N5167A

Service difficulty reports · 42

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N5167A' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SCNA20260916394SRelease Mech · faultedFORWARD PLASTIC CLIP ON R1 GIRT BAR BROKEN. REMOVED AND REPLACED R1 GIRT BAR RELEASE ASSY REF AMM 25-66-01 THIS CLEARS MEL 52-16-2 MDDR# 141517Sep 15, 2026 · N5167A · Boeing 73783N · Emergency EquipmentSDR SCNA20260916394Holder · brokenFORWARD PLASTIC CLIP ON R1 GIRT BAR BROKEN (MAIN CABIN EXIT/SLIDE (-800BCF) R-1 DOOR SLIDE INOPERATIVE OR MISSING PROVIDED L1 OPERATES NORMALLY.) (WORK IN PROGRESS)Sep 15, 2026 · N5167A · Boeing 73783N · Emergency EquipmentSDR SCNA20260518206Oxygen Bottle · emptyCREW O2 LEVEL AT ZERO IN FLIGHT DECK. (OXYGEN PRESSURE INDICATOR; FLIGHT DECK CREW OXYGEN INDICATOR). ACCOMPLISHED FAULT ISO MANUAL FIM 35-1 TASK 804. NO FAULTS FOUND OK FOR SERVICE THIS CLEARS MEL 35-3-1 MDDR 138901. REMOVED PLACARDS.May 18, 2026 · N5167A · Boeing 73783N · Crew Oxygen SystemSDR SCNA20260512195Girt Bar · disengagedL1 GIRT BAR WILL NOT DISENGAGE FROM HOLDER ON FLOOR. PERFORMED OPERATIONAL CHECK OF THE FLOOR MOUNTED ESCAPE SLIDE BRACKET INSTALLATION IAW AMM 25-66-02. OPS CHECKS GOOD. NO DEFECTS NOTED. ACFT OK FOR SERVICE.May 12, 2026 · N5167A · Boeing 73783N · Emergency EquipmentSDR SCNA20260202051Bulb · inoperativeTWO EMERGENCY LIGHTS ABOVE R1 DOOR INOP. R & R THE TWO EMERGENCY LIGHT BULBS ABOVE R1 DOOR IAW AMM 33-51-01. OPS CHECKED GOOD.Jan 31, 2026 · N5167A · Boeing 73783N · Emergency LightingSDR SCNA20251201453Wire · shortedINTERMITTENT SMELL OF SHORTING WIRE OR ELECTRICAL NEAR CAPTAINS SIDE MASTER CAUTION DURING FLIGHT PERFORMED AMM TASK 21-00 TASK 801 NO SMELL NOTED AT THIS TIMENov 27, 2025 · N5167A · Boeing 73783N · Electrical Power System WiringSDR SCNA20251103426Slide · detachedL1 DOOR MOUNTED ESCAPE SLIDE FELL OUT OF SHROUD ( MAIN CABIN EXIT/SLIDE (-800BCF) L-1 DOOR SLIDE INOPERATIVE OR MISSING PROVIDED R1 OPERATES NORMALLY. ) INSTALLED SLIDE AT L1 DOOR THIS CLEARS MEL MDDR# 134811, 52-16-1 REF AMM25-61-1Nov 1, 2025 · N5167A · Boeing 73783N · Escape SlideSDR UIEA2025071100906Skin · crackedR/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 138.7, 23" FROM FRONT SPAR.(<P>ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT LOWER SKIN R/H HORIZONTAL STABILIZER STA 138.7, 23" FROM FRONT SPAR IAW B737 SRM 55-10-01-2R-1Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/SkinSDR UIEA2025071100907Skin · crackedR/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 101 FROM FRONT SPAR.(<P>ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT LOWER SKIN R/H HORIZONTAL STABILIZER STA 101 FROM FRONT SPAR IAW B737 SRM 55-10-01-2R-11, REPAIR 11 FJul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/SkinSDR UIEA2025071100908Skin · crackedL/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 147.9, 14.72" FROM FRONT SPAR.(<P>ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT L/H HORIZONTAL STABILIZER LOWER SKIN STA 147.9, 14.72" FROM FRONT SPAR, MATERIAL USED: DOUBJul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/SkinSDR UIEA2025071100909Skin · crackedR/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 138.7, 9.02" FROM AFT SPAR.(<P>ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT LOWER SKIN R/H HORIZONTAL STABILIZER STA 138.7, 9.02" FROM AFT SPAR IAW B737 SRM 55-10-01-2R-1Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/SkinSDR UIEA2025071100910Skin · crackedR/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 175.5, 10" FROM T/E BEAM. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT LOWER SKIN R/H HORIZONTAL STABILIZER STA 175.5, 10" FROM T/E BEAM IAW B737 SRM 55-10-01-2R-11, REPJul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/SkinSDR UIEA2025071100914Skin · crackedL/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 147.9, 7.09" FROM FRONT SPAR. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT L/H HORIZONTAL STABILIZER LOWER SKIN STA 147.9, 7.09" FROM FRONT SPAR, MATERIAL USED: DOUBLER Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/SkinSDR UIEA2025071100915Skin · crackedL/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 138.7, 9" FROM AFT SPAR. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT L/H HORIZONTAL STABILIZER LOWER SKIN STA 138.7, 9" FROM AFT SPAR, MATERIAL USED: DOUBLER REPAIR (20Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/SkinSDR UIEA2025071100916Skin · crackedL/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 101.9, 9.05" FROM AFT SPAR. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT L/H HORIZONTAL STABILIZER LOWER SKIN STA 101.9, 9.05" FROM AFT SPAR, MATERIAL USED: DOUBLER REPAJul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/SkinSDR UIEA2025071100917Skin · crackedL/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 101.9, 18.83" FROM AFT SPAR. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT L/H HORIZONTAL STABILIZER LOWER SKIN STA 101.9, 18.83" FROM AFT SPAR, MATERIAL USED: DOUBLER REJul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/SkinSDR UIEA2025071100918Skin · crackedL/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 138.7, 16.96" FROM AFT SPAR. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT L/H HORIZONTAL STABILIZER LOWER SKIN STA 138.7, 16.96" FROM AFT SPAR, MATERIAL USED: DOUBLER REJul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/SkinSDR UIEA2025071100919Stiffener · crackedR/H HORIZONTAL STABILIZER NUMBER 2 STA 92.7 HAS VERTICAL STIFFENERS #4 CRACKED LOWER SIDE.(<P>ACCOMPLISHED CATEGORY "A" REPAIR, PERMANENT REPAIR ON R/H HORIZONTAL STABILIZER RIB #2 STA 92.7 STIFFENER #4 LOWER SIDE 37.3" FROM FRONT SPAR, MEASURED CRACK 0.562" IJul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer StructureSDR UIEA2025071100920Stiffener · crackedR/H HORIZONTAL STABILIZER NUMBER 2 STA 92.7 HAS VERTICAL STIFFENERS #3 CRACKED LOWER SIDE.(<P>ACCOMPLISHED CATEGORY "A" REPAIR, PERMANENT REPAIR ON R/H HORIZONTAL STABILIZER RIB #2 STA 92.7 STIFFENER #3 LOWER SIDE 28" FROM FRONT SPAR, MEASURED CRACK 1.687" IAWJul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer StructureSDR UIEA2025071100921Stiffener · crackedR/H HORIZONTAL STABILIZER NUMBER 2 STA 92.7 HAS VERTICAL STIFFENERS #2 CRACKED LOWER SIDE.(<P>ACCOMPLISHED CATEGORY "A" REPAIR, PERMANENT REPAIR ON R/H HORIZONTAL STABILIZER RIB #2 STA 92.7 STIFFENER #2, MEASURED CRACK 1.812" IAW B-737 SRM 55-10-09-2R-4 REPAIRJul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer StructureSDR UIEA2025071100922Stiffener · crackedR/H HORIZONTAL STABILIZER NUMBER 6 STA 129.5 HAS VERTICAL STIFFENERS #3 CRACKED LOWER SIDE.(<P>ACCOMPLISHED AT R/H HORIZONTAL STABILIZER RIB #6 STA 129.5 STIFFENER #3, <SPAN>CATEGORY "A" REPAIR, PERMANENT REPAIR. LOCATION 23" FROM FRONT SPAR,</SPAN><SPAN> CRACJul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer StructureSDR UIEA2025071100923Stiffener · crackedR/H HORIZONTAL STABILIZER NUMBER 10 STA 166.3 HAS VERTICAL STIFFENERS #3 CRACKED LOWER SIDE.(<P>ACCOMPLISHED CATEGORY "A" REPAIR, PERMANENT REPAIR ON R/H HORIZONTAL STABILIZER RIB #10 STA 166.3 STIFFENER #3 AT 21" FROM FRONT SPAR, MEASURED CRACK 1.750" IAW B-7Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer StructureSDR UIEA2025071100924Stiffener · crackedL/H HORIZONTAL STABILIZER NUMBER 2 STA 92.7 HAS VERTICAL STIFFENERS #3 CRACKED LOWER SIDE.(<P>ACCOMPLISHED CATEGORY "A" REPAIR, PERMANENT REPAIR ON L/H HORIZONTAL STABILIZER RIB #2 STA 92.7 STIFFENER #3, MEASURED CRACK 2.100", LOCATED 28" FROM FRONT SPAR APROXJul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer StructureSDR UIEA2025011400056Warning Light · false activationSPEED TRIM FAIL ILLUMINATED SHORTLY AFTER TAKEOFF. STAB OUT OF TRIM ILLUMINATED AT ABOUT 18,000 FT. RAN QRH, INSTRUCTED US NOT TO RE-ENGAGE AUTOPILOT AND AUTOTHROTTLE. T/S PER FIM 22-11 TASK 849. OPS CHECK GOOD. PERFORMED STAB TRIM MOTOR TEST IAW AMM 22-1Jan 14, 2025 · N5167A · Boeing 73783N · Central WarningSDR UIEA2024100800967Warning Message · false indicationCABIN DID NOT PRESURIZE AFTER T/O(<P>PERFORMED DPCS BITE PER FIM 21-31 TASK 801. FOUND AIRCRAFT RATE TO HIGH MSG. PERFORMED FIM 21-31 TASK 815, MSG NO LONGER PRESENT AFTER SYSTEM TEST. LP 1818183 M4: PERFORMED CABIN PRESSURE LEAK TEST IAW AMM 05-51-91, NO LEAKOct 7, 2024 · N5167A · Boeing 73783N · Cabin Pressure Control SystemSDR UIEA2024052400433Door · openSTRONG VIBRATION FELT AND HEARD OVER 280KTS. SOUND REDUCED AS WE SLOWED AND INCREASED AS WE SPED UP. SLOWED TO 250KTS REMAINDER OF FLIGHT. VIBRATION STRONG ENOUGH TO BE FELT THROUGH SEATS(<P>INSPECTED A/C PER B737 AMM 05-51-67. FOUND EXTERNAL POWER DOOR OPEN. May 24, 2024 · N5167A · Boeing 73783N · DoorsSDR UIEA2023052500522Unknown · unknownPAX CABIN FWD ENTRY AREA WL 208.1 AT LBL 60, BETWEEN BS 332.1 AND BS 294.5 SIDE BEAM WITH CRACK.(<P>PERFORMED PERMANENT REPAIR ON LOWER MAIN SILL INNER CHORD FWD ENTRY AREA AT BWL 208.1, LBL 60 AT BS 303.9 DUE TO CRACK I/A/W COOPESA E.O #COO-EO-2023-17712-R00 Jun 3, 2023 · N5167A · Boeing 73783N · Fuselage Structure (General)SDR UIEA2023052500523Unknown · unknownWHILE PERFORMING AFT BULKHEAD INSPECTION WAS FOUND PERMANENT REPAIR LOCATED BETWEEN B/S 1016 & B/S 1046, BETWEEN STR 13L & STR 16L WITH LIGHT CORROSION(<P>PERFORMED PERMANENT REPAIR FUSELAGE SKIN SECTION FROM BS 1016 TO BS 1040 BETWEEN STR 13L AND STR 16L. DUEJun 3, 2023 · N5167A · Boeing 73783N · Fuselage Structure (General)SDR UIEA2023053000530Unknown · unknownDURING PAINT REMOVAL PROCESS FOR N.D.T. INSPECTION, WAS FOUND FASTENERS HEADS WITH CORROSION ON R/H WING, REAR SPAR UPPER CHORD FROM RIB 5 TO RIB 14,(<P>REMOVED CORROSION I/A/W B737-800 BCF SRM 51-10-02-0G-0 PARAG 15A AND EVALUATED REWORK AREA AND FOUND IT WIJun 3, 2023 · N5167A · Boeing 73783N · Wing StructureSDR UIEA2023053000531Unknown · unknownLOWER FUSELAGE FWD CARGO COMPARMENT DOOR EXTERNAL SKIN SECTION AT BSTA 457 BETWEEN BEAM B AND BEAM C; BSTA 470 BETWEEN BEAM B AND BEAM C; BSTA 474 BETWEEN BEAM D AND BEAM E AND BSTA 485 BETWEEN BEAM B AND BEAM C SKIN WITH DENTS.(<P>PERFORMED PERMANENT REPAIR AJun 3, 2023 · N5167A · Boeing 73783N · Fuselage Structure (General)SDR UIEA2023053000532Unknown · unknownFAA FINDING AFT CARGO COMPARTMENT STR 25LH EVIDENCE OF CORROSION ON ENTIRE LENGTH OF FLOOR CHANNEL SUPPORT(<P>EVALUATED REWORKED AREA AS FOUND WITHIN ALLOWABLE DAMAGE LIMITS I/A/W B737-800 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 PARAG 4A(2) FIG 103 DETAIL D, ORIGJun 3, 2023 · N5167A · Boeing 73783N · Fuselage Structure (General)SDR UIEA2023053000533Unknown · unknownLT WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT LBL 41 WITH CRACK. (FOUND DURING ACCESS PROCESS TO THE W/O A1N080-7-549)(<P>PERFORMED PERMANENT REPAIR AT LH WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE FROM LBL 5 TO LBL 41, DUE TO CRJun 3, 2023 · N5167A · Boeing 73783N · Wing StructureSDR UIEA2023053000534Unknown · unknownLT WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT LBL 6 WITH CRACK. (FOUND DURING ACCESS PROCESS TO THE W/O A1N080-7-549)(<P ><SPAN LANG="EN-US">PERFORMED PERMANENT REPAIR AT LH WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE FROM LBL 5 TJun 3, 2023 · N5167A · Boeing 73783N · Wing StructureSDR UIEA2023053000535Unknown · unknownRT WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT RBL 6 WITH CRACK.( FOUND DURING ACCESS PROCESS TO THE W/O A1N080-7-550)(<P><SPAN LANG="EN-US">PERFORMED PERMANENT REPAIR AT WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE BETWEEN RBL 5 TOJun 3, 2023 · N5167A · Boeing 73783N · Wing StructureSDR UIEA2023053000536Unknown · unknownRT WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT RBL 41 WITH CRACK.( FOUND DURING ACCESS PROCESS TO THE W/O A1N080-7-550)(<P ><SPAN LANG="EN-US">PERFORMED PERMANENT REPAIR AT WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE BETWEEN RBL 5 Jun 3, 2023 · N5167A · Boeing 73783N · Wing StructureSDR UIEA2023053000537Unknown · unknownDURING PAINT REMOVAL PROCESS FOR N.D.T. INSPECTION, WAS FOUND FASTENERS HEADS WITH CORROSION ON L/H WING, REAR SPAR UPPER CHORD FROM RIB 5 TO RIB 14.(<P>REMOVED CORROSION I/A/W B737-800 BCF SRM 51-10-02-0G-0 PARAG 15A. EVALUATED REWORKED AREA AND FOUND IT WITHJun 3, 2023 · N5167A · Boeing 73783N · Wing StructureSDR UIEA2023053000538Unknown · unknownPAX CABIN FWD ENTRY AREA, RH SIDE BEAM WITH CORROSION BETWEEN BS 303.9 AND BS 344 WL 208.1 RBL 60.(<P>REMOVED CORROSION AT R/H SIDE BEAM (INNER CHORD) I/A/W B737-800 SRM 51-10-02-0G-0 PARAG 15A AND EVALUATION. REWORKED AREA AND IT WAS FOUND WITHIN ALLOWABLE DAJun 3, 2023 · N5167A · Boeing 73783N · Fuselage Structure (General)SDR UIEA2023053100545Doubler · unknownFUSELAGE - SECTION 41- RHS ELECTRICAL GROUND RECEPTACLE (EGPR) CUTOUT DOUBLER ( PN 141A3722-12) DEFORMATION - CATEGORY C TIME LIMITED REPAIR IAW ATLAS AIR EO 3853A157 REV.0, PARTS 2.(<P>REPLACED DOUBLER P/N: 141A3722-12 FUSELAGE SECTION 41 RHS ELECTRICAL GROUNJun 3, 2023 · N5167A · Boeing 73783N · Fuselage Structure (General)SDR UIEA2023053100546Check Valve · unknownLEFT WING CENTER FUEL TANK, FOUND A FLAPPER VALVE WITH HALF THE LUGS BROKEN AT BOTTOM ROOT OF SKIN RIB 1.(<P>REPLACED REFUELING CHECK VALVE AT CENTER TANK, RH AND LH TANKS, I/A/W BOEING 737-800 AMM TASK 28-21-32-00-801 AND AMM TASK 28-21-32-400-801 PARAG 3 A TJun 3, 2023 · N5167A · Boeing 73783N · Wing StructureSDR UIEA2023053100547Antenna · unknownUPPER FUSELAGE, MAIN CARGO COMPARTMENT, DURING ELT SYSTEM TEST FOUND ELT UNIT SHOWING 3 FLASHES FAULT CODE.(<P>PERFORMED T/S AND FOUND ELT SYSTEM ANTENNA INTERNAL IMPEDANCE OUT OF RANGE AND ELT UNIT DISPLAYING INCORRECT A/C'S REGISTRATION NUMBER REPLACED AND TJun 3, 2023 · N5167A · Boeing 73783N · Emergency Locator BeaconSDR UIEA2023053100548Unknown · unknownWHILE PERFORMING LH HORIZONTAL STAB. REAR SPAR LOWER LUG BUSHING REPLACEMENT WAS FOUND LOWER LUG AFT FACE WITH CORROSION(<P>REMOVED CORROSION FROM L/H HORIZONTAL STAB REAR SPAR LOWER LUG AFT FACE I/A/W S/B 737-55-1074 ISSUE R00 DATED 15-AUG-02 FIG 10 PART D SHJun 3, 2023 · N5167A · Boeing 73783N · Empennage StructureSDR UIEA2022100801100Processor · unbalancedFUEL IMBAL (QRH 12-15). LH ENGINE SHUTDOWN (QRH R 6). SINGLE ENGINE EMERGENCY LANDING(PERFORMED INITIAL VISUAL INSPECTION FOR LEAKS IN THE SYSTEM, OPERATED BOTH ENGINES & INSPECTED FUEL LINES & NOZZLE FOR EVIDENCE OF LEAKS. PERFORMED FQIS BITE, FOUND FAULTS 28Oct 7, 2022 · N5167A · Boeing 73783N · Fuel Quantity Indicator
Back to N5167A