N947ML, cancelled Oct 31, 2000

Service difficulty reports · 80

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 = 'N947ML' AND deregistration_id = 'N947ML-2000-10-31'
  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 GTIA000142Light · inoperativeACY - FLT 812 - ONE FORWARD EMERGENCY TRACK LIGHT INOPERATIVE. DEFERRED TO DMI 81030-1 MEL 33-24, CAT C, PLACARDS INSTALLED. REPLACED FORWARD EMERGENCY TRACK LIGHT SOCKET. OPS CHECK GOOD IAW MM 33-53-0. THIS CLEARS DMI 81030-1. PLACARD REMOVED. (M)Mar 18, 2000 · N947ML · Doug DC932 · Emergency LightingSDR GTIA9901159Wire · brokenMLB - DURING DAILY, FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE AND REPLACED BULB AND LENSE AND ROW 4. OPERATION CHECK NORMAL IAW 33-53-0. (M)Oct 14, 1999 · N947ML · Doug DC932 · Light System WiringSDR GTIA9900054Light · inoperativeDTW - EMERGENCY EXIT LIGHT INOPERATIVE. MAIN ENTRY DOOR WAY. REMOVED AND REPLACED LIGHT ASSEMBLY. FUNCTIONAL CHECK GOOD DC-9 MM CHAP 33-50-0. (M)Apr 3, 1999 · N947ML · Doug DC932 · Emergency LightingSDR GTIA9800079Slide · looseMAIN CABIN DOOR ESCAPE SLIDE FELL OUT DUE TO JET BLAST. REINSTALLED ESCAPE SLIDE AS REQUIRED. NO DEFECTS NOTED AT THIS TIME IAW DC9 MM 25-61-0. ALL ACCOMPLISHED. (M)Jul 1, 1998 · N947ML · Doug DC932 · Emergency EquipmentSDR GTIA9800051Prox Switch · dirtyLRD - FLT 902 - LANDING GEAR EXTENSION WAS NORMAL. ABOUT 700 FEET ABOVE THE RUNWAY, RT MAIN GEAR RED UNSAFE LIGHT CAME ON FOR 1-2 SECONDS, EVER 5-10 SECONDS. WENT AROUND BUT THE LEFT GEAR DOWN. UNSAFE INDICATIONS STOPPED. USED QRH PROCEDURES, RECYCLED GEARApr 23, 1998 · N947ML · Doug DC932 · Landing Gear Position and WarningSDR GTIA9700407Lights · missingDTW - FLT 626 - MISSING 2 LIGHTS IN THE EMERGENCY TRACK LIGHTING (RED ONES) BY FWD EXITS. REINSTALLED LENS AND LAMPS IN EMERGENCY TRACK LIGHTING. OPS CHECK GOOD. (M)Nov 22, 1997 · N947ML · Doug DC932 · Emergency LightingSDR GTIA9700401Bulb · missingFLL - FLT 411 - MOST FORWARD EMERGENCY FLOOR LIGHT IS INOPERATIVE AND 4TH LIGHT FROM FORWARD IS MISSING. INSTALLED BULB, OPS CHECK GOOD. (M)Nov 17, 1997 · N947ML · Doug DC932 · Emergency LightingSDR GTIA9700398Bulbs · missingPIE - FORWARD SECTION OF RED FLOOR TRACK LIGHTING MISSING 2 LENSES AND LAMPS. REPLACED 2 RED LENSES AND LAMPS IN FORWARD SECTION OF FLOOR TRACK LIGHTING. OPS CHECKS OK PER DC-9 MM CHAPTER 33. (M)Nov 3, 1997 · N947ML · Doug DC932 · Emergency LightingSDR GTIA9700346Bulb · missingDTW - FLT 640 - FORWARD FIRST ROW OF RED EMERGENCY EXITS LIGHTS HAS BULB MISSING. INSTALLED NEW BULB, OPS CHECK GOOD. (M)Jul 21, 1997 · N947ML · Doug DC932 · Emergency LightingSDR GTIA970338Relay · stickingPIT - FLT 202 - APPARENTLY THE RIGHT A/C BUS HAS AN APU RELAY STICKING WHICH WILL NOT ALLOW ANY OTHER POWER SOURCE TO POWER THE RIGHT A/C BUS. THIS OCCURS EVEN WITH THE APU SHUT DOWN. RESET CROSS-TIE RELAY. APU GEN SYSTEM INOP. TRANSFERRED DMI LOG NR 00712Jul 7, 1997 · N947ML · Doug DC932 · AC Power Distribution SystemSDR GTIA9700319Battery · dischargedDTW - ON DAILY INSPECTION, FOUND TRACK LIGHTING NOT TESTING PROPERLY. REPLACED TRACK LIGHTING EMERGENCY BATTERY ASSEMBLY. SYSTEM TESTED NORMAL IAW DC-9 MM 33-50-00. (M)Jun 26, 1997 · N947ML · Doug DC932 · Emergency LightingSDR GTIA9700309Altimeter · failedACY - FLT 178 - BARO ALTIMETER IS READING 150 FEET AT FIELD ELEVATION OF 76 FEET ON CAPTAIN'S SIDE. REMOVED AND REPLACED CAPTAIN'S ALTIMETER PER MM 34-10-6. CLEARS DMI NR 00594. PER GMM CHAPTER 4, PAGE 8.1, REV 25, ITEM 2.B.1. PITOT/STATIC LEAK CHECK TO BEJun 4, 1997 · N947ML · Doug DC932 · Altimeter, Barometric/EncoderSDR GTIA9700306Tire · failedMYR - FLT 111 - LEFT OTBD TIRE BLEW OUT ON EXITING RUNWAY. NORMAL BRAKING, BUT BRAKES APPEARED UNUSUALLY SENSITIVE. EXITING RUNWAY SPEED ABOUT 30 KNOTS ON HIGH SPEED TAXI-WAY MYR. NR 2 MLG TIRE DUE CHANGE, DUE TO NR 1 TIRE BLOW OUT PER GMM CHAP 4, PG 7.5. May 31, 1997 · N947ML · Doug DC932 · TireSDR GTIA9700300Elev Pwr Light · malfunctionedBOS - FLT 243 - ON TAXI OUT, ELEV POWER LIGHT CAME ON PRIOR TO TEST. DURING TEST, LIGHT ON, THEN OFF, NORMAL IND. WITHIN 30 SECONDS LIGHT REAPPEARED VERY DIM, BUT INCREASED IN INTENSITY TO FULL BRIGHT. SHUT DOWN LEFT ENGINE, NORMAL IND RESTARTED LEFT, NORMAMay 26, 1997 · N947ML · Doug DC932 · Elevator Control SystemSDR GTIA9700294Warning Light · illuminatedMYR - FLT 1706 - STAIRWAY DOOR LIGHT CAME ON APPROXIMATELY 1 HOUR INTO FLIGHT, BUT DID EXTINGUISH PRIOR TO LANDING. (2ND OCCURRENCE). TRANSFERRED TO DMI LOG, DMI NR 00574, FORWARD AIRSTAIR DOOR LGIHT PER MEL 33-17 (CAT C). FORWARD AIRSTAIR VERIFIED CLOSED AMay 26, 1997 · N947ML · Doug DC932 · Door Warning SystemSDR GTIA9700293Lens Cover · out of positionMYR - FLT 243 - STAIRWAY DOOR LIGHT CAME ON APROXIMATELY 1 HOUR INTO FLIGHT. FOUND BOTTOM STAIR LIGHT LENS INTERFERRING WITH DOOR CLOSURE. SECURED LENS COVER. STAIRS AND DOOR OPS CHECKS GOOD. (X)May 26, 1997 · N947ML · Doug DC932 · Emergency LightingSDR GTIA9700292Bulb · failedACY - FLT 210 - THIRD LIGHT AFT ON FLOOR LIGHTING INOPERABLE. REPLACED BULB. OPS CHECK GOOD IAW 33-50-0. (X)May 24, 1997 · N947ML · Doug DC932 · Emergency LightingSDR GTIA9700305Mic Jack · shortedMYR - FLT 182 - LOSS OF BOTH RADIOS WHILE SITTING ON END OF RUNWAY FOR TAKEOFF. AFTER TAXI BACK TO RAMP AND DURING ENGINE SHUT DOWN, RADIOS STARTED WORKING NORMALLY. INSPECTED COMM SYSTEMS AND FOUND FAULTY MIC JACK (SHORTED INTERNALLY) AT OB'S POSITION. REMMay 13, 1997 · N947ML · Doug DC932 · Audio Integrating SystemSDR GTIA9700273Locking Mech · lack of lubeACY - FLT 196 - COCKPIT DOOR WILL NOT LOCK DURING TAXI OUT. LUBED AND CLEANED LOCKING MECHANISM. OPS CHECK GOOD OK FOR FURTHER FLIGHT. (M)Apr 6, 1997 · N947ML · Doug DC932 · Fixed Inner DoorsSDR GTIA9700266Annunciator Pnl · malfunctionedDTW - FLT 428 - STAIRWAY DOOR LIGHT CAME ON DURING FLIGHT. TROUBLESHOT SYSTEM, FOUND INTERMITTENT ANNUNCIATOR LIGHT. REMOVED AND REPLACED ANNUNCIATOR PANEL. SYSTEM OPS CHECK GOOD IAW DC9 MM CH 52-70-0. (M)Apr 1, 1997 · N947ML · Doug DC932 · Central WarningSDR GTIA9700265Warning Light · illuminatedDTW - FLT 428 - IN CRUISE, STAIRWAY DOOR LIGHT ILLUMINATED. THERE WAS NOT ANY ADDITIONAL NOISE BY CABIN DOOR OR ANY PRESSURIZATION CHANGES. CYCLED AIRSTAIR SEVERAL TIMES AND LIGHT WENT OUT WITH EVERY CYCLE. OPS CHECK GOOD. (M)Mar 28, 1997 · N947ML · Doug DC932 · Door Warning SystemSDR GTIA9700263Hinge · brokenDTW - FLT 428 - AFT ENTRY DOOR, LOWER HINGE BROKEN. REMOVED AND REPLACED LOWER HINGE, AFT ENTRY DOOR, OVBD HINGE HALF ONLY IAW DC-9 MM 52-20. (M)Mar 27, 1997 · N947ML · Doug DC932 · Passenger/Crew DoorsSDR GTIA9700234Air Data Comp · malfunctionedYIP - REF DME NR 00127 (MRR NR 97-01-27-003/GTIA9700147). AUTOPILOT PORPOISES IN ALL FLIGHT MODES (CLIMB, CRUISE, DESCENT, STABILIZED FLIGHT). FUNCTIONAL CHECK PERFORMED IAW DC-9 MM 22-10-0. READ WIRING TO PITCH CHANNELS. REMOVED AND REPLACED AIR DATA COMPMar 14, 1997 · N947ML · Doug DC932 · Air Data ComputerSDR GTIA9700188Aileron Trim · bindingDTW - AILERON TRIM BINDING AND POSITION INDICATOR WILL NOT CENTER. FOUND SPIRAL DRIVE PLATE ON AILERON TRIM INDICATOR TO BE BINDING AND EXCESSIVELY WORN. REPLACED IAW DC-9 MM 27-10-7. OPS CHECK GOOD. (X)Mar 9, 1997 · N947ML · Doug DC932 · Aileron Tab Control SystemSDR GTIA9700182Wire · looseACY - FLT 825 - NOSE GEAR GREEN LIGHT STAYS ON WITH LANDING GEAR UP. UPLATCH CHECKS OK. LANDING GEAR INDICATIONS NORMAL IN DOWN POSITION. NOSE GEAR RED LIGHT OUT IN UP POSITION AS IT SHOULD BE. REMOVED LANDING GEAR LIGHT CLUSTER. FOUND WIRE GROUNDING OUT Mar 7, 1997 · N947ML · Doug DC932 · Landing Gear System WiringSDR GTIA9700239Autopilot · malfunctionedACY - FLT 700 - AUTOPILOT PORPOISES PLUS OR MINUS 2,000 PER MINUTE VERTICALLY IN CLIMB, CRUISE, DESCENT, IN-FLIGHT. UNUSABLE. ENTER IN DMI LOG NR 00230 PER MEL 22-1 CAT 'C' DUE 3-15-97 ID NR 120. (MRR NR GTIA9700229). REMOVED AND REPLACED AVG COMPUTERS IAWMar 5, 1997 · N947ML · Doug DC932 · Autopilot SystemSDR GTIA9700211Skin · damagedYIP - REPAIR FUSELAGE SKIN DAMAGE AT FS 465-500, LONGERON 23R AND 24R PER SPIRIT EA 5330-97-003. FABRICATED REPAIR IAW SPIRIT EA 5330-97-003. REPAIRED FUSELAGE SKIN FS AT 465-500 PER SPIRIT EA 5330-97-003. (M)Feb 28, 1997 · N947ML · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA9700204Skin · corrodedYIP - REPAIR FUSELAGE SKIN BETWEEN FS 270 - FS 370, LONGERONS 23R TO 26R PER SPIRIT EA 5330-97-004. REPAIRED FUSELAGE SKIN AT FS 270-370, LONGERONS 23R - 26R PER SPIRIT EA 5330-97-004. (X)Feb 28, 1997 · N947ML · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA9700210Panel · delaminatedYIP - LEFT ADF PANEL DELAMINATED. MANUFACTURED FIXTURE TO TRANSFER HOLES. DRILLED HOLES AND COUNTERSUNK AS REQUIRED. TEST FIT AND TRIMMED ALL EDGES OF EXCESS MATERIAL. PAINTED ANTENNA. INSTALLED USING PROPER SCREWS. (X)Feb 27, 1997 · N947ML · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA9700205Sill · corrodedYIP - FORWARD CARGO DOOR SILL LOWER - SPOTS OF CORROSION AROUND SCREW HOLES. REMOVED CORROSION AND TREATED IAW DC-9 SRM 51-10-3. (X)Feb 26, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA9700201Doubler · damagedYIP - EXTERNAL REPAIR DOUBLER ON LOWER EDGE OF CARGO DOOR, FS 928 NEEDS TO BE REMOVED. REMOVED OLD DOUBLER AND INSTALLED NEW REPAIR DOUBLER PER EA 5330-97-005. (X)Feb 26, 1997 · N947ML · Doug DC932 · Cargo/Baggage DoorsSDR GTIA9700198Doubler · loose rivetsYIP - REMOVE RIVETS, INSTALL HI-LOCKS IN REPAIR DOUBLER FS 937 BETWEEN LONGERONS 23L AND 24L. REMOVED RIVETS IN REPAIR DOUBLER, INSTALLED HI-LOCKS IN DOUBLER PER EA 5330-97-006. (X)Feb 26, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA9700206Panel · delaminatedYIP - RIGHT ADF PANEL DELAMINATED. MANUFACTURED FIXTURE TO TRANSFER HOLES. DRILLED HOLES AND COUNTERSUNK AS REQUIRED. TEST FIT AND TRIMMED ALL EDGES OF EXCESS MATERIAL. PAINTED ANTENNA. INSTALLED USING PROPER HARDWARE. (X)Feb 24, 1997 · N947ML · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA9700202Mount · damagedYIP - LEFT NACELLE, ENGINE MOUNT: UPPER AFT VIBRATION ABSORBER ASSY LOOSE, STEM BENT. ALSO, SUSPECT THREADS DAMAGED. REMOVED AND REPLACED ABSORBER IAW DC-9 MM 71-20-3. THREADS IN PYLON YOKE ATTACH BOLT GOOD. (X)Feb 23, 1997 · N947ML · Doug DC932 · Engine Mount SectionSDR GTIA9700190Oxygen Line · leakingYIP - DURING FUNCTIONAL CHECK OF OXYGEN MASK DEPLOYMENT TEST, FOUND DEFECTIVE LEAKING LINE AT SUPPLY MANIFOLD (L13 OVERHEAD PANEL LOCATION). REQUIRES LEAK CHECK. SERVICEABLE LINE INSTALLED IAW DC-9 MM 35-20-2. NO LEAKS NOTED. (X)Feb 23, 1997 · N947ML · Doug DC932 · Passenger Oxygen SystemSDR GTIA9700189Splice · crackedYIP - FORWARD BELLY COMPARTMENT, NR 22 LONGERON CORRODED AND SPLICE PLATE CRACKED AT FS 229. REPAIRED LONGERON AT FS 229 PER DC-9 SRM 53-02. (X)Feb 21, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA9700224Control Cable · frayedYIP - LEFT WING - AILERON CABLE FRAYED NEAR FAIR LEAD AT APPROXIMATELY STA XRS 353. MANUFACTURED AND INSTALLED CABLE, TENSIONED AND SAFTIED IAW DC-9 MM CHAPTER 27-10-0 PAGES 9 AND 10, AND CABLE TENSION CHART. (X)Feb 20, 1997 · N947ML · Doug DC932 · Aileron Control SystemSDR GTIA9700216Skin · damagedYIP - REPAIR ON RIGHT FLAP TRAILING EDGE AT APPROXIMATELY STATION XRS 138-156 BE REMOVED AND REPLACED WITH NEW. REMOVED AND REPLACED RIGHT FLAP TRAILING EDGE WITH NEW PART IAW DC9 SRM 57-03 PAGE 11. (M)Feb 19, 1997 · N947ML · Doug DC932 · Trailing Edge FlapsSDR GTIA9700197Doubler · damagedYIP - EXTERNAL REPAIR DOUBLER FS 351 BETWEEN LONGERONS 18R AND 20R REQUIRES REWORK. REWORKED REPAIR DOUBLER AT RIGHT FUS 351 TO C/W REQUIREMENTS OF DC-9 SRM 53-04 FIG 12B (INSTALLATION OF FINGER DOUBLER AND PROPER FASTENERS). (X)Feb 19, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA9700200Bracket · crackedYIP - LEFT FLAP, INBOARD ATTACH BRACKET CRACKED. (CONFIRMED WITH EDDY CURRENT.) REMOVED AND REPLACED LEFT INBOARD ATTACH BRACKET WITH NEW BRACKET IAW DC-9 MM 20-16-0 PAGE 207. (X)Feb 18, 1997 · N947ML · Doug DC932 · Trailing Edge FlapsSDR GTIA9700227Trap Panel · crackedYIP - ULTRASONIC INDICATION FROM FORWARD MOST END OF UPPER ATTACH FLANGE THROUGH FIRST ATTACH HOLE TO FORWARD END OF SECOND ATTACH HOLE OF LEFT TRAP PANEL (APPROXIMATE LENGTH, 2 INCHES). REMOVED OUTBOARD PORTION OF CRACKED FLANGE AND CORROSION IAW DC-9 SRM 57Feb 17, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA9700199Fairing · corrodedYIP - LEFT HORIZONTAL STABILIZER LOWER SCRAPPER FAIRING: INTERIOR BOX CHANNEL HAS SURFACE CORROSION ALONG ATTACH EDGES. REMOVED MINOR SURFACE CORROSION IAW DC-9 SRM 51-10-3. (X)Feb 17, 1997 · N947ML · Doug DC932 · Horizontal Stabilizer StructureSDR GTIA9700195Rivet · failedYIP - LEFT UPPER HORIZONTAL STABILIZER FAIRING - POPPED RIVET AT AFT ATTACH AND AFT CDCC AREA CRACKED. REPAIRED CRACK AND INSTALLED EXTERNAL DOUBLER AND FILLER PER DC-9 SRM 55-01 PAGE 7, 51-30-2 AND USING MATERIAL AS PRESCRIBED IN DC-9 SRM 55-10-0, PAGE 11, FFeb 14, 1997 · N947ML · Doug DC932 · Horizontal Stabilizer StructureSDR GTIA9700192Clip · brokenYIP - FS 148 CIRCUMFERENTIAL APPROXIMATELY 12 INCHES LEFT OF CENTER OVERHEAD, BROKEN ANGLE CLIP. MANUFACTURED REPAIR ANGLE IAW DC-9 SRM 51-10-1. INSTALLED ANGLE IAW DC-9 SRM 51-30-1. (X)Feb 14, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA9700223Bute Door · damagedYIP - LEFT WING, CENTER BUTE DOOR INBOARD EDGE, SKIN DAMAGED. INSTALLED NEW DOOR ASSEMBLY IAW MM 57-20-3. (X)Feb 13, 1997 · N947ML · Doug DC932 · Wing, Plate/SkinSDR GTIA9700196Skin · damagedYIP - AFT CARGO DOOR, DOOR HANDLE CUT OUT - SKIN DAMAGED. REPAIRED SKIN DAMAGE IAW DC-9 SRM 52-05, FIG 30. (X)Feb 12, 1997 · N947ML · Doug DC932 · Cargo/Baggage DoorsSDR GTIA9700222Skin · corrodedYIP - LEFT WING UPPER SURFACE EVIDENCE OF CORROSION IN 'NO STEP' AREA BETWEEN STA XRS 383-581 (TRAILING EDGE). CLEANED SURFACE CORROSION, TREATED AREA, AND PAINTED IAW DC-9 SRM 51-10-3. (X)Feb 11, 1997 · N947ML · Doug DC932 · Wing, Plate/SkinSDR GTIA9700217Skin · corrodedYIP - RIGHT WING UPPER SURFACE TRAILING EDE HAS EVIDENCE OF CORROSION AT STA XRS 383-531 'NO STEP' AREA. BLENDED OUT CORROSION AND TREATED (REF: DC-9 SRM 51-10-3) IN NO STEP AREA STA 383-531. PREPPED, PRIMED, AND PAINTED RIGHT WING UPPER SURFACE TRAILING EDFeb 11, 1997 · N947ML · Doug DC932 · Wing, Plate/SkinSDR GTIA9700214Angle · corrodedYIP - FORWARD CARGO COMPARTMENT O/H STATION 370 SPOTS OF CORROSION ON LINER SUPPORT ANGLE FROM 0 TO 16 INCH LEFT OF CENTER. REMOVED CORROSION AND TREATED IAW DC-9 SRM 51-10-3. PAINTED IAW 51-10-3B. (M)Feb 11, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA9700213Mount · corrodedYIP - FORWARD CARGO DOOR AFT BUNGEE MOUNT BRACKET SPOTS OF CORROSION AT BOLT HOLES. REMOVED AND TREATED CORROSION FORWARD CARGO DOOR AFT BUNGEE MOUNT BRACKET IAW DC-9 SRM 51-10-3. (M)Feb 11, 1997 · N947ML · Doug DC932 · Cargo/Baggage Doors
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