# Service difficulty reports: N656UA

A list on [N656UA](https://openairdocs.org/aircraft/N656UA.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 · 336 reports

- [SDR CALA2026101320319](https://openairdocs.org/sdr/CALA2026101320319.md): Light · no test · Oct 10, 2026 · N656UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHTS TEST WITH TEST SWITCHES - 30F SEAT PATH LIGHT INOPERATIVE THE RED PATH LIGHT HAS BEEN REPLACED REF AMM 33-51-10/201 AND CMM 25-21-53 TEST OK PARTS USED: 99-3350-3-0009,QTY:1
- [SDR CALA2026082118796](https://openairdocs.org/sdr/CALA2026082118796.md): Lens · broken · Aug 20, 2026 · N656UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY ESCAPE PATH LIGHTING SYSTEM PERFORM AN OPS CHK, LIGHT LENSES AT POSITIONS 33D, 34D, 39D AND 41F BROKEN. REMOVED AND REPLACED THE LENSES IAW AMM 33-51-10/201, ITEM GOOD FOR SERVICE.
- [SDR CALA2026031614594](https://openairdocs.org/sdr/CALA2026031614594.md): Extinguisher · damaged · Mar 16, 2026 · N656UA · Boeing 767322 · Extinguishing System
  > FWD LAVATORY FIRE ALARM ACTIVATED IN FLT, NO FIRE, FUMES, OR SMOKE. CIRCUIT BREAKER PULLED. AFFECTED LAV IS 1A-1L (FWD LEFT). SMOKE DETECTOR TEST OK. FIRE EXTINGUSHER HAS MELTED TIPS AND REQUIRES REPLACEMENT IAW FIM 26-13, FAULT TREE 806. LAVATORY SMOKE DE
- [SDR CALA2026031714609](https://openairdocs.org/sdr/CALA2026031714609.md): Fire Detector · faulted · Mar 15, 2026 · N656UA · Boeing 767322 · Fire Detection
  > CREW REPORTED WHILE IN FLIGHT ONE OF THE LAV FIRE ALARMS CONTINUOUSLY GOES OFF IN FLIGHT BRIEFED THE CREW AND THEY ADVISED THEY DID NOT SEE OR SMELL ANY SMOKE WHILE INFLIGHT REFER TO L/P 8225721 FOR THE R/R OF FIRE EXTINGUISHER IN LAV 1A-1L AND OPS CHK OK FIRE
- [SDR CALA2025092509251](https://openairdocs.org/sdr/CALA2025092509251.md): Oven · dirty · Sep 22, 2025 · N656UA · Boeing 767322 · Buffet/Galleys
  > OVEN 109 BLACK RESIDUE ON HEATING ELEMENT. SMOKED WHEN TURNED ON. STOPPED WHEN TURNED OFF REQUESTED NEF, DDP FOLLOWED AND CB OVEN 109 OPEN AND SECURED. DEFERRED IAW NEF 25178; CIRCUIT BREAKER OPEN AND SAFETY. REMOVED AND REPLACED OVEN AT POSITION 109 IAW AM
- [SDR CALA2025072206841](https://openairdocs.org/sdr/CALA2025072206841.md): Switch · loose · Jul 21, 2025 · N656UA · Boeing 767322 · Emergency Lighting
  > EMER LIGHT SWITCH ASSEMBLY LOOSE. ADJUSTED EMERGENCY LIGHT SWITCH ASSEMBLE REF AMM TASK 33-51-08-004-002;ASSY SECURE.
- [SDR CALA2025052004840](https://openairdocs.org/sdr/CALA2025052004840.md): Housing · broken · May 18, 2025 · N656UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY AISLE LIGHT SHROUD BRACK BROKEN AND HANGING FROM UNDER SEAT 36F. REMOVED AND REPLACED BRACKET. REF, AMM 33-50-00. PARTS USED: 58-2523-3-0048, QTY:1
- [SDR CALA2025050204413](https://openairdocs.org/sdr/CALA2025050204413.md): Indicator · faulted · May 1, 2025 · N656UA · Boeing 767322 · Cabin Pressure Control System
  > CABIN ALTITUDE DIFFERENTIAL GAUGE READS 8.8 PSI WHICH IS IN AMB ER BAND. FL370 CABIN PRESSURE CONTROLLER BITE PROCEDURE CARRIED OUT AS PER FIM 21-31 FAULT TREE 803. NO FAULTS FOUND. CABIN PRESSURE INDICATION TEST CARRIED OUT AS PER AMM 21-33-00-705-025 FOUND
- [SDR CALA2025050104384](https://openairdocs.org/sdr/CALA2025050104384.md): Bottle · not reported · Apr 27, 2025 · N656UA · Boeing 767322 · Escape Slide
  > OVER WING EMERGENCY ESCAPE SLIDE DEACTIVATION REF AMM 25-65-00-042-001. INSTALLED SAFETY PIN ON RIGHT OVERWING INFLATION CYLINDER REF AMM 25-65-00-042-001. PULLED CBS AND TAGGED K14, 15, 16 & 17 AND K17 & 18 ON P6. AS WELL AS C6, 7, 8, & 9; G17, 18, 26 & 27; P
- [SDR CALA2025041804021](https://openairdocs.org/sdr/CALA2025041804021.md): Bottle · low pressure · Apr 18, 2025 · N656UA · Boeing 767322 · Emergency Equipment
  > REAR SLIDE DOOR PRESSURE LOW. DOOR 2R INPECTED R2 DOOR SLIDE PRESSURE FOUND NON THE LIMITS AT THE HIGH END PER MM 25-66-02-206-001.
- [SDR CALA2025032403123](https://openairdocs.org/sdr/CALA2025032403123.md): Bottle · low pressure · Mar 21, 2025 · N656UA · Boeing 767322 · Escape Slide
  > R1 DOOR SLIDE PRESSSURE IS LOW DOOR 1R SLIDE PRESSURE WAS FOUND SERVICEABLE. THIS LP WAS ENTERED IN ERROR, DOOR WITH DISCREPANT SLIDE PRESSURE IS DOOR R2. SEE LP 4245458. REF AMM 25-66-99.
- [SDR CALA2024040500986](https://openairdocs.org/sdr/CALA2024040500986.md): Skate Angle · cracked · Apr 2, 2024 · N656UA · Boeing 767322 · Wing Structure
  > GEN ITEM: 63-0600-1-2803 (B767-06-3-7290) THE I/B SKATE ANGLE IS CRACKED, LOCATED ON THE UPPER I/B EDGE OF WHERE PANEL 447DR ATTACHES TO THE LOWER SURFAC E OF THE RIGHT WING.#6173 REF AMES NR 167037-0400-0059 REPAIRED I/B SKATE ANGLE ON THE #2 ENG INBD EDGE IA
- [SDR CALA2024040300964](https://openairdocs.org/sdr/CALA2024040300964.md): Skate Angle · cracked · Apr 2, 2024 · N656UA · Boeing 767322 · Wing, Attach Fittings
  > GEN ITEM: 63-0600-1-2803 (B767-06-3-7290) THE I/B SKATE ANGLE IS CRACKED, LOCATED ON THE UPPER I/B EDGE OF WHERE PANEL 447DR ATTACHES TO THE LOWER SURFAC E OF THE RIGHT WING.#6173 REF AMES NR 167037-0400-0059 REPAIRED I/B SKATE ANGLE ON THE #2 ENG INBD EDGE IA
- [SDR CALA2024040300949](https://openairdocs.org/sdr/CALA2024040300949.md): Stringer · corroded · Mar 29, 2024 · N656UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > STRINGER-35L IS CORRODED AT LFS-1302. REPAIRED STRINGER 35L AT F.S.1302 IAW AMES REA DOC NO 47601REA08 AND UNITED EC/RA NO 5360-01767. SEE NON-ROUTINE 167037-0100-018 7 FOR DETAILS
- [SDR CALA2024040300948](https://openairdocs.org/sdr/CALA2024040300948.md): Floorbeam · corroded · Mar 29, 2024 · N656UA · Boeing 767322 · Fuselage Main, Floor Beam
  > GEN ITEM: 63-5330-1-2610 FLOOR BEAM CAP CORRODED AT STA720 LBL48 MARKED FLAGGED #2196 T.K ELLY REMOVED CORRODED FLOOR BEAM CAP AT STA 720 FROM LBL 48- RBL 48 A ND INSTALLED SERVICEABLE NEW UPPER CHORD, PN 143T1060T33 IAW 767 -300 SRM 51-40-02 PAR 7. SEE NON-RO
- [SDR CALA2024040300947](https://openairdocs.org/sdr/CALA2024040300947.md): Web · cracked · Mar 29, 2024 · N656UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > GEN ITEM: 63-5330-1-2610 FLOOR WEB AT STA676 RBL 48 IS CRACKED MARKED FLAGGED #2197 T.KEL LY REMOVED & REPLACED WEB STA 676 RBL 48 IAW B767 SRM 51-40-02 PARA 4 AND 9. SEE NON-ROUTINE 167037-0100-0141 FOR DETAILS
- [SDR CALA2024040300943](https://openairdocs.org/sdr/CALA2024040300943.md): Skin · cracked · Mar 27, 2024 · N656UA · Boeing 767322 · Nacelle/Pylon, Plate/Skin
  > 1 1/2 INCH CRACK IN THE UPPER AFT CORNER OF THE CUTOUT, FOR THE FWD ACCESS PANEL, ON THE O/B SIDE OF THE RIGHT ENGINE PYLON.#6204 REF AMES NR 167037-0400-0184. CRACK IN UPPER AFT CORNER OF CUTOUT REPAIRED IAW B767 SRM 54-53- 01-2R-G REPAIR 6 SEE PARTIAL WORK A
- [SDR CALA2024040300953](https://openairdocs.org/sdr/CALA2024040300953.md): Skin · cracked · Mar 23, 2024 · N656UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > GENERATING ITEM EA 5315-01152 LOWER AFT CORNER OF R1 DOOR FUSELAGE SKIN AND BEAR STRAP STA 335 STRINGER 20R HAS CRACK INDICATION WHILE PERFORMING HFEC OPEN HOLE SCAN. INSTALLED REPAIR PARTS IAW SRM 53-10-01-2R-1, REPAIR 1 53-10-01-2R-1, REPAIR 1, FIG 201, SHT
- [SDR CALA2024032500851](https://openairdocs.org/sdr/CALA2024032500851.md): Shear Tie · corroded · Mar 22, 2024 · N656UA · Boeing 767322 · Fuselage Internal Mounting Structure
  > AFT LOWER CARGO HAS CORROSION AT SHEAR TIE BL-5 STATION 1285 IN- BETWEEN S-39R AND S-38R, MARKED WITH STREAMER 2369 (T. GREGORY V 921207) REMOVED AND REPLACED SHEAR TIE AT BL-5 STA 1285, STR 38R IAW B767 SRM 51-40-02 PARA4. ACCOMPLISHED AT AMES BY V946986 & V9
- [SDR CALA2024040300971](https://openairdocs.org/sdr/CALA2024040300971.md): Skin · corroded · Mar 19, 2024 · N656UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > CORROSION ALC F/S 1544 SKIN BETWEEN STR 39R & 39L AT DRAIN AREA, TAG 5368. 7 NDTM 51-00-19 PT 6, NO FINDINGS. REPAIRED AREA IAW UAL ECRA 53 ECRA 5330-07196 PT 2 TO BE PERMANENT. INSP PER PART 2 OF THE LA REPEAT INSP AT INTERVALS NOT TO EXCEED 9000 FC THEREAFTE
- [SDR CALA2024032200827](https://openairdocs.org/sdr/CALA2024032200827.md): Stringer · cracked · Mar 19, 2024 · N656UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > WHILE WORKING N/R 0100-0205 FOUND STRINGER 38R AT BS 1542 CRACKED JUST FWD OF DRAIN HOLE IN STRINGER. REPAIRED STR 38L FROM STA 1530-1550 IAW SRM 53-00-03-2R-2 REPAIR 2 DETAIL II PG. 7
- [SDR CALA2024032200826](https://openairdocs.org/sdr/CALA2024032200826.md): Shear Tie · corroded · Mar 19, 2024 · N656UA · Boeing 767322 · Fuselage Internal Mounting Structure
  > CORROSION BS 1540 SHEAR TIE BETWEEN STR 38L & 39L, BLENDED & CHECKED LIMITS, FOUND TO BE OUT OF LIMITS. REMOVED & RE PLACED SHEAR TIE AT STA 1540 BETWEEN STR 38L & 39L IAW SRM 51-40-02 PARA 4 & 9.
- [SDR CALA2024032200825](https://openairdocs.org/sdr/CALA2024032200825.md): Stringer · cracked · Mar 19, 2024 · N656UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > GEN ITEM: 167037-0100-0205 WHILE WORKING SKIN CORROSION ON N/R 0100-0205, FOUND STRINGER 39 R AT STA 1544 CRACKED NEAR TANK SUPPORT. REPAIRED STR 39R FROM STA 1530-1562 IAW SRM 53-00-03-2R-2 REPAIR 2 DETAIL 11 PG. 7.
- [SDR CALA2024032200824](https://openairdocs.org/sdr/CALA2024032200824.md): Shear Tie · corroded · Mar 19, 2024 · N656UA · Boeing 767322 · Fuselage Internal Mounting Structure
  > WHILE WORKING SKIN CORROSION ON N/R 0100-0205, FOUND SHEAR TIE CORRODED AT STA 1540 BL 0 BETWEEN STR 39R-39L. BLENDED & CHECKED LIMITS FOUND TO BE OUT OF LIMITS. REMOVED & RE PLACED SHEAR TIE AT STA 1540 BETWEEN STR 39R-39L IAW SRM 51-40-02 PARA 4 & 9.
- [SDR CALA2024032200821](https://openairdocs.org/sdr/CALA2024032200821.md): Shear Tie · corroded · Mar 19, 2024 · N656UA · Boeing 767322 · Fuselage Internal Mounting Structure
  > CORROSION F/S 1540 SHEAR TIE O/B OF STR 39R, TAG 6257. BLEND & CHECKED LIMITS FOUND TO BE OUT OF LIMITS. REMOVED & REPL ACED SHEAR TIE AT STA 1540 BETWEEN 39R & 38R STR IAW B767 SRM 51 -40-02 PARA 4 & 9.
- [SDR CALA2024032200823](https://openairdocs.org/sdr/CALA2024032200823.md): Floorbeam · corroded · Mar 18, 2024 · N656UA · Boeing 767322 · Fuselage Main, Floor Beam
  > CORROSION ON TOP SIDE OF FLOORBEAM IN UPPER CABIN STA 325 LBL 55. THIS IS A CATEGORY A REPAIR. FLOORBEAM AT STA 325 LBL 55 WAS RE PAIRED IAW SRM 53-00-51-2R-4 REPAIR 4.
- [SDR CALA2024032200822](https://openairdocs.org/sdr/CALA2024032200822.md): Floorbeam · corroded · Mar 18, 2024 · N656UA · Boeing 767322 · Fuselage Main, Floor Beam
  > CORROSION ON TOP SIDE OF FLOOR BEAM IN UPPER CABIN STA 303 LBL 42. THIS REPAIR IS A CATEGORY A REPAIR. FLOORBEAM AT STA 303 LBL 42 -60 WAS REPAIRED IAW B767-300 SRM 53-00-51-2R-4 REPAIR 4.AND PWS #5 PAGES 1-8 OF 8.
- [SDR CALA2024031900782](https://openairdocs.org/sdr/CALA2024031900782.md): Skin · cracked · Mar 18, 2024 · N656UA · Boeing 767322 · Nacelle/Pylon, Plate/Skin
  > GEN ITEM: 63-54-1-2805// INNER SKIN CRACK AT AFT UPPER CORNER ON NO1 PYLON AT ACCESS PANEL 436BR CUTOUT (M) 2328. STOPPED DRILL CRACK FABRICATED AND INSTALLED REPAIR DOUBLER INST ALLED RUB STRIP IAW B767 SRM 54-53-01-2R-7 REPAIR 7. SEE PARTIAL WORK ACCOMPLISH
- [SDR CALA2024031800748](https://openairdocs.org/sdr/CALA2024031800748.md): Attach Angle · cracked · Mar 15, 2024 · N656UA · Boeing 767322 · Nacelle/Pylon, Main Frame
  > REMOVED AND REPLACED #2 PYLON IB AFT FAIRING ATTACHED ANGLE IAW B767-300 SRM 51-40-02 PARA 7
- [SDR CALA2024031800746](https://openairdocs.org/sdr/CALA2024031800746.md): Floor Support · cracked · Mar 15, 2024 · N656UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > FABRICATED DOUBLER AND FILLER INSTALLED ON AFT END OF FLOOR SUPPORT IAW B767 SRM 51-70-11-0G-0 AND DWG 146T5002 146T5006 SEE PART IAL WORK ACCOMPLISHED AND PARTIAL WORK SHEET 96 FOR DETAILS.
- [SDR CALA2024031800751](https://openairdocs.org/sdr/CALA2024031800751.md): Floorbeam · corroded · Mar 15, 2024 · N656UA · Boeing 767322 · Fuselage Main, Floor Beam
  > THE FLOOR BEAM CAP CORRODED AT STA 654+121 LBL 44.
- [SDR CALA2024031800749](https://openairdocs.org/sdr/CALA2024031800749.md): Angle · corroded · Mar 13, 2024 · N656UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > GEN ITEM: 63-5330-1-2610 PDU DRIVE STRUCTURE CORRODED AT STA654+70 RBL23 MARKED FLAGGED.
- [SDR CALA2024031500735](https://openairdocs.org/sdr/CALA2024031500735.md): Shear Tie · corroded · Mar 12, 2024 · N656UA · Boeing 767322 · Fuselage Internal Mounting Structure
  > AFT LOWER CARGO SHEAR TIE HAS CORROSION AT STATION 1395 BL-0 APPR OXIMATELY, AFT LOWER CARGO SHEAR TIE HAS BEEN FOUND TO BE OUT OF LIMITS, RE MOVE AND INSTALL OF NEW SHEAR TIE HAS BEEN INSTALLED ON N/R 1670 37-0100-0212 ENTRY #7.
- [SDR CALA2024031500737](https://openairdocs.org/sdr/CALA2024031500737.md): Stringer · corroded · Mar 12, 2024 · N656UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > REF AMES NR 167037-0100-0212 GENERATING ITEM: 167037-0100.0167, STRINGER 39L STA 1395 FOUND CORRODED. WORK WITH N/R 0100-0167. REMOVED AND REPAIRED STR 39L STA 1395 IAW B767-300 SRM 53-00-03- 2R-2 DETAIL IV.
- [SDR CALA2024031500734](https://openairdocs.org/sdr/CALA2024031500734.md): Bracket · corroded · Mar 7, 2024 · N656UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO AT STATION 137 3 HAS CORROSION BL-0 TO S-38L ON SUPPORT STRUCTURE IN FRONT OF POTABLE WATER SERVICE BOX, REMOVED AND REPLACED 2 EACH CLIPS PN-146T3006-23 AND 146T3006-24 IN ALC AT STATION 1373 BL-0 TO S-38L IAW B767 SRM 51-40-02 PARA 7.
- [SDR CALA2024031500733](https://openairdocs.org/sdr/CALA2024031500733.md): Shear Tie · corroded · Mar 7, 2024 · N656UA · Boeing 767322 · Fuselage Internal Mounting Structure
  > AFT LOWER CARGO HAS CORROSION AT SHEAR TIE BL-0 IN-BETWEEN S-39R AND S-39L STA 1285, REMOVED AND INSTALLED NEW SHEAR TIE BETWEEN STR 39R AND 39L AND BS 1285 IAW B767 SRM 51-40-02 PARA 4. WORK COMPLETED AND IAW DWG 146T121 0 SHT 2.
- [SDR CALA2024030700651](https://openairdocs.org/sdr/CALA2024030700651.md): Skin · corroded · Mar 4, 2024 · N656UA · Boeing 767322 · Wing, Plate/Skin
  > RIGHT WING UPPER SKIN AT OVER WING FUEL FILL PORT IS CORRODED. FOUND R/W UPPER SKIN FILL PORT TO BE OUT OF LIMITS PER B767-300 ACCOMPLISHED ON BACK OF NR AND PWS #27 PAGES 1 AND 2. REF AMES SRM 57-20-01, ALLOWABLE DAMAGE 1, TABLE 1. MIN REMAINING (ILN) NRC 167
- [SDR CALA2024030500634](https://openairdocs.org/sdr/CALA2024030500634.md): Web · corroded · Mar 2, 2024 · N656UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > CORROSION ON TOP SIDE OF FLOORBEAM CLOSEOUT WEB AND JUST FWD ON ADJACENT WEB IN UPPER CABIN STA 285 LBL 42 (M) 4615 REMOVED DAMAGE FROM WEB AT STA 285 100% MATERIAL LOSS VERIFIED M ATERIAL AND FABRICATED NEW WEB AND INSTALLED AT STA 285 IAW SRM 53-00-51-1
- [SDR CALA2024022200494](https://openairdocs.org/sdr/CALA2024022200494.md): Bracket · corroded · Feb 17, 2024 · N656UA · Boeing 767322 · Nacelle/Pylon, Main Frame
  > AN ANGLE SUPPORT BRACKET IS DAMAGED, LOCATED AT THE INTERIOR UPPER AFT CORNER OF 437BL ACCESS, OB SIDE IF NO 1 PYLON. REMOVED AND REPLACED BRACKET P/N 313T3380-133 IAW B767 SRM 51-40-02 PAR 7 AND PAR 9 AND BOEING DWG 313T3380. REF AMES (ILN) NRC167037-0400-0
- [SDR CALA2024031800747](https://openairdocs.org/sdr/CALA2024031800747.md): Door Frame · gouged · Feb 16, 2024 · N656UA · Boeing 767322 · Fuselage Main, Structure
  > GEN ITEM: 63-5230-1-2103 BULK CARGO DOOR LOWER FRAME HAS EXISTING REPAIR THAT IS GOUGED M ARKED FLAGGED #9268 REMOVED AND REPLACED GOUGED REPAIR PART ON THE BULK CARGO DOOR LOWER FRAME WITH A NEW REPAIR PART IAW B767 SRM 51-70-11-0G-0 AND SRM 51-40-02, PG 9. R
- [SDR CALA2024022200493](https://openairdocs.org/sdr/CALA2024022200493.md): Bracket · worn · Feb 16, 2024 · N656UA · Boeing 767322 · Nacelle/Pylon Structure
  > NUMBER 2 ENGINE I/B FAN COWL HAS EXCESSIVE PLAY AT HLD OPEN ROD STOWAGE BRACKET (6222) STOWAGE BRACKET DAMAGED AND FOUND TO BE OUT OF LIMITS IAW B767 SRM 54-23-90-1A-1. NEW REPLACEMENT BRACKET FABRICATED IAW B767 ENGINEERING DWG 314T3114 AND NEW BRACKET INSTAL
- [SDR CALA2024021200391](https://openairdocs.org/sdr/CALA2024021200391.md): Bracket · worn · Feb 10, 2024 · N656UA · Boeing 767322 · Nacelle/Pylon, Main Frame
  > NO 2 ENG O/B FAN COWL HOLD OPEN ROD HAS EXCESSIVE PLAY AT STOWAGE BRACKET (REFERENCE STREAMER) FABRICATED NEW PLATE PN 314T3114-35 INSTALLED PLATE AMD GROMMET IAW B7567 SRM 51-40-02 PARA 7. REFERENCE NON-ROUTINE 167037-0400 -0203 FOR DETAAILS
- [SDR CALA2023100902995](https://openairdocs.org/sdr/CALA2023100902995.md): Insulation · missing · Sep 28, 2023 · N656UA · Boeing 767322 · Cabin Equipment/Furnishings
  > **POTENTIAL CHRONIC LVL 0 **DUE TO FLIGHT ATTENDENTS OBERSERVATI ON THAT THE L AFT LAV GETS VERY HOT WHEN THE APU IS RUNNING, PLE ASE INSPECT AFT LAV FOR POSSIBLY APU AIR LEAK WHEN RUNNING. REPA IR ALL FAULTS FOUND. ORDLM MARTINEZ 09/28/2023 CARRIED BY ELB RE
- [SDR CALA2023092002824](https://openairdocs.org/sdr/CALA2023092002824.md): Controller · faulty · Sep 19, 2023 · N656UA · Boeing 767322 · Airborne Auxiliary Power Unit (APU) System
  > IMMEDIATELY AFTER APU SHUTDOWN FLT ATTENDANTS REPORTED HOT AFT L LAV +SMELLED SMOKE IN LAV SMOKE/ODOR IN THE PLANE QUESTIONAIRE FILLED OUT BY FLT CREW PERFORMED INITIAL INSPECTION AS PER REF AMM 05-51-56. NO DEFECTS NOTED. A/C OK TO CONTINUE ADD EMP:U375129,U
- [SDR CALA2023091502799](https://openairdocs.org/sdr/CALA2023091502799.md): Latch · unknown · Sep 12, 2023 · N656UA · Boeing 767322 · Cabin Equipment/Furnishings
  > ROW 36 CENTER OVERHEAD PANEL FELL DOWN FOUND PSU LATCH OPEN, ARMED LATCH AND CLOSED PSU PER AMM 25-23-01.
- [SDR CALA2023091502800](https://openairdocs.org/sdr/CALA2023091502800.md): Fuel Cap · missing · Sep 11, 2023 · N656UA · Boeing 767322 · Aircraft Fuel System
  > FUEL CAP LEFT MISSING AT WING FUEL STATION. REPLACED FUEL CAP REF IPC 28-21-01-01.
- [SDR CALA2023083002660](https://openairdocs.org/sdr/CALA2023083002660.md): Slat System · warning message · Aug 28, 2023 · N656UA · Boeing 767322 · Leading Edge Slat Control System
  > LE SLAT DISAGREE AT FLAP 25. GO AROUND. QRH. FLAPS 20 LAND. LAND AT 147 KIAS. AB 3. BETWEEN POSITIONS 1 AND 5 LE SLAT DISAGREE FOR FRACTION OF A SECOND BEFORE DISAPPEARING. NO DISAGREE FROM POSITION 5 ALL THE WAY TO 30. NO DISAGREE FROM 30 BACK TO UP. CYCLED F
- [SDR CALA2023031500757](https://openairdocs.org/sdr/CALA2023031500757.md): Charger · inoperative · Mar 14, 2023 · N656UA · Boeing 767322 · Lighting System
  > B767-33-3-7000 - ZONE A SEAT 1-3 EEPL INOP TRANSFER REF HXWO 1594233 AND ORIGINATED BY EMP V920570 EMER LT PWR SUPPLY (M9043) REPLACED AND TESTED NORMAL AS PER AMM33-51-07, EMER LT OP TEST CARRIED OUT AND FOUND NORMAL AS PER AMM33-51-00 WORK ACCOMPLISHED BY M
- [SDR CALA2023031300718](https://openairdocs.org/sdr/CALA2023031300718.md): Stiffener · cracked · Mar 12, 2023 · N656UA · Boeing 767322 · Wing Structure
  > B767-57-3-7014 RHW LES 664 FRONT SPAR STIFFENER FOUND CRACK TRANSFER TO NR WO.1500719 AND ORIGINATED BY V898549 RHW LES664 FRONT SPAR STIFFENER REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 WORK ACCOMPLISHED BY MECHANIC V897473 INSPECTE
- [SDR CALA2023031000680](https://openairdocs.org/sdr/CALA2023031000680.md): Lamp · inoperative · Mar 9, 2023 · N656UA · Boeing 767322 · Lighting System
  > B767-33-3-7000 - SEAT 44A EMER AISLE LIGHT INOP TRANSFER REF HXWO 1594230 AND ORIGINATED BY EMP V920570 SEAT 44A EMER AISLE LT LAMP REPLACED, LT ASSY RE-SECURED AND OP TEST CARRIED OUT AND FOUND NORMAL AS PER AMM33-51-05 WORK ACCOMPLISHED BY MECHANIC V920570

Next page: https://openairdocs.org/aircraft/N656UA/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 = 'N656UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N656UA/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.