# N7734H: 2006 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 CFM56-7B22 series](https://openairdocs.org/engine/cfm-international-cfm56-7b22-series) (registry code 13043)
- Serial number: 33923
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 18, 2012
- Certificate issued: August 14, 2012
- Expires: August 31, 2028
- Mode S code: AA7718
- 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=7734H
- Page: https://openairdocs.org/aircraft/N7734H

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 CFM56-7B22 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 CFM56-7B22 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 (2)

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 DCA24LA290](https://openairdocs.org/ntsb/DCA24LA290), Aug 19, 2024: Boeing 737 (N7734H), Highland Meadows, NM, no damage. Probable cause: An encounter with convectively induced turbulence during descent.
- [NTSB OPS23FA010](https://openairdocs.org/ntsb/OPS23FA010), Aug 11, 2023: Boeing 737-7BD (N7734H), San Diego, CA, incident, no damage. Probable cause: The local control controller’s poor judgment in duty prioritization which distracted them from monitoring arriving and departing traffic and resulted in a runway incursion and loss of same runway…

## FAA accident and incident reports

None matched to N7734H.

## Service difficulty reports (213, 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 SWAA2026091617558](https://openairdocs.org/sdr/SWAA2026091617558), Sep 12, 2026: BATTERY PACK. INOPERATIVE. AFT RIGHT EMERGENCY EXIT LIGHT INOP R&R AFT LEFT EMERGENCY BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2026060207582](https://openairdocs.org/sdr/SWAA2026060207582), May 29, 2026: LAMP. INOPERATIVE. RH SIDEWALL LT ABOVE EMERGENCY EXIT INOP. REPLACED THE RH EMER EXIT WINDOW LIGHT LAMP IAW AMM 33-21-00. OPS CHECKED GOOD.
- [SDR SWAA2026020364600](https://openairdocs.org/sdr/SWAA2026020364600), Jan 25, 2026: ACCESS PANEL. DELAMINATED. DELAMINATED INTERNAL AREA ON ACCESS PANEL 193CR BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-1, REPAIR 1.
- [SDR SWAA2026020362164](https://openairdocs.org/sdr/SWAA2026020362164), Jan 16, 2026: ACCESS PANEL. DELAMINATED. DELAMINATED ACCESS PANEL 431DR ON THE LT PYLON. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026020359998](https://openairdocs.org/sdr/SWAA2026020359998), Jan 9, 2026: TIE CLIP. CRACKED. CRACK ON TIE CLIP LOCATED BS 380 AND STRINGER 8L ON FWD PASS CABIN. REPLACED TIE CLIP AND FASTENERS LOCATED BS 380 AND STRINGER 8L ON FWD PASS CABIN IAW SRM 51-
- [SDR SWAA2026020358926](https://openairdocs.org/sdr/SWAA2026020358926), Jan 6, 2026: ACCESS PANEL. ELONGATED. ELONGATED HOLES ON THE ACCESS PANEL 192E OF BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.
- [SDR SWAA2026020358555](https://openairdocs.org/sdr/SWAA2026020358555), Jan 5, 2026: VAPOR BARRIER. NO DISCREPANCY. CRACKED VAPOR BARRIER, BS 663, LBL 36. PERFORMED A DETAIL VISUAL INSPECTION OF THE AREA AND FOUND NOT A CRACK, ONLY THE REMAINS OF SEALANT IAW SRM 51-10-02-0G. 
- [SDR SWAA2026020358554](https://openairdocs.org/sdr/SWAA2026020358554), Jan 5, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET, BS 540, LBL 6 IN THE AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET IAW SRM 51-10-02-0G-0, ITEM 9, MEASUREMENT OF CRACK: L=0.9360.
- [SDR SWAA2026020358007](https://openairdocs.org/sdr/SWAA2026020358007), Jan 4, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500C FWD OF STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, AND DWG 143A7505, SHEET 82, REV -.
- [SDR SWAA2026020358003](https://openairdocs.org/sdr/SWAA2026020358003), Jan 4, 2026: NUT PLATE. CORRODED. CORROSION ON THE INTERNAL CAVITY, FRONT SPAR OTBD RAIL NUT PLATE OFSS 460, LT WING. REPLACED RAIL NUT-PLATE IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-
- [SDR SWAA2026020360964](https://openairdocs.org/sdr/SWAA2026020360964), Jan 4, 2026: ISOLATION MOUNT. DEBONDED. DEBONDED ISOLATOR MOUNT, BS 540, S10 - 11R. THE ISOLATOR MOUNT WAS BONDED IAW DWG 144A2201, SHEET 7, REV B.
- [SDR SWAA2026020358004](https://openairdocs.org/sdr/SWAA2026020358004), Jan 4, 2026: NUT PLATE. CRACKED. CRACKED INTERNAL CAVITY FRONT SPAR OTBD RAIL NUT PLATE LT WING OFSS 332. REPLACED RAIL NUT PLATE IAW SRM 51-40-02, AND DWG 112A4402, SHEET 13, REV -.
- [SDR SWAA2026020358006](https://openairdocs.org/sdr/SWAA2026020358006), Jan 4, 2026: NUT PLATE. CRACKED. CRACKED INTERNAL CAVITY, FRONT SPAR OTBD RAIL NUT PLATE, RT WING OFSS 594. REPLACED RAIL NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 112A4402, SHEET
- [SDR SWAA2026020357892](https://openairdocs.org/sdr/SWAA2026020357892), Jan 3, 2026: STRAP. CORRODED. CORROED STRAP, BTWN BS 847 - 853, RBL 20, WL 155.8. REPLACED THE STRAP AND FASTENERS IAW SRM 51-10-02, ITEM 9, 51-40-02-0G-0, AND DWG 146A0081, SHEET 31, REV -.
- [SDR SWAA2026020358000](https://openairdocs.org/sdr/SWAA2026020358000), Jan 3, 2026: FRAME. CRACKED. CRACKED FRAME, BS 440, BTW S8 - 9R. PERFORMED A PERMANENT REPAIR ON THE FRAME IAW EA 26-153-00093-WIP1, EA 26-153-00093-WIP2, AND SUMMARY 26-153-00093.
- [SDR SWAA2026020358001](https://openairdocs.org/sdr/SWAA2026020358001), Jan 3, 2026: SHIELD. CORRODED. CORRODED SHIELD WEB, BTW BS 492.4 - 500A, RBL 22, WL 152.7, IN THE FWD CARGO BAY, REPLACED THE SHIELD WEB AND FASTENERS IAW SRM 51-40-02, AND DWG 143A0080, SHEE
- [SDR SWAA2026012957894](https://openairdocs.org/sdr/SWAA2026012957894), Jan 3, 2026: FRAME. CRACKED. CRACKED FRAME, BS 440, S8 - 9L. REPAIRED THE FRAME IAW EA 26-153-00085-WIP1, 26-153-00085-WIP2, & SUMMARY 26-153-00085.
- [SDR SWAA2026012957999](https://openairdocs.org/sdr/SWAA2026012957999), Jan 3, 2026: FRAME. CRACKED. CRACKED FRAME, BS 400, S8 - 9R. REPAIRED THE FRAME IAW 26-153-00066-WIP1, 26-153-00066-WIP2, & SUMMARY 26-153-00066.
- [SDR SWAA2026012957893](https://openairdocs.org/sdr/SWAA2026012957893), Jan 3, 2026: FRAME. CRACKED. CRACKED FRAME, BS 400 S8 - 9L. REPAIRED THE FRAME, BS 400 S7 - 9L IAW EA 26-153-00091-WIP1, 26-153-00091-WIP2, & SUMMARY 26-153-00091.
- [SDR SWAA2026012957886](https://openairdocs.org/sdr/SWAA2026012957886), Jan 3, 2026: STRAP. CORRODED. CORROSION STRAP LOCATED BETWEEN BS 842 - 847, RBL 20, WL 155.8 IN THE AFT CARGO BAY. REPLACED THE STRAP & FASTENERS IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-
- [SDR SWAA2026012957884](https://openairdocs.org/sdr/SWAA2026012957884), Jan 3, 2026: SUPPORT ANGLE. CORRODED. CORROSION ON SUPPORT ANGLE LOCATED BTW BS 767 - 787, RBL 21, WL 156.1 IN THE AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, SR
- [SDR SWAA2026012957889](https://openairdocs.org/sdr/SWAA2026012957889), Jan 3, 2026: SHIELD. CORRODED. CORROSION SHIELD WEB LOCATED BS 767 - 794, RBL 21 AND WL156 AFT CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, I
- [SDR SWAA2026020357622](https://openairdocs.org/sdr/SWAA2026020357622), Jan 2, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 291.5 - 294.5, STR 17R IN THE FWD GALLEY AREA. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 141A8310, SHEET 25, REV -.
- [SDR SWAA2026020357620](https://openairdocs.org/sdr/SWAA2026020357620), Jan 2, 2026: ANGLE. CRACKED. CRACKED ANGLE ON BODY FAIRING SUPPORT STRUCTURE BS 500D, STRINGER 19L, LOWER FUSELAGE. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, & DW
- [SDR SWAA2026012957750](https://openairdocs.org/sdr/SWAA2026012957750), Jan 2, 2026: FRAME. CRACKED. CRACKED FRAME, BS 380 S8 - 9L. REPAIRED THE FRAME IAW EA 26-153-00092-WIP1, 26-153-00092-WIP2, & SUMMARY 26-153-00092.
- [SDR SWAA2026012957626](https://openairdocs.org/sdr/SWAA2026012957626), Jan 2, 2026: FRAME. CRACKED. CRACKED FRAME, BS 360 BTW S8 - 9R. REPAIRED THE FRAME IAW EA 26-153-00109-WIP1, 26-153-00109-WIP2, & SUMMARY 26-153-00109.
- [SDR SWAA2026020358541](https://openairdocs.org/sdr/SWAA2026020358541), Dec 31, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 194CL BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.
- [SDR SWAA2026020358542](https://openairdocs.org/sdr/SWAA2026020358542), Dec 31, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 194CR BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-8, REPAIR 8.
- [SDR SWAA2026020358543](https://openairdocs.org/sdr/SWAA2026020358543), Dec 31, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 195AL BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCES PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.
- [SDR SWAA2026020358544](https://openairdocs.org/sdr/SWAA2026020358544), Dec 31, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 195AR BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.
- [SDR SWAA2026020358545](https://openairdocs.org/sdr/SWAA2026020358545), Dec 31, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 194HL BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-8, REPAIR 8.
- [SDR SWAA2026020358548](https://openairdocs.org/sdr/SWAA2026020358548), Dec 31, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES OF ACCESS PANEL 194DL WING TO BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-8, REPAIR 8.
- [SDR SWAA2026020358546](https://openairdocs.org/sdr/SWAA2026020358546), Dec 31, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 195BL OF THE BODY FAIRING FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.
- [SDR SWAA2026020358547](https://openairdocs.org/sdr/SWAA2026020358547), Dec 31, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 195BR, BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.
- [SDR SWAA2026020357122](https://openairdocs.org/sdr/SWAA2026020357122), Dec 31, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON THE ACCESS PANEL 661BB AT TRAILING EDGE, RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING T/E IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026020356928](https://openairdocs.org/sdr/SWAA2026020356928), Dec 30, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 193CL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193CL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-9, RE
- [SDR SWAA2026020356929](https://openairdocs.org/sdr/SWAA2026020356929), Dec 30, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 193CR BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-8, REPAIR 8.
- [SDR SWAA2026020356927](https://openairdocs.org/sdr/SWAA2026020356927), Dec 30, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 561BB AT THE RT WING T/E. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026012956608](https://openairdocs.org/sdr/SWAA2026012956608), Dec 30, 2025: SKIN PANEL. CRACKED. CRACK INDICATION FOUND ON THE LT HORIZONTAL STAB LOWER SKIN PANEL HSS 193.9 RIB & 16 INCHES FROM FRONT SPAR, INBD SIDE OF RIB. CRACK LENGTH: 0.900 INCH. REPAIRE
- [SDR SWAA2026020356605](https://openairdocs.org/sdr/SWAA2026020356605), Dec 29, 2025: WIRE. DETERIORATED. DETERIORATED ELECTRICAL WIRING OF EMERGENCY EXIT LIGHT ON CEILING PANEL 231YDC. REPLACED EMERGENCY EXIT LIGHT IAW AMM 33-51-01-960-802, PERFORMED AN OPS TEST. T
- [SDR SWAA2026020356601](https://openairdocs.org/sdr/SWAA2026020356601), Dec 29, 2025: STUB FRAME. CRACKED. CRACK INDICATION ON STUB FRAME, BETWEEN BS 294.5 - 296.5, S8 - 9R IN THE FWD GALLEY DOOR AREA. CRACK LENGTH: 0.875 IN. REPLACED THE STUB FRAME IAW SRM 51-40-02-
- [SDR SWAA2026012956593](https://openairdocs.org/sdr/SWAA2026012956593), Dec 29, 2025: SCUFF PLATE. CRACKED. CRACK ON THE FWD CORNER OF THE SCUFF PLATE IN FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975.
- [SDR SWAA2026012956602](https://openairdocs.org/sdr/SWAA2026012956602), Dec 29, 2025: SCUFF PLATE. CRACKED. CRACK ON THE FWD CORNER OF THE SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.
- [SDR SWAA2025091013319](https://openairdocs.org/sdr/SWAA2025091013319), Sep 10, 2025: SENSOR. FAULTY. WITH FLAP 1 SELECTED FLAPS REMAINED AT 0 AND WOULD NOT EXTEND. FOLLOWED QRH. ALTERNATE FLAPS WERE USED AND PERFORMED 0 FLAP LANDING<[01] TS AND FOUND FC 27-5325
- [SDR SWAA2025090209832](https://openairdocs.org/sdr/SWAA2025090209832), Aug 29, 2025: SEAT. OUT OF ADJUST. SEAT 11 D RECLINES TOO FAR INTO EXIT ROW, SEAT 11D ADJUSTED RECLINE LOCK PER AMM 25-22-00.
- [SDR SWAA2025061281103](https://openairdocs.org/sdr/SWAA2025061281103), Jun 12, 2025: LENS. MISSING. R/H OVERWING EMER EXIT LIGHT LENS MISSING.<[01] REPLACED MISSING LIGHT COVER ON R/H SIDE OVERWING EMER EXIT PER AMM 33-51-01.
- [SDR SWAA2025041523718](https://openairdocs.org/sdr/SWAA2025041523718), Apr 11, 2025: BRACKET. CRACKED. #2 ENG. HIGH STAGE REGULATOR BRACKET HAS A CRACK.
- [SDR SWAA2024120574335](https://openairdocs.org/sdr/SWAA2024120574335), Dec 5, 2024: POWER SUPPLY. DEPLETED. AIRCRAFT ON GROUND POWER EMER EXIT LIGHTS IN ARMED POSITION HALF THE EMERGENCY EXIT LIGHTS ARE ON.<[01] RECHARGED & RESET FWD POWER SUPPLY L&R PER AMM 33-51-06.
- [SDR SWAA2024110856880](https://openairdocs.org/sdr/SWAA2024110856880), Nov 4, 2024: OVERHEAT SENSOR. FAULTED. LEFT WING BODY OVERHEAT LIGHT ILLUMINATED IN CLIMB THEN EXTINGUISHED WHEN ENGINE 1 BLEED SWITCH TURNED OFF<[01] REPLACED M1761 OVHT DETECTOR ON #1 ENGINE FWD ST
- [SDR SWAA2024091236274](https://openairdocs.org/sdr/SWAA2024091236274), Sep 11, 2024: BRACKET. CRACKED. DOOR PANEL 834 DZ AFT MOUNTING BRACKET CRACKED. REPLACED AFT SVC DOOR PANEL 834 DZ AFT MOUNTING BRACKET PER AMM 20-50-11. REPLACED AFT ENTRY DOOR PANEL 834 DZ P

All 213: https://openairdocs.org/aircraft/N7734H/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 CFM56-7B22 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 N7734H

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7734H before.

- [Cancelled 2003-05-20](https://openairdocs.org/deregistered/N7734H-2003-05-20): Robinson Helicopter R22 BETA, S/N 0743, built 1988. Triennial form not returned. Owner: [Holt Helicopters Inc](https://openairdocs.org/faa-owner/HOLT%20HELICOPTERS%20INC), [Uvalde, TX](https://openairdocs.org/faa-place/TX/Uvalde)
- [Cancelled 1973-05-25](https://openairdocs.org/deregistered/N7734H-1973-05-25): Piper PA-12, S/N 12-630. Owner: [Gabaldon Gillie C](https://openairdocs.org/faa-owner/GABALDON%20GILLIE%20C), [East Palatka, FL](https://openairdocs.org/faa-place/FL/East%20Palatka)

## Related

- Other Boeing 737-7BD aircraft: https://openairdocs.org/model/boeing-737-7bd/aircraft.md
- The CFM International CFM56-7B22 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b22-series.md

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