# Service difficulty reports: N327AW, cancelled Jul 31, 2007

A list on [N327AW, cancelled Jul 31, 2007](https://openairdocs.org/deregistered/N327AW-2007-07-31.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 · 190 reports

- [SDR AWXA200500701](https://openairdocs.org/sdr/AWXA200500701.md): Indicator · failed · Jun 14, 2005 · N327AW · Boeing 7373Q8 · Airspeed/Mach Indicator
  > PHX - ABORTED TAKEOFF - FLT 792 - DURING TAKEOFF CAPTAINS AIRSPEED INDICATOR WAS FLAGGED AND NO AIRSPEED INDICATION. ABORTED TAKEOFF AT 90 KNOTS, RETURNED TO THE GATE IN PHOENIX WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 MACH AIRSPEED IN
- [SDR AWXA200500193](https://openairdocs.org/sdr/AWXA200500193.md): Light · broken · Feb 12, 2005 · N327AW · Boeing 7373Q8 · Light System Wiring
  > PHX - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT INOPERATIVE. MAINTENANCE FOUND WIRES PULLED FROM CONNECTOR OF EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 7 LT, REMOVED AND REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK W
- [SDR AWXA200500134](https://openairdocs.org/sdr/AWXA200500134.md): Reveal · cracked · Jan 20, 2005 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, A 3/4 INCH CRACK WAS FOUND IN R-1 DOOR FORWARD UPPER CORNER REVEAL. MAINTENANCE REMOVED CRACKED REVEAL FROM BS 298 TO BS 306, STR 10 RT TO STR 11 RT, INSTALLED NEW REPLACEMENT PART IAW B737-300 SRM 51-40-02.
- [SDR AWXA200500115](https://openairdocs.org/sdr/AWXA200500115.md): Stringer Clip · cracked · Jan 8, 2005 · N327AW · Boeing 7373Q8 · Fuselage Main, Attach Fittings
  > MCN - MAJOR REPAIR - DURING C-17 CHECK A 5/16 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 867, STR 1. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 867, STR 1; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-30
- [SDR AWXA200500069](https://openairdocs.org/sdr/AWXA200500069.md): Intercostal · cracked · Jan 8, 2005 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON LT AFT LAVATORY SUBFLOOR PAN TO AFT PRESSURE BULKHEAD CLOSEOUT WEB (INTERCOSTAL FLOOR SEAL) AT BS 1032, LBL 27.38. MAINTENANCE REMOVED DAMAGED PORTION OF INTERCOSTAL FLOOR SEAL AT BS 1032, LBL
- [SDR AWXA200500028](https://openairdocs.org/sdr/AWXA200500028.md): Wedge · delaminated · Jan 6, 2005 · N327AW · Boeing 7373Q8 · Leading Edge Devices
  > MCN - MAJOR REPAIR - DURING C-17 CHECK A DISBOND AREA WAS FOUND IN NR 5 SLAT WEDGE ON UPPER SURFACE AT INBOARD END BETWEEN SS 131.50 AND SS 132.50. MAINTENANCE CUT OUT DAMAGE IN NR 5 SLAT WEDGE AT UPPER INBOARD END; FABRICATED A FILLER AND DOUBLER; BONDED REP
- [SDR AWXA200500138](https://openairdocs.org/sdr/AWXA200500138.md): Frame · corroded · Jan 3, 2005 · N327AW · Boeing 7373Q8 · Fuselage Main, Frame
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, GALVANIC CORROSION WAS FOUND ON UPPER SURFACE, UPPER FLANGE, OF FRAME AT BS 847, RBL 17.50. MAINTENANCE CUTOUT CORRODED SECTION OF FRAME AT BS 847, RBL 17.50; FABRICATED A 2 EACH ANGLES, A FILLER, SUPPORT CHANNEL, CLIP,
- [SDR AWXA200500035](https://openairdocs.org/sdr/AWXA200500035.md): Skin · cracked · Jan 3, 2005 · N327AW · Boeing 7373Q8 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-17 CHECK A 6 INCHES CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727D+17, STR 22 LT. MAINTENANCE CUT OUT CRACK IN FUSELAGE SKIN AT BS 727D+17, STR 22 LT; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUBLER
- [SDR AWXA200500118](https://openairdocs.org/sdr/AWXA200500118.md): Web · corroded · Jan 2, 2005 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON R-1 DOOR THRESHOLD SHEAR WEB BETWEEN BS 344 AND BS 360, RBL 64 AND RBL 68. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 344 TO BS 360, RBL 64 TO RBL 68; FABRICATED A NEW REPLACEMENT SH
- [SDR AWXA200500047](https://openairdocs.org/sdr/AWXA200500047.md): Skin · cracked · Jan 2, 2005 · N327AW · Boeing 7373Q8 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-17 CHECK A 3 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727D + 17 INCHES, STR 24 RT. MAINTENANCE CUTOUT CRACKED SECTION OF FUSELAGE SKIN AT BS 727D + 17 INCH, STR 24 RT; FABRICATED A FILLER, DOUBLER AND TRIPLER; INSTALLED REPAIR
- [SDR AWXA200500023](https://openairdocs.org/sdr/AWXA200500023.md): Skin · cracked · Jan 2, 2005 · N327AW · Boeing 7373Q8 · Fuselage Main, Plate/Skin
  > DURING C-17 CHECK A 3 INCH CRACK WAS FOUND IN FUSELAGE SKIN EXTENDING FROM RIVET HOLE AT BS 727C, STR 15 LT. MAINTENANCE CUT OUT DAMAGE IN FUSELAGE AT BS 727C, STR 15 LT, PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUB
- [SDR AWXA200500025](https://openairdocs.org/sdr/AWXA200500025.md): Stringer Clip · cracked · Dec 29, 2004 · N327AW · Boeing 7373Q8 · Fuselage Main, Attach Fittings
  > DURING C-17 CHECK A.1875 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT AFT SIDE OF BS 1006, STR 14 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 1006, STR 14 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35364; INSTALLED REPAIR PART IAW B737-
- [SDR AWXA200500119](https://openairdocs.org/sdr/AWXA200500119.md): Attach Bracket · corroded · Dec 28, 2004 · N327AW · Boeing 7373Q8 · Escape Slide
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON L-1 DOOR AFT GIRT BAR ATTACH BRACKET AT BS 344 LBL 58. MAINTENANCE REMOVED CORRODED L-1 DOOR AFT GIRT BAR ATTACH BRACKET AT BS 344 LBL 58; FABRICATED A NEW REPLACEMENT BRACKET; INSTALLED REPAIR PA
- [SDR AWXA200500117](https://openairdocs.org/sdr/AWXA200500117.md): Stiffener · corroded · Dec 28, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON AFT PRESSURE BULKEAD FORWARD FACE STIFFENER CHANNEL REPAIR ANGLE AT BS 1022, LBL 0.5, WL 195. MAINTENANCE REMOVED CORRODED PREVIOUS REPAIR ON AFT PRESSURE BULKEAD FORWARD FACE STIFFENER CHANNEL AT
- [SDR AWXA200500116](https://openairdocs.org/sdr/AWXA200500116.md): Floor Support · corroded · Dec 28, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT BS 324, RBL 10, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 324, RBL 10; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-
- [SDR AWXA200500100](https://openairdocs.org/sdr/AWXA200500100.md): Intercostal · corroded · Dec 28, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF INTERCOSTAL UPPER LEG AT BS 270, BETWEEN LBL 7 AND RBL 1. MAINTENANCE CUTOUT DAMAGE IN INTERCOSTAL UPPER LEG AT BS 270, FROM LBL 7 TO RBL 1; FABRICATED A FILLER AND RE
- [SDR AWXA200500099](https://openairdocs.org/sdr/AWXA200500099.md): Floorbeam · corroded · Dec 28, 2004 · N327AW · Boeing 7373Q8 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 328, FROM BL "0" TO RBL 53. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM UPPER CHORD AT BS 328, FROM BL "0" TO RBL 53; FABRICATED A NEW
- [SDR AWXA200500070](https://openairdocs.org/sdr/AWXA200500070.md): Web · cracked · Dec 28, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.5 INCH CRACK WAS FOUND ON LT AFT OUTBOARD SHEAR WEB, ADJACENT TO WATER LINE FITTING BETWEEN BS 996 AND BS 1005, LBL 39 AND LBL 42, WL 208. MAINTENANCE REMOVED DAMAGED AREA OF LT AFT OUTBOARD SHEAR WEB FROM BS 996 TO
- [SDR AWXA200500068](https://openairdocs.org/sdr/AWXA200500068.md): Floorbeam · corroded · Dec 28, 2004 · N327AW · Boeing 7373Q8 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 344 BETWEEN LBL 15 AND RBL 10. MAINTENANCE REMOVED CORRODED UPPER CHORD AT BS 344 FROM LBL 15 TO RBL 40; FABRICATED A NEW REPLACEMENT UPPER CH
- [SDR AWXA200500060](https://openairdocs.org/sdr/AWXA200500060.md): Angle · cracked · Dec 28, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK 3 EACH CRACKS WERE FOUND IN CABIN FLOOR STIFFENER ANGLE BETWEEN BS 380 AND BS 400, AT BL 0. MAINTENANCE REMOVED CRACKED STIFFENER ANGLE FROM BS 380 TO BS 400, AT BL 0; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-35365;
- [SDR AWXA200500046](https://openairdocs.org/sdr/AWXA200500046.md): Intercostal · cracked · Dec 28, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK A 2 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 342, LBL 46, WL 208. MAINTENANCE REMOVED CRACKED INTERCOSTAL FROM BS 328 TO BS 344, LBL 46; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-45834; INSTALLED REPAIR PART I
- [SDR AWXA200500045](https://openairdocs.org/sdr/AWXA200500045.md): Intercostal · cracked · Dec 28, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK A 2 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 326, RBL 34, WL 208. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 326, RBL 34; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-300
- [SDR AWXA200500133](https://openairdocs.org/sdr/AWXA200500133.md): Channel · corroded · Dec 27, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON STRINGER 28 RT BETWEEN BS 353 AND BS 363. MAINTENANCE REMOVED STRINGER TIE CLIP AND CORRODED SECTION OF STRINGER 28 RT FROM BS 353 TO BS 363; FABRICATED A NEW REPLACEMENT SECTION OF ST
- [SDR AWXA200500132](https://openairdocs.org/sdr/AWXA200500132.md): Skin · corroded · Dec 27, 2004 · N327AW · Boeing 7373Q8 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF LOWER SKIN AT BS 358, ON INBOARD AND OUTBOARD SIDE OF STR 27 LT. MAINTENANCE CUTOUT CORRODED SECTION OF SKIN AT BS 358, STR 27 LT; PERFORMED HFEC INSPECTION OF CUTOUT
- [SDR AWXA200500126](https://openairdocs.org/sdr/AWXA200500126.md): Channel · cracked · Dec 27, 2004 · N327AW · Boeing 7373Q8 · Vertical Stabilizer Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK A 1/2" CRACK WAS FOUND IN VERTICAL STABILIZER LOWER ANGLE (CHANNEL) ON AFT SIDE OF RT AFT LUGS BS 1016, STR 2 RT. MAINTENANCE REMOVED CRACKED VERTICAL STABILIZER LOWER CHANNEL AT BS 1016, STR 2 RT; FABRICATED A NEW REPLAC
- [SDR AWXA200500123](https://openairdocs.org/sdr/AWXA200500123.md): Channel · corroded · Dec 27, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON STRINGER SPLICE BETWEEN BS 355 AND BS 363, STR 27 LT. MAINTENANCE REMOVED CORRODED STRINGER SPLICE FROM BS 355 TO BS 363, 27 LT; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER SPLICE
- [SDR AWXA200500122](https://openairdocs.org/sdr/AWXA200500122.md): Angle · corroded · Dec 27, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON INTERCOSTAL ATTACH ANGLE AT BS 357, OUTBOARD OF STRINGER 28 LT. MAINTENANCE REMOVED CORRODED INTERCOSTAL ATTACH ANGLE AT BS 357, STR 28 LT; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLE
- [SDR AWXA200500113](https://openairdocs.org/sdr/AWXA200500113.md): Frame · corroded · Dec 27, 2004 · N327AW · Boeing 7373Q8 · Fuselage Main, Frame
  > MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SIDE OF FRAME AT BS 360, BETWEEN STR 27 LT AND STR 28 LT. MAINTENANCE REMOVED SHEAR TIE AND CUTOUT DAMAGE IN FRAME FOOT AT BS 360, BETWEEN STR 27 LT AND STR 28 LT; FABRICATED A NEW
- [SDR AWXA200500105](https://openairdocs.org/sdr/AWXA200500105.md): Shear Tie · corroded · Dec 27, 2004 · N327AW · Boeing 7373Q8 · Fuselage Main, Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON SHEAR TIE AT BS 1006, BETWEEN STR 27 LT AND STR 27 RT. MAINTENANCE REMOVED CORRODED SHEAR TIE AT BS 1006, FROM STR 27 LT TO STR 27 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 65
- [SDR AWXA200500156](https://openairdocs.org/sdr/AWXA200500156.md): Pan · corroded · Dec 24, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF LT AFT LAVATORY SUB-FLOOR PAN BETWEEN BS 1016 AND BS 1031, LBL 2 AND LBL 17, WL 208. MAINTENANCE REMOVED CORRODED LT AFT LAVATORY SUB-FLOOR WEB AND STRAP; FABRIC
- [SDR AWXA200500149](https://openairdocs.org/sdr/AWXA200500149.md): Sill · corroded · Dec 24, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHEC, EXFOLIATION CORROSION FOUND ON R-1 DOOR SILL INNER CHORD (CREASE BEAM) AT RBL 58, BETWEEN BS 298 AND 360, WL 208 AND WL 209. MAINTENANCE REMOVED DAMAGED INNER CHORD AT RBL 58, FROM BS 298 TO 360, WL 208 TO WL 209; FABRIC
- [SDR AWXA200500137](https://openairdocs.org/sdr/AWXA200500137.md): Web · corroded · Dec 24, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, GALVANIC CORROSION WAS FOUND IN 3 PLACES ON INBOARD SIDE OF WEB BETWEEN BS 847 AND BS 867, RBL 17.50. MAINTENANCE REMOVED CORRODED SECTION OF WEB FROM BS 847 TO BS 867, RBL 17.50; FABRICATED A NEW REPLACEMENT SECTION OF
- [SDR AWXA200500125](https://openairdocs.org/sdr/AWXA200500125.md): Panel · chafed · Dec 24, 2004 · N327AW · Boeing 7373Q8 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND THE DORSAL FIN DOUBLER ON TOP OF FUSELAGE CHAFED IN 2 PLACES BETWEEN BS 857 AND BS 907, STR 2 LT AND STR 2 RT. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN ON TOP OF FUSELAGE FROM BS 857 TO BS 907, STR 2 LT TO STR 2 RT;
- [SDR AWXA200500124](https://openairdocs.org/sdr/AWXA200500124.md): Pan · corroded · Dec 24, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT LAVATORY SUB-FLOOR PAN BETWEEN BS 1017 AND BS 1025, RBL 1 AND RBL 35, WL 208. MAINTENANCE REMOVED CORRODED RT AFT LAVATORY SUB-FLOOR WEB AND STRAP; FABRI
- [SDR AWXA200500120](https://openairdocs.org/sdr/AWXA200500120.md): Strap · corroded · Dec 24, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CENTER FLOOR STRAP BETWEEN BS 1012 AND BS 1027, LBL 6 AND RBL 6. MAINTENANCE REMOVED CORRODED AFT CENTER FLOOR STRAP FROM BS 1012 TO BS 1027, LBL 6 TO RBL 6; FABRICATED A NEW REPLACE
- [SDR AWXA200500114](https://openairdocs.org/sdr/AWXA200500114.md): Floorbeam · corroded · Dec 24, 2004 · N327AW · Boeing 7373Q8 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 1016, BETWEEN RBL 4 AND RBL 34, WL 208. MAINTENANCE CUTOUT DAMAGE IN FLOORBEAM UPPER CHORD AT BS 1016, FROM RBL 4 TO RBL 34; FABRICATED A NEW
- [SDR AWXA200500110](https://openairdocs.org/sdr/AWXA200500110.md): Web · corroded · Dec 24, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT OUTBOARD WEB, BETWEEN BS 995 AND BS 1012, RBL 39 AND RBL 44, WL 208. MAINTENANCE REMOVED CORRODED RT AFT OUTBOARD WEB, FROM BS 995 TO BS 1012, RBL 39 T
- [SDR AWXA200500108](https://openairdocs.org/sdr/AWXA200500108.md): Floor Support · corroded · Dec 24, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT AT RBL 38, BETWEEN BS 997 AND BS 1004, WL 208. MAINTENANCE CUTOUT DAMAGE ON FLOOR SUPPORT AT RBL 38, FROM BS 997 TO BS 1004; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED R
- [SDR AWXA200500106](https://openairdocs.org/sdr/AWXA200500106.md): Floor Support · corroded · Dec 24, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT LBL 38, BETWEEN BS 1007 AND BS 1014, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT LBL 38, FROM BS 1007 TO BS 1014; FABRICATED A NEW REP
- [SDR AWXA200500103](https://openairdocs.org/sdr/AWXA200500103.md): Floorbeam · corroded · Dec 24, 2004 · N327AW · Boeing 7373Q8 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 1016, BETWEEN LBL 4 AND LBL 34, WL 208. MAINTENANCE CUTOUT DAMAGE IN FLOORBEAM UPPER CHORD AT BS 1016, FROM LBL 4 TO LBL 34; FABRICATED A NEW
- [SDR AWXA200500059](https://openairdocs.org/sdr/AWXA200500059.md): Web · corroded · Dec 24, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF LT AFT OUTBOARD SHEAR WEB BETWEEN BS 996 AND BS 1005, LBL 39 TO LBL 42, WL 208. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 996 TO BS 1005, LBL 39 TO LBL 42; FABRICA
- [SDR AWXA200500030](https://openairdocs.org/sdr/AWXA200500030.md): Sill · corroded · Dec 24, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON L-1 DOOR SILL INNER CHORD (CREASE BEAM) BETWEEN BS 300 AND BS 349, LBL 60, WL 208. MAINTENANCE REMOVED CORRODED L-1 DOOR SILL CREASE BEAM FROM BS 300 TO BS 349, LBL 60; FABRICATED A NEW REPLACEMENT
- [SDR AWXA200500148](https://openairdocs.org/sdr/AWXA200500148.md): Structure · corroded · Dec 23, 2004 · N327AW · Boeing 7373Q8 · Service Doors
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION FOUND ON L-2 DOOR INNER CHORD (CREASE BEAM) AT LBL 48, BETWEEN BS 940 AND 996, WL 208 AND WL 209. MAINTENANCE REMOVED DAMAGED INNER CHORD AT LBL 48, FROM BS 940 TO 996, WL 208 TO WL 209; FABRICATED
- [SDR AWXA200500112](https://openairdocs.org/sdr/AWXA200500112.md): Floor Support · corroded · Dec 23, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT RBL 18, BETWEEN BS 969 AND BS 984, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT RBL 18, FROM BS 969 TO BS 984; FABRICATED A NEW REPLACE
- [SDR AWXA200500111](https://openairdocs.org/sdr/AWXA200500111.md): Floor Support · corroded · Dec 23, 2004 · N327AW · Boeing 7373Q8 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT LBL 18, BETWEEN BS 979 AND BS 983, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT LBL 18, FROM BS 979 TO BS 983; FABRICATED A NEW REPLA
- [SDR AWXA200500109](https://openairdocs.org/sdr/AWXA200500109.md): Floorbeam · corroded · Dec 23, 2004 · N327AW · Boeing 7373Q8 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 986, BETWEEN LBL 45 AND RBL 45, WL 208. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM UPPER CHORD AT BS 986, FROM LBL 45 TO RBL 45; FABRICAT
- [SDR AWXA200500107](https://openairdocs.org/sdr/AWXA200500107.md): Floorbeam · corroded · Dec 23, 2004 · N327AW · Boeing 7373Q8 · Fuselage Main, Floor Beam
  > DURING C-17 CHECK, CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 967, BETWEEN LBL 50 AND RBL 38, WL 208. MAINTENANCE CUTOUT DAMAGE IN FLOORBEAM UPPER CHORD AT BS 967, FROM LBL 50 TO RBL 38; FABRICATED A NEW REPLACEMENT SECTION
- [SDR AWXA200500104](https://openairdocs.org/sdr/AWXA200500104.md): Floorbeam · corroded · Dec 23, 2004 · N327AW · Boeing 7373Q8 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT BS 956, BETWEEN RBL 26 AND RBL 40, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 956, FROM RBL 26 TO RBL 40; FABRICATED A NEW REP
- [SDR AWXA200500031](https://openairdocs.org/sdr/AWXA200500031.md): Bolt · corroded · Dec 23, 2004 · N327AW · Boeing 7373Q8 · Horizontal Stabilizer, Attach Fittings
  > MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON LT HORIZONTAL STABILIZER LOWER FORWARD ATTACH BOLT BS 1096.428, LBL 35.50. MAINTENANCE REMOVED AND REPLACED CORRODED LT HORIZONTAL STABILIZER LOWER FORWARD ATTACH BOLT IAW BMM 27-41-11.
- [SDR AWXA200500131](https://openairdocs.org/sdr/AWXA200500131.md): Skin · corroded · Dec 22, 2004 · N327AW · Boeing 7373Q8 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-17 CHECK, 2 EACH CRACKS WERE FOUND IN FUSELAGE SKIN AT L-1 DOOR LOWER AFT CORNER CUTOUT BS 339, STR 17 LT. MAINTENANCE CUTOUT DAMAGE IN OUTER FUSELAGE SKIN AND BEAR STRAP AT L-1 DOOR LOWER AFT CORNER CUTOUT BS 339, STR 17 LT; PER

Next page: https://openairdocs.org/deregistered/N327AW-2007-07-31/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 = 'N327AW' AND deregistration_id = 'N327AW-2007-07-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N327AW-2007-07-31/reports

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