Douglas DC-8-73
Service difficulty reports · 821
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Query with SQL
duckdb -csv -c "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 aircraft_model_key = 'DC873' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 aircraft_model_key = 'DC873' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DHL2005803510Fitting · crackedITEM REF NR 033357: MAIN CARGO COMPT FITTING CRACKED 3.500 INCHES STA 680.000 L-11R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IASDR DHL2005803507Skin · wornITEM REF NR 038897: LT WING INBD FLAP PLATING UPPER PART WORN 1" XW 104.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG. 1. REMOVED DAMAGED PLATING IAW SRM 51-1-21. FABRICATED NEW PLATING (AL 2024T3 0.040") IAW SRM 57-7-1 FIG. 1 ITEM D. CLEANED, TSDR DHL2005803505Skin · wornITEM REF NR 032704: RT OUTBD FLAP UPPER SURFACE WORN (STA XF 203.000-210.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG. 4, TR 57-94. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG. 1, SRM 51-1-21. FABRICATED NEW PLATING (AL 2024T3 0.040") IAW SRM 57-SDR DHL2005803502Floor Panel · corrodedITEM REF. NR. 033228: MAIN CARGO COMPT INTERIOR FLOOR PANEL SUPPORT CORRODED, STA 1726.000 RBL 30. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. MEASURED THICKNESS 0.090". BLEND OUT 0.024", REMAINING MATERIAL 0.066". FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-2-0 SDR DHL2005803503Fitting · crackedITEM REF. NR. 033307: MAIN CARGO COMPT SPLICE FITTING CRACKED 5.500 INCHES, STA 857.000 L-1 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG. 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLESDR DHL2005803500Floor Panel · corrodedITEM REF. NR. 033352: MAIN CARGO COMPT. FLOOR PANEL CORRODED, STA 0440.000 LBL 56. REMOVED CORROSION FROM FLOOR PANEL STA 1440.000 LBL 56" IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2P. CUT OUT DAMAGED SECTION AND FABRICATED DOUBLER (7075SDR DHL2005803501Floor Panel · corrodedITEM REF NR 033351: MAIN CARGO COMPT. FLOOR PANEL CORRODED, STA 1360.000 LBL 56". REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18 FLOOR PANEL THICKNESS 0.071". BLEND OUT 0.035", REMAINING MATERIAL 0.036". FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-2-0 PG. 2P. TRIMMEDSDR DHL2005803515Fitting · crackedMAIN CARGO COMPT INTERIOR SPLICE FITTING CRACKED 2 INCHES STA 902.000 - STA 909.000 L-6R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTSDR DHL2005802009Fire Detector · malfunctionedAT FL 320 NR 2 ENGINE HAD INTERMITTENT FIRE WARNING. COMPLETED PHASE 1 OF ENGINE FIRE CHECKLIST, NO INDICATION OF FIRE, COMPLETED CHECKLIST. CHECKED BOTH LOOP A AND B. FIRE BOTTLE WAS NOT DISCHARGED. PLACED FIRE DETECTION LOOP A ON NR 2 ENGINE ON MEL 26-2-SDR DHL2005802008Fire Loop · failedENROUTE AT FL 370 WE HAD AN INTERMITTENT NR 2 FIRE INDICATION. AFTER BOTH BOTTLES WERE FIRED THE FIRE INDICATION REMAINED CONSTANT FOR APPROX 10 MIN AND WAS INTERMITTENT THROUGH REMAINDER OF FLT. LOOP-A FAILED TO TEST FOR FIRE WARNING, SHORT TEST GOOD.SDR DHL2005803002Proximity Sensor · malfunctionedDURING PREFLIGHT PERFORMED GEAR UNSAFE LIGHT CHECK LEFT DOOR UNSAFE LIGHT WOULD NOT ILLUMINATE DURING CHECK. ITEM TRANSF TO DMI NR 21967 IAW MEL 32-14 CAT "A"3.) REF DMI #21967 DURING PREFLIGHT PERFORMED GEAR UNSAFE LIGHT CHECK LEFT DOOR UNSAFE LIGHT WOULD NSDR DHL2005802542Support Bracket · crackedRUDDER TAB HINGE SUPPORT BRACKET CRACKED. REMOVED RUDDER TAB IAW MM 27-21-2 PG. 201. REMOVED CRACKED BRACKET IAW SRM 51-1-21. FABRICATED BRACKET IAW JC EA55100013-001-D, DWG DOUGLAS 4701452 AND BOEING COMPANY MSG 1-109638692-2. PERFORMED NDT INSP IAW DC8 NDT SSDR DHL2005802538Skin · corrodedITEM REF. NR. 045009: FWD ACCY COMPT. FUSELAGE INTERNAL SKIN CORRODED, STA 20.000 L-31R TO L-32R (STA 20.000-70.000) MAJOR REPAIR. CORR.: PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-18-05 DWG Z20-R14 REV IR DATED 06-24-05. REMOVED EXISTING REPAIR IAW SSDR DHL2005802533Fitting · brokenFWD ACCY COMPT. FITTING BROKEN 0.500 STA 70.000 L-31R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG. 1. REMOVED DAMAGED FITTING IAW SRM 51-1-20D PG. 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-SDR DHL2005802544Frame · crackedCARGO COMPT. FRAME 3.000 CRACK STA 278.000 L-20L (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 27 JUN 05, BOEING MSG 1-105552361-2, 1-105552361-3 DATED 27 JUN 05. REMOVED SUB FLOOR IAW SRM 51-1-21A PG. 1-4. REMOVED FITTING IAW SRM 51-SDR DHL2005802543Frame · crackedRT MLG WW FRAME CRACK 5.000 STA 868.000 RBL 50 (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 2 SHEET 3,6. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. CUT OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 FIG. 2 SHEET 3. PERFORMED DSDR DHL2005802541Web · crackedRUDDER L/E FRONT SPAR FWD NOSE RIB WEB CRACK 1.500 STA ZR 71.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DOUGLAS DWG 5700556, JC EA55100012-001-D. REMOVED DAMAGED RIB IAW SRM 51-1-21 PG. 1. FABRICATED NEW RIB (AL2024"O" 0.063) IAW DWG 5700556, EA SEMAN 2005SDR DHL2005802539Skin · corrodedFUSELAGE INTERNAL SKIN CORRODED STA 220.000 L-35L TO L-36 (FWD CARGO COMPT. BILGE) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-15-05 DWG Z20-R06 REV. IR DATED 06-24-05. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. REMOVEDSDR DHL2005802535Doubler · brokenEXTERIOR FUSELAGE NR 2 ACCESS DOOR INTERNAL DOUBLER BROKEN STA -165.000 TO -156.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-15-05 DWG Z20-R15 REV IR DATED 06-24-05. REMOVED INTERNAL REPAIR DOUBLER AND EXTERNAL PLATING IAW SRM 51-1-21 SDR DHL2005802523Fitting · crackedMAIN TANK INTERIOR LWR SECTION INBD AFT FITTING CRACK STA XRS 74.689 S-61. PERFORMED MAJOR RELPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. CLEANED AND APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-12 PG 7. SDR DHL2005802545Door Frame · crackedCARGO DOOR AFT LWR JAMB CORNER 0.500 CRACKED STA 1440.000 L-32R TO L-33R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 BOEING MESSAGE 1-106666113-2, 1-106666113-3 DATED 07-01-03. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. CUT OUSDR DHL2005802540Frame · crackedRT UPPER CUSP EXTRUSION FRAME FWD FLANGE CRACK 0.750 STA 240.000 L-20R TO L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 2 SHEET 1,2,6, SRM 53-2-0 FIG. 2 SHEET 7-8, TR 53-110, SRM 53-2-0 FIG. 2 SHEET 1, SRM 53-4-1 FIG. 40 SHEET 7-9, SRM 51-2SDR DHL2005802525Skin · crackedFUSELAGE EXTERNAL SKIN AFT OF HOLD OPEN HOOK PIN CRACKED 0.375 STA 1610.000 L-14L TO L-15L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-11-05, DWG Z20-R04 REV IR DATED 06-24-05. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 2SDR DHL2005802524Fitting · crackedLT STUB WING INTERIOR FITTING CRACKED 2.000 (MAJOR REPAIR)STA XOLDO 67.750 PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYINGSDR DHL2005802520Fitting · crackedFUSELAGE TAIL SECTION L-17R FITTING CRACKED 0.250 STA 1766.000-1782.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLSDR DHL2005802516Panel · delaminatedLT WING T/E UPPER PANEL DELAMINATED (STA XW 5.000 - 47.000). REMOVED AND REPLACED LT WING TE UPPER PANEL (STA XW 5.000-47.000) IAW SRM 51-3-0 PG. 1. TORQUED IAW3 SRM 51-3-1.SDR DHL2005802536Fitting · crackedNR 2 MAIN TANK INTERIOR OUTBD FWD FITTING CRACKED STA XRS 74.869 S-61 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG. 21. CLEANED AND APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-SDR DHL2005802532Doubler · crackedEXTERIOR FUSELAGE NOSE SECTION STRUCTURAL MODIFICATION DOUBLER (ACS) CRACKED 0.750 AT AFT LWR CORNER OF RT PRIMARY HEAT EXCHANGER STA -12.000 L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-13-05, DWG Z20-R01 REV. IR DATED 06-24-05. SDR DHL2005802530Fitting · crackedNR 2 MAIN TANK INTERIOR LWR SECTION OUTBD AFT FITTING CRACKED STA XRS 74.869 S-61 (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG. 21. CLEANED AND APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-SDR DHL2005802527Fitting · crackedNR 2 MAIN TANK INTERIOR LOWER SECTION INBD FWD FITTING CRACK, STA XRS 74.869 S-61 (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG. 21. CLEANED AND APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-SDR DHL2005802526Doubler · crackedEXTERIOR FUSELAGE NOSE SECTION ESTRUCTURAL MODIFICATION DOUBLER (ACS) CRACKED 0.250 AT AFT UPPER CORNER OF PRIMARY HEAT EXCHANGER STA -12.000 L-24L (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-11-05, DWG Z20-R02 REV. IR DATED 06-2SDR DHL2005802531Longeron · crackedFUSELAGE TAIL SECTION L-17L CRACKED 2.000 (STA 1766.000-1786.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1, SRM 53-5-3 PG. 16 FIG. 5. REMOVED CRACKED LONGERON IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. FABRICATED NEW LONGERON P/N S1616757 IASDR DHL2005802509Angle · corrodedMAIN CARGO COMPT. PNEU. DUCT COVER SUPPORT ANGLE CORRODED STA 8.000 - 17.000, RBL 59. REMOVED CORROSION FRON SUPPORT ANGLE IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-3 PG. 2P. FABRICATED NEW SUPPORT ANGLE IAW SRM 53-2-0 PG.1. CLEANED, TREATED SDR DHL2005802510Floor Support · corrodedAFT ACCY COMPT. FLOOR SUPPORT ANGLE CORRODED, STA 1710.000 RBL 19. REMOVED CORROSION FROM SUPPORT ANGLE IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2P. FABRICATED REINFORCING ANGLE IAW SRM 53-7-3 FIG. 5A, SRM 53-2-0 PG. 2E/2F. CLEANED, TRESDR DHL2005802515Longeron · crackedFWD CARGO COMPT. CROSS SLIDE DOOR AREA L-35L CRACKED 1.000 STA 300.000-310.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 1B. REMOVED FASTENERS IAW SRM 51-1-20D PG. 21. PERFORMED STOP HOLE IAW SRM 53-2-0 FIG. 1B SHEET 3. PERFORMED NDT INSP IAW DCSDR DHL2005802513Longeron · crackedFWD CARGO COMPT CROSS SLIDE DOOR AREA L-35L CRACKED STA 280.000-300.000 MAJOR REPAIR. CORR.: PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 1B. REMOVED FASTENERS IAW SRM 51-1-20D PG. 21. PERFORMED STOP HOLE IAW SRM 53-2-0 FIG. 1B (SHEET 3). PERFORMED NDT INSPECTIOSDR DHL2005802507Stiffener · crackedITEM REF. NR 030753: FWD ACCESSORY COMPT. FWD PRESSURE BULKHEAD STIFFENER CRACK 2.000 STA 8.000 LBL 20. REMOVED CRACKED STIFFENER IAW SRM 51-1-21 PG.1. FABRICATED NEW STIFFENER IAW SRM 53-3-3 FIG. 3. HEAT TREATED IAW SRM 51-1-1 PG. 1,13,17. INSTALLED NEW STIFFSDR DHL2005802506Stiffener · crackedITEM REF. NR. 030754: FWD ACCESSORY COMPT. FWD PRESSURE BULKHEAD STIFFENER CRACK 1.500" STA 8.000 RBL 20. CORR.: REMOVED CRACKED STIFFENER IAW SRM 51-1-21 PG.1. FABRICATED NEW STIFFENER IAW SRM 53-3-3 FIG. 3 ITEM A. HEAT TREATED STIFFENER IAW SRM 51-1-1 PG. 1,SDR DHL2005802508Fitting · crackedAFT CARGO COMPT. INTERCOSTAL FITTING 2.000 CRACK STA 1300.000 L-33R. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG. 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG. 9. TORQUED IAW SRM 51-3-1 PG. 2A.SDR DHL2005802505Doubler · crackedRT OUTER WING INBD L/E LWR DOUBLER CRACKED 0.250. REMOVED CRACKED DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED DOUBLER (AL7075T6 0.050) IAW SRM 57-3-3. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG SDR DHL2005802504Cargo Track · brokenUPPER CARGO COMPT NR 6 TRACK LUGS BROKEN STA 310.000 - 370.000. CUT OUT NR 6 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50 FIG 14. FABRICATED SPLICES IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA AND APLICES IAW SRM 51-1-8B. INSTALLED NESDR DHL2005802503Drive Link · crackedRT OUTBD FLAP DRIVE LINK ASSY CRACKED 0.500 INCH LENGTH AT POINT J STA XF 219.498. REMOVED AND REPLACED RH OUTBD FLAP DRIVE LINK ASSY AT STA XF 219.498 IAW MM 27-51-4 PG. 201-204. REFER TO NR 030703 FOR OPS CHECK.SDR DHL2005802502Skin · crackedRT OUTBD FLAP UPPER SKIN CRACKED 0.500 APPROX. AT STA XF 304.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-7-1 FIG. 4, TR 57-94. REMOVED CRACKED PLATING IAW SRM 51-1-21 PG.1. FABRICATED NEW PLATING IAW SRM 57-7-1 FIG. 4, TR 57-94 ITESDR DHL2005802501Skin · damagedRT INBD FLAP UPPER EXTERNAL SKIN INTERIM REPAIR, STA XW 104.000-110.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-7-1 FIG. 1. REMOVED PLATING WITH EXISTING INTERIM REPAIR IAW SRM 51-1-21 PG.1. FABRICATED NEW PLATING (AL2024Y3 0.040) ISDR DHL2005802500Cargo Track · corrodedUPPER CARGO COMPT NR 2 TRACK CORRODED, STA 780.000 - 786.000. REMOVED CORROSION FROM TRACK NR 2 IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-3 FIG. 12. CUT OUT NR 2 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG. 49-50 FIG. 14. FABRICATED SPLICES IAW SDR UPS05844813Floorbeam · corrodedINSPECTION TYPE:C3, MAIN CABIN FLOORBEAM, EXISTING REPAIR UNDER AREA HAS HEAVY CORROSION AT STA 940 RBL 65. REMOVED EXISTING 2 FLOORBEAM REPAIRS, 1 FILLER AND FLOORBEAM. FABRICATED AND INSTALLED FLOORBEAM AND 4 REPAIR ANGLES IAW EO DC8-53-20466 AND SAA SK840SDR DHL2005802007Control Panel · malfunctionedNR 1 BUS FAILED ON ENGINE START. DEFERRED NR 1 GEN AND CSD REF MEL 24-1-1A DMI NR 20731 ASSIGNED PLACARD INSTALLED MPEREZ 8427. REF DMI 20731 NR 1 BUSS FAILED ON ENGINE START. REMOVED AND REPLACED BUSS PROTECTION PANEL IAW 24-20-7. OPS CHECKS OK IAW JRH ENSDR DHL2005802006Wire · shortedLEFT GEAR DOOR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. JACKED PLANE PER DACO M/M 7-11-0. PERFORMED GEAR DOOR CHECKOUT PER DACO M/M 32-31-4. FOUND SHORTED POWER WIRE PIN 1 JUST FWD OF DOOR SWITCH. REPAIRED PER DACO M/M 20-50-1. DOOR CHECKS SERV.SDR DHL2005802005Connector · dirtyDOORS NOT LATCHED AND LEFT DOOR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTED LIGHT WENT OUT APPROX ONE 1/2 MINUTES AFTER RETRACTION. CLEANED AND RESECURED CONNECTOR ON LT DOOR SW. OPS CK GOOD PER MM 32-60-0.SDR DHL2005802004Uplock · out of adjustDOOR NOT LATCHES LIGHT ILLUMINATED AFTER TAKEOFF. PERFORMED ABNORMAL PROCEDURE. LEFT AND RIGHT DOOR UNSAFE LIGHT ILLUMINATED. PERFORMED ADJUSTED/TET AT MAIN GEAR DOOR UPLATCH MECHANISM IAW 32-21-4, OPS CKD NORMAL.
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