# N5113A: 2002 Boeing 737-83N - Status: Valid registration - Airframe: [Boeing 737-83N](https://openairdocs.org/model/boeing-737-83n) (registry code 13844HI, 149 seats) - Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044) - Serial number: 32611 - Year built: 2002 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 13, 2019 - Certificate issued: April 1, 2019 - Expires: April 30, 2029 - Mode S code: A667E8 - 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=5113A - Page: https://openairdocs.org/aircraft/N5113A 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 737-83N) 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 N5113A. ## FAA accident and incident reports None matched to N5113A. ## Service difficulty reports (64, 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 SCNA20260922405](https://openairdocs.org/sdr/SCNA20260922405), Sep 19, 2026: WASHER. DAMAGED. L1 DOOR DIFFICULT TO OPEN, FOUND HINGE HARDWARE BROKEN REMOVED PIN AND SCREW FOR L1 DOOR GUIDE ARM HINGE. AND REINSTALLED KEY WASTER AND WASHERS IAW AMM 52-11-2 - [SDR SCNA20260831376](https://openairdocs.org/sdr/SCNA20260831376), Aug 30, 2026: SMOKE GOGGLES. MISSING. PILOT AND CO PILOT EMERGENCY EQUIPMENT MISSING GOGGLES. REPLACED GOGGLES ASSY ON CAPTIAN AND CO-PILOT EMERGENCY EQUIPMENT IAW AMM 25-61-00 - [SDR SCNA20260323130](https://openairdocs.org/sdr/SCNA20260323130), Mar 21, 2026: WINDOW. ARCED. R1 WINDOW ARCHING DURING FLIGHT. COMPLETED INSTALL OF R1 WINDOW IAW AMM 56-141-11 OPS AND LEAK CHECK GOOD. - [SDR SCNA20251031421](https://openairdocs.org/sdr/SCNA20251031421), Oct 27, 2025: PUMP. FAULTED. LOST A SYSTEM PRESSURE DURING GEAR RETRACTION. LOW PRESURE WENT OUT AFTER GEAR RETRACTION. C/W QRH AND TURNED PUMPS OFF. ACCOMPLISHED ENGINE RUNS-IDLE- RAN ENGI - [SDR SCNA20251031420](https://openairdocs.org/sdr/SCNA20251031420), Oct 16, 2025: HYDRAULIC LINE. RUPTURED. AFTER 10000, MASTER CAUTION LOW PRESSURE ENGINE 1 LIGHT A HYDRAULIC QTY 0. FOUND HYD PRESSURE TUBE ASSY BURST IN CEILING OF WHEEL WELL. INSTALLED TEMPORARY FLEX - [SDR SCNA20250902344](https://openairdocs.org/sdr/SCNA20250902344), Aug 29, 2025: COMMS UNIT. FAULTED. CAPT COMMS HAVE LOUD FEEDBACK ISSUE IN ALL MODES INCLUDING RADIO TRANSMIT AND ICG. AUDIO WARNINGS ARE EXTERMELY LOUD AND NOT SAFE FOR FLIGHT. PERFORMED OPS TEST - [SDR SCNA20250714256](https://openairdocs.org/sdr/SCNA20250714256), Jul 13, 2025: BATTERY PACK. INOPERATIVE. LEFT AND FWD GALLEY EMERGENCY LIGHTS INOP. R&R L1 EMERGENCY LIGHT BATTERY PACK REF AMM 33-51-06, OPS CHECK OKAY. - [SDR UIEA2025041200454](https://openairdocs.org/sdr/UIEA2025041200454), Apr 22, 2025: FRAME. MECHANIC ERROR. FWD CARGO COMPARTMENT STA 500B LBL 21.5" FRAME I/B FLANGE WITH MIS DRILLED HOLE.(

REPAIRED FUSELAGE FRAME I/B FLANGE SECTION AT STA 500B BTWN STR 25LH I/A/W C - [SDR UIEA2025041400457](https://openairdocs.org/sdr/UIEA2025041400457), Apr 22, 2025: FRAME. MECHANIC ERROR. FWD CARGO COMPARTMENT STA 500G LBL 21.5" FRAME I/B FLANGE WITH MIS DRILLED HOLE.(

REPAIRED FUSELAGE FRAME I/B FLANGE SECTION AT STA  500G BETWEEN STR 25L - [SDR UIEA2025041400458](https://openairdocs.org/sdr/UIEA2025041400458), Apr 22, 2025: SKIN. DENTED. LOWER EXTERNAL FUSELAGE AT STA 893 BETWEEN STR 24R AND 25R SKIN WITH DENT.(

REPAIRED FUSELAGE SKIN SECTION FROM STA 887.75 TO STA 900 BETWEEN STR 23R AND 26R - [SDR UIEA2025041400460](https://openairdocs.org/sdr/UIEA2025041400460), Apr 22, 2025: CARGO TRACK. CORRODED. LOWER FUSELAGE FWD CARGO COMPARTMENT AT STA 500G RBL 14, TIE DOWN TRACK WITH CORROSION. NOTE: IT WAS FOUND DURING PROCESS WITH NRI 1-61.(

REPAIRED TIE DOWN TR - [SDR UIEA2025041400466](https://openairdocs.org/sdr/UIEA2025041400466), Apr 22, 2025: FLOORBEAM. CORRODED. UPPER FUSELAGE MAIN CABIN, AT STA 986, BTWN RBL 50 AND LBL50, FLOOR BEAM UPPER FLANGE WITH CORROSION IN SEVERAL PLACES.(

REPAIRED FUSELAGE FLOOR BEAM AT STA 9 - [SDR UIEA2025041400467](https://openairdocs.org/sdr/UIEA2025041400467), Apr 22, 2025: FLOORBEAM. CORRODED. UPPER FUSELAGE FWD ENTRY CABIN AREA, STA 312 AT LBL1 AND LBL 8, UPPER CHORD AFT FLANGE WITH CORROSION.(

REPAIRED FUSELAGE FLOOR BEAM, STA 312, UPPER CHORD SEC - [SDR UIEA2025041400470](https://openairdocs.org/sdr/UIEA2025041400470), Apr 22, 2025: FLOORBEAM. CORRODED. UPPER FUSELAGE FWD ENTRY CABIN AREA, STA 328 AT RBL 47 , UPPER CHORD FWD FLANGE WITH CORROSION.(

REPAIRED FUSELAGE FLOOR BEAM STA 328, UPPER CHORD SECTION BET - [SDR UIEA2025041400472](https://openairdocs.org/sdr/UIEA2025041400472), Apr 22, 2025: SKIN. CRACKED. RH HORIZONTAL STABILIZER - LOWER INSPAR SKIN CRACKED AT STAB STA 101.90 (I/B SIDE OF THE RIB), 11 INCHES FWD OF THE REAR SPAR.(

REPAIRED R/H HORIZONTAL STABIL - [SDR UIEA2025041400474](https://openairdocs.org/sdr/UIEA2025041400474), Apr 22, 2025: CARGO TRACK. CRACKED. FWD CARGO COMPARTMENT AT STA 460, STA 480 RBL 13.8" CARGO TIE DOWN TRACK CRACKED AND STA 492 CORRODED AROUND ANCHOR NUT AREA. NOTE: THIS WAS FOUND WHEN PERFORMI - [SDR UIEA2025041400475](https://openairdocs.org/sdr/UIEA2025041400475), Apr 22, 2025: SKIN. CRACKED. LEFT WING L/E SLAT #2 SKIN WITH CRACK AT ACTUATOR ATTACHEMENT FITTING LOWER SURFACE.(

REPAIRED L/H WING SLAT #2 (P/N:114A5020-3, S/N:001150) LEADING EDGE LOWE - [SDR UIEA2025041600478](https://openairdocs.org/sdr/UIEA2025041600478), Apr 22, 2025: SKIN. CRACKED. LEFT WING L/E SLAT #4 SKIN WITH CRACK AT ACTUATOR ATTACHEMENT FITTING LOWER SURFACE .
(

REPAIRED LH WING SLAT #4 (P/N:114A5040-3, S/N:001143) LEADING EDGE - [SDR UIEA2025041600479](https://openairdocs.org/sdr/UIEA2025041600479), Apr 22, 2025: FASTENER. LOOSE. RH WING, SLAT N°5, IN LINE WITH HYD ACTUATOR ROD END, EXTERNAL LOWER SKIN WITH LOOSE FASTENER HEADS.(

REPAIRED R/H WING SLAT #5 (P/N:114A5040-4, S/N: 001120) - [SDR UIEA2025041600480](https://openairdocs.org/sdr/UIEA2025041600480), Apr 22, 2025: FASTENER. LOOSE. RH WING, SLAT N°7, IN LINE WITH HYD ACTUATOR ROD END, EXTERNAL LOWER SKIN WITH LOOSE FASTENER HEADS(

REPAIRED R/H WING SLAT #7 (P/N:114A5020-4, S/N: 001108) - [SDR UIEA2025041600481](https://openairdocs.org/sdr/UIEA2025041600481), Apr 22, 2025: FASTENER. LOOSE. RH WING, SLAT N°8, IN LINE WITH HYD ACTUATOR ROD END, EXTERNAL LOWER SKIN WITH LOOSE FASTENER HEADS.(

REPAIRED RH WING SLAT N°8 (P/N 114A5010-4) NOSE BEAM S - [SDR UIEA2025041600482](https://openairdocs.org/sdr/UIEA2025041600482), Apr 22, 2025: FLOORBEAM. CRACKED. UPPER FUSELAGE FWD ENTRY AREA, AT STA 303.9 AND LBL 60, FLOOR ANGLE WITH CRACK.(

REPAIRED INNER CHORD ANGLE AT FWD ENTRY DOOR LOWER SILL, STA 303.9 WL 208, LB - [SDR UIEA2025041600483](https://openairdocs.org/sdr/UIEA2025041600483), Apr 22, 2025: SKIN. DAMAGED. UPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 328.5 AND STR2R + 3.750", SKIN WITH LIGHTNING STRIKE.(

PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER - [SDR UIEA2025041600484](https://openairdocs.org/sdr/UIEA2025041600484), Apr 22, 2025: SKIN. DAMAGED. UPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 283 AND 5" BELOW STR 2R SKIN WITH LIGHTNING STRIKE.(

PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER IN - [SDR UIEA2025041600485](https://openairdocs.org/sdr/UIEA2025041600485), Apr 22, 2025: SKIN. DAMAGED. UPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 284 AND 4.5" BELOW STR 2L SKIN WITH LIGHTNING STRIKE.(

PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER - [SDR UIEA2025041600486](https://openairdocs.org/sdr/UIEA2025041600486), Apr 22, 2025: SKIN. DAMAGED. UPPER FUSELAGE EXTENAL SKIN SECTION AT STA 500E + 10.250" AND 2.5" BELOW STR-2L SKIN WITH LIGHTNING STRIKE.(

PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR - [SDR UIEA2025041600487](https://openairdocs.org/sdr/UIEA2025041600487), Apr 22, 2025: SKIN. DAMAGED. UPPER FUSELAGE EXTENAL SKIN SECTION AT STA 590 AND 1.5" ABOVE STR-3R SKIN WITH LIGHTNING STRIKE.(

PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER IN - [SDR UIEA2025041600488](https://openairdocs.org/sdr/UIEA2025041600488), Apr 22, 2025: SKIN. DAMAGED. UPPER FUSELAGE EXTENAL SKIN SECTION AT STA 649" AND 2.250" ABOVE STR-1R SKIN WITH LIGHTNING STRIKE.(

PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER - [SDR UIEA2025042100553](https://openairdocs.org/sdr/UIEA2025042100553), Apr 22, 2025: SKIN. DAMAGED. UPPER FUSELAGE EXTENAL SKIN SECTION AT STA 819.5 AND STR-14R SKIN WITH LIGHTNING STRIKE.(

PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATI - [SDR UIEA2025042100554](https://openairdocs.org/sdr/UIEA2025042100554), Apr 22, 2025: SKIN. DAMAGED. UPPER FUSELAGE EXTENAL SKIN SECTION AT STA 778.5 AND STR-1 + 2.750 INCH R, SKIN WITH LIGHTNING STRIKE.(

PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTE - [SDR UIEA2025042100555](https://openairdocs.org/sdr/UIEA2025042100555), Apr 22, 2025: SKIN. DAMAGED. UPPER FUSELAGE EXTENAL SKIN SECTION AT STA 620 AND 1 INCH BELOW STR-3L SKIN WITH LIGHTNING STRIKE.(

PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER - [SDR UIEA2025042100556](https://openairdocs.org/sdr/UIEA2025042100556), Apr 22, 2025: LOCK FASTENER. LOOSE. LEFT WING, SLAT #4 LOWER L/E ACTUATOR FITTING HI-LOCKS LOOSE.(

REPAIRED L/H WING SLAT #4 (P/N:114A5040-3, S/N:001143) LEADING EDGE LOWER SURFACE SKIN SECTION - [SDR UIEA2025042100557](https://openairdocs.org/sdr/UIEA2025042100557), Apr 22, 2025: FASTENER. NOT REPORTED. WINGS - WING LEADING EDGE - UPPER SKIN PANEL - FASTENER CHANGE - SB 737-57-1336 R0 IAW PAR-B1920 REV.0.(

REPLACED FASTENER IAW ATLAS AIR PAR-B REV 0 DATED: 17 - [SDR UIEA2025042100558](https://openairdocs.org/sdr/UIEA2025042100558), Apr 22, 2025: SKIN. CRACKED. L/H WING, INBOARD LEADING EDGE SKIN PANEL, KRAS 206, 1 (E.A.) HOLE WITH CRACK INDICATION. CONTACT ENGINEERING FOR FURTHER REPAIR INSTRUCTIONS.(

PERFORMED LH W - [SDR UIEA2025042100559](https://openairdocs.org/sdr/UIEA2025042100559), Apr 22, 2025: SKIN. CRACKED. R/H WING, INBOARD LEADING EDGE SKIN PANEL, KRAS 206, 1 (E.A.) HOLE WITH CRACK INDICATION. CONTACT ENGINEERING FOR FURTHER REPAIR INSTRUCTIONS.(

PERFORMED RH W - [SDR UIEA2025021400146](https://openairdocs.org/sdr/UIEA2025021400146), Feb 14, 2025: CABIN PRESSURE. PILOT ERROR. O2 MASK USED IN-FLIGHT, CABIN ALTITUDE WARNING DUE TO CREW ERROR, ENG BLEED 1 & 2 OFF DURING T/O & INITIAL CLIMB.(

RE-STOWED CAPTAIN O2 MASK IAW AMM 3 - [SDR UIEA2024082400844](https://openairdocs.org/sdr/UIEA2024082400844), Aug 24, 2024: WIRE. UNSECURE. WINDOW OVERHEAT CAUTION MSG(

FOUND VERY LOOSE WIRE ON #1 WINDOW. TIGHTENED WIRE FASTNER PER AMM 56-11-11. BITE CHECK AND OPS CHECK SATISFACTORY. NO FURTHER DE - [SDR UIEA2024072400739](https://openairdocs.org/sdr/UIEA2024072400739), Jul 24, 2024: AUTOTHROTTLE SYS. FAULTED. A/T DISCONNECTED DURING THRUST SET, DISCONTINUED TAKEOFF AT 47 KTS. TAKEOFF THRUST HAD NOT BEEN SET. TRANSFERRED TO MDDR 213360 PER MEL 22-04 CAT "C" DUE DATE 0 - [SDR UIEA2024031500151](https://openairdocs.org/sdr/UIEA2024031500151), Mar 15, 2024: PRESSURE SWITCH. FAULTED. #2 FWD FUEL PUMP LOW-PRESSURE LIGHT ILLUMINATED IN FLIGHT(

R/R #2 MAIN TANK LOW PRESSURE FWD SW PER AMM 28-42-11, LEAK & OPS CHECK GOOD.

) - [SDR UIEA2024031400147](https://openairdocs.org/sdr/UIEA2024031400147), Mar 13, 2024: PUMP. LOW PRESSURE. LOW SPEED REJECTED, APPROX 20 KNOTS, RH MAIN TANK FWD AND AFT FUEL PUMP LOW-PRESSURE LIGHTS ILLUMINATED(

FLIGHT CREW REPORTED BRAKES NOT USED FOR REJECTED TAK - [SDR UIEA2023031500255](https://openairdocs.org/sdr/UIEA2023031500255), Mar 17, 2023: UNKNOWN. UNKNOWN. AFT CARGO COMPARTMENT DOOR OUTER SKIN WITH DENTS IN SEVERAL PLACES.(

REPAIR FUSELAGE AFT CARGO COMPTARTMENT DOOR OUTER SKIN SECTION FROM BS796 TO BS844 BETWEE - [SDR UIEA2023031500256](https://openairdocs.org/sdr/UIEA2023031500256), Mar 17, 2023: UNKNOWN. UNKNOWN. FWD CARGO COMPARTMENT BETWEEN STA. 500A TO STA. 500I, STRA. 26R WITH CORROSION(

REPAIRED FUSELAGE STRINGER 26RH, SECTION BETWEEN BS500+14,250" AND BS500H+17,2 - [SDR UIEA2023031600257](https://openairdocs.org/sdr/UIEA2023031600257), Mar 17, 2023: UNKNOWN. UNKNOWN. FWD CARGO COMPARTMENT AT BS 500D BETWEEN STR. 23L AND STR. 25L. FRAME I/B FLANGE WITH ELONGATED HOLES. NOTE: WHEN PERFORMED ACCESS WITH NRI 1-55 WAS DETECTED(

REPAIRED FUSELAGE STRINGER.26R BETWEEN BS.727E AND BS.727G+18.5" IAW B737-800 BCF SRM 53- - [SDR UIEA2023031600259](https://openairdocs.org/sdr/UIEA2023031600259), Mar 17, 2023: UNKNOWN. UNKNOWN. FWD CARGO COMPARTMENT BETWEEN STA. 500C TO STA. 500I STR.27R WITH CORROSION(

REPAIRED FUSELAGE STRINGER 27R BETWEEN  BS. 500A+4" AND BS 500G+17.5" IAW B7 - [SDR UIEA2023031600260](https://openairdocs.org/sdr/UIEA2023031600260), Mar 17, 2023: UNKNOWN. UNKNOWN. FWD CARGO COMPARTMENT AT STA. 540 STR. 25R WITH CRACK(

REPAIRED FUSELAGE STRINGER 25R BETWEEN BS500H+3.875MM AND BS540 IAW B737-800 BCF SRM 53-00-03-2R-1, REP - [SDR UIEA2023031600261](https://openairdocs.org/sdr/UIEA2023031600261), Mar 17, 2023: UNKNOWN. UNKNOWN. FWD CARGO COMPARMENT BETWEEN STA. 460 TO STA. 500I STR.26L WITH CORROSION(

REPAIRED FUSELAGE STRINGER 26L SECTION BETWEEN BS.465,25" AND BS500H+17,25" IAW B73 - [SDR UIEA2023031600262](https://openairdocs.org/sdr/UIEA2023031600262), Mar 17, 2023: UNKNOWN. UNKNOWN. FWD CARGO COMPARTMENT DOOR OUTER SKIN WITH DENTS IN SEVERAL PLACES.(

REPAIRED FUSELAGE FWD CARGO COMPARTMENT DOOR OUTER SKIN SECTION FROM B442.550 TO BS 489,9 - [SDR UIEA2023031600263](https://openairdocs.org/sdr/UIEA2023031600263), Mar 17, 2023: UNKNOWN. UNKNOWN. FWD CARGO COMPARMENT BETWEEN STA. 500B TO STA. 500I STR.28R WITH CORROSION(

REPAIRED FUSELAGE STRINGER 28R SECTION, BETWEEN BS.500B AND BS 500E+19.5"I/A/W B73 - [SDR UIEA2023031600265](https://openairdocs.org/sdr/UIEA2023031600265), Mar 17, 2023: UNKNOWN. UNKNOWN. AFT CARGO COMPARTMENT AT LBL 17.24 BETWEEN BS 786 AND BS 794 CARGO TRACK-TIE DOWN WITH CORROSION(

REPAIRED CARGO TRACK TIE DOWN AT LBL 17.24" BETWEEN BS774 AN All 64: https://openairdocs.org/aircraft/N5113A/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 N5113A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N5113A before. - [Cancelled 2013-06-18](https://openairdocs.org/deregistered/N5113A-2013-06-18): Cessna 172, S/N 28113, built 1955. Registration expired, pending cancellation. Owner: [Kagarice Robert H](https://openairdocs.org/faa-owner/KAGARICE%20ROBERT%20H), [Mission Viejo, CA](https://openairdocs.org/faa-place/CA/Mission%20Viejo) ## Related - Other Boeing 737-83N aircraft: https://openairdocs.org/model/boeing-737-83n/aircraft.md - The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.