# Service difficulty reports: N954UP, cancelled Sep 2, 2008

A list on [N954UP, cancelled Sep 2, 2008](https://openairdocs.org/deregistered/N954UP-2008-09-02.md).

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

Page 1 of 5 · 219 reports

- [SDR UPS06247313](https://openairdocs.org/sdr/UPS06247313.md): Extinguisher · unserviceable · Jul 12, 2006 · N954UP · Boeing 727185C · Fire Bottle, Portable
  > MAIN PORTABLE FIRE EXTINGUISHER NEEDLE IS OUT OF GRN BAND. REMOVED AND REPLACED PORTABLE FIRE EXTINGUISHER BY LAV DOOR. OK FOR SERVICE.
- [SDR UPS06246858](https://openairdocs.org/sdr/UPS06246858.md): Stringer · corroded · May 6, 2006 · N954UP · Boeing 727185C · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER AT FRAME 540 RBL22 HAS CORROSION, PLS. REMOVE CORROSION AND CHECK WITHIN LIMITS. DAMAGED PART OF STR FOUND TO BE OUTSIDE LIMITS IAW SRM 53-10-1. DAMAGED STR REMOVED IAW SRM 51-40-4. NEW SPLICES FABRICATED IAW SRM 51-4 0-4. REPROTECTED NEW S
- [SDR UPS06246868](https://openairdocs.org/sdr/UPS06246868.md): Intercostal · cracked · May 5, 2006 · N954UP · Boeing 727185C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C&SI ON REMOVAL OF FRAME AT BS 540 INTERCOSTAL AT BS 520-540 IS CRACKED PLS. REPAIR/REPLACE AS REQUIRED. REMOVED CRACKED INTERCOSTAL AT BS 520-540 IAW SRM 51-30-2. FABRICATED INTERCOSTAL IAW SRM 51-20-1 FIG 7. INSTALLED INTERCOSTAL IAW SRM
- [SDR UPS06246867](https://openairdocs.org/sdr/UPS06246867.md): Skin · cracked · May 5, 2006 · N954UP · Boeing 727185C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C&SI ON REMOVAL OF FRAME AT BS 540 WEB SKIN AT 500-540 S18R HAS EVIDENCE OF MECHANICAL DAMAGE AND CRACKS. NEW WEB SKIN FABRICATED IAW SRM 51-20-01. NEW SKIN DRILLED OFF EXISTING HOLES IAW SRM 51-30-02 ALSO NUT PLATES INSTALLED AS REQ'D IAW SR
- [SDR UPS06246797](https://openairdocs.org/sdr/UPS06246797.md): Intercostal · cracked · May 2, 2006 · N954UP · Boeing 727185C · Fuselage Miscellaneous Structure
  > FOUND INTERCOSTAL CRACKED AT BS 272 RHS BELOW STR 23R. INTERCOSTAL REMOVED IAW SRM 51-30-02. FABRICATED INTERCOSTAL IAW SRM 51-20-01. INSTALLED INTERCOSTAL IAW SRM 51-30-02.
- [SDR UPS06246795](https://openairdocs.org/sdr/UPS06246795.md): Seat Track · cracked · May 2, 2006 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CABIN UPPER FLANGE AFT END CRACKED AT BS 850 LBL51 HAS SURFACE CORROSION SEAT TRACK REMOVED IAW SRM 51-30-02. NEW SEAT TRACK FABRICATED IAW SRM 53-10-02. INSTALLED NEW SEAT TRACK IAW SRM 51-30-02.
- [SDR UPS06246878](https://openairdocs.org/sdr/UPS06246878.md): Door Frame · cracked · Apr 28, 2006 · N954UP · Boeing 727185C · Fuselage Main, Structure
  > INSPECTION TYPE:C NDT CONFIRMED TWO CRACKS ON THE FWD FRAME OF THE FWD CARGO DOOR CUTOUT. REMOVED EXISTING REPAIR AND DOOR STOP IAW SRM 51-30-02. ANGLES BETWEEN STR 19R AND STR 24R REMOVED IAW SRM 51-30-02. FRAME WEB SKIN REMOVED IAW SRM 51-30-02. FRAME RE
- [SDR UPS06246796](https://openairdocs.org/sdr/UPS06246796.md): Stringer · corroded · Apr 28, 2006 · N954UP · Boeing 727185C · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STR 22R AT BS 460. CORROSION FOUND OUT OF LIMITS IAW SRM 51-10-01. REMOVED CORRODED STRINGER IAW SRM 53-10-3 REPAIRED STRINGER IAW SRM 53-10-03.
- [SDR UPS06246794](https://openairdocs.org/sdr/UPS06246794.md): Seat Track · corroded · Apr 28, 2006 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CABIN SEAT TRACK I/B FLANGE CORRODED BETWEEN BS 760- BS 779 LBL 75 CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-02. NEW SEAT TRACK FABRICATED AND INSTALLED IAW SRM 53-10-02 AND SRM 51-30-02.
- [SDR UPS06246838](https://openairdocs.org/sdr/UPS06246838.md): Skin · corroded · Apr 25, 2006 · N954UP · Boeing 727185C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C AREA OF LITE SURFACE CORROSION ON SKIN BS 800 TO 840 STR 10 LT. CORROSION REMOVED AS REQUIRED IAW SRM 51-10-06 AND FOUND WITHIN LIMITS IAW SRM 53-30-01.
- [SDR UPS06246837](https://openairdocs.org/sdr/UPS06246837.md): Skin · corroded · Apr 25, 2006 · N954UP · Boeing 727185C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C AREA OF LITE SURFACE CORROSION ON SKIN BELOW STR 10L BS 465. CORROSION REMOVED IAW SRM 51-10-06. FOUND WITHIN LIMITS IAW SRM 53-30-01.
- [SDR UPS06246836](https://openairdocs.org/sdr/UPS06246836.md): Skin · corroded · Apr 25, 2006 · N954UP · Boeing 727185C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C AREAS OF CORROSION ON SKIN BS 640-700 AT VARIOUS LOCATIONS. AREAS OF CORROSION CLEANED UP AND FOUND WITHIN LIMITS IAW SRM 53-30-01 AND SRM 51-10-02.
- [SDR UPS06246829](https://openairdocs.org/sdr/UPS06246829.md): Stringer · corroded · Apr 25, 2006 · N954UP · Boeing 727185C · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, AREA OF CORROSION ON SKIN BS 358 BELOW STR 10 LT. CORRROSION REMOVED IAW SRM 51-10-06 AND FOUND WITHIN LIMITS IAW SRM 53-30-01 AREA REPROTECTED IAW SRM 51-10-02.
- [SDR UPS06246883](https://openairdocs.org/sdr/UPS06246883.md): Rib · cracked · Apr 24, 2006 · N954UP · Boeing 727185C · Leading Edge Devices
  > INSPECTION TYPE:C LT 2 SLAT SUPPORT RIB CRACKED 2ND FROM LEADING EDGE O/B END, NUT PLATE DE-RIVETED IAW SRM 51-30-02. CRACK FOUND ON BOTH ENDS OF NUT PLATE AND RIB END CRACKED. REPAIR DOUBLER FABRICATED IAW SRM 51-40-3. NUT PLATE RIVETED IAW SRM 51-40-02.
- [SDR UPS06246880](https://openairdocs.org/sdr/UPS06246880.md): Floor Panel · corroded · Apr 24, 2006 · N954UP · Boeing 727185C · Fuselage Floor Panel
  > INSPECTION TYPE:C SECTION OF COCKPIT FLOOR BEHIND CAPTAIN SEAT IS CORRODED AT SCREW HOLES. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-10-06. FLOOR PANEL FABRICATED IAW BOEING DRWG 65-17593.
- [SDR UPS06246879](https://openairdocs.org/sdr/UPS06246879.md): Rib · cracked · Apr 24, 2006 · N954UP · Boeing 727185C · Leading Edge Devices
  > INSPECTION TYPE:C LT NR 2 SLAT SUPPORT RIB CRACKED 2ND FROM LEADING EDGE O/B END NUT PLATE DE-RIVETED IAW SRM 51-30-02. CRACKS FOUND ON NUT PLATE, END BROKEN ON RIB. FABRICATED REPAIR DOUBLER IAW SRM 51-40-03. NUT PLATE RIVETED PER SRM 51-30-02. RIB REPAIR
- [SDR UPS06246874](https://openairdocs.org/sdr/UPS06246874.md): Angle · cracked · Apr 24, 2006 · N954UP · Boeing 727185C · Leading Edge Devices
  > INSPECTION TYPE:C LEFT NR 4, 2 RIBS CRACKED I/B AND O/B OF SLAT ACTUATOR FWD ATTACH POINT. DISCONNECTED ACTUATOR ROD END IAW MM 27-81-32 AND FOUND RIB ANGLES BROKEN. REMOVED FASTENERS IAW SRM 51-30-02. FABRICATED REPAIR DOUBLERS IAW SRM 51-40-03. REPAIR DO
- [SDR UPS06246889](https://openairdocs.org/sdr/UPS06246889.md): Structure · corroded · Apr 20, 2006 · N954UP · Boeing 727185C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C AS PER TC C53-111-01-1B TENSION BOLTS FOUND CORRODED. ALL CORRODED IAW MM 20-80-01. BOLTS TORQUED IAW MM 53-11-01. CORROSION REMOVED OUT OF HOLES IAW SRM 51-10-01, AND AREA REPROTECTED IAW SRM 51-10-02. BOLT HOLES INSPECTED AFTER SURFACE
- [SDR UPS06246885](https://openairdocs.org/sdr/UPS06246885.md): Support Beam · corroded · Apr 20, 2006 · N954UP · Boeing 727185C · Wing, Landing Gear Attach Fittings
  > INSPECTION TYPE:C RT MLG SUPPORT BEAM, PITTING IN BORE OF HOLE. CORROSION REMOVED IAW SRM 51-10-01. HFEC CARRIED OUT IAW B727-NDTM-51-00-00, NO CORROSION FOUND. REF AAAE EO 2006-024-005 FOR REPAIR OF HOLE.
- [SDR UPS06246884](https://openairdocs.org/sdr/UPS06246884.md): Support Beam · corroded · Apr 20, 2006 · N954UP · Boeing 727185C · Wing, Landing Gear Attach Fittings
  > INSPECTION TYPE:C LT MLG SUPPORT BEAM PITTING CORROSION IN BORE OF HOLE. CORROSION REMOVED IAW SRM 51-40-01. HFEC CARRIED OUT IAW B727-NDTM 51-00-00, NO CORROSION FOUND. REF AAAE EO 2006-024-005 FOR REPAIR OF HOLE.
- [SDR UPS06246882](https://openairdocs.org/sdr/UPS06246882.md): Carriage · corroded · Apr 20, 2006 · N954UP · Boeing 727185C · Trailing Edge Flaps
  > INSPECTION TYPE:C T/E FLAP CARRIAGE NR 4 PITTING CORROSION IN BORE OF SPINDLE CARRIAGE ASSY REPLACED IAW OHM 27-58-02.
- [SDR UPS06246881](https://openairdocs.org/sdr/UPS06246881.md): Floor Panel · corroded · Apr 20, 2006 · N954UP · Boeing 727185C · Fuselage Floor Panel
  > INSPECTION TYPE:C SLIGHT SURFACE CORROSION ON FLOOR WEB BS 560 LBL 45.5. CORROSION ON FLOOR PANEL WEB BS 560 LBL 45.5 OUT OF LIMITS IAW SRM 51-10-06. REPAIR CARRIED OUT IAW SRM 51-40-02.
- [SDR UPS06246839](https://openairdocs.org/sdr/UPS06246839.md): Seat Track · corroded · Apr 20, 2006 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C LITE SPOTS OF SURFACE CORROSION BS 380 ON SEAT TRACK FLANGE LBL 45.5. CORROSION REMOVED IAW SRM 51-10-06 AND FOUND WITHIN LIMITS IAW SRM 53-30-01.
- [SDR UPS06246871](https://openairdocs.org/sdr/UPS06246871.md): Pressure Panel · cracked · Apr 19, 2006 · N954UP · Boeing 727185C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C CRACK ON RT NWW BS 268 AT LOWER EDGE OF AFT PRESSURE PANEL CUTOUT. HFEC INSPECTION CARRIED OUT ON ABOVE AREA IAW B727-NDTM 51-00-00 FIG 6. CRACK CONFIRMED. REMOVED INTERCOSTAL AND WEB IAW SRM 51-30-02. FABRICATED NEW WEB AND DOUBLERS IAW
- [SDR UPS06246851](https://openairdocs.org/sdr/UPS06246851.md): Pin · corroded · Apr 19, 2006 · N954UP · Boeing 727185C · Fuselage Main, Structure
  > INSPECTION TYPE:C BS 740 LT BOTTLE PIN FOUND CORRODED. REPLACED BS 740 LT SIDE IN CONJUNCTION WITH MM 57-41-01.
- [SDR UPS06246835](https://openairdocs.org/sdr/UPS06246835.md): Seat Track · cracked · Apr 19, 2006 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C SEAT TRACK UPPER FLANGE AFT END CRACKED AT BS 850 LBL 51. SEAT TRACK REMOVED IAW SRM 51-30-02. SEAT TRACK FABRICATED IAW SRM 53-10-02. INSTALLED SEAT TRACK AND REPROTECTED IAW SRM 51-30-02 AND MM 51-20-91.
- [SDR UPS06246834](https://openairdocs.org/sdr/UPS06246834.md): Seat Track · corroded · Apr 19, 2006 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C CABIN SEAT TRACK I/B FLANGE CORRODED BETWEEN BS 760 AND 779 LBL 20. CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-01. SEAT TRACK FABRICATED AND INSTALLED IAW SRM 53-10-02 AND SRM 51-30-02. REPROTECTED IAW MM 51-20-91.
- [SDR UPS06246831](https://openairdocs.org/sdr/UPS06246831.md): Pressure Panel · cracked · Apr 19, 2006 · N954UP · Boeing 727185C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C SUSPECT CRACK ON NWW PRESSURE WEB RT AT BS 330. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 FIG 4 AND CRACK CONFIRMED. DAMAGE REMOVED IAW SRM 51-10-01. REPAIR PARTS FABRICATED IAW SRM 51-40-02. HFEC CARRIED OUT AROUND CUTOUT IAW B727-NDTM 51-
- [SDR UPS06246830](https://openairdocs.org/sdr/UPS06246830.md): Door · corroded · Apr 19, 2006 · N954UP · Boeing 727185C · Emergency Exits
  > INSPECTION TYPE:C LT AFT ESCAPE HATCH HAS LIGHT SURFACE CORROSION ON LOWER EDGE. HATCH CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 52-00-02. HATCH REPLACED IAW MM 52-21-00.
- [SDR UPS06246887](https://openairdocs.org/sdr/UPS06246887.md): Support · cracked · Apr 18, 2006 · N954UP · Boeing 727185C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CRACKS ON SUPPORT STRUCTURE FOR SYSTEM -B- HYDRAULIC PUMP AT LOWER RADIUS FWD AND AFT CORNERS. HFEC CARRIED OUT ON PREVIOUS LT STOP DRILLED HOLES IAW B727 NDTM 51-00- 00, CRACK CONFIRMED ENDS MARKED. SUPPORT STRUCTURE REMOVED IAW SRM 51-30-
- [SDR UPS06246888](https://openairdocs.org/sdr/UPS06246888.md): Plate · corroded · Apr 15, 2006 · N954UP · Boeing 727185C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CORROSION ON TOP PLATE RIVETED TO FLOOR STRUCTURE AT BS 850 LBL 55. CORROSION FOUND OUTSIDE LIMITS IAW SRM 51-10-06. REPAIR CARRIED OUT IAW SRM 51-40-03.
- [SDR UPS06246833](https://openairdocs.org/sdr/UPS06246833.md): Floorbeam · corroded · Apr 15, 2006 · N954UP · Boeing 727185C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C CORROSION AROUND ANCHOR NUT ON FLOORBEAM AFT CARGO STA 1148. CORROSION FOUND OUT OF LIMITS AT ABOVE AREA IAW SRM 51-10-01. CUTOUT MADE IAW SRM 53-10-08. HFEC CARRIED OUT IAW B727-NDTM PT6 51-00-00 FIG 4. REPAIR COMPLETED IAW SRM 53-10-08.
- [SDR UPS06246877](https://openairdocs.org/sdr/UPS06246877.md): Fitting · cracked · Apr 14, 2006 · N954UP · Boeing 727185C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C NEW CRACKS FOUND ON BS 740 LT FITTING BETWEEN STR 22L AND 23L. STRINGER STRIPS REMOVED IAW SRM 51-30-03. FASTENERS INSTALLED ON FITTING FROM UPPER SPLICE TO STR 17 IAW DRWG 65C13724. SKIN TRIMMED IAW AAA E EO 2006-024-004. REPAIR FASTENER
- [SDR UPS06246832](https://openairdocs.org/sdr/UPS06246832.md): Skin · cracked · Apr 13, 2006 · N954UP · Boeing 727185C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SUSPECT SKIN CRACK AT UPPER VHF ANTENNA CUT OUT AFT EDGE. HFEC INSPECTION CARRIED OUT ON THE ABOVE AREA IAW B727-NDTM PT 6 51-1 00-00 FIG 4. REMOVED ANTENNA IAW SRM 51-30-02. CUTOUT CARRIED OUT IAW EQR 2006024-6. HFEC CARRIED OUT ON FASTE
- [SDR UPS05245641](https://openairdocs.org/sdr/UPS05245641.md): Battery · inoperative · Oct 21, 2005 · N954UP · Boeing 727185C · Emergency Lighting
  > EXIT LIGHT OVER COCKPIT DOOR INOP. REMOVED AND REPLACED LIGHT ASSY AND BATTERIES. OPS CK GOOD PER AMM 33-50-01-5.
- [SDR UPS04243374](https://openairdocs.org/sdr/UPS04243374.md): Tab · corroded · Oct 20, 2004 · N954UP · Boeing 727185C · Aileron Tab Control System
  > INSPECTION TYPE:C, I/B RIGHT AILERON TAB HINGE CASTINGS ARE CORRODED AND SUSPECT CRACK ON AILERON REAR SPAR. REMOVED AILERON IAW AMM 27-10-00, REMOVED HINGES & SPAR IAW SRM 51-3 -30-02. SPAR REPAIRED IAW SRM 57-30-2 FIG 7 & SRM 51-40-02 FIG 1. NEW HINGES IN
- [SDR UPS04243410](https://openairdocs.org/sdr/UPS04243410.md): Intercostal · cracked · Oct 11, 2004 · N954UP · Boeing 727185C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, ON REMOVAL OF INTERCOSTAL TO FACILITATE RIGHT FITTING REPLACEMENT AT BS 740, A CRACK WAS FOUND. REPLACED INTERCOSTAL WEB IAW SRM 51-20-04.
- [SDR UPS04243413](https://openairdocs.org/sdr/UPS04243413.md): Web · cracked · Oct 8, 2004 · N954UP · Boeing 727185C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, BS 740 LOWER WEB RBL 35, WL 160 SUSPECT CRACK IN THIS LOCATION. HFEC CARRIED OUT IAW NDTM 51-00-00, CRACK CONFIRMED WITHIN FASTENER HOLE. REPAIR CARRIED OUT IAW SRM 53-10-9 FIG 4.
- [SDR UPS04243383](https://openairdocs.org/sdr/UPS04243383.md): Web · cracked · Oct 8, 2004 · N954UP · Boeing 727185C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C BS 740 LOWER WEB RT BL 35 WL160 APPROX SUSPECT CRACK IN THIS LOCATION. HFEC CARRIED OUT ON ABOVE AREA IAW NDTM 51-00-00 PT 6 FIG 4 CRACKS CONTAINED WITHIN FASTENER HOLE. REPAIR PARTS FABRICATED IAW SRM 53-10-09. REPROTECTED REP PARTS AND DA
- [SDR UPS04243393](https://openairdocs.org/sdr/UPS04243393.md): Door · cracked · Oct 6, 2004 · N954UP · Boeing 727185C · Landing Gear Doors
  > INSPECTION TYPE:C, BRACKET CRACKED ON WING DOOR FWD OF HINGE CASTING. STOP DRILLED CRACK IAW SRM 51-10-01. HFEC CARRIED OUT AROUND STOP DRILLED AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4. CRACK CONTAINED WITHIN STOP DRILLED AREA. REPAIRED IAW SRM 51-20-01.
- [SDR UPS04243392](https://openairdocs.org/sdr/UPS04243392.md): Skin · corroded · Oct 6, 2004 · N954UP · Boeing 727185C · Ailerons
  > INSPECTION TYPE-C RT OB AILERON HAS PITTING CORROSION ON CONTROL ROD ATTACH CASTING. AILERON REPLACED IAW MM 27-10-14.
- [SDR UPS04243406](https://openairdocs.org/sdr/UPS04243406.md): Bracket · cracked · Oct 5, 2004 · N954UP · Boeing 727185C · Cargo/Baggage Doors
  > INSPECTION TYPE: C, FWD CARGO DOOR BRACKETS CRACKED AT UPPER AFT HINGE ATTACH POINT. REMOVED BRACKETS IAW 51-30-02. NEW BRACKETS FABRICATED IAW BOEING DRAWING 69-18203. NEW BRACKETS INSTALLED IAW 51-30-02.
- [SDR UPS04243405](https://openairdocs.org/sdr/UPS04243405.md): Fitting · corroded · Oct 5, 2004 · N954UP · Boeing 727185C · Aileron Control System
  > INSPECTION TYPE:C, LEFT O/B AILERON TAB MAST FITTINGS HAVE PITTING CORROSION AROUND BUSHINGS. ON INVESTIGATION LEFT O/B AILERON TAB FITTINGS FOUND TO BE OUTSIDE LIMITS. LEFT O/B AILERON TAB REPLACED IAW 27-10-19.
- [SDR UPS04243394](https://openairdocs.org/sdr/UPS04243394.md): Fitting · corroded · Oct 5, 2004 · N954UP · Boeing 727185C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C DURING REMOVAL OF RIGHT 740 FITTING CORROSION FOUND ON CENTER WING SECTION FRONT SPAR UPPER CHORD AT RBBL 65-70 APPROX CORROSION REMOVED IAW SRM 51-10-06. REPAIR ANGLES FABRICATED IAW SRM 53-30-03. HFEC CARRIED OUT ON ABOVE AREA IAW B727-ND
- [SDR UPS04243382](https://openairdocs.org/sdr/UPS04243382.md): Skin · cracked · Oct 5, 2004 · N954UP · Boeing 727185C · Wing, Plate/Skin
  > INSPECTION TYPE: C, SUSPECT CRACK AT FWD UPPER CORNER OF LEFT WING ICE LIGHT CUTOUT. HFEC CARRIED OUT ON ABOVE AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4, CRACKS CONFIRMED, ENDS MARKED. DOUBLER AND FILLER INSTALLED IAW SRM 53-30-03. WEIGHT OF REPAIR 2.37 LBS.
- [SDR UPS04243411](https://openairdocs.org/sdr/UPS04243411.md): Bulkhead · cracked · Oct 4, 2004 · N954UP · Boeing 727185C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C, BS 178 BULKHEAD: EVIDENCE OF CRACK ON FWD FACE AT RBL 10 WL 235.1 EMANATING FROM FASTENER HOLE. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. CRACK CONFIRMED AND ENDS MARKED. CUT OUT DAMAGED AREA IAW SRM 53-10-9. HFEC CARRIED OUT, NO DEFECTS
- [SDR UPS04243409](https://openairdocs.org/sdr/UPS04243409.md): Stringer · corroded · Oct 4, 2004 · N954UP · Boeing 727185C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C, SKIN BULGING AT BS 1307-1315 STR 8L. FOUND BULGING WAS CAUSED BY CORROSION ON STRINGER EXTRUSION. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIR DOUBLER INSTALLED IAW SRM 53-30-3.
- [SDR UPS04243403](https://openairdocs.org/sdr/UPS04243403.md): Terminal · cracked · Oct 4, 2004 · N954UP · Boeing 727185C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C, TAIL SKID BAY STABILIZING LINKS UPPER AND LOWER LEFT AFT TERMINALS CRACKED AND LOWER AFT RIGHT TERMINAL CRACKED. INSTALLED NEW UPPER AND LOWER LEFT AFT TERMINALS ON TAILSKID BAY, FABRICATED LOWER AFT RIGHT TERMINAL AND FITTED IAW SRM 51-30
- [SDR UPS04243397](https://openairdocs.org/sdr/UPS04243397.md): Hinge · corroded · Oct 4, 2004 · N954UP · Boeing 727185C · Ailerons
  > INSPECTION TYPE-C RT IB AILERON TAB HINGE CASTINGS ARE CORRODED AND SUSPECT CRACK ON AILERON REAR SPAR. REPLACED REAR SPAR IAW SRM 51-30-02. NEW TAB HINGES INSTALLED IAW SRM 51-30-02
- [SDR UPS04243396](https://openairdocs.org/sdr/UPS04243396.md): Fitting · cracked · Oct 4, 2004 · N954UP · Boeing 727185C · Fuselage Main, Structure
  > INSPECTION TYPE:C, TO GAIN ACCESS FOR NDT PLEASE REMOVE FASTENERS BETWEEN STR 23 & 24 BS 740 FITTING RIGHT. REMOVED FASTENERS IAW SRM 51-30-02. HFEC CARRIED OUT ON ABOVE AREA IAW B727 NDTM 51-00-00 PT6 FIG 4, CRACK CONFIRMED, ENDS MARKED. REF UPS EO B727-53

Next page: https://openairdocs.org/deregistered/N954UP-2008-09-02/reports.md?page=2

## 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 = 'N954UP' AND deregistration_id = 'N954UP-2008-09-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N954UP-2008-09-02/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.