# N770SA: 2000 Boeing 737-7H4, registration cancelled 2024-10-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 4, 2024
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-7H4](https://openairdocs.org/model/boeing-737-7h4) (registry code 1384404)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 30589
- Year built: 2000
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 28, 2000
- Certificate issued: August 2, 2000
- Last registry action: April 21, 2023
- Mode S code: AA6A98
- Owner when cancelled: [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 was based
- The mark today: https://openairdocs.org/aircraft/N770SA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=770SA
- Page: https://openairdocs.org/deregistered/N770SA-2024-10-04

From the FAA registry file of November 12, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 737-7H4: https://openairdocs.org/model/boeing-737-7h4.md

## Service difficulty reports (290, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR SWAA2023080284897](https://openairdocs.org/sdr/SWAA2023080284897), Aug 2, 2023: GIRT BAR. OUT OF ADJUST. FWD ENTRY DOOR RIGHT SIDE GIRT BAR STOWAGE BRACKET LOOSE<[01] ADJUSTED FWD ENTRY SLIDE RH GIRT BAR BRACKET PER AMM 25-66-01
- [SDR SWAA2023071979812](https://openairdocs.org/sdr/SWAA2023071979812), Jul 17, 2023: GIRT BAR. OUT OF ADJUST. CREW REPORTS FWD SERVICE DOOR EMERGENCY ESCAPE SLIDE GIRT BAR TIGHT<[01] ADJUSTED FWD SERVICE DOOR GIRT BAR PER AMM 25-66-01
- [SDR SWAA2023062771542](https://openairdocs.org/sdr/SWAA2023062771542), Jun 25, 2023: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS IN BIN NOSE AT LT OVERWING EXIT INOP<[01] R&R?D BATTERY AND CHARGER ASSEMBLY AT STA.729C LT 33-51-06
- [SDR SWAA2023062771543](https://openairdocs.org/sdr/SWAA2023062771543), Jun 25, 2023: LIGHT. INOPERATIVE. REF [TTG8Q00LUTTB] MULTIPLE OVERHEAD BIN EMERGENCY LIGHTS INOP. PART CORRECTION.<[01] CORRECTION TO PART USEAGE. REF TTG8Q00LUTTB FOR ORIGINAL CORRECTIVE ACTION
- [SDR SWAA2023062771541](https://openairdocs.org/sdr/SWAA2023062771541), Jun 25, 2023: BATTERY PACK. INOPERATIVE. MULTIPLE OVERHEAD BIN EMERGENCY LIGHTS INOP.<[01] REPLACED FWD CABIN BATTERY PACK AND BATTERY CHARGER ASSY; SATISFACTORY OP CK REF AMM 33-51-06.
- [SDR SWAA2023052451271](https://openairdocs.org/sdr/SWAA2023052451271), May 23, 2023: BATTERY PACK. INOPERATIVE. AFT ASILE EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06
- [SDR SWAA2023041124598](https://openairdocs.org/sdr/SWAA2023041124598), Apr 7, 2023: LENS. MISSING. CAPT SIDE LOWER EMERGENCY EXIT LIGHT LENSE MISSING.<[01] RE-INSTALLED CAPTAIN SIDE EMERGENCY EXIT SIGN LENSE REF AMM 33-51-01
- [SDR SWAA2023031616087](https://openairdocs.org/sdr/SWAA2023031616087), Mar 14, 2023: SEAL. CRACKED. RH HORIZONTAL STAB UPPER SLIDER BROKEN<[01] REMOVED AND REPLACED SEAL PER AMM 53-31-31.
- [SDR SWAA2023030210609](https://openairdocs.org/sdr/SWAA2023030210609), Feb 27, 2023: SIGN. BROKEN. FORWARD EMERGENCY EXIT SIGN BROKEN<[01] R AND R SIGN PER MM 33-51-01
- [SDR SWAA2023022409620](https://openairdocs.org/sdr/SWAA2023022409620), Feb 23, 2023: STRIP. LOOSE. APPROX 18 INCHES OF PHOTOLUMINESCENT STRIP NOT SECURED AT ROW 12<[01] REF AMM 33-51-15 SECURED STRIP AS REQUIRED. OK FOR SERVICE
- [SDR SWAA2022120678848](https://openairdocs.org/sdr/SWAA2022120678848), Dec 5, 2022: MEGAPHONE. INOPERATIVE. FORWARD CABIN FLIGHT ATTENDANT MEGAPHONE INOP. R & R FWD GALLEY MEGAPHONE PER AMM 25-64-00.
- [SDR SWAA2022112373857](https://openairdocs.org/sdr/SWAA2022112373857), Nov 21, 2022: LENS. UNSECURE. THE LOWER EXIT SIGN COVER AT THE LEFT OVER WING EXIT IS NOT SECURE. RE-INSTALLED COVER PER SIP
- [SDR SWAA2022050904878](https://openairdocs.org/sdr/SWAA2022050904878), May 5, 2022: SENSOR. POPPED. FLAPS DID NOT EXTEND WHEN FLAPS 5 SELECTED. ALTERNATED ALTERNATE FLAP EXTENSION. ONLY RH SIDE FLAPS MOVED. LEFT STAYED UP. PERFORMED A NO FLAP LAND. UNEVENTFUL 
- [SDR SWAA2022050903692](https://openairdocs.org/sdr/SWAA2022050903692), May 4, 2022: SENSOR. FAULTY. FLAPS DID NOT COME DOWN WHEN SELECTING FLAPS TO 5. WHEN USING ALTERNATE FLAP EXTENSION; ONLY RIGHT SIDE FLAPS STARTED MOVING. LEFT SIDE FLAPS STAYED AT UP POSIT
- [SDR SWAA2022050301406](https://openairdocs.org/sdr/SWAA2022050301406), May 1, 2022: BULB. INOPERATIVE. BULBS OUT ON EMERGENCY EXIT LIGHTS JUST FORWARD OF FED & FSD. / [01] REMOVED AND RELAMPED FLIGHT ENTRY DOOR EMERGENCY EXIT LIGHT BULB (1) EACH AND PERFORMED GOO
- [SDR SWAA2022050302438](https://openairdocs.org/sdr/SWAA2022050302438), May 1, 2022: BULB. INOPERATIVE. BULBS OUT ON EMERGENCY EXIT LIGHTS JUST FORWARD OF FED & FSD. / [01] REMOVED AND RELAMPED FLIGHT ENTRY DOOR EMERGENCY EXIT LIGHT BULB (1) EACH AND PERFORMED GOO
- [SDR SWAA2022050400884](https://openairdocs.org/sdr/SWAA2022050400884), Apr 29, 2022: SUPPORT. CRACKED. CRACKED FLOOR SUPPORT AT STA 540; RBL 1; WL 208. / [01] REMOVED AND REPLACED FLOOR SUPPORT AT STA 540; RBL1; WL 208 IAW SRM 51-40-02 AND BOEING DWG 143A0060. MA
- [SDR SWAA2022050400886](https://openairdocs.org/sdr/SWAA2022050400886), Apr 29, 2022: SUPPORT. CRACKED. CRACKED FLOOR SUPPORT AT STA 540; LBL 1; WL 208. / [01] REMOVED AND REPLACED FLOOR SUPPORT AT STA 540; LBL1; WL 208 IAW SRM 51-40-02 AND BOEING DWG 143A0060. MA
- [SDR SWAA2022010655176](https://openairdocs.org/sdr/SWAA2022010655176), Dec 21, 2021: STRINGER. CORRODED. SUPPLEMENTAL INFORMATION: CORROSION FOUND ON STR28R AT 364 ; / [01] REMOVED PAINT BY STRIPPING AT LWR FUSELAGE SKIN S-28R BETWEEN STA 360 AND STA 400 REF B737-7
- [SDR SWAA2022010454625](https://openairdocs.org/sdr/SWAA2022010454625), Dec 20, 2021: BATTERY PACK. INOPERATIVE. EMERGENCY BATTERY PACK POSITION M1664 INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK POSITION M1668 AS PER REF B737- AMM- 33-51-06-960-805.OPERATIONAL TEST F
- [SDR SWAA2022010454626](https://openairdocs.org/sdr/SWAA2022010454626), Dec 20, 2021: BATTERY PACK. INOPERATIVE. EXTERIOR EMERGENCY LIGHT L/H AT EMERGENCY EXIT DOOR INOP. ; EXTERIOR EMERGENCY LIGHT LH AT EMERGENCY EXIT DOOR INOP. / [01] REMOVED AND REPLACED EMERGENCY BATTE
- [SDR SWAA2022010652738](https://openairdocs.org/sdr/SWAA2022010652738), Dec 13, 2021: STRINGER SPLICE. CORRODED. ***CORROSION*** FOUND ON THE E&E STA 354 STR28R TWO RIVETS ; / [01] REMOVED DAMAGE EXISTING SPLICE AT E&E STA 354 S-28R REF B737-700 SRM 51-40-02-0G-0.; [02] FA
- [SDR SWAA2022011050665](https://openairdocs.org/sdr/SWAA2022011050665), Dec 6, 2021: BRACKET. OUT OF POSITION. DURING P-18 WALL INSTALLATION FOUND TWO SUPPORT BRACKETS (STGR-6L AND STGR 8L) OUT OF POSITION. ; / [01] REMOVED P-18 SUPPORT BRACKETS AT STR 6L AND STR 8L; REI
- [SDR SWAA2021120649603](https://openairdocs.org/sdr/SWAA2021120649603), Dec 2, 2021: SKIN. CORRODED. FUSELAGE SKIN UNDER DORSAL HAS MINOR CORROSION SPOTS BS 882-893 LBL 6- RBL 5. 8-143. REMOVED MINOR CORROSION ON AREAS IAW SRM 51-10-02-0G-0. PERFORMED UT THICKN
- [SDR SWAA2022010647564](https://openairdocs.org/sdr/SWAA2022010647564), Nov 24, 2021: SHEAR TIE. CRACKED. FOUND SHEAR TIE CRACKED AT FLIGHT DECK STA 225 RBL 40 ; / [01] INSTALLED EWS PROTECTION AT FLIGHT DECK R/H SIDE BETWEEN STA 220 AND STA 230 REF B737-700 AMM 20-
- [SDR SWAA2022010646849](https://openairdocs.org/sdr/SWAA2022010646849), Nov 23, 2021: BULKHEAD WEB. CRACKED. FUEL VAPOR BARRIER WEB LOWER EDGE CLIP CRACKED RBL 25.0 STA 663 ; / [01] REMOVED LOWER EDGE CLIP AT FUEL VAPOR BARRIER WEB; RBL 25.0 STA 663 AS PER B737-700 SRM
- [SDR SWAA2022011045658](https://openairdocs.org/sdr/SWAA2022011045658), Nov 18, 2021: FITTING. CORRODED. VERTICAL STAB FRONT SPAR LEFT FWD FUSELAGE FITTING FWD SURFACE HAS LIGHT PITTING ON SURFACE. ; / [01] PERFORMED PENETRANT INSPECTION ON VERTICAL STAB.FRONT SPAR
- [SDR SWAA2022011045434](https://openairdocs.org/sdr/SWAA2022011045434), Nov 18, 2021: FITTING. CORRODED. VERTICAL STAB FRONT SPAR RIGHT FWD FUSELAGE FITTING FWD SURFACE HAS LIGHT PITTING ON SURFACE. ; / [01] PERFORMED PENETRANT INSPECTION ON VERTICAL STAB.FRONT SPA
- [SDR SWAA2022011045661](https://openairdocs.org/sdr/SWAA2022011045661), Nov 18, 2021: FITTING. CORRODED. VERTICAL STAB FRONT SPAR LEFT FWD FUSELAGE FITTING BORE HAS PITTING ; / [01] REMOVED CORROSION AT VERTICAL STAB. FUSELAGE FRONT SPAR LH SIDE LUG BORE ; REAM FIT
- [SDR SWAA2022011045662](https://openairdocs.org/sdr/SWAA2022011045662), Nov 18, 2021: FITTING. CORRODED. VERTICAL STAB FRONT SPAR RIGHT FWD FUSELAGE FITTING BORE HAS PITTING ; / [01] REMOVED CORROSION AT VERTICAL STAB. FUSELAGE FRONT SPAR RH SIDE LUG BORE ; REAM HO
- [SDR SWAA2022010645663](https://openairdocs.org/sdr/SWAA2022010645663), Nov 18, 2021: SEAT TRACK. CORRODED. CAPT LH FWD SEAT TRACK HAS CORROSION ON LOWER SURFACE. 8-135 ; / [01] REPLACED CAPTAIN'S L/H FWD SEAT TRACK REF AMM 25-11-11-200-801-NG . REFER TO CUSTOMER BARC
- [SDR SWAA2022010645664](https://openairdocs.org/sdr/SWAA2022010645664), Nov 18, 2021: SEAT TRACK. CORRODED. F/O LH FWD SEAT TRACK HAS CORROSION ON LOWER SURFACE. 8-133 ; / [01] RECEIVED NEW F/O LEFT FWD FROM STOCK. PART WILL BE INSTALLED ON ROUTINE CARD TTG8Q001RUZP.;
- [SDR SWAA2022010644265](https://openairdocs.org/sdr/SWAA2022010644265), Nov 16, 2021: BEAR STRAP. DAMAGED. DURING REPAIR OF R1 BEAR STRAP AT STA 291 TO 295 SR 9R AND 10R 4 FASTENER HOLE WHERE FOUND ELONGATED. ; / [01] CLEANED UP DAMAGE FROM HOLES 4 (EA) LOCATED AT R1
- [SDR SWAA2022010643902](https://openairdocs.org/sdr/SWAA2022010643902), Nov 16, 2021: TEE ANGLE. CORRODED. CORROSION ON E&E COMPARTMENT LOWER AUXILIARY SILL S-23L FROM BS 294.5 TO 312 . REMOVED EXFOLIATED TEE ANGLE IAW SRM 51-40-02-0G-0. PERFORMED PENETRANT INSP ON F
- [SDR SWAA2022010643904](https://openairdocs.org/sdr/SWAA2022010643904), Nov 16, 2021: ANGLE. CORRODED. E&E COMPARTMENT LOWER AUXILIARY SILL; BETWEEN S-21L AND-23L AT STA 320 FOUND CORRODED ON ANGLE. REMOVED EXFOLIATED ANGLE IAW SRM 51-40-02-0G-0. PERFORMED PENETR
- [SDR SWAA2022010643901](https://openairdocs.org/sdr/SWAA2022010643901), Nov 16, 2021: ANGLE. CORRODED. E&E COMPARTMENT LOWER AUXILIARY SILL; BETWEEN S-21L AND-23L AT STA 336 APPX. FOUND CORROSION ON ANGLE CHORD. ; / [01] REMOVED EXFOLIATED ANGLE E&E COMPARTMENT L
- [SDR SWAA2022010643903](https://openairdocs.org/sdr/SWAA2022010643903), Nov 16, 2021: ANGLE. CORRODED. E&E COMPARTMENT LOWER AUXILIARY SILL BETWEEN S-21L AND-23L AT STA 320. FOUND CORROSION ON ANGLE. REMOVED EXFOLIATED ANGLE CHORD AT E&E COMPARTMENT LOWER AUXILIA
- [SDR SWAA2022010643889](https://openairdocs.org/sdr/SWAA2022010643889), Nov 15, 2021: PANEL. CORRODED. CORROSION ON FLIGHT DECK ENTRY FLOOR PANEL 211AF MATING SURFACE MKD DOT ; / [01] RECEIVED NEW PANEL 211AF ;THIS PANEL WILL BE INSTALL ON FAULY TTG8Q006JDOU; [02
- [SDR SWAA000043262](https://openairdocs.org/sdr/SWAA000043262), Nov 13, 2021: BRACKET. CORRODED. SUPPLEMENTAL INFORMATION: **CORROSION**JACKSCREW COMPARTMENT BEHIND ACCESS 311BL; APU'S INLET PLENUM AFT ATTACHING BRACKETS TO STRUCTURE; CORRODED. DOT#208-26 ;
- [SDR SWAA2022010643247](https://openairdocs.org/sdr/SWAA2022010643247), Nov 13, 2021: PANEL. CRACKED. PNL 193D HAS CRACKS AT 8 EACH AFT EDGE FASTENER HOLES. REPAIR THE PANEL PER SRM 53-40-70 OR CONTACT ENGINEERING VIA TSR FOR INSTRUCTIONS. REF CARD 5351-I-14642-
- [SDR SWAA2022010543245](https://openairdocs.org/sdr/SWAA2022010543245), Nov 13, 2021: GUSSET. CRACKED. FWD CARGO GUSSET CRACKED AT BS 500D S-19R. 8-105 ; / [01] REMOVED FWD CARGO GUSSET AT BS 500D S-19R AS PER B737-700 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED 
- [SDR SWAA2022010443237](https://openairdocs.org/sdr/SWAA2022010443237), Nov 12, 2021: FRAME. CRACKED. SUPPLEMENTAL INFORMATION: ABOVE L1 CUTOUT LWR END OF FRAME BS 312 APPEARS TO BE CRACKED AT RADIUS BETWEEN S-5L AND S-6L. 8-95 ; / [01] REMOVED EXISTING FASTENER
- [SDR SWAA2022010643233](https://openairdocs.org/sdr/SWAA2022010643233), Nov 12, 2021: ATTACH BRACKET. CRACKED. P-18 ATTACH BRACKET CRACKED BS 273 AT S-8L. 8-91 ; / [01] REMOVED ATTACH BRACKET AT BS 273;S-8L AS PER B737-700 SRM 51-40-02-0G-0; [02] FABRICATED P-18 ATTACH B
- [SDR SWAA2022010643234](https://openairdocs.org/sdr/SWAA2022010643234), Nov 12, 2021: ATTACH BRACKET. CRACKED. P-18 ATTACH BRACKET CRACKED BS 273 AT S-10L. 8-92 ; / [01] REMOVED ATTACH BRACKET AT BS 273;S-10L AS PER B737-700 SRM 51-40-02-0G-0; [02] FABRICATED P-18 ATTACH
- [SDR SWAA2022010643243](https://openairdocs.org/sdr/SWAA2022010643243), Nov 12, 2021: PANEL. CRACKED. PNL 194E HAS CRACK ON AFT EDGE AT 3RD HOLE FROM THE LEFT. REPAIR THE PANEL PER SRM 53-60-70 OR CONTACT ENGINEERING VIA TSR FOR INSTRUCTIONS. REF CARD 5351-I-146
- [SDR SWAA2022011042561](https://openairdocs.org/sdr/SWAA2022011042561), Nov 11, 2021: LUG. CORRODED. VERTICAL LEADING EDGE LEFT I/B AND O/B FRONT SPAR FITTING LUG FACE AREA PITTING/CORROSION NOTED.
- [SDR SWAA2022010642558](https://openairdocs.org/sdr/SWAA2022010642558), Nov 11, 2021: WEB. CORRODED. E&E COMPARTMENT LOWER AUXILIARY SILL; BETWEEN S-21L AND-23L AT STA 320 APPX. FOUND CORROSION ON WEB. REMOVED WEB AT E&E COMPARTMENT LOWER AUXILIARY SILL IAW SRM
- [SDR SWAA2022010642559](https://openairdocs.org/sdr/SWAA2022010642559), Nov 11, 2021: WEB. CORRODED. E&E COMPARTMENT LOWER AUXILIARY SILL; BETWEEN S-21L AND-23L AT STA 336 APPX. FOUND CORROSION ON WEB. REMOVED WEB AT E&E COMPARTMENT LOWER AUXILIARY SILL; BETWEE
- [SDR SWAA2022011042546](https://openairdocs.org/sdr/SWAA2022011042546), Nov 10, 2021: ATTACH FITTING. BROKEN. RT BODY PNL 192BR ATTACH FLANGES HAVE 2 BROKENRECPTICALS IN FWD AREA. 8-81 ; / [01] REMOVED AND REPLACED 2 ATTACHED FLANGES AT RT BODY PNL 192BR IAW SRM 51-40-0
- [SDR SWAA2022011042548](https://openairdocs.org/sdr/SWAA2022011042548), Nov 10, 2021: ATTACH FITTING. BROKEN. LT BODY PNL 192BL ATTACH FLANGES HAVE 8 BROKEN RECPTICALS. 8-80 ; / [01] REMOVED RECPTICALS AT LT BODY PNL 192BL ATTACH FLANGES AS PER B737 SRM 51-40-02-0G-0; [

All 290: https://openairdocs.org/deregistered/N770SA-2024-10-04/reports.md

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