# Service difficulty reports: N659UA

A list on [N659UA](https://openairdocs.org/aircraft/N659UA.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 · 330 reports

- [SDR CALA2026072017868](https://openairdocs.org/sdr/CALA2026072017868.md): Door · no discrepancy · Jul 17, 2026 · N659UA · Boeing 767322 · Passenger/Crew Doors
  > DOOR 2L WOULD NOT ARM FOR DEPARTURE ACCOMPLISHED ENTRY SERVICE DOOR INSPECTION CHECK. SYSTEM WORKING PROPERLY. GOOD FOR SERVICE. INSPECTION/CHECK IAW AMM 52-11-00/601.
- [SDR CALA2026072017866](https://openairdocs.org/sdr/CALA2026072017866.md): Light · broken · Jul 17, 2026 · N659UA · Boeing 767322 · Emergency Lighting
  > OPERATIONAL TEST - EMERGENCY ESCAPE PATH LIGHTING (EEL) SYSTEM PERFORM OPS CHECK - ESCAPE PATH LIGHT 46F AND 47F IS BROKEN. REPLACED BOTH PATH LIGHTS REF. AMM 33-51-10/301, OPS GOOD.
- [SDR CALA2026060816912](https://openairdocs.org/sdr/CALA2026060816912.md): Battery Pack · failed · Jun 4, 2026 · N659UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHT AT 2R DOESNT APPEAR TO BE CHARGING REMOVED AND REPLACED BATTERY PACK ON EMERGENCY LIGHT AT 2R. OPS CHECK GOOD.PARTS USED: 78-2525-3-0058, QTY:1
- [SDR CALA2026060116697](https://openairdocs.org/sdr/CALA2026060116697.md): Light · broken · May 29, 2026 · N659UA · Boeing 767322 · Emergency Lighting
  > DURING INSPECTIN WAS OBSERVED EMERGENCY ESCAPE PATH LIGHTING (EEL) BROKED AT SEAT 50F. IT WAS REPLACED PATH LIGHT AT SEAT 50F IN REFER AMM 33-51-10/201. ITEM RELEASED TO USE.
- [SDR CALA2026060116694](https://openairdocs.org/sdr/CALA2026060116694.md): Lamp · burned out · May 29, 2026 · N659UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHT NEAR AFTER RT DOOR IS BURNED. IT WAS REPLACED EMERGENCY LAMP IN REFER AMM 33-51-00/201. ITEM RELEASED TO USE.
- [SDR CALA2026020213493](https://openairdocs.org/sdr/CALA2026020213493.md): Shutoff Valve · faulted · Jan 30, 2026 · N659UA · Boeing 767322 · Pneumatic Distribution System
  > RIGHT ENG BLEED & RT PACK OFF CAUTION LIGHTS ILLUMINATED AFTER TAKEOFF. UPON ARRIVAL OF AIR RETURN, ACCOMPLISHED AIR SUPPLY BITE MODULE TEST IAW FIM 36-20 FT 804 & RT PRSOV FAULT LIGHT ILLUMINATED. REMOVAL OF RT PRSOV ACCOMPLISHED ON LP 7776435, OPS TESTED
- [SDR CALA2025100909836](https://openairdocs.org/sdr/CALA2025100909836.md): Elec Connector · broken · Oct 8, 2025 · N659UA · Boeing 767322 · Light System Wiring
  > EMERGENCY CEILING LIGHT CONNECTER BROKEN AT RT CEILING PANEL AT SEAT ROWS 36, 37, 38. R & R CONNECTOR REF WDM 33-51-12, SWPM 20-61-28, N0542-D73, AMM 33-51-00. OPS CHECK GOOD.
- [SDR CALA2025100809785](https://openairdocs.org/sdr/CALA2025100809785.md): Light Sys · no discrepancy · Oct 6, 2025 · N659UA · Boeing 767322 · Emergency Lighting
  > DOOR 2R EMER EXIT LIGHT IS ON WHEN THE MASTER SWITCH IN FLIGHT DECK IS OFF WITH MASTER EMERGENCY LIGHT SWITCH OFF, DOOR 2R EMER EXIT LIGHT REMAINS OFF. EMERGENCY LIGHTING OPS CHECK REF AMM 33-51-00 PERFORMED SEVERAL TIMES; LIGHTS ARE FUNCTIONING AND EXTINGUISH
- [SDR CALA2025090808606](https://openairdocs.org/sdr/CALA2025090808606.md): Access Panel · missing · Sep 5, 2025 · N659UA · Boeing 767322 · Nacelle/Pylon, Plate/Skin
  > DURING WALK AROUND, NR 2 ENG PYLON OTBD PANEL 446AR FOUND MISSING.
- [SDR CALA2025072806952](https://openairdocs.org/sdr/CALA2025072806952.md): Cable · out of adjust · Jul 24, 2025 · N659UA · Boeing 767322 · Emergency Equipment
  > RIGHT OVERWING SLIDE, NITROGEN BOTTLE ACTIVATION CABLE. REMOVED FOR REPLACEMENT PART NUMBER VERIFICATION PRIOR TO INSTALL VERIFIED RT OFFWING ESCAPE SYS INFLATION CABLE P/N REF IPC 25-65-02-01. INSTALLED THE NEW RIGHT HAND OFF WING SCAPE SYSTEM INFLATION CABL
- [SDR CALA2025072806951](https://openairdocs.org/sdr/CALA2025072806951.md): Actuator · faulted · Jul 24, 2025 · N659UA · Boeing 767322 · Escape Slide
  > RIGHT OFF-WING ESCAPE SLIDE OPERATIONAL CHECK {B767-25-3-7036} - RIGHT OVERWING DOOR LATCH ACTUATOR REQUIRES REPLACEMENT. MARKED FOR RII REQUEST CLEARANCE TO INSTALL. IPC REFERENCE # MFG SN OFF NOT ON AC ACTUATOR, ASSY OFF 76-2565-9-0003 4625 ON 76-2565-9-0
- [SDR CALA2025072806955](https://openairdocs.org/sdr/CALA2025072806955.md): Cable · stretched · Jul 23, 2025 · N659UA · Boeing 767322 · Emergency Equipment
  > RIGHT OFF-WING ESCAPE SLIDE OPERATIONAL CHECK - SLIDE FAILS TO INFLATE. NR 7 SPOILER SQUIB, LATCH ACTUATOR AND BOTH DOOR ACTUATORS BLEW BUT BOTTLE FAILED TO PRESSURIZE SLIDE TO INFLATE AND DEPLOY. INSPECTED CAUSE OF SLIDE NON-INFLATION AND FOUND CROSS PIN TWI
- [SDR CALA2025070906410](https://openairdocs.org/sdr/CALA2025070906410.md): Light · no test · Jul 8, 2025 · N659UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - DURING OPERATIONAL CHECK WAS FOUND AFTER EXTERNAL LIGHT SIDE RIGHT DOOR 2RH INOP. IT WAS SLIDE AND OVERWING ESCAPE LIGHT LAMP REPLACEMENT AFTER DOOR RIGHT 2RH AS PER AMM-TASK 33-51-06-902-082, CHECKED OK.
- [SDR CALA2025061205525](https://openairdocs.org/sdr/CALA2025061205525.md): Guard · damaged · Jun 10, 2025 · N659UA · Boeing 767322 · Emergency Lighting
  > FOUND FLT DECK EMERGENCY LIGHT SWITCH GUARD DAMAGED. REPLACED EMERGENCY LIGHT SWITCH GUARD ON FLTDE K PVERHEAD PANEL, OPS CHECKS GOOD.
- [SDR CALA2025060105153](https://openairdocs.org/sdr/CALA2025060105153.md): Panel · missing · Jun 1, 2025 · N659UA · Boeing 767322 · Nacelle/Pylon, Main Frame
  > PDA 2 REF LP 5040261, #1 ENGINE PANEL 436BR MISSING UPON ARRIVAL. REF LP 5039727, GOING TO APPLY CDL 54D INSTALLED INBOARD ACCESS DOOR ON #1 ENG PYLON IN REF TO AMM 54-53-00 PARTS USED: 76-5453-3-0063,QTY:1
- [SDR CALA2025051604737](https://openairdocs.org/sdr/CALA2025051604737.md): Transmitter · faulted · May 14, 2025 · N659UA · Boeing 767322 · Hydraulic Quantity Indicator
  > L HYD QTY EICAS PRESSURE 3100 LEFT A/P DISCONNECTEDTECH SUPPORT UPDATE. REF WDM 29-33-11-2 TEST WIRING WITH A MEGGER FROM CONNECTOR D38 ON HYDRAULIC QUANTITY TRANSMITTER TO D4474P. SHAKE WIRES WHILE TESTING. BE SURE TO ISOLATE WIRING BEFORE TESTING. IADLM MACI
- [SDR CALA2025040303491](https://openairdocs.org/sdr/CALA2025040303491.md): Controller · failed · Apr 2, 2025 · N659UA · Boeing 767322 · Cabin Pressure Controller
  > STATUS CABIN ALT AUTO 1 PERFORMED CABIN PRESS CONTROLLER BITE PROCEDURE. AC MOTOR FAULT LIGHT CAME ON. REF FIM 21-31 FAULT TREE 803. CABIN ALT AUTO 1 INOP, VERIFIED MANUAL MODE WORK REQUESTING FOR DEFERRAL. STATUS CABIN ALT AUTO 1 CABIN PRESSURE CONTROL SYSTE
- [SDR CALA2025032803287](https://openairdocs.org/sdr/CALA2025032803287.md): Lens · broken · Mar 27, 2025 · N659UA · Boeing 767322 · Emergency Lighting
  > EPL LENS BROKEN FROM SEAT 49F IT WAS REMOVED AND REPLACED EPL LIGHT,OPERATINAL TEST GOOD. ITEM OK FOR SERVICE. REF CMM 25-21-53.
- [SDR CALA2025032803286](https://openairdocs.org/sdr/CALA2025032803286.md): Light · inoperative · Mar 27, 2025 · N659UA · Boeing 767322 · Emergency Lighting
  > EPL FROM SEAT 33F INOP REMOVED AND REPLACED EPL LIGHT REF CMM 25-21-53 OPS CHECK GOOD SYSTEM OK FOR SERVICE.
- [SDR CALA2025032803285](https://openairdocs.org/sdr/CALA2025032803285.md): Light · inoperative · Mar 27, 2025 · N659UA · Boeing 767322 · Emergency Lighting
  > EPL FROM SEAT 30 INOP REMOVED AND REPLACED EPL LIGHT FROM SEAT 30F OPS CHECK GOOD, SYSTEM OK FOR SERVICE. REF CMM 25-21-53.
- [SDR CALA2025032803284](https://openairdocs.org/sdr/CALA2025032803284.md): Lens · broken · Mar 27, 2025 · N659UA · Boeing 767322 · Emergency Lighting
  > 34F EPL LENS BROKEN REMOVED AND REPLACED EPL REF CMM 25-21-53 OPS CHECK GOOD SYSTEM OK FOR SERVICE.
- [SDR CALA2024122401641](https://openairdocs.org/sdr/CALA2024122401641.md): Girt Bar · fod · Dec 22, 2024 · N659UA · Boeing 767322 · Emergency Equipment
  > DOOR 1R SLIDE WILL NOT ARM FOLLOWING FIM 52-11-FAULT TREE 804 FOUND DEBRIS ON BOTTOM OF GIRT BAR, REMOVED DEBRIS, DOOR ARMED AND DISARMED WITH EASE
- [SDR CALA2024121601533](https://openairdocs.org/sdr/CALA2024121601533.md): Lamp · burned out · Dec 15, 2024 · N659UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - DURING THE EXTERNAL OPERATIONAL CHECK FOUND OF THE DOOR 2 RH INOP. REMOVED AND REPLACED THE SLIDE AND OVERWING ESCAPE LIGHT LAMP REPLACEMENT AS PER AMM-TASK 33-51-06-902-082, POSITION DOOR 2RH, CHECKED OK P
- [SDR CALA2024081200402](https://openairdocs.org/sdr/CALA2024081200402.md): Control Panel · unserviceable · Aug 10, 2024 · N659UA · Boeing 767322 · Lighting System
  > SMOKE AND FUMES IN FD WHEN TAKING RWY. AIRCRAFT BACK TO STAND AS SMIKE IN THE COCKPIT NOTICED - FOUND C B N6 OVERHEAD PANEL POPPED, WITH STRONG ELECTRICAL SMELL IN THE COCKPIT.SMELL NOTICED COMING OUT THE L BOTTOM OVHD PANEL, NEAR L RUNWAY TURNOFF LIGHT CTL SW
- [SDR CALA2024052401570](https://openairdocs.org/sdr/CALA2024052401570.md): Pcb · malfunctioned · May 21, 2024 · N659UA · Boeing 767322 · Navigation System Wiring
  > CREW REPORTS LOW SPEED AMBER BAND ON CAPTAINS SIDE EFIS AIRSPEED TAPE FLUCTUATING AND 30KT SPLIT WITH FO. ALL MACH AIRSPEED INDICATORS OPS NML. TO BE DEFERRED IAW MEL 3422BS DEFERRED IAW MEL 3422BS CAPT EFIS SPEED TAPE AIRSPEED INDICATION(S) INOPERATIVE. DUPL
- [SDR CALA2024051301433](https://openairdocs.org/sdr/CALA2024051301433.md): Control Valve · damaged · May 11, 2024 · N659UA · Boeing 767322 · Cabin Cooling System
  > R PACK OFF IN FLT UNABLE TO RESET HAD BOTH EICAS AND OVHD PAN EL PACK OFF LIGHT LOCKED FOR POSITIVE FIX FOUND PACK TEMP VALVE BAD WHILE PERFORMING RT PACK TEMP CONTROLLER BITE PER AMM 21-51 CONTROL VALVE FAULTED AGAIN. FOUND DAMAGE ON THE POSITION CONTROLLER P
- [SDR CALA2024043001275](https://openairdocs.org/sdr/CALA2024043001275.md): Switch · faulty · Apr 25, 2024 · N659UA · Boeing 767322 · Hydraulic Power System
  > CREW REPORTED ON APPROACH TO MUC, FLT HAD TO ACP GO-AROUND. DURING FLAP AND GEAR RETRACTION, CTR HYD DEMAND PUMP LOW PRESSURE LIGHT AND EICAS DISPLAYED. CREW SELECTED PUMP TO "ON" POSITION, LOW PRESS LIGHT AND EICAS REMAINED DISPLAYED. REQ TOMC APRVL TO DEF M
- [SDR CALA2024040200938](https://openairdocs.org/sdr/CALA2024040200938.md): Skin · cracked · Mar 28, 2024 · N659UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > SUPPORT TASK - EA5315-01152 OP 002, 1EA FASTENER HOLE FOUND CRACK ON BEAR STRAP AND 1EA FASTENER HOLE FOUND CRACK ON FUSELAGE SKIN AND BEAR STRAP ON RH SERVICE DOOR - TRANSFER REFER NON-ROUTINE WO.2843280 FUSELAGE SKIN REPAIRED ON RH SERVICE DOOR AFT LOWER CU
- [SDR CALA2024032800893](https://openairdocs.org/sdr/CALA2024032800893.md): Skin · corroded · Mar 28, 2024 · N659UA · Boeing 767322 · Wing, Plate/Skin
  > B767-53-3-7034 - CABIN - STA 852 L/H WING CENTER SECTION MOST O/B PRESSURE DECK SURFACE FOUND CORRODED AS RED MARK - TRANSFER REFER NON-ROUTINE WO.2885899 AND ORIGINATED BY CENTER SECTION WING UPPER SKIN AT STA 852 LH MOST O/B STR-U17 TO PART 2 BEFORE 22MAR202
- [SDR CALA2024032700874](https://openairdocs.org/sdr/CALA2024032700874.md): Skin · cracked · Mar 22, 2024 · N659UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > FUSELAGE LWR EXT SKIN BS 1214 S37L FOUND CRACKED. PERFORM INTERNAL HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTI THE REPAIR REFERENCING ECRA FIGURE 9. PART 3: PERMANENT REPAIR: ON OF THE SKIN AT THE CRITICAL FASTENER ROW ALONG THE EDGE OF PAR THE REPAIR ACCOMPL
- [SDR CALA2024032800892](https://openairdocs.org/sdr/CALA2024032800892.md): Skin · cracked · Mar 19, 2024 · N659UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > SUPPORT TASK - EA5315-01152 OP001, 1EA FASTENER HOLE FOUND CRACK ON FUS SKIN AND BEAR STRAP ON LH ENTRY DR. TRANSFER REF NON - ROUTINE WO.2843296 AND ORIG PAIR 1. SCUFF PLATE REMOVAL REQUIRED AS NECESSARY FOR INSPECTION IVERY OR 6000 MAXIMUM FLIGHT CYCLES FROM
- [SDR CALA2024032000794](https://openairdocs.org/sdr/CALA2024032000794.md): Stringer · corroded · Mar 19, 2024 · N659UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > AFT OF BULK CGO COMPT STA1540-1562 S39R FOUND CORROSION TRANSFER REF NON - ROUTINE WO.2907957. AFT OF BULK CGO COMPT STA1540-1562 STRINGER S39R REPAIRED IAW SRM53-00-03-2R-2 REPAIR2 FIG201 AND REPAIR FASTENER LOCATIONS INSTALLED IAW ECRA5300-03077 REV.
- [SDR CALA2024032000792](https://openairdocs.org/sdr/CALA2024032000792.md): Stringer · corroded · Mar 19, 2024 · N659UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > AFT OF BULK CGO COMPT STA1540-1562 S38R FOUND CORROSION TRANSFER REF NO - ROUTINE WO.2907940. AFT OF BULK CGO COMPT STA 1540-1562 STRINGER S-38R REPAIRED AS PER SRM53-00-03-2R-2 REPAIR 2 FIG 201 AND REPAIR FASTENER LOCATIONS INSTALLED AS PER EC/RA 5300-03077
- [SDR CALA2024032200830](https://openairdocs.org/sdr/CALA2024032200830.md): Beam · cracked · Mar 18, 2024 · N659UA · Boeing 767322 · Fuselage Main, Structure
  > 1EA CRACK FOUND AT STA325 LBL13 FLR BEAM WEB. STA325 FLR BEAM WEB LBL13" CRACK AREA REPAIRED IAW ECRA 5315-01207 REV.
- [SDR CALA2024032000796](https://openairdocs.org/sdr/CALA2024032000796.md): Floorbeam · corroded · Mar 18, 2024 · N659UA · Boeing 767322 · Fuselage Main, Floor Beam
  > B767-53-3-7062 CABIN -FWD ZONE FLR PNL P27 STA 325 LBL 33-55 FLR SUPPORT SURFACE FOUND CORRODED. FWD ZONE FLR PNL P27 STA325 LBL2"-LBL62" FLR BEAM UPR CHORD REPAIRED IAW SRM53-00-51-2R-1 REPAIR1 FIG201.
- [SDR CALA2024031200695](https://openairdocs.org/sdr/CALA2024031200695.md): Floorbeam · corroded · Mar 9, 2024 · N659UA · Boeing 767322 · Fuselage Main, Floor Beam
  > B767-53-3-7079 CABIN - AFT GAL AREA FLR PNL P136 FLR SUPPORT STA 1582 LBL 50 SCREW HOLE CORRODED AS RED MARK. TRANSFER REF NR HX WO.2894650 AND ORIGINATED BY EMP V927004. CAB - AFT GAL AREA FLR PNL P136 FLR BEAM REPAIRED IAW SRM53-00-51-2R-1 REPAIR1 FIG201 JUS
- [SDR CALA2024030700655](https://openairdocs.org/sdr/CALA2024030700655.md): Pressure Blkhd · dented · Mar 5, 2024 · N659UA · Boeing 767322 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD BS 1586 S35L-S36L FOUND DENTED. TRANSFER REF NON - ROUTINE WO.2955261.
- [SDR CALA2024030700656](https://openairdocs.org/sdr/CALA2024030700656.md): Frame · cracked · Feb 28, 2024 · N659UA · Boeing 767322 · Fuselage Main, Frame
  > BS 1809 RT FWD OUTER CHORD BTW STR 7R-8R FOUND 1EA CRACKED.
- [SDR CALA2023101303046](https://openairdocs.org/sdr/CALA2023101303046.md): Shutoff Valve · failed · Oct 10, 2023 · N659UA · Boeing 767322 · Fuel Controlling System
  > AIR RETURN FOR L ENG BLEED OFF/L PACK OFF PER IDT REQUIREMENTS, VERIFIED PROPER INSTALL OF E1 EEC PER AMM 73-21-04-404-016-N00. SLAVED NEW EEC RAN ENGINE, NO FIX, REINSTALLED ORIGINAL SERVICABLE EEC REF AMM 73-21-04-404-016-N00. FOLLOWED FIM 36-10 TASK 868, SW
- [SDR CALA2023101003016](https://openairdocs.org/sdr/CALA2023101003016.md): Shutoff Valve · faulty · Oct 8, 2023 · N659UA · Boeing 767322 · Pneumatic Distribution System
  > PIREP CLIMBING UP OUT OF FL210 AUDIBLE LOUD BANG. LT ENG ROLLBACK FROM CLIMB THRUST, ROLLOFF TO THE LEFT. COMPLETED COMPRESSOR STALL CHECKLIST. NO FAULT DURING CHECKLIST. PER POWERPLANT ENGINEERING, NEED TO PERFORM FIM 71-05 TREE 803. PERFORM #1 ENG HPC STAGE
- [SDR CALA2023092202849](https://openairdocs.org/sdr/CALA2023092202849.md): Fuel Cap · missing · Sep 20, 2023 · N659UA · Boeing 767322 · Fuel Storage
  > FUEL RECEPTACLE CAP LEFT MISSING. MEL 2821J REQUESTED. FUEL RECEPTACLE CAP LEFT PLACED ON MAL 2821J.DDP C/W. FUEL RECEPTACLE CAP LEFT MISSING. DEFERRED REF MEL 2821J FUEL CAP LANYARD ATTACHING BRACKET BROKEN. AIRPLANE ARRIVED WITH TWO RECTABLE CAPS. THIS CLEAR
- [SDR CALA2023032000816](https://openairdocs.org/sdr/CALA2023032000816.md): Lavatory · inoperative · Mar 20, 2023 · N659UA · Boeing 767322 · Waste Disposal System
  > ALL LAVS WILL NOT FLUSH ON ARRIVAL DISCOVERED BOTH TANKS FULLL AND FOUL INDICATION FLAGGED. DUMPED THE TANKS LAVS CAME ONLINE IMMEDIATELY.
- [SDR CALA2023031300726](https://openairdocs.org/sdr/CALA2023031300726.md): Hinge · missing · Mar 13, 2023 · N659UA · Boeing 767322 · Landing Gear System
  > PDA 3 LEFT FWD NOSEGEAR DOOR HINGE COVER MISSING OK, ITEM IS PREVIOUSLY DOCUMENTED SEECDL.
- [SDR CALA2022122603500](https://openairdocs.org/sdr/CALA2022122603500.md): Cap · missing · Dec 26, 2022 · N659UA · Boeing 767322 · Fuel Storage
  > DURING PRE-FUELING, FOUND LEFT FUEL TANK CAP MISSING. INSTALLED FUELING PANEL LEFT FUEL TANK CAP.
- [SDR CALA2022050901172](https://openairdocs.org/sdr/CALA2022050901172.md): Brake · broken · May 7, 2022 · N659UA · Boeing 767322 · Landing Gear Brake System
  > PDA 2 DURING ETOPS CHECK FOUND #5 BRAKE DAMAGED. BOTH PINS MISSING AND PIN HOUSING BENT AND AT LEAST ONE ROTOR MISSING (DAMAGED). DUE TO PDA LOG PAGE, NOTIFIED LINE MX CONTROL THAT A SDR FLAG MUST BE SET AND ESFR NEEDS TO BE FILED..
- [SDR CALA2022031000630](https://openairdocs.org/sdr/CALA2022031000630.md): Skin · damaged · Mar 10, 2022 · N659UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE STA1488 AT STR24L DAMAGE BY CATERING TRUCK C/W HFEC REF. NDT PART 6-51-00-19. NO CRACKS NOTED. VERIFIED MATERIAL. OK TO CONTINUE. VERIFIED FILLER MATERIAL. OK TO CONTINUE. INCORRECT MATERIAL NOTED. REMOVED DAMAGED AREA IN REF TO SRM 53-00-01-2R-
- [SDR CALA2022031000629](https://openairdocs.org/sdr/CALA2022031000629.md): Skin · damaged · Mar 10, 2022 · N659UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE STA 1488 AT STR34L DAMAGED BY CATERING TRUCK C/W HFEC REF. NDT PART 6-51-00-19. NO CRACKS NOTED. VERIFIED MATERIAL. OK TO CONTINUE. VERIFIED FILLER MATERIAL. OK TO CONTINUE. INCORRECT MATERIAL NOTED. REMOVED DAMAGED AREA IN REF TO SRM 53-00-01-2
- [SDR CALA2022021100363](https://openairdocs.org/sdr/CALA2022021100363.md): Smoke Detector · failed · Feb 10, 2022 · N659UA · Boeing 767322 · Smoke Detection
  > CARGO DET AIR STATUS STATUS MESSAGE "CARGO DET AIR" WILL NOT ERASE. COMPLIED WITH MEL VERIFED FAULT "FWD DET FAN" SEE PHOTO. CARD 2616E NOC DESK: 767 NAME: DM DATE: 05-FEB-22- FWD DET FAN FAULTED.. FWD CARGO COMPARTMENT REMAIN EMPTY. SE
- [SDR CALA2022020700322](https://openairdocs.org/sdr/CALA2022020700322.md): Circuit Card · power loss · Feb 7, 2022 · N659UA · Boeing 767322 · Fire Protection System
  > CARGO DET AIR STATUS POWER DROPPED CARGO DET AIR FWD MEL 2616E WILL CLEAR AFTER RESET RESET CBS ON P35 PANEL. RESET RELAY K331. MSG CLEARED. PER LP 7945651 ON MEL.
- [SDR CALA2021122902469](https://openairdocs.org/sdr/CALA2021122902469.md): Fitting · cracked · Dec 28, 2021 · N659UA · Boeing 767322 · Wing Structure
  > AD 2012-15-12, EA 5710-02220 REV.D OP 003 LH UNDERWING LONGERON FITTING TENSION BOLT HOLE INSP FOUND 3EA CRACKS AT 1ST LAYER COUNT FROM AFT TRANSFER REF. NON-ROUTINE ZGY511880 & ORIGINATED BY EMP V924733 RII APPROVED LH UNDERWING LONGERON FITTING (BATHTUB FITT

Next page: https://openairdocs.org/aircraft/N659UA/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 = 'N659UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N659UA/reports

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