# Service difficulty reports: N364CM

A list on [N364CM](https://openairdocs.org/aircraft/N364CM.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 3 · 112 reports

- [SDR ABXA20260917427](https://openairdocs.org/sdr/ABXA20260917427.md): Battery · defective · Sep 17, 2026 · N364CM · Boeing 767338 · Emergency Lighting
  > DURING INSP/MTC, 2 EACH EMERGENCY LIGHTS INOP, SUPERNUMERY AREA. REPLACED BATTERY PACK AT POSITION M736 PER B767 AMM 33-51-07. SYSTEM CHECKS NORMAL. A/C RETURNED TO SERVICE.
- [SDR ABXA20260916412](https://openairdocs.org/sdr/ABXA20260916412.md): Smoke Goggles · deteriorated · Sep 16, 2026 · N364CM · Boeing 767338 · Emergency Equipment
  > DURING INSP/MTC, FOUND FO SMOKE GOGGLES DETERIORATED. REMOVED F.O. SMOKE GOGGLES. REPLACED WITH SERV. GOGGLES IAW AMM 25-64-00. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.
- [SDR ABXA20260901377](https://openairdocs.org/sdr/ABXA20260901377.md): Resistor · faulted · Sep 1, 2026 · N364CM · Boeing 767338 · Door System Wiring
  > DURING TAXI EMERGENCY DOORS LIGHT ILLUMINATED. CREW RETURNED TO THE BLOCKS (BTB). REMOVED AND INSTALLED RESISTOR 59032 IAW B767-WDM 52-71-12, PERFORMED PSEU BITE TEST IAW B767 FIM 32-09 FAULT TREE803, BITE TEST GOOD. A/C REMAINS NO ETOPS AND RETURNED TO SERVI
- [SDR ABXA20260901392](https://openairdocs.org/sdr/ABXA20260901392.md): Skin · dented · Sep 1, 2026 · N364CM · Boeing 767338 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, INSPECTION AT FUSELAGE SKIN, LOWER SKIN PANEL, AT BS 1373, BETWEEN STR 27R AND ABOVE STR 29R WAS FOUND DENTED OUT OF SRM LIMITS 53-00-01, FIG 101, DETAIL 3 AND WHILE PERFORMING SRM 53-00-01, REPAIR 14, FOUND DOUBLER TO STOP ON AN INTERNAL DOU
- [SDR ABXA20260901391](https://openairdocs.org/sdr/ABXA20260901391.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Wing, Plate/Skin
  > DURING C-CHECK, CORROSION WAS OBSERVED ON THE RT WING UPPER SURFACE SKIN PANEL NR 1 AT WS 434 OVER UPPER RIB FLANGE PIN 113T1545-6, THE DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA IAW SRM 51-10-02 WITH MEASURED MATERIAL REMAINING OF0.112 INCHES FROM INITIAL T
- [SDR ABXA20260901390](https://openairdocs.org/sdr/ABXA20260901390.md): Skin · damaged · Sep 1, 2026 · N364CM · Boeing 767338 · Wing, Plate/Skin
  > DURING AN INSPECTION, LEFT WING LOWER SKIN EXISTING BLEND REPAIRS AT WS 110, STRINGER 10 WAS FOUND. THE AFFECTED FASTENERS WERE REMOVED, AND HFEC ROTO AND SURFACE INSPECTIONS WERE ACCOMPLISHED WITH NO ADDITIONAL DAMAGE. THE BLEND AFFECTS SKIN PANEL AND SKIN PA
- [SDR ABXA20260901389](https://openairdocs.org/sdr/ABXA20260901389.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Wing, Plate/Skin
  > DURING C-CHECK AT AMES (TPA), DURING STRUCTURAL INSPECTION OF THE RIGHT-WING TOP SKIN PANEL NO.1 UPPER SURFACE, CORROSION WAS FOUND AT WS 350 UNDER WING FIXED TRAILING EDGE PANEL 113T1609-2. CORROSION WAS REMOVED BY BLENDING AND FOUND TO BE OUT OF LIMITS PER S
- [SDR ABXA20260901388](https://openairdocs.org/sdr/ABXA20260901388.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, DURING STRUCTURAL INSPECTION THE LT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS 300.105 AND RS 323.281, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLENDED IAW SRM. DAMAGE REPAIRED IAW FVCI EO 26099-5, & ABX-REA-5513-
- [SDR ABXA20260901387](https://openairdocs.org/sdr/ABXA20260901387.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, DURING STRUCTURAL INSPECTION THE LT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS STA 300.105 AND RS STA 323.281, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLENDED PER SRM. ENGINEERING CONTACTED FOR FURTHER EVALUATION AN
- [SDR ABXA20260901386](https://openairdocs.org/sdr/ABXA20260901386.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, LT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX" 3" LONG AT 165" FROM FUSELAGE BODY. (AROUND FASTERNERS) FOUND WITH CORROSION BETWEEN RS STA 160 AND RS STA 180, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLENDED PER SR
- [SDR ABXA20260901385](https://openairdocs.org/sdr/ABXA20260901385.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, LT HORIZONTAL STAB, UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX" 3" LONG AT 8" FROM FUSELAGE BODY. (AROUND FASTERNERS) LT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS STA 13.986 AND RS STA 30.605, UPPER REA
- [SDR ABXA20260901384](https://openairdocs.org/sdr/ABXA20260901384.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX 2" LONG AT 70"" O/B SIDE. (AROUND FASTERNERS) RT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION AT RS 275.605, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BL
- [SDR ABXA20260901383](https://openairdocs.org/sdr/ABXA20260901383.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX" 2" LONG AT 47" FROM OTBD SIDE. (AROUND FASTERNERS) RT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS 290 & RS 310, UPPER REAR SPAR AREA STRG-1) CO
- [SDR ABXA20260901382](https://openairdocs.org/sdr/ABXA20260901382.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APPROX 3" LONG AT 22" FROM OTBD SIDE & 2.5" FWD OF REAR SPAR. (AROUND FASTERNERS). CORROSION BLENDED IAW SRM. DAMAGE REPAIRED IAW FVCI EO 26099-10 AND ABX-REA-5513-66201
- [SDR ABXA20260901381](https://openairdocs.org/sdr/ABXA20260901381.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX 4" LONG AT 161" FROM FUSELAGE BODY. (AROUND FASTERNERS) CORROSION WAS BLENDED IAW SRM. DAMAGE REPAIRED IAW FVCI EO 26099-7, & ABX-REA-5513-66193-00.
- [SDR ABXA20260901380](https://openairdocs.org/sdr/ABXA20260901380.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, R/H HORIZONTAL STAB UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX 5" LONG AT 95" FROM FUSELAGE BODY. (AROUND FASTERNERS) FOUND CORROSION BTWN RS STA 104.105, UPPER REAR SPAR AREA AND STRG 1. CORROSION WAS BLENDED IAW SRM. ENGINEERING
- [SDR ABXA20260901379](https://openairdocs.org/sdr/ABXA20260901379.md): Skin · dented · Sep 1, 2026 · N364CM · Boeing 767338 · Fuselage Main, Plate/Skin
  > DURING C-CHECK & INSPECTION, FUSELAGE SKIN, LOWER SKIN PANEL AT BS 1373, BTWN STR 27R & ABOVE STR 29R WAS FOUND WITH A DENT OUT OF SRM LIMITS 53-00-01, FIG 101, DETAIL 3, & WHILE PERFORMING SRM 53-00-01, REPAIR 14, FOUND DOUBLER TO STOP ON AN INTERNAL DOUBLER
- [SDR ABXA20260514202](https://openairdocs.org/sdr/ABXA20260514202.md): Lamp · inoperative · May 14, 2026 · N364CM · Boeing 767338 · Smoke Detection
  > EQUIPMENT COOLING SMOKE DISCRETE LIGHT WON'T ILLUMINATE DURING TEST ON GROUND BY MTC. RELAMPED EQUIPMENT COOLING SMOKE DETECTOR LAMP PER B767 AMM 21-58-19. OPS CHECK SATISFACTORY. A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.
- [SDR ABXA20260409159](https://openairdocs.org/sdr/ABXA20260409159.md): Skin · cracked · Apr 9, 2026 · N364CM · Boeing 767338 · Fuselage Main, Plate/Skin
  > DURING A-9 CHECK, WO 16376144 EXTERNAL DVI OF FUSELAGE SKIN, FORWARD SERVICE DOOR (R1) FOUND 1INCH CRACK ON AFT LWR CORNER AFTER REMOVING AFT SCUFF PLATE., FOUND CRACK TOTAL LENGTH 3.5 INCHES,FOUND TO BE OUT OF LIMITS. CALLING. MAINTENANCE REPAIRED CRACKE
- [SDR ABXA20260404146](https://openairdocs.org/sdr/ABXA20260404146.md): Control Handle · binding · Apr 4, 2026 · N364CM · Boeing 767338 · Landing Gear Selector
  > GEAR HANDLE LEVER GETS JAMMED DURING ACTUATION. HAD TO CYCLE IT TO LOCK IN POSITION MTX GROUNDED A/C MTX PERFORMED OPERATION OF LANDING GEAR RETRACT & EXTEND HANDLE SEVERAL TIMES IAW B767 AMM 32-31-00. NO DEFECTS NOTED OPS CHECK GOOD.RETURNED A/C TO SERVICE..
- [SDR ABXA20260127028](https://openairdocs.org/sdr/ABXA20260127028.md): Stringer · corroded · Jan 27, 2026 · N364CM · Boeing 767338 · Fuselage Main, Longeron/Stringer
  > CORROSION,FOUND UPPER AND LOWER SKIN PANEL, AND S-36R STRINGER, STA 1241 TO 1263. THIS AIRCRAFT WAS RECEIVING A HARD LANDING INSPECTION IN CVG AND BULGED SKIN WAS FOUND AT STA 1253 ALONG S-36R. FURTHER INVESTIGATION REVEALED CORROSION BEYOND THE SRM LIMITS O
- [SDR ABXA20251106289](https://openairdocs.org/sdr/ABXA20251106289.md): Sensor · defective · Nov 6, 2025 · N364CM · Boeing 767338 · Engine Integrated Instrument System
  > DURING TAXI, RIGHT ENGINE N1 STARTED ON 2 STARTS AND NO N1 INDICATION ON SEI SHOWS 0. AIRCRAFT RETURNED TO BLOCKS (BTB). REMOVED AND REPLACED N1 SPEED SENSOR IAW B767 AMM 77-12-01. OPS CHECK GOOD. A/C REMAINS ETOPS 180. STANDBY INDICATOR REINSTALLED IAW B
- [SDR ABXA20251019275](https://openairdocs.org/sdr/ABXA20251019275.md): Smoke Goggles · cracked · Oct 19, 2025 · N364CM · Boeing 767338 · Emergency Equipment
  > DURING INSPECTION, MAINTENANCE FOUND SMOKE GOGGLE CRACKED AT SUPERNUMERARY MID SEAT. REMOVED AND REPLACED SMOKE GOGGLE AT SUPERNUMERARY MID SEAT PER REF. AMM 25-64-00. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA20250924238](https://openairdocs.org/sdr/ABXA20250924238.md): Cdu · odor · Sep 24, 2025 · N364CM · Boeing 767338 · Fire Protection System
  > ON CLIMBOUT, THERE WAS A STRONG ODOR OF ELECTRIC WIRE BURNING. EMERGENCY DECLARED. AIR TURN BACK (ATB) TO CVG. REF LP 39228-63/3 & 39228-65/2 FOR TROUBLESHOOTING & WORK PERFORMED. NO DEFECTS NOTED. LP 39228-63/3 PERFORMED INSPECTION OF ALL C/BS & PACK BAYS
- [SDR ABXA20250911222](https://openairdocs.org/sdr/ABXA20250911222.md): Fmc · intermittent · Sep 11, 2025 · N364CM · Boeing 767338 · Flight Management Computing Hardware System
  > ON TAXI OUT, RIGHT FMC MOMENTARILY BLANKED. A/C RETURNED TO BLOCKS. (BTB). DEFERRED IAW MEL C ABX-34-61-1-1A. REMOVED AND REPLACED R FMC IAW B767 AMM 34-61-01. OPS CHECK GOOD. A/C RETURNED TO SERVICE.
- [SDR ABXA20250715160](https://openairdocs.org/sdr/ABXA20250715160.md): Warning Message · false activation · Jul 15, 2025 · N364CM · Boeing 767338 · Rudder Tab Control System
  > ON TAXI, RUDDER RATIO ON EICAS MSG., ALL HYDRAULIC PRESSURES NORMAL. AIRCRAFT RETURNED TO BLOCKS. (BTB) ACCOMPLISHED OPERATIONAL TEST OF RUDDER AND RUDER TRIM CONT IAW AMM 27-21-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA2025621133](https://openairdocs.org/sdr/ABXA2025621133.md): Start Valve · defective · Jun 21, 2025 · N364CM · Boeing 767338 · Engine Start Valves/Controls
  > DURING PUSHBACK, #2 ENGINE RIGHT ENGINE STARTER VALVE INOP. AIRCRAFT RETURNED TO BLOCKS. (BTB). DEFERRED IAW MEL C ABX-80-00-2-1. REPLACED RH ENGINE START VALVE IAW AMM 80-11-02 / 401. DI 63480 REMAINS OPEN DUE OPS CHECK PENDING. RH ENG START VALVE OPS
- [SDR ABXA20250430087](https://openairdocs.org/sdr/ABXA20250430087.md): Engine · power loss · Apr 30, 2025 · N364CM · Boeing 767338 · Engine (Turbine/Turboprop)
  > ABORTED TAKEOFF (ATO) SLIGHTLY UNDER 80 KTS. RT ENGINE MADE TO POWER, HOWEVER, LT ENGINE ONLY MADE IT TO 88% N1. AIRCRAFT RETURNED TO BLOCKS. (BTB). RAN ENGINES AT TAKEOFF POWER WITH EEC'S OFF, ENGINES MADE TAKEOFF POWER IAW 71-00-00, ITEM TRANSFERRED TO D
- [SDR ABXA20250123021](https://openairdocs.org/sdr/ABXA20250123021.md): Heater · malfunctioned · Jan 23, 2025 · N364CM · Boeing 767338 · Pitot/Static Anti-Ice System
  > AFTER PUSHBACK CAPT PITOT DISCREET LIGHT ILLUMINATED W/ EICAS MSG A/C RETURNED TO GATE(BTB) AND MTX GROUNDED AC MTX PERF FIM 30-31 FT 805 WITH PITOT HT BREAKER PULLED (CAPT) AND TEST SWITCH HELD WARMING LIGHT NEVER ILLUMINATES, VERIFIED NO POWER TO K241 CURRE
- [SDR ABXA20250117019](https://openairdocs.org/sdr/ABXA20250117019.md): Fmc · odor · Jan 17, 2025 · N364CM · Boeing 767338 · Flight Management Computing Hardware System
  > DURING MAINTENANCE PRE FLIGHT THE F/O FMC CDU BURN SMELL AND C/B P11 E29 POP OUT. MTX GROUNDED AC DEFERRED PER MEL 34-61-1-1A MX PROCED C/W PLACARD INSTALLED A/C RELIESED NO ETOPS.VERIFIED WARN ELEX STATIS MSG.NOT IN VIEW SEE LOG 39126-13/1 FOR ABX REA-3060-6
- [SDR ABXA20250106502](https://openairdocs.org/sdr/ABXA20250106502.md): Warning Light · illuminated · Jan 5, 2025 · N364CM · Boeing 767338 · Door Warning System
  > DURING CLIMB MAIN CARGO DOOR LIGHT ON AT 30.0' AND EXSTINGUISHED AT 20.0' AC RETURND TO FIELD (ATB) AND LANED MTX GROUNDED AC.MTX DEFERRED MAIN CARGO INDICATION FOR DEPARTURE IAW MEL-ABX-52-71-1-2. AND RETURNED AC TO SERVICE.
- [SDR ABXA20241215258](https://openairdocs.org/sdr/ABXA20241215258.md): Control Unit · malfunctioned · Dec 15, 2024 · N364CM · Boeing 767338 · Hydraulic Power System
  > DURING TAXI OUT C HYD PRIMARY 1 EICAS MESSAGE APPEARED, AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC. TROUBLESHOT, AND REMOVED AND REPLACED ELECTRICAL LOAD CONTROL UNIT IAW B767 AMM 29-11-14 OPS CHECK OK AT THIS TIME. AND RETURNED AC TO SERVICE.
- [SDR ABXA20241210249](https://openairdocs.org/sdr/ABXA20241210249.md): Warning Message · false activation · Dec 10, 2024 · N364CM · Boeing 767338 · Flight Control System
  > ABORTED TAKE-OFF AT ~75KTS DUE TO WARNING HORNING, RED FLAPS EICAS MESSAGE. AC ABORTED T/O DURING ABORT AFTER EXPENDING, SPOILERS, NOTED REF SPOILER EICAS MESSAGE AFTER ABORT WHILE TAXING NOTED FLAP/SLAT ELEC STATUS MTX GROUNDED AC. UPON INSPECTION FOUND NO A
- [SDR ABXA20241114225](https://openairdocs.org/sdr/ABXA20241114225.md): Pneumatic System · faulted · Nov 14, 2024 · N364CM · Boeing 767338 · Airborne Auxiliary Power Unit (APU) System
  > DURING TAXI THERE WERE NO APU PNEUMATICS. ACFT RETURNED TO GATE (BTB) AND MTX GROUNDED AC. MTX DEFERRED APU. PNEUMATICS FOR DEPARTURE IAW MEL ABX-49-11-1-1 AND RETURNED AC TO SERVICE.
- [SDR ABXA20241023202](https://openairdocs.org/sdr/ABXA20241023202.md): Pin · no discrepancy · Oct 23, 2024 · N364CM · Boeing 767338 · Standard Practices/Structures
  > ON PUSH OUT TOW BAR LOCK SNAPED DUE TO BYPASS PIN NOT INSTALLED AC RETURNED TO GATE AND MTX GROUNDED AC AND COMPLIED WITH INSPECTION OF THE NLG IAW B767 AMM 05-51-29 AND NO DAMAGE NOTED.MTX RETURNED AC TO SERVICE
- [SDR ABXA20240916175](https://openairdocs.org/sdr/ABXA20240916175.md): Oil System · low · Sep 16, 2024 · N364CM · Boeing 767338 · Turbine Engine Oil System
  > RH ENGINE LOW OIL UPON ENGINE START AND PUSH.BACK LH 19 ON START DROPPED TO 18 THEN TO 13 AND STABLE AT 14. RH 21 THEN 17 ON IDLE, NO ISSUES. AC RETURNED TO GATE AND MTX GROUNDED AC MTX CHECKED OIL @ SIGHT GLASS, FULL. EICAS READING 19 LH + 21 RH. SERVICED LH
- [SDR ABXA20240913173](https://openairdocs.org/sdr/ABXA20240913173.md): Fmc · failed · Sep 13, 2024 · N364CM · Boeing 767338 · Flight Management Computing Hardware System
  > ON ROLL OUT TO TAKEOFF LEFT FMC FAIL EICAS MESSAGE DISPLAYED, AC ABORTED TAKE OFF AND TAXIED OFF RUNWAY, THEY PERFORMED QHR AND PERFORMED A FLIGHT CREW DEFFERRAL IAW MEL ABX-34-61-1-1A. AND AC DEPARTED.
- [SDR ABXA20240829166](https://openairdocs.org/sdr/ABXA20240829166.md): Skin · corroded · Aug 29, 2024 · N364CM · Boeing 767338 · Wing, Plate/Skin
  > DURING MAINTENANCE CHECK DURING INSPECTION CORROSION BEYOND ALLOWABLE LIMITS PER THE BOEING SRM (57-20- 01) AT RH UPPER WING SKIN AT WING STRINGER U-2 TO U-4 AND RUNS UNDER THE RIB CHORD TO SKIN EDGE AT BL 97.95. CORROSION BETWEEN THE SKIN IN THE FASTENER HOLE
- [SDR ABXA20240829165](https://openairdocs.org/sdr/ABXA20240829165.md): Skin · corroded · Aug 29, 2024 · N364CM · Boeing 767338 · Wing, Plate/Skin
  > "DURING MAINTENANCE CHECK AT PEMCO (TPA) AND DURING INSPECTION CORROSION BEYOND ALLOWABLE LIMITS PER THE BOEING SRM (57-20-01) AT RH UPPER WING SKIN AT WINGS STRINGER S-15 AND RUNS UNDER THE PLUS CHORD TO SKIN EDGE AT BL 97.95. CORROSION BETWEEN THE SKIN IN TH
- [SDR ABXA20240619118](https://openairdocs.org/sdr/ABXA20240619118.md): Apu · auto shutdown · Jun 19, 2024 · N364CM · Boeing 767338 · APU Core Engine
  > APU SHUT DOWN AFTER AC LEFT THE BLOCK AC RETUREN TO BLOCKS AND MAINTENANCE GROUNDED AC AND DEFERRED THE APU IAW 49-11-1B AND RETURNED TO SERVICE AND AC DEPARTED.
- [SDR ABXA20240619117](https://openairdocs.org/sdr/ABXA20240619117.md): Control Panel · faulted · Jun 19, 2024 · N364CM · Boeing 767338 · Autopilot System
  > CREW DISCREPANCY: CAPT FD NOT SHOWING SELECTED ALTITUDE, ALSO NOT SHOWING TO AND FD AT TOP OF PFD. WENT BACK TO BLOCK. REMOVED AND REPALCED MCP PER AMM 22-11-02. OPS CK GOOD PER AMM 22-00-02, MCDP TEST NO. 4 A/C REMAINS CAT I PENDING MCDP TEST 30/40 SEE LP 386
- [SDR ABXA20240618116](https://openairdocs.org/sdr/ABXA20240618116.md): Apu · auto shutdown · Jun 18, 2024 · N364CM · Boeing 767338 · APU Core Engine
  > APU SHUT DOWN DURING PUSH, AC RETURUNED TO GATE AND MANTENANCE GROUNDED AC AND DEFERRED APU FOR FLIGHT IAW MEL ABX-49-11-1A AND RETURNED AC TO SERVICE AC DEPARTED
- [SDR ABXA20240618115](https://openairdocs.org/sdr/ABXA20240618115.md): Indicator · faulted · Jun 18, 2024 · N364CM · Boeing 767338 · Navigation System
  > LOST FLIGHT DIRECTOR DURING PUSHBACK AC RETURNED TO THE GATE AND MAINTENANCE GROUNDED ACFT AND TRANSFERED POWER FD CAME BACK C/W MCDP GROUND TEST 30 IAW AMM 22-00-01. ALL INDICATIONS NORMAL A/C REMAINS CAT 3B OPERATIONAL RETURNED AC TO SERVICE
- [SDR ABXA2024041078](https://openairdocs.org/sdr/ABXA2024041078.md): Door · unsecure · Apr 10, 2024 · N364CM · Boeing 767338 · Cargo/Baggage Doors
  > MCD WARNING ANNUCIATORS INDICATOR ILLUMINATED DURING PUSH-BACK, AC RETURED TO THE GATE AND MAINTENANCE CLOSED AND LATCHED MAIN CARGO DOOR IAW B767 AMM 52-32-00 DOOR OPS CHECK GOOD.AC TAXIED OUT AND DEPARTED IN SERVICABE CONDITION,.
- [SDR ABXA2024031558](https://openairdocs.org/sdr/ABXA2024031558.md): Apu · shutdown · Mar 15, 2024 · N364CM · Boeing 767338 · APU Core Engine
  > APU SHUTDOWN ON PUSHBACK AC RETURNED TO THE GATE AND MAINTENANCE GROUNDED AC. AND DEFERRRED THE APU FOR DEPARTURE IAW MEL ABX-49-11-1A AND RETURNED AC TO SERVICE. AC DEPARTED
- [SDR ABXA20240304151](https://openairdocs.org/sdr/ABXA20240304151.md): Fseu · faulted · Mar 1, 2024 · N364CM · Boeing 767338 · Trailing Edge Flap Control System
  > DURING ILS 31R AT KJFK, WHEN FLAPS SELECTED TO 25, FLAPS STAYED AT 20. EXECUTED MISSED APPROACH. HELD AT CHANT. DECLARED AN EMERGENCY. REBRIEFED AND COMPLETED VISUAL APPROACH TO 31L. LANDED SAFELY.C/W FSEU BYTE CHECK I/A/W FIM27-51 FT 809. NO FAULTS. INSPECTED
- [SDR ABXA20231230231](https://openairdocs.org/sdr/ABXA20231230231.md): Unknown · unknown · Dec 30, 2023 · N364CM · Boeing 767338 · Navigation System
  > CAPT FD INOP AND ALT IND ON A/S INOP.A/C RETURNED TO GATE MAINTENANCE GROUNDED A/C.C/W TURNING OFF FLIGHT DIRECTOR AND COMPLETE IRU REALIGNMENT PER AMM 34-24-01 OPS CHECK GOOD ON CAPT'S AND FO'S FLIGHT DIRECTOR A/C REMAINS CAT IIIB STATUS.MAINTENANCE RETU
- [SDR ABXA202312263228](https://openairdocs.org/sdr/ABXA202312263228.md): Pitot Tube · malfunctioned · Dec 23, 2023 · N364CM · Boeing 767338 · Pitot/Static Anti-Ice System
  > L AUX PITOT EICAS AND OVERHEAD DISCREATE LT ILLUMINATED AFTER ENGINE STARTED AC RETURNED TO BLOCK AND MAINTENACE GROUNDED AC.T/S FIM PER 30-31 FT. 804, FOUND PITOT FAULTY, REPLACED L AUX PITOT PROBE IAW AMM 34-11-01, PART EFFECTIVITY VERIFIEDPERFORMED L AUX P
- [SDR ABXA2023113210](https://openairdocs.org/sdr/ABXA2023113210.md): Unknown · unknown · Nov 3, 2023 · N364CM · Boeing 767338 · Fuel Boost Pump
  > RIGHT CENTER FUEL PUMP INOP, CENTER RT PUMP DID NO OPERATE AFTER START OF RIGHT A/C RETURNED TO BLOCK AND MAINTENANCE GROUNDED A/C.DEFERRED SYSTEM IAW MEL 28-22-2A. FOR DISPATCH. AC FLOWN TO LIM. PERFORMED GROUND FAULT INTERRUPTOR OPS TEST. FOUND RELAY K1
- [SDR ABXA20231025206](https://openairdocs.org/sdr/ABXA20231025206.md): Module · leaking · Oct 25, 2023 · N364CM · Boeing 767338 · Leading Edge Slat Actuator
  > AFTER TAKEOFF EICAS MSG 1) CHYD QTY 2)C HYD 2 OVHT CENTER HYD SYSTEM REAAD 0.16 AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT GROUNDED BY MAINTENANCE. TROUBLE SHOT AND FOUND OUTBOARD SLAT PDU CONTROL VALVE MODULE LEAKING.REMOVED AND REPLACED LEFT OUTB

Next page: https://openairdocs.org/aircraft/N364CM/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 = 'N364CM' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N364CM/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.