# Service difficulty reports: N618UA, cancelled Jul 13, 2007

A list on [N618UA, cancelled Jul 13, 2007](https://openairdocs.org/deregistered/N618UA-2007-07-13.md).

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

- [SDR 2004UALA00418](https://openairdocs.org/sdr/2004UALA00418.md): Bolt · sheared · Mar 18, 2004 · N618UA · Boeing 767222 · Fasteners
  > NOSE GEAR LT DOOR LINK ROD HINGE BOLT IS SHEARED. FOUND DURING NR 1 SERVICE. BOLT NOT RECOVERED, CAUSE OF FAILURE UNKNOWN. REPLACED BOLT.
- [SDR 2003UALA00618](https://openairdocs.org/sdr/2003UALA00618.md): Keelbeam · corroded · Aug 12, 2003 · N618UA · Boeing 767222 · Fuselage Main, Keel
  > KEELBEAM WEB DRAIN HOLE HAS CORROSION AT BS 786, BL0.
- [SDR 2003UALA00632](https://openairdocs.org/sdr/2003UALA00632.md): Wedge · delaminated · Aug 4, 2003 · N618UA · Boeing 767222 · Leading Edge Devices
  > T/E WEDGE DELAMINATED. T/E WEDGE REPLACED.
- [SDR 2003UALA00285](https://openairdocs.org/sdr/2003UALA00285.md): Skin · gouged · Mar 16, 2003 · N618UA · Boeing 767222 · Fuselage Main, Plate/Skin
  > A/C DAMAGED BY LOADER AFT OF FWD CARGO DOOR. VARIOUS DENTS AND GOUGES MAJOR REPAIR ACCOMPLISHED WITH DOUBLERS IN AREA FWD OF CARGO DOOR BELOW RT WING LITE.
- [SDR 2001UALA01977](https://openairdocs.org/sdr/2001UALA01977.md): Controller · failed · Aug 31, 2001 · N618UA · Boeing 767222 · Air Distribution System
  > FWD EQUIPMENT NO COOLING LIGHT ON FOR 3 MINUTES. REPLACED CONTROLLER AND CLEANED EQUIPMENT COOLING AIR CLEANER.
- [SDR 2001UALA00886](https://openairdocs.org/sdr/2001UALA00886.md): Engine · malfunctioned · May 10, 2001 · N618UA · Boeing 767222 · Engine (Turbine/Turboprop)
  > AT LOW POWER SETTING ON CLIMB UNDER 1.20 EPR RT ENG LAGGED LT BY.15 EPR AND 15 PERCENT N1, ABOVE 1.20 EPR AT CRUISE OKAY. ON DESCENT AT LOW ALT RT LAGGED BY.15 EPR AND 20.0 EPR.
- [SDR 2001UALA00156](https://openairdocs.org/sdr/2001UALA00156.md): Stringer · corroded · Feb 24, 2001 · N618UA · Boeing 767222 · Fuselage Main, Longeron/Stringer
  > AFT PIT BS 1307 - 1329 STRINGER 35L CORRODED. INSTALLED STRINGER REPAIR REF: SRM 53-00-03 FIG 202.
- [SDR 2001UALA00154](https://openairdocs.org/sdr/2001UALA00154.md): Shear Tie · corroded · Feb 24, 2001 · N618UA · Boeing 767222 · Fuselage Main, Structure
  > AFT PIT BS 1153 BETWEEN STRINGERS 38R - 39R SHEAR TIE CORRODED. REPLACED SHEAR TIE REF: BAC DWG 140T2102, SRM 53-00-07, 51-40-02.
- [SDR 2001UALA00155](https://openairdocs.org/sdr/2001UALA00155.md): Shear Tie · corroded · Feb 23, 2001 · N618UA · Boeing 767222 · Fuselage Main, Structure
  > AFT PIT BS 1263 BETWEEN STRINGERS 37L - 38L SHEAR TIE CORRODED. REPLACED SHEAR TIE REF: BAC DWG 140T2101, SRM 51-10-00, AND 51-40-02.
- [SDR 2001UALA00153](https://openairdocs.org/sdr/2001UALA00153.md): Rib · corroded · Feb 23, 2001 · N618UA · Boeing 767222 · Cargo/Baggage Doors
  > AFT CARGO DOOR BS 1270-1350 RIB NR 3 CORRODED. REPAIRED DOOR BEAM PER TIMCO REO-GO7862 REF: SRM 52-30-02.
- [SDR 2001UALA00124](https://openairdocs.org/sdr/2001UALA00124.md): Shear Tie · corroded · Feb 15, 2001 · N618UA · Boeing 767222 · Fuselage Main, Structure
  > AFT CARGO PIT BS 1197 BETWEEN STR 37L AND 38L SHEAR TIE CORRODED. REPLACED SHEAR TIE BY OSV TIMCO, REFERENCE SRM 51-40-02 FOR FASTENER INSTALLATION PROCEDURES.
- [SDR 2001UALA00118](https://openairdocs.org/sdr/2001UALA00118.md): Frame · damaged · Feb 15, 2001 · N618UA · Boeing 767222 · Fuselage Main, Frame
  > AFT PIT BS 1153 BETWEEN STRINGER 39L AND 39R FRAME WEB HAS ELONGATED HOLE. *S/D* WEB REPAIR INSTALLED BY OSV TIMCO, REFERENCE SRM 51-40-02 FOR FASTENER INSTALLATION PROCEDURES.
- [SDR 2001UALA00189](https://openairdocs.org/sdr/2001UALA00189.md): Splice · corroded · Feb 14, 2001 · N618UA · Boeing 767222 · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON INBOARD SIDE BETWEEN 2 SIDE PANELS, ATTACH SPLICE IS CORRODED. REPLACED SPLICE PER SRM 51-40-02.
- [SDR 2001UALA00186](https://openairdocs.org/sdr/2001UALA00186.md): Shear Tie · corroded · Feb 14, 2001 · N618UA · Boeing 767222 · Fuselage Main, Structure
  > AFT PIT SHEAR TIE CORRODED BS 1480. REPLACED SHEAR TIE REF: BAC 140T2102 AND SRM 51-40-02.
- [SDR 2001UALA00183](https://openairdocs.org/sdr/2001UALA00183.md): Shear Tie · corroded · Feb 14, 2001 · N618UA · Boeing 767222 · Fuselage Main, Structure
  > AFT PIT SHEAR TIE BETWEEN STR 39L AND 39R CORRODED. INSTALLED NEW SHEAR TIE PER BAC DRAWING 146T1206 AND SRM 51-40-2.
- [SDR 2001UALA00182](https://openairdocs.org/sdr/2001UALA00182.md): Seat Track · corroded · Feb 14, 2001 · N618UA · Boeing 767222 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK FITTING CORRODED AT STATION 1421 T0 1471, RBL 90, UNDER FLANGE. REPLACED FITTING PER BAC DWG 146T5204-2 AND INSTALLED FITTING PER SRM 51-40-2.
- [SDR 2001UALA00134](https://openairdocs.org/sdr/2001UALA00134.md): Stringer · corroded · Feb 14, 2001 · N618UA · Boeing 767222 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT AT BS 1395, STRINGER 39L END FITTING IS CORRODED BOTH SIDES OF STRINGER. REMOVED CORROSION FROM STRINGER PER GN-MM 5-0-6-1. REPLACED STRINGER SPLICE CLIPS PER BAC DWG 146T3006 STRINGER SPLICE CLIPS PER BAC DWG 146T3006 AND INSTALLED PER SRM 51-
- [SDR 2001UALA00111](https://openairdocs.org/sdr/2001UALA00111.md): Attach Angle · corroded · Feb 12, 2001 · N618UA · Boeing 767222 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT BS 1087 STRINGER 39R FRAME TO STRINGER ATTACH ANGLE CORRODED. *S/D* STRINGER ATTACH ANGLE WAS REPLACED BY OSV TIMCO, REFERENCE SRM 51-40-02 FOR FASTENER INSTALLATION PROCEDURES.
- [SDR 2001UALA00107](https://openairdocs.org/sdr/2001UALA00107.md): Shear Tie · corroded · Feb 9, 2001 · N618UA · Boeing 767222 · Fuselage Main, Structure
  > AFT CARGO PIT AT BS 1307 BETWEEN STRINGERS 36L AND 36R SHEAR TIE IS CORRODED. *S/D* SHEAR TIE WAS REPLACED BY OSV TIMCO, REFERENCE SRM 51-40-02 FOR FASTENER INSTALLATION PROCEDURES.
- [SDR 2001UALA00093](https://openairdocs.org/sdr/2001UALA00093.md): Frame · corroded · Feb 8, 2001 · N618UA · Boeing 767222 · Fuselage Main, Frame
  > AFT CARGO PIT AT BS 1197 FROM RBL 13-19, FRAME CAP IS CORRODED. *S/D* FRAME T-CAP WAS REPLACED BY OSV TIMCO, REFRENCE 51-40-02 FOR FASTENER INSTALLATION PROCEDURES.
- [SDR 2001UALA00092](https://openairdocs.org/sdr/2001UALA00092.md): Skin Panel · corroded · Feb 7, 2001 · N618UA · Boeing 767222 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE VHF RIGHT ANTENNA SKIN CUTOUT CORRODED STATION 510 BL 0. *S/D* SKIN REPAIRED PER SRM 53-30-01 AT OSV TIMCO.
- [SDR 99UAL900211](https://openairdocs.org/sdr/99UAL900211.md): Heat Tape · failed · Apr 14, 1999 · N618UA · Boeing 767222 · Water Line Anti-Ice System
  > FLIGHT ATTENDANT REPORTED SMOKE IN CABIN/COCKPIT AREA, NOTIFIED MAINTENANCE. *S/D* HEATER TAPE B109 FAILED CAUSING INSULATION ON FORWARD GALLEY CHILLER DUCT TO IGNITE. 767 ENGINEERING ISSUED CALLOUT TO INSPECT 767 AIRCRAFT WITH THIS HEATER TAPE CONFIGURATION
- [SDR 98UAL900545](https://openairdocs.org/sdr/98UAL900545.md): Battery Pack · discharged · Nov 15, 1998 · N618UA · Boeing 767222 · Emergency Lighting
  > LEFT EMERGENCY ESCAPE LIGHT DOES NOT COME ON WHEN TEST 1 BUTTON IS PUSHED. BATTERY PACK WAS REPLACED. PROBLEM WAS CORRECTED.
- [SDR 98UAL900267](https://openairdocs.org/sdr/98UAL900267.md): Seal · misinstalled · Jun 17, 1998 · N618UA · Boeing 767222 · Emergency Exits
  > RIGHT OVERWING HATCH MAJOR AIR LEAK. UNABLE TO MAINTAIN CABIN PRESSURIZATION. RETURNED TO SFO. *S/D* FOUND DOOR SEAL AT RIGHT OVERWING EXIT DOOR TO BE INSTALLED INCORRECTLY. SEAL REINSTALLED PER MM, OPS CHECK NORMAL.
- [SDR 98UAL900227](https://openairdocs.org/sdr/98UAL900227.md): Squib · failed · May 31, 1998 · N618UA · Boeing 767222 · Emergency Equipment
  > NR 1 SQUIBB WILL NOT TEST FOR THE LEFT OVERWING EXIT.
- [SDR 96UAL900864](https://openairdocs.org/sdr/96UAL900864.md): Heater · malfunctioned · Nov 12, 1996 · N618UA · Boeing 767222 · Heating System
  > DIVERTED TO ORD DUE TO AN ELECTRICAL ODOR IN THE COCKPIT. *S/D* THE FIRST OFFICER'S SHOULDER HEATER OVERHEATED. THE HEATER WAS REPLACED, OPERATIONS CHECK NORMAL.
- [SDR 96UAL900862](https://openairdocs.org/sdr/96UAL900862.md): Heater · malfunctioned · Nov 12, 1996 · N618UA · Boeing 767222 · Heating System
  > DIVERTED TO DEN UNDER AMBER ALERT WITH SMOKE IN THE COCKPIT. *S/D* THE FIRST OFFICER'S SHOULDER HEATER OVERHEATED. THE HEATER WAS REPLACED, OPERATIONS CHECK NORMAL.
- [SDR 96UAL900658](https://openairdocs.org/sdr/96UAL900658.md): Compressor · stalled · Aug 27, 1996 · N618UA · Boeing 767222 · Turbine Engine Compressor Section
  > ON LANDING ROLL-OUT. THE RIGHT ENGINE HAD A COMPRESSOR STALL WHILE COMING OUT OF REVERSE THRUST. ENGINE EXCEEDED EXHAUST GAS TEMPERATURE LIMIT AND WAS IMMEDIATELY SHUT DOWN. THE AIRCRAFT FLIGHT RECORDER INDICATED THAT THE ENGINE HAD BEEN IN REVERSE THRUST BE
- [SDR 96UAL900422](https://openairdocs.org/sdr/96UAL900422.md): Fire Warning · activated · Jun 7, 1996 · N618UA · Boeing 767222 · Fire Protection System
  > CREW REPORTED APU AUTO SHUT DOWN AND FIRE WARNING. FLIGHT CREW DISCHARGED THE FIRE BOTTLE. SUPPLEMENTAL DATA UPDATE: REPLACED APU FIRE BOTTLE AND SQUIBB PER MM 26-22-02. RAN APU AND CHECKED FOR PNEUMATIC LEAKS, NO LEAKS FOUND. APU RAN FOR SEVERAL HOURS WIT
- [SDR 96UAL900179](https://openairdocs.org/sdr/96UAL900179.md): Battery Pack · discharged · Mar 11, 1996 · N618UA · Boeing 767222 · Emergency Lighting
  > THREE EXTERIOR EMERGENCY LIGHTS ON RIGHT SIDE INOP. TWO OVER THE WING AND ONE BY THE RIGHT FORWARD ENTRY DOOR. REPLACED BATTERY PACK.
- [SDR 96UAL900178](https://openairdocs.org/sdr/96UAL900178.md): Auto Buss · malfunctioned · Mar 11, 1996 · N618UA · Boeing 767222 · AC Power Distribution System
  > RIGHT AC AUTO BUS TIE DID NOT PICK UP LOAD WHEN RIGHT GENERATOR TRIPPED. AT CRUISE TRIED TURNING OFF RIGHT BUS WITH APU GEN ON LINE. RIGHT BUS TIE BREAKER WOULD NOT PICK UP POWER FROM OTHER SOURCE WITH BTB SWITCH IN AUTO.
- [SDR 95UAL900103](https://openairdocs.org/sdr/95UAL900103.md): Eel Connector · inop · Aug 21, 1995 · N618UA · Boeing 767222 · Emergency Lighting
  > EMERGENCY EEL LIGHT INOP, RIGHT FWD AISLE. REPLACED POWER STRIP CONNECTOR, CHECKS NORMAL.

## 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 = 'N618UA' AND deregistration_id = 'N618UA-2007-07-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N618UA-2007-07-13/reports

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