Boeing 767-31K

Service difficulty reports · 1,002

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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 aircraft_model_key = '76731K'
  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 ABXA20260929441Switch · failedEMER LIGHTS SWITCH DOES NOT CHANGE INTO ARMED WITH SWITCH GUARD DOWN. MTC REMOVED AND REPLACED EMERGENCY LIGHT SWITCH GUARD IAW AMM 33-51-00. OPS CHECK GOOD. A/C RETURNED TO SERVICE.Sep 29, 2026 · N1489A · Boeing 76731K · Emergency LightingSDR ABXA20260906396Warning Message · false activationDURING APPROACH MESSAGE "FIRE/ OVHT SYS" ILLUMINATED , MTX PERFORMED AFOLTS TEST IAW B767 AMM 26-10-00. OPS CHECK GOOD. NFF RETURNED A/C TO SERVICE.Sep 6, 2026 · N1489A · Boeing 76731K · Fire DetectionSDR ABXR2026082800015Support · corrodedCORROSION ON THE CUTOUT/ SUPPORT STRUCTURE FOR PANEL 195ML, AT THE LEFT UPPER FILLET AREA, AS VIEWED WITH DOOR OPEN. REMOVED CORROSION FROM PNL 195ML'S SUPPORT STRUCTURE, LH UPR FILLET AREA LOST .037 FROM .080 MATERIAL IS FOUND TO BE OUT OF LIMITS. REPAIRED INAug 28, 2026 · N1373A · Boeing 76731K · Fuselage Structure (General)SDR ABXR082800014Stiffener · crackedSTA. 246 FLOORBEAM HAS CRACKED VERTICAL STIFFENER AT LBL 43 IN LEFT TUNNEL OF MEC .REPAIRED VERTICAL STIFFENER AT STA 246 FLOORBEAM LBL 43 IN LEFT TUNNEL OF MEC IAW B767-300 SRM 53-10-51 REPAIR 3 TABLE 1.Aug 28, 2026 · N1373A · Boeing 76731K · Fuselage Miscellaneous StructureSDR ABXR082800013Stiffener · crackedSTA. 246 FLOORBEAM HAS A CRACKED VERTICAL STIFFENER ON FWD SIDE AT LBL 28 IN LEFT TUNNEL OF MEC . REPAIRED VERTICAL STIFFENER ON FWD SIDE FLOORBEAM OF STA 246 LBL 28 IN LEFTTUNNEL OF MEC IAW B767-300 SRM 53-10-51 REPAIR 3 TABLE 1.Aug 28, 2026 · N1373A · Boeing 76731K · Fuselage Miscellaneous StructureSDR ABXA20260804347Module · defectiveAT APPROXIMATELY 300FT AGL THE FLIGHT CREW RECEIVED THE AURAL WARNING, TOO LOW, FLAPS. BOTH THE FO AND PILOT CONFIRMED FLAPS 25 WAS INDICATED. THE PILOT CALLED FOR A GO-AROUND ANYWAY AND THEY EXECUTED A MISSED APPROACH. THE SECOND APPROACH RESULTED IN A SAFEAug 4, 2026 · N1489A · Boeing 76731K · Trailing Edge Flap Control SystemSDR ABXA20260707310Escape Reel · expiredDURING INSP/MTC, NR 3 ESCAPE REEL FOUND OUT OF DATE. DEFERRED THE NR 3 ESCAPE REEL IAW MEL 25-61-1-1 C/W MAINTENANCE PROCEDURE 25-61-1 MBCB 07/17/26 PLACARDS INSTALLED. ACFT RETURNED TO SERVICE.Jul 7, 2026 · N1489A · Boeing 76731K · Emergency EquipmentSDR ABXA20260623277Extinguisher · unsecurePIN TO COCKPIT FIRE EXTINGUISHER NEAR LAV DISCOVERED ON FLOOR BY MTC. REATTACHED PIN TO FIRE EXTINGUISHER HANDLE USING BREAKAWAY WIRE. PLACARDS INSTALLED. ACFT RETURNED TO SERVICE.Jun 23, 2026 · N1489A · Boeing 76731K · Fire Bottle, PortableSDR ABXA20260622274Warning Message · illuminatedAFTER PUSHBACK, DURING TAXI, LT REV ISLN VALVE. RETURNED TO GATE (BTB). PLACED LEFT T/R ON DI PER MEL 78-31-1 MBCB 07/02/2026 PLACARD INSTALLED A/C DOWNGRADED TO CATIIIA. A/C RETURNED TO SERVICE.Jun 22, 2026 · N1489A · Boeing 76731K · Engine Thrust ReverserSDR ABXA20260619271Fire Loop · faultedLT ENG FIRE LP 1, STATUS MESSAGE IN FLIGHT ACFT LANDED NO PROBLEMS, MTX GROUNDED ACFT AND DEFERRED LP 1 LOOP IAW MEL ABX-26-11-1-1 AND RETURNED A/C TO SERVICE.Jun 19, 2026 · N1489A · Boeing 76731K · Smoke DetectionSDR ABXA20260616263Extinguisher · damagedDURING CREW PREFLIGHT, CREW SAID THE RT PORTABLE FIRE EXTINGUISHER BY LAV MOUNTED ON GROUND HAD A CROOKED PRESSURE GAUGE AND WAS WORRIED IT COULD RUPTURE IN FLIGHT OR ON USE. PORTABLE FIRE EXTINGUISHER R & R IAW AMM 26-26-02. ACFT RETURNED TO SERVICE.Jun 16, 2026 · N1489A · Boeing 76731K · Fire Bottle, PortableSDR ABXA20260427178Actuator · malfunctionedRUDDER RATIO EICAS MESSAGE ON TAXI OUT. REMOVED AND REPLACED RUDDER RATIO CHANGER ACTUATOR IAW B767 AMM 27-21-15 LEAK CHECK GOOD, OPS CHECK GOOD.RAN BOTH ENGINES @ IDLE, NO RUDDER RATIO MSG PRESENT. PERFORMED RUDDER RATIO OPS CHECK PER B767 AMM 27-21-00. NOApr 27, 2026 · N1489A · Boeing 76731K · Rudder Tab Control SystemSDR ABXA20260424172Eec · faultedDURING TAXI, ON ENGINE START BOTH EEC TO ALT W/ L & R ENG EEC MODE EICAS MESSAGES. CREW RETURNED TO THE GATES (BTB). MTC DEFERRED IAW MEL 73-21-1-3 NO MX ACTIONS REQUIRED. PLACARD INSTALLED. MBCB 05-04-2026. ALSO: ANOTHER ISSUE CAUSING THE (BTB), ON ENGIApr 24, 2026 · N1489A · Boeing 76731K · Fuel Controlling SystemSDR ABXA20260422170Pitot Tube · defectiveAFTER ENGINE START AND TAXI OUT, CAPT PITOT ANNUNCIATOR AND EICAS MESSAGE. CREW RETURNED TO BLOCKS (BTB). MAINTENANCE REMOVED AND REPLACED CAPT PITOT IAW B767 AMM 34-11-01 PITOT STATIC LEAK/OPS TEST GOOD AT THIS TIME NO EICAS MESSAGES PRESENT. AIRCRAFT REMAIApr 22, 2026 · N1489A · Boeing 76731K · Pitot/Static SystemSDR 2026F00020Skin · crackedEXTERIOR FUSELAGE SKIN ONLY IS CRACKED AT ONE FASTENER HOLE LOCATED L1 DOOR CUT OUT AFT CORNER STA 335 JUST ABOVE STR 20L(VERIFIED WITH HFEC).REPAIRED EXTERIOR FUSELAGE SKIN CRACK AT ONE FASTENER HOLE LOCATED L1 DOOR CUT OUT, AFT CORNER, STA 335 JUST ABOVE STRMar 3, 2026 · N1487A · Boeing 76731K · Fuselage Main, Plate/SkinSDR ABXA20260221074Relay · faultedL AUX PITOT EICAS MSG DURING TAXI OUT, AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX . REMOVED AND REPLACED L AUX PITOT IAW B767 AMM 34-11-01 OPS AND LEAK CHECK GOOD CHECK.ALSO ACCOMPLISH LOW RANGE LEAK CHECK ON THE L/H AUX PITOT PROBE IAW AMM 34-11-00.Feb 21, 2026 · N1489A · Boeing 76731K · Pitot/Static Anti-Ice SystemSDR ABXA20251122306Sensor · faultedRIGHT ENGINE CONTROL EICAS MESSAGE AFTER PUSHBACK FROM GATE AFTER ENGINE START, ACFT RETURNED TO GATE (BTB), AND MTX GROUNDED ACFT, MTX TROUBLESHOT & PERFORMED BIT PROCEDURE ON RH PIMU. FOUND SENSOR T25 FAULTING. R & R T25 CIT SENSOR ON RT ENGINE IAW FIM 7Nov 22, 2025 · N1489A · Boeing 76731K · Fuel Controlling SystemSDR ABXA20250419082Indicator · unreliableDURING CLIMB, AIRSPEED UNRELIABLE / STUCK AT 270 KTS INDICATION OF OVERSPEED WITH FLAPS & GEAR UP AT 270 KTS. EMERGENCY DECLARED, AIR TURN BACK. (ATB) . MAINTENANCE T/S - ALT VMO SWITCH SELECTED IAW CDL 32-12-1. AIRSPEED TAPE WILL SHOW 270 KTS. PERFORMED LANApr 19, 2025 · N1489A · Boeing 76731K · Airspeed/Mach IndicatorSDR UIEA2025031900344Fitting · corrodedHORIZONTAL STABILIZER PIVOT FITTING RH UPPER ATTACHMENTS, TWO HOLES WITH CORROSION. SEE NDT INSPECTION REPORT.(<P>TWO HOLES WITH CORROSION AT HORIZONTAL STABILIZER PIVOT FITTING RH UPPER ATTACHMENTS, WERE REPAIRED I.A.W. TRE6755081 ISSUED DATE 03MAR25 & CMA-TLMar 15, 2025 · N1373A · Boeing 76731K · Horizontal Stabilizer StructureSDR UIEA2025031900343Skin · puncturedPUNCTURE DAMAGE TO UPPER SPOILER SKIN 6, REPAIR AS REQUIRED.(<P>UPPER SPOILER SKIN 6 WAS REPAIRED I.A.W B767 SRM 57-70-01-2R-1 AND SRM 51-70-04-0G-0 PAR 5 B AND 51-70-17-0G-0 PAR 4 B FIG 24 REV 127 15DEC24. NO FURTHER DEFECTS NOTED.</P>)Mar 15, 2025 · N1373A · Boeing 76731K · SpoilersSDR UIEA2025031900342Support · corrodedLH WING INBOARD FLAP TRACK #3 SUPPORT AFT ATTACHMENT HOLES, BORE WITH CORROSION (4EA).(<P>LH WING INBOARD FLAP TRACK #3 SUPPORT AFT ATTACHMENT HOLES WERE REPAIRED I.A.W. TRE6757277 ISSUED DATE 04/ MAR/25 & CMA-TLS-25-0017. APPROVAL BY FAA FORM 8100-9 (2-02) ISMar 15, 2025 · N1373A · Boeing 76731K · Leading Edge DevicesSDR UIEA2025031900341Fitting · corrodedHORIZONTAL STABILIZER PIVOT FITTING RH LOWER ATTACHMENTS, HOLE WITH CORROSION. SEE NDT INSPECTION REPORT.(<P>HOLE WITH CORROSION AT HORIZONTAL STABILIZER PIVOT FITTING RH LOWER ATTACHMENTS WAS REPAIRED IAW TRE6755081 ISSUED DATE 03MAR25 FAA FORM 8100-9 (2-02) Mar 15, 2025 · N1373A · Boeing 76731K · Horizontal Stabilizer StructureSDR UIEA2025031900340Packing · leakingRH WING, PDU SLATS, HYDRAULIC MOTOR WITH EVIDENCE OF HYD LEAK.(<P>RH WING PDU HYD MOTOR PACKING WAS REPLACED AND LINES WERE TIGHTEN I.A.W AMM 27-81-11-424-029 REV. 144 22/DEC/24 TORQUE WAS APPLIED 170 LB/IN, 500 LB/IN AND 270 LB/IN, TORQUE DA TA S/N: 052412188Mar 15, 2025 · N1373A · Boeing 76731K · Hydraulic System, MainSDR UIEA2025031900339Bushing · corrodedHORIZONTAL STAB, RH PIVOT PIN, SLEEVE WITH CORROSION.(<P><SPAN>HORIZONTAL STAB RH PIVOT PIN SLEEVE WAS REPLACED </SPAN>WITH NR00439 IAW SRM 51-10-02-0G-0 REV 127 DATE 15 DEC 24. NO FURTHER DEFECTS NOTED.</P>)Mar 15, 2025 · N1373A · Boeing 76731K · Horizontal Stabilizer StructureSDR UIEA2025031900338Longeron · corrodedAFT CARGO COMPARTMENT, BTW STA 1065 AND 1087, STRG 23L AND 24L, LONGERON WITH CORROSION, L=4" W=1.580".(<P>AFT CARGO COMPARTMENT, BTW STA 1065 AND 1087, STRG 23L AND 24L, LONG ERON WITH CORROSION LEVEL 2 WAS REPLA CED IAW SRM 51-10-02-0G-0 PAR 9 REV 127 15 DECMar 15, 2025 · N1373A · Boeing 76731K · Fuselage Miscellaneous StructureSDR UIEA2025031900337Support · corrodedRIGHT WING TRAILING EDGE OUTBOARD FLAP SUPPORT #7, SUPPORT ACTUATOR HOLE WITH CRACK INDICATION AT 6 O´CLOCK APPROX.(<P>RIGHT WING TRAILING EDGE OUTBOARD FLAP SUPPORT #7, SUPPORT ACTUATOR HOLE WAS REPAIRED IAW TRE6757276 ISSUED DATE 21/FEB/25 & CMA-TLS-25-0006Mar 15, 2025 · N1373A · Boeing 76731K · Trailing Edge FlapsSDR UIEA2025031940336Support · corrodedRIGHT WING TRAILING EDGE OUTBOARD FLAP SUPPORT #8, SUPPORT ACTUATOR HOLE WITH CORROSION INDICATION.(<P>RIGHT WING TRAILING EDGE OUT BOARD FLAP SUPPORT #8, SUPPORT ACTUATOR HOLE WITH CORROSION LEVEL 2 WAS REPAIRED IAW TRE6757275 ISSUED DATE FEBRUARY 21, 2025. FMar 15, 2025 · N1373A · Boeing 76731K · Trailing Edge FlapsSDR UIEA2025031200280Skin · damagedDURING THE REMOVAL OF SLAT #6 FOR REPAIR (NR 00005), HIDDEN DAMAGE WAS FOUND ON LH WING FIXED LEADING EDGE AT RIB LES 351.10, WITH EXCESSIVE WEAR AND HOLE.(<P>ON LH WING FIXED LEADING EDGE AT RIB LES 351.10, DAMAGE WAS REPAIRED I. A.W. SRM 57-41-09-2R-2 FIGUREMar 15, 2025 · N1373A · Boeing 76731K · Leading Edge DevicesSDR UIEA2025031200279Case · corrodedENG 2, FAN CASE, AT 6' O CLOCK, UNDER STRUT AREA, BASE WITH CORROSION L=2.100" W=1"(<P>ENG 2, FAN CASE, AT 6' O CLOCK, UNDER STRUT AREA, BASE, CORROSION LEVEL 1 WAS REWORKED, EVALUATED, INSPECTED AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW AMM 72-33-00-206-001Mar 15, 2025 · N1373A · Boeing 76731K · Turbine Engine Air Inlet SectionSDR UIEA2025031200278Case · corrodedENG 1, AFT FAN CASE, AT 5 TO 6 O'CLOCK APROX, WITH SEVERAL POINTS OF CORROSION (3EA).(<P>ENG 1, AFT FAN CASE, AT 5 TO 6 O'CLOCK APROX, CORROSIONS LEVEL 1 WAS REWORKED, EVALUATED, INSPECTED AND FOUND TO BE WITHIN ALLOWABLE LIMITS. NO FURTHER DEFECTS NOTED.</P>)Mar 15, 2025 · N1373A · Boeing 76731K · Turbine Engine Air Inlet SectionSDR UIEA2025031900255Skin · dentedLH WING INBOARD TRAILING EDGE FLAP, LOWER AREA UPPER SKIN WITH SEVERAL DENTS.(<P>ONE DENT WAS REPAIRED IAW SRM 57-53-01-2R-1 PAG.1-7 FIG. 201 SHEET 4 AND SRM 51-70-10-2R-4 REPAIR 4</P> / <P>FIG.201 SHEET 1 PAG.1-22 AND THREE FOUND WITHIN LIMITS IAW B767 SRM 57Mar 15, 2025 · N1373A · Boeing 76731K · Trailing Edge FlapsSDR UIEA2025031900254Skin · puncturedRH OUTBOARD ELEVATOR, LOWER AND UPPER SKIN WITH A PUNCTURE BTW ELEV STA 200 AND 176, AT 2" FROM TRAILING EDGE.(<P>RH OUTBOARD ELEVATOR, LOWER AND UPPER SKIN WAS REPAIRED IAW SRM 55-20-01-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-04-0G-0 PAR.5.D FIG.6 PAG.17,3Mar 15, 2025 · N1373A · Boeing 76731K · Elevator, Plate/SkinSDR UIEA2025031900253Beam · corrodedAFT CARGO DOOR, BEAM INNER CHORD, BTW STA 1285 AND STA 1329 STRG 23 WITH CORROSION AROUND FASTENER HOLES (L= 1.250" W=1 ").(<P>REPAIRED IN ACCORDANCE WITH TRE6752056 (BOEING COMMUNICATION MESSAGE CMA-TLS-25-0012). NO FURTHER DEFECTS NOTED</P>)Mar 15, 2025 · N1373A · Boeing 76731K · Cargo/Baggage DoorsSDR UIEA2025031000252Skin · dentedLEFT WING, SLAT 6 INBOARD FACE WITH DENT APRX 10€Œ OF OUTBOARD EDGE.(<P>LEFT WING, SLAT 6 INBOARD FACE WITH DENT APRX 10€Œ OF OUTBOARD EDGE WAS REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 PAG.2-3 AND SRM 51-70-10-2R-4 REPAIR 4 FIG.202 SHEET 1 PAG.1,8,16. NO FURTHMar 15, 2025 · N1373A · Boeing 76731K · Leading Edge DevicesSDR UIEA2025031000251Support · corrodedRIGHT WING TRAILING EDGE INBOARD FLAP #5 SUPPORT MECHANISM 6-6 OUTER PIN WITH SEVERAL CORROSION IN THE INNER BORE.(<P>RIGHT WING TRAILING EDGE INBOARD FLAP #5 SUPPORT MECHANISM 6-6 OUTER PIN WAS REPLACED IAW AMM TASK 27-51-04-402-135 REV 144. NO FUTHER DEFECTSMar 15, 2025 · N1373A · Boeing 76731K · Wing Main, Frame StructureSDR UIEA2025031900250Skin · corrodedCORROSION ON THE UPPER SKIN OF THE HORIZONTAL STABILIZER CENTER SECTION, RH SIDE.(<P>THE UPPER SKIN OF THE HORIZONTAL STABILIZER CENTER SECTION, RH SIDE MWAS REWORKED, BLEND OUT AND INSPECTIONS PER MXA EO NO. TRE6755080 (BOEING COMMUNICATION MESSAGE CMA-TLS-25Mar 15, 2025 · N1373A · Boeing 76731K · Horizontal Stabilizer, Plate/SkinSDR UIEA2025031900247Skin · dentedSLAT #5, LEADING EDGE EXTERNAL SKIN, LOWER INBOARD EDGE WITH A DENT.(<P>SLAT #5, LEADING EDGE EXTERNAL SKIN, LOWER INBOARD EDGE DAMAGE WAS REPAIRED IAW. TRE6757274 ISSUED DATE 14FEB25 & CMA-TLS-25-0003 DATE 25FEB25. NO FURTHER DEFECTS NOTED</P>)Mar 15, 2025 · N1373A · Boeing 76731K · Leading Edge DevicesSDR UIEA2025031900246Skin · corrodedFUSELAGE SECTION 48, APU INTAKE DOOR CUTOUT, UPPER STRIP BROKEN AND WITH CORROSION.(<P>FUSELAGE SECTION 48, APU INTAKE DOOR CUTOUT, UPPER STRIP WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 127 15DEC24. NO FURTHER DEFECTS NOTED.</P>)Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Main, Plate/SkinSDR UIEA2025031900244Skin · damagedRH WING, FIXED LEADING EDGE, BETWEEN WS 538.2 AND WS 564.2 (SLAT # 9, INBOARD MAIN TRACK, CUT OUT) WITH EDGE BROKEN.(<P>RH WING, FIXED LEADING EDGE, BETWEEN WS 538.2 AND WS 564.2 WAS REPAIRED IAW B767 SRM 57-41-01-2R-1 AND SRM 51-70-08-0G-0 PAR 5 G FIG 14 REV Mar 15, 2025 · N1373A · Boeing 76731K · Wing, Plate/SkinSDR UIEA2025031900243Spacer · corrodedHORIZONTAL STABILIZER RH PIVOT PIN, OUTER SPACER WITH CORROSION.(<P>HORIZONTALSTABILIZER RH PIVOT PIN, OUTER SPACER WAS REPLACED I.A.W AMM 55-17-51-404-013 REV 144 22DEC24. NO FURTHER DEFECTS NOTED.</P>)Mar 15, 2025 · N1373A · Boeing 76731K · Horizontal Stabilizer StructureSDR UIEA2025031900241Stringer · brokenBULK CARGO COMPARTMENT, BTW STA 1480 AND STA 1502, STRINGER 30L BROKEN.(<P>BULK CARGO COMPARTMENT, BTW STA 1480 AND STA 1502, STRINGER 30L WAS REPAIRED IAW. TRE6753717 ISSUED DATE 21FEB25 FVCI EO #25037-1 REV. A. ISSUED DATE EO 20FEB25 FAA FORM 8110-3 ISSUED DMar 15, 2025 · N1373A · Boeing 76731K · Fuselage Main, Longeron/StringerSDR UIEA2025030800240Control Module · leakingHORIZONTAL STABILIZER WITH EVIDENCE OF HYDRAULIC LEAKAGE STAB TRIM CONTROL MODULE RH.(<P>LEAKAGE CHECK IN STAB TRIM CONTROL MODULE RH WAS PERFORMED IAW AMM 29-11-00-796-053 REV.144 DATE: 22DEC24. NO LEAK FOUND.</P>)Mar 15, 2025 · N1373A · Boeing 76731K · Flight Control SystemSDR UIEA2025031900237Door Frame · corrodedAFT CARGO COMPARTMENT, CUT OUT LOWER DOOR, BETWEEN STA 1263 AND STA 1285, FRAME WITH CORROSION, L=2", W=1.5".(<P>AFT CARGO COMPARTMENT, CUT OUT LOWER DOOR, BETWEEN STA 1263 AND STA 1285, FRAME CORROSION LEVEL 2 WAS REPAIRED IAW TRE 6753718 ISSIED DATE 21FEB25.Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Main, StructureSDR UIEA2025031900235Lens · brokenSWITCH "MAIN DECK CARGO", LENS BROKEN.(<P>MAIN DECK CARGO LIGHTS SWITCH LENS WAS REPLACED IAW AMM 33-34-00-900-801 REV 144 22DEC24 MAIN DECK CAR GO LIGHTS SWITCH, SATISFACTORY TEST IAW AMM 33-34-00-700-801 REV 144 22DEC24. NO FURTHER DEFECTS NOTED.</P>)Mar 15, 2025 · N1373A · Boeing 76731K · Flight Compartment LightingSDR UIEA2025031900234Skin · gougedENG 1, LH SIDE, SKIN ON AFT TORQUE BOX WITH A GOUGE.(<P>ENG 1, LH SIDE, SKIN ON AFT TORQUE BOX DAMAGE WAS REPAIRED IAW TRE6754205 ISSUED DATE 01MAR25. RDR NUMBER: CMA-TLS-25-0015-03B DATE 01MAR25. NO FURTHER DEFECTS</P>)Mar 15, 2025 · N1373A · Boeing 76731K · Nacelle/Pylon StructureSDR UIEA2025031980233Bracket · corrodedCORROSION ON PROXIMITY SENSORS BASE SUPPORT (S234, S235) AT FWD BULKHEAD OF NLG WHEEL WELL. (L= 1 IN, W= 2 IN).(<P>PROXIMITY SENSORS BASE SUPPORT (S234, S235) AT FWD BULKHEAD OF NLG WHEEL WELL, WAS REPLACED IAW SRM 51-10-02-OG-0 PARG 9 REV 127. NO FURTHER DEFEMar 15, 2025 · N1373A · Boeing 76731K · Fuselage Miscellaneous StructureSDR UIEA2025030800232Elec Connector · corrodedCORROSION ON UPPER CONNECTOR OF PROXIMITY SENSOR S234 AT FWD BULKHEAD OF NLG WHEEL WELL.(<P>CONNECTOR S234 WAS REPLACED IAW SWPM 20-61-00 REV 88, TEST SATISFACTORY, A/C GOOD FOR SERVICE.</P>)Mar 15, 2025 · N1373A · Boeing 76731K · Electrical Power System WiringSDR UIEA2025030800230Lamp · inoperativeREF DMI 225254 PARKING BRAKE LIGHT INOP, PARKING BRAKE LIGHTS, PARK BRAKE LIGHT 300 ANTISKID LIGHT VERIFIED OPERATIVE.(<P>PARK BRAKE LIGHT 300 ANTISKID LIGHT VERIFIED OPERATIVE. LAMPS WERE REPLACED IAW 32-44-08-712-016 REV 114 WITH A SATISFACTORY TEST. DMI 225Mar 15, 2025 · N1373A · Boeing 76731K · Landing Gear Brake SystemSDR UIEA2025031980228Skin · dentedLEFT WING, OUTBOARD SLAT #1 IN REAR SKIN WITH DENT.(<P>LEFT WING, SLAT 1 T/E WEDGE, LOWER SURFACE WAS REPAIRED IAW SRM 57- 43-02-2R-1 FIG.201 PAG.2-3 AND SRM 51-70-10-2R-4 REPAIR 4 FIG.201 SHEET 2 PAG.1,4,7 REV .127. NO FURTHER DEFECTS NOTED.</P>)Mar 15, 2025 · N1373A · Boeing 76731K · Leading Edge DevicesSDR UIEA2025031960223Support · crackedLEFT WING TRAILING EDGE INBOARD FLAP 4 SUPPORT MECHANISM 6-6 OUTER PIN WITH CRACK INDICATION.(<P>THE 6-6 OUTER PIN OF THE LH WING INB FLAP SUPPORT #4 WAS REPLACED IAW AMM 27-51-04-402-135 REV.144 DATE: 22DEC24 TORQUE WERE APPLIED 1000 LB/IN S/N: 0823114442 D/DMar 15, 2025 · N1373A · Boeing 76731K · Trailing Edge Flaps
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