# N7889A: 2005 Boeing 737-79L

- Status: Valid registration
- Airframe: [Boeing 737-79L](https://openairdocs.org/model/boeing-737-79l) (registry code 13844LA, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 34023
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 10, 2018
- Certificate issued: December 12, 2017
- Expires: December 31, 2027
- Mode S code: AAB1D2
- Registered owner: [Aerolease 34023 Trust](https://openairdocs.org/faa-owner/AEROLEASE%2034023%20TRUST)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=7889A
- Page: https://openairdocs.org/aircraft/N7889A

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 737-79L)

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 N7889A.

## FAA accident and incident reports

None matched to N7889A.

## Service difficulty reports (226, 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 SWAA2026092810393](https://openairdocs.org/sdr/SWAA2026092810393), Sep 24, 2026: ASSIST HANDLE. BROKEN. HANDLE ON FWD GALLEY SERVICE DOOR BROKE OFF. R & R FWD SERVICE DOOR ASSIST HANDLE IAW MM 52-11-31.
- [SDR SWAA2026092129957](https://openairdocs.org/sdr/SWAA2026092129957), Sep 15, 2026: BATTERY PACK. FAILED. FWD LT BATTERY PACK M1674 FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026092166439](https://openairdocs.org/sdr/SWAA2026092166439), Sep 15, 2026: BATTERY PACK. FAILED. AFT LEFT EMERGENCY LIGHT SYS BATTERY PACK M1672 FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026091660805](https://openairdocs.org/sdr/SWAA2026091660805), Sep 15, 2026: TAIL CONE. DELAMINATED. DELAMINATION ON TAIL CONE AT 6 O'CLOCK POSITION. REMOVED DAMAGED EXTERIOR SKIN PER SRM.53-80-70-2R-1 REPAIR 1. 51-70-05-2R-11 REPAIR 11 SRM.51-70-05-2R-1 REPAIR
- [SDR SWAA2026091677980](https://openairdocs.org/sdr/SWAA2026091677980), Sep 15, 2026: TAIL CONE. DELAMINATED. DELAMINATION ON TAIL CONE AT 4 O'CLOCK. REMOVED DAMAGED SKIN IAW SRM.53-80-70-2R-1, REPAIR 1, 51-70-05-2R-11, REPAIR 11, SRM 51-70-05-2R-1, REPAIR 1. APPLIED PO
- [SDR SWAA2026082115845](https://openairdocs.org/sdr/SWAA2026082115845), Jul 30, 2026: FIRE DETECTOR. NO TEST. NR 1 ENGINE FIRE LOOP A WILL NOT TEST. R & R NR 1 ENG RIGHT CORE A FIRE DETECTOR ASSY IAW AMM 26-11-01. OK FOR SERVICE.
- [SDR SWAA2026073058297](https://openairdocs.org/sdr/SWAA2026073058297), Jul 26, 2026: FUEL FEED. ERRATIC. NR 2 FUEL FLOW INDICATION ERRATIC. R & R #2 FUEL FLOW TRANSMITTER IAW AMM 73-31-01. OPS CHECK AND LEAK CHECK GOOD
- [SDR SWAA2026051803879](https://openairdocs.org/sdr/SWAA2026051803879), May 16, 2026: SLIDE. OUT OF ADJUST. FWD SERVICE DOR SLIDE SKIRT LOOSE. READJUSTED SLIDE PER AMM 25-66-01
- [SDR SWAA2026050695196](https://openairdocs.org/sdr/SWAA2026050695196), May 4, 2026: HANDLE. LOOSE. FWD ENTRY DOOR LINER ASSIST HANDLE LOOSE. SECURED FWD ENTRY DOOR ASSIST HANDLE IAW AMM 52-11-31.
- [SDR SWAA2026042090387](https://openairdocs.org/sdr/SWAA2026042090387), Apr 17, 2026: TRANSMITTER. FAULTED. FLAP LOCKOUT ON APPROACH WHEN SELECTING FLAPS 5; FLAPS DID NOT REACH 5<[01] R/R LEFT FLAP TRANSMITTER PER AMM 27-58-01. OPS CHECKS OKAY.
- [SDR SWAA2026032380959](https://openairdocs.org/sdr/SWAA2026032380959), Mar 18, 2026: LIGHT. INOPERATIVE. PAX CABIN 1EA EMERGENCY LIGHT INOP AT AFT CEILING PANEL. REPLACED EMERGENCY LIGHT OF AFT CEILING PANEL AT PASSENGER CABIN IAW AMM 33-51-03-960-801 TESTED OK.
- [SDR SWAA2026032375867](https://openairdocs.org/sdr/SWAA2026032375867), Mar 3, 2026: ACCESS PANEL. ELONGATED. ELONGATED HOLES ON ACCESS PANEL 561BB AT LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2026032074299](https://openairdocs.org/sdr/SWAA2026032074299), Feb 25, 2026: WEB. CRACKED. CRACKED WEB BTW BS 500 - 500A, STRINGER 26R. REPLACED THE WEB, BS 500 - 500A, STRINGER 26R IAW SRM 51-10-02, ITEM 9, & DWG 143A0080, SHEET 23, REV -.
- [SDR SWAA2026032372981](https://openairdocs.org/sdr/SWAA2026032372981), Feb 21, 2026: GLOWSTRIP. DETERIORATED. DETERIORATED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA). REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) IAW AMM 33-51-15-400-802;
- [SDR SWAA2026032372323](https://openairdocs.org/sdr/SWAA2026032372323), Feb 19, 2026: FITTING. CRACKED. CRACKED FITTING, BS 947.5, STRINGER 26L REPLACED THE FITTING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 149A8103, SHEET 7, REC A.
- [SDR SWAA2026032072325](https://openairdocs.org/sdr/SWAA2026032072325), Feb 19, 2026: WEB. CRACKED. CRACKED WEB BTW BS 500A - 500B, STRINGER 26R, WL 152. REPAIRED THE WEB, BS 500A - 500B, S26R, WL 152. IAW SRM 53-30-53-2R-1, REPAIR 1.
- [SDR SWAA2026032072326](https://openairdocs.org/sdr/SWAA2026032072326), Feb 19, 2026: SHIELD. CORRODED. CORROSION SHIELD WEB LOCATED BTW BS 492.4 TO BS 500A RBL 23 WL 208. 1 AT FWD CARGO COMPARTMENT. REPLACED SHIELD WEB LOCATED BTW BS 492.4 TO BS 500A RBL 23 WL 20
- [SDR SWAA2026032372089](https://openairdocs.org/sdr/SWAA2026032372089), Feb 18, 2026: SUPPORT. CRACKED. CRACKED SUPPORT ZEE, BTWN BS 747 - 847, STRINGER 25L. REPLACED THE SUPPORT ZEE SECTION IAW SRM 51-40-02, SRM 53-00-53-2R-5, SRM 51-10-02, ITEM 9, AND DWG 146A75
- [SDR SWAA2026032372087](https://openairdocs.org/sdr/SWAA2026032372087), Feb 18, 2026: BULKHEAD. CORRODED. CORRODED BULKHEAD BS 727, BTWN STRINGERS 27L - 27R, RBL 5, WL 150.1. REPAIRED THE BULKHEAD IAW 26-153-00585-WIP1.
- [SDR SWAA2026032072090](https://openairdocs.org/sdr/SWAA2026032072090), Feb 18, 2026: CARGO TRACK. CRACKED. CRACK CARGO TRACK BS 460 ; RBL 14 FWD CARGO COMPARTMENT. REPAIRED CARGO TRACK LOCATED BTW BS400 TO BS500 PLUS 14INCH AND RBL14 FWD CARGO COMPARMENT IAW SRM 53-0
- [SDR SWAA2026032371373](https://openairdocs.org/sdr/SWAA2026032371373), Feb 16, 2026: RUB STRIP. WORN. WORN RUB STRIP, BODY FAIRING BS 540 + 10. RBL 41. REPAIRED IAW SRM 57-10-13-2R-3, REPAIR 3, & SRM 51-40-02.
- [SDR SWAA2026032371282](https://openairdocs.org/sdr/SWAA2026032371282), Feb 16, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2026032371375](https://openairdocs.org/sdr/SWAA2026032371375), Feb 16, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING. REPAIRED THE ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2026032370959](https://openairdocs.org/sdr/SWAA2026032370959), Feb 15, 2026: NUT PLATE. CORRODED. CORROSION RAIL NUT PLATE LOCATED ON INTERNAL CAVITY LEADING EDGE OFSS308 AT RT WING. REPLACED RAIL NUT PLATE LOCATED ON INTERNAL CAVITY LEADING EDGE OFSS308 AT 
- [SDR SWAA2026032370826](https://openairdocs.org/sdr/SWAA2026032370826), Feb 14, 2026: CROSSBEAM. CRACKED. CRACKED CROSSBEAM, BS 540, LBL 1. REPLACED THE CROSSBEAM IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A5240, SHEET 1, REV-.
- [SDR SWAA2026032370181](https://openairdocs.org/sdr/SWAA2026032370181), Feb 12, 2026: SKIN. CORRODED. CORROSION AROUND WATER TANK EXHAUST PORT AT EXTERNAL LOWER SKIN BTWN BS 907 - 927, S21 - 22L. REPAIRED EXTERNAL LOWER SKIN
- [SDR SWAA2026032370406](https://openairdocs.org/sdr/SWAA2026032370406), Feb 12, 2026: LENS. BROKEN. BROKEN LENS OF EMERGENCY LIGHT OF SIDEWALL PANEL 232YHW AT PASSENGER CABIN. REPLACED LENS OF EMERGENCY LIGHT OF SIDEWALL PANEL 232YHW AT PASSENGER CABIN IAW AMM
- [SDR SWAA2026032370182](https://openairdocs.org/sdr/SWAA2026032370182), Feb 12, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026032369671](https://openairdocs.org/sdr/SWAA2026032369671), Feb 10, 2026: SEAL. CRACKED. TWO CRACKED SEALS ON ACCESS PANEL 333AB ON THE HORIZONTAL STAB. REPLACED THE SEALS IAW SRM 51-10-02, ITEM 9.
- [SDR SWAA2025121651707](https://openairdocs.org/sdr/SWAA2025121651707), Dec 12, 2025: HOUSING. DISPLACED. PASSENGER CABIN LT OVERWING EXIT DOOR STRAP HANDLE COMPARTMENT DISPLACED. INSTALLED LT OVERWING EXIT DOOR STRAP HANDLE COMPARTMENT IAW AMM 52-22-51.
- [SDR SWAA2025031704476](https://openairdocs.org/sdr/SWAA2025031704476), Mar 12, 2025: BRACKET. CRACKED. UPPER T/E SHELF PANEL JUST AFT OF #1 PYLON FWD UPPER BRACKET CRACKED. <[01] R&R UPPER T/E SHELF PANEL JUST AFT OF #1 PYLON FWD UPPER BRACKET PER SRM 51-40-02;[0
- [SDR SWAA2024110154466](https://openairdocs.org/sdr/SWAA2024110154466), Oct 29, 2024: LIGHT. INOPERATIVE. ROW 14 ABC EMERGENCY FLOOD LIGHT INOP<[01] RELAMPED ROW 14 ABC EMERGENCY AREA LIGHT PER AMM 33-51-03. OPS CHECK GOOD AT THIS TIME.
- [SDR SWAA2024073019852](https://openairdocs.org/sdr/SWAA2024073019852), Jul 27, 2024: STRUT. CRACKED. WORKING MT 7256-I-14342-NG FOUND CRACK ATSTRUT 15 LOCATION C-1 MEASURING .750<[01] OK TO CONTINUE PER EA 7256-I-14342 AND TSR 2024005238
- [SDR SWAA2024042468401](https://openairdocs.org/sdr/SWAA2024042468401), Mar 28, 2024: TEE ANGLE. CRACKED. CRACK ON T-ANGLE LOCATED ON VAPOR VARRIER LOWER AREA BS 663.75 AND BTW RBL5 TO RBL 70 AT MAIN WHELL WELL COMPARTMENT. REPAIRED T-ANGLE LOCATED ON VAPOR VARRIER 
- [SDR SWAA2024042568397](https://openairdocs.org/sdr/SWAA2024042568397), Mar 27, 2024: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS214 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS214 AT RT WING I.A.W B737-700 SRM 51-40-02-
- [SDR SWAA2024042568396](https://openairdocs.org/sdr/SWAA2024042568396), Mar 27, 2024: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS242 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS242 AT RT WING IAW B737-700 SRM 51-40-02 AN
- [SDR SWAA2024042568395](https://openairdocs.org/sdr/SWAA2024042568395), Mar 27, 2024: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING IAW SRM 51-40-02-0G-0 AND DW
- [SDR SWAA2024042568398](https://openairdocs.org/sdr/SWAA2024042568398), Mar 27, 2024: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS273 RT WING 2024-211791<[01] FAULT RESOLVED ON OTHER FAULT. SEE TTG8Q00SB7UQ;[02] FAULT RESOLVED ON OTHER FAULT.
- [SDR SWAA2024042568091](https://openairdocs.org/sdr/SWAA2024042568091), Mar 26, 2024: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED ON PNEUMATIC DUCT BTW BS540 TO BS559 RH SIDE AT AIR CONDITIONING BAY 2024-211774<[01] REPLACED SUPPORT BRACKET LOCATED ON PNEUMATI
- [SDR SWAA2024042567680](https://openairdocs.org/sdr/SWAA2024042567680), Mar 25, 2024: PLATE. CRACKED. CRACK CORRUGATED PLATE ON TRAILING EDGE LOCATED ORSS242 AT LT WING. REPLACED CORRUGATED PLATE AND FASTENERS ON TRAILING EDGE LOCATED ORSS242 AT LT WING; IAW BOE
- [SDR SWAA2024042567679](https://openairdocs.org/sdr/SWAA2024042567679), Mar 25, 2024: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 214 AT LT WING 2024-211768<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 214 AT LT WING IAW B737-7
- [SDR SWAA2024042567681](https://openairdocs.org/sdr/SWAA2024042567681), Mar 25, 2024: SERVICE PANEL. CORRODED. CORROSION FUEL STATION PANEL LOCATED LEADING EDGE AT LEVEL OFSS 385 AT RT WING. REPAIRED FUEL STATION PANEL LOCATED L/E AT LEVEL OFSS 385 AT RT WING. IAW EA #24
- [SDR SWAA2024042567395](https://openairdocs.org/sdr/SWAA2024042567395), Mar 24, 2024: STIFFENER. DAMAGED. ELONGATED HOLE VERTICAL STIFFENER LOCATED STA 907 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-211745<[01] REPLACED VERTICAL STIFFENER LOCATED STA 907 AT LEVE
- [SDR SWAA2024042567393](https://openairdocs.org/sdr/SWAA2024042567393), Mar 24, 2024: DOOR. CORRODED. CORROSION TOILET SERVICE DOOR 145AL AT FUSELAGE EXTERIOR. PERFORMED REPAIR ON TOILET SERVICE DOOR 145AL LOCATED AT FUSELAGE EXTERIOR. IAW B737-700 SRM 52-40-01-
- [SDR SWAA2024042567291](https://openairdocs.org/sdr/SWAA2024042567291), Mar 24, 2024: CARGO TRACK. CRACKED. CRACK TRACK LBBL 17.24 LOCATED STA 727C AT AFT CARGO COMPARTMENT. PERFORMED REPAIR ON TRACK LBBL 17.24 LOCATED STA 727C AT AFT CARGO COMPARTMENT. IAW B737-700 S
- [SDR SWAA2024042467296](https://openairdocs.org/sdr/SWAA2024042467296), Mar 24, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BTW STA 380 TO STA 400 AND BL0 AT PASSENGER CABIN 2024-211730<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW STA 380 TO STA 4
- [SDR SWAA2024042467295](https://openairdocs.org/sdr/SWAA2024042467295), Mar 24, 2024: SUPPORT ANGLE. CRACKED. CRACK ANGLE SUPPORT ANGLE LOCATED BTW STA 380 TO STA 400 RBL 10 AT PASSENGER CABIN 2024-211731<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW STA 380 TO 
- [SDR SWAA2024041967189](https://openairdocs.org/sdr/SWAA2024041967189), Mar 24, 2024: FITTING. DETERIORATED. DETERIORATED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT FWD GALLEY AREA 2024-211704<[01] REPLACED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT F
- [SDR SWAA2024041967192](https://openairdocs.org/sdr/SWAA2024041967192), Mar 24, 2024: FITTING. DETERIORATED. DETERIORATED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT AFT GALLEY AREA 2024-211708<[01] REPLACED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT A
- [SDR SWAA2024041967290](https://openairdocs.org/sdr/SWAA2024041967290), Mar 24, 2024: HOUSING. BROKEN. BROKEN EXIT SIGN HOUSING ASSY ON LOWERED CEILING AT AFT GALLEY AREA 2024-211711<[01] REPLACED EXIT SIGN HOUSING ASSY ON LOWERED CEILING AT AFT GALLEY AREA I.A.W

All 226: https://openairdocs.org/aircraft/N7889A/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 N7889A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7889A before.

- [Cancelled 1971-09-09](https://openairdocs.org/deregistered/N7889A-1971-09-09): Cessna 180, S/N 32786. Exported to Bolivia. Owner: [Missionary Aviation Fellowship](https://openairdocs.org/faa-owner/MISSIONARY%20AVIATION%20FELLOWSHIP), [Fullerton, CA](https://openairdocs.org/faa-place/CA/Fullerton)

## Related

- Other Boeing 737-79L aircraft: https://openairdocs.org/model/boeing-737-79l/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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