# Service difficulty reports: N662UA

A list on [N662UA](https://openairdocs.org/aircraft/N662UA.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 · 337 reports

- [SDR CALA2026101220299](https://openairdocs.org/sdr/CALA2026101220299.md): Skin · damaged · Oct 7, 2026 · N662UA · Boeing 767322 · Ailerons
  > DURING THERMOGRAPHY INSPECTION OF OUTBOARD AILERON LH WAS FOUND WATER INGRESS INDICATION. PICTURES ATTACHED. AFTER THERMOGRAPHY INSPECTION WAS FOUND WATER INGRESSION ON LOWER SKIN. DAMAGED AREA WAS REMOVED & REPAIRED FOLLOWING SRM.DONE NEW INSPECTION ON REPA
- [SDR CALA2026083119076](https://openairdocs.org/sdr/CALA2026083119076.md): Skin · punctured · Aug 29, 2026 · N662UA · Boeing 767324 · Fuselage Main, Plate/Skin
  > PUNCTURE BETWEEN AFT CARGO DOOR AND R3 ENTRY DOOR ON THE RIGHT SIDE OF ACFT. DAMAGE LOCATED BTWN BS 1439 & 1461 IAW SRM 53-00-00-0G-0. FOUND DAMAGE TO BE 5.4 INCH LONG BY 2.6 INCH WIDE, ON BS 1439 - 1461, STR 21-22R. DAMAGE IS OUT OF LIMITS IAW SRM 53-00-
- [SDR CALA2025082208058](https://openairdocs.org/sdr/CALA2025082208058.md): Windshield · no discrepancy · Aug 20, 2025 · N662UA · Boeing 767322 · Flight Compartment Windows
  > BIRD STRIKE ON F/O WINDSHIELD AFTER TAKEOFF CREW REPORTED NO ENGINE INDICATION ISSUES. FOUND NO EVIDENCE OF A BIRD STRIKE ON F/O WINDSHIELD NOR ON CROWN AREA REF PICS OF A/C WHEN BLOCKED INTO GATE AND PIC TAKEN OF CROWN AREA. PERFORMED BIRDSTRIKE INSPECTION IA
- [SDR CALA2025073107181](https://openairdocs.org/sdr/CALA2025073107181.md): Unknown · odor · Jul 31, 2025 · N662UA · Boeing 767322 · Air Distribution System
  > AFTER ENG START, SELECTED PACKS ON HAD STRONG FUME ODORS IN BACK OF CABIN, REPORTED BY THE AFT CABIN AREA FLIGHT ATTENDANTS THAT WAS A FUEL ODOR AFTER ENG START FOR ABOUT 5 MINS UNTIL IT CLEAR OUT OF CABIN. REPORTED ONLY HAVING THIS ISSUE OUT OF LHR. VERIFI
- [SDR CALA2025073007077](https://openairdocs.org/sdr/CALA2025073007077.md): Slide · loose · Jul 27, 2025 · N662UA · Boeing 767322 · Escape Slide
  > DOOR 2L SLIDE PACK IS SUSPECTED TO HAVE BECOME LOOSE THUS MOVING THE BUSTLE COVER LOWER DOOR 2L SLIDE BUSTLE LOWER FWD LATCH BECAME DISENGAGED, BUSTLE REMOVED SLIDE PACK CHECKED IAW AMM 25-66-98-206-001, NO DEFECTS NOTED. SLIDE BUSTLE RE-FITTED, ARM/DISARM LEV
- [SDR CALA2025072806973](https://openairdocs.org/sdr/CALA2025072806973.md): Lamp · inoperative · Jul 26, 2025 · N662UA · Boeing 767322 · Emergency Lighting
  > RH AFT EXTERIOR EMERGENCY LIGHT NOT LIGHT DURING TEST. RH AFT SLIDE ESCAPE LIGHT LAMP REPLACED IAW AMM 33-51-06-902-082.
- [SDR CALA2025061205492](https://openairdocs.org/sdr/CALA2025061205492.md): None · none · Jun 9, 2025 · N662UA · Boeing 767322 · Standard Practices/Structures
  > DOOR BUSTLE INSPECTION POST INSTALL REF LOG 5137002 DOOR 1L BUSTLE INSTALLED AS PER AMM 25-66-01-424-070 RII INSPECTION REQUIRED RII OF PASSENGER SERVICE DOOR BUSTLE C/O REF AMM: 26-66-01-404-072. VERIFIED INSTALLED CORRECTLY, NO OTHER SYSTEMS DISTURBED. RENDE
- [SDR CALA2025060905386](https://openairdocs.org/sdr/CALA2025060905386.md): Wire · damaged · Jun 7, 2025 · N662UA · Boeing 767322 · Door System Wiring
  > DOOR 1R ENTRY DOOR POWER OPENING ASSIST HAS A INTERMITTENT FAULT ACTIVATING EMER LIGHTS WHEN DOWN MODE SWITCH PRESSEDCORRECTION DOOR 1L NOT DOOR 1R UPDATE - DOOR 1L ELECTRICAL CLOSING SWITCH ON FA PANEL AND EXTERNAL DOOR TOGGLE SWITCH WHEN SELECTED DOWN (CLOSE
- [SDR CALA2025060905383](https://openairdocs.org/sdr/CALA2025060905383.md): Lamp · inoperative · Jun 7, 2025 · N662UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - EXTERIOR D2L EMERGENCY LIGHT INOP D2L SLIDE EMERGENCY LIGHT LAMP REPLACED AS PER AMM 33-51-06-902-082. NOW OK.
- [SDR CALA2025060905382](https://openairdocs.org/sdr/CALA2025060905382.md): Lamp · inoperative · Jun 7, 2025 · N662UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - EXTERIOR RIGHT EMERGENCY LIGHT (FWD OF AFT CARGO) INOP MID RIGHT SLIDE LIGHT LAMP REPLACED AS PER AMM 33-51-06-902-082. NOW OK.
- [SDR CALA2025060905363](https://openairdocs.org/sdr/CALA2025060905363.md): Light · inoperative · Jun 7, 2025 · N662UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - ESCAPE PATH AISLE LIGHTING ON SEATS 38F, 39F AND 40F NOT ILLUMINATING ESCAPE PATH LIGHTS REPLACED AS PER CMM 25-23-52. PARTS USED: 29-3326-3-0013, QTY:1 ESCAPE PATH LIGHT FIXTURES INSPECTED AND CONFIRMED C
- [SDR CALA2025060405267](https://openairdocs.org/sdr/CALA2025060405267.md): Idg · faulted · Jun 3, 2025 · N662UA · Boeing 767322 · AC Generator-Alternator
  > AT CRUISE ALT, LEFT GEN DRIVE LIGHT FIRST THEN GEN OFF. 1X GEN OFF RESET FAILED REF FM 2.60.35 ON ARRIVAL LEFT IDG DELTA P POPPED OUT. IDG FILTER REMOVED AND FOUND CONTAMINATION. IDG REMOVAL/ INSTALLATION CARRIED OUT I.A.W AMM 24-11-01-004-002-006/ 24-11-01-40
- [SDR CALA2025051404672](https://openairdocs.org/sdr/CALA2025051404672.md): Warning Message · false activation · May 12, 2025 · N662UA · Boeing 767322 · Central Warning
  > IN FLT GOT MASTER CAUT AND LE SLAT ASYM EICAS MSG. COMPLIED W/ Q RH. CREW DEBRIEF: LE SLAT ASYM MSG ON SELECTION OF FLAPS 5, QRH COMPLETED TE FLAPS SELECTED TO 20 WITH NO ISSUE. NO REPORTED FLIGHT CONTROL HANDLING ISSUES FELT. RETRACTED LEADING EDGE SLATS ON A
- [SDR CALA2025041804019](https://openairdocs.org/sdr/CALA2025041804019.md): Light · inoperative · Apr 18, 2025 · N662UA · Boeing 767322 · Emergency Lighting
  > EXTERNAL EMERGENCY LIGHT, RIGHT SIDE (L391) INOP PERFORMED EMERGENCY LIGHT TEST IAW AMM TASK 33-51-00-705-029-001. FOUND L391 LIGHT FUNCTIONAL. OK TO CONTINUE.
- [SDR CALA2025041703925](https://openairdocs.org/sdr/CALA2025041703925.md): Light · malfunctioned · Apr 15, 2025 · N662UA · Boeing 767322 · Emergency Lighting
  > IN REFERENCE WITH LOGPAGE#4512799 PERFORMED SYSTEM TEST OF THE EMERGENCY LIGHTS IRW AMM 33-51-00-705-029-001. EMERGENCY LIGHTS FAILED TO STAY ON DURING THE 1 MINUTE PERIOD REQUIREMENT. LEFT SIDE OF THE AC EMERGENCY LIGHTS TURNED OFF WITHIN 10-20 SECONDS WITH E
- [SDR CALA2025031302795](https://openairdocs.org/sdr/CALA2025031302795.md): Slide · faulted · Mar 9, 2025 · N662UA · Boeing 767322 · Escape Slide
  > FOUND R/H OVERWING SLIDE HOSE CLAMP DETACH REMOVED AND REPLACED RH OFF WING SLIDE ASSY PER AMM 25-65-01/401 CONFIG 1 UPTO AND INCLUDING STEP 3 G(8). NEED TO CONTINUE INSTALLATION FROM STEP H. C/W RII REQUIREMENTS FOR R/H OVERWING SLIDE ASSY INSTALLATION REF
- [SDR CALA2025030300471](https://openairdocs.org/sdr/CALA2025030300471.md): Fseu · faulted · Mar 1, 2025 · N662UA · Boeing 767322 · Leading Edge Slat Position Indicating System
  > LE SLAT ASYM EICAS B LE SLAT ASYMMETRY CREW DEBRIEF: ON APPROACH WHEN FLAPS/SLATS WERE EXTENDED, GOT A SECOND REPORT. LE SLAT ASSYMETRY EICAS. NO ABNORMAL ROLL EXPERIENCED. FLAPS REMAIN EXTENDED AND HANDLE IS AT 20. PER FIM 27-81 FAULT TREE 809 SYSTEM IS OK.
- [SDR CALA2025010601790](https://openairdocs.org/sdr/CALA2025010601790.md): Fseu · faulted · Jan 3, 2025 · N662UA · Boeing 767322 · Leading Edge Slat Control System
  > LE SLAT DISAGREE EICAS CREW REPORTS THEY ACCOMPLISHED PROCEDURE AND LE SLAT DISAGREE MSG CLEARED. PERFORMED BITE CK OF FSEU PER REF FIM 27-51 FAULT TREE 809. FOUND MESSAGE NUMBER 27-51333. REMOVED AND REPLACED FSEU REF AMM 27-51-01. OPS CK GOOD. NO STATUS MESS
- [SDR CALA2024102102699](https://openairdocs.org/sdr/CALA2024102102699.md): Skin · corroded · Oct 20, 2024 · N662UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > IT WAS FOUND CORROSION ON THE SKIN (P/N 146T3241-12) AT THE DRAIN HOLE AREA LOCATED BETWEEN STA 1540 AND 1562 & STR 39LH AND 39RH. MANENT SOLUTION WITH INSPECTION REQUIREMENTS THAT MUST BE ACCOMP ON OR BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLES. AC
- [SDR CALA2024102102697](https://openairdocs.org/sdr/CALA2024102102697.md): Stringer · damaged · Oct 20, 2024 · N662UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > BULK CARGO COMPARTMENT WAS FOUND TOOL MARK AT STGR 38LH BETWEEN STA 1562/1582. (NR 2236807)
- [SDR CALA2024102102700](https://openairdocs.org/sdr/CALA2024102102700.md): Stringer · corroded · Oct 19, 2024 · N662UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > BULK CARGO COMPARTMENT WAS FOUND CORROSION AT STGR 39LH BETWEEN STA 1540/1562. (NR 2231086) UPGRADE OF ATTRIBUTES PERFORMED REPAIR AT STRINGER 39LH AS PER SRM 53-00-03-2R-2 TYPE III AND TABLE III DETAIL IV.
- [SDR CALA2024102102689](https://openairdocs.org/sdr/CALA2024102102689.md): Floorbeam · corroded · Oct 17, 2024 · N662UA · Boeing 767322 · Fuselage Main, Floor Beam
  > INSPECTING BODY BELLOW AFT CARGO FLOOR WAS FOUND CORROSION SIGNS ON FRAME SURFACE, STA 1197, STRINGER 36L.
- [SDR CALA2024102102688](https://openairdocs.org/sdr/CALA2024102102688.md): Skin · damaged · Oct 17, 2024 · N662UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > THERE ARE OLD SCRIBE MARKS ON EXTERNAL SKIN OF FUSELAGE, LOCATED BETWEEN STA 654 PLUS 110/STA 785.9 AND BETWEEN STR20LH/36LH. FOR REFERENCE SEE SRM 53-30-01-0I-1 FIG 1, SHEET 2(ITEM 3) AND SHEET 4(ITEM 6). IS A PERMANENT SOLUTION WITH INSPECTION REQUIREMENTS T
- [SDR CALA2024101802677](https://openairdocs.org/sdr/CALA2024101802677.md): Floor Support · corroded · Oct 16, 2024 · N662UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > INSPECTING THE BODY BELLOW THE AFT CARGO FLOOR WAS FOUND SIGNS OF CORROSION ON THE FRAME SURFACE, STA 1197/110, STRINGER 34L.
- [SDR CALA2024101402635](https://openairdocs.org/sdr/CALA2024101402635.md): Pressure Blkhd · dented · Oct 11, 2024 · N662UA · Boeing 767322 · Fuselage Main, Bulkhead
  > DURING CLEAN PROCESS WAS FOUND STA 1582.0 PRESSURE BULKHEAD WITH DAMAGE LOCATED IN DOME WEB. REPAIR IS A PERMANENT SOLUTION WITH INSPECTION REQUIREMENTS. REVISION OF EC/RA 5380-01408 ON OR BEFORE THE AIRCRAFT REACHES ACCOMPLISH INSPECTION REQUIREMENTS PER PART
- [SDR CALA2024101102632](https://openairdocs.org/sdr/CALA2024101102632.md): Skin · cracked · Oct 10, 2024 · N662UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > DURING HFEC INSPECTION OF THE FASTENER OPEN HOLE, WAS FOUND A CRACK LENGTH 0.040" AT THE FWD SERVICE DOOR CUTOUT AFTER LOWER CORNER.
- [SDR CALA2024060301667](https://openairdocs.org/sdr/CALA2024060301667.md): Panel · missing · Jun 2, 2024 · N662UA · Boeing 767322 · Nacelle/Pylon, Main Frame
  > PDA 2 ON ETOPS WALKROUND FOUND PANEL 446BR MISSING. PYLON PANEL 446BR FITTED, AMM REF 54-53-01-404-007 FOR INSTALLATION. PARTS USED: 76-5453-3-0063,QTY:1
- [SDR CALA2024042601243](https://openairdocs.org/sdr/CALA2024042601243.md): Control Module · defective · Apr 25, 2024 · N662UA · Boeing 767322 · Flight Control System Wiring
  > STAB TRIM LIGHT CAME ON AFTER T/O WITH FLAPS OUT. WITH FLAPS UP EICAS WENT OUT LEFT AND RIGHT EICAS COMPUTERS. PERFORMED FIM TASK 27-48FT809, FOUND COL TRIM SW FAULT BALL PERFORMED FIM TASK 27-48FT809, COMPLETED TEST 30 MCPD TEST, TEST PRESENT ON RT SAM, NO FA
- [SDR CALA2024020500327](https://openairdocs.org/sdr/CALA2024020500327.md): Relay · inoperative · Feb 4, 2024 · N662UA · Boeing 767322 · Waste Disposal System
  > LAV SYS 2 FLUSH CB R-35 POPED ONLY 3 LAVS WORKING R&R LAV FLUSH CONTROL RELAY (K2311) IAW WDM 38-32-11. PERFORM OPS CHECK OF LAV SYSTEM IAW 38-32-00/201, OPS CHECK GOOD. BREAKER NOT POPPING OUT. PARTS USED: 99-2332-3-0034,QTY:1. RNWY TURN OFF CD POPPED N-6 PE
- [SDR CALA2024011900156](https://openairdocs.org/sdr/CALA2024011900156.md): Wire Harness · chafed · Jan 15, 2024 · N662UA · Boeing 767322 · Fire Protection System Wiring
  > L ENG FIRE LP 2 EICAS. THE LEFT ENGINE FIRE LOOP 2 HAS A FIRE OR THERE IS A FAILURE OUT PUT. INTERMITTENT STATUS MESSAGE NO EICAS MESSAGE ON ARRIVAL. L ENG LP 2 INTERMITANT DURING CRUISE. TALKED TO CREW, WRITE UP IS IN REFERENCE TO LOGPAGE 6821086. MESSAGE WAS
- [SDR CALA2023121103623](https://openairdocs.org/sdr/CALA2023121103623.md): Light · missing · Dec 8, 2023 · N662UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - 2X FWD GALLEY 227F/R & 228F/R EPL MISSING CLEAR LENSES. PLEASE REPLACE. BOTH EPL LENSES REPLACED IAW CMM 25-07-22.
- [SDR CALA2023110303272](https://openairdocs.org/sdr/CALA2023110303272.md): Electronic Unit · faulty · Nov 1, 2023 · N662UA · Boeing 767322 · Leading Edge Slat Control System
  > CONT. LE FLAP ASSYM AGAIN AT FL300 DOING 320 KTS.RTB AFTER SLOWING NORM IND ACFT LANDED @ 318000LBS, OVERWEIGHT LANDING NOT REQD. FLT CREW DEBRIEF: LE ASYM EICAS MSG WITH ASSOCIATED LE EDGE ANNUNCIATOR LT DURING CLIMB FOR 1MIN, THEN AGAIN AT 33000FT @ 320KTS F
- [SDR CALA2023110203256](https://openairdocs.org/sdr/CALA2023110203256.md): Connector · unknown · Oct 29, 2023 · N662UA · Boeing 767322 · Auto Flight System Wiring
  > THRUST MANAGEMENT SYSTEM A/T DISC LIGHT ILLUMINATED WITH AUTOTHR OTTLE ENGAGED IN (STATE MODE) MODE. THRUST REFERENCE MODE DISPLA Y ON EICAS & F/S POINTER DISPLAY ON EADI NORMAL IN VNAV PATH MODE ARRIVAL CREW INFORMATION: A/T DISCONNECTED IN CRUISE, RESET
- [SDR CALA2023102503171](https://openairdocs.org/sdr/CALA2023102503171.md): Engine · faulted · Oct 21, 2023 · N662UA · Boeing 767322 · Engine Fuel and Control
  > VIBRATION & STEADY HUM SOUND IN ACFT SINCE REACHING CRUISE ALT. ENTIRE FLT. LOUD HUMMING NOISE NOTABLE INCREASE IN EGT, FUEL FLOW. FLUCTUATING N2 AND VIB INDS. NOISE CHANGED WITH THROTTLE. ON ARRIVAL FOUND RT ENG INTAKE BLOW OUT PANEL UNLATCHED. WITH A SSO
- [SDR CALA2023101603089](https://openairdocs.org/sdr/CALA2023101603089.md): Sensor · intermittent · Oct 13, 2023 · N662UA · Boeing 767322 · Leading Edge Slat Position Indicating System
  > LE SLAT ASYM CAME ON RETRACTING FLAPS 1 TO ZERO AND INDCATOR DISPLAY OUT OF UP ACCOMPLISHED FIM 27-81-00/301 LEADING EDGE (LE) SLAT SENSOR INDUCTANCE/RESISTENCE TEST AND IT WAS FOUND SENSOR S279 WITH INDUCTANCE 6.52 (OVER LIMIT). PERFORMED ADJUST REF. AMM SU
- [SDR CALA2023100902997](https://openairdocs.org/sdr/CALA2023100902997.md): Cylinder · activated · Oct 7, 2023 · N662UA · Boeing 767322 · Escape Slide
  > DURING THE ACTIVATION OF THE "OFF WING ESCAPE SYSTEM", ACCIDENTALLY THE SPOILER OVERRIDE ACTUATORS AND AND DOORS LATCH OPENING/SNUBBING ACTUATOR WERE FIRED. REMOVED AND REPLACED CYLINDER,ASSY, OFFWING EVACUATION REPLACED SPOILER OVERRIDE ACTUATOR SQUIB LH PN O
- [SDR CALA2023071702270](https://openairdocs.org/sdr/CALA2023071702270.md): Extinguisher · unknown · Jul 16, 2023 · N662UA · Boeing 767322 · Fire Protection System
  > RAISING SDR FOR INCORRECT FITMENT OF COMPONENT PER TASK CARD 63-2620-1-2827. SDR RAISED FOR DISCOVERY OF INCORRECT FITMENT OF COMPONENT DURING TASK CARD 63-2620-1-2827 ON 15-JUL-23. TSAP RAISED.
- [SDR CALA2022070401634](https://openairdocs.org/sdr/CALA2022070401634.md): Controller · failed · Jul 1, 2022 · N662UA · Boeing 767322 · Cabin Temperature Controller
  > MID CABIN TEMP EICAS C THE MID CABIN SUPPLY DUCT TEMPERATURE IS MORE THAN 190 DEGREES F (88 DEGREES C); OR THE ZONE TEMPERATURE MID CABIN CHANNEL HAS A FAILURE OR THE SYSTEM IS OFF.REMOVED AND REPLACED THE MAIN CABIN ZONE TEMP CONTROLLER. ALL TEMPS NORMAL.CREW
- [SDR CALA2022030700603](https://openairdocs.org/sdr/CALA2022030700603.md): None · none · Mar 7, 2022 · N662UA · Boeing 767322 · Communications System
  > AIRCRAFT REPORTED TO BE TRANSMITTING ON GUARD FREQ (NO VOICE) GROUND MONITORING STATION REPORTS THAT NORMAL ATC COMS FROM AIRCRAFT BEING HEARD ON GUARD FREQ. REPLACED NO.1 TRANSCEIVER PER AMM 23-12-01-424-004 & REPLACED NO.2 (FO SIDE) AUDIO SELECTOR PANEL PER
- [SDR CALA2021111702123](https://openairdocs.org/sdr/CALA2021111702123.md): Skin · corroded · Nov 16, 2021 · N662UA · Boeing 767322 · Fuselage Structure (General)
  > REFER NRC L/P 9131558 FUSELAGE STA 1205 STR 36L STRINGER SECTION CUTOFF FOUND ATTACH SKIN CORROSION. TRANSFER REF NR LP 9131765 AND ORIGINATED BY V896890. AFTER REF NDT PART 6, 53-00-06 REPAIR INSP REQUIREMENTS ARE AS FOLLOWS PER SRM 53-00-01-2R-31 RPR 31 TABL
- [SDR CALA2021111702115](https://openairdocs.org/sdr/CALA2021111702115.md): Stringer · cracked · Nov 15, 2021 · N662UA · Boeing 767322 · Fuselage Structure (General)
  > AFT CARGO COMPT STA 1205 S-36L AREA FOUND CORROSION CRACK. TRANSFER REF NR LP 9131558 AND ORIGINATED BY V897013. AFT CARGO COMPT STRINGER 36L BETWEEN STA 1197+120VAND STA 1219 REPAIRED AS PER SRM 53-00-03 REPAIR 2 FIG 201. WORK ACCOMPLISHED BY MECHANIC V897532
- [SDR CALA2021111502105](https://openairdocs.org/sdr/CALA2021111502105.md): None · corroded · Nov 14, 2021 · N662UA · Boeing 767322 · Fuselage Structure (General)
  > AFT CGO COMPT STA 1285 LBL 24" FLOOR BEAM UPPER CHORD FOUND CORROSION CRACK. TRANSFER REF. HX NON-ROUTINE LP 9131773 AND ORIGINATED BY EMP NO. V896921 AFT CARGO COMPT STA 1285 LBL 20.5 - LBL 25.5 WL 123 FRAME INNER CHORD J SECTION REPAIRED AS PER EC/RA 5360-01
- [SDR CALA2021110502041](https://openairdocs.org/sdr/CALA2021110502041.md): Beam · elongated · Nov 4, 2021 · N662UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7141 CABIN STA 544 LBL 55-68 FLOOR SUPPORT HOLE FOUND ELONGATE. TRANSFER REF. NON-ROUTINE LP 9131173 AND ORIGINATED BY EMP V927004. CABIN BS 544 FLOOR BEAM UPPER CHORD BETWEEN LBL 55 AND LBL 88 REPAIRED AS PER EC/RA 5315-01163 REV-. ADD EMP:V896920
- [SDR CALA2021110302031](https://openairdocs.org/sdr/CALA2021110302031.md): None · none · Nov 3, 2021 · N662UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7141 CABIN STA 544 LBL 55-68 FLOOR SUPPORT HOLE FOUND ELONGATE. TRANSFER REF. NON-ROUTINE LP 9131173 AND ORIGINATED BY EMP V927004. CABIN BS 544 FLOOR BEAM UPPER CHORD BETWEEN LBL 55 AND LBL 88 REPAIRED AS PER EC/RA 5315-01163 REV-. ADD EMP:V896920
- [SDR CALA2021110302021](https://openairdocs.org/sdr/CALA2021110302021.md): Beam · none · Nov 2, 2021 · N662UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-0166 CABIN - BS1500 RBL10 FLOOR SUPPORT HOLE ELONGATED AS MARK. TRANSFER REF. NON-ROUTINE LP 9131246 AND ORIGINATED BY EMP V896926. CABIN BS 1500 FLOOR BEAM UPPER CHORD RBL 10 REPAIRED AS PER SRM 53-00-51 REPAIR 2 FIG 201. ATTACHED FORM 44-0008 ITEM
- [SDR CALA2019032500463](https://openairdocs.org/sdr/CALA2019032500463.md): Bulkhead · cracked · Mar 22, 2019 · N662UA · Boeing 767322 · Fuselage Main, Bulkhead
  > REF NR LP B767-06-3-7059 CABIN: STA 955 TO 975 RBL 30 CANTED PRESSURE DECK WEB FOUND CRACK CABIN STA 955 TO STA 975 RBL 30 CANTED PRESSURE DECK WEB INTERIM REPAIRED AS PER EC/RA 5358-01001 REV - PART 1.
- [SDR CALA2019020100202](https://openairdocs.org/sdr/CALA2019020100202.md): Structure · cracked · Jan 31, 2019 · N662UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > 02MAR HKG CF -L:LH STA 1809 HORIZ INNER CHORD 1 EA FAST FN D CRK AT 8 O''CLK POS RUNNING TO EDGE.AREA REPAIRED PER EA 5312-0 1059 REV B OP9 STEP 1 AND SRM 53-80-08 REP 10 FIG 201 DET II.REP EAT INSPECTION AS PER SRM 53-80-08 REP 10 TBL 202, INSP THRESHOL D IS
- [SDR CALA2018022300763](https://openairdocs.org/sdr/CALA2018022300763.md): Fuse · inoperative · Feb 23, 2018 · N662UA · Boeing 767322 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT LEFT SIDE OF AIRCRAFT INOPERATIVE. REPLACED THE FUSES IN M738 CHARGER. OPS CHECKED NORMAL
- [SDR CALA2018022300765](https://openairdocs.org/sdr/CALA2018022300765.md): Lamp · inoperative · Feb 23, 2018 · N662UA · Boeing 767322 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT AT SEAT ROW 19K INOPERATIVE. REPLACED THE LAMPS. OK FOR SERVICE.
- [SDR CALA2018022300764](https://openairdocs.org/sdr/CALA2018022300764.md): Lamp · inoperative · Feb 23, 2018 · N662UA · Boeing 767322 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT AT ROW 4K INOPERATIVE. REPLACED THE LAMPS, OK FOR SERVICE.

Next page: https://openairdocs.org/aircraft/N662UA/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 = 'N662UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N662UA/reports

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