# N7737E: 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 CFM56-7B20 series](https://openairdocs.org/engine/cfm-international-cfm56-7b20-series) (registry code 13042)
- Serial number: 33929
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 24, 2014
- Certificate issued: August 19, 2014
- Expires: August 31, 2027
- Mode S code: AA777E
- 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=7737E
- Page: https://openairdocs.org/aircraft/N7737E

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 CFM56-7B20 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 CFM56-7B20 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 N7737E.

## 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.

- [Incident 20181019020379I](https://openairdocs.org/incident/20181019020379I), Oct 19, 2018: Boeing 737-7BD (N7737E), Chicago, IL, Minor damage. Review of the security footage indicated that the tug driver started turning the aircraft to the left too soon after pushback. This caused the aircraft to be…

## Service difficulty reports (217, 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 SWAA2025100821659](https://openairdocs.org/sdr/SWAA2025100821659), Oct 6, 2025: LAMP. INOPERATIVE. EMERGENCY LIGHT AT SEAT ROW 19DEF INOPERATIVE. REPLACED THE LAMP EMERGENCY LIGHT AREA LIGHT AT 19DEF PER AMM 33-51-03.
- [SDR SWAA2025061280284](https://openairdocs.org/sdr/SWAA2025061280284), Jun 11, 2025: SEAT BACK. OUT OF ADJUST. SEAT 11B (IN EMERGENCY EXIT ROW) RECLINES.<[01] C/W;[02] ADJUSTED HYDRO-LOCKS TO THE LOCKED POSITION PER AMM 25-22-00
- [SDR SWAA2025061280564](https://openairdocs.org/sdr/SWAA2025061280564), Jun 11, 2025: LAMP. INOPERATIVE. RIGHT EMERGENCY EXIT OVERHEAD LIGHT IS INOP.<[01] RELAMPED PER AMM 33-51-01;[02] VERIFIED RELAMPED PER AMM 33-51-01
- [SDR SWAA2025061180289](https://openairdocs.org/sdr/SWAA2025061180289), Jun 11, 2025: SCUFF PLATE. CRACKED. FORWARD CARGO THRESHOLD BULLNOSE IS SPLIT; CRACKED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-11-02-401-NG (CARGO DOOR SCUFF PLATE - REMOVAL/INSTALLATION - PER
- [SDR SWAA2025012288226](https://openairdocs.org/sdr/SWAA2025012288226), Jan 22, 2025: GIRT BAR. OUT OF POSITION. R1 DOOR ESCAPE SLIDE GIRT REQUIRES REPACK.<[01] REPACKED R1 DOOR ESCAPE SLIDE GIRT PER MT257-61-06 AND AMM 25-66-01
- [SDR SWAA2024091236467](https://openairdocs.org/sdr/SWAA2024091236467), Sep 11, 2024: LAMP. INOPERATIVE. R2 DOOR EMERGENCY LIGHT INOP. RELAMPED R2 DOOR EMERGENCY LIGHT PER AMM 33-51-04-960-801.
- [SDR SWAA2024090331237](https://openairdocs.org/sdr/SWAA2024090331237), Aug 28, 2024: SEAL. CRACKED. RIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDER CRACKED.<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL PER AMM 53-31-31.
- [SDR SWAA2024083031236](https://openairdocs.org/sdr/SWAA2024083031236), Aug 28, 2024: SLIDE. OUT OF POSITION. R2 GALLEY DOOR SLIDE LOWER FLAP REQUIRES REPOSITION.<[01] REPOSITIONED ESCAPE SLIDE LOWER FLAP PER AMM 25-66-01 R2 DOOR
- [SDR SWAA2024072214639](https://openairdocs.org/sdr/SWAA2024072214639), Jul 19, 2024: POWER SUPPLY. FAULTY. EMERGENCY EXIT LIGHTS ARC HALF ON HALF OFF WITH AIRCRAFT ON GROUND POWER ON APU POWER.<[01] R/R RIGHT AFT POWER SUPPLY AS PER AMM 33-51-06. OPS CK OK. NO FAULTS
- [SDR SWAA2024071512491](https://openairdocs.org/sdr/SWAA2024071512491), Jul 14, 2024: ADIRU. UNRELIABLE. CREW REPORTS F/O LOST FLIGHT DISPLAY; AIRSPEED UNRELIABLE AND MACH A/S WARNING CONTINUOUS.<[01] R/R #2 ADIRU PER AMM 34-21-01. OPS CHECK GOOD. AIRCRAFT RECERTIF
- [SDR SWAA2024071108301](https://openairdocs.org/sdr/SWAA2024071108301), Jul 3, 2024: BATTERY PACK. INOPERATIVE. ALL EMERGENCY LIGHTS ASSOCIATED WITH EMERGENCY EXIT LIGHT BATTERY PACKS M1669 AND M1668 ARE INOP<[01] REMOVED AND REPLACED BOTH BATTERY PACKS M1669 AND M1668; P
- [SDR SWAA2024071106961](https://openairdocs.org/sdr/SWAA2024071106961), Jun 28, 2024: LENS. BROKEN. G4 GALLEY EMERGENCY LIGHT LENS BROKEN<[01] REMOVED AND REPLACED G4 GALLEY EMERGENCY LIGHT LENS PER AMM 33-51-01-960-802.;[02] VERIFIED REPLACEMENT OF G4 GALLEY 
- [SDR SWAA2024071106062](https://openairdocs.org/sdr/SWAA2024071106062), Jun 26, 2024: CONNECTOR. DAMAGED. G4 GALLEY LOWER EMERGENCY EXIT LIGHT HAS DAMAGED CONNECTORS.<[01] REPLACED CONNECTORS FOR G4 GALLEY LOWER EMERGENCY EXIT LIGHT AND PERFORMED GOOD OPERATIONAL CH
- [SDR SWAA2024071105682](https://openairdocs.org/sdr/SWAA2024071105682), Jun 25, 2024: LENS. BROKEN. FWD LAV 'A' EMERGENCY EXIT LIGHT LENS BROKEN<[01] REMOVED AND REPLACED FWD LAV 'A' EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01-960-802.;[02] VERIFIED FWD LAV 'A'
- [SDR SWAA2024071100096](https://openairdocs.org/sdr/SWAA2024071100096), Jun 10, 2024: ATTACH ANGLE. CRACKED. L/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL8 WL167.68<[01] CORRECTION ON STEPS 8 AND 10 (ITEMS 3;4) REFERENCE SHOULD BE SRM 57-10-10-2R-5 REPAI
- [SDR SWAA2024071198551](https://openairdocs.org/sdr/SWAA2024071198551), Jun 5, 2024: SEAT TRACK. CORRODED. CORROSION ON RH SEAT TRACK BS 559+ 3 WELL; 597-5 WELL; 685-3 CROWN; 685-6 WELL; 694 CROWN; 694 WELL; 706-3 WELL; 727-3 WELL; 727A+8 WELL; 727A+8 CROWN; RBL 45; 
- [SDR SWAA2024071198731](https://openairdocs.org/sdr/SWAA2024071198731), Jun 5, 2024: FLOORBEAM. CORRODED. CORROSION ON FLOOR BEAM BS 986 BL0-RBL 43 AND LBL 43 WL 208.<[01] REMOVED AND REPAIRED DAMAGE UPPER FLANGES OF THE BS986 T-CHORD LBL50-RBL50 I.A.W SRM 53-70-51-
- [SDR SWAA2024071198734](https://openairdocs.org/sdr/SWAA2024071198734), Jun 5, 2024: SHEAR WEB. CORRODED. CORROSION ON R/H AFT SHEAR WEB BS 1016-1029 BL0-RBL 14 WL 208.<[01] REMOVED AND REPLACED R/H SHEAR WEB BS 1016-1029 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5
- [SDR SWAA2024071198727](https://openairdocs.org/sdr/SWAA2024071198727), Jun 5, 2024: SHEAR WEB. CORRODED. CORROSION ON L/H AFT SHEAR WEB BS 1016-1026 BL0-LBL 12 WL 208.<[01] REMOVED AND REPLACED SHEAR WEB BS 1016-1029 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5600;
- [SDR SWAA2024071198735](https://openairdocs.org/sdr/SWAA2024071198735), Jun 5, 2024: STRAP. CORRODED. CORROSION ON REINFORCEMENT STRAP BS 1027 RBL 17 WL 208.<[01] COMPLETED STEPS 1 & 3.;[02] REMOVED AND REPLACED A NEW TENSION STRAP BS1006-BS1027 RBL 17 WL208 I.A
- [SDR SWAA2024071198728](https://openairdocs.org/sdr/SWAA2024071198728), Jun 5, 2024: STRAP. CORRODED. CORROSION ON REINFORCEMENT STRAP BS 1018-1027 RBL 2.5 WL 208.<[01] COMPLETED STEPS 1 AND 3.;[02] REMOVED AND REPLACED A NEW TENSION STRAP BS1006-BS1027 RBL 3 WL
- [SDR SWAA2024071198729](https://openairdocs.org/sdr/SWAA2024071198729), Jun 5, 2024: STRAP. CORRODED. CORROSION ON REINFORCEMENT STRAP BS 1023 LBL 3.5 WL 208.<[01] REMOVED AND REPLACED A NEW TENSION STRAP BS1006-BS1027 LBL 3.5 WL208 I.A.W SRM 51-40-02-0G-0 AND B
- [SDR SWAA2024071198730](https://openairdocs.org/sdr/SWAA2024071198730), Jun 5, 2024: STRAP. CORRODED. CORROSION ON REINFORCEMENT STRAP BS 1025-1028 LBL 17.5 WL 208.<[01] OK TO INSTALL STRAP.;[02] REMOVED AND REPLACED A NEW TENSION STRAP BS1006-BS1027 LBL 17.5 WL
- [SDR SWAA2024071098722](https://openairdocs.org/sdr/SWAA2024071098722), Jun 5, 2024: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BS 380-400 RBL 8 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL BS 380-400 RBL 8 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 143A5400;[02] 
- [SDR SWAA2024071098721](https://openairdocs.org/sdr/SWAA2024071098721), Jun 5, 2024: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BS 380-400 LBL 14 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL BS 380-400 LBL 14 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 143A5400
- [SDR SWAA2024071098720](https://openairdocs.org/sdr/SWAA2024071098720), Jun 5, 2024: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BS 380-400 LBL 1 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 380-400 LBL1 WL 208. I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 143A5400;[0
- [SDR SWAA2024071098719](https://openairdocs.org/sdr/SWAA2024071098719), Jun 5, 2024: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BS 380-400 RBL 41 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL BS 380-400 RBL 41 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 143A5400
- [SDR SWAA2024071098713](https://openairdocs.org/sdr/SWAA2024071098713), Jun 5, 2024: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BS 328-344 LBL 46 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL BS328-BS344 LBL46 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DOCUMENT 141A540
- [SDR SWAA2024071098718](https://openairdocs.org/sdr/SWAA2024071098718), Jun 5, 2024: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BS 312-328 LBL 44 WL 208.<[01] INSTALLED NEW INTERCOSTAL BS 312-328 LBL 44 WL 208 I.A.W. SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION E
- [SDR SWAA2024071098717](https://openairdocs.org/sdr/SWAA2024071098717), Jun 5, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL BS 312-328 RBL 31 WL 208.<[01] INSTALLED INTERCOSTAL BS 312-328 RBL 31 WL 208 SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WIT
- [SDR SWAA2024071098716](https://openairdocs.org/sdr/SWAA2024071098716), Jun 5, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL BS 277-294 RBL 1 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL BS 277-294 RBL 1 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5400
- [SDR SWAA2024071098715](https://openairdocs.org/sdr/SWAA2024071098715), Jun 5, 2024: ANGLE. CRACKED. CRACKED ANGLE BS 294 RBL 55 WL 208.<[01] UPDATED STEPS 4 AND 5.;[02] REMOVED DAMAGE ANGLE AND INSTALLED REPAIR ANGLE BS291-294.5 RBL55 WL 208 IAW SRM 53-10-15-2
- [SDR SWAA2024071098714](https://openairdocs.org/sdr/SWAA2024071098714), Jun 5, 2024: FLOORBEAM. CRACKED. CRACKED FLOOR BEAM BS 294 RBL 53 WL 208.<[01] REMOVED DAMAGED SECTION OF UPPER CHORD; REPLACED WITH NEW SECTION OF UPPER CHORD AND INSTALLED REPAIR PARTS AT BS2
- [SDR SWAA2024071198007](https://openairdocs.org/sdr/SWAA2024071198007), Jun 3, 2024: CARGO TRACK. CRACKED. AFT CARGO BAY CARGO TRACK IS CRACKED BS747 AND BS767 RBL13 WL155<[01] REMOVED AND REPLACED TRACK AS PER 737-700 SRM 53-00-53-3; EA 24-153-01519 AND DRAWING 146A
- [SDR SWAA2024071198012](https://openairdocs.org/sdr/SWAA2024071198012), Jun 3, 2024: STRAP. CORRODED. CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727D+6 RBL11.5 WL156<[01] EVALUATED CORROSION ON FLOOR SPLICE STRAP BS 727D+6 RBL 11.5 WL 156
- [SDR SWAA2024071198008](https://openairdocs.org/sdr/SWAA2024071198008), Jun 3, 2024: SUPPORT PLATE. CORRODED. CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] EVALUATED CORROSION; FOUN
- [SDR SWAA2024071198000](https://openairdocs.org/sdr/SWAA2024071198000), Jun 3, 2024: ANGLE. CRACKED. RIGHT WING; I/B UPPER T/E PANEL JUST AFT OF REAR SPAR; UPPER U SUPPORT CHANEL FWD ATTACH ANGLE IS CRACKED<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-
- [SDR SWAA2024071097642](https://openairdocs.org/sdr/SWAA2024071097642), Jun 2, 2024: SCUFF PLATE. CRACKED. FSD; SCUFF PLATE AFT SIDE IS CRACKED 3 INCHES.<[01] FUSION WELDED THE DAMAGED AREA ON SCUFF PLATE IAW SRM53-10-15-2R-2. PT INSPECTED WELDED AREA PER SOPM 20-20-
- [SDR SWAA2024071197337](https://openairdocs.org/sdr/SWAA2024071197337), Jun 1, 2024: FLOORBOARD. DELAMINATED. PASSENGER CABIN FLOOR BOARD 241ZF IS DELAMINATED<[01] PASSENGER CABIN FLOOR BOARD 241ZF WITH UPPER SKIN DELAMINATION WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] JO
- [SDR SWAA2024071197339](https://openairdocs.org/sdr/SWAA2024071197339), Jun 1, 2024: FLOORBOARD. DELAMINATED. PASSENGER CABIN FLOOR BOARD 242VF IS DELAMINATED<[01] DELAMINATION ON PASSENGER CABIN FLOOR PANEL 242VF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORREC
- [SDR SWAA2024071197340](https://openairdocs.org/sdr/SWAA2024071197340), Jun 1, 2024: FLOORBOARD. DELAMINATED. PASSENGER CABIN FLOOR BOARD 242SF IS DELAMINATED<[01] DELAMINATED UPPER SURFACE OF PASSENGER CABIN FLOOR PANEL 242SF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JO
- [SDR SWAA2024071197343](https://openairdocs.org/sdr/SWAA2024071197343), Jun 1, 2024: FLOORBOARD. DELAMINATED. PASSENGER CABIN FLOOR BOARD 242AF IS DELAMINATED<[01] PASSENGER CABIN FLOOR BOARD 242AF WITH DELAMINATED WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SR
- [SDR SWAA2024071197346](https://openairdocs.org/sdr/SWAA2024071197346), Jun 1, 2024: FLOORBOARD. DELAMINATED. PASSENGER CABIN FLOOR BOARD 232RF IS DELAMINATED<[01] PASSENGER CABIN FLOOR BOARD 232RF WITH DELAMINATED WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SR
- [SDR SWAA2024071197336](https://openairdocs.org/sdr/SWAA2024071197336), Jun 1, 2024: FLOORBOARD. DELAMINATED. PASSENGER CABIN FLOOR BOARD 241XF IS DELAMINATED<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR BOARD 241XF IAW SRM 51-10-02-0G-0 PARA 9 AND D
- [SDR SWAA2024071197338](https://openairdocs.org/sdr/SWAA2024071197338), Jun 1, 2024: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR BOARD 241UF IS DELAMINATED<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241UF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1553922-1; INSTALLED 
- [SDR SWAA2024071097341](https://openairdocs.org/sdr/SWAA2024071097341), Jun 1, 2024: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR BOARD 241EF IS DELAMINATED<[01] FABRICATED 241EF FLOORBOARD IAW SRM 53-00-50-2R-0 ALONG WITH DWG: 144A5810 SHEET: 129;[02] VERIFIED CORREC
- [SDR SWAA2024071097342](https://openairdocs.org/sdr/SWAA2024071097342), Jun 1, 2024: FLOORBOARD. DELAMINATED. PASSENGER CABIN FLOOR BOARD 242DF IS DELAMINATED<[01] FABRICATED 242DF FLOORBOARD IAW SRM 53-00-50-2R-0 ALONG WITH DWG: 144A5810 SHEET: 3.;[02] VERIFIED CORRECT
- [SDR SWAA2024071097344](https://openairdocs.org/sdr/SWAA2024071097344), Jun 1, 2024: FLOORBOARD. DELAMINATED. PASSENGER CABIN FLOOR BOARD 241BF IS DELAMINATED<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241BF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.
- [SDR SWAA2024071097345](https://openairdocs.org/sdr/SWAA2024071097345), Jun 1, 2024: FLOORBOARD. DELAMINATED. PASSENGER CABIN FLOOR BOARD 241AF IS DELAMINATED<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 241AF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.
- [SDR SWAA2024071097333](https://openairdocs.org/sdr/SWAA2024071097333), Jun 1, 2024: FLOORBOARD. DELAMINATED. PASSENGER CABIN FLOOR BOARD 222B IS DELAMINATED<[01] DELAMINATIONS ON PASSENGER CABIN FLOOR BOARD 222B WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.

All 217: https://openairdocs.org/aircraft/N7737E/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 CFM56-7B20 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 N7737E

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7737E before.

- [Cancelled 1973-06-25](https://openairdocs.org/deregistered/N7737E-1973-06-25): Cessna 150, S/N 150-17537. Owner: [Ruby Glenn](https://openairdocs.org/faa-owner/RUBY%20GLENN), [Sigourney, IA](https://openairdocs.org/faa-place/IA/Sigourney)

## Related

- Other Boeing 737-7BD aircraft: https://openairdocs.org/model/boeing-737-7bd/aircraft.md
- The CFM International CFM56-7B20 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b20-series.md

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