# Service difficulty reports: N649UA

A list on [N649UA](https://openairdocs.org/aircraft/N649UA.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 · 271 reports

- [SDR CALA2026091419394](https://openairdocs.org/sdr/CALA2026091419394.md): Light · inoperative · Sep 12, 2026 · N649UA · Boeing 767322 · Emergency Lighting
  > FWD AND AFT EMERGENCY LIGHT PATH AT SEAT 20F ON THE RIGHT SIDE IS OUT. ALREADY ORDERED THE NEW LIGHT ASSEMBLYS R & R FWD EMERGENCY PATH LIGHT. FWD AND AFT OPS CHECK GOOD REF AMM 33-51-10
- [SDR CALA2026090819307](https://openairdocs.org/sdr/CALA2026090819307.md): Wheel · vibration · Sep 5, 2026 · N649UA · Boeing 767322 · Wheel/Ski/Float
  > EXCESSIVE NOSE WHEEL AREA AND FLIGHT CONTROL VIBRATIONS AFTER TAKE-OFF.
- [SDR CALA2026083119025](https://openairdocs.org/sdr/CALA2026083119025.md): Relief Valve · faulted · Aug 29, 2026 · N649UA · Boeing 767322 · Cabin Pressure Control System
  > THUMPING NOISE AT DOOR 1R INFLIGHT. DURING A DETAILED VISUAL INSPECTION OF R1 DOOR, FOUND LOWER DOOR BUSTLE DETACHED & LOOSE ON FWD SIDE. BUSTLE RESECURED IAW AMM 25-66-01-416-010. WHILE CARRING OUT THE EXCESSIVE CABIN PRESSURE LEAKAGE TEST IAW AMM 05-51-2
- [SDR CALA2026083119023](https://openairdocs.org/sdr/CALA2026083119023.md): Outflow Valve · faulted · Aug 29, 2026 · N649UA · Boeing 767322 · Pressure Regulator/Outflow Valve
  > CABIN ALT AUTO 1 EICAS M THE AUTOMATIC PRESSURIZATION CONTROLLER 1 BITE FOUND A FAILURE. CABIN ALT UP TO APPROX 13000 FEETAS PER TOMC REQUEST REPLACED CABIN AUTO 1 PRESSURE CONTROLLER IAW AMM 21-31-02-004-00 & AMM 21-31-02-404-005 UP TO SECTION 3(D)1. REPLACE
- [SDR CALA2026081418625](https://openairdocs.org/sdr/CALA2026081418625.md): Actuator · faulty · Aug 11, 2026 · N649UA · Boeing 767322 · Pressure Regulator/Outflow Valve
  > CABIN ALTITUDE EICAS WARNING. CABIN ALTITUDE 10000 FT PILOTS REPORT EICAS WARNING AT FL330. AT THE TIME CABIN PRESSURE SHOWED 10000 WITH DIFFERENTIAL PRESSURE AT 7. ON DESCENT TO FL320 CABIN PRESSURE SHOWED 8500 WITH DIFFERENTIAL REMAINING AT 7. PERFORMED B
- [SDR CALA2026052516492](https://openairdocs.org/sdr/CALA2026052516492.md): Stringer · corroded · May 22, 2026 · N649UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > BULK CARGO COMPARTMENT: CORROSION FOUND AT S34L & BS 1562. PERFORMED STRINGER REPAIR IAW SRM 53-00-03-2R-2 REPAIR 2, DETAIL IV & EC/RA 5360-02139. PERFORMED INSPECTION OF THE STRINGER REPAIR IAW SRM 53-00-03-2R-2 REPAIR 2, DETAIL IV & EC/RA 5360-02139. PERF
- [SDR CALA2026052116448](https://openairdocs.org/sdr/CALA2026052116448.md): Stiffener · cracked · May 20, 2026 · N649UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > DURING REMOVAL OF FASTENERS BETWEEN BS 955 AND 977 RBL 54.75 ON THE ZEE CHORD CRACKS WERE FOUND IN TWO FASTENERS.. THE STEPS OF REPAIR HAVE BEEN PERFORMED ON NON ROUTINE 3389289. FOR THIS REPAIR WAS ISSUED ECRA 5350-02639. NO MORE MAINTENANCE IS REQUIRED. ALL
- [SDR CALA2026051716317](https://openairdocs.org/sdr/CALA2026051716317.md): Aileron · contaminated · May 15, 2026 · N649UA · Boeing 767322 · Ailerons
  > PERFORMING THERMOGRAFIC INSPECTION ON THE RH WING OUTBOARD AILERON IT WAS NOTICED MOISTURE INGRESSION INDICATION AT THE INBOARD END OF THE AILERON. PERFORMED UPDATE OF THE ATTRIBUTES TO MAJOR REPAIR AND IT WAS CREATED THE SFR, IT`S NECESSARY THE QC REVIEW THE
- [SDR CALA2026051116132](https://openairdocs.org/sdr/CALA2026051116132.md): Skin · contaminated · May 8, 2026 · N649UA · Boeing 767322 · Ailerons
  > PERFORMING THERMOGRAFIC INSPECTION ON THE LH WING OTBD AILERON IT WAS NOTICED MOISTURE INGRESSION INDICATION IN TWO POINTS OF THE AILERON, ONE AT THE INBD END OF THE AILERON AND ANOTHER ABOUT 15 INCHES FROM OF THE OTBD END. ALL THE STEPS WERE ACCOMPLISHED WIT
- [SDR CALA2025112811535](https://openairdocs.org/sdr/CALA2025112811535.md): Engine · fod · Nov 24, 2025 · N649UA · Boeing 767322 · Engine (Turbine/Turboprop)
  > IN CLIMB WITH CLIMB POWER SET EXCESSIVE VIBRATION LEFT ENGINE. 5.0 VIB WITH FEEL/SOUND.AFTER LANDING IT WAS FOUND AT THE ENGINE NR 1 SIGNALS OF BIRD STRIKE, WITH BLOOD AND STRONG SMELL OF BIRD. AFTER INSPECTION OF BIRD STRIKE REFER AMM 05-51-18-212-001, REMOV
- [SDR CALA2025103010723](https://openairdocs.org/sdr/CALA2025103010723.md): Handle · out of adjust · Oct 28, 2025 · N649UA · Boeing 767322 · Passenger/Crew Doors
  > DOOR 1R YELLOW. EMERG EXIT. FLAG POPS UP BEHIND VICE IN FRONT OF RED. PULL. HANDLE ADJUSTED DOOR 1R YELLOW EMERGENCY FLAG SO THE FLAG GOES INTO ITS PROPPER POSITION ADD EMP: U376824
- [SDR CALA2025100709726](https://openairdocs.org/sdr/CALA2025100709726.md): Lamp · no test · Oct 6, 2025 · N649UA · Boeing 767322 · Emergency Lighting
  > OPERATIONAL TEST - EMERGENCY ESCAPE PATH LIGHTING (EEL) SYSTEM PERFORM OPERATIONAL CHECK - PATH LIGHT 6D DOESN'T WORK. REMOVED AND REPLACED LAMP ASSY REF 33-51-10-962-105, GOOD FOR SERVICE.
- [SDR CALA2025092909390](https://openairdocs.org/sdr/CALA2025092909390.md): Control Module · faulted · Sep 25, 2025 · N649UA · Boeing 767322 · Cabin Cooling System
  > AFTER TO ALL FWD GALLEY OVENS AND CHILLERS INOP. AFT R COFFEPOT INOP OPERATED GALLEY OVENS/CHILLERS FOR APPROX 25 MIN AT HIGH PWR UNABLE TO DUP. PLEASE CHECK KVA SETTING OF FWD ELCU PER NAT DRAWING N0542-D73 WD 25-31-11, PINS 11 & 14 ARE JUMPERED. IF NO DEFECT
- [SDR CALA2025091108768](https://openairdocs.org/sdr/CALA2025091108768.md): Light · broken · Sep 10, 2025 · N649UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHTS OPERATIONAL CHECK, EMERGENCY LIGHT ON SEATS 35F AND 48F ARE BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT ON SEATS 35F AND 48F REF CMM 25-21-53. GOOD FOR SERVICE.
- [SDR CALA2025021002269](https://openairdocs.org/sdr/CALA2025021002269.md): Sign · damaged · Feb 6, 2025 · N649UA · Boeing 767322 · Emergency Lighting
  > 30R EXIT ROW PLASTIC NOT SECURED BRACKET FOR LENS COVER IS DAMAGED. INSTALLED TAPE TO SECURE IN PLACES WAITING ON ECRA FOR SIGN OFF. PICTURES ADDED COMPLIED WITH ECRA 3351-01489 PART 1 AND 2 INITIATED DIP TO COMPLY WITH PART 3 IN 3 FLIGHT CYCLES OK TO CARRY FO
- [SDR CALA2025012301978](https://openairdocs.org/sdr/CALA2025012301978.md): Engine · bird ingestion · Jan 20, 2025 · N649UA · Boeing 767322 · Turbine Engine Compressor Section
  > REJECTED T/O ENG SRG D2 PSBL BIRD INGEST RT ENG SPEED 160 HIGHE ST BTMS 9+ CREW DEBRIEF: 160 KTS, APPROACHING T/O SPEEDS, SAW BIRD FLY IN F RONT OF ACFT, HEARD A BANG ON E2, OBSERVED MOMENTARY DROP AND RE COVERY OF EPR. CAPT SIMULTANEOUSLY THROTTLED DOWN FOR
- [SDR CALA2024070500138](https://openairdocs.org/sdr/CALA2024070500138.md): Trim Switch · faulted · Jul 1, 2024 · N649UA · Boeing 767322 · Stabilizer Position Indicating
  > STAB TRIM EICAS CAME ON ON INIT CLIMBOUT PERFORMED TROUBLESHOOTING PROCEDURE FOR STAB TRIM REF FIM 27-48 TASK 809, FAULTING LEFT HYDRAULIC BRAKE PRESSURE SWITCH STAB TRIM MESSAGE NO LONGER ACTIVE REFERENCE LOG PAGE 8475892 FOR ACTION TAKEN. LEFT HYDRAULIC BRAK
- [SDR CALA2024032900909](https://openairdocs.org/sdr/CALA2024032900909.md): Battery Pack · inoperative · Mar 25, 2024 · N649UA · Boeing 767322 · Passenger Compartment Lighting
  > CABIN LIGHTING OPERATIONAL CHECK {B767-33-3-7008} - DIRECT CELING LIGHT AT POSITION 10A, 10D, 10D INOPERATIVE REPLACED THE LAMP REF AMM TASK 33-22-00-962-036 NO HELP.MEL DIRECT CELING LIGHT AT POS ITION 10A, 10D, 10L(CORRECTION) 3321A NEED MORE TIME TO FURTHER
- [SDR CALA2024011200093](https://openairdocs.org/sdr/CALA2024011200093.md): None · none · Jan 10, 2024 · N649UA · Boeing 767322 · Standard Practices/Structures
  > PASSENGER AT SEAT 9L LOST LAPTOP DOWN THE SIDEWALL. LAPTOP WAS POWERED UP AT THE TIME IT WAS LOST LAPTOP WAS FOUND AND RETURNED TO PAX AT. 9L.
- [SDR CALA2023080702431](https://openairdocs.org/sdr/CALA2023080702431.md): Relay · damaged · Aug 4, 2023 · N649UA · Boeing 767322 · Lighting System
  > ELETRICAL BURNING ODOR FROM FWD GALLEY/FWD PORTION OF FIRST CLASS 10 MINUTES INTO FLIGHT. PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-56-940-801-C1. FOUND SIDEWALL LIGHT BALLAST AT SEAT 1A TO BE SOURCE OF ELEC ODOR. NEEDS BALLAST 76-3321-3-0013. R+R BALLAST
- [SDR CALA2023062602029](https://openairdocs.org/sdr/CALA2023062602029.md): Pressure Switch · no test · Jun 24, 2023 · N649UA · Boeing 767322 · Hydraulic Power System
  > RAT DID NOT PRESSURIZE CENTER HYDRAULIC SYSTEM. RAM AIR TURB MODULE PRESSURE SWITCH REPLACED AND TEST RESULT NORMAL AS PER AMM 29-21-11 AMD 29-21-00. WORK ACCOMP BY MECH V924756 INSP BY V924743. ADD EMP:V924743
- [SDR CALA2023062301990](https://openairdocs.org/sdr/CALA2023062301990.md): Skin · corroded · Jun 22, 2023 · N649UA · Boeing 767322 · Wing Structure
  > B767-28-3-0067, RHW FUEL TANK OVERWING FILL PORT ATTACH UPPER SKIN FOUND CORROSION REF HX NR WO.1865480, ORIG BY V897897 RHW FUEL TANK OVERWING FILL PORT UPPER SKIN PANEL CORROSION REPAIRED AS PER ECRA 5725-01126 REV.- ATTACHED MAINTENANCE WORK SHEET FORM 44.
- [SDR CALA2023062301989](https://openairdocs.org/sdr/CALA2023062301989.md): Skin · cracked · Jun 22, 2023 · N649UA · Boeing 767322 · Service Doors
  > SUPPORT TASK - EA5315-01152 OP 002 1EA FASTENER HOLE FOUND CRACK AT 2O''CLOCK AND 8O''CLOCK (COUNT FROM INBOARD) ON FUSELAGE SKIN LAYER- TRNAFER REFER NON-ROUTINE WO.1843964 AND ORIGINATED BY V924735 RII INSPECTED OKAY BY HX 310582 ADD EMP:V896895 FUSELAGE SKI
- [SDR CALA2023062301988](https://openairdocs.org/sdr/CALA2023062301988.md): Skin · cracked · Jun 22, 2023 · N649UA · Boeing 767322 · Passenger/Crew Doors
  > SUPPORT TASK - EA3515-01152 OP001 - 1EA FASTENER HOLE FOUND CRACK AT 8O''CLOCK (COUNT FROM INBOARD) ON FUSELAGE SKIN LAYER TRANSFER REFER NON-ROUTINE WO.1843962 AND ORIGINATED BY EMP V924735 RII INSPECTED OKAY BY HX 310582 ADD EMP:V896895 FUSELAGE SKIN DOOR 1L
- [SDR CALA2023062201976](https://openairdocs.org/sdr/CALA2023062201976.md): Intercostal · corroded · Jun 21, 2023 · N649UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7025 - FWD CARGO COMPT STA595 RH PDU LH AND RH MOUNT NUTS SUPPORT BEAMS FOUND CORROSION TRANSFER REF HXWO 1858999 AND ORIGINATED BY EMP V896810 FWD CARGO COMPT STA588-610 RBL33 SUPPORT BEAM (143T0019-11) (MINOR REPAIR) ATTACH MAINTENANCE WORK SHEET F
- [SDR CALA2023062101965](https://openairdocs.org/sdr/CALA2023062101965.md): Channel · corroded · Jun 20, 2023 · N649UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7023, FWD CGO COMPT- STA 478 TO 500, RBL 33" LONGITUDINAL FLR SUPPORT LWR SURFACE FOUND CORROSION CRACK TRANSFER REF HXWO 1883016 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA470 TO STA498 RBL30" LONGITUDINAL FLOOR WORK ACCOMPLISHED BY MECHANIC V
- [SDR CALA2023062101964](https://openairdocs.org/sdr/CALA2023062101964.md): Intercostal · corroded · Jun 20, 2023 · N649UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7025 FWD CGO BTW STA 527 - STA 544 UNDER GR PDU INTERNAL 2EA WEB SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1858981 AND ORIGINATED BY EMP V896375 FWD CARGO STA524-541 RBL33.08 FLOOR SUPPORT BEAM REPLACED WORK ACCOMPLISHED BY MECHANIC V897467 INSP
- [SDR CALA2023062101950](https://openairdocs.org/sdr/CALA2023062101950.md): Unknown · corroded · Jun 20, 2023 · N649UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7025 FWD CGO COMPT STA 583 RH PDU LH MOUNT NUT SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1858982 AND ORIGINATED BY EMP V896810 FWD CARGO COMPT STA583 RBL30-RBL40 SUPPORT BEAM REPLACED WORK ACCOMPLISHED BY MECHANIC V897467 INSPECTED BY V896375 AS
- [SDR CALA2023062101969](https://openairdocs.org/sdr/CALA2023062101969.md): Unknown · corroded · Jun 19, 2023 · N649UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7025 FWD CGO BTW STA 500 - 522 R/H TORQUE BOX WEB FOUND CORROSION TRANSFER REF HXWO 1858980 AND ORIGINATED BY EMP V896375 FWD CARGO STA497 TO STA541 RBL25 TO RBL40 TORQUE BOX WEB WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V898550 REPLACED AS
- [SDR CALA2023061901914](https://openairdocs.org/sdr/CALA2023061901914.md): Fastener · damaged · Jun 16, 2023 · N649UA · Boeing 767322 · Cargo/Baggage Doors
  > SUPPORT TASK FWD CARGO COMPT DOOR EXTERIOR FASTENER HAS LIGHTNING STRIKE 65" FROM AFT & 46" FROM LOWER EDGE TRANSFER REF HXWO 1857673 AND ORIGINATED BY EMP V896888 FWD CARGO COMPT DOOR EXTERIOR SKIN STA552 INTERIM REPAIRED AS PER ECRA 5232-01174 REV - PART 1 A
- [SDR CALA2023061901913](https://openairdocs.org/sdr/CALA2023061901913.md): Web · corroded · Jun 16, 2023 · N649UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > B767-06-3-7050, FWD CGO COMPT STA 592 "9R" PDU BELOW MOUNTING SUPPORT BRACKET SHEAR WEB AREA FOUND CORROSION TRANSFER REF HXWO 1878888 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA541-STA600 RBL25 TO RBL40 FLOOR BEAM WEB WORK ACCOMPLISHED BY MECHANIC V8975
- [SDR CALA2023061901912](https://openairdocs.org/sdr/CALA2023061901912.md): Skin · damaged · Jun 16, 2023 · N649UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > B767-06-3-7083 - FUSELAGE SKIN HAS LIGHTNING STRIKE AT BS654+44-BS654+66 BTW S22R / S23R TRANSFER REF HXWO 1839295 AND ORIGINATED BY EMP V896888 FUSELAGE SKIN AT STA654+44 TO STA654+66 BETWEEN STR22R-23R WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V8963
- [SDR CALA2023061601884](https://openairdocs.org/sdr/CALA2023061601884.md): Floor Support · corroded · Jun 16, 2023 · N649UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7023, FWD CGO COMPT- STA 498 RBL 39" LATERAL TORQUE BOX PNL SUPPORT CHORD LWR SURFACE FOUND CORROSION TRANSFER REF HXWO 1883060 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA498 RBL30 TO RBL40 LATERAL TORQUE BOX WORK ACCOMPLISHED BY MECHANIC V8975
- [SDR CALA2023061601883](https://openairdocs.org/sdr/CALA2023061601883.md): Intercostal · corroded · Jun 16, 2023 · N649UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7023, FWD CGO COMPT- STA 478 TO 500 RBL 39" LONGITUDINAL FLR SUPPORT LWR SURFACE FOUND CORROSION AS MARK TRANSFER REF HXWO 1883040 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA478 TO 497 RBL39" LONGITUDINAL FLOOR WORK ACCOMPLISHED BY MECHANIC V89
- [SDR CALA2023061601882](https://openairdocs.org/sdr/CALA2023061601882.md): Intercostal · corroded · Jun 16, 2023 · N649UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7025 - FWD CARGO FLOOR STA502-512 RBL36.88 SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1877224 AND ORIGINATED BY EMP V896810 FWD CARGO FLOOR STA502 TO STA512 RBL36.88 FLOOR SUPPORT BEAM WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 RE
- [SDR CALA2023061601881](https://openairdocs.org/sdr/CALA2023061601881.md): Unknown · corroded · Jun 16, 2023 · N649UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7025 - FWD CARGO FLOOR STA512 RBL30-34 SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1877229 AND ORIGINATED BY EMP V896810 FWD CARGO FLOOR STA512 RBL30-40 SUPPORT BEAM REPLACED AS WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 PER SRM51-
- [SDR CALA2023061601880](https://openairdocs.org/sdr/CALA2023061601880.md): Unknown · corroded · Jun 16, 2023 · N649UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7023, FWD CGO COMPT STA 502 RBL 39" LATERAL TORQUE BOX PNL SUPPORT CHORD LWR SURFACE FOUND CORROSION TRANSFER REF HXWO 1883048 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA502 RBL30 TO RBL40 LATERAL TORQUE BOX PANEL SUPPORT CHORD REPLACED AS PER
- [SDR CALA2023061601879](https://openairdocs.org/sdr/CALA2023061601879.md): Intercostal · corroded · Jun 16, 2023 · N649UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7025 FWD CGO COMPT STA 550 TR PDU LH MOUNT NUT SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1858966 AND ORIGINATED BY EMP V896510 FWD CARGO COMPT STA544-566 RBL25 AND RBL33.08 SUPPORT WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 BEAM
- [SDR CALA2023061601871](https://openairdocs.org/sdr/CALA2023061601871.md): Stringer · corroded · Jun 14, 2023 · N649UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7058 AFT OF BULK CGO BILGE STA 1540 S38L STRINGER FOUND CORROSION TRANSFER REF HXWO 1856266 AND ORIGINATED BY EMP V896810 BULK CARGO COMPT BILGE AREA STA1540 STRINGER 38L INTERIM REPAIRED AS PER ECRA 5361-01114 REV - PART 1 ATTCH FORM 44-0008 ITEM 1
- [SDR CALA2023061601870](https://openairdocs.org/sdr/CALA2023061601870.md): Skin · corroded · Jun 14, 2023 · N649UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7058 AFT OF BULK CGO BILGE STA 1540 S39 POS INNER SKIN FOUND CORROSION TRANSFER REF HXWO 1856087 AND ORIGINATED BY EMP V896810 FUSELAGE STA1540-STA1562 BETWEEN STR39L AND STR39R SKIN INTERIM REPAIRED AS PER ECRA5361-01114 REV - PART 1 ATTACH FORM 44-
- [SDR CALA2023061601869](https://openairdocs.org/sdr/CALA2023061601869.md): Stringer · corroded · Jun 14, 2023 · N649UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7058 AFT OF BULK CGO BILGE STA1540 TO STA1562 S39L STRINGER FOUND CORROSION TRANSFER REF HXWO 1856237 AND ORIGINATED BY EMP V896810 BULK CARGO COMPT BILGE AREA STA1540 TO STA1562 STRINGER 39L INTERIM REPAIRED AS PER ECRA 5361-01114 REV - PART 1 ATTAC
- [SDR CALA2023061201825](https://openairdocs.org/sdr/CALA2023061201825.md): Door Frame · cracked · Jun 11, 2023 · N649UA · Boeing 767322 · Fuselage Main, Structure
  > B767-06-3-7011 FWD CARGO: FWD CARGO DOOR AT STA 542 FRAME LOWER PORTION FOUND CRACKED TRANSFER REF HXWO 1851416 AND ORIGINATED BY EMP V898555 FWD CARGO DOOR STA542.4 FRAME INNER CHORD REPAIRED AS PER ECRA5234-01095 REV - ATTACH FORM 44.0008 ITEM 1 TO ITEM 19
- [SDR CALA2023061201821](https://openairdocs.org/sdr/CALA2023061201821.md): Floor Support · corroded · Jun 9, 2023 · N649UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > CABIN STA 303 LBL 40"-55" FLR SUPPORT CORRDED TRANSFER REF. NON-ROUTINE HX NRC WO.1843972 AND ORIGINATED BY EMP NO. V927576 CABIN STA 303 FLOOR BEAM LBL 40" - LBL 55" UPPER CHORD REPAIRED AS PER SRM 53-00-51-2R-1 REPAIR 1 FIG 201. ATTACHED FORM 44-0008 ITEM 1-
- [SDR CALA2022122803512](https://openairdocs.org/sdr/CALA2022122803512.md): Nipple · missing · Dec 28, 2022 · N649UA · Boeing 767322 · Waste Disposal System
  > PDA 3 VERBAL LAV SERVICE REPORT -- NIPPLE MISSING FOR LAV SERVICE -- SEE PHOTO PHOTO ADDED INSTALLED NEW LAV SERVICE NIPPLE. OK FOR SERVICE. CALLED LAV SERVICE TRUCK. REFERENCE 38-32-03-50.
- [SDR CALA2022070801675](https://openairdocs.org/sdr/CALA2022070801675.md): Egt Indication · warning message · Jul 8, 2022 · N649UA · Boeing 767322 · Cylinder Head Temperature (CHT) Indicating System
  > RT ENG HIGH EGT ON TAKE OFF. MAX EGT 737 SECONDS DURATION. DUE TO PREVIOUS HISTORY OF EGT FAULTS A POSITIVE FIX IS UNLOCKED FOR UPDATE. REQUIRED. PER CREW WHEN THROTTLES WERE PULLED BACK RIGHT ENGINE EGT DEBRIEF CREW, CAPTAIN STATED THAT ONCE THROTTLES BACK T
- [SDR CALA2022010500035](https://openairdocs.org/sdr/CALA2022010500035.md): Autothrottle Sys · failed · Jan 5, 2022 · N649UA · Boeing 767322 · Auto Flight System
  > AUTO THROTTLES FAILED TO ENGAGE ON TAKEOFF THRUST MANAGEMENT SYS (INCLUDING A/T SYS) PLACED ON MEL. MEL STICKER AND C/B COLLARED F16 ON THE P11. DOWNGRADED A/C TO "AUTOLAND LIMIT-LAND 2". DISPATCH DESK: 82 NAME: JERRY DATE: 02-JAN-22- NOC
- [SDR CALA2021110102015](https://openairdocs.org/sdr/CALA2021110102015.md): None · none · Oct 31, 2021 · N649UA · Boeing 767322 · Navigation System
  > AUTO THOTTLES WILL NOT ENGAGE. CREW DEBRIEFED, STATED NO FMA ON EADI. TRIED IN MULTIPLE MODES LOCKED FOR T/S. PER LP 7341532 R IDG STATUS MESSAGE. FURTHER DETAILS AWAITED
- [SDR CALA2021051900698](https://openairdocs.org/sdr/CALA2021051900698.md): Sensor · faulted · May 19, 2021 · N649UA · Boeing 767322 · Leading Edge Slat Position Indicating System
  > ON APP ICAS LE SLAT ASSY MESSAGE ON ICAS COMPLIED WITH QRH AND L ANDED BIT THE FSEU AND FOUND THE FOLLOWING FAULT: LE OUTBD ASYM MSG NO. 27-81021. FDE LE ASYM LATCHED. PRIMARY A/S <90 A-A02 FR PSEU, IB SLAT +1.21V, OB SLAT +5.54V, LRV POS -2.33V. INTERROGATED
- [SDR CALA2021051000632](https://openairdocs.org/sdr/CALA2021051000632.md): Hydraulic Line · leaking · May 10, 2021 · N649UA · Boeing 767322 · AC Indicating System
  > DURING CHECK NO 2 SERVICE HMG BLOCK 8 OPRATIONAL CHECK FOUND HYDRAULIC LEAK THRU BODY OF HMG. PERFORMED INTERIM REPAIR PER ECRA 2420-01623 PART 1. HYD LINES PLUGGED,UNIONS REMOVED NO LEAKS NOTED FROM HYDRAULIC LINES PRESSURIZED.INITIATE A DIP TO PERFORM PERMA
- [SDR CALA2021050600618](https://openairdocs.org/sdr/CALA2021050600618.md): Hydraulic System · leaking · May 6, 2021 · N649UA · Boeing 767322 · Hydraulic System, Main
  > IN REFERENCE LOG PAGE 625880 HMG INOP. IN REFERENCE LOG PAGE 6258880 HMG INOP DEFERRED PER MEL 2425A. ADD EMP:U288719,U235671 DISPATCH DESK: 76 HMG CAPPED DUE TO HYD LEAK PER ECRA 2420-01623 LOG PAGE 6258880. NO LEAKS WITH LINES AND HMG CAPPED 64-2425-9-0001

Next page: https://openairdocs.org/aircraft/N649UA/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 = 'N649UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N649UA/reports

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