# Service difficulty reports: N186AW, cancelled Mar 16, 2005

A list on [N186AW, cancelled Mar 16, 2005](https://openairdocs.org/deregistered/N186AW-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 · 152 reports

- [SDR AWXA200401010](https://openairdocs.org/sdr/AWXA200401010.md): Light · inoperative · Sep 11, 2004 · N186AW · Boeing 737277 · Emergency Lighting
  > FLIGHT CREW REPORTED THE COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE COCKPIT EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400893](https://openairdocs.org/sdr/AWXA200400893.md): Flashlight · inoperative · Aug 16, 2004 · N186AW · Boeing 737277 · Emergency Equipment
  > DFW - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD GALLEY EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400565](https://openairdocs.org/sdr/AWXA200400565.md): Light · inoperative · May 24, 2004 · N186AW · Boeing 737277 · Emergency Lighting
  > DURING 8-DAY CHECK THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400407](https://openairdocs.org/sdr/AWXA200400407.md): Skin · delaminated · Apr 25, 2004 · N186AW · Boeing 737277 · Trailing Edge Flaps
  > FLIGHT CONTROL - DURING 4-DAY CHECK FOUND THE LT OUTBOARD TRAILING FLAP DELAMINATED AND SEPARATING ALONG TRAILING EDGE, APPROXIMATELY 12 INCHES BY 1 INCH, AND 3 INCHES BY 3/4 INCH WITH A 8 INCH SEPARATION. MAINTENANCE REMOVED AND REPLACED THE LT OUTBOARD TRAIL
- [SDR AWXA200400048](https://openairdocs.org/sdr/AWXA200400048.md): Skin · cracked · Jan 14, 2004 · N186AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > PHX - MAJOR REPAIR - A 2.5 INCH CRACK WAS FOUND IN FUSELAGE SKIN LEFT SIDE OF AIRCRAFT AT STR 24 LEFT BETWEEN BS 927 AND BS 947. MAINTENANCE CUT OUT DAMAGE IN FUSELAGE SKIN AT STR 24 LEFT BETWEEN BS 927 AND BS 947; PERFORMED HFEC INSPECTION TO VERIFY NO CRACK
- [SDR AWXA200301646](https://openairdocs.org/sdr/AWXA200301646.md): Light · worn · Dec 30, 2003 · N186AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHT OVER THE L-2 DOOR FLICKERS ON AND OFF DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY ABOVE THE L-2 DOOR, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200301060](https://openairdocs.org/sdr/AWXA200301060.md): Panel · cracked · Sep 14, 2003 · N186AW · Boeing 737277 · Leading Edge Devices
  > DURING C-16 CHECK.1875 INCH CRACK WAS FOUND ON CLOSE OUT PANEL BELOW NR 2 SLAT INBOARD MAIN TRACK AT WBL 355. MAINTENANCE REMOVED CRACKED NR 2 SLAT CLOSE OUT PANEL AT WBL 355; FABRICATED A NEW REPLACEMENT PANEL IAW DWG 69-53316; INSTALLED REPAIR PART IAW B737
- [SDR AWXA200301046](https://openairdocs.org/sdr/AWXA200301046.md): Clip · cracked · Sep 9, 2003 · N186AW · Boeing 737277 · Nacelle/Pylon Miscellaneous Structure
  > DURING C-16 CHECK A.1250 CRACK WAS FOUND IN RADIUS OF NR 1 ENGINE LT FIXED FAIRING CLIP AT AFT END, 1ST RIB. MAINTENANCE REMOVED CRACKED CLIP ON NR 1 ENGINE LT FIXED FAIRING AFT END, 1ST RIB; FABRICATED A NEW REPLACEMENT CLIP IAW DWG 65-52263; INSTALLED REPAI
- [SDR AWXA200301045](https://openairdocs.org/sdr/AWXA200301045.md): Gusset · cracked · Sep 9, 2003 · N186AW · Boeing 737277 · Nacelle/Pylon, Main Frame
  > DURING C-16 CHECK A.1250 INCH CRACK WAS FOUND AT FASTENER HOLE ON NR 1 ENGINE FIXED FAIRING COVER PLATE (GUSSET) AT AFT END, 1ST RIB. MAINTENANCE REMOVED CRACKED GUSSET ON NR 1 ENGINE FIXED FAIRING AFT END, 1ST RIB; FABRICATED A NEW REPLACEMENT GUSSET IAW DW
- [SDR AWXA200301062](https://openairdocs.org/sdr/AWXA200301062.md): Battery Pack · discharged · Sep 8, 2003 · N186AW · Boeing 737277 · Emergency Lighting
  > DURING C-16 CHECK, FUNCTIONAL CHECK OF EMERGENCY EVACUATION LIGHT SYSTEM FOUND THE RT OVER WING, RT AND LT EMERGENCY ESCAPE SLIDE, AND RT AFT WING (EXTERNAL) LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT OVER WING, AND RT AFT CARGO COMPARTMENT EM
- [SDR AWXA200301047](https://openairdocs.org/sdr/AWXA200301047.md): Angle · cracked · Sep 3, 2003 · N186AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-16 CHECK A.3125 INCH CRACK WAS FOUND AT FASTENER HOLE ON L ANGLE AT BS 663 IN LT AFT AIR CONDITIONING BAY ABOVE TURBO FAN. MAINTENANCE REMOVED CRACKED HORIZONTAL (L) ANGLE AT BS 663; FABRICATED A NEW REPLACEMENT (L) ANGLE IAW DWG 65-45402; INSTALLED
- [SDR AWXA200301040](https://openairdocs.org/sdr/AWXA200301040.md): Angle · cracked · Aug 28, 2003 · N186AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-16 CHECK A.1875 INCH CRACK WAS FOUND ON ATTACH ANGLE AFT OF L-1 DOOR CUTOUT BS 348.20, WL 222. MAINTENANCE REMOVED CRACKED ATTACH ANGLE BS 348.20, WL 222; FABRICATED A NEW REPLACEMENT ATTACH ANGLE IAW DWG 69-26555; INSTALLED REPAIR PART IAW B737-20
- [SDR AWXA200301053](https://openairdocs.org/sdr/AWXA200301053.md): Fitting · corroded · Aug 27, 2003 · N186AW · Boeing 737277 · Fuselage, Landing Gear Attach Fittings
  > DURING C-16 CHECK CORROSION WAS FOUND ON RT MAIN LANDING GEAR BEAM INBOARD STABILIZER FITTING AT TRAILING EDGE OF WING. MAINTENANCE REMOVED AND REPLACED CORRODED STABILIZER FITTING IAW AMM 57-01-000-4, PG. 1-2.
- [SDR AWXA200301044](https://openairdocs.org/sdr/AWXA200301044.md): Attach Angle · cracked · Aug 27, 2003 · N186AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-16 CHECK 2 EACH CRACKS WERE FOUND ON ATTACH ANGLES AFT OF BS 348.20, LT SIDE OF FUSELAGE, WL 222. MAINTENANCE REMOVED CRACKED ATTACH ANGLE BS 348.20, WL 222; FABRICATED 2 EACH NEW REPLACEMENT ATTACH ANGLES IAW DWG'S 69-16970-501 AND 69-76555-3; INSTAL
- [SDR AWXA200301039](https://openairdocs.org/sdr/AWXA200301039.md): Angle · cracked · Aug 27, 2003 · N186AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-16 CHECK A.5 INCH CRACK WAS FOUND ON WEB ANGLE JUST AFT OF BS 348.20, LT SIDE OF FUSELAGE, WL 216. MAINTENANCE REMOVED CRACKED WEB ANGLE BS 348.20; FABRICATED A NEW REPLACEMENT WEB ANGLE IAW DWG 69-16509; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-
- [SDR AWXA200300991](https://openairdocs.org/sdr/AWXA200300991.md): Intercostal · cracked · Aug 21, 2003 · N186AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-16 CHECK A 3 INCH CRACK WAS FOUND ON UPPER FLANGE OF INTERCOSTAL (BAFFLE) AT BS 440-460, OUTBOARD OF STR 26 LT. MAINTENANCE REMOVED DAMAGED INTERCOSTAL FROM BS 440 TO BS 460; FABRICATED A NEW REPLACEMENT INTERCOASTAL PER DWG 65-41473; INSTALLED REPAIR
- [SDR AWXA200301050](https://openairdocs.org/sdr/AWXA200301050.md): Connector · damaged · Aug 20, 2003 · N186AW · Boeing 737277 · Light System Wiring
  > DURING C-16 CHECK NUMEROUS CONNECTORS AND SPLICES WERE FOUND DAMAGED ON SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT HARNESS LT SIDE OF AIRCRAFT. MAINTENANCE REMOVED AND REPLACED DAMAGED CONNECTORS AND SPLICES ON SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT HARNESS LT
- [SDR AWXA200300997](https://openairdocs.org/sdr/AWXA200300997.md): Bulkhead · cracked · Aug 17, 2003 · N186AW · Boeing 737277 · Fuselage Main, Bulkhead
  > MCN - MAJOR REPAIR - DURING C-16 CHECK A.375 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 17.1, WL 230. MAINTENANCE CUT OUT DAMAGE ON BS 178 BULKHEAD WEB AT RBL 17.1, WL 230. PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED
- [SDR AWXA200300996](https://openairdocs.org/sdr/AWXA200300996.md): Bulkhead · cracked · Aug 17, 2003 · N186AW · Boeing 737277 · Fuselage Main, Bulkhead
  > DURING C-16 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT LBL 17.1, WL 230. MAINTENANCE CUT OUT DAMAGE ON BS 178 BULKHEAD WEB AT LBL 17.1, WL 230. PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A NEW SECTION OF WEB AND
- [SDR AWXA200301028](https://openairdocs.org/sdr/AWXA200301028.md): Fairing · cracked · Aug 16, 2003 · N186AW · Boeing 737277 · Trailing Edge Flaps
  > DURING C-16 CHECK A.7500 INCH CRACK WAS FOUND ON LT WING NR 1 FLAP TRACK MOVEABLE FAIRING AT UPPER LT AFT CORNER. MAINTENANCE PERFORMED A BOND REPAIR ON LT WING NR 1 FLAP TRACK MOVEABLE FAIRING AT UPPER LT AFT CORNER IAW B737-200 SRM 51-40-09, PG. 3, 8-9.
- [SDR AWXA200300984](https://openairdocs.org/sdr/AWXA200300984.md): Stringer Clip · cracked · Aug 16, 2003 · N186AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-16 CHECK A 1/2 INCH CRACK WAS FOUND ON TOP LEG OF STRINGER CLIP 22 RT, FORWARD SIDE OF BS 787. MAINTENANCE REMOVED CRACKED STRINGER CLIP 22 RT, BS 787; FABRICATED A NEW REPLACEMENT STRINGER CLIP; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, STEP 4
- [SDR AWXA200300983](https://openairdocs.org/sdr/AWXA200300983.md): Stringer Clip · cracked · Aug 16, 2003 · N186AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-16 CHECK A 1/2 INCH CRACK WAS FOUND ON TOP LEG OF STRINGER CLIP 21 RT, FORWARD SIDE OF BS 787. MAINTENANCE REMOVED CRACKED STRINGER CLIP 21 RT, BS 787; FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, STEP 4B-4E,
- [SDR AWXA200301058](https://openairdocs.org/sdr/AWXA200301058.md): Angle · corroded · Aug 15, 2003 · N186AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND AROUND NUT PLATE HOLES ON FORWARD CARGO COMPARTMENT LT TRANSITION ANGLE BETWEEN BS 380 AND BS 480. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED ANGLE BETWEEN BS 38
- [SDR AWXA200301048](https://openairdocs.org/sdr/AWXA200301048.md): Door · cracked · Aug 15, 2003 · N186AW · Boeing 737277 · Leading Edge Devices
  > DURING C-16 CHECK A.3125 INCH CRACK WAS FOUND ON NR 5 SLAT ACTUATOR CLOSE OUT DOOR. MAINTENANCE REMOVED CLOSE OUT DOOR ON NR 5 SLAT AT WBL 435; FABRICATED A NEW REPLACEMENT CLOSE OUT DOOR PER DWG 65C26191; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, PG.
- [SDR AWXA200301041](https://openairdocs.org/sdr/AWXA200301041.md): Skin · cracked · Aug 15, 2003 · N186AW · Boeing 737277 · Leading Edge Devices
  > DURING C-16 CHECK A.1250 INCH CRACK WAS FOUND ON NR 3 SLAT INBOARD MAIN TRACK CLOSE OUT DOOR AT WBL 230 LT. MAINTENANCE REMOVED AND REPLACED NR 3 SLAT INBOARD MAIN TRACK CLOSE OUT DOOR ASSEMBLY AT WBL 230 LT IAW B737-200 SRM 51-30-02, PARA B & E.
- [SDR AWXA200301023](https://openairdocs.org/sdr/AWXA200301023.md): Skin · delaminated · Aug 15, 2003 · N186AW · Boeing 737277 · Trailing Edge Flaps
  > DURING C-16 CHECK THE LT OUTBOARD HINGED FLAP TRAILING EDGE SKIN WAS FOUND DELAMINATED. MAINTENANCE PERFORMED HONEYCOMB REPAIR ON TRAILING EDGE SKIN OF LT OUTBOARD HINGED FLAP IAW B737-200 SRM 51-40-20, FIG. 10, PG. 40-41.
- [SDR AWXA200301024](https://openairdocs.org/sdr/AWXA200301024.md): Skin · delaminated · Aug 15, 2003 · N186AW · Boeing 737277 · Trailing Edge Flaps
  > MCN - MAJOR REPAIR - DURING C-16 CHECK THE RT OUTBOARD HINGED FLAP TRAILING EDGE WEDGE WAS FOUND DELAMINATED ALONG EDGE. MAINTENANCE PERFORMED HONEYCOMB REPAIR ON TRAILING EDGE WEDGE OF RT OUTBOARD HINGED FLAP IAW B737-200 SRM 51-40-20 FIG 10 PG 40-41.
- [SDR AWXA200301019](https://openairdocs.org/sdr/AWXA200301019.md): Frame · cracked · Aug 15, 2003 · N186AW · Boeing 737277 · Leading Edge Devices
  > DURING C-16 CHECK A 1.75 INCH CRACK WAS FOUND ON LT WING LEADING EDGE FORMER AT WS 222.7, JUST INBOARD OF NR 1 PYLON. MAINTENANCE CUT OUT DAMAGE ON LT WING LEADING EDGE FORMER AT WS 222.7 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A
- [SDR AWXA200301011](https://openairdocs.org/sdr/AWXA200301011.md): Skin · cracked · Aug 15, 2003 · N186AW · Boeing 737277 · Trailing Edge Flaps
  > - DURING C-16 CHECK A 0.080 INCH CRACK WAS FOUND ON EDGE OF RT INBOARD HINGED FLAP UPPER SKIN AT WBL 180.75. MAINTENANCE TRIMMED OUT CRACK ON RT INBOARD HINGED FLAP UPPER SKIN AT WBL 180.75 IAW B737-200 SRM 57-50-01 PG 1 FIG 3, SHEETS 2-4.
- [SDR AWXA200300998](https://openairdocs.org/sdr/AWXA200300998.md): Frame · cracked · Aug 15, 2003 · N186AW · Boeing 737277 · Fuselage Main, Frame
  > MCN - MAJOR REPAIR - DURING C-16 CHECK A.625 INCH CRACK WAS FOUND IN RADIUS OF BS 727B FRAME AT STR 25 LT. MAINTENANCE CUTOUT DAMAGE ON BS 727B FRAME AT STR 25 LT; FABRICATED A RADIUS FILLER AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-200 SRM 5
- [SDR AWXA200300987](https://openairdocs.org/sdr/AWXA200300987.md): Beam · cracked · Aug 15, 2003 · N186AW · Boeing 737277 · Fuselage Main, Structure
  > DURING C-16 CHECK A 1/8 INCH CRACK WAS FOUND ON BEAM WEB AT INSULATION MOUNT HOLE BS 184, RBL 17.1, WL 178. MAINTENANCE CUTOUT DAMAGED AREA OF VERTICAL BEAM WEB AT BS 184, RBL 17.1, WL 178, AND PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACK EXISTS; F
- [SDR AWXA200300985](https://openairdocs.org/sdr/AWXA200300985.md): Attach Angle · cracked · Aug 15, 2003 · N186AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-16 CHECK A 5/8 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT SILL WEB TO FRAME ATTACH ANGLE UPPER LEG AT BS 807, RBL 19.5. MAINTENANCE REMOVED CRACKED FRAME ATTACH ANGLE AT BS 807, RBL 19.5; FABRICATED A NEW REPLACEMENT FRAME ATTACH ANGLE; INSTALLED R
- [SDR AWXA200301059](https://openairdocs.org/sdr/AWXA200301059.md): Door · cracked · Aug 14, 2003 · N186AW · Boeing 737277 · Leading Edge Devices
  > DURING C-16 CHECK.1250 INCH CRACK WAS FOUND ON NR 4 SLAT ACTUATOR CLOSE OUT DOOR, WBL 279.25. MAINTENANCE REMOVED CRACKED NR 4 SLAT ACTUATOR CLOSE OUT DOOR; FABRICATED A NEW REPLACEMENT DOOR; INSTALLED REPAIR PART IAW BMM 20--050-011-2, FIG. 203.
- [SDR AWXA200301049](https://openairdocs.org/sdr/AWXA200301049.md): Skin · cracked · Aug 14, 2003 · N186AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > DURING C-16 CHECK A 1.250 CRACK WAS FOUND ON FUSELAGE EXTERNAL SKIN FROM FASTENER HOLE AT AFT RADIO ALTIMETER ANTENNA CUTOUT BS 450, BL 0. MAINTENANCE CUTOUT DAMAGED SKIN AT BS 450, BL 0 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A R
- [SDR AWXA200301052](https://openairdocs.org/sdr/AWXA200301052.md): Skin · cracked · Aug 13, 2003 · N186AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > DURING C-16 CHECK A.5625 INCHES CRACK WAS FOUND ON EXTERNAL FUSELAGE SKIN OF L-1 DOOR CUTOUT AT FASTENER HOLE LOWER AFT CORNER. MAINTENANCE CUTOUT CRACK ON SKIN OF L-1 DOOR CUTOUT LOWER AFT CORNER AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST;
- [SDR AWXA200301038](https://openairdocs.org/sdr/AWXA200301038.md): Skin · cracked · Aug 13, 2003 · N186AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > DURING C-16 CHECK 2 EACH CRACKS WERE FOUND ON EXTERNAL FUSELAGE SKIN AT FASTENER HOLE OF R-2 DOOR CUTOUT AT FORWARD LOWER CORNER. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED AN INNER PLATE, OUTER
- [SDR AWXA200301022](https://openairdocs.org/sdr/AWXA200301022.md): Floorbeam · cracked · Aug 13, 2003 · N186AW · Boeing 737277 · Fuselage Main, Floor Beam
  > DURING C-16 CHECK A.5 INCH CRACK WAS FOUND ON PASSENGER CABIN FLOORBEAM AT BS 520, LBL 24. MAINTENANCE STOP DRILLED CRACK ON FLOORBEAM AT BS 520, LBL 24 AND PERFORMED HFEC INSPECTION TO VERIFY CRACK IS CONTAINED; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED RE
- [SDR AWXA200301016](https://openairdocs.org/sdr/AWXA200301016.md): Skin · cracked · Aug 13, 2003 · N186AW · Boeing 737277 · Leading Edge Devices
  > DURING C-16 CHECK A.75 INCH CRACK WAS FOUND ON LOWER LEADING EDGE OF NR 1 KRUEGER FLAP AT L/E STA 205. MAINTENANCE BLENDED OUT CRACK ON LOWER LEADING EDGE OF NR 1 KRUEGER FLAP AT L/E STA 205 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICAT
- [SDR AWXA200301012](https://openairdocs.org/sdr/AWXA200301012.md): Skin · cracked · Aug 13, 2003 · N186AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > DURING C-16 CHECK A 0.090 INCH CRACK WAS FOUND ON R-2 DOOR EXTERNAL SKIN AT CORNER OF UPPER HINGE CUTOUT. MAINTENANCE TRIMMED OUT CRACK ON R-2 DOOR EXTERNAL SKIN AT CORNER OF UPPER HINGE CUTOUT IAW B737-200 SRM 52-00-2 PG 3, FIG 1 & 6, SHEETS 3 & 6.
- [SDR AWXA200301010](https://openairdocs.org/sdr/AWXA200301010.md): Strap · cracked · Aug 13, 2003 · N186AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-16 CHECK A.5 INCH CRACK WAS FOUND ON FLOOR STRUCTURE TIE STRAP AT BS 342, LBL 1. MAINTENANCE REMOVED CRACKED TIE STRAP AT BS 342, LBL 1; FABRICATED A NEW REPLACEMENT TIE STRAP AND A REPAIR PLATE; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-09 PG 1
- [SDR AWXA200300988](https://openairdocs.org/sdr/AWXA200300988.md): Gusset · cracked · Aug 13, 2003 · N186AW · Boeing 737277 · Fuselage, Landing Gear Attach Fittings
  > DURING C-16 CHECK A 2 INCH CRACK WAS FOUND IN RADIUS OF NOSE LANDING GEAR ACTUATOR MOUNT FITTING ATTACH ANGLE. MAINTENANCE REMOVED AND REPLACED DAMAGED NOSE LANDING GEAR ACTUATOR MOUNT FITTING ATTACH ANGLE IAW B737-200 SRM 51-30-02, PG. 1, FIG. 007, & SRM 51-3
- [SDR AWXA200300986](https://openairdocs.org/sdr/AWXA200300986.md): Bracket · cracked · Aug 13, 2003 · N186AW · Boeing 737277 · Trailing Edge Flaps
  > DURING C-16 CHECK A 3/16 INCH CRACK WAS FOUND ON NR 2 SLAT INBOARD AUXILIARY TRACK CLOSE-OUT DOOR AFT SPRING ATTACH BRACKET AT WS 404.8. MAINTENANCE REMOVED AND REPLACED THE CRACKED NR 2 SLAT INBOARD AUXILIARY TRACK CLOSEOUT DOOR AFT SPRING ATTACH BRACKET AT W
- [SDR AWXA200301051](https://openairdocs.org/sdr/AWXA200301051.md): Angle · cracked · Aug 12, 2003 · N186AW · Boeing 737277 · Nacelle/Pylon, Main Frame
  > DURING C-16 CHECK A 1 1/8 INCH CRACK WAS FOUND ON NR 1 ENGINE RT FORWARD COWL LOWER ZEE ANGLE AT RIB 7, NAC STA 151. MAINTENANCE CUTOUT CRACK ON RIB 7; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-200 SRM 54-40-03, FIG. 001.
- [SDR AWXA200301042](https://openairdocs.org/sdr/AWXA200301042.md): Floorbeam · cracked · Aug 12, 2003 · N186AW · Boeing 737277 · Fuselage Main, Floor Beam
  > DURING C-16 CHECK A.5625 INCH CRACK WAS FOUND ON FLOORBEAM REPAIR BS 677, RBL 24. MAINTENANCE REMOVED REPAIR ANGLE AND 2 EACH DOUBLERS; FABRICATED A NEW REPLACEMENT REPAIR CHANNEL AND 3 EACH DOUBLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 15-5715-03240-ES2.
- [SDR AWXA200301021](https://openairdocs.org/sdr/AWXA200301021.md): Floorbeam · cracked · Aug 12, 2003 · N186AW · Boeing 737277 · Fuselage Main, Floor Beam
  > DURING C-16 CHECK.875 INCH CRACK WAS FOUND ON PASSENGER CABIN FLOORBEAM AT BS 644, LBL 45. MAINTENANCE CUT OUT DAMAGE ON FLOORBEAM AT BS 694, LBL 45; FABRICATED A FILLER AND 3 EACH REPAIR PLATES; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-40-04 FIG 1 PG 1.
- [SDR AWXA200301020](https://openairdocs.org/sdr/AWXA200301020.md): Floorbeam · cracked · Aug 12, 2003 · N186AW · Boeing 737277 · Fuselage Main, Floor Beam
  > DURING C-16 CHECK 2 EACH 1.25 INCH CRACKS WERE FOUND ON PASSENGER CABIN FLOORBEAM AT BS 674, RBL 45. MAINTENANCE CUT OUT DAMAGE ON FLOORBEAM AT BS 674, RBL 45; FABRICATED A REPAIR EXTRUSION AND 3 EACH REPAIR PLATES; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-
- [SDR AWXA200301043](https://openairdocs.org/sdr/AWXA200301043.md): Skin · cracked · Aug 11, 2003 · N186AW · Boeing 737277 · Nacelle/Pylon, Plate/Skin
  > DURING C-16 CHECK A 1 INCH CRACK WAS FOUND ON NR 2 ENGINE LT FORWARD COWL INNER SKIN UNDER UPPER FORWARD SAFETY LATCH. MAINTENANCE CUTOUT CRACKED SKIN ON NR 2 ENGINE LT FORWARD COWL INNER SKIN NAC STA 120 RT; FABRICATED A DOUBLER, SHIM AND FILLER; INSTALLED RE
- [SDR AWXA200301029](https://openairdocs.org/sdr/AWXA200301029.md): Flap · debonded · Aug 11, 2003 · N186AW · Boeing 737277 · Trailing Edge Flaps
  > DURING C-16 CHECK THE UPPER SURFACE OF THE RT INBOARD FORE-FLAP WAS FOUND DISBONDING 33 INCH TO 37 INCH FROM THE OUTBOARD END. MAINTENANCE PERFORMED HONEYCOMB CORE REPAIR ON RT INBOARD FORE-FLAP IAW B737-200 SRM 51-40-20, REPAIR NR 9, FIG. 18, PG. 63-67.
- [SDR AWXA200300689](https://openairdocs.org/sdr/AWXA200300689.md): Light · defective · Jun 11, 2003 · N186AW · Boeing 737277 · Emergency Lighting
  > LAS - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200300605](https://openairdocs.org/sdr/AWXA200300605.md): Battery · discharged · May 28, 2003 · N186AW · Boeing 737277 · Emergency Lighting
  > DURING 8-DAY CHECK THE EMERGENCY EXIT LIGHT ABOVE THE R-2 DOOR WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY AT EMERGENCY EXIT LIGHT ABOVE THE R-2 DOOR, OPERATIONAL CHECK WAS GOOD.

Next page: https://openairdocs.org/deregistered/N186AW-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 = 'N186AW' AND deregistration_id = 'N186AW-2005-03-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N186AW-2005-03-16/reports

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