# Service difficulty reports: N173AW, cancelled Jul 13, 2006

A list on [N173AW, cancelled Jul 13, 2006](https://openairdocs.org/deregistered/N173AW-2006-07-13.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 · 184 reports

- [SDR AWXA200600531](https://openairdocs.org/sdr/AWXA200600531.md): Skin · cracked · Mar 14, 2006 · N173AW · Boeing 73733A · Fuselage Main, Plate/Skin
  > MCN - DURING C22 CHECK DISCOVERED FUSELAGE SKIN CRACKED AT STR 22R AND BS 727E. MAINTENANCE TRIMMED OUT DAMAGE IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5361-06062-RC2. FABRICATED DOUBLER, TRIPLER, FILLER, TEAR STRAP INTERNAL DOUBLER AND TAPERED FIL
- [SDR AWXA200600527](https://openairdocs.org/sdr/AWXA200600527.md): Rib · cracked · Mar 8, 2006 · N173AW · Boeing 73733A · Horizontal Stabilizer, Spar/Rib
  > MCN - DURING C22 CHECK DISCOVERED LOWER CHORD OF STAB STA 138.7 RIB, CRACKED.7 INCHES AT FORWARD ATTACH POINT OF THE LT HORIZONTAL STABILIZER. MAINTENANCE REMOVED DAMAGED SECTION OF CHORD IAW BOEING 737-300 SRM 55-10-09-2R2 FIG 201. FABRICATED FILLER AND RE
- [SDR AWXA200600520](https://openairdocs.org/sdr/AWXA200600520.md): Support Angle · corroded · Feb 27, 2006 · N173AW · Boeing 73733A · Fuselage Main, Attach Fittings
  > MCN - MAJOR REPAIR - DURING C22 CHECK DISCOVERED LEVEL 2 EXFOLIATION CORROSION ON LOWER SURFACE OF THRESHOLD SUPPORT ANGLE FROM BS 947 TO BS 967, BL 55R AND WL 207. CORROSION WAS REMOVED AND RE-WORK WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-1
- [SDR AWXA200600583](https://openairdocs.org/sdr/AWXA200600583.md): Stringer Clip · cracked · Feb 19, 2006 · N173AW · Boeing 73733A · Fuselage Main, Attach Fittings
  > MCN - DURING C22 CHECK DISCOVERED STRINGER CLIP AT BS 947 STR 22L CRACKED, 0.350 INCHES. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 947 STR 22L IAW BOEING 737-300V SRM 51-40-02-0G PARA E FIG 8. FABRICATED STRINGER CLIP IAW BOIENG 737-300 SRM 51-30-01-0G
- [SDR AWXA200600543](https://openairdocs.org/sdr/AWXA200600543.md): Stringer · corroded · Feb 19, 2006 · N173AW · Boeing 73733A · Fuselage Main, Longeron/Stringer
  > MCN - DURING C22 CHECK DISCOVERED LEVEL 2 EXFOLIATION CORROSION ON STR 27L AND BS 967. CORROSION WAS REMOVED AND RE-WORK WAS FOUND OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-03-1A1 FIG 101. MAINTENANCE CUT OUT DAMAGED AREA ON STRINGER IAW BOEING 737-300 SRM
- [SDR AWXA200600528](https://openairdocs.org/sdr/AWXA200600528.md): Strap · cracked · Feb 19, 2006 · N173AW · Boeing 73733A · Fuselage Miscellaneous Structure
  > MCN - DURING C22 CHECK DISCOVERED 3 CRACKS,.25 INCHES IN LENGTH, ON INTERNAL STRAP AT BS 1006 FROM STR 27R TO STR 25R. MAINTENANCE CUT OUT AND REMOVED CRACKS ON INTERNAL STRAP AT BS 1006 BETWEEN STR 27R AND STR 25R IAW AMERICA WEST AIRLINES ENGINEERING REPAI
- [SDR AWXA200600519](https://openairdocs.org/sdr/AWXA200600519.md): Stringer · corroded · Feb 19, 2006 · N173AW · Boeing 73733A · Fuselage Main, Longeron/Stringer
  > MCN - DURING C22 CHECK DISCOVERED LEVEL 2 EXFOLIATION CORROSION ON STRINGER 26R AT BS 1006. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-03-1A1 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER, 26R, FROM BS 1006 TO BS 1016 IAW
- [SDR AWXA200600472](https://openairdocs.org/sdr/AWXA200600472.md): Stringer · corroded · Feb 19, 2006 · N173AW · Boeing 73733A · Fuselage Main, Longeron/Stringer
  > MCN - DURING C22 DISCOVERED LEVEL 2 CORROSION ON STRINGER 25L AT BS 967. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-03-1A1. MAINTENANCE REMOVED AND INSTALLED REPLACEMENT STRINGER FROM BS 967 TO BS 1016 AT STR 25L IAW BOEING 737-300
- [SDR AWXA200600584](https://openairdocs.org/sdr/AWXA200600584.md): Attach Bracket · cracked · Feb 18, 2006 · N173AW · Boeing 73733A · Fuselage Main, Attach Fittings
  > MCN - DURING C22 CHECK DISCOVERED ATTACH CLIP TO FRAME CRACKED, 0.500 INCHES, AT BS 706 TO STR 11L. MAINTENANCE REMOVED CRACKED CLIP AT BS 706 STR 11L IAW BOEING 737-300 SRM 51-40-02-0G PARA D FIGS 8 AND 12. INSTALLED NEW CLIP AT BS 706 FRAME TO STR 11L IAW
- [SDR AWXA200600585](https://openairdocs.org/sdr/AWXA200600585.md): Stringer Clip · cracked · Feb 13, 2006 · N173AW · Boeing 73733A · Fuselage Main, Attach Fittings
  > MCN - DURING C22 CHECK DISCOVERED STRINGER TO FRAME CLIP CRACKED, 0.25 INCHES, AT BS 663 TO STR 10R. MAINTENANCE REMOVED CRACKED CLIP AT BS 663 TO STR 10R IAW BOIENG 737-300 SRM 51-40-02-0G FIGS 8 AND 12. INSTALLED NEW CLIP AT BS 663 TO STR 10R IAW BOEING 73
- [SDR AWXA200600582](https://openairdocs.org/sdr/AWXA200600582.md): Clip · cracked · Feb 13, 2006 · N173AW · Boeing 73733A · Fuselage Main, Attach Fittings
  > MCN - DURING C22 CHECK DISCOVERED STRINGER TO FRAME CLIP CRACKED, 0.35 INCHES AT BS 639 STR 1. MAINTENANCE REMOVED CRACKED CLIP AT FRAME BS 639 STR 1 IAW BOEING 737-300 SRM 51-40-02-0G FIGS 8 AND 12. INSTALLED NEW CLIP AT FRAME BS 639 STR 1 IAW BOEING 737-30
- [SDR AWXA200600556](https://openairdocs.org/sdr/AWXA200600556.md): Stringer Clip · cracked · Feb 13, 2006 · N173AW · Boeing 73733A · Fuselage Main, Attach Fittings
  > MCN - DURING C22 CHECK DISCOVERED CRACKED STRINGER TIE CLIP, CRACKED.25 INCHES, AT BS 639 STR 2R. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE CLIP AT BS 639 STR 2R IAW BOEING 737-300 SRM 51-40-02-0G.
- [SDR AWXA200600555](https://openairdocs.org/sdr/AWXA200600555.md): Stringer Clip · cracked · Feb 13, 2006 · N173AW · Boeing 73733A · Fuselage Main, Attach Fittings
  > MCN - DURING C22 CHECK DISCOVERED STRINGER CLIP CRACKED,.400 INCHES IN LENGTH, AT BS 616 AND STR 2L. MAINTENANCE REMOVED AND INSTALLED NEW CLIP AT BS 616 AND STR 2L IAW BOEING 737-300 SRM 51-40-02-0G FIG 8 AND 12.
- [SDR AWXA200600550](https://openairdocs.org/sdr/AWXA200600550.md): Stringer Clip · cracked · Feb 13, 2006 · N173AW · Boeing 73733A · Fuselage Main, Attach Fittings
  > MCN - MAJOR REPAIR - DURING C22 CHECK DISCOVERED STRING 10L CLIP CRACKED,.375 INCHES, AT BS 663. MAINTENANCE REMOVED AND REPLACED THE STRINGER TIE CLIP AT STR 10L AND BS 663 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 6, 7, AND 8.
- [SDR AWXA200600547](https://openairdocs.org/sdr/AWXA200600547.md): Stringer Clip · cracked · Feb 13, 2006 · N173AW · Boeing 73733A · Fuselage Main, Attach Fittings
  > MCN - MAJOR REPAIR - DURING C22 CHECK DISCOVERED STRINGER TO FRAME CLIP CRACKED,.4 INCHES, AT BS 639, STR 4R. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE CLIP ON FRAME AT BS 639 AND STR 4R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 6, 7, AND 8.
- [SDR AWXA200600526](https://openairdocs.org/sdr/AWXA200600526.md): Frame · corroded · Feb 13, 2006 · N173AW · Boeing 73733A · Fuselage Main, Frame
  > MCN - DURING C22 CHECK DISCOVERED LEVEL 2 EXFOLIATION CORROSION ON AFT SIDE OF FRAME TIE AT BS 967 BETWEEN STR 27L AND STR 27R. CORROSION WAS REMOVED AND RE-WORK WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-07-1A1 FIG 101. DAMAGED AREA WAS REMO
- [SDR AWXA200600471](https://openairdocs.org/sdr/AWXA200600471.md): Web · cracked · Feb 13, 2006 · N173AW · Boeing 73733A · Fuselage Miscellaneous Structure
  > MCN - DURING C22 CHECK DISCOVERED WEB CRACKED, 3.0 INCHES, FROM BS 616 TO BS 639 AT STR 17R, CREASE BEAM 5-17 RT. MAINTENANCE REMOVED AND INSTALLED REPLACEMENT WEB FROM BS 616 TO BS 639 AT STR 17R, CREASE BEAM 5-17 RT IAW BOEING 737-300 SRM 51-10-02-0G FIG 8
- [SDR AWXA200600470](https://openairdocs.org/sdr/AWXA200600470.md): Frame · cracked · Feb 13, 2006 · N173AW · Boeing 73733A · Fuselage Main, Frame
  > MCN - MAJOR REPAIR - DURING C22 CHECK DISCOVERED FRAME 639 WEB CRACKED,.75 INCHES, ABOVE CREASE BEAM AT STR 16R. NO REPAIR DATA COULD BE FOUND IN THE SRM. MAINTENANCE CUT OUT DAMAGED AREA OF WEB AT BS 639 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5
- [SDR AWXA200600460](https://openairdocs.org/sdr/AWXA200600460.md): Skin · cracked · Feb 11, 2006 · N173AW · Boeing 73733A · Fuselage Main, Plate/Skin
  > DURING C22 CHECK DISCOVERED FUSELAGE SKIN CRACKED AT STR 24R AND BS 870. THREE EXISTING REPAIRS IN AREA, BETWEEN 847 AND BS 875 BELOW STR 20R, WHICH WOULD EXCEED THE DAMAGE PARAMETERS OF BOEING 737-300 SRM 53-00-01 FIG 201 REPAIR 31 OR REPAIR 32 GUIDELINES.
- [SDR AWXA200600586](https://openairdocs.org/sdr/AWXA200600586.md): Shear Web · cracked · Feb 9, 2006 · N173AW · Boeing 73733A · Fuselage Miscellaneous Structure
  > MCN - DURING C22 CHECK DISCOVERED WEB CRACKED, 1.1 INCHES, AT BS 560 TO BS 580 BL 65L. MAINTENANCE REMOVED DAMAGE FROM WEB AT BS 560 TO BS 580, BL 65L IAW BOEING 737-300 SRM 51-70-13-0G FIG. 1. FABRICATED PLATE IAW BOEING 737-300 SRM 41-70-13-0G FIG. 1. INS
- [SDR AWXA200600542](https://openairdocs.org/sdr/AWXA200600542.md): Skin · cracked · Feb 8, 2006 · N173AW · Boeing 73733A · Fuselage Main, Plate/Skin
  > MCN - DURING C22 CHECK DISCOVERED FUSELAGE SKIN CRACKED,.5 INCHES IN LENGTH, AT BS 727E+7" AT STR 19R. MAINTENANCE CUT OUT DAMAGED AREA IAW BOEING 737-300 SRM 53-00-01-2R31. FABRICATED REPAIR DOUBLER IAW BOEING 737-300 SRM 53-00-01-2R31. INSTALLED FABRICAT
- [SDR AWXA200600522](https://openairdocs.org/sdr/AWXA200600522.md): Skin · corroded · Feb 8, 2006 · N173AW · Boeing 73733A · Fuselage Main, Plate/Skin
  > MCN - DURING C22 CHECK DISCOVERED LEVEL 2 CORROSION ON AFT CARGO COMPARTMENT FUSELAGE SKIN AT BS 985, BOTH SIDES OF STR 27L. ALSO AT BS 1006 OUTBOARD SIDE OF STR 27L AND BS 985 AT STR 25R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-
- [SDR AWXA200600521](https://openairdocs.org/sdr/AWXA200600521.md): Attach Angle · corroded · Feb 8, 2006 · N173AW · Boeing 73733A · Fuselage Main, Attach Fittings
  > MCN - DURING C22 CHECK DISCOVERED CORROSION ON AFT CARGO FLOOR WEB ATTACH ANGLE AT BS 767+6" TO 785 AND BL 19R. CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW ATTACH ANGL
- [SDR AWXA200600338](https://openairdocs.org/sdr/AWXA200600338.md): Skin · debonded · Feb 8, 2006 · N173AW · Boeing 73733A · Trailing Edge Flaps
  > MCN - MAJOR REPAIR - DURING C22 CHECK DISCOVERED DISBOND AREA ON THE UPPER SURFACE OF THE LT OUTBOARD AFT FLAP AT THE INBOARD END, FROM WS 230.68L TO WS 239.68L. MAINTENANCE REMOVED DISBOND AREA FROM THE LT OUTBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R
- [SDR AWXA200600337](https://openairdocs.org/sdr/AWXA200600337.md): Skin · debonded · Feb 7, 2006 · N173AW · Boeing 73733A · Trailing Edge Flaps
  > MCN - DURING C22 CHECK DISCOVERED DISBOND AREA ON THE UPPER SURFACE OF THE LT OUTBOARD FORE FLAP, 93 INCHES FROM THE INBOARD END, FROM WS 290.69L TO WS 296.69L. MAINTENANCE REMOVED DISBOND AREA FROM THE LT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-2R
- [SDR AWXA200600336](https://openairdocs.org/sdr/AWXA200600336.md): Skin · debonded · Feb 7, 2006 · N173AW · Boeing 73733A · Trailing Edge Flaps
  > MCN - DURING C22 CHECK DISCOVERED DISBOND ARE ON THE LOWER SURFACE OF THE RT INBOARD MID FLAP TRAILING EDGE WEDGE, 32 INCHES FROM THE INBOARD END, FROM WS 101.75R TO WS 109.25R. MAINTENANCE REMOVED DISBOND AREA FROM THE RT INBOARD MID FLAP IAW BOEING 737-300
- [SDR AWXA200600132](https://openairdocs.org/sdr/AWXA200600132.md): Battery · inoperative · Jan 24, 2006 · N173AW · Boeing 73733A · Emergency Lighting
  > PHX - EEL - DURING INSPECTION MAINTENANCE REPORTED THAT SEATS 1A AND 1B EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED 3 BATTERIES IN FIRST CLASS AISLE AND INSPECTED ALL THE WIRING ON THE FLOOR INTO THE SIDEWALL, NO DISCREPANCIES WERE FOU
- [SDR AWXA200501564](https://openairdocs.org/sdr/AWXA200501564.md): Trim System · malfunctioned · Dec 19, 2005 · N173AW · Boeing 73733A · Stabilizer Position Indicating
  > PHX - ABORTED TAKEOFF - FLT 227 - CREW REPORTED THAT THE TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF. ABORTED TAKEOFF AT APPROXIMATELY 45 KNOTS. CAPTAINS TRIM SHOWED 4.8 WHILE THE F/O'S SHOWED 5.2. CREW RESET STAB TRIM AND RECEIVED NO FURTHER WARNINGS.
- [SDR AWXA200501094](https://openairdocs.org/sdr/AWXA200501094.md): Light · inoperative · Sep 22, 2005 · N173AW · Boeing 73733A · Emergency Lighting
  > PHX - EEL - DURING 4 DAY CHECK, DISCOVERED PASSENGER ROW NR 18 EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE DURING TEST. MAINTENANCE REMOVED AND REPLACED ROW NR 18 EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL TESTS WERE GOOD.
- [SDR AWXA200501016](https://openairdocs.org/sdr/AWXA200501016.md): Battery · inoperative · Aug 30, 2005 · N173AW · Boeing 73733A · Emergency Lighting
  > PHX - EEL - DURING INSPECTION DISCOVERED EMERGENCY EXIT PATHWAY LIGHTS AT ROWS 1, 2, 3, AND 4 ARE ON DIM WITH SWITCH IN OFF OR ARMED POSITION. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTER IAW MAINTENANCE MANUAL 33-51. OPERATIONAL CHECKS WERE GOOD.
- [SDR AWXA200500982](https://openairdocs.org/sdr/AWXA200500982.md): Skin · cracked · Aug 17, 2005 · N173AW · Boeing 73733A · Fuselage Main, Plate/Skin
  > PHX - DURING 4 DAY CHECK, FOUND SKIN CRACK ON LEFT SIDE OF FUSELAGE APPROX 1' AFT AND 1' BELOW EMERGENCY LIGHT AFT OF MLG WHEEL WELL. MAINTENANCE REMOVED DAMAGED SKIN AT STA JUST FWD OF 747, STR 24L PER BOEING 737-300 SRM 51-00-01. FABRICATED DOUBLER AND INS
- [SDR AWXA200500718](https://openairdocs.org/sdr/AWXA200500718.md): Charger · inoperative · Jun 14, 2005 · N173AW · Boeing 73733A · Emergency Lighting
  > DURING C-21 CHECK EMERGENCY EXIT LIGHTS AT SEATS 1-4 INOPERATIVE AND SEAT 17 LAMP OUT. MX REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER IAW BOEING 737-300 AMM 31-51-51-962-016. OPS CHECK GOOD IAW AMERICA WEST AIRLINES TASK CARD A1C33006.
- [SDR AWXA200500700](https://openairdocs.org/sdr/AWXA200500700.md): Fitting · corroded · Jun 13, 2005 · N173AW · Boeing 73733A · Fuselage, Landing Gear Attach Fittings
  > MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND CORROSION ON LEFT MAIN LANDING GEAR STABILIZER BEAM ATTACH FITTING ON WING AT RSS 197.56. MAINTENANCE BLENDED CORROSION ON LEFT MAIN LANDING GEAR STABILIZER BEAM ATTACH FITTING AND DETERMINED TO BE OUT OF LIMITS.
- [SDR AWXA200500699](https://openairdocs.org/sdr/AWXA200500699.md): Stiffener · cracked · Jun 13, 2005 · N173AW · Boeing 73733A · Fuselage Main, Bulkhead
  > MCN - MAJOR REPAIR - DURING C-21 CHECK DISCOVERED 2 CRACKS.113 INCHES IN LENGTH ON ANGLE LOCATED AT BULKHEAD STA 178 LBL 5.7 WL 184. MAINTENANCE CUT OUT AND REMOVED DAMAGED AREA FROM BULKHEAD LOCATED AT STA 178. FABRICATED REPAIR ANGLES, STRAPS, FILLERS IAW
- [SDR AWXA200500717](https://openairdocs.org/sdr/AWXA200500717.md): Spar · cracked · Jun 12, 2005 · N173AW · Boeing 73733A · Horizontal Stabilizer, Spar/Rib
  > DURING C-21 CHECK, DISCOVERED RT HORIZONTAL STAB CHANNEL CRACKED ON AFT SPAR WEB AT STAB STATION 170. MX CUT OUT CRACKED SECTION ON AFT SPAR WEB AT STAB STATION 170 AND FABRICATED REPLACEMENT PARTS IAW BOEING 737-300 SRM 51-70-11-0 FIG 1. BONDED AND INSTALLE
- [SDR AWXA200500696](https://openairdocs.org/sdr/AWXA200500696.md): Stiffener · cracked · Jun 7, 2005 · N173AW · Boeing 73733A · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-21 CHECK DISCOVERED CRACK.322 INCHES LONG AT FORMED CHANNEL LOCATED AT BS 178 WL 230 RBL 17.1. MAINTENANCE REMOVED AND FABRICATED NEW CHANNEL IAW BOEING DWG 9-63089. INSTALLED FABRICATED REPAIR PARTS AT BS 178 WL 230 RBL 17.1 I
- [SDR AWXA200500693](https://openairdocs.org/sdr/AWXA200500693.md): Stiffener · cracked · Jun 7, 2005 · N173AW · Boeing 73733A · Fuselage Main, Bulkhead
  > MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND SUPPORT ANGLE CRACKED AT BS 178 WL 230 RBL 17.1. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE AND FABRICATED SUPPORT ANGLE IAW BOEING DWG 65-17582. INSTALLED FABRICATED REPAIR PARTS AT BS 178 WL 230 RBL 17.1 IAW BOEI
- [SDR AWXA200500713](https://openairdocs.org/sdr/AWXA200500713.md): Doubler · cracked · Jun 2, 2005 · N173AW · Boeing 73733A · Fuselage Main, Structure
  > MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND TOP 3 OUTBOARD SCREW HOLES ON FIRST OFFICERS NR 1 WINDOW FRAME TO HAVE EVIDENCE OF CRACKING INSIDE HOLES. MAINTENANCE REMOVED CRACKED DOUBLER IAW BOEING 737-300 SRM 53-10-01-2 FIG 210. INSTALLED REPLACEMENT DOUBLE
- [SDR AWXA200500710](https://openairdocs.org/sdr/AWXA200500710.md): Skin · cracked · Jun 2, 2005 · N173AW · Boeing 73733A · Leading Edge Devices
  > MCN - DURING C-21 CHECK FOUND 2 CRACKS.275 INCHES IN LENGTH. BOTH CRACKS LOCATED ON THE BOTTOM OF THE NR 4 SLAT SKIN, AT SS 72 TO SS 74. MAINTENANCE CUT OUT DAMAGED AREA AT NR 4 SLAT SKIN AND FABRICATED REPAIR DOUBLER AND FILLER IAW BOEING 737-300 SRM 57-43
- [SDR AWXA200500692](https://openairdocs.org/sdr/AWXA200500692.md): Bulkhead · cracked · Jun 2, 2005 · N173AW · Boeing 73733A · Fuselage Main, Bulkhead
  > MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND 3 CRACKS.271 INCHES LONG AT FRAME WEB STA 178 WL 230 RBL 17.1. MAINTENANCE REMOVED DAMAGED AREA FROM FRAME WEB STA 178 WL 230 RBL 17.1 AND FABRICATED WEB AND TAPERED SHIMS IAW BOEING 737-300 SRM 53-10-08-2 FIG 212
- [SDR AWXA200500691](https://openairdocs.org/sdr/AWXA200500691.md): Skin · cracked · Jun 2, 2005 · N173AW · Boeing 73733A · Leading Edge Devices
  > MCN - MAJOR REPAIR - DURING C-21 CHECK DISCOVERED 2 CRACKS.275 INCHES LONG LOCATED AT THE BOTTOM OF THE NR 6 SLAT SKIN, SLAT STATION 307 TO SLAT STATION 309. MAINTENANCE REMOVED DAMAGED AREA FROM THE BOTTOM OF NR 6 SLAT SKIN FROM SLAT STATION 307 TO SLAT STA
- [SDR AWXA200500678](https://openairdocs.org/sdr/AWXA200500678.md): Web · cracked · Jun 2, 2005 · N173AW · Boeing 73733A · Fuselage Miscellaneous Structure
  > DURING C-21 CHECK, FOUND FLOOR WEB CRACKED AT BS 196.5, WL 207, RIGHT BL 28. MAINTENANCE REMOVED CRACKED FLOOR WEB AT BS 196.5, WL 207, RIGHT BL 28 AND FABRICATED NEW WEB IAW BOEING 737-300 SRM 51-40-02 FIGURE 2 AND DWG 65-45833. INSTALLED FABRICATED REPAIR
- [SDR AWXA200500677](https://openairdocs.org/sdr/AWXA200500677.md): Web · cracked · Jun 2, 2005 · N173AW · Boeing 73733A · Fuselage Miscellaneous Structure
  > DURING C-21 CHECK, FOUND FLOOR WEB CRACKED AT BS 196.5, WL 207, LEFT BL 28. MAINTENANCE REMOVED CRACKED FLOOR WEB AT BS 196.5, WL 207, LEFT BL 28 AND FABRICATED NEW WEB IAW BOEING 737-300 SRM 51-40-02 FIGURE 2 AND DWG 65-45833. INSTALLED FABRICATED REPAIR PA
- [SDR AWXA200500741](https://openairdocs.org/sdr/AWXA200500741.md): Skin · delaminated · Jun 1, 2005 · N173AW · Boeing 73733A · Leading Edge Devices
  > FOUND DISBOND AREA ON UPPER SURFACE OF NR 5 SLAT, 1.75 IN FROM OUTBOARD END, FROM RT SS 252 TO RT SS 253. MAINTENANCE CUTOUT SKIN AND DISBOND CORE FROM UPPER SURFACE OF NR 5 SLAT, 1.75 IN FROM OUTBOARD END, IAW BOEING 737-300 SRM 51-70-10-0 REPAIR 7, FIG 16.
- [SDR AWXA200500690](https://openairdocs.org/sdr/AWXA200500690.md): Bulkhead · cracked · Jun 1, 2005 · N173AW · Boeing 73733A · Fuselage Main, Bulkhead
  > DURING C-21 CHECK FOUND A CRACK.275 INCHES IN LENGTH AT BULKHEAD WEB BS 178, WL 234, AND LBL 14. MAINTENANCE REMOVED CRACKED AREA AT BULKHEAD WEB BS 178, WL 234, LBL 14 AND FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2 FIG 209. INSTALLED F
- [SDR AWXA200500689](https://openairdocs.org/sdr/AWXA200500689.md): Frame · cracked · Jun 1, 2005 · N173AW · Boeing 73733A · Fuselage Main, Frame
  > MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND CRACK.211 INCHES LONG AT 178 BULKHEAD FRAME WEB, RBL 17, WL 182. MAINTENANCE REMOVED DAMAGED AREA AT BULKHEAD FRAME WEB 178, RBL 17, WL 182 AND FABRICATED NEW WEB IAW BOEING 737-300 SRM 53-10-08-2 FIGURE 212. INS
- [SDR AWXA200500688](https://openairdocs.org/sdr/AWXA200500688.md): Support Beam · corroded · Jun 1, 2005 · N173AW · Boeing 73733A · Fuselage Main, Structure
  > MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND CORROSION ON DIAGONAL SUPPORT BEAM BOTTOM SIDE AROUND FASTENER HOLES FROM BS 1006 TO BS 1016, RBL 6. MAINTENANCE BLENDED OUT CORROSION AT BS 1006 TO BS 1016, RBL 6 AND FOUND REMAINING MATERIAL TO BE OUT OF LIMITS.
- [SDR AWXA200500719](https://openairdocs.org/sdr/AWXA200500719.md): Door Frame · cracked · May 31, 2005 · N173AW · Boeing 73733A · Fuselage Main, Structure
  > DURING C-21 CHECK, FOUND CRACK.750 INCHES IN LENGTH AT FORWARD CARGO DOOR LOCATED ON FORWARD EDGE BELOW HOLD OPEN HOOK. MX REMOVED CRACKED CARGO DOOR FRAME IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. INSTALLED NEW FRAME ASSEMBLY IAW BOEING 737-300 SRM 51-40-02
- [SDR AWXA200500687](https://openairdocs.org/sdr/AWXA200500687.md): Angle · cracked · May 31, 2005 · N173AW · Boeing 73733A · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND CRACK.5 INCH IN LENGTH AT R1 DOOR CUTOUT ANGLE ON BS 294.5 AND BS 294.6, BETWEEN STRINGER 7R AND STRINGER 8R. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 737-300 SRM 51-70-11 AND FABRICATED NEW ANGLE IAW BOEING 73
- [SDR AWXA200500686](https://openairdocs.org/sdr/AWXA200500686.md): Bulkhead · cracked · May 31, 2005 · N173AW · Boeing 73733A · Fuselage Main, Bulkhead
  > MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND A CRACK.375 INCH AT 178 BULKHEAD WEB, WL 207, RBL 10. MAINTENANCE REMOVED DAMAGED AREA FROM 178 BULKHEAD WEB, WL 207, RBL 10 IAW BOEING 737-300 SRM 53-10-08 FIG 209. FABRICATED DOULBER AND INSTALLED REPAIR PARTS

Next page: https://openairdocs.org/deregistered/N173AW-2006-07-13/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 = 'N173AW' AND deregistration_id = 'N173AW-2006-07-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N173AW-2006-07-13/reports

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