# Service difficulty reports: N187AW, cancelled Mar 16, 2005 A list on [N187AW, cancelled Mar 16, 2005](https://openairdocs.org/deregistered/N187AW-2005-03-16.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 4 · 166 reports - [SDR AWXA200401275](https://openairdocs.org/sdr/AWXA200401275.md): Power Supply · discharged · Nov 12, 2004 · N187AW · Boeing 737277 · Emergency Lighting > PHX - EEL - DURING 8-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM FOUND THE LT EXTERIOR OVERWING EMERGENCY LIGHT AND LT LOWER AFT WING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT POWER SUPPLY, OPERATIONAL C - [SDR AWXA200401223](https://openairdocs.org/sdr/AWXA200401223.md): Light · inoperative · Nov 4, 2004 · N187AW · Boeing 737277 · Emergency Lighting > DURING 8-DAY CHECK, FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 13 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. - [SDR AWXA200401103](https://openairdocs.org/sdr/AWXA200401103.md): Battery · discharged · Oct 5, 2004 · N187AW · Boeing 737277 · Emergency Lighting > DURING INSPECTION MAINTENANCE, FOUND THE EMERGENCY EXIT LIGHT ABOVE THE L-2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY IN EMERGENCY EXIT LIGHT ABOVE THE L-2 DOOR, OPERATIONAL CHECK WAS GOOD. - [SDR AWXA200400660](https://openairdocs.org/sdr/AWXA200400660.md): Turbine Blades · overheated · Jun 18, 2004 · N187AW · Boeing 737277 · Turbine Section > ON TAKEOFF ROLL AT OAK EN ROUTE FOR LAS FELT A STRONG VIBRATION NR 1 ENGINE, REJECTED TAKEOFF AT 50 KTS AND PULLED OFF ONTO TAXIWAY WHERE EMERGENCY EQUIPMENT INSPECTED THE AIRCRAFT. TAXIED BACK TO GATE USING NR 2 ENGINE. MAINTENANCE REMOVED AND REPLACED NR 1 - [SDR AWXA200400633](https://openairdocs.org/sdr/AWXA200400633.md): Light · defective · Jun 12, 2004 · N187AW · Boeing 737277 · Emergency Lighting > LAS - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 8 LT, OPERATIONAL CHECK WAS GOOD. - [SDR AWXA200400580](https://openairdocs.org/sdr/AWXA200400580.md): Battery · discharged · May 30, 2004 · N187AW · Boeing 737277 · Emergency Lighting > LAS - EEL - DURING 4-DAY CHECK THE L-1 AND R-1 DOOR EMERGENCY SLIDE LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK, OPERATIONAL CHECK WAS GOOD. - [SDR AWXA200400063](https://openairdocs.org/sdr/AWXA200400063.md): Light · inoperative · Jan 23, 2004 · N187AW · Boeing 737277 · Emergency Lighting > DURING A1 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. - [SDR AWXA200301604](https://openairdocs.org/sdr/AWXA200301604.md): Light · damaged · Dec 25, 2003 · N187AW · Boeing 737277 · Emergency Lighting > PHX - EEL - DURING A-01 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 10 LT WAS FOUND HANGING FROM SEAT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH SEAT LIGHT ASSEMBLY AT SEAT ROW 10 LT, OPERATIONAL CHECK WAS GOOD. - [SDR AWXA200301522](https://openairdocs.org/sdr/AWXA200301522.md): Battery · discharged · Dec 9, 2003 · N187AW · Boeing 737277 · Emergency Lighting > DURING FUNCTIONAL CHECK OF EMERGENCY LIGHT SYSTEM THE EMERGENCY EXIT SIGN ABOVE THE R-2 FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK ABOVE THE R-2 DOOR, OPERATIONAL CHECK WAS GOOD. - [SDR AWXA200301483](https://openairdocs.org/sdr/AWXA200301483.md): Firewall · cracked · Nov 14, 2003 · N187AW · Boeing 737277 · Nacelle/Pylon, Bulkhead/Firewall > LCQ - MAJOR REPAIR - DURING C-14 CHECK 5 EACH CRACKS WERE FOUND ON NR 1 ENGINE PYLON FORWARD FIREWALL. MAINTENANCE PERFORMED WELD REPAIR ON FORWARD FIREWALL PAN ASSEMBLY IAW AWA ER 15-5412-03322-SS1. - [SDR AWXA200301476](https://openairdocs.org/sdr/AWXA200301476.md): Frame · cracked · Nov 5, 2003 · N187AW · Boeing 737277 · Engine Cowling System > LCQ - MINOR REPAIR - DURING C-14 CHECK.75 INCH CRACK WAS FOUND IN NR 1 ENGINE FORWARD OUTBOARD COWLING FRAME NR 7 AT PREVIOUS CUTOUT. MAINTENANCE CUTOUT CRACK IN NR 1 ENGINE FORWARD OUTBOARD COWLING FRAME NR 7; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PAR - [SDR AWXA200301475](https://openairdocs.org/sdr/AWXA200301475.md): Rib · cracked · Nov 4, 2003 · N187AW · Boeing 737277 · Wing, Rib/Bulkhead > LCQ - MINOR REPAIR - DURING C-14 CHECK 1.1875 INCH CRACK WAS FOUND IN LT WING LEADING EDGE RIB, INBOARD OF NR 1 ENGINE AT L/E STA 222.7. MAINTENANCE REMOVED CRACKED LT WING LEADING EDGE RIB AT L/E STA 222.7; FABRICATED A NEW REPLACEMENT RIB PER DWG 65-49353; - [SDR AWXA200301474](https://openairdocs.org/sdr/AWXA200301474.md): Rib · cracked · Nov 2, 2003 · N187AW · Boeing 737277 · Wing, Rib/Bulkhead > LCQ - MAJOR REPAIR - DURING C-14 CHECK.5 INCH CRACK WAS FOUND IN LT WING LEADING EDGE RIB, INBOARD OF NR 1 ENGINE AT L/E STA 222.7. MAINTENANCE REMOVED CRACKED LT WING LEADING EDGE RIB AT L/E STA 222.7; FABRICATED A NEW REPLACEMENT RIB PER DWG 65-49353; INST - [SDR AWXA200301484](https://openairdocs.org/sdr/AWXA200301484.md): Skin · cracked · Oct 31, 2003 · N187AW · Boeing 737277 · Fuselage Main, Plate/Skin > LCQ - MAJOR REPAIR - DURING C-14 CHECK A CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727, STR 16 RT. MAINTENANCE REMOVED DAMAGED SKIN FROM BS 727 TO BS 777, STR 16 RT; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH FILLERS, 4 EACH DOUBLERS, - [SDR AWXA200301289](https://openairdocs.org/sdr/AWXA200301289.md): Wire · broken · Oct 22, 2003 · N187AW · Boeing 737277 · Light System Wiring > DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 LT WAS FOUND INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 LT, REPAIRED BROKEN WIRE, OPERATIONAL CHECK WAS GOOD. - [SDR AWXA200301473](https://openairdocs.org/sdr/AWXA200301473.md): Frame · cracked · Oct 7, 2003 · N187AW · Boeing 737277 · Fuselage Main, Frame > LCQ - MAJOR REPAIR - DURING C-14 CHECK 2 EACH CRACKS WERE FOUND IN FASTENER HOLES ON THE RT FUSELAGE FRAME AT BS 727, BETWEEN WL 195 AND WL 202. MAINTENANCE OVERSIZED HOLES AND PERFORMED HFEC INSPECTION TO VERIFY CRACKS CONTAINED, NO CRACK INDICATIONS WERE NO - [SDR AWXA200300054](https://openairdocs.org/sdr/AWXA200300054.md): Wire · broken · Jan 19, 2003 · N187AW · Boeing 737277 · Emergency Lighting > PHX - EEL - DURING INSPECTION A WIRE WAS FOUND PULLED OUT OF SPLICE ON THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 L/H. MAINTENANCE REPAIRED BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 L/H, OPERATIONAL CHECK WAS GOOD. - [SDR AWXA200300028](https://openairdocs.org/sdr/AWXA200300028.md): Battery · discharged · Jan 11, 2003 · N187AW · Boeing 737277 · Emergency Lighting > AUS - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHT ABOVE THE L-2 DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULBS AND BATTERY PACK ON EMERGENCY EXIT LIGHT ABOVE THE L-2 DOOR; OPERATIONAL CHECK WAS GOOD. - [SDR AWXA200201053](https://openairdocs.org/sdr/AWXA200201053.md): Battery · discharged · Oct 27, 2002 · N187AW · Boeing 737277 · Emergency Lighting > DURING A CHECK EMERGENCY ESCAPE PATH LIGHTS FAILED OPERATIONAL TEST ON TASKCARD I1M05002. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY BATTERY PACK AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD. - [SDR AWXA200201029](https://openairdocs.org/sdr/AWXA200201029.md): Battery Pack · discharged · Oct 21, 2002 · N187AW · Boeing 737277 · Emergency Lighting > DURING INSPECTION THE L-2 DOOR INTERIOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR EMERGENCY EXIT LIGHT BATTERY PACK IAW 33-51-01, OPERATIONAL CHECK WAS GOOD. - [SDR AWXA200200995](https://openairdocs.org/sdr/AWXA200200995.md): Light · broken · Oct 11, 2002 · N187AW · Boeing 737277 · Emergency Lighting > DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE DAMAGED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT, FUNCTIONAL CHECK WAS GOOD. - [SDR AWXA200200932](https://openairdocs.org/sdr/AWXA200200932.md): Attach Angle · cracked · Sep 23, 2002 · N187AW · Boeing 737277 · Fuselage Main, Attach Fittings > MCN - MAJOR REPAIR - DURING C-13 CHECK A.5 INCH CRACK WAS FOUND ON THE FORWARD OUTBOARD ATTACH ANGLE AT THE LT WHEEL WELL OPENING, CRACK RUNS FROM TOP FASTENER HOLE TO THE UPPER EDGE OF THE ANGLE, BS 679, LBL 70, WL 172. MAINTENANCE REMOVED THE DAMAGED ATTAC - [SDR AWXA200200943](https://openairdocs.org/sdr/AWXA200200943.md): Skin · cracked · Sep 22, 2002 · N187AW · Boeing 737277 · Trailing Edge Flaps > MCN - MAJOR REPAIR - DURING C-13 CHECK A 3/16" CRACK WAS FOUND ON THE L/H WING INBOARD HINGED FLAP UPPER SKIN AT THE R/H SIDE APPROXIMATELY 7" FROM THE TRAILING EDGE GOING FORWARD. MAINTENANCE TRIMMED OUT DAMAGED AREA ON HINGED FLAP UPPER SKIN; FABRICATED AN - [SDR AWXA200200939](https://openairdocs.org/sdr/AWXA200200939.md): Doubler · corroded · Sep 18, 2002 · N187AW · Boeing 737277 · Fuselage Main, Plate/Skin > MCN - MAJOR REPAIR - DURING C-13 CHECK EXFOLIATION CORROSION WAS FOUND ON THE FORWARD LAV PAN RING AT BS 275. MAINTENANCE REMOVED EXTERNAL DOUBLER AND LAV PAN RING; FABRICATED A NEW EXTERNAL DOUBLER; INSTALLED REPAIR PART AND LAV PAN RING IAW B737-200 SRM 51- - [SDR AWXA200200941](https://openairdocs.org/sdr/AWXA200200941.md): Skin · cracked · Sep 11, 2002 · N187AW · Boeing 737277 · Fuselage Main, Plate/Skin > MCN - MAJOR REPAIR - DURING C-13 CHECK A 1 1/4" CRACK WAS FOUND ON FUSELAGE SKIN 6" BELOW THE UPPER HINGE CUTOUT OF THE L-1 DOOR, BS 306, WL 236.68. MAINTENANCE REMOVED EXISTING DOUBLER AND FOUND 2 CRACKS EMANATING FROM EXISTING STOP DRILL HOLES. CUTOUT DAMAG - [SDR AWXA200200918](https://openairdocs.org/sdr/AWXA200200918.md): Skin · cracked · Sep 7, 2002 · N187AW · Boeing 737277 · Fuselage Main, Plate/Skin > MCN - MAJOR REPAIR - DURING C-13 CHECK A.125 INCH CRACK WAS FOUND ON SKIN AT TEAR STRAP AFT, BS 420, STR 10 RT, CONFIRMED HFEC INSPECTION. MAINTENANCE CUTOUT DAMAGE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED 2 EACH REPAIR DOUBLERS - [SDR AWXA200200933](https://openairdocs.org/sdr/AWXA200200933.md): Frame · cracked · Sep 3, 2002 · N187AW · Boeing 737277 · Fuselage Main, Frame > MCN - MAJOR REPAIR - DURING C-13 CHECK A 3/4" CRACK WAS FOUND ON THE AFT CARGO DOOR FORWARD FRAME AT BS 794, WL 167, RBL 44. MAINTENANCE STOP DRILLED THE CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY THE CRACK WAS CONTAINED. FABRICATED A DOUBLER, 2 EACH SUP - [SDR AWXA200200874](https://openairdocs.org/sdr/AWXA200200874.md): Stringer Clip · Sep 3, 2002 · N187AW · Boeing 737277 · Fuselage Main, Longeron/Stringer > MCN - MAJOR REPAIR - DURING C-13 CHECK A 1/2" CRACK WAS FOUND ON STRINGER CLIP AT BS 663, STRINGER 10 R/H. MAINTENANCE REMOVED DAMAGED STRINGER CLIP AT BS 663, STRINGER 10 R/H, FABRICATED A NEW STRINGER CLIP, AND INSTALLED REPAIR IAW DWG 69-35352, AND B737-200 - [SDR AWXA200200873](https://openairdocs.org/sdr/AWXA200200873.md): Stringer Clip · cracked · Sep 3, 2002 · N187AW · Boeing 737277 · Fuselage Main, Longeron/Stringer > MCN - MAJOR REPAIR - DURING C-13 CHECK A 1/2" CRACK WAS FOUND ON STRINGER CLIP AT BS 597, STRINGER 9 R/H. MAINTENANCE REMOVED DAMAGED STRINGER CLIP AT BS 597, STRINGER 9 R/H, FABRICATED A NEW STRINGER CLIP, AND INSTALLED REPAIR IAW DWG 69-35352, AND B737-200 S - [SDR AWXA200200872](https://openairdocs.org/sdr/AWXA200200872.md): Stringer Clip · cracked · Sep 3, 2002 · N187AW · Boeing 737277 · Fuselage Main, Longeron/Stringer > MCN - MAJOR REPAIR - DURING C-13 CHECK A 1/2" CRACK WAS FOUND ON STRINGER CLIP AT BS 559, STRINGER 10 R/H. MAINTENANCE REMOVED DAMAGED STRINGER CLIP AT BS 559, STRINGER 10 R/H, FABRICATED A NEW STRINGER CLIP, AND INSTALLED REPAIR IAW DWG 69-35352, AND B737-200 - [SDR AWXA200200871](https://openairdocs.org/sdr/AWXA200200871.md): Stringer Clip · cracked · Sep 3, 2002 · N187AW · Boeing 737277 · Fuselage Miscellaneous Structure > MCN - MAJOR REPAIR - DURING C-13 CHECK A.75 INCH CRACK WAS FOUND ON STRINGER CLIP AT BS 706, STRINGER 3 LT. MAINTENANCE REMOVED DAMAGED STRINGER CLIP AT BS 706, STRINGER 3 LT, FABRICATED A NEW STRINGER CLIP, AND INSTALLED REPAIR IAW DWG 69-35352, AND B737-20 - [SDR AWXA200200931](https://openairdocs.org/sdr/AWXA200200931.md): Angle · cracked · Sep 2, 2002 · N187AW · Boeing 737277 · Fuselage Miscellaneous Structure > MCN - MAJOR REPAIR - DURING C-13 CHECK A.5 INCH CRACK WAS FOUND ON CREASE BEAM SHEAR WEB ANGLE AT BS 616, RBL 64, WL 208. MAINTENANCE REMOVED DAMAGED CREASE BEAM SHEAR WEB ANGLE, FABRICATED A NEW SECTION OF CREASE BEAM SHEAR WEB ANGLE, AND INSTALLED REPAIR PA - [SDR AWXA200200877](https://openairdocs.org/sdr/AWXA200200877.md): Web · cracked · Sep 2, 2002 · N187AW · Boeing 737277 · Fuselage Miscellaneous Structure > MCN - MAJOR REPAIR - DURING C-13 CHECK A 1/2" CRACK WAS FOUND ON VERTICAL WEB AT BS 695, LBL 58-62, WL 206. MAINTENANCE REMOVED DAMAGED VERTICAL WEB AT BS 695, LBL 58-62, WL 206. FABRICATED A NEW VERTICAL WEB AND WEB SPLICE, AND INSTALLED REPAIR PARTS IAW DWG - [SDR AWXA200200876](https://openairdocs.org/sdr/AWXA200200876.md): Skin · cracked · Sep 2, 2002 · N187AW · Boeing 737277 · Cargo/Baggage Doors > MCN - MAJOR REPAIR - DURING C-13 CHECK A 3/8" CRACK WAS FOUND ON THE AFT CARGO DOOR INNER SKIN AT THE CENTER ACCESS OPENING JUST BELOW THE HANDLE, BS 787-847. MAINTENANCE BLENDED OUT CRACK ON THE AFT CARGO DOOR INNER SKIN AT THE CENTER ACCESS OPENING JUST BELO - [SDR AWXA200200942](https://openairdocs.org/sdr/AWXA200200942.md): Skin · worn · Sep 1, 2002 · N187AW · Boeing 737277 · Trailing Edge Flaps > MCN - MAJOR REPAIR - DURING C-13 CHECK THE L/H WING INBOARD MID FLAP UPPER SURFACE WAS FOUND TO HAVE A WORN SPOT AT THE INBOARD EDGE. MAINENANCE CUTOUT WORN SPOT ON MID FLAP UPPER SURFACE; FABRICATED AN EXTERNAL DOUBLER, AND INSTALLED REPAIR PART IAW AWA E.R. - [SDR AWXA200200940](https://openairdocs.org/sdr/AWXA200200940.md): Skin · cracked · Sep 1, 2002 · N187AW · Boeing 737277 · Engine Cowling System > MCN - MAJOR REPAIR - DURING C-13 CHECK EXFOLIATION CORROSION WAS FOUND ON THE FORWARD LAV PAN RING AT BS 275. MAINTENANCE REMOVED EXTERNAL DOUBLER AND LAV PAN RING; FABRICATED A NEW EXTERNAL DOUBLER; INSTALLED REPAIR PART AND LAV PAN RING IAW B737-200 SRM 51- - [SDR AWXA200200881](https://openairdocs.org/sdr/AWXA200200881.md): Skin · cracked · Sep 1, 2002 · N187AW · Boeing 737277 · Fuselage Main, Plate/Skin > MCN - MAJOR REPAIR - DURING C-13 CHECK A 1" CRACK WAS FOUND ON OUTER SKIN NEAR THE R/H MAIN LANDING GEAR WHEEL WELL KEEL BEAM AREA, BETWEEN 2 REPAIR DOUBLERS, BS 707. MAINTENANCE REMOVED DAMAGED SECTION OF OUTER SKIN, FABRICATED A SECTION OF KEEL BEAM OUTER SK - [SDR AWXA200200867](https://openairdocs.org/sdr/AWXA200200867.md): Stringer Clip · cracked · Sep 1, 2002 · N187AW · Boeing 737277 · Fuselage Miscellaneous Structure > MCN - MAJOR REPAIR - DURING C-13 CHECK THE OUTBOARD UPPER LEG OF STRINGER CLIP WAS FOUND CRACKED ON THE AFT SIDE OF FRAME 663, STR 11 LT, ABOVE CABIN WINDOW. MAINTENANCE REMOVED DAMAGED STRINGER CLIP AT BS 663, STR 11 LT, FABRICATED A NEW STRINGER CLIP AND IN - [SDR AWXA200200897](https://openairdocs.org/sdr/AWXA200200897.md): Frame · cracked · Aug 31, 2002 · N187AW · Boeing 737277 · Fuselage Main, Frame > MCN - MAJOR REPAIR - DURING C-13 CHECK A 2 1/2" CRACK WAS FOUND ON THE FORWARD CARGO COMPARTMENT FRAME BODY ABOVE STRINGER 21 L/H, BS 480. MAINTENANCE CUTOUT DAMAGED SECTION OF FRAME, REMOVED 3 EACH INTERCOASTALS FOR ACCESS, REMOVED 2 EACH STRINGER TIE CLIPS C - [SDR AWXA200200896](https://openairdocs.org/sdr/AWXA200200896.md): Skin · cracked · Aug 31, 2002 · N187AW · Boeing 737277 · Service Doors > MCN - MAJOR REPAIR - DURING C-13 CHECK A.25 INCH CRACK WAS FOUND ON THE R2 DOOR EXTERNAL SKIN AT THE LOWER HINGE CUTOUT UPPER AFT CORNER, BS 962. MAINTENANCE TRIMMED OUT DAMAGE AT LOWER HINGE CUTOUT UPPER AFT CORNER AND PERFORMED A HFEC INSPECTION TO VERIFY - [SDR AWXA200200857](https://openairdocs.org/sdr/AWXA200200857.md): Skin · cracked · Aug 31, 2002 · N187AW · Boeing 737277 · Passenger/Crew Doors > MCN - MAJOR REPAIR - DURING C-13 CHECK A.5 INCH CRACK WAS FOUND ON L1 DOOR INNER SKIN AT UPPER CORNER ACCESS HOLE FOR FOR UPPER END OF VERTICAL TORQUE TUBE. MAINTENANCE REMOVED DAMAGED AREA OF SKIN, FOUND MATERIAL LOSS TO BE WITHIN LIMITS PER B737-200 SRM 5 - [SDR AWXA200200618](https://openairdocs.org/sdr/AWXA200200618.md): Battery · discharged · Jul 14, 2002 · N187AW · Boeing 737277 · Emergency Lighting > DURING INSPECTION THE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE ABOVE L2 DOOR. MAINTENANCE REMOVED AND REPLACED THE BATTERIES AT THE EMERGENCY EXIT LIGHT ABOVE THE L2 DOOR, OPERATIONAL CHECK WAS GOOD. - [SDR AWXA200200617](https://openairdocs.org/sdr/AWXA200200617.md): Battery · discharged · Jul 14, 2002 · N187AW · Boeing 737277 · Emergency Lighting > DURING INSPECTION THE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE AT THE COCKPIT ENTRANCE. MAINTENANCE REMOVED AND REPLACED BATTERIES FOR FORWARD EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD. - [SDR AWXA200200616](https://openairdocs.org/sdr/AWXA200200616.md): Wire · broken · Jul 14, 2002 · N187AW · Boeing 737277 · Emergency Lighting > PHX - EEL - DURING INSPECTION THE EMERGENCY EXIT PATHWAY LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 7 L/H. MAINTENANCE SPLICED A BROKEN WIRE AT SEAT ROW 7 L/H IAW CHAP 20 SWPM, OPERATIONAL CHECK WAS GOOD. - [SDR AWXA200200506](https://openairdocs.org/sdr/AWXA200200506.md): Wire · broken · Jun 9, 2002 · N187AW · Boeing 737277 · Emergency Lighting > PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 L/H WAS FOUND INOPERATIVE. MAINTENANCE FOUND THE WIRING UNDER SEAT COMING OUT OF THE SPLICE. RE-SPLICED BROKEN E-PATH WIRE UNDER SEAT ROW 4 L/H, OPERATIONAL CHECK WAS GOOD. - [SDR AWXA200200427](https://openairdocs.org/sdr/AWXA200200427.md): Wire · broken · May 15, 2002 · N187AW · Boeing 737277 · Emergency Lighting > LAS - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHTS WERE FOUND INOPERATIVE AT SEAT ROWS 17 AND 19 L/H. MAINTENANCE REPAIRED A BROKEN WIRE AT SEAT ROW 17 L/H AND REPLACED BULB ON SEAT LIGHT 19, FUNCTIONAL TEST GOOD IAW T/C A1C33006. - [SDR AWXA200200149](https://openairdocs.org/sdr/AWXA200200149.md): Battery · discharged · Feb 16, 2002 · N187AW · Boeing 737277 · Emergency Lighting > PHX - EEL - C - DURING INSPECTION THE EMERGENCY EXIT LIGHT AT L-2 DOOR WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT FOR L-2 DOOR EMERGENCY EXIT LIGHT IAW T/C A1C33005, OPERATIONAL CHECK WAS GOOD. - [SDR AWXA0002158](https://openairdocs.org/sdr/AWXA0002158.md): Keelbeam · damaged · Aug 4, 2001 · N187AW · Boeing 737277 · Fuselage Main, Keel > OIL CANNING AND LOOSE RIVETS ON KEEL BEAM PANEL BS 663-673. REPAIRED FASTENER HOLES IN KEEL BEAM CHORD AND REPAIRED PANEL IAW AWA ER 15-5315-01215-DL. - [SDR AWXA0002157](https://openairdocs.org/sdr/AWXA0002157.md): Angle · corroded · Aug 4, 2001 · N187AW · Boeing 737277 · Fuselage Main, Bulkhead > D: Corrosion on torque box outlet support (BS 1088 bulkhead)C: Removed and replaced BS 1088 outlet support angle IAW BAC DWG 65-46572 and B737 SRM 51-10-6 Pg 4-6, 53-10-1 fig 8n Pg 4-5, 51-10-2 pg 7-8, 51-30-5 pg 5 and 51-30-2 pg 32 - [SDR AWXA0002155](https://openairdocs.org/sdr/AWXA0002155.md): Floorbeam · corroded · Aug 4, 2001 · N187AW · Boeing 737277 · Fuselage Main, Floor Beam > CORROSION ON FLOORBEAM BS 1016 LBL 33.5 TOP AND BOTTOM OF UPPER FLANGE. REPAIRED BS 1016 FLOORBEAM UPPER CHORD IAW AWA ER 15-5365-01209-DD1. Next page: https://openairdocs.org/deregistered/N187AW-2005-03-16/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 = 'N187AW' AND deregistration_id = 'N187AW-2005-03-16' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N187AW-2005-03-16/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.