# Service difficulty reports: N326UA, cancelled Oct 1, 2012

A list on [N326UA, cancelled Oct 1, 2012](https://openairdocs.org/deregistered/N326UA-2012-10-01.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR 2008UALA05719](https://openairdocs.org/sdr/2008UALA05719.md): Connector · underserviced · Sep 13, 2008 · N326UA · Boeing 737322 · Communications System Wiring
  > F/O SIDE OXYGEN MASK COMM CONNECTOR DISCONNECTED. REPAIRED O2 BOX CONNECTOR.
- [SDR 2008UALA04357](https://openairdocs.org/sdr/2008UALA04357.md): Light · inoperative · Aug 20, 2008 · N326UA · Boeing 737322 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT AFT OF DOOR 1L IS INOP. *S/D* REPLACED LIGHT ASSEMBLY. OP CHECKS GOOD.
- [SDR 2008UALA03925](https://openairdocs.org/sdr/2008UALA03925.md): Light · inoperative · Jul 19, 2008 · N326UA · Boeing 737322 · Emergency Lighting
  > AFT SECTION OF EEL STRIP LIGHTING INOP. REPLACED AFT EEL STRIP CABLE. OPS CKS GOOD.
- [SDR 2008UALA00511](https://openairdocs.org/sdr/2008UALA00511.md): Light · inoperative · Jan 29, 2008 · N326UA · Boeing 737322 · Emergency Lighting
  > EMERGENCY EXIT FLOOR LIGHTS INOPERATIVE PAST ROW 15. REPLACED POWER SUPPLY, BATTERY AND LIGHT STRIP.
- [SDR 2008UALA00102](https://openairdocs.org/sdr/2008UALA00102.md): Light · inoperative · Jan 6, 2008 · N326UA · Boeing 737322 · Emergency Lighting
  > EEL FLOOR LIGHTS FROM ROW 15 TO REAR OF PLANE IS INOP. REPLACED POWER STRIP.
- [SDR 2007UALA05254](https://openairdocs.org/sdr/2007UALA05254.md): Feeder Cable · inoperative · Dec 24, 2007 · N326UA · Boeing 737322 · Light System Wiring
  > EEL LIGHTS INOP AFT OF ROW 15. CLEANED AND REPLACED CABLE. RELAMPED
- [SDR 2007UALA03623](https://openairdocs.org/sdr/2007UALA03623.md): Skin · cracked · Sep 7, 2007 · N326UA · Boeing 737322 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN CRACKED AT AFT END OF AVIONIC EXHAUST OUTLET. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED LARGE EXTERNAL SKIN DOUBLER AROUND E&E EXHAUST OUTLET & PREVENTIVE MODIFICATION DOUBLERS TO AFT RADIO ALTIMETER CUTOUTS.
- [SDR 2007UALA03622](https://openairdocs.org/sdr/2007UALA03622.md): Stringer Clip · cracked · Sep 7, 2007 · N326UA · Boeing 737322 · Fuselage Main, Attach Fittings
  > STRINGER CLIP BS 400 STRINGER 27L CRACKED IN CORNER. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW STRINGER CLIP BS 400 STR (HMV)
- [SDR 2007UALA03603](https://openairdocs.org/sdr/2007UALA03603.md): Skin · damaged · Sep 6, 2007 · N326UA · Boeing 737322 · Cargo/Baggage Doors
  > AFT CARGO DOOR OUTER SKIN HAS DEEP CREASES FWD LOWER AREA. DENT IS 6 INCHES LONG AND 6 INCHES WIDE,.125 DEEP. LOCATED 3 INCHES FROM LOWER EDGE AND 5 INCHES AFT OF LEADING EDGE, IT HAS 2 CREASES ABOUT 4 INCHES LONG, 3 INCHES APART.
- [SDR 2007UALA03233](https://openairdocs.org/sdr/2007UALA03233.md): Controller · failed · Aug 19, 2007 · N326UA · Boeing 737322 · Cabin Pressure Controller
  > EN ROUTE AIRCRAFT LOST CABIN PRESSURE. FLIGHT DESCENDED AND MADE NORMAL LANDING. REPLACED CABIN PRESSURE CONTROLLER AND AFT OUTFLOW VALVE. REPLACED UPPER CABIN SAFETY VALVE. FWD CARGO PIT, AFT BULKHEAD BLOWOUT PANEL IS POPPED OUT ALONG THE LOWER EDGE. SECUR
- [SDR 2007UALA02741](https://openairdocs.org/sdr/2007UALA02741.md): Lamp · inoperative · Jul 19, 2007 · N326UA · Boeing 737322 · Emergency Lighting
  > EEL LIGHTS INOP FROM SEAT 15 TO BACK OF CABIN. REPLACED TO FLEXIBLE LAMPS PER MM 33-51-90. TEST OK 33-51-02.
- [SDR 2007UALA02274](https://openairdocs.org/sdr/2007UALA02274.md): Light · inoperative · Jun 27, 2007 · N326UA · Boeing 737322 · Emergency Lighting
  > LEFT SIDE EXTERIOR EMERGENCY OVERWING LIGHT INOP. RELAMPED, TEST NORMAL.
- [SDR 2007UALA01985](https://openairdocs.org/sdr/2007UALA01985.md): Light · inoperative · Jun 12, 2007 · N326UA · Boeing 737322 · Emergency Lighting
  > ALL FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOP AFT OF ROW 15. [06-22-07] LIFTED AND DRIED AREA OF ALL MOISTURE FROM AFT GALLEY. REPLACED AFT GALLEY EEL STRIP AND AFT 15 FEET OF POWER CABLE. CLEANED, DRIED AND REINSTALLED EEL LAMPS TO NEW POWER CABLE.
- [SDR 2007UALA00277](https://openairdocs.org/sdr/2007UALA00277.md): Fuse · blown · Jan 31, 2007 · N326UA · Boeing 737322 · Emergency Lighting
  > LEFT AFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BLOWN FUSE.
- [SDR 2006UALA01708](https://openairdocs.org/sdr/2006UALA01708.md): Smoke · detected · Sep 1, 2006 · N326UA · Boeing 737322 · Air Distribution System
  > SMOKE IN CABIN IN AREA OF AFT GALLEY OVERHEAD. SMELL WAS ACTUALLY REPORTED TO BE "LIKE COFFEE" AND NOT SMOKE. COULD NOT DUPLICATE ODOR.
- [SDR 2006UALA00451](https://openairdocs.org/sdr/2006UALA00451.md): Skin · dented · Mar 9, 2006 · N326UA · Boeing 737322 · Horizontal Stabilizer, Plate/Skin
  > LH HORIZONTAL STAB UPPER SKIN DENTED 6 FEET FROM INBD. NEW REPAIR SKIN SPLICED IN PER AAR EA 1060102.
- [SDR 2006UALA00447](https://openairdocs.org/sdr/2006UALA00447.md): Floorbeam · cracked · Mar 9, 2006 · N326UA · Boeing 737322 · Fuselage Main, Floor Beam
  > CABIN LONGITUDINAL FLOOR SUPPORT AT LBL45.5 WAS FOUND CRACKED AT THE OUTBOARD FLANGE FASTENER HOLE OF THE UPPER CHORD WHERE THE ASSY IS ATTACHED TO THE BS 727B FLOORBEAM. REMOVED DAMAGED AREA. ACP NDT FOR CRACKS. FABRICATED & INSTALLED TWO STRAPS, FILLER & S
- [SDR 2006UALA00446](https://openairdocs.org/sdr/2006UALA00446.md): Stringer · cracked · Mar 8, 2006 · N326UA · Boeing 737322 · Fuselage Main, Longeron/Stringer
  > CABIN BS 296 S10L IS CRACKED AT UPPER FLANGE. REMOVED DAMAGE, MANUFACTURED AND INSTALLED STRINGER REPAIR, STRINGER CLIP AND INTERCOSTAL.
- [SDR 2006UALA00432](https://openairdocs.org/sdr/2006UALA00432.md): Bushing · migrated · Mar 8, 2006 · N326UA · Boeing 737322 · Horizontal Stabilizer Structure
  > LT HORIZ STAB FWD SPAR UPPER LUG FWD & AFT BUSHINGS MIGRATED. REMOVED BUSHINGS, FOUIND CORROSION, REMOVED CORROSION, FABRICATED ADN INSTALLED NEW BUSHINGS PER BOEING DRAWINGS 65-72039-29, 30, AND 31. WORK ACCOMPLISHED PER AAR EA I060104 AND SUPPORTED WITH 810
- [SDR 2006UALA00445](https://openairdocs.org/sdr/2006UALA00445.md): Skin · damaged · Mar 8, 2006 · N326UA · Boeing 737322 · Rudder, Plate/Skin
  > RUDDER AT NR 4 HINGE CUTOUT RIGHT UPPER EDGE DAMAGED. DAMAGE TO RUDDER AT NR 4 HINGE CUTOUT WAS REPAIR PER AAR EO I060062.
- [SDR 2006UALA00399](https://openairdocs.org/sdr/2006UALA00399.md): Skin · punctured · Mar 4, 2006 · N326UA · Boeing 737322 · Leading Edge Devices
  > NR 1 KRUGER FLAP DAMAGED, PUNCTURED APPROXIMATELY 1.2 BY 100 PERCENT THRU. PERMANENT REPAIR DOUBLER WAS INSTALLED PER AAR EA I060103 SUPPORTED WITH 8100-9 FORM.
- [SDR 2006UALA00394](https://openairdocs.org/sdr/2006UALA00394.md): Skin · eroded · Mar 4, 2006 · N326UA · Boeing 737322 · Fuselage Main, Plate/Skin
  > AFT UPPER EXTERNAL FUSELAGE BS 860 TO 887 BTWN STR 2L & 2R DORSAL FIN FWD FRG. PHENOLIC WEAR STRIP UNDER BLADE SEAL IS ERRODED TO THE EDGE OF BLADE IN SEVERAL SPOTS, BLADE SEAL SHOULD BE CENTERED ON WEAR STRIP. REMOVED DAMAGE AND INSTALLED A DOUBLER, TRIPLER
- [SDR 2006UALA00382](https://openairdocs.org/sdr/2006UALA00382.md): Stiffener · cracked · Mar 3, 2006 · N326UA · Boeing 737322 · Fuselage Miscellaneous Structure
  > MAIN WHEEL WELL FWD BULKHEAD STIFFENER IS CRACKED WL 170 LBL 6.5. STIFFENER WAS REMOVED AND REPLACED AT MAIN WHEEL WELL STA. 663, LBL 6.15 PER MM57-12-96 PAGE 401 REPAIR 2. PER ADVANCE MM 57-12-96 PAGE 404 ITEM 6. B. CREATED A CF ITEM TO REPLACE BOTH STIFFENER
- [SDR 2006UALA00403](https://openairdocs.org/sdr/2006UALA00403.md): Slide · no test · Mar 3, 2006 · N326UA · Boeing 737322 · Escape Slide
  > DURING DEPLOYMENT OF FWD GALLEY DOOR SLIDE, SLIDE TWISTED AND DEPLOYED VERTICALLY AT DOOR THRESHOLD AREA.
- [SDR 2006UALA00366](https://openairdocs.org/sdr/2006UALA00366.md): Stringer Clip · cracked · Mar 1, 2006 · N326UA · Boeing 737322 · Fuselage Main, Attach Fittings
  > FOUND AFT PIT STA 727A RBL 24" STRINGER CLIP CRACKED AT STR 25R. INSTALLED NEW STRINGER CLIP REF SRM 51-40-02.
- [SDR 2006UALA00364](https://openairdocs.org/sdr/2006UALA00364.md): Frame · dented · Feb 28, 2006 · N326UA · Boeing 737322 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT STA 727B AT S22L FRAME DENTED. REPAIRED FRAME AT STA 727B AT STRINGER 22L WITH REF TO MM CHAPTER 53-11-99. REPLACED STRINGER CLIP ON FRAME 727B AND STRINGER 22L DUE TO REPAIR WITH REF TO SRM 51-40-02.
- [SDR 2006UALA00341](https://openairdocs.org/sdr/2006UALA00341.md): Floorbeam · corroded · Feb 26, 2006 · N326UA · Boeing 737322 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM UPPER FLG IS CORRODED BS 947 LBL 4-20, WL 208. REPAIRED WITH ANGLE (REF MM 53-10-95-801) REPAIR #VII. TREATED, PRIMED AND PAINTED. INSTALLED NESTED ANGLE.
- [SDR 2006UALA00340](https://openairdocs.org/sdr/2006UALA00340.md): Skin · damaged · Feb 26, 2006 · N326UA · Boeing 737322 · Fuselage Main, Plate/Skin
  > LT FUSELAGE SKIN AT 1" FWD OF FRAME STA 727A STR 25L HAS TOOLING DAMAGE. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED REF SRM 53-60-01 REPAIR 31 PG 338. ADD REPAIR DOUBLER AND STRUCTURAL FILLER.
- [SDR 2006UALA00339](https://openairdocs.org/sdr/2006UALA00339.md): Frame · gouged · Feb 26, 2006 · N326UA · Boeing 737322 · Fuselage Main, Frame
  > FOUND FUSELAGE BODY FRAME WEB IS GOUGED NEAR BLEED AIR CUTOUT BS 1040, STR 26L - 27L. CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED REPAIR REF MM 53-11-86. REPAIR SCHEME DOUBLER AND TRIPLER.
- [SDR 2006UALA00357](https://openairdocs.org/sdr/2006UALA00357.md): Wire · exposed · Feb 24, 2006 · N326UA · Boeing 737322 · Fuel System Wiring
  > THE NR 1 AFT FUEL BOOST PUMP WIRING WAS FOUND CHAFED THROUGH PLASTIC SHEATHING AND INTO WIRING INSULATION WITH BARE WIRING EXPOSED IN THREE AREAS DURING INSPECTION MANDATED BY AD99-21-15 ON UAL JIC 2S124. REPLACED WIRE ASSEMBLY AS REQUIRED PER AD 99-21-15. C
- [SDR 2006UALA00335](https://openairdocs.org/sdr/2006UALA00335.md): Stringer Clip · damaged · Feb 24, 2006 · N326UA · Boeing 737322 · Fuselage Main, Attach Fittings
  > AFT CARGO COMPARTMENT STA 767 S23L STRINGER CLIP DAMAGED. REMOVED AND REPLACED STRINGER CLIP REF SRM 51-40-02.
- [SDR 2006UALA00334](https://openairdocs.org/sdr/2006UALA00334.md): Skin · cracked · Feb 24, 2006 · N326UA · Boeing 737322 · Electrical/Electronic Compartment Doors
  > ELECTRONIC ACCESS DOOR AT STA 328 HAS A CRACK ON RT SIDE OF SKIN. REMOVED DAMAGE, INSTALLED DOUBLER REPAIR PER SRM 52-00-01. NO FURTHER SERVICE, OK FOR SERVICE.
- [SDR 2006UALA00299](https://openairdocs.org/sdr/2006UALA00299.md): Door Frame · cracked · Feb 18, 2006 · N326UA · Boeing 737322 · Galley Doors
  > FWD GALLEY DOOR AFT FRAME CRACKED IN 3 PLACES: LWR AFT FRAME AT LOWER O/B STOP FITTING FASTENER HOLE, 3RD AND 4TH STOP FITTING CUTOUTS FROM BOTTOM OF DOOR. REMOVED DAMAGED FRAME, REPLACED WITH NEW FRAME P/N 65-45871Y140 AND 69-69430-6. AAR-IND MECH 10820 AN
- [SDR 2005UALA01232](https://openairdocs.org/sdr/2005UALA01232.md): Relay · failed · Nov 5, 2005 · N326UA · Boeing 737322 · Navigation System
  > BOTH IRS ON DC LIGHTS ILLUM JUST AFTER LIFTOFF. SUA IRS POWER FAULT HAS NOT REOCCURRED.
- [SDR 2002UALA00271](https://openairdocs.org/sdr/2002UALA00271.md): Frame · cracked · Feb 14, 2002 · N326UA · Boeing 737322 · Fuselage Main, Frame
  > OVERWING FRAME AT BODY STATION 616, LBL 65 ATTACH CHORD CRACKED OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED ANGLE REPAIR.
- [SDR 2002UALA00272](https://openairdocs.org/sdr/2002UALA00272.md): Angle · cracked · Feb 13, 2002 · N326UA · Boeing 737322 · Fuselage Miscellaneous Structure
  > FORWARD PIT STATION 495 FLOOR WEB ANGLE HAS CRACK AT S-28R. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW WEB ANGLE.
- [SDR 2002UALA00270](https://openairdocs.org/sdr/2002UALA00270.md): Skin · damaged · Feb 13, 2002 · N326UA · Boeing 737322 · Fuselage Main, Plate/Skin
  > RIGHT HAND LOWER FUSELAGE AT BODY STATION 460 - BODY STATION 480 BETWEEN STRINGER 26R - 27R, SKIN IN CREASED, BULGING AND DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER AND FILLER.
- [SDR 2002UALA00269](https://openairdocs.org/sdr/2002UALA00269.md): Skin · damaged · Feb 13, 2002 · N326UA · Boeing 737322 · Fuselage Main, Plate/Skin
  > RIGHT HAND FORWARD FUSELAGE AT BODY STATION 328 - 344 AT STRINGER 19R - STRINGER 20R, PREVIOUS REPAIR INSTALLED WITH BLIND FASTENERS. MAJOR REPAIR ACCOMPLISHED. REMOVED TEMPORARY REPAIR. FABRICATED AND INSTALLED REPAIR DOUBLER.

## 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 = 'N326UA' AND deregistration_id = 'N326UA-2012-10-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N326UA-2012-10-01/reports

---
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