# Service difficulty reports: N326AW, cancelled May 29, 2007

A list on [N326AW, cancelled May 29, 2007](https://openairdocs.org/deregistered/N326AW-2007-05-29.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 · 168 reports

- [SDR AWXA200601127](https://openairdocs.org/sdr/AWXA200601127.md): Battery Pack · inoperative · Jul 5, 2006 · N326AW · Boeing 737301 · Emergency Lighting
  > PHX - EEL - FLT 33 - LG 4104284 - LEFT EMERGENCY OVERWING EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-51-2. OPERATIONAL CHECKS GOOD.
- [SDR AWXA200600855](https://openairdocs.org/sdr/AWXA200600855.md): Coalescer Bag · odor · May 24, 2006 · N326AW · Boeing 737301 · Humidity Control System
  > LAS - BURNING SMELL - F/A`S REPORTED A BURNING SMELL OF RUBBER COMING FROM THE AFT GALLEY AREA AT CRUISE ABOUT 25 MINS PRIOR TO LANDING IN LAS WITH NO IND OF SMOKE. ODOR WENT AWAY BUT THEN RETURNED DURING DESCENT AND THEN WENT AWAY AGAIN LATER IN DESCENT. MX
- [SDR AWXA200600767](https://openairdocs.org/sdr/AWXA200600767.md): Unknown · low pressure · May 2, 2006 · N326AW · Boeing 737301 · Cabin Pressure Control System
  > EN ROUTE, CREW REPORTED THAT AT FL 340 AUTO STANDBY DID NOT HOLD ALTITUDE. CREW DESCENDED TO FL 100. MASKS DID NOT DEPLOY DUE TO GRADUAL LOSS OF PRESSURIZATION. CREW DIVERTED TO ICT AND LANDED WITHOUT FURTHER EVENT. MAINT PERFORMED LINE MAINT PRESSURIZATIO
- [SDR AWXA200501105](https://openairdocs.org/sdr/AWXA200501105.md): Circuit Breaker · damaged · Sep 25, 2005 · N326AW · Boeing 737301 · AC Power Distribution System
  > CREW REPORTED "ON CLIMB OUT LEFT GENERATOR CAME OFF LINE FOLLOWED BY RIGHT GENERATOR. AC POWER LOST MOMENTARY. CYCLED BOTH GENERATORS. BOTH CAME BACK ON." CREW ELECTED TO RETURN TO PHX. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT DUPLICATE DIS
- [SDR AWXA200500900](https://openairdocs.org/sdr/AWXA200500900.md): Warning System · false activation · Jul 29, 2005 · N326AW · Boeing 737301 · Central Warning
  > SJC - ABORTED TAKEOFF - FLT 165 - ABORTED TAKEOFF FOR UNSPECIFIED WARNING. CLEARED RUNWAY THEN RE-ATTEMPTED T/O. TAKEOFF WAS UNEVENTFUL.
- [SDR AWXA200500831](https://openairdocs.org/sdr/AWXA200500831.md): Light · inoperative · Jul 19, 2005 · N326AW · Boeing 737301 · Emergency Lighting
  > DEN - EEL - DURING 4 DAY CHECK DISCOVERED THE EMERGENCY EXIT LIGHT AT ROW 19C IS INOPERATIVE. MAINTENANCE PLACED ON MEL. REQUIRES NEW LIGHT ASSEMBLY.
- [SDR AWXA200500614](https://openairdocs.org/sdr/AWXA200500614.md): Altimeter · faulty · May 26, 2005 · N326AW · Boeing 737301 · Altimeter, Barometric/Encoder
  > AT CRUSE ALTITUDE OF 360FL CABIN ALTITUDE HORN CAME ON & CABIN PRESSURE UNCONTROLLABLE. A BLEED TRIP OCCURRED ON NR 1 PACK ALONG WITH 2 DUCT OVERHEATS IN 3 MIN ACFT DESCENDED TO 11,000 FT IN STANBY MODE & CABIN PRESSURE RETURNED 10 MIN LATER. DIVERTED TO ELP
- [SDR AWXA200500297](https://openairdocs.org/sdr/AWXA200500297.md): Channel · corroded · Feb 19, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND AFT CARGO DOOR SILL LOWER CHANNEL AT BS 837, STR 25 RT. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL LOWER CHANNEL AT BS 837, STR 25 RT; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 65-47957; INST
- [SDR AWXA200500307](https://openairdocs.org/sdr/AWXA200500307.md): Frame · corroded · Feb 17, 2005 · N326AW · Boeing 737301 · Fuselage Main, Frame
  > MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON FRAME AT FORWARD SIDE OF BS 847 JUST INBOARD OF STR 25 RT. MAINTENANCE REMOVED DAMAGED SECTION OF FRAME AT BS 847 FROM STR 25 RT TO STR 26 RT; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR
- [SDR AWXA200500298](https://openairdocs.org/sdr/AWXA200500298.md): Clip · cracked · Feb 15, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.25 INCH CRACK WAS FOUND IN AFT CARGO COMPARTMENT FRAME ATTACH CLIP AT BS 807, STR 25 RT. MAINTENANCE REMOVED CRACKED AFT CARGO COMPARTMENT FRAME ATTACH CLIP AT BS 807, STR 25 RT; FABRICATED A NEW REPLACEMENT CLIP PER
- [SDR AWXA200500309](https://openairdocs.org/sdr/AWXA200500309.md): Bear Strap · corroded · Feb 13, 2005 · N326AW · Boeing 737301 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND INTERNAL SURFACE OF AFT CARGO DOOR CUTOUT LOWER FORWARD BEAR STRAP BS 807, STR 25 RT. MAINTENANCE CUT OUT DAMAGE IN AFT CARGO DOOR CUTOUT LOWER FORWARD BEAR STRAP AT BS 807, STR 25 RT; FABRICATED 2 EA
- [SDR AWXA200500334](https://openairdocs.org/sdr/AWXA200500334.md): Web · corroded · Feb 12, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR SILL WEB BETWEEN BS 794 AND BS 799, AT STR 25 RT. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL WEB AT STR 25 RT, FROM BS 794 TO BS 799; FABRICATED A NEW REPLACEMENT WEB PER DWG 6
- [SDR AWXA200500332](https://openairdocs.org/sdr/AWXA200500332.md): Angle · corroded · Feb 12, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR SILL ATTACH ANGLE AT BS 847, BETWEEN STR 24 RT AND STR 25 RT. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL ATTACH ANGLE AT BS 847, FROM STR 24 RT TO STR 25 RT; FABRICATED A NEW R
- [SDR AWXA200500315](https://openairdocs.org/sdr/AWXA200500315.md): Frame · corroded · Feb 12, 2005 · N326AW · Boeing 737301 · Fuselage Main, Frame
  > MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR FORWARD TORQUE BOX FRAME AT BS 794.3, STR 25 RT. MAINTENANCE REMOVED CORRODED SECTION AFT CARGO DOOR FORWARD TORQUE BOX FRAME AT BS 794.3, STR 25 RT; FABRICATED A NEW REPLACEMENT SEC
- [SDR AWXA200500314](https://openairdocs.org/sdr/AWXA200500314.md): Strap · corroded · Feb 12, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL UPPER STRAP BETWEEN BS 794 AND BS 847 AT STR 25 RT. MAINTENANCE REMOVED CORRODED SECTION AFT CARGO DOOR SILL UPPER STRAP FROM BS 794 TO BS 847 AT STR 25 RT; FABRICAT
- [SDR AWXA200500303](https://openairdocs.org/sdr/AWXA200500303.md): Frame · cracked · Feb 10, 2005 · N326AW · Boeing 737301 · Fuselage Main, Frame
  > MCN - MAJOR REPAIR - DURING C-18 CHECK 3 EACH.25 INCH CRACKS WERE FOUND IN FUSELAGE FRAME AT BS 663.75, BETWEEN STR 2 RT & STR 3 LT. MAINTENANCE CUT OUT CRACKS IN FRAME AT BS 663.75, BETWEEN STR 2 RT & STR 3 LT; FABRICATED FILLERS AND A REPAIR ANGLE; INSTALL
- [SDR AWXA200500293](https://openairdocs.org/sdr/AWXA200500293.md): Frame · cracked · Feb 10, 2005 · N326AW · Boeing 737301 · Fuselage Main, Frame
  > MCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH.1875 INCH CRACKS WERE FOUND IN R-2 DOOR LOWER FORWARD FRAME SECTION BS 957, STR 16 RT. MAINTENANCE CUT OUT DAMAGE IN R-2 DOOR LOWER FORWARD FRAME SECTION; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PA
- [SDR AWXA200500235](https://openairdocs.org/sdr/AWXA200500235.md): Floorbeam · corroded · Feb 8, 2005 · N326AW · Boeing 737301 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM STIFFENER ANGLE ON AFT SIDE FLOORBEAM AT BS 328, BETWEEN RBL 43 AND RBL 60. MAINTENANCE REMOVED CORRODED FLOORBEAM STIFFENER ANGLE AT BS 328, FROM RBL 43 TO RBL 60; FABRICATE
- [SDR AWXA200500310](https://openairdocs.org/sdr/AWXA200500310.md): Reveal · cracked · Feb 7, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND IN R-2 DOOR LOWER FORWARD REVEAL AT 957, STR 17 RT. MAINTENANCE REMOVED AND REPLACED R-2 DOOR LOWER FORWARD REVEAL IAW B737-300 SRM 51-40-02.
- [SDR AWXA200500232](https://openairdocs.org/sdr/AWXA200500232.md): Crease Beam · cracked · Feb 7, 2005 · N326AW · Boeing 737301 · Fuselage Main, Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.75 INCH CRACK WAS FOUND IN WEB UNDER CREASE BEAM INNER CHORD AT BS 986.5, LBL 43. MAINTENANCE REMOVED DAMAGED WEB FROM BS 986.5 TO BS 1016, LBL 37 TO LBL 45; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-46812; INSTALLE
- [SDR AWXA200500292](https://openairdocs.org/sdr/AWXA200500292.md): Skin · worn · Feb 3, 2005 · N326AW · Boeing 737301 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-18 CHECK FOUND FUSELAGE SKIN WORN IN SEVERAL AREAS AT LT AND RT DORSAL FIN SEALS BETWEEN BS 860 AND BS 907.5. MAINTENANCE CUT OUT DAMAGE IN FUSELAGE SKIN AT LT AND RT DORSAL FIN SEALS FROM BS 860 TO BS 907.5; PERFORMED HFEC INSPE
- [SDR AWXA200500326](https://openairdocs.org/sdr/AWXA200500326.md): Support · corroded · Jan 31, 2005 · N326AW · Boeing 737301 · Trailing Edge Flaps
  > MCN - FLIGHT CONTROL - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBAL OUTER SUPPORT WBL 185.0. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP OUTBOARD GIMBAL OUTER SUPPORT IAW T/C I3R57057.
- [SDR AWXA200500325](https://openairdocs.org/sdr/AWXA200500325.md): Gimbal Joint · corroded · Jan 31, 2005 · N326AW · Boeing 737301 · Trailing Edge Flaps
  > MCN - FLIGHT CONTROL - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBAL INDEX PLATE WBL 185.0. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP OUTBOARD GIMBAL ASSEMBLY IAW T/C I3R57057.
- [SDR AWXA200500324](https://openairdocs.org/sdr/AWXA200500324.md): Support · corroded · Jan 31, 2005 · N326AW · Boeing 737301 · Trailing Edge Flaps
  > MCN - FLIGHT CONTROL - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT WBL 71.24. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT IAW BOEING SOPM 20-50-01.
- [SDR AWXA200500226](https://openairdocs.org/sdr/AWXA200500226.md): Skin · delaminated · Jan 31, 2005 · N326AW · Boeing 737301 · Leading Edge Devices
  > MCN - MAJOR REPAIR - DURING C-18 CHECK THE UPPER SURFACE SKIN OF THE NR 2 SLAT WAS FOUND DELAMINATED AT THE OUTBOARD END, SLAT STA 251. MAINTENANCE CUT OUT DAMAGED AREA OF UPPER NR 2 SLAT SKIN FROM SS 249.77 TO SS 254.27; FABRICATED A CORE FILLER AND EXTERNAL
- [SDR AWXA200500191](https://openairdocs.org/sdr/AWXA200500191.md): Gimbal Joint · corroded · Jan 31, 2005 · N326AW · Boeing 737301 · Trailing Edge Flaps
  > MCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MIDFLAP OUTBOARD GIMBAL INDEX PLATE AT WBL 184. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTBOARD GIMBAL ASSEMBLY IAW SOPM 20-50-01.
- [SDR AWXA200500190](https://openairdocs.org/sdr/AWXA200500190.md): Gimbal Joint · corroded · Jan 31, 2005 · N326AW · Boeing 737301 · Trailing Edge Flaps
  > MCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MIDFLAP OUTBOARD GIMBAL OUTER SUPPORT AT WBL 184. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTBOARD GIMBAL OUTER SUPPORT IAW SOPM 20-50-01.
- [SDR AWXA200500329](https://openairdocs.org/sdr/AWXA200500329.md): Skin · cracked · Jan 28, 2005 · N326AW · Boeing 737301 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.25 INCH CRACK WAS FOUND IN FUSELAGE SKIN EMANATING FROM FASTENER HOLE AT FORWARD LOWER CUTOUT OF R-2 DOOR BS 947. MAINTENANCE CUT OUT CRACK IN FUSELAGE SKIN AT FORWARD LOWER CUTOUT OF R-2 DOOR BS 947; FABRICATED 2 EAC
- [SDR AWXA200500296](https://openairdocs.org/sdr/AWXA200500296.md): Strap · cracked · Jan 28, 2005 · N326AW · Boeing 737301 · Fuselage Main, Frame
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.3125 INCH CRACK WAS FOUND IN LOWER FORWARD INBOARD EDGE OF FRAME STRAP AT BS 349, STR 16 LT. MAINTENANCE REMOVED DAMAGED FRAME STRAP AT BS 349, STR 16 LT; INSTALLED A NEW REPLACEMENT FRAME STRAP IAW ER 03-5300-05053-S
- [SDR AWXA200500248](https://openairdocs.org/sdr/AWXA200500248.md): Skin · cracked · Jan 28, 2005 · N326AW · Boeing 737301 · Passenger/Crew Doors
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.375 INCH CRACK WAS FOUND IN L-1 DOOR EXTERNAL SKIN AT LOWER HINGE CUTOUT BS 317, STR 14 LT. MAINTENANCE CUT OUT CRACK IN L-1 DOOR EXTERNAL SKIN AT LOWER HINGE CUTOUT BS 317, STR 14 LT; FABRICATED REPAIR DOUBLER; INSTA
- [SDR AWXA200500294](https://openairdocs.org/sdr/AWXA200500294.md): Intercostal · cracked · Jan 27, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH.0625 INCH CRACKS WERE FOUND IN L-1 DOOR FORWARD FRAME INTERCOSTAL WEB BS 294.5, STR 7 LT. MAINTENANCE REMOVED DAMAGED L-1 DOOR FORWARD FRAME INTERCOSTAL WEB FROM BS 294.5 TO BS 303.9; FABRICATED A NEW REPLACEMENT
- [SDR AWXA200500287](https://openairdocs.org/sdr/AWXA200500287.md): Clip · cracked · Jan 27, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.0265 INCH CRACK WAS FOUND IN RADIUS OF ANGLE CLIP AT AFT SIDE OF STRINGER SPLICE CHANNEL BS 348.2, STR 16 LT. MAINTENANCE REMOVED CRACKED ANGLE CLIP FROM BS 348.2 TO BS 351.2, STR 16 LT; FABRICATED NEW REPLACEMENT CLI
- [SDR AWXA200500286](https://openairdocs.org/sdr/AWXA200500286.md): Stringer Clip · cracked · Jan 27, 2005 · N326AW · Boeing 737301 · Fuselage Main, Attach Fittings
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.3125 INCH CRACK WAS FOUND IN INBOARD FORWARD LOWER EDGE OF STRINGER SPLICE CHANNEL CLIP & FRAME STRAP AT BS 349, STR 16 LT. MAINTENANCE REMOVED CRACKED STRINGER SPLICE CHANNEL CLIP & FRAME STRAP AT BS 349, STR 16 LT;
- [SDR AWXA200500282](https://openairdocs.org/sdr/AWXA200500282.md): Web · chafed · Jan 27, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK FOUND L-1 DOOR UPPER HINGE CUTOUT UPPER WEB CHAFED ON LOWER SIDE BETWEEN BS 294.5 AND BS 303.9, STR 13 LT. MAINTENANCE REMOVED CHAFED WEB AT L-1 DOOR UPPER HINGE CUTOUT FROM BS 294.5 TO BS 303.9, STR 13 LT; FABRICATED A N
- [SDR AWXA200500261](https://openairdocs.org/sdr/AWXA200500261.md): Clip · cracked · Jan 27, 2005 · N326AW · Boeing 737301 · Fuselage Main, Attach Fittings
  > MCN - MAJOR REPAIR - DURING C-18 CHECK, A 3" CRACK WAS FOUND IN AFT SIDE L-1 DOOR FRAME INTERCOSTAL ATTACH CLIP AT BS 348.2, STR 17 LT. MAINTENANCE REMOVED CRACKED L-1 DOOR FRAME INTERCOSTAL ATTACH CLIP AT BS 348.2, STR 17 LT; FABRICATED A NEW REPLACEMENT ATT
- [SDR AWXA200500302](https://openairdocs.org/sdr/AWXA200500302.md): Light · inoperative · Jan 26, 2005 · N326AW · Boeing 737301 · Emergency Lighting
  > MCN - EEL - DURING C-18 CHECK FOUND THE L-2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED L-2 DOOR EMERGENCY EXIT SIGN, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200500328](https://openairdocs.org/sdr/AWXA200500328.md): Plate · cracked · Jan 25, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 1.25 INCH CRACK WAS FOUND IN CLOSE PANEL BETWEEN FORWARD END OF R-2 DOOR CUTOUT AND BS 947. MAINTENANCE REMOVED CRACKED CLOSE PANEL FROM BS 947 TO BS 957, STR 14 RT TO STR 16 RT; FABRICATED A NEW REPLACEMENT CLOSE PANE
- [SDR AWXA200500327](https://openairdocs.org/sdr/AWXA200500327.md): Reveal · cracked · Jan 25, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND IN R-1 DOOR UPPER AFT REVEAL. MAINTENANCE REMOVED CRACKED R-1 DOOR UPPER AFT REVEAL FROM BS 320 TO BS 328 AT STR 10 RT; FABRICATED A NEW REPLACEMENT REVEAL PER DWG 65-53594; INSTALLED REPAIR PART
- [SDR AWXA200500301](https://openairdocs.org/sdr/AWXA200500301.md): Skin · cracked · Jan 25, 2005 · N326AW · Boeing 737301 · Passenger/Crew Doors
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.3125 INCH CRACK WAS FOUND IN R-1 DOOR EXTERNAL SKIN EMANATING FASTENER HOLE AT LOWER HINGE CUTOUT BS 328, STR 15-16 RT. MAINTENANCE REMOVED EXISTING DOUBLER AND CUT OUT CRACK IN R-1 DOOR EXTERNAL SKIN; FABRICATED A FI
- [SDR AWXA200500300](https://openairdocs.org/sdr/AWXA200500300.md): Flashlight · inoperative · Jan 25, 2005 · N326AW · Boeing 737301 · Emergency Equipment
  > MCN - EMERGENCY EQUIPMENT - DURING C-18 CHECK FOUND THE LT AFT LAVATORY WALL EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT AFT LAVATORY WALL EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200500299](https://openairdocs.org/sdr/AWXA200500299.md): Flashlight · inoperative · Jan 25, 2005 · N326AW · Boeing 737301 · Emergency Equipment
  > MCN - EMERGENCY EQUIPMENT - DURING C-18 CHECK FOUND THE LT FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA200500285](https://openairdocs.org/sdr/AWXA200500285.md): Skin · cracked · Jan 25, 2005 · N326AW · Boeing 737301 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.375 INCH CRACK WAS FOUND IN FUSELAGE SKIN EMANATING FROM FASTENER HOLE AT FORWARD UPPER CORNER CUTOUT OF R-1 DOOR. MAINTENANCE TRIMMED OUT CRACK IN FUSELAGE SKIN FORWARD UPPER CORNER CUTOUT OF R-1 DOOR; FABRICATED FIL
- [SDR AWXA200500331](https://openairdocs.org/sdr/AWXA200500331.md): Floorbeam · corroded · Jan 24, 2005 · N326AW · Boeing 737301 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON FLOORBEAM T-CAP AT BS 986, LBL 44, WL 208. MAINTENANCE CUT OUT DAMAGE IN FLOORBEAM T-CAP AT BS 986, FROM BL 0 TO LBL 50; FABRICATED A NEW REPLACEMENT SECTION OF T-CAP, AND 2 EACH SUPPORT ANGLES & S
- [SDR AWXA200500290](https://openairdocs.org/sdr/AWXA200500290.md): Sill · corroded · Jan 24, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON L-2 DOOR SILL INNER CHORD BETWEEN BS 950 AND BS 994, LBL 50. MAINTENANCE REMOVED CORRODED L-2 DOOR SILL INNER CHORD FROM BS 917 TO BS 1016, LBL 50; FABRICATED A NEW REPLACEMENT INNER CHORD PER DWG
- [SDR AWXA200500262](https://openairdocs.org/sdr/AWXA200500262.md): Intercostal · cracked · Jan 24, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK, A 0.8125 INCH CRACK WAS FOUND IN UPPER AFT CORNER OF INTERCOSTAL AT BS 293, LBL 33, WL 208. MAINTENANCE CUTOUT DAMAGE IN INTERCOSTAL AT BS 293, LBL 33; FABRICATED A REPAIR ANGLE AND SHIM; INSTALLED REPAIR PARTS IAW B737
- [SDR AWXA200500249](https://openairdocs.org/sdr/AWXA200500249.md): Intercostal · cracked · Jan 24, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.1875 INCH CRACK WAS FOUND IN UPPER RADIUS OF INTERCOSTAL AT BS 306, LBL 27. MAINTENANCE CUT OUT DAMAGE IN UPPER RADIUS OF INTERCOSTAL AT BS 306, LBL 27; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW
- [SDR AWXA200500333](https://openairdocs.org/sdr/AWXA200500333.md): Floorbeam · corroded · Jan 23, 2005 · N326AW · Boeing 737301 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON FLOORBEAM T-CAP AT BS 1016, RBL 5, WL 208. MAINTENANCE CUT OUT DAMAGE IN FLOORBEAM T-CAP AT BS 1016, RBL 5; FABRICATED A 3 EACH REPAIR PLATES AND A FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 5
- [SDR AWXA200500295](https://openairdocs.org/sdr/AWXA200500295.md): Floorbeam · corroded · Jan 23, 2005 · N326AW · Boeing 737301 · Fuselage Main, Floor Beam
  > MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND LOWER SURFACE OF TRANVERSE FLOORBEAM T-CAP AT BS 986, BETWEEN RBL 40 AND RBL 44, WL 208. MAINTENANCE REMOVED CORRODED FLOORBEAM T-CAP AT BS 986 FROM RBL 0 TO RBL 50; FABRICATED A NEW REPLACEMENT SECTI
- [SDR AWXA200500229](https://openairdocs.org/sdr/AWXA200500229.md): Skin · cracked · Jan 23, 2005 · N326AW · Boeing 737301 · Fuselage Main, Plate/Skin
  > MCN - MAJOR REPAIR - DURING C-18 CHECK A.1875 INCH CRACK WAS FOUND IN FUSELAGE SKIN EMANATING FROM FASTENER HOLE AT BS 445, BL 0. MAINTENANCE REMOVED EXISTING REPAIR DOUBLER AND CUT OUT DAMAGED AREA OF SKIN AT BS 445, BL 0; PERFORMED A HFEC INSPECTION OF CUT
- [SDR AWXA200500185](https://openairdocs.org/sdr/AWXA200500185.md): Web · corroded · Jan 23, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous Structure
  > MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF SHEAR WEB BETWEEN BS 1009 AND BS 1015, LBL 41 AND LBL 45, WL 207.5. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 1009 TO BS 1015, LBL 41 TO LBL 45; FABRICATED A NEW R

Next page: https://openairdocs.org/deregistered/N326AW-2007-05-29/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 = 'N326AW' AND deregistration_id = 'N326AW-2007-05-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N326AW-2007-05-29/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.