# N7885A: 2002 Boeing 737-76N

- Status: Valid registration
- Airframe: [Boeing 737-76N](https://openairdocs.org/model/boeing-737-76n) (registry code 13844CH, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 33379
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 13, 2017
- Certificate issued: December 20, 2022
- Expires: December 31, 2029
- Mode S code: AAB146
- 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=7885A
- Page: https://openairdocs.org/aircraft/N7885A

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 737-76N)

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 N7885A.

## FAA accident and incident reports

None matched to N7885A.

## Service difficulty reports (180, 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 SWAA2026070618719](https://openairdocs.org/sdr/SWAA2026070618719), Jul 5, 2026: PIN. OUT OF POSITION. PIN PROTRUDING FROM SLIDE PACK ON R1 DOOR. RESECURED PIN ON R1 DOOR IAW SIP.
- [SDR SWAA2026050493437](https://openairdocs.org/sdr/SWAA2026050493437), Apr 28, 2026: SLIDE. OUT OF POSITION. R1 GALLEY SLIDE LOWER FLAP REQUIRES REPOSITION. R1 GALLEY SLIDE LOWER FLAP REPOSITIONED PER MT 725-61-06
- [SDR SWAA2026042390778](https://openairdocs.org/sdr/SWAA2026042390778), Apr 18, 2026: BATTERY PACK. INOPERATIVE. FWD EMERGENCY EXIT LIGHTS (5 EACH) INOPERATIVE. REMOVED / REPLACED AND PERFORMED SUCCESSFUL OPS CHECK OF EMERGENCY LIGHTS BATTERY PACKS M1675 AND M1674 IAW B737
- [SDR SWAA2026042392140](https://openairdocs.org/sdr/SWAA2026042392140), Apr 18, 2026: BATTERY PACK. INOPERATIVE. FWD EMERGENCY EXIT LIGHTS (5 EACH) INOPERATIVE. REMOVED & REPLACED, PERFORMED SUCCESSFUL OPS CHECK OF EMERGENCY LIGHTS BATTERY PACKS M1675 AND M1674 IAW B737 AM
- [SDR SWAA2026041489118](https://openairdocs.org/sdr/SWAA2026041489118), Apr 13, 2026: ENGINE. NO DISCREPANCY. AFTER BEING GIVEN LINE UP AND WAIT INSTRUCTIONS FROM KSAN TOWER, TOWER REPORTED A TAIL PIPE FIRE ON NR 1 ENGINE. UNITED CONFIRMED THEY SAW THE FIRE BUT WHEN POW
- [SDR SWAA2026041388288](https://openairdocs.org/sdr/SWAA2026041388288), Apr 11, 2026: FSEU. FAULTY. LE FLAP TRANSIT LIGHT ILLUMINATED DURING APPROACH.<[01] FOLLOWED FIM 27-88 TASK 820 UP TO STEP F SUBSTEP (D) AND REPLACED THE FSEU IAW AMM 27-51-01; OPC GOOD.;[
- [SDR SWAA2025082606972](https://openairdocs.org/sdr/SWAA2025082606972), Aug 22, 2025: SPRING. DAMAGED. FORWARD SERVICE DOOR'S ESCAPE SLIDE GIRTH BAR'S FORWARD SPRING CLIP IS DAMAGED. R&R GIRT BAR FWD SPRING CLIP IN REF WITH AMM 25-66-01.
- [SDR SWAA2025081905058](https://openairdocs.org/sdr/SWAA2025081905058), Aug 15, 2025: FSEU. INOPERATIVE. FLAPS & SLATS PRIMARY CONTROL INOP. ALT FLAPS NORMAL. PERFORMED BITE CHECK ON FSEU AND FOUND 27-81224, FOLLOWED FIN TASK AND FOUND FSEU BAD. R & R FSEU PER AMM 
- [SDR SWAA2025021996941](https://openairdocs.org/sdr/SWAA2025021996941), Feb 17, 2025: BATTERY PACK. NO TEST. EMERGENCY BATTERY PACK M1675 FAIL TEST<[01] REPLACED BATTERY PACK M1673; PERFORMED GOOD TEST PER AMM 33-51-06-960-805;[02] CORRECTIVE ACTION COMPLETED.
- [SDR SWAA2025021996725](https://openairdocs.org/sdr/SWAA2025021996725), Feb 16, 2025: WIRE. DETACHED. EMERGENCY AISLE LIGHT L1065 IS NOT ILLUMINATING APPROX LOCATION OF AISLE LIGHT IS STA 500D WL 274 RBL 30 PER WDM.<[01] UPON FURTHER INVESTIGATION; FOUND TWO DEP
- [SDR SWAA2025021996531](https://openairdocs.org/sdr/SWAA2025021996531), Feb 15, 2025: BATTERY PACK. NO TEST. ALL LIGHTS RELATED TO EMERGENCY BATTERY PACK M2235 FAIL TEST ALL LIGHTS RELATED TO EMERGENCY BATTERY PACK M2335 FAIL TEST<[01] REMOVED; REPLACED AND PERFORMED G
- [SDR SWAA2025021996532](https://openairdocs.org/sdr/SWAA2025021996532), Feb 15, 2025: BATTERY PACK. NO TEST. EMERGENCY BATTERY PACK M673 FAIL TEST EMERGENCY BATTERY PACK M1673 FAIL TEST<[01] REMOVED; REPLACED; AND PERFORMED GOOD TEST OF M1673 BATTERY PACK PER AMM 33-51
- [SDR SWAA2025021991720](https://openairdocs.org/sdr/SWAA2025021991720), Jan 30, 2025: STIFFENER. CORRODED. CORROSION ON STIFFENER AT MID CABIN BS692 RBL64 WL203. MARKED<[01] THIS CARD WILL BE ACCOMPLISHED ON CARD NBR TTG8Q00YEMTL;[02] VERIFIED COMPLETION CORRECTIVE A
- [SDR SWAA2025022091296](https://openairdocs.org/sdr/SWAA2025022091296), Jan 29, 2025: SKIN. CRACKED. CRACK FOUND ON LH HORIZONTAL STABILIZER LOWER SKIN AT STA193.90; 17.5' FROM FWD EDGE; L: 0.6' MARKED<[01] REPAIRED LH HORIZONTAL STABILIZER LOWER SKIN AT STA193
- [SDR SWAA2025021991051](https://openairdocs.org/sdr/SWAA2025021991051), Jan 29, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 231XF HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 231XF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR
- [SDR SWAA2025021991052](https://openairdocs.org/sdr/SWAA2025021991052), Jan 29, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241DF HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241DF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR
- [SDR SWAA2025021991053](https://openairdocs.org/sdr/SWAA2025021991053), Jan 29, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241AF HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR
- [SDR SWAA2025021991281](https://openairdocs.org/sdr/SWAA2025021991281), Jan 29, 2025: WEB. CORRODED. CORROSION ON SUBTHRESHOLD WEB AT ACB BS807 - BS847 RBL28 WL160. MARKED<[01] REMOVED AND REPLACED SUBTHRESHOLD WEB IAW SRM 51-40-02 AND DWG 146A8340 ID:0028 REV:
- [SDR SWAA2025021991297](https://openairdocs.org/sdr/SWAA2025021991297), Jan 29, 2025: STRAP. CORRODED. CORROSION ON STRAP AT MID CABIN BS692 RBL65 WL203. MARKED<[01] REMOVED AND REPLACED NEW INNER CHORD IAW SRM 51-40-02 & DWG 144A5900;[02] VERIFIED COMPLETION COR
- [SDR SWAA2025021991298](https://openairdocs.org/sdr/SWAA2025021991298), Jan 29, 2025: FLOOR PANEL. CRACKED. CRACKED PANEL BREAK AT MID CABIN BS540 LBL1 WL208.<[01] REMOVED AND REPLACED NEW PANEL BREAK AT MID CABIN BS540 LBL1 TO LBL24 IAW SRM 51-40-02 AND DWG 143A0060 
- [SDR SWAA2025021990520](https://openairdocs.org/sdr/SWAA2025021990520), Jan 28, 2025: STIFFENER. CRACKED. LEFT HAND HORIZONTAL STABILIZER #3 INSPAR RIB; AT STABILIZER STATION 111.10; 4TH VERTICAL STIFFENER IS CRACKED.<[01] REMOVED THE DAMAGED PART AT LH HORIZONTAL S
- [SDR SWAA2025021990521](https://openairdocs.org/sdr/SWAA2025021990521), Jan 28, 2025: STIFFENER. CRACKED. RIGHT HAND HORIZONTAL STABILIZER #3 INSPAR RIB; AT STABILIZER STATION 111.10; 4TH VERTICAL STIFFENER IS CRACKED.<[01] REMOVED THE DAMAGED PART AT RH HORIZONTAL 
- [SDR SWAA2025021990370](https://openairdocs.org/sdr/SWAA2025021990370), Jan 28, 2025: CONNECTOR. BROKEN. BROKEN CONNECTOR AT FSD EXIT INDICATOR LIGHT; WIRE LABEL W4142 D03658 M/W L01186<[01] REPLACED CONNECTOR D03658 PER SWPM 20-30-12 AND WM 33-51-21.;[02] VERIFIED
- [SDR SWAA2025021997681](https://openairdocs.org/sdr/SWAA2025021997681), Jan 28, 2025: WIRE. BROKEN. BROKEN CONNECTOR AT FSD EXIT INDICATOR LIGHT; WIRE LABEL W4142 D03658 M/W L01186<[01] REPLACED CONNECTOR D03658 PER SWPM 20-30-12 AND WM 33-51-21.;[02] VERIFIED
- [SDR SWAA2024121675519](https://openairdocs.org/sdr/SWAA2024121675519), Dec 10, 2024: SKIN. CRACKED. EXTERNAL POWER PLUG CUTOUT HAS A CRACK AT 6 O'CLOCK<[01] CUT AND REMOVED DAMAGE IN ZONE 2 PER SRM 53-10-15-2R-4;[02] PERFORMED VISUAL INSPECTION WITH 10X MAGNIF
- [SDR SWAA2024121675517](https://openairdocs.org/sdr/SWAA2024121675517), Dec 10, 2024: BRACKET. CRACKED. L/H WING FWD ATTACH BRACKET FOR SUPPORT FOR PANEL 551BT IS CRACKED.<[01] REMOVED AND REPLACED BRACKET IAW SRM 51-40-02.
- [SDR SWAA2024121075208](https://openairdocs.org/sdr/SWAA2024121075208), Dec 8, 2024: GIRT BAR. OUT OF POSITION. EMERGENCY SLIDE DOES NOT SEAT PROPERLY IN GUIDE ON FWD SVC DOOR<[01] REPOSITIONED GIRT BAR W/SIP. GIRT BAR NOW PROPERLY ENGAGES WITH STOW CLIPS.
- [SDR SWAA2024080823276](https://openairdocs.org/sdr/SWAA2024080823276), Aug 7, 2024: LENS. OUT OF ADJUST. 9 ABC EMERGENCY LIGHT LENS LOOSE ON BULLNOSE MKD<[01] SECURED EMERGENCY LIGHT LENS COVER ON BULLNOSE AT 9 ABC BULLNOSE. REF 33-51-03
- [SDR SWAA2024072918210](https://openairdocs.org/sdr/SWAA2024072918210), Jul 27, 2024: LIGHT. INOPERATIVE. AFT LEFT HAND EMERGENCY AREA LIGHT INOP<[01] REMOVED AND REPLACED AFT LEFT HAND EMERGENCY AREA LIGHT IAW AMM 33-51-03
- [SDR SWAA2024031463046](https://openairdocs.org/sdr/SWAA2024031463046), Mar 14, 2024: BATTERY PACK. INOPERATIVE. INOP EMERGENCY LIGHT R/H OVERWING EXIT FWD LIGHT; 6ABC-9ABC; 14ABC; CENTER AISLE 23ABC<[01] RELAMPED R/H FWD OVWG LIGHT AND CTR AISLE 23ABC; REPLACED BATTERY PA
- [SDR SWAA2024031463377](https://openairdocs.org/sdr/SWAA2024031463377), Mar 14, 2024: CHARGER. INOPERATIVE. INOP EMERGENCY LIGHT R/H OVERWING EXIT FWD LIGHT; 6ABC-9ABC; 14ABC; CENTER AISLE 23ABC<[01] RELAMPED R/H FWD OVWG LIGHT AND CTR AISLE 23ABC; REPLACED BATTERY PA
- [SDR SWAA2023121330355](https://openairdocs.org/sdr/SWAA2023121330355), Dec 11, 2023: LIGHT. INOPERATIVE. LH OVER-WING EMERGENCY LIGHT INOP<[01] RE-LAMPED LH OVER-WING EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2023112223481](https://openairdocs.org/sdr/SWAA2023112223481), Nov 21, 2023: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT AT L1 DOOR INOP<[01] REMOVED AND REPLACED LIGHT ASSEMBLY REF AMM 33-51-12
- [SDR SWAA2023101911495](https://openairdocs.org/sdr/SWAA2023101911495), Oct 16, 2023: COVER. BROKEN. FWD LOWER EXIT SIGN COVER BROKEN.<[01] SECURED COVER AS REQ PER SIP.
- [SDR SWAA2023072882753](https://openairdocs.org/sdr/SWAA2023072882753), Jul 27, 2023: ROD. BROKEN. L/H WING TRAILING EDGE; AFT OF PYLON; SHELF SUPPORT ROD BROKEN.<[01] REMOVED AND REPLACED ROD ASSY PER SOPM 20-50-01. CLEARANCE CHECK GOOD
- [SDR SWAA2023030311405](https://openairdocs.org/sdr/SWAA2023030311405), Mar 2, 2023: LIGHT. OUT OF ADJUST. EMERGENCY EXIT AISLE LIGHT ASSEMBLY AT ROW 9ABC HAS DETACHED FROM OVERHEAD BIN<[01] REATTACHED ROW 9ABC EMERGENCY LIGHT HOUSING ASSY TO EMERGANCY LIGHT HOUSING 
- [SDR SWAA2023030311782](https://openairdocs.org/sdr/SWAA2023030311782), Mar 2, 2023: LIGHT. INOPERATIVE. AFT SERVICE DOOR EMERGENCY EXIT LIGHT IS INOP<[01] REPLACED LAMP AND PERFORMED GOOD TEST PER AMM 33-51-04-960-801;[02] VERIFIED ACTION ITEM 1;[03] VERIFIED CORR
- [SDR SWAA2023030211067](https://openairdocs.org/sdr/SWAA2023030211067), Mar 1, 2023: BATTERY PACK. ICED. EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1669 ARE INOP.<[01] INSTALLED SERVICEABLE EMERGENCY EXIT LIGHT BATTERY PACK M1669; PERFORMED A GOOD OPERATIO
- [SDR SWAA2023030211068](https://openairdocs.org/sdr/SWAA2023030211068), Mar 1, 2023: BATTERY PACK. INOPERATIVE. EMERGENY EXIT LIGHT ASSOCIATED WITH BATTERY PACK M1668 ARE INOP.<[01] INSTALLED SERVICEABLE EMERGENCY EXIT LIGHT BATTERY PACK M1668; PERFORMED A GOOD OPERATIONA
- [SDR SWAA2023030211065](https://openairdocs.org/sdr/SWAA2023030211065), Mar 1, 2023: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1672 BATTERY PACK ARE INOP.<[01] INSTALLED SERVICEABLE EMERGENCY EXIT LIGHT BATTERY PACK M1672; PERFORMED A GOOD OPERATIO
- [SDR SWAA2023030211066](https://openairdocs.org/sdr/SWAA2023030211066), Mar 1, 2023: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1673 ARE INOP.<[01] INSTALLED SERVICEABLE EMERGENCY EXIT LIGHT BATTERY PACK M1673; PERFORMED A GOOD OPERATIO
- [SDR SWAA2023030211402](https://openairdocs.org/sdr/SWAA2023030211402), Mar 1, 2023: FUSE. INOPERATIVE. EMERGENCY EXIT AISLE LIGHT AT ROW 9CBA IS INOP<[01] RELAMPED EMERGENCY EXIT AISLE LIGHT AT SEAT ROW 9 ABC AND PERFORMED INSTALLATION TEST PER AMM 33-51-03-960-8
- [SDR SWAA2023030605237](https://openairdocs.org/sdr/SWAA2023030605237), Feb 20, 2023: CONNECTOR. FAULTY. EMERGENCY EXIT WIRING BEHIND SIDEWALL PANEL 232YHW HAS A BROKEN CONNECTOR<[01] INSPECTED EMERGENCY EXIT LIGHTING CONNECTORS AND LIGHTING CONNECTORS BEHIND AND N
- [SDR SWAA2023030600724](https://openairdocs.org/sdr/SWAA2023030600724), Feb 8, 2023: SUPPORT. CRACKED. BRACKET HAS A CRACK BS 540+7 RBL 19 ON R/H SIDE SUPPORT BEAM - WING CENTER SECTION.<[01] EVALUATED BRACKET SUPPORT RH SIDE A/C SYSTEM PIPE AND NO FOUND ALLOWABL
- [SDR SWAA2023030699757](https://openairdocs.org/sdr/SWAA2023030699757), Feb 6, 2023: INTERCOSTAL. CRACKED. INTERCOSTAL IN AFT CARGO BAY BS 927-947 RBL 21 UNDER R/H FLOOR TO SIDEWALL SUPPORT IS CRACKED<[01] CRACKED ON INTERCOSTAL IN AFT CARGO BAY BS 927-947 RBL 21 WIT
- [SDR SWAA2023030698978](https://openairdocs.org/sdr/SWAA2023030698978), Feb 4, 2023: SUPPORT. CRACKED. CRACK ON SUPPORT OF SIDEWALL AT FRAME BS 827 BETWEEN STR 14R AND STR 15R.<[01] REMOVED AND REPLACED CRACKED SIDEWALL SUPPORT (ISOLATOR) AT FRAME BS 827 BETWEEN 
- [SDR SWAA2023030698682](https://openairdocs.org/sdr/SWAA2023030698682), Feb 3, 2023: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-26R WL153. MARKED<PERFORMED CUT OUT ON S-26R FCB; REMOVED DAMAGE PART FROM BS 500D+10 TO BS 540 IAW SRM 53
- [SDR SWAA2023030698685](https://openairdocs.org/sdr/SWAA2023030698685), Feb 3, 2023: FRAME. CRACKED. CRACK ON FRAME BS 312 BETWEEN STR 4L AND STR 5L (MARKRED)<[01] CUT AND REMOVED THE DAMAGED AT BS 312 BETWEEN STR4L - STR5L IAW SRM 51-10-02;[02] REQUESTED DVI O
- [SDR SWAA2023030698678](https://openairdocs.org/sdr/SWAA2023030698678), Feb 3, 2023: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-23R WL164. MARKED<[01] UPDATE PARTIAL STEPS 1-2;[02] SRM 53-00-03-2R-1 REPAIR 1 IS APPLICABLE TO THIS A/C 
- [SDR SWAA2023030698683](https://openairdocs.org/sdr/SWAA2023030698683), Feb 3, 2023: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-27R WL150. MARKED<[01] SRM 53-00-03-2R-1 REPAIR 1 IS APPLICABLE TO THIS A/C AND REPIR.;[02] PERFORMED CUT 

All 180: https://openairdocs.org/aircraft/N7885A/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 N7885A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7885A before.

- [Cancelled 1981-12-09](https://openairdocs.org/deregistered/N7885A-1981-12-09): Nord 262-A, S/N 21. Exported to Denmark. Owner: [Altair Airlines Inc](https://openairdocs.org/faa-owner/ALTAIR%20AIRLINES%20INC), [Philadelphia, PA](https://openairdocs.org/faa-place/PA/Philadelphia)

## Related

- Other Boeing 737-76N aircraft: https://openairdocs.org/model/boeing-737-76n/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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