# Service difficulty reports: N174AW, cancelled Jul 31, 2006

A list on [N174AW, cancelled Jul 31, 2006](https://openairdocs.org/deregistered/N174AW-2006-07-31.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 · 173 reports

- [SDR AWXA200600406](https://openairdocs.org/sdr/AWXA200600406.md): Slide · unknown · Mar 1, 2006 · N174AW · Boeing 73733A · Escape Slide
  > PHX - EES - DURING SCHEDULED DEPLOYMENT OF THE R-1 DOOR, THE SLIDE ENDED UP NOT BEING PERPENDICULAR TO THE AIRCRAFT, THE SLIDE CAME OUT TWISTED. MAINTENANCE REMOVED AND REPLACED THE R1 DOOR SLIDE IAW AMERICA WEST AIRLINES TASK CARD R1C25001. UNABLE TO DUPLI
- [SDR AWXA200600206](https://openairdocs.org/sdr/AWXA200600206.md): Proximity Sensor · faulty · Feb 5, 2006 · N174AW · Boeing 73733A · Landing Gear Position and Warning
  > PHX - AIR TURN BACK - FLT 504 - CREW REPORTED THAT AFTER T/O HAD NORMAL GEAR RETRACTION, PASSING THROUGH 10000 FEET GOT A RED NOSE GEAR INDICATION. CREW LOWERED GEAR AS PER MX CONTROL AND RECEIVED NORMAL MAIN DOWN AND LOCKED INDICATION BUT UNSAFE RED NOSE GEA
- [SDR AWXA200600008](https://openairdocs.org/sdr/AWXA200600008.md): Terminal Block · loose · Jan 2, 2006 · N174AW · Boeing 73733A · Engine Indicating System Wiring
  > LAS - AIR TURN BACK - FLT 421 - AFTER CLIMB-OUT, CREW REPORTED THAT THE NR 2 ENG OVERHEATED WITH AN EGT INDICATION OF 1130 DEG C FOR 2 TO 3 SECONDS WITH ASSOCIATED RED LIGHT. CREW REDUCED POWER AND EGT RETURNED WITHIN LIMITS. CREW RETURNED TO LAS AND LANDED
- [SDR AWXA200501610](https://openairdocs.org/sdr/AWXA200501610.md): Windshield · cracked · Dec 27, 2005 · N174AW · Boeing 73733A · Flight Compartment Windows
  > DURING CRUISE, DEPARTED FROM DFW EN ROUTE TO LAS, AT FL 340 CREW REPORTED CAPT OUTER WINDSHIELD CRACKED. CREW DIVERTED & LANDED WITHOUT FURTHER INCIDENT. MX R & R CAPT WINDSHIELD. OPS CHECKS GOOD. HIGH TIME WINDOW. WINDOW WAS SCRAPPED AT VENDOR.
- [SDR AWXA200501261](https://openairdocs.org/sdr/AWXA200501261.md): Skin · damaged · Oct 20, 2005 · N174AW · Boeing 73733A · Fuselage Main, Plate/Skin
  > PHX - MAJOR REPAIR - DURING OVERNIGHT INSPECTION DISCOVERED 3.5 INCH CRACK IN FUSELAGE LOCATED AT STA 927 AND STR 25R. MAINTENANCE REMOVED DAMAGED SKIN IAW BOEING 737-300 SRM 53-00-01. FABRICATED DOUBLER, TRIPLER AND FILLER IAW BOEING 737-300 SRM 53-00-01 FI
- [SDR AWXA200500756](https://openairdocs.org/sdr/AWXA200500756.md): Connector · dirty · Jun 24, 2005 · N174AW · Boeing 73733A · Flight Control System Wiring
  > ON LANDING, FLAPS AT ZERO, HOT LANDING. LANDED WITHOUT FURTHER INCIDENT. CREW REPORTED FLAP PROBLEM TO TOWER PRIOR TO LANDING. CREW REQUESTED PRIORITY LANDING DUE TO FLAP PROBLEM. UPON LANDING, CREW WROTE UP FLAP INDICATOR SHOWS SPILT FLAPS AT FLAPS UP PO
- [SDR AWXA200500535](https://openairdocs.org/sdr/AWXA200500535.md): Battery · discharged · May 3, 2005 · N174AW · Boeing 73733A · Emergency Equipment
  > MCI - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200500482](https://openairdocs.org/sdr/AWXA200500482.md): Bracket · cracked · Apr 16, 2005 · N174AW · Boeing 73733A · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-19 CHECK 2 INCH CRACK WAS FOUND AT FASTENER HOLE AND A 1 INCH CRACK WAS FOUND IN INBOARD FLANGE RADIUS OF GUSSET BRACKET AT FR 335, BETWEEN STR 17 LT AND STR 18 LT. MAINTENANCE REMOVED DAMAGED GUSSET BRACKET AT FR 335, BETWEEN ST
- [SDR AWXA200500489](https://openairdocs.org/sdr/AWXA200500489.md): Clip · cracked · Apr 15, 2005 · N174AW · Boeing 73733A · Fuselage Main, Attach Fittings
  > MCN - MAJOR REPAIR - DURING C-19 CHECK A.5625 INCH CRACK WAS FOUND ON FRAME ATTACH CLIP AT BS 827 BETWEEN STR 25 RT AND STR 26 RT. MAINTENANCE REMOVED CRACKED FRAME ATTACH CLIP AT BS 827 BETWEEN STR 25 RT AND STR 26 RT; FABRICATED A NEW REPLACEMENT CLIP PER
- [SDR AWXA200500492](https://openairdocs.org/sdr/AWXA200500492.md): Frame · cracked · Apr 4, 2005 · N174AW · Boeing 73733A · Cargo/Baggage Doors
  > MCN - MAJOR REPAIR - DURING C-19 CHECK A.375 INCH CRACK WAS FOUND IN FORWARD EDGE OF AFT CARGO DOOR AT FASTENER HOLES FOR PULLEY BRACKET BS 801. MAINTENANCE CUT OUT DAMAGED SECTION OF FRAME ON FORWARD EDGE OF AFT CARGO DOOR; FABRICATED A NEW REPLACEMENT FRAM
- [SDR AWXA200500488](https://openairdocs.org/sdr/AWXA200500488.md): Skin · delaminated · Apr 4, 2005 · N174AW · Boeing 73733A · Leading Edge Devices
  > MCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE UPPER SURFACE OF THE NR 3 SLAT T/E WEDGE ASSEMBLY DELAMINATED AT SLAT STA 54 LT. MAINTENANCE CUT OUT DELAMINATED AREA OF NR 3 SLAT WEDGE UPPER SURFACE SKIN FROM SS 46.6 TO SS 63.3; FABRICATED A CORE FILLER AND
- [SDR AWXA200500487](https://openairdocs.org/sdr/AWXA200500487.md): Skin · delaminated · Apr 4, 2005 · N174AW · Boeing 73733A · Leading Edge Devices
  > MCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE UPPER SURFACE OF THE NR 3 SLAT T/E WEDGE ASSEMBLY DELAMINATED AT SLAT STA 84 LT. MAINTENANCE CUT OUT DELAMINATED AREA OF NR 3 SLAT WEDGE UPPER SURFACE SKIN FROM SS 74.5 TO SS 94.4; FABRICATED A CORE FILLER AND
- [SDR AWXA200500486](https://openairdocs.org/sdr/AWXA200500486.md): Skin · delaminated · Apr 4, 2005 · N174AW · Boeing 73733A · Rudder, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE RIGHT TOP AFT SECTION OF RUDDER DELAMINATED AT RUDDER STA 238. MAINTENANCE REMOVED DELAMINATED SECTION OF RT TOP AFT RUDDER CONDUCTIVE FRAME; FABRICATED A NEW REPLACEMENT SECTION OF CONDUCTIVE FRAME PER DWG 65C
- [SDR AWXA200500464](https://openairdocs.org/sdr/AWXA200500464.md): Skin · delaminated · Apr 4, 2005 · N174AW · Boeing 73733A · Leading Edge Devices
  > MCN - MAJOR REPAIR - DURING C-19 CHECK THE NR 2 SLAT WEDGE WAS FOUND DELAMINATED ON THE UPPER & LOWER SURFACE AT OUTBOARD END BETWEEN SLAT STA 250.9 AND SLAT STA 254.4 LT. MAINTENANCE REMOVED DAMAGE IN UPPER AND LOWER SURFACE SKIN OF NR 2 SLAT WEDGE FROM SS 2
- [SDR AWXA200500463](https://openairdocs.org/sdr/AWXA200500463.md): Skin · delaminated · Apr 4, 2005 · N174AW · Boeing 73733A · Leading Edge Devices
  > MCN - MAJOR REPAIR - DURING C-19 CHECK THE NR 1 SLAT WEDGE WAS FOUND DELAMINATED ON THE UPPER & LOWER SURFACE AT SLAT STA 348 LT. MAINTENANCE REMOVED DAMAGE IN UPPER AND LOWER SURFACE SKIN OF NR 1 SLAT WEDGE FROM SS 343 TO SS 350 LT; FABRICATED A CORE FILLER
- [SDR AWXA200500462](https://openairdocs.org/sdr/AWXA200500462.md): Skin · delaminated · Apr 4, 2005 · N174AW · Boeing 73733A · Leading Edge Devices
  > MCN - MAJOR REPAIR - DURING C-19 CHECK THE NR 4 SLAT WEDGE WAS DELAMINATED AT THE BOTTOM OUTBOARD END BETWEEN SLAT STA 120-124 RT. MAINTENANCE REMOVED DAMAGE IN LOWER SURFACE SKIN OF NR 4 SLAT WEDGE; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SLA
- [SDR AWXA200500490](https://openairdocs.org/sdr/AWXA200500490.md): Skin · chafed · Apr 2, 2005 · N174AW · Boeing 73733A · Trailing Edge Flaps
  > MCN - MAJOR REPAIR - DURING C-19 CHECK THE LEFT INBOARD MID-FLAP LOWER SKIN WAS FOUND CHAFED AT WS 100. MAINTENANCE BLENDED OUT DAMAGE ON LEFT INBOARD MID-FLAP LOWER SKIN AT WS 100; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5753-05112-RC2.
- [SDR AWXA200500493](https://openairdocs.org/sdr/AWXA200500493.md): Skin · chafed · Apr 1, 2005 · N174AW · Boeing 73733A · Trailing Edge Flaps
  > MCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE LOWER CENTER SECTION SKIN OF THE LEFT OUTBOARD FORE-FLAP CHAFED AT WBL 298. MAINTENANCE CUT OUT CHAFED SKIN ON LOWER CENTER LT OUTBOARD FORE-FLAP AT WBL 298; FABRICATED NEW SKIN SECTION AND A DOUBLER; BONDED RE
- [SDR AWXA200500491](https://openairdocs.org/sdr/AWXA200500491.md): Skin · delaminated · Apr 1, 2005 · N174AW · Boeing 73733A · Trailing Edge Flaps
  > MCN - MAJOR REPAIR - DURING C-19 CHECK THE LT OUTBOARD FORE-FLAP WAS FOUND DELAMINATED AT THE UPPER AFT OUTBOARD CORNER. MAINTENANCE CUT OUT DAMAGE ON LT OUTBOARD FORE-FLAP AT UPPER AFT OUTBOARD CORNER BETWEEN WBL 410.11 AND WBL 413.6; FABRICATED A FILLER AND
- [SDR AWXA200500471](https://openairdocs.org/sdr/AWXA200500471.md): Door Frame · cracked · Apr 1, 2005 · N174AW · Boeing 73733A · Service Doors
  > DURING C-19 CHECK A.3125 INCH CRACK WAS FOUND ON R-1 DOOR AFT FRAME AT 3RD DOOR STOP CUTOUT FROM BOTTOM BS 329, STR 12 RT. MAINTENANCE TRIMMED OUT DAMAGE R-1 DOOR AFT FRAME AT 3RD DOOR STOP CUTOUT FROM BOTTOM BS 329, STR 12 RT; FABRICATED A REPAIR DOUBLER; I
- [SDR AWXA200500470](https://openairdocs.org/sdr/AWXA200500470.md): Door Frame · cracked · Apr 1, 2005 · N174AW · Boeing 73733A · Service Doors
  > DURING C-19 CHECK A.375 INCH CRACK WAS FOUND ON R-1 DOOR AFT FRAME AT 4TH DOOR STOP FROM BOTTOM BS 344, STR 13 RT. MAINTENANCE TRIMMED OUT DAMAGE R-1 DOOR AFT FRAME AT 4TH DOOR STOP FROM BOTTOM BS 344, STR 13 RT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR
- [SDR AWXA200500378](https://openairdocs.org/sdr/AWXA200500378.md): Wire · broken · Mar 30, 2005 · N174AW · Boeing 73733A · Light System Wiring
  > PHX - EEL - DURING 4-DAY CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT PIN FOR CONNECTOR, RETERMINATED WIRE AT PIN AT SEAT ROW 14 LT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200500361](https://openairdocs.org/sdr/AWXA200500361.md): Switch · shorted · Mar 24, 2005 · N174AW · Boeing 73733A · Central Warning
  > PHX - ABORTED TAKEOFF - FLT 0506 - ON TAKEOFF AT PHX EN ROUTE TO YVR UPON ADVANCING THROTTLES AND BRAKE RELEASE THE TAKEOFF CONFIGURATION WARNING HORN SOUNDED, ALL EFFORTS TO SILENCE HORN FAILED. RETURNED TO GATE. MAINTENANCE FOUND STABILIZER NOSE UP SWITCH
- [SDR AWXA200500363](https://openairdocs.org/sdr/AWXA200500363.md): Circuit Breaker · defective · Mar 2, 2005 · N174AW · Boeing 73733A · Central Warning
  > LAS - ABORTED TAKEOFF - FLT 0399 - ON TAKEOFF AT LAS EN ROUTE FOR DFW THE TAKEOFF CONFIGURATION WARNING HORN SOUNDED COUNTINUOUSLY, RETURNED TO GATE. MAINTENANCE REMOVED EXCESSIVE GREASE AT SWITCHED S132 AND S546, REPLACED LEADING EDGE FLAP CIRCUIT BREAKER AS
- [SDR AWXA200401358](https://openairdocs.org/sdr/AWXA200401358.md): Light · inoperative · Dec 6, 2004 · N174AW · Boeing 73733A · Emergency Lighting
  > DFW - EEL - DURING A-01 CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 18 LT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400850](https://openairdocs.org/sdr/AWXA200400850.md): Wire · loose · Aug 4, 2004 · N174AW · Boeing 73733A · Light System Wiring
  > DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A LOOSE WIRE AT SPLICE SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400812](https://openairdocs.org/sdr/AWXA200400812.md): Wire · broken · Jul 25, 2004 · N174AW · Boeing 73733A · Light System Wiring
  > PHX - EEL - DURING 4-DAY CHECK EMERGENCY ESCAPE PATH LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 16 LT. MAINTENANCE REPAIRED A BROKEN WIRE FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400535](https://openairdocs.org/sdr/AWXA200400535.md): Light · inoperative · May 18, 2004 · N174AW · Boeing 73733A · Emergency Lighting
  > DEN - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY EXIT LIGHT JUST FORWARD OF THE L-2 DOOR IN THE LT AFT GALLEY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT AFT GALLEY EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400260](https://openairdocs.org/sdr/AWXA200400260.md): Wire · broken · Mar 10, 2004 · N174AW · Boeing 73733A · Light System Wiring
  > PHX - EEL - DURING 4-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN SPLICE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT; OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400198](https://openairdocs.org/sdr/AWXA200400198.md): Connector · loose · Feb 15, 2004 · N174AW · Boeing 73733A · Trailing Flap Position Indicating System
  > PHX - EMERGENCY LANDING - FLT 0769 - ON APPROACH INTO PHX EN ROUTE FROM MZT TRAILING EDGE FLAPS WENT ASYMMETRIC BETWEEN FLAP POSITION 1 & 2. ABORTED APPROACH AND RECYCLED FLAPS WITH SAME RESULTS, ACCOMPLISHED TRAILING EDGE FLAP ASYMMETRICAL CHECKLIST AND AS A
- [SDR AWXA200400169](https://openairdocs.org/sdr/AWXA200400169.md): Battery · discharged · Feb 10, 2004 · N174AW · Boeing 73733A · Emergency Equipment
  > LAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED CABIN EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400144](https://openairdocs.org/sdr/AWXA200400144.md): Wire · broken · Feb 4, 2004 · N174AW · Boeing 73733A · Light System Wiring
  > PHX - EEL - FLIGHT CREW REPORTED ELECTRICAL WIRE FOR EMERGENCY LIGHTING BROKEN IN AFT GALLEY AT LT TRASH BIN COMPARTMENT. MAINTENANCE REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT IN AFT GALLEY; OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200400137](https://openairdocs.org/sdr/AWXA200400137.md): Skin · cracked · Jan 30, 2004 · N174AW · Boeing 73733A · Fuselage Main, Plate/Skin
  > PHX - MAJOR REPAIR - DURING 8-DAY CHECK A 3 INCH CRACK WAS FOUND IN FUSELAGE SKIN JUST AFT OF WING TO BODY FAIRING BETWEEN BS 727D AND 727 E, AT STR 23 LT. MAINTENANCE CUT OUT DAMAGED SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED
- [SDR AWXA200400043](https://openairdocs.org/sdr/AWXA200400043.md): Support · corroded · Jan 7, 2004 · N174AW · Boeing 73733A · Trailing Edge Flaps
  > MCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MIDFLAP, INBOARD SPINDLE, OUTER BEARING SUPPORT. MAINTENANCE REMOVED AND REPLACED LT INBOARD MIDFLAP, INBOARD SPINDLE, OUTER BEARING SUPPORT PER AWA T/C I3R57057.
- [SDR AWXA200400042](https://openairdocs.org/sdr/AWXA200400042.md): Support · corroded · Jan 7, 2004 · N174AW · Boeing 73733A · Trailing Edge Flaps
  > MCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT INBOARD FLAP, INBOARD SPINDLE, OUTER BEARING SUPPORT. MAINTENANCE REMOVED AND REPLACED RT INBOARD FLAP, INBOARD SPINDLE, OUTER BEARING SUPPORT PER AWA T/C I3R57057.
- [SDR AWXA200400023](https://openairdocs.org/sdr/AWXA200400023.md): Spar · delaminated · Jan 4, 2004 · N174AW · Boeing 73733A · Ailerons
  > MCN - MINOR REPAIR - DURING C-18 CHECK THE RT AILERON FORWARD SPAR LOWER FLANGE WAS FOUND DELAMINATED AT ACCESS PANEL ATTACHMENT WS 430. MAINTENANCE TRIMMED OUT DAMAGE ON RT AILERON FORWARD SPAR, LOWER FLANGE; CLEANED AND PREPARED SURFACE; PERFORMED BOND REPAI
- [SDR AWXA200400008](https://openairdocs.org/sdr/AWXA200400008.md): Angle · cracked · Dec 21, 2003 · N174AW · Boeing 73733A · Fuselage Miscellaneous Structure
  > MCN - MINOR REPAIR - DURING C-18 CHECK A.5 INCH CRACK WAS FOUND ON LT AIR CONDITIONING BAY FORWARD OUTBOARD DUCT SUPPORT (TEE ANGLE) BS 530, LBL 58, WL 156. MAINTENANCE REMOVED CRACKED TEE ANGLE BS 530, LBL 58, WL 156; FABRICATED A NEW REPLACEMENT TEE ANGLE
- [SDR AWXA200400009](https://openairdocs.org/sdr/AWXA200400009.md): Clip · cracked · Dec 19, 2003 · N174AW · Boeing 73733A · Fuselage Miscellaneous Structure
  > MCN - MINOR REPAIR - DURING C-18 CHECK A.5 INCH CRACK WAS FOUND ON LT AIR CONDITIONING BAY FORWARD DUCT SUPPORT CLIP AT BS 530, LBL 56, WL 158. MAINTENANCE REMOVED CRACKED CLIP AT BS 530, LBL 56, WL 158; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-37254; IN
- [SDR AWXA200301540](https://openairdocs.org/sdr/AWXA200301540.md): Bracket · cracked · Dec 9, 2003 · N174AW · Boeing 73733A · Fuselage Miscellaneous Structure
  > DURING C-18 CHECK A.375 INCH CRACK WAS FOUND IN BRACKET FOR JUNCTION BOX J10 AT BS 380. MAINTENANCE REMOVED BRACKET FOR JUNCTION BOX J10 AT BS 380; FABRICATED A NEW REPLACEMENT BRACKET PER DWG 69-45146; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 6 &
- [SDR AWXA200301605](https://openairdocs.org/sdr/AWXA200301605.md): Floorbeam · cracked · Dec 8, 2003 · N174AW · Boeing 73733A · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND AT RT CENTER FLOORBEAM T-CAP ANGLE BS 540, BL-0. MAINTENANCE REMOVED CRACKED T-CAP ANGLE AT BS 540, BL-0; FABRICATED A NEW REPLACEMENT T-CAP ANGLE PER DWG 65-52894; INSTALLED REPAIR PART IAW B737
- [SDR AWXA200301598](https://openairdocs.org/sdr/AWXA200301598.md): Floorbeam · debonded · Dec 8, 2003 · N174AW · Boeing 73733A · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-18 CHECK THE CENTER LT FLOORBEAM T-CAP ANGLE WAS DISBONDED AT BS 540, LBL 22. MAINTENANCE REMOVED CRACKED T-CAP ANGLE AT BS 540, LBL 22; FABRICATED A NEW REPLACEMENT T-CAP ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, F
- [SDR AWXA200301579](https://openairdocs.org/sdr/AWXA200301579.md): Intercostal · cracked · Dec 8, 2003 · N174AW · Boeing 73733A · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.25 INCH CRACK WAS FOUND ON L-1 DOOR FORWARD INTERCOSTAL AT BS 294.5, STR 12 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT L-1 DOOR BS 294.5, STR 12 LT; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART
- [SDR AWXA200301595](https://openairdocs.org/sdr/AWXA200301595.md): Stringer · cracked · Dec 6, 2003 · N174AW · Boeing 73733A · Fuselage Main, Longeron/Stringer
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON STRINGER 16 LT AT LIGHT ASSEMBLY BS 500C. MAINTENANCE TRIMMED OUT CRACK ON STRINGER 16 LT AT LIGHT ASSEMBLY BS 500C; FABRICATED A REPAIR CHANNEL AND RADIUS FILLER; INSTALLED REPAIR PART IAW AW
- [SDR AWXA200301586](https://openairdocs.org/sdr/AWXA200301586.md): Stringer · cracked · Dec 6, 2003 · N174AW · Boeing 73733A · Fuselage Main, Longeron/Stringer
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.2500 INCH CRACK WAS FOUND ON STRINGER 16 RT AT LIGHT ASSEMBLY BS 500C. MAINTENANCE REMOVED DAMAGE FROM END OF STRINGER 16 RT AT BS 500C; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A RADIUS FILLER A
- [SDR AWXA200301542](https://openairdocs.org/sdr/AWXA200301542.md): Stringer Clip · cracked · Dec 6, 2003 · N174AW · Boeing 73733A · Fuselage Main, Attach Fittings
  > DURING C-18 CHECK A.25 INCH CRACK WAS FOUND IN STRINGER CLIP BS 520, STR 14 LT. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 520, STR 14 LT; RECEIVED A NEW REPLACEMENT STRINGER CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 45 & 64, FIG 12 & 14
- [SDR AWXA200400058](https://openairdocs.org/sdr/AWXA200400058.md): Wedge · delaminated · Dec 5, 2003 · N174AW · Boeing 73733A · Leading Edge Devices
  > MCN - MAJOR REPAIR - DURING C-18 CHECK FOUND THE NR 3 SLAT OUTBOARD END UPPER WEDGE SKIN DELAMINATED. MAINTENANCE CUT OUT DELAMINATED AREA NR 3 SLAT OUTBOARD END UPPER WEDGE SKIN; CLEANED AND PREPARED AREA; FABRICATED REPAIR DOUBLERS; INSTALLED BOND REPAIR IA
- [SDR AWXA200400004](https://openairdocs.org/sdr/AWXA200400004.md): Floorbeam · corroded · Dec 5, 2003 · N174AW · Boeing 73733A · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM AT FASTENER HOLE BS 344, RBL 7. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM CHORD; FABRICATED A NEW REPLACEMENT SECTION OF CHORD, 2 EACH REPAIR ANGLES, & 3 EACH WEB STIFF
- [SDR AWXA200301592](https://openairdocs.org/sdr/AWXA200301592.md): Skin · delaminated · Dec 5, 2003 · N174AW · Boeing 73733A · Leading Edge Devices
  > DURING C-18 CHECK THE NR 1 SLAT TRAILING EDGE WEDGE UPPER SKIN WAS FOUND DELAMINATED AT OUTBOARD MAIN TRACK. MAINTENANCE REMOVED DAMAGED NR 1 SLAT TRAILING EDGE WEDGE UPPER SKIN; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10
- [SDR AWXA200301591](https://openairdocs.org/sdr/AWXA200301591.md): Skin · delaminated · Dec 5, 2003 · N174AW · Boeing 73733A · Leading Edge Devices
  > DURING C-18 CHECK THE NR 1 SLAT TRAILING EDGE UPPER SKIN WAS FOUND DELAMINATED AT OUTBOARD AUXILIARY TRACK. MAINTENANCE REMOVED DAMAGED NR 1 SLAT TRAILING EDGE UPPER SKIN; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, FIG.
- [SDR AWXA200301589](https://openairdocs.org/sdr/AWXA200301589.md): Wedge · delaminated · Dec 5, 2003 · N174AW · Boeing 73733A · Leading Edge Devices
  > DURING C-18 CHECK THE NR 5 SLAT OB END UPPER WEDGE TRAILING EDGE SKIN WAS FOUND DELAMINATED AROUND PREVIOUS REPAIR. MAINTENANCE REMOVED PREVIOUS REPAIR AND DELAMINATED SKIN; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW 737-300 SRM 51-70-10, FIG.

Next page: https://openairdocs.org/deregistered/N174AW-2006-07-31/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 = 'N174AW' AND deregistration_id = 'N174AW-2006-07-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N174AW-2006-07-31/reports

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