# Service difficulty reports: N399CM, cancelled Nov 15, 2024 A list on [N399CM, cancelled Nov 15, 2024](https://openairdocs.org/deregistered/N399CM-2024-11-15.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 5 · 231 reports - [SDR NACA2024100300001](https://openairdocs.org/sdr/NACA2024100300001.md): Cooling Fan · inoperative · Oct 3, 2024 · N399CM · Boeing 767323 · Air Distribution Fan > FWD EQUIP COOLING FAN INOP. CORRECTIVE ACTION PENDING PAPERWORK - [SDR NACA2024091300002](https://openairdocs.org/sdr/NACA2024091300002.md): Stop Fitting · worn · Sep 13, 2024 · N399CM · Boeing 767323 · Engine Thrust Reverser > FOUND NO.2 ENGINE I/B TR LOWER FWD STOP FITTING WORN. EO 767-78-0021 REV IR (12 SEP 24) FAA 8110-3 EARN N399CM-0028 REF CARD 0665 REPLACE DEFLECTION LIMITER IN 10 CYCLES - [SDR NACA2024091100002](https://openairdocs.org/sdr/NACA2024091100002.md): Skin · corroded · Sep 11, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1540 1273 AND S-17R NAC EO 767-53-0061REV IR (09-10-2020) SRM 53-00-01-1A-1 RELATED NRC 0530. EARN N399CM-022 - [SDR NACA2024091100001](https://openairdocs.org/sdr/NACA2024091100001.md): Skin · corroded · Sep 11, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1219 TO 1197+66 AND S-2R. FAA 8110-3 REFER TO NAC EO 767-53-0061 REV IR (09/10/2024) FOR DISPOSITION. SRM 53-00-01-1A-1 FLIGHT VEHICLES CONSULTING EO #24155-1 REV A 6 SEPT 2024. EARN N399CM -022 LONGITUDINAL LAP - [SDR NACA2024090900011](https://openairdocs.org/sdr/NACA2024090900011.md): Skin · corroded · Sep 9, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 676 TO 742 AND S-8R. NAC EO 767-53-0058REV IR (09-10-2020) SRM 53-00-01-1A-1 / NRC 0412, 0527, 0354, 0403, 0388, 0389, 0524, 0737, 0387,0356, 0397, 0375 EARN N399CM-015 RDR SJX-NAC-24-0113-14B /SJX-NAC-24-0122-0 - [SDR NACA2024090900010](https://openairdocs.org/sdr/NACA2024090900010.md): Skin · corroded · Sep 9, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1329 AFT 6 INCH AND S-25L. EARN -N399CM-001 FAA 8110-3 ISSUED 6SEPT 2024 / IAI CS-25451-004 REPAIR INSTRUCTION EO-767-53-0056 REV 1R 09 JUNE 2024 - [SDR NACA2024090090000](https://openairdocs.org/sdr/NACA2024090090000.md): Skin · corroded · Sep 9, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1329 AFT 10 INCH AND S-24L UPPER 3.5 INCH. EARN -N399CM-001 FAA 8110-3 ISSUED 6SEPT 2024 / IAI CS-25451-004 REPAIR INSTRUCTION EO-767-53-0056 REV 1R 09 JUNE 2024 - [SDR NACA2024090900008](https://openairdocs.org/sdr/NACA2024090900008.md): Skin · corroded · Sep 9, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1329 AFT 16.5 INCH AND S-23L UPPER 6.5 INCH. EARN -N399CM-001 FAA 8110-3 ISSUED 6SEPT 2024 / IAI CS-25451-004 REPAIR INSTRUCTION EO-767-53-0056 REV 1R 09 JUNE 2024 - [SDR NACA2024090900007](https://openairdocs.org/sdr/NACA2024090900007.md): Skin · corroded · Sep 9, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1329 AFT 12 INCH AND S-23L UPPER 4 INCH. EARN -N399CM-001 FAA 8110-3 ISSUED 6SEPT 2024 / IAI CS-25451-004 REPAIR INSTRUCTION EO-767-53-0056 REV 1R 09 JUNE 2024 - [SDR NACA2024090900006](https://openairdocs.org/sdr/NACA2024090900006.md): Skin · corroded · Sep 9, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1329 AFT 6 INCH AND S-23L UPPER 2 INCH. EARN -N399CM-001 FAA 8110-3 ISSUED 6SEPT 2024 / IAI CS-25451-004 REPAIR INSTRUCTION EO-767-53-0056 REV 1R 09 JUNE 2024 - [SDR NACA2024090900005](https://openairdocs.org/sdr/NACA2024090900005.md): Skin · corroded · Sep 9, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1329 AFT 10.5 INCH AND S-26L. REPAIR INSTRUCTION EO-767-53-0056 REV 1R 09 JUNE 2024 - [SDR NACA2024090900004](https://openairdocs.org/sdr/NACA2024090900004.md): Skin · corroded · Sep 9, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1329 AFT 12 INCH AND S-26L UPPER 3 INCH. EARN -N399CM-001 FAA 8110-3 ISSUED 6SEPT 2024 / IAI CS-25451-004 REPAIR INSTRUCTION EO-767-53-0056 REV 1R 09 JUNE 2024 - [SDR NACA2024090900003](https://openairdocs.org/sdr/NACA2024090900003.md): Skin · corroded · Sep 9, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1307 AFT 16 INCH AND S-22L. EARN -N399CM-001 FAA 8110-3 ISSUED 6SEPT 2024 / IAI CS-25451-004 REPAIR INSTRUCTION EO-767-53-0056 REV 1R 09 JUNE 2024 - [SDR NACA2024090900002](https://openairdocs.org/sdr/NACA2024090900002.md): Skin · corroded · Sep 9, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1307 AFT 10 INCH AND S-26L UPPER 5.5 INCH. EARN -N399CM-001 FAA 8110-3 ISSUED 6SEPT 2024 / IAI CS-25451-004 REPAIR INSTRUCTION EO-767-53-0056 REV 1R 09 JUNE 2024 - [SDR NACA2024090800016](https://openairdocs.org/sdr/NACA2024090800016.md): Skin · corroded · Sep 8, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORR0SION AT STA 1678 TO 1702 AND S8R. REFERENCE NAC EO 767-53-0058 (09-04-2024) REF SRM53-00-01-1A-1 EARN N399CM-0031 - [SDR NACA2024090800015](https://openairdocs.org/sdr/NACA2024090800015.md): Skin · corroded · Sep 8, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 889 TO 955 AND S-8R. NAC EO 767-53-0058REV IR (09-10-2020) SRM 53-00-01-1A-1 / NRC 0412, 0527, 0354, 0403, 0388, 0389, 0524, 0737, 0387,0356, 0397, 0375 EARN N399CM-024 RDR SJX-NAC-24-0113-14B /SJX-NAC-24-0122- - [SDR NACA2024090800014](https://openairdocs.org/sdr/NACA2024090800014.md): Skin · corroded · Sep 8, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1629 TO 1654 AND S-8R TO S-9R. NAC EO 767-53-0058REV IR (09-10-2020) SRM 53-00-01-1A-1 / NRC 0412, 0527, 0354, 0403, 0388, 0389, 0524, 0737, 0387,0356, 0397, 0375 EARN N399CM-030 RDR SJX-NAC-24-0113-14B /SJX-NAC - [SDR NACA2024090800013](https://openairdocs.org/sdr/NACA2024090800013.md): Skin · corroded · Sep 8, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 852 TO 915 AND S-2R. NAC EO 767-53-0058REV IR (09-10-2020) SRM 53-00-01-1A-1 / NRC 0412, 0527, 0354, 0403, 0388, 0389, 0524, 0737, 0387,0356, 0397, 0375 EARN N399CM-023RDR SJX-NAC-24-0113-14B /SJX-NAC-24-0122-06 - [SDR NACA2024090800012](https://openairdocs.org/sdr/NACA2024090800012.md): Skin · corroded · Sep 8, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1043 TO 999 AND S-2R. NAC EO 767-53-0058REV IR (09-10-2020) SRM 53-00-01-1A-1 / NRC 0412, 0527, 0354, 0403, 0388, 0389, 0524, 0737, 0387,0356, 0397, 0375 EARN N399CM-023RDR SJX-NAC-24-0113-14B /SJX-NAC-24-0122 - [SDR NACA2024090800011](https://openairdocs.org/sdr/NACA2024090800011.md): Skin · corroded · Sep 8, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1065 AND S-2R TO S-4R. NAC EO 767-53-0058REV IR (09-10-2020) SRM 53-00-01-1A-1 / NRC 0412, 0527, 0354, 0403, 0388, 0389, 0524, 0737, 0387,0356, 0397, 0375 EARN N399CM-025 - RDR SJX-NAC-24-0113-14B /SJX-NAC-24-01 - [SDR NACA2024090800010](https://openairdocs.org/sdr/NACA2024090800010.md): Skin · corroded · Sep 8, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1605 TO 1654 AND S-8L. NAC EO 767-53-0058REV IR (09-10-2020) SRM 53-00-01-1A-1 / NRC 0412, 0527, 0354, 0403, 0388, 0389, 0524, 0737, 0387,0356, 0397, 0375 EARN N399CM-027RDR SJX-NAC-24-0113-14B /SJX-NAC-24-0122- - [SDR NACA2024090800009](https://openairdocs.org/sdr/NACA2024090800009.md): Skin · inoperative · Sep 8, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1725 AND S-8L TO S-6L. NAC EO 767-53-0058REV IR (09-10-2020) SRM 53-00-01-1A-1 / NRC 0412, 0527, 0354, 0403, 0388, 0389, 0524, 0737, 0387,0356, 0397, 0375 EARN N399CM-027RDR SJX-NAC-24-0113-14B /SJX-NAC-24-0122- - [SDR NACA2024090800008](https://openairdocs.org/sdr/NACA2024090800008.md): Skin · corroded · Sep 8, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1654 TO 1678 AND S-23R. NAC EO 767-53-0058REV IR (09-10-2020) SRM 53-00-01-1A-1 / NRC 0412, 0527, 0354, 0403, 0388, 0389, 0524, 0737, 0387,0356, 0397, 0375. EARN N399CM-032RDR SJX-NAC-24-0113-14B /SJX-NAC-24-0 - [SDR NACA2024090800007](https://openairdocs.org/sdr/NACA2024090800007.md): Skin · corroded · Sep 8, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1605 TO 1629 AND S-23R. NAC EO 767-53-0058REV IR (09-10-2020) SRM 53-00-01-1A-1 / NRC 0412, 0527, 0354, 0403, 0388, 0389, 0524, 0737, 0387,0356, 0397, 0375 EARN N399CM-032 RDR SJX-NAC-24-0113-14B /SJX-NAC-24-012 - [SDR NACA2024090800006](https://openairdocs.org/sdr/NACA2024090800006.md): Skin · corroded · Sep 8, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1582 TO 1605 AND S-23R. NAC EO 767-53-0058REV IR (09-10-2020) SRM 53-00-01-1A-1 / NRC 0412, 0527, 0354, 0403, 0388, 0389, 0524, 0737, 0387,0356, 0397, 0375. EARN N399CM-027RDR SJX-NAC-24-0113-14B /SJX-NAC-24-012 - [SDR NACA2024090800005](https://openairdocs.org/sdr/NACA2024090800005.md): Skin · corroded · Sep 8, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1832 AND S-25R. NAC EO 767-53-0058REV IR (09-10-2020) SRM 53-00-01-1A-1 / NRC 0412, 0527, 0354, 0403, 0388, 0389, 0524, 0737, 0387,0356, 0397, 0375 EARN N399CM-027RDR SJX-NAC-24-0113-14B /SJX-NAC-24-0122-06B / - [SDR NACA2024090800004](https://openairdocs.org/sdr/NACA2024090800004.md): Skin · corroded · Sep 8, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1678 TO 1702 AND S-23L. NAC EO 767-53-0058REV IR (09-10-2020) SRM 53-00-01-1A-1 / NRC 0412, 0527, 0354, 0403, 0388, 0389, 0524, 0737, 0387,0356, 0397, 0375 EARN N399CM-029RDR SJX-NAC-24-0113-14B /SJX-NAC-24-0122 - [SDR NACA2024090800002](https://openairdocs.org/sdr/NACA2024090800002.md): Skin · corroded · Sep 8, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1605 TO 1629 AND S-23L. NAC EO 767-53-0058REV IR (09-10-2020) SRM 53-00-01-1A-1 / NRC 0412, 0527, 0354, 0403, 0388, 0389, 0524, 0737, 0387,0356, 0397, 0375 EARN N399CM-029RDR SJX-NAC-24-0113-14B /SJX-NAC-24-0122 - [SDR NACA2024090500006](https://openairdocs.org/sdr/NACA2024090500006.md): Duct · worn · Sep 5, 2024 · N399CM · Boeing 767323 · Air Distribution System > FOUND FWD CARGO COMPARTMENT AIR EXHAUST DUCT ASSY WORN STA 434. EXHAUST DUCT REPLACED FAA 8130-3 RECEIVED - [SDR NACA2024090500005](https://openairdocs.org/sdr/NACA2024090500005.md): Floorbeam · corroded · Sep 5, 2024 · N399CM · Boeing 767323 · Fuselage Main, Floor Beam > FWD CARGO FLOOR PANEL INNER CHORD FOUND CORROSION AT STA522 RBL30. FAA FORM 8100-9 ISSUED 3 SEP 2024 CHORD REPLACED - [SDR NACA2024090500004](https://openairdocs.org/sdr/NACA2024090500004.md): Skin · cracked · Sep 5, 2024 · N399CM · Boeing 767323 · Nacelle/Pylon, Plate/Skin > FOUND OUT LH PYLON SKIN CRACKED AT ACCESS PANEL 432BR CUT OUT 2 O'CLOCK. FAA 8100-9 ISSUED 30 AUG 2024 N399CM - EARN 0006 REFER TO EO 767-54-0008 (09/04/2024) AS ATTACHED FOR DISPOSITION. - [SDR NACA2024090500003](https://openairdocs.org/sdr/NACA2024090500003.md): Skin · unknown · Sep 5, 2024 · N399CM · Boeing 767323 · Horizontal Stabilizer, Plate/Skin > LH HORIZONTAL STABILIZER EXTERIOR SURFACE BLEND OUT FROM FUSELAGE 136 INCH AND LEADING EDGE 37.5 INCH. FAA 8100-9 SEPT 3, 2024 REPETATIVE INSPECTION 3000FC OR 24 MTHS EARN N399CM-0017 - EO 767-57-0030 - [SDR NACA2024090500002](https://openairdocs.org/sdr/NACA2024090500002.md): Spar · corroded · Sep 5, 2024 · N399CM · Boeing 767323 · Wing Spar > FOUND OUT LH WING IB FWD FLAP REAR SPAR LOWER CHORD CORROSION AT 34 INCHES TO OB EDGE. FLAP CHORD REPLACED TO REMOVE CORROSION - [SDR NACA2024090400004](https://openairdocs.org/sdr/NACA2024090400004.md): Stringer · cracked · Sep 4, 2024 · N399CM · Boeing 767323 · Fuselage Main, Longeron/Stringer > FOUND FWD CARGO COMPT THE STRINGER CARCK AT S-34L STA 480. SRTRINGER REPAIRED IAW SRM - [SDR NACA2024090300001](https://openairdocs.org/sdr/NACA2024090300001.md): Door Sill · corroded · Sep 3, 2024 · N399CM · Boeing 767323 · Fuselage Miscellaneous Structure > FOUND BULK CARGO DOOR CUTOUT LOWER SILL INNER CHORD CORROSION AT STA1453-STA1475. BULK CARGO DOOR CUT OUT LOWER SILL INNER CHORD CORROSION. - [SDR NACA2024090200002](https://openairdocs.org/sdr/NACA2024090200002.md): Skin · corroded · Sep 2, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1043 TO 1021 AND S-1R. REPAIR CARRIED IAW SRM - [SDR NACA2024083000001](https://openairdocs.org/sdr/NACA2024083000001.md): Structure · corroded · Aug 30, 2024 · N399CM · Boeing 767323 · Fuselage Structure (General) > FWD CARGO THE UPPER CHORD FOUND CORROSION AT RBL 43 STA 588. REMOVE AND REPLACE THE DAMAGED UPPR CHORD 143T8236-7. NO FURTHER ENGINEERING ACTION IS REQUIRED. - [SDR NACA2024082900001](https://openairdocs.org/sdr/NACA2024082900001.md): Skin · worn · Aug 29, 2024 · N399CM · Boeing 767323 · Nacelle/Pylon, Plate/Skin > FOUND OUT NO.1 ENG RH CORE COWL FLANGE WORN AT 14 INCHES TO LOWER EDGE AND 13 INCHES TO AFT EDGE. EO 5423 - 081 REV 1R REPAIR CARRIED OUT - [SDR NACA2024082800005](https://openairdocs.org/sdr/NACA2024082800005.md): Skin · corroded · Aug 28, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE RH SKIN EXTERIOR SURFACE CORROSION AT STA 188 AND WL 170 -220. CORROSION REMOVED IAW EO 767-53-0059 EARN N399CM-0019 - [SDR NACA2024082800004](https://openairdocs.org/sdr/NACA2024082800004.md): Skin · cracked · Aug 28, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > OPEN HOLE HFEC INSPECTION FOUND 01 EA CRACK AT THE BOTTOM HOLE OF FORWARD SERVICE DOOR(R1) CUTOUT AFT LOWER CORNER FUSELAGE SKIN.AND THE CRACK LENGTH IS ABOUT 0.3 INCH LONG AS MARKED. REPAIRED IAW SRM - [SDR NACA2024082800003](https://openairdocs.org/sdr/NACA2024082800003.md): Skin · corroded · Aug 28, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 188 TO 212 AND S-19L TO S-16L. EO 767-53-0059 BOEING RDRSJX-NAC-24-0105-11B. STAG EARN 0012 &0013 - [SDR NACA2024082800002](https://openairdocs.org/sdr/NACA2024082800002.md): Web · cracked · Aug 28, 2024 · N399CM · Boeing 767323 · Fuselage Miscellaneous Structure > RH WHEEL WELL UPPER WEB CRACK AT STA 955+8 AND RBL 33, EARN N399CM-009 11-AUG-2024: EARN PICKED 12-AUG-2024: EARN CLOSED PER SRM53-50-51 REPAIR 5 - [SDR NACA2024082700002](https://openairdocs.org/sdr/NACA2024082700002.md): Skin · cracked · Aug 27, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > OPEN HOLE HFEC INSPECTION FOUND 02 EA CRACKS AT TWO BOTTOM HOLES OF FORWARD ENTRY DOOR(L1) CUTOUT AFT LOWER CORNER FUSELAGE SKIN.AND THE CRACK LENGTH IS ABOUT 0.1 INCH AND 0.3 INCH LONG AS MARKED. REPAIRED IAW SRM - [SDR NACA2024082600001](https://openairdocs.org/sdr/NACA2024082600001.md): Spar · corroded · Aug 26, 2024 · N399CM · Boeing 767323 · Trailing Edge Flaps > FOUND RH WING IB FWD FLAP REAR SPAR LOWER CHORD CORROSION AT 30 INCHES TO OB EDGE. REMOVED CORROSION, REWORKED AREA AND REPLACED DAMAGED PART IAW SRM 51-40-02 - [SDR NACA2024082500001](https://openairdocs.org/sdr/NACA2024082500001.md): Turbine Case · cracked · Aug 25, 2024 · N399CM · Boeing 767323 · Turbine Section > FOUND NR 2 ENGINE LPT CASE MANIFOLD CRACK AT 5 OCLOCK. REMOVED AND REPLACED #2 ENGINE LPT CASE MANIFOLD IAW AMM 75-29-03 - [SDR NACA2024082300002](https://openairdocs.org/sdr/NACA2024082300002.md): Structure · cracked · Aug 23, 2024 · N399CM · Boeing 767323 · Fuselage Structure (General) > FWD CARGO COMPT UPPER CHORD FOUND CRACK AT LBL 42 STA 412. REPAIRED IAW SRM - [SDR NACA2024082200001](https://openairdocs.org/sdr/NACA2024082200001.md): Stringer · corroded · Aug 22, 2024 · N399CM · Boeing 767323 · Fuselage Main, Longeron/Stringer > FWD CARGO COMPT THE S - 39L STRINGER FOUND CORROSION AT STA 780. CORROSION REMOVED IAW SRM - [SDR NACA2024082100002](https://openairdocs.org/sdr/NACA2024082100002.md): Skin · scratched · Aug 21, 2024 · N399CM · Boeing 767323 · Fuselage Main, Plate/Skin > FOUND RH LOWER AFT FUSELAGE SCRATCH AT STA1351 - STA1373 & S-28R TO S-29R. CORROSION REMOVED IAW SRM - [SDR NACA2024081900003](https://openairdocs.org/sdr/NACA2024081900003.md): Converter · unknown · Aug 19, 2024 · N399CM · Boeing 767323 · Cabin Cooling System > REPLACE COOLING PACK SYSTEM CATALYTIC CONVERTER. REMOVED AND REPLACED COOLING PACK SYSTEM CATALYTIC CONVERTER IAW AMM 21-033-00-02 - [SDR NACA2024081900002](https://openairdocs.org/sdr/NACA2024081900002.md): Shear Tie · corroded · Aug 19, 2024 · N399CM · Boeing 767323 · Fuselage Internal Mounting Structure > BULK CARGO SHEAR TIE FOUND CORROSION AT STA 1307, S39L TO S39R. RECTIFIED IAW SRM Next page: https://openairdocs.org/deregistered/N399CM-2024-11-15/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 = 'N399CM' AND deregistration_id = 'N399CM-2024-11-15' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N399CM-2024-11-15/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.