# Service difficulty reports: N651UA

A list on [N651UA](https://openairdocs.org/aircraft/N651UA.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 · 341 reports

- [SDR CALA2026083119005](https://openairdocs.org/sdr/CALA2026083119005.md): Light · broken · Aug 27, 2026 · N651UA · Boeing 767322 · Emergency Lighting
  > ESCAPE PATH LIGHT ASSEMBLY ON SEAT 42D AND 30F ARE BROKEN. R & R ESCAPE PATH LIGHT ASSEMBLY ON SEAT 30F AND 42D IAW AMM 33-51-10-962-104. ESCAPE PATH LIGHT SYSTEM, GOOD FOR SERVICE.
- [SDR CALA2026083119003](https://openairdocs.org/sdr/CALA2026083119003.md): Lens · broken · Aug 27, 2026 · N651UA · Boeing 767322 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT L396 IS WITH LENS BROKEN. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT LENS IAW AMM 33-51-06-960-801. GOOD FOR SERVICE.
- [SDR CALA2026081818706](https://openairdocs.org/sdr/CALA2026081818706.md): Controller · faulty · Aug 18, 2026 · N651UA · Boeing 767322 · Cabin Cooling System
  > AT 30000 FT BOTH PACK TEMP AND PACK OFF LIGHTS ILLUMINATED, EICAS AUTO EVENT RECORDED. PERF. PACK TEMP. CONTROLLER BITE REF. FIM 21-51 FAULT TREE 803. NO FAULTS. OPERATED BOTH PACKS WITH APU BLEED AIR FOR 1 HOUR REF. AMM 21-00-00. UNABLE TO DUPLICATE FAULTS. P
- [SDR CALA2026062917401](https://openairdocs.org/sdr/CALA2026062917401.md): Skin · contaminated · Jun 26, 2026 · N651UA · Boeing 767322 · Ailerons
  > DURING ACCOMPLISHMENT OF THERMOGRAPHIC INSPECTION OF THE RT OTBD AILERON, IT WAS FOUND LIQUID INGRESS ON LOWER SURFACE, BETWEEN HINGE NR 2 AND HOIST FITTING.
- [SDR CALA2026062417309](https://openairdocs.org/sdr/CALA2026062417309.md): Skin · cracked · Jun 23, 2026 · N651UA · Boeing 767324 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN CRACKED, BTW BS 1809 - 1832, S36R. ALL STEPS OF THE REPAIR HAVE BEEN PERFORMED, NO ACTION REQUIRED.
- [SDR CALA2026070117513](https://openairdocs.org/sdr/CALA2026070117513.md): Skin · damaged · Jun 17, 2026 · N651UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > DUE TO NON ROUTINE 3493866 AND ECRA 5300-03218 REV. A PART 3: PERMANENT REPAIR, ITS NECESSARY TO COMPLY WITH B767 SRM 53-00-01-2R-1.ACCORDING TO NON ROUTINE 3493866 IT WAS ACCOMPLISHED PERMANENT R EPAIR ON THE UPPER FUSELAGE SKIN AT BS 522 AND 544, STR 6L & 7L
- [SDR CALA2026051816327](https://openairdocs.org/sdr/CALA2026051816327.md): Panel · damaged · May 17, 2026 · N651UA · Boeing 767322 · Emergency Equipment
  > 2R EMERGENCY LIGHT EVAC TOGGLE COVER IS POPPING OPEN. REPLACED DOOR 2R EMERGENCY EVAC SIGNAL PANEL REF. AMM 25-63-01 OPS CK GOOD.
- [SDR CALA2026030314294](https://openairdocs.org/sdr/CALA2026030314294.md): Control Module · faulted · Feb 28, 2026 · N651UA · Boeing 767322 · Flight Control System
  > STAB TRIM CAUTION ON EICAS NO MESSAGE ACTIVE ON ARRIVAL, PERFORMED TEST 65 NO FAULTS OBSERVED. FOUND ONE (1) FAULT BALL ON THE LT STABILIZER TRIM, AILERON LOCKOUT MODULE, RESET SYSTEM TEST PASSED. AS A PRECAUTION WILL REPLACED LT SAM.
- [SDR CALA2026021313765](https://openairdocs.org/sdr/CALA2026021313765.md): Battery · inoperative · Feb 9, 2026 · N651UA · Boeing 767322 · Emergency Lighting
  > SEAT ROW 43-48 LT, AISLE EMERGENCY LIGHTS INOPERATIVE. USING WIRING DIAGRAM N0706-D73 REV-. CONNECTOR D1982 PINS 9+11 TO GROUND IS 1.6 OHMS- NORMAL. TRIED NEW BATTERY PACK & POWER SUPPLY UNIT, NO HELP, RETURNED ORIGINAL UNITS. CHECKED SMALL FLOOR ACCESS P
- [SDR CALA2026021013685](https://openairdocs.org/sdr/CALA2026021013685.md): Light · no test · Feb 9, 2026 · N651UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHT FAILED TEST. LIGHT DOES NOT ILLUMINATE WITH TEST 1 SWITCH, PTT OK. RESEARCHING, NEED MORE INFO OR A PICTURE WOULD BE HELPFUL. TESTED GOOD, REFERENCE: 25-65-00/001 CONFIG 1
- [SDR CALA2025102710612](https://openairdocs.org/sdr/CALA2025102710612.md): Heat Exchanger · leaking · Oct 26, 2025 · N651UA · Boeing 767322 · Turbine Engine Oil System
  > RIGHT ENG LOST QTY AND PRESS. BOTH WENT TO ZERO. EICAS ENG OIL PRESS R CREW REPORTED QUICK DROP OF OIL QUANTITY ALONG WITH DECREASING OIL PRESSURE AND ENG WAS SHUTDOWN. ENG WINDMILL TIME APPROXIMATELY 25 MINUTES WITH ZERO PSI & ZERO QTY OBSERVED. INSPECT PER A
- [SDR CALA2025092909380](https://openairdocs.org/sdr/CALA2025092909380.md): Light · inoperative · Sep 26, 2025 · N651UA · Boeing 767322 · Emergency Lighting
  > OPERATIONAL TEST - EMERGENCY ESCAPE PATH LIGHTING (EEL) SYSTEM PERFORM OPERATIONAL CHECK - OBSERVED EMERGENCY LIGHT AT SEAT 37F AND 31D INOPERATIVE. REMOVED AND REPLACED REF CMM 25-21-53 OPS CHECK GOOD SYSTEM FOR SERVICE.
- [SDR CALA2025092609309](https://openairdocs.org/sdr/CALA2025092609309.md): Transmitter · faulted · Sep 24, 2025 · N651UA · Boeing 767322 · Engine Oil Quantity
  > LEFT ENGINE AT ZERO OIL QTY AT TAKEOFF. REMOVED AND REPLACED NR 1 ENG OIL QUANTITY TRANSMITTER IAW AMM 79-31-01. PERFORMED IDLE RUN ON BOTH ENGINES. OPS CHECKED GOOD, OIL QUANTITY DISPLAYS AS NORMAL.
- [SDR CALA2025091008752](https://openairdocs.org/sdr/CALA2025091008752.md): Autothrottle Sys · malfunctioned · Sep 7, 2025 · N651UA · Boeing 767322 · Auto Throttle System
  > AUTOTHROTTLES WOULD NOT ENGAGE WHEN AUTOTHROTTLE SWITCH PUSHED ON TAKE-OFF RESET TMC SERVO, TMC AC, AND TMC DC CB'S F 14,15, 16 PER AMM 22-32-00. CREW TO ATTEMPT ANOTHER T/O USING AUTOTHROTLLES.
- [SDR CALA2025091008739](https://openairdocs.org/sdr/CALA2025091008739.md): Anti-Ice Valve · faulted · Sep 6, 2025 · N651UA · Boeing 767322 · Engine Anti-Icing System
  > R ENG AI LIGHT WHEN SELECTED ON R&R ENGINE INLET THERMAL ANTI-ICE PRESSURE SWITCH REF AMM 30-21-01 REMOVED AND REPLACED THE #2 ENGINE NOSE COWL ANTI ICE SHUT OFF VALVE. PER AMM REF. 30-21-03 ENGINE RUN WAS PERFORMED. RIGHT ENGINE ANTI ICE LIGHT CHECKED GOOD AT
- [SDR CALA2025082608122](https://openairdocs.org/sdr/CALA2025082608122.md): Engine · leaking · Aug 23, 2025 · N651UA · Boeing 767322 · Turbine Engine Oil System
  > OIL QTY WENT TO ZERO OIL PRESSURE TO RED LINE & ENG SHUTDOWN. ONLY LEFT SIDE OF NR 1 ENGINE COATED WITH OIL. INBD SIDE WAS DRY. AFTER SPEAKING WITH CREW WHEN ACFT WAS COMING INTO IAD AT AROUND 6000FT LT ENGINE OIL QTY DROPPED TO ZERO FOLLOWED BY OIL PRESSUR
- [SDR CALA2025072907024](https://openairdocs.org/sdr/CALA2025072907024.md): Girt Bar · faulted · Jul 26, 2025 · N651UA · Boeing 767322 · Emergency Equipment
  > DOOR 1L DISARM BAR DOESNT STOW ALL THE WAY 52-11-00-862-001AND CLOSING THE ENTRY/SERVICE DOOR EXTERNALLY, TASK 52-11-00-862-002+OPENING THE ENTRY/SERVICE DOOR INTERNALLY, TASK 52-11-00-862-003 AND CLOSING THE ENTRY/SERVICE DOOR INTERNALLY, TASK 52-11-00-862-00
- [SDR CALA2025060305200](https://openairdocs.org/sdr/CALA2025060305200.md): Hose · collapsed · May 28, 2025 · N651UA · Boeing 767322 · Emergency Equipment
  > RIGHT OVERWING DOOR SLIDE INFLATION HOSE IS COLLAPSED APPROX 4 FOOT SECTION AS VIEWED FROM PANEL 198CR ADDING PARTS DISARMED AND INSTALLED SAFETY PIN FOR THE RIGHT-HAND OVERWING DOOR INFLATION CYLINDER PER AMM 25-65-00-042-001 REACTIVATED RIGHT HAND OVERWING D
- [SDR CALA2024062101878](https://openairdocs.org/sdr/CALA2024062101878.md): Frame · corroded · Jun 19, 2024 · N651UA · Boeing 767322 · Fuselage Main, Frame
  > DURING C-CK IN ILN (WILMINGTON, OH) AMES MAINTENANCE FOUND THE L WR CHORD CORRODED LOCATED AT STA 1809.5 BULKHEAD FRAME INSTALLATION(P/N-148T1150-1). CORROSION WAS COMMON TO THE VERTICAL & HORIZONTAL FLANGE AS SHOWN IN FIGURES. DAMAGE WAS RE MOVED BY BLENDING
- [SDR CALA2024061901873](https://openairdocs.org/sdr/CALA2024061901873.md): Fitting · worn · Jun 14, 2024 · N651UA · Boeing 767322 · Nacelle/Pylon, Bulkhead/Firewall
  > DURING C-CHECK, AMES MAINT DISCOVER ED 2 FASTENER HOLES ON NR 2 PYLON BULKHEAD FITTING WAS WORN & ELONGATED. BOTH INBD & OTBD FASTENER HOLES MEASURED 0.3125" DIA WITH DISTANCE BETWEEN HOLES MEASURING NG 0.250". ATTACHING ANGLE WAS CRACKED & REPLACED. AS T
- [SDR CALA2024061701827](https://openairdocs.org/sdr/CALA2024061701827.md): Access Door · corroded · Jun 14, 2024 · N651UA · Boeing 767322 · Accessory Compartment Doors
  > AFT FLIGHT CONTROLS BAY ACCESS DOOR 313AL IS CORRODED. REMOVED ALL CORRODED PARTS DEEMED OUT OF LIMITS AND INSTALLED NE W PARTS IAW B767 SRM 51-40-02 ALONG WITH BOEING DWG 148T6602. SE E NON-ROUTINE 170098-0300-0005 FOR DETAILS
- [SDR CALA2024061701826](https://openairdocs.org/sdr/CALA2024061701826.md): Bear Strap · cracked · Jun 14, 2024 · N651UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > L-1 DOOR CUTOUT AFT LOWER CORNER HAS A CRACK INDICATION IN BEARS TRAP ONLY AT THE LOWEST HOLE OUT OF FIVE LOCATIONS. REPAIRED CRACK IN L1 DOOR BEARSTRAP AT THE LOWEST HOLE OUT OF FIVE LOCATIONS IAW B767-300 SRM 53-10-01-2R-1 REPAIR 1.
- [SDR CALA2024061301791](https://openairdocs.org/sdr/CALA2024061301791.md): Bracket · cracked · Jun 11, 2024 · N651UA · Boeing 767322 · Nacelle/Pylon Miscellaneous Structure
  > BRACKETS AT AFT UPPER SIDE OF LOWER SKIRT FAIRING WHERE THE STIN GER PANEL ATTACHES FOUND TO BE CRACKED #2 PYLON. REF AMES NR 170098-0600-0110 AND WORK SHEET 83 REMOVED AND REPLACED 2 BRACKET ON THE NO 2 PYLON AFT LOWER SKIRT FAIRING WITH NEWLY FABRICATED BR
- [SDR CALA2024061301790](https://openairdocs.org/sdr/CALA2024061301790.md): Floor Support · corroded · Jun 11, 2024 · N651UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > CORROSION UNDER THE NUTPLATES ON THE LOWER SURF ACE OF THE ALC FLOOR SUPPORT, FROM STA.1329 TO STA.1351, RBL17.# 3449 REF AMES NR 170098-0100-0133 51-31-01-392-034. REMOVED CORROSION IN FLOOR SUPPORT FOUND TO BE REF EC/RA 5360-01811 REMOVED AND REINSTALLED ROL
- [SDR CALA2024061001763](https://openairdocs.org/sdr/CALA2024061001763.md): Floor Support · corroded · Jun 7, 2024 · N651UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > GEN ITEM: 63-5310-1-2512 (B767-53-3-7154) CORROSION ON THE LOWER SURFACE OF THE PANEL SUP PORTS/ INTERCOSTALS, IN THE "BOX" AREA, FROM STA.1153 TO STA.117 5, LBL24 TO RBL24, LOCATED JUST BELOW THE ALC FLOOR.#3422 FWD SUPPORT WAS REMOVED AND FOUND TO BE OUT OF
- [SDR CALA2024060701736](https://openairdocs.org/sdr/CALA2024060701736.md): Floor Support · loose · Jun 4, 2024 · N651UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > UPPER CABIN STA 1053 LBL 34 FLOOR SUPPORT LOOSE ON I/B SIDE, ATTACH HOLE IS ENLARGED.
- [SDR CALA2024060501710](https://openairdocs.org/sdr/CALA2024060501710.md): Angle · cracked · Jun 3, 2024 · N651UA · Boeing 767322 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON AFT OB INTERNAL "L" ANGLE CRACKED AT MOST UPPER FASTENER,
- [SDR CALA2024061301792](https://openairdocs.org/sdr/CALA2024061301792.md): Floor Support · corroded · Jun 2, 2024 · N651UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > CORROSION UNDEER THE NUTPLATES ON THE LOWER SURFACE OF THE ALC FLOOR SUPPORT FROM STA 1329 TO STA 1351 LBL19 NO 3447. REF AMES NR 170098-0100-0131 BLENDED CORROSION FOUND TO BE OUT OF LIMITS HAD TO FABRICATE NEW FLOOR SUPPORT IAW 47613FAAB01. SEE PARTIAL WORK
- [SDR CALA2024053001647](https://openairdocs.org/sdr/CALA2024053001647.md): Angle · cracked · May 30, 2024 · N651UA · Boeing 767322 · Nacelle/Pylon Miscellaneous Structure
  > GEN ITEM: EA 5700-03285 REV F OP 010 #2 PYLON OB AFT HYDRAULIC BAY "L" ANGLE IS CRACKED
- [SDR CALA2024053001648](https://openairdocs.org/sdr/CALA2024053001648.md): Skin · cracked · May 29, 2024 · N651UA · Boeing 767322 · Nacelle/Pylon, Plate/Skin
  > GEN ITEM: 63-5410-1-2501 #1 PYLON O/B SIDE ACCESS 436BL PYLON SKIN CRACKED FWD UPPER CORN ER & AFT CHAFE STRIP IS LOOSE/DAMAGED UPPER & LWR
- [SDR CALA2024052001533](https://openairdocs.org/sdr/CALA2024052001533.md): Web · cracked · May 19, 2024 · N651UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > AFTER REMOVING CAP (FLOOR SUPPORT) AT STA 1153 FOUND WEB TO BE CRACKED AT HOLE JUST INBD OF FRAME FITTING ON LH SIDE. REPAIRED CRACKED WEB AT STA 1153 IAW B767-300 SRM 51-70-13-0G-0 DETAIL II. SEE NONROUTINE 170098-0100-0268 FOR DETAILS
- [SDR CALA2024052001538](https://openairdocs.org/sdr/CALA2024052001538.md): Shear Tie · corroded · May 17, 2024 · N651UA · Boeing 767322 · Fuselage Internal Mounting Structure
  > GEN ITEM: 63-5310-1-2638 SHEAR TIE T-FITTING AT STA 1562 BTWN STRINGER 38R AND 38L IS COR RODED.REMOVED & REPLACED SHEAR TIE T-FITTING AT STA 1562 BTWN STR 38R AND 38L IAW B767 SRM 51-40-02 PARA 9. SEE NONROUTINE 170098-0100 -0084 FOR DETAILS
- [SDR CALA2024051001425](https://openairdocs.org/sdr/CALA2024051001425.md): Floor Support · cracked · May 7, 2024 · N651UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > GEN ITEM: 63-5310-1-2621 (B767-53-3-7055) NDT VERIFIED CRACK, IN BRACKET THAT ATTACHES TH E BULK CARGO FLOOR SUPPORT TO FRAME 1417, LOCATED ON THE FWD SID E OF FRAME 1417, AT RBL16.#3462
- [SDR CALA2024051001424](https://openairdocs.org/sdr/CALA2024051001424.md): Floor Support · cracked · May 7, 2024 · N651UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > GEN ITEM: 63-5310-1-2621 (B767-53-3-7055) NDT VERIFIED CRACK, IN BRACKET THAT ATTACHES TH E BULK CARGO FLOOR SUPPORT TO FRAME 1417, LOCATED ON THE FWD SID E OF FRAME 1417, AT RBL9.#3461
- [SDR CALA2023110303278](https://openairdocs.org/sdr/CALA2023110303278.md): Drive Assy · failed · Nov 1, 2023 · N651UA · Boeing 767322 · Weather Radar System
  > WEATHER RADAR FAILED. TRIED WX RADAR TRANSCEIVER, NO HELP, INSTALLED ORIGINAL - SHOWS "WX FAIL ANT" DRIVE, SCANNER- OFF 75-3443-9-0001 8782 ON 75-3443-9-0001 8778 DRIVE, SCANNER- OFF 75-3443-9-0001 8782 ON 0000 REMOVED AND REPLACED WRX RADAR PEDESTAL DRIVE SCA
- [SDR CALA2023101103031](https://openairdocs.org/sdr/CALA2023101103031.md): Buss · inoperative · Oct 2, 2023 · N651UA · Boeing 767322 · Electrical Power System Wiring
  > BOTH UTILITY BUSSES INOP. RESET CIRCUIT BRAKES P11T4 AND P11T31(UTL BUS L&R), SYSTEM OPERATES NORMAL.REF SSM 24-51-02.
- [SDR CALA2023081802573](https://openairdocs.org/sdr/CALA2023081802573.md): Door · damaged · Aug 12, 2023 · N651UA · Boeing 767322 · Engine Thrust Reverser
  > BLOCKER DOOR HONEYCOMB MISSING. REPORTING PARTS DEPARTING AIRCRAFT ON FLT #2206 APPROXIMATELLY 12X12 HONEYCOMB BLOCKER DOOR WAS R & R ON CDL NO DAMAGE FOUND C DUCT OR ENGINE. BLOCKER DOOR. NR 1 ENGINE INBOARD THRUST REVERSER C SECTION 1 EACH BLOCKER DOOR DA
- [SDR CALA2023051501520](https://openairdocs.org/sdr/CALA2023051501520.md): Floorbeam · corroded · May 14, 2023 · N651UA · Boeing 767322 · Fuselage Main, Floor Beam
  > CABIN STA 325 LBL 23 FLOOR BEAM SURFACE FOUND CORROSION,ORIGINAT ED BY EMP V902610,REF TO HAECO NON ROUTINE NO.9454610 EA 2500-1 2983 OP 002. PERFORMED BY EMP V902610, RII BY V905036. CABIN STA325 LBL23 FLO OR BEAM UPPER SURFACE CORROSION AREA REPAIRED AS PER
- [SDR CALA2023051501498](https://openairdocs.org/sdr/CALA2023051501498.md): Battery · discharged · May 12, 2023 · N651UA · Boeing 767322 · Emergency Lighting
  > REMOVE AND REINSTALL EMERGENCY LIGHT BATTERY PACK PREVENT ALL EM ERGENCY LIGHT BATTERY (P/N:AD2013-1A) LOW VOLTAGE REF HAECO NON- ROUTINE NO.9453799, EA 2500-13033 OP022 PERFORMED BY EMP V905488, IDT BY EMP V905449, REMOVED AND REINST AMM 33-51-07-612-056,AMM
- [SDR CALA2023051501490](https://openairdocs.org/sdr/CALA2023051501490.md): Connector · damaged · May 12, 2023 · N651UA · Boeing 767322 · Light System Wiring
  > CEILING EMERGENCY LIGHT CONNECTOR DAMAGE AT 20AB 23AB 35AB 38AB 41AB 44AB 47AB 49AB 2A 6L 4L 8L 23LK 30LK 33LK 35LK 38LK 44LK 47 LK 50LK - ORIGINATED BY EMP V905488 ON HAECO NR 9454640, RAISED FROM EA 4420-03294 REV D OP001. PERFORMED BY EMP V905488, IDT BY V9
- [SDR CALA2023051501489](https://openairdocs.org/sdr/CALA2023051501489.md): Charger · out of limits · May 12, 2023 · N651UA · Boeing 767322 · Emergency Lighting
  > L/H AISLE L323 AND L1049 EXIT SIGN LIGNT DIM REF HAECO NON-ROUTI NE NO.9454390,ORIGINATED BY EMP V905488, SPEC NO.B767-33-3-7004 PERFORMED BY EMP V905488,IDT BY EMP V905449, PERFORMED T/S AND AMM 33-51-07-402-010 REV.138 WIRING CHECK FOUND M737 POWER SUPPLY MA
- [SDR CALA2023051501506](https://openairdocs.org/sdr/CALA2023051501506.md): Floorbeam · corroded · May 12, 2023 · N651UA · Boeing 767322 · Fuselage Main, Floor Beam
  > CABIN STA 303 LBL 35 FLOOR BEAM SURFACE FOUND CORROSION,ORIGINAT ED BY EMP V902610,REF TO HAECO NON ROUTINE NO.9454611,EA 2500-12 983 OP 002. PERFORMED BY EMP V902610, RII BY V905036. CABIN STA 303 LBL35 FL OOR BEAM UPPER SURFACE CORROSION AREA REPAIRED AS PER
- [SDR CALA2023051201463](https://openairdocs.org/sdr/CALA2023051201463.md): Floorbeam · corroded · May 10, 2023 · N651UA · Boeing 767322 · Fuselage Main, Floor Beam
  > CABIN STA 303 LBL 35 FLOORBEAM SURFACE FOUND CORROSION, CABIN STA 303 LBL35 FL OOR BEAM UPPER SURFACE CORROSION AREA REPAIRED AS PER SRM 53-00- 51-2R-1 REV 122 AND ECRA 5315-01194 REV -.
- [SDR CALA2023051201462](https://openairdocs.org/sdr/CALA2023051201462.md): Floorbeam · corroded · May 10, 2023 · N651UA · Boeing 767322 · Fuselage Main, Floor Beam
  > CABIN STA 325 LBL 23 FLOOR BEAM SURFACE FOUND CORROSION, CABIN STA325 LBL23 FLO OR BEAM UPPER SURFACE CORROSION AREA REPAIRED AS PER SRM 53-00-5 1-2R-4 REV 122 AND ECRA 5315-01193 REV -.
- [SDR CALA2023050801415](https://openairdocs.org/sdr/CALA2023050801415.md): Lamp · unknown · May 8, 2023 · N651UA · Boeing 767322 · Emergency Lighting
  > R/H FWD WING SLIDE LIGHT L391 INOP - ORIGINATED BY EMP V905488 O N HAECO NR 9453840, SPEC NO.B767-33-3-7004. PERFORMED BY EMP V905488, REPLACED R/H FWD WING SLIDE LIGHT L391 LAMP AND NEW LAMP TEST FOUND PASS, AS PER AMM 33-51-06-902-082 REV 138.
- [SDR CALA2023050801419](https://openairdocs.org/sdr/CALA2023050801419.md): Lamp · unknown · May 8, 2023 · N651UA · Boeing 767322 · Emergency Lighting
  > R/H FWD DOOR SLIDE LIGHT L393 INOP - ORIGINATED BY EMP V905488 O N HAECO NR 9453842, SPEC NO.B767-33-3-7004. PERFORMED BY EMP V905488, REPLACED R/H FWD DOOR SLIDE LIGHT L393 LAMP AND NEW LAMP TEST FOUND PASS, AS PER AMM 33-51-06-902-082 REV 138.
- [SDR CALA2023050801418](https://openairdocs.org/sdr/CALA2023050801418.md): Connector · unknown · May 8, 2023 · N651UA · Boeing 767322 · Light System Wiring
  > CEILING PANEL EMERGENCY LIGHT CONNECTORS DAMAGE AT 2A, 5A, 7A, 9 A, 21AB, 30AB, 32AB, 2L, 4L, 6L, 8L 16LK, 21LK, 41LK - ORIGINATE D BY EMP V905488 ON HAECO NR 9454018, EA 4420-03294 REV D OP001 PERFORMED BY EMP V905488, REPLACED CEILING PANEL EMERGENCY LIGHT C
- [SDR CALA2023050801417](https://openairdocs.org/sdr/CALA2023050801417.md): Lamp · unknown · May 8, 2023 · N651UA · Boeing 767322 · Emergency Lighting
  > R/H FWD OVERING EGRESS LIGHT L394 INOP - ORIGINATED BY EMP ON HAECO NR 9453843, SPEC NO.B767-33-3-7004. PERFORMED BY EMP REPLACED R/H FWD OVERWING EGRESS LIGHT L394 LAMPS AND NEW LAMPS TEST FOUND PASS, AS PER AMM 33-51-06-9 02-082 REV 138.
- [SDR CALA2023050801416](https://openairdocs.org/sdr/CALA2023050801416.md): Lamp · unknown · May 8, 2023 · N651UA · Boeing 767322 · Emergency Lighting
  > L/H AFT DOOR ERMERGENCY SLIDE LIGHT L397 INOP - ORIGINATED BY EM P V905488 ON HAECO NR 9453836, SPEC NO.B767-33-3-7004. PERFORMED BY EMP V905488, REPLACED L/H AFT DOOR EMERGENCY SLIDE LIGHT L397 LAMP AND NEW LAMP TEST FOUND PASS, AS PER AMM 33-51-0 6-902-082 R
- [SDR CALA2022090902317](https://openairdocs.org/sdr/CALA2022090902317.md): Rivet · missing · Sep 9, 2022 · N651UA · Boeing 767 · Nacelle/Pylon, Main Frame
  > PDA 3 DURING WALKAROUND FOUND 3 MISSING RIVETS AND 3 LOOSE RIVETS AT #2 ENGINE PYLON AFT AREA BY ENGINE EXHAUST. PHOTOS ADDED. REMOVED AND REPLACE LOOSE RIVETS ON AFT ENGINE. PYLON PER SRM 51-50-02.

Next page: https://openairdocs.org/aircraft/N651UA/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 = 'N651UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N651UA/reports

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