# Service difficulty reports: N653UA

A list on [N653UA](https://openairdocs.org/aircraft/N653UA.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 7 · 315 reports

- [SDR CALA2026083119047](https://openairdocs.org/sdr/CALA2026083119047.md): Ground Wire · detached · Aug 30, 2026 · N653UA · Boeing 767322 · Light System Wiring
  > EMERGENCY EXIT SIGN ABOVE RT OVERWING EXIT, FOUND INOPERATIVE. RT EMER EXIT DOOR EMER EXIT SIGN FOUND GND WIRE SNAPPED FROM THE TERMINAL LUG. WIRE AND TERMINAL LUG RECRIMPED AND TESTED NORMAL REM. SWPM 20-30-11 AND AMM 33-51-01. WIRE AND TERMINAL LUG RECRIMP
- [SDR CALA2026083119045](https://openairdocs.org/sdr/CALA2026083119045.md): Light · damaged · Aug 30, 2026 · N653UA · Boeing 767322 · Emergency Lighting
  > 33D ECONOMY SEAT EMERGENCY LIGHT FOUND IN POOR CONDITION. SEAT EMERGENCY LIGHT REPLACED IAW AMM 33-51-10.
- [SDR CALA2026062517333](https://openairdocs.org/sdr/CALA2026062517333.md): Access Door · missing · Jun 23, 2026 · N653UA · Boeing 767322 · Cargo/Baggage Doors
  > FOUND AFT CARGO HANDLING ACCESS DOOR MISSING PERFORMED A VISUAL INSPETION AND WALKAROUND NO DEFECT NOTED. FOUND PANEL IN EWR MYSTERIOUSLY. PLACING THE "AFT CARGO HANDLING ACCESS DOOR" IN EWR "RON" HOLD AT TERMINAL C.
- [SDR CALA2026040114996](https://openairdocs.org/sdr/CALA2026040114996.md): Wire Harness · damaged · Mar 28, 2026 · N653UA · Boeing 767322 · Equipment/Furnishings Wiring
  > RAMP REPORTED PALLET STUCK IN FWD CARGO, UPON REMOVAL, NOTED MULTIPLE PDU'S INOPERATIVE AT POSITIONS 5R, 8R, 8C, 5C, 8L. AFTER INVESTIGATION LOOM W0704 FOUND WITH 15 BROKEN WIRES DUE TO BURNING. MANY OTHER WIRES SHOWING SIGNS OF BURNING BUT HAVE NOT BROKEN. D
- [SDR CALA2026031714628](https://openairdocs.org/sdr/CALA2026031714628.md): Computer · faulted · Mar 15, 2026 · N653UA · Boeing 767322 · Auto Throttle System
  > A/T DISC LT AT 105KTS ON TO A/T INOP DISCREPANCY HAS PREVIOUS HISTORY, REF LOGS 8154689 AND 8085051 THRUST MANAGEMENT COMPUTER M&E 76-2231-9-0001, HAS BEIN ORDERED AND READY TO BE PICK UP AT TERMINAL STORES IN CASE NEEDED REF IPC 22-31-01-01 AND FIM 22-02 FAUL
- [SDR CALA2026021713828](https://openairdocs.org/sdr/CALA2026021713828.md): Oxygen Mask · split · Feb 15, 2026 · N653UA · Boeing 767322 · Crew Oxygen System
  > CAPTAINS CREW OXYGEN MASK HARNESS IS SPLIT, CAUSING OXYGEN LEAKAGE WHEN THE HARNESS IS INFLATED RAISING AND UPDATING SDR ORIGINAL CAPT OXYGEN MASK SWAPPED WITH SECOND OBSERVER OXYGEN MASK IAW AMM 35-11-51-004-059 AND 35-11-51-404-060. CAPT & SECOND OBSERVER OX
- [SDR CALA2025121712183](https://openairdocs.org/sdr/CALA2025121712183.md): Skin · damaged · Dec 15, 2025 · N653UA · Boeing 767322 · Ailerons
  > AFTER INPECTION REQUESTED IN AVO15988 REV.A, WAS FOUND MOISTURE INGRESSION ON LT OTBD AILERON. NECESSARY REMOVE THE MOISTURE AND REPAIR. ALL STEPS OF THE ECRA: 5760-01130 WERE ACCOMPLISHED WITHOUT DEVIATION. ALL STEPS OF THE ECRA: 5760-01130 WERE ACCOMPLISHED
- [SDR CALA2025121612159](https://openairdocs.org/sdr/CALA2025121612159.md): Skin · contaminated · Dec 15, 2025 · N653UA · Boeing 767322 · Ailerons
  > AFTER INPECTION REQUESTED IN AVO15988 REV.A WAS FOUND MOISTURE INGRESSION ON RH OUTBOARD AILERON. NECESSARY REMOVE THE MOISTURE AND REPAIR. ALL STEPS OF THE ECRA: 5760-01131 WERE ACCOMPLISHED WITHOUT DEVIATION. PERFORMED NDT INSPECTIONS, REMOVED THE DAMAGES ON
- [SDR CALA2025121612141](https://openairdocs.org/sdr/CALA2025121612141.md): Structure · damaged · Dec 12, 2025 · N653UA · Boeing 767322 · Wing Main, Frame Structure
  > LEFT WING CENTER TANK LOWER CHORD AND WEB DAMAGE LOCATED AT LBL 62.05 FROM BSS 785.9 TO BSS 955.1 BTW STRINGER L-4 TO L-6. THIS LP WAS CLASSIFIED AS RII IAW GMM 03-20-20. QC AWARE. REMOVED FASTENERS, PERFORMED TRIMMED THE DAMAGED AREA AND PERFORMED NDT INSPECT
- [SDR CALA2025101309965](https://openairdocs.org/sdr/CALA2025101309965.md): Light · damaged · Oct 10, 2025 · N653UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY PATHWAY LIGHT AT SEAT AT SEAT 44D DAMAGED PARTS ORDERED AGAINST AIRCRAFT AND IN STOCK AT LHR ALSO PATHWAY LIGHT (M&E 29-3326-3-0013) SEMERGENCY PATHWAY LIGHT ENDCAP ASSY AT SEAT 44D REPLACED IAW CMM: 25-23-52.
- [SDR CALA2025100709727](https://openairdocs.org/sdr/CALA2025100709727.md): Light Sys · malfunctioned · Oct 6, 2025 · N653UA · Boeing 767322 · Emergency Lighting
  > INTERIOR EMERGENCY LIGHTS CAME ON FOR 3-5 MIN 6+30 INTO FLIGHT. NO DOOR LGHT OR ELECT ANOMOLY OPS CK EMERGENCY LIGHT NO FAULT NOTED IAW MM 33-51-00 COULD NOT DUPLICATE AT THIS TIME.
- [SDR CALA2025072506911](https://openairdocs.org/sdr/CALA2025072506911.md): Hose · damaged · Jul 22, 2025 · N653UA · Boeing 767322 · Hydraulic System, Main
  > HYD C QUAN LOW HEAVY HYDRAULIC LEAK FOUND AT CENTER SYSTEM C1 ELEC PUMP PRESSURE FLEX HOSE B-NUT SWAGING AT THE PUMP HOUSING. REQUIRED PART IAW IPC 29-11-02-02 ITEM 150 P/N AS115-06D0130 OR AS115-06K0130 PLEASE SHIP THE DAMAGED REMOVED HYDRAULIC HOSE. ACMP CE
- [SDR CALA2025071406566](https://openairdocs.org/sdr/CALA2025071406566.md): Slide · no discrepancy · Jul 11, 2025 · N653UA · Boeing 767322 · Escape Slide
  > DOOR 1R ESCAPE SLIDE NEEDS TO BE REMOVED FOM. REMOVED DOOR 1R ESCAPE SLIDE REF MM TASK 25-66-01-004-001. ENTRY DOOR R1 ESCAPE SLIDE WAS REINSTALLED IN REF AMM 25-66-01-404-072. VERIFIED DOOR R1 ESCAPE SLIDE INSTALLATION IAW AMM 25-66-01-404-072, AND GMM 09-25
- [SDR CALA2025070306197](https://openairdocs.org/sdr/CALA2025070306197.md): Panel · missing · Jun 30, 2025 · N653UA · Boeing 767322 · Nacelle/Pylon, Main Frame
  > AIRCRAFT (EXTERNAL) INSPECT. PANEL 446AR IS MISSING FROM NR 2 ENG PYLON OUTBOARD SIDE.
- [SDR CALA2025030400474](https://openairdocs.org/sdr/CALA2025030400474.md): Ehsi · unserviceable · Mar 2, 2025 · N653UA · Boeing 767322 · Indicating/Recording System
  > TEN MINS AFTER TAKE OFF NOTICEABLE SMOKE FROM CA SIDE UNDER HSI WITH ELEC SMELL. LASTED 15 SECS. WERE REINSTALLED WITH PREVIOUS AMM REF, AIRCRAFT REQUIRES FURTHER T/S TO DETERMINE SOURCE OF SMOKE.. SMOKE IN THE CABIN FORM UPLOADED. PERFORMED AN INITIAL VISUAL
- [SDR CALA2025030402571](https://openairdocs.org/sdr/CALA2025030402571.md): Packing · leaking · Mar 1, 2025 · N653UA · Boeing 767322 · Hydraulic System, Main
  > RIGHT WING HYD VALVE EICAS ILLINUMATED AFER TAKEOFF, CREW SELECTED THE RT WING HYD VALVE TO OPEN BUT THE VALVE REMAINS CLOSED. ON ARRIVAL LHR, CREW REPORTED NO AIRCRAFT FLIGHT CONTROL PROBLEMS.RESET FLT CONTROL SHUTOFF WING R CB H26 ON THE P11 AND CYCLED SWITC
- [SDR CALA2024121301494](https://openairdocs.org/sdr/CALA2024121301494.md): Brake · faulted · Dec 10, 2024 · N653UA · Boeing 767322 · Landing Gear Brake System
  > NO.7 BRAKE PACK SERIOUSLY DAMAGED, WHEEL TILTED AND NOT SITTING CORRECTLY NO 7 MAIN WHEEL REMOVED REF AMM 32-41-08-004-001. NO 7 WHEEL FOUND WITH SERIOUS INTERNAL DAMAGE NO 7 BRAKE REMOVED REF AMM 32-41-08-004-001 INFORMATION UPDATE, ITEM FLAGGED AS SDR DUE B
- [SDR CALA2024101000812](https://openairdocs.org/sdr/CALA2024101000812.md): Control Unit · faulted · Oct 6, 2024 · N653UA · Boeing 767322 · Equipment/Furnishings Wiring
  > DUE TO FWD AND RT AFT GALLEY POWER LOAD SHED. HIGHLY SUSPECT WE ARE LOSING GROUND COMING FROM BPCU D278B (C12) TO PIN 9 FOR BOTH ELCU'S M225/226. WHEN THIS GRD GOES AWAY, ONLY WAY TO RESET GALLEY'S IS TO CYCLE RIGHT UTILITY BUS SWITCH OR TRANSFER OF ELECTRICAL
- [SDR CALA2024070800163](https://openairdocs.org/sdr/CALA2024070800163.md): Monitor · faulty · Jul 8, 2024 · N653UA · Boeing 767322 · Hydraulic Indicating System
  > DURING TAKEOFF ROLL GOT R HYD QTY EICAS. RT HYD QTY INDICATED.4 0. REJECTED T/O CHECKED AND APPROVED FOR DEFERRAL I.A.W. B763MEL 2933E. M PROCEDURE CARRIED OUT AND PLACARD INSTALLED. TOMC APPROVED REF MEL 2933E DEFERRAL 2933E APPROVED. PLACARD INSTALLED *DM*
- [SDR CALA2024050801398](https://openairdocs.org/sdr/CALA2024050801398.md): Shear Tie · not reported · May 5, 2024 · N653UA · Boeing 767322 · Fuselage Internal Mounting Structure
  > - REMOVE / INSTALL BULK CARGO COMPT STA 1562 BTW STR 33L AND STR 33R FRAME WEB, LOWER CHORD, SHEAR TIE & SPLICE FOR ACCESS. STA 1562 BETWEEN STR 32L AND STR 32R FRAME WO.3128962 SEQ. 5.1349 AND WO.3168714 SEQ.5.1411 FOR DETAIL WEB, LOWER CHORD, SHEAR TIE AND
- [SDR CALA2024050801405](https://openairdocs.org/sdr/CALA2024050801405.md): Skin · delaminated · May 4, 2024 · N653UA · Boeing 767322 · Elevator, Plate/Skin
  > RIGHT O/B ELEVATOR UPPER PANEL L/E CUTOUT AREA FOUND DEEP CHAFING AND DELAM (2 LOCATIONS) RH O/B ELEVATOR UPPER PANEL L/E CUTOUT AREA 2 LOCATIONS PERFORMED COMPOSITE REPAIR AS PER UNITED EC/RA 5524-01001 REV- REFER FORM 44-0008 ITEM 1 TO 10.
- [SDR CALA2024050701362](https://openairdocs.org/sdr/CALA2024050701362.md): Floorbeam · cracked · May 3, 2024 · N653UA · Boeing 767322 · Fuselage Main, Floor Beam
  > BULK CARGO STA 1540 FLOOR BEAM WEB FOUND CRACK ABOVE STR 39R. BULK CARGO STA 1540 FRAME WEB AT STR 39R AREA REPAIRED AS PER EC/RA 5360-01800 REV-. ATTACH FORM 44-0008 ITEM 1 TO ITEM 23 ACCOMPLISHED.
- [SDR CALA2024050801404](https://openairdocs.org/sdr/CALA2024050801404.md): Frame · cracked · Apr 30, 2024 · N653UA · Boeing 767322 · Fuselage Main, Frame
  > LEFT BHD CHORD INSPECTION (1EA) CRACK FOUND RUNNING AT 9 O''CLOCK POSITION THROUGH THICKNESS IN DEPTH ON FWD OUTER CHORD FROM O/B. REPAIRED AS PER EC/RA 5380-01390 REV A PART 1. INTERIM REPAIR AND REFER EA 5300-01600 REV.A OP 002 CR.3058156 SEQ. 1.1697 FOR WO
- [SDR CALA2024050801403](https://openairdocs.org/sdr/CALA2024050801403.md): Stringer · corroded · Apr 27, 2024 · N653UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > AFT OF BULK CGO COMPT STA 1540-1562 S38R STRINGER FOUND CORROSION. AFT OF BULK CARGO COMPT STA 1502 - STA 1562 STRINGER 38R REPAIRED AS PER EC/RA 5360-01799 REV.-
- [SDR CALA2024050801402](https://openairdocs.org/sdr/CALA2024050801402.md): Stringer · corroded · Apr 27, 2024 · N653UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > AFT OF BULK CGO COMPT STA 1540-1562 S39R STRINGER FOUND CORROSION. AFT OF BULK CARGO COMPT STRINGER 39R BETWEEN STA 1518 AND STA 1562 REPLACED AS PER EC/RA 5360-01799 REV- ATTACH FORM 44-0008 ITEM 1 TO ITEM 38.
- [SDR CALA2024050801401](https://openairdocs.org/sdr/CALA2024050801401.md): Skin · misrepaired · Apr 27, 2024 · N653UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > FUSELAGE AT STA 1540, STR 39R MISDRILL THE REPAIR DOUBLER. FUSELAGE SKIN STA 1540 BETWEEN STR 38L AND STR 38R REPAIRED AS PER EC/RA 5360-01798 REV.- PART 1 ATTACH FORM 44-0008 ITEM 1 TO ITEM 29
- [SDR CALA2024050801400](https://openairdocs.org/sdr/CALA2024050801400.md): Stringer · corroded · Apr 27, 2024 · N653UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > AFT OF BULK CGO COMPT STA 1540-1562 S39L STRINGER FOUND CORROSION. TRANSFER REF NR HX WO.3092202 AND ORIGINATED BY V896921. AFT IF BULK CARGO COMPT STRINGER 39L BETWEEN STA 1518 AND STA 1562 REPAIRED AS PER EC/RA 5360-01799 REV- ATTACH FORM 44-0008 ITEM 1 TO I
- [SDR CALA2024050701354](https://openairdocs.org/sdr/CALA2024050701354.md): Skin · cracked · Apr 27, 2024 · N653UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DOUBLER FOUND CRACK AT WASTE SYSTEM SERVICE PANEL #163AL CUTOUT AREA. FUSELAGE SKIN STA 1562 TO STA 1582 BETWEEN STR 38L AND STR 38R INTERNAL DOUBLER REPLACED AS PER SRM 51-10-02.
- [SDR CALA2024050701369](https://openairdocs.org/sdr/CALA2024050701369.md): Frame · cracked · Apr 27, 2024 · N653UA · Boeing 767322 · Fuselage Main, Frame
  > STA 1809 L/H BHD CHORD (2EA) CRACK FOUND RUNNING AT 1 O`CLOCK AND 7 O`CLOCK POSITION THROUGH THICKNESS IN DEPTH ON SECOND LAYER. FX STA 1809-1788 STR-8L - STR12AL DOUBLER REPLACED AS PER EC/RA 5380-01390 REV- PART 1: INTERIM REPAIR.
- [SDR CALA2024050701368](https://openairdocs.org/sdr/CALA2024050701368.md): Shear Tie · damaged · Apr 27, 2024 · N653UA · Boeing 767322 · Fuselage Internal Mounting Structure
  > BULK CGO STA 1562, STR 38L TO STR 38R SHEAR TIE FOUND ELONGATED. BULK CARGO STA 1562 BETWEEN STR 38L AND STR 38R FAIL SAFE. REPAIRED AND SHEAR TIE REPLACED AS PER EC/RA 5360-01801 REV-PART 1. ATTACHED FORM 44-0008 ITEM 1 TO ITEM 24 ACCOMPLISHED.
- [SDR CALA2024050701367](https://openairdocs.org/sdr/CALA2024050701367.md): Failsafe · cracked · Apr 27, 2024 · N653UA · Boeing 767322 · Fuselage Main, Structure
  > BULK CARGO COMPT (1EA) HOLE FOUND CRACK ON FAIL-SAFT CHORD LOWER FLANGE AT STA 1562 BETWEEN S32L-33L. BULK CARGO COMPT STA 1562 BETWEEN STR 32L AND STR 34L FAIL SAFE CHORD INTERIM REPAIRED AS PER EC/RA 5360-01801 REV- PART 1. ATTACH FORM 44-0008 ITEM 1 TO ITE
- [SDR CALA2024050701363](https://openairdocs.org/sdr/CALA2024050701363.md): Skin · cracked · Apr 27, 2024 · N653UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > EA 5315-01152 OP002, STEP B(4), 2EA HOLES FOUND CRACK ON SKIN LAYER. DOOR 1R CUTOUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP INTERIM REPAIRED AS PER EC/RA 5315-01212 REV. ORIG PART 1
- [SDR CALA2024050701361](https://openairdocs.org/sdr/CALA2024050701361.md): Skin · cracked · Apr 27, 2024 · N653UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > EA 5315-01152 OP 001, STEP B(4), 1EA HOLE FOUND THROUGH THICKNESS CRACK ON SKIN LAYER. TRANSFER REF NR HX WO.3049623. FX-DOOR 1L CUTOUT AFT LOWER CORNER FUSELAGE SKIN INTERIM WORK REPAIRED AS PER EC/RA 5315-01213 REV.- PART 1. ATTACHED FORM 44-0008 ITEM 1 T
- [SDR CALA2023122903757](https://openairdocs.org/sdr/CALA2023122903757.md): Gcu · failed · Dec 27, 2023 · N653UA · Boeing 767322 · Electrical Power System
  > L GEN TRIP. L EEC ALTN MODE. L BUS TIE ISOLTD DISCUSSION WITH PILOTS LEFT BUS TIE BREAKER WOULD NOT RESET DURING FLIGHT, L ENG EEC WENT INTO ALTERNATE MODE, STATUS MESSAGE EEC C1 AND LEFT IDG VALVE STATUS MESSAGE PLEASE PERFORM WIRING CHECK OF THE W3538 BUNDL
- [SDR CALA2023111703410](https://openairdocs.org/sdr/CALA2023111703410.md): Wire · damaged · Nov 15, 2023 · N653UA · Boeing 767322 · Electrical Power System Wiring
  > L GEN OFF EICAS RIGHT AFTER TAKEOFF QRH RESET REPEAT WRITE-UP CAPT STATES AFTER ROTATION WHEN GEAR UP WAS SELECETED L IDG ACP BPCU BITE REF FIM 24-20 FT 801. HAD THE FOLLOWING MESSAGES: TRIPPED. CREW QRH CHECKLIST, IDG RESET AND REMAINED ON FOR REST REPLACE GC
- [SDR CALA2023080902471](https://openairdocs.org/sdr/CALA2023080902471.md): Slide · unwanted deploy · Aug 5, 2023 · N653UA · Boeing 767322 · Escape Slide
  > WHILE PERFORMING FCD #2565-01155 ACCIDENTAL DEPLOYMENT OF THE LH OVERWING ESCAPE SLIDE DOOR WITH THE SAFETY PIN INSTALLED. NEED TO REPLACE INFLATION CABLE & INFLATION CYLINDER AS PER SLIDE REMOVAL AMM 25-65-01-024-001-001 STEP #3. VERIFIED INSTALLATION OF INFL
- [SDR CALA2023060501750](https://openairdocs.org/sdr/CALA2023060501750.md): Socket · burned · Jun 3, 2023 · N653UA · Boeing 767322 · Flight Compartment Lighting
  > SMOKE ODOR ORIGINATE FROM JUST ABOVE FORWARD GALLEY LIGHT CONTROL PANEL TO CEILING AREA. TURNED OFF GALLEY LIGHTS AND SMOKE ODOR DISSIPATED. PULLED ALL CB''S AND TURNED OFF REMAINING ON-OFF SWITCHES ON CONTROL PANEL. MUST MEET FLIGHT CREW AND FILL OUT SMOKE OD
- [SDR CALA2023041301108](https://openairdocs.org/sdr/CALA2023041301108.md): Start Valve · unserviceable · Apr 13, 2023 · N653UA · Boeing 767322 · Engine Starter
  > R STARTER CUTOUT MESSAGE ON EICAS DURING CLIMB OUT AS PER FIM TASK 80-11-02/401. R ENGEINE START VALVE REQUIERES. REMOVAL. REMOVED AND REPLACED R ENGINE STARTE S/O VALVE AS PER MM 80-11-02-004-001-NOO. OPS. CHECK GOOD. AIRCRAFT OK TO CONTINUE. PARTS USED: 76-
- [SDR CALA2023010600035](https://openairdocs.org/sdr/CALA2023010600035.md): Access Panel · missing · Jan 6, 2023 · N653UA · Boeing 767322 · Wing Structure
  > DRUING ETOPS PRE DEPARTURE SERVICE CHECK FOUND LEADIND EDGE SLAT LUBRICATION ACCESS PANEL R/H SLAT # 12 MISSING REQUESTING CDL PART NIS EWR M&E 76-5741-3-0002. REPLACED. OPS CHK GOOD.
- [SDR CALA2023010200014](https://openairdocs.org/sdr/CALA2023010200014.md): Access Panel · missing · Jan 2, 2023 · N653UA · Boeing 767322 · Wing, Plate/Skin
  > PDA 3, ON ARRIVAL FOUND ONE LEADING EDGE SLAT LUBRICATION ACCESS PANEL MISSING AT R/H SLAT NO. 8. COMPLIED WITH CDL 57F. INSTALLED LEADING EDGE SLAT LUBRICATION ACCESS PANEL 621VB AT R/H SLAT NO.8.
- [SDR CALA2022072701893](https://openairdocs.org/sdr/CALA2022072701893.md): Cover · missing · Jul 27, 2022 · N653UA · Boeing 767322 · Emergency Lighting
  > EMER LTS ACROSS FROM FWD LEFT LAV ARE MISSIN G COVERS. INSTALLED SATIS AS PER AMM 33-51-10 REV136
- [SDR CALA2022041400993](https://openairdocs.org/sdr/CALA2022041400993.md): Light · inoperative · Apr 14, 2022 · N653UA · Boeing 767322 · Emergency Lighting
  > DURING EMERGENCY LIGHTS TESTING A-CHECK FOUND ROW 40 TO 44 LIGHTS NOT WORKING ON BOTH SIDE. FLAGGING SDR WHILE TROUBLESHOOTING ENCOUNTER FLOOR PROXIMITY EMERGENCY LIGHT CABLE DISCONNECTED AT SEAT 44E. RECONNECTED CABLE AND LIGHTS WORKED FROM ROW 40 TO ROW 44.
- [SDR CALA2022011800172](https://openairdocs.org/sdr/CALA2022011800172.md): Altimeter · fluctuates · Jan 18, 2022 · N653UA · Boeing 767322 · Rate of Climb Indicator
  > CAPTAINS ALTIMETER WOULD SHOW ALTITUDE BOUNCING UP TO 200FT DURI NG FLIGH T IN LEVEL FLIGHT. CAPTAIN''S ALTIMETER REPLACED IAW AMM. 34-13-01-404-004. ALL OPS NORMAL. ADD EMP:314121 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1152089 SN OFF 2356 IPC REFERENCE #
- [SDR CALA2022010500027](https://openairdocs.org/sdr/CALA2022010500027.md): Transmitter · unserviceable · Jan 4, 2022 · N653UA · Boeing 767322 · Hydraulic Power System
  > L HYD QTY ZEROINFLT. PRESS NORMAL. INSPECTED LH PYLON AREA FOR ANY EVIDANCE OF LEAK AND EDP ALL DRY REMOVED AND REPLACED LEFT HYD QTY TRANSMITTER I.A.W. M/M NO LEAK NOTED ALSO FLIGHT CNT NO LEK NOTED VERIFIED RESERVOIR 29-33-02-004-001 AND 29-33-02-404-014 UP
- [SDR CALA2021062500961](https://openairdocs.org/sdr/CALA2021062500961.md): Eec · defective · Jun 24, 2021 · N653UA · Boeing 767322 · Fuel Controlling System
  > RIGHT EPR GAUGE FAILED ON POWER UP FOR T/O R ENG EEC MODE EICAS DISPLAYED TROUBLESHOT #2 ENGINE EPR INDICATION PER FIM 77-11 FAULT TREE 803 AND PERFORMED BITE OF PIMU PER FIM 71-01 FAULT TREE 803. ON LEG #0, HAD EEC UNIT FAIL, FAULT CAT 2, AND P5 LINE FAULT, A
- [SDR CALA2019061000923](https://openairdocs.org/sdr/CALA2019061000923.md): Light · broken · Jun 10, 2019 · N653UA · Boeing 767322 · Emergency Lighting
  > ST 25D EXIT PATH LT HANGING BY THE WIRES REQUEST DEFERRAL FOR 25D EMERGENCY PATH LIGHT 25D EMERGENCY LT INOP DEFERRED 25D PATH LIGHT FOUND EPL ASSY BROKEN OFF AT SCREW MOUNTING LOCATIONS.... PN 1013436-001 REQUIRES REPLACE...REF... IFM 25-21-52 NEXT STATION PL
- [SDR CALA2017122604608](https://openairdocs.org/sdr/CALA2017122604608.md): Fan · failed · Dec 23, 2017 · N653UA · Boeing 767322 · Buffet/Galleys
  > SMOKE IN CABIN. EMERGENCY DECLARED. FOUND THE FWD CHILLER FAN FAILED, CAUSING SMOKE ODOR IN THE CABIN. THE FWD GALLEY CHILLER HAD NO OUTPUT. REMOVED AND REPLACE THE FWD GALLEY CHILLER IAW AMM 25-33-01. THE CHILLER OPS CHECKED GOOD IAW AMM 25-33-01-706-004.
- [SDR CALA2017120904374](https://openairdocs.org/sdr/CALA2017120904374.md): Warning Message · false activation · Dec 9, 2017 · N653UA · Boeing 767322 · Trailing Edge Flap Control System
  > FLAPS TE DISAGREE MSG WHEN SELECTING FLAPS FROM 1 TO 5. FOLLOWED QRH FLAP 20 LANDING. EMERGENCY DECLARED. FSEU LAST FAULT SHOW FDE TE DISAGREE INTERMITTENT. FIM 27-51-00-810-81 5 APPLIED. FLAPS FUNCTION PERFORMED SATIS.
- [SDR CALA2017111704104](https://openairdocs.org/sdr/CALA2017111704104.md): Power Supply · faulty · Nov 17, 2017 · N653UA · Boeing 767322 · Emergency Lighting
  > R1 DOOR EMERGENCY EXIT SIGN FOUND DIM. THE POWER SUPPLY M1552 WAS REPLACED AND OPS TESTED NORMAL IAW AMM 33-31-07.
- [SDR CALA2017111704103](https://openairdocs.org/sdr/CALA2017111704103.md): Light · dim · Nov 17, 2017 · N653UA · Boeing 767322 · Emergency Lighting
  > R2 DOOR FWD EMERGENCY LIGHT FOUND DIM. THE EMERGENCY LIGHT REPLACED AND OPS CHECKED NORMAL IAW AMM 33-51-10.

Next page: https://openairdocs.org/aircraft/N653UA/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 = 'N653UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N653UA/reports

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