# Service difficulty reports: N658UA

A list on [N658UA](https://openairdocs.org/aircraft/N658UA.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 · 282 reports

- [SDR CALA2026082118777](https://openairdocs.org/sdr/CALA2026082118777.md): Wire · shorted · Aug 20, 2026 · N658UA · Boeing 767322 · Light System Wiring
  > EMERGENCY LIGHTS TEST WITH TEST SWITCHES. GALLEY G2(8X) AND G2A (4X) EMERGENCY ESCAPE PATH LIGHTS INOP. WIRING CHECK AS PER 767-N0624-D74, SSM SUPPLEMENT 25-00-00, FOUND SHORTED. DISCONNECTED AND REMOVED ALL 12 EMERGENCY LIGHT ASSY FROM G2 & G2A, FOUND ONE OF
- [SDR CALA2026070117499](https://openairdocs.org/sdr/CALA2026070117499.md): Washer · missing · Jul 1, 2026 · N658UA · Boeing 767322 · Wheel/Ski/Float
  > SUSPECT SPACER MISSING FROM RIGHT NOSE WHEEL. RIGHT NOSE WHEEL REMOVED PER AMM 32-45-02, NOTED THAT THE OUTBOARD TANG WASHER IS MISSING. WHEEL AND AXLE INSPECTED PER AMM 32-45-03. NO DAMAGE NOTED TO EITHER AND INBOARD SPACER FOUND FITTED. WHEEL REFITTED WITH
- [SDR CALA2026031014456](https://openairdocs.org/sdr/CALA2026031014456.md): Unknown · odor · Mar 7, 2026 · N658UA · Boeing 767322 · Air Distribution System
  > STRONG FUEL ODOR AFTER ENGINE SHUTDOWN THRU-OUT COCKPIT AND CABIN. RAN ENGINES TWICE, NO DEFECTS NOTED. FOLLOWED AMM 05-51-56-940-801-C1 UP TO AND INCLUDING STEP D8. FOUND NO DEFECTS. PERFORMED IDLE ENGINE RUN AND CHECKED FOR LEAKS ON ENG 2, NO LEAKS OR OD
- [SDR CALA2026012613275](https://openairdocs.org/sdr/CALA2026012613275.md): Regulator · no discrepancy · Jan 26, 2026 · N658UA · Boeing 767322 · Cabin Equipment/Furnishings
  > DISARM THE OFF-WING ESCAPE SYSTEM-INSTALLED THE SAFETY PIN INTO THE SAFETY HOLE OF THE LEFT INFLATION CYLINDER REGULATOR FOR MX.PER AMM 25-65-00. REMOVED AND STOWED SAFETY PIN FROM LEFT INFALTION CYLINDER REGULATOR IAW 25-65-01 VERIFIED REMOVAL AND STOWAGE OF
- [SDR CALA2026012613272](https://openairdocs.org/sdr/CALA2026012613272.md): Regulator · no discrepancy · Jan 26, 2026 · N658UA · Boeing 767322 · Cabin Equipment/Furnishings
  > DISARM THE OFF-WING ESCAPE SYSTEM. INSTALLED THE SAFETY PIN INTO THE SAFETY HOLE OF THE RT INFLATION CYLINDER REGULATOR FOR MX IAW AMM 25-65-00. REARMED THE OFF WING ESCAPE SYS & REMOVED SAFETY PIN TO RT INFLATION CYLINDER REGULATOR IAW AMM 25-65-00-442-010.
- [SDR CALA2026011312914](https://openairdocs.org/sdr/CALA2026011312914.md): Lock · failed · Jan 10, 2026 · N658UA · Boeing 767322 · Fixed Inner Doors
  > FLT DECK DOOR LOCK FAILED AFTER PUSHBACK AND WOULD NOT RESET. MEL 5251C APPLIED BY FLIGHT CREW NOC.MEL 5251C APPROVED MEL 5251C APPLIED *DM* RECOMMEND FIM 52-52 FAULT TREE 812 FOR INITIAL T/S ON INITIAL EVAL COULD NOT GET FLT DK ELECTRIC DOOR LOCK TO FAIL. OPE
- [SDR CALA2025090308417](https://openairdocs.org/sdr/CALA2025090308417.md): Slide · no discrepancy · Aug 29, 2025 · N658UA · Boeing 767322 · Escape Slide
  > DOOR 1R SLIDE RAFT PRESS GUAGE HAS CONDENSATION IS HARD TO READ. COMPLETED A GAS CYLINDER GAUGE CHECK IAW AMM 25-66 OPS CHECK GOOD OKAY TO CONTINUE
- [SDR CALA2025081407764](https://openairdocs.org/sdr/CALA2025081407764.md): Skin · delaminated · Aug 9, 2025 · N658UA · Boeing 767322 · Ailerons
  > RIGHT WING OUTBOARD AILERON HAS DELAMINATIONDELAMINATED AREA TAP TESTED AND MAPPED. LOWER SURFACE DIMENSIONS OF DELAM MEASURE AT 18" IN LEGNTH BY 9" IN WIDTH. IT HAS AN EDGE DISTANCE 1.5" AND A TRAILING EDGE DISTANCE OF 5" UPPER SURFACE OF AILERON TAP TESTED
- [SDR CALA2025060905378](https://openairdocs.org/sdr/CALA2025060905378.md): Stringer · corroded · Jun 5, 2025 · N658UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > BULK CARGO - FUSELAGE INTERNAL SKIN - DURING PRELIMINARY INSPECTION WAS FOUND STRINGER 39R WITH CORROSION AT STA 1542. IT WAS CREATED ESFR NECESSARY QC REVIEW AND APPROVAL. IT WAS CREATED ESFR NECESSARY QC REVIEW AND APPROVAL. PERFORMED INSPECTION AND APPROVED
- [SDR CALA2025060905377](https://openairdocs.org/sdr/CALA2025060905377.md): Floorbeam · corroded · Jun 5, 2025 · N658UA · Boeing 767322 · Fuselage Main, Floor Beam
  > BODY BELOW AFT CARGO COMPARTMENT FLOOR (INTERNAL) INSPECTION: IT WAS FOUND SIGNS OF CORROSION BELOW FLOORBEAM AT BS 1131, S-34R IT WAS CREATED ESFR NECESSARY QC REVIEW AND APPROVAL. PERFORMED INSPECTION AND APPROVED THE REPAIR AS PER EC/RA #5360-01963, PERFOR
- [SDR CALA2025060605339](https://openairdocs.org/sdr/CALA2025060605339.md): Stringer · corroded · Jun 5, 2025 · N658UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > DURING BODY BELOW AFT CARGO COMPARTMENT FLOOR (INTERNAL) CDP INSPECTION IT WAS FOUND SIGNS OF CORROSION AT STRINGER S-39R (UNDER STRINGER) LOCATED AT STA 1219. ALL OF STEPS OF ECRA 5360-01960 WERE PERFORMED WITHOUT ANY DEVIATION, NO MORE ACTION IS REQUIRED.F
- [SDR CALA2025061005433](https://openairdocs.org/sdr/CALA2025061005433.md): Skin · cracked · Jun 4, 2025 · N658UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > FWD SERVICE DOOR AFTER CORNER - IT WAS FOUND A CRACK INDICATION IN TWO HOLES (LOWEST HOLES) AT 1 AND 2 O'CLOCK POSITION. THE CRACK IS PRESENT ON THE SKIN AND BEARSTRAP. PERFORMED REPAIR AS PER EC/RA #5310-08602. PERFORMED INSPECTION AND ALL STEPS OF THE REPAIR
- [SDR CALA2025061005432](https://openairdocs.org/sdr/CALA2025061005432.md): Skin · cracked · Jun 4, 2025 · N658UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > FWD ENTRY DOOR AFTER CORNER - IT WAS FOUND A CRACK INDICATION IN ONE HOLE (LOWEST HOLE) AT 11 O'CLOCK POSITION THE CRACK IS PRESENT ON THE SKIN AND BEARSTRAP. PERFORMED REPAIR AS PER SRM 53-10-01-2R-1. PERFORMED INSPECTION AND ALL STEPS WERE ACCOMPLISHED WI
- [SDR CALA2025042104063](https://openairdocs.org/sdr/CALA2025042104063.md): Wire · broken · Apr 20, 2025 · N658UA · Boeing 767322 · Light System Wiring
  > R/H EMERGENCY DOOR LIGHT PANEL WIRE BROKEN.SEAT 20. REMOVED AND TERMINATED NEW LUGS ONTO EXIT SIGN ABOVE R OVER WING EXIT DOOR. IAW SWPM 20-30-11 AND WDM 33-51-14. REINSTALLED PANEL AND OPS CHECKED GOOD IAW AMM 33-51-00-715.
- [SDR CALA2025040903653](https://openairdocs.org/sdr/CALA2025040903653.md): Slide · failed · Apr 6, 2025 · N658UA · Boeing 767322 · Escape Slide
  > REF WC 64-2560-1-3800, SCHEDULED MX, R&R L4 SLIDE DUE TO 2 SLIDES BAD FROM STOCK, REINSTALLED ORIGINAL SLIDE AT LOCATION L4, IAW WC 64-2560-1-3800. PARTS NIS @ EWR, DEFERRING SLIDE CHANGE, IAW TOMC. QC VERIFIED L4 WC 64-2560-1-3800
- [SDR CALA2024122701669](https://openairdocs.org/sdr/CALA2024122701669.md): Idg · faulty · Dec 25, 2024 · N658UA · Boeing 767322 · AC Generator-Alternator
  > R GEN DRIVE EICAS LITE COMPLETED REMOVAL OF RH IDG IRT AMM 24-11-01-004-002-006. ALL UNIONS AND PARTS ARE LOCATED ON WORK TABLE NEXT TO ENGINE. ORDERED NEW O RINGS WAITING FOR THEM TO BE DELIVERED. START INSTALLATION OF R/H IDG REF AMM 24-11-01-404-001-006 UP
- [SDR CALA2024071800243](https://openairdocs.org/sdr/CALA2024071800243.md): Access Panel · missing · Jul 17, 2024 · N658UA · Boeing 767322 · Nacelle/Pylon, Plate/Skin
  > PDA 2 ON AIRCRAFT ARRIVAL, LEFT ENGINE INBOARD PYLON PANEL 436AR MISSING. REPORTING SDR FOR PDA 2.
- [SDR CALA2024071600201](https://openairdocs.org/sdr/CALA2024071600201.md): Roller · damaged · Jul 13, 2024 · N658UA · Boeing 767322 · Service Doors
  > R-2 SERVICE DOOR (AFT. GALLEY) REQUIRES R.I.R. / D.V.I. OF AFT. ROLLER TRACK ASSY. EVERY 15 DAYS PER. EC/RA # 5211-01872 REV. [A]. PART # 2 (INSPECTIONS PROCEDURE) AND PART # 3 (PERMANENT REPAIR PROCEDURE) WITHIN 60 CALENDAR DAYS. [ACFT. # 6458]. REQUEST DIP A
- [SDR CALA2024040300956](https://openairdocs.org/sdr/CALA2024040300956.md): Wire · sheared · Apr 3, 2024 · N658UA · Boeing 767322 · Oxygen System Wiring
  > PANEL CAME DOWN AT 33 DEF REDO 1 PIN OR REPLACEMENT OF MODULE PER WDM 35-21-14. HANDED OVER TO OPPOSITE CREW. PRELIMINARY INSPECTIONS OF 33DEF FOUND OXY MASK DEPLOYMENT WIRING FOR MODULE M00064 WITH WIRE BUNDLE W1170 AND WIRES121-20R AND W1170-122-20G OF CANN
- [SDR CALA2024031900789](https://openairdocs.org/sdr/CALA2024031900789.md): Control Module · intermittent · Mar 17, 2024 · N658UA · Boeing 767322 · Rudder Tab Control System
  > UNSCHED STAB TRIM EICAS DURING TO ROLL X2 REMOVED AND REPLACED AND TESTED STAB TRIM CONTROL MODULE PER AMM 27-09-00.
- [SDR CALA2024020800352](https://openairdocs.org/sdr/CALA2024020800352.md): Seal · missing · Feb 6, 2024 · N658UA · Boeing 767322 · Ailerons
  > R/H I/B AILERON, I/B LOWER SEAL MISSING. PICTURES ADDED. CONTACTING TOMC FOR DISPOSITION, NIL STOCK LHR. IPC REF 27-11-01-05 ITEM 155, PART NUMBER: 113T6105Y2 1 QUANTITY. INBD LOWER SEAL FOR INBD AILERON REPLACED I.A.W DWG 113T6100 SHEET 2, AILERON ACTUATED T
- [SDR CALA2023100402944](https://openairdocs.org/sdr/CALA2023100402944.md): Cylinder · unknown · Oct 1, 2023 · N658UA · Boeing 767322 · Escape Slide
  > REF AMM 25-65-01-024 PARAG E (3): IF THE OFF WING ESC SYS OPERATED WITH THE REGULATOR SAFETY PIN INSTALLED, YOU MUST REPLACE THE INFLATION CABLE AND THE INFLATION CYLINDER. LEFT OFFWING ESCAPE SLIDE CYLINDER AND AND CABLE REPLACED AS PER AMM TASK 25-65-02-201
- [SDR CALA2023100402938](https://openairdocs.org/sdr/CALA2023100402938.md): Unknown · unknown · Oct 1, 2023 · N658UA · Boeing 767322 · Cabin Equipment/Furnishings
  > DURING OFF WING ESCAPE SLIDE INSPECPTION LEFT HAND WING SLIDE DOOR ACTATED OPEN. SLIDE AND BOTTLE NOT ACTIVATED. OFF-WING ESCAPE SYSTEM SPOLIER OVERRIDE ACTUATOR REPLACED IN UPDATE DUE TO PART HAVING ASSIGNED SERIAL NUMBER ACCORDANCE WITH AMM-25-65-20. SQUIB T
- [SDR CALA2023090502716](https://openairdocs.org/sdr/CALA2023090502716.md): Engine · damaged · Aug 27, 2023 · N658UA · Boeing 767322 · Engine (Turbine/Turboprop)
  > UPON REACHING TO EPR LOUD BANG WITH SWERVE RIGHT. REJECTED T/O. NO FIRE. R REV ISLN VAL EICAS ENG2 SN. 724371 (TSI= 16306) SURGED AT T/OFF POWER, CHEK INLET, LOST N1, OIL PRESSURE IN RED 60 TO 70PSI PER FLIGHT CREW EXHAUST, TAIL PIPE FOR METAL, CHECK ALL CHI
- [SDR CALA2023010900063](https://openairdocs.org/sdr/CALA2023010900063.md): Panel · missing · Jan 9, 2023 · N658UA · Boeing 767322 · Nacelle/Pylon, Main Frame
  > PDA 1 REF LP 3518403. E2 INBD STRUT PNL 447AL BROKEAND PARTIALLY DEPARTED THE A/C INBD STRUT PNL 447AL INSTALLED WITH FIRE SEAL.
- [SDR CALA2022051601244](https://openairdocs.org/sdr/CALA2022051601244.md): Skin · cracked · May 14, 2022 · N658UA · Boeing 767322 · Fuselage, Stabilizer Attach Fittings
  > B767-53-3-7018 RH HORI STAB LOWER FAIRING QATTACH SKIN FOUND CRACK AT BS 1809-1820, TRANSFER TO HX NRC WO 738612 AND ORIGINATED BY V896832 R/H HORI STAB LOWER FAIRING ATTACH SKIN AT BS1809-1820 BETWEEN STA 12AR TO STR 22R SKIN REPAIRED AS PER EC/RA 5381-01018
- [SDR CALA2022050401129](https://openairdocs.org/sdr/CALA2022050401129.md): Frame · chafed · May 3, 2022 · N658UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7006 BULK CGO DOOR LWR MID AREA DOUBLER FOUND CHAFING, TRANSFER TO HX NRC WO745751 AND ORIGINATED BY V898555 BULK CGO DOOR LOWER MID AREA FRAME CHAFING DOUBLER REMOVED AS PER SRM 51-70-11-0G-0 FIG 1 FORM 44.0008 WORSHEET AND DISCARD AS PER SRM 51-40
- [SDR CALA2021091701602](https://openairdocs.org/sdr/CALA2021091701602.md): Access Panel · missing · Sep 17, 2021 · N658UA · Boeing 767322 · Wing, Plate/Skin
  > PDA 3 ACCESS PANEL 621 ADB MISSING DURING WALK AROUND. REPLACED ACCESS PANEL 621 ADB AS REQUIRED A/C OK TO CONTINUE.
- [SDR CALA2021080201244](https://openairdocs.org/sdr/CALA2021080201244.md): Light · damaged · Aug 2, 2021 · N658UA · Boeing 767322 · Emergency Lighting
  > STAR PRE-DEPARTURE CHECKLIST - EMERGENCY PARH LIGHT RED DAMAGED AT SEAT 20D REPLACED LIGHT ASSY, GRD OPS EMERGENCY PATH LIGHT SYS, NO DEFECTS NOTE
- [SDR CALA2021051000630](https://openairdocs.org/sdr/CALA2021051000630.md): Skin · debonded · May 8, 2021 · N658UA · Boeing 767322 · Trailing Edge Flaps
  > B767-06-3-7222 RHW I/B AFT FLAP UPPER AND BOTTOM SURFACE FOUND DISBOND - REFER NR LP 9130574. RHW I/B AFT FLAP DISBOND AREA PERFORMED REPAIR AS PER EC/RA 5752-01851 REV - REFER FORM 44-0008 ITEM 1-29 ACCOMPLISHED ADD EMP:V912779 RII INSPECTED OK BY HX198855 R
- [SDR CALA2019081201350](https://openairdocs.org/sdr/CALA2019081201350.md): Spar · damaged · Aug 9, 2019 · N658UA · Boeing 767322 · Wing Spar
  > LT WING L/E FRONT SPAR WEB FOUND DAMAGED AT OFSS1025 REF NRC 9131148 DVI SURROUNDING STRUCTURAL WITHIN 16'' NIL FINDINGS. HFEC INSP CARRIED OUT PER B767 NTM PART 6 51-00-19, NO CRACK FOUND AT TRIM MED EDGE. HFEC OPEN HOLE INSP CARRIED OUT AT EXISTING FASTENER
- [SDR CALA2019080901327](https://openairdocs.org/sdr/CALA2019080901327.md): Skin · corroded · Aug 7, 2019 · N658UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN PREVIOUS REPAIR DOUBLER SKIN FOUND SURFACE CORROSION AT STA 1197+120 BETWEEN STR 37L-38L CORROSION REMOVED PER SRM 51-10-02, ORG 0.065'' BLEND OUT AREA REMAIN 0.045'' WIDTH 2'' LENGTH 2'', CHECKED NOT WITHIN SRM53-00-01 ALLOWABLE DAMAGE 1 FIG 101
- [SDR CALA2019080431295](https://openairdocs.org/sdr/CALA2019080431295.md): Stringer Splice · corroded · Aug 1, 2019 · N658UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > STA 1219-1215 S-19R STRINGER SPLICE BRACKET FOUND CORRODED, THE STRINGER SPLICE WAS REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.
- [SDR CALA2019080431296](https://openairdocs.org/sdr/CALA2019080431296.md): Floorbeam · damaged · Aug 1, 2019 · N658UA · Boeing 767322 · Fuselage Main, Floor Beam
  > CABIN - STA 1087 LBL 23 FLOOR BEAM FOUND FLOOR PANEL HOLE ELONGATED. (REF NR LP 9131027). CABIN STA 1087 LBL 23 FLOOR BEAM UPPER FLANGE REPAIRED AS PER SRM 53-00-51 REPAIR 2 FIG 201.
- [SDR CALA2019080101290](https://openairdocs.org/sdr/CALA2019080101290.md): Floorbeam · damaged · Aug 1, 2019 · N658UA · Boeing 767322 · Fuselage Main, Floor Beam
  > BS 1087, LBL 23 FOUND FLOORBEAM HOLE ELONGATED.. THE FLOORBEAM WAS REPAIRED AS PER SRM 53-00-51 REPAIR 2 FIG 201.
- [SDR CALA2019080101288](https://openairdocs.org/sdr/CALA2019080101288.md): Stringer Splice · corroded · Aug 1, 2019 · N658UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > CABIN STA 1219-1215 S-19R STRINGER SPLICE BRACKET FOUND CORRODED, REFERENCE NRC 9131413. CABIN STA 1219-1225 STR 19R STRINGER SPLICE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02. RII INSPECTED.
- [SDR CALA2019021100244](https://openairdocs.org/sdr/CALA2019021100244.md): Control Rod · damaged · Feb 11, 2019 · N658UA · Boeing 767322 · Leading Edge Slat Control System
  > EICAS LE SLAT ASYM DEBRIEFED INBD FLIGHT CREW REPORTS NO OVERWEIGHT LANDING. REF FIM TASK 27-81-00-815-809 BLOCK 5, BITE TEST OF PSEU SHOWS INSPECTION FOUND OUTBOARD ROD ASSEMBLY BROKEN WITH DAMAGE TO THE WING LEADING EDGE ABOVE THE ROD MEASURING APPROX 2 AND
- [SDR CALA2017122404585](https://openairdocs.org/sdr/CALA2017122404585.md): Warning Light · false activation · Dec 24, 2017 · N658UA · Boeing 767322 · Trailing Flap Position Indicating System
  > FLAP DISAGREE AT FLAPS 5 EXTENSION. EMERGENCY DECLARED. TE FLAP DISAGREE SELF RESET AFTER PRESSURIZING ADP AND HYD ELEC PUMPS. FLAPS-SLATS FULLY EXTENDED AND ALL ROTARY ACTUATORS INSPECTED FOR OVERLOAD TRIP INDICATORS, NO FINDINGS. SEVERAL FLAPS-SLATS FULL FU
- [SDR CALA2017120904375](https://openairdocs.org/sdr/CALA2017120904375.md): Transmitter · out of limits · Dec 9, 2017 · N658UA · Boeing 767322 · Trailing Edge Flap Control System
  > TE FLAP DISAGREE EICAS MSG ON APR LANDED F20 MSG ON APR WHEN FLAP LEV ER TO FLAPS 1 LANDED. EMERGENCY DECLARED. PERFORMED FSEU BITE REF FIM 27-51-00-815-808 AND NO CURRENT FAUL TS DISPLAYED. CYCLED FLAPS TO FULL TRAVEL WITH ELEC HYD PUMPS ON AND HAD A TRAILI
- [SDR CALA2017111804137](https://openairdocs.org/sdr/CALA2017111804137.md): Altimeter · inaccurate · Nov 18, 2017 · N658UA · Boeing 767322 · Altimeter, Barometric/Encoder
  > STANDBY ALTIMETER NEEDLE INDICATES 540, DIGITS INDICATE 100. REMOVED AND REPLACED THE STANDBY ALTIMETER IAW MM 34-13-06. OPS CHECKED GOOD.
- [SDR CALA2016062200379](https://openairdocs.org/sdr/CALA2016062200379.md): Skin · cracked · Jun 21, 2016 · N658UA · Boeing 767322 · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON PANEL 426BR CUTOUT SKIN FOUND CRACKED. AD STRUCTURAL INSPECTION FINDING 76-5400-1-2512, NR 2 PYLON PANEL 426BR CUTOUT SKIN CRACKED. CRACK LENGTH 0.156", AREA REPAIRED IAW SRM 54-53-01, REPAIR 6, FIG 201, DETAIL III AND ATTACH FORM 44.0008 WORKSHEE
- [SDR CALA2016061700367](https://openairdocs.org/sdr/CALA2016061700367.md): Floorbeam · corroded · Jun 15, 2016 · N658UA · Boeing 767322 · Fuselage Main, Floor Beam
  > CABIN BS1518, LBL 1 TO RBL 3 FLOORBEAM FOUND CORROSION. CABIN FLOORBEAM AT BS1518, LBL1 TO RBL 3 UPPER CHORD CORROSION REMOVED IAW SRM 51-10-02. BLENDED AREA D 0.065", ORIGINAL THICKNESS 0.090", WITHIN 2" X 8" LENGTH OUT OF SRM 53-00-51. ALLOWABLE DAMAGE 1,
- [SDR CALA2016061700366](https://openairdocs.org/sdr/CALA2016061700366.md): Skin · cracked · Jun 15, 2016 · N658UA · Boeing 767322 · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON PANEL 446BL CUTOUT SKIN FOUND CRACKED, AD STRUCTURAL INSPECTION FINDING. NR 2 PYLON PANEL 446BL CUTOUT SKIN CRACKED LENGTH 0.125" AND CRACKED AREA REPAIR IAW SRM 54-53-01, REPAIR 7, FIG 201, DETAIL I.
- [SDR CALA2016052000320](https://openairdocs.org/sdr/CALA2016052000320.md): Housing · broken · May 19, 2016 · N658UA · Boeing 767322 · Emergency Equipment
  > LEFT OFF WING ESCAPE SLIDE CABLE SYS DISCONNECT HOUSING FOUND BROKEN AT THE ARM, AD FINDING IAW EA 2560-02662 REV A. FX LT OFF WING ESCAPE SLIDE CABLE SYS DISCONNECT HOUSING REPLACED & ADJUSTED IAW EA 2560-02662 REV A OP 001 & AMM 25-65-04.
- [SDR CALA2016052000319](https://openairdocs.org/sdr/CALA2016052000319.md): Hose · kinked · May 19, 2016 · N658UA · Boeing 767322 · Escape Slide
  > RIGHT FX OFF WING SLIDE CYLINDER INFLATION HOSE FOUND CONTAMINATED WITH HYD FLUID & KINKED AT CLAMPS AREA. REPLACED IAW AMM 25-65-02 & FORM 44.0008 ITEM 1 ACCOMPLISHED.
- [SDR CALA2016020895093](https://openairdocs.org/sdr/CALA2016020895093.md): Light · inoperative · Feb 5, 2016 · N658UA · Boeing 767322 · Emergency Lighting
  > EXTERIOR EMER EXIT LIGHT INOPERATIVE. RT SIDE OF FUSELAGE JUST FWD OF AFT CARGO DOOR. RELAMPED EXTERIOR EMER EXIT LIGHT.
- [SDR CALA2015122494916](https://openairdocs.org/sdr/CALA2015122494916.md): Light · inoperative · Dec 22, 2015 · N658UA · Boeing 767322 · Emergency Lighting
  > EXTERNAL EMERGENCY LIGHT AT R2 DOOR INOPERATIVE. RELAMPED, R & R AFT RT LIGHT ASSEMBLY. FOUND PUSHED BACK PIN AT CONNECTOR M733, SECURED IAW WDM 33-51-06. OPERATIONS NORMAL.
- [SDR CALA2015102094610](https://openairdocs.org/sdr/CALA2015102094610.md): Spar · cracked · Oct 15, 2015 · N658UA · Boeing 767322 · Wing Spar
  > ECRA 5710-02320, DURING A SPECIAL HOLD & THE ACCOMPLISHMENT OF EA 5710-02220 OP 03, A CRACK WAS DISCOVERED ON THE WING CTR SECTION, FRONT SPAR RING CHORD PN 111T2023-5. THE CRACK WAS FOUND AT A FASTENER HOLE, BETWEEN STRINGER 28L & 29L. THE REPAIR IAW ECRA 5
- [SDR CALA2015052693811](https://openairdocs.org/sdr/CALA2015052693811.md): Connector · unsecure · May 19, 2015 · N658UA · Boeing 767322 · Light System Wiring
  > EMERGENCY EXIT FLOOR LIGHT INOPERATIVE, JUST OUTSIDE OF AFT INBD LAVATORY. SECURED CONNECTOR. OPERATIONS CHECKED NORMAL.
- [SDR CALA2015052193802](https://openairdocs.org/sdr/CALA2015052193802.md): Connector · unsecure · May 19, 2015 · N658UA · Boeing 767322 · Light System Wiring
  > EMERGENCY EXIT FLOOR EEL INOPERATIVE JUST OUTSIDE OF AFT INBD LAVATORY. SECURED CONNECTOR, OPERATIONS CHECKED NORMAL.

Next page: https://openairdocs.org/aircraft/N658UA/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 = 'N658UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N658UA/reports

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