# Service difficulty reports: N162AT, cancelled Jan 12, 2016 A list on [N162AT, cancelled Jan 12, 2016](https://openairdocs.org/deregistered/N162AT-2016-01-12.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 73 reports - [SDR AMTA200800031](https://openairdocs.org/sdr/AMTA200800031.md): Charger · inoperative · Jan 23, 2008 · N162AT · Lkheed 10113853 · Emergency Lighting > EMERGENCY POWERPACK AT R2 DOOR, INOPERATIVE. REPLACED EMERGENCY POWERPACK WITH SERVICEABLE UNIT. OPS CHECKS GOOD REF AMM 33-51-03. (K) - [SDR AMTA200800010](https://openairdocs.org/sdr/AMTA200800010.md): Wire · shorted · Jan 7, 2008 · N162AT · Lkheed 10113853 · Light System Wiring > EMERGENCY LIGHT PATHWAY LIGHT AT FWD GALLEY AND RT FWD CABIN INOPERATIVE. DRIED OUT WET WIRES AND PLUGS BY A2 LAVATORY. OPS CHECK GOOD. (K) - [SDR AMTA200700506](https://openairdocs.org/sdr/AMTA200700506.md): Computer · unserviceable · Oct 15, 2007 · N162AT · Lkheed 10113853 · Rudder Control System > RUDDER HYDR LIMITER ANNUNCIATION LIGHT ON. RUDDER LIMITER PANEL HYDR PUSH LT OFF. REMOVED AND REPLACED NR 2, CADC IAW MM 34-14-01, OPS CHECK GOOD. (K) - [SDR AMTA200700478](https://openairdocs.org/sdr/AMTA200700478.md): Unknown · unknown · Oct 4, 2007 · N162AT · Lkheed 10113853 · Standard Practices/Structures > REJECTED T/O, SPEED 70 KTS, WEIGHT 380.0 LBS. PERFORMED CLAPPER LUB IAW MM 72-31-05. INSPECTED MASTER GB CHIP DETECTOR, NO DEBRIS DETECTED. NO EVIDENCE OF ENG FAILURE. NR 3 ENG. (K) - [SDR AMTA200700248](https://openairdocs.org/sdr/AMTA200700248.md): Connector · contaminated · May 24, 2007 · N162AT · Lkheed 1011* · Light System Wiring > FWD GALLEY AND FIRST SECTION OF ESCAPE PATH LIGHTING RT SIDE INOPERATIVE. SYS WAS SHORTED BY WATER. DRIED CONNECTORS AND INSULATED THEM. OPS CHECK NORMAL. (K) - [SDR AMTA200700126](https://openairdocs.org/sdr/AMTA200700126.md): Light · inoperative · Mar 1, 2007 · N162AT · Lkheed 10113853 · Emergency Lighting > AFT GALLEY EGRESS STRIP INOPERATIVE. REMOVED AND REPLACED AFT GALLEY EGRESS STRIP OPS CHECKS NORMAL. (K) - [SDR AMTA200700037](https://openairdocs.org/sdr/AMTA200700037.md): Beam · cracked · Jan 25, 2007 · N162AT · Lkheed 10113853 · Wing Main, Frame Structure > RIGHT WING TE BAT STRUCTURE AREA UPPER LATERAL BEAM FOUND CRACKED AT TWO LOCATIONS, ONE CRACK 2 INCHES AND ONE CRACK.5 INCHES. RIGHT WING TE BAT STRUCTURE CAP REPLACED PER L1011 SRM 51-10-01 AND 51-40-01. (M) 10-17-07 CARRIED OUT PAINT TOUCH UP, UPPER - [SDR AMTA200700036](https://openairdocs.org/sdr/AMTA200700036.md): Structure · cracked · Jan 25, 2007 · N162AT · Lkheed 10113853 · Landing Gear Doors > NOSE LANDING GEAR RT DOOR FOUND CRACKED ON UPPER EDGE BETWEEN MID AND AFT HINGE. NLG RT FWD DOOR REMOVED, ROUTED TO SHOP IAW AMM 32-22-01. NLG DOOR CRACK BEYOND REPAIRABLE LIMITS IAW SRM 52-82-00 AND EER NR 13225. INST NEW DOOR IAW AMM 32-22-01. NOSE GEAR - [SDR AMTA200700035](https://openairdocs.org/sdr/AMTA200700035.md): Bushing · migrated · Jan 25, 2007 · N162AT · Lkheed 10113853 · Fuselage, Landing Gear Attach Fittings > RT MAIN LANDING GEAR TRUNNION FITTING FORWARD AND AFT LANDING GEAR ATTACHING LUG BUSHINGS FOUND MIGRATED AT IWS 346. REPAIRED IAW EER 13226 WO 319386. REMOVED GEAR AMM 32-11-02, BUSHINGS REMOVED FWD AND AFT LUG AMM 20-71-10, CORROSION REWORK SRM 51-21-01, NDT - [SDR AMTA200700020](https://openairdocs.org/sdr/AMTA200700020.md): Support Angle · cracked · Jan 21, 2007 · N162AT · Lkheed 10113853 · Fuselage Miscellaneous Structure > CENTER SECTION LOWER AREA SUPPORT ATTACHMENT ANGLE FOUND CRACKED AT FS 1212, LBL 42.5. REPAIR CARRIED OUT ON CRACKED SUPPORT ANGLE AT FS 1212, LBL 42.5 CENTER SECTION AREA IAW L1011 SRM 51-50-04. PAINT TOUCH-UP AS IAW AMM 20-51-08. (M) - [SDR AMTA200600706](https://openairdocs.org/sdr/AMTA200600706.md): Feeder Cable · broken · Dec 6, 2006 · N162AT · Lkheed 10113853 · Emergency Lighting > THE FORWARD RIGHT SECTION OF EGRESS FLOOR PATH LIGHTING IS INOPERATIVE. FOUND 1 LIGHT STRIP NOT WORKING AND TRACK CABLE ASSEMBLY BROKEN. REPLACED LIGHT STRIP AND CABLE ASSEMBLY. OPS CHECK GOOD PER MM 33-51-00. (M) - [SDR AMTA200600690](https://openairdocs.org/sdr/AMTA200600690.md): Light · inoperative · Nov 29, 2006 · N162AT · Lkheed 10113853 · Emergency Lighting > EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT FWD GALLEY. REMOVED AND REPLACED FWD GALLEY LIGHT STRIP, OPS CHECK NORMAL IAW MM. (K) - [SDR AMTA200600335](https://openairdocs.org/sdr/AMTA200600335.md): Light · inoperative · May 15, 2006 · N162AT · Lkheed 10113853 · Emergency Lighting > EGRESS LTS AT FWD GALLEY AND ROW 5 HJK INOPERATIVE. REPLACED FWD GALLEY LIGHT STRIP. OPS CHECK GOOD. MM REF 33. (K) - [SDR AMTA200600303](https://openairdocs.org/sdr/AMTA200600303.md): Fixture · inoperative · May 1, 2006 · N162AT · Lkheed 10113853 · Emergency Lighting > EGRESS TRACK IN FRONT OF FWD GALLEY INOPERATIVE. REMOVED AND REPLACED EGRESS TRACK IN FRONT OF FWD GALLEY. OPS CHECK GOOD. (K) - [SDR AMTA200600235](https://openairdocs.org/sdr/AMTA200600235.md): Flap · cracked · Mar 31, 2006 · N162AT · Lkheed 10113853 · Trailing Edge Flaps > AN EXISTING REPAIR ON THE L/E OF THE NR 3 LT FLAP OB FOUND TO BE CRACKED ADJACENT TO THE INSERT REPAIR. CRACK IS 1 INCH IN LENGTH AND STARTS AT THE LOWER EDGE OF REPAIR COUTOUT GOING DOWNWARD. CARRIED OUT PERMANENT REPAIR IAW SRM USING SOLID FASTENERS. PREV - [SDR AMTA200600147](https://openairdocs.org/sdr/AMTA200600147.md): Flap · gouged · Feb 28, 2006 · N162AT · Lkheed 10113853 · Trailing Edge Flaps > DEEP GOUGE MARKS WERE FOUND ON LT FLAP NR 3 IB RIB ASSY. REPAIRED IAW RS L57-50-34. (K) - [SDR AMTA200600146](https://openairdocs.org/sdr/AMTA200600146.md): Skin · gouged · Feb 28, 2006 · N162AT · Lkheed 10113853 · Elevator, Plate/Skin > LT ELEVATOR IB TOP SKIN NEAR LEADING EDGE HAS GOUGES LOCATED JUST AFT OF FWD SPAR SKIN ATTACHMENT AND BETWEEN RIB ATTACHMENT AT ES 113.350 AND 140.349. DAMAGE REPAIRED IAW RS L55-20-7. (K) - [SDR AMTA200600123](https://openairdocs.org/sdr/AMTA200600123.md): Structure · cracked · Feb 9, 2006 · N162AT · Lkheed 10113853 · Service Doors > BOLT HOLE EDDY CURRENT INSPECTION ON L2 DOOR UPPER FORWARD CORNER DETECTED FOUR CRACKS. L2 DOOR UPPER FORWARD CORNER CRACK DETECTED, UNABLE TO STOP DRILL. NO REWORK REQUIRED IAW EER L1-53-00-00-11419. L2 DOOR REPAIR KIT INSTALLED, REFER TO ATA EO L19-53AD-0 - [SDR AMTA200600107](https://openairdocs.org/sdr/AMTA200600107.md): Intercostal · corroded · Feb 2, 2006 · N162AT · Lkheed 10113853 · Fuselage Miscellaneous Structure > CABIN FLOORBOARD SUPPORT INTERCOSTAL FOUND WITH CORROSION BETWEEN FS 313-328 AT APPROX RBL 64. CLEANED AND BLENDED AREA AND FOUND BEYOND NEGLIGIBLE DAMAGE LIMITS IAW SRM 51-21-01 AND 51-50-02 FIG 1. DAMAGE AREA REMOVED AND REPAIRED IAW SRM 51-50-02 FIG 2. P - [SDR AMTA200600113](https://openairdocs.org/sdr/AMTA200600113.md): Inlet · corroded · Feb 1, 2006 · N162AT · Lkheed 10113853 · Fuselage Main, Structure > NR 2 RAM AIR INLET HAS SURFACE CORROSION AT SEVERAL PLACES. CORROSION AT THE NR 2 RAM AIR INLET WAS BLENDED OUT AND FOUND WITHIN LIMITS IAW SRM 51-50-02 FIG 01. REPROTECTED BLEND AREA IAW SRM 51-21-02. (M) - [SDR AMTA200600118](https://openairdocs.org/sdr/AMTA200600118.md): Scoop · corroded · Feb 1, 2006 · N162AT · Lkheed 10113853 · Fuselage Main, Structure > NR 1 RAM AIR INLET SCOOP, INTERNAL AREA HAS SURFACE CORROSION. CLEANED UP CORROSION ON THE RAM AIR LEADING EDGE SCOOP DOUBLER AND FOUND BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 51-50-01 FIG 1. REPLACED LEADING EDGE PART 1565850-146 IAW 51-40-01. (M) - [SDR AMTA200600110](https://openairdocs.org/sdr/AMTA200600110.md): Skin · cracked · Feb 1, 2006 · N162AT · Lkheed 10113853 · Passenger/Crew Doors > X-RAY CARRIED OUT ON R1 DOOR UPPER FORWARD CORNER AND DETECTED FIVE FASTENER HOLES CRACKED. FURTHER INSPECTION FURTHER REVEALED 3 ADDITIONAL HOLES CRACKED. EIGHT TOTAL HOLE CRACKS FOUND. R1 DOOR UPPER FWD CUTOUT CORNER REPAIRED IAW ATA EO L10-53AD-0659, EER - [SDR AMTA200600109](https://openairdocs.org/sdr/AMTA200600109.md): Sill · corroded · Feb 1, 2006 · N162AT · Lkheed 10113853 · Fuselage Miscellaneous Structure > L1 DOOR LOWER SILL BETWEEN FS 281-297 WL 200 FOUND WITH SURFACE CORROSION. L1 DOOR LWR SILL INBOARD TEE ANGLE CORROSION AT CLIP NUT HOLE FOUND BEYOND ALLOWABLE LIMITS PER SRM 53-50-02 FIG 2 AND 51-50-02 FIG 1. REPAIRED DAMAGED CLIP NUT HOLE ARE IAW SRM 51-50 - [SDR AMTA200600112](https://openairdocs.org/sdr/AMTA200600112.md): Skin · corroded · Feb 1, 2006 · N162AT · Lkheed 10113853 · Fuselage Main, Plate/Skin > NOSE GEAR DOOR CUTOUT ALL FOUR CORNER DOUBLERS FOUND WITH RUST. RUST AND CORROSION CLEANED AND BLENDED IAW SRM 51-50-01 FIG 1. BLEND AREA WITHIN SRM 51-50-01 FIG 1 LIMITS. REAPPLIED CADMIUM PLATING AT ALL FOUR NLG DOOR CORNERS IAW LCP77-1237A. (M) - [SDR AMTA200600102](https://openairdocs.org/sdr/AMTA200600102.md): Support Bracket · corroded · Jan 31, 2006 · N162AT · Lkheed 10113853 · Fuselage Miscellaneous Structure > FORWARD CABIN AREA LONGITUDINAL SUPPORTING BRACKET FOUND CORRODED BETWEEN FS 281.5-297 RBL 40. BLENDED FLOOR SUPPORT IAW WITH SRM 51-21-02 AND FOUND WITHIN LIMITS OF SRM 51-50-02 FIG 1. MATERIAL ORIGINAL THICKNESS.063, MATERIAL LOSS.003. AREA PRIMED, PAIN - [SDR AMTA200600106](https://openairdocs.org/sdr/AMTA200600106.md): Pressure Panel · corroded · Jan 31, 2006 · N162AT · Lkheed 10113853 · Fuselage Main, Bulkhead > NLG COMPT PRESS DECK FOUND WITH CORROSION BETWEEN FS 349-36 LBL 29-31. FORWARD PRESSURE DECK CORROSION DAMAGE BEYOND SRM 53-11-00 FIG 6 LIMITS. REPAIRED DAMAGED AREA IAW EER L1-53-00-00-11447 AND LOCKHEED DWG LCC-7622-500 REV A. CLEANED, PRIMED AND TREATED - [SDR AMTA200600101](https://openairdocs.org/sdr/AMTA200600101.md): Floorbeam · corroded · Jan 31, 2006 · N162AT · Lkheed 10113853 · Fuselage Main, Floor Beam > AFT CABIN FLOOR STRUCTURE FLOORBEAM UPPER FLANGE FOUND WITH CORROSION AT FS 1763 LBL 39-55. FLOORBEAM WAS BLENDED AND FOUND BEYOND LIMITS PER SRM 53-21-00. CUTOUT DAMAGED FLOOR T-CAP AND REPAIRED IAW SRM 53-21-00 FIG 815 AND SRM 51-40-01. (M) - [SDR AMTA200600099](https://openairdocs.org/sdr/AMTA200600099.md): Structure · corroded · Jan 31, 2006 · N162AT · Lkheed 10113853 · Fuselage Main, Structure > NR 3 RAM AIR SCOOP UPPER AFT CORNER BETWEEN FS 315-398 AND BETWEEN STRINGER 21-22 FOUND WITH CORROSION INSIDE THE FESC. REMOVED BADLY DAMAGED FITTING P/N 1540520-120 AND ATTACHING STIFFENER AND ANGLES. REPAIRED AND REPLACED FITTING 1540520-1 02, STIFFENERS A - [SDR AMTA200600095](https://openairdocs.org/sdr/AMTA200600095.md): Intercostal · cracked · Jan 30, 2006 · N162AT · Lkheed 10113853 · Fuselage Miscellaneous Structure > MID CABIN FLOOR AT FS 1163 LEFT SIDE AT LBL 98 WL 200 INTERCOSTAL DOUBLER FOUND CRACKED. (M) - [SDR AMTA200600096](https://openairdocs.org/sdr/AMTA200600096.md): Support Fitting · corroded · Jan 30, 2006 · N162AT · Lkheed 10113853 · Fuselage Main, Attach Fittings > FORWARD WASTE TANK BALL VALVE SUPPORT FITTING CORRODED. SUPPORT FITTING REMOVED AND AREA CORROSION CLEANED IAW SRM 51-20-01. AREA CLEANED WAS FOUND BEYOND LIMITS IAW SRM 51-50-02 FIG 01. REPAIRED DAMAGED AREA IAW SRM 51-50-02 FIG 2. - [SDR AMTA200600087](https://openairdocs.org/sdr/AMTA200600087.md): Floor Support · corroded · Jan 30, 2006 · N162AT · Lkheed 10113853 · Fuselage Miscellaneous Structure > PAX CABIN AT FS 1794 LBL 48 DIAGONAL SUPPORT BEAM FOUND CORRODED. CLEANED AND BLENDED CORROSION AND FOUND BEYOND NEGLIGIBLE DAMAGE LIMITS IAW SRM 53-21-00 FIG 801. REMOVED AND REPAIRED DIAGONAL SUPPORT BEAM UPPER FLANGE IAW EER L1-530000-11455 AND SRM 53-21- - [SDR AMTA200600089](https://openairdocs.org/sdr/AMTA200600089.md): Floor Support · corroded · Jan 30, 2006 · N162AT · Lkheed 10113853 · Fuselage Miscellaneous Structure > PAX CABIN AT FS 1763 AT LBL 61 FLOOR SUPPORT FOUND WITH CORROSION. FOUND AREA TO HAVE BEEN PREVIOUSLY REPAIRED. BLENDED CORROSION AN FOUND BEYOND LIMITS OF SRM 53-21-00 FIG 809. REMOVED DAMAGED PARTS AND INSTALLED REPLACEMENTS IAW SRM 51-40-01 AND 53-21-00 - [SDR AMTA200600086](https://openairdocs.org/sdr/AMTA200600086.md): Floor Support · corroded · Jan 30, 2006 · N162AT · Lkheed 10113853 · Fuselage Miscellaneous Structure > FORWARD CABIN FLOOR SUPPORT STRUCTURE FOUND CORRODED BETWEEN FS 3690389 AND RBL 42-74. FORWARD CABIN FLOOR SUPPORT STRUCTURE CORRODED ON PREVIOUS REPAIR. REPAIR PART REMOVED BETWEEN RBL 42-74 IAW SRM 51-20-01 AND 51-40-02. REPAIRED SPLICE AND ANGLES IAW EER - [SDR AMTA200600084](https://openairdocs.org/sdr/AMTA200600084.md): Intercostal · corroded · Jan 30, 2006 · N162AT · Lkheed 10113853 · Fuselage Miscellaneous Structure > FORWARD CABIN FLOOR STRUCTURE BETWEEN FS 328-349 AND LBL 30-56 HAS CORROSION. CLEANED AND BLENDED CORROSION ON INTERCOSTAL AND FOUND BEYOND NEGLIGIBLE DAMAGE IAW SRM 51-50-02 FIG 01. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-01 AND LOCKHEED DWG 1613022. - [SDR AMTA200600077](https://openairdocs.org/sdr/AMTA200600077.md): Floor Support · corroded · Jan 25, 2006 · N162AT · Lkheed 10113853 · Fuselage Miscellaneous Structure > FORWARD CABIN FLOOR SUPPORT STRUCTURE FOUND CORRODED BETWEEN FS 313 TO 297 AND BETWEEN LBL 0-15. CLEAN AND BLENDED CORRODED FLOOR SUPPORT IAW SRM 51-21-01. BLEND AREA EVALUATED AND FOUND OUT OF LIMIT IAW SRM 51-50-02 FIG 1 AND 2. REPAIRED FLOOR SUPPORT IAW - [SDR AMTA200600049](https://openairdocs.org/sdr/AMTA200600049.md): Access Panel · corroded · Jan 20, 2006 · N162AT · Lkheed 10113853 · Wing, Plate/Skin > LT UNDER WING SURFACE FUEL TANK 2L ACCESS CUTOUT HOLES FOUND WITH SURFACE CORROSION ON THE FOLLOWING PANELS, 532BB, 532DB, 532FB, 533BB, 533DB, 533FB, 533HB, 533KB, 532CB, 532EB, 533AB, 533CB, 533EB, 533GB, 533JB, 534AB. FUEL ACCESS PANEL CUTOUT AREA MINOR SU - [SDR AMTA200600048](https://openairdocs.org/sdr/AMTA200600048.md): Access Panel · corroded · Jan 20, 2006 · N162AT · Lkheed 10113853 · Wing, Plate/Skin > LT OVERWING FUEL TANK ACCESS PANEL CUTOUT IS PITTED AND CORRODED AT OWS 452. LT WING UPPER SURFACE AT OWS 452 FUEL TANK ACCESS CUTOUT FLANGE SURFACE CORROSION CLEANED IAW SRM 51-21-01. NDT AND FOUND NO CRACKS. UT THICKNESS 134 MM. (M) - [SDR AMTA200600047](https://openairdocs.org/sdr/AMTA200600047.md): Access Panel · corroded · Jan 20, 2006 · N162AT · Lkheed 10113853 · Wing, Plate/Skin > LEFT OVERWING FUEL TANK ACCESS CUTOUT FLANGE PITTED AND CORRODED AT OWS 70. LEFT WING UPPER SURFACE AT OWS 70 CORROSION CLEANED FROM FUEL TANK ACCESS CUTOUT IAW SRM 51-21-01. FOUND NO CRACKS. UT THICKNESS REMAINING.291 MM. (M) - [SDR AMTA200600046](https://openairdocs.org/sdr/AMTA200600046.md): Access Panel · corroded · Jan 20, 2006 · N162AT · Lkheed 10113853 · Wing, Plate/Skin > LT OVERWING IWS 412 FUEL TANK ACCESS CUTOUT FLANGES PITTING AND CORRODED. LEFT WING UPPER SURFACE AT IWS 412 CORROSION CLEANED FROM FUEL TANK ACCESS CUTOUT IAW SRM 51-21-01. NDT FOUND NO CRACK. UT THICKNESS TEST SHOWED MATERIAL THICKNESS.310 MM. (M) - [SDR AMTA200600045](https://openairdocs.org/sdr/AMTA200600045.md): Spar · corroded · Jan 20, 2006 · N162AT · Lkheed 10113853 · Wing Spar > LT WING OVERWING IWS 241.08 TO 372.64 TE REAR SPAR DOUBLER IS RUSTY. CLEANED MINOR RUST CORROSION IAW SRM 51-10-02. CORROSION CLEANED ARE FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW 51-50-01 FIG 01. CADMIUN PLATED CLEANUP AREA IAW LCCP 77-1237A. (M) - [SDR AMTA200600044](https://openairdocs.org/sdr/AMTA200600044.md): Bracket · cracked · Jan 20, 2006 · N162AT · Lkheed 10113853 · Fuselage Main, Attach Fittings > LEFT WHEEL WELL AT FS 1346 FRAME TO KEELBEAM LONGERON ATTACHMENT ANGLE BRACKET CRACKED. LEFT W/W AT FS 1349 FRAME TO KEELBEAM LONGERON ATTACHMENT FWD AND AFT SUPPORT CLIPS AND BRACKETS REMOVED IAW SRM 51-40-01. REPLACED BRACKET IAW SRM 51-40-01. (M) - [SDR AMTA200600043](https://openairdocs.org/sdr/AMTA200600043.md): Angle · corroded · Jan 20, 2006 · N162AT · Lkheed 10113853 · Fuselage Miscellaneous Structure > LT NR 4 TORQUE BOX OWS 20.00 AREA INBOARD UPPER ANGLE CORRODED. LEFT NR 4 TORQUE BOX OWS 020.00 AREA INBOARD UPPER CAP MINOR SURFACE CORROSION CLEANED. CLEANED AREA STRUCTURALLY ACCEPTABLE AS A PERMENANT REPAIR IAW EER L1-570000-11404. (M) - [SDR AMTA200500514](https://openairdocs.org/sdr/AMTA200500514.md): Compressor · stalled · Jun 12, 2005 · N162AT · Lkheed 10113853 · Turbine Engine Compressor Section > NR 3 ENGINE COMPRESSOR STALLED ON CLIMB AT FL 27.0 TGT SPIKED AT 860 DEGREES FOR LESS THAN 2 SECONDS. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN WINDMILLED FOR 40 MINUTES WITH POSITIVE OIL PRESSURE INDICATION. PERFORMED CLAPPER LUBE, REPLACED SPINNER, BORESCOPE - [SDR AMTA200401464](https://openairdocs.org/sdr/AMTA200401464.md): Powerpack · discharged · Dec 2, 2004 · N162AT · Lkheed 10113853 · Emergency Lighting > R3 AND R4 EXTERIOR EMERGENCY LIGHT SHUT OFF WITHIN 2 MINUTES. REMOVED AND REPLACED EMERGENCY POWER PACK. IAW MM 33-51-03. OK FOR SERVICE. - [SDR AMTA200401463](https://openairdocs.org/sdr/AMTA200401463.md): Powerpack · discharged · Dec 2, 2004 · N162AT · Lkheed 10113853 · Emergency Lighting > DURING WALK AROUND, L3 AND L3A DOOR LIGHTS TURN OFF IN 2 MINUTES. REMOVED AND REPLACED EMERGENCY POWER PACK FOR L3 AND L3A DOOR LIGHTS (EXTERIOR). IAW MM 33-51-03. OK FOR SERVICE. - [SDR AMTA200301364](https://openairdocs.org/sdr/AMTA200301364.md): Warning Light · malfunctioned · Nov 5, 2003 · N162AT · Lkheed 10113853 · Engine Thrust Reverser > NR 2 THRUST REVERSER PRESSURE LIGHT CAME ON INFLIGHT. NO INDICATION THRUST REVERSER DEPLOYED. LIGHT COMES ON AT 95 PERCENT N1. - [SDR AMTA200301131](https://openairdocs.org/sdr/AMTA200301131.md): Slide · malfunctioned · Sep 4, 2003 · N162AT · Lkheed 10113853 · Escape Slide > R-1 DOOR WOULD NOT ARM BEFORE FLIGHT. REMOVED AND REPLACED R-1 DOOR SLIDE PER M-11-25-36. OPS CHECK GOOD. (M) - [SDR AMTA200301126](https://openairdocs.org/sdr/AMTA200301126.md): Actuator · inoperative · Sep 2, 2003 · N162AT · Lkheed 10113853 · Passenger/Crew Doors > R-1 DOOR IS INOPERATIVE ELECTRICALLY. REMOVED AND REPLACED R-1 DOOR ELECT ACTUATOR IAW 52-12-01, OPS CHECKED OK. (M) - [SDR AMTA200301097](https://openairdocs.org/sdr/AMTA200301097.md): Mechanism · inoperative · Aug 27, 2003 · N162AT · Lkheed 10113853 · Passenger/Crew Doors > R1 DOOR INOPERATIVE ELECTRICALLY. (M) - [SDR AMTA200300903](https://openairdocs.org/sdr/AMTA200300903.md): Attach Fitting · cracked · Jun 21, 2003 · N162AT · Lkheed 10113853 · Wing, Control Surface Attach Fittings > RIGHT WING AFT SPAR OUTBOARD AILERON ATTACH FITTING CRACKED AT SECOND HINGE FROM OUTBOARD. REPLACED FITTING IAW SRM 51-10-01 AND ER/A L10-57R-5202. (M) Next page: https://openairdocs.org/deregistered/N162AT-2016-01-12/reports.md?page=2 ## 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 = 'N162AT' AND deregistration_id = 'N162AT-2016-01-12' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N162AT-2016-01-12/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.