# Service difficulty reports: N5113A A list on [N5113A](https://openairdocs.org/aircraft/N5113A.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 64 reports - [SDR SCNA20260922405](https://openairdocs.org/sdr/SCNA20260922405.md): Washer · damaged · Sep 19, 2026 · N5113A · Boeing 73783N · Passenger/Crew Doors > 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 52-11-21 OPS CHECK GOOD - [SDR SCNA20260831376](https://openairdocs.org/sdr/SCNA20260831376.md): Smoke Goggles · missing · Aug 30, 2026 · N5113A · Boeing 73783N · Emergency Equipment > 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.md): Window · arced · Mar 21, 2026 · N5113A · Boeing 73783N · Flight Compartment Windows > 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.md): Pump · faulted · Oct 27, 2025 · N5113A · Boeing 73783N · Hydraulic System, Main > 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 ENGINES FOR 5 MINUTES, NO DEFECTS NOTED- AIRCRAFT OK FOR SERVICE SEE LP 816482 ITEM 1 816482 ITEM 1. - [SDR SCNA20251031420](https://openairdocs.org/sdr/SCNA20251031420.md): Hydraulic Line · ruptured · Oct 16, 2025 · N5113A · Boeing 73783N · Hydraulic System, Main > 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 FLEXIBLE TUBING REF GMM 840-020. ACCOMPLISHED LEAK CHECK & SERVICED L HYD SYSTEM - NO LEAKS NOTED - REF - [SDR SCNA20250902344](https://openairdocs.org/sdr/SCNA20250902344.md): Comms Unit · faulted · Aug 29, 2025 · N5113A · Boeing 73783N · Communications System > 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 ON ACP IAW AMM TASK 23-51-02-400-801 & FOUND OBS ACP WAS CAUSING STATIC FEEDBACK ON CAPT SPEAKER - [SDR SCNA20250714256](https://openairdocs.org/sdr/SCNA20250714256.md): Battery Pack · inoperative · Jul 13, 2025 · N5113A · Boeing 73783N · Emergency Lighting > 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.md): Frame · mechanic error · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Frame > 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 COOPESA COO-EO-2025-21962-R00 DATED MAR/25/2025 CATEGORY B REPAIR. DOCUMENTED ON FAA FORM 8110-3. NO - [SDR UIEA2025041400457](https://openairdocs.org/sdr/UIEA2025041400457.md): Frame · mechanic error · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Frame > 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 AND STR 27L I/A/W COOPESA COO-EO-20-25-21968- R00 REV00, DATED MAR 15-25, CATEGORY B REPAIR. DOCUMENTED - [SDR UIEA2025041400458](https://openairdocs.org/sdr/UIEA2025041400458.md): Skin · dented · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/Skin > 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 I/A/W COOPESA COO-EO-2025-22084-R00 REV: 00 DATED: MAR 27-25 AND BOEING MESSAGE COO-TLS-0049-03B DAT - [SDR UIEA2025041400460](https://openairdocs.org/sdr/UIEA2025041400460.md): Cargo Track · corroded · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage, Seat/Cargo Attach Fittings > 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 TRACK SECTION AT RBL 13.84 FROM STA 500A + 8" TO 500G+ 19", SPLICED BETWEEN STA 500A/STA 500B AND BETW - [SDR UIEA2025041400466](https://openairdocs.org/sdr/UIEA2025041400466.md): Floorbeam · corroded · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Floor Beam > 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 986.5, UPPER CHORD SECTION BETWEEN LBL 50" AND RBL 50" I/A/W COOPESA COO-EO-2025-22114-R00 REV:00, D - [SDR UIEA2025041400467](https://openairdocs.org/sdr/UIEA2025041400467.md): Floorbeam · corroded · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Floor Beam > 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 SECTION BETWEEN LBL 21 AND 12.25 I/A/W B-737-800 BCF SRM 53-10-51-2R-12 REPAIR 12 PARAG 1 THRU PARAG 4, - [SDR UIEA2025041400470](https://openairdocs.org/sdr/UIEA2025041400470.md): Floorbeam · corroded · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Floor Beam > 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 BETWEEN RBL 32 AND RBL 64 I/A/W B-737-800 BCF SRM 53-10-21-2R-7, REPAIR 7 PARAG, FIG 204 DETAIL A SHEET - [SDR UIEA2025041400472](https://openairdocs.org/sdr/UIEA2025041400472.md): Skin · cracked · Apr 22, 2025 · N5113A · Boeing 73783N · Horizontal Stabilizer, Plate/Skin > 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 STABILIZER LOWER IN SPAR SKIN SECTION AT STAB STA 101.90+ 11" FWD OF THE LOWER SKIN AFT EDGE I/A/W B-737-8 - [SDR UIEA2025041400474](https://openairdocs.org/sdr/UIEA2025041400474.md): Cargo Track · cracked · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage, Seat/Cargo Attach Fittings > 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 PERFORMING JOB WITH NRI 1-1.(

REPAIRED TIE DOWN TRACK SECTION AT RBL 13.84 FROM STA 400 TO STA 500A + 16", - [SDR UIEA2025041400475](https://openairdocs.org/sdr/UIEA2025041400475.md): Skin · cracked · Apr 22, 2025 · N5113A · Boeing 73783N · Leading Edge Devices > 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 LOWER SURFACE SKIN SECTION AT THE ACTUATOR RIB AREA (PERMANENT REPAIR) I/A/W B737-800 BCF SRM 57-42-01-2 - [SDR UIEA2025041600478](https://openairdocs.org/sdr/UIEA2025041600478.md): Skin · cracked · Apr 22, 2025 · N5113A · Boeing 73783N · Leading Edge Devices > 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 LOWER SURFACE SKIN SECTION AT THE ACTUATOR RIB AREA (PERMANENT REPAIR) I/A/W B737-800 BCF SRM 57-42- - [SDR UIEA2025041600479](https://openairdocs.org/sdr/UIEA2025041600479.md): Fastener · loose · Apr 22, 2025 · N5113A · Boeing 73783N · Leading Edge Devices > 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) LEADING EDGE LOWER SURFACE SKIN SECTION AT THE ACTUATOR RIB AREA (PERMANENT REPAIR) DUE TO COUNTERS - [SDR UIEA2025041600480](https://openairdocs.org/sdr/UIEA2025041600480.md): Fastener · loose · Apr 22, 2025 · N5113A · Boeing 73783N · Leading Edge Devices > 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) WING LEADING EDGE SLAT NOSE BEAM SECTION AT THE ACTUATOR RIB AREA, PERMANENT REPAIR I/A/W B737-800 B - [SDR UIEA2025041600481](https://openairdocs.org/sdr/UIEA2025041600481.md): Fastener · loose · Apr 22, 2025 · N5113A · Boeing 73783N · Wing Main, Frame Structure > 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 SECTION AT ACTUATOR RIB AREA I.A.W ATLAS AIR EA-1957A223 REV 0 DATED 16-APR-25. NO FURTHER DEFECTS NO - [SDR UIEA2025041600482](https://openairdocs.org/sdr/UIEA2025041600482.md): Floorbeam · cracked · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Floor Beam > 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, LBL 60 I/A/W COOPESA COO-EO-2025-22069-R00 REV:00 DATED: MAR-27-25, DOCUMENTED ON F.A.A FORM 8110-3. N - [SDR UIEA2025041600483](https://openairdocs.org/sdr/UIEA2025041600483.md): Skin · damaged · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/Skin > UPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 328.5 AND STR2R + 3.750", SKIN WITH LIGHTNING STRIKE.(

PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) I/A/W B737-800 SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP(1) THRU (5)(6) (PROTRUDING HE - [SDR UIEA2025041600484](https://openairdocs.org/sdr/UIEA2025041600484.md): Skin · damaged · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/Skin > UPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 283 AND 5" BELOW STR 2R SKIN WITH LIGHTNING STRIKE.(

PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) I/A/W B737-800 BCF SRM 53-00-01-2R-38, REPAIR 38 PARG 4E STEP (1) THRU STEP(5) (6)(PROTR - [SDR UIEA2025041600485](https://openairdocs.org/sdr/UIEA2025041600485.md): Skin · damaged · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/Skin > 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 INSTALLATION) I/A/W B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP(1) THRU STEP (5)(6)( PROT - [SDR UIEA2025041600486](https://openairdocs.org/sdr/UIEA2025041600486.md): Skin · damaged · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/Skin > 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 FASTENER INSTALLATION) I/A/W B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP(1) THRU STEP (5) - [SDR UIEA2025041600487](https://openairdocs.org/sdr/UIEA2025041600487.md): Skin · damaged · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/Skin > 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 INSTALLATION) I/A/W B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP(1) THRU STEP (5)(6)( PROTRU - [SDR UIEA2025041600488](https://openairdocs.org/sdr/UIEA2025041600488.md): Skin · damaged · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/Skin > 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 INSTALLATION) I/A/W B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP(1) THRU STEP (5)(6)( PRO - [SDR UIEA2025042100553](https://openairdocs.org/sdr/UIEA2025042100553.md): Skin · damaged · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/Skin > UPPER FUSELAGE EXTENAL SKIN SECTION AT STA 819.5 AND STR-14R SKIN WITH LIGHTNING STRIKE.(

PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) IAW B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP (1) THRU STEP (5)(6) (PROTRUDING HEAD - [SDR UIEA2025042100554](https://openairdocs.org/sdr/UIEA2025042100554.md): Skin · damaged · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/Skin > 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 FASTENER INSTALLATION) IAW B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP (1) THRU STEP (5)(6) (P - [SDR UIEA2025042100555](https://openairdocs.org/sdr/UIEA2025042100555.md): Skin · damaged · Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/Skin > 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 INSTALLATION) IAW B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP (1) THRU STEP (5)(6)( PROTR - [SDR UIEA2025042100556](https://openairdocs.org/sdr/UIEA2025042100556.md): Lock Fastener · loose · Apr 22, 2025 · N5113A · Boeing 73783N · Leading Edge Devices > 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 AT THE ACTUATOR RIB AREA (PERMANENT REPAIR) IAW B373-800 BCF SRM 57-42-01-2R-8 REPAIR 8 PARG 4A THRU - [SDR UIEA2025042100557](https://openairdocs.org/sdr/UIEA2025042100557.md): Fastener · not reported · Apr 22, 2025 · N5113A · Boeing 73783N · Wing Structure > 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: 17JAN25 AND BOEING 737-800 BCF SRM 57-41-01-2R-7 REPAIR 7 PARG 4 TABLE 201 FIG 202, REV 23 DATED: 10MA - [SDR UIEA2025042100558](https://openairdocs.org/sdr/UIEA2025042100558.md): Skin · cracked · Apr 22, 2025 · N5113A · Boeing 73783N · Wing, Plate/Skin > 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 WING AT KRAS 206 INBD LEADING EDGE SKIN PANEL FASTENERS OVERSIZE HOLE REPAIR IAW COO-EO-2025-2221-R00 - [SDR UIEA2025042100559](https://openairdocs.org/sdr/UIEA2025042100559.md): Skin · cracked · Apr 22, 2025 · N5113A · Boeing 73783N · Wing, Plate/Skin > 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 WING AT KRAS 206 INBD LEADING EDGE SKIN PANEL FASTENERS OVERSIZE HOLE REPAIR IAW COOPESA COO-EO-2025 - [SDR UIEA2025021400146](https://openairdocs.org/sdr/UIEA2025021400146.md): Cabin Pressure · pilot error · Feb 14, 2025 · N5113A · Boeing 73783N · Cabin Pressure Control System > 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 35-12-85. OPS TEST GOOD. O2 PSI 1500.

) - [SDR UIEA2024082400844](https://openairdocs.org/sdr/UIEA2024082400844.md): Wire · unsecure · Aug 24, 2024 · N5113A · Boeing 73783N · Ice/Rain Protection System Wiring > 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 DEFECTS NOTED.

) - [SDR UIEA2024072400739](https://openairdocs.org/sdr/UIEA2024072400739.md): Autothrottle Sys · faulted · Jul 24, 2024 · N5113A · Boeing 73783N · Auto Throttle System > 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 03AUG24. PLACARDS INSTALLED. - [SDR UIEA2024031500151](https://openairdocs.org/sdr/UIEA2024031500151.md): Pressure Switch · faulted · Mar 15, 2024 · N5113A · Boeing 73783N · Fuel Boost Pump > #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.md): Pump · low pressure · Mar 13, 2024 · N5113A · Boeing 73783N · Fuel Boost Pump > 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 TAKE OFF REF AMM 5-51-07. T/S PER FIM 28-22 TASK 806. TANK #2 FWD PUMP OPS NORMAL, NO HISTORY. TANK #2 - [SDR UIEA2023031500255](https://openairdocs.org/sdr/UIEA2023031500255.md): Unknown · unknown · Mar 17, 2023 · N5113A · Boeing 73783N · Standard Practices/Structures > AFT CARGO COMPARTMENT DOOR OUTER SKIN WITH DENTS IN SEVERAL PLACES.(

REPAIR FUSELAGE AFT CARGO COMPTARTMENT DOOR OUTER SKIN SECTION FROM BS796 TO BS844 BETWEEN UPPER FRAME AND LOWER FRAME CUTOUTS IAW B737-800 SRM 52-30-01-2R-3 REPAIR 3 PARAG 4, FIG 203

) - [SDR UIEA2023031500256](https://openairdocs.org/sdr/UIEA2023031500256.md): Unknown · unknown · Mar 17, 2023 · N5113A · Boeing 73783N · Fuselage Structure (General) > FWD CARGO COMPARTMENT BETWEEN STA. 500A TO STA. 500I, STRA. 26R WITH CORROSION(

REPAIRED FUSELAGE STRINGER 26RH, SECTION BETWEEN BS500+14,250" AND BS500H+17,256", IAW B737-800 BCF SRM 53-00-03-2R-1 REPAIR 1, PARAG 4, FIG 205.

) - [SDR UIEA2023031600257](https://openairdocs.org/sdr/UIEA2023031600257.md): Unknown · unknown · Mar 17, 2023 · N5113A · Boeing 73783N · Fuselage Structure (General) > 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(

PERFORMED PERMANENT REPAIR ON SECTION 43, FWD CARGO COMPARMENT AT BS. 500D BETWEEN STR. 23L AND STR - [SDR UIEA2023031600258](https://openairdocs.org/sdr/UIEA2023031600258.md): Unknown · unknown · Mar 17, 2023 · N5113A · Boeing 73783N · Fuselage Structure (General) > AFT CARGO COMPARTMENT AT BS. 727G+9.5" STRINGER 26R WITH CORROSION.(

REPAIRED FUSELAGE STRINGER.26R BETWEEN BS.727E AND BS.727G+18.5" IAW B737-800 BCF SRM 53-00-03-2R-1 REPAIR 1, PARAG 4, FIG 202, REV 16 DATED NOV/10/22

) - [SDR UIEA2023031600259](https://openairdocs.org/sdr/UIEA2023031600259.md): Unknown · unknown · Mar 17, 2023 · N5113A · Boeing 73783N · Fuselage Structure (General) > 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 B737-800 BCF SRM 53-00-03-2R-1 REPAIR 1 PARAG 4, FIG 205.

) - [SDR UIEA2023031600260](https://openairdocs.org/sdr/UIEA2023031600260.md): Unknown · unknown · Mar 17, 2023 · N5113A · Boeing 73783N · Fuselage Structure (General) > 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, REPAIR 1, PARAG 4, FIG 205.

) - [SDR UIEA2023031600261](https://openairdocs.org/sdr/UIEA2023031600261.md): Unknown · unknown · Mar 17, 2023 · N5113A · Boeing 73783N · Fuselage Structure (General) > 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 B737-800 BCF SRM 53-00-03-2R-1 REPAIR 1 PARAG.4, FIG 205.

) - [SDR UIEA2023031600262](https://openairdocs.org/sdr/UIEA2023031600262.md): Unknown · unknown · Mar 17, 2023 · N5113A · Boeing 73783N · Fuselage Structure (General) > 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 489,900 BETWEEN UPPER FRAME AND LOWER FRAME CUTOUT IAW B737-800 BCF SRM 52-30-01-2R-3 REPAIR 3, PARAG.4 - [SDR UIEA2023031600263](https://openairdocs.org/sdr/UIEA2023031600263.md): Unknown · unknown · Mar 17, 2023 · N5113A · Boeing 73783N · Fuselage Structure (General) > 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 B737-800 BCF SRM 53-00-03-2R-1 REPAIR 1 PARAG.4, FIG 205.

) - [SDR UIEA2023031600265](https://openairdocs.org/sdr/UIEA2023031600265.md): Unknown · unknown · Mar 17, 2023 · N5113A · Boeing 73783N · Fuselage Structure (General) > 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 AND BS803 I/A/W B737-800BCF SRM 53-00-53-2R-3 REPAIR 3 PARAG 4, FIG 201. REV16 DATED NOV/10/22

) Next page: https://openairdocs.org/aircraft/N5113A/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N5113A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N5113A/reports --- 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.