# Service difficulty reports: N211UP, cancelled Sep 26, 2003

A list on [N211UP, cancelled Sep 26, 2003](https://openairdocs.org/deregistered/N211UP-2003-09-26.md).

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

- [SDR UPS01237343](https://openairdocs.org/sdr/UPS01237343.md): Engine · failed · Nov 28, 2001 · N211UP · Boeing 727247 · Engine (Turbine/Turboprop)
  > INSPECTION TYPE:N/A NR 1 ENGINE FAILURE - NOSE COWL AND BULLET DAMAGED. RETURNED TO LAN. REMOVED AND REPLACED NR 1 ENGINE PER UPS TC 1201 S/N OFF P687435B, ON 6 87439.
- [SDR UPS01236969](https://openairdocs.org/sdr/UPS01236969.md): Light · inoperative · Sep 30, 2001 · N211UP · Boeing 727247 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ABOVE ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AS PER MM 35-50-101. OPS CHECKS GOOD.
- [SDR UPS01236727](https://openairdocs.org/sdr/UPS01236727.md): Smoke Detector · malfunctioned · Aug 28, 2001 · N211UP · Boeing 727247 · Smoke Detection
  > INSPECTION TYPE:IN MAIN CARGO SMOKE DETECTION SYSTEM (RT SIDE) WARNING LIGHT ILLUMINATED IN FLIGHT. AC DIVERTED TO IND. LIGHT EXTINGUISHED WHEN MAIN CARGO DOOR OPENED. NO EVIDENCE OF SMOKE FOUND. WHILE TESTING SYSTEMS, NR 3 SYSTEM RIGHT DETECTOR LIGHT STAYED I
- [SDR UPS01236817](https://openairdocs.org/sdr/UPS01236817.md): Shear Tie · corroded · Jun 19, 2001 · N211UP · Boeing 727247 · Fuselage Main, Structure
  > INSPECTION TYPE:C WHILE WORKING FUSELAGE, DISCOVERED SHEAR TIE CORRODED BS 970, RBL 8 OUTBOARD OF STR 29R. CORROSION FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-4.
- [SDR UPS01236153](https://openairdocs.org/sdr/UPS01236153.md): Shear Tie · corroded · Jun 19, 2001 · N211UP · Boeing 727247 · Fuselage Main, Structure
  > INSPECTION TYPE:C, WHILE WORKING FUSELAGE DISCOVERED SHEAR TIE CORRODED BS 970, RBL 8 OUTBOARD OF STR 29R. CORROSION FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-4.
- [SDR UPS01236816](https://openairdocs.org/sdr/UPS01236816.md): Sill · corroded · Jun 6, 2001 · N211UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C FOUND CORROSION ON AFT CARGO DOOR CUTOUT SILL CHORD AT BS 950E+19. REPAIRED CHORD IAW SRM 51-40-4, 53-10-1, 51-10-1, 51-30-2.
- [SDR UPS01236138](https://openairdocs.org/sdr/UPS01236138.md): Sill · corroded · Jun 6, 2001 · N211UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, FOUND CORROSION ON AFT CARGO DOOR CUTOUT LOWER SILL CHORD AT BS 950+19. REPAIRED CHORD IAW SRM 51-40-4, 53-10-1, 51-10-1, 51-30-2.
- [SDR UPS01236815](https://openairdocs.org/sdr/UPS01236815.md): Floorbeam · corroded · May 21, 2001 · N211UP · Boeing 727247 · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C WHILE WORKING FUSELAGE, DISCOVERED CORROSION ON BS 328 FLOORBEAM, LBL 18, WL 208. REMOVED CORROSION FROM THE FLOORBEAM UPPER CHORD. FLAP PEENED AREA. FABRICATED AND INSTALLED REPAIR PARTS. ALL WORK ACCOMPLISHED IAW ER 01-0537.
- [SDR UPS01236814](https://openairdocs.org/sdr/UPS01236814.md): Skin · corroded · May 15, 2001 · N211UP · Boeing 727247 · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C CORROSION ON CROWN SKIN B.S. 848 4" BELOW STR 7L BLENDED CORROSION AT B.S. 848 4" BELOW STR 7L IN AN AREA OF 1"X2" REMOVED.032" FROM ORIGINAL THICKNESS OF.090", FOUND TO BE OUT LIMITS IAW SRM 53-30-1 PG 1 - 2B REPAIRED AREA IAW SRM 53-3
- [SDR UPS01236022](https://openairdocs.org/sdr/UPS01236022.md): Skin · corroded · May 15, 2001 · N211UP · Boeing 727247 · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, CORROSION ON CROWN SKIN BS 848 4 INCHES BELOW STR 7L. BLENDED CORROSION AT BS 848 4 INCHES BELOW STR 7L IN AN AREA OF 1 X 2 INCHES. REMOVED.032 INCH FROM ORIGINAL THICKNESS OF.090 INCH FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 PG 1 2B.
- [SDR UPS00234258](https://openairdocs.org/sdr/UPS00234258.md): Smoke Detector · inoperative · Oct 26, 2000 · N211UP · Boeing 727247 · Smoke Detection
  > INSPECTION TYPE:N/A, MCD SMOKE DETECTOR NO TEST. RELAMPED SMOKE DETECTOR.
- [SDR UPS00233510](https://openairdocs.org/sdr/UPS00233510.md): Regulator · inoperative · Aug 3, 2000 · N211UP · Boeing 727247 · Crew Oxygen System
  > INSPECTION TYPE:N/A, CAPTS O2 REG INOP. *S/D* REMOVED AND REPLACED 02 REG.
- [SDR UPS99228620](https://openairdocs.org/sdr/UPS99228620.md): Fire Light · malfunctioned · Feb 3, 1999 · N211UP · Boeing 727247 · Fire Detection
  > INSPECTION TYPE-N/A, BLOCK TURN BACK DUE TO APU FIRE LIGHT ON INDICATION. PULLED THE SWITCH AND PRESS THE DISCHARGE BUTTON. DEFERRED APU PER MEL 49-1 AND DEFERRED FIRE WARNING SYSTEM PER MEL 26-11-0-2.
- [SDR UPS98226822](https://openairdocs.org/sdr/UPS98226822.md): Coalescer Bag · dirty · May 28, 1998 · N211UP · Boeing 727247 · Humidity Control System
  > CREW REPORTED STRONG FUMES IN COCKPIT SHUT DOWN PAX INFLIGHT, PREVIOUS WRITE-UP SDF, MX DEFERED APU M 152622. SUBMITTER STATES, SUSPECT FUEL FUMES, VAPORS IN COALESTER BAGS AOG NEW BAGS AND O-RINGS FOR T-FITTING FOR SOLENOID VALVE. REPLACED BAGS AND O-RINGS
- [SDR UPS98226588](https://openairdocs.org/sdr/UPS98226588.md): Skin · cracked · May 6, 1998 · N211UP · Boeing 727247 · Leading Edge Devices
  > INSPECTION TYPE-SI, NR 2 SLAT LOWER SKIN FASTENERS SHEARED AND CRACK EMITTING FROM FASTENER HOLE JUST BELOW UPSTOP (I/B). REMOVED AND REPLACED NR 2 SLAT IAW MM 27-81-11.
- [SDR UPS98226518](https://openairdocs.org/sdr/UPS98226518.md): Fitting · corrosion · Apr 29, 1998 · N211UP · Boeing 727247 · Trailing Edge Flaps
  > INSPECTION TYPE:SI CORROSION (C57-581-06.00-03) NR 1 FORWARD TRACK FITTING ON ONE LUG FACE AND THE LARGE FASTENER ATTACH HOLES. REMOVED FITTING, REWORKED PER ER NR98-2405, REINSTALLED SERVICABLE FITTING.
- [SDR UPS98226517](https://openairdocs.org/sdr/UPS98226517.md): Skin · corrosion · Apr 29, 1998 · N211UP · Boeing 727247 · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SI CORROSION (C53-224-05.00-01) ON UPPER SKIN OF FUEL CELL BS 823 LBL 34 WL 196. REMOVED CORROSION BLENDED AND REFINISHED PER ER NR 98-2375.
- [SDR UPS98226479](https://openairdocs.org/sdr/UPS98226479.md): Shear Tie · corrosion · Apr 23, 1998 · N211UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-SI, CORROSION (C53-111-01.00-02) FWD CARGO BAY SHEAR TIE AT BS 660 AT STR 26 RT ON FWD FACE. CORROSION OUT OF LIMITS. REMOVED SHEAR TIE AND INSTALLED NEW SHEAR TIE IAW SRM 51-30-2.
- [SDR UPS98226481](https://openairdocs.org/sdr/UPS98226481.md): Track · corrosion · Apr 22, 1998 · N211UP · Boeing 727247 · Trailing Edge Flaps
  > INSPECTION TYPE-SI, CORROSION (C57-581-06.00-03) NR 1 FLAP TRACK FWD LUG INTERFACE. FLAP TRACK REMOVED, REPAIRED AND RETURNED TO SERVICEABLE CONDITION AT MACHINE SHOP TO BE INSTALLED ON TC NR C57-581-04-3D.
- [SDR UPS98226480](https://openairdocs.org/sdr/UPS98226480.md): Track · corrosion · Apr 22, 1998 · N211UP · Boeing 727247 · Trailing Edge Flaps
  > INSPECTION TYPE-SI, CORROSION (C57-581-06.00-03) IN NR 2 FLAP TRACK CENTER MOUNT HOLE. FLAP TRACK REMOVED, REPAIRED AND RETURNED TO SERVICEABLE CONDITION BY NEWELL CORP JOB NR 11804 TRACK TO BE INSTALLED ON TC NR C57-581-04-3D.
- [SDR UPS98226482](https://openairdocs.org/sdr/UPS98226482.md): Skin · corrosion · Apr 21, 1998 · N211UP · Boeing 727247 · Fuselage Main, Plate/Skin
  > INSPECTION TYPE-SI, CORROSION (6-53-20) AT ANTENNA CUT OUT BOTTOM OF FUSELAGE 20 AFT OF E-BAY DOOR, BS 470 WL 138.5 BL 0. REMOVED CORROSION, FABRICATED DOUBLER AND INSTALLED IAW SRM 53-30-1, 51-10-6, 53-30-3, 51-30-5.
- [SDR UPS98226520](https://openairdocs.org/sdr/UPS98226520.md): Clip · corroded · Apr 20, 1998 · N211UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SI CORROSION (C53-224-01.00-01) ON FRAME AND STRINGER CLIPS AT STA 720B STR CLIPS 5-8 RT FRAME AT STR 2-10 RT STR CLIPS 4-9 LT CORROSION ON STRINGER CLIPS AT BS 720B STR 5 AND 6 RIGHT, 9 RIGHT AND STR 5 AND 6 LEFT WERE FOUND OUT OF LIMITS P
- [SDR UPS98226521](https://openairdocs.org/sdr/UPS98226521.md): Floorbeam · corroded · Apr 13, 1998 · N211UP · Boeing 727247 · Fuselage Main, Floor Beam
  > INSPECTION TYPE:SI CORROSION (C53-111-01.00-02)FWD CARGO BAY BS 720 LOWER FLANGE OF FLOORBEAM IN AND AROUND NUT PLATE HOLES LBL 45 TO RBL 25 WL 200, A 2.2 BY.9 BY.125 AREA OF THE LOWER FLANGE AT LBL 16 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. A STANDA
- [SDR UPS98226519](https://openairdocs.org/sdr/UPS98226519.md): Seat Track · corroded · Apr 13, 1998 · N211UP · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:SI MAIN DECK SEAT TRACK BS 520-683 RBL 45 WL 208 HAS CORROSION ON FLANGE AND IN WELL AREA, AS MARKED. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. NEW SEAT TRACK FABRICATED PER SRM 53-10-5 AND INSTALLED PER SRM 51-10-2.
- [SDR UPS97221872](https://openairdocs.org/sdr/UPS97221872.md): E1 Rack · water contam · Jan 28, 1997 · N211UP · Boeing 727247 · Electrical Power System
  > ON FINAL APPROACH, FLAPS WERE SELECTED TO 2 DEGREES. ALL POWER TO AIRCRAFT WAS LOST EXCEPT CAPTAIN'S INSTRUMENTS. ALL LIGHTS DIMMED AND NO INDICATION ON ENGINEER'S PANEL (PANEL WAS DARK) AFTER A PACK WAS DOWNLOADED. POWER CAME BACK ON. NR 1 AND NR 2 BUS. F
- [SDR UPS96221300](https://openairdocs.org/sdr/UPS96221300.md): Shear Tie · corroded · Oct 7, 1996 · N211UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C. CORROSION ON SHEAR TIE AT BS 1130 RBL 10 WL 149. REMOVED CORROSION FROM SHEAR TIE AT STA 1130 RBL 10 WL 149. REWORK DEEMED OUT OF LIMITS IAW 53-10-1. REPAIRED SHEAR TIE IAW SRM 53-10-4.
- [SDR UPS96221299](https://openairdocs.org/sdr/UPS96221299.md): Skin · delamination · Oct 7, 1996 · N211UP · Boeing 727247 · Trailing Edge Flaps
  > INSPECTION TYPE: C. RIGHT WING INBOARD FOREFLAP HAS AREA OF DELAMINATION ON LOWER SURFACE INBOARD TRAILING EDGE. REPAIRED PER SRM 51-40-06.
- [SDR UPS96221298](https://openairdocs.org/sdr/UPS96221298.md): Rib · cracked · Oct 7, 1996 · N211UP · Boeing 727247 · Trailing Edge Flaps
  > INSPECTION TYPE: C. RIGHT WING INBOARD MIDFLAP HAS CRACKED RIB AT CENTER FOREFLAP TRACK OUTBOARD RIB. REMOVED AND REPLACED CRACKED RIB IAW SRM 51-30-2, OHM 57-52-01 MM 27-51-00.
- [SDR UPS96221255](https://openairdocs.org/sdr/UPS96221255.md): Hat Section · corroded · Oct 3, 1996 · N211UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C. CORROSION AT BS 304 RBL 12 WL 207.5 AT HAT SECTION. REMOVED, FABRICATED FROM EXTRUSION STOCK, AND REPLACED FLOOR STRUCTURE HAT SECTION IAW SRM'S 51-30-2, 51-20-4, 51-10-6, 51-10-2.
- [SDR UPS96221248](https://openairdocs.org/sdr/UPS96221248.md): Skin · disbond · Oct 3, 1996 · N211UP · Boeing 727247 · Trailing Edge Flaps
  > INSPECTION TYPE: C. RIGHT WING INBOARD FOREFLAP 65 FROM INBOARD END UPPER SURFACE HAS SMALL DISBOND. REPAIRED DISBOND ON RT WING INBOARD FOREFLAP IAW SRM 51-40-6.
- [SDR UPS96221247](https://openairdocs.org/sdr/UPS96221247.md): Skin · disbond · Oct 3, 1996 · N211UP · Boeing 727247 · Trailing Edge Flaps
  > INSPECTION TYPE-C, RIGHT WING I/B FOREFLAP 10 INCHES FROM I/B END UPPER SURFACE HAS AREA OF DISBOND. REPAIRED DISBONDS, 10 INCHES FROM I/B END AND AT 39 INCHES FROM I/B END IAW SRM 51-40-6.
- [SDR UPS96221257](https://openairdocs.org/sdr/UPS96221257.md): Web · corroded · Oct 2, 1996 · N211UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C. CORROSION ON WEB STA 575-580 RBL 22 WL 152. MECH REMOVED CORROSION, REWORK DEEMED OUT OF LIMITS IAW SRM'S 53-20-1 51-30-2, 51-10-2 AND MM 51-20-151.
- [SDR UPS96221256](https://openairdocs.org/sdr/UPS96221256.md): Channel · corroded · Oct 2, 1996 · N211UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C. CORROSION AT BS 302 LBL 12-RBL 12 WL 207.5 AT NUTPLATES IN U-CHANNEL. REMOVED, FABRICATED, AND REPLACED FLOOR STRUCTURE U-CHANNEL IAW SRM'S 51030-3, 51-30-8, 51-20-4, AND 51-10-6, 51-10-2.
- [SDR UPS96221258](https://openairdocs.org/sdr/UPS96221258.md): Frame · corroded · Oct 1, 1996 · N211UP · Boeing 727247 · Fuselage Main, Frame
  > INSPECTION TYPE: C. CORROSION ON LOWER FLANGE OF FRAME STA 720A WL 149 RBL 7-10. CUT OUT DAMAGED SECTION AND ACCOMPLISHED REPAIR IAW SRM 53-10-4.
- [SDR UPS96221254](https://openairdocs.org/sdr/UPS96221254.md): Angle · corroded · Sep 30, 1996 · N211UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C. CORROSION ON SUPPORT ANGLE STA 610-613 RBL 13 WL 158. REMOVED, FABRICATED AND REPLACED ANGLE IAW SRM'S 51-30-2, 53-10-2 AND MM 57-20-31.
- [SDR UPS96221253](https://openairdocs.org/sdr/UPS96221253.md): Splice · corroded · Sep 30, 1996 · N211UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C. CORROSION ON STR 27R SPLICE STA 675-685 AREA MARKED. REMOVED, FABRICATED FROM STOCK, AND REPLACED STRINGER SPLICE IAW SRM'S 51-10-1, 51-10-6, AND 51-10-5 AND 51-30-2.
- [SDR UPS96221252](https://openairdocs.org/sdr/UPS96221252.md): Splice · corroded · Sep 30, 1996 · N211UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C. CORROSION ON STR 28R SPLICE STA 675-685 WL 149. REMOVED, FABRICATED FROM STOCK, AND REPLACED STRINGER SPLICE IAW SRM'S 51-10-6, 51-10-1, 51-30-2, AND 51-10-5.
- [SDR UPS96221251](https://openairdocs.org/sdr/UPS96221251.md): Shear Tie · corroded · Sep 30, 1996 · N211UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C. CORROSION ON FRAME AROUND FASTENERS AT BS 950F RBL 3 WL 151. REMOVED CORROSION FROM FRAME AT STA 950F RBL 3 WL 151. REWORKED FRAME FOUND TO BE WITHIN LIMITS IAW SRM 53-10-1, HOWEVER, CORROSION WAS FOUND ON SHEAR TIE OUT OF LIMITS IAW SR
- [SDR UPS96221250](https://openairdocs.org/sdr/UPS96221250.md): Shear Tie · corroded · Sep 30, 1996 · N211UP · Boeing 727247 · Wing Miscellaneous Structure
  > INSPECTION TYPE: C. CORROSION ON SHEAR TIE STA 500 RBL 17-22 WL 150. MECH REMOVED CORROSION FROM SHEAR TIE AT STA 500 RBL 17-22 WL 150. REWORKED DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED SHEAR TIE IAW SRM 53-10-4.
- [SDR UPS96221249](https://openairdocs.org/sdr/UPS96221249.md): Rib · cracked · Sep 27, 1996 · N211UP · Boeing 727247 · Trailing Edge Flaps
  > INSPECTION TYPE: C. RT WING INBOARD MIDFLAP HAS CRACKED NOSE RIB IN L/E AT CENTER FOREFLAP TRACK INBOARD OF TRACK. REMOVED DAMAGED RIB, INSTALLED NEW RIB, ALL WORK DONE PER SRM'S 51-30-2 AND 51-30-5.
- [SDR UPS205161](https://openairdocs.org/sdr/UPS205161.md): Battery · discharged · Dec 26, 1995 · N211UP · Boeing 727247 · Emergency Lighting
  > MAINTENANCE FOUND CREW FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES. OPS CHECK GOOD.
- [SDR UPS201906](https://openairdocs.org/sdr/UPS201906.md): Eel Battery · discharged · Jan 4, 1995 · N211UP · Boeing 727247 · Emergency Lighting
  > MAINTENANCE REPORTED EMERGENCY EXIT LIGHT ON OVERHEAD ON ENTRY DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES. PERFORMED OPS CHECK. OP CHK GOOD ON GROUND.

## 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 = 'N211UP' AND deregistration_id = 'N211UP-2003-09-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N211UP-2003-09-26/reports

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