N977ML, cancelled Sep 11, 2002

Service difficulty reports · 32

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N977ML' AND deregistration_id = 'N977ML-2002-09-11'
  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.

SDR EISA99059Gasket · tornADDED 5 QUARTS OIL TO NR 2 ENGINE IN LAS, TOTAL 13 QUARTS. HALF WAY TO SAN, QUANTITY WAS DOWN TO 4 QUARTS. (KEPT SLOWLY DECREASING IN-FLIGHT). SHUT DOWN NR 2 ENGINE. TEMPERATURE NEVER EXCEEDED 110 DEGREES EVEN AFTER IDLING AND SHUT DOWN. DETERMINED OIL FIMar 24, 1999 · N977ML · Doug DC931 · Turbine Engine Oil SystemSDR EISA98283Battery Pack · dischargedFORWARD EMERGENCY LIGHTS DIM ON TEST. GENERATED BY MAINTENANCE REPORT. REPLACED BATTERY PACK SUPPLY AT BS 24 PER MM 33-00 CHECKS GOOD. (M)Nov 20, 1998 · N977ML · Doug DC931 · Emergency LightingSDR EISA98282Battery Pack · dischargedMIDDLE OVERHEAD EMERGENCY LIGHT DIM ON TEST. GENERATED BY MAINTENANCE REPORT. REPLACED BATTERY PACK SUPPLY AT BS 32 PER MM 33-53-0 CHECKS GOOD. (M)Nov 20, 1998 · N977ML · Doug DC931 · Emergency LightingSDR EISA98281Battery Pack · dischargedFORWARD RIGHT EMERGENCY LIGHTS DIM ON TEST. GENERATED FROM MAINTENANCE REPORT. REPLACED BATTERY PACK SUPPLY AT BS 3 PER MM 33-53-0 CHECK GOOD. (M)Nov 20, 1998 · N977ML · Doug DC931 · Emergency LightingSDR EISA98216Fire Loop · failedRIGHT ENGINE LOOP 'A' FAILS TO TEST, LOOP 'B' CHECK OK. FOUND ON PREFLIGHT. GENERATED FROM PILOT REPORT. FOUND CONTACTS ON CONNECTOR TO BE DIRTY. CLEANED AND RESEATED CONTACTS. CHECK GOOD. (M)Sep 10, 1998 · N977ML · Doug DC931 · Fire DetectionSDR EISA98215Switch · inoperativeRIGHT SIDE A/C PACK SHUT DOWN AT 35,000 FT, CABIN PRESSURE WARNING LIGHT CAME ON, PRESSURE ALTITUDE INDICATED 7000 FT IN THE CABIN. RETURNED TO EL PASO. GENERATED FROM PILOT REPORT. DETERMINED 2 SWITCHES BAD ON A/C SYSTEM REMOVED AND REPLACED 190 DEGREES SWSep 9, 1998 · N977ML · Doug DC931 · Cabin Pressure Control SystemSDR 98ZZZM785Switch · inoperativeRIGHT SIDE A/C PACK SHUT DOWN AT 35,000 FT, CABIN PRESSURE WARNING LIGHT CAME ON, PRESSURE ALTITUDE INDICATED 7000 FT IN THE CABIN. RETURNED TO EL PASO. GENERATED FROM PILOT REPORT. DETERMINED 2 SWITCHES BAD ON A/C SYSTEM REMOVED AND REPLACED 190 DEGREES SWSep 9, 1998 · N977ML · Doug DC931 · Cabin Pressure Control SystemSDR EISA98207Battery Charger · inoperativeAFT SECTION FLOOR MOUNTED EMERGENCY EXIT LIGHTING INOP. REPLACED AFT EMERGENCY LIGHT BATTERY CHARGER IAW MM 33-00. (M)Aug 16, 1998 · N977ML · Doug DC931 · Emergency LightingSDR EISA98202Link · damagedVIBRATION IN NOSHE WHEEL AFTER GEAR RETRACTION, RETURNED TO ELP. GENERATED FROM PILOT REPORT. FOUND RIGHT NOSE GEAR DOOR FORWARD LINK BAD. REMOVED AND REPLACED DOOR LINK. OPS CHECK COMPLETED. NO FURTHER DEFECTS NOTED PER MM 32-22-1. RETRACTION CHECKED GOAug 6, 1998 · N977ML · Doug DC931 · Landing Gear Door Retract SectionSDR EISA98100Floorbeam · corrodedDURING ACCOMPLISHMENT OF CPCP WORKCARD, FOUND AFT CARGO PIT CORROSION AROUND NUTPLATE ON FLOORBEAM FS 965 RIGHT-HAND SIDE. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-05, FIGURE 20 AND 51-30-2. TT: 66,670:41 HOURS. TC: 61,562. (X)Apr 18, 1998 · N977ML · Doug DC931 · Fuselage Main, Floor BeamSDR EISA98099Extrusion · corrodedDURING ACCOMPLISHMENT OF CPCP WORKCARD, FOUND RIGHT-HAND AFT LAV SUPPORT STRUCTURE CORRODED AT STA 1098. REMOVED AND REPLACED EXTRUSION PER SRM 53-05. TT: 66,670:41 HOURS. TC: 61,562. (X)Apr 18, 1998 · N977ML · Doug DC931 · Fuselage Miscellaneous StructureSDR EISA98098Floor · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND FLOOR PANEL AT STA 579 TO STA 680, RIGHT-HAND OF CENTER, WITH CRACKED OUT FASTENER HOLES. FABRICATED AND INSTALLED REPAIR PER 53-03, 51-70-0, AND 51-30-2. TT: 66,670:41 HOURS. TC: 61,562. (X)Apr 18, 1998 · N977ML · Doug DC931 · Fuselage Floor PanelSDR EISA98097Floor · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND LEFT-HAND CENTER FLOORBOARD, STA 579 TO STA 680, WITH 6 EACH FASTENER HOLES CRACKED OUT. FABRICATED AND INSTALLED REPAIR PER 53-05, 51-70-0, AND 51-30-2. TT: 66,670:41 HOURS. TC: 61,562. (X)Apr 18, 1998 · N977ML · Doug DC931 · Fuselage Floor PanelSDR EISA98096Seat Track · corrodedDURING ACCOMPLISHMENT OF CPCP WORKCARD, FOUND SEAT TRACK CORRODED AT STA 737, 757, 775, 850, 870, 887, AND 908, RIGHT-HAND OUTBOARD TRACK. REPLACED RIGHT-HAND OUTBOARD TRACK FROM STA 737 TO STA 965 PER SRM 53-05. TT: 66,670:41 HOURS. TC: 61,562. (X)Apr 18, 1998 · N977ML · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR EISA98095Seat Track · corrodedDURING ACCOMPLISHEMNT OF CPCP WORKCARD, FOUND CORROSION ON RIGHT-HAND INBD SEAT TRACK AT STA 690, 718, 737, 756, 813, 832, 870, AND 889. CORROSION REMOVED FROM STA 690 - STA 737 AND MATERIAL LOSS WITHIN SRM LIMITS 53-05, FIG 4. REPLACED SEAT TRACK FROM STA 7Apr 18, 1998 · N977ML · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR EISA98094Stiffeners · crackedDURING ACCOMPLISHMENT OF CPCP WORKCARD, FOUND RIGHT-HAND FLOOR PANEL AT STA 160 TO STA 200 WITH 2 CRACKED STIFFENERS. FABRICATED AND INSTALLED NEW STIFFENERS PER SRM 53-21-0 AND SRM 51-30-2. (X)Apr 18, 1998 · N977ML · Doug DC931 · Fuselage Miscellaneous StructureSDR EISA98093Skin · dentedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND DENT 1.5 INCHES BY 1.75 INCHES AT FS 1039 BELOW CUSPLINE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-04 AND SRM 51-30-2. (X)Apr 18, 1998 · N977ML · Doug DC931 · Fuselage Main, Plate/SkinSDR EISA98092Skin · corrodedDURING ACCOMPLISHMENT OF CPCP WORKCARD, CORROSION WAS FOUND ON LEFT-HAND WING TRAILING EDGE AT APPROXIMATELY STA XRS 447.3 AS SEEN FROM BELOW. FABRICATED AND INSTALLED NEW SKIN AND DOUBLERS PER SRM 51-70-2. (X)Apr 18, 1998 · N977ML · Doug DC931 · Wing, Plate/SkinSDR EISA98091Bracket · crackedDURING ACCOMPLISHMENT OF AD 80-02-06, NOTED ONE EACH BRACKET CRACKED ON AFT EMERGENCY DOOR. FABRICATED NEW BRACKET PER SRM 51-40-3 AND INSTALLED PER SRM 51-10-3. TT: 66,670:41 HOURS. TC: 61,562. (X)Apr 18, 1998 · N977ML · Doug DC931 · Emergency ExitsSDR EISA98090Structure · corrodedDURING ACCOMPLISHMENT OF CPCP WORKCARD, FOUND CORROSION IN RIGHT AFT LAVATORY FLOOR PAN ATTACH STRUCTURE. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-16, FIGURE 1 AND 51-30-2. (M)Apr 18, 1998 · N977ML · Doug DC931 · Fuselage Main, StructureSDR EISA98089Angle · crackedDURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORKCARD, NOTED A 2 INCH CRACK IN RIGHT AFT EMERGENCY DOOR STRUCTURE LOWER ANGLE. REPLACED ANGLE IN DOOR STRUCTURE PER SRM 52-21-1. (M)Apr 18, 1998 · N977ML · Doug DC931 · Emergency ExitsSDR EISA98088Angle · crackedDURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORKCARD, NOTED A .25 INCH LONG CRACK IN LEFT AFT EMERGENCY EXIT LOWER ANGLE. REPLACED ANGLE IN DOOR STRUCTURE PER SRM 52-21-00. (M)Apr 18, 1998 · N977ML · Doug DC931 · Emergency ExitsSDR EISA98087Angle · crackedDURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORKCARD, NOTED A 1.5 INCH CRACK IN LEFT AFT EMERGENCY EXIT LOWER STRUCTURE ANGLE. REPLACED ANGLE IN DOR STRUCTURE PER SRM 52-21-00. (M)Apr 18, 1998 · N977ML · Doug DC931 · Emergency ExitsSDR EISA98086Angle · crackedDURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORKCARD, NOTED A 1 INCH CRACK IN RIGHT FORWARD EMERGENCY EXIT DOOR STRUCTURE LOWER ANGLE AFT END. REPLACED ANGLE IN DOOR STRUCTURE PER SRM 52-21-1. (M)Apr 17, 1998 · N977ML · Doug DC931 · Emergency ExitsSDR EISA97105Emergency Exit · misinstalledON TAKEOFF FROM ACY, AIRCRAFT WOULD NOT PRESSURIZE LEVELED AT 9000 FEET. LEAK DISCOVERED AT RIGHT OVERWING EXIT RETURNED TO ACY. EMERGENCY EXIT AT 21 DEF INCORRECTLY INSTALLED. REINSTALLED CORRECTLY IAW MM 52-20. (M)Jun 2, 1997 · N977ML · Doug DC931 · Emergency ExitsSDR EISA97102Retract Mech · malfunctionedLOUD VIBRATION FELT ON TAKEOFF FROM NOSE WHEEL AREA. RETURN TO ACY. FOUND FWD NOSE LANDING GEAR DOORS IN DOWN POSITION, CLOSED DOORS PER MM 32-20, OK FOR FLIGHT. (X)May 23, 1997 · N977ML · Doug DC931 · Landing Gear Door Retract SectionSDR EISA97084Light · looseEMERGENCY FLOOR TRACK LIGHTING STRIP LOOSE. RESECURED TRACK LIGHTING COVER. (M)Apr 26, 1997 · N977ML · Doug DC931 · Emergency LightingSDR EISA97082Cover · missingEMERGENCY EXIT LIGHT LENS COVER BY LEFT LAV MISSING. INSTALLED NEW EXIT LENS COVER. (M)Apr 24, 1997 · N977ML · Doug DC931 · Emergency LightingSDR EISA97085Slide · low pressureFORWARD ENTRY DOOR EMERGENCY SLIDE PRESSURE LOW. REPLACED FORWARD EMERGENCY SLIDE IAW MM CHAPTER 25. (M)Apr 21, 1997 · N977ML · Doug DC931 · Escape SlideSDR 96ZZZX2913Frame · crackedDURING A SCHEDULED INSPECTION, CANTED FRAME WAS FOUND CRACKED AT FS 1074 L3 LT. STOP DRILLED CRACK. FABRICATED AND INSTALLED 5 EACH REPAIR PARTS IAW DC-9 SR 09530086.May 9, 1996 · N977ML · Doug DC931 · Fuselage Main, FrameSDR 96ZZZX2912Shear Clip · crackedDURING A SCHEDULED INSPECTION, SHEAR CLIP LOCATED BETWEEN LONGERONS 15R AND 16R WAS FOUND CRACKED 2 INCHES. REMOVED CRACKED SHEAR, FABRICATED AND INSTALLED NEW CLIP IAW DC-9 SRM 53-03, FIGURE 28 AND DC-9, MM 55-00.May 9, 1996 · N977ML · Doug DC931 · Fuselage Miscellaneous StructureSDR EISA95019Eel Connector · corrodedDURING PREFLIGHT AT MCO, FOUND OVERWING EMERGENCY EXIT LIGHTS TOO DIM. BATTERIES CHECKED GOOD, FOUND CORROSION ON LIGHT ASSEMBLIES CONNECTION, CLEANED CORRODED AREAS, LIGHTS CHECKED GOOD. (Z)Feb 23, 1995 · N977ML · Doug DC931 · Emergency Lighting
Back to N977ML, cancelled Sep 11, 2002