# Service difficulty reports: N220US, cancelled Jun 14, 2000 A list on [N220US, cancelled Jun 14, 2000](https://openairdocs.org/deregistered/N220US-2000-06-14.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 99ZZZM403](https://openairdocs.org/sdr/99ZZZM403.md): Engine · lost power · May 17, 1999 · N220US · Boeing 7372H5 · Engine (Turbine/Turboprop) > DURING TAKEOFF AT 80-90 KNOTS, NR 2 ENGINE LOST POWER, WAS SHUTDOWN AND TAKEOFF ABORTED. CAUSE UNDER INVESTIGATION AS TO FOD INGESTION OR NOT. (M) - [SDR 98ZZZX3002](https://openairdocs.org/sdr/98ZZZX3002.md): Turbine · failed · Jul 28, 1998 · N220US · Boeing 7372H5 · Turbine Section > ON TAKEOFF FROM GSO ON FLT 405 AT 500 FEET AGL, THE NR 1 ENGINE SHUT DOWN DUE TO APPARENT LPT FAILURE. THE TURBINE WAS CONTAINED AND NO FIRE OR OTHER DAMAGE OCCURRED. THE FLIGHT CREW CONTINUED TO 2,000 FEET, DECLARED EMERGENCY TO GSO TOWER, WAS CLEARED VISUA - [SDR 98ZZZX2562](https://openairdocs.org/sdr/98ZZZX2562.md): Flashlight · failed · Jul 2, 1998 · N220US · Boeing 7372H5 · Emergency Lighting > DURING PRE-FLIGHT CHECK, THE F/A REPORTED THAT ONE OF THE 2 FLASHLIGHTS IN THE AFT GALLEY DID NOT BLINK WITHIN THE REQUIRED 7 SECONDS. PLACED FLASHLIGHT ON MEL 25-12. - [SDR 98ZZZM496](https://openairdocs.org/sdr/98ZZZM496.md): Wire · chafed · May 22, 1998 · N220US · Boeing 7372H5 · Light System Wiring > EMERGENCY EXIT LIGHT PATH INOP. REPAIRED BROKEN WIRE UNDER SEAT 2ABC. (M) - [SDR 98ZZZM495](https://openairdocs.org/sdr/98ZZZM495.md): Bulb · failed · May 22, 1998 · N220US · Boeing 7372H5 · Emergency Lighting > FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB. (M) - [SDR 98ZZZX1075](https://openairdocs.org/sdr/98ZZZX1075.md): Hydraulic Tube · chafed · Feb 13, 1998 · N220US · Boeing 7372H5 · Hydraulic System, Main > FLT 992/23 NCO - LOST A-HYDRAULIC SYSTEM PRESSURE AND QUANTITY AFTER TAKEOFF CLIMBING THROUGH APPROX 3,500 FEET. COMPLETED EMERGENCY CHECK LIST. BURNED OFF EXCESS FUEL AND LANDED WITH AIRCRAFT WEIGHT AT 96,100 POUNDS. GEAR PINS INSTALLED FOR TOWING. INSPEC - [SDR 98ZZZX900](https://openairdocs.org/sdr/98ZZZX900.md): Stator · damaged · Feb 4, 1998 · N220US · Boeing 7372H5 · Compressor Bleed Control > DURING B-CHECK, NR 2 ENGINE INSPECTION FOUND FIRST STAGE COMPRESSOR STATOR VANE DAMAGE. ONE VANE HAD RIVETS SHEARED, VANE SHIFTED AND CAUSED DAMAGE TO ADJACENT VANE. REPLACED 1ST STAGE COMPRESSOR STATOR ASSY ON WING PER MM 72-00-21, 72-00-23, AND 72-00-33. - [SDR 98ZZZX902](https://openairdocs.org/sdr/98ZZZX902.md): Power Supply · inoperative · Jan 25, 1998 · N220US · Boeing 7372H5 · Emergency Lighting > INTERIOR AND EXTERIOR EMERGENCY LIGHTS AT FORWARD ENTRY AND FORWARD SERVICE DOORS DO NOT ILLUMINATE. FOUND ON RON SVC CHECK. REPLACED EMERGENCY LIGHT BATTERY AND POWER SUPPLY IAW B737 MM 33-50. OPERATIONAL CHECKS OK. REF: OPERATOR CONTROL NR 98ZZZX901. - [SDR 98ZZZX901](https://openairdocs.org/sdr/98ZZZX901.md): Battery · discharged · Jan 25, 1998 · N220US · Boeing 7372H5 · Emergency Lighting > INTERIOR AND EXTERIOR EMERGENCY LIGHTS AT FORWARD ENTRY AND FORWARD SERVICE DOORS DO NOT ILLUMINATE. FOUND ON RON SVC CHECK. REPLACED EMERGENCY LIGHT BATTERY AND POWER SUPPLY IAW B737 MM 33-50. OPERATIONAL CHECKS OK. REF: OPERATOR CONTROL NR 98ZZZX902. - [SDR 98ZZZM79](https://openairdocs.org/sdr/98ZZZM79.md): Light · damaged · Dec 10, 1997 · N220US · Boeing 7372H5 · Emergency Lighting > L2 DOOR EMERGENCY EXITLIGHT DAMAGED DURING REAR STAIR EXTENSION DURING TRAINING EXCERISE. UNIT WAS REPLACED WITH FLT COMPT EMERGENCY EXIT LIGHT, DUE PART NIS. FLT COMPT EMERGENCY EXIT LIGHT WAS MEL'D. AIRCRAFT RELEASED PER MEL 33-15 AND FLT COMPT. EMERGENC - [SDR 97ZZZM1069](https://openairdocs.org/sdr/97ZZZM1069.md): Tab Hinge · worn · Sep 11, 1997 · N220US · Boeing 7372H5 · Elevator Tab, Attach Fittings > VIBRATION FELT IN CONTROL YOKE AS WELL AS THROUGHOUT THE AIRCRAFT F/A'S STATE VIBRATION WAS MORE PROMINENT IN AFT OF AIRCRAFT, MORE PROMINENT ON RIGHT SIDE. INSPECTED AND FOUND INBOARD TAB BEARING BLOCK AND FWD HINGE BRACKET WORN, PER MM 27-31-31A. INSPECTED - [SDR 97ZZZX2605](https://openairdocs.org/sdr/97ZZZX2605.md): Power Supply · inoperative · May 7, 1997 · N220US · Boeing 7372H5 · Emergency Lighting > ON ROUTINE CHECK, OVERNIGHT INSPECTION, MAINTENANCE REPORTED AFT SERVICE DOOR EMERGENCY LIGHT INOPERABLE. REPLACED POWER SUPPLY. - [SDR 97ZZZM245](https://openairdocs.org/sdr/97ZZZM245.md): Skin · corrosion · Jan 27, 1997 · N220US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION VISUALLY AND BY NDT/HFEC FOUND CORRODED AREA MEASURING APPROX 15 INCHES BY 20 INCH LOCATED AT FUSELAGE BS 312, STRINGER 27R AND BEAR STRAP AND E-E CUTOUT. INSPECTION CARD NR J 2C-50-9012. INSTALLED TRIPLER, FILLER AND SKIN REPAIR AS PER EA N - [SDR 97ZZZM244](https://openairdocs.org/sdr/97ZZZM244.md): Stringer · corrosion · Jan 27, 1997 · N220US · Boeing 7372H5 · Fuselage Main, Longeron/Stringer > CLT - INSPECTION VISUALLY, FOUND CORROSION APPROXIMATELY 14 INCH BY 20 INCH LOCATED AT BS 344, STRINGER 27R-28R. INSPECTION CARD NR J2C-40-5325-1, SSID/SIP REF NR SSI F-9. REPLACED INTERNAL BEAM CHORD SECTION AT BS 351, RBL 15.47. INSTALLED DOUBLER, EXTERNA - [SDR 97ZZZM23](https://openairdocs.org/sdr/97ZZZM23.md): Connector · shorted · Dec 5, 1996 · N220US · Boeing 7372H5 · Fire Detection > NR 1 ENGINE FIRE WARNING CAME ON INTERMITTENTLY ON LANDING. FOUND DEFECTIVE CANNON PLUG, MANUFACTURERS PART NR 42839 KS 14S-5SX SHORTED. - [SDR 96ZZZX2793](https://openairdocs.org/sdr/96ZZZX2793.md): Skin · cracked · Apr 30, 1996 · N220US · Boeing 7372H5 · Fuselage Main, Plate/Skin > GSO - VISUAL INSPECTION FOUND.9 INCH CRACK IN OUTER SKIN AT FS 767, STR 19R DURING WALK-AROUND. INSTALLED DOUBLER USING BLIND FASTENERS (OM-7 32938), PER SRM 53-30-3, FIGURE 6. - [SDR 96ZZZX1405](https://openairdocs.org/sdr/96ZZZX1405.md): Skin · cracked · Jan 24, 1996 · N220US · Boeing 7372H5 · Fuselage Main, Plate/Skin > GSO - DURING SCHEDULED MAINTENANCE CHECK, VISUAL INSPECTION FOUND.625 INCH CRACK IN OUTER SKIN AT FS 271, STR 16L. INSTALLED EXTERNAL REPAIR PER SRM 53-30-3. (X) - [SDR USAA950013](https://openairdocs.org/sdr/USAA950013.md): Hyd Line · failed · Jan 8, 1995 · N220US · Boeing 7372H5 · Hydraulic System, Main > CLT - FLT 1243 - FLIGHT EN ROUTE PHL TO ATL WHEN 'A' SYSTEM HYDRAULIC QUANTITY INDICATED ZERO. FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED HYDRAULIC PRESSURE LINE ABOVE LEFT MAIN GEAR AND 'A' SYSTEM PRESSURE FILTER ## 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 = 'N220US' AND deregistration_id = 'N220US-2000-06-14' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N220US-2000-06-14/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.