# Service difficulty reports: N183AW, cancelled Feb 1, 2005

A list on [N183AW, cancelled Feb 1, 2005](https://openairdocs.org/deregistered/N183AW-2005-02-01.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 · 129 reports

- [SDR TSAA0171060](https://openairdocs.org/sdr/TSAA0171060.md): Engine · false indication · Aug 11, 2004 · N183AW · Boeing 737277 · Power Indicating System
  > NON-ETOPS FLIGHT 64, HNL-ITO: ABORTED TAKEOFF DUE TO 4 THRUST LEVER SPLIT. WITH THE NR 1 LEVER FORWARD OF THE NR 2, THE NR 2 ENGINE INDICATES 2.0 EPR WHILE THE NR 1 ENGINE INDICATED 1.7 EPR. JET-CAL THE NR 1 AND NR 2 ENGINES IAW FORM M-215, GROUND OPS CHECK
- [SDR AWXA200301206](https://openairdocs.org/sdr/AWXA200301206.md): Pump · inoperative · Oct 11, 2003 · N183AW · Boeing 737277 · Hydraulic Pump (Electric/Engine), Main
  > ON CLIMB OUT OF PHX EN ROUTE FOR SJC LOST (A) SYS HYDS, TURNED BACK TO PHX & LANDED WITHOUT EVENT. MAINT R & R NR 2 EDP IAW T/C R5M29001. R & R (A) HYD SYS CASE DRAIN, PRESSURE, & RETURN FILTERS, FLUSHED SYSTEM IAW BMM 29-11-0, PG. 204. LEAK AND OPERATIONAL CH
- [SDR AWXA200301086](https://openairdocs.org/sdr/AWXA200301086.md): Wire · broken · Sep 22, 2003 · N183AW · Boeing 737277 · Light System Wiring
  > DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200301006](https://openairdocs.org/sdr/AWXA200301006.md): Valve · binding · Sep 1, 2003 · N183AW · Boeing 737277 · Fuel Heater
  > EN ROUTE FROM ONT TO PHX AT CRUISE RECEIVED HIGH OIL TEMPERATURE LIGHT, FOLLOWED QUICK REFERENCE HANDBOOK AND SHUTDOWN THE NO. 1 ENGINE, LANDED AT PHX WITHOUT FURTHER EVENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE FUEL HEAT VALVE STUCK IN THE OPEN POSIT
- [SDR AWXA200300575](https://openairdocs.org/sdr/AWXA200300575.md): Wire · broken · May 21, 2003 · N183AW · Boeing 737277 · Light System Wiring
  > DURING INSPECTION MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 14 AND 19 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 14 LT, AND REPAIRED A BROKEN WIRE AT SEAT ROW 19 LT. OPERATIONAL C
- [SDR AWXA200300217](https://openairdocs.org/sdr/AWXA200300217.md): Indicator · failed · Mar 2, 2003 · N183AW · Boeing 737277 · Attitude and Direction Data System
  > ON CLIMB OUT FROM SLC EN ROUTE TO PHX THE CAPTAINS ATTITUDE DIRECTOR INDICATOR (ADI) "ATT" RED FLAG APPEARED, AND "PITCH" AND "ROLL" COMPARATOR LIGHTS ILLUMINATED. SWITCHED TO CAPTAINS ON AUX WITH NO HELP; TURNED BACK TO SLC. MAINTENANCE REMOVED AND REPLACED T
- [SDR AWXA20030021A](https://openairdocs.org/sdr/AWXA20030021A.md): Turbine Blades · fractured · Feb 27, 2003 · N183AW · Boeing 737277 · Turbine Section
  > SLC - ABORTED TAKEOFF - FLT 0220 - ON TAKEOFF ROLL AT SLC EN ROUTE FOR PHX FELT STRONG VIBRATION FROM R/H SIDE OF AIRCRAFT AND IN R/H THRUST LEVER. ALL ENGINE INDICATIONS WERE NORMAL AT THIS POINT WITH NO WARNING INDICATIONS. REJECTED TAKEOFF AT 130 KTS INDICA
- [SDR AWXA200300214](https://openairdocs.org/sdr/AWXA200300214.md): Engine · malfunctioned · Feb 27, 2003 · N183AW · Boeing 737277 · Engine (Turbine/Turboprop)
  > ON TAKEOFF ROLL AT SLC EN ROUTE FOR PHX FELT STRONG VIBRATION FROM RT SIDE OF AIRCRAFT AND IN RT THRUST LEVER. ALL ENGINE INDICATIONS WERE NORMAL AT THIS POINT WITH NO WARNING INDICATIONS. REJECTED TAKEOFF AT 130 KTS INDICATED AIRSPEED. AS POWER WAS PULLED TO
- [SDR AWXA200300099](https://openairdocs.org/sdr/AWXA200300099.md): Actuator · worn · Jan 31, 2003 · N183AW · Boeing 737277 · Drag Control Actuator
  > SLC - AIR TURN BACK - ON CLIMB OUT FROM SLC EN ROUTE FOR PHX FLIGHT ATTENDANT REPORTED AN EXTREMELY LOUD NOISE AND VIBRATION IN FLOOR BOARDS OF AFT CABIN, TURNED BACK TO SLC AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE PERFORMED GROUND INSPECTION OF FUSELAGE
- [SDR AWXA200201229](https://openairdocs.org/sdr/AWXA200201229.md): Wire · broken · Dec 17, 2002 · N183AW · Boeing 737277 · Light System Wiring
  > FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 16 LT, LIGHT REMAINS INOPERATIVE. SUSPECT BAD SPLICE, PLACED EMERGENCY LIGHT AT SEAT
- [SDR AWXA200201165](https://openairdocs.org/sdr/AWXA200201165.md): Hydraulic System · low · Dec 5, 2002 · N183AW · Boeing 737277 · Hydraulic Indicating System
  > AIR TURN BACK - FLT 0624 - SHORTLY AFTER TAKEOFF OBSERVED HYD QTY STARTING TO DROP, QUANTITY CONTINUED TO DROP TO 1.5 GALLONS. QUANTITY LEVEL WAS JUST ABOVE REFILL LINE PRIOR TO DEPARTURE, TURNED BACK TO OAK AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE IN OAK
- [SDR AWXA200200859](https://openairdocs.org/sdr/AWXA200200859.md): Battery Pack · discharged · Sep 3, 2002 · N183AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - DURING INSPECTION OF EMERGENCY LIGHT SYSTEM THE COCKPIT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT THE COCKPIT EMERGENCY LIGHT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200200824](https://openairdocs.org/sdr/AWXA200200824.md): Web · cracked · Aug 20, 2002 · N183AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 2" CRACK WAS FOUND ON TORQUE BOX WEB AT BS 1138 L/H. MAINTENANCE CUTOUT DAMAGE AT TORQUE BOX WEB, FABRICATED A REPAIR DOUBLER, AND INSTALLED REPAIR IAW B737-200 SRM 51-40-2, PG. 1-3, FIG. 1, SRM 51-10-2, PG.7 & 32, FIG.
- [SDR AWXA200200806](https://openairdocs.org/sdr/AWXA200200806.md): Intercostal · cracked · Aug 15, 2002 · N183AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.5 INCH CRACK WAS FOUND ON INTERCOSTAL IN THE AFT CARGO COMPARTMENT AT BS 800, RBL 43, WL 164. MAINTENANCE REMOVED DAMAGED INTERCOSTAL AT BS 800, RBL 43, WL 164. FABRICATED A NEW REPLACEMENT INTERCOSTAL, AND INSTALLED
- [SDR AWXA200200831](https://openairdocs.org/sdr/AWXA200200831.md): Floorbeam · cracked · Aug 12, 2002 · N183AW · Boeing 737277 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.75 INCH CRACK WAS FOUND IN THE UPPER FLANGE OF LONGITUDINAL FLOORBEAM AT RBL 45 APPROXIMATELY 2 INCHES FROM BS 727B, WL 208.1. MAINTENANCE CUT OUT CRACK IN UPPER FLANGE OF LONGITUDINAL FLOORBEAM RBL 45 AND PERFORMED H
- [SDR AWXA200200795](https://openairdocs.org/sdr/AWXA200200795.md): Frame · cracked · Aug 12, 2002 · N183AW · Boeing 737277 · Fuselage Main, Frame
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 3/4" CRACK WAS FOUND ON THE R-1 DOOR FRAME AT INBOARD LOWER END, BS 300, RBL 55. MAINTENANCE REMOVED DAMAGED SECTION OF R-1 DOOR LOWER FORWARD STUB BEAM FRAME AND FOUND SILL CLIP ALSO CRACKED. REMOVED SILL CLIP, FABRICA
- [SDR AWXA200200820](https://openairdocs.org/sdr/AWXA200200820.md): Web · cracked · Aug 10, 2002 · N183AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK HFEC INSPECTION INDICATED A 7/8" CRACK ON VERTICAL PRESSURE BEAM AT BS 663, RBL 32, WL 199. MAINTENANCE TRIMMED OUT DAMAGE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED 2 EACH REPAIR DOUBLERS, AND
- [SDR AWXA200200770](https://openairdocs.org/sdr/AWXA200200770.md): Stringer · corroded · Aug 10, 2002 · N183AW · Boeing 737277 · Fuselage Main, Longeron/Stringer
  > MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON THE UPPER AFT END OF STRINGER 26 R/H, BS 380 (E&E COMPARTMENT). MAINTENANCE REMOVED 1 EACH STRINGER SPLICE BS 360, 2 EACH STRINGER CLIPS BS 360 & BS 380, AND CUTOUT DAMAGED SECTION OF STRINGER BS 3
- [SDR AWXA200200805](https://openairdocs.org/sdr/AWXA200200805.md): Web · cracked · Aug 7, 2002 · N183AW · Boeing 737277 · Passenger/Crew Doors
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.5 INCH CRACK WAS FOUND ON R-2 DOOR INTERCOSTAL WEB AT BS 954, WL 252. MAINTENANCE REMOVED 3 STRAPS AND CRACKED INTERCOSTAL WEB AT BS 954, WL 252. FABRICATED A NEW INTERCOSTAL WEB, AND INSTALLED NEW WEB AND 3 STRAPS I
- [SDR AWXA200200803](https://openairdocs.org/sdr/AWXA200200803.md): Angle · cracked · Aug 6, 2002 · N183AW · Boeing 737277 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/2" CRACK WAS FOUND ON TOP OF CABIN FLOOR BEAM SUPPORT ANGLE BS 344, LBL 12, WL 206. MAINTENANCE REMOVED DAMAGED FLOOR BEAM SUPPORT ANGLE BS 344, LBL 12. FABRICATED A NEW FLOOR BEAM SUPPORT ANGLE, AND INSTALLED REPAIR
- [SDR AWXA200200823](https://openairdocs.org/sdr/AWXA200200823.md): Shear Tie · corroded · Aug 5, 2002 · N183AW · Boeing 737277 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON THE AFT CARGO PIT FLOOR FRAME ON TOP OF THE FORWARD LEG OUTBOARD SIDE, INBOARD OF STR 27 L/H, WL 149, BS 807. MAINTENANCE REMOVED STIFFNER, STRINGER CLIP, AND CUTOUT DAMAGED SKIN ATTACHMENT (SHEAR T
- [SDR AWXA200200822](https://openairdocs.org/sdr/AWXA200200822.md): Stringer · corroded · Aug 5, 2002 · N183AW · Boeing 737277 · Fuselage Main, Longeron/Stringer
  > MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON CENTER INBOARD SIDE OF STRINGER 22 L/H, AFT OF DOME PLATE NUT AND ABOVE EMERGENCY LIGHT ASSEMBLY AT BS 776. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS. CUTOUT DA
- [SDR AWXA200200821](https://openairdocs.org/sdr/AWXA200200821.md): Skin · cracked · Aug 3, 2002 · N183AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/16" CRACK WAS FOUND ON EXTERNAL FUSELAGE SKIN EXTENDING FROM FASTENER HOLE AT BS 303, STR 17 R/H, WL 210. MAINTENANCE CUTOUT DAMAGED SKIN AND BONDED DOUBLER AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. F
- [SDR AWXA200200819](https://openairdocs.org/sdr/AWXA200200819.md): Floorbeam · corroded · Aug 3, 2002 · N183AW · Boeing 737277 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION WAS FOUND ON THE UPPER SURFACE OF TEE CHORD AT BS 986, LBL 21 TO RBL 40, WL 208. MAINTENANCE BLENDED DAMAGED SECTION OF TEE CHORD, MATERIAL LOSS OUT OF LIMITS. REMOVED FLOOR SUPPORTS BS 966 TO BS 986.5, AND
- [SDR AWXA200200765](https://openairdocs.org/sdr/AWXA200200765.md): Floorbeam · corroded · Aug 3, 2002 · N183AW · Boeing 737277 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF TEE CHORD BS 967, RBL 27 - 41, WL 208. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED TEE CHORD BS 967 FROM BL 0 TO RBL 43. FABRI
- [SDR AWXA200200802](https://openairdocs.org/sdr/AWXA200200802.md): Floorbeam · cracked · Aug 2, 2002 · N183AW · Boeing 737277 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 2.7 INCH CRACK WAS FOUND ON THE LOWER SIDE OF FLOORBEAM UPPER CHORD AT BS 663, RBL 24, WL 202; VERIFIED BY HFEC INSPECTION. MAINTENANCE REMOVED CRACKED SECTION OF UPPER CHORD BS 663, RBL 24, WL 202. FABRICATED 2 REPAI
- [SDR AWXA200200767](https://openairdocs.org/sdr/AWXA200200767.md): Stringer · corroded · Aug 2, 2002 · N183AW · Boeing 737277 · Fuselage Main, Longeron/Stringer
  > MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON BOTH SIDES OF STRINGER 26 R/H BETWEEN BS 887 AND BS 927. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED STRINGER 26 R/H FROM BS 885 TO BS 917, REMOVED T
- [SDR AWXA200200834](https://openairdocs.org/sdr/AWXA200200834.md): Frame · cracked · Aug 1, 2002 · N183AW · Boeing 737277 · Fuselage Main, Frame
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/2" CRACK WAS FOUND IN THE AFT CARGO DOORWAY FORWARD DOOR CUTOUT FRAME BS 827, RBL 43, WL 164. MAINTENANCE REMOVED THE THRESHOLD WEB, CLIP FROM STRINGER 27 R/H, INTERCOASTAL ASSEMBLY, 3 EACH STIFFNERS, AND THE CRACKED
- [SDR AWXA200200796](https://openairdocs.org/sdr/AWXA200200796.md): Web · cracked · Aug 1, 2002 · N183AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.5 INCH CRACK WAS FOUND IN CLOSE OUT WEB AT BS 1005, RBL 43, CORROSION WAS ALSO FOUND ON LOWER SIDE OF SAME WEB AT RBL 44. MAINTENANCE REMOVED THE DAMAGED CLOSE OUT WEB BS 986.5 TO 1016, RBL 44. FABRICATED A NEW CLOSE
- [SDR AWXA200200768](https://openairdocs.org/sdr/AWXA200200768.md): Intercostal · cracked · Aug 1, 2002 · N183AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.5 INCH CRACK WAS FOUND ON INTERCOSTAL AT BS 500A, STRINGER 25 RT. MAINTENANCE REMOVED INTERCOSTAL FROM BS 500A, STRINGER 25 RT, FABRICATED A NEW INTERCOSTAL PER DWG 69-41473, AND INSTALLED REPAIR IAW B737-200 SRM 51-3
- [SDR AWXA200200848](https://openairdocs.org/sdr/AWXA200200848.md): Web · cracked · Jul 31, 2002 · N183AW · Boeing 737277 · Cargo/Baggage Doors
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.25 INCH CRACK WAS FOUND IN THE FORWARD END OF LOWER WEB ON FORWARD CARGO DOOR BS 446, STR 23 RT. MAINTENANCE REMOVED CRACKED SECTION OF WEB, FABRICATED 2 FILLERS, AND INSTALLED REPAIR PARTS IAW EO 52-31-04, FIG 2, PG
- [SDR AWXA200200835](https://openairdocs.org/sdr/AWXA200200835.md): Gusset · cracked · Jul 31, 2002 · N183AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 1" CRACK WAS FOUND ON GUSSET AT AFT END OF NOSE GEAR ACTUATOR SUPPORT FITTING BS 240, BL 0, WL 190. MAINTENANCE REMOVED NOSE GEAR ACTUATOR SUPPORT FITTING AND THE CRACKED GUSSET BS 240, BL 0, WL 190. FABRICATED A NEW G
- [SDR AWXA200200804](https://openairdocs.org/sdr/AWXA200200804.md): Skin · cracked · Jul 31, 2002 · N183AW · Boeing 737277 · Wing, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-18 CHECK.25 INCH CRACKS WERE FOUND ON RT WING LEADING EDGE AT THE NR 6 SLAT CENTER STOP FITTING CUTOUT, WS 557. MAINTENANCE BLENDED OUT CRACKS ON RT WING LEADING EDGE NR 6 SLAT CENTER STOP CUTOUT IAW AWA ER 15-5741-02232-SS1.
- [SDR AWXA200200801](https://openairdocs.org/sdr/AWXA200200801.md): Web · cracked · Jul 31, 2002 · N183AW · Boeing 737277 · Fuselage, Landing Gear Attach Fittings
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 3/8" CRACK WAS FOUND ON THE NOSE LANDING GEAR ACTUATOR SUPPORT BEAM WEB EXTENDING FROM UPPER CENTER RIVET HOLE, HFEC INSPECTION CONFIRMED CRACK. MAINTENANCE REMOVED NOSE LANDING GEAR ACTUATOR SUPPORT BEAM AND WEB, FABRI
- [SDR AWXA200200791](https://openairdocs.org/sdr/AWXA200200791.md): Door Frame · cracked · Jul 31, 2002 · N183AW · Boeing 737277 · Fuselage Main, Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.5 INCH CRACK WAS FOUND L-1 DOOR FRAME CUTOUT FORWARD LOWER STOP FITTING ATTACH PLATE WEB DOUBLER, BS 294.5, STR 16 LT. MAINTENANCE REMOVED THE L-1 DOOR FORWARD LOWER STOP FITTING ATTACH PLATE; REMOVED CLOSE OUT ANGLE
- [SDR AWXA200200790](https://openairdocs.org/sdr/AWXA200200790.md): Longeron · cracked · Jul 31, 2002 · N183AW · Boeing 737277 · Nacelle/Pylon, Main Frame
  > MCN - MAJOR REPAIR - DURING C-18 CHECK THE #1 ENGINE FIXED FAIRING LOWER END "Z" ANGLE WAS FOUND CRACKED BETWEEN 1ST AND 2ND ATTACH FITTINGS FROM THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE LOWER END "Z" ANGLE ON THE #1 ENGINE FIXED FAIRING IAW B737-
- [SDR AWXA200200789](https://openairdocs.org/sdr/AWXA200200789.md): Angle · broken · Jul 31, 2002 · N183AW · Boeing 737277 · Nacelle/Pylon, Main Frame
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A "T" ANGLE CLIP WAS FOUND BROKEN ON INBOARD SIDE OF THE #1 ENGINE FIXED FAIRING BETWEEN 2ND AND 3RD ATTACH FITTINGS FROM THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE "T" ANGLE CLIP ON INBOARD SIDE OF THE #1 ENGI
- [SDR AWXA200200788](https://openairdocs.org/sdr/AWXA200200788.md): Angle · broken · Jul 31, 2002 · N183AW · Boeing 737277 · Nacelle/Pylon, Main Frame
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A "T" ANGLE CLIP WAS FOUND BROKEN ON INBOARD SIDE OF THE #2 ENGINE FIXED FAIRING BETWEEN 2ND AND 3RD ATTACH FITTINGS FROM THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE "T" ANGLE CLIP ON INBOARD SIDE OF THE #2 ENGI
- [SDR AWXA200200769](https://openairdocs.org/sdr/AWXA200200769.md): Plate · cracked · Jul 31, 2002 · N183AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT FORWARD CORNER SCUFF PLATE. MAINTENANCE PREPARED, TREATED, AND WELDED THE CRACK ON FORWARD CORNER SCUFF PLATE IAW AWA ER 15-5333-01016-JS2.
- [SDR AWXA200200764](https://openairdocs.org/sdr/AWXA200200764.md): Skin · cracked · Jul 31, 2002 · N183AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4" CRACK WAS FOUND ON L-1 DOOR INTERNAL SKIN AT THE AFT UPPER CORNER DOOR STOP ADJUSTMENT CUTOUT, BS 346. MAINTENANCE CUTOUT CRACK AT L-1 DOOR AFT UPPER CORNER DOOR STOP ADJUSTMENT CUTOUT, BS 346. FABRICATED REPAIR DO
- [SDR AWXA200200750](https://openairdocs.org/sdr/AWXA200200750.md): Angle · cracked · Jul 31, 2002 · N183AW · Boeing 737277 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 1" CRACK WAS FOUND ON FLOOR BEAM SUPPORT ANGLE BS 400, BL 0. MAINTENANCE REMOVED DAMAGED FLOOR BEAM SUPPORT ANGLE AT BS 400, BL 0. FABRICATED A NEW FLOOR BEAM SUPPORT ANGLE, AND INSTALLED REPAIR IAW B737-200 SRM 51-30-2
- [SDR AWXA200201046](https://openairdocs.org/sdr/AWXA200201046.md): Skin · delaminated · Jul 30, 2002 · N183AW · Boeing 737277 · Trailing Edge Flaps
  > MCN - MAJOR REPAIR - DURING C-18 CHECK THE R/H WING INBOARD FORE FLAP WAS FOUND TO HAVE DELAMINATION ON UPPER SKIN 6" INBOARD OF THE #3 FORE FLAP TRACK. MAINTENANCE CUTOUT DELAMINATED AREA OF SKIN ON R/H WING INBOARD FORE FLAP; BONDED AND POTTED REPAIR CORE; F
- [SDR AWXA200200766](https://openairdocs.org/sdr/AWXA200200766.md): Skin · cracked · Jul 30, 2002 · N183AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4" CRACK WAS FOUND ON R-1 DOOR EXTERNAL SKIN AT UPPER AFT CORNER OF HINGE CUTOUT, CONFIRMED BY HFEC INSPECTION. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN AT R-1 DOOR UPPER AFT CORNER OF HINGE CUTOUT AND PERFORMED HFEC I
- [SDR AWXA200200763](https://openairdocs.org/sdr/AWXA200200763.md): Attach Angle · cracked · Jul 30, 2002 · N183AW · Boeing 737277 · Fuselage Main, Longeron/Stringer
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 1/2" CRACK WAS FOUND ON WEB UPPER CHORD (ATTACH ANGLE) AT FASTENER HOLES BS 500B TO BS 520, BL 0, WL 208.1. MAINTENANCE REMOVED WEB UPPER CHORD BS 500B TO BS 520, FABRICATED A REPAIR ANGLE AND INSTALLED REPAIR IAW DWG
- [SDR AWXA200200619](https://openairdocs.org/sdr/AWXA200200619.md): Flashlight · discharged · Jul 15, 2002 · N183AW · Boeing 737277 · Emergency Equipment
  > FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT AFT LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LT EMERGENCY FLASHLIGHT.
- [SDR AWXA200100597](https://openairdocs.org/sdr/AWXA200100597.md): Strap · cracked · Nov 14, 2001 · N183AW · Boeing 737277 · Fuselage Main, Frame
  > PHX - MAJOR REPAIR - "C" - CRACK FOUND ON FRAME RADIUS STRAP ON UPPER FLANGE ABOVE STRINGER 27R FOWARD PIT STA 492. MAINTENANCE REMOVED RADIUS STRAP FABRICATED STRAP AND FILLER AND INSTALLED IAW DWG 65-20723 AND SRM 50-30-2
- [SDR AWXA200100593](https://openairdocs.org/sdr/AWXA200100593.md): Skin · cracked · Nov 12, 2001 · N183AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > PHX - MAJOR REPAIR - C - 9 CRACKS FOUND IN FUSELAGE SKIN.125 INCH LONG ORIGINATING FROM FASTENER HOLES ALONG STR 17L, STA 390 TO 415 VERIFIED BY HFEC. MAINTENANCE CUT OUT AND REMOVED DAMAGED AREA OF SKIN AND FABRICATED FILLER AND DOUBLER, INSTALLED IAW SRM 5
- [SDR AWXA0002100](https://openairdocs.org/sdr/AWXA0002100.md): Web · cracked · Aug 3, 2001 · N183AW · Boeing 737277 · Fuselage Main, Longeron/Stringer
  > D: S-18A R/H shear beam web cracked.C: Replaced web 65-46877-82 per DWG 65-46877 - 76 INST. IAW SRM 51-10-1 page 8,9,10
- [SDR AWXA0002101](https://openairdocs.org/sdr/AWXA0002101.md): Floor Support · corroded · Aug 2, 2001 · N183AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > AFT CABIN - CORROSION ON FLOOR SUPPORT BEAMS BETWEEN STN 1000-1010 LBL 45. REPLACED BOTH FLOOR SUPPORT PER DRAW 65-46812 PART NUMBER 65-46812-87 AND 65-46812-91 IAW SRM 51-10-1 PAGE 8, 9, 10.
- [SDR AWXA0002099](https://openairdocs.org/sdr/AWXA0002099.md): Seat · corroded · Aug 2, 2001 · N183AW · Boeing 737277 · Fuselage Main, Structure
  > D: Aft cabin R/H track F.STN.1006-1016 RBL 45 corroded.C: R/H floor track F.STN.1006-1016 RBL 45 DRAW 65C80735 - part no. 65C80735-115 and IAW SRM 51-10-1 Page 8,9,10

Next page: https://openairdocs.org/deregistered/N183AW-2005-02-01/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 = 'N183AW' AND deregistration_id = 'N183AW-2005-02-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N183AW-2005-02-01/reports

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