N652UA

Service difficulty reports · 303

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 = 'N652UA' AND registry_match = 'registration'
  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 CALA2015071094075Skin · dentedBULK CARGO DOOR, SKIN DENTED 2 PLACES ABOVE EXISTING DOUBLER. DENTS FOUND OUT OF SRM LIMITS. REMOVED DOUBLER & ENCOMPASSED INTO ONE REPAIR. REPAIRED IAW SRM 52-30-01 FIG 201 REPAIR 6. THIS IS A CAT B REPAIR.Jul 8, 2015 · N652UA · Boeing 767322 · Cargo/Baggage DoorsSDR CALA2015031793435Battery · dischargedSEAT MOUNTED EEL INOPERATIVE AT SEAT ROWS 35 RT - 39 RT. IAW WD 33 51 12 & MM 33 51 07, FOUND BATTERY M99084 BAD. CONNECTED NEW BATTERY & CHARGER TO CONNECTOR D9819P. ALL LIGHTS CAME ON.Mar 13, 2015 · N652UA · Boeing 767322 · Emergency LightingSDR CALA2015031793434Light · inoperativeFLOOR MOUNTED EEL STRIP INOPERATIVE AT LT AISLE JUST FWD OF LT AFT DOOR. CRIMPED CABLE IAW SWPM 20- 30-12 & AMM 33-51-10. OPERATIONS CHECKED OK.Mar 12, 2015 · N652UA · Boeing 767322 · Emergency LightingSDR CALA2015031793433Light · inoperativeSEAT MOUNTED EMER EXIT LIGHT INOPERATIVE AT SEAT ROW 28 LT. CRIMPED FEEDER. OPERATIONS CHECKED IAW MM 33-51-00-501.Mar 12, 2015 · N652UA · Boeing 767322 · Emergency LightingSDR CALA2015031793432Light · inoperativeFLOOR MOUNTED EEL STRIP INOPERATIVE AT MID LT LAVATORY. REPLACED BATTERY FLOOR MOUNTED EEL STRIP AT MID LT LAVATORY. OPERATIONS CHECKED NORMAL.Mar 12, 2015 · N652UA · Boeing 767322 · Emergency LightingSDR CALA2015031793431Light · inoperativeFLOOR MOUNTED EEL STRIP INOPERATIVE AT CTR SEAT ROW 19. REPLACED BATTERY FLOOR EEL STRIP AT ROW 19. OPERATIONS CHECKED NORMAL.Mar 12, 2015 · N652UA · Boeing 767322 · Emergency LightingSDR CALA2015031793430Sign · inoperativeGREEN EMER EXIT SIGNS INOPERATIVE AT BOTH LT OVERWING EXIT DOORS. REPLACED BATTERY EXIT SIGNS. OPERATIONS CHECKED NORMAL.Mar 12, 2015 · N652UA · Boeing 767322 · Emergency LightingSDR CALA2014102992623Structure · corrodedAFT PIT STATION 1285 HAS CORROSION ON J CHORD UNDER SIDE. REMOVED, FABRICATED & REPLACED STATION 1285 J CHORD PN 146T1210-20 IAW DWG 146T1210 REV C & SRM 51-40-02.Oct 27, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014102792618Skin · damagedNUMBER 1 ENG LT & RT TR'S LOWER INNER AFT BIFURCATION FAIRING S SKIN FOUND PITTED DURING GSO C-16 VISIT. AFTER DAMAGE REMOVAL & BLENDING REMAINING MATERIAL IS .081 INCHES WITH .019 INCHES REMOVED, OUT OF LIMITS OF SRM 54-33-01. WORK STEPS OF ECRA 7830-02831 Oct 26, 2014 · N652UA · Boeing 767322 · Nacelle/Pylon, Plate/SkinSDR CALA2014102192541Door Sill · corrodedFORWARD CGO DOOR CUT OUT SILL SUPPORT STRUCTURE CORRODED AT FS 588. R & R FWD CGO DOOR LOWER SILL PN 143T8204-1 WITH NEW SILL IAW SRM 51-40-02 & DWG 143T8513. THIS IS A PSE REPLACEMENT WITH NO INSPECTIONS REQUIRED OUTSIDE OF NORMAL MPD REQUIREMENTS. OPERATIOct 18, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014102192540Web · corrodedFORWARD PIT LOWER DOOR SILL BALL PANEL SUPPORT BEAM HAS CORROSION ON WEB & CHANNEL STATION 540 - 565 RBL 45. REMOVED WEB, FABRICATED WEB PN 451T2603-41 IAW DWG 451T2603 REV C. INSTALLED WEB & NEW CHANNEL PN 452T1137-23 IAW SRM 51-40- 02 & DWG 451T1602. THISOct 18, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014101692455Frame · corrodedFORWARD CARGO FLOOR FRAME AT BS 500 RBL 15 J CHORD IS CORRODED UNDER NUTPLATES. REMOVED DAMAGED FRAME J CHORD ENTIRE LENGTH & FABRICATED & INSTALLED A NEW 143T1060-25 J CHORD IAW DWG 143T1203 REV A & SRM 51-40-02.Oct 11, 2014 · N652UA · Boeing 767322 · Fuselage Main, FrameSDR CALA2014101692454Frame · corrodedFORWARD CARGO FLOOR STATION 544 RBL 19 FRAME J CHORD IS CORRODED UNDER NUTPLATES. REMOVED DAMAGED FRAME J CHORD ENTIRE LENGTH, FABRICATED A NEW PN 143T1060-27 J CHORD & INSTALLED IAW DWG 143T1205. CAT A PERMANENT REPAIR.Oct 11, 2014 · N652UA · Boeing 767322 · Fuselage Main, FrameSDR CALA2014101692453Frame · corrodedFORWARD CARGO FLOOR BS 632 RBL 28 FRAME J CHORD CORRODED UNDER NUTPLATES. REMOVED ENTIRE J CHORD SECTION & REPLACED WITH A NEW J CHORD PN 143T1060-29 IAW DWG 143T1209 SHEET 4 REV C & SRM 51-40-02 ON NON-ROUTINE 40976.Oct 11, 2014 · N652UA · Boeing 767322 · Fuselage Main, FrameSDR CALA2014101692452Stringer · dentedAREA AFT OF BULK CARGO COMPARTMENT LOWER BILGE STRINGER IS DENTED SEVERAL AREAS AT BS 1540 - 1560 STRINGER 36L. DENTS EXCEED SRM 53-00-03 DETAIL III LIMITS. REMOVED DAMAGED SECTION OF STRINGER 36L, FABRICATED STRINGER REPAIR CHANNEL, SPLICE ANGLES, FILLERS &Oct 11, 2014 · N652UA · Boeing 767322 · Fuselage Main, Longeron/StringerSDR CALA2014101692451Frame · crackedBS 1263 FRAME UPPER J CHORD IS CORRODED AT NUTPLATES LBL 36. REMOVED FRAME J CHORD, FABRICATED & INSTALLED A NEW J CHORD PN 146T1209-26 IAW DWG 146T109 & SRM 51-40-02 ON NON-ROUTINE 41233.Oct 11, 2014 · N652UA · Boeing 767322 · Fuselage Main, FrameSDR CALA2014101692440Floorbeam · corrodedBS 347 FLOORBEAM T CAP CORROSION REMOVED & REMAINING MATERIAL BEYOND SRM LIMITS. DAMAGED T CAP CUT OUT BETWEEN RBL 4 & RBL 87. AFTER TRIMMING THE CHORD THERE IS SHORT ED IN THE WEB DUE TO EXISTING FASTENER LOCATIONS FROM A PREVIOUS REPAIR AT RBL 27 - 33. REOct 10, 2014 · N652UA · Boeing 767322 · Fuselage Main, Floor BeamSDR CALA2014101692438Strap · corrodedWEB UPPER STRAP IS CORRODED AT NUTPLATES BS 1219, LBL 22 - LBL 30. REMOVED DAMAGED CORROSION FROM AFT PIT FRAME J CHORD AT BS 1219, MATERIAL REMAINING EXCEEDS SRM 53-00-07 LIMITS. CUT OUT DAMAGED CHORD & REPLACED ENTIRE PN 146T1060-2 CHORD IAW DWG 146T0250 ROct 10, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014100792382Structure · corrodedMAIN CABIN STATION 1562 LBL 54 SHOWS SIGNS OF CORROSION ON UPPER SURFACE. REMOVED DAMAGED SECTION & REPAIRED IAW SRM 53-00-51 REPAIR 1 STATION 1562 LBL 52 - LBL 90.Oct 6, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014100792381Structure · corrodedAFT CARGO FLOOR STRUCTURE STATION 1175 LBL 24 - 23 SHOWS SIGNS OF CORROSION. REMOVED & INSTALLED NEW J CHORD IAW DWG 146T1060 & SRM 51-40-02 SHEET 3.Oct 6, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014100792380Structure · corrodedAFT CARGO PIT STATION 1197 + 66 RBL 8 - 18 SHOWS SIGNS OF CORROSION ON UPPER J CHORD. R & R CORD IAW DWG 146T1226 SHEET 1 & SRM 51-40-02.Oct 6, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014100792379Floorbeam · corrodedMAIN CABIN FLOORBEAM STATION 1518 UPPER CAP LBL 1 SHOWS SIGNS OF CORROSION. REPAIRED FLOORBEAM AT STATION 1518 UPPER CAP IAW SRM 53-00-51 REPAIR 2.Oct 6, 2014 · N652UA · Boeing 767322 · Fuselage Main, Floor BeamSDR CALA2014100792378Structure · corrodedAC4 CORROSION FOUND ON UPPER SURFACE STATION 1502 RBL 1 - LBL 1 SHOWS SIGNS OF CORROSION. REPAIRED CORROSION FOUND IAW SRM 53-00-51 REPAIR 4. CAT A REPAIR NO FURTHER ACTION NECESSARY.Oct 6, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014092992348Seat Track · corrodedFLOORBOARD FASTENER HOLES ARE CORRODED, FOUR EACH UNDER FLOORBOARD P83, RBL 11. MATERIAL REMAINING ON UPPER CHORD AT BS 933, RBL 11 EXCEEDS SRM 53-00-51 DETAIL II LIMITS. REMOVED UPPER CHORD & SEAT TRACK CROWN. FABRICATED & INSTALLED IAW DWG 145T5211 REV L BSep 28, 2014 · N652UA · Boeing 767322 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2014092992347Web · corrodedWEB UNDER STRAP CORRODED IN SEVERAL PLACES AT BS 1197+44, LBL 36 - RBL 45. J CHORD R & R IAW SRM 51-40 -02 & DWG 146T1225.Sep 28, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014092992335Shear Tie · corrodedAREA AFT OF BULK CARGO COMPARTMENT LOWER BILGE FRAME SHEAR TIE IS CORRODED AT BS 1540, STRINGER 39L TO 39R. REMOVED CORRODED SHEAR TIE & FABRICATED A NEW SHEAR TIE IAW DWG 140T2102 REV C. INSTALLED PN 140T2102-607 IAW SRM 51-40-05.Sep 27, 2014 · N652UA · Boeing 767322 · Fuselage Internal Mounting StructureSDR CALA2014092992334Floor Support · corrodedTRANSVERSE FLOORBEAM HAS CORROSION AT FASTENER HOLES APPROX BS 852 & RBL 76. REMOVED CORROSION & FOUND MATERIAL REMOVED EXCEEDS SRM 53-50-51 LIMITS. ORIGINAL THICKNESS IS .120, REMOVED .028, REMAINING IS .092. REMOVED DAMAGED SECTION OF UPPER CHORD. FABRICSep 27, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014092292271Structure · corrodedFORWARD CARGO COMPARTMENT FLOOR FRAME J CHORD CORRODED AT BS 566 RBL 24 & LBL 24. REPLACED J CHORD IAW SRM 51-40-02.Sep 18, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014092292270Angle · corrodedFORWARD CARGO COMPARTMENT, CHORD ANGLE CORRODED AT BS 478 - 632 RBL 29.5. REPLACED CHORD IAW SRM 51-40-02.Sep 18, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014092292269Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER SURFACE CORRODED AT BS 325 RBL 36 - 46. REMOVED DAMAGE. MANUFACTURED REPAIR PARTS & INSTALLED REPAIR IAW SRM 53-00-51 REPAIR 1.Sep 18, 2014 · N652UA · Boeing 767322 · Fuselage Main, Floor BeamSDR CALA2014092292268Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER SURFACE CORRODED AT BS 303 RBL 50. REMOVED DAMAGE. MANUFACTURED REPAIR PARTS & INSTALLED REPAIR IAW SRM 53-00-51 REPAIR 1.Sep 18, 2014 · N652UA · Boeing 767322 · Fuselage Main, Floor BeamSDR CALA2014092292266Skin · dentedBULK CARGO DOOR SKIN DENTED 2 PLACES ABOVE EXISTING DOUBLER. DENTS FOUND OUT OF SRM LIMITS. REMOVED DOUBLER & ENCOMPASSED INTO ONE REPAIR, REPAIRED IAW SRM 52-30-01 FIG 201 REPAIR 6. THIS IS A CAT B REPAIR WITH LFEC EXTERNAL INSPECTIONS TO BEGIN AT 30000 PTSep 18, 2014 · N652UA · Boeing 767322 · Cargo/Baggage DoorsSDR CALA2014092292265Support · corrodedFORWARD CARGO FLOOR STATION 580 RBL 30 PDU SUPPORT CHORD CORRODED UNDER NUTPLATES. REMOVED PDU SUPPORT CHORD IAW SRM 51-40-0 2. RECEIVED NEW CHORD PN 143T8236-17. LOCATED, DRILLED & DEBURRED IAW SRM 51-40-05. INSTALLED IAW DWG 143T8201 REV C & SRM 51-40-02Sep 18, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014092292264Support · corrodedFORWARD CARGO FLOOR STATION 520 RBL 44 PDU SUPPORT CHORD CORRODED UNDER NUTPLATES. REMOVED PDU SUPPORT CHORD IAW SRM 51-40-0 2. RECEIVED NEW CHORD PN 143T8236-4. LOCATED, DRILLED & DEBURRED IAW SRM 51-40-05. INSTALLED IAW DWG 143T8201 REV C & SRM 51-40-02.Sep 18, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014092292262Support · corrodedFORWARD CARGO FLOOR STATION 577 RBL 44 PDU SUPPORT CHORD CORRODED UNDER NUTPLATES. REMOVED PDU SUPPORT CHORD, RECEIVED NEW CHORD 143T8236-8, LOCATED, DRILLED & DEBURRED IAW SRM 51-40-05. INSTALLED IAW DWG 143T8201 REV C & SRM 51-40-02.Sep 18, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014091892242Strap · corrodedAFT PIT WEB UPPER STRAP IS CORRODED IN SEVERAL PLACES ON FRAME AT BS 1153 LBL 8 TO 37. REMOVED SKIN WEB AT STATION 1153, RBL 15 & DAMAGED FLOOR STRUCTURE. RECEIVED NEW J CHORD PN 146T1060-2 & INSTALLED IAW DWG 146T1204 & SRM 51- 40-05 & 51-40-02 ENTIRE LENGTSep 16, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014091892240Strap · mechanic errorSEAT TRACK STRAP HAS A DRILL START NEXT TO REPAIR FASTENER COMMON TO TRANSVERSE FLOORBEAM AT BS 873 & RBL 34. REMOVED TRANSVERSE FLOORBEAM SPLICE REPAIR, FABRICATED UPPER CHORD ANGLE & INSTALLED SPLICE REPAIR IAW SRM 53-00-51. THIS IS A CAT A PERMANENT REPAISep 16, 2014 · N652UA · Boeing 767322 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2014091892232Floorbeam · corrodedBS 287 FLOORBEAM CORRODED AT LBL 12. REMOVED CORROSION & HAD MATERIAL LOSS OF .049 INCHES FROM ORIGINAL THICKNESS OF .125 INCHES, EXCEEDING SRM 53-00-51 FIG 101 DETAIL II LIMITS. REMOVED DAMAGED SECTION OF FLOORBEAM, FABRICATED -1 & -2 ANGLE, -3 STRAP & INSTSep 13, 2014 · N652UA · Boeing 767322 · Fuselage Main, Floor BeamSDR CALA2014091292116Strap · corrodedWEB UPPER STRAP IS CORRODED & NUTPLATES AT BS 1197 & 110, RBL 42 - 44. R & R J CHORD AT STATION 1197 & 110, RBL 42 - 44 IAW SRM 51-40-02.Sep 11, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014091292114Heating Element · crackedRIGHT FWD OVERWING INSULATION HEATER ELEMENT CRACKED. REMOVED RT FWD OVERWING EXIT LINER. INSTALLED ON EXIT HATCH & INSTALLED ON ACFT. OPERATIONS TESTED IAW MM 21-45-61.Sep 10, 2014 · N652UA · Boeing 767322 · Emergency ExitsSDR CALA2014091292112Heating Element · crackedRIGHT AFT OVERWING INSULATION HEATER ELEMENT IS CRACKED. REMOVED RT AFT OVERWING EXIT LINER. INSTALLED ON EXIT HATCH & INSTALLED ON ACFT. OPERATIONS TESTED IAW MM 21-45-61.Sep 10, 2014 · N652UA · Boeing 767322 · Emergency ExitsSDR CALA2014091292111Insulation · burnedLEFT FWD OVERWING EXIT INSULATION IS BURNED AT HEATER ELEMENT. REMOVED LT FWD OVERWING EXIT LINER. INSTALLED ON EXIT HATCH & INSTALLED ON ACFT. OPERATIONS TESTED IAW MM 21-45-61.Sep 10, 2014 · N652UA · Boeing 767322 · Emergency ExitsSDR CALA2014091292109Floorbeam · corrodedFLOORBEAM UPPER CORD FOUND CORRODED NEAR NUTPLATES STATION 1197 & 88 LBL 44 - 41. R & R FLOORBEAM CORD PN 146T1060-1 IAW DWG 146T1227SH1 & SRM 51-40-02. NO FURTHER ACTION NECESSARY.Sep 9, 2014 · N652UA · Boeing 767322 · Fuselage Main, Floor BeamSDR CALA2014090892075Beam · corrodedTRANSVERSE BEAM UPPER STRAP IS CORRODED UNDER FLOORBOARD P 85 BS 880 LBL 32. REMOVED, FABRICATED & INSTALLED TRANSVERSE BEAM BS 860 - 900 LBL 33.09 IAW SRM 51-40-02 & 53-00-51 FIG 201 REPAIR 3 THIS IS A CATEGORY A REPAIR WITH NO REQUIRED INSPECTIONS OUTSIDE OSep 4, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014090892073Web · corrodedFORWARD CARGO FLOOR WEB CORRODED ON BOTTOM SIDE STATION 610 RBL 24. CORROSION BEYOND SRM LIMITS. REMOVED, DRILLED UP NEW WEB IAW SRM 51-40-05 & DWG 143T5012 REV G.Sep 3, 2014 · N652UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR CALA2014050690972Seal · damagedHYD CTR SYS LOSS OF QTY AT GR EXTENSION. REPLACED LEAKING NR 10 SPOILER ACTUATOR FILTER HOUSING SEAL MM27-61-01. LEAK CHECKED NORMAL & C SYS REPLENISHED.May 6, 2014 · N652UA · Boeing 767322 · Drag Control ActuatorSDR CALA2014033190716Warning Bell · false activationFIRE BELLS SOUNDING WITH NO FIRE INDICATION & UNABLE TO SILENCE.Mar 30, 2014 · N652UA · Boeing 767322 · Fire DetectionSDR CALA2013122693937Pressure Switch · inoperativeLT HYD DEMAND PUMP INOPERATIVE IN AUTO & ON MODE IAW IAHMM. REPLACED LT ENG DRIVEN PUMP LOW PRESS SW IAW AMM 29-11-17. OPERATIONS CHECKED GOOD NO LEAKS. ENG LOW PRESS SW WAS PREVENTING AUTO FUNCTION OF DEMAND PUMP.Dec 24, 2013 · N652UA · Boeing 767322 · Hydraulic System, MainSDR CALA2013122393891Fseu · malfunctionedSTATUS MESSAGE FLAP SLAT ELECTRICAL. STAB POSITION CARD M838 & FLAP SLAT ELECTRICAL UNIT AT FAULT. R & R STAB MODULE & FLAP SLAT MODULE IAW 27-51-01, 27-58-01. SYS OPERATIONS CHECKED GOOD. ALSO PERFORMED TEST 30 ALL SYS PASSED.Dec 22, 2013 · N652UA · Boeing 767322 · Trailing Edge Flap Control SystemSDR CALA2013121893777Sdu · failedSATCOM DOES NOT PASS INSTALL TEST IAW WORK CARD 6-2013-2C. FAILED SDU CH 5 TX & RX FAULT. REPLACED SATCOM SDU IAW MM, CHECKED OK. SOFTWARE VERIFIED CORRECT IAW IPC 31-00-00-99 & DIS 39908.Dec 17, 2013 · N652UA · Boeing 767322 · Communications System
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