# Service difficulty reports: N158US, cancelled Jun 20, 2002 A list on [N158US, cancelled Jun 20, 2002](https://openairdocs.org/deregistered/N158US-2002-06-20.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 0100571158](https://openairdocs.org/sdr/0100571158.md): Engine · leaking · Feb 16, 2001 · N158US · Doug DC1040 · Turbine Engine Oil System > DURING CLIMB AFTER TAKEOFF, THE CREW REPORTED SMOKE ENTERING THE CABIN FROM A PNEUMATIC SOURCE. THE FLIGHT RETURNED TO LAX AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THE NR 1 ENGINE TO BE LEAKING OIL AND CONTAMINATING THE - [SDR 0004391158](https://openairdocs.org/sdr/0004391158.md): Service difficulty · Dec 1, 2000 · N158US · Doug DC1040 · Landing Gear Position and Warning > AFTER TAKEOFF, FOUR GEAR UNSAFE LIGHTS ILLUMINATED WHEN GEAR SELECTED UP. FOLLOWED COM PROCEDURE. VERIFIED GEAR UP VISUALLY. RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND GEAR HANDLE INTERLOCK RELAY INOPERATIVE. REPLACED RELAY. OPERATIONAL CHECK OK. - [SDR 9903391158](https://openairdocs.org/sdr/9903391158.md): Power Lever · out of adjust · Aug 9, 1999 · N158US · Doug DC1040 · Power Lever > AFTER TOUCHDOWN WHEN REVERSE THRUST WAS APPLIED, THE NR 3 ENGINE DID NOT ACCELERATE. THE NR 2 ENGINE DEVELOPED MAXIMUM REVERSE THRUST WHILE THE NR 1 THRUST REVERSER WAS INOPERATIVE ON MEL. MAXIMUM BRAKING WAS APPLIED BUT THE AIRCRAFT DID NOT STOP UNTIL APPRO - [SDR 9900131158](https://openairdocs.org/sdr/9900131158.md): Light · smoking · Jan 11, 1999 · N158US · Doug DC1040 · Passenger Compartment Lighting > DURING APPROACH INTO BOS, FLIGHT ATTENDANT NOTICED SMOKE FROM CABIN LIGHT ABOVE SEAT 2H AND 2J. NOTIFIED COCKPIT AND SHUT LIGHTS OFF. SMOKE DISSIPATED. CAPTAIN DECLARED A PRECAUTIONARY EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED BALLAST ON LIGHT - [SDR 9710501158](https://openairdocs.org/sdr/9710501158.md): Prox Box · malfunctioned · May 25, 1997 · N158US · Doug DC1040 · Landing Gear Position and Warning > DURING TAKEOFF, GEAR VIBRATION WAS FELT UPON RETRACTION AND ALL UNSAFE GEAR LIGHTS REMAINED RED. RECYCLED GEAR AND OPERATION WAS NORMAL. MAINTENANCE REPLACED BOTH NOSE GEAR TIRES. RESET MAIN LANDING GEAR PROXIMITY BOX AND NO FAULTS WERE FOUND WITH GEAR INDI - [SDR 9710111158](https://openairdocs.org/sdr/9710111158.md): Compressor · stalled · May 21, 1997 · N158US · Doug DC1040 · Turbine Engine Compressor Section > AT 1,400 FEET DURING TAKEOFF, THE NR 2 ENGINE COMPRESSOR STALLED TWICE WITH EGT MOMENTARILY REACHING 900C ON BOTH OCCASIONS. NO OTHER ABNORMAL INDICATIONS. MAINTENANCE CONTROL RECOMMENDED DIVERSION TO BOS FOR MAINTENANCE. INSPECTION FOUND COMPRESSOR BLADE P - [SDR 9702791158](https://openairdocs.org/sdr/9702791158.md): Apu · failed · Feb 9, 1997 · N158US · Doug DC1040 · APU Core Engine > DURING BOARDING, THE APU FAILED, FIRE BOTTLES WERE FIRED AND CABIN FILLED WITH SMOKE. REPLACED APU, WATER SEPARATOR BAGS AND PURGED PACKS. - [SDR 9701501158](https://openairdocs.org/sdr/9701501158.md): Pressure Switch · failed · Jan 27, 1997 · N158US · Doug DC1040 · Pneumatic Indicating System > DURING TAKEOFF, THE NR 3 MANIFOLD FAIL LIGHT ILLUMINATED. DUMPED 76,500 LBS OF FUEL AND RETURNED TO IAD. REPLACED THE MANIFOLD PRESSURE SWITCH. - [SDR 9624011158](https://openairdocs.org/sdr/9624011158.md): Compressor · stalled · Nov 10, 1996 · N158US · Doug DC1040 · Turbine Engine Compressor Section > AT FL310 WHEN POWER WAS REDUCTED FOR DESCENT, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. THERE WAS A SUBSEQUENT VIBRATION UNTIL THE ENGINE WAS SHUT DOWN. NO ABNORMAL EGT OR FUEL FLOW INDICATION AT THE TIME OF INCIDENT. FLIGHT CONTINUED TO DTW WITHOUT F - [SDR 9617151158](https://openairdocs.org/sdr/9617151158.md): Engine · overtemp · Aug 7, 1996 · N158US · Doug DC1040 · Engine (Turbine/Turboprop) > DURING LANDING ROLLOUT, THE NR 1 ENGINE EGT WENT ABOVE RED LIMIT LINE FOR ABOUT THREE SECONDS. THE ENGINE WAS THEN SHUTDOWN WHILE STILL IN REVERSE AND A/C TAXIED TO GATE WITHOUT FURTHER INCIDENT. PERFORMED ENGINE OVER TEMPERATURE INSPECTION AND NO DISCREPANC - [SDR 9615891158](https://openairdocs.org/sdr/9615891158.md): Skin · cracked · Jul 11, 1996 · N158US · Doug DC1040 · Wing, Plate/Skin > DURING L-CHECK, FOUND A CRACK IN THE RIGHT WING FIXED LEADING EDGE SKIN AT XOS 610. REPAIRED SKIN (P/N ARB2887-502) PER EA 11-105354. - [SDR 9615881158](https://openairdocs.org/sdr/9615881158.md): Skin · cracked · Jul 11, 1996 · N158US · Doug DC1040 · Wing, Plate/Skin > DURING L-CHECK, FOUND A CRACK IN THE LEFT WING FIXED LEADING EDGE SKIN AT XOS 610. REPAIRED SKIN (P/N ARB2887-501) PER EA 11-105353. - [SDR 9609471158](https://openairdocs.org/sdr/9609471158.md): Fuel Control · malfunctioned · Apr 30, 1996 · N158US · Doug DC1040 · Fuel Control/Turbine Engines > WHILE WAITING FOR TAKEOFF, THE NR 1 ENGINE COMPRESSOR STALL OCCURRED AT ENGINE IDLE POWER. EGT TEMPERATURE REACHED 700 CELSIUS AND THE NR 1 ENGINE WAS SHUTDOWN. AIRCRAFT RETURNED TO THE GATE. GROUND MAINTENANCE REPLACED THE ENGINE VANE CONTROL, PERFORMED EN - [SDR 9600451158](https://openairdocs.org/sdr/9600451158.md): Power Supply · failed · Jan 2, 1996 · N158US · Doug DC1040 · Emergency Lighting > DURING LINE CHECK, FOUND THE AFT EMERGENCY LIGHT POWER SUPPLY FAILED BITE TEST. REPLACED THE AFT POWER SUPPLY AND BATTERY PACK. - [SDR 9520631158](https://openairdocs.org/sdr/9520631158.md): Pneu Manifold · failed · Dec 18, 1995 · N158US · Doug DC1040 · Pneumatic Distribution System > DURING CLIMB, THE NR 2 PNEUMATIC MANIFOLD FAIL LIGHT ILLUMINATED INTERMITTENTLY. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. ITEM ENTERED IN MINIMUM EQUIPMENT LIST AND AIRCRAFT APPROVED FOR SERVICE. - [SDR 9519761158](https://openairdocs.org/sdr/9519761158.md): Pt2 Probe · cracked · Dec 2, 1995 · N158US · Doug DC1040 · Fuel Controlling System > DURING START OF DESCENT, THE NR 2 ENGINE EGT WENT TO 1010 DEGREES FOR 90 SECONDS. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT CONTINUED TO AN UNEVENTFUL TWO-ENGINE LANDING AT MSP. THE PRBC AND EVC WERE REPLACED AND A PT2 PROBE WAS FOUND CRACKED AND REPLACED. - [SDR 9507661158](https://openairdocs.org/sdr/9507661158.md): Pan · corroded · May 7, 1995 · N158US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT LAV SERVICE PAN INNER SURFACE FS 1980. REPAIRED PAN PER EA 11-98056. MFG PART NUMBER AGA3098-501. - [SDR 9508241158](https://openairdocs.org/sdr/9508241158.md): Bulkhead · corroded · May 4, 1995 · N158US · Doug DC1040 · Fuselage Main, Bulkhead > DURING PERIODIC CHECK, FOUND CORROSION ON THE CENTER ACCESS PRESSURE BULKHEAD FS 1156 AT LONGERON 43R. REPAIRED PER EA 11-98042. - [SDR 9507741158](https://openairdocs.org/sdr/9507741158.md): Skin · corroded · May 4, 1995 · N158US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT LAV SERVICE PAN AND SKIN DOUBLER AT FS 1980 - 1986, L50L TO L50R. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER EA 11-98047 AND 11-98056. MFG PART NUMBER: AGA3098-501. - [SDR 9507641158](https://openairdocs.org/sdr/9507641158.md): Web · corroded · May 2, 1995 · N158US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, FOUND CORROSION ON FLOOR WEB AND DOUBLER FS 1900 TO 1928, LBL 107. REPAIRED PER EA 11-98053. MFG PART NUMBER AGA3807-5. - [SDR 9507621158](https://openairdocs.org/sdr/9507621158.md): Frame · cracked · May 1, 1995 · N158US · Doug DC1040 · Fuselage Main, Frame > DURING PERIODIC CHECK, FOUND CRACK IN THE FORWARD CARGO FLOOR FRAME FLANGE FS 879, LBL 38. REPAIRED PER EA 11-98027. MFG PART NUMBER ADA7034-3. - [SDR 9507611158](https://openairdocs.org/sdr/9507611158.md): Seat Track · corroded · Apr 28, 1995 · N158US · Doug DC1040 · Fuselage, Seat/Cargo Attach Fittings > DURING PERIODIC CHECK, FOUND CORROSION ON SEAT TRACK LBL 107, FS 1521. REPAIRED PER EA 11-98049. - [SDR 9506731158](https://openairdocs.org/sdr/9506731158.md): Support · corroded · Apr 27, 1995 · N158US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE FLOOR SUPPORT AT FS 459, LBL 6 TO RBL 56. REPLACED FLOOR SUPPORT. - [SDR 9506721158](https://openairdocs.org/sdr/9506721158.md): Seat Track · corroded · Apr 27, 1995 · N158US · Doug DC1040 · Fuselage, Seat/Cargo Attach Fittings > DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 1311 - 1399, LBL 107. REMOVED CORROSION AND REPAIRED SEAT TRACK. - [SDR 9506711158](https://openairdocs.org/sdr/9506711158.md): Support · corroded · Apr 27, 1995 · N158US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE FLOOR SUPPORT AT FS 440, RBL 2 - 6. REPLACED THE FLOOR SUPPORT. - [SDR 9507761158](https://openairdocs.org/sdr/9507761158.md): Fasteners · broken · Apr 26, 1995 · N158US · Doug DC1040 · Nacelle/Pylon Structure > DURING PERIODIC CHECK, FOUND BROKEN FASTENERS COMMON TO THE NR 4 BANJO FITTING AFT FLANGE AND THE PYLON CARRY THROUGH CAP. INSTALLED BUSHINGS AND REPAIRED CHANNELS PER EA 11-098170. MFG PART NUMBER AJC7054-1. - [SDR 9506671158](https://openairdocs.org/sdr/9506671158.md): Seat Track · corroded · Apr 26, 1995 · N158US · Doug DC1040 · Fuselage, Seat/Cargo Attach Fittings > DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 1476 - 1510, LBL 107. REMOVED CORROSION AND INSTALLED REPAIR. - [SDR 9506441158](https://openairdocs.org/sdr/9506441158.md): Seat Track · corroded · Apr 24, 1995 · N158US · Doug DC1040 · Fuselage, Seat/Cargo Attach Fittings > DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 440 - 485, RBL 9. REPLACED SEAT TRACK. - [SDR 9506431158](https://openairdocs.org/sdr/9506431158.md): R3 Door · cracked · Apr 24, 1995 · N158US · Doug DC1040 · Emergency Exits > DURING PERIODIC CHECK, CRACKS WERE FOUND IN THE FORWARD AND AFT LOWER DOOR 3R STRUCTURE AT FS 1260 AND 1305. STOP DRILLED AND INSTALLED DOUBLER. - [SDR 9506391158](https://openairdocs.org/sdr/9506391158.md): L3 Door · cracked · Apr 21, 1995 · N158US · Doug DC1040 · Emergency Exits > DURING PERIODIC CHECK, A CRACK WAS FOUND ON THE DOOR 3L AFT LOWER LIGHTENING HOLE AT FS 1305. STOP DRILLED CRACK AND INSTALLED DOUBLER. - [SDR 9506291158](https://openairdocs.org/sdr/9506291158.md): Skin · damaged · Apr 20, 1995 · N158US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING PERIODIC CHECK, FUSELAGE SKIN WAS FOUND DENTED AND GOUGED AT FS 1801, STR 2L TO 4L. REMOVED DAMAGED AREA AND INSTALLED DOUBLERS. - [SDR 9507751158](https://openairdocs.org/sdr/9507751158.md): Frame · cracked · Apr 4, 1995 · N158US · Doug DC1040 · Fuselage Main, Frame > DURING PERIODIC CHECK, FOUND A CRACK IN THE FORWARD CARGO FLOOR FRAME AT FS 879, LBL 38. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER EA 11-98027. MFG PART NUMBER: ADA7034-3. ## 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 = 'N158US' AND deregistration_id = 'N158US-2002-06-20' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N158US-2002-06-20/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.