# N7829B: 2003 Boeing 737-7CT

- Status: Valid registration
- Airframe: [Boeing 737-7CT](https://openairdocs.org/model/boeing-737-7ct) (registry code 13844NE, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 32751
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 21, 2015
- Certificate issued: June 3, 2015
- Expires: June 30, 2028
- Mode S code: AA9B89
- 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=7829B
- Page: https://openairdocs.org/aircraft/N7829B

From the FAA registry file of October 27, 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 737-7CT)

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 N7829B.

## FAA accident and incident reports

None matched to N7829B.

## Service difficulty reports (165, 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 SWAA2023081487954](https://openairdocs.org/sdr/SWAA2023081487954), Aug 10, 2023: SIGN. LOOSE. AFT EMERGENCY EXIT SIGN LOOSE.<[01] RE-SECURED AFT EMERGENCY EXIT SIGN; REF AMM 33-51-14.
- [SDR SWAA2023050946535](https://openairdocs.org/sdr/SWAA2023050946535), May 7, 2023: LIGHT. BROKEN. EMERGENCY LIGHT NEAR FLOOR FORWARD OF RIGHT EMERGENCY EXIT IS BROKEN<[01] REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY FORWARD OF RIGHT EMERGENCY EXIT DOOR NEA
- [SDR SWAA2023050846639](https://openairdocs.org/sdr/SWAA2023050846639), May 6, 2023: SIGN. MISSING. SMALL VERTICAL EMERGENCY EXIT SIGN MISSING FO SIDE OVERWING EXIT<[01] REPLACED FO SIDE OVERWING EMERGENCY EXIT SIGN LENS; IAW AMM 33-51-03.
- [SDR SWAA2023042028428](https://openairdocs.org/sdr/SWAA2023042028428), Apr 18, 2023: PANEL. ELONGATED. PANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES.<[01] R&R PANEL 193B PER SRM 51-40-02
- [SDR SWAA2023041726407](https://openairdocs.org/sdr/SWAA2023041726407), Apr 12, 2023: BATTERY PACK. INOPERATIVE. R/H EMERGENCY LIGHT BATTERY PACK M1669 WILL NOT HOLD A CHARGE<[01] REPLACED M1669 MID CABIN R/H SIDE EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06-960-805. TEST
- [SDR SWAA2023041718234](https://openairdocs.org/sdr/SWAA2023041718234), Mar 17, 2023: BATTERY PACK. INOPERATIVE. LH FWD EMERGENCY EXIT LIGHTS ARE INOP (M1675)<[01] REMOVED BATTERY PACK IN M1675 IAW AMM 33-51-06-960-805 STEP 4E.(1) UP TO (4).;[02] VERIFIED INSTALLATION OF B
- [SDR SWAA2023041915034](https://openairdocs.org/sdr/SWAA2023041915034), Mar 10, 2023: WEB. DEBONDED. LEFT HAND PRESSURE DECK WEN (P/N144A7732-3) IS DISBONDED IN SEVERAL PLACES<[01] VERIFIED PART USING P/N 144A7732-3 AND DWG 1447730 REV A AND ATAG WN23127;[02] V
- [SDR SWAA2023041915035](https://openairdocs.org/sdr/SWAA2023041915035), Mar 10, 2023: SHEAR TIE. CRACKED. SHEAR TIE (P/N 144A7716-8) FOR RIGHT HAND PRESSURE DECK ASSY IS CRACKED<[01] VERIFIED PART USING PART NUMBER 144A7716-8 AND ATAG A171211;[02] AND USING DWG -4 1
- [SDR SWAA2023041914733](https://openairdocs.org/sdr/SWAA2023041914733), Mar 9, 2023: DOUBLER. CRACKED. EXTERNAL GROUND POWER CUTOUT. AFT LOWER SKIN DOUBLER IS CRACKED<[01] STARTED REMOVING EXTERNAL GROUND POWER CUTOUT AFT LOWER SKIN IAW SRM 51-40-02-0G-0;[02] AUD
- [SDR SWAA2023020799159](https://openairdocs.org/sdr/SWAA2023020799159), Feb 4, 2023: BATTERY PACK. INOPERATIVE. VARIOUS EMERGENCY LIGHTS DO NOT ILLUMINATE IN THE CABIN.<[01] REPLACED 8 EMERGENCY LIGHT BATTERY PACKS IN POWER SUPPLIES W/ SERVICEABLE OF SAME. OPS CK NORMAL A
- [SDR SWAA2023013094485](https://openairdocs.org/sdr/SWAA2023013094485), Jan 24, 2023: FORK. CRACKED. RHS UPPER PICKLE FORK FRAME CRACKED AT FASTENER # 6<
- [SDR SWAA2022122684862](https://openairdocs.org/sdr/SWAA2022122684862), Dec 22, 2022: HANDLE. BROKEN. FWD ENTRY DOOR ASSIST HANDLE BROKE OFF. REMOVED AND REPLACED HANDLE IAW AMM 52-11-00.
- [SDR SWAA2022111771643](https://openairdocs.org/sdr/SWAA2022111771643), Nov 16, 2022: LIGHT. INOPERATIVE. LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED THE LIGHT ASSY IAW MM 33-51-01.
- [SDR SWAA2022090851192](https://openairdocs.org/sdr/SWAA2022090851192), Sep 7, 2022: NONE. BROKEN. AFT SERVICE DOOR EMERGENCY EXIT SIGN COVER BROKEN / [01] REPLACED AFT SERVICE DOOR EMERGENCY EXIT SIGN COVER PER AMM 33-51-01
- [SDR SWAA2022052610184](https://openairdocs.org/sdr/SWAA2022052610184), May 22, 2022: LIGHT. INOPERATIVE. AFT OH CEILING LIGHT ABEAM LAST ROW INOP AFT OH CEILING LIGHT ABEAM LAST ROW / [01] RELAMPED AFT OVERHEAD CEILING LIGHTS OPS CHECK GOOD REFERENCE AMM33-22-00.
- [SDR SWAA2022031783227](https://openairdocs.org/sdr/SWAA2022031783227), Mar 13, 2022: LIGHT. INOPERATIVE. LH ROW 1 CENTER CEILING FLOURECENT LIGHT INOP / [01] R&R LIGHT ASSY IAW AMM 33-22-00
- [SDR SWAA2022021170479](https://openairdocs.org/sdr/SWAA2022021170479), Feb 9, 2022: INDICATOR. INOPERATIVE. LT. OVERWING LOWEREMERGENCY EXIT SIGN INOP. ; / [01] R & R INDICATOR ASSY I/A/W M/M 33-51-04.
- [SDR SWAA2021111531022](https://openairdocs.org/sdr/SWAA2021111531022), Oct 19, 2021: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT ; 2021-466316 / [01] EVALUATED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT FOUND CRACK ( 1 EA )L=0.582
- [SDR SWAA2021111531021](https://openairdocs.org/sdr/SWAA2021111531021), Oct 19, 2021: SCUFF PLATE. CRACKED. CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMEN ; 2021-466315 / [01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N B20189362; DUE DATE 23-NOV-21.; [02] REP
- [SDR SWAA2021102031019](https://openairdocs.org/sdr/SWAA2021102031019), Oct 16, 2021: BRACKET. CRACKED. CRACK ON BRACKET LOC ON FRONT SPAR CUT OUT FWD BOOST PUMP IFFSS 120 AND WBL 94.24 AT LT WING. REPLACED BRACKET AND FASTENERS IAW SRM 51-40-02 AND DWG 112A2004 R
- [SDR SWAA2021101428821](https://openairdocs.org/sdr/SWAA2021101428821), Oct 10, 2021: FLOOR PANEL. DELAMINATED. SUPPLEMENTAL INFORMATION: DELAMINATED FLOOR PANEL 231AF AT PASSENGER CABIN 2021-466201 / FAULT WAS RAISED IN ERROR. REFERENCE TTG8Q006UQGP FAULT WAS RAISED IN E
- [SDR SWAA2021101428825](https://openairdocs.org/sdr/SWAA2021101428825), Oct 10, 2021: FLOOR PANEL. DELAMINATED. SUPPLEMENTAL INFORMATION: DELAMINATED FLOOR PANEL 232DF AT PASSENGER CABIN 2021-466206 / FAULT WAS RAISED IN ERROR. REFERENCE TTG8Q006UQJ8 FAULT WAS RAISED IN E
- [SDR SWAA2021111528817](https://openairdocs.org/sdr/SWAA2021111528817), Oct 10, 2021: ACCESS PANEL. CRACKED. CRACK ACCESS PANEL 194E BODY FAIRING AROUND FASTENERS HOLES AT LOWER FUSELAGE ; 2021-466191 / [01] TOOL USED HOT BONDER P/N:HCS9200B-AV; S/N: 18196021; DUE DATE
- [SDR SWAA2021110928834](https://openairdocs.org/sdr/SWAA2021110928834), Oct 10, 2021: FLOOR PANEL. CRACKED. CRACK FLOOR PANEL 221GF AT PASSENGER CABIN ; 2021-466215 / [01] REPLACED FLOOR PANEL 221GF AT PASSENGER CABIN DUE TO CUSTOMER REQUEST; [02] CORRECTED STEP 1; RE
- [SDR SWAA2021110928838](https://openairdocs.org/sdr/SWAA2021110928838), Oct 10, 2021: FLOOR PANEL. CRACKED. CRACK FLOOR PANEL 221EF AT PASSENGER CABIN ; 2021-466216 / [01] REPLACED FLOOR PANEL 221EF AT PASSENGER CABIN DUE TO CUSTOMER REQUEST; [02] CORRECTED STEP 1; RE
- [SDR SWAA2021101328814](https://openairdocs.org/sdr/SWAA2021101328814), Oct 9, 2021: NONE. CRACKED. SUPPLEMENTAL INFORMATION: CRACK FLOOR BEAM LOCATED BS294.5 AND RBL57 AT FWD GALLEY AREA 2021-466136 / EVALUATED ALLOWABLE DAMAGE FOR CRACK ON FLOOR BEAM LOCATED
- [SDR SWAA2021111528811](https://openairdocs.org/sdr/SWAA2021111528811), Oct 9, 2021: WEB. CRACKED. CRACK WEB LOCATED BTW BS277 TO BS294.5 AND BL0 AT FWD GALLEY AREA ; 2021-466135 / [01] REPLACED WEB AND FASTENERS LOCATED BTW BS277 TO BS294.5 AND BL0 AT FWD GA
- [SDR SWAA2021111528813](https://openairdocs.org/sdr/SWAA2021111528813), Oct 9, 2021: NONE. CRACKED. CRACK INNER CHORD LOCATED BS303.9 AND STRINGER 17L AT FWD GALLEY AREA ; 2021-466134 / [01] TOOK MEASURE OF THE CRACK ON INNER CHORD IS L : 0.850 INCH LOCATED BS
- [SDR SWAA2021110928812](https://openairdocs.org/sdr/SWAA2021110928812), Oct 9, 2021: STRINGER. CRACKED. CRACK ENTRY DOOR CUT OUT STRINGER 7L AND BS 294.5 AT FWD GALLEY AREA ; 2021-466120 / [01] TOOK MEASURE OF THE CRACK IS L: 1.056 INCH ; LOCATED ENTRY DOOR CUT OU
- [SDR SWAA2021111528790](https://openairdocs.org/sdr/SWAA2021111528790), Oct 8, 2021: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE AT LT WING (1 EA) ; 2021-466113 / [01] REPLACED CORRUGATED PLATE AND FASTENER LOC.TRAILING EDGE AT LT WING (1 EA). IAW B737
- [SDR SWAA2021110928792](https://openairdocs.org/sdr/SWAA2021110928792), Oct 8, 2021: STUB FRAME. CRACKED. CRACK FLOOR STRUCTURE STUD FRAME LOCATED BS 294.5 AND STRINGER 17R AT FWD GALLEY AREA ; 2021-466119 / [01] CRACK FLOOR STRUCTURE STUD FRAME LOCATED BS 294.5 MUS
- [SDR SWAA2021101228793](https://openairdocs.org/sdr/SWAA2021101228793), Oct 8, 2021: ACCESS PANEL. BROKEN. BROKEN ACCESS PANEL 324AL ANGLE AT VERTICAL STABILIZER. REPLACED ACCESS PANEL 324AL ANGLE AT VERTICAL STABILIZER IAW SRM B737-700 51-40-02 AND 51-10-02 ITEM 9.
- [SDR SWAA2021111528046](https://openairdocs.org/sdr/SWAA2021111528046), Oct 7, 2021: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE BETWEEN WS 236 TO WS 285 ON REAR SPAR LT WING ; 2021-466068 / [01] REPLACED ANGLE LOCATED ON TRAILING EDGE BETWEEN WS 236 TO WS 285 ON
- [SDR SWAA2021111528045](https://openairdocs.org/sdr/SWAA2021111528045), Oct 7, 2021: PANEL. ELONGATED. ELONGATED HOLE ACCESS PANEL 193B AT LOWER FUSELAGE ; 2021-466063 / [01] TOOL USED: CALIPER P/N:500-197-30; S/N:A18234364; DUE DATE: 25-SEP-22.; [02] TOOL USED H
- [SDR SWAA2021111528047](https://openairdocs.org/sdr/SWAA2021111528047), Oct 7, 2021: PANEL. ELONGATED. ELONGATED HOLE ACCESS PANEL 194E AT LOWER FUSELAGE ; 2021-466076 / [01] REPAIRED ACCESS PANEL 194E AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-8 REPAIR 8.
- [SDR SWAA2021111528049](https://openairdocs.org/sdr/SWAA2021111528049), Oct 7, 2021: PANEL. DELAMINATED. DELAMINATED ACCESS PANEL 192AR AT LOWER FUSELAGE ; 2021-466054 / [01] APPLIED CONDUCTIVE COATING ON REPAIR AREAS ON ACCESS PANEL 192AR AS PER B737-700 SRM 51-70
- [SDR SWAA2021111528044](https://openairdocs.org/sdr/SWAA2021111528044), Oct 7, 2021: GUSSET. CRACKED. CRACK GUSSET STR 19R BS 500D FWD CARGO COMPARTMENT ; 2021-466067 / [01] REMOVED GUSSET AND FASTENER IAW SRM 51-40-02 LOC AT STR 19R BS 500D; DUE TO NO FOUND ALL
- [SDR SWAA2021111527492](https://openairdocs.org/sdr/SWAA2021111527492), Oct 6, 2021: SKIN. DEBONDED. CUSTOMER REQUEST - DEBONDED OB AFT FLAP EXTERNAL SKIN LOWER SURFACE LOCATED AT INBOARD CORNER ON LT WING ; 2021-466030 / [01] EVALUATED DAMAGED ON OUTBOARD AFT 
- [SDR SWAA2021111527485](https://openairdocs.org/sdr/SWAA2021111527485), Oct 6, 2021: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED AT BS 690 BL 0 FWD SIDE CENTER SECTION ; 2021-466000 / [01] REMOVE SUPPORT ANGLE LOCATED AT BS 690 BL 0 FWD SIDE CENTER SECTION IAW 
- [SDR SWAA2021111527481](https://openairdocs.org/sdr/SWAA2021111527481), Oct 6, 2021: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED AT BS 690 RBL 24.5 CENTER SECTION ; 2021-466004 / [01] REMOVE SUPPORT ANGLE LOCATED AT BS 690 RBL 24.5 CENTER SECTION IAW B737-700 S
- [SDR SWAA2021101126975](https://openairdocs.org/sdr/SWAA2021101126975), Oct 5, 2021: FLOOR PANEL. DELAMINATED. SUPPLEMENTAL INFORMATION: DELAMINATED FLOOR PANEL 242CF AT PASSENGER CABIN 2021-465808 / REPLACED FLOOR PANEL 242CF AT PASSENGER CABIN DUE TO CUSTOMER REQUEST I
- [SDR SWAA2021111526976](https://openairdocs.org/sdr/SWAA2021111526976), Oct 5, 2021: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 241FF AT PASSENGER CABIN ; 2021-465816 / [01] REPLACED FLOOR PANEL 241FF AT PASSENGER CABIN DUE TO CUSTOMER REQUEST IAW B737-700 AMM 53-
- [SDR SWAA2021101126974](https://openairdocs.org/sdr/SWAA2021101126974), Oct 5, 2021: RIB. CRACKED. CRACK INSPAR RIB LOCATED AT STAB STA 92.70 AND 21 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER. REPAIRED INSPAR RIB LOCATED AT STAB STA 92.70 AND 21 INCH FR
- [SDR SWAA2021111126484](https://openairdocs.org/sdr/SWAA2021111126484), Oct 4, 2021: FLOOR PANEL. ELONGATED. ELONGATED HOLE FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT ; 2021-465625 / [01] FABRICATED NEW PANEL 140BF AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-05 ; 5
- [SDR SWAA2021092219693](https://openairdocs.org/sdr/SWAA2021092219693), Sep 18, 2021: SUPPORT FITTING. CORRODED. LT MLG FWD TRUNNION SUPPORT FITTING; LOWER INBD (#4);INNER FACE HAS EVIDENCE OF CORROSION. ; / [01] REPAIRED PER. EA 1-A57-3246 REV. 14
- [SDR SWAA2021092219694](https://openairdocs.org/sdr/SWAA2021092219694), Sep 18, 2021: FITTING. CORRODED. LT MLG FWD TRUNNION SUPPORT FITTING; LOWER OTBD (#3);INNER FACE HAS EVIDENCE OF CORROSION. ; / [01] REPAIRED PER. EA 1-A57-3246 REV. 14
- [SDR SWAA2021092220592](https://openairdocs.org/sdr/SWAA2021092220592), Sep 18, 2021: FITTING. CORRODED. LT MLG FWD TRUNNION SUPPORT FITTING; LOWER INBD (#4);INNER FACE HAS EVIDENCE OF CORROSION. ; / [01] REPAIRED PER. EA 1-A57-3246 REV. 14
- [SDR SWAA2021092220593](https://openairdocs.org/sdr/SWAA2021092220593), Sep 18, 2021: FITTING. CORRODED. LT MLG FWD TRUNNION SUPPORT FITTING; LOWER OTBD (#3);INNER FACE HAS EVIDENCE OF CORROSION. ; / [01] REPAIRED PER. EA 1-A57-3246 REV. 14
- [SDR SWAA2021052474543](https://openairdocs.org/sdr/SWAA2021052474543), May 19, 2021: HOOK AND LOOP. LOOSE. FWD SERVICE DOOR ESCAPE SLIDE VELCRO STRIPS ON THE GIRT ARE NOT ATTACHED TO VELCRO STRIPS ON THE BACKING PAN SHELF. ; / REATTACHED FWD SERVICE DOOR ESCAPE SLIDE
- [SDR SWAA2021052474542](https://openairdocs.org/sdr/SWAA2021052474542), May 19, 2021: HOOK AND LOOP. LOOSE. AFT ENTRY DOOR ESCAPE SLIDE VELCRO STRIPS ON THE GIRT ARE NOT ATTACHED TO VELCRO STRIPS ON THE BACKING PAN SHELF. ; / REATTACHED AFT ENTRY DOOR ESCAPE SLIDE VEL

All 165: https://openairdocs.org/aircraft/N7829B/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 N7829B

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7829B before.

- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N7829B-undated): Robertson M-287 RAINBOW, S/N 1. Owner: [Robertson Aircraft Corp](https://openairdocs.org/faa-owner/ROBERTSON%20AIRCRAFT%20CORP), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth)

## Related

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

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