# Service difficulty reports: N162US, cancelled Sep 4, 2002 A list on [N162US, cancelled Sep 4, 2002](https://openairdocs.org/deregistered/N162US-2002-09-04.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 0202021162](https://openairdocs.org/sdr/0202021162.md): Landing Gear · malfunctioned · Jun 11, 2002 · N162US · Doug DC1040 · Main Landing Gear > ON TAKEOFF UPON GEAR RETRACTION, THE LEFT MAIN GEAR RED LIGHT REMAINED ON. PROCEEDED WITH COCKPIT OPERATING MANUAL PROCEDURE. VISUALLY CHECKED GEAR WHICH APPEARED DOWN. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN - [SDR 0101111162](https://openairdocs.org/sdr/0101111162.md): Accelerometer · failed · Mar 23, 2001 · N162US · Doug DC1040 · Auto Throttle System > WITH NR 1 AUTOPILOT IN COMMAND AND IAS HOLD ENGAGED AT FL 250, AIRCRAFT BEGAN A RAPID DESCENT AND NR 1 AUTOPILOT DISCONNECTED. AIRCRAFT LEVELED OFF AT FL 237 AND FLIGHT CONTINUED WITH MANUAL CONTROL. FLIGHT LANDED AT MCO WITHOUT INCIDENT. REPLACED ACCELEROM - [SDR 0000791162](https://openairdocs.org/sdr/0000791162.md): Fcu · malfunctioned · Mar 1, 2000 · N162US · Doug DC1040 · Fuel Control/Turbine Engines > WHILE DESCENDING AT FL290, THE NR 2 ENGINE FLAMED OUT. THE ENGINE OUT CHECKLIST WAS COMPLETED AND THE ENGINE WAS RESTARTED. OPERATION FOR THE REMAINDER OF THE FLIGHT WAS NORMAL MAINTENANCE PERFORMED A BOROSCOPE INSPECTION WITH NO TROUBLE FOUND. THE FUEL CON - [SDR 9904491162](https://openairdocs.org/sdr/9904491162.md): Rib · cracked · Sep 14, 1999 · N162US · Doug DC1040 · Wing Spar > DURING M-CHECK, FOUND CRACK IN RIGHT WING LEADING EDGE RIB AT WS XW344 RIGHT. REPAIRED PER EA 11-167483. - [SDR 9904191162](https://openairdocs.org/sdr/9904191162.md): Jamb · corroded · Sep 13, 1999 · N162US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING M CHECK, FOUND CORROSION ON CENTER CARGO DOOR JAMB RAIL AND FRAME OUTER CAP BETWEEN FS 1701 - 1708. REPAIRED PER EA 11-170067. - [SDR 9904481162](https://openairdocs.org/sdr/9904481162.md): Angle · corroded · Sep 7, 1999 · N162US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING M-CHECK, FOUND CORROSION ON T ANGLE FROM FS 1741 TO 1746 BETWEEN LONGERON 42L AND 43L. REPAIRED PER EA 11-170503. - [SDR 9904211162](https://openairdocs.org/sdr/9904211162.md): Fitting · cracked · Sep 2, 1999 · N162US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING M CHECK, FOUND CRACK ON NR 1 RIGHT DOOR FITTING AT FS 420, LONGERON 27R. REPAIRED PER EA 11-170063. - [SDR 9904201162](https://openairdocs.org/sdr/9904201162.md): Beam · cracked · Sep 1, 1999 · N162US · Doug DC1040 · Fuselage Main, Floor Beam > DURING M CHECK, FOUND CRACK ON FLOORBEAM AT FS 879, RBL 30. REPAIRED PER EA 11-167477. - [SDR 9903401162](https://openairdocs.org/sdr/9903401162.md): Web · cracked · Aug 26, 1999 · N162US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING M-CHECK, FOUND CRACK IN RIGHT NOSE WHEEL WEB AT FS 475 9 INCHES BELOW UPPER PRESSURE DECK. REPAIRED PER EA 11-170427. - [SDR 9903911162](https://openairdocs.org/sdr/9903911162.md): Floorbeam · cracked · Aug 23, 1999 · N162US · Doug DC1040 · Fuselage Main, Floor Beam > DURING M-CHECK, FOUND CRACK IN FLOORBEAM AT FS 1099, LBL 58. REPAIRED PER EA 11-106300. - [SDR 9903131162](https://openairdocs.org/sdr/9903131162.md): Dnlock Sensor · failed · Aug 6, 1999 · N162US · Doug DC1040 · Landing Gear Position and Warning > ON DESCENT INTO SFO, UPON GEAR EXTENSION, GOT RMG UNSAFE INDICATION. RECYCLED GEAR AND STILL INDICATED UNSAFE. VISUAL CHECK OF GEAR SHOWED DOWN. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED GEAR DOWNLOCK SENSOR. OPERATION CHECKS GOOD. - [SDR 9902351162](https://openairdocs.org/sdr/9902351162.md): Line · leaking · Jun 16, 1999 · N162US · Doug DC1040 · Alternator-Generator Drive > EN ROUTE TO HNL FROM SEA, NR 2 CSD OIL PRESSURE LOW LIGHT ILLUMINATED, NR 3 CSD ON MEL. FLIGHT RETURNED TO SEA AND LANDED WITHOUT INCIDENT. FOUND CSD LINE LEAKING. REPAIRED FILL LINE. OPERATIONAL CHECK OK. - [SDR 9810531162](https://openairdocs.org/sdr/9810531162.md): Battery Pack · discharged · Nov 27, 1998 · N162US · Doug DC1040 · Emergency Lighting > DURING LINE CHECK, LEFT AND RIGHT AISLE ESCAPE PATH LIGHTS OUT FROM ROW 22 TO 27. REPLACED BATTERY PACK AND CHARGER, OPERATIONAL CHECK OK. - [SDR 9809601162](https://openairdocs.org/sdr/9809601162.md): Proximity Box · failed · Jun 19, 1998 · N162US · Doug DC1040 · Landing Gear Position and Warning > RECEIVED NOSE GEAR UNSAFE INDICATION WHEN GEAR EXTENDED FOR LANDING. RECYCLED GEAR AND FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE. VISUALLY CONFIRMED GEAR DOWN. FLIGHT LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SWITCH ELECTRONIC BOX. FOUND NOSE GEAR DOW - [SDR 9808621162](https://openairdocs.org/sdr/9808621162.md): Compressor · stalled · May 6, 1998 · N162US · Doug DC1040 · Turbine Engine Compressor Section > DURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 3 ENGINE COMPRESSOR STALLED. THE EGT ROSE TO 880C BEFORE THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE PER TAFI STALL PROCEDURE WITH NO TROUBLE FOUND. RABS CHECK WAS NOT ACCOMPLISHED AND TH - [SDR 9806901162](https://openairdocs.org/sdr/9806901162.md): Compressor · stalled · Apr 17, 1998 · N162US · Doug DC1040 · Turbine Engine Compressor Section > DURING LANDING ROLLOUT WHILE COMING OUT OF REVERSE THRUST AT 80 KTS, THE NR 3 ENGINE COMPRESSOR STALLED. EGT PEAKED AT 1000C BEFORE THE ENGINE WAS SHUT DOWN AND THE COM COMPLIED WITH. MAINTENANCE INSPECTED THE ENGINE PER MAINTENANCE MANUAL INCLUDING A BORESC - [SDR 9806321162](https://openairdocs.org/sdr/9806321162.md): Frame · corroded · Mar 29, 1998 · N162US · Doug DC1040 · Fuselage Main, Frame > DURING L-CHECK, FOUND CORROSION ON ANGLE AT FORWARD CARGO DOOR LOWER AFT JAMB FS 1009, RBL 75. REPAIRED PER EA 11-156221. - [SDR 9806311162](https://openairdocs.org/sdr/9806311162.md): Frame · cracked · Mar 14, 1998 · N162US · Doug DC1040 · Fuselage Main, Frame > DURING L-CHECK, FOUND CRACK IN LOWER NOSE FUSELAGE FRAME LEFT SIDE, FS 459, LBL 61. REPAIRED PER EA 11-155558. - [SDR 9806301162](https://openairdocs.org/sdr/9806301162.md): Frame · cracked · Mar 14, 1998 · N162US · Doug DC1040 · Fuselage Main, Frame > DURING L-CHECK, FOUND CRACK IN LOWER NOSE FUSELAGE FRAME RIGHT SIDE, FS 459, RBL 61. REPAIRED PER EA 11-155559. - [SDR 9724101162](https://openairdocs.org/sdr/9724101162.md): Duct Seal · failed · Dec 20, 1997 · N162US · Doug DC1040 · Pneumatic Distribution System > DURING APU START WHILE PARKED AT GATE, APU FIRE WARNING ANNUNCIATED. APU FIRE BOTTLE WAS DISCHARGED. MAINTENANCE INSPECTED APU AND FOUND NO EVIDENCE OF FIRE. FIRE BOTTLE WAS REPLACED. SURGE VALVE DUCT SEAL WAS FOUND RUPTURED AND WAS REPLACED. - [SDR 9706061162](https://openairdocs.org/sdr/9706061162.md): Prox Control · failed · Mar 19, 1997 · N162US · Doug DC1040 · Landing Gear Position and Warning > DURING LANDING, FOUR RED GEAR LIGHTS ILLUMINATED. RECYCLED GEAR, THE FOUR GREEN LIGHTS ILLUMINATED. MAINTENANCE REPLACED THE MAIN LANDING GEAR PROXIMITY CONTROL. - [SDR 9627401162](https://openairdocs.org/sdr/9627401162.md): Epr Indicator · malfunctioned · Dec 30, 1996 · N162US · Doug DC1040 · Engine Pressure Ratio (EPR) > DURING TAKEOFF, THE NR 3 ENGINE EPR INDICATION WAS LOW. TAKEOFF WAS ABORTED. MAINTENANCE REPLACED THE EPR INDICATOR. ENGINE GROUND RUN CHECKED GOOD. - [SDR 9619601162](https://openairdocs.org/sdr/9619601162.md): Longeron · corroded · Aug 31, 1996 · N162US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING T-CHECK, FOUND CORROSION ON THE FUSELAGE OVERWING EXTERNAL LONGERONS 30L, 32L, 37L, AND 32R FROM FS 1407 - FS 1548. REPAIRED LONGERONS PER EA 11-110189. - [SDR 9619241162](https://openairdocs.org/sdr/9619241162.md): Skin · cracked · Aug 30, 1996 · N162US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING T-CHECK, FOUND A CRACK IN THE NR 3 AIR CONDITIONING PACK CUTOUT SKIN UPPER AFT CORNER FS 535. REPAIRED SKIN (P/N ACA 3108-501) PER EA 11-110184. - [SDR 9619231162](https://openairdocs.org/sdr/9619231162.md): Support · cracked · Aug 29, 1996 · N162US · Doug DC1040 · Trailing Edge Flaps > DURING T-CHECK, FOUND A CRACK IN THE LEFT FLAP INBOARD FLAP SUPPORT BASE PLATE AT STA 1521. REPAIRED PLATE (P/N ANB 7170) PER EA 11-110179. - [SDR 9619121162](https://openairdocs.org/sdr/9619121162.md): Floor Beam · cracked · Aug 29, 1996 · N162US · Doug DC1040 · Fuselage Main, Floor Beam > DURING T-CHECK, FOUND A CRACK IN THE FS 1099 FORWARD CARGO FLOOR BEAM AT LBL 60. REPAIRED BEAM (P/N ADA 0039-5) PER EA 11-106300. - [SDR 9619581162](https://openairdocs.org/sdr/9619581162.md): Frame · cracked · Aug 28, 1996 · N162US · Doug DC1040 · Fuselage Main, Frame > DURING T-CHECK, FOUND A.75 INCH CRACK IN THE LEFT FORWARD ACCESSORY COMPARTMENT DOOR JAMB FS 547 FRAME INBOARD CHORD. REPAIRED FRAME (P/N ACA 0051-3) PER EA 11-106313. - [SDR 9619571162](https://openairdocs.org/sdr/9619571162.md): Door Jamb · cracked · Aug 28, 1996 · N162US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND A CRACK IN THE NR 3R DOOR JAMB WEB, LOWER FORWARD CORNER. REPAIRED WEB (P/N AEA 0115-2) PER EA 11-105144. - [SDR 9619211162](https://openairdocs.org/sdr/9619211162.md): Web · cracked · Aug 28, 1996 · N162US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND THREE CRACKS IN DOOR 3L LOWER FORWARD SIDE WEB. REPAIRED WEB (P/N AEA 0115-1) PER EA 11-106311. - [SDR 9618711162](https://openairdocs.org/sdr/9618711162.md): Longeron · corroded · Aug 24, 1996 · N162US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING T-CHECK, FOUND CORROSION ON LONGERON 52 AT FS 1781. REPAIRED LONGERON (P/N AGA7045) PER EA 11-106299. - [SDR 9618701162](https://openairdocs.org/sdr/9618701162.md): Fitting · corroded · Aug 23, 1996 · N162US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND CORROSION ON THE LONGERON 51R END FITTING AT FS 1521 - 1531. REPLACED FITTING. - [SDR 9615111162](https://openairdocs.org/sdr/9615111162.md): Transmitter · leaking · Jul 13, 1996 · N162US · Doug DC1040 · Hydraulic Quantity Sensor > DURING CLIMB, THE NR 2 HYDRAULIC SYSTEM SHOWED A SLOW LEAK. RETURNED TO HNL, DUMPED 38,000 LBS OF FUEL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 PRESSURE TRANSMITTER. - [SDR 9603941162](https://openairdocs.org/sdr/9603941162.md): Seal · leaking · Feb 14, 1996 · N162US · Doug DC1040 · Turbine Engine Oil System > DURING DESCENT, THE NR 2 ENGINE WAS SHUTDOWN DUE TO OIL PRESSURE DROPPING BELOW 35 PSI AND OIL QUANTITY DROPPING TO 1 GALLON. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND CONTINUED FLIGHT TO HNL WITHOUT FURTHER INCIDENT. REPLACED THE RIGHT GARLOCK SEAL THAT - [SDR 9601751162](https://openairdocs.org/sdr/9601751162.md): Gear Box · leaking · Jan 22, 1996 · N162US · Doug DC1040 · Turbine Engine Accessory Drive > AFTER TAKEOFF, THE NR 2 ENGINE OIL DECREASED RAPIDLY. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND RETURNED TO MSP. REPLACED STARTER DRIVE SEAL, BOTH HYDRAULIC PUMP DRIVE SEALS, GEAR BOX, AND BREATHER VALVE. PERFORMED LEAK CHECK. ENGINE RUN-UP WAS NORMAL. - [SDR 9502641162](https://openairdocs.org/sdr/9502641162.md): Floor Beam · cracked · Jan 20, 1995 · N162US · Doug DC1040 · Fuselage Main, Floor Beam > DURING PERIODIC CHECK, A CRACK WAS FOUND ON THE CENTER CARGO FLOOR BEAM AT FS 1701, RBL 33. REMOVED DAMAGE AND INSTALLED DOUBLERS PER EA 11-93754. - [SDR 9503191162](https://openairdocs.org/sdr/9503191162.md): Skin · damaged · Jan 19, 1995 · N162US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING PERIODIC CHECK, DAMAGE WAS FOUND ON THE LEFT FUSELAGE NOSE SKIN AT FS 275 - 343, Z-2.90 TO Z-20.15. INSTALLED REPAIR DOUBLERS PER EA 11-96599. - [SDR 9500561162](https://openairdocs.org/sdr/9500561162.md): Floor Support · corroded · Jan 11, 1995 · N162US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE AFT GALLEY FLOOR SUPPORT AT FS 1970 - 1978, LBL 27. REPAIRED PER EA 11-96399. - [SDR 9500551162](https://openairdocs.org/sdr/9500551162.md): Support · corroded · Jan 11, 1995 · N162US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE GALLEY SUPPORT AT FS 1947 - 1969. LBL 55. REPAIRED PER EA 11-96398. - [SDR 9502411162](https://openairdocs.org/sdr/9502411162.md): Support · corroded · Jan 9, 1995 · N162US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE UPPER SIDE OF THE LEFT OUTBOARD AFT GALLEY SUPPORT. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER EA 11-96398. ## 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 = 'N162US' AND deregistration_id = 'N162US-2002-09-04' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N162US-2002-09-04/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.