# Service difficulty reports: N184AW, cancelled Jul 16, 2013

A list on [N184AW, cancelled Jul 16, 2013](https://openairdocs.org/deregistered/N184AW-2013-07-16.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 3 · 134 reports

- [SDR AWXA200400021](https://openairdocs.org/sdr/AWXA200400021.md): Bearing · seized · Jan 7, 2004 · N184AW · Boeing 737277 · Air Distribution Fan
  > AFTER LANDING & TAXING TO HOLD BAY, SHORTLY AFTER NR 2 ENG SHUTDOWN COCKPIT BEGAN TO DEVELOP AN ACRID ELEC BURNING ODOR FOLLOWED BY LIGHT BLUE SMOKEY HAZE. TURNED OFF GASPER FAN & WINDOW HEAT, ODOR SUBSIDED. MAINT TROUBLESHOT, FOUND FLT DECK CABIN AIR COND FAN
- [SDR AWXA200400024](https://openairdocs.org/sdr/AWXA200400024.md): Wire · damaged · Jan 4, 2004 · N184AW · Boeing 737277 · Auto Flight System Wiring
  > ON CLIMBOUT, WHEN AUTOPILOT-B ENGAGED A/C BANKED HARD RT PAST 30 DEGREES. REATTEMPTED TO ENGAGE AUTOPILOT-B SAME RESULTS. AS SOON AS AUTOPILOT-B ENGAGED CONTROL WHEEL STEERING INDICATED ROLL RT, AUTOPILOT-A NORMAL. MAINT TROUBLESHOT AUTOPILOT SYS, B-SYS GOE
- [SDR AWXA200301095](https://openairdocs.org/sdr/AWXA200301095.md): Line · leaking · Sep 23, 2003 · N184AW · Boeing 737277 · Hydraulic System, Main
  > DURING DECENT INTO DFW EN ROUTE FROM PHX (A) SYSTEM HYDRAULIC QUANTITY INDICATOR BEGAN SHOWING LOSS OF FLUID. FLUID LEVEL DROPPED TO APPROX.7500 OF A GAL REMAINING. EMERGENCY EQUIPMENT CALLED OUT AS A PRECAUTION. MAINTENANCE FOUND THE NOSE LANDING GEAR ACTUA
- [SDR AWXA200300721](https://openairdocs.org/sdr/AWXA200300721.md): Pump · failed · Jun 20, 2003 · N184AW · Boeing 737277 · Hydraulic Pump (Electric/Engine), Main
  > ON DEPARTURE, LOST A-SYSTEM HYDRAULIC PRESSURE, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. AIRCRAFT TOWED BACK TO GATE. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP HAD FAILED, REMOVED AND REPLACED PUMP. A-SYSTEM HYDRAULICS FLUSHED, OPERATIONAL
- [SDR AWXA200300142](https://openairdocs.org/sdr/AWXA200300142.md): Module · failed · Feb 14, 2003 · N184AW · Boeing 737277 · Leading Edge Slat Position Indicating System
  > PHX - ABORTED TAKEOFF - FLT 0445 - ON TAKEOFF AT PHX EN ROUTE FOR TUS RECEIVED AMBER LEADING EDGE FLAP IN TRANSIT LIGHT ON FORWARD PANEL WHILE FLAPS SELECTED TO 2 UNIT; REJECTED TAKEOFF AT 50 KTS. AFTER TAXI OFF RUNWAY AND SITTING ON TAXIWAY, THE IN TRANSIT LI
- [SDR AWXA200201041](https://openairdocs.org/sdr/AWXA200201041.md): Sign · broken · Oct 18, 2002 · N184AW · Boeing 737277 · Emergency Lighting
  > DURING C-20 CHECK THE FORWARD SERVICE DOOR EMERGENCY EXIT SIGN WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE FORWARD SERVICE DOOR EMERGENCY EXIT SIGN, OPERATIONAL CHECK WAS GOOD IAW AWA T/C A1C33006.
- [SDR AWXA200201031](https://openairdocs.org/sdr/AWXA200201031.md): Door Frame · corroded · Oct 15, 2002 · N184AW · Boeing 737277 · Fuselage Main, Structure
  > DURING C-20 CHECK CORROSION WAS FOUND AT THE L-1 DOOR SILL INNER CHORD UNDER DRAIN TROUGH BS 333, LBL 50. MAINTENANCE REMOVED 2 EACH ANGLES AT BS 312 AND 344, A WEB AT BS 277 - 306, A FRAME BS 300, AND AN ANGLE BS 277 - 284 FOR ACCESS, REMOVED DAMAGED DOOR SIL
- [SDR AWXA200201030](https://openairdocs.org/sdr/AWXA200201030.md): Stiffener · cracked · Oct 15, 2002 · N184AW · Boeing 737277 · Fuselage Main, Floor Beam
  > YVR - MAJOR REPAIR - DURING C-20 CHECK A 1/2" CRACK WAS FOUND ON AFT SIDE OF CABIN FLOOR BEAM INTERCOASTAL ATTACH ANGLE (STIFFENER) BS 328, LBL 47. MAINTENANCE REMOVED DAMAGED INTERCOASTAL ATTACH ANGLE AT BS 328, LBL 47; FABRICATED A NEW REPLACEMENT ATTACH ANG
- [SDR AWXA200201056](https://openairdocs.org/sdr/AWXA200201056.md): Crease Beam · cracked · Oct 7, 2002 · N184AW · Boeing 737277 · Fuselage Main, Structure
  > DURING C-20 CHECK A 1/2 INCH CRACK WAS FOUND ON CREASE BEAM STRINGER 17 LT, BS 360 - BS 380. MAINTENANCE REMOVED WEBS BETWEEN BS 360 TO BS 400 AND BS 400 TO BS 420; CUT STRINGER 17 AT BS 396; FABRICATED A REPAIR ANGLE; INSTALLED STRINGER REPAIR AND WEBS IAW B7
- [SDR AWXA200201027](https://openairdocs.org/sdr/AWXA200201027.md): Skin · cracked · Oct 4, 2002 · N184AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > DURING C-20 CHECK A 1 1/2 INCH CRACK WAS FOUND ON FUSELAGE SKIN L-1 DOOR CUTOUT BELOW LOWER SCUFF PLATE, APPROXIMATELY 10 INCH FORWARD OF AFT LOWER CORNER BS 334 - 336, STR 17 LT. MAINTENANCE REMOVED EXISTING REPAIR DOUBLER, STRAP, WEB, AND COVER PLATE AT BS 3
- [SDR AWXA200201026](https://openairdocs.org/sdr/AWXA200201026.md): Frame · cracked · Oct 4, 2002 · N184AW · Boeing 737277 · Fuselage Main, Frame
  > YVR - MAJOR REPAIR - DURING C-20 CHECK A 1/4" CRACK WAS FOUND ON FRAME AT BS 312, BETWEEN STR 5 - STR 6 L/H. MAINTENANCE STOP DRILLED CRACK AT BS 312, BETWEEN STR 5 - STR 6 L/H; PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A FRAME REPA
- [SDR AWXA200201025](https://openairdocs.org/sdr/AWXA200201025.md): Attach Angle · cracked · Oct 4, 2002 · N184AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > YVR - MAJOR REPAIR - DURING C-20 CHECK A 3/4" CRACK WAS FOUND ON ATTACH ANGLE AT BS 360, STR 11 L/H, JUST AFT OF L-1 DOOR. MAINTENANCE REMOVED THE DAMAGED ATTACH ANGLE AT BS 360, STR 11 L/H; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW
- [SDR AWXA200201024](https://openairdocs.org/sdr/AWXA200201024.md): Flap Track · cracked · Oct 4, 2002 · N184AW · Boeing 737277 · Trailing Edge Flaps
  > DURING C-20 CHECK A 1/4 INCH CRACK WAS FOUND ON THE NR 7 FLAP TRACK AT THE INBOARD ROLLER OF UPPER TRACK, AFT END. MAINTENANCE REMOVED AND REPLACED THE DAMAGED NR 7 FLAP TRACK AT THE INBOARD ROLLER OF UPPER TRACK, AFT END IAW AWA T/C R3R27004.
- [SDR AWXA200201057](https://openairdocs.org/sdr/AWXA200201057.md): Skin · corroded · Oct 3, 2002 · N184AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > YVR - MAJOR REPAIR - DURING C-20 CHECK PITTING CORROSION WAS FOUND ON THE L/H WING LOWER SKIN AT THE #2 TRAILING EDGE FLAP TRACK ATTACH POINT WS 254 L/H. MAINTENANCE PREPARED AREA AT L/H WING LOWER SKIN FLAP TRACK ATTACH POINT WS 254 L/H; REMOVED CORROSION; TR
- [SDR AWXA200201028](https://openairdocs.org/sdr/AWXA200201028.md): Skin · cracked · Oct 3, 2002 · N184AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > YVR - MAJOR REPAIR - DURING C-20 CHECK A 1/4" CRACK WAS FOUND ON FUSELAGE SKIN OF R-2 DOOR UPPER HINGE CUTOUT AT FORWARD UPPER CORNER BS 957.5, WL 240. MAINTENANCE TRIMMED OUT R-2 DOOR UPPER HINGE CUTOUT AT FORWARD UPPER CORNER BS 957.5, WL 240 BY.040" AND PE
- [SDR AWXA200200686](https://openairdocs.org/sdr/AWXA200200686.md): Light · inoperative · Jul 31, 2002 · N184AW · Boeing 737277 · Emergency Lighting
  > LAS - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 6 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 6 LT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200200671](https://openairdocs.org/sdr/AWXA200200671.md): Terminal · broken · Jul 26, 2002 · N184AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 6 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE TERMINAL CONNECTOR AT SEAT ROW 6 L/H, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200200426](https://openairdocs.org/sdr/AWXA200200426.md): Hose · burst · May 15, 2002 · N184AW · Boeing 737277 · Hydraulic Pressure Indicator
  > PHX - EMERGENCY LANDING - FLT 0332 - EN ROUTE FROM SLC TO PHX THE "A" HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED AND THEN THE GAUGE FLUCTUATED BACK AND FORTH, FLIGHT CREW DECLARED AN EMERGENCY AND LANDED SAFELY AT SCHEDULED DESTINATION. MAINTENANCE PRESSU
- [SDR AWXA200200356](https://openairdocs.org/sdr/AWXA200200356.md): Battery · discharged · Apr 22, 2002 · N184AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - EMERGENCY ESCAPE PATH SEAT LIGHTS ON ALL SEATS EXCEPT LAST FIVE ROWS AND EMERGENCY EXIT LIGHTS AT L1 AND L2 DOOR ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED 2 EACH EMERGENCY LIGHTING BATTERY PACKS UNDER SEATS AT ROWS 3 AND 11 LT IAW BMM 33-5
- [SDR AWXA200200210](https://openairdocs.org/sdr/AWXA200200210.md): Wire · broken · Mar 10, 2002 · N184AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - "C" - EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 L/H INOPERATIVE. MAINTENANCE REPAIRED WIRE PULLED FROM SPLICE AT SEAT ROW 13 L/H, FUNCTIONAL CHECK WAS GOOD IAW T/C A1C33006.
- [SDR AWXA200200186](https://openairdocs.org/sdr/AWXA200200186.md): Charger · failed · Mar 2, 2002 · N184AW · Boeing 737277 · Battery/Charger System
  > CLIMBOUT ELEC ODOR 7000 FT, NO SMOKE. TURNED BACK. PWR REDUCED, ODOR SUBSIDED. MX ENTERED COCKPIT, SMELL SIMILAR TO BURNT RESISTOR. ALL C/B PNL LT & RT LOAD CNTL CENTER INSP FOR DAMAGE/ELEC ODOR, NONE FOUND. CIRCUIT CARDS IN P6 PNL INSP, M560 FOUND W/ OVER
- [SDR AWXA200200121](https://openairdocs.org/sdr/AWXA200200121.md): Light · inoperative · Feb 9, 2002 · N184AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - C - DURING INSPECTION EMERGENCY EXIT LIGHT ON SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SEAT LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK C/W IAW T/C A1C33009.
- [SDR AWXA200200022](https://openairdocs.org/sdr/AWXA200200022.md): Warning System · malfunctioned · Jan 12, 2002 · N184AW · Boeing 737277 · Brake Anti-Skid Section
  > PHX - ABORTED T/O - FLT 644 - S - UPON RELEASE OF BRAKES FLIGHT CREW RECEIVED AMBER WARNING MESSAGES FOR INBOARD AND OUTBOARD ANTI-SKID CHANNELS INOPERATIVE AND AUTO-BRAKES, AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE. AT GATE MAINTENANCE ISSUED A DPI, MEL
- [SDR AWXA200100672](https://openairdocs.org/sdr/AWXA200100672.md): Light · missing · Dec 27, 2001 · N184AW · Boeing 737277 · Emergency Lighting
  > LAS - EEL - EMERGENCY PATH LIGHT ASSEMBLY MISSING SEAT ROW 12 LT SIDE. MAINTENANCE REPLACED LIGHT ASSEMBLY AT SEAT ROW 12 LT SIDE, FUNCTIONAL CHECK WAS GOOD.
- [SDR AWXA200100599](https://openairdocs.org/sdr/AWXA200100599.md): Battery Pack · discharged · Nov 27, 2001 · N184AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - C - DURING ROUTINE MAINTENANCE INSPECTION FOUND R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT R1 DOOR, OPERATIONAL CHECK GOOD.
- [SDR AWXA200100577](https://openairdocs.org/sdr/AWXA200100577.md): Connector · worn · Nov 5, 2001 · N184AW · Boeing 737277 · Autopilot Trim Servo
  > AFTER T/O, HEARD LOUD THUMP DURING GEAR RETRACTION, INDICATIONS NORM. IN FLT W/AP ENGAGED ACFT STARTED PORPOISING. AP WAS DISENGAGED, DIFFICULTY CONTROLLING PITCH ATTITUDE. DIVERTED. ON APPROACH 165 KTS BUFFETING FELT, FLAPS 15, 170 KTS. FERRIED, A COMPLETE V
- [SDR AWXA200100498](https://openairdocs.org/sdr/AWXA200100498.md): Floorbeam · cracked · Sep 27, 2001 · N184AW · Boeing 737277 · Fuselage Main, Floor Beam
  > YVR - C19 CK -LONGITUDINAL SEAT TRACK SUPPORT BEAM, LBL 24.5 CRACKED AT BOLT RELIEF HOLE, BS 679. MAINTENANCE MADE REPAIRS IAW AWA ER 15-5710-01269-JS1, REFERENCING BOEING S/B 737-57-1139, REV 4, FIG6.
- [SDR AWXA200100495](https://openairdocs.org/sdr/AWXA200100495.md): Floorbeam · cracked · Sep 13, 2001 · N184AW · Boeing 737277 · Fuselage Main, Floor Beam
  > YVR - C19 CK -RT OVERWING SEAT TRACK AILERON CUTOUT STRUCTURE AT RT I/B SEAT TRACK BS 658 VERT FLANGE CRACKED.3125 INCH. VISIBLE THROUGH CUTOUT UNDER STRUCTURE OF CLOSED FLOOR PANEL. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR IAW AWA ER 15-5710-0126
- [SDR AWXA200100494](https://openairdocs.org/sdr/AWXA200100494.md): Floorbeam · cracked · Sep 13, 2001 · N184AW · Boeing 737277 · Fuselage Main, Floor Beam
  > YVR - C19 CK - RT OVERWING PRESSURE DECK LOWER VERT CHORD AT BS 698, RBL 24.82 CRACKED.5 INCH. MAINTENANCE TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED IAW AWA ER 15-5702-01271-SS2.
- [SDR AWXA200100492](https://openairdocs.org/sdr/AWXA200100492.md): Skin · cracked · Sep 9, 2001 · N184AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > YVR - C19 CK - L2 DOOR CUTOUT, LOWER FWD CORNER, FUSELAGE SKIN CRACKED IN 3 PLACES (1 INCH). MAINTENANCE ROUTED OUT THE CRACK IN THE FUSELAGE SKIN, DOUBLER AND BEARSTRAP. FABRICATED AND INSTALLED REPAIR IAW B737 SRM 53-30-3, FIG 24, PG 83.
- [SDR AWXA200100497](https://openairdocs.org/sdr/AWXA200100497.md): Floorbeam · corroded · Sep 7, 2001 · N184AW · Boeing 737277 · Fuselage Main, Floor Beam
  > YVR - C19 CK - FLOORBEAM AT BS 987 TOP SURFACE HAS CORROSION BETWEEN LBL 30 AND RBL 12. MAINTENANCE REMOVED PREVIOUS BEAM CAP REPAIR, FABRICATED NEW BEAM CAP AND INSTALLED IAW B737 SRM 53-10-9, FIG 2, PG 7.
- [SDR AWXA200100496](https://openairdocs.org/sdr/AWXA200100496.md): Floorbeam · corroded · Sep 7, 2001 · N184AW · Boeing 737277 · Fuselage Main, Floor Beam
  > YVR - C19 CK - FLOORBEAM AT BS 967 HAS CORROSION BETWEEN BL 0 AND RBL 30 ON TOP SURFACE. AFTER CORROSION REMOVAL, MATERIAL LOSS BEYOND SRM LIMITS. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM TOP CAP AND REPLACED IAW B737 SRM 53-10-9, FIG 2, PG 7.
- [SDR AWXA200100491](https://openairdocs.org/sdr/AWXA200100491.md): Skin · cracked · Sep 6, 2001 · N184AW · Boeing 737277 · Fuselage, Door Hinge
  > YVR - C19 CK - "C" - L2 DOOR, FUSELAGE TORQUE BOX INNER SKIN 2" CRACK BS 952, BETWEEN STR 11R & 12R. MAINTENANCE FABRICATED REINFORCEMENT STRAP AND INSTALLED IAW AWA ER 15-5345-01264-TB4, REFERENCING PROCEDURES IN BOEING SB 737-53-1094.
- [SDR AWXA200100499](https://openairdocs.org/sdr/AWXA200100499.md): Angle · cracked · Sep 4, 2001 · N184AW · Boeing 737277 · Fuselage, Landing Gear Attach Fittings
  > YVR - C19 CK - "C" - NOSE LANDING GEAR ACTUATOR UPPER ATTACH SUPPORT FITTING VERTICAL WEB CRACKS EMINATING FROM 3 RIVIT HOLES, EACH CRACK ABOUT.25". MAINTENANCE REMOVED DAMAGED FITTING, FABRICATED A NEW ANGLE (FITTING) AND INSTALLED IAW BOEING INSTALLATION
- [SDR AWXA200100493](https://openairdocs.org/sdr/AWXA200100493.md): Bulkhead · cracked · Sep 4, 2001 · N184AW · Boeing 737277 · Fuselage Main, Bulkhead
  > YVR - C19 CK - BS 178 PRESS. BULKHEAD FWD FACE,.050 CRACK EMANATING FROM FASTENER HOLE, WL 234, RBL 5.7. MAINTENANCE REPAIRED IAW B737 SRM 53-10-11, FIG 1, DETAIL II, PG 5.
- [SDR AWXA200100490](https://openairdocs.org/sdr/AWXA200100490.md): Crossbeam · cracked · Sep 4, 2001 · N184AW · Boeing 737277 · Cargo/Baggage Doors
  > YVR - C19 CK - "C" - FWD CARGO DOOR LOWER CROSSBEAM WEB, TWO CRACKS FOUND, ONE ON FWD END AND ONE ON THE AFT END. BOTH CRACKS ARE.5 INCH. MAINTENANCE REPAIRED THE CARGO DOOR IAW AWA E.O.52-31-04, SHEETS 1 - 18.
- [SDR AWXA0001045](https://openairdocs.org/sdr/AWXA0001045.md): Frame · cracked · Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, Frame
  > BS 178 WL 207 BULKHEAD L/H O/B SIDE CHORD CRACKED. CHORD REPLACED IAW SRM 51-10-01 DWG 65-16300
- [SDR AWXA0001044](https://openairdocs.org/sdr/AWXA0001044.md): Intercostal · cracked · Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, Bulkhead
  > STA 178 WL 207 LBL 28 LT O/B WEB CRACKED AT RIVET HOLE. WEB REPLACED IAW SRM 51-10-01 DWG 65-45833
- [SDR AWXA0001043](https://openairdocs.org/sdr/AWXA0001043.md): Attach Angle · cracked · Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, Structure
  > RT O/B ANGLE AT STA 178 WL 195 RBL 25 CRACKED IN RADIUS. ANGLE REPLACED IAW SRM 51-10-01 DWG 65-16300
- [SDR AWXA0001042](https://openairdocs.org/sdr/AWXA0001042.md): Attach Angle · cracked · Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, Structure
  > LEFT OUTBOARD T CHORD AT STA 178 WL 195 LBL 24.67 WAS CRACKED. ATTACHED ANGLES REPLACED IAW SRM 51-10-01 DWG 65-16300
- [SDR AWXA0001041](https://openairdocs.org/sdr/AWXA0001041.md): Bulkhead · cracked · Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, Bulkhead
  > FWD PRESSURE BULKHEAD HAS TWO CRACK INDICATIONS ON WEB AT STA 178 WL 218 BEHIND STIFFENERS L&R OF BL 0. WEB CRACKS REPAIRED IAW SRM 53-10-11 FIG 1 DET. III.
- [SDR AWXA0001040](https://openairdocs.org/sdr/AWXA0001040.md): Frame · cracked · Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, Frame
  > STA 178 WL 200 RBL 26 SIDE CHORD CRACKED. CHORD REPLACED IAW SRM 51-10-01 DWG 65-16300
- [SDR AWXA0001039](https://openairdocs.org/sdr/AWXA0001039.md): Intercostal · cracked · Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, Bulkhead
  > INTERCOSTAL AT BS 178 WL 207 RBL 26 CRACKED. REPLACED WEB/INTERCOSTAL IAW SRM 51-10-01 DWG 61-45833
- [SDR AWXA0001038](https://openairdocs.org/sdr/AWXA0001038.md): Floorbeam · cracked · Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, Floor Beam
  > OUTBOARD T-CHORD AT STA 178 WL 207 IS CRACKED THROUGH AT FWD FASTENER HOLE. REPAIRED IAW SRM 51-40-4 FIG 1 DWG 65-45833
- [SDR AWXA0001037](https://openairdocs.org/sdr/AWXA0001037.md): Skin · cracked · Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > CRACK INDICATION ON FUSELAGE APPROX BS 747 STR 17R. REPAIR CARRIED OUT IAW ENG. REPAIR NO. 15-5331-00334-J51
- [SDR AWXA0001036](https://openairdocs.org/sdr/AWXA0001036.md): Bracket · cracked · Dec 8, 2000 · N184AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > STA 178 GLIDE SLOPE ANTENNA SUPPORT BRACKET LOWER LT CORNER CRACKED. STOP DRILLED END OF CRACK AND REPAIRED IAW SRM 51-40-3
- [SDR AWXA0000573](https://openairdocs.org/sdr/AWXA0000573.md): Shear Tie · cracked · Aug 18, 2000 · N184AW · Boeing 737277 · Fuselage Main, Structure
  > C-CHECK, SHEAR TIE CRACKED AT STA 887 27R - 27L. REMOVED DAMAGED PORTION OF SHEAR TIE, FABRICATED AND INSTALLED REPAIR PARTS IAW 737 SRM 53-10-4 AND SRM 53-10-4.
- [SDR AWXA0000572](https://openairdocs.org/sdr/AWXA0000572.md): Stringer Clip · misdrilled · Aug 18, 2000 · N184AW · Boeing 737277 · Fuselage Main, Longeron/Stringer
  > C-CHECK, LONGERON CLIP AT FS 887 LONG 27R HAS ELONGATED HOLES. REMOVED AND REPLACED CLIP IAW 737 SRM 51-30-2.
- [SDR AWXA0000571](https://openairdocs.org/sdr/AWXA0000571.md): Bulkhead · misdrilled · Aug 18, 2000 · N184AW · Boeing 737277 · Fuselage Main, Bulkhead
  > C-CHECK, INADVERTANT 1.25 HOLES DRILLED IN BULKHEAD AT FS 727 LBL 40.5, WL 193. REPAIRED IAW ER 15-5363-00214-BA2.
- [SDR AWXA0000570](https://openairdocs.org/sdr/AWXA0000570.md): Bracket · cracked · Aug 18, 2000 · N184AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > C-CHECK, LEFT FS 663.75 AFT SIDE OF FRAME PRESSURE DECK HAS CRACK. REMOVED CRACKED BRACKET, FABRICATED NEW BRACKET AND INSTALLED IAW 737 SRM 51-30-2 AND DWG 65-50733.

Next page: https://openairdocs.org/deregistered/N184AW-2013-07-16/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 = 'N184AW' AND deregistration_id = 'N184AW-2013-07-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N184AW-2013-07-16/reports

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