# Service difficulty reports: N5179A A list on [N5179A](https://openairdocs.org/aircraft/N5179A.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SCNA20260615248](https://openairdocs.org/sdr/SCNA20260615248.md): Power Supply · inoperative · Jun 14, 2026 · N5179A · Boeing 737800* · Emergency Lighting > GALLEY EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR AND L1 DOOR INOP. REMOVED & REPLACED GALLEY EMERGENCY EXIT SIGN POWER PACK IAW AMM 33-51-06. OPS CHECK GOOD AT THIS TIME. - [SDR SCNA20251211481](https://openairdocs.org/sdr/SCNA20251211481.md): Placard · missing · Dec 10, 2025 · N5179A · Boeing 73783N · Placards and Markings > FO SIDE EMERGENCY ESCAPE ROPE PLACARD MISSING. - [SDR SCNA20251211480](https://openairdocs.org/sdr/SCNA20251211480.md): Placard · missing · Dec 10, 2025 · N5179A · Boeing 73783N · Placards and Markings > CA SIDE EMERGENCY ESCAPE ROPE PLACARD MISSING. INSTALLED PROPER PLACARD IAW AMM 11-32-02. - [SDR SCNA20251030419](https://openairdocs.org/sdr/SCNA20251030419.md): Door · not reported · Oct 27, 2025 · N5179A · Boeing 737800* · Doors > REMOVE & REINSTALL RT LOWER HP AIR DOOR. REMOVED RT LOWER HP AIR DOOR & INSTALLED NEW HP AIR DOOR WITH NEW HINGES AND LATCHES. - [SDR SCNA20251030418](https://openairdocs.org/sdr/SCNA20251030418.md): Plate · worn · Oct 27, 2025 · N5179A · Boeing 737800* · Doors > REPLACE STRIKER PLATE (DOUBLER) ON RT PACK DOOR FWD INNER SURFACE WORN. REMOVED & REPLACED (DOUBLER) STRIKER PLATE ON RT PACK ACCESS DOOR FWD INNER SURFACE IAW SRM 51-40-02 - [SDR SCNA20251028413](https://openairdocs.org/sdr/SCNA20251028413.md): Placard · missing · Oct 26, 2025 · N5179A · Boeing 737800* · Placards and Markings > AFT CARGO CAUTION DO NOT BLOCK SMOKE DETECTOR MISSING IN 2 AREAS. INSTALLED 2EA. CAUTION SMOKE DETECTOR DO NOT BLOCK IN AFT CARGO CEILINGS ADJACENT TO SMOKE DETECTORS IAW B-737 MM 20-10-11. - [SDR SCNA20251030417](https://openairdocs.org/sdr/SCNA20251030417.md): Support Beam · damaged · Oct 22, 2025 · N5179A · Boeing 737800* · Wing Main, Frame Structure > GROUND CREW FOUND HP AIR DOOR PARTIALLY HANGING. LATCH AND LANDING DAMAGED. PERFORMED PERMANENT REPAIR ON WING CENTOR SECTION LWR SUPPORT BEAM LWR CHORD AT RBL 40.875 IAW B-737 SRM 50-10-13-2R-3. REV24 10. REMOVED & REPLACED DOUBLE ASSY ITEM:149A7244IAATSMRO - [SDR SCNA20250808310](https://openairdocs.org/sdr/SCNA20250808310.md): Flap System · faulted · Aug 8, 2025 · N5179A · Boeing 737800* · Trailing Edge Flap Control System > FLIGHT NUMBER 3080. DURING LAND FLAPS WERE STUCK AT 15 AND WOULD NOT RETRACT UP OR EXTEND RAN QRH PROCEDURE TRAILING EDGE FLAP DISAGREE. PERFORMED FIM 27-51 TASK 836, NO DEFECTS NOTED. OPS CHECK GOOD IAW FIM 27-51 TASK 836. - [SDR UIEA2025061200742](https://openairdocs.org/sdr/UIEA2025061200742.md): Channel · corroded · Jun 11, 2025 · N5179A · Boeing 73783N · Fuselage Miscellaneous Structure > AFT CARGO COMP RAIL-CHANNEL LBL 8.10 CORROSION NOTED BETWEEN STA 787 TO STA 767.(

REMOVED CORROSION ON AFT CARGO COMP RAIL-CHANNEL LBL 8.10 BETWEEN STA 787 TO STA 767 +5" IAW SRM 51-10-02 REV 23. ORIGINAL THICKNESS 0.063", REMAINING THICKNESS 0.032", FOUND T - [SDR UIEA2025061200745](https://openairdocs.org/sdr/UIEA2025061200745.md): Channel · corroded · Jun 11, 2025 · N5179A · Boeing 73783N · Fuselage Miscellaneous Structure > AFT CARGO COMP RAIL-CHANNEL RBL 8.10 CORROSION NOTED BETWEEN STA 787 TO STA 767.(

REMOVED CORROSION ON AFT CARGO COMP RAIL-CHANNEL RBL 8.10 BETWEEN STA 787 TO STA 767 +4" IAW SRM 51-10-02 REV 23. ORIGINAL THICKNESS 0.063", REMAINING THICKNESS 0.042", FOUND T - [SDR UIEA2025061300759](https://openairdocs.org/sdr/UIEA2025061300759.md): Skin · cracked · Jun 11, 2025 · N5179A · Boeing 73783N · Horizontal Stabilizer, Plate/Skin > RH HORIZONTAL STABILIZER, LOWER SKIN STAB STA 120.30 +10" FROM AFT SPAR, CRACK LENGTH 1.25".(

ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER ALUMINUM 2024-T3 0.090" AND FILLER REPAIR ALUMINUM 2024-T3 0.071" AT RH HORIZONTAL STABILIZER, LOWER SKIN - [SDR UIEA2025061300760](https://openairdocs.org/sdr/UIEA2025061300760.md): Skin · cracked · Jun 11, 2025 · N5179A · Boeing 73783N · Horizontal Stabilizer, Plate/Skin > RH HORIZONTAL STABILIZER, LOWER SKIN STAB STA 129.50 +34.25" FROM AFT SPAR, CRACK LENGTH 1.0".(

ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER ALUMINUM 2024-T3 0.080" AND FILLER REPAIR ALUMINUM 2024-T3 0.063" AT RH HORIZONTAL STABILIZER, LOWER SK - [SDR UIEA2025061300761](https://openairdocs.org/sdr/UIEA2025061300761.md): Skin · cracked · Jun 11, 2025 · N5179A · Boeing 73783N · Horizontal Stabilizer, Plate/Skin > LH HORIZONTAL STABILIZER, LOWER SKIN STAB STA 120.30+10" FROM AFT SPAR, CRACK LENGTH 1.0".(

ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER ALUMINUM 2024-T3 0.090" AND FILLER REPAIR ALUMINUM 2024-T3 0.071" AT LH HORIZONTAL STABILIZER, LOWER SKIN S - [SDR UIEA2025061300762](https://openairdocs.org/sdr/UIEA2025061300762.md): Skin · cracked · Jun 11, 2025 · N5179A · Boeing 73783N · Horizontal Stabilizer, Plate/Skin > LH HORIZONTAL STABILIZER, LOWER SKIN STAB STA 129.50+26" FROM AFT SPAR, CRACK LENGTH 1.0".(

ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER ALUMINUM 2024-T3 0.080" AND FILLER REPAIR ALUMINUM 2024-T3 0.063" AT LH HORIZONTAL STABILIZER, LOWER SKIN S - [SDR UIEA2025061300763](https://openairdocs.org/sdr/UIEA2025061300763.md): Channel · corroded · Jun 11, 2025 · N5179A · Boeing 73783N · Fuselage Miscellaneous Structure > AFT CARGO COMP RAIL-CHANNEL RBL 3.00 CORROSION NOTED BETWEEN STA 787 TO STA 767.(

REMOVED CORROSION ON AFT CARGO COMP RAIL-CHANNEL RBL 3.00 BETWEEN STA 787 TO STA 767 +5" IAW SRM 51-10-02 REV 23. ORIGINAL THICKNESS 0.063", REMAINING THICKNESS 0.045", FOUND T - [SDR UIEA2025061300764](https://openairdocs.org/sdr/UIEA2025061300764.md): Floorbeam · corroded · Jun 11, 2025 · N5179A · Boeing 73783N · Fuselage Main, Floor Beam > MDCC, FLOOR STRUCTURE, BS 986.5 BETWEEN LBL 24.75 TO L2 DOOR INNER CHORD WITH SURFACE CORROSION.(

PERFORMED PERMANENT REPAIR AT TRANSVERSAL FLOOR BEAM STA 986.5 BTW BL 0.00 AND LBL 50.00 UPPER HORIZONTAL FLANGE AS PER ENGINEERING ORDER CONTROL #25101-1 REV A - [SDR UIEA2025061300765](https://openairdocs.org/sdr/UIEA2025061300765.md): Rib · cracked · Jun 11, 2025 · N5179A · Boeing 73783N · Horizontal Stabilizer, Spar/Rib > DURING VISUAL INSPECTION OF RH HORIZONTAL STABILIZER IN THE INSPAR RIB, LOWER CHORD STAB STA 92.70 WERE FOUND 2 CRACKS AT STIFFENER #2 AND STIFFENER #3.(

ACCOMPLISHED CATEGORY "A" REPAIR, PERMANENT REPAIR ON R/H HORIZONTAL STABILIZER INSPAR RIB STA 92.70 AT - [SDR UIEA2025061300766](https://openairdocs.org/sdr/UIEA2025061300766.md): Rib · cracked · Jun 11, 2025 · N5179A · Boeing 73783N · Horizontal Stabilizer, Spar/Rib > CRACK FOUND ON R/H FIXED HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 95.96.(

REMOVED R/H HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 95.96 AND INSTALLED SAME RIB CHORD (PN 186A1303-2) L/E STA 95.96 AS PER SRM BCG-D634A209 AND 51-40-02-0G-0 REV 23. NO FURTHER - [SDR UIEA2025061300767](https://openairdocs.org/sdr/UIEA2025061300767.md): Rib · cracked · Jun 11, 2025 · N5179A · Boeing 73783N · Horizontal Stabilizer, Spar/Rib > CRACK FOUND ON R/H FIXED HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 105.26.(

REMOVED R/H HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 105.26 AND INSTALLED SAME RIB CHORD L/E STA 105.26 (PN 186A1304-2) AS PER SRM BCG-D634A209 AND SRM 51-40-02-0G-0 REV 23. NO - [SDR UIEA2025061300768](https://openairdocs.org/sdr/UIEA2025061300768.md): Tail Cone · dented · Jun 11, 2025 · N5179A · Boeing 73783N · Aerodynamic Fairings > REF DMI #194100: PERFORM PERMANENT REPAIR FOR DENT FOUND ON TAIL CONE STA 1200 BOTTOM SECTION.(

PERMANENT REPAIR FOR DENT FOUND ON TAIL CONE STA 1200 BOTTOM SECTION WAS ACCOMPLISHED BY OUTSIDE VENDOR SAL AEROSPACE TECHNOLOGIES W/O #400100088. NO FURTHER DEFE - [SDR UIEA2025061300769](https://openairdocs.org/sdr/UIEA2025061300769.md): Rib · cracked · Jun 11, 2025 · N5179A · Boeing 73783N · Horizontal Stabilizer, Spar/Rib > CRACK FOUND ON R/H FIXED HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 114.55.(

REMOVED R/H HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 114.55 AND INSTALLED SAME RIB CHORD (PN 186A1305-1) L/E STA 114.55 AS PER SRM BCG-D634A209 AND SRM 51-40-02-0G-0 REV 23. NO - [SDR UIEA2025061300770](https://openairdocs.org/sdr/UIEA2025061300770.md): Panel · corroded · Jun 11, 2025 · N5179A · Boeing 73783N · Fuselage Main, Structure > COVER OF AFT BULKHEAD OF FWD CARGO COMPARTMENT, INTERNAL SQUARE WITH CORROSION ON HOLES FOR FASTENERS.(

UPON EVALUATION ON FWD CARGO AFT BULKHEAD PANEL WAS FOUND TO BE OUT OF LIMITS PER SRM 51-10-02-0G-0. REMOVED AND REPLACED PANEL AS REQUIRED PER 25-52-17-4 - [SDR UIEA2025061300771](https://openairdocs.org/sdr/UIEA2025061300771.md): Battery Pack · inoperative · Jun 11, 2025 · N5179A · Boeing 73783N · Emergency Lighting > RH SIDE EMERGENCY LIGHTS INOP.(

REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805 REV 86. OPERATIONAL TEST SATISFACTORY.

) - [SDR UIEA2025021200131](https://openairdocs.org/sdr/UIEA2025021200131.md): Lens · damaged · Feb 12, 2025 · N5179A · Boeing 73783N · Emergency Lighting > RH EXTERNAL EMERGENCY LENS & LIGHT INOP AFT OF RIGHT WING.(

EMERGENCY LIGHT L00548 DEACTIVATED ELECTRICALLY INOP REF AMM 33-51-04. THIS CLOSES MDDR 225774. PLACARD REMOVED. INSTALLED R/H EXT EMERGENCY LIGHT LENS IAW AMM 33-51-04 NO OTHER DEFECTS NOTED THIS C - [SDR UIEA2024092700961](https://openairdocs.org/sdr/UIEA2024092700961.md): Indication Sys · false indication · Sep 27, 2024 · N5179A · Boeing 73783N · Cargo/Baggage Doors > AFT CARGO DOOR OPEN LIGHT ON TAKE OFF ROLL(

FOUND DOOR SWITCH STICKS. CLEANED AFT CARGO DOOR OPEN MECHANISM AND DOOR SWITCH TESTED PER BOEING AMM TASK 52-31-00-700-801, OPS CHECK GOOD. LIGHT GOES OUT

) - [SDR UIEA2024092200914](https://openairdocs.org/sdr/UIEA2024092200914.md): Proximity Sensor · faulted · Sep 22, 2024 · N5179A · Boeing 73783N · Trailing Flap Position Indicating System > LE FLAP TRANSIT ILLUMINATED DURING T/O. IMMEDIATELY AT THRUST, LEVER INCREASE. DISCONTINUED TAKEOFF(

R/R LE FLAP PROXIMITY SENSOR POSITION F4 IAW B737 AMM 27-88-11. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

) - [SDR UIEA2023122001007](https://openairdocs.org/sdr/UIEA2023122001007.md): Pump · unknown · Dec 20, 2023 · N5179A · Boeing 73783N · Fuel Boost Pump > LEFT CENTER FUEL PUMP "LOW PRESSURE ILLUMINATED IN FLIGHT. RAN QRH ACCORDINGLY(

21DEC23 - 1699547 - ITEMS M1-M3- PDX - FOUND BOOST PUMP TANK CTR LEFT C/B TRIPPED UPON A/C RETURN. TROUBLESHOOT PER B737 FIM 28-22 FT 801. PER MCC DIRECTION, REPLACED R54 (BOOST - [SDR UIEA2023063000673](https://openairdocs.org/sdr/UIEA2023063000673.md): Doubler · unknown · Aug 13, 2023 · N5179A · Boeing 73783N · Fuselage Structure (General) > LOWER FUSELAGE, EXTERNAL POWER RECEPTACLE, INNER DOUBLER WITH CRACK.(

R/R INNER DOUBLER P/N: 141A3722-12 AT EXTERNAL POWER RECEPTABLE IAW B737-800 BCF SRM 51-10-02-0G-0 PARAG 9

) - [SDR UIEA2023063000674](https://openairdocs.org/sdr/UIEA2023063000674.md): Unknown · unknown · Aug 13, 2023 · N5179A · Boeing 73783N · Wing Structure > LH WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT RBL 7 WITH CRACK (FOUND DURING ACCESS PROCESS TO THE W/O A1N080-7-522)(

PERFORMED PERMANENT REPAIR ON REAR SPAR VAPOR BARRIER ATTACH ANGLE BETWEEN LBL 5 TO LBL 18.5 DUE TO CRACKS IAW B737-800 BCF - [SDR UIEA2023063000675](https://openairdocs.org/sdr/UIEA2023063000675.md): Radio Altimeter · unknown · Aug 13, 2023 · N5179A · Boeing 73783N · Navigation System > NAVIGATION - RADIO ALTIMETER SYSTEM - INSTALLATION OF COLLINS LRA-900 LOW RANGE RADIO ALTIMETERS - STC ST02002WI - AD 2021-23-12 IAW ATLAS AIR EO 3834A029 REV.0, PARTS 1.(

PERFORMED NAVIGATION - RADIO ALTIMETER SYSTEM - INSTALLATION OF COLLINS LRA-900 LOW RA - [SDR UIEA2023063000676](https://openairdocs.org/sdr/UIEA2023063000676.md): Unknown · unknown · Aug 13, 2023 · N5179A · Boeing 73783N · Water and Waste System > FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - POST PREVENTIVE MODIFICATION INSPECTION - SB 737-53-1335 - AD 2013-19-23 AMOC IAW ATLAS AIR EO 3853A035 REV.0, PARTS 2-3.(

PEFORMED POST PREVENTIVE MODIFICATION INSPECTION - SB 737-53-1335 - AD 2 - [SDR UIEA2023072800763](https://openairdocs.org/sdr/UIEA2023072800763.md): Unknown · unknown · Aug 13, 2023 · N5179A · Boeing 73783N · Wing Structure > RT WING FUEL TANK STIFFENER WITH CRACK, BETWEEN RIB 21 & RIB 22 (OBSERVED WHILE PERFORMING THE 20 YEARS INSPECTION)(

PERFORMED PERMANENT REPAIR ON RH OUTBOARD WING UPPER STRINGER U-9 DUE TO CRACK IAW COOPESA EO #: COO-EO-17861-R01 (JUL/15/23) DOCUMENTED AND - [SDR Q2SA20210224443](https://openairdocs.org/sdr/Q2SA20210224443.md): Wire · damaged · Feb 24, 2021 · N5179A · Boeing 73783N · Flight Control System Wiring > AIRCRAFT GROUNDED. SELECTED FLAPS 1 WITH NO MOVEMENT. RAN VARIOUS FLAP QRH PROCEDURES AND EVENTUALLY ENDED WITH ALL FLAPS UP LANDING QRH PROCEDURE. NO ABNORMALLY HARD LANDING. AUTO BRAKES MAX. TROUBLESHOOT PER WDM 27-53-21. REPAIRED WIRES W1024-2008R, W1024-20 ## 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 = 'N5179A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N5179A/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.