# N799SW: Boeing 737-7Q8

- Status: Valid registration
- Airframe: [Boeing 737-7Q8](https://openairdocs.org/model/boeing-737-7q8) (registry code 1384418, 149 seats)
- Serial number: 28209
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Certificate issued: February 15, 2017
- Expires: February 28, 2030
- Mode S code: AADB19
- Registered owner: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=799SW
- Page: https://openairdocs.org/aircraft/N799SW

From the FAA registry file of October 20, 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.

## ADs that may apply (OpenAirDocs): 0 in force

### Matched by airframe (Boeing 737-7Q8)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA11IA047](https://openairdocs.org/ntsb/DCA11IA047), Apr 26, 2011: Boeing 737-7Q8 (N799SW), Chicago, IL, incident, minor damage. Probable cause: The flight crew's delayed deployment of the speedbrakes and thrust reversers, resulting in insufficient runway remaining to bring the airplane to a stop. Contributing to the delay in deployment of…

## 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; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20110426006929I](https://openairdocs.org/incident/20110426006929I), Apr 26, 2011: Boeing 737-7Q8 (N799SW), Chicago, IL, Minor damage. Aircraft landed 13C at Chicago midway and went off the left side at the end. The runway was wet with standing water.

## Service difficulty reports (334, newest 50)

As reported by operators and repair stations.

- [SDR SWAA2022011260075](https://openairdocs.org/sdr/SWAA2022011260075), Jan 10, 2022: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1675 ARE INOP. ; / [01] REPLACED BATTERY PACK M1675 AND PERFORMED GOOD INSTALLATION TEST PER PER AMM 33-51-0
- [SDR SWAA2022011260076](https://openairdocs.org/sdr/SWAA2022011260076), Jan 10, 2022: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1672 ARE INOP ; / [01] EMERGENCY LIGHTS BATTERY PACK M1672 REPLACED WITH SERVICEABLE BATTERY PACK AND PERFOR
- [SDR SWAA2021091015055](https://openairdocs.org/sdr/SWAA2021091015055), Sep 6, 2021: LAMP. INOPERATIVE. FWD SERVICE DOOR SLIDE EMERGENCY LIGHT INOP ; / [01] REPLACED LAMP PER MM 33-51-04
- [SDR SWAA2021080400541](https://openairdocs.org/sdr/SWAA2021080400541), Jul 31, 2021: COVER. LOOSE. LH OVERWING EXIT COVER FELL OFF ; / [01] REATTACHED COVER PER SIP
- [SDR SWAA2021080298996](https://openairdocs.org/sdr/SWAA2021080298996), Jul 27, 2021: BATTERY PACK. FAILED. EMERGENCY EXIT LIGHT BATTERY PACK M1668 (STA 603 WL 213 LBL67) INOP; WILL NOT TAKE CHARGE / [01] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1668 PER AMM 33-51-
- [SDR SWAA2021080298995](https://openairdocs.org/sdr/SWAA2021080298995), Jul 27, 2021: BATTERY PACK. INOPERATIVE. EMER AISLE LIGHT BETWEEN SEAT ROW 6ABC AND 7ABC INOP / [01] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1668 PER AMM 33-51-06-960-805 ATAG PS0937 OPS CHECK GOOD
- [SDR SWAA2021072697812](https://openairdocs.org/sdr/SWAA2021072697812), Jul 22, 2021: SCUFF PLATE. CRACKED. AFT CARGO CENTER SCUFF PLATE FOUND TO BE CRACKED DURING INSPECTION. REMOVED DAMAGED CENTER SCUFF PLATE FROM AFT CARGO DOOR CUTOUT IAW SRM 51-40-02-0G-0. INSTALL
- [SDR SWAA2021071994541](https://openairdocs.org/sdr/SWAA2021071994541), Jul 13, 2021: FASTENER. MISSING. PASSENGER CABIN RIGHT EMERGENCY EXIT HANDLE MISSING HARDWARE ; / [01] INSTALLED MISSING 1/4 TURN FASTENER PER S.I.P.
- [SDR SWAA2021062586282](https://openairdocs.org/sdr/SWAA2021062586282), Jun 21, 2021: SLIDE. OUT OF POSITION. FORWARD SERVICE DOOR SLIDE NEEDS TO BE REPACKED- COMING LOOSE ; / [01] REPOSITIONED SLIDE PER STEP C OF MX TASK 725-61-06
- [SDR SWAA2021050768140](https://openairdocs.org/sdr/SWAA2021050768140), May 3, 2021: HANDLE. EXPOSED. FWD SERVICE DOOR SLIDE HANDLE EXPOSED ; FWD SERVICE DOOR SLIDE HANDLE EXPOSED / REPOSITIONED FWD SVC DOOR SLIDE HANDLE IAW AMM 25-66-01
- [SDR SWAA2020122938623](https://openairdocs.org/sdr/SWAA2020122938623), Dec 27, 2020: SLIDE. OUT OF POSITION. THE RED 'PULL HANDLE' IS VISIBLE WHEN RIGHT (FIRST OFFICER) SIDE SERVICE DOOR IS ARMED. REPACKED SLIDE IN SHELL, PER MT 725-61-06 FOR R2 DOOR CHECKS OK.
- [SDR SWAA2020032442783](https://openairdocs.org/sdr/SWAA2020032442783), Mar 18, 2020: RETAINER. FAULTY. L2 HEADER PANEL EMERGENCY EXIT SIGN LENS RETAINER WILL NOT ENGAGE REMOVED AND REPLACED/REINSTALLED L2 HEADER PANEL EMERGENCY EXIT SIGN LENS RETAINER IAW BOEING 
- [SDR SWAA2020040131301](https://openairdocs.org/sdr/SWAA2020040131301), Mar 13, 2020: DOOR FRAME. CRACKED. PASSENGER CABIN; L-2 DOOR CUTOUT; STA 951+5; 15' ABOVE FLOOR; STUB FRAME IS CRACKED JUST ABOVE ROLLER LATCH RECIVER (MARKED IN RED) MOD / REPAIRED THE L2 DOOR S
- [SDR SWAA2021082727071](https://openairdocs.org/sdr/SWAA2021082727071), Mar 9, 2020: BALANCE WEIGHT. CORRODED. RIGHT AILERON 2 BALANCE WEIGHTS BETWEEN 2 AND 3 HINGE CORRODED / REMOVED AND REPLACED THE R/H AILERON 2 BALANCE WEIGHTS BETWEEN 2 AND 3 HINGE IAW SOPM 20-50-01 
- [SDR SWAA2020032442782](https://openairdocs.org/sdr/SWAA2020032442782), Mar 8, 2020: WIRE. PULLED. PASSENGER CABIN EMERGENCY LIGHTS, GROUND BLOCK NO. GD03764 AT STATION 767 STRINGER 4L WIRE NO. W3142-0456-20 PULLED FROM CONNECTION. REPAIRED WIRE W3142-0456-20
- [SDR SWAA2020040127052](https://openairdocs.org/sdr/SWAA2020040127052), Feb 27, 2020: SPLICE PLATE. DAMAGED. (AD RELATED REF. SWA SI # 11932-53) UPPER FUSELAGE BUTT JOINT SPLICE PLATE AT STA 360 BETWEEN STR 4L-6L HAS SCRIBE DAMAGE APPROX 4' LONG. / REPAIRED SCRIBE DAMA
- [SDR SWAA2020040127044](https://openairdocs.org/sdr/SWAA2020040127044), Feb 26, 2020: SEAT TRACK. CRACKED. COCKPIT FLOOR CAPTAIN FWD INBD SEAT TRACK RAIL IS CRACKED AT FWD STOP PIN HOLE. / INSTALLED REPLACEMENT SEAT TRACK FOR CAPTAIN FWD INBD POSITION IAW AMM 25-11-1
- [SDR SWAA2020040127045](https://openairdocs.org/sdr/SWAA2020040127045), Feb 26, 2020: SEAT TRACK. CRACKED. COCKPIT FLOOR CAPTAIN AFT INBD SEAT TRACK STOP PIN RAIL HAS HEAVY WEAR. / INSTALLED REPLACEMENT SEAT TRACK FOR CAPTAIN AFT INBD TRACK IAW AMM 25-11-11-400-801 A
- [SDR SWAA2020040127046](https://openairdocs.org/sdr/SWAA2020040127046), Feb 26, 2020: SEAT TRACK. WORN. COCKPIT FLOOR CAPTAIN AFT OTBD SEAT TRACK & STOP PIN RAILS HAVE HEAVY WEAR. / INSTALLED REPLACEMENT SEAT TRACK FOR CAPTAIN AFT OUTBD TRACK IAW AMM 25-11-11-400-
- [SDR SWAA2020040127047](https://openairdocs.org/sdr/SWAA2020040127047), Feb 26, 2020: SEAT TRACK. CRACKED. COCKPIT FLOOR FIRST OFFICER FWD INBD SEAT TRACK RAIL IS CRACKED AT FWD STOP PIN HOLE. / INSTALLED REPLACEMENT SEAT TRACK FOR FIRST OFFICER FWD INBD POSITION IAW
- [SDR SWAA2020040127048](https://openairdocs.org/sdr/SWAA2020040127048), Feb 26, 2020: SEAT TRACK. WORN. COCKPIT FLOOR FIRST OFFICER AFT INBD SEAT TRACK STOP PIN RAIL HAS HEAVY WEAR. / INSTALLED REPLACEMENT SEAT TRACK FOR FIRST OFFICER AFT INBD POSITION IAW AMM 25-
- [SDR SWAA2021082727040](https://openairdocs.org/sdr/SWAA2021082727040), Feb 25, 2020: BALANCE WEIGHT. CORRODED. RIGHT WING AILERON NOSE FITTING BAY #5; 5 EACH BALANCE WEIGHTS SHOW SIGNS OF CORROSION / REMOVED; REPLACED; AND VERIFIED PARTS FOR RIGHT WING AILERON NOSE FITTI
- [SDR SWAA2020040127039](https://openairdocs.org/sdr/SWAA2020040127039), Feb 25, 2020: SPLICE. CORRODED. AFT CARGO BAY FLOOR SPLICE AT BS 887; LBL16 TO RBL 16; WL 162 CORRODED. / REFERENCE NRC Y174595 FOR WORK ACCOMPLISHED. AFT CARGO BAY FLOOR SPLICE AT BS 887 LBL 
- [SDR SWAA2020030642207](https://openairdocs.org/sdr/SWAA2020030642207), Feb 25, 2020: FLOOR PANEL. DELAMINATED. FLOOR PANEL 221DF LOWER SURFACE O/B SCALLOPED AREA IS DELAMED. REPAIRED FLOOR PANEL 221 DF LOWER SURFACE O/B SCALLOPED AREA IAW B 737-700 SRM'S 53-00-50-2R-1 RE
- [SDR SWAA2020040127029](https://openairdocs.org/sdr/SWAA2020040127029), Feb 18, 2020: FITTING. CORRODED. AFT CARGO COMPT. STA 727D+6; S-27R; WL150 (FWD) CLIP P/N 146A7734-2 HAS CORROSION REPLACED ON NON-ROUTINE Y174547 / AFT CARGO COMPARTMENT STA 727D+6' S-27R WL 1
- [SDR SWAA2020040127030](https://openairdocs.org/sdr/SWAA2020040127030), Feb 18, 2020: FITTING. CORRODED. AFT CARGO COMPT. STA 727D+6; S-27R; WL150 (AFT) CLIP P/N 146A7734-2 HAS CORROSION REPLACED ON NON-ROUTINE Y174547 / AFT CARGO COMPARTMENT STA 727D+6' WL 150 (AF
- [SDR SWAA2020040127031](https://openairdocs.org/sdr/SWAA2020040127031), Feb 18, 2020: FITTING. CORRODED. AFT CARGO COMPT. STA 727D+6; S-27L; WL150 (AFT) CLIP P/N 146A7734-2 HAS CORROSION REPLACED ON NON-ROUTINE Y174548 / AFT CARGO COMPARTMENT STA 727D+6' S-27L WL 1
- [SDR SWAA2020040127027](https://openairdocs.org/sdr/SWAA2020040127027), Feb 18, 2020: FLOOR PANEL. FRAYED. FLOOR PANEL 221DF; TOP SURFACE FRAYED IN SEVERAL AREAS. (NOTE: RED DOT IS NUMBER 101-002) / REAPIRED FLOOR PANEL 221DF TOP SURFACE AS MARKED FRAYED SURFACES I/A
- [SDR SWAA2020022874835](https://openairdocs.org/sdr/SWAA2020022874835), Feb 14, 2020: FLOOR SUPPORT. CRACKED. AFT CARGO INTERCOSTAL CRACKED BETWEEN BS. 927 TO BS. 947.5, RBL 20. / R&R INTERCOSTAL IAW SRM & DWG.
- [SDR SWAA2020032442803](https://openairdocs.org/sdr/SWAA2020032442803), Feb 12, 2020: ATTACH ANGLE. CRACKED. RIGHT LOWER FUSELAGE - STA. 663 - WHERE VAPOR BARRIER ANGLE ATTACHES TO THE 663 ANGLE - IS CRACKED AT RBL 7. REPAIRED LOWER FUSELAGE BS 663 VAPOR BARRIER ANGLE 
- [SDR SWAA2020031242403](https://openairdocs.org/sdr/SWAA2020031242403), Feb 12, 2020: STRINGER SPLICE. CORRODED. CUSTOMER REQUEST SWA QC REP MDB. AD DRIVEN. E&E COMPARTMENT AFT OF STA 360, STR 27R STRINGER SPLICE IS CORRODED (STA 362, STR 27R, WL 150). STRINGER SPLICE IN E
- [SDR SWAA2020040126970](https://openairdocs.org/sdr/SWAA2020040126970), Feb 11, 2020: STIFFENER. CRACKED. BS 663; VAPOR BARRIER WEB; VERTICAL STIFFENER AT RBL 28; LOWER END CRACKED. / REMOVED AND REPLACED STIFFNER PART# 111A130816 AT STA 663 RBL 25 PER SRM 51-40-02-
- [SDR SWAA2020040126988](https://openairdocs.org/sdr/SWAA2020040126988), Feb 11, 2020: STRINGER. CORRODED. E/E COMPARTMENT AFT END OF STRINGER 29 STA 312+11 HAS CORROSION ON RIGHT VERTICAL WEB CAUSING A LARGE FLAKE TO COME OFF / REPAIRED S-29 AT BS 312+11' IAW EA# 20
- [SDR SWAA2020021941465](https://openairdocs.org/sdr/SWAA2020021941465), Feb 10, 2020: BULKHEAD WEB. CRACKED. EXISTING REPAIR ON VAPOR BARRIER WEB CRACKED AND DISBONDED AT BS. 663, RBL 11. / REPAIRED WEB IAW SRM.
- [SDR SWAA2020022741779](https://openairdocs.org/sdr/SWAA2020022741779), Feb 8, 2020: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED BETWEEN BS. 294 TO BS. 312, STR. 4L. / R&R INTERCOSTAL IAW SRM AND DWG.
- [SDR SWAA2020040126838](https://openairdocs.org/sdr/SWAA2020040126838), Feb 7, 2020: FLOOR PANEL. DAMAGED. FLOOR PANEL 231XF HAS FIBERS PULLED FROM TOP SURFACE FROM TAPE REMOVAL / FABRICATED NEW PASSENGER CABIN FLOOR PANEL 231 XF PER SAMPLE OF ORIGINAL I/A/W SRM 53-0
- [SDR SWAA2020040126839](https://openairdocs.org/sdr/SWAA2020040126839), Feb 7, 2020: FLOOR PANEL. DAMAGED. FLOOR PANEL 232RF HAS FIBERS PULLED FROM TOP SURFACE FROM TAPE REMOVAL / FABRICATED NEW PASSENGER CABIN FLOOR PANEL 232 RF PER SAMPLE OF ORIGINAL I/A/W SRM 53-0
- [SDR SWAA2020040126840](https://openairdocs.org/sdr/SWAA2020040126840), Feb 7, 2020: FLOOR PANEL. DAMAGED. FLOOR PANEL 231ZF HAS FIBERS PULLED FROM TOP SURFACE FROM TAPE REMOVAL / FABRICATED NEW FLOOR PANEL 231ZF (NEW) PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 R
- [SDR SWAA2020040126841](https://openairdocs.org/sdr/SWAA2020040126841), Feb 7, 2020: FLOOR PANEL. DAMAGED. FLOOR PANEL 232SF HAS FIBERS PULLED FROM TOP SURFACE FROM TAPE REMOVAL / FABRICATED NEW FLOOR PANEL 232SF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69;
- [SDR SWAA2020040126842](https://openairdocs.org/sdr/SWAA2020040126842), Feb 7, 2020: FLOOR PANEL. DAMAGED. FLOOR PANEL 242BF HAS FIBERS PULLED FROM TP SURFACE FROM TAPE REMOVAL / FABRICATED NEW FLOOR PANEL 242 BF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69;
- [SDR SWAA2020040126843](https://openairdocs.org/sdr/SWAA2020040126843), Feb 7, 2020: FLOOR PANEL. DAMAGED. FLOOR PANEL 231YF HAS FIBERS PULLED FROM TOP SURFACE FROM TAPE REMOVAL / FABRICATED NEW FLOOR PANEL 231 XF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69
- [SDR SWAA2020040126877](https://openairdocs.org/sdr/SWAA2020040126877), Feb 7, 2020: FLOORBOARD. DAMAGED. AFT GALLEY/LAV WET AREA; FLOORBOARD 241ABF; HAS COMPOSITE FIBER DAMAGE. / REPAIRED PASSENGER CABIN FLOOR PANEL 241ABF IAW SRM 53-00-50-2R-0 GENERAL REPAIR REV 6
- [SDR SWAA2020040126872](https://openairdocs.org/sdr/SWAA2020040126872), Feb 7, 2020: FLOORBOARD. DAMAGED. AFT GALLEY/LAV WET AREA; FLOORBOARD 241ACF;HAS COMPOSITE FIBER DAMAGE . / REPAIRED PASSENGER CABIN FLOOR PANEL 241ACF IAW SRM 53-00-50-2R-0 GENERAL REPAIR 69 AN
- [SDR SWAA2020040126867](https://openairdocs.org/sdr/SWAA2020040126867), Feb 7, 2020: FLOORBOARD. DAMAGED. AFT GALLEY/LAV WET AREA; FLOORBOARD 241XF;HAS COMPOSITE FIBER DAMAGE . / REPAIRED PASSENGER CABIN FLOOR PANEL 241XF IAW SRM 53-00-50-2R-0 GENERAL REPAIR AND SRM
- [SDR SWAA2020040126860](https://openairdocs.org/sdr/SWAA2020040126860), Feb 7, 2020: FLOORBOARD. DAMAGED. PASSENGER CABIN FLOOR BOARD # 242 AF TOP SKIN PLY SURFACE AREA ;IN THE CENTER FWD SECTION OF BOARD; FIBERS ARE DAMAGED / REPAIRED PASSENGER CABIN FLOOR PANEL 24
- [SDR SWAA2020040126861](https://openairdocs.org/sdr/SWAA2020040126861), Feb 7, 2020: FLOORBOARD. PUNCTURED. PASSENGER CABIN FLOOR BOARD # 242 AF OUTBD OF #4 INSERT ON THE L/H/S TOP SKIN PLIES OF BOARD ARE PUNTURED AS MARKED / REPAIRED PASSENGER CABIN FLOOR PANEL 242 A
- [SDR SWAA2020040126862](https://openairdocs.org/sdr/SWAA2020040126862), Feb 7, 2020: FLOORBOARD. DAMAGED. PASSENGER CABIN FLOOR BOARD # 241 AF TOP SKIN PLY SURFACE THE LENGTH AND WIDTH OF BOARD; IN SEVERAL AREAS FIBERS ARE DAMAGED / FABRICATED NEW PASSENGER CABIN FL
- [SDR SWAA2020040126859](https://openairdocs.org/sdr/SWAA2020040126859), Feb 7, 2020: FLOORBOARD. DAMAGED. PASSENGER CABIN FLOOR BOARD # 241 BF TOP SKIN PLY SURFACE THE LENGTH AND WIDTH OF BOARD; IN SEVERAL AREAS FIBERS ARE DAMAGED / FABRICATED NEW PASSENGER CABIN FL
- [SDR SWAA2020040126858](https://openairdocs.org/sdr/SWAA2020040126858), Feb 7, 2020: FLOORBOARD. DAMAGED. PASSENGER CABIN FLOOR BOARD # 241 DF TOP SKIN PLY SURFACE THE LENGTH AND WIDTH OF BOARD; IN SEVERAL AREAS FIBERS ARE DAMAGED / FABRICATED NEW PASSENGER CABIN FL
- [SDR SWAA2020040126857](https://openairdocs.org/sdr/SWAA2020040126857), Feb 7, 2020: FLOORBOARD. DAMAGED. PASSENGER CABIN FLOOR BOARD # 241 EF TOP SKIN PLY SURFACE THE LENGTH AND WIDTH OF BOARD; IN SEVERAL AREAS FIBERS ARE DAMAGED / FABRICATED NEW PASSENGER CABIN FL

All 334: https://openairdocs.org/aircraft/N799SW/reports.md

## Related

- Other Boeing 737-7Q8 aircraft: https://openairdocs.org/model/boeing-737-7q8/aircraft.md
- STCs for the Boeing 737-7Q8: https://openairdocs.org/model/boeing-737-7q8/stcs.md

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