# Service difficulty reports: N660UA

A list on [N660UA](https://openairdocs.org/aircraft/N660UA.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 · 346 reports

- [SDR CALA2026092919973](https://openairdocs.org/sdr/CALA2026092919973.md): Unknown · smoke · Sep 28, 2026 · N660UA · Boeing 767322 · Ice/Rain Protection System
  > PUFFS OF WHITE SMOKE FROM THE LEFT SIDE OF THE NOSE DURING TAXI OUT. OBSERVED SEVERAL TIMES AND APPEARED MORE THAN USUAL. INSPECTED LEFT SIDE AREA WHERE WHITE SMOKE WAS OBSERVED. NO ANOMALIES FOUND. POSSIBLE WATER VAPOR COMING FROM TOTAL AIR TEMP PROBE. PEFORM
- [SDR CALA2026072417981](https://openairdocs.org/sdr/CALA2026072417981.md): Lamp · broken · Jul 23, 2026 · N660UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY ESCAPE PATH LIGHT ASSEMBLY ON SEAT 37F IS BROKEN. REMOVED AND REPLACED ESCAPE PATH LIGHT ASSEMBLY ON SEAT 37F REF AMM 33-51-10-962-104. ESCAPE PATH LIGHT SYSTEM IS GOOD FOR SERVICE.
- [SDR CALA2026072417978](https://openairdocs.org/sdr/CALA2026072417978.md): Battery Pack · no test · Jul 23, 2026 · N660UA · Boeing 767322 · Emergency Lighting
  > DURING EMERGENCY ESCAPE PATH LIGHT SYSTEM CHECK ON LOG PAGE 9707422 FOUND EMERGENCY CEILING LIGHTS FROM SEATS ROW 47LK TO 50LK DO NOT TURN ON. PERFORMED TROBLESHOOTING AND FOUND BATTERY PACK ON POWER SUPPLY M734 DISCHARGED. REMOVED AND REPLACED BATTERY PACK RE
- [SDR CALA2026051416260](https://openairdocs.org/sdr/CALA2026051416260.md): Fan · faulty · May 13, 2026 · N660UA · Boeing 767300 · Air Distribution Fan
  > R RECIR FAN EICAS C THE RIGHT RECIRCULATION FAN HAS A FAILURE. BURNING WIRE SMELL IN FLIGHT AT FL350 AND EICAS MSG R RECIR FAN SDR FLAGGED TOMC APPROVAL THIS MEL IS REQUIRED, DUE TO R RECIRCULATION FAN INOP (, R REC SWITCH SET OFF STIKER INOP WAS APLIED. R
- [SDR CALA2026020913640](https://openairdocs.org/sdr/CALA2026020913640.md): Sensor · faulted · Feb 4, 2026 · N660UA · Boeing 767322 · Door Warning System
  > EICAS MSG: L AFT ENT DOOR CAME ON AT FL310 OFF AT FL390. BACK ON IN DESCNT AT FL350 REQUEST MEL. APPROVED COMPLIED WITH MEL 52130. PERFORMED DOOR WARNING SENSOR TEST IAW AMM TASK 52-71-00-735-072. CLEANED AND RETIGHTENED SENSORS AS PRECAUTIONARY. OPENED AN
- [SDR CALA2026020413580](https://openairdocs.org/sdr/CALA2026020413580.md): Skin · corroded · Feb 2, 2026 · N660UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > ETOPS PREDEPARTURE SERVICE CHECK PROCEDURE, AFT WASTE SYS VACUUM BLOWER VENT PORT HAS AREA WITH SKIN BULGE AND POSSIBLE CORROSION.. CUT-OUT OF CORRODED SKIN, HFEC OF CUT-OUT, & MATERIAL VERFICATION WERE ACCOMPLISHED. IAW SRM 53-60-01-2R-3. VERIFIED HFEC OF
- [SDR CALA2026020513597](https://openairdocs.org/sdr/CALA2026020513597.md): Light · inoperative · Jan 30, 2026 · N660UA · Boeing 767322 · Emergency Lighting
  > LEFT, AFT EMERGENCY LIGHT IS INOPERATIVE. R & R AFT EMERGENCY LIGHT IAW AMM 33-51-06-902-082, OPS CHECKED GOOD
- [SDR CALA2026010812795](https://openairdocs.org/sdr/CALA2026010812795.md): Lamp · inoperative · Jan 7, 2026 · N660UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHTS TEST WITH TEST SWITCHES, EMERGENCY LIGHTS IN CEILING ABOVE POSITIONS 36K, 21B AND 6L DO NOT COME ON WHEN SWITCH IN TEST. IT WAS VERIFIED LAMP BURNED AND REPLACED IN REF AMM 33-51-04-002-001. IT IS OK FOR SERVICE.
- [SDR CALA2025092509263](https://openairdocs.org/sdr/CALA2025092509263.md): Idg · faulted · Sep 24, 2025 · N660UA · Boeing 767322 · AC Generator-Alternator
  > RIGHT GEN OFF EICAS. UNABLE TO RESET AFTER ONE ATTEMPT. PERFORMED BPCU BITE CHECK IAW FIM 24-20 TASK 801. FAULTS FOR RT GEN AS FOLLOWS: IDG HIGH RISE TEMP, & GEN/FIELD/WIRING/GCU. REF FIM 24-20 TASK 804 FOR IDG HIGH RISE TEMP, VERIFIED DPI WAS NOT EXTENDED, R
- [SDR CALA2025081107546](https://openairdocs.org/sdr/CALA2025081107546.md): Bottle · low pressure · Aug 8, 2025 · N660UA · Boeing 767322 · Emergency Equipment
  > DOOR 2R SLIDE PRESSURE BELOW GREEN ARC. AFTER DETAILS INSPECTION FOUND PRESSURE INDICATOR NEEDLE SLIDE DOOR 2R WITHIN LIMITS AS PER AMM:25-66-98-206-001.CHECK GOOD.
- [SDR CALA2025061805665](https://openairdocs.org/sdr/CALA2025061805665.md): Bottle · no discrepancy · Jun 14, 2025 · N660UA · Boeing 767322 · Escape Slide
  > SLIDE PRESSURE GAUGE AT 2L APPEARS TO BE LOW CHECKED L2 DOOR SLIDE PRESSURE AS REQUIRED, DOOR L2 PRESSURE CK NORMAL. REF. AMM 25-66-02
- [SDR CALA2025061805664](https://openairdocs.org/sdr/CALA2025061805664.md): Bottle · no discrepancy · Jun 14, 2025 · N660UA · Boeing 767322 · Escape Slide
  > SLIDE PRESSURE GAUGE APPEARS TO BE LOW. AT 2R APPEARS TO BE LOW CHECKED R2 DOOR SLIDE PRESSURE AS REQUIRED, DOOR 2R PRESSURE CK NORMAL. REF. AMM 25-66-02
- [SDR CALA2025031202743](https://openairdocs.org/sdr/CALA2025031202743.md): Actuator · faulted · Mar 8, 2025 · N660UA · Boeing 767322 · Escape Slide
  > RT WING OFF WING SLIDE FWD DOOR ACTUATOR/SNUBBER REQUIRES REPLACEMENT DUE TO DEPLOYMENT. REMOVED AND REPLACED FWD DOOR ACTUATOR/SNUBBER IAW AMM 25-65-10-404-016-001.PARTS USED: 76-2565-9-0002, QTY:1ROTABLE PARTS CHANGE WAS INDICATED - TT # 1643046 SN OFF 60
- [SDR CALA2025031202742](https://openairdocs.org/sdr/CALA2025031202742.md): Actuator · faulted · Mar 8, 2025 · N660UA · Boeing 767322 · Escape Slide
  > RT WING EMER ESCAPE SLIDE DOOR LATCH ACFUATOR REMOVED FOR REPLACEMENT REF AMM 25-65-11. ACTUATOR INSTALLED REF AMM 25-65-11, OPERATIONAL CHECKS REQUIRED WITH ACTIVATION OF EMERGENCY SLIDES INSTALLATION IN COMPLIANCE WITH AMM 25-65-11 AND RII
- [SDR CALA2025031202741](https://openairdocs.org/sdr/CALA2025031202741.md): Cylinder · malfunctioned · Mar 8, 2025 · N660UA · Boeing 767322 · Escape Slide
  > REMOVED RH OFF-WING SLIDE INFLATION CYLINDER REF AMM 25-65-02-004-001 REF LOG PAGE # 4103460 FOR THE DISARM OFF- WING SLIDE SYSTEM INSTALLED NEW INFLATION BOTTLE REF AMM TASK 25-65-02-404-010 STOPPED AT STEP G.9.(24) PARTS USED: 76-2565-9-9002, QTY:1 ROTABLE
- [SDR CALA2025031202735](https://openairdocs.org/sdr/CALA2025031202735.md): Battery · inoperative · Mar 8, 2025 · N660UA · Boeing 767322 · Escape Slide
  > PER AMM 25-65-00, REMOVED LEFT AND RIGHT OFF-WING ESCAPE SYS EMERGENCY BATTERIES REF AMM 25-65-17 REMOVED AND REPLACED LT AND RT OVERWING ESCAPE SYSTEM BATTERIES IAW AMM 25-65-17.PARTS USED: 75-3351-3-0041,QTY:1
- [SDR CALA2025031102729](https://openairdocs.org/sdr/CALA2025031102729.md): Slide · faulty · Mar 8, 2025 · N660UA · Boeing 767322 · Escape Slide
  > RH OFFWING SLIDE DEPLOYED DURRING REACTIVATION PROCEDURE.FOUND RH OVERWING SLIDE PACK REMOVED FROM A/C INSTALLED NEW RIGHT OFF-WING SLIDE PER TASK 25-65-01-424-060-001 UP TO AND INCLUDING STEP (3)(I)(3) LEFT EMERGENCY OFF WING SLIDE SYSTEM DISARMED. AMM TASK 2
- [SDR CALA2025031102728](https://openairdocs.org/sdr/CALA2025031102728.md): Slide · abnormal · Mar 8, 2025 · N660UA · Boeing 767322 · Escape Slide
  > OFF-WING ESCAPE SLIDE SYSTEM DISARMED REF AMM TASK 25-65-00-042-001 REARMED LT AND RT OFF-WING EASCAPE SLIDE SYSTEMS IAW AMM 25-65-00-442-010 REARMED IN COMPLIANCE WITH AMM 25-65-00-442-010 AND RII
- [SDR CALA2025021102282](https://openairdocs.org/sdr/CALA2025021102282.md): Sign · detached · Feb 9, 2025 · N660UA · Boeing 767322 · Emergency Lighting
  > 31D EMERGENCY EXIT SIGN DETACHED AND HANGING BY WIRES FASTNED EXIT SIGN.
- [SDR CALA2024110402786](https://openairdocs.org/sdr/CALA2024110402786.md): Skin · cracked · Oct 30, 2024 · N660UA · Boeing 767322 · Passenger/Crew Doors
  > SUPPORT TASK- REF EA 5315-01152 RAV A OP 001, AD 2024-05-03, 2EA FASTENER HOLES FOUND CRACKED ON SKIN LAYER AT LH FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER. UIRED TO ACCOMPLISH INSPECTION REQUIREMENTS ON REPAIR INSTALLED PART 2 OF LATEST REVISION OF EC5310-08
- [SDR CALA2024110402787](https://openairdocs.org/sdr/CALA2024110402787.md): Skin · cracked · Oct 28, 2024 · N660UA · Boeing 767322 · Passenger/Crew Doors
  > FOUND 1 FASTENER HOLE FUSE SKIN CRACKED AT 1R SERVICE DOOR LWR AFT CORNER CUTOUT DURING ACCOMPLISHMENT OF EA 5315-01152 REV A OP2. DIP LOGPAGE TO ACCOMPLISH INSPECTION REQUIREMENTS ON REPAIR INST TOUT PER PART 2 OF LATEST REVISION OF EC5310-08445 ON OR BEFORE
- [SDR CALA2024102802746](https://openairdocs.org/sdr/CALA2024102802746.md): Structure · cracked · Oct 24, 2024 · N660UA · Boeing 767322 · Fuselage Main, Structure
  > SUPPORT TASK EA 5312-01059 REV C OP 004 1EA CRACK FOUND AT STA 1809 RH HORI INNER CHORD. DETAIL REFER NDT INSPECTION FINDING RECORD REFER HX NR WO.3797716. REQUIREMENTS ON REPAIR INSTALLED AT STA 1809.5 BULKHEAD INNER AIRCRAFT REACHES 37,500 TOTAL FLT CYCLES
- [SDR CALA2024110102771](https://openairdocs.org/sdr/CALA2024110102771.md): Skin · unknown · Oct 23, 2024 · N660UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > RH FUS SKIN FND PREVIOUS DOUBLER REPAIR AT BS 347-368 STR 33R REFER HX NR WO.3882226 AND. EEN STA 246-434 AT STR 33R NO LATER THAN 37,500 TOTAL FLIGHT CYC VE INTERNAL HFEC INSPECTION AND DETAILED VISUAL INSPECTION PER P OF EC/RA 5310- 08447". LES PER PART 2 I
- [SDR CALA2024102502727](https://openairdocs.org/sdr/CALA2024102502727.md): Floorbeam · corroded · Oct 23, 2024 · N660UA · Boeing 767322 · Fuselage Main, Floor Beam
  > CABIN STA 287 RH FLR BEAM UPR CORD FOUND CORROSION AFTER FLOOR W EB REMOVED REFER HX NR WO.3827295 AND ORIGINAL BY V923416. CABIN STA 287 RBL 83" FLOOR BEAM UPPER CHORD PERMANENT REPAIRED AS PER ECRA 5310-08446 REV- ATTACH FORM ITEM 1-41 ACCOMPLISHED BY MECH V
- [SDR CALA2024101502652](https://openairdocs.org/sdr/CALA2024101502652.md): Shear Tie · corroded · Oct 9, 2024 · N660UA · Boeing 767322 · Fuselage Internal Mounting Structure
  > AFT CARGO COMPT - BELOW FLOOR SHEAR TIE FOUND CORROSION AT STA 1 197+22 BTN S39L - S39R. AFT CGO COMPT BELOW FLOOR SHEAR TIE AT STA 1197+22 BTN S-39L -S-39R REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 ATTACHED FORM 44-0008 ITEM 1-8.
- [SDR CALA2024101502651](https://openairdocs.org/sdr/CALA2024101502651.md): Shear Tie · corroded · Oct 9, 2024 · N660UA · Boeing 767322 · Cabin Equipment/Furnishings
  > AFT CARGO COMPT - BELOW FLOOR SHEAR TIE FOUND CORROSION AT STA 1 197+66 BTN S39L - S39R AFT CARGO COMPT BELOW FLOOR SHEAR TIE AT STA 1197+66 BTN STR 39L-39R REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 ATTACHED FORM 44-0008 ITEM 1-8.
- [SDR CALA2024101502650](https://openairdocs.org/sdr/CALA2024101502650.md): Shear Tie · corroded · Oct 9, 2024 · N660UA · Boeing 767322 · Fuselage Internal Mounting Structure
  > AFT CARGO COMPT - BELOW FLOOR SHEAR TIE FOUND CORROSION AT STA 1 197+22 BTN S38R - S39R AFT CARGO COMPT BELOW FLOOR SHEAR TIE AT STA 1197+22 BTW STR 38R-39R REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 ATTACHED FORM 44-0008 ITEM 1-8.
- [SDR CALA2024102802742](https://openairdocs.org/sdr/CALA2024102802742.md): Frame · cracked · Oct 8, 2024 · N660UA · Boeing 767322 · Fuselage Main, Frame
  > CABIN AFT ZONE LH SW FRAME SL 16 STA 1268 FOUND CRACK REFER HX NR WO.3833404. PER PART 2 OF LATEST REVISION OF EC5300-03166 ON OR BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLT CYCLES PER PART 1.2, INITIATE A DTA DIP TO ACCOMPLISH INSPECTION REQUIREMENTS ON REP
- [SDR CALA2024101502649](https://openairdocs.org/sdr/CALA2024101502649.md): Shear Tie · corroded · Oct 8, 2024 · N660UA · Boeing 767322 · Fuselage Internal Mounting Structure
  > AFT CARGO COMPT BELOW FLOOR SHEAR TIE FOUND CORROSION AT STA 1285 BTN S37L-S38L. AFT CARGO COMPT BELOW FLOOR AT STA 1285 BTN STR 37L AND STR 38L SHEAR TIE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 ATTACHED FORM 44-0008 ITEM 1-8.
- [SDR CALA2024081600440](https://openairdocs.org/sdr/CALA2024081600440.md): Wheel · damaged · Aug 14, 2024 · N660UA · Boeing 767322 · Wheel/Ski/Float
  > UPON PARKING..LEFT MAIN GEAR SHOWED SMOKE FROM POSSIBLE HYDRAU LIC FLUI D DRIPPING ON THE GEAR 4 PICS ADDED... SEE LOGPAGES 8918794 AND 8918788 FOR RECITIFICATION.REF LOGS 8916746 AND 8916737 REPLACE WHEEL 2 REPLACE BRAKE 2 INSPECT WHEEL AXLE 2 FOR HEATIN
- [SDR CALA2024080100345](https://openairdocs.org/sdr/CALA2024080100345.md): Door · missing · Jul 30, 2024 · N660UA · Boeing 767322 · Nacelle/Pylon, Main Frame
  > PDA 1 #1 ENG NACELLE STRUT PRESSURE RELIEF DOOR MISSING. PICTURE UPDATE TOMC NOTIFIED. NO VISUAL DAMAGE.
- [SDR CALA2024052401573](https://openairdocs.org/sdr/CALA2024052401573.md): Fuel Cap · missing · May 23, 2024 · N660UA · Boeing 767322 · Fuel Storage
  > PDA 2 BOTH FUELING RECEPTACLE CAP MISSING (02 EA). REQUESTING MEL 2821L FOR BOTH FUELING RECEPTACLE CAP. PLACED BOTH MISSING STATION RECEPTACLE CAP ON MEL 2821L, AS REQUESTED. NO PRESENCE OF FUEL LEAKAGE. DDP COMPLIED WITH. OK TO DEF.BOTH FUELING RECEPTACLE C
- [SDR CALA2023091802806](https://openairdocs.org/sdr/CALA2023091802806.md): Fuel Cap · missing · Sep 15, 2023 · N660UA · Boeing 767322 · Fuel Storage
  > LEFT FUEL RECEPTACLE CAP MISSING. MEL 2821J APPROVAL REQUIRED LEFT FUEL RECEPTACLE CAP PLACED ON MEL. 2821J DDP C/W. APPROVED MEL 2821J. REPLACED REFUELING CAP REF AMM28-00-00.REMOVED MEL
- [SDR CALA2023072102305](https://openairdocs.org/sdr/CALA2023072102305.md): Fastener · missing · Jul 11, 2023 · N660UA · Boeing 767322 · Nacelle/Pylon Structure
  > PDA 3 #2 ENGINE AFT PYLON OUTSIDE STRUT FAIRING PAN ASSEMBLY MISSING ONE FASTENER. ONE MISSING FASTENER. SEE DETAIL III AND IV. CONFIRMED ONE MISSING FASTER. NO PART AVAILABLE GIGJL. AS PER SRM 51-10-05-2R-1 PARAGRAPH 4, ALL CONDITIONS ARE PERMITTED FOR DIP 5
- [SDR CALA2023060201741](https://openairdocs.org/sdr/CALA2023060201741.md): Bolt · missing · May 22, 2023 · N660UA · Boeing 767322 · Nacelle/Pylon, Main Frame
  > PDA 3 LEFT PYLON INB SIDE AFT FAIRING MISSING ONE BOLT. SEE PICTURE. INSTALLED BOLT IN THE AFTER FAIRING OF LEFT PYLON. REF AMM 54-53. ITEM OK FOR SERVICE
- [SDR CALA2023052201593](https://openairdocs.org/sdr/CALA2023052201593.md): Tire · worn · May 19, 2023 · N660UA · Boeing 767322 · Tire
  > #2 TIRE PRESSURE IS LOW. TIRE NEEDS TO BE REPLACED PER MM. WORN ROTABLE PARTS CHANGE WAS INDICATED - TT # 1368312 SN OFF 6620 WHEEL, TIRE, AS OFF 76-3245-9-9001 6620 ON 76-3245-9-9001 0284 REPLACED #2 MLG TIRE. REF AMM 32-45-01-404-027.
- [SDR CALA2023033100954](https://openairdocs.org/sdr/CALA2023033100954.md): Light · dim · Mar 31, 2023 · N660UA · Boeing 767322 · Lighting System
  > CABIN SEAT 21 TO 24DEF CEILING EMER LIGHT DIM AFTER 3 MINUTES POWER ON TEST. TRANSFER REF NR HX WO.1576589 AND ORIGINATED BY EMP NO.V905892. M737 BATTERY CHARGER AND BATTERY REPLACED AND EMER LIGHT OP TEST RESULT NORMAL REF AMM 33-51-07. WORK ACCOMPLISHED BY M
- [SDR CALA2021092801716](https://openairdocs.org/sdr/CALA2021092801716.md): Module · damaged · Sep 28, 2021 · N660UA · Boeing 767322 · Trailing Edge Flap Control System
  > REF LOG PAGES 7121337 & 7121340 FOUND FLAP SLAT HYD SHUT OFF MODULE CAP RUPTURED AND SPOOL SLIDER AND SPRING DISLODGED IN RH WHEEL WELL ON AFT BULKHEAD. PARTS INFO ADDED. FLAGGED FOR SERVICE DIFFICULTY REPORTABLE. STARTED REMOVING VALVE PER AMM 27-51-48-022-
- [SDR CALA2020110601250](https://openairdocs.org/sdr/CALA2020110601250.md): Support Bracket · cracked · Nov 6, 2020 · N660UA · Boeing 767322 · Nacelle/Pylon Miscellaneous Structure
  > REF AMES NR 0561 PANEL ATTACHED SUPPORT BRACKET IS CRACK UNDER PANEL 437AR. REMOVED AND INSTALLED PANEL SUPPORT UNDER PANEL 437AR. FABRICATED PART USING 7075 T6-.063, IAW BOEING DWG 313T4310 AND SRM 51-40-02 PARAGRAPH 7. SEE BACK FOR PARTIAL WORK ADD EMP:V
- [SDR CALA2020110601249](https://openairdocs.org/sdr/CALA2020110601249.md): Panel · chafed · Nov 6, 2020 · N660UA · Boeing 767322 · Nacelle/Pylon, Plate/Skin
  > REF AMES NR 0128 PANEL 447AR CHAFED(M) PANEL 447AR DEEPEST DEPTH WAS.025" EXCEEDED MAXIMUM LIMITS THE METAL WAS VERIFIED. FABRICATED AND TREATED, PRIMED AND APPLIED TOP COAT, IAW B767 54-53-70 DETAIL V ALLOWABLE DAMAGE, PL313T1200, DWG 313T1200, AMM 51-21-04
- [SDR CALA2020032000643](https://openairdocs.org/sdr/CALA2020032000643.md): Connector · broken · Mar 13, 2020 · N660UA · Boeing 767322 · Navigation System Wiring
  > PER CREW: MINIMUM MANEUVERING SPEED BAR ON CAPT AND FO EHSI''S FLUCTUATES DURING FLT FROM 0 TO 300KTS. SWITCHING TO ALT CADC HAD NO EFFECT. DEBRIEFED CREW, FUEL AT 62800. NOT OVERWEIGHT LANDING. FLIGHT CREW TRIED ALT EFI,ADC WITH NO CHANGE IN DISPLAYS,FLUCTUA
- [SDR CALA2019050300685](https://openairdocs.org/sdr/CALA2019050300685.md): O-Ring · leaking · May 1, 2019 · N660UA · Boeing 767322 · Aircraft Fuel Distribution System
  > THE AIRCRAFT DIVERTED FOR PLACARD ON ANTI-SKID SYSTEM 3242A. DISPATCH RELEASED AIRCRAFT BASED ON WEATHER PREDICTION OF DRY RUNWAYS IN ORD AT TIME OF ARRIVAL. RAIN LASTED LONGER THAN FORECAST, MEL RESTRICTIONS PROHIBIT LANDING ON WET RUNWAYS. REQUIRED DIVERSION
- [SDR CALA2019020800218](https://openairdocs.org/sdr/CALA2019020800218.md): Floor Support · corroded · Feb 4, 2019 · N660UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > REFER NR LP 9131318 B767-53-3-6223 CABIN - BS 852 RBL 55 FLR BEAM FOUND CORRODED CABIN FLOOR BEAM UPPER CHORD AT BS 786 TO BS 890 RBL 55 REPAIRED AS PER SRM 53-00-51 REPAIR 3 FIG 201 ATTACHED FORM 44.0008 ITEM 1 TO ITEM 4 ACCOMPLISHED ADD EMP:V897526 RII BY HX
- [SDR CALA2019020800217](https://openairdocs.org/sdr/CALA2019020800217.md): Floorbeam · corroded · Feb 4, 2019 · N660UA · Boeing 767322 · Fuselage Main, Floor Beam
  > REFER NR LP 9131310 B767-53-3-6222 CABIN - BS 346 RBL 30-50 FLR BEAM FOUND CORRODED CABIN STA 346 BL 0 TO RH MOST O/B FLOOR BEAM UPPER CHORD REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND ATTACH FORM 44.0008 MAINTENANCE WORKSHEET ITEM 1-24 WORK ACCOMPLISHED
- [SDR CALA2019020800215](https://openairdocs.org/sdr/CALA2019020800215.md): Floorbeam · corroded · Feb 4, 2019 · N660UA · Boeing 767322 · Fuselage Main, Floor Beam
  > REF NR LP 9132172 B767-53-3-6165 CABIN STA 325 RBL 19 FLOOR BEAM FOUND CORROSION CABIN STA 325 RBL 19 FLOOR BEAM UPPER CHORD REPAIRED AS PER ECRA 5315-01113 REV - ATTACHED FORM 44.0008 ITEM 1 TO ITEM 21 ACCOMPLISHED ADD EMP:V913116 INSPECTED BY HX202044, APPRO
- [SDR CALA2019020400213](https://openairdocs.org/sdr/CALA2019020400213.md): Floorbeam · corroded · Feb 4, 2019 · N660UA · Boeing 767322 · Fuselage Main, Floor Beam
  > CABIN BS 346 RBL 30-50 FLOORBEAM FOUND CORRODED CABIN STA 346 BL 0 TO RT MOST O/B. FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND ATTACH FORM 44.0008 MAINTENANCE WORKSHEET ITEM 1-24 WORK ACCOMPLISHED BS346 FLOORBEAM ORIGINAL THICKNESS
- [SDR CALA2019020400212](https://openairdocs.org/sdr/CALA2019020400212.md): Floorbeam · corroded · Feb 4, 2019 · N660UA · Boeing 767322 · Fuselage Main, Floor Beam
  > CABIN BS 852 RBL 55 FLOORBEAM FOUND CORRODED. CABIN FLOORBEAM UPPER CHORD AT BS 786 TO BS 890 RBL 55 REPAIRED AS PER SRM 53-00-51 REPAIR 3 FIG 201 ATTACHED FORM 44.0008 ITEM 1 TO ITEM 4 ACCOMPLISHED.
- [SDR CALA2019020400209](https://openairdocs.org/sdr/CALA2019020400209.md): Panel · corroded · Feb 4, 2019 · N660UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT MOST RT TORQUE BOX PANEL FOUND CORRODED AT STA 544 AS MARK FWD CARGO COMPT MOST RT TORQUE BOX PANEL AT STA 544 TOP SURFACE. CORROSION CLEANED UP PER SRM 51-10-02 AND REPROTECTED PER SRM 51-20-01 AND WIRH MAINTENANCE WORKSHEET ITEM 1 TO ITEM 11
- [SDR CALA2019020100203](https://openairdocs.org/sdr/CALA2019020100203.md): Floor Support · corroded · Jan 31, 2019 · N660UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > REF NR LP 9131321 B767-53-3-6223 CABIN - BS 842-852 LBL 55 FLR BEAM FOUND CORRODED CABIN FLOOR BEAM UPPER CHORD REPAIRED AT BS790 TO BS901 LBL 55 AS PER SRM 53-00-51 REPAIR 3 FIG 201 ATTACHED FORM 44-0008 ITEM 1 TO ITEM 21 ACCOMPLISHED ADD EMP:V897532 INSPECTE
- [SDR CALA2018121402560](https://openairdocs.org/sdr/CALA2018121402560.md): Pawl · broken · Dec 10, 2018 · N660UA · Boeing 767322 · Service Doors
  > DOOR 1R WILL NOT ARM DOOR 1R HAS BOTH INTERLOCK PAWL ARMS BROKEN. PAWL REMOVED FROM HOUSING REF AMM52-11-26-401. PER AMM 52-11-26-350-801C1 WITHIN 10 DAYS REMOVE AND REPLACE BROKEN PAWL IAW 52-11-26-401. PRIOR TO EACH FLT UNTIL PAWL IS REPLACED ENSURE EXTERIOR

Next page: https://openairdocs.org/aircraft/N660UA/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 = 'N660UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N660UA/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.