# N7744A: 2007 Boeing 737-7BD

- Status: Valid registration
- Airframe: [Boeing 737-7BD](https://openairdocs.org/model/boeing-737-7bd) (registry code 1384511, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 33931
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 12, 2013
- Certificate issued: September 11, 2013
- Expires: September 30, 2029
- Mode S code: AA7AC8
- 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=7744A
- Page: https://openairdocs.org/aircraft/N7744A

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 737-7BD)

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 N7744A.

## FAA accident and incident reports

None matched to N7744A.

## Service difficulty reports (265, 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 SWAA2026092862922](https://openairdocs.org/sdr/SWAA2026092862922), Sep 22, 2026: BATTERY PACK. FAILED. FWD RT BATTERY PACK M1674 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTER PACK PER AMM 33-51-06.
- [SDR SWAA2026092193182](https://openairdocs.org/sdr/SWAA2026092193182), Sep 17, 2026: BRAKE ASSY. LOCKED. RIGHT BRAKE FEELS LIKE IT LOCKS UP DURING TAXI OUT. NR 4 BRAKE ASSY R&R PER AMM 32-41-41.
- [SDR SWAA2026081772182](https://openairdocs.org/sdr/SWAA2026081772182), Aug 12, 2026: LINK PIN. INOPERATIVE. L1 DOOR DOES NOT FULLY OPEN, R & R THE GUIDE ARM RADIUS LINK PIN WASHER AND SCREW. OPS CHKD GOOD IAW AMM 52-11-21, & AMM 52-11-00.
- [SDR SWAA2026080706421](https://openairdocs.org/sdr/SWAA2026080706421), Aug 3, 2026: HANDLE. DETACHED. FORWARD ENTRY ASSIST HANDLE IS NOT ATTACHED, ADJUSTED HANDLE IAW SIP
- [SDR SWAA2026070617604](https://openairdocs.org/sdr/SWAA2026070617604), Jul 1, 2026: GIRT BAR. OUT OF POSITION. F/A REPORTS AFT ENTRY GIRT BAR DOES NOT FIT PROPERLY. AFT ENTRY GIRT BAR FITMENT OK IAW AMM 25-66-02 AND PER LSC, STEP 9, TASK 05-00-02-SWA-002
- [SDR SWAA2025082206579](https://openairdocs.org/sdr/SWAA2025082206579), Aug 21, 2025: LIGHT. INOPERATIVE. PASSENGER CABIN EMERGENCY FLOOR LIGHTING GLOW STRIP NOT SECURE INBOARD OF FORWARD RIGHT WINDSCREEN. SECURED EMERGENCY FLOOR LIGHTING GLOW STRIP INBOAR OF FORWAR
- [SDR SWAA2025072895930](https://openairdocs.org/sdr/SWAA2025072895930), Jul 28, 2025: FUSE. LEAKING. AFTER GEAR RETRACTION LOSS OF HYD SYST. A; HYD A ENG1 AND ELEC2 LOW PRESSURE LIGHTS; FLT CTRL A LOW PRESSURE LIGHTS AND FEEL DIFF PRESS LIGHTS ALL ILLUMINATED A
- [SDR SWAA2025070788863](https://openairdocs.org/sdr/SWAA2025070788863), Jul 4, 2025: TIRE. BLOWN. #2 MAIN TIRE BLOWN ON TAKEOFF FROM MCO. R&R #2 MLG WHEEL AND TIRE ASSY IAW AMM 32-45-11.
- [SDR SWAA2025070888307](https://openairdocs.org/sdr/SWAA2025070888307), Jul 3, 2025: SKIN. BULGED. LH INBD TRAILING EDGE AFT FLAP UPPER FLAP SKIN AREA HAS BULGE 2.5IN FROM TRAILING EDGE AND 7IN FROM INBD EDGE<[01] REF TTG8Q013J5AB FOR REMOVAL AND INSTALLATION
- [SDR SWAA2025041424455](https://openairdocs.org/sdr/SWAA2025041424455), Apr 13, 2025: SLIDE. OUT OF LIMITS. FA REPORTS AFT SERVICE SLIDE PRESSURE IN RED<[01] R+R AFT SERVICE SLIDE PER MT 725-61-06
- [SDR SWAA2025033118982](https://openairdocs.org/sdr/SWAA2025033118982), Mar 28, 2025: SEAL. CRACKED. L/H HORIZONTAL STABILIZER FORWARD UPPER SLIDER SEAL CRACKED/TORN<[01] REMOVED AND REPLACED SEAL PER AMM 53-31-31.;[02] C/W INSPECTION OF REMOVED AND REPLACED SE
- [SDR SWAA2025033118983](https://openairdocs.org/sdr/SWAA2025033118983), Mar 28, 2025: SEAL. CRACKED. R/H HORIZONTAL STABILIZER FORWARD UPPER SLIDER CRACKED/TORN<[01] REMOVED AND REPLACED SEAL PER AMM 53-31-31.;[02] C/W INSPECTION OF REMOVED AND REPLACED SEAL PE
- [SDR SWAA2024123080552](https://openairdocs.org/sdr/SWAA2024123080552), Dec 24, 2024: BULB. INOPERATIVE. AFT GALLEY ENTRY DOOR LOWER EMERGENCY EXIT LOCATOR SIGN HAS INOP BULBS<[01] RELAMPED AFT GALLEY ENTRY DOOR LOWER EMERGENCY EXIT LOCATOR AND PERFORMED A SATISFAC
- [SDR SWAA2024123080546](https://openairdocs.org/sdr/SWAA2024123080546), Dec 23, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1668 INOP. REMOVED EMERGENCY LIGHT BATTERY PACK M1668 AND INSTALLED SERVICEABLE BATTERY PACK AND PERFORMED INSTAL
- [SDR SWAA2024123080547](https://openairdocs.org/sdr/SWAA2024123080547), Dec 23, 2024: LIGHT. INOPERATIVE. FWD EMERGENCY CEILING COVE LIGHT INOP. REMOVED; REPLACED AND PERFORMED GOOD OPS CHECK OF THE FWD EMERGENCY CEILING COVE LIGHT IAW AMM 33-51-03-960-801.
- [SDR SWAA2024123077904](https://openairdocs.org/sdr/SWAA2024123077904), Dec 16, 2024: SCUFF PLATE. CRACKED. AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] REPAIRED AFT CARGO BAY FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1.;[02] VERIFIED CORRECTIVE ACTION ENTRY 
- [SDR SWAA2024123077054](https://openairdocs.org/sdr/SWAA2024123077054), Dec 13, 2024: WIRE. BROKEN. EMERGENCY EXIT LIGHT JUST FWD OF R/H OVERWING EXIT HAS A BROKEN WIRE; W4142. RETERMINATED PLUG SIDE OF D3666 PER WDM 33-51-21 AND SWPM 20-30-12; AND PERFORMED G
- [SDR SWAA2024123174367](https://openairdocs.org/sdr/SWAA2024123174367), Dec 5, 2024: BEAM. CRACKED. CRACK FOUND ON FSD NO.4 (141A6536-14) BEAM AT MOST I/B FASTENER LOCATION; L: 0.5' MARKED<[01] UPDATED PARTS REMOVAL;[02] REMOVAL AND REPLACEMENT OF FORWARD SERV
- [SDR SWAA2024123174368](https://openairdocs.org/sdr/SWAA2024123174368), Dec 5, 2024: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727B S-5L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727B S-5L IAW SRM 51-40-02-0G-0 AND DWG# 146A1102.;[02] VERI
- [SDR SWAA2024123174366](https://openairdocs.org/sdr/SWAA2024123174366), Dec 5, 2024: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727C S-7L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727C S-7L IAW SRM 51-40-02-0G-0 AND DWG# 146A1103.;[02] VERI
- [SDR SWAA2024123174369](https://openairdocs.org/sdr/SWAA2024123174369), Dec 5, 2024: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727D S-7L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727D S-7L IAW SRM 51-40-02-0G-0 AND DWG# 146A1111.;[02] VERI
- [SDR SWAA2024123174370](https://openairdocs.org/sdr/SWAA2024123174370), Dec 5, 2024: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727D S-6L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727D S-6L IAW SRM 51-40-02-0G-0 AND DWG# 146A1111.;[02] VERI
- [SDR SWAA2024123173720](https://openairdocs.org/sdr/SWAA2024123173720), Dec 3, 2024: SEAT TRACK. CORRODED. CORROSION ON PAX CABIN SEAT TRACK CROWN AND WELL AT BS 360+9 TO BS360+18 LBL25 WL208.<[01] REMOVED AND REPLACED SEATTRACK AT BS 360+9 TO BS360+18 LBL25 WL208 IA
- [SDR SWAA2024123073297](https://openairdocs.org/sdr/SWAA2024123073297), Dec 2, 2024: STUB FRAME. CRACKED. CRACK FOUND ON STUB FRAME BS291.5 + 8.5; .2' ABOVE SEAL DEPRESSOR AND .8' IN LENGTH. REMOVED AND REPLACED STUB FRAME FSD UPPER FWD AREA PER SRM 51-40-02 AND DWG
- [SDR SWAA2024123072021](https://openairdocs.org/sdr/SWAA2024123072021), Nov 27, 2024: SHIELD. CORRODED. CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT FWD SHIELD FROM STA 767 TO 787; RBL 26; WL 158.<[01] REMOVED AND REPLACED AFT CARGO COMPARTMENT DOOR CUTOUT FWD S
- [SDR SWAA2024123072017](https://openairdocs.org/sdr/SWAA2024123072017), Nov 27, 2024: SUPPORT. CORRODED. CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT FROM STA 727A TO 767; RBL 24; WL 158.<[01] REMOVED AND REPLACED ON AFT CARGO COMPARTMENT FLOOR TO S
- [SDR SWAA2024123072018](https://openairdocs.org/sdr/SWAA2024123072018), Nov 27, 2024: SUPPORT. CORRODED. CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT FROM STA 727 TO STA 807+2; LBL 24; WL 158.<[01] AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT WITH CORRO
- [SDR SWAA2024123072022](https://openairdocs.org/sdr/SWAA2024123072022), Nov 27, 2024: SUPPORT. CORRODED. CORROSION ON AFT CARGO COMPARTMENT AFT BULKHEAD SUPPORT AT STA 947.5; LBL3 AND RBL 15; WL 158.<[01] REJECTED; FOUND CORROSION ON AFT CARGO COMPARTMENT AFT BULKH
- [SDR SWAA2024123072020](https://openairdocs.org/sdr/SWAA2024123072020), Nov 27, 2024: SUPPORT. CORRODED. CORROSION ON AFT CARGO COMPARTMENT BULKHEAD SUPPORT AT STA 947; RBL 22; WL 159.<[01] REJECTED; FOUND CORROSION ON AFT CARGO COMPARTMENT BULKHEAD SUPPORT AT STA 
- [SDR SWAA2024123171512](https://openairdocs.org/sdr/SWAA2024123171512), Nov 26, 2024: INSERT. DAMAGED. PANEL 222DF HAS A DAMAGED GIRT BAR INSERT.<[01] PANEL 222DF DAMAGED INSERTS REMOVED & REPLACED IAW SRM 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2024123172003](https://openairdocs.org/sdr/SWAA2024123172003), Nov 26, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL AT FWD WET AREA BS349 BL0 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL BETWEEN BS 344 TO BS 360 BL 0 WL 208 PER SRM 51-40-02 AND DWG 141A540
- [SDR SWAA2024123172004](https://openairdocs.org/sdr/SWAA2024123172004), Nov 26, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL AT FWD WET AREA BS317 RBL31 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD WET AREA<BR>BS 317 RBL 31 WL 208 IAW SRM 51-40-05 AND DWG# 1
- [SDR SWAA2024123172005](https://openairdocs.org/sdr/SWAA2024123172005), Nov 26, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT AT FWD WET AREA BS303 LBL11 WL208. MARKED<[01] REMOVED AND INSTALLED NEW INTERCOSTALL SUPPORT BETWEEN BS 294 TO BS 312 LBL 11 PER SRM
- [SDR SWAA2024123072006](https://openairdocs.org/sdr/SWAA2024123072006), Nov 26, 2024: STRAP. CORRODED. CORROSION ON STRAP AT MID CABIN BS707 LBL61 WL203. MARKED<[01] 'REFER TO FAULT TTG8Q00XAD3G WHERE EA 24-153-03359 WAS ADDED AS A SUBTASK'.;[02] VERIFIED ACTION 
- [SDR SWAA2024123072009](https://openairdocs.org/sdr/SWAA2024123072009), Nov 26, 2024: STRAP. CORRODED. CORROSION ON STRAP AT MID CABIN BS707 RBL61 WL203. MARKED<[01] 'REFER TO FAULT TTG8Q00XAD3G WHERE EA 24-153-03359 WAS ADDED AS A SUBTASK'.;[02] VERIFIED ACTION 
- [SDR SWAA2024123072007](https://openairdocs.org/sdr/SWAA2024123072007), Nov 26, 2024: STRAP. CORRODED. CORROSION ON STRAP AT MID CABIN BS713 RBL61 TO RBL67 WL203. MARKED<[01] 'REFER TO FAULT TTG8Q00XAD3G WHERE EA 24-153-03359 WAS ADDED AS A SUBTASK'.;[02] VERIFIE
- [SDR SWAA2024123072008](https://openairdocs.org/sdr/SWAA2024123072008), Nov 26, 2024: STRAP. CORRODED. CORROSION ON STRAP AT MID CABIN BS713 LBL61 WL203. REMOVED CORROSION; REWORKED; AND TREATED STRAP AT MID CABIN BS713 LBL61 WL203 IAW EA 24-153-03359.
- [SDR SWAA2024123071527](https://openairdocs.org/sdr/SWAA2024123071527), Nov 26, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2
- [SDR SWAA2024123071522](https://openairdocs.org/sdr/SWAA2024123071522), Nov 26, 2024: FLOOR PANEL. BUCKLED. AFT FLOOR PANEL 242SF O/B AFT CORNER IS BUCKLED. AFT FLOOR PANEL 242SF O/B AFT CORNER WITH BUCKLED WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BDWG D1040M003-301; BD
- [SDR SWAA2024123071508](https://openairdocs.org/sdr/SWAA2024123071508), Nov 26, 2024: FLOOR PANEL. PULLED. PANEL 222A UPPER SKIN HAS AREAS OF PULLED STRANDS. PANEL 222A UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.
- [SDR SWAA2024123071513](https://openairdocs.org/sdr/SWAA2024123071513), Nov 26, 2024: FLOOR PANEL. PULLED. PANEL 231MF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 231MF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLE
- [SDR SWAA2024123071526](https://openairdocs.org/sdr/SWAA2024123071526), Nov 26, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ACF UPPER SKIN HAD AREAS OF PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-1
- [SDR SWAA2024123071506](https://openairdocs.org/sdr/SWAA2024123071506), Nov 26, 2024: FLOOR PANEL. PULLED. PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE. FLOOR PANEL 221EF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).
- [SDR SWAA2024123071509](https://openairdocs.org/sdr/SWAA2024123071509), Nov 26, 2024: FLOOR PANEL. PULLED. PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE; FLOOR PANEL 221CF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).
- [SDR SWAA2024123071510](https://openairdocs.org/sdr/SWAA2024123071510), Nov 26, 2024: FLOOR PANEL. PULLED. PANEL 221FF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE; FLOOR PANEL 221FF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).
- [SDR SWAA2024123071514](https://openairdocs.org/sdr/SWAA2024123071514), Nov 26, 2024: FLOOR PANEL. PULLED. PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED PER [SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2024123071515](https://openairdocs.org/sdr/SWAA2024123071515), Nov 26, 2024: FLOOR PANEL. PULLED. PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED NEW FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID:0127.
- [SDR SWAA2024123071516](https://openairdocs.org/sdr/SWAA2024123071516), Nov 26, 2024: FLOOR PANEL. PULLED. PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF ALL OF THE DAMAGE; PANEL 241BF WAS REPLACED WITH A NEWLY FABRICATED PANEL ALL OF THE WO
- [SDR SWAA2024123071517](https://openairdocs.org/sdr/SWAA2024123071517), Nov 26, 2024: FLOOR PANEL. PULLED. PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE. PANEL 242AF WAS REPLACED WITH A NEWLY FABRICATED PANEL. ALL OF 
- [SDR SWAA2024123071518](https://openairdocs.org/sdr/SWAA2024123071518), Nov 26, 2024: FLOOR PANEL. PULLED. PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241UF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANE

All 265: https://openairdocs.org/aircraft/N7744A/reports.md

## STCs that may be installed (OpenAirDocs) (2)

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 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

## Earlier aircraft with N7744A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7744A before.

- [Cancelled 1956-12-18](https://openairdocs.org/deregistered/N7744A-1956-12-18): Cessna 180, S/N 32641. Exported to Argentina. Owner: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)

## Related

- Other Boeing 737-7BD aircraft: https://openairdocs.org/model/boeing-737-7bd/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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