# Service difficulty reports: N605TW, cancelled Jan 25, 2019

A list on [N605TW, cancelled Jan 25, 2019](https://openairdocs.org/deregistered/N605TW-2019-01-25.md).

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

- [SDR TWAA0104103](https://openairdocs.org/sdr/TWAA0104103.md): Power Supply · intermittent · Mar 3, 2001 · N605TW · Boeing 767231 · Emergency Lighting
  > THE EGRESS LIGHTS FLICKERED ON AND OFF IN THE B-ZONE, RT SIDE OF THE CABIN. REPLACED THE POWER SUPPLY. CHECK-C 12-23-00.
- [SDR TWAA0102702](https://openairdocs.org/sdr/TWAA0102702.md): Battery Pack · discharged · Feb 11, 2001 · N605TW · Boeing 767231 · Emergency Lighting
  > THE CABIN FLOOR EGRESS LIGHTS WERE INOPERATIVE ON THE RT SIDE FROM ROW 11 TO THE MID-CABIN LAVATORIES. REPLACED THE BATTERY PACK. CHECK-C 12-23-00 MCI.
- [SDR TWAA0017102](https://openairdocs.org/sdr/TWAA0017102.md): Battery Pack · discharged · Nov 2, 2000 · N605TW · Boeing 767231 · Emergency Lighting
  > THE LT SIDE OF CABIN AFT OF OVERWING SLIDE, THE AFT 3 EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 7-27-00 LAX.
- [SDR TWAA0012104](https://openairdocs.org/sdr/TWAA0012104.md): Skin · damaged · Jul 26, 2000 · N605TW · Boeing 767231 · Horizontal Stabilizer, Plate/Skin
  > DURING CHECK-C MAINT, CHECK FOUND ON LT HORIZONTAL STABILIZER LOWER SURFACE, 15 FEET FROM THE FUSELAGE AND 2 FEET FROM THE LEADING EDGE, AN OLD REPAIR HAD COME LOOSE. INSTALLED AN 8 INCH BY 9 INCH HOT BOND METAL DOUBLER PER SRM 55-10-01 AND 51-70-10. PRIMED
- [SDR TWAA0009102](https://openairdocs.org/sdr/TWAA0009102.md): Light · inoperative · Jun 11, 2000 · N605TW · Boeing 767231 · Emergency Lighting
  > THE LT OVERWING EXIT DOOR LIGHT WAS INOPERATIVE. FOUND GROUND WIRE PULLED AWAY FROM THE TERMINAL LUG. REPLACED THE TERMINAL LUG TO THE GROUND WIRE. CHECK-C 4-19-00 LAX.
- [SDR TWAA0007201](https://openairdocs.org/sdr/TWAA0007201.md): Light · worn · May 6, 2000 · N605TW · Boeing 767231 · Emergency Lighting
  > THE EGRESS LIGHTS WERE INOPERATIVE AT THE CENTER GALLEY AND ROWS 18 TO 20 ON RT SIDE OF CABIN. REPAIRED DRIVER CONNECTIONS. CHECK-C 5-16-00 LAX.
- [SDR TWAA0001209](https://openairdocs.org/sdr/TWAA0001209.md): Floorbeam · corroded · Jan 5, 2000 · N605TW · Boeing 767231 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINT, LATERIAL FLOORBEAM WAS EXTENSIVELY CORRODED AT WL 700, TOP OF FLOOR AND STA 266.5 AND RBL 11. INSTALLED A 4 IN BY 22 1/2 IN DOUBLER REPAIR PER SRM 51-70-11.
- [SDR TWAA9909802](https://openairdocs.org/sdr/TWAA9909802.md): Logic Card · worn · Jul 12, 1999 · N605TW · Boeing 767231 · Smoke Detection
  > EICAS MESSAGES FOR AFT CARGO COMPARTMENT SMOKE DETECTOR NUMBER 2 FLASHED CONTINUOUSLY AND NUMBER 1 DETECTOR FLASHED INTERMITTENTLY. MADE AN UNSCHEDULED LANDING AT JFK. ON THE GROUND THERE WERE NO MESSAGES. REPLACED THE LOGIC CARD (P/N 85N0028-136) AND THE N
- [SDR TWAA9909001](https://openairdocs.org/sdr/TWAA9909001.md): Battery Pack · discharged · Jun 27, 1999 · N605TW · Boeing 767231 · Emergency Lighting
  > FOUND THE RT OVERWING SLIDE LIGHT AND THE EMERGENCY LIGHT FORWARD OF THE RIGHT AFT CABIN DOOR WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 5-8-99 LAX.
- [SDR TWAA9907804](https://openairdocs.org/sdr/TWAA9907804.md): Skin · torn · May 7, 1999 · N605TW · Boeing 767231 · Leading Edge Devices
  > DURING OP 16 MAINT CHECK, FOUND NUMBER 5 LE SLAT INSIDE TE INBD OF OTBD TRACK, BOTTOM SKIN TORN 1 IN BY.5 INCH. INSTALLED 3 IN BY 2.5 IN FIBERGLASS WET LAY PER SRM 51-70-17 AND SRM 57-41-01 PAGE 204. SEALED AND PAINTED.
- [SDR TWAA9901402](https://openairdocs.org/sdr/TWAA9901402.md): Seal · damaged · Jan 22, 1999 · N605TW · Boeing 767231 · Leading Edge Devices
  > DURING CHECK-C, FOUND THE INBD END OF THE NR 2 LE SLAT, LOWER AFT SEAL, REPAIR DELAMINATING ON UPPER SIDE. BONDED SURFACES WITH 150 DEGREE CURE RESIN PER SRM 51-70-06, FIG 11.
- [SDR TWAA9901711](https://openairdocs.org/sdr/TWAA9901711.md): Skin · damaged · Jan 20, 1999 · N605TW · Boeing 767231 · Trailing Edge Flaps
  > DURING CHECK-C MAINT, THE RT WING O/B TRAILING EDGE FLAP, BOTTOM SIDE HAD A 4.25 INCH BY 4.5 INCH REPAIR PULLED LOOSE, 14 INCHES FROM I/B END OF FLAP 30 INCHES FROM TRAILING EDGE. REPAIRED TRAILING EDGE FLAP WITH METAL TO METAL 5.5 INCH CIRCULAR PATCH. HOT B
- [SDR TWAA9901603](https://openairdocs.org/sdr/TWAA9901603.md): Skin · damaged · Jan 20, 1999 · N605TW · Boeing 767231 · Leading Edge Devices
  > DURING CHECK-C MAINT, ON LT WING THE NR 1 LE SLAT LOWER SURFACE, O/B END HAD HOLE. INSTALLED 2 INCH BY 2 IN METAL TO METAL HOT BOND PER SRM 51-70-10.
- [SDR TWAA9812502](https://openairdocs.org/sdr/TWAA9812502.md): Skin · delaminated · Jul 28, 1998 · N605TW · Boeing 767231 · Wing, Plate/Skin
  > DURING CHECK-C MAINT, FOUND DELAMINATION ON LT WING UPPER LE 2.5 FEET BEHIND NR 6 LE SLAT, OTBD END, 5 INCHES LONG. REPAIRED SURFACE WITH A 3 IN BY 5 IN HOT BOND REPAIR PER SRM 51-70-08, PG 6 THRU 32.
- [SDR TWAA9812114](https://openairdocs.org/sdr/TWAA9812114.md): Strap · cracked · Jul 19, 1998 · N605TW · Boeing 767231 · Fuselage Miscellaneous Structure
  > STRAP CRACKED AND TORN AT RIVET HOLES STA 456, BETWEEN S35 AND S36. REPAIRED PER ARA 11576.
- [SDR TWAA9812113](https://openairdocs.org/sdr/TWAA9812113.md): Splice · cracked · Jul 19, 1998 · N605TW · Boeing 767231 · Fuselage Miscellaneous Structure
  > DURING DAMAGE REPAIRS FOUND SPLICE PLATE CRACKED AT RIVET HOLE TO MATERIAL EDGE AT STA 434, STR 36. REPAIRED PER ARA 11576.
- [SDR TWAA9812112](https://openairdocs.org/sdr/TWAA9812112.md): Stringer · corroded · Jul 19, 1998 · N605TW · Boeing 767231 · Fuselage Main, Longeron/Stringer
  > FOUND DURING DAMAGE REPAIRS STRINGER 33L HAD CORROSION AT STA 448. REPAIRED PER SRM 53-00-03 DETAIL III. CHECK-C 4-20-98 LAX.
- [SDR TWAA9812111](https://openairdocs.org/sdr/TWAA9812111.md): Stringer · corroded · Jul 19, 1998 · N605TW · Boeing 767231 · Fuselage Main, Longeron/Stringer
  > DURING WORK ON A DAMAGE INCIDENT FOUND STRINGER 34L WITH SURFACE CORROSION AT STA 460, JUST FWD OF FORMER. REPAIRED PER SRM 53-00-03, DETAIL III. CHECK-C 4-20-98 LAX.
- [SDR TWAA9812110](https://openairdocs.org/sdr/TWAA9812110.md): Stringer · cracked · Jul 19, 1998 · N605TW · Boeing 767231 · Fuselage Main, Longeron/Stringer
  > DUE TO A DAMAGE INCIDENT STRINGER 36L SPLICE AREA CRACKED AT STA 434. REPAIRED PER 767 SRM 53-00-03 DETAIL III.
- [SDR TWAA9812109](https://openairdocs.org/sdr/TWAA9812109.md): Skin · dented · Jul 19, 1998 · N605TW · Boeing 767231 · Fuselage Main, Plate/Skin
  > DUE TO A DAMAGE INCIDENT FOUND 14 IN BY 1 IN DEEP DENT ON FUSELAGE SKIN, STA 430 TO 440, LOCATED BETWEEN STR 35L AND 37L. REPAIRED PER ARA 11576.
- [SDR TWAA9812108](https://openairdocs.org/sdr/TWAA9812108.md): Stringer · bent · Jul 19, 1998 · N605TW · Boeing 767231 · Fuselage Main, Longeron/Stringer
  > DUE TO A DAMAGE INCIDENT STR 37L WAS BENT AND TWISTED AND RIVETS POPPED. CENTER STRAP TWISTED BETWEEN STA 429 AND 456. REPAIRED PER 767 SRM 53-00-03, DETAIL III, AND ARA 11576.
- [SDR TWAA9812107](https://openairdocs.org/sdr/TWAA9812107.md): Stringer · cracked · Jul 19, 1998 · N605TW · Boeing 767231 · Fuselage Main, Longeron/Stringer
  > DUE TO A DAMAGE INCIDENT STR 35L WAS CRACKED AT STA 456. REPAIRED PER 767 SRM 53-00-03, DETAIL III.
- [SDR TWAA9812106](https://openairdocs.org/sdr/TWAA9812106.md): Stringer · cracked · Jul 19, 1998 · N605TW · Boeing 767231 · Fuselage Main, Longeron/Stringer
  > DUE TO A DAMAGE INCIDENT STR 36L WAS CRACKED AT STA 456. REPAIRED PER 767 SRM 53-00-03 DETAIL III.
- [SDR TWAA9812105](https://openairdocs.org/sdr/TWAA9812105.md): Skin · dented · Jul 19, 1998 · N605TW · Boeing 767231 · Fuselage Main, Plate/Skin
  > DUE TO DAMAGE INCIDENT THE LT SIDE OF FUSELAGE WAS DENTED FROM STA 428 TO 470, STR 34L TO 37L, WITH A SKIN TEAR 14 IN BY 6 IN. REPAIRED PER ARA 11576. CHECK-C 4-20-98 LAX.
- [SDR TWAA9806004](https://openairdocs.org/sdr/TWAA9806004.md): Skin · gouged · Apr 19, 1998 · N605TW · Boeing 767231 · Elevator, Plate/Skin
  > LAX - DURING C-CHECK, FOUND THE LEFT OUTBOARD HORIZONTAL STABILIZER ELEVATOR WITH A 6 INCH GOUGE AT TOP TRAILING EDGE, APPROX 4.5 FT FROM INBOARD TE APPROX.0625 IN DEEP. FILLED GOUGE WITH FILLER 934NA AND HOT BONDED AND PAINTED PER SRM 55-20-01. (M)
- [SDR TWAA9805908](https://openairdocs.org/sdr/TWAA9805908.md): Skin · delaminated · Apr 17, 1998 · N605TW · Boeing 767231 · Trailing Edge Flaps
  > LAX - DURING C-CHECK, MAINTENANCE FOUND ON RT WING THE NR 4 OUTBOARD TE FLAP, THE UNDERSIDE HAD A 1 INCH BY 4 INCH DELAMINATION TWO FEET FROM OUTBOARD END. MADE HOT BOND REPAIR PER SRM 51-70-05. (M)
- [SDR TWAA9804801](https://openairdocs.org/sdr/TWAA9804801.md): Inverter · worn · Mar 31, 1998 · N605TW · Boeing 767231 · AC Inverter
  > YQX - FLT 818 - BOTH FLIGHT MANAGEMENT COMPUTER SYSTEMS MALFUNCTIONED, STANDBY INSTRUCTIONS LIGHTING BECAME INOP, AND EICAS MESSAGE STANDBY INVERTER DISPLAYED. DIVERTED TO YQX. REPLACED THE STANDBY INVERTER AND K105. (M)
- [SDR TWAA9802602](https://openairdocs.org/sdr/TWAA9802602.md): Idg · failed · Feb 21, 1998 · N605TW · Boeing 767231 · AC Generator-Alternator
  > JFK - FLT 12 - THE RIGHT ENGINE GENERATOR FAILED. EICAS MESSAGE RT GEN OFF DISPLAYED. FLT RETURNED TO JFK. PLACARDED GEN INOP PER MEL. ON LAYOVER, THE RT IDG WAS REPLACED. (M)
- [SDR TWAA9804010](https://openairdocs.org/sdr/TWAA9804010.md): Skin · delaminated · Jan 22, 1998 · N605TW · Boeing 767231 · Leading Edge Devices
  > LAX - DURING C-CHECK MAINTENANCE, FOUND THE RT WING NR 8 LE SLAT REPAIR DELAMINATED AT INBOARD UPPER EDGE. INSTALLED HOT BOND REPAIR PER SRM 51-70-10 PAGE 23. (M)
- [SDR TWAA9713704](https://openairdocs.org/sdr/TWAA9713704.md): Light · inoperative · Nov 24, 1997 · N605TW · Boeing 767231 · Emergency Lighting
  > JFK - FLT 22 - GROUND MAINTENANCE CHECK EMERGENCY EGRESS LIGHTING INOP. FOUND MOISTURE IN LIGHT TRACK. DRIED SAME WITH ALCOHOL. (M)
- [SDR TWAA9770002](https://openairdocs.org/sdr/TWAA9770002.md): Pump · worn · Jun 20, 1997 · N605TW · Boeing 767231 · Engine Oil Pressure
  > DURING CRUISE NUMBER 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. ENGINE WAS CHANGED. CHECK-C 4-3-97. *S/D* MAIN OIL PUMP ASSEMBLY WAS REPLACED.
- [SDR TWAA9771002](https://openairdocs.org/sdr/TWAA9771002.md): Engine · surged · Jun 20, 1997 · N605TW · Boeing 767231 · Engine (Turbine/Turboprop)
  > DTW - FLT 5046 - DURING CRUISE, LEFT ENGINE SURGED AT CONSTANT THRUST. CHECKED INLET AND EXHAUST, CHIP DETECTORS AND BLEED SCREENS. OPERATIONAL CHECK NORMAL. (M)
- [SDR TWAA9752001](https://openairdocs.org/sdr/TWAA9752001.md): Logic Card · failed · Apr 24, 1997 · N605TW · Boeing 767231 · Fire Detection
  > JFK - FLT 925 - DURING CRUISE, APU FIRE LIGHT ILLUMINATED; NO FIRE WAS PRESENT. REMOVED AND REPLACED LOGIC TEST CARD, MFG P/N 285N0028-36, MANUFACTURED BY THE BOEING COMPANY. FIRE CHECK C-2B - 2-5-97 - LAX. (X)
- [SDR TWAA9701001](https://openairdocs.org/sdr/TWAA9701001.md): Serving Cart · overheated · Jan 16, 1997 · N605TW · Boeing 767231 · Buffet/Galleys
  > STL - FLT 161 - DURING CRUISE SERVING CART, S/N 0074, OVERHEATED. DISCONNECTED SERVING CART. FOUND SHORTED HEATING PADS. REPLACED SERVING CART, MFG P/N 88801-1. SERVING CART OPERATION THEN CHECKED NORMAL. (M)
- [SDR 96ZZZM1177](https://openairdocs.org/sdr/96ZZZM1177.md): Fuel Control · out of adjust · Jul 1, 1996 · N605TW · Boeing 767231 · Fuel Control/Turbine Engines
  > SJU - DURING CRUISE NR 1 ENGINE, S/N 4623, EXPERIENCED A POWER SURGE. ADJUSTED BETA RATE 1/4 TURN CLOCKWISE. ENGINE THEN CHECKED NORMAL. (M)
- [SDR 96ZZZM1030](https://openairdocs.org/sdr/96ZZZM1030.md): Bleed Control · out of adjust · May 10, 1996 · N605TW · Boeing 767231 · Compressor Bleed Control
  > CDG - DURING CRUISE, NR 1 ENGINE SURGED AT CONSTANT THRUST. ENGINE PARAMETERS WERE NORMAL AFTER THE SURGE. CHECKED ENGINE INLET, EXHAUST, 3.5 BLEED VALVE SCREENS AND OIL MAGNETIC CHIP DETECTORS. ALL CHECKS WERE NORMAL. ADJUSTED ENGINE VANE BLEED CONTROL.
- [SDR 96ZZZM915](https://openairdocs.org/sdr/96ZZZM915.md): Bleed Control · malfunctioned · Apr 25, 1996 · N605TW · Boeing 767231 · Compressor Bleed Control
  > JFK - FLT 31 - AT TOP OF CLIMB, NR 1 ENGINE ENCOUNTERED POWER SURGE. REDUCED POWER AND REAPPLIED POWER. FOUND ENGINE VANE BLEED CONTROL, MFG P/N 766555-7, MALFUNCTIONING. CHANGED ENGINE VANE BLEED CONTROL AND ENGINE OPERATION CHECKED NORMAL.
- [SDR 95ZZZM528](https://openairdocs.org/sdr/95ZZZM528.md): Serving Cart · failed · Aug 22, 1995 · N605TW · Boeing 767231 · Buffet/Galleys
  > JFK - DURING CRUISE AFT GALLEY SERVING CART NR 4, EMITTED SMOKE AND ELECTRICAL ODOR. TURNED OFF AND DISCONNECTED CART, MFG P/N 88801-1. FOUND MALFUNCTIONING HEATING PLATES. REPLACED SERVING CART AND OPERATION CHECKED NORMAL.
- [SDR 95ZZZM449](https://openairdocs.org/sdr/95ZZZM449.md): Serving Cart · smoking · Aug 22, 1995 · N605TW · Boeing 767231 · Buffet/Galleys
  > JFK - FLT NR 740 - DURING CRUISE AFT GALLEY SERVING CART NR 4, EMITTED SMOKE AND ELECTRICAL ODOR. TURNED OFF AND DISCONNECTED CART, MFG P/N 88801-1. FOUND MALFUNCTIONING HEATING PLATES. REPLACED SERVING CART AND OPERATION CHECKED NORMAL.
- [SDR 95ZZZM297](https://openairdocs.org/sdr/95ZZZM297.md): Eec · out of adjust · Jul 18, 1995 · N605TW · Boeing 767231 · Fuel Controlling System
  > DURING HOLDING PATTERN RIGHT ENGINE DID NOT RESPOND TO THROTTLE AND ENGINE ROLLED BACK TO IDLE. TURNED OFF EEC. CHECKED ENGINE OPERATION AND ADJUSTED ENGINE IDLE. ENGINE OPERATION CHECKED 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 = 'N605TW' AND deregistration_id = 'N605TW-2019-01-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N605TW-2019-01-25/reports

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