# Service difficulty reports: N671UA

A list on [N671UA](https://openairdocs.org/aircraft/N671UA.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 8 · 382 reports

- [SDR CALA2026101920459](https://openairdocs.org/sdr/CALA2026101920459.md): Panel · missing · Oct 14, 2026 · N671UA · Boeing 767322 · Wing Main, Frame Structure
  > ON ARRIVAL, FOUND LT WING PANEL NR 551VB JUST ABOVE LANDING GEAR DOOR HAS DEPARTED FROM ACFT. TOTAL PANEL LENGTH 103IN, MISSING 65 IN, PANEL WIDITH 10IN.ACCOMPLISHED GVI TO TRUNNION NO EVIDANCE OF DAMAGED NOTED, A SLIGHT DAMAGE NOTED ON TRUNNION DOOR AFT TOP C
- [SDR CALA2026100920255](https://openairdocs.org/sdr/CALA2026100920255.md): Wire · broken · Oct 6, 2026 · N671UA · Boeing 767322 · Light System Wiring
  > EMERGENCY FLOOR PATH PROXIMITY LIGHTING ON ROWS 35 FED TO 39 FED FOUND INOP. HARNESS 4NS103-1 FOUND WITH BROKEN WIRE AT SEAT 35 FED. HARNESS REPLACED AS PER WDM 33-51-15-1C, SWPM 20-10-11. EMERGENCY LIGHT FUNCTION TEST CARRIED OUT SATIS IAW AMM 33-51-00-715-
- [SDR CALA2026091519424](https://openairdocs.org/sdr/CALA2026091519424.md): Tat Probe · faulted · Sep 13, 2026 · N671UA · Boeing 767322 · Outside Air Temperature Indicator/Sensor
  > LOSS OF ALL TAT DATA CLIMBING THROUGH 330 LOSS OF AP/AT LNAV/VNA V TCAS/WINDSHEAR TROUBLESHOT IAW SSM 34-12-01-103. FOUND TAT PROBE TS161L AT FAULT. R & R TAT PROBE IAW AMM 34-12-02-401. PERFORMED TAT PROBE TEST IAW AMM 34-12-02-404-008. PROBE TESTED GOOD. OTH
- [SDR CALA2026081018423](https://openairdocs.org/sdr/CALA2026081018423.md): Light · detached · Aug 9, 2026 · N671UA · Boeing 767322 · Emergency Lighting
  > SEAT 41F FLOOR EMERGENCY LIGHT ASSY FOUND DETACHED FROM SEAT. EMERGENCY LIGHT ASSY REPLACED. CHECKED OPS. ALL NORMAL. WRT AMM 33-51-10-972-104.
- [SDR CALA2026071517790](https://openairdocs.org/sdr/CALA2026071517790.md): Fan · faulted · Jul 9, 2026 · N671UA · Boeing 767322 · Air Distribution Fan
  > STRONG ELEC BURNING ODOR, FOLLOWED BY LT RECIRC FAN CAS MESSAGE ODOR, ODOR DISAPATED WITH FAN OFF. DEBRIEF WITH CREW, NO SMOKE JUST ODOR WHEN EICAS MESSAGE CAME ON AND LT RECIRC FAN OFF,ODOR THEN DISSIPATED NO EVIDENCE OR SMOKE OR ODOR DURING THE REST OF T
- [SDR CALA2026042015516](https://openairdocs.org/sdr/CALA2026042015516.md): Light · detached · Apr 19, 2026 · N671UA · Boeing 767322 · Emergency Lighting
  > 32D SEAT FLOOR PATH LIGHT FITTING ASSY DETACHED FROM SEAT. REPLACED EMERGENCY LIGHT FITTING AT 32D IAW AMM TASK 33-51-10-962-104. LIGHT OPERATION CHKD NORMAL.
- [SDR CALA2026030314232](https://openairdocs.org/sdr/CALA2026030314232.md): Structure · cracked · Feb 28, 2026 · N671UA · Boeing 767322 · Nacelle/Pylon, Main Frame
  > LEFT ENGINE NACELLE, FWD TORQUE BOX UPPER SURFACE, AROUND DRAIN HOLE FOUND TWO CRACKS. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5450-03104, PART 1, STEP 1 WITHOUT DEVIATION.
- [SDR CALA2026030314230](https://openairdocs.org/sdr/CALA2026030314230.md): Structure · cracked · Feb 28, 2026 · N671UA · Boeing 767322 · Nacelle/Pylon, Main Frame
  > NR 2 ENGINE NACELLE, FWD TORQUE BOX UPPER SURFACE INBD SIDE, AROUND DRAIN HOLE FOUND TWO CRACKS, & OTBD SIDE ARROUND DRAIN HOLE FOUND TWO CRACKS. INTERIM REPAIR WAS ACCOMPLISHED IAW ECRA 5450-03106, PART 1, STEP 1, WITHOUT DEVIATION.
- [SDR CALA2025101410039](https://openairdocs.org/sdr/CALA2025101410039.md): Slide · no discrepancy · Oct 10, 2025 · N671UA · Boeing 767322 · Escape Slide
  > INSTALED THE SAFETY PINS INTO THE SAFETY HOLES OF THE LEFT AND RIGHT INFLATION CYLINDER REGULATORS REF.AMM 25-65-00-042-001. REMOVED THE SAFETY PINS FROM THE SAFETY HOLES OF THE LEFT AND RIGHT INFLATION CYLINDER REGULATORS REF AMM 25-65-00-442-010. VERIFIED RE
- [SDR CALA2025082608139](https://openairdocs.org/sdr/CALA2025082608139.md): Fan · failed · Aug 24, 2025 · N671UA · Boeing 767322 · Air Distribution Fan
  > SMOKE/FUMES SMELLED ON FLIGHT DECK AND IN FORWARD GALLEY.FWD EQ EXH FAN STATUS MESSAGE. CREW AND FA'S AT FORWARD GALLEY SMELL ELECTRICAL ACRID SMELL ON AND OFF WITH AN ASSOCIATED VIBRATION AT RIGHT FORWARD GALLEY FLOOR. PERFORMED CONDITIONAL INSPECTION PER
- [SDR CALA2025072907028](https://openairdocs.org/sdr/CALA2025072907028.md): Shade · torn · Jul 20, 2025 · N671UA · Boeing 767322 · Passenger Compartment Equipment
  > 20L WINDOW SHADE ON EMER DOOR IS TORN WINDOW SHADE REMOVED FROM EMERGENCY EXIT ROW 20L. PLACED ON MEL WINDOW SHADE REMOVED FROM EMERGENCY EXIT ROW 20L. REMOVED. DEFERRED REF 2520LY PACED ON MEL R&R WINDOW SHADE REF AMM 25-21-00
- [SDR CALA2025052204903](https://openairdocs.org/sdr/CALA2025052204903.md): Tube · corroded · May 20, 2025 · N671UA · Boeing 767322 · Extinguishing System
  > DURING ENGINE INSPECTION FOUND R ENG FIRE EXTINGUISHING TUBE BROKEN. IPC REF 26-21-55-02, ITEM 65. RT ENG FIRE EXTINGUISHING TUBE REMOVED AND REPLACED IAW AIPC: 26-21-55-02 AND AMM: 20-10-09.
- [SDR CALA2025040303463](https://openairdocs.org/sdr/CALA2025040303463.md): Unknown · unknown · Apr 1, 2025 · N671UA · Boeing 767322 · Standard Practices/Structures
  > AT THE CONCLUSION OF ALL WORK ON APU AND AIR CONDITIONING SYSTEM ACTIVATE THE BLEED ON #2 ENGINE AND PERFORM NORMAL ENGINE START USING APU FOR BOTH ENGINES. RUN ENGINES SEPARATELY AT POWER LEV ELS SIMILAR TO TEST 8 PER AMM 71-00-00-725-008-N00 FOR 5 MINUTES WI
- [SDR CALA2025040303462](https://openairdocs.org/sdr/CALA2025040303462.md): Unknown · odor · Mar 29, 2025 · N671UA · Boeing 767322 · Air Distribution System
  > REF L/P 4310473 - FA REPORTED SMELL OF SMOKE AFTER DEPARTURE FOR SHORT PERIOD AND AGAIN AT GEAR DOWN. CONDITIONAL INSPECTION AMM TASK 05-51-56-940-801-C1
- [SDR CALA2025020502204](https://openairdocs.org/sdr/CALA2025020502204.md): Battery Pack · no test · Feb 5, 2025 · N671UA · Boeing 767322 · Emergency Equipment
  > EMERGENCY FLASHLIGHT BATTERY INSPECT {B767-25-3-0189} - DOOR 2 LH FWD FACING & CTR AFT FACING FLT CREWSEAT EMERG FLASHLIGHT BATTERY EXPIRED BATTERY REPLACED, IAW AMM 25-60-00-210-801-C1. PARTS USED: 78-2525-3-0058, QTY:1
- [SDR CALA2024111802883](https://openairdocs.org/sdr/CALA2024111802883.md): Probe · faulted · Nov 15, 2024 · N671UA · Boeing 767322 · Fuel Quantity Indicator
  > RT FUEL QTY BLANK TOTALIZER BLANK LOCKED FOR POSITIVE FIX UNLOCKED FOR FUEL WORK ASSIGNMENT WORK ORDER 3122454 CREATED FOR TANK TIGERS MECHANICS. UNLOCKED TO CLEAR CYCLED CBS ON FIM 28-41 TASK 803 FUEL QTY AND TOTALIZER DISPLAY UPDATED MAA CODE FIX USING VENDO
- [SDR CALA2024111501159](https://openairdocs.org/sdr/CALA2024111501159.md): Totalizer · malfunctioned · Nov 14, 2024 · N671UA · Boeing 767322 · Fuel Quantity Indicator
  > RIGHT FUEL QTY AND FUEL TOTALIZER BLANK PERFORMED FQIS OPERATIONAL TEST PER AMM 28-41-00-715-001-002. FQIS SELF TEST PASSED. R/H FUEL QTY AND FUEL TOTALLIZER BACK TO NORMAL CONFIGURATION.
- [SDR CALA2024110400983](https://openairdocs.org/sdr/CALA2024110400983.md): Contact · dirty · Nov 3, 2024 · N671UA · Boeing 767322 · Light System Wiring
  > EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - EXTERNAL EMERGENCY LIGHTS 3 EACH LH AFT FUSELAGE INOP. RELAMPED AND OPS CHECKED 3 EACH LH AFT FUSELAGE EXTERNAL SLIDE EMERGENCY LIGHTS, ALL GOOD AS PER AMM TASK 33-51-06-902-082.PARTS USED: 99-3351-3-0014,
- [SDR CALA2024110400982](https://openairdocs.org/sdr/CALA2024110400982.md): Contact · dirty · Nov 3, 2024 · N671UA · Boeing 767322 · Light System Wiring
  > EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - EXTERNAL EMERGENCY LIGHT 1 EACH INOP AT RH AFT FUSELAGE ADJACENT TO AFT CARGO DOOR RELAMPED AND OPS CHECKED SLIDE EMERGENCY LIGHT AT RH AFT FUSELAGE, GOOD AS PER AMM TASK 33-51-06-902-082.PARTS USED: 99-335
- [SDR CALA2024053001640](https://openairdocs.org/sdr/CALA2024053001640.md): Lens · missing · May 29, 2024 · N671UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - FWD GALLEY OVERHEAD R/H EMERGENCY LIGHT LENS MISSING.
- [SDR CALA2024052901601](https://openairdocs.org/sdr/CALA2024052901601.md): Lens · missing · May 27, 2024 · N671UA · Boeing 767322 · Emergency Lighting
  > CABIN CREW REPORTED EMERGANCY 2 OFF LIGHTS LENS MISSISING.LIGHT IS STILL OPERATING NORMALLY SEE PHOTO ATTACH LLIGHTS OPPOSITE LAV A SEE PHOTO MEL 3351G. PHOTO ATTACH PHOTO ATTACH NEW LIGHT LENS 2 OFF INSTALLED AND EMERGACY LIGHT TESTED OK IAW AMM 33-51-05
- [SDR CALA2024040200936](https://openairdocs.org/sdr/CALA2024040200936.md): Floor Support · corroded · Mar 21, 2024 · N671UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > DURING THE INSPECTION OF FWD GALLEY, IT WAS FOUND A CORROSION ON THE FLOOR STRUCTURE OF THE MAIN CABIN LOCATED AT BS 325 AND LBL 24. REPAIRED THE FLOOR STRUCTURE AT BS325 WAS LBL24 AS PER B767-300 STRUCTURE WITH THIS REPAIR INSTALLED. SRM 53-00-51-2R-1. THIS R
- [SDR CALA2024040200935](https://openairdocs.org/sdr/CALA2024040200935.md): Rib · cracked · Mar 20, 2024 · N671UA · Boeing 767322 · Wing, Rib/Bulkhead
  > DURING INSPECTION OF ACCESS PANEL 541DB, IT WAS A CRACKED RIB AT POSITION RIB 13 AND BETWEEN STGR 4/5 ON LH SIDE. THE JACKING OF THE AC FULLY ACCOMPLISHED AS PER ECRA#0711-01085 INSTRUCTIONS AND FULLY ACCOMPLISHED RIB#13 WEB REPLACEMENT AS PER ECRA#5220-03391.
- [SDR CALA2024040200934](https://openairdocs.org/sdr/CALA2024040200934.md): Skin · cracked · Mar 20, 2024 · N671UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > PERFORMED HFEC NDT MANUAL PART 6 51-00-16 AT FWD SERV DOOR CUTOUT AFT LOWER CORNER FUSELAGE, AND WERE FOUND CRACK INDICATION AT 4TH FASTENER HOLE ON, 1ST LAYER SKIN ABOUT 0 DEGRESS AND 4TH LAYER BEAR STRAP ABOUT 270 DEGRESS. PART-1. IT'S NECESSARY TO ACCOMPLI
- [SDR CALA2024040200937](https://openairdocs.org/sdr/CALA2024040200937.md): Stringer · cracked · Mar 4, 2024 · N671UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > DURING THE INSPECTION OF THE BULK CARGO REPAIR AREA, IT WAS FOUND A CRACKED STRINGER AT POSITION 38R BETWEEN STA 1562/1582. EC/RA#5360-01770. IT IS NECESSARY TO ACCOMPLISH AN INITIAL CYCLES AND ACCOMPLISH REPETITIVE INSPECTIONS PER ECRA 5360-01770 INSPECTION A
- [SDR CALA2023110603293](https://openairdocs.org/sdr/CALA2023110603293.md): Lens · missing · Nov 5, 2023 · N671UA · Boeing 767322 · Emergency Lighting
  > CEILING EMERGENCY LIGHT LENSES ABOVE SEATS 35A AND 35L MISSING. REPAIR TO BE ACCOMPLISHED WITHIN 10 CALENDAR DAYS. ECRA 3351-01427 PART 1 INTERIM REPAIR COMPLIED WITH. PART 2 INSPECTION REQUIREMENTS TO BE PERFORMED DAILY. PART 3 PERMANENT APPROVED FOR 10 DAY D
- [SDR CALA2023051501503](https://openairdocs.org/sdr/CALA2023051501503.md): Densitometer · unknown · May 13, 2023 · N671UA · Boeing 767322 · Aircraft Fuel System
  > INDICATED FUEL INBALANCE OF 2500LBS. FLUCTUATED ALL THE WAY TO EWR UPON REACHING OUT TO THE CREW. CAPTAIN STATES ISSUE IS T/S PER WDM 28-41-21, CHECKED WIRING BTW L FMC AND FQIS, NO INDICATION ONLY. NO ACTUAL LEAK SUSPECTED. WHILE IN FLIGHT, FMC FAULTS. PERFOR
- [SDR CALA2022102702948](https://openairdocs.org/sdr/CALA2022102702948.md): Hydraulic System · warning message · Oct 25, 2022 · N671UA · Boeing 767322 · Hydraulic Power System
  > RTO AT 100KTS DUE TO RT HYD QTY EICAS MSG REQUEST MEL FOR R/H HYD INDICATION. PLACED R/H HYD ON MEL. PERFORMED BRAKE PRESS CHCK RIGHT GEAR OPS INDICATION INSPECTION LOOK 93 ON R/H HYD. NORMAL ALSO NO LEAKS FOUND, BRAKE PINS LOOK NORMAL AND VISUAL R HYD QTY EI
- [SDR CALA2022102402911](https://openairdocs.org/sdr/CALA2022102402911.md): None · stuck · Oct 22, 2022 · N671UA · Boeing 767 · Navigation System
  > CLIMBING THROUGH 10000 BOTH CA AND FO AIRSPEED MAX LIMIT STUCK AT 260 AIR RETURN TO EWR UPON ARRIVAL CONFIRMED BOTH AIRSPEED INDICATORS STUCK AT 260 KNTS. CYCLED S591 VMO/MMO SWITCH MAX AIRSPEED LIMIT INDICATOR CKED NORMAL. SECURED SWITCH WITH SAFETY WIRE.
- [SDR CALA2022102402910](https://openairdocs.org/sdr/CALA2022102402910.md): None · missing · Oct 21, 2022 · N671UA · Boeing 767 · Wing, Control Surfaces
  > PDA 2 FOUND L/H WING AFT FAIRING FOR MAIN GEAR SIDE BRACE TRUNNION MISSING. REQUEST CDL DEFERRAL # 57EC. DEFERRED AS PER CDL. DISPATCH DESK: 62 NAME: JERRY DATE: 21-OCT-22- L/H WING AFT FAIRING FOR MAIN GEAR SIDE BRACE TRUNNION - CDL 57EC ADDE
- [SDR CALA2022071501754](https://openairdocs.org/sdr/CALA2022071501754.md): Hydraulic System · warning message · Jul 14, 2022 · N671UA · Boeing 767322 · Hydraulic Power System
  > HIGH SPEED REJECTED TAKE OFF DUE TO R HYD QTY EICAS MSG. REJECT AT 135 KTS. BTMS 8-9 ON WHEELS ON AC ARRIVAL CREW REPORT R/H HYD QTY EICAS CAUTION MSG SHOWN ON ON ARRIVAL TO AC HYD QTY INDICATIONS WERE L/H 0.97 C 0.94 R/H TAKE OFF ROLL IT EXTINGUISHED AND RET
- [SDR CALA2021071201075](https://openairdocs.org/sdr/CALA2021071201075.md): Screw · missing · Jul 11, 2021 · N671UA · Boeing 767322 · Nacelle/Pylon, Main Frame
  > PDA 3 #1 ENGINE PYLON MISSING 2EA SCREWS AT INBD LEADING EDGE OF FAIRING 437DB STAINLESS PANEL. INSTALLED CORRECT SCREWS AT PANEL 437DB L/E.
- [SDR CALA2020121601384](https://openairdocs.org/sdr/CALA2020121601384.md): Battery Pack · discharged · Dec 15, 2020 · N671UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK AT L1 FA SEAT INOPERABLE. REPLACED BATTERY PACK, AS PER AMM 33-51-07-422-012. OPERATIONS CHECKS GOOD.
- [SDR CALA2020121601382](https://openairdocs.org/sdr/CALA2020121601382.md): Battery Pack · discharged · Dec 15, 2020 · N671UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK INOPERABLE AT DOOR R2 REPLACED BATTERY PACK, AS PER AMM 33-51-07-422-012. OPERATIONS CHECKS GOOD.
- [SDR CALA2020121601381](https://openairdocs.org/sdr/CALA2020121601381.md): Battery Pack · discharged · Dec 15, 2020 · N671UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK INOPERABLE AT DOOR R2 REPLACED BATTERY PACK, AS PER AMM 33-51-07-422-012. OPERATIONS CHECKS GOOD.
- [SDR CALA2020030900611](https://openairdocs.org/sdr/CALA2020030900611.md): Skin · punctured · Mar 8, 2020 · N671UA · Boeing 767322 · Elevator, Plate/Skin
  > LH INBD ELEVATOR UPPER SKIN IS PUNCTURED APPROX 3.0" IN LENGTH. LOCATED 11.0" FROM INBD EDGE AND 12.0" FROM AFT EDGE IN ZONE 2. SUPPORT TASK IAC DAMAGE. REF. HAECO NR# 22001, SERVICE ORDER# 41 8147. REPAIRED LH INBD ELEVATOR UPPER SKIN PUNCTURE IAW B767 SRM 55
- [SDR CALA2019090201491](https://openairdocs.org/sdr/CALA2019090201491.md): Relay · faulty · Sep 2, 2019 · N671UA · Boeing 767322 · Pitot/Static Anti-Ice System
  > TAT OVERHEAD LIGHT ON TAT PROBE LIGHT FIM 30-33-00-815-805 FOLLOWED. CURRENT SENSING RELAY FOUND AT FAULT. RELAY REPLACED AS PER WDM 30-33-11. RELAY PN 7705402 SN 08711.
- [SDR CALA2018101502128](https://openairdocs.org/sdr/CALA2018101502128.md): Connector · disconnected · Oct 15, 2018 · N671UA · Boeing 767322 · Light System Wiring
  > INTERIOR EMERGENCY LIGHT AT DOOR R2 INOP. SECURED CONNECTORS TO LIGHT ASSY REF. AMM 33-51-00 OPS NORMAL.
- [SDR CALA2018101302093](https://openairdocs.org/sdr/CALA2018101302093.md): Battery Pack · unsecure · Oct 10, 2018 · N671UA · Boeing 767322 · Emergency Lighting
  > AFT CENTER GALLEY FLOOR EMERGENCY LIGHTS INOP. SECURED BATTERY PACK AT PWR SUPPLY M1210. OPS NORMAL REF MM 33-51-00.
- [SDR CALA2018060601414](https://openairdocs.org/sdr/CALA2018060601414.md): Check Valve · failed · Jun 1, 2018 · N671UA · Boeing 767322 · Engine (Turbine/Turboprop)
  > DURING DECENT, THE CREW REPORTED A RUMBLE FROM THE RT ENGINE, FOLLOWED BY AN EGT OF 666 DEGREES. THE ENGINE WAS SHUTDOWN, RAN QRH AND THE ENGINE WAS RESTARTED BUT UNABLE TO ADVANCE THROTTLE, ENGINE CONTINUED TO RUN AT IDLE. REMOVED IP CHECK VALVE IAW AM
- [SDR CALA2018043001200](https://openairdocs.org/sdr/CALA2018043001200.md): Heater · defective · Apr 29, 2018 · N671UA · Boeing 767322 · Heating System
  > ELECTRICAL ODOR FROM AREA AROUND FWD GALLEY AND CABIN SPEAKER. A SSOCIATED SPEAKER IS NOT WORKING WITH A TEST PA ANNOUNCEMENT. CARRIED OUT CHECKS IAW AMM 05-51-56-940-801C1.FOUND OUTLINED CHECKS. ODOR FOUND FROM AREA OF R1 DOOR. CARRIED OUT OPERATION OF FWD D
- [SDR CALA2018030800864](https://openairdocs.org/sdr/CALA2018030800864.md): Frame · cracked · Mar 7, 2018 · N671UA · Boeing 767322 · Fuselage Main, Frame
  > BS 1725.5 BULKHEAD OUTER FRAME CRACKED ABOVE STRINGER 7R. REPAIRED THE FRAME IAW SRM 53-80 -01.
- [SDR CALA2018022600820](https://openairdocs.org/sdr/CALA2018022600820.md): Tee Fitting · gouged · Feb 23, 2018 · N671UA · Boeing 767322 · Fuselage Main, Attach Fittings
  > ONE HOLE IN THE LT MLG WW FAIL SAFE TEE FITTING IS GOUGED, REMOVED AND REPLACED THE TEE FITTING IAW J/C EA 5340-01478, REV C, STEP 18 (1-14).
- [SDR CALA2018022700821](https://openairdocs.org/sdr/CALA2018022700821.md): Tee Fitting · damaged · Feb 23, 2018 · N671UA · Boeing 767322 · Fuselage Main, Attach Fittings
  > RT MLG WW FAIL SAFE TEE FITTING HAS ONE HOLE WITH A DEFECT. REMOVED AND REPLACED THE TEE FITTING IAW J/C 5340-01478, REV C, STEP 18 (1-14).
- [SDR CALA2018030800860](https://openairdocs.org/sdr/CALA2018030800860.md): Skin · cracked · Feb 21, 2018 · N671UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > LEFT EXTERIOR FUSELAGE SKIN CRACKED AT A RIVET, BS 1654.5 JUST BELOW STRINGER 3L. REPAIRED THE SKIN IAW EC/RA 5330-06296.
- [SDR CALA2018012600310](https://openairdocs.org/sdr/CALA2018012600310.md): Skin · cracked · Jan 26, 2018 · N671UA · Boeing 767322 · Wing, Plate/Skin
  > A CRACK WS FOUND ON LOWER LT WING SKIN AT WS 990.2. REPAIRED THE SKIN IAW EA 5720-02611, REV B.
- [SDR CALA2018012600309](https://openairdocs.org/sdr/CALA2018012600309.md): Skin · cracked · Jan 26, 2018 · N671UA · Boeing 767322 · Wing, Plate/Skin
  > A CRACK WAS FOUND ON THE LOWER RT WING SKIN WS 990.2. REPAIRED CRACK ON LOWER SKIN WS 990.2 FASTENER HOLE 1 ON RIGHT WING IAW EA 5720-02611 REV B.
- [SDR CALA2017102003712](https://openairdocs.org/sdr/CALA2017102003712.md): Pin · worn · Oct 20, 2017 · N671UA · Boeing 767322 · Escape Slide
  > RIGHT OVERWING SLIDE HAS WORN PINS FOR THE DOOR LATCH CONNECTING RODS. REMOVED AND REPLACED THE OVERWING PINS ON DOOR CONNECTING LATCH RODS.
- [SDR CALA2017100903557](https://openairdocs.org/sdr/CALA2017100903557.md): Lamp · inoperative · Oct 9, 2017 · N671UA · Boeing 767322 · Light System Wiring
  > L2 DOOR EMERGENCY LIGHT INOPERATIVE. CLEANED THE CONNECTORS AND REPLACED THE LAMPS. OPS CHECKED GOOD IAW WDM 33-51-21.
- [SDR CALA2017080802523](https://openairdocs.org/sdr/CALA2017080802523.md): Charger · inoperative · Aug 2, 2017 · N671UA · Boeing 767322 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT SECOND TO THE LAST LIGHT ON LT SIDE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND CHARGER M738 IAW AMM 33-51-07. OPS NORMAL.

Next page: https://openairdocs.org/aircraft/N671UA/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 = 'N671UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N671UA/reports

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