N941ML, cancelled Nov 17, 2000

Service difficulty reports · 86

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 = 'N941ML' AND deregistration_id = 'N941ML-2000-11-17'
  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 GTIA000263Slide · dislodgedUPON ARRIVAL OF A/C, FLIGHT ATTENDANT OPENED FORWARD L-1 DOOR AND ESCAPE SLIDE FELL TO GROUND. INSPECTED SLIDE PACK, NOTIFIED M/C AND INSPECTION. RE-INSTALLED SLIDE PACK ON L-1 DOOR IAW CH 25. (M)Jul 22, 2000 · N941ML · Doug DC932 · Escape SlideSDR GTIA000261Light · inoperativeDTW - FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE FROM ROW 6 THROUGH ROW 12. FOUND BATTERIES IN EMERGENCY LIGHTING BATTERY PACK FOR ROWS 6-12 LOOSE. RE-SEATED BATTERIES, EMERGENCY LIGHTS OPS CHECK GOOD. REF DC-9 MM 33-53-0. (M)Jul 17, 2000 · N941ML · Doug DC932 · Emergency LightingSDR GTIA000258Light · inoperativeFLT 856 - ACY - EMERGENCY LIGHTS WILL NOT OPERATED IN CABIN. FOUND BATTERY PACK GOOD, EMERGENCY PATH LIGHTING IS NOT PROPERLY MAKING CONTACT, RESECURED IAW MM 35-50-0. OPS CHECK WAS NORMAL. (M)Jul 15, 2000 · N941ML · Doug DC932 · Emergency LightingSDR GTIA000194Light · inoperativeMLG - FLT 403 - EMERGENCY PATH LIGHTING FORWARD OF ROW 7 INOPERABLE. COULD NOT DUPLICATE INOPERATIVE PATH LIGHTING. SYSTEM OPS CHECKED NORMALLY IAW DC-9 MM 33-00. (X)May 4, 2000 · N941ML · Doug DC932 · Emergency LightingSDR GTIA000190Light · inoperativeMLB - FLT 718 - EMERGENCY FLOOR EXIT LIGHTS INOPERABLE. CLEANED CONNECTION AND BATTERY PACK AT STA 160. OPS CHECK OK IAW MM 33-00. (X)May 2, 2000 · N941ML · Doug DC932 · Emergency LightingSDR GTIA000095Light · obstructedACY - LAST ROW 24 D, E, F CARPET IS COVERING UP EMERGENCY TRACK LIGHTING. ADJUST CARPET ALONG EMERGENCY FLOOR TRACK LIGHT OPS CHECK GOOD PER DC9 MM 33-53-0. (M)Feb 10, 2000 · N941ML · Doug DC932 · Emergency LightingSDR GTIA000094Cover · displacedEMERGENCY TRACK LIGHTING COVER HAS MOVED EXPOSING THE FLOOR WIRES. SECURED FLOOR TRACK THAT SLID FORWARD. CHECKS GOOD PER DC-9 MM 33-53-0. (M)Feb 10, 2000 · N941ML · Doug DC932 · Emergency LightingSDR GTIA0000007Switch · inoperativeCLE - FLOOR TRACK LIGHTS DO NOT ILLUMINATE WHEN SELECTED TO 'ON' POSITION IN COCKPIT. REPLACED EMERGENCY LIGHT SWITCH IN COCKPIT. OPS CHECK GOOD. (M)Dec 28, 1999 · N941ML · Doug DC932 · Emergency LightingSDR GTIA9901098Connector · looseDTW - CABIN EMERGENCY FLOOR LIGHTS INTERMITTENTLY OFF IN FIRST 6 ROWS. CLEANED AND RESEATED CANNON PLUGS ON BATTERY PACKS PERFORMED OPS CHECK IAW MM 33-50-00. OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME. (M)Aug 28, 1999 · N941ML · Doug DC932 · Emergency LightingSDR GTIA9900636Bulb · failedMLB - CO-PILOTS EMERGENCY FLOOR LIGHTS DO NOT COME ON. RELAMPED FIRST OFFICERS EMERGENCY FLOOD LIGHTS. OPERATIONS CHECK GOOD PER DC-9 MM 33-11-2. NO OTHER DISCREPANCIES NOTED. (M)Apr 1, 1999 · N941ML · Doug DC932 · Emergency LightingSDR GTIA9800056Bulb · failedDTW - ROW 8 EMERGENCY TRACK LIGHT INOPERATIVE. RELAMPED ROW 8 EMERGENCY LIGHT OPERATIONAL CHECK GOOD. (M)May 9, 1998 · N941ML · Doug DC932 · Emergency LightingSDR GTIA9800018Battery Pack · dischargedFOUND ON 'A' CHECK, LEFT EMERGENCY OVERWING EVACUATION LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AS REQUIRED IAW DC-9 MM CHAPTER 33-53-0, OPS CHECKED NORMAL. (M)Jan 23, 1998 · N941ML · Doug DC932 · Emergency LightingSDR GTIA9700389Tire · failedACY - FLT 201 - NR 2 MAIN WHEEL BLEW ON LANDING. REMOVED AND REPLACED NR 2 MAIN WHEEL ASSEMBLY PER MM 32-40-1. (M)Oct 27, 1997 · N941ML · Doug DC932 · TireSDR GTIA9700382Pushrod · outof adjustMYR - FLT 1703 - WHEN DEPLOYING FLIGHT SPOILER, A/C ROLLED. FOUND LEFT OUTBOARD SPOILER CONTROL VALVE LINK, PUSHROD OUT OF ADJUSTMENT. ADJUSTED PUSHROD IAW DC-9 MM CHAPTER 27-61. OPS CHECK GOOD. RIGGED LATERAL MIXERS IAW MM 27-61. (M)Oct 12, 1997 · N941ML · Doug DC932 · Drag Control SystemSDR GTIA9700377Fairing · looseACY - FLT 177 - JUST PASSED DOWNWING WITH FLAPS 25 AND GEAR DOWN NOTICED A PRONOUNCED LOW FREQUENCY VIBRATION. PASSENGERS IN AFT ALSO NOTICED THIS VIBRATION UPON DEPARTING THE AIRCRAFT. FOUND INBOARD TRAILING EDGE FLAP TO FUSELAGE FAIRING ON LEFT FLAP VERY LSep 26, 1997 · N941ML · Doug DC932 · Aerodynamic FairingsSDR GTIA9700340Socket · brokenDTW - ON DAILY FOUND EMERGENCY FLOOR TRACK LIGHT INOP BY SEAT 8A, SOCKET TORN APART. TRANSFERRED TO DMI LOG IAW MEL 33-24, CAT 'C' DMI NR 00711. BOS - INSTALL NEW LIGHT BULB SOCKET AND WIRES. OPS CHECK OK IAW MM 33-53-0. THIS CLEARS DMI NR 00711. DISPATCHJul 7, 1997 · N941ML · Doug DC932 · Emergency LightingSDR GTIA9700321Lens · missingMYR - FLT 1606 - RED LENS MISSING FROM EMERGENCY FLOOR LIGHTING (THIRD FROM THE FRONT). REPLACED MISSING LENSES AND BULB FOR EMERGENCY FLOOR LIGHTING. OPS CHECK GOOD. (X)Jun 28, 1997 · N941ML · Doug DC932 · Emergency LightingSDR GTIA9700320Lamp · missingMYR - FLT 1606 - EMERGENCY LIGHT IN FLOR TRACK LIGHTING (ROW 2) OUT. REPLACED MISSING LAMP AND WHITE COER. OPS CHECK GOOD. (M)Jun 28, 1997 · N941ML · Doug DC932 · Emergency LightingSDR GTIA9700288Tire · failedEWR - FLT 1600 - NR 2 MAIN TIRE REQUIRED REPLACMENT DUE NR 1 MAIN TIRE BLOWOUT. CARRY OVER ITEM NR 2 TIRE REPLACMENT PER GTIA GMM CH 4 PG 7.5, PARA 2A2. CARRY OVER NR 0038. REPLACED NR 2 WHEEL AND TIRE ASSY IAW DC-9 MM 32-40-1 SERVICED 160 PSI WITH NITROGENMay 19, 1997 · N941ML · Doug DC932 · TireSDR GTIA9700278Hinge · brokenDTW - DURING COMPLIANCE WITH AD 91-22-07 (AS PER WORK CARD N-3298) THE LEFT AND RT MLG OUTBOARD DOORS AND HINGES WERE INSPECTED AND THE FOLLOWING DISCREPANCY WAS NOTED. LEFT OUTBOARD MLG DOOR UPPER HINGE, AFT LOBE CRACKED. REMOVED AND REPLACED LEFT OUTBOARD Apr 24, 1997 · N941ML · Doug DC932 · Landing Gear DoorsSDR GTIA9700247Tire · failedEWR - FLT 1605 - ON POST/PREFLIGHT, FOUND NR 1 MAIN TIRE BLOWN. NR 2 MAIN TIRE NEEDS REPLACED DUE TO AIRCRAFT TAXIED ON NR 1 MAIN WHEN BLOWN. REMOVED AND REPLACED NR 1 MAIN TIRE AND WHEEL ASSEMBLY PER MM CHAPTER 32-40-1, PAGE 201. REMOVED AND REPLACED MAIN Mar 15, 1997 · N941ML · Doug DC932 · TireSDR 97ZZZM485Tire · failedEWR - FLT 1605 - ON POST/PREFLIGHT, FOUND NR 1 MAIN TIRE BLOWN. NR 2 MAIN TIRE NEEDS REPLACED DUE TO AIRCRAFT TAXIED ON NR 1 MAIN WHEN BLOWN. REMOVED AND REPLACED NR 1 MAIN TIRE AND WHEEL ASSEMBLY PER MM CHAPTER 32-40-1, PAGE 201. REMOVED AND REPLACED MAIN Mar 15, 1997 · N941ML · Doug DC932 · TireSDR GTIA9700246Switch · failedMDW - FLT 1704 - AFTER PUSH BACK AT MYR, SPOILER DEPLOYED LIGHT ILLUMINATED, ACCOMPLISHED PROCEDURE AS PER MEL 27-32, CONTINUED FLIGHT AS PER MEL. LIGHT EXTINGUISHED AFTER TAKEOFF AND NEVER RE-ILLUMINATED. TRANSFERRED TO DMI LOG NR 00252 IAW DC-9 MEL 27-32 CMar 10, 1997 · N941ML · Doug DC932 · Drag Control SystemSDR GTIA9700231Warning Light · illuminatedMDW - FLT 1701 - AFTER PUSH-BACK AT MYR, SPOILER DEPLOYED, LIGHT ILLUMINATED. ACCOMPLISHED PROCEDURE PER MEL 27-32, CONTINUED FLIGHT PER MEL. LIGHT EXTINGUISHED AFTER TAKEOFF AND NEVER RE-ILLUMINATED. TRANSFERRED TO DMI LOG NR 00252 IAW DC-9 MEL 27-32 CAT 'Mar 10, 1997 · N941ML · Doug DC932 · Drag Control SystemSDR GTIA9700230Press System · malfunctionedBOS - FLT 248 - ON TAKEOFF, AUTO PORTION OF CABIN PRESSURIZATION DID NOT WORK. MANUAL WORKED WELL FOR REMAINDER OF FLIGHT USING FCOM PROCEDURES. DEFERRED PER MEL 21-24. MX CONTROL AUTHORIZED DMI NR 00250 CAT 'C'. (X)Mar 10, 1997 · N941ML · Doug DC932 · Cabin Pressure Control SystemSDR GTIA9700179Wheel · rattlesDTW - FLT 626 - NOSE WHEEL RATTLES DURING TURNS AT SLOW SPEED. REMOVED BOTH NOSE WHEEL ASSEMBLIES AND INSPECTED. NO FAULTS FOUND. RE-INSTALLED TIRE ASSEMBLIES IAW DC-9 MM 32-42. OPS CHECK GOOD. (X)Mar 3, 1997 · N941ML · Doug DC932 · Wheel/Ski/FloatSDR GTIA9700184Tire · failedACY - FLT 700 - NR 2 MAIN TIRE REQUIRES REPLACMENT DUE TO NR 1 MAIN TIRE BLOW OUT. TRANSFERRED TO CARRY OVER LOG ITEM 0019 IAW GTIA GMM CHAPTER 4, PAGE 7.5, PARAGRAPH 2.A.2. 3-1-97 - REPLACED NR 2 MAIN TIRE ASSY IAW MM CHAPTER 32-40-1. TIRE SERVICED TO 160 Feb 28, 1997 · N941ML · Doug DC932 · TireSDR GTIA9700183Tire · failedACY - FLT 700 - NR 1 MAIN TIRE EXPERIENCED A BLOW OUT. REMOVED AND REPLACED NR 1 MAIN WHEEL ASSY IAW DC9 MM CHAPTER 32. OK FOR SERVICE. (X)Feb 28, 1997 · N941ML · Doug DC932 · TireSDR GTIA9700164Aoa Transducer · failedDTW - FLT 428 - STALL WARNING FAILURE LIGHT COMES ON INTERMITTENTLY AND SHAKER ACTIVATES. REMOVED AND REPLACED LEFT ANGLE OF ATTACH TRANSDUCER IAW DC-9-MM 94-14-0 PAGE 210. OPS AND PREFLIGHT CHECK GOOD. (M)Feb 7, 1997 · N941ML · Doug DC932 · Stall Warning SystemSDR GTIA96NK217Trapezoidal Pnl · crackedDURING INSPECTION OF LEFT AND RIGHT TRAPEZOIDAL PANEL PER SERVICE BULLETIN 53-182 RIGHT TRAP PANEL CRACKED EXTENDING FROM LEADING EDGE OF PANEL TO SECOND FASTENER. EDDY CURRENT BOLT HOLE INSPECTION CONFIRMS CRACK IS ONLY FROM FIRST HOLE TO FRONT EDGE OF PANELNov 5, 1996 · N941ML · Doug DC932 · Wing Miscellaneous StructureSDR GTIA96NK216Trapezoidal Pnl · crackedDURING INSPECTION OF LEFT AND RIGHT TRAPEZOIDAL PANEL PER S/B 53-182. LEFT TRAP PANEL CRACKED EXTENDED BEYOND EXISTING APPROVED SRM 57-09 FIGURE 6 SHEET 4 REPAIR IT RUNS PAST 4 FASTENER. DAC NOTIFIED ROUTED OUT CRACKED AREA .090 PAST AFT EDGE OF 4TH HOLE. ENov 5, 1996 · N941ML · Doug DC932 · Wing Miscellaneous StructureSDR GTIA96NK210Door Lock · out of adjustREF - CABIN LOG ENTRY NR 1 FROM C/N 8113 EMERGENCY EXIT HATCH ROW 15. AIRCRAFT RIGHT COMES LOOSE ON LANDING. INSPECTED AND ADJUSTED DOOR LOCK BAR IAW DC-9 MM 52-20-0. (M)Sep 30, 1996 · N941ML · Doug DC932 · Emergency ExitsSDR GTIANK198Connector · looseFOUND ON DAILY, NR 1 ENGINE FIRE DETECTOR B-LOOP INOP. FOUND BAD CONNECTOR FORWARD PYLON B-LOOP. CONNECTOR ON ORDER DEFERRED B-LOOP SYSTEM. NR 1 ENGINE PER MEL 26-1 DMI NR 002701. S/D REMOVED AND REPLACED CONNECTOR AT B-LOOP HARNESS APRON. OPS CHECK SATISSep 16, 1996 · N941ML · Doug DC932 · Fire DetectionSDR GTIA96NK201Oxy Hose · failedDURING CLIMB-OUT OF 18,000 FEET, CREW OXYGEN BOTTLE INDICATED JUST BELOW 1500 PSI. RETURNED TO DTW. SHUT OFF BOTTLE AT 1300 PSI. WITH BOTTLE OFF, OXYGEN STILL DECREASED TO 1200 PSI. REMOVED AND REPLACED CREW OXYGEN BOTTLE. FOUND CRACKED OXYGEN FITTING ON Sep 13, 1996 · N941ML · Doug DC932 · Crew Oxygen SystemSDR GTIA96NK198Connector · inopNR 1 ENGINE FIRE DETECTOR B-LOOP INOP, FOUND ON DAILY. FOUND BAD CONNECTOR FORWARD PYLON B-LOOP. CONNECTOR ON ORDER DEFERRED B-LOOP SYSTEM. NR 1 ENGINE PER MEL 26-1 DMI NR 002701. (M)Sep 7, 1996 · N941ML · Doug DC932 · Fire DetectionSDR GTIA96NK191Wire · deterioratedRIGHT LANDING GEAR UNSAFE LIGHT FLICKERS INTERMITTENTLY DURING TRANSIT OF LANDING GEAR BOTH IN RETRACTION AND EXTENSION. REPAIRED WIRING AT AND REPLACE CANNON PLUG ON RIGHT LANDING GEAR UPLIMIT SWITCH. (M)Aug 18, 1996 · N941ML · Doug DC932 · Landing Gear System WiringSDR GTIA96NK184Wire · brokenLEFT MAIN INTRANSIT RED LIGHT DID NOT ILLUMINATE DURING GEAR RETRACTION. FOUND BROKEN WIRES IN LEFT MAIN WHEEL WELL, REPAIRED SAME. (M)Jul 30, 1996 · N941ML · Doug DC932 · Landing Gear System WiringSDR 96NK171Fuel Control · out of adjustLOG PAGE 7770. ABORTED TAKEOFF. ON TAKEOFF, LEFT ENGINE DEVELOPED ONLY 1.8 EPR AT 90 PERCENT N1, RIGHT ENGINE DEVELOPED 1.78 EPR AT 88 PERCENT N1, BOTH POWER LEVERS WERE AGAINST THE STOPS. CORRECTIVE ACTION: TRIMMED NR 1 AND NR 2 ENGINES IAW MM 71-00. REFEMay 24, 1996 · N941ML · Doug DC932 · Fuel Controlling SystemSDR GTIA96NK001Pax Door · would not closeMAIN CABIN DOOR WOULD NOT CLOSE. CLOSED FORWARD AIR STAIR DOOR IAW DC-9MM 52-11-0. (M)Jan 1, 1996 · N941ML · Doug DC932 · Passenger/Crew DoorsSDR GTIANK018Longeron · crackedDURING C-CHECK, FOUND THE FUSELAGE LONGERON 25 LEFT BETWEEN STATION Y446 TO Y465 CRACKED. REPAIRED THE LONGERON 25 IAW SRM 53-02 FIG 2A. (M)Nov 21, 1995 · N941ML · Doug DC932 · Fuselage Main, Longeron/StringerSDR GTIA96NK115Skin · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT SKIN WITH LIGHT CORROSION BETWEEN Y756 AND Y775, LONGERON 26 LEFT AND LONGERON 28 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-04 FIG 38. (M)Nov 21, 1995 · N941ML · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA96NK114Support · corrodedDURING C-CHECK, FOUND AFT CARGO COMPT FITTING SUPPORT FLOOR PANELS WITH CORROSION IN Y815 BETWEEN LONGERON 27 RT AND 28 RT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)Nov 21, 1995 · N941ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA96NK113Floor Beam · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT FLOOR BEAM Y965.09 WITH CORROSION BETWEEN XO AND PLUS X58. REPAIRED FLOOR BEAM LOWER CHORD AT Y965.09 BETWEEN PLUS X6.7 TO PLUS X 18 AND BETWEEN PLUS 21.5 TO PLUS X535 IAW EO NR COO-9-53-138-95. (M)Nov 21, 1995 · N941ML · Doug DC932 · Fuselage Main, Floor BeamSDR GTIA96NK074Longeron · crackedDURING C-CHECK, FOUND FUSELAGE LONGERON 30 SECTION, P/N 592030350, IN BETWEEN STATION Y756 TO STATION Y802 CRACKED. REPLACED LONGERON 30 IAW SRM 51-01 PARA C, SRM 51-30-2. THE FRAMES AT STATION Y775 AND STATION Y794 WERE CUT FOR ACCESS AND REPAIRED IAW SRM 5Nov 21, 1995 · N941ML · Doug DC932 · Fuselage Main, Longeron/StringerSDR GTIA96NK019Floor Beam · corrodedDURING C-CHECK, FOUND THE PAX/FLOOR BEAM LOWER CHORD AT STATION Y965.09 BETWEEN PLUS X6.7 TO PLUS X18 AND BETWEEN PLUS X21.5 TO PLUS 53.5 CORRODED. REPAIRED PAX/FLOOR BEAM LOWER CHORD AT IAW COOPESA DWG NO HSE9-53-140 REV A DATED NOV 12, 1995 AND FAA FORM 811Nov 21, 1995 · N941ML · Doug DC932 · Fuselage Main, Floor BeamSDR GTIA96NK017Fitting · corrodedDURING C-CHECK, FOUND FUSELAGE LONGERON 20 RIGHT END FITTING AT STATION Y996 CORRODED. REPLACED LONGERON 20 END FITTING IAW SRM 51-01 PARAGRAPH C AND SRM 51-10-2. (M)Nov 21, 1995 · N941ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA96NK016Longeron · corrodedDURING C-CHECK, FOUND FUSELAGE LONGERON 30 SECTION BETWEEN STATION Y356.7 TO STATION Y415 CORRODED. REPLACED LONGERON 30 SECTION IAW SRM 51-01 PARAGRAPH C, SRM 51-30-2, SRM 53-02 FIG 14, DATED NOV 13, 1995 AND FAA FORM 8110-3 DATED NOV 13, 1995. (M)Nov 21, 1995 · N941ML · Doug DC932 · Fuselage Main, Longeron/StringerSDR GTIA96NK015Frame · crackedDURING C-CHECK, FOUND RIGHT CENTER OVER WHEEL FRAME, P/N 9919618-2N, AT STATION Y718, CRACKED. REPLACED RIGHT CENTER FRAME IAW MD S/B 53-131 REV 3, DATED FEB 11, 1988 OPTION 2, GROUP III, FIG 4. (M)Nov 21, 1995 · N941ML · Doug DC932 · Fuselage Main, FrameSDR GTIA96NK014Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN SECTION AT PITOT STATIC PORT AREA BETWEEN STATION Y451 TO STATION Y465, LONGERONS 23 LEFT TO 26 LEFT CORRODED. REPAIRED FUSELAGE SKIN IAW SRM 53-04, FIG 31, SHEET 1. (M)Nov 21, 1995 · N941ML · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA96NK013Longeron · corrodedDURING C-CHECK, FOUND FUSELAGE LONGERON 14 LEFT BETWEEN STATION Y1109 TO STATION Y1114 CORRODED. REPAIRED LONGERON 14 LEFT IAW SRM 53-02, FIG 2A. (M)Nov 21, 1995 · N941ML · Doug DC932 · Fuselage Main, Longeron/Stringer
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