# N7815L: 2003 Boeing 737-76Q

- Status: Valid registration
- Airframe: [Boeing 737-76Q](https://openairdocs.org/model/boeing-737-76q) (registry code 13845AA, 149 seats)
- Engine: [CFM International CFM56-7B22 series](https://openairdocs.org/engine/cfm-international-cfm56-7b22-series) (registry code 13043)
- Serial number: 30288
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 14, 2014
- Certificate issued: February 9, 2022
- Expires: February 28, 2029
- Mode S code: AA974F
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, 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=7815L
- Page: https://openairdocs.org/aircraft/N7815L

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 CFM56-7B22 model are included.

## ADs that may apply (OpenAirDocs): 19 in force

### Matched by airframe (Boeing 737-76Q)

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 N7815L.

## FAA accident and incident reports

None matched to N7815L.

## Service difficulty reports (227, 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 SWAA2026042890560](https://openairdocs.org/sdr/SWAA2026042890560), Apr 18, 2026: WEB. CRACKED. APB APEX DOME HAS SURFACE WEB CRACK AT STR23R FROM UPPER LH RIVET GOING TO CENTER EDGE OF DOME. REPAIRED PER EA 26-153-01061 WITH AN INSPECTION THRESHOLD DEFINE
- [SDR SWAA2025082606374](https://openairdocs.org/sdr/SWAA2025082606374), Aug 20, 2025: CAP. MISSING. FORWARD CARGO DOOR HANDLE HAS MISSING STUD CAP. INSTALLED STUD CAP IAW AMM 52-31-14.
- [SDR SWAA2025082206375](https://openairdocs.org/sdr/SWAA2025082206375), Aug 20, 2025: HANDLE. MISSING. AFT CARGO DOOR HANDLE HAS MISSING STUD CAP<[01] REMOVED AND REPLACED AFT CARGO DOOR HANDLE STUD CAP REFERENCE AMM52-31-14.
- [SDR SWAA2025081299599](https://openairdocs.org/sdr/SWAA2025081299599), Aug 8, 2025: GIRT BAR. DAMAGED. FWD ENTRY DOOR GURT BAR HOOK HAS MISSING RIVET. INSTALLED NEW RIVET IN FWD ENTRY GURT BAR HOOK REF SIP
- [SDR SWAA2025060276185](https://openairdocs.org/sdr/SWAA2025060276185), May 28, 2025: GIRT BAR. LOOSE. R1 DOOR GIRT BAR LOOSE <[01]. RE-SECURED R1 DOOR GIRT BAR RETAINER CLIPS PER AMM 25-66-01. OPS CHK GOOD.
- [SDR SWAA2025051971778](https://openairdocs.org/sdr/SWAA2025051971778), May 15, 2025: SLIDE. LOOSE. R1 SLIDE CAME LOOSE. REINSTALLED SLIDE PER MT#25-66-01.
- [SDR SWAA2025050622175](https://openairdocs.org/sdr/SWAA2025050622175), Apr 7, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M2335 INOP<[01] REMOVED; REPLACED WITH SERVICEABLE UNIT AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY BAT
- [SDR SWAA2025050608576](https://openairdocs.org/sdr/SWAA2025050608576), Mar 23, 2025: STRIP. CRACKED. FWD CARGO BAY SIDEWALL PNL 122AW CAPSTRIP CRACKED<[01] RECEIVED NEW CAPSTRIP; CAPSTRIP WILL BE INSTALLED ON TTG8Q00YJCE7;[02] CORRECTIVE ACTION ITEM 1 VERIFIED;
- [SDR SWAA2025050615939](https://openairdocs.org/sdr/SWAA2025050615939), Mar 23, 2025: STRIP. CRACKED. FWD CARGO BAY SIDEWALL PNL 122EW CAPSTRIP CRACKED<[01] RECEIVED NEW CAPSTRIP; CAPSTRIP WILL BE INSTALLED ON TTG8Q00YJCE1;[02] VERIFIED CORRECTIVE ACTION ENTRY 1
- [SDR SWAA2025050615928](https://openairdocs.org/sdr/SWAA2025050615928), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727D S-6L. MARKED<[01] REMOVED STR CLIP AT BS727D S-6L IAW SRM 51-40-02;[02] OK TO INSTALL;[03] REMOVED AND REPLACED NEW STRINGE
- [SDR SWAA2025050615929](https://openairdocs.org/sdr/SWAA2025050615929), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727C S-7L. MARKED<[01] REMOVED SRT CLIP AT BS727C S-7L IAW SRM 51-40-02;[02] REMOVED AND REPLACED NEW STRINGER CLIP BS727C S-7L 
- [SDR SWAA2025050615930](https://openairdocs.org/sdr/SWAA2025050615930), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727D S-4R. REMOVED STR CLIP AT BS727D S-4R IAW SRM 51-40-02. REMOVED AND REPLACED NEW STRINGER CLIP BS727D S-4R PER DWG 146A1111
- [SDR SWAA2025050615931](https://openairdocs.org/sdr/SWAA2025050615931), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727A S-5R. REMOVED STR CLIP AT BS727A S-5R IAW SRM 51-40-02. REMOVED AND REPLACED NEW STRINGER CLIP AT BS727A S-5R PER DWG 146A1
- [SDR SWAA2025050606638](https://openairdocs.org/sdr/SWAA2025050606638), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727B S-5R. MARKED. REMOVED AND REPLACED NEW STRINGER CLIP BS727B S-5R PER DWG 146A1103 REV D AND SRM 51-40-02. CORRECTIVE ACTION
- [SDR SWAA2025040906636](https://openairdocs.org/sdr/SWAA2025040906636), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727D S-6L. MARKED <[01]. REMOVED STR CLIP AT BS727D S-6L IAW SRM 51-40-02; [02] OK TO INSTALL; [03] REMOVED AND REPLACED NEW STR
- [SDR SWAA2025040906637](https://openairdocs.org/sdr/SWAA2025040906637), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727C S-7L. MARKED <[01]. REMOVED SRT CLIP AT BS727C S-7L IAW SRM 51-40-02; [02] REMOVED AND REPLACED NEW STRINGER CLIP BS727C S-
- [SDR SWAA2025040906639](https://openairdocs.org/sdr/SWAA2025040906639), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727D S-4R. MARKED <[01]. REMOVED STR CLIP AT BS727D S-4R IAW SRM 51-40-02; [02] REMOVED AND REPLACED NEW STRINGER CLIP BS727D S-
- [SDR SWAA2025040906640](https://openairdocs.org/sdr/SWAA2025040906640), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727A S-5R. MARKED <[01]. REMOVED STR CLIP AT BS727A S-5R IAW SRM 51-40-02; [02] REMOVED AND REPLACED NEW STRINGER CLIP AT BS727A
- [SDR SWAA2025050606464](https://openairdocs.org/sdr/SWAA2025050606464), Mar 17, 2025: SKIN. CORRODED. CORROSION ON UPPER FUSELAGE SKIN UNDER VERTICAL STAB LBL12 TO RBL12 BS1016 - BS1078 WL308.5. MARKED<[01] UPDATED TABLE; COMPLETED STEP 9.;[02] ' AS PER EA 25-15
- [SDR SWAA2025040906466](https://openairdocs.org/sdr/SWAA2025040906466), Mar 17, 2025: ANGLE. CORRODED. CORROSION ON ANGLE UNDER VERTICAL STAB BS1036 LBL2 WL308.5. MARKED <[01]. ADDED DIMENSIONS TO STEP 2.
- [SDR SWAA2025050615901](https://openairdocs.org/sdr/SWAA2025050615901), Mar 15, 2025: PLATE. CRACKED. WIGGLE PLATE ON L/W T/E ORSS 261 IS CRACKED. REMOVED AND REPLACED WIGGLE PLATE ON L/W T/E AT ORSS 261 IAW SRM 51-40-02-0G-0 PARA. 4. VERIFIED CORRECTIVE ACTION 
- [SDR SWAA2025040905686](https://openairdocs.org/sdr/SWAA2025040905686), Mar 15, 2025: PLATE. CRACKED. WIGGLE PLATE ON L/W T/E ORSS 261 IS CRACKED <[01]. REMOVED AND REPLACED WIGGLE PLATE ON L/W T/E AT ORSS 261 IAW SRM 51-40-02-0G-0 PARA. 4.; [02] VERIFIED CORREC
- [SDR SWAA2025050605541](https://openairdocs.org/sdr/SWAA2025050605541), Mar 14, 2025: SCUFF PLATE. CRACKED. ACB FWD CORNER SCUFF PLATE CRACKED(MARKED)<[01] 04 - REPAIRED PER [SRM 53-60-15-2R-1-A00967 (REPAIR 1 - AFT CARGO DOOR SURROUND STRUCTURE - PERMANENT)]
- [SDR SWAA2025050639172](https://openairdocs.org/sdr/SWAA2025050639172), Mar 13, 2025: ATTACH FITTING. CORRODED. CORROSION ON LEFT WING FRONT SPAR AROUND BOOST PUMP UPPER BONDING STRAP ATTACHMENT POINT - IFSS 121.<[01] REPAIRED CORROSION ON LEFT WING FRONT SPAR BOOST PUMP 
- [SDR SWAA2025050615880](https://openairdocs.org/sdr/SWAA2025050615880), Mar 13, 2025: PRESSURE DECK. CRACKED. CRACK FOUND ON HORIZONTAL PRESSURE DECK AT MID PASSENGER CABIN BS663+8' RBL 40 L: 0.6'( MARKED)<[01] REMOVED AND REPLACED BEADED PRESSURE DECK WEB SECTION AT BS
- [SDR SWAA2025040905218](https://openairdocs.org/sdr/SWAA2025040905218), Mar 13, 2025: PRESSURE DECK. CRACKED. CRACK FOUND ON HORIZONTAL PRESSURE DECK AT MID PASSENGER CABIN BS663+8' RBL 40 L: 0.6'( MARKED) <[01]. REMOVED AND REPLACED BEADED PRESSURE DECK WEB SECTION AT 
- [SDR SWAA2025050604854](https://openairdocs.org/sdr/SWAA2025050604854), Mar 12, 2025: STRUT. CRACKED. L/H MLG GEAR STRUT DOOR IS CRACKED<[01] UPDATED STEPS 1;2 FOR REMOVAL L/H MLG SHOCK STRUT DOORS;[02] COMPLETED STEPS 2;4;[03] COMPLETED STEP 1 INSTALL L/H MLG S
- [SDR SWAA2025022699061](https://openairdocs.org/sdr/SWAA2025022699061), Feb 23, 2025: CONTROL UNIT. MALFUNCTIONED. INTERMITTANT RIGHT WING/BODY OVERHEAT LIGHT ON APPROACH LIGHT EXTINGUISHED SHORT AFTER ILLUMINATION<[01] PERFORMED COMPARTMENT OVERHEAT DETECTION CONTROL UNIT B
- [SDR SWAA2024092740908](https://openairdocs.org/sdr/SWAA2024092740908), Sep 24, 2024: BATTERY PACK. FAILED. EMERGENCY LIGHTING BATTERY PACK AT R/H OVER WING EXIT FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2024082629575](https://openairdocs.org/sdr/SWAA2024082629575), Aug 22, 2024: HOLDER. OUT OF ADJUST. R1 SLIDE GIRT BAR FALLS OUT OF THE HOLDER WHEN YOU OPEN THE DOOR<[01] ADJUSTED THE SLIDE CLIP GIRT DOOR HOLDER PER AMM 25-66-01 OPS CHECK GOOD
- [SDR SWAA2024082228076](https://openairdocs.org/sdr/SWAA2024082228076), Aug 19, 2024: RETAINER. LOOSE. FWD SERVICE DOOR SLIDE RETAINING CLIP LOOSE.<[01] R & R?D FASTENER PER SRM 51-40-02
- [SDR SWAA2023101710687](https://openairdocs.org/sdr/SWAA2023101710687), Oct 14, 2023: COVER. BROKEN. RIGHT SIDE OVER WING LOWER LEVEL EXIT LIGHT COVER IS BROKEN.<[01] R&R?D RIGHT SIDE OVER WING EXIT DOOR EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01.
- [SDR SWAA2023090596938](https://openairdocs.org/sdr/SWAA2023090596938), Sep 4, 2023: GIRT BAR. OUT OF ADJUST. FWD ENTRY DOOR GIRT BAR OUT OF HOLDER<[01] FOUND GIRT BAR OUT OF HOLDER; RESECURED GIRT BAR IN HOLDER REF AMM 25-66-01; SLIDE NOT AFFECTED REMAINED IN SLIDE COM
- [SDR SWAA2023090596497](https://openairdocs.org/sdr/SWAA2023090596497), Sep 2, 2023: BLADE. DAMAGED. BIRD STRIKE #2 ENGINE; VIB 1.8 FOR 15 SECONDS. NO OTHER ABNORMAL ENGINE PARAMETERS. F/A REPORTED TURKEY SMELL IN CABIN.<[01] FOUND DAMAGE TO FAN BLADES # 11; 12
- [SDR SWAA2023053147111](https://openairdocs.org/sdr/SWAA2023053147111), May 9, 2023: RIB. CRACKED. CRACK INSPAR RIB 129.50 LOWER CHORD LOCATED BTW 13.5 INCH AND 17.5 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER 2023-258231<[01] TOOL USED: EDDY CURRENT EQU
- [SDR SWAA2023053145335](https://openairdocs.org/sdr/SWAA2023053145335), May 4, 2023: STIFFENER. CRACKED. CRACK ON STIFFENER LOCATED FRONT SPAR INSPAR RIB 129.50 AT RT HORIZONTAL STABILIZER 2023-258212<[01] REPLACED STIFFENER LOCATED ON FRONT SPAR INSPAR RIB 129.50 
- [SDR SWAA2023053144548](https://openairdocs.org/sdr/SWAA2023053144548), May 3, 2023: RIB. CRACKED. CRACK ON INSPAR RIB 129.5 AND 34 INCHES FROM FRONT SPAR AT LT HORIZONTAL 2023-258208<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022237; DUE DA
- [SDR SWAA2023053144546](https://openairdocs.org/sdr/SWAA2023053144546), May 2, 2023: RIB. CRACKED. REJECT. CRACK INSPAR RIB 92.70 LOWER FLANGE AT 25 INCH FROM FRONT SPAR AT LT HORIZONTAL STABILIZER 2023-258206<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: 
- [SDR SWAA2023053144547](https://openairdocs.org/sdr/SWAA2023053144547), May 2, 2023: RIB. CRACKED. REJECT. CRACK INSPAR RIB 92.70 LOWER FLANGE AT 38 INCH FROM FRONT SPAR AT LT HORIZONTAL STABILIZER 2023-258207<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORT
- [SDR SWAA2023053143463](https://openairdocs.org/sdr/SWAA2023053143463), Apr 30, 2023: ANGLE. CRACKED. CRACK SUPPORT ANGLE LOC BS 360 ON LOWER AREA AT EQUIPMENT ELECTRONIC COMP 2023-258190<[01] REPLACED SUPPORT ANGLE LOC BS 360 ON LOWER AREA AT EQUIPMENT ELECTRON
- [SDR SWAA2023053142509](https://openairdocs.org/sdr/SWAA2023053142509), Apr 27, 2023: RIB. CRACKED. CRACK LEADING EDGE RIB LOCATED LE STA 114.55 AT LT HORIZONTAL STABILIZER 2023-258183<[01] REPLACED LEADING EDGE RIB LOCATED LE STA 114.55 AT LT HORIZONTAL STABI
- [SDR SWAA2023053142510](https://openairdocs.org/sdr/SWAA2023053142510), Apr 27, 2023: RIB. CRACKED. CRACK LEADING EDGE RIB LOCATED LE STA 142.45 AT LT HORIZONTAL STABILIZER 2023-258184<[01] REPLACED LEADING EDGE RIB LOCATED LE STA 142.45 AT LT HORIZONTAL STABI
- [SDR SWAA2023053130241](https://openairdocs.org/sdr/SWAA2023053130241), Apr 21, 2023: BATTERY PACK. INOPERATIVE. INOP EMERGENCY LIGHT BATTERY (3EA) AT PASSENGER CABIN 2023-258105<[01] REPLACED EMERGENCY LIGHT BATTERY PACK (3EA) AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-
- [SDR SWAA2023053130242](https://openairdocs.org/sdr/SWAA2023053130242), Apr 21, 2023: BRACKET. ELONGATED. ELONGATED HOLE SUPPORT BRACKET LOCATED IFSS 193 IB LEADING EDGE AT LT WING 2023-258140<[01] REPLACED SUPPORT BRACKET LOCATED IFSS 193 IB LEADING EDGE AT LT WING
- [SDR SWAA2023053129767](https://openairdocs.org/sdr/SWAA2023053129767), Apr 20, 2023: BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED IFSS 193 IB LEADING EDGE AT RT WING 2023-258133<[01] REPLACED SUPPORT BRACKET LOCATED IFSS 193 IB LEADING EDGE AT RT WING IAW B737
- [SDR SWAA2023053129768](https://openairdocs.org/sdr/SWAA2023053129768), Apr 20, 2023: RIB. CRACKED. CRACK LEADING EDGE RIB LOCATED LE STA198.23 RT HORIZONTAL STAB 2023-258134<[01] REPLACED LEADING EDGE RIB LOCATED LE STA198.23 RT HORIZONTAL STAB IAW B737-700 S
- [SDR SWAA2023053129210](https://openairdocs.org/sdr/SWAA2023053129210), Apr 19, 2023: ANGLE. CRACKED. CRACK ON ANGLE LOCATED BS 727 RBL 3 FWD PARTITION AT AFT CARGO COMPARTMENT 2023-258112<[01] REMOVED ANGLE DUE TO CRACK LOCATED BS 727 RBL 3 FWD PARTITION AT AFT
- [SDR SWAA2023053129209](https://openairdocs.org/sdr/SWAA2023053129209), Apr 19, 2023: PLATE. CRACKED. CRACK ON SHIELD PLATE LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT 2023-258109<[01] REPLACED SHIELD PLATE LOCATED BTW BS 767 TO BS 787
- [SDR SWAA2023053129208](https://openairdocs.org/sdr/SWAA2023053129208), Apr 19, 2023: ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BS 907 PLUS 11 INCHES BTW STR 23R TO STR 25R AT AFT CARGO COMPARTMENT 2023-258108<[01] REPLACED SUPPORT ANGLE LOCATED BS 907 BTW 
- [SDR SWAA2023053129211](https://openairdocs.org/sdr/SWAA2023053129211), Apr 19, 2023: WEB. CORRODED. CORROSION ON WEB LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R RBL 22 WL 156 AT AFT CARGO COMPARTMENT 2023-258113<[01] REPLACED WEB LOCATED BTW BS 767 TO BS 787

All 227: https://openairdocs.org/aircraft/N7815L/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

## Related

- Other Boeing 737-76Q aircraft: https://openairdocs.org/model/boeing-737-76q/aircraft.md
- The CFM International CFM56-7B22 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b22-series.md

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