# Service difficulty reports: N655UA

A list on [N655UA](https://openairdocs.org/aircraft/N655UA.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 8 · 382 reports

- [SDR CALA2026100820228](https://openairdocs.org/sdr/CALA2026100820228.md): Light · broken · Oct 7, 2026 · N655UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY ESCAPE PATH LIGHT ASSEMBLY ON SEAT 49D IS BROKEN. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY ON SEAT 49D REF AMM 33-51-10-962-104. EMERGENCY ESCAPE PATH LIGHT SYSTEM IS GOOD FOR SERVICE.
- [SDR CALA2026081918727](https://openairdocs.org/sdr/CALA2026081918727.md): Light · broken · Aug 18, 2026 · N655UA · Boeing 767322 · Emergency Lighting
  > ESCAPE PATH LIGHT ASSEMBLY ON SEAT 33D, 40F AND 50F ARE BROKEN. REMOVED AND REPLACED ESCAPE PATH LIGHT ASSEMBLY ON SEATS 40F AND 50F REF AMM 33-51-10-962-104. ESCAPE PATH LIGHT SYSTEM IS GOOD FOR SERVICE.
- [SDR CALA2026042015483](https://openairdocs.org/sdr/CALA2026042015483.md): Floorbeam · corroded · Apr 18, 2026 · N655UA · Boeing 767322 · Fuselage Main, Floor Beam
  > ON THE FLOOR STRUCTURE CABIN PAX, PRESSURE DECK AREA WAS FOUND THE FITTING WITH CORROSION AT BS 977, RBL95, WL 189. PERFORMED INTERIM REPAIR OF THE RT BS 977 FRAME AT WL 190 OTBD CHORD CORROSION IAW ECRA 5310-08324, PART 1, IT IS NECESSARY TO ACCOMPLISH THE P
- [SDR CALA2026031214519](https://openairdocs.org/sdr/CALA2026031214519.md): Fuel Cap · missing · Mar 8, 2026 · N655UA · Boeing 767322 · Fuel Storage
  > FUELERS REPORT LT AND RT REFUEL CAP MISSING. NO LEAKS OR FOREIGN MATERIAL. MAINTENANCE DDP COMPLIED WITH INSTALLED BOTH FUEL CAPS IAW AMM 28-00-00.
- [SDR CALA2025122912509](https://openairdocs.org/sdr/CALA2025122912509.md): Skin · damaged · Dec 20, 2025 · N655UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > DURING WALKAROUND, OBSERVED SMALL DAMAGED ON RT LOWER FUSELAGE BETWEEN BS 1219 & 1241, S36 & 37R. REMOVED PAINT. PERFORMED HFEC AS PER NDT PART 6 51-00-19, IT WAS FOUND A CRACK IN THE AREA. MEASUREMENT: CRACK: 1,5 IN; CRACK TO BS 1219: 15 IN; CRACK TO S-38R 6,
- [SDR CALA2025111811298](https://openairdocs.org/sdr/CALA2025111811298.md): Gas Cylinder · low pressure · Nov 15, 2025 · N655UA · Boeing 767322 · Escape Slide
  > L2 DOOR GAUGE OUT OF THE GREEN. PERFORMED INSPECTION IAW AMM GAS CYLINDER GAUGE CHECK.IAW TASK 25-66-99-702-001, ITEM WITHIN LIMITS. THE PRESSURE IS AT 3100PSI. ITEM GOOD TO GO.
- [SDR CALA2025101510125](https://openairdocs.org/sdr/CALA2025101510125.md): Eec · faulted · Oct 13, 2025 · N655UA · Boeing 767322 · Fuel Controlling System
  > LEFT ENGINE HUNG UP AT LOW POWER SETTING AND WOULD NOT INCREASE ON FINAL ON FINAL, DURING THROTTLE LEVER MOVEMENTS. THROTTLES PULLED BACK & LT ENG N1 DID NOT INCREASE WITH THROTTLE LEVER INPUT, PARTIAL RPM LOSS. EPR DID SHOW THE COMMAND BAR TARGET, BUT NO
- [SDR CALA2025100109516](https://openairdocs.org/sdr/CALA2025100109516.md): Slide · no discrepancy · Sep 30, 2025 · N655UA · Boeing 767322 · Escape Slide
  > L2 DOOR GAUGE NOT IN THE GREEN. SLIDE PRESSURE IN LIMITS IAW AMM 25-66-99-702-001.
- [SDR CALA2025082708180](https://openairdocs.org/sdr/CALA2025082708180.md): Slide · none · Aug 23, 2025 · N655UA · Boeing 767322 · Standard Practices/Structures
  > DEACTIVATED L1 SLIDE IN REF WITH AMM 25-66-03 FOR GIRT BAR CARRIER REMOVAL. REACTIVATED DOOR 1L SLIDE REF AMM 25-66-03-404-098. REMOVED AND STOWED SAFETY PIN FROM INFLATION CYLINDER. FLAGGING FOR INSPECTION INSPECTED REACTIVATION OF DOOR SLIDE AS REQUIRED PER
- [SDR CALA2025082708179](https://openairdocs.org/sdr/CALA2025082708179.md): Pin · installed · Aug 23, 2025 · N655UA · Boeing 767322 · Standard Practices/Structures
  > INSTALLED GROUND LOCK PIN ON L1 DOOR FOR GIRT BAR CARRIER REMOVAL. REMOVED GROUND LOCK PIN ON L1 DOOR AFTER GIRT BAR CARRIER INSTALLATION REF AMM 52-11-13
- [SDR CALA2025082107988](https://openairdocs.org/sdr/CALA2025082107988.md): Door · leaking · Aug 18, 2025 · N655UA · Boeing 767322 · Emergency Exits
  > PAX REPORTED LOUDER AIR NOISE AT 31D. CONFIRMED BY F/A AND PILOT COMPARE D TO 31A. BOTH EMERGENCY EXIT NO PRESSURIZATION ISSUE REPORTED, GVI OF ALL 4 EMERGENCY EXITS SATIS, FLUSHNESS OF ALL 4 EMERGENCY EXITS ALSO CHECKED SATIS
- [SDR CALA2025051904786](https://openairdocs.org/sdr/CALA2025051904786.md): Battery Pack · inoperative · May 16, 2025 · N655UA · Boeing 767322 · Emergency Lighting
  > EMER EXIT LIGHT COVER BY 1L CAME OFF RESECURED COVER, WHILE OPS CHECK PERFORMED BOTH L1 & R1 DOOR EMERGENCY LIGHT INOP REF AMM TASK 33-51-00-715-019-001. R&R POWER SUPPLY FOR BATTERY PACK M1208 REF AMM 33-51-07, OPS CHECKED GOOD.
- [SDR CALA2025051204622](https://openairdocs.org/sdr/CALA2025051204622.md): Idg · faulted · May 8, 2025 · N655UA · Boeing 767322 · AC Generator-Alternator
  > GENERATOR DRIVE SYSTEM EICAS MESSAGE (01=L, 02=R) GEN DRIVE SHOW N. DRIVE LGT ON. GEN DRIVE DISC. NOTE: RECURRENT IDG TEMP AND CO OLING VLV EICAS MSG & ON/OFF OR STEADY ON OF THE DRIVE LGT, MAY BE CAUSED BY IDG TEMP BULB (PIN/SOCKET WEAR). TO VERIFY, FI 02UNAB
- [SDR CALA2025041703955](https://openairdocs.org/sdr/CALA2025041703955.md): Window · cracked · Apr 15, 2025 · N655UA · Boeing 767322 · Door Windows
  > DOOR 1L INNER PRISM WINDOW CRACKED FOUND HEATED PANE CRACKED. PRISM AND OUTER PANE ARE OK. SEE ATTACHED PIC. REMOVED AND REPLACED INNER MOST HEATED WINDOW. OPS CHECK GOOD. REF AMM 56-31-01 ADD EMP:409288
- [SDR CALA2024110601031](https://openairdocs.org/sdr/CALA2024110601031.md): Light · no test · Nov 4, 2024 · N655UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - DUNRING WALK AROUND FOUND TREE EMERGENCY LIGHTS INOP, POSITION ONE LH AND TWO RH. REPLACEMENT THE SLIDE AND OVERWING ESCAPE LIGHT LAMP AS PER AMM- TASK 33-51-06-902-082, CHECKED OK.
- [SDR CALA2024071802061](https://openairdocs.org/sdr/CALA2024071802061.md): Trim System · unknown · Jul 14, 2024 · N655UA · Boeing 767322 · Rudder Tab Control System
  > AFTER TAKEOFF NEEDED ALMOST 8 DEGREES RIGHT RUDDER. TRIED TO ALS O USE AILERON TRIM. NO HELP DEBRIEFIED CREW, BOTH ENGINE EPR WAS SAME PASSED. TRIM TEMPERATURE COMPENSATING LINKAGE. NO DEFECTS FOUND. NO SIGNIFICANT FINDINGS AT THIS TIME. FIM: 27-09 TASK 814,
- [SDR CALA2024061301788](https://openairdocs.org/sdr/CALA2024061301788.md): Overhead Bin · broken · Jun 10, 2024 · N655UA · Boeing 767322 · Passenger Compartment Equipment
  > OVERHEAD BIN AT 9 CTR BROKEN. THE BIN WHERE THE AVIOX IS LOCATED. REPOSITIONED LOOSEN ATTACHING SCREW REF AMM 25-00-00. ADDING CORRECT AMM REFERENCE: 25-28-01-902-003 (SUBTASK 25-28-01-422-005).
- [SDR CALA2024052401589](https://openairdocs.org/sdr/CALA2024052401589.md): Floorbeam · corroded · May 24, 2024 · N655UA · Boeing 767322 · Fuselage Main, Floor Beam
  > SEC 45- ON THE FLOOR STRUCTURE CABIN PAX, PRESSURE DECK AREA WAS FOUND THE FITTING WITH CORROSION AT STA 977, LBL95, WL 189
- [SDR CALA2024052701593](https://openairdocs.org/sdr/CALA2024052701593.md): Floor Support · corroded · May 20, 2024 · N655UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > FLOOR STRUCTURE CABIN PAX, PRESSURE DECK AREA WAS FOUND THE FITTING WITH CORROSION AT BS 977, RBL95, WL 189 ACCOMPLISH THE INSPECTIONS AS PER PART 2 OF THE LATEST REV C, WHICHEVER OCCURS FIRST. PERFORM REPEAT I VER OCCURS FIRST. ISION OF EC/RA 5310-08324 ON O
- [SDR CALA2024052401590](https://openairdocs.org/sdr/CALA2024052401590.md): None · none · May 20, 2024 · N655UA · Boeing 767322 · Standard Practices/Structures
  > DURING AGING INSPECTION FOUND DOUBLER REPAIR WITH NO RECORDS AT STA. 1788 STR 38R. TEGORY B REPAIR AND REQUIRES RIR, IT IS NECESSARY TO ACCOMPLISH 5375-01010 ON OR BEFORE A/C REACHES 37,500 TOTAL FC. ACCOMPLISH RVALS NOT TO EXCEED 12,000 FC THEREAFTER. INSPECT
- [SDR CALA2024052401588](https://openairdocs.org/sdr/CALA2024052401588.md): Skin · cracked · May 20, 2024 · N655UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > DURING NDT PROCEDURE AS PER PART 6, 51-00-16. IT WAS FOUND A CRACK HOLE AT STA 340 AND STGR 20R ON THE FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER. GENERATE UPDATE TO ATTACH IMAGES FROM THE DAMAGED HOLE AND CHANGE THE ATTRIBUTES TO MAJOR REPAIR AND SDR.
- [SDR CALA2024052401584](https://openairdocs.org/sdr/CALA2024052401584.md): Skin · corroded · May 20, 2024 · N655UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF NR:1896678 WAS FOUND CORROSION IN THE INTERNAL FUSELAGE SKIN PANEL LOCATED BTW STA. 1562/1582 AND STGR 24/25 LH SIDE. FOR REFERENCE SEE: SRM 53-60-01-0I-1.
- [SDR CALA2024052201556](https://openairdocs.org/sdr/CALA2024052201556.md): Skin · damaged · May 20, 2024 · N655UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > DURING INSPECTION AT 321BL; 322AL & 323AL LH UPPER SKIN B.L 0.0 AT SEC 48 BS 1582 TO BS 1654; WAS FOUND SKIN WITH SCRATCHES AND NICK. NECESSARY EVALUATION PROCESS. SEE IMAGES FOR FUTHER DETAILS. 7245 PART 1.A AND PART 1.B. THIS REPAIR IS A CATEGORY ''''B'''' R
- [SDR CALA2024052401585](https://openairdocs.org/sdr/CALA2024052401585.md): Skin · damaged · May 18, 2024 · N655UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > DURING "OK TO CLOSE" FOR PANEL 196NR FOUND A SCRIBE LINE ALONG UPPER FAIRING EDGE IN AIRCRAFT SKIN BTW STA 1153 - 1219 RH SIDE, SEE PICS FOR DETAILS.
- [SDR CALA2024052001527](https://openairdocs.org/sdr/CALA2024052001527.md): Landing · corroded · May 18, 2024 · N655UA · Boeing 767322 · Fuselage Main, Structure
  > DURING INSPECTION AT 313AL TAIL COMPARTMENT SEC 48 STA 1809.5 RH TO STA 1832 RH WAS FOUND RS-39 TO RS-37 STRINGERS WITH CORROSION. SEE IMAGES FOR FUTHER DETAILS. REPLACED THE STRINGER 30RH, 32RH AND 36RH AS PER BOEING 767 SRM 51-40-02 AND DWG 148T3280. ITEM OK
- [SDR CALA2024052001526](https://openairdocs.org/sdr/CALA2024052001526.md): Landing · corroded · May 18, 2024 · N655UA · Boeing 767322 · Fuselage Main, Structure
  > AT 313AL SEC 48 TAIL COMPARTMENT ACESS BETWEEN STA 1809.5 LH AND S-30 TO S-36WAS FOUND CORROSION. SEE IMAGES FOR FUTHER DETAILS. TION ON THE EXISTENT HOLES ON AIRCRAFT SKIN, AT AREA OF STRINGER S 30LH, 32LH AND 36LH, ACCORDING TO B767 NDT MANUAL PART 6, 51-0 0
- [SDR CALA2024052001534](https://openairdocs.org/sdr/CALA2024052001534.md): Stringer · corroded · May 18, 2024 · N655UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT - FOUND SIGNS OF CORROSION AT AREA OF STRINGER S-36L BETWEEN BS 1131-1153.
- [SDR CALA2024052701592](https://openairdocs.org/sdr/CALA2024052701592.md): Skin · cracked · May 16, 2024 · N655UA · Boeing 767322 · Passenger/Crew Doors
  > DURING VISUAL INSPECTION AFTER SCUFF PLATE REMOVAL, FOUND SCRIBE LINES IN THE AREA UNDER SCUFF PLATE AT FUSELAGE SKIN 1L DOOR FWD & AFT LOWER CORNER. LOCATED BTW BS 287 & 347 BTW S20L & 21L. THIS IS A CATEGORY B REPAIR. PERFORMED INTERIM REPAIR OF FUSELAGE
- [SDR CALA2024052401587](https://openairdocs.org/sdr/CALA2024052401587.md): None · none · May 8, 2024 · N655UA · Boeing 767322 · Standard Practices/Structures
  > DURING AGING INSPECTION FOUND REPAIR AT APPROX. STA. 1562 STR. 20L-21L WITH NO RECORDS. ART 1. THE REPAIR ACCOMPLISHED IN PART 1 OF ECRA 5330-07244 IS A UIRED REPETITIVE INSPECTION REQUIREMENTS (RIR). IT IS NECESSARY VISION OF ECRA 5330-07244 ON OR BEFORE 37,5
- [SDR CALA2024052401582](https://openairdocs.org/sdr/CALA2024052401582.md): None · none · Apr 17, 2024 · N655UA · Boeing 767322 · Standard Practices/Structures
  > DURING AGING INSPECTION WAS FOUND A REPAIR AT STA 202-208 STR 29LT SRM 53-00-01 AMIS ITEM 2182092 CATEGORY B REPAIR WITH NO DIP.
- [SDR CALA2024052401586](https://openairdocs.org/sdr/CALA2024052401586.md): Floorbeam · corroded · Apr 1, 2024 · N655UA · Boeing 767322 · Fuselage Main, Floor Beam
  > DURING INSPECTION WAS FOUND FLOOR BEAM STA 325 UPPER CHORD FLANGE LBL 40- 54.75 CLOSE TO THE PASSENGER DOOR WITH CORROSION SPOTS UPPER SURFACE.
- [SDR CALA2023121803659](https://openairdocs.org/sdr/CALA2023121803659.md): Engine · fire · Dec 18, 2023 · N655UA · Boeing 767322 · Engine (Turbine/Turboprop)
  > L ENG TAIL PIPE FIRE ON FUEL INTRO NO FIRE INDICATIONS BUT LARGE FIRE REPORTED
- [SDR CALA2023121103626](https://openairdocs.org/sdr/CALA2023121103626.md): Valve · faulty · Dec 11, 2023 · N655UA · Boeing 767322 · Aircraft Fuel Distribution System
  > R SPAR VALVE EICAS AND LIGHT ON ENGINE START. REMOVED AND REPLACED RH SPAR VAVE PER AMM 28-22-01.DEVICE WORKS FINE. PARTS USED: 1165583,QTY:1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1165583 SN OFF 6128 IPC REFERENCE # 28-22-01-02 ACTUATOR, VALVE OFF 29-2
- [SDR CALA2023111503363](https://openairdocs.org/sdr/CALA2023111503363.md): Unknown · unknown · Nov 10, 2023 · N655UA · Boeing 767322 · Air Conditioning System
  > L PACK OVER TEMP. CREW REJECTED TAKE OFF AROUND 80KNOTS. CREW REPORT NOT SURE LEFT OR RIGHT PACK TEMP MSG REQ TOMC APRVL DEFERRED LT AND RIGHT PACK AUTO FUNCTION PER MEL TO DEF AUTO MODE LT AND RT PACK NO FAULTS NOTICED. ON CONTROLLERS... PRECAUTIONARY PUT B
- [SDR CALA2023110603287](https://openairdocs.org/sdr/CALA2023110603287.md): Modulating Valve · faulty · Nov 2, 2023 · N655UA · Boeing 767322 · Cabin Cooling System
  > FLT DK PACK INOP ANNUNCIATOR LIGHT INOP.FLT DECK TEMP EICAS MESSAGE. REQUEST MEL FOR FLIGHT DECK ANNUN LIGHT. DDP COMPLIED WITH. OK TO DEF TRIM AIR FLIGHT DECK ANNUNCIATOR LIGHT. AFFECTED ITEM IS TRIM AIR FLIGHT DECK ANNUNCIATOR LIGHT. SEE PICTURE OF LIGHT REP
- [SDR CALA2023102703211](https://openairdocs.org/sdr/CALA2023102703211.md): Light · inoperative · Oct 25, 2023 · N655UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - THE FLIGHT DECK EXIT SIGN LIGHT IS INOPERATIVE AFTER PUT SWITCH EMERGENCY LIGHT, P5, TO ON. ADD PHOTO INFO. REMOVED AND REPLACED LIGHT EMERG EXIT, OPS CHECK GOOD PER AMM 33-51-01. PARTS USED: 1550953,QTY
- [SDR CALA2023030600628](https://openairdocs.org/sdr/CALA2023030600628.md): Terminal · damaged · Mar 3, 2023 · N655UA · Boeing 767322 · Lighting System
  > OVERWING HATCH EXIT SIGN DIM AT L322 AND L297 REF HAECO NON-ROUT INE NO.:9407719,ORIGINATED BY EMP V905488,SPEC NO.:B767-33-3-700 0. PERFORMED BY EMP V905488,PERFORMED WIRING CHECK FOUND L297 LIGHT TERMINAL POOR CONDITION,REPLACED L297 TERMINAL AND INSTALLATIO
- [SDR CALA2023030300601](https://openairdocs.org/sdr/CALA2023030300601.md): None · damaged · Mar 3, 2023 · N655UA · Boeing 767322 · Lighting System
  > CEILING PANEL EMERGENCY LIGHT CONNECTOR DAMAGE AT FWD ZONE R/H NO.2,AFT ZONE R/H NO.4,AFT ZONE R/H NO.9,AFT ZONE L/H NO.9 CEILI NG PANEL,1A-10A,1L-10L CEILING PANEL REF HAECO NON-ROUTINE NO.: 9404868,ORIGINATED BY EMP V905488,EA 2500-12986 OP001. PERFORMED BY
- [SDR CALA2023030300615](https://openairdocs.org/sdr/CALA2023030300615.md): Skin · none · Mar 1, 2023 · N655UA · Boeing 767322 · Fuselage Structure (General)
  > FUS STA 456-478 S-32L TO S-35L FOUND A DENT ON EXISTING SKIN REPAIR DOUBLER. SEE MRO ENGINEERING DOCUMENT EN.: EG 53-1105 (INCLUDED IN ECRA 5330-07058). PART 2 INSPECTION REQUIREMENTS FOR THE REINFORCING SKIN DOUBLER INSPECTION REQUIREMENTS EVERY 9,000 FLIGHT
- [SDR CALA2023030100585](https://openairdocs.org/sdr/CALA2023030100585.md): Skin · dented · Feb 28, 2023 · N655UA · Boeing 767322 · Fuselage Main, Structure
  > FUS STA 412 S 33L-34L FOUND A DENT ON EXISTING REPAIR DOUBLER. REVISION OF ECRA 5310-08118 BEFORE AIRCRAFT REACHES 37,500 TOTAL NOT TO EXCEED 9,000 FLIGHT CYCLES. FLIGHT CYCLES. REPEAT THE INSPECTIONS THEREAFTER AT INTERVALS ACCOMPLISH INSPECTION OF REINFORCIN
- [SDR CALA2023022400543](https://openairdocs.org/sdr/CALA2023022400543.md): Lamp · malfunctioned · Feb 23, 2023 · N655UA · Boeing 767322 · Emergency Lighting
  > R/H FIRST OVER WING EGRESS LIGHT L394 INOP,REF TO HAECO NON ROUT INE NO.9403697,ORIGINATED BY EMP V905488,SPEC NO.B767-33-3-7004. PERFORMED BY EMP V905488,REPLACED R/H FIRST OVER WING EGRSS LIGH T L394 LAMPS AND NEW LAMP TEST FOUND PASS AS PER AMM 33-51-06-90
- [SDR CALA2023022400542](https://openairdocs.org/sdr/CALA2023022400542.md): Lamp · malfunctioned · Feb 23, 2023 · N655UA · Boeing 767322 · Emergency Lighting
  > L/H WING AFT SLIDE LIGHT L645 INOP,REF TO HAECO NON ROUTINE NO.9 403690,ORIGINATED BY EMP V905488,SPEC NO.B767-33-3-7004. PERFORMED BY EMP V905488,REPLACED L/H WING AFT SLIDE LIGHT L645 LAMP AND NEW LAMP TEST FOUND PASS AS PER AMM 33-51-06-902-082 RE V 138,IDT
- [SDR CALA2023022400541](https://openairdocs.org/sdr/CALA2023022400541.md): Lamp · malfunctioned · Feb 23, 2023 · N655UA · Boeing 767322 · Emergency Lighting
  > R/H AFT DOOR SLIDE LIGHT L392 INOP,REF TO HAECO NON ROUTINE NO.9 403694,ORIGINATED BY EMP V905488,SPEC NO.B767-33-3-7004. PERFORMED BY EMP V905488,REPLACED R/H AFT DOOR SLIDE LIGHT L392 LAMP AND NEW LAMP TEST FOUND PASS,AS PER AMM 33-51-06-902-082 RE V 138,IDT
- [SDR CALA2023022400540](https://openairdocs.org/sdr/CALA2023022400540.md): Connector · cracked · Feb 23, 2023 · N655UA · Boeing 767322 · Emergency Lighting
  > CEILING PANEL EMERGENCY LIGHT CONNECTOR LOOSEN AT 33AB,23AB,44AB,9L,21LK,30LK,33LK,36LK,39LK,42LK,45LK,50LK,REF TO HAECO NON ROU TINE NO.9404153,ORIHINATED BY EMP V905488,EA 4420-03294 REV B OP 001. PERFORMED BY EMP V905488,REPLACED CEILING PANEL EMERGENCY LI
- [SDR CALA2023010400018](https://openairdocs.org/sdr/CALA2023010400018.md): Stand Off · broken · Jan 3, 2023 · N655UA · Boeing 767322 · Engine Thrust Reverser
  > DURING THRUST REVERSE MEL T/S(3421891), FOUND PANEL ASSY FOR RELAY K10359 LOOSE SUPPORTS BROKEN. FIM 78-34. REMOVED AND REPLACED 04EA STANDOFFS IAW SRM 51-40-02-0G-0 PARAGRAPH 7. SUPPLYED ELECTRICAL POWER ON A/C AS PER AMM 24-22-00-201. NO DISCREPANCIES FOUN
- [SDR CALA2021021900187](https://openairdocs.org/sdr/CALA2021021900187.md): Skin · corroded · Feb 18, 2021 · N655UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > BULK CARGO - STA 1542 STR 39 BL0 WATER DRAIN VALVE SURROUNDING SKIN FOUND CORR REFER NR LP 9131165 BULK CARGO STA 1542 STR 39 BLD WATER DRAIN VALVE SKIN AREA. REPLACED AS PER ECRA 5360-01578 REV - PART 1 INTERIM REPAIR ADD.
- [SDR CALA2021021700185](https://openairdocs.org/sdr/CALA2021021700185.md): Skin · dented · Feb 16, 2021 · N655UA · Boeing 767322 · Cargo/Baggage Doors
  > B767-53-3-7006 BULK CGO - CGO DOOR EXTERIOR AREA STA 1461 EXISTING PATCH FOUND DENT AS MARKED REF NR LP 9130916 ACCOMPLISH INITIAL INSPECTIONS AS DEFINED IN LATEST REVISION EC5236-01021 PART 2 ON OR BEFORE THE BULK CARGO DOOR REACHES 30,000 FLT CYCLES. PERFORM
- [SDR CALA2021021700184](https://openairdocs.org/sdr/CALA2021021700184.md): Shear Tie · corroded · Feb 16, 2021 · N655UA · Boeing 767322 · Fuselage Internal Mounting Structure
  > B767-53-3-7058 BULK CARGO - STA 1540 STR 38R-39R INTERNAL SHEAR TIE FOUND CORR REF NR LP 9131254 BULK CARGO STA 1540 STR 38R-39R SHEAR TIE REPLACED AS PER SRM 51 -10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02.
- [SDR CALA2021021700183](https://openairdocs.org/sdr/CALA2021021700183.md): Shear Tie · corroded · Feb 16, 2021 · N655UA · Boeing 767322 · Fuselage Internal Mounting Structure
  > B767-53-3-7154 AFT CGO - STA 1219 BILGE AREA S36R - S38R SHEAR TIE FOUND CORRODED AS MARKED REF NR LP 9131157 AFT CARGO STA 1219 S36R-S38R 2EA SHEAR TIE REPLACED AS PER SRM 5 1-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02
- [SDR CALA2021021700182](https://openairdocs.org/sdr/CALA2021021700182.md): Shear Tie · corroded · Feb 16, 2021 · N655UA · Boeing 767322 · Fuselage Internal Mounting Structure
  > B767-53-3-7154 AFT CGO - STA 1197+110 BETWEEN S38R-S39R SHEAR TIE FOUND CORRODED AS MARKED REF NR LP 9131151 AFT CARGO STA 1197+110 S38R-S39R SHEAR TIE REPLACED AS PER SRM 5 1-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02.

Next page: https://openairdocs.org/aircraft/N655UA/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 = 'N655UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N655UA/reports

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