# Service difficulty reports: N182AW, cancelled Mar 9, 2005

A list on [N182AW, cancelled Mar 9, 2005](https://openairdocs.org/deregistered/N182AW-2005-03-09.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 · 167 reports

- [SDR AWXA200401179](https://openairdocs.org/sdr/AWXA200401179.md): Light · inoperative · Oct 30, 2004 · N182AW · Boeing 737277 · Emergency Lighting
  > FLIGHT CREW REPORTED R-2 DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED R-2 DOOR EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200401089](https://openairdocs.org/sdr/AWXA200401089.md): Brake · seized · Oct 4, 2004 · N182AW · Boeing 737277 · Landing Gear Brake System
  > ABORTED TAKEOFF, FLT 0109, ON TAKEOFF, EN ROUTE WHEN APPROACHING V1 THE AIRCRAFT NOSE STARTED TO ROTATE ON ITS OWN, LOWERED NOSE AND REJECTED TAKEOFF AT 138 KTS. MAINTENANCE PERFORMED HORIZONTAL STABILIZER TRIM TEST, ALL TRIM INDICATIONS AGREE WITH (B) DIMENS
- [SDR AWXA200401011](https://openairdocs.org/sdr/AWXA200401011.md): Packing · torn · Sep 10, 2004 · N182AW · Boeing 737277 · Engine Fuel and Control
  > EN ROUTE, NR 1 ENG SHUTDOWN AT 27,000 FT, ATTEMPTED RESTART WITHOUT SUCCESS, DECLARED EMERGENCY & LANDED WITHOUT FURTHER EVENT. MX FOUND SEALS ON PRESS DUMP VALVE INPUT FUEL LINE TORN & LEAKING. REPLACED SEALS, ENGINE RUN OPERATIONAL CHECK WAS GOOD. MX R/R L
- [SDR AWXA200401022](https://openairdocs.org/sdr/AWXA200401022.md): Skin · cracked · Sep 8, 2004 · N182AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > DURING 4-DAY CHECK, A 1 1/2 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727A, STR 16 RT. MAINTENANCE REMOVED EXISTING REPAIR, CUTOUT DAMAGED AREA OF SKIN AT BS 727A, STR 16 RT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR
- [SDR AWXA200400886](https://openairdocs.org/sdr/AWXA200400886.md): Motor · binding · Aug 13, 2004 · N182AW · Boeing 737277 · Flight Control System
  > ON CLIMB-OUT OF PHX EN ROUTE FOR SJC AT APPROXIMATELY 3000 FT, FLIGHT CONTROLS SHOOK VIOLENTLY FROM SIDE TO SIDE AS IF IN SEVERE TURBULENCE. NOTICED FEEL DIFFERENTIAL LIGHT ILLUMINATED, TURNED BACK TO PHX, ADJUSTED AILERON TRIM AND ONCE AILERON INPUT WAS ACHI
- [SDR AWXA200400816](https://openairdocs.org/sdr/AWXA200400816.md): Power Supply · discharged · Jul 24, 2004 · N182AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - DURING INSPECTION THE EMERGENCY LIGHTS SEAT ROW 15 LEFT AND AFT WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNDER SEAT ROW 17 LEFT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400815](https://openairdocs.org/sdr/AWXA200400815.md): Light · failed · Jul 24, 2004 · N182AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400802](https://openairdocs.org/sdr/AWXA200400802.md): Warning Light · false indication · Jul 20, 2004 · N182AW · Boeing 737277 · Fire Detection
  > FALSE FIRE WARNING ON CLIMB OUT, AFTER SELECTING FLAPS UP RECEIVED FWD CARGO FIRE LIGHT AND FIRE BELL, DISCHARGED NR 1 CARGO FIRE BOTTLE AND LIGHT EXTINGUISHED, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINT MET AC AND PERFORMED A MAINT BITE TEST
- [SDR AWXA200400636](https://openairdocs.org/sdr/AWXA200400636.md): Socket · shorted · Jun 13, 2004 · N182AW · Boeing 737277 · Emergency Lighting
  > PHX - EMERGENCY LANDING - FLT 0628 - ON DESCENT INTO PHX EN ROUTE FROM OAK AT FL 120 EXPERIENCED AN ELECTRICAL BURNING ODOR FOLLOWED BY SMOKE IN COCKPIT, DONNED O2 MASKS AND DECLARED AN EMERGENCY. AT FL 030 FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN COMING FRO
- [SDR AWXA200400344](https://openairdocs.org/sdr/AWXA200400344.md): Hydraulic Line · ruptured · Apr 2, 2004 · N182AW · Boeing 737277 · Hydraulic System, Main
  > SAT - AIR TURNBACK - FLT 0679 - ON CLIMBOUT OF SAT EN ROUTE FOR PHX LOST A-HYDRAULIC SYSTEM, FOLLOWED QRH AND TURNED BACK TO SAT. MAINTENANCE REMOVED AND REPLACED RUPTURED HYDRAULIC PRESSURE LINE BETWEEN A-SYSTEM MODULE AND LT MAIN LANDING GEAR ACTUATOR. REM
- [SDR AWXA200400354](https://openairdocs.org/sdr/AWXA200400354.md): Skin · cracked · Mar 30, 2004 · N182AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > PHX - MAJOR REPAIR - A.25 INCH CRACK WAS FOUND IN FUSELAGE SKIN LT SIDE AT LAP SEAM BETWEEN WINDOWS 11 & 12, BS 540, STR 14 LEFT. MAINTENANCE CUT OUT DAMAGED SECTION OF SKIN JUST BELOW WINDOW BELT BS 540, STR 14 LEFT; FABRICATED 4 EACH FILLERS, A DOUBLER & T
- [SDR AWXA200400179](https://openairdocs.org/sdr/AWXA200400179.md): Wire · broken · Feb 14, 2004 · N182AW · Boeing 737277 · Light System Wiring
  > DURING INSPECTION A BROKEN WIRE WAS FOUND ON THE EMERGENCY ESCAPE PATH LIGHT SEAT ROW 17 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200301385](https://openairdocs.org/sdr/AWXA200301385.md): Bracket · cracked · Nov 6, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-21 CHECK A.375 INCH CRACK WAS FOUND IN A BRACKET AT BS 334, LBL 56, WL 206. MAINTENANCE REMOVED THE CRACKED BRACKET AT BS 334, LBL 56, WL 206; FABRICATED A NEW REPLACEMENT BRACKET; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02
- [SDR AWXA200301389](https://openairdocs.org/sdr/AWXA200301389.md): Tie Clip · cracked · Nov 2, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-21 CHECK A 1.5 INCH CRACK WAS FOUND IN TIE CLIP BS 344-350, STR 16 LT. MAINTENANCE REMOVED THE CRACKED TIE CLIP BS 344-350, STR 16 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 65-17685; INSTALLED REPAIR PART IAW B737-200 SRM 51
- [SDR AWXA200301369](https://openairdocs.org/sdr/AWXA200301369.md): Floorbeam · corroded · Nov 2, 2003 · N182AW · Boeing 737277 · Fuselage Main, Floor Beam
  > DURING C-21 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF UPPER T-CAP REPAIR AT BS 986.5, RBL 0.5 TO RBL 45. MAINTENANCE REMOVED UPPER T-CAP REPAIR AT BS 986.5, LBL 11 TO RBL 51; FABRICATED A NEW REPLACEMENT T-CAP; INSTALLED REPAIR PART IAW B737-200
- [SDR AWXA200301422](https://openairdocs.org/sdr/AWXA200301422.md): Web · cracked · Oct 30, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-21 CHECK 2 EACH CRACKS WERE FOUND ON SHEAR WEB AT BS 344, AFT OF L-1 DOOR. MAINTENANCE REMOVED DAMAGED SHEAR WEB BS 344; FABRICATED A NEW REPLACEMENT SHEAR WEB; INSTALLED REPAIR PART IAW B737-200 SRM 51-20-02, FIG 7.
- [SDR AWXA200301398](https://openairdocs.org/sdr/AWXA200301398.md): Clip · cracked · Oct 30, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-21 CHECK A 1.5 INCH CRACK WAS FOUND IN RADIUS OF INTERCOSTAL CLIP ANGLE BS 344, STR 16 LT. MAINTENANCE REMOVED DAMAGED INTERCOSTAL CLIP ANGLE BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT FUSELAGE CLIP ANGLE; INSTALLED REPAIR P
- [SDR AWXA200301397](https://openairdocs.org/sdr/AWXA200301397.md): Frame · cracked · Oct 30, 2003 · N182AW · Boeing 737277 · Fuselage Main, Frame
  > MCN - MAJOR REPAIR - DURING C-21 CHECK A 1.125 INCH CRACK WAS FOUND IN RADIUS OF FUSELAGE FRAME CHORD, AFT OF L-1 DOOR BS 344, STR 15 LT. MAINTENANCE REMOVED DAMAGED FUSELAGE FRAME CHORD AFT OF L-1 DOOR BS 344, STR 15 LT; FABRICATED A NEW REPLACEMENT FUSELAGE
- [SDR AWXA200301392](https://openairdocs.org/sdr/AWXA200301392.md): Angle · cracked · Oct 30, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-21 CHECK A 1 INCH CRACK WAS FOUND IN CLIP ANGLE ON BOTTOM OF INTERCOSTAL AT STRINGER 16 LT, BS 344. MAINTENANCE REMOVED THE CRACKED CLIP ANGLE BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT CLIP ANGLE PER DWG 69-16509; INSTALLED
- [SDR AWXA200301391](https://openairdocs.org/sdr/AWXA200301391.md): Angle · cracked · Oct 30, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-21 CHECK A 1.125 INCH CRACK WAS FOUND IN CLIP ANGLE ON TOP OF INTERCOSTAL AT STRINGER 16 LT, BS 344. MAINTENANCE REMOVED THE CRACKED CLIP ANGLE BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT CLIP ANGLE PER DWG 69-26555; INSTALLE
- [SDR AWXA200301390](https://openairdocs.org/sdr/AWXA200301390.md): Attach Angle · cracked · Oct 30, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-21 CHECK A 2.875 INCH CRACK WAS FOUND IN STRINGER 15 LT TO FRAME 344 ATTACH ANGLE. MAINTENANCE REMOVED THE CRACKED ATTACH ANGLE BS 344, STR 15 LT; FABRICATED A NEW REPLACEMENT ATTACH ANGLE DWG 69-16970; INSTALLED REPAIR PART IAW
- [SDR AWXA200301386](https://openairdocs.org/sdr/AWXA200301386.md): Clip · cracked · Oct 28, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-21 CHECK A.375 INCH CRACK WAS FOUND IN FRAME ATTACH CLIP ON L-1 DOOR AFT FRAME AT NR 6 DOOR STOP BS 344, STR 16 LT. MAINTENANCE REMOVED THE CRACKED FRAME ATTACH CLIP AT BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT CLIP PER DW
- [SDR AWXA200301365](https://openairdocs.org/sdr/AWXA200301365.md): Floor Support · corroded · Oct 27, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-21 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 1003, LBL 38. MAINTENANCE REMOVED FLOOR SUPPORT FROM BS 986.5 TO BS 1006, LBL 38; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02 FIG 11
- [SDR AWXA200301338](https://openairdocs.org/sdr/AWXA200301338.md): Stringer Clip · cracked · Oct 23, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-21 CHECK A 1 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 380, STR 25 LT. MAINTENANCE REMOVED AND REPLACED STRINGER TIE CLIP AT BS 380, STR 25 LT IAW B737-300 SRM 51-30-02, PG 2-3, & 8-10.
- [SDR AWXA200301399](https://openairdocs.org/sdr/AWXA200301399.md): Fairing · cracked · Oct 22, 2003 · N182AW · Boeing 737277 · Engine Thrust Reverser
  > MCN - MAJOR REPAIR - DURING C-21 CHECK A 2 INCH CRACK WAS FOUND ON NR 1 THRUST REVERSER LOWER DEFLECTOR DOOR LT FAIRING AT 2ND FASTENER HOLE FROM FORWARD END. MAINTENANCE CUT OUT DAMAGE SECTION OF NR 1 THRUST REVERSER LOWER DEFLECTOR DOOR LT FAIRING; PERFORME
- [SDR AWXA200301387](https://openairdocs.org/sdr/AWXA200301387.md): Clip · cracked · Oct 22, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-21 CHECK A.375 INCH CRACK WAS FOUND IN FRAME ATTACH CLIP ON L-1 DOOR AFT FRAME AT NR 6 DOOR STOP BS 344, STR 16 LT. MAINTENANCE REMOVED THE CRACKED FRAME ATTACH CLIP AT BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT CLIP PER DW
- [SDR AWXA200301370](https://openairdocs.org/sdr/AWXA200301370.md): Floorbeam · corroded · Oct 22, 2003 · N182AW · Boeing 737277 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-21 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF UPPER T-CAP REPAIR AT BS 967, RBL 10 TO RBL 48. MAINTENANCE REMOVED UPPER T-CAP REPAIR AT BS 967, RBL 10 TO RBL 48; FABRICATED A NEW REPLACEMENT T-CAP; INSTALLED REPAIR P
- [SDR AWXA200301367](https://openairdocs.org/sdr/AWXA200301367.md): Splice · corroded · Oct 22, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-21 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR ATTACH STRAP BS 771, STR 26 LT TO STR 26 RT. MAINTENANCE REMOVED DAMAGED FLOOR ATTACH STRAP BS 771, STR 26 LT TO STR 26 RT; FABRICATED A NEW REPLACEMENT STRAP; INSTALLED REPAIR PART IAW B737-200
- [SDR AWXA200301364](https://openairdocs.org/sdr/AWXA200301364.md): Floorbeam · corroded · Oct 22, 2003 · N182AW · Boeing 737277 · Fuselage Main, Floor Beam
  > DURING C-21 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER AFT LEG AT BS 947 FROM RBL 5 TO LBL 53. MAINTENANCE CUT OUT DAMAGED FLOORBEAM UPPER AFT LEG AT BS 947 FROM RBL 5 TO LBL 53; FABRICATED A FILLER AND 2 EACH REPAIR ANGLES; INSTA
- [SDR AWXA200301342](https://openairdocs.org/sdr/AWXA200301342.md): Tail Cone · delaminated · Oct 22, 2003 · N182AW · Boeing 737277 · Aerodynamic Fairings
  > MCN - MINOR REPAIR - DURING C-21 CHECK THE TAIL CONE WAS FOUND DELAMINATED AT LOWER CENTER 7 INCHES, 11 INCHES, & 24 INCHES FROM FORWARD END, 7.5 INCHES LT LOWER SIDE 12.5-15 INCHES FROM FORWARD END, 4-7 INCHES RT SIDE OF CENTER LOWER 16.5 INCHES FROM FORWARD
- [SDR AWXA200301419](https://openairdocs.org/sdr/AWXA200301419.md): Web · cracked · Oct 21, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-21 CHECK A 1 INCH CRACK WAS FOUND ON SHEAR WEB AT FORWARD INBOARD SIDE END OF CREASE BEAM BS 995.5, LBL 43.5. MAINTENANCE REMOVED CRACKED SHEAR WEB AT FORWARD INBOARD SIDE END OF CREASE BEAM BS 995.5, LBL 43.5; FABRICATED A NEW R
- [SDR AWXA200301418](https://openairdocs.org/sdr/AWXA200301418.md): Clip · cracked · Oct 21, 2003 · N182AW · Boeing 737277 · Engine Cowling System
  > MCN - MINOR REPAIR - DURING C-21 CHECK A.25 INCH CRACK WAS FOUND ON L-ANGLE CLIP AT UPPER AFT END OF NR 2 ENGINE COWLING. MAINTENANCE REMOVED CRACKED L-ANGLE CLIP; FABRICATED A NEW REPLACEMENT CLIPPER DWG 65-552263-27; INSTALLED REPAIR PART IAW B737-22 SRM 5
- [SDR AWXA200301388](https://openairdocs.org/sdr/AWXA200301388.md): Angle · corroded · Oct 21, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-21 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT FLOOR ZEE ANGLE AT BS 520, RBL 20. MAINTENANCE CUT OUT DAMAGED SECTION OF ZEE ANGLE AT BS 520, RBL 20; FABRICATED A ZEE ANGLE AND 4 EACH REPAIR ANGLES; INSTALL
- [SDR AWXA200301366](https://openairdocs.org/sdr/AWXA200301366.md): Web · cracked · Oct 21, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-21 CHECK A 1 INCH CRACK WAS FOUND ON FORWARD END OF LT SHEAR WEB AT BS 995.5, LBL 43.5, AND EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF LT OUTBOARD SHEAR WEB, BS 1002, LBL 40. MAINTENANCE REMOVED DAMAGED SHEAR WEB FROM BS 995.5 TO BS 1014, LB
- [SDR AWXA200301363](https://openairdocs.org/sdr/AWXA200301363.md): Angle · cracked · Oct 21, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > DURING C-21 CHECK A 1 INCH CRACK WAS FOUND ON ANGLE (CLIP) FORWARD SIDE OF BS 500B FRAME, ABOVE STR 26 LT. MAINTENANCE REMOVED CRACKED ANGLE FORWARD SIDE OF BS 500B FRAME, ABOVE STR 26 LT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-51411; INSTALLED REPAIR
- [SDR AWXA200301343](https://openairdocs.org/sdr/AWXA200301343.md): Intercostal · cracked · Oct 21, 2003 · N182AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > MCN - MINOR REPAIR - DURING C-21 CHECK A.5 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 480, LBL 24. MAINTENANCE REMOVED INTERCOSTAL FROM BS 460 TO BS 480, LBL 24; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 69-41473; INSTALLED REPAIR PART IAW B737-200 SRM
- [SDR AWXA200301395](https://openairdocs.org/sdr/AWXA200301395.md): Skin · cracked · Oct 20, 2003 · N182AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-21 CHECK A 1.375 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT FASTENER HOLE LOWER AFT CORNER OF L-1 DOOR, BS 344. MAINTENANCE CUTOUT DAMAGE ON FUSELAGE SKIN AT LOWER AFT CORNER OF L-1 DOOR; PERFORMED HFEC INSPECTION TO VERIFY NO CRA
- [SDR AWXA200301368](https://openairdocs.org/sdr/AWXA200301368.md): Frame · cracked · Oct 20, 2003 · N182AW · Boeing 737277 · Passenger/Crew Doors
  > DURING C-21 CHECK A.3125 INCH CRACK WAS FOUND ON AFT SIDE OF R-1 DOOR INBOARD OF THE 3RD AFT STOP FITTING FROM THE BOTTOM BS 327, STR 14 RT. MAINTENANCE CUT OUT DAMAGE ON AFT SIDE OF R-1 DOOR 3RD AFT STOP FITTING FROM THE BOTTOM BS 327, STR 14 RT; FABRICATED
- [SDR AWXA200301341](https://openairdocs.org/sdr/AWXA200301341.md): Slat · delaminated · Oct 20, 2003 · N182AW · Boeing 737277 · Leading Edge Devices
  > MCN - MAJOR REPAIR - DURING C-21 CHECK THE NR 1 LEADING EDGE SLAT WAS FOUND DELAMINATED AT THE INBOARD UPPER SURFACE WS 510 TO WS 512 LT. MAINTENANCE CUT OUT DELAMINATED AREA ON NR 1 L/E SLAT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-2
- [SDR AWXA200301396](https://openairdocs.org/sdr/AWXA200301396.md): Skin · cracked · Oct 19, 2003 · N182AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-21 CHECK A.5 INCH CRACK WAS FOUND ON PREVIOUS REPAIR AT FASTENER HOLE OF LOWER FUSELAGE SKIN BS 454, RBL 3. MAINTENANCE TRIMMED OUT DAMAGE ON PREVIOUS REPAIR AT FASTENER HOLE OF LOWER FUSELAGE SKIN BS 454, RBL 3; PERFORMED HFEC
- [SDR AWXA200301394](https://openairdocs.org/sdr/AWXA200301394.md): Skin · cracked · Oct 19, 2003 · N182AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-21 CHECK A.75 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT FASTENER HOLE ON FORWARD UPPER CORNER OF R-1 DOOR, BS 292.50. MAINTENANCE PERFORMED HFEC ON CRACK AND IDENTIFIED CRACK END; STOP DRILLED CRACK IN FUSELAGE SKIN AT R-1 DOOR F
- [SDR AWXA200301030](https://openairdocs.org/sdr/AWXA200301030.md): Circuit Breaker · inoperative · Sep 7, 2003 · N182AW · Boeing 737277 · Landing Gear Position and Warning
  > ON APPROACH INTO PHX EN ROUTE FROM BUR AFTER LANDING GEAR EXTENSION THERE WAS NO LANDING GEAR DOWN AND LOCKED OR UNSAFE GEAR INDICATIONS, ABORTED APPROACH. FOUND CIRCUIT BREAKER (SECT5) EXTENDED, AFTER DISCUSSION WITH MAINTENANCE CONTROL, CIRCUIT BREAKER WAS R
- [SDR AWXA200300995](https://openairdocs.org/sdr/AWXA200300995.md): Light · broken · Aug 27, 2003 · N182AW · Boeing 737277 · Emergency Lighting
  > FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200300944](https://openairdocs.org/sdr/AWXA200300944.md): Light · broken · Aug 19, 2003 · N182AW · Boeing 737277 · Emergency Lighting
  > DURING 8-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200300941](https://openairdocs.org/sdr/AWXA200300941.md): Controller · malfunctioned · Aug 19, 2003 · N182AW · Boeing 737277 · Cabin Pressure Controller
  > ON INITIAL TAKEOFF ROLL EN ROUTE, THE CABIN CLIMB INDICATOR NEEDLE WENT TO RAPID RATE OF DESCENT OF ABOUT 4000 FPM, REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER IAW BMM 21-31-21, PERFORMED OPERATIONAL C
- [SDR AWXA200300812](https://openairdocs.org/sdr/AWXA200300812.md): Bleed Valve · malfunctioned · Jul 18, 2003 · N182AW · Boeing 737277 · Compressor Bleed Valve
  > DEN - ABORTED TAKEOFF - FLT 0640 - DURING TAKEOFF ROLL AT DEN EN ROUTE FOR PHX, A LOUD "BANG" CAME FROM THE NR 1 ENGINE, REJECTED TAKEOFF, SUSPECT COMPRESSOR STALL. MAINTENANCE PERFORMED A BORESCOPE INSPECTION IAW T/C I5M72008, NO DAMAGE NOTED. REMOVED AND REP
- [SDR AWXA200300550](https://openairdocs.org/sdr/AWXA200300550.md): Transmitter · malfunctioned · May 16, 2003 · N182AW · Boeing 737277 · Engine Pressure Ratio (EPR)
  > PHX - ABORTED TAKEOFF - FLT 0445 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR TUS, SETTING REDUCED FOR POWER 1.96, NR 2 ENGINE EPR DID NOT COME UP TO POWER, EPR STAGNATED AT 1.45 EPR WHILE THRUST LEVER ADVANCED. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TR
- [SDR AWXA200300300](https://openairdocs.org/sdr/AWXA200300300.md): Engine · out of trim · Mar 22, 2003 · N182AW · Boeing 737277 · Engine (Turbine/Turboprop)
  > ON TAKEOFF AT PHX EN ROUTE FOR ONT WHEN SELECTING TAKEOFF POWER, TAKEOFF POWER WAS SET TO 2.11 EPR AND THE NR 2 ENGINE ONLY CAME UP TO 1.59 EPR. FURTHER ADVANCEMENT OF THROTTLE DID NOT VARY 1.99 EPR, REJECTED TAKEOFF. MAINTENANCE PERFORMED ENGINE TRIM RUNS PE
- [SDR AWXA200300273](https://openairdocs.org/sdr/AWXA200300273.md): Battery · discharged · Mar 16, 2003 · N182AW · Boeing 737277 · Emergency Equipment
  > FLIGHT CREW REPORTED THAT THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200300270](https://openairdocs.org/sdr/AWXA200300270.md): Vane · damaged · Mar 13, 2003 · N182AW · Boeing 737277 · Turbine Engine Compressor Section
  > WHEN PREPARING FOR TAKEOFF AT DFW EN ROUTE FOR PHX WHEN THROTTLES ADVANCED RECEIVED COMPRESSOR VANE FAULT. MAINTENANCE REMOVED AND REPLACED THE PRESSURE RATIO BLEED CONTROL IAW T/C R5M75002, AND LUBRICATED THE 13TH STAGE BLEED VALVE IAW BMM 75-31-0, PG. 602.

Next page: https://openairdocs.org/deregistered/N182AW-2005-03-09/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 = 'N182AW' AND deregistration_id = 'N182AW-2005-03-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N182AW-2005-03-09/reports

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