Boeing 767-31K

Service difficulty reports · 1,002

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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 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 UIEA2025031900218Web · corrodedBULK CARGO COMPARTMENT, CUT OUT DOOR, BETWEEN STA 1480 AND STA 1502, INTERCOSTAL SKIN WITH CORROSION, L=2", W=1".(<P>BULK CARGO COMPARTMENT, CUT OUT DOOR, BETWEEN STA 1480 AND STA 1502, INTERCOSTAL SKIN WAS FABRICATED IAW. DWG / PL 146T5404 REV. E AND WAS INSTMar 15, 2025 · N1373A · Boeing 76731K · Fuselage Miscellaneous StructureSDR UIEA2025030190216Antenna · corrodedCORROSION ON BOTTOM TCAS ANTENNA.(<P>TCAS ANTENNA BOTTOM WAS REPLACED, ON P/N 071-50001-8102 S/N 582-34534, OFF P/N 071-50001-8102 S/N TLS33506. TEST SATISFACTORY. IAW. AMM 34-45-02-344-160 REV 144 DATE 22DEC24. TORQUE APPLIED 22.5 IN.LB S/N 924401137 DATE 30SMar 15, 2025 · N1373A · Boeing 76731K · Air Collision Avoidance SystemSDR UIEA2025030600215Bolt · corrodedENG 2, FAN CASE, OGVS BOLTS AREA, 113 BOLTS, BETWEEN 7 - 11 WITH CORROSION.(<P>ENG 2, FAN CASE, OGVS BOLTS AREA, 113 BOLTS, BETWEEN 7 - 11, CORROSION WAS EVALUATED, REMOVED, AND PERFORMED DVI, FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS IAW. AMM 72-33-00-206-00Mar 15, 2025 · N1373A · Boeing 76731K · Turbine Engine Air Inlet SectionSDR UIEA2025030190204Retainer · corrodedCORROSION ON FWD SEAL RETAINER AT FWD BULKHEAD AT NLG WHEEL WELL. (BELOW TO PROXIMITY SENSORS S234, S235) (L= 4 IN, W= 0.5 IN).(<P>FWD SEAL RETAINER AT FWD BULKHEAD AT NLG WHEEL WELL. (BELOW TO PROXIMITY SENSORS S234, S235), WAS REPLACED IAW. SRM 51-10-02-0G-0Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Miscellaneous StructureSDR UIEA2025030400203Retainer · corrodedCORROSION ON LH SEAL RETAINER AT FWD BULKHEAD AT NLG WHEEL WELL. (NEXT TO PROXIMITY SENSOR S256) (L= 4 IN, W= 0.5 IN).(<P>LH AT FWD BULKHEAD AT NLG WHEEL WELL SEAL RETAINER WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 127. NO FURTHER DEFECTS NOTED.Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Miscellaneous StructureSDR UIEA2025030194202Case · corrodedENG 1, FWD FAN CASE, AT 6 O'CLOCK APPROX, FWD MATING FLANGE WITH SEVERAL POINTS OF CORROSION (2EA).(<P>ENG 1, FWD FAN CASE, AT 6 O'CLOCK APPROX, FWD MATING FLANGE CORROSION LEVEL 1 WERE REWORKED, EVALUATED, INSPECTED AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAWMar 15, 2025 · N1373A · Boeing 76731K · Turbine Engine Air Inlet SectionSDR UIEA2025030194201Skin · crackedFWD ENTRY DOOR, AFT LOWER CORNER, CRACK INDICATION AT HOLE 3 ON SKIN AT APPROX 10 O´CLOCK. AND CRACK INDICATION AT HOLE 4, THROUGH THE HOLE (SKIN AND BEAR STRAP) APPROX. 10 O´CLOCK AND CROSS DOWN.(<P>FWD ENTRY DOOR, AFT LOWER CORNER, CRACK INDICATION AT HOLEMar 15, 2025 · N1373A · Boeing 76731K · Fuselage Main, Plate/SkinSDR UIEA2025030400200Wedge · dentedLEFT WING, SLAT 6 INBOARD FACE, TRAILING EDGE WEDGE WITH DENT APRX 42€Œ OF OUTBOARD EDGE.(<P>LEFT WING, SLAT 6 INBOARD FACE, T/E WEDGE AT APRX 42" 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. 201 SHEEMar 15, 2025 · N1373A · Boeing 76731K · Leading Edge DevicesSDR UIEA2025030400199Wedge · bentLEFT WING, SLAT 6 INBOARD FACE WITH BENT APRX 50€Œ OF INBOARD EDGE.(<P>LEFT WING, SLAT 6 T/E WEDGE INBOARD FACE AT APRX 50" OF INBOARD 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. 201 SHEET 2. NO FURTHER DEFECTSMar 15, 2025 · N1373A · Boeing 76731K · Leading Edge DevicesSDR UIEA2025030400198Skin · crackedFWD SERVICE DOOR, AFT LOWER CORNER, CRACK INDICATION AT HOLE 3 ON SKIN AT APPROX 2 O´CLOCK AND CRACK INDICATION AT HOLE 4, THROUGH THE HOLE (SKIN AND BEAR STRAP) APPROX. 2 O´CLOCK AND CROSS DOWN AND AT 4 O´CLOCK.(<P>CRACK AT HOLE 4 THROUGH THE HOLE APROX. 2Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Main, Plate/SkinSDR UIEA2025022500165Bracket · corrodedHORIZONTAL STABILIZER ENTER SECTION, UPPER SURFACE, LBL 41.5 AND BETWEEN REAR SPAR AND S-1, BRACKET WITH CORROSION.<BR>(<P>HORIZONTAL STABILIZER ENTER SECTION, UPPER SURFACE, LBL 41.5 AND BETWEEN REAR SPAR AND S-1, BRACKET WAS REPLACED IAW SRM 51-10-02-0G-0 PAMar 15, 2025 · N1373A · Boeing 76731K · Horizontal Stabilizer Miscellaneous StructureSDR UIEA2025022500164Frame · corrodedBULK CARGO COMPARTMENT, AT STA 1518, BTW STRG 28L AND 29L FRAME WITH CORROSION (L=2" W=1.5").(<P>BULK CARGO COMPARTMENT, AT STA 1518, BTW STRG 28L AND 29L FRAME, CORROSION LEVEL 1 WAS EVALUATED. REWORKED, AND INSPECTED, FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMIMar 15, 2025 · N1373A · Boeing 76731K · Fuselage Main, FrameSDR UIEA2025022500163Support · corrodedCORROSION ON LH ANGLE STRAP SUPPORT (NEXT TO PROXIMITY SENSOR S256 CONNECTOR BOX) AT LH MID SIDE AREA OF FWD BULKHEAD AT NLG WHEEL WELL. (L= 0.260 IN, W= 0.1 IN)(<P>CORROSION LEVEL 1 WAS REMOVED, EVALUATED, INSPECTED, AND FOUND TO BE IN ALLOWABLE DAMAGE LIMITSMar 15, 2025 · N1373A · Boeing 76731K · Fuselage Miscellaneous StructureSDR UIEA2025022500162Case · corrodedENG 2, FAN CASE AREA AT 6 O´CLOCK POSITION, AROUND THE ANCHORED NUT WITH CORROSION.(<P>ENG 2, FAN CASE AREA AT 6 O´CLOCK POSITION, AROUND THE ANCHORED NUT WAS REMOVED, CORROSION LEVEL 1 WAS REWORKED, INSPECTED, EVALUATED AND ALLOWABLE LIMITS FOUND IAW AMM 72Mar 15, 2025 · N1373A · Boeing 76731K · Turbine Engine Air Inlet SectionSDR UIEA2025022500161Fitting · corrodedCORROSION AT LH LOWER FITTING ON FWD BULKHEAD OF NLG WHEEL WELL. (L= 0.1 IN, W= 0.2 IN)(<P>CORROSION LEVEL 1 WERE REMOVED, EVALUATED, INSPECTED AND FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS AT LH LOWER FITTING ON FWD BULKHEAD OF NLG WHEEL WELL IAW SRM 53-10-0Mar 15, 2025 · N1373A · Boeing 76731K · Fuselage Miscellaneous StructureSDR UIEA2025022500160Frame · corrodedAFT CARGO COMPARTMENT, CUT OUT UPPER DOOR, BETWEEN STA 1263 AND STA 1285, BEHIND OF CARGO DOOR CONTROL PANEL, FRAME WITH CORROSION, L=1", W =0.560".(<P>AFT CARGO COMPARTMENT, CUT OUT UPPER DOOR, BETWEEN STA 1263 AND STA 1285, BEHIND OF CARGO DOOR CONTROL PANELMar 15, 2025 · N1373A · Boeing 76731K · Fuselage Main, FrameSDR UIEA2025022100158Hose · brokenSEVERAL HOSES OF SMOKE DETECTOR BROKEN ON CEILING OF MAIN DECK CARGO.(<P>HOSES OF SMOKE DETECTOR ON CEILING OF MAIN DECK CARGO WERE REPLACED IAW AMM 26-19-01-400-801. NO FURTHER DEFECTS NOTED.</P>)Mar 15, 2025 · N1373A · Boeing 76731K · Smoke DetectionSDR UIEA2025022000157Skin · corrodedUPPER LOBE INTERIOR STRUCTURE, ON BODY STA 1021, BETWEEN STR 19 AND 20 RH, A CORROSION L=0.5" W=0.5"(<P>UPPER LOBE INTERIOR STRUCTURE, ON BODY STA 1021, BETWEEN STR 19 AND 20 RH CORROSION LEVEL 1 WAS REWORKED, INSPECTED, EVALUATED AND WITHIN ALLOWABLE LIMITS IMar 15, 2025 · N1373A · Boeing 76731K · Fuselage Main, Plate/SkinSDR UIEA2025022000156Lamp · inoperativeFUSELAGE SEC 48, APU EXT BOTTLE ZONE, SERVICE LIGHT L79 INOP.(<P>SERVICE LIGHT (TAILCONE L179) WAS REPLACED AND TEST WAS PERFORMED SUCCESFULLY IAW AMM 33-31-00-962-001 REV 144 DATE 22DEC24. NO FURTHER DEFECTS NOTED.</P>)Mar 15, 2025 · N1373A · Boeing 76731K · Extinguishing SystemSDR UIEA2025022000155Bulb · inoperativeEMERGENCY LIGHT LH INOP(<P>EMERGENCY LIGHT LH (SUPERNUMERARY DOME) WAS REPLACED AND TEST WAS PERFORMED SUCCESSFULLY IAW AMM 33-22-02-960-801 REV 144 22DEC24. NO FURTHER DEFECTS NOTED.</P>)Mar 15, 2025 · N1373A · Boeing 76731K · Emergency LightingSDR UIEA2025031600351Proximity Sensor · looseLE SLAT ASYM EICAS MSG - EMERGENCY DECLARED(<P>T/S SLAT ASSYM MSG PER FIM 21-81 FT 809. PROX SENSOR 303 AT L/E SLAT 9' LOOSE SHIMMED, ADJUSTED AND SECURED PROX SENSOR 303 IAW AMM 27-88-01. PERFORMED OPS CHECK IAW 27-81-00, OPS CHK SATISFACTORY</P>)Mar 15, 2025 · N1373A · Boeing 76731K · Leading Edge Slat Position Indicating SystemSDR UIEA2025031500349Longeron · corrodedAFT CARGO COMPARTMENT, BTW STA 1065 AND 1087, STRG 23R AND 24R, LONGERON WITH CORROSION, L=5" W=1.500"(<P>AFT CARGO COMPARTMENT, BTW STA 1065 AND 1087, STRG 23R AND 24R, LONGERON WITH CORROSON LEVEL 2 WAS REPLACED IAW SRM 51-10-02-OG-O PAR 9 REV 127 15DEC24 ANMar 15, 2025 · N1373A · Boeing 76731K · Fuselage Main, StructureSDR UIEA2025031500348Flap Track · corrodedRH WING INBOARD FLAP TRACK #6 SUPPORT AFT ATTACHMENT HOLES, BORE WITH CORROSION (4EA).(<P>CORROSION ON RH WING INBOARD FLAP TRACK #6, AFT ATTACHMENT HOLES WAS REPAIRED I.A.W. TRE6757278 R1 ISSUED DATE 05/MAR/25. FAA FORM 8100-9 (2-02) ISSUED DATE 14/MAR/25. NOMar 15, 2025 · N1373A · Boeing 76731K · Trailing Edge FlapsSDR UIEA2025031500347Flap Track · corrodedLH WING INBOARD FLAP TRACK #3 SUPPORT FWD INBOARD ATTACHMENT HOLE, BORE WITH CORROSION (FLAP STRUCTURE).(<P>LH WING INBOARD FLAP TRACK #3 SUPPORT FWD INBOARD ATTACHMENT HOLES (FLAP STRUCTURE) WERE REPAIRED I.A.W. TRE6757280 ISSUED DATE 04MAR25 AND TRE6757279 RMar 15, 2025 · N1373A · Boeing 76731K · Trailing Edge FlapsSDR UIEA2025031500346Support · corrodedRH WING INBOARD FLAP TRACK #6 SUPPORT FWD ATTACHMENT HOLES, BORE WITH CORROSION (2EA).(<P>CORROSION ON RH WING INBOA RD FLAP TRACK #6 FWD ATTACHMENT HOLES, WAS REPAIRED I.A.W. TRE5757281 ISSUED DATE 05MAR25 & CMA-TLS-25-0018. FAA FORM 8100-9 (2-02) ISSUED DATEMar 15, 2025 · N1373A · Boeing 76731K · Trailing Edge FlapsSDR UIEA2025031500345Fitting · corrodedHORIZONTAL STABILIZER RH OUTBOARD PIVOT FITTING BORE WITH CORROSION.(<P>DAMAGE ON RH HORIZONTAL STABILIZER, OUTBOARD PIVOT FITTING BORE WAS REPAIRED I.A.W. TRE6753719 ISSUED DATE 05MAR25 & CMA-TLS-25-0013. FAA FORM 8100-9 (2-02) ISSUED DATE 14MAR25. LEVEL CORRMar 15, 2025 · N1373A · Boeing 76731K · Horizontal Stabilizer StructureSDR ABXA20250315057Starter · malfunctionedDURING TAXI WHILE STARTING #2 ENGINE THE ENGINE FAILED TO START, A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C. MTX TROUBLESHOT AND FOUND STARTER HAD FAILED INTERNALLY AND STARTVALVE WAS STICKING OPEN. MTX REMOVED AND REPLACED RH START VALVE IAW AMM 80-11-01Mar 15, 2025 · N1489A · Boeing 76731K · Engine StarterSDR ABXA20250214037Valve · malfunctionedDURING TAXI WHILE DEICING A/C L ENGINE ANTI-ICE EICAS 5PSI L ENGINE PACK ILLUMINATED ON EICAS, A/C THEN RETURED TO THE GATE AND MTX GROUNDED A/C, MTX THEN TROUBLESHOT PER FIM 36-20 FT 804 FOUND PRSOV VALVE STUCK CLOSED WITH ZERO PSI.REPLACED LH PRSOV PER AMMFeb 14, 2025 · N1489A · Boeing 76731K · Pneumatic Distribution SystemSDR ABXA20250131029Relay · malfunctionedDURING TAXI CREW REPORTED AFTER STARTING L&R ENG. EEC MODE AND PROBE HEAT EICAS MESSAGE DISPLAYED , A/C RETERNED TO THE GATE (BTB) AND MTX GROUNDED A/C , FOUND RELAY K528 AND RELAY SOCKET MELTED, REPLACED K528 RELAY SOCKET AND RETERMINATED ASSOCIATED WIRING IJan 31, 2025 · N1489A · Boeing 76731K · Pitot/Static Anti-Ice SystemSDR ABXA20250130027Proximity Switch · malfunctioned"ATC DECARED EMERGENCY CREW REPORTS LND GEAR MONITOR, NOSE A/G DISAGREE, AIR/GROUND DISAGREE STATUS MESSAGES DISPLAYED IN FLIGHT UPON LANDING NO AUTOBRAKES, NO GROUND SPOILERS, NO THRUST REVERSERS AVAILABLE ON TAXI IN MN CARGO DOOR, + L REV ISLN VAL STATUS MJan 30, 2025 · N1489A · Boeing 76731K · Landing Gear Position and WarningSDR ABXA20241214256Warning Message · false activationDURING TAXI, PARKING BRAKE EICAS MSG ILLUMINATED AND PARKING BRAKE ILLUMINATED AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX PERFORMED OPS CHECK OF THE PARKING BRAKE SYSTEM ,UNABLE TO DUPLICATE .OPS CHECK GOOD IAW AMM 32-44-00. AND RETURNED AC TO SERVICDec 14, 2024 · N1489A · Boeing 76731K · Landing Gear Brake SystemSDR ABXA20241204242Shutoff Valve · malfunctionedDURING DE-ICE BOTH L & R PACKS & L & R ENGINE BLEEDS OFF. L ENG BLEED DID NOT DISPLAY "OFF" NOR WAS A "L ENG BLEED OFF" EICAS MSG DISPLAYED .AC RETURNED TO THE GATE (BTB) AND MTX GROUNDED AC . TROUBLESHOT AND REMOVED AND REPLACED L/H ENG PRSOV IAW AMM 36-11-09Dec 4, 2024 · N1489A · Boeing 76731K · Pneumatic Distribution SystemSDR UIEA2024110801082Elt · inoperativePORTABLE ELT NEAR L1 DOOR INOP(<P>REMOVED AND REPLACED PORTABLE ELT IAW B767 AMM 25-63-03, OPS CHECK GOOD. THIS CLEARS DMI 220245, PLACARDS REMOVED.</P>)Nov 9, 2024 · N1373A · Boeing 76731K · Emergency Locator BeaconSDR ABXA2024118219Generator · warning lightLH GEN DRIVE LIGHT ON PUSHBACK FOLLOWED QRH PROCRDURES AC RETURNED TO THE GATE AND MTX GROUNDED AC , MTX DEFERRED GEN FOR DEPARTURE AND RETURNED AC TO SERVICE .Nov 8, 2024 · N1489A · Boeing 76731K · AC Generator-AlternatorSDR ABXA20241008185Unknown · odorCREW REPORTS THERE WAS A STRONG BURNT RUBBER SMELL IN COCKPIT ON DECENT AND AFTER LANDING. MTX GROUNDED AC AND PERFORMED AR CONDITIONING SYSTEM OIL SMOKE /FUME PRACTICE IAW B767 AMM 21-00-21 . NO ODER PRESENT / NO OIL CONTAMINATION NOTED .OPERATIONAL TEST OFOct 8, 2024 · N1489A · Boeing 76731K · Air Distribution SystemSDR UIEA2024093000964Firebane · leakingFIREBANE IN OVERHEAD COMPARTMENT LEAKING.(<P>R/R FIREBANE (OVERHEAD COMP) IAW EO 6725A212. VERIFIED EFFECTIVITY IAW EO 6725A212. NO FURTHER DEFECTS NOTED</P>)Sep 30, 2024 · N1373A · Boeing 76731K · Fire Bottle, PortableSDR ABXA20240925179Drive Assy · malfunctionedWXR RADAR FAIL MULTIPLE TIMES ON CLIMB OUT. WXR SYS STATUS MSG DISPLAYED. AC PERFORMED ATB AND LANDED MTX GOUNDED AC. REMOVED AND  REPLACED WXR DRIVE UNIT IAW B767 AMM 34-45-07. NO ADJUSTMENT REQ. DPS CHECK IAW B767 AMM 34-43-00. NO DEFECTS NOTED AT THIS TIMESep 25, 2024 · N1489A · Boeing 76731K · Weather Radar SystemSDR UIEA2024092000910Engine · no discrepancyBIRD STRIKE ON #1 ENG(<P>PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-18 & PERFORMED BIRD STRIKE CLEANING IAW AMM 12-25-04. NO DEFECTS AT THIS TIME.</P>)Sep 20, 2024 · N1373A · Boeing 76731K · Engine (Turbine/Turboprop)SDR ABXA202408275157Pressure Switch · malfunctionedON PUSH BACK C HYD PRES EICAS MSG AND CENTER HYD DISCRETE LIGHT ILLUMINATED AC RETURNED TO GATE AND MTX GROUNDED AC TROUBLE SHOT FOUND CENTER HYD PRESSURE SITCH FAULTY R/R CENTER HYD PRESS SWITCH S35 REF AMM 29-11-09. OPS CHECK LK CHECK OK. AND RETURNED AC TO Aug 25, 2024 · N1489A · Boeing 76731K · Hydraulic System, MainSDR UIEA2024071200646Control Module · leakingCREW REPORTED IN FLIGHT THAT HYDRAULIC QUANTITY FOR LEFT SYS DROPPED TO 0.49, AFTER CONTINUED LOSS, AIRCRAFT DIVERTED TO MIA FROM ITS ORIGINAL DESTINATION OF SJU. ALL FLUID FROM LH HYD DRAINED UPON LANDING(<P>DETERMINED LEFT STABILZER TRIM CONTROL MODULE LEAKJul 11, 2024 · N1373A · Boeing 76731K · Stabilizer Control SystemSDR UIEA2024052400435Cap · inoperativeEMER LIGHT UNARMED KORRY SWITCH INOP(<P>REMOVED AND REPLACED LED CAP MODULE ASSY FOR EMER LIGHT IAW AMM 33-13-00. OPS TEST GOOD.</P>)May 21, 2024 · N1373A · Boeing 76731K · Emergency LightingSDR UIEA2024052300415Flashlight · noneFLASHLIGHT AT L1 DOOR INDICATOR FLASHING(<P>PERFORMED TEST OF L1 DOOR FLASHLIGHT IAW AMM 25-64-02, OPS TEST GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME</P>)May 21, 2024 · N1373A · Boeing 76731K · Emergency EquipmentSDR UIEA2024071900692Module · faultedAIR TURN BACK FOR SPOILER ADVISORY MESSAGE. UPON ARRIVAL, PERFORMED MULTIPLE OPS TEST IAW AMM 27-61-00, COULD NOT DUPLICATE. PERF FIM 31-51 FT 809. R/R PCA TAKEOFF CONFIG WARNING MODULE (M620) IAW AMM 31-51-04, BIT ALL SCM'S WITH NO FAULTS PRESENT IN PREVIOUSMay 18, 2024 · N1487A · Boeing 76731K · Drag Control ActuatorSDR UIEA2024072000707Control Module · faultedSPOILER EICAS MESSAGE. PERFORMED FIM 27-09 FT 803 & FIM 27-09 FT 808, FOUND PCA FAULTING ON SCM #3 MSG. R & R #4 SPOILER PCA IAW AMM 27-61-02. DURING OPS CHECK FOUND #4 PCA STUTTERING WHILE DEPLOYING, SUSPECT BFS PCA. R & R #4 SPOILER PCA IAW AMM 27-61-02, NOMay 18, 2024 · N1487A · Boeing 76731K · Drag Control ActuatorSDR UIEA2024041900287Frame · corrodedCORROSION ON FRAME WEB AT STA 1562 BETWEEN STGR 38RH AND STGR 39RH(<P>CORROSION ON FRAME WEB WAS REPAIRED PER CMA-TLS 24-0135-03B. NO FURTHER DEFECTS NOTED.</P>)Apr 24, 2024 · N1489A · Boeing 76731K · Fuselage Main, FrameSDR UIEA2024041900288Skin · delaminatedLH HORIZONTAL STABILIZER, LH ELEVATOR, DELAMINATION ON THE OUTBOARD LOWER SKIN BETWEEN OF ELEV STA 325.109 AND ELEV STA 251.665(<P>DELAMINATION ON LH ELEVATOR LOWER SKIN BETWEEN ELEV STA 325.109 AND ELEV STA 251.665 WAS REPAIRED PER SRM 55-20-01-2R-1. NO FURTHApr 24, 2024 · N1489A · Boeing 76731K · Elevator, Plate/SkinSDR UIEA2024041900289Flap Track · damagedLEFT WING TRAILING EDGE OUTBOARD FLAP, TRACK #2 ON INBOARD STAP AFT LOWER HOLE ELONGATED.(<P>FLAP TRACK #2 FITTING ASSY 1-3 WITH ELONGATED HOLES (2 EA) WERE REPAIRED PER CMA-TLS 24-0138-11B. NO FURTHER DEFECTS NOTED.</P>)Apr 24, 2024 · N1489A · Boeing 76731K · Trailing Edge FlapsSDR UIEA2024041900290Skin · dentedFOUR DENTS ON RH WING, INB AFT FLAP UPPER SKIN AT: 1) IFS 114.5 AND 7" FROM T/E 2) IFS 119.5 AND 5.5" FROM T/E 3) IFS 121.75 AND 3" FROM T/E 4) IFS 122.5 AND 5.8" FROM T/E(<P>DENTS (ITEM 2,3 AND 4) ON RH WING, INB AFT FLAP UPPER SKIN WERE REPAIRED PER SRM 57-5Apr 24, 2024 · N1489A · Boeing 76731K · Trailing Edge FlapsSDR UIEA2024041900291Flap Track · corrodedRH WING INB FLAP, TRACK #6 ATTACHMENT BOLT HOLES WITH CORROSION.(<P> </P> / <P>CORROSION ON RH WING INB FLAP, TRACK #6 BOLT HOLES (2 EA) WERE REPAIRED PER CMA-TLS 24-0132-06B. NO FURTHER DEFECTS NOTED.</P> / <P> </P>)Apr 24, 2024 · N1489A · Boeing 76731K · Trailing Edge FlapsSDR UIEA2024042000299Support Beam · corrodedLH WING, MAIN LANDING GEAR SUPPORT BEAM, BUSHING OUTER RACE CAVITY, WITH CORROSION.(<P>CORROSION ON LH MLG SUPPORT BEAM AT HOLE FOR AFT TRUNNION BUSHINGS WAS REMOVED AND REPAIRED PER CMM 57-54-13. NO FURTHER DEFECTS NOTED.</P>)Apr 24, 2024 · N1489A · Boeing 76731K · Wing, Landing Gear Attach Fittings
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