# N902WN: 2007 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 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 36615
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 15, 2007
- Certificate issued: January 10, 2008
- Expires: June 30, 2029
- Mode S code: AC789B
- 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=902WN
- Page: https://openairdocs.org/aircraft/N902WN

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 model are included.

## ADs that may apply (OpenAirDocs): 19 in force

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

None in force.

### Matched by engine (CFM International CFM56-7B24 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 2021-16-08](https://openairdocs.org/ad/2021-16-08): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 55 more. Effective Sep 28, 2021
- [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 2008-03-09](https://openairdocs.org/ad/2008-03-09): Low pressure turbine rear frames (TRFs) · CFM International CFM56-7B18, CFM56-7B20, CFM56-7B22 and 10 more. Effective Mar 10, 2008
- [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
- [AD 2002-16-18](https://openairdocs.org/ad/2002-16-18): Low pressure turbine (LPT) nozzle segments · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 33 more. Effective Sep 18, 2002
- [AD 2002-13-03](https://openairdocs.org/ad/2002-13-03): Turbofan Engines · CFM International CFM56-2, CFM56-2A, CFM56-2B and 55 more. Effective Aug 1, 2002
- [AD 2001-11-05](https://openairdocs.org/ad/2001-11-05): No. 4 Bearings · CFM International CFM56-2, CFM56-2B, CFM56-3 and 45 more. Effective Jun 11, 2001
- [AD 2001-02-12](https://openairdocs.org/ad/2001-02-12): On-Wing Torque Inspection · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 11 more. Effective Feb 14, 2001
- [AD 98-21-23](https://openairdocs.org/ad/98-21-23): Electronic Engine Control · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Nov 2, 1998
- [AD 98-19-20](https://openairdocs.org/ad/98-19-20): Hydromechanical Unit · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 7 more. Effective Oct 7, 1998
- [AD 98-14-51](https://openairdocs.org/ad/98-14-51): Accessory Gearbox · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Oct 1, 1998

### 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 2019-12-05](https://openairdocs.org/ad/2019-12-05) (historical): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 39 more. Effective Jul 5, 2019
- [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
- [AD 2000-12-01](https://openairdocs.org/ad/2000-12-01) (historical): Critical Life-Limited Parts · CFM International CFM56-2, CFM56-2A, CFM56-2B and 54 more. Effective Dec 11, 2000

## 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 N902WN.

## 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 20081018849979I](https://openairdocs.org/incident/20081018849979I), Oct 18, 2008: Boeing 7377H4 (N902WN), Phoenix, AZ, Minor damage. (-23) While being pushed back from gate 1 at Phoenix Sky Harbor International Airport (phx), flight 789, southwest airlines B-737, N902WN, struck aircraft…

## Service difficulty reports (252, 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 SWAA2026060809642](https://openairdocs.org/sdr/SWAA2026060809642), Jun 6, 2026: CARTRIDGE. CRACKED. LEFT WING OTBD AFT FLAP INBD PROGRAM ROLLER CARTRIDGE ASSY; HAS A HFEC CRACK INDICATION ON THE LOWER AFT SURFACE. R & R LT WING OTBD FLAP IAW AMM 27-51-21, INSP
- [SDR SWAA2025102325987](https://openairdocs.org/sdr/SWAA2025102325987), Oct 20, 2025: MEGAPHONE. DAMAGED. FWD MEGA PHONE HANDLE RETAINING SCREW HOLE STRIPPED OUT.<[01] REMOVED AND REPLACED FWD MEGA PHONE PER MT 725-340-00-01
- [SDR SWAA2025081400262](https://openairdocs.org/sdr/SWAA2025081400262), Aug 10, 2025: LENS. DAMAGED. AFT LAV B EMERGENCY EXIT LIGHT LENS DAMAGED. REPLACED EMERGENY EXIT LIGHT LENS PER AMM 33-51-01-960-801.
- [SDR SWAA2025081892565](https://openairdocs.org/sdr/SWAA2025081892565), Jul 17, 2025: SUPPORT BRACKET. CRACKED. CRACKED LOWER O/B PULLEY BRACKET SUPPORT BS 692 LBL 25 WL 203. REMOVED. FABRICATED, AND INSTALLED LOWER O/B PULLEY BRACKET SUPPORT BS 692 LBL 25 WL 203 IAW SRM 
- [SDR SWAA2025081592307](https://openairdocs.org/sdr/SWAA2025081592307), Jul 17, 2025: STRINGER. CORRODED. CORROSION ON STRINGER; S-28L END SPLICE IN BILGE AREA AFT OF E/E COMPARTMENT DOOR CUTOUT BS350+8 LBL10 WL140.<[01] REMOVED 2 FASTENERS ON REPORTED CORROSION ARE
- [SDR SWAA2025081592012](https://openairdocs.org/sdr/SWAA2025081592012), Jul 16, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727C S-6L. REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727C S-6L IAW SRM 51-40-02-0G-0 AND DWG 146A1103 SHEET 11 REV - .
- [SDR SWAA2025081592013](https://openairdocs.org/sdr/SWAA2025081592013), Jul 16, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727E S-6L. REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727E S-6L IAW SRM 51-40-02-0G-0 AND DWG 146A1112 SHEET 1 REV C.
- [SDR SWAA2025081592014](https://openairdocs.org/sdr/SWAA2025081592014), Jul 16, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727D S-6R. REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727D S-6R IAW SRM 51-40-02-0G-0 AND DWG 146A1111 SHEET 11 REV -.
- [SDR SWAA2025081592017](https://openairdocs.org/sdr/SWAA2025081592017), Jul 16, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727E S-7R. REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727E S-7R IAW SRM 51-40-02-0G-0 AND DWG 146A1112 SHEET 1 REV C .
- [SDR SWAA2025081592015](https://openairdocs.org/sdr/SWAA2025081592015), Jul 16, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS 727C S-5R. REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727C S-5R IAW SRM 51-40-02-0G-0 AND DWG 146A1103 SHEET 11 REV - .
- [SDR SWAA2025081592016](https://openairdocs.org/sdr/SWAA2025081592016), Jul 16, 2025: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT PAX CABIN BS 727B S5R. REMOVED AND REPLACED STR CLIP AT PAX CABIN BS 727B S5R IAW SRM 51-40-02-0G-0 AND DWG 146A1102 SHEET 15 REV -.
- [SDR SWAA2025081591783](https://openairdocs.org/sdr/SWAA2025081591783), Jul 15, 2025: STUB FRAME. CRACKED. CRACK FOUND ON R1 STUB FRAME AT BS 291.5+7.5; .15' ABOVE SEAL DEPRESSOR; .6' LENGTH (MARKED)<[01] TASK CARD COMPLETED; SUMMARY STATEMENT; NO ALLOWABLE LIMITS FO
- [SDR SWAA2025081591789](https://openairdocs.org/sdr/SWAA2025081591789), Jul 15, 2025: ANGLE. CRACKED. CRACKED ANGLE BS 294.5 RBL 60 WL 208 COMMON TO I/B CHORD UPPER SIDE OF CREASE BEAM WEB.<[01] REMOVED AND REPLACED ANGLE AT BS 294.5 RBL 60; WL 208 COMMON TO I/B
- [SDR SWAA2025081591782](https://openairdocs.org/sdr/SWAA2025081591782), Jul 15, 2025: BEAR STRAP. CRACKED. CRACK FOUND ON R1 BEAR STRAP AT BS 291.5+4; WL 265.6; .6' IN LENGTH (MARKED)<[01] REPAIRED BY 737 SRM 53-10-01-2R-6 AND EA M-25-153-01539 CCN TTG8Q013R942;[02] 
- [SDR SWAA2025081491414](https://openairdocs.org/sdr/SWAA2025081491414), Jul 15, 2025: SIDEWALL SUPPORT. CORRODED. CORROSION AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B+10 TO 787+14, LBL 22, WL 156. CORROSION ON AFT CARGO BA
- [SDR SWAA2025081491415](https://openairdocs.org/sdr/SWAA2025081491415), Jul 15, 2025: SIDEWALL SUPPORT. CORRODED. CORROSION AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B+10 TO 767, RBL 22, WL 156. CORROSION ON AFT CARGO B
- [SDR SWAA2025081491416](https://openairdocs.org/sdr/SWAA2025081491416), Jul 15, 2025: SHIELD. CORRODED. CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS 767+3 TO 794, RBL 22, WL 156. CORROSION ON AFT CARGO BAY FWD SHIELD FOUND TO
- [SDR SWAA2025081491417](https://openairdocs.org/sdr/SWAA2025081491417), Jul 15, 2025: CARGO TRACK. CRACKED. AFT CARGO BAY CARGO TRACK IS CRACKED, BS 727E AND 747, RBL 13, WL 156. CRACK FOUND TO BE OUT OF LIMITS. REMOVED, AND REPLACED CARGO TRACK IAW EA 25-153-01951, A
- [SDR SWAA2025081491418](https://openairdocs.org/sdr/SWAA2025081491418), Jul 15, 2025: SPLICE STRAP. CORRODED. CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE, BS 727D+5, LBL 3 - RBL 12, WL 156. RECEIVED A NEW STRAP, APPLIED WHITE ENAMEL IAW ACO 5360-E-1
- [SDR SWAA2025081591408](https://openairdocs.org/sdr/SWAA2025081591408), Jul 14, 2025: FLOORBEAM. CRACKED. CRACKED BREAKER PANEL AT BS 540 RBL 0 - RBL 25 WL 208. REPLACED NEW BREAKER PANEL AT BS 540 RBL 0 - RBL 25 WL 208 IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND B
- [SDR SWAA2025081591409](https://openairdocs.org/sdr/SWAA2025081591409), Jul 14, 2025: FLOORBEAM. CRACKED. CRACKED BREAKER PANEL AT BS 540 LBL 0 - LBL 25 WL 208. REPLACED NEW BREAKER PANEL AT BS 540 LBL 0 - LBL 25 WL 208 IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND B
- [SDR SWAA2025081591412](https://openairdocs.org/sdr/SWAA2025081591412), Jul 14, 2025: STIFFENER. CRACKED. RIGHT HORIZONTAL STAB INSPAR AT RIB NR 1, HSS 92.70. FOUND STIFFENER NR 1 CRACKED AT LOWER END. REPAIRED RT HORIZONTAL STAB INSPAR AT RIB NR 1 VERTICAL STIFFENE
- [SDR SWAA2025081591413](https://openairdocs.org/sdr/SWAA2025081591413), Jul 14, 2025: STIFFENER. CRACKED. RIGHT HORIZONTAL STAB INSPAR AT RIB NR 4, HSS 120.30, FOUND STIFFENER NR 4 CRACKED AT LOWER END. REPAIRED RT HORIZONTAL STAB INSPAR RIB NR 4, STIFFENER NR 4 IAW
- [SDR SWAA2025081591411](https://openairdocs.org/sdr/SWAA2025081591411), Jul 14, 2025: RIB. CRACKED. LEFT HORIZONTAL STAB INSPAR AT RIB NR 4, HSS 120.30, FOUND STIFFENER NR 3 CRACKED AT LOWER END. REPAIRED LT HORIZONTAL STAB INSPAR RIB NR 4 AT STIFFENER NR 3 IA
- [SDR SWAA2025081590854](https://openairdocs.org/sdr/SWAA2025081590854), Jul 13, 2025: ANGLE. CRACKED. CRACKED ANGLE AT BS 380 - 400, LBL 11, WL 208. REMOVED, REPLACED, AND INSTALLED A NEW ANGLE IAW SRM 51-40-02 AND DWG 143A5400, SH 105, REV-.
- [SDR SWAA2025081590952](https://openairdocs.org/sdr/SWAA2025081590952), Jul 13, 2025: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM AT BS 328 RBL 25 WL 208<[01] NO ALLOWABLE DAMAGE PERMITTED UNDER SEAT TRACK ATTACHMENT PER SRM 737-700 SRM 53-10-51-1A-1 ALLOWABLE DAMAGE
- [SDR SWAA2025081591054](https://openairdocs.org/sdr/SWAA2025081591054), Jul 13, 2025: FLOORBEAM. CORRODED. CORROSION ON FASTENER HOLE ON FLOORBEAM AT BS 986 LBL 44 WL 208. EVALUATED CORROSION ON FASTENER HOLE ON FLOOR BEAM AT BS 986 LBL 44 WL 208. BLEND WAS .3'X.3'X.
- [SDR SWAA2025081590956](https://openairdocs.org/sdr/SWAA2025081590956), Jul 13, 2025: SEAT TRACK. CORRODED. CORROSION ON PASSENGER CABIN SEAT TRACK ON TOP/CROWN AND IN WELL AT BS 480 - 520 LBL 25 WL 208. SEAT TRACK TO BE REPLACED ON TTG8Q013Q2ZW.
- [SDR SWAA2025081590963](https://openairdocs.org/sdr/SWAA2025081590963), Jul 13, 2025: SEAT TRACK. CORRODED. CORROSION ON PASSENGER CABIN SEAT TRACK ON TOP/CROWN AND IN WELL AT BS 480 - 520 LBL 45 WL 208. SEAT TRACK WILL BE REPLACED ON TTG8Q013Q302.
- [SDR SWAA2025081590964](https://openairdocs.org/sdr/SWAA2025081590964), Jul 13, 2025: SEAT TRACK. CORRODED. CORROSION ON PASSENGER CABIN SEAT TRACK ON TOP/CROWN AND IN WELL AT BS 540 - 727B LBL 25 WL 208. AREA BLENDED IS L=5'' BY W=.5'' BY D=.024''. FOUND TO BE OUT OF
- [SDR SWAA2025081590960](https://openairdocs.org/sdr/SWAA2025081590960), Jul 13, 2025: SEAT TRACK. CORRODED. CORROSION ON PASSENGER CABIN SEAT TRACK ON TOP/CROWN AND IN WELL AT BS 540 - 727B LBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK SECTION BS 540 - 727B LBL 45 DU
- [SDR SWAA2025081590974](https://openairdocs.org/sdr/SWAA2025081590974), Jul 13, 2025: SEAT TRACK. CORRODED. CORROSION ON PASSENGER CABIN SEAT TRACK ON TOP/CROWN AND IN WELL AT BS 540 - 727B RBL 25 WL 208. REMOVED CORROSION ON TOP OF PAX CABIN SEAT TRACK AT BS 540-0727
- [SDR SWAA2025081491050](https://openairdocs.org/sdr/SWAA2025081491050), Jul 13, 2025: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT AT BS 951, RBL 35, WL 208. EVALUATED CORROSION ON FLOOR SUPPORT AT BS 951 RBL 35 WL 208. BLEND WAS 4'X.6'X.008'. FOUND TO BE OUT OF L
- [SDR SWAA2025081491053](https://openairdocs.org/sdr/SWAA2025081491053), Jul 13, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 232RF DELAMINATED. REPLACEMENT FLOOR PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0 ALONG WITH DWG 144A5810 SHEET 124.
- [SDR SWAA2025081590853](https://openairdocs.org/sdr/SWAA2025081590853), Jul 12, 2025: ANGLE. CRACKED. CRACKED ANGLE AT BS 380 - 400 RBL 11 WL 208<[01] REMOVED; REPLACED; AND INSTALLED A NEW ANGLE AT BS 380-400; RBL11; WL 208 IAW SRM 51-40-02 AND BOEING DWG 143A5
- [SDR SWAA2025081590605](https://openairdocs.org/sdr/SWAA2025081590605), Jul 11, 2025: SHEAR WEB. CORRODED. CORROSION ON L/H SHEAR WEB AT BS 1026 LBL 22 WL 208<[01] SHEAR WEB FOUND TO BE OUT LIMITS; PART REMOVED AND REPLACED SHEAR WEB AT BS 1016 TO BS 1033 LBL0 TO LBL
- [SDR SWAA2025081590606](https://openairdocs.org/sdr/SWAA2025081590606), Jul 11, 2025: STRAP. CORRODED. CORROSION ON STRAP AT BS 1016 LBL 3 WL 208<[01] STRAP FOUND TO BE OUT LIMITS; PART REMOVED AND REPLACED AT BS 1016 TO BS 1029 LBL3 TO LBL39 WL 208 PER I.A.W SRM
- [SDR SWAA2025081590609](https://openairdocs.org/sdr/SWAA2025081590609), Jul 11, 2025: SHEAR WEB. CORRODED. CORROSION ON STRAP ON R/H SHEAR WEB AT BS 1028.5 RBL 18 WL 208. STRAP FOUND TO BE OUT LIMITS; PART REMOVED AND REPLACED BS 1016-BS1029 RBL18 WL 208 PER I.A.W SR
- [SDR SWAA2025081590612](https://openairdocs.org/sdr/SWAA2025081590612), Jul 11, 2025: FLOORBEAM. CORRODED. CORROSION AROUND NUT PLATE HOLE FASTENER AT BS 986 RBL 43 WL 208. EVALUATED CORROSION AROUND NUT PLATE HOLE FASTENER AT BS 986 RBL 43 WL 208. BLEND WAS 1'X.3'X.
- [SDR SWAA2025081490433](https://openairdocs.org/sdr/SWAA2025081490433), Jul 11, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 241XF DELAMINATED. CABIN FLOOR PANEL 241XF WITH DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025081490434](https://openairdocs.org/sdr/SWAA2025081490434), Jul 11, 2025: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 241ZF DELAMINATED. CABIN FLOOR PANEL 241ZF DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025081490608](https://openairdocs.org/sdr/SWAA2025081490608), Jul 11, 2025: SUPPORT FITTING. CORRODED. CORROSION ON AFT LAV MOUNT SUPPORT FITTING ON STRUCTURE AT BS 1021, LBL 1, WL 208. REMOVED AFT LAV MOUNT SUPPORT FITTING ON STRUCTURE AT BS 1021 LBL 1 WL 208 IA
- [SDR SWAA2025081590303](https://openairdocs.org/sdr/SWAA2025081590303), Jul 10, 2025: SCUFF PLATE. CRACKED. AED (L2) SCUFF PLATE REQUIRES REPLACEMENT<[01] UPDATED TABLE MEASUREMENT;[02] REPLACED DAMAGE SCUFF PLATE DUE TO NO LIMITS FOUND ALL I.A.W SRM 51-10-02-0G-0 PAR
- [SDR SWAA2025081489866](https://openairdocs.org/sdr/SWAA2025081489866), Jul 10, 2025: LIGHT. DAMAGED. G-4 EXIT LIGHT IS DAMAGED. REMOVED AND REPLACED G-4 EXIT LIGHT PER AMM 33-51-01-960-802. OPS CHECK TEST GOOD.
- [SDR SWAA2025081589592](https://openairdocs.org/sdr/SWAA2025081589592), Jul 9, 2025: DOOR. CRACKED. LEFT MAIN GEAR CENTER DOOR IS CRACKED, JUST FWD OF FWD HINGE ATTACH POINT. REMOVED AND REINSTALLED LT MLG CENTER DOOR IAW AMM 32-13-11.
- [SDR SWAA2025081489273](https://openairdocs.org/sdr/SWAA2025081489273), Jul 8, 2025: LENS. BROKEN. LAV A EXIT LENS IS BROKEN. REMOVED AND REPLACED LAV A EXIT LENS PER AMM 33-51-01-960-802. OPS CHECK TEST GOOD.
- [SDR SWAA2024110155088](https://openairdocs.org/sdr/SWAA2024110155088), Oct 31, 2024: BATTERY PACK. NO TEST. PASSENGER CABIN; FWD EMERGENCY EXIT LT BATTERY PACK M1674 FAILED CAPACITY TEST/CHECK.<[01] R&R PASSENGER CABIN FWD EMERGENCY EXIT LT BATTERY PACK M1674 IAW AMM 
- [SDR SWAA2024110155089](https://openairdocs.org/sdr/SWAA2024110155089), Oct 31, 2024: BATTERY PACK. NO TEST. PASSENGER CABIN; FWD EMERGENCY EXIT LT BATTERY PACK M1675 FAILED CAPACITY TEST/CHECK.<[01] R&R PASSENGER CABIN; FWD EMERGENCY EXIT LT BATTERY PACK M1675 IAW AMM
- [SDR SWAA2024102149323](https://openairdocs.org/sdr/SWAA2024102149323), Oct 16, 2024: BATTERY. NO TEST. FA REPORTS AFT GAL FLASH LIGHT NOT TESTING<[01] OK TO CONTINUE PER MEL 25-12-01 SP1B AUTHORIZATION# 219007;[02] REMOVED AND REPLACED AFT GALLEY EMERGENCY FLASHL
- [SDR SWAA2024101446436](https://openairdocs.org/sdr/SWAA2024101446436), Oct 8, 2024: LIGHT. INOPERATIVE. EMERGENCY EXIT LT AT 13DEF INOP.<[01] RELAMPED EMERGENCY EXIT LIGHT AT 13DEF IAW AMM 31-51-03.

All 252: https://openairdocs.org/aircraft/N902WN/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 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 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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