# Service difficulty reports: N5167A A list on [N5167A](https://openairdocs.org/aircraft/N5167A.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SCNA20260916394S](https://openairdocs.org/sdr/SCNA20260916394S.md): Release Mech · faulted · Sep 15, 2026 · N5167A · Boeing 73783N · Emergency Equipment > FORWARD 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# 141517 - [SDR SCNA20260916394](https://openairdocs.org/sdr/SCNA20260916394.md): Holder · broken · Sep 15, 2026 · N5167A · Boeing 73783N · Emergency Equipment > FORWARD 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) - [SDR SCNA20260518206](https://openairdocs.org/sdr/SCNA20260518206.md): Oxygen Bottle · empty · May 18, 2026 · N5167A · Boeing 73783N · Crew Oxygen System > CREW 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. - [SDR SCNA20260512195](https://openairdocs.org/sdr/SCNA20260512195.md): Girt Bar · disengaged · May 12, 2026 · N5167A · Boeing 73783N · Emergency Equipment > L1 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. - [SDR SCNA20260202051](https://openairdocs.org/sdr/SCNA20260202051.md): Bulb · inoperative · Jan 31, 2026 · N5167A · Boeing 73783N · Emergency Lighting > TWO EMERGENCY LIGHTS ABOVE R1 DOOR INOP. R & R THE TWO EMERGENCY LIGHT BULBS ABOVE R1 DOOR IAW AMM 33-51-01. OPS CHECKED GOOD. - [SDR SCNA20251201453](https://openairdocs.org/sdr/SCNA20251201453.md): Wire · shorted · Nov 27, 2025 · N5167A · Boeing 73783N · Electrical Power System Wiring > INTERMITTENT 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 TIME - [SDR SCNA20251103426](https://openairdocs.org/sdr/SCNA20251103426.md): Slide · detached · Nov 1, 2025 · N5167A · Boeing 73783N · Escape Slide > L1 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 AMM25-61-1 - [SDR UIEA2025071100906](https://openairdocs.org/sdr/UIEA2025071100906.md): Skin · cracked · Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/Skin > R/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 138.7, 23" FROM FRONT SPAR.(

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-1 - [SDR UIEA2025071100907](https://openairdocs.org/sdr/UIEA2025071100907.md): Skin · cracked · Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/Skin > R/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 101 FROM FRONT SPAR.(

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 F - [SDR UIEA2025071100908](https://openairdocs.org/sdr/UIEA2025071100908.md): Skin · cracked · Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/Skin > L/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 147.9, 14.72" FROM FRONT SPAR.(

ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT L/H HORIZONTAL STABILIZER LOWER SKIN STA 147.9, 14.72" FROM FRONT SPAR, MATERIAL USED: DOUB - [SDR UIEA2025071100909](https://openairdocs.org/sdr/UIEA2025071100909.md): Skin · cracked · Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/Skin > R/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 138.7, 9.02" FROM AFT SPAR.(

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-1 - [SDR UIEA2025071100910](https://openairdocs.org/sdr/UIEA2025071100910.md): Skin · cracked · Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/Skin > R/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, REP - [SDR UIEA2025071100914](https://openairdocs.org/sdr/UIEA2025071100914.md): Skin · cracked · Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/Skin > L/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 - [SDR UIEA2025071100915](https://openairdocs.org/sdr/UIEA2025071100915.md): Skin · cracked · Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/Skin > L/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 (20 - [SDR UIEA2025071100916](https://openairdocs.org/sdr/UIEA2025071100916.md): Skin · cracked · Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/Skin > L/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 REPA - [SDR UIEA2025071100917](https://openairdocs.org/sdr/UIEA2025071100917.md): Skin · cracked · Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/Skin > L/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 RE - [SDR UIEA2025071100918](https://openairdocs.org/sdr/UIEA2025071100918.md): Skin · cracked · Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer, Plate/Skin > L/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 RE - [SDR UIEA2025071100919](https://openairdocs.org/sdr/UIEA2025071100919.md): Stiffener · cracked · Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer Structure > R/H HORIZONTAL STABILIZER NUMBER 2 STA 92.7 HAS VERTICAL STIFFENERS #4 CRACKED LOWER SIDE.(

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" I - [SDR UIEA2025071100920](https://openairdocs.org/sdr/UIEA2025071100920.md): Stiffener · cracked · Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer Structure > R/H HORIZONTAL STABILIZER NUMBER 2 STA 92.7 HAS VERTICAL STIFFENERS #3 CRACKED LOWER SIDE.(

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" IAW - [SDR UIEA2025071100921](https://openairdocs.org/sdr/UIEA2025071100921.md): Stiffener · cracked · Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer Structure > R/H HORIZONTAL STABILIZER NUMBER 2 STA 92.7 HAS VERTICAL STIFFENERS #2 CRACKED LOWER SIDE.(

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 REPAIR - [SDR UIEA2025071100922](https://openairdocs.org/sdr/UIEA2025071100922.md): Stiffener · cracked · Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer Structure > R/H HORIZONTAL STABILIZER NUMBER 6 STA 129.5 HAS VERTICAL STIFFENERS #3 CRACKED LOWER SIDE.(

ACCOMPLISHED AT R/H HORIZONTAL STABILIZER RIB #6 STA 129.5 STIFFENER #3, CATEGORY "A" REPAIR, PERMANENT REPAIR. LOCATION 23" FROM FRONT SPAR, CRAC - [SDR UIEA2025071100923](https://openairdocs.org/sdr/UIEA2025071100923.md): Stiffener · cracked · Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer Structure > R/H HORIZONTAL STABILIZER NUMBER 10 STA 166.3 HAS VERTICAL STIFFENERS #3 CRACKED LOWER SIDE.(

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-7 - [SDR UIEA2025071100924](https://openairdocs.org/sdr/UIEA2025071100924.md): Stiffener · cracked · Jul 10, 2025 · N5167A · Boeing 73783N · Horizontal Stabilizer Structure > L/H HORIZONTAL STABILIZER NUMBER 2 STA 92.7 HAS VERTICAL STIFFENERS #3 CRACKED LOWER SIDE.(

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 APROX - [SDR UIEA2025011400056](https://openairdocs.org/sdr/UIEA2025011400056.md): Warning Light · false activation · Jan 14, 2025 · N5167A · Boeing 73783N · Central Warning > SPEED 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 22-1 - [SDR UIEA2024100800967](https://openairdocs.org/sdr/UIEA2024100800967.md): Warning Message · false indication · Oct 7, 2024 · N5167A · Boeing 73783N · Cabin Pressure Control System > CABIN DID NOT PRESURIZE AFTER T/O(

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 LEAK - [SDR UIEA2024052400433](https://openairdocs.org/sdr/UIEA2024052400433.md): Door · open · May 24, 2024 · N5167A · Boeing 73783N · Doors > STRONG 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(

INSPECTED A/C PER B737 AMM 05-51-67. FOUND EXTERNAL POWER DOOR OPEN. - [SDR UIEA2023052500522](https://openairdocs.org/sdr/UIEA2023052500522.md): Unknown · unknown · Jun 3, 2023 · N5167A · Boeing 73783N · Fuselage Structure (General) > PAX CABIN FWD ENTRY AREA WL 208.1 AT LBL 60, BETWEEN BS 332.1 AND BS 294.5 SIDE BEAM WITH CRACK.(

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 - [SDR UIEA2023052500523](https://openairdocs.org/sdr/UIEA2023052500523.md): Unknown · unknown · Jun 3, 2023 · N5167A · Boeing 73783N · Fuselage Structure (General) > WHILE PERFORMING AFT BULKHEAD INSPECTION WAS FOUND PERMANENT REPAIR LOCATED BETWEEN B/S 1016 & B/S 1046, BETWEEN STR 13L & STR 16L WITH LIGHT CORROSION(

PERFORMED PERMANENT REPAIR FUSELAGE SKIN SECTION FROM BS 1016 TO BS 1040 BETWEEN STR 13L AND STR 16L. DUE - [SDR UIEA2023053000530](https://openairdocs.org/sdr/UIEA2023053000530.md): Unknown · unknown · Jun 3, 2023 · N5167A · Boeing 73783N · Wing Structure > DURING 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,(

REMOVED CORROSION I/A/W B737-800 BCF SRM 51-10-02-0G-0 PARAG 15A AND EVALUATED REWORK AREA AND FOUND IT WI - [SDR UIEA2023053000531](https://openairdocs.org/sdr/UIEA2023053000531.md): Unknown · unknown · Jun 3, 2023 · N5167A · Boeing 73783N · Fuselage Structure (General) > LOWER 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.(

PERFORMED PERMANENT REPAIR A - [SDR UIEA2023053000532](https://openairdocs.org/sdr/UIEA2023053000532.md): Unknown · unknown · Jun 3, 2023 · N5167A · Boeing 73783N · Fuselage Structure (General) > FAA FINDING AFT CARGO COMPARTMENT STR 25LH EVIDENCE OF CORROSION ON ENTIRE LENGTH OF FLOOR CHANNEL SUPPORT(

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, ORIG - [SDR UIEA2023053000533](https://openairdocs.org/sdr/UIEA2023053000533.md): Unknown · unknown · Jun 3, 2023 · N5167A · Boeing 73783N · Wing Structure > LT 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)(

PERFORMED PERMANENT REPAIR AT LH WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE FROM LBL 5 TO LBL 41, DUE TO CR - [SDR UIEA2023053000534](https://openairdocs.org/sdr/UIEA2023053000534.md): Unknown · unknown · Jun 3, 2023 · N5167A · Boeing 73783N · Wing Structure > LT 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)(

PERFORMED PERMANENT REPAIR AT LH WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE FROM LBL 5 T - [SDR UIEA2023053000535](https://openairdocs.org/sdr/UIEA2023053000535.md): Unknown · unknown · Jun 3, 2023 · N5167A · Boeing 73783N · Wing Structure > RT 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)(

PERFORMED PERMANENT REPAIR AT WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE BETWEEN RBL 5 TO - [SDR UIEA2023053000536](https://openairdocs.org/sdr/UIEA2023053000536.md): Unknown · unknown · Jun 3, 2023 · N5167A · Boeing 73783N · Wing Structure > RT 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)(

PERFORMED PERMANENT REPAIR AT WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE BETWEEN RBL 5 - [SDR UIEA2023053000537](https://openairdocs.org/sdr/UIEA2023053000537.md): Unknown · unknown · Jun 3, 2023 · N5167A · Boeing 73783N · Wing Structure > DURING 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.(

REMOVED CORROSION I/A/W B737-800 BCF SRM 51-10-02-0G-0 PARAG 15A. EVALUATED REWORKED AREA AND FOUND IT WITH - [SDR UIEA2023053000538](https://openairdocs.org/sdr/UIEA2023053000538.md): Unknown · unknown · Jun 3, 2023 · N5167A · Boeing 73783N · Fuselage Structure (General) > PAX CABIN FWD ENTRY AREA, RH SIDE BEAM WITH CORROSION BETWEEN BS 303.9 AND BS 344 WL 208.1 RBL 60.(

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 DA - [SDR UIEA2023053100545](https://openairdocs.org/sdr/UIEA2023053100545.md): Doubler · unknown · Jun 3, 2023 · N5167A · Boeing 73783N · Fuselage Structure (General) > FUSELAGE - 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.(

REPLACED DOUBLER P/N: 141A3722-12 FUSELAGE SECTION 41 RHS ELECTRICAL GROUN - [SDR UIEA2023053100546](https://openairdocs.org/sdr/UIEA2023053100546.md): Check Valve · unknown · Jun 3, 2023 · N5167A · Boeing 73783N · Wing Structure > LEFT WING CENTER FUEL TANK, FOUND A FLAPPER VALVE WITH HALF THE LUGS BROKEN AT BOTTOM ROOT OF SKIN RIB 1.(

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 T - [SDR UIEA2023053100547](https://openairdocs.org/sdr/UIEA2023053100547.md): Antenna · unknown · Jun 3, 2023 · N5167A · Boeing 73783N · Emergency Locator Beacon > UPPER FUSELAGE, MAIN CARGO COMPARTMENT, DURING ELT SYSTEM TEST FOUND ELT UNIT SHOWING 3 FLASHES FAULT CODE.(

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 T - [SDR UIEA2023053100548](https://openairdocs.org/sdr/UIEA2023053100548.md): Unknown · unknown · Jun 3, 2023 · N5167A · Boeing 73783N · Empennage Structure > WHILE PERFORMING LH HORIZONTAL STAB. REAR SPAR LOWER LUG BUSHING REPLACEMENT WAS FOUND LOWER LUG AFT FACE WITH CORROSION(

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 SH - [SDR UIEA2022100801100](https://openairdocs.org/sdr/UIEA2022100801100.md): Processor · unbalanced · Oct 7, 2022 · N5167A · Boeing 73783N · Fuel Quantity Indicator > FUEL 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 28 ## 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 = 'N5167A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N5167A/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.