# N755SA: 1999 Boeing 737-7H4, registration cancelled 2024-09-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 16, 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: 27871
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 11, 1999
- Certificate issued: December 18, 1999
- Last registry action: July 22, 2023
- Mode S code: AA2E2D
- 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/N755SA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=755SA
- Page: https://openairdocs.org/deregistered/N755SA-2024-09-16

From the FAA registry file of November 5, 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 (293, newest 50)

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

- [SDR SWAA2023041426547](https://openairdocs.org/sdr/SWAA2023041426547), Apr 12, 2023: COVER. MISSING. CAPT SIDE EMERGENCY EXIT LENS COVER MISSING AT LEFT OVER WING<[01] INSTALLED EMERGENCY EXIT LENS COVER AT CAPT SIDE OVER WING IAW S.I.P.
- [SDR SWAA2023041124557](https://openairdocs.org/sdr/SWAA2023041124557), Apr 7, 2023: LIGHT. INOPERATIVE. INTERIOR EMERGENCY LIGHT AT 17ABC INOP<[01] FOUND CONNECT FOR INTERIOR EMERGENCY LIGHT AT 17ABC NOT CONNECTED. CONNECTED THE CONNECTOR FOR AREA LIGHT AT 17ABC P
- [SDR SWAA2023030812872](https://openairdocs.org/sdr/SWAA2023030812872), Mar 5, 2023: SLIDE. OUT OF ADJUST. CREW REPORTED R2 SLIDE HANGING TO FAR BELOW SLIDE CASE.<[01] ADJUSTED SLIDE PER MT 725-61-06 AND AMM 25-66-00
- [SDR SWAA2022101359190](https://openairdocs.org/sdr/SWAA2022101359190), Oct 13, 2022: NONE. CRACKED. LEFT HORIZONTAL STABILIZER UPPER FORWARD SLIDER CRACKED. / [01] R&R LEFT HORIZONTAL STABILIZER UPPER FORWARD SLIDER PER AMM 53-31-31-401 CONFIG 2-NG.
- [SDR SWAA2022101157475](https://openairdocs.org/sdr/SWAA2022101157475), Oct 8, 2022: SIGN. INOPERATIVE. CUSTOMER REQUEST: ONE BULB INOP EMERGENCY LOWER AT L-1 DOOR / [01] RELAMPED EMERGENCY LOWER EXIT SIGN AT L-1 DOOR PER REF. AMM 33-51-01-960-801. PERFORMED OPS C
- [SDR SWAA2022101157477](https://openairdocs.org/sdr/SWAA2022101157477), Oct 8, 2022: BATTERY PACK. INOPERATIVE. CUSTOMER REQUEST: EXTERIOR EMERGENCY LIGHT AFT OF R-1 DOOR INOP / [01] REMOVED AND REPLACED BATTERY PACK M1674 ON TTG8Q00F9CTY. R-1 DOOR EXTERIOR EMERGENCY LIGH
- [SDR SWAA2022101157476](https://openairdocs.org/sdr/SWAA2022101157476), Oct 8, 2022: BATTERY PACK. INOPERATIVE. CUSTOMER REQUEST: RT STOW BIN ROW 3/ROW 6 EMERGENCY LIGHT INOP / [01] REMOVED AND REPLACED M1674 EMERGENCY BATTERY PACK PER AMM 35-51-06-960-805. TEST NORMAL.;[
- [SDR SWAA2022101157474](https://openairdocs.org/sdr/SWAA2022101157474), Oct 8, 2022: BATTERY PACK. INOPERATIVE. CUSTOMER REQUEST: L-1 DOOR UPPER EMERGENCY EXIT SIGN INOPERATIVE / [01] REMOVED AND REPLACED M1674 EMERGENCY BATTERY PACK ON TTG8Q 00F9CTY. L-1 DOOR EMERGENCY E
- [SDR SWAA2022101157473](https://openairdocs.org/sdr/SWAA2022101157473), Oct 7, 2022: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS INOP AT AFT CABIN AREA LEFT AND RIGHT SIDE / [01] REMOVED AND REPLACED BATTERY PACK M1673 PER AMM 33-51-06-960-805. TEST NORMAL.;[02] VERIFIED 
- [SDR SWAA2022101195083](https://openairdocs.org/sdr/SWAA2022101195083), Sep 20, 2022: BULKHEAD. CANNING. OIL CANNING FOUND ON BS1016 AFT PRESSURE BULKHEAD AT STRINGER 2L - 60 IN. FROM APEX. / [01] CUT OUT DAMAGE AREA AT BS1016 AFT PRESSURE BULKHEAD AT STRINGER 2L -
- [SDR SWAA2022101195081](https://openairdocs.org/sdr/SWAA2022101195081), Sep 20, 2022: BULKHEAD. CANNING. OIL CANNING FOUND ON BS AFT PRESSURE BULKHEAD 5 IN. BELOW STRINGER 11R - 60 IN. FROM APEX. / [01] CUT OUT DAMAGE AREA AT AFT PRESSURE BULKHEAD 5 IN. BELOW STRIN
- [SDR SWAA2022100683004](https://openairdocs.org/sdr/SWAA2022100683004), Sep 19, 2022: NONE. WARPED. OIL CANNING FOUND ON BS AFT PRESSURE BULKHEAD 5 IN. BELOW STRINGER 11R - 60 IN. FROM APEX. / [01] TRANSFERRED TO N/R FAULT TTG8Q00EXJBY
- [SDR SWAA2022100683005](https://openairdocs.org/sdr/SWAA2022100683005), Sep 19, 2022: NONE. WARPED. OIL CANNING FOUND ON BS1016 AFT PRESSURE BULKHEAD AT STRINGER 2L - 60 IN. FROM APEX. / [01] N/A'D REMAINING MEASUREMENTS; MEASUREMENTS TRANSFERRED TO FAULT TTG8
- [SDR SWAA2022080437783](https://openairdocs.org/sdr/SWAA2022080437783), Aug 2, 2022: DOUBLER. CRACKED. EXTERNAL GROUND POWER DOOR CUTOUT INTERNAL SKIN DOUBLER IS CRACKED ON LOWER SIDE OF DOOR. REMOVED DAMAGE SECTION IAW SRM 53-10-15-2R-4.FIG 204. HFEC IAW NDT PAR
- [SDR SWAA2021112446248](https://openairdocs.org/sdr/SWAA2021112446248), Nov 20, 2021: FAIRING. DELAMINATED. RH MLG AFT W/W FAIRING DENTED & DELAMINATED. PANEL 194GR MEASURES 1.75'H X 4.25'W X 2/32'DREF LOGBOOK#1831149 ; / [01] REF LOG# 178451. COMPLY WITH MPM 3 DAYS M
- [SDR SWAA2021112346247](https://openairdocs.org/sdr/SWAA2021112346247), Nov 20, 2021: TIRE. FAILED. #3 MAIN TIRE BLOWN ON TAKEOFF. DAMAGE TO WING & FLAPS NOTED AFTER LANDING. ; / [01] C/W TIRE THREADLOSS OR TIRE BURST CONDITIONAL INSPECTION PER AMM 05-51-54.RE
- [SDR SWAA2021112346766](https://openairdocs.org/sdr/SWAA2021112346766), Nov 20, 2021: TIRE. FAILED. #3 MAIN TIRE BLOWN ON TAKEOFF. DAMAGE TO WING & FLAPS NOTED AFTER LANDING. ; / [01] C/W TIRE THREADLOSS OR TIRE BURST CONDITIONAL INSPECTION PER AMM 05-51-54.RE
- [SDR SWAA2021102832842](https://openairdocs.org/sdr/SWAA2021102832842), Oct 25, 2021: NONE. BROKEN. AFT GALLEY ENTRY DOOR EXIT SIGN MID DOOR BROKEN ; / [01] REPLACED AFT GALLEY SVC DOOR EXIT SIGN LENS RH SIDE REF AMM 33-51-01
- [SDR SWAA2021090814892](https://openairdocs.org/sdr/SWAA2021090814892), Sep 3, 2021: MOUNT. BROKEN. MID CABIN EMERGENCY EXIT LIGHT HANGING FROM CEILING HAS BROKEN MOUNT. ; / [01] ACCOMPLISH EA 21-133-02605 ASSIGNED AS A SUBTASK.; [02] L/P 1686559 INSTALLED INT
- [SDR SWAA2021090714154](https://openairdocs.org/sdr/SWAA2021090714154), Sep 1, 2021: LAMP. INOPERATIVE. FWD GALLEY EXIT SIGN HAS A BULB OUT / [01] RELAMPED AND PERFORMED GOOD TEST OF FWD GALLEY EXIT SIGN PER AMM 33-25-00-960-801.; [02] CORRECTION FOR REF. S/B 33-5
- [SDR SWAA2021090712630](https://openairdocs.org/sdr/SWAA2021090712630), Aug 27, 2021: LAMP. MISSING. R/H OVERWING EMERGENCY LIGHT MISSING BULBS. ; / [01] RE-LAMPED R/H OVERWING EMERGENCY LIGHT AND PERFORMED A GOOD OP CHECK ALL AS PER AMM 33-51-03-960-801.; [02]
- [SDR SWAA2021090710659](https://openairdocs.org/sdr/SWAA2021090710659), Aug 23, 2021: INTERCOSTAL. CORRODED. CORROSION; AFT CARGO; BS 807 + 2; RBL 19; WL 156; SUBTHRESHOLD INTERCOSTAL UPPER FLANGE; LWR SURFACE AT NUTPLATE HOLE; MARKED. ; / [01] REMOVED DAMAGE IN ACB BS
- [SDR SWAA2021090710661](https://openairdocs.org/sdr/SWAA2021090710661), Aug 23, 2021: WEB. CORRODED. CORROSION; AFT CARGO BS 789; RBL 20; WL 155; INTERCOSTAL WEB UPPER END; OB SURFACE; MARKED ; / [01] REMOVED CORROSION IN ACB BS789 RBL20 WL 155 IN A 1'X1' AREA 
- [SDR SWAA2021090709346](https://openairdocs.org/sdr/SWAA2021090709346), Aug 21, 2021: SUPPORT. DAMAGED. FCB AFT R/H BS500D BULKHEAD SUPPORT HAS OVERSIZE ON LOWER END RBL21 WL 156 ; / [01] EVALUATED OVERSIZE HOLE ON R/H BS 500D BULKHEAD SUPPORT RBL 21 WL 156 FOUND 
- [SDR SWAA2021090709344](https://openairdocs.org/sdr/SWAA2021090709344), Aug 21, 2021: SPLICE. DAMAGED. AFT CARGO BAY FLOOR PANEL SPLICE STRAP AT BS 767+4 HAS OVERSIZE HOLES RBL 10 TO LBL10 WL 156 ; / [01] UPDATED MEASUREMENT TABLE; [02] EVALUATED OVERSIZE HOLES O
- [SDR SWAA2021090708356](https://openairdocs.org/sdr/SWAA2021090708356), Aug 18, 2021: FRAME. DAMAGED. OVERSIZE HOLE IN FRAME AT BS727A RBL21.5 WL156 COMMON TO UPPER FLOOR TO SIDEWALL SUPPORT FASTENER HOLE ; / [01] REMOVED DAMAGE ON FRAME BS727A RBL21.5 WL156 IAW
- [SDR SWAA2021090708355](https://openairdocs.org/sdr/SWAA2021090708355), Aug 18, 2021: ANGLE. CRACKED. FORWARD CARGO BAY L/H BAFFLE CLIP BS 400 LBL 23 WL 155 IS CRACKED ; / [01] EVALUATED DAMAGE ON BAFFLE CLIP AND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE
- [SDR SWAA2021090708354](https://openairdocs.org/sdr/SWAA2021090708354), Aug 18, 2021: GUSSET. CRACKED. FCB GUSSET BS 500D STRINGER 21 L/H IS CRACKED ; / [01] EVALUATED CRACK; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 5
- [SDR SWAA2021090708353](https://openairdocs.org/sdr/SWAA2021090708353), Aug 18, 2021: GUSSET. CRACKED. FCB GUSSET BS 500D STRINGER 19 L/H IS CRACKED ; / [01] EVALUATED CRACK; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 5
- [SDR SWAA2021090708352](https://openairdocs.org/sdr/SWAA2021090708352), Aug 18, 2021: GUSSET. CRACKED. FCB GUSSET BS 500D STRINGER 19 R/H IS CRACKED ; / [01] EVALUATED CRACK; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 5
- [SDR SWAA2021090707206](https://openairdocs.org/sdr/SWAA2021090707206), Aug 12, 2021: PANEL. CHAFED. PANEL 192F HAS CHAFING DAMAGE TO FWD AND AFT INNER MATING SURFACES ; / [01] IDENTIFIED PANEL 192F IAW SRM 53-40-70-0I-1 FIGURE 2. TABLE 2. ITEM 15.<BR><BR>FOUND
- [SDR SWAA2021090707209](https://openairdocs.org/sdr/SWAA2021090707209), Aug 12, 2021: STIFFENER. CRACKED. LT HORIZ. STAB RIB ASSY. 4 (STAB STA 120.30) LOWER CHORD AT THE 4TH VERT STIFFENER IS CRACKED. ; / [01] REMOVED CRACK DAMAGE LOWER CHORD AT 4TH VERTICAL STIFFEN
- [SDR SWAA2021090707208](https://openairdocs.org/sdr/SWAA2021090707208), Aug 12, 2021: STIFFENER. CRACKED. LT HORIZ. STAB RIB ASSY. 4 (STAB STA 120.30) 2ND VERT STIFFENER IS CRACKED. ; / [01] REMOVED CRACK DAMAGE LOWER RADIUS OF VERTICAL STIFFENER AND WEB L=0.45' X W
- [SDR SWAA2021090706323](https://openairdocs.org/sdr/SWAA2021090706323), Aug 11, 2021: STRINGER CLIP. CRACKED. CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS827 LBL6 WL156. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES R
- [SDR SWAA2021090706310](https://openairdocs.org/sdr/SWAA2021090706310), Aug 11, 2021: STRINGER CLIP. CORRODED. CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS867 LBL6 WL162. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES R
- [SDR SWAA2021090706300](https://openairdocs.org/sdr/SWAA2021090706300), Aug 11, 2021: SHIELD. CORRODED. CORROSION ON SHIELD IN FWD CARGO BAY AFT OF DOOR BS500 RBL 21 WL 156 ; / [01] UPDATED MEASUREMENTS TABLE; [02] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DU
- [SDR SWAA2021090706326](https://openairdocs.org/sdr/SWAA2021090706326), Aug 11, 2021: SHIELD. CORRODED. CORROSION ON FWD SHIELD AT AFT CARGO BAY BS767 - BS775 RBL21 WL157. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQU
- [SDR SWAA2021090706332](https://openairdocs.org/sdr/SWAA2021090706332), Aug 11, 2021: SUPPORT. CORRODED. CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS767- BS727C RBL21 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X20'
- [SDR SWAA2021090706324](https://openairdocs.org/sdr/SWAA2021090706324), Aug 11, 2021: WEB. CORRODED. CORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS807- BS827 RBL26 WL159. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X20' AREA FOUN
- [SDR SWAA2021090706304](https://openairdocs.org/sdr/SWAA2021090706304), Aug 11, 2021: SHIELD. CORRODED. CORROSION ON SHIELD IN FWD CARGO BAY FORWARD OF DOOR BS430 RBL 21 WL 156 ; / [01] UPDATED MEASUREMENT TABLE; [02] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS
- [SDR SWAA2021090706328](https://openairdocs.org/sdr/SWAA2021090706328), Aug 11, 2021: SUPPORT. CORRODED. CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727A- BS807 LBL21 WL157. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.040 IN A 1'X160
- [SDR SWAA2021090706309](https://openairdocs.org/sdr/SWAA2021090706309), Aug 11, 2021: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS928 RBL3 WL168. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REP
- [SDR SWAA2021090706308](https://openairdocs.org/sdr/SWAA2021090706308), Aug 11, 2021: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS928 LBL3 WL168. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REP
- [SDR SWAA2021090706327](https://openairdocs.org/sdr/SWAA2021090706327), Aug 11, 2021: WEB. CORRODED. CORROSION ON WEB AT AFT CARGO BAY BS773 RBL20 WL157 ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT
- [SDR SWAA2021090706336](https://openairdocs.org/sdr/SWAA2021090706336), Aug 11, 2021: TRACK. CORRODED. CORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS727A+19 LBL17 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' ARE
- [SDR SWAA2021090706333](https://openairdocs.org/sdr/SWAA2021090706333), Aug 11, 2021: ANGLE. CORRODED. CORROSION ON CLIP AT AFT CARGO BAY BS727D+4 LBL7 WL151. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACE
- [SDR SWAA2021090706329](https://openairdocs.org/sdr/SWAA2021090706329), Aug 11, 2021: ANGLE. CORRODED. CORROSION ON CLIP AT AFT CARGO BAY BS727D+9 RBL7 WL151. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACE
- [SDR SWAA2021090706335](https://openairdocs.org/sdr/SWAA2021090706335), Aug 11, 2021: TRACK. CORRODED. CORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS727A+17 LBL17 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' ARE
- [SDR SWAA2021090706334](https://openairdocs.org/sdr/SWAA2021090706334), Aug 11, 2021: TRACK. CORRODED. CORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS727A+10 LBL17 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' ARE
- [SDR SWAA2021090706331](https://openairdocs.org/sdr/SWAA2021090706331), Aug 11, 2021: TRACK. CORRODED. CORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS727B+3 LBL17 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' AREA

All 293: https://openairdocs.org/deregistered/N755SA-2024-09-16/reports.md

## NTSB investigations (1)

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

- [NTSB LAX06LA009](https://openairdocs.org/ntsb/LAX06LA009), Oct 13, 2005: Boeing 737-7H4 (N755SA), Phoenix, AZ, minor damage. Probable cause: The failure of the other flight crew to maintain an adequate clearance from obstructions while taxiing.

## 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.

- [Accident 20051012026429A](https://openairdocs.org/incident/20051012026429A), Oct 12, 2005: Boeing 7377H4 (N755SA), Phoenix, AZ, Minor damage. (-23) Swa 2080, N624SW, was holding behind another aircraft near spot 5 on delta 13 for departure on runway 25R when his right horizontal stabilizer was struck…

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