# N7735A: 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: 34862
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 29, 2012
- Certificate issued: September 13, 2012
- Expires: September 30, 2028
- Mode S code: AA7734
- 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=7735A
- Page: https://openairdocs.org/aircraft/N7735A

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

None matched to N7735A.

## NTSB investigations on N7735A not matched to an aircraft (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 MKC88FA018](https://openairdocs.org/ntsb/MKC88FA018), Nov 19, 1987: Cessna 310Q (N7735A), Augusta, KS, destroyed, 1 fatal
- [NTSB FTW79DA074](https://openairdocs.org/ntsb/FTW79DA074), Apr 21, 1979: Lear Jet 35A (N7735A), Rogers, AR, substantial damage

## FAA accident and incident reports

None matched to N7735A.

## Reports on N7735A not matched to an aircraft (2)

They name N7735A, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Accident 19871119066609A](https://openairdocs.org/incident/19871119066609A), Nov 19, 1987: Cessna 310Q (N7735A), Augusta, KS, Destroyed, 1 fatal. Crashed and burned shortly after takeoff. No mechanical defects found. Reason for pilot losing control unknown.
- [Accident 19790421009709A](https://openairdocs.org/incident/19790421009709A), Apr 21, 1979: Lear 35A (N7735A), Rogers, AR, Substantial damage. Pilot was not aligned with the runway on an instrument approach. Made steep turn, hit wing on ground.

## Service difficulty reports (188, 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 SWAA2026021369657](https://openairdocs.org/sdr/SWAA2026021369657), Feb 11, 2026: LENS. DAMAGED. LEFT AND RIGHT OVERWING EXIT LIGHTS ARE DIM. R & R THE OVERWING EXIT LIGHT LENSES IAW AMM 33-21-00.
- [SDR SWAA2026021370219](https://openairdocs.org/sdr/SWAA2026021370219), Feb 11, 2026: DOOR. CRACKED. RIGHT MAIN GEAR CENTER GEAR DOOR IS CRACKED ON FWD WEB. REMOVED THE RT CENTER AND INNER GEAR DOOR IAW MM 32-13-11. OK TO CONTINUE.
- [SDR SWAA2026021269646](https://openairdocs.org/sdr/SWAA2026021269646), Feb 11, 2026: ISOLATOR. CRACKED. AFT ENTRY DOOR FWD UPPER SLIDE ISOLATOR CRACKED. R & R AFT ENTRY DOOR FWD UPPER SLIDE ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2026021269658](https://openairdocs.org/sdr/SWAA2026021269658), Feb 11, 2026: ISOLATOR. CRACKED. PASSENGER CABIN, FORWARD GALLEY SERVICE DOOR AFT UPPER SLIDE ISOLATOR CRACKED. R & R THE UPPER SLIDE ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2025123055899](https://openairdocs.org/sdr/SWAA2025123055899), Dec 27, 2025: HOOK. LOOSE. L1 DOOR SLIDE J HOOK LOOSE PERM RESOLUTION. REMOVED TEMP FASTENER AND INSTALLED PERM FASTENER PER SRM 51-40-02 AND AIPC 25-66-00.
- [SDR SWAA2025122354578](https://openairdocs.org/sdr/SWAA2025122354578), Dec 21, 2025: HOOK. LOOSE. L1 SLIDE FWD J HOOK LOOSE. ACCOMPLISHED EA M-23-01859. INSTALLED NEW FASTNER IN L1 SLIDE FWD J HOOK.
- [SDR SWAA2025071189749](https://openairdocs.org/sdr/SWAA2025071189749), Jul 10, 2025: PLATE. DETACHED. F/A REPORTS 1R DOOR HANDLE TRIM PLATE DETACHED. REMOVED AND REPLACED DOOR HANDLE INSERT ASSY REF M/M 52-41-00.
- [SDR SWAA2025070186321](https://openairdocs.org/sdr/SWAA2025070186321), Jun 28, 2025: BATTERY PACK. INOPERATIVE. LH OVER WING EXIT EMER LIGHT OUT. R & R LH OVER WING EXIT EMER LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2025050565264](https://openairdocs.org/sdr/SWAA2025050565264), Apr 29, 2025: BATTERY PACK. INOPERATIVE. LEFT SIDE EMERGENCY OVERWING LIGHT OUT<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024111358366](https://openairdocs.org/sdr/SWAA2024111358366), Nov 10, 2024: LIGHT. DETACHED. LIGNTING STRIP LAST ROW ON CA SIDE DETACHED<[01] ATTACHED PHOTOLUMIECENT STRIP ON LAST ROW CA SIDE PER AMM 33-51-15
- [SDR SWAA2024090935109](https://openairdocs.org/sdr/SWAA2024090935109), Sep 6, 2024: SLIDE. OUT OF ADJUST. R1 DOOR SCAPE SLIDE REQUIRES REPACKING<[01] REMOVED AND REINSTALLED ORIGINAL R1 DOOR SLIDE REF SWA MT 725-61-06
- [SDR SWAA2024042377514](https://openairdocs.org/sdr/SWAA2024042377514), Apr 21, 2024: LIGHT. INOPERATIVE. INOP EXTERNAL SKIN EMERGENCY EGRESS EXIT LIGHT NEXT TO AFT SERVICE DOOR AT UPPER FUSELAGE (1 EA) 2024-206689<[01] REPLACED FUSE AT POWER SUPPLY AND TEST IS OK I
- [SDR SWAA2024041968330](https://openairdocs.org/sdr/SWAA2024041968330), Mar 27, 2024: BATTERY PACK. INOPERATIVE. INOP LOWERED CEILING PANEL BATTERY PACK AT AFT GALLEY AREA (2 EA) 2024-206646<[01] REPLACED LOWERED CEILING PANEL BATTERY PACK AT AFT GALLEY AREA (2 EA) IAW B73
- [SDR SWAA2024042577422](https://openairdocs.org/sdr/SWAA2024042577422), Mar 26, 2024: INTERCOSTAL. CRACKED. A FASTENER INSTALLED ON INTERCOSTAL REPAIR; STA 312; STR 23L MAY NOT MEET THE 2D MINIMUM EDGE MARGIN SPECIFIED IN THE REPAIR. REPLACED REPAIR PARTS -2 ANGLE AND
- [SDR SWAA2024042467997](https://openairdocs.org/sdr/SWAA2024042467997), Mar 26, 2024: FLOORBEAM. CRACKED. (CUSTOMER REQUEST) PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75 2024-206638<[01] REPLACED STRUCTURE SUPPORT LOC PASSENGER CA
- [SDR SWAA2024042467996](https://openairdocs.org/sdr/SWAA2024042467996), Mar 26, 2024: FLOORBEAM. CRACKED. (CUSTOMER REQUEST) PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75 2024-206637<[01] REPLACED FLOOR STRUCTURE SUPPORT LOC STA 54
- [SDR SWAA2024042567084](https://openairdocs.org/sdr/SWAA2024042567084), Mar 23, 2024: PLATE. CRACKED. CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED IRSS217 AT RT WING. REPLACED CORRUGATED PLATE AND FASTENER TRAILING EDGE LOCATED IRSS217 AT RT WING. IAW SRM 51-
- [SDR SWAA2024042567155](https://openairdocs.org/sdr/SWAA2024042567155), Mar 23, 2024: BRACKET. CRACKED. CRACK ON SUPPORT BRACKET LOCATED IRSS140 UPPER POSITION TRAILING EDGE RT WING. REPLACED SUPPORT BRACKET LOCATED IRSS140 UPPER POSITION TRAILING EDGE RT WING IAW
- [SDR SWAA2024042567154](https://openairdocs.org/sdr/SWAA2024042567154), Mar 23, 2024: BRACKET. CORRODED. CORROSION ON BRACKET LOCATED BOOST PUMP TANK 2 TRAILING EDGE IRSS144 RT WING (2E/A). BONDING RESISTANCE CHECK IS OK. REPLACED BRACKET LOC BOOST PUMP TANK 2 TRAI
- [SDR SWAA2024042567159](https://openairdocs.org/sdr/SWAA2024042567159), Mar 23, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE ON AUXILIARY TRACK SLAT 6 INBOARD POSITION RT WING 2024-206585<[01] REPLACED SUPPORT ANGLE LOCATED ON AUXILIARY TRACK SLAT 6 INBOARD POSITIO
- [SDR SWAA2024042567156](https://openairdocs.org/sdr/SWAA2024042567156), Mar 23, 2024: BRACKET. CORRODED. CORROSION ON BRACKET LOCATED BOOST PUMP TANK 1 TRAILING EDGE IRSS144 LT WING (2E/A). REPLACED BRACKET LOCATED BOOST PUMP TANK 1 TRAILING EDGE IRSS144 LT WING (2
- [SDR SWAA2024042566924](https://openairdocs.org/sdr/SWAA2024042566924), Mar 22, 2024: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BS 500D, STR19R AT WING TO BODY FAIRING. REPLACED SUPPORT ANGLE IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, & DRAWING 116A3010 REV. C 
- [SDR SWAA2024042566108](https://openairdocs.org/sdr/SWAA2024042566108), Mar 21, 2024: CARGO TRACK. CRACKED. CRACK ON TRACK RBL 13.84 LOCATED BS747 AFT CARGO COMPARTMENT 2024-206507<[01] PERFORMED PERMANENT REPAIR ON CARGO TRACK RBL 13.84 LOCATED BTW BS 727E TO BS 787 
- [SDR SWAA2024042566105](https://openairdocs.org/sdr/SWAA2024042566105), Mar 21, 2024: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS907 PLUS 11 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT 2024-206504<[01] REPLACED ANGLE - SUPPORT LOCATED BS907 PLUS 1
- [SDR SWAA2024042566106](https://openairdocs.org/sdr/SWAA2024042566106), Mar 21, 2024: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS867 AND BTW STR26L TO STR27L AFT CARGO COMPARTMENT 2024-206505<[01] REPLACED ANGLE - SUPPORT LOCATED BS867 AND BTW STR26L TO STR
- [SDR SWAA2024042566509](https://openairdocs.org/sdr/SWAA2024042566509), Mar 21, 2024: SUPPORT ANGLE. CRACKED. CRACK ANGLE SUPPORT TRAILING EDGE LOCATED ORSS273 LT WING. REPLACED ANGLE SUPPORT TRAILING EDGE LOCATED ORSS273 LT WING IAW B737-700 SRM 51-10-02 ITEM 9.
- [SDR SWAA2024042466107](https://openairdocs.org/sdr/SWAA2024042466107), Mar 21, 2024: CARGO TRACK. CRACKED. CRACK ON TRACK RBL 13.84 LOCATED BS767 AFT CARGO COMPARTMENT 2024-206506<[01] PERFORMED PERMANENT REPAIR ON CARGO TRACK RBL 13.84 LOCATED BTW BS 727E TO BS 787 
- [SDR SWAA2024042565596](https://openairdocs.org/sdr/SWAA2024042565596), Mar 19, 2024: FLOORBEAM. CORRODED. CORROSION FLOOR BEAM LOCATED BS 294.5; RBL 28; WL 208.1 AT PASSENGER CABIN 2024-206368<[01] TOOL USED ON STEP 3. UT EQUIPMENT P/N: 45MG; S/N: 130061901; CAL DUE
- [SDR SWAA2024042465603](https://openairdocs.org/sdr/SWAA2024042465603), Mar 19, 2024: SUPPORT. CRACKED. CRACK SUPPORT -ZEE LOCATED STA 500A AND STR 26L AT FWD CARGO COMPARTMENT 2024-206391<[01] REPLACED SUPPORT-ZEE LOCATED STA 400 TO STA 500D S26L AT FWD CARGO COM
- [SDR SWAA2024042465601](https://openairdocs.org/sdr/SWAA2024042465601), Mar 19, 2024: WEB. CRACKED. CRACK WEB - INTERCOSTAL LOCATED BTW STA 500 TO STA 500A AT LEVEL STR 26L FWD CARGO COMPARTMENT 2024-206375<[01] REPLACED WEB - INTERCOSTAL LOCATED BTW STA 500 T
- [SDR SWAA2024042465602](https://openairdocs.org/sdr/SWAA2024042465602), Mar 19, 2024: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL LOCATED BTW STA 440 TO STA 460 AND STR 26L FWD CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL LOCATED BTW STA 440 TO STA 460 AND STR 26L 
- [SDR SWAA2024042565226](https://openairdocs.org/sdr/SWAA2024042565226), Mar 18, 2024: FLOORBEAM. CORRODED. CORROSION ON FLOOR BEAM LOCATED BS986.5 AT LEVEL RBL44 AND WL208.1 AT AFT GALLEY AREA 2024-206339<[01] EDDY CURRENT EQUIPMENT USED P/N : NORTE 600D ; S/N : 2101
- [SDR SWAA2024042465229](https://openairdocs.org/sdr/SWAA2024042465229), Mar 18, 2024: WEB. CRACKED. CRACK WEB LOCATED BS294.5 TO BS303.9 AT LEVEL STR16L AT PASSENGER CABIN 2024-206345<[01] REPLACED WEB LOCATED BS294.5 TO BS303.9 AT LEVEL STR16L AT PASSENGER CA
- [SDR SWAA2024042465222](https://openairdocs.org/sdr/SWAA2024042465222), Mar 18, 2024: NOT REPORTED. CRACKED. CRACK INNER CHORD LOCATED BS 294.5 PLUS 8 INCHES; LBL 55 AT FWD GALLEY AREA 2024-206333<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A20231600 DUE DATE: 
- [SDR SWAA2024042365221](https://openairdocs.org/sdr/SWAA2024042365221), Mar 18, 2024: WEB. CRACKED. CRACK FLOOR STRUCTURE WEB LOCATED BETWEEN BS 312 AND BS 328; RBL 30.5 AT FWD GALLEY AREA 2024-206332<[01] REPLACED WEB LOCATED BETWEEN BS 312 AND BS 328; RBL 30
- [SDR SWAA2024041965228](https://openairdocs.org/sdr/SWAA2024041965228), Mar 18, 2024: FRAME. CRACKED. CRACK FRAME LOCATED BS 312 AT LEVEL STR 5L TO 6L AT PASSENGER CABIN. REPAIRED FRAME LOCATED BS312 AT LEVEL STR5L TO STR6L AT PASSENGER CABIN IAW EA#M-22-153-012
- [SDR SWAA2024041965223](https://openairdocs.org/sdr/SWAA2024041965223), Mar 18, 2024: TIE CLIP. CRACKED. CRACK TIE CLIP LOCATED BS277 AT LEVEL STR10R AT PASSENGER CABIN 2024-206334<[01] REPLACED TIE CLIP LOCATED BS277 AT LEVEL STR10R AT PASSENGER CABIN IAW B737-700
- [SDR SWAA2024042464448](https://openairdocs.org/sdr/SWAA2024042464448), Mar 16, 2024: FLOOR PANEL. DAMAGED. ELONGATED HOLE FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT 2024-206192<[01] REPLACED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-05; SRM 51
- [SDR SWAA2024042464551](https://openairdocs.org/sdr/SWAA2024042464551), Mar 16, 2024: PRESSURE DECK. CRACKED. CRACK INDICATION FOUND IN HORIZONTAL PRESSURE DECK WEB LOCATED AT BS 663 AND LBL 32. CRACK LENGTH IS L= 0.350 INCHES. REPAIRED HORIZONTAL PRESSURE DECK WEB LOC 
- [SDR SWAA2024042464547](https://openairdocs.org/sdr/SWAA2024042464547), Mar 16, 2024: FITTING. DETERIORATED. DETERIORATE GIRT BAR FITTING PLATE (4EA) AND SHIM (4EA) ON POSITION SERVICE DOOR AND ENTRY DOOR AT AFT GALLEY AREA 2024-206212<[01] REPLACED GIRT BAR FITTING PL
- [SDR SWAA2024041964438](https://openairdocs.org/sdr/SWAA2024041964438), Mar 16, 2024: FLOOR PANEL. DAMAGED. ELONGATED HOLE FLOOR PANEL 140DF AT AFT CARGO COMPARTMENT 2024-206193<[01] FABRICATED FLOOR PANEL 140DF AT AFT CARGO COMPARTMENT IAW AMM 25-52-01-201-801 SEE IN
- [SDR SWAA2024041964548](https://openairdocs.org/sdr/SWAA2024041964548), Mar 16, 2024: LIGHT. BROKEN. BROKEN EMERGENCY LIGHT ASSY ON LOWERED CEILING PANEL AT AFT GALLEY AREA (1EA) 2024-206213<[01] REPLACED EMERGENCY LIGHT ASSY ON LOWERED CEILING PANEL AT AFT GAL
- [SDR SWAA2024041964200](https://openairdocs.org/sdr/SWAA2024041964200), Mar 15, 2024: SCUFF PLATE. CRACKED. CRACK SCUFF PLATE FWD CORNER AT FWD CARGO COMPARTMENT 2024-206148<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30; S/N: A23329368; DUE DATE: 06/MAR/25.;[02] TOOL 
- [SDR SWAA2024042463466](https://openairdocs.org/sdr/SWAA2024042463466), Mar 14, 2024: NUT. DETERIORATED. DETERIORATE NUT OF HANDLE ON ENTRY DOORWAY LINING AT FWD GALLEY AREA (2EA) 2024-206070<[01] REPLACED NUT OF HANDLE ON ENTRY DOORWAY LINING AT FWD GALLEY AREA (2
- [SDR SWAA2024022053680](https://openairdocs.org/sdr/SWAA2024022053680), Feb 18, 2024: GIRT BAR. LOOSE. FWD SERVICE DOOR EMERGENCY SLIDE GIRT BAR BRACKET LOSE<[01] REPAIRED FWD SERVICE DOOR SLIDE GIRT BAR BRACKET IAW EA M-23-125-01839.
- [SDR SWAA2024013146546](https://openairdocs.org/sdr/SWAA2024013146546), Jan 30, 2024: RETAINER. DAMAGED. DURING ROTATION LEFT INNER MAIN TIRE BLEW; AND ANTI-SKID LIGHT ILLUMINATED. RETURNED FOR A NORMAL LANDING W/NO ABNORMAL INDICATIONS. NO OVERWEIGHT LANDING; NO H
- [SDR SWAA2024013147039](https://openairdocs.org/sdr/SWAA2024013147039), Jan 30, 2024: ELECTRICAL BOX. DAMAGED. DURING ROTATION LEFT INNER MAIN TIRE BLEW; AND ANTI-SKID LIGHT ILLUMINATED. RETURNED FOR A NORMAL LANDING W/NO ABNORMAL INDICATIONS. NO OVERWEIGHT LANDING; NO H
- [SDR SWAA2024013147040](https://openairdocs.org/sdr/SWAA2024013147040), Jan 30, 2024: GUIDE. DAMAGED. DURING ROTATION LEFT INNER MAIN TIRE BLEW; AND ANTI-SKID LIGHT ILLUMINATED. RETURNED FOR A NORMAL LANDING W/NO ABNORMAL INDICATIONS. NO OVERWEIGHT LANDING; NO H
- [SDR SWAA2024013147041](https://openairdocs.org/sdr/SWAA2024013147041), Jan 30, 2024: BRACKET. DAMAGED. DURING ROTATION LEFT INNER MAIN TIRE BLEW; AND ANTI-SKID LIGHT ILLUMINATED. RETURNED FOR A NORMAL LANDING W/NO ABNORMAL INDICATIONS. NO OVERWEIGHT LANDING; NO H
- [SDR SWAA2023120828839](https://openairdocs.org/sdr/SWAA2023120828839), Dec 7, 2023: BATTERY PACK. FAILED. FWD SERVICE & FWD ENTRY DOOR EMERGENCY LIGHTS (GROUP) DID NOT WORK<[01] R&R FWD GALLEY L/H & R/H BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD.

All 188: https://openairdocs.org/aircraft/N7735A/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 N7735A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7735A before.

- [Cancelled 1956-10-17](https://openairdocs.org/deregistered/N7735A-1956-10-17): Cessna 180, S/N 32632. 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 CFM56-7B22 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b22-series.md

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