# Service difficulty reports: N266US, cancelled Sep 26, 2013

A list on [N266US, cancelled Sep 26, 2013](https://openairdocs.org/deregistered/N266US-2013-09-26.md).

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

- [SDR 2002F00644](https://openairdocs.org/sdr/2002F00644.md): Regulator · malfunctioned · Apr 12, 2002 · N266US · Boeing 727251 · AC Regulator
  > DURING CLIMB-OUT OF PHL, GEN 1 BTB, GB AND FIELD LIGHTS ILLUMINATED FOLLOWED ABNORMAL PROCEDURES DUMPED 22,000 LBS RETURNED TO AIRPORT ONE GENERATOR ALREADY ON DMI SWAPPED RN 1 AND NR 2 VOLTAGE REGULATOR. OPS CHECK GOOD PER MM 24-20. AIRCRAFT RETURNED TO SER
- [SDR 2002F00400](https://openairdocs.org/sdr/2002F00400.md): Window · cracked · Mar 27, 2002 · N266US · Boeing 727251 · Flight Compartment Windows
  > R2 WINDOW OUTER PANEL CRACKED A/C DIVERTED TO KMIA FROM KMCO EN ROUTE TO CCS. REMOVED AND REPLACED R2 WINDOW PER MM 56-12-11 A/C RETURNED TO SERVICE. (M)
- [SDR 2002F00403](https://openairdocs.org/sdr/2002F00403.md): Inverter · malfunctioned · Mar 22, 2002 · N266US · Boeing 727251 · Attitude Gyro and Indicating System
  > ON PUSHBACK, POWER FLAG ON STANDBY ATTITUDE INDICTOR RERACKED STATIC INVERTER AND CLEANED CONNECTOR. OPS CHECKED NORMAL PER MM 34-25. A/C RETURNED TO SERVICE. (M)
- [SDR 2002F00026](https://openairdocs.org/sdr/2002F00026.md): Control Box · faulty · Nov 23, 2001 · N266US · Boeing 727251 · Central Warning
  > DURING TAXIING SPEED BRAKE/FLAP WARNING TEST FAILED A/C RETURNED TO GATE AURAL WARNING BOX WAS REPLACED PER MM 31-26. AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR FX72001F00001](https://openairdocs.org/sdr/FX72001F00001.md): Pin · loose · Jul 26, 2001 · N266US · Boeing 727251 · Nose/Tail Landing Gear Strut/Axle
  > UPON LANDING INC CCS, NOSE GEAR SCISSOR LINK CAME LOOSE. RECONNECTED PIN AND CONTINUE TO THE RAMP. PRECAUTIONARY REPLACED NLG APEX PIN RETURNED AIRCRAFT TO SERVICE.
- [SDR 20010214SG001](https://openairdocs.org/sdr/20010214SG001.md): Mount Bracket · broken · Dec 31, 2000 · N266US · Boeing 727251 · Leading Edge Slat Actuator
  > ON TAKEOFF FROM CAE SLAT INDICATION SHOWED RIGHT WING NR 3 SLAT EXTENDED. FLIGHT CREW RECYCLED THE FLAP SYSTEM AND SLAT REMAINED EXTENDED. CREW REPORTED HEARING A NOISE AND THEN LOSS OF THE ''''A'''' HYDRAULIC SYSTEM PRESSURE AND QT. THE CREW CONDUCTED A AI
- [SDR S84A2000001](https://openairdocs.org/sdr/S84A2000001.md): Light · inoperative · Jan 2, 2000 · N266US · Boeing 727251 · Emergency Lighting
  > MBJ - FLT 302 - R1 DOOR O/H EMERGENCY LIGHT INOPERABLE. RESECURED OPS CHECK IAW 33-50-01. OPS CHECK GOOD. (X)
- [SDR 99ZZZX4172](https://openairdocs.org/sdr/99ZZZX4172.md): Bracket · corroded · Oct 8, 1999 · N266US · Boeing 727251 · Emergency Equipment
  > DURING A C-CHECK, CORROSION WAS NOTED ON GIRT BAR BASES NR 1 GALLEY.
- [SDR 99ZZZX4169](https://openairdocs.org/sdr/99ZZZX4169.md): Pin · corroded · Oct 6, 1999 · N266US · Boeing 727251 · Landing Gear Retraction/Extension System
  > DURING A C-CHECK, CORROSION WAS NOTED ON LEFT MAIN LANDING GEAR LOWER TORSION LINK PIN RETAINING PIN.
- [SDR 99ZZZX4168](https://openairdocs.org/sdr/99ZZZX4168.md): Floorbeam · corroded · Oct 6, 1999 · N266US · Boeing 727251 · Fuselage Main, Floor Beam
  > DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM UPPER T-CHORD LBL 24 AT STA 344.
- [SDR 99ZZZX3957](https://openairdocs.org/sdr/99ZZZX3957.md): Seat Track · corroded · Sep 27, 1999 · N266US · Boeing 727251 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C-CHECK, CORROSION WAS NOTED AT FS 344 - FS 380 (RT) SEAT TRACK.
- [SDR 99ZZZX3956](https://openairdocs.org/sdr/99ZZZX3956.md): Channel · corroded · Sep 27, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON RT AFT LAVATORY WALL HAT CHANNEL AND ATTACH ANGLES.
- [SDR 99ZZZX3955](https://openairdocs.org/sdr/99ZZZX3955.md): Angle · corroded · Sep 27, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON RT AFT LAVATORY WALL HAT CHANNEL AND ATTACH ANGLES.
- [SDR 99ZZZX3954](https://openairdocs.org/sdr/99ZZZX3954.md): Channel · corroded · Sep 27, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED LT AFT LAVATORY FORWARD WALL HAT CHANNEL AND SUPPORT ANGLES.
- [SDR 99ZZZX3953](https://openairdocs.org/sdr/99ZZZX3953.md): Angle · corroded · Sep 27, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED LT AFT LAVATORY FORWARD WALL HAT CHANNEL AND SUPPORT ANGLES.
- [SDR 99ZZZX3952](https://openairdocs.org/sdr/99ZZZX3952.md): Floor Pan · corroded · Sep 27, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON FLOOR PAN, RT AFT LAVATORY.
- [SDR 99ZZZX3951](https://openairdocs.org/sdr/99ZZZX3951.md): Angle · corroded · Sep 27, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON T-ANGLE STA 812 KEEL BEAM.
- [SDR 99ZZZX3950](https://openairdocs.org/sdr/99ZZZX3950.md): Web · corroded · Sep 27, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON KEEL BEAM WEB STA 770.
- [SDR 99ZZZX3948](https://openairdocs.org/sdr/99ZZZX3948.md): Tie · corroded · Sep 27, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON TENSION TIES FS 1183 - 29R AND 23L.
- [SDR 99ZZZX3949](https://openairdocs.org/sdr/99ZZZX3949.md): Tie · corroded · Sep 18, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON TENSION TIE STR 17 FS 1183.
- [SDR 99ZZZX2917](https://openairdocs.org/sdr/99ZZZX2917.md): Frame · corroded · Jun 18, 1999 · N266US · Boeing 727251 · Fuselage Main, Frame
  > DURING A C-CHECK, CORROSION WAS NOTED ON FRAME AT BS 1166 OUTBOARD OF MOP SILL AT FLOOR LEVEL.
- [SDR 99ZZZX2916](https://openairdocs.org/sdr/99ZZZX2916.md): Channel · corroded · Jun 18, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON FORWARD LAVATORY HAT CHANNEL.
- [SDR 99ZZZX2915](https://openairdocs.org/sdr/99ZZZX2915.md): Floorbeam · corroded · Jun 18, 1999 · N266US · Boeing 727251 · Fuselage Main, Floor Beam
  > DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM FS 344, LBL 24 OUTBOARD.
- [SDR 99ZZZX2914](https://openairdocs.org/sdr/99ZZZX2914.md): Web · corroded · Jun 18, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON SHEAR WEB UNDER BS 1176 CHORD LBL 25 - RBL 25.
- [SDR 99ZZZX2913](https://openairdocs.org/sdr/99ZZZX2913.md): Seat Track · corroded · Jun 18, 1999 · N266US · Boeing 727251 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK RT CENTER BS 344 - BS 460. (ALSO ON LT INBOARD).
- [SDR 99ZZZX2912](https://openairdocs.org/sdr/99ZZZX2912.md): Seat Track · corroded · Jun 18, 1999 · N266US · Boeing 727251 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK BS 1070- BS 1130 LBL 48 AND LBL 25.
- [SDR 99ZZZX2228](https://openairdocs.org/sdr/99ZZZX2228.md): Skin · corroded · May 12, 1999 · N266US · Boeing 727251 · Fuselage Main, Plate/Skin
  > DURING A C-CHECK, CORROSION WAS NOTED ON EXTERIOR AFT FUSELAGE LAMP SEAM FS 1283 - FS 1343 BELOW NR 1 ENGINE PYLON.
- [SDR 99ZZZX2227](https://openairdocs.org/sdr/99ZZZX2227.md): Angle · corroded · May 12, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED IN RADOME AREA FS 178 LOWER MOST Z-ANGLE LBL 18 TO RBL 18.
- [SDR 99ZZZX2226](https://openairdocs.org/sdr/99ZZZX2226.md): Beam · corroded · May 12, 1999 · N266US · Boeing 727251 · Horizontal Stabilizer Structure
  > DURING A C-CHECK, COROSION WAS NOTED ON RT HORIZONTAL STABILIZER, UPPER TRAILING EDGE BEAM.
- [SDR 99ZZZX2225](https://openairdocs.org/sdr/99ZZZX2225.md): Skin · corroded · May 12, 1999 · N266US · Boeing 727251 · Trailing Edge Flaps
  > DURING A C-CHECK, CORROSION WAS NOTED ON UPPER SURFACE AFT EDGE OF RT INBOARD AFT FLAP (ABOVE NR 5 CANOE).
- [SDR 99ZZZX2224](https://openairdocs.org/sdr/99ZZZX2224.md): Beam · corroded · May 12, 1999 · N266US · Boeing 727251 · Horizontal Stabilizer Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON THE LEFT HORIZ STABILIZER, LOWER T/E BEAM BETWEEN NR 5 AND NR 6 ELEVATOR HINGES.
- [SDR 99ZZZX2223](https://openairdocs.org/sdr/99ZZZX2223.md): Beam · corroded · May 12, 1999 · N266US · Boeing 727251 · Horizontal Stabilizer Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM ABOVE NR 7 ELEVATOR HINGE.
- [SDR 99ZZZX2459](https://openairdocs.org/sdr/99ZZZX2459.md): Door · corroded · May 1, 1999 · N266US · Boeing 727251 · Fixed Inner Doors
  > DURING A C-CHECK, CORROSION WAS NOTED ON AFT LAVATORY SERVICE DOOR.
- [SDR 99ZZZX1750](https://openairdocs.org/sdr/99ZZZX1750.md): Angle · corroded · Apr 12, 1999 · N266US · Boeing 727251 · APU Cowling/Containment
  > DURING A C-CHECK, CORROSION WAS NOTED ON APU AIR INLET SCREEN MOUNT FLANGE (ANGLES).
- [SDR 99ZZZX1749](https://openairdocs.org/sdr/99ZZZX1749.md): Hinge · corroded · Apr 12, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON UPPER/LOWER HINGES ON AFT LAVATORY SERVICE DOOR.
- [SDR 99ZZZX1748](https://openairdocs.org/sdr/99ZZZX1748.md): Hinge · corroded · Apr 12, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON UPPER/LOWER HINGES ON AFT LAVATORY SERVICE DOOR.
- [SDR 99ZZZX1747](https://openairdocs.org/sdr/99ZZZX1747.md): Hinge · corroded · Apr 12, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON UPPER/LOWER HINGES ON AFT LAVATORY SERVICE DOOR.
- [SDR 99ZZZX1746](https://openairdocs.org/sdr/99ZZZX1746.md): Hinge · corroded · Apr 12, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON UPPER/LOWER HINGES ON AFT LAVATORY SERVICE DOOR.
- [SDR 98ZZZM296](https://openairdocs.org/sdr/98ZZZM296.md): Pressurization · malfunctioned · Feb 6, 1998 · N266US · Boeing 727251 · Cabin Pressure Control System
  > FLT 758 - DURING CLIMB-OUT, LOST PRESSURIZATION, AFTER DUMPING FUEL RETURNED TO KMIA, LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED FOR OPEN DOORS AND COMPARTMENTS, NONE FOUND, DOOR SEAL INSPECTED FOUND NORMAL. ACCOMPLISHED GROUND PRESSURIZATION CHECK, NOR
- [SDR 97ZZZM573](https://openairdocs.org/sdr/97ZZZM573.md): Bracket · failed · Apr 7, 1997 · N266US · Boeing 727251 · Landing Gear Door Retract Section
  > MDSD - AT PUSHBACK FROM GATE, FOUND THE NOSE LANDING DOOR OPERATIONAL BRACKET BROKEN. INSPECTED DOOR OPERATIONAL ASSEMBLY AND AREA, FOUND NO ADDITIONAL DAMAGE. REPLACED DOOR OPERATOR BRACKET, RETURNED AIRCRAFT TO SERVICE. (M)
- [SDR 97ZZZM574](https://openairdocs.org/sdr/97ZZZM574.md): Outflow Valve · jammed · Apr 5, 1997 · N266US · Boeing 727251 · Pressure Regulator/Outflow Valve
  > FRY KBWI-KMIA - FLT F429 - DURING CLIMB STAGE LOST PARTIAL PRESSURIZATION. DESCENDED TO A LOWER ALTITUDE AND WERE ABLE TO HOLD PRESSURIZATION, LANDING UNEVENTFUL. INSPECTED AIRCRAFT FOR ABNORMAL CONDITIONS, FOUND ONE INSULATION BLANKET, P/N (6567242475) STUC
- [SDR 97ZZZM273](https://openairdocs.org/sdr/97ZZZM273.md): Window · failed · Feb 10, 1997 · N266US · Boeing 727251 · Flight Compartment Windows
  > CAPTAIN'S SLIDING WINDOW (L2) ARCHING WITH WINDOW HEAT ON. NO ELECTRICAL FIRE, LANDING UNEVENTFUL. INSPECTED WINDOW AREA, NO EVIDENCE OF FIRE OR BURNING. REPLACED NR 2 LEFT SLIDING WINDOW. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR 96ZZZX3735](https://openairdocs.org/sdr/96ZZZX3735.md): Turbine · damaged · Jun 8, 1996 · N266US · Boeing 727251 · Turbine Section
  > KMIA - AFTER DEPARTURE DURING CLIMB STAGE, SEVERE VIBRATION ON NR 2 ENGINE. INITIATED EMERGENCY PROCDURES, SHUT DOWN NR 2 ENGINE, DUMPED FUEL AND RETURNED TO KMIA LANDING UNEVENTFULLY. FOUND NR 2 ENGINE TURBINE DAMAGED.
- [SDR 96ZZZX3734](https://openairdocs.org/sdr/96ZZZX3734.md): Connector · loose · Jun 3, 1996 · N266US · Boeing 727251 · Cabin Pressure Control System
  > KMIA - AFTER DEPARTURE DURING CLIMB STAGE, UNABLE TO OBTAIN CABIN PRESSURE. DUMPED FUEL AND RETURNED TO KMIA LANDING UNEVENTFULLY. FOUND LOOSE ELECTRICAL CONNECTOR AT THE PNEUMATIC FLOW CONTROL/SHUT-OFF VALVE, P/N 39608831. TIGHTENED THE CONNECTOR, OPERATIO

## 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 = 'N266US' AND deregistration_id = 'N266US-2013-09-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N266US-2013-09-26/reports

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