N326UA, cancelled Oct 1, 2012

Service difficulty reports · 38

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 2008UALA05719Connector · underservicedF/O SIDE OXYGEN MASK COMM CONNECTOR DISCONNECTED. REPAIRED O2 BOX CONNECTOR.Sep 13, 2008 · N326UA · Boeing 737322 · Communications System WiringSDR 2008UALA04357Light · inoperativeEXTERIOR EMERGENCY LIGHT AFT OF DOOR 1L IS INOP. *S/D* REPLACED LIGHT ASSEMBLY. OP CHECKS GOOD.Aug 20, 2008 · N326UA · Boeing 737322 · Emergency LightingSDR 2008UALA03925Light · inoperativeAFT SECTION OF EEL STRIP LIGHTING INOP. REPLACED AFT EEL STRIP CABLE. OPS CKS GOOD.Jul 19, 2008 · N326UA · Boeing 737322 · Emergency LightingSDR 2008UALA00511Light · inoperativeEMERGENCY EXIT FLOOR LIGHTS INOPERATIVE PAST ROW 15. REPLACED POWER SUPPLY, BATTERY AND LIGHT STRIP.Jan 29, 2008 · N326UA · Boeing 737322 · Emergency LightingSDR 2008UALA00102Light · inoperativeEEL FLOOR LIGHTS FROM ROW 15 TO REAR OF PLANE IS INOP. REPLACED POWER STRIP. Jan 6, 2008 · N326UA · Boeing 737322 · Emergency LightingSDR 2007UALA05254Feeder Cable · inoperativeEEL LIGHTS INOP AFT OF ROW 15. CLEANED AND REPLACED CABLE. RELAMPEDDec 24, 2007 · N326UA · Boeing 737322 · Light System WiringSDR 2007UALA03623Skin · crackedEXTERNAL 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.Sep 7, 2007 · N326UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2007UALA03622Stringer Clip · crackedSTRINGER CLIP BS 400 STRINGER 27L CRACKED IN CORNER. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW STRINGER CLIP BS 400 STR (HMV)Sep 7, 2007 · N326UA · Boeing 737322 · Fuselage Main, Attach FittingsSDR 2007UALA03603Skin · damagedAFT 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.Sep 6, 2007 · N326UA · Boeing 737322 · Cargo/Baggage DoorsSDR 2007UALA03233Controller · failedEN 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. SECURAug 19, 2007 · N326UA · Boeing 737322 · Cabin Pressure ControllerSDR 2007UALA02741Lamp · inoperativeEEL LIGHTS INOP FROM SEAT 15 TO BACK OF CABIN. REPLACED TO FLEXIBLE LAMPS PER MM 33-51-90. TEST OK 33-51-02.Jul 19, 2007 · N326UA · Boeing 737322 · Emergency LightingSDR 2007UALA02274Light · inoperativeLEFT SIDE EXTERIOR EMERGENCY OVERWING LIGHT INOP. RELAMPED, TEST NORMAL.Jun 27, 2007 · N326UA · Boeing 737322 · Emergency LightingSDR 2007UALA01985Light · inoperativeALL 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.Jun 12, 2007 · N326UA · Boeing 737322 · Emergency LightingSDR 2007UALA00277Fuse · blownLEFT AFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BLOWN FUSE.Jan 31, 2007 · N326UA · Boeing 737322 · Emergency LightingSDR 2006UALA01708Smoke · detectedSMOKE IN CABIN IN AREA OF AFT GALLEY OVERHEAD. SMELL WAS ACTUALLY REPORTED TO BE "LIKE COFFEE" AND NOT SMOKE. COULD NOT DUPLICATE ODOR.Sep 1, 2006 · N326UA · Boeing 737322 · Air Distribution SystemSDR 2006UALA00451Skin · dentedLH HORIZONTAL STAB UPPER SKIN DENTED 6 FEET FROM INBD. NEW REPAIR SKIN SPLICED IN PER AAR EA 1060102.Mar 9, 2006 · N326UA · Boeing 737322 · Horizontal Stabilizer, Plate/SkinSDR 2006UALA00447Floorbeam · crackedCABIN 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 & SMar 9, 2006 · N326UA · Boeing 737322 · Fuselage Main, Floor BeamSDR 2006UALA00446Stringer · crackedCABIN BS 296 S10L IS CRACKED AT UPPER FLANGE. REMOVED DAMAGE, MANUFACTURED AND INSTALLED STRINGER REPAIR, STRINGER CLIP AND INTERCOSTAL.Mar 8, 2006 · N326UA · Boeing 737322 · Fuselage Main, Longeron/StringerSDR 2006UALA00432Bushing · migratedLT 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 810Mar 8, 2006 · N326UA · Boeing 737322 · Horizontal Stabilizer StructureSDR 2006UALA00445Skin · damagedRUDDER AT NR 4 HINGE CUTOUT RIGHT UPPER EDGE DAMAGED. DAMAGE TO RUDDER AT NR 4 HINGE CUTOUT WAS REPAIR PER AAR EO I060062.Mar 8, 2006 · N326UA · Boeing 737322 · Rudder, Plate/SkinSDR 2006UALA00399Skin · puncturedNR 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.Mar 4, 2006 · N326UA · Boeing 737322 · Leading Edge DevicesSDR 2006UALA00394Skin · erodedAFT 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, TRIPLERMar 4, 2006 · N326UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2006UALA00382Stiffener · crackedMAIN 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 STIFFENERMar 3, 2006 · N326UA · Boeing 737322 · Fuselage Miscellaneous StructureSDR 2006UALA00403Slide · no testDURING DEPLOYMENT OF FWD GALLEY DOOR SLIDE, SLIDE TWISTED AND DEPLOYED VERTICALLY AT DOOR THRESHOLD AREA.Mar 3, 2006 · N326UA · Boeing 737322 · Escape SlideSDR 2006UALA00366Stringer Clip · crackedFOUND AFT PIT STA 727A RBL 24" STRINGER CLIP CRACKED AT STR 25R. INSTALLED NEW STRINGER CLIP REF SRM 51-40-02.Mar 1, 2006 · N326UA · Boeing 737322 · Fuselage Main, Attach FittingsSDR 2006UALA00364Frame · dentedAFT 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.Feb 28, 2006 · N326UA · Boeing 737322 · Fuselage Main, FrameSDR 2006UALA00341Floorbeam · corrodedCABIN 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.Feb 26, 2006 · N326UA · Boeing 737322 · Fuselage Main, Floor BeamSDR 2006UALA00340Skin · damagedLT 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.Feb 26, 2006 · N326UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2006UALA00339Frame · gougedFOUND 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.Feb 26, 2006 · N326UA · Boeing 737322 · Fuselage Main, FrameSDR 2006UALA00357Wire · exposedTHE 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. CFeb 24, 2006 · N326UA · Boeing 737322 · Fuel System WiringSDR 2006UALA00335Stringer Clip · damagedAFT CARGO COMPARTMENT STA 767 S23L STRINGER CLIP DAMAGED. REMOVED AND REPLACED STRINGER CLIP REF SRM 51-40-02.Feb 24, 2006 · N326UA · Boeing 737322 · Fuselage Main, Attach FittingsSDR 2006UALA00334Skin · crackedELECTRONIC 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.Feb 24, 2006 · N326UA · Boeing 737322 · Electrical/Electronic Compartment DoorsSDR 2006UALA00299Door Frame · crackedFWD 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 ANFeb 18, 2006 · N326UA · Boeing 737322 · Galley DoorsSDR 2005UALA01232Relay · failedBOTH IRS ON DC LIGHTS ILLUM JUST AFTER LIFTOFF. SUA IRS POWER FAULT HAS NOT REOCCURRED.Nov 5, 2005 · N326UA · Boeing 737322 · Navigation SystemSDR 2002UALA00271Frame · crackedOVERWING FRAME AT BODY STATION 616, LBL 65 ATTACH CHORD CRACKED OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED ANGLE REPAIR.Feb 14, 2002 · N326UA · Boeing 737322 · Fuselage Main, FrameSDR 2002UALA00272Angle · crackedFORWARD PIT STATION 495 FLOOR WEB ANGLE HAS CRACK AT S-28R. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW WEB ANGLE.Feb 13, 2002 · N326UA · Boeing 737322 · Fuselage Miscellaneous StructureSDR 2002UALA00270Skin · damagedRIGHT 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.Feb 13, 2002 · N326UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2002UALA00269Skin · damagedRIGHT 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.Feb 13, 2002 · N326UA · Boeing 737322 · Fuselage Main, Plate/Skin
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