](https://openairdocs.org/sdr/SWAA2024072909595), Jul 5, 2024: SUPPORT BEAM. CRACKED. RT WING T/E; LOWER PANEL 661AB SUPPORT BEAM CRACKED AT I/B END.<[01] REMOVED SUPPORT BEAM AT R/W T/E ON LOWER PANEL 661AB AS PER SRM 51-40-02-0G-0. LOCATED AND 
- [SDR SWAA2024072509612](https://openairdocs.org/sdr/SWAA2024072509612), Jul 5, 2024: FLOOR PANEL. CRACKED. AFT CARGO FLOOR PANEL 140BF HAS CRACK<[01] REMOVED AND FABRICATED NEW PANEL 140BF PER SRM 51-40-02-0G-0 AND AMM 25-52-01-201-801 INSTALLATION TO BE ACCOMPLISHED
- [SDR SWAA2024072909167](https://openairdocs.org/sdr/SWAA2024072909167), Jul 3, 2024: DOUBLER. CRACKED. CRACK FOUND AT RT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 ; 16' FROM LEADING EDGE ;I/B ROW. CRACK LENGTH : 1'. CRACK FOUND AT RT HORIZONTAL STABILIZ
- [SDR SWAA2024031463332](https://openairdocs.org/sdr/SWAA2024031463332), Mar 13, 2024: SIGN. DETACHED. RT OVERAWING EMERGENCY DOOR EXIT SIGN OFF<[01] INSTALLED RT. OVERAWING DOOR EXIT SIGN IAW AMM 33-51-04
- [SDR SWAA2024021552049](https://openairdocs.org/sdr/SWAA2024021552049), Feb 14, 2024: GIRT BAR. LOOSE. L1 DOOR ESCAPE SLIDE AFT GIRT BAR HANGER LOOSE.<[01] TIGHTENED GIRT BAR RIVETS PER SRM 51-40-02
- [SDR SWAA2024021552048](https://openairdocs.org/sdr/SWAA2024021552048), Feb 14, 2024: SEAL. CRACKED. R/H HORIZONTAL STAB AFT LOWER SLIDING SEAL CRACKED<[01] R&R RH HORIZONTAL STAB AFT LOWER SLIDING SEAL REF. SRM 51-40-02.
- [SDR SWAA2024011139740](https://openairdocs.org/sdr/SWAA2024011139740), Jan 10, 2024: HANDLE. OUT OF ADJUST. AFT ENTRY DOOR HANDLE WILL NOT FULLY STOW<[01] INSPECTED AFT ENTRY DOOR AND HANDLE; OPEN AND CLOSED DOOR SEVERAL TIMES REF AMM 52-13-00. DOOR OPS NORMAL AC OK F
- [SDR SWAA2023101109341](https://openairdocs.org/sdr/SWAA2023101109341), Oct 10, 2023: UNKNOWN. UNKNOWN. LANDING GEAR DISAGREE (RIGHT MAIN GEAR). RAN QRH AND LANDED NORMALLY<[01] COMPLETED BITE CHECK ON PSEU. NO FAULTS FOUND. CLEANED ALL SENSORS AND CHECKED THE REA
- [SDR SWAA2023100406151](https://openairdocs.org/sdr/SWAA2023100406151), Oct 1, 2023: PANEL. DELAMINATED. WTB PANEL 193B HAS SMALL AREA OF EROSION AND DELAMINATION AT L/E R/H CORNER (MARKED).<[01] R & R WTB PANEL 193B PER SRM 51-40-02
- [SDR SWAA2023081689699](https://openairdocs.org/sdr/SWAA2023081689699), Aug 14, 2023: LIGHT. MISSING. F/A REPORTS ONE STRIP OF PHOTOLUMESCENT FLOOR LIGHTING MISSING PRIOR TO AFT GALLEY LEFT HAND<[01] REPLACE MISSING PHOTO LUMINESCENT STRIP PER MM 33-51-15
- [SDR SWAA2023072883328](https://openairdocs.org/sdr/SWAA2023072883328), Jul 28, 2023: LAMP. INOPERATIVE. L/H OVERWING EMERGENCY LIGHT INOP<[01] REPLACED LAMP REF AMM 33-51-04 OPS CHECK GOOD A/C OK TO CONTINUE
- [SDR SWAA2023070573359](https://openairdocs.org/sdr/SWAA2023070573359), Jun 30, 2023: LOCK. OUT OF ADJUST. PASSENGER SEAT 11B; 11C RECLINE INTO EMERGENCY EXIT ROW<[01] ADJUSTED HYDRO-LOCKS PER AMM 25-22-00
- [SDR SWAA2023050343316](https://openairdocs.org/sdr/SWAA2023050343316), Apr 29, 2023: PANEL. ELONGATED. PANEL 193B HAS SEVERAL ELONGATED; OVERSIZED FASTENER HOLES AND DAMAGED COUNTERSINKS.<[01] LOCATED HOLES IN NEW PANEL PER SRM 51-40-05;[02] REMOVED AND REPLACED 
- [SDR SWAA2023040422890](https://openairdocs.org/sdr/SWAA2023040422890), Apr 1, 2023: STRIP. BROKEN. LIGHT STRIP ON FLOOR NEAR AFT GALLEY BROKE OFF<[01] SECURED EGRESS LIGHT STRIP PER M/M 33-51-15
- [SDR SWAA2023010989162](https://openairdocs.org/sdr/SWAA2023010989162), Jan 7, 2023: LAMP. INOPERATIVE. LEFT OVERWING EXIT WINDOW LIGHT INOP.<[01] RELAMPED LEFT OVERWING EXIT WINDOW LIGHT; SATISFACTORY OP CK REF AMM 33-21-00.
- [SDR SWAA2022090649761](https://openairdocs.org/sdr/SWAA2022090649761), Sep 3, 2022: NONE. INOPERATIVE. FWD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP / [01] RELAMPED FWD SERVICE DOOR SLIDE EMERGENCY LIGHT IAW AMM 33-51-04.
- [SDR SWAA2022081131838](https://openairdocs.org/sdr/SWAA2022081131838), Jul 21, 2022: ATTACH ANGLE. CRACKED. R/H HORIZ STAB INSPAR STA 120.30 RIB FWD ATTACH ANGLE CRACKED / [01] REMOVED AND REPLACED R/H HORIZ. STAB. INSPAR RIB ASSY. STAB. STA. 120.30 FWD ATTACH ANGLE I
- [SDR SWAA2022081029350](https://openairdocs.org/sdr/SWAA2022081029350), Jul 14, 2022: PANEL. DEBONDED. R/W L/E PANEL 621YB CONER METAL STRIP DISBONDED / [01] IDENTIFIED PANEL 621YB MATERIAL IAW SRM 57-41-01-0I-4; FIGURE 2; SHEET1; TABLE 2; ITEM [1]. <BR><BR>CLEAN

All 178: https://openairdocs.org/aircraft/N951WN/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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