# Service difficulty reports: N1489A A list on [N1489A](https://openairdocs.org/aircraft/N1489A.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 6 · 293 reports - [SDR ABXA20260929441](https://openairdocs.org/sdr/ABXA20260929441.md): Switch · failed · Sep 29, 2026 · N1489A · Boeing 76731K · Emergency Lighting > EMER 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. - [SDR ABXA20260906396](https://openairdocs.org/sdr/ABXA20260906396.md): Warning Message · false activation · Sep 6, 2026 · N1489A · Boeing 76731K · Fire Detection > DURING 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. - [SDR ABXA20260804347](https://openairdocs.org/sdr/ABXA20260804347.md): Module · defective · Aug 4, 2026 · N1489A · Boeing 76731K · Trailing Edge Flap Control System > AT 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 SAFE - [SDR ABXA20260707310](https://openairdocs.org/sdr/ABXA20260707310.md): Escape Reel · expired · Jul 7, 2026 · N1489A · Boeing 76731K · Emergency Equipment > DURING INSP/MTC, NR 3 ESCAPE REEL FOUND OUT OF DATE.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. - [SDR ABXA20260623277](https://openairdocs.org/sdr/ABXA20260623277.md): Extinguisher · unsecure · Jun 23, 2026 · N1489A · Boeing 76731K · Fire Bottle, Portable > PIN 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. - [SDR ABXA20260622274](https://openairdocs.org/sdr/ABXA20260622274.md): Warning Message · illuminated · Jun 22, 2026 · N1489A · Boeing 76731K · Engine Thrust Reverser > AFTER 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. - [SDR ABXA20260619271](https://openairdocs.org/sdr/ABXA20260619271.md): Fire Loop · faulted · Jun 19, 2026 · N1489A · Boeing 76731K · Smoke Detection > LT 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. - [SDR ABXA20260616263](https://openairdocs.org/sdr/ABXA20260616263.md): Extinguisher · damaged · Jun 16, 2026 · N1489A · Boeing 76731K · Fire Bottle, Portable > DURING 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. - [SDR ABXA20260427178](https://openairdocs.org/sdr/ABXA20260427178.md): Actuator · malfunctioned · Apr 27, 2026 · N1489A · Boeing 76731K · Rudder Tab Control System > RUDDER 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. NO - [SDR ABXA20260424172](https://openairdocs.org/sdr/ABXA20260424172.md): Eec · faulted · Apr 24, 2026 · N1489A · Boeing 76731K · Fuel Controlling System > DURING 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 ENGI - [SDR ABXA20260422170](https://openairdocs.org/sdr/ABXA20260422170.md): Pitot Tube · defective · Apr 22, 2026 · N1489A · Boeing 76731K · Pitot/Static System > AFTER 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 REMAI - [SDR ABXA20260221074](https://openairdocs.org/sdr/ABXA20260221074.md): Relay · faulted · Feb 21, 2026 · N1489A · Boeing 76731K · Pitot/Static Anti-Ice System > L 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. - [SDR ABXA20251122306](https://openairdocs.org/sdr/ABXA20251122306.md): Sensor · faulted · Nov 22, 2025 · N1489A · Boeing 76731K · Fuel Controlling System > RIGHT 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 7 - [SDR ABXA20250419082](https://openairdocs.org/sdr/ABXA20250419082.md): Indicator · unreliable · Apr 19, 2025 · N1489A · Boeing 76731K · Airspeed/Mach Indicator > DURING 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 LAN - [SDR ABXA20250315057](https://openairdocs.org/sdr/ABXA20250315057.md): Starter · malfunctioned · Mar 15, 2025 · N1489A · Boeing 76731K · Engine Starter > DURING 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 80-11-01 - [SDR ABXA20250214037](https://openairdocs.org/sdr/ABXA20250214037.md): Valve · malfunctioned · Feb 14, 2025 · N1489A · Boeing 76731K · Pneumatic Distribution System > DURING 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 AMM - [SDR ABXA20250131029](https://openairdocs.org/sdr/ABXA20250131029.md): Relay · malfunctioned · Jan 31, 2025 · N1489A · Boeing 76731K · Pitot/Static Anti-Ice System > DURING 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 I - [SDR ABXA20250130027](https://openairdocs.org/sdr/ABXA20250130027.md): Proximity Switch · malfunctioned · Jan 30, 2025 · N1489A · Boeing 76731K · Landing Gear Position and Warning > "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 M - [SDR ABXA20241214256](https://openairdocs.org/sdr/ABXA20241214256.md): Warning Message · false activation · Dec 14, 2024 · N1489A · Boeing 76731K · Landing Gear Brake System > DURING 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 SERVIC - [SDR ABXA20241204242](https://openairdocs.org/sdr/ABXA20241204242.md): Shutoff Valve · malfunctioned · Dec 4, 2024 · N1489A · Boeing 76731K · Pneumatic Distribution System > DURING 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 36-11-09 - [SDR ABXA2024118219](https://openairdocs.org/sdr/ABXA2024118219.md): Generator · warning light · Nov 8, 2024 · N1489A · Boeing 76731K · AC Generator-Alternator > LH 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. - [SDR ABXA20241008185](https://openairdocs.org/sdr/ABXA20241008185.md): Unknown · odor · Oct 8, 2024 · N1489A · Boeing 76731K · Air Distribution System > CREW 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 OF - [SDR ABXA20240925179](https://openairdocs.org/sdr/ABXA20240925179.md): Drive Assy · malfunctioned · Sep 25, 2024 · N1489A · Boeing 76731K · Weather Radar System > WXR 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 TIME - [SDR ABXA202408275157](https://openairdocs.org/sdr/ABXA202408275157.md): Pressure Switch · malfunctioned · Aug 25, 2024 · N1489A · Boeing 76731K · Hydraulic System, Main > ON 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 - [SDR UIEA2024041900287](https://openairdocs.org/sdr/UIEA2024041900287.md): Frame · corroded · Apr 24, 2024 · N1489A · Boeing 76731K · Fuselage Main, Frame > CORROSION ON FRAME WEB AT STA 1562 BETWEEN STGR 38RH AND STGR 39RH(

CORROSION ON FRAME WEB WAS REPAIRED PER CMA-TLS 24-0135-03B. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024041900288](https://openairdocs.org/sdr/UIEA2024041900288.md): Skin · delaminated · Apr 24, 2024 · N1489A · Boeing 76731K · Elevator, Plate/Skin > LH HORIZONTAL STABILIZER, LH ELEVATOR, DELAMINATION ON THE OUTBOARD LOWER SKIN BETWEEN OF ELEV STA 325.109 AND ELEV STA 251.665(

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 FURTH - [SDR UIEA2024041900289](https://openairdocs.org/sdr/UIEA2024041900289.md): Flap Track · damaged · Apr 24, 2024 · N1489A · Boeing 76731K · Trailing Edge Flaps > LEFT WING TRAILING EDGE OUTBOARD FLAP, TRACK #2 ON INBOARD STAP AFT LOWER HOLE ELONGATED.(

FLAP TRACK #2 FITTING ASSY 1-3 WITH ELONGATED HOLES (2 EA) WERE REPAIRED PER CMA-TLS 24-0138-11B. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024041900290](https://openairdocs.org/sdr/UIEA2024041900290.md): Skin · dented · Apr 24, 2024 · N1489A · Boeing 76731K · Trailing Edge Flaps > FOUR 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(

DENTS (ITEM 2,3 AND 4) ON RH WING, INB AFT FLAP UPPER SKIN WERE REPAIRED PER SRM 57-5 - [SDR UIEA2024041900291](https://openairdocs.org/sdr/UIEA2024041900291.md): Flap Track · corroded · Apr 24, 2024 · N1489A · Boeing 76731K · Trailing Edge Flaps > RH WING INB FLAP, TRACK #6 ATTACHMENT BOLT HOLES WITH CORROSION.(

/

CORROSION ON RH WING INB FLAP, TRACK #6 BOLT HOLES (2 EA) WERE REPAIRED PER CMA-TLS 24-0132-06B. NO FURTHER DEFECTS NOTED.

/

) - [SDR UIEA2024042000299](https://openairdocs.org/sdr/UIEA2024042000299.md): Support Beam · corroded · Apr 24, 2024 · N1489A · Boeing 76731K · Wing, Landing Gear Attach Fittings > LH WING, MAIN LANDING GEAR SUPPORT BEAM, BUSHING OUTER RACE CAVITY, WITH CORROSION.(

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.

) - [SDR UIEA2024042000300](https://openairdocs.org/sdr/UIEA2024042000300.md): Support Beam · corroded · Apr 24, 2024 · N1489A · Boeing 76731K · Wing, Landing Gear Attach Fittings > RH WING, MAIN LANDING GEAR SUPPORT BEAM, BUSHING OUTER RACE CAVITY, WITH CORROSION.(

CORROSION ON RH MLG SUPPORT BEAM AT HOLE FOR AFT TRUNNION BUSHINGS WAS REMOVED AND REPAIRED PER CMM 57-54-13. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024042000301](https://openairdocs.org/sdr/UIEA2024042000301.md): Shear Web · corroded · Apr 24, 2024 · N1489A · Boeing 76731K · Fuselage Miscellaneous Structure > ELECTRONIC ELECTRIC COMPARTMENT, CORROSION ON THE BEAM AT STA 266.5, ON 40RBL(

SHEAR WEB WAS REPLACED PER DWG 141T5400. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024042900323](https://openairdocs.org/sdr/UIEA2024042900323.md): Panel · corroded · Apr 24, 2024 · N1489A · Boeing 76731K · Fuselage Main, Structure > AFT FUSELAGE, AFT CARGO HANDLING PANEL, CUTOUT AT RH UPPER CORNER, WITH CORROSION(

CORROSION ON SECTION 46 FUSELAGE BEAR STRAP AT CUT OUT WAS REPAIRED PER CMS-TLS 24-0150-03B. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024042900324](https://openairdocs.org/sdr/UIEA2024042900324.md): Torque Tube · corroded · Apr 24, 2024 · N1489A · Boeing 76731K · Trailing Edge Flaps > RH WING INB FLAP, INB RIB TORQUE TUBE SUPPORT UPPER ATTACHMENT BOLT HOLE WITH CORROSION.(

CORROSION ON RH WING INBOARD MAIN FLAP END RIB AT TORQUE TUBE SUPPORT HOLES (2 EA) WERE REPAIRED PER CMA-TLS 24-0152-02B. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024042900325](https://openairdocs.org/sdr/UIEA2024042900325.md): Panel · gouged · Apr 24, 2024 · N1489A · Boeing 76731K · Fuselage Main, Structure > FUSELAGE, FWD CARGO HANDLING PANEL, LH SIDE OF CUTOUT, WITH GOUGES.(

GOUGE ON SECTION 43 FUSELAGE BEARSTRAP AT THE CUTOUT BETWEEN STA 453/478 AND STGR 23 RH WAS REPAIRED PER CMA-TLS 24-0155-03B. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024042900326](https://openairdocs.org/sdr/UIEA2024042900326.md): Flap Track · damaged · Apr 24, 2024 · N1489A · Boeing 76731K · Trailing Edge Flaps > RIGHT WING TRAILING EDGE OUTBOARD FLAP, TRACK #8 ON INBOARD STRAP AFT LOWER HOLE ELONGATED.(

(3 EA) ELONGATED HOLES, HOLE WITH GOUGE AND HOLE WITH CORROSION ON RH WING FLAP TRACK #8 FITTING ASSY 1-3 WERE REPAIRED PER CMA-TLS 24-0137-11B. NO FURTHER DEFECTS N - [SDR UIEA2024042900327](https://openairdocs.org/sdr/UIEA2024042900327.md): Flap Track · damaged · Apr 24, 2024 · N1489A · Boeing 76731K · Trailing Edge Flaps > LEFT WING TRAILING EDGE OUTBOARD FLAP, TRACK #1 ON INBOARD STAP AFT LOWER HOLE ELONGATED(

TWO (2 EA) ELONGATED HOLES ON LH WING FLAP TRACK #1 FITTING ASSY 1-3 WERE REPAIRED PER CMS-TLS 24-0139-17B. NO FURTHER DEFECTS NOTED.

) - [SDR ABXA20241121229](https://openairdocs.org/sdr/ABXA20241121229.md): Apu · low pressure · Feb 21, 2024 · N1489A · Boeing 76731K · APU Bleed Air System > STARTED RIGHT ENGINE DURING TAXI. GOT 2 HUNG STARTS. N 2 MAX WAS 40. QRC DID NOT FIX IT(APU AIR DUCT PRESS LOW) AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC.AND DEFERRED APU AIR FOR DEPARTURE IAW ABX-49-11-1-1.AND RETURNED AC TO SERVICE. - [SDR UIEA2023080100767](https://openairdocs.org/sdr/UIEA2023080100767.md): Ecu · unknown · Jul 27, 2023 · N1489A · Boeing 76731K · Engine (Turbine/Turboprop) > ENGINE FAILURE ( ROLLBACK) RIGHT SIDE.(

PERFORMED TROUBLESHOOTING OF #2 ENGINE FLAMEOUT IAW B767 FIM 71-05 FT 841 TO BLOCK 4 ITEM 23 SHEET 2.

/

# 2 ENGINE REQUIRES REPLACEMENT OF WIRING FOR R/H RVDT FROM EEC TO RVDT. R/R WIRING FROM R/H RVDT TO EEC ON - [SDR UIEA2023072700762](https://openairdocs.org/sdr/UIEA2023072700762.md): Ecu · unknown · Jun 27, 2023 · N1489A · Boeing 76731K · Engine (Turbine/Turboprop) > ENGINE FAILURE (ROLL BACK) RIGHT SIDE (IFSD)(

PERFORMED T/S OF #2 ENG FLAEMOUT IAW FIM 71-05 FT 841 TO BLOCK 4 ITEM 23 SHEET 2. #2 ENGINE REQ REPLACEMENT OF WIRING FOR RH RVDT FROM EEC TO RVDT. R/R WIRING FROM RH RVDT TO EEC ON #2 ENG T/R IAW SWPM, OPS CHECK - [SDR UIEA2023050900436](https://openairdocs.org/sdr/UIEA2023050900436.md): Unknown · unknown · May 8, 2023 · N1489A · Boeing 76731K · Nacelle/Pylon, Main Frame > NACELLE STRUT # 1 AFT FAIRING LOWER PANEL HAS ONE SCREW MISSING AT O/B SIDE.(

INSTALLED MISSING SCREW AT NACELLE STRUT #1 AFT FAIRING O/B SIDE IAW B767 SRM 51-40-02. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2023050900437](https://openairdocs.org/sdr/UIEA2023050900437.md): Unknown · unknown · May 8, 2023 · N1489A · Boeing 76731K · Nacelle/Pylon Structure > LEFT NACELLE STRUT # 1 AFT FAIRING O/B FWD INSPECTION PANEL HAS ONE SCREW LOOSE.(

SECURED SCREW AT L/H NACELLE STRUT #1 AFT FAIRING IAW B767 SRM 51-40-02. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2023050900438](https://openairdocs.org/sdr/UIEA2023050900438.md): Seal · unknown · May 8, 2023 · N1489A · Boeing 76731K · Spoilers > LEFT WING O/B FLAP INBOARD EDGE HAS THE UPPER SEAL DAMAGED AT AFT END.(

REMOVED DAMAGED SEAL, CLEANED RETAINER LOCATED AND INSTALLED NEW SEAL AT L/H WING O/B FLAP I/B EDGE PER B767-300 AMM 20-10-23-963-001. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2023050900439](https://openairdocs.org/sdr/UIEA2023050900439.md): Elt · unknown · May 8, 2023 · N1489A · Boeing 76731K · Communications System > SUPERNUMERARY PORTABLE ELT AUTOMATIC RELEASE SEAL DAMAGE. P/N 1151324-1 S/N 1151324-05962 06 NOV 23(

REMOVED AND INSTALLED PORTABLE ELT AT SUPERNUMERARY POSITION AS PER B767-300F AMM 25-60-10. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2023050900440](https://openairdocs.org/sdr/UIEA2023050900440.md): Snubber · unknown · May 8, 2023 · N1489A · Boeing 76731K · Landing Gear System > NLG WHEEL WELL SNUBBERS BRAKE PADS WORN OUT.(

REMOVED WORN OUT SNUBBERS PADS LOCATED DRILLED AND INSTALLED NEW SNUBBERS PADS AT NOSE LANDING GEAR WHEEL WELL PER B767-300 AMM 32-45-05-022-001 & AMM 32-45-05-422-007. NO FURTHER DEFECTS N - [SDR UIEA2023050900441](https://openairdocs.org/sdr/UIEA2023050900441.md): Unknown · unknown · May 8, 2023 · N1489A · Boeing 76731K · Oxygen System > FWD E& E CREW OXYGEN NEED SERVICE TO FULL.(

SERVICED CREW OXYGEN CYLINDER @ LOWER E&E COMPARTMENT IAW 767-300 AMM 12-15-08, AMM 35-00-00, AMM 35-11-00 & AC. 43.13-1B PAR 9-46 THRU 9-51. NO LEAKS NOTED DURING NORMAL OPERATIONAL CHECK

) - [SDR UIEA2023050900442](https://openairdocs.org/sdr/UIEA2023050900442.md): Unknown · unknown · May 8, 2023 · N1489A · Boeing 76731K · Airborne Auxiliary Power Unit (APU) System > #2 ENG PNEU DUCT SUPPORT ROD BOLT MISSING 12 O'CLOCK POS FWD OF PRV.(

INSTALLED BOLT #2 ENG PNEU DUCT AT 12 O'CLOCK POS FWD OF PRV PER AMM 20-11-0

) - [SDR UIEA2023050900443](https://openairdocs.org/sdr/UIEA2023050900443.md): Surge Valve · unknown · May 8, 2023 · N1489A · Boeing 76731K · Airborne Auxiliary Power Unit (APU) System > APU SURGE VALVE PNEUMATIC DUCT ASSY RUBBER COUPLING IS DAMAGED(

REMOVED AND REPLACED APU SURGE VALVE PNEUMATIC DUCT ASSY PER AMM 44-53-01-404-010. LEAK CHECK OK

) - [SDR UIEA2023050900435](https://openairdocs.org/sdr/UIEA2023050900435.md): Latch · unknown · May 8, 2023 · N1489A · Boeing 76731K · Nacelle/Pylon, Main Frame > NACELLE STRUT #1 ACCESS DOOR AFT LATCH IS NOT PROPERLY SEATED(

REMOVED AND REPLACED 4EA LATCHES AT #1 ENG NACELLE STRUT ACCESS DOORS IAW B767 SRM 51-40-02. OPS CHECK GOOD.

) - [SDR UIEA2022120601205](https://openairdocs.org/sdr/UIEA2022120601205.md): Proximity Switch · faulted · Dec 6, 2022 · N1489A · Boeing 76731K · Leading Edge Slat Control System > LE FLAP ASSYMETRY EICAS MASSAGE WAS LE SLAT ASYM NOT FLAP. C/W FIM PROCEDURE 27-90-14 AND FOUND CODE 284 ON PSEU. REMOVED AND REPLACED LT INBD PROX SWITCH 284 IAW AMM 27-88-01, OPS CHECKED GOOD. Next page: https://openairdocs.org/aircraft/N1489A/reports.md?page=2 ## 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 = 'N1489A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N1489A/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.