# Service difficulty reports: N1409A

A list on [N1409A](https://openairdocs.org/aircraft/N1409A.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 10 · 458 reports

- [SDR ABXR2026031600004](https://openairdocs.org/sdr/ABXR2026031600004.md): Rib · cracked · Mar 16, 2026 · N1409A · Boeing 767306 · Wing, Rib/Bulkhead
  > CRACK ON L/E UPPER RIGHT WING AIRLOAD RIB
- [SDR ABXR2026031600003](https://openairdocs.org/sdr/ABXR2026031600003.md): Skin · cracked · Mar 16, 2026 · N1409A · Boeing 767306 · Fuselage Main, Plate/Skin
  > CRACK ON R-1 DOOR CUTOUT LOWER AFT CORNER
- [SDR 2026F00029](https://openairdocs.org/sdr/2026F00029.md): Skin · cracked · Mar 16, 2026 · N1409A · Boeing 767306 · Fuselage Main, Plate/Skin
  > CRACK ON LOWER CORNER OF L-1 DOOR CUTOUT
- [SDR 21GA20250709015](https://openairdocs.org/sdr/21GA20250709015.md): Target · out of position · Jul 9, 2025 · N1409A · Boeing 767306 · Leading Edge Devices
  > AFTER LIFT OFF RECEIVED LE SLAT ASSYMETRY MESSAGE. RETURNED TO THE FIELD.
- [SDR UIEA2024101801054](https://openairdocs.org/sdr/UIEA2024101801054.md): Skin · dented · Oct 21, 2024 · N1409A · Boeing 767306 · Trailing Edge Flaps
  > INBOARD TRAILING EDGE FLAP RH WING, UPPER SIDE INNER CORNER WITH DENTS(<P> RH WING INBOARD AFT FLAP DENT 1 WAS EVALUATED AND FOUN WITHIN ALLOWABLE LIMITS IAW SRM 57-53-01-1A-1 TABLE I NOTE C DETAIL IV DOT 89020 WAS INSTALLED AS PER ATLAS AIR GMM 3.19.1.</P> /
- [SDR UIEA2024102101057](https://openairdocs.org/sdr/UIEA2024102101057.md): Heater · inoperative · Oct 21, 2024 · N1409A · Boeing 767306 · Windshield/Door Rain/Ice Removal
  > RIGHT SIDE WINDOW HEAT INOP FLIGHT DECK WINDOW HEAT SYSTEM, #2 SIDE WINDOWS(<P>RIGHT SIDE WINDOW HEAT INOP FLIGHT DECK WINDOW HEAT SYSTEM, #2 SIDE WINDOWS WAS REPLACED, ADJUSTED AND OPERATIONAL CHECK WAS PERFORMED IAW AMM 56-11-02-004-001 REV. 143 DATE: 22 AUG
- [SDR UIEA2024102101058](https://openairdocs.org/sdr/UIEA2024102101058.md): Fitting · cracked · Oct 21, 2024 · N1409A · Boeing 767306 · Wing, Attach Fittings
  > LH WING, INTERNAL FIXED LEADING EDGE, NEAR LES 281.82 WITH CRACK IN TORQUE TUBE GUIDE(<P>TORQUE TUBE GUIDE FITTING ASSY WAS REPLACED IAW SRM 51-10-02-0G-0, NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024102101059](https://openairdocs.org/sdr/UIEA2024102101059.md): Skin · cracked · Oct 21, 2024 · N1409A · Boeing 767306 · Elevator, Plate/Skin
  > RH OUTBOARD ELEVATOR, LEADING EDGE AREA, BETWEEN ELEV STA188.221 AND ELEV STA 261.665 WITH CRACK(<P>RH OUTBOARD ELEVATOR WAS EVALUATED AND REPAIRED IAW SRM 55-20- 02-2R-1 FIG. 201 AND SRM 51-70-04-0G-0 PAR. 5A. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024102101060](https://openairdocs.org/sdr/UIEA2024102101060.md): Light · no discrepancy · Oct 21, 2024 · N1409A · Boeing 767306 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS INOP(<P>EXTERIOR EMERGENCY LIGHTS OPERATIONAL TEST WAS PERFORMED, TEST SATISFACTORY IAW AMM 33-51-00-715-001 REV 143 DATE 22-AUG-2024 </P>)
- [SDR UIEA2024102101061](https://openairdocs.org/sdr/UIEA2024102101061.md): Fire Seal · degraded · Oct 21, 2024 · N1409A · Boeing 767306 · Engine Thrust Reverser
  > ENGINE 2, LH THRUST REVERSER, IDG OIL SERVICE ACCESS DOOR, INNER AREA, DEGRADED FIRE SEAL.(<P>SEAL WAS REPAIRED IAW AMM 78-31-00-308-072-H00 REV 143 22-AUG-2024. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024080400788](https://openairdocs.org/sdr/UIEA2024080400788.md): Line · leaking · Aug 4, 2024 · N1409A · Boeing 767306 · Crew Oxygen System
  > CREW O2 PRESSURE 10PSI. FND 1ST OBS O2 BOX SUPPLY LINE LEAK. REPLACED LINE IAW AMM 35-00-00 & LEAK CHK OK. R/R CREW O2 BOTTLES IAW AMM 12-15-08 & LEAK CHECK GOOD. PART VERIFIED PER IPC 35-11-00 ITEM 1.
- [SDR UIEA2024051400390](https://openairdocs.org/sdr/UIEA2024051400390.md): Connector · faulted · May 14, 2024 · N1409A · Boeing 767306 · Auto Flight System Wiring
  > REJECTED TAKEOFF DUE TO NO AUTO THROTTLE AFT ENGAGING, EPR, AND V SPEEDS. DELETE TMC ANNC LIGHT(<P>REMOVED AND REPLACED CONNECTOR D4224P REF WDM 73-21-11. OPS CHECK GOOD AT THIS TIME.</P>)
- [SDR UIEA2023102800933](https://openairdocs.org/sdr/UIEA2023102800933.md): Unknown · unknown · Sep 28, 2023 · N1409A · Boeing 767306 · Extinguishing System
  > FIRE EXTINGUISHER UNDER SIDE PANEL CANNOT BE PROPERLY SECURED. CLASP WILL NOT STAY LATCHED(<P>ADJUSTED FIRE EXTINGUISHER CLASP IAW AMM B676 AMM 51-40-02. OPS CHECKS GOOD AT THIS TIME. VERIFIED PROPERLY CLOSED IAW AMM 25-60-00</P>)
- [SDR UIEA2023082900816](https://openairdocs.org/sdr/UIEA2023082900816.md): Unknown · unknown · Sep 1, 2023 · N1409A · Boeing 767306 · Engine Thrust Reverser
  > FAA AGING AIRCRAFT FINDINGS #1 T/R AFT FIRE BLANKET DAMAGED AFT SIDE(<P>ON #1 T/R AFT FIRE BLANKET AFT SIDE SEAL WAS APPLIED IAW AMM 78-31-00-308-072-H00 REV 139 22APR2023. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023082900817](https://openairdocs.org/sdr/UIEA2023082900817.md): Unknown · unknown · Sep 1, 2023 · N1409A · Boeing 767306 · Aircraft Fuel System
  > CENTER WING FRONT SPAR STA 785.9 AND LBL 97.95 FUEL LEAK(<P>CENTER WING FRONT SPAR STA 785.9 AND LBL 97.95 FUEL LEAK WAS REPAIRED AND THE TEST WAS SATISFACTORY PER AMM 28-11-00-308-013 REV 139 22APR-2023.</P>)
- [SDR UIEA2023082900818](https://openairdocs.org/sdr/UIEA2023082900818.md): Unknown · unknown · Sep 1, 2023 · N1409A · Boeing 767306 · Vertical Stabilizer
  > RH VERTICAL STABILIZER EXTERIOR BTW FSS 220.521 TO FSS 270.784 WITH DELAMINATIONS.(<P>RH VERTICAL STABILIZER EXTERIOR BTW FSS 220.521 TO FSS 270.784 WAS REPAIRED IAW SRM 55-30-01-2R-1 REP 1 NOTE F FIG 201 PAGE 2 AND SRM 51-70-10-2R-4 REP 4 FIG 201 PAGE 1. REV
- [SDR UIEA2023082900819](https://openairdocs.org/sdr/UIEA2023082900819.md): Unknown · unknown · Sep 1, 2023 · N1409A · Boeing 767306 · Vertical Stabilizer
  > LH VERTICAL STABILIZER EXTERIOR BTW FSS 220.521 TO FSS 270.784 WITH DELAMINATION.(<P>LH VERTICAL STABILIZER EXTERIOR BTW FSS 220.521 TO FSS 270.784 WAS REPAIRED IAW SRM 55-30-01-2R-1 REP 1 NOTE F FIG 201 PAGE 2 AND SRM 51-70-10-2R-4 REP 4 FIG 201 PAGE 1. REV 4
- [SDR UIEA2023082900820](https://openairdocs.org/sdr/UIEA2023082900820.md): Unknown · unknown · Sep 1, 2023 · N1409A · Boeing 767306 · Main Landing Gear
  > RH MAIN LANDING GEAR, AT AFT SIDE BRACE ON ATTACH WITH GOUGE.(<P>RH MAIN LANDING GEAR, AT AFT SIDE BRACE ON ATTACH GOUGE WAS REPAIRED IAW TRE6757208. APROV FAA FORM 8100-9, AUGUST 20, 2023</P> / <P> </P>)
- [SDR UIEA2023051700461](https://openairdocs.org/sdr/UIEA2023051700461.md): Module · unknown · May 17, 2023 · N1409A · Boeing 767306 · Central Warning
  > AFTER V1, FIRE BELL HORN SOUNDED WITH NO EICAS MSG OR LIGHTS. UNABLE TO CANCEL THE HORN. RETURNED TO CVG. LANDING WIEGHT 308000.(<P>R/R MODULE ASSY-WARNING ELEC IAW B767 AMM 31-51-04. OPS CKKS GOOD AT THIS TIME. NO DEFEATS NOTED.</P>)
- [SDR UIEA2022111701191](https://openairdocs.org/sdr/UIEA2022111701191.md): First Aid Kit · open · Nov 15, 2022 · N1409A · Boeing 767306 · Emergency Equipment
  > FIRST AID KIT SEAL BROKEN.(<P>REMOVED AND REPLACED FIRST AID KIT IAW B767 AMM 25-64-03.
- [SDR UIEA2022070500719](https://openairdocs.org/sdr/UIEA2022070500719.md): None · none · Jun 30, 2022 · N1409A · Boeing 767 · Landing Gear System
  > ON WALK AROUND AFTER LANDING FOUND R/H MAIN LANDING GEAR SHOCK STRUT DOOR MISSING.(<P>PERFORMED DVI IAW AMM 05-51-59/201. TRANSFRRED TO CDL 168008, CDL 32-12-01, DUE 12 NOV 22 T & I BM 0040Z, PLACARDS INSTALLED</P>)
- [SDR UIEA2022061900611](https://openairdocs.org/sdr/UIEA2022061900611.md): Seal · damaged · Jun 19, 2022 · N1409A · Boeing 767306 · Trailing Edge Flap Control System
  > R/W I/B AFT FLAP HAS DAMAGED SEAL AT O/B SIDE. REMOVED AND REPLACED DAMAGED SEAL AT RIGHT WING I/B AFT FLAP O/B SIDE AS PER 767-300 AMM 20-10-23-964-001</P>)
- [SDR UIEA2022061900612](https://openairdocs.org/sdr/UIEA2022061900612.md): Bonding Jumper · broken · Jun 19, 2022 · N1409A · Boeing 767306 · Pneumatic Distribution System
  > #2 ENG R/H SIDE HAS 1EA BROKEN BONDING WIRE ( LOCATED ABOVE FUEL FILTER) REMOVED & REPLACED #2 ENG R/H SIDE BONDING JUMPER TO THE HPSOV IAW B767 AMM 36-11-07</P>)
- [SDR UIEA2022061900613](https://openairdocs.org/sdr/UIEA2022061900613.md): Bolt · broken · Jun 19, 2022 · N1409A · Boeing 767306 · Nacelle/Pylon, Bulkhead/Firewall
  > BOLT IS BROKEN FOR CLAMP LOCATED ON #2 ENG R/H SIDE AFT OF HEAT EXCHANGER. INSTALLED BOLT AS PER B767-300 AMM 70-50-00. OPS CHECK GOOD</P>)
- [SDR UIEA2022061900614](https://openairdocs.org/sdr/UIEA2022061900614.md): Fastener · missing · Jun 19, 2022 · N1409A · Boeing 767306 · Fuselage, Powerplant Attach Fittings
  > #2 ENG AFT STRUT FAIRING MISSING 2EA FASTENERS ON R/H SIDE INSTALLED MISSING FASTENERS AT #2 ENGINE AFT STRUT FAIRING ON RH SIDE AS PER 767-300 SRM 51-40-02-0G-0</P>)
- [SDR UIEA2022061900615](https://openairdocs.org/sdr/UIEA2022061900615.md): Rub Strip · worn · Jun 19, 2022 · N1409A · Boeing 767306 · Engine Collector/Tailpipe/Nozzle
  > #1 ENGINE EXHAUST DUCT RUB PADS (ALL) LOOSE/WORN. REMOVED AND REPLACED WORN WEAR PADS AND SECURED LOOSE PADS AS PER 767-300 SRM 51-40-02-0G-0</P>)
- [SDR UIEA2022061900616](https://openairdocs.org/sdr/UIEA2022061900616.md): Door Track · lack of lube · Jun 19, 2022 · N1409A · Boeing 767306 · Passenger/Crew Doors
  > FWD ENTRY DOOR (L1) TRACK REQUIRES CLEANING & LUBRICATION. CLEANED & LUBRICATED FWD ENTRY DOOR (L1) TRACKS PER; B767-300 AMM 12-21-108. OPS CHECK GOOD</P>)
- [SDR UIEA2022061900617](https://openairdocs.org/sdr/UIEA2022061900617.md): Hose · frayed · Jun 19, 2022 · N1409A · Boeing 767306 · Crew Oxygen System
  > COCKPIT CAPT OXYGEN MASK HOSE FRAYED. REMOVED & REPLACED CAPT O2 MASK PER B767-300 AMM 35-11-51. OPS CHECK GOOD NO LEAKS</P>)
- [SDR UIEA2022061900618](https://openairdocs.org/sdr/UIEA2022061900618.md): Evas Unit · loose · Jun 19, 2022 · N1409A · Boeing 767306 · Emergency Equipment
  > COCKPIT CAPT EVAS TOP COVER LOOSE READJUSTED CAPT EVAS COVER PER B767-300 AMM 25-60-99
- [SDR UIEA2022061900619](https://openairdocs.org/sdr/UIEA2022061900619.md): Fastener · missing · Jun 19, 2022 · N1409A · Boeing 767306 · Engine Air Intake System
  > # 2 ENGINE INLET CASE CHAFING STRIP MISSING PLASTIC FASTENERS AT 5 AND 9 O'CLOCK POSITIONS. INSTALLED MISSING PLASTIC FASTENERS AT ENGINE INLET CASE CHAFING STRIP AS PER 767-300 SRM 51-40-02-0G-0
- [SDR UIEA2022020200083](https://openairdocs.org/sdr/UIEA2022020200083.md): None · none · Feb 4, 2022 · N1409A · Boeing 767306 · Fuselage Structure (General)
  > CRACK ON FWD UPPER CHORD AT STA 1809.5 BULKHEAD, STRINGER S-7LH.(<P ><SPAN>REPAIR WAS INSTALLED ON FWD UPPER CHORD AT STA 1809.5 AND STRINGERS S-6LH TO S-8LH PER 767 SRM 53-80-08 REPAIR 9</SPAN></P> / <P> </P>)
- [SDR UIEA2022020200084](https://openairdocs.org/sdr/UIEA2022020200084.md): None · none · Feb 4, 2022 · N1409A · Boeing 767306 · Wing Miscellaneous Structure
  > CORROSION ON THE UPPER SURFACE OF U-17 STRINGER OF RH WING SKIN PANEL 1 & 2 AND RIB 1 AND RIB 3(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM:.0001PT;"><SPAN>AFFECTED U-17 STRINGER SEGMENT WAS TRIMMED TO REMOVE ALL CORROSION.</SPAN></P> / <P STYLE="MARGIN: 0IN 0IN 0.0
- [SDR UIEA2022020200085](https://openairdocs.org/sdr/UIEA2022020200085.md): None · none · Feb 4, 2022 · N1409A · Boeing 767306 · Nacelle/Pylon Structure
  > CRACK ON LH STRUT OUTBD SKIN PANEL P/N 311T2450-23 BETWEEN NAC STA 221.25 / NAC STA 237.5 (CUTOUT FOR ACCESS PANEL 432AL)(<P ><SPAN>LH STRUT OUTBD SKIN PANEL P/N 311T2450-23 WAS REPAIRED PER BOEING SR 4-5340563504</SPAN></P> / <P> </P>)
- [SDR UIEA2022020200086](https://openairdocs.org/sdr/UIEA2022020200086.md): None · none · Feb 4, 2022 · N1409A · Boeing 767306 · Wing Miscellaneous Structure
  > CUT OUT ON UPPER CHORD, RIB #2 BETWEEN U-16 STRINGER TO U-18 STRINGER. THIS WAS REQUIRED TO GET ACCESS DURING U-17 STRINGER REMOVAL(<P ><SPAN>UPPER CHORD, RIB #2 BETWEEN U-16 STRINGER TO U-18 STRINGER WAS REPAIRED PER 767 SRM 57-20-09 REPAIR 1</SPAN></P> / <P>
- [SDR UIEA2022020200087](https://openairdocs.org/sdr/UIEA2022020200087.md): Splice · none · Feb 4, 2022 · N1409A · Boeing 767306 · Fuselage Structure (General)
  > CORROSION ON SPLICE TEE P/N 145T8629-2 OF KEEL BEAM FAIRING PANEL AT STA 887 APPROXIMATELY(<P ><SPAN>AFFECTED SPLICE TEE P/N 145T8629-2 WAS REPLACED PER 767 SRM 51-10-02-0G-0 PAR. 9 & 767 IPC 53-52-54-01 ITEM 25</SPAN></P> / <P> </P>)
- [SDR UIEA2021111202403](https://openairdocs.org/sdr/UIEA2021111202403.md): None · none · Nov 11, 2021 · N1409A · Boeing 767306 · Air Conditioning System
  > HI FLOW INHIBIT STATUS MSG(<P><SPAN>PERFORMED T/S PER FIM21-51 F/T 854, SYSTEM OPS CHECK NORMAL, MESSAGE CLEARED.</SPAN></P>)
- [SDR UIEA2021111202404](https://openairdocs.org/sdr/UIEA2021111202404.md): None · none · Nov 11, 2021 · N1409A · Boeing 767306 · Airborne Auxiliary Power Unit (APU) System
  > NO APU DUCT PRESS.(<P><SPAN>APU SHUTDOWN AND PERFORMED OPERATIONAL CYCLE CHECK IAW AMM 49-00-00 AND DUCT PRESSURE RESTORED.</SPAN></P>)
- [SDR UIEA2021102902303](https://openairdocs.org/sdr/UIEA2021102902303.md): None · none · Oct 29, 2021 · N1409A · Boeing 767306 · Fuel Boost Pump
  > RIGHT FWD FUEL PUMP EICAS ON DESCENT.(<P>PERF FIM 28-22 FT 819 AND RESET K10704 GFI RELAY, OPS CHECK NORMAL PER AMM 28-22-00, WIRING CHECK OK PER WDM 28-22-11.</P>)
- [SDR UIEA2021102502283](https://openairdocs.org/sdr/UIEA2021102502283.md): None · none · Oct 22, 2021 · N1409A · Boeing 767306 · Fuel Boost Pump
  > DURING BEFORE START FLOW EICAS MESSAGE L AFT FUEL PUMP DISPLAYED EVEN WITH L AFT FUEL PUMP SWITCH ON, NOTICED L AFT FUEL BOOST PUMP CB POPPED(<P>CYCLED CB IAW AMM 20-60-01. OPS CHECK GOOD IAW AMM 28-21-00. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2021102202272](https://openairdocs.org/sdr/UIEA2021102202272.md): Mask · none · Oct 21, 2021 · N1409A · Boeing 767306 · Oxygen System
  > F/O O2 MASK HARD TP BREATHE.(<P>REMOVED AND REPLACED O2 MASK IAW AMM 35-11-51 OPS CHECK GOOD.</P>)
- [SDR UIEA2021100202164](https://openairdocs.org/sdr/UIEA2021100202164.md): None · none · Oct 2, 2021 · N1409A · Boeing 767306 · Fuel Boost Pump
  > L AFT FUEL PUMP "PRESS" LIGHT NOT ILLUMINATED WITH SWITCH OFF.(<P>TURNED APU POWER OFF AND PERFORMED FUEL BOOST PUMP PRESSURE SWITCH TEST IAW AMM 28-42-01. NO DEFECT NOTED, PRESS LIGHT & ASSOCIATED EICAS MSG'S APPEAR AS REQ'. OK FOR SERVICE.</P>)
- [SDR UIEA2021090801987](https://openairdocs.org/sdr/UIEA2021090801987.md): Oxygen System · malfunctioned · Sep 7, 2021 · N1409A · Boeing 767306 · Crew Oxygen System
  > CREW O2 INDICATION INOP.(<P>TRANSFERRED TO MDDR 153132 IAW MEL 35-11-02-01, CAT B.</P> / <P>REMOVED AND REPLACED AVERAGING UNIT IAW AMM 35-11-06. THIS CLEARS MDDR 153132.</P>)
- [SDR UIEA2021080501712](https://openairdocs.org/sdr/UIEA2021080501712.md): Blade · nicked · Aug 5, 2021 · N1409A · Boeing 767306 · Turbine Engine Compressor Section
  > DURING #1 ENGINE FAN BLADE INSPECTION FOUND NICK ON LEADING EDGE TIP OF #36 FAN BLADE(<P>REPAIRED LEFT ENGINE #36 FAN BLADE TIP DAMAGE IAW AMM 72-31-02. FLUORESENT PENETRANT TEST REQUIRED BEFORE RETURN TO SERVICE. COMPLETED FPI INPSECT NBR 1 ENG FAN BLADE NBR
- [SDR UIEA2021071601576](https://openairdocs.org/sdr/UIEA2021071601576.md): Control Panel · failed · Jul 15, 2021 · N1409A · Boeing 767306 · Air Collision Avoidance System
  > TCAS/ ATC CONTROL PANEL FAILED, RELEASED SMOKE FROM DISPLAY. REF L/P 1390638/ M8 SMOKE OR FUMES IN THE CABIN, INSP. REQUIRED.(<P>REMOVED AND REPLACED TCAS/ATC CONTROL PANEL. OPS CHECK PASS. NO FAULTS AT THIS TIME IAW B767-300 AMM 34-53-02.</P> / <P>LP 1390638/
- [SDR UIEA2021070801494](https://openairdocs.org/sdr/UIEA2021070801494.md): Display · failed · Jul 8, 2021 · N1409A · Boeing 767306 · Directional Gyro and Indicating System
  > CAPTAINS ADI DISPLAY FLICKERED ON OFF. SMELL OF ELECTRIC BURNING. ALSO HEARD RELAY CLICKING NOISE. TURNED BRIGHTNESS DOWN, NO FURTHER PROBLEMS. PERFORMED SMOKE OR FUMES IN CABIN INSP. IAW AMM 05-51-56. NO SIGNS OF SMOKE OR OIL CONTAMINATION NOTED OPS NORMAL.
- [SDR UIEA2021070801489](https://openairdocs.org/sdr/UIEA2021070801489.md): Circuit Breaker · tripped · Jul 2, 2021 · N1409A · Boeing 767306 · Weather Radar System
  > PRIOR TO TAKE OFF WXRDR F23 AND F21 CIRCUIT BRAKERS POPPED. THUNDERSTORMS IN VICINITY AT DEPARTURE AIRPORT.(<P>PERFORMED OPS CK WXR RADAR PER AMM 34-43-00. OPS CHECK GOOD @ THIS TIME. NO DEFECTS NOTED.</P>)
- [SDR UIEA2021061601355](https://openairdocs.org/sdr/UIEA2021061601355.md): Battery · faulted · Jun 16, 2021 · N1409A · Boeing 767306 · Emergency Lighting
  > EMERGENCY LIGHTS ILLUMINATE AND CYCLE IN FLIGHT(<P>REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND CHARGER IAW B767 AMM 33-51-07. OPS CHECK GOOD AT THIS TIME.</P>)
- [SDR UIEA2021061401351](https://openairdocs.org/sdr/UIEA2021061401351.md): Bulb · inoperative · Jun 14, 2021 · N1409A · Boeing 767306 · Emergency Lighting
  > EXIT OVERHEAD & ENTRY LIGHTS BLINK INTERMITTENTLY AT LOWER ALTITUDES.(<P>ON CHECK FOUND EMERGENCY CEILING LIGHT BULB INOP. REMOVED AND REPLACED CELING EMERGENCY LIGHT BULB PER B767-300 AMM 33-51-11. OPS CHECK EMERGENCY LIGHTS PER B767-300 TASK 33-51-00-715-227
- [SDR UIEA2021061301341](https://openairdocs.org/sdr/UIEA2021061301341.md): Oxygen Mask · no test · Jun 13, 2021 · N1409A · Boeing 767306 · Crew Oxygen System
  > CAPTAIN 02 MASK HARNESS DOES NOT INFLATE DURING TEST(<P>REMOVED AND REPLACED CAPTAIN 02 MASK IAW AMM 35-11-51. OPS CHECK GOOD.</P>)
- [SDR UIEA2021060901302](https://openairdocs.org/sdr/UIEA2021060901302.md): Warning Message · false indication · Jun 9, 2021 · N1409A · Boeing 767306 · Central Warning
  > EICAS MSG "FWD EQPT VAL" PRIOR TO BLOCK OUT(<P>EQUIP COOL AUTO MODE DEFERRED IAW MEL 21-51-01-01, MDDR # 148275, CAT C, EXP 19 JUN 21.</P><P>LOG PAGE 1453746: PERFORMED SYSTEM OPERATIONAL CHECK IAW 21-58-00, NO DEFECTS NOTED. THIS CLEARS MDDR 148275.<BR /></P>

Next page: https://openairdocs.org/aircraft/N1409A/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 = 'N1409A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N1409A/reports

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