# Service difficulty reports: N905UP, cancelled May 10, 2007

A list on [N905UP, cancelled May 10, 2007](https://openairdocs.org/deregistered/N905UP-2007-05-10.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 3 · 111 reports

- [SDR UPS03241647](https://openairdocs.org/sdr/UPS03241647.md): Warning Light · illuminated · Dec 9, 2003 · N905UP · Boeing 72751C · Engine Fuel Indicating System
  > NR 3 ENG FUEL FILTER WARNING LIGHT ILLUMINATED.
- [SDR UPS02239943](https://openairdocs.org/sdr/UPS02239943.md): Pressure Panel · cracked · Nov 25, 2002 · N905UP · Boeing 72751C · Fuselage Main, Structure
  > INSPECTION TYPE:C SEVERAL CRACKS ON NLG WHEEL WELL PRESSURE WEB RHS FROM BS 260 DOWN 1 1" FROM CEILING AND 1" FWD OF THE AFT PRESSURE PANEL TP BS 279 6" BE LOW AFT PRESSURE PANEL DAMAGED AREAS REPAIRED IAW SRM51-40-2 FIG 1
- [SDR UPS02239946](https://openairdocs.org/sdr/UPS02239946.md): Pressure Panel · cracked · Nov 21, 2002 · N905UP · Boeing 72751C · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C, NLG WHEEL WELL PRESSURE PANEL CRACKED AT BS 268, 3 INCHES DOWN FROM W/W CEILING. DAMAGED AREA CUTOUT IAW SRM 51-40-2 FIG 1 HFEC CONFIRMS A DEFECT FREE CONDITION, AREA REPAIR IAW SRM 51-40-2 F IG 1.
- [SDR UPS02239949](https://openairdocs.org/sdr/UPS02239949.md): Bolt · cracked · Nov 19, 2002 · N905UP · Boeing 72751C · Main Landing Gear Attach Section
  > INSPECTION TYPE: C, DURING REMOVAL OF LT HAND TRUNNION LINK, THE LT MAIN GEAR AFT TRUNNION BOLT AND TRUNNION HOUSING FOUND SHEARED. ON REMOVAL OF LT MLG, AFT BEARING MOUNTING JOURNAL FOUND CRACKED & PIECE BROKEN OFF. END OF JOURNAL.BEARING RETAINING BOLT SH
- [SDR UPS02239945](https://openairdocs.org/sdr/UPS02239945.md): Pressure Panel · cracked · Nov 19, 2002 · N905UP · Boeing 72751C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C SUSPECT CRACK ON NLG CEILING AT BS 273 LBL14. HFEC CONFIRMS CRACK, DAMAGED ARE CUTOUT IAW SRM 51-40-02 FIG, HFEC CONFIRMS NDF. REPAIR CARRIED OUT SRM 51-40-02 FIG 1.
- [SDR UPS02239944](https://openairdocs.org/sdr/UPS02239944.md): Pressure Panel · cracked · Nov 19, 2002 · N905UP · Boeing 72751C · Fuselage Main, Structure
  > INSPECTION TYPE:C CRACK ON NLG WHEEL WELL PRESSURE WEB @ BS 243.6 LHS 4" AFT FROM FWD PRESSURE PANEL. DAMAGED AREA CUT OUT IAW SRM 51-40-02 FIG1, HFEC AROUND CUTOUT NDF, REPAIR CARRIED OUT IAW SRM 51-40-02 FIG 1
- [SDR UPS02239940](https://openairdocs.org/sdr/UPS02239940.md): Fitting · cracked · Nov 18, 2002 · N905UP · Boeing 72751C · Fuselage Main, Structure
  > INSPECTION TYPE:C SUSPECT CRACK ON L/H BS 910 FITTING REPAIR CARRIED OUT IAW EO B727-5310-1896-B APPENDIX B
- [SDR UPS02239937](https://openairdocs.org/sdr/UPS02239937.md): Fitting · cracked · Nov 18, 2002 · N905UP · Boeing 72751C · Fuselage Main, Structure
  > INSPECTION TYPE:C SUSPECT CRACK ON RH BS 910 FITTING REPAIR CARRIED OUT IAW EO B727-5310-1896-B APPENDIX B
- [SDR UPS02239938](https://openairdocs.org/sdr/UPS02239938.md): Pin · corroded · Nov 16, 2002 · N905UP · Boeing 72751C · Horizontal Stabilizer Miscellaneous Structure
  > INSPECTION TYPE:C PITTING FOUND ON RT STAB INNER PINS. RT STAB INNER PIN REPLACED IAW MM 55-10-01.
- [SDR UPS02239950](https://openairdocs.org/sdr/UPS02239950.md): Spar · cracked · Nov 15, 2002 · N905UP · Boeing 72751C · Trailing Edge Flaps
  > INSPECTION TYPE: C, DURING LFEC INSPECTION OR RT INBOARD MID FLAP REAR SPAR UPPER CHORD, A CRACK WAS FOUND AROUND A FASTENER HOLE. REPAIRED PER EO.B727-5750-3582.
- [SDR UPS02239948](https://openairdocs.org/sdr/UPS02239948.md): Beam · cracked · Nov 15, 2002 · N905UP · Boeing 72751C · Fuselage Main, Structure
  > INSPECTION TYPE: C, DURING INSPECTION OF VERTICAL BEAM 17.8 RT, A CRACK WAS FOUND ON THE BEAM FLANGE. STOP CUT-OUT AT WL 273, BS 1183 REPAIR PARTS DRILLED OFF IAW EO B727-5310-11743. REPAIR ANGLES INSTALLED WET WITH SEALANT IAW EO B727-5310-11743 REPAIR
- [SDR UPS02239942](https://openairdocs.org/sdr/UPS02239942.md): Intercostal · cracked · Nov 15, 2002 · N905UP · Boeing 72751C · Fuselage Main, Structure
  > INSPECTION TYPE:C HORIZONTAL INTERCOSTAL CRACKED ON VERTICAL BEAM 17.8 L/H AT WL 283 1 183 BULKHEAD NEW INTERCOSTAL FABRICATED & INSTALLED PER BOEING DRAWING 65-16350 S HEET 6 & 65C15764 SH. 5 & SRM 51-30-2
- [SDR UPS02239941](https://openairdocs.org/sdr/UPS02239941.md): Floorbeam · cracked · Nov 14, 2002 · N905UP · Boeing 72751C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C BEAM TIE CRACKED ON FLOORBEAM LWR FLANGE BS 328 RBL 40. REPAIR PLATE FABRICATED AND FITTED AS PER ARM 53-10-8.
- [SDR UPS02239947](https://openairdocs.org/sdr/UPS02239947.md): Fitting · cracked · Nov 13, 2002 · N905UP · Boeing 72751C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C&SI, WHILE CARRY OUT HFEC INSPECTION ON LT BS 950 FITTING. CRACK FOUND IN ROW 1 UP PER FASTENER HOLE, COMMON TO STR 9. DISCREPANT HOLE REPAIRED IAW SMRO EO 2002-061-003 UPS ENG. FILE NO. B727-5310-17956
- [SDR UPS02238710](https://openairdocs.org/sdr/UPS02238710.md): Relay · failed · Jun 28, 2002 · N905UP · Boeing 72751C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHTS ABOVE COCKPIT DOOR ILLUMINATED IN FLIGHT WITH ARM SWITCH IN THE ARMED POSITION. REMOVED R70 RELAY. OPS CHECKS GOOD.
- [SDR UPS01236733](https://openairdocs.org/sdr/UPS01236733.md): Stiffener · cracked · Aug 30, 2001 · N905UP · Boeing 72751C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:N/A RT MLG ACT BEAM SUPPORT PANEL. FWD STIFFENER CRACKED AT INBD HINGE. REPAIRED CRACKED STIFFENER RT MLG ACT BEAM SUPPORT PANEL PER B727 SRM 51-40-3
- [SDR UPS01236532](https://openairdocs.org/sdr/UPS01236532.md): Slide · inoperative · Aug 5, 2001 · N905UP · Boeing 72751C · Escape Slide
  > INSPECTION TYPE:IN MAIN CABIN SLIDE INOP REF DEF M220206 FWD ENTRY SLIDE DEPLOYED. REPLACED SLIDE AND LATCH ASSY REF 25-60-14.
- [SDR UPS01236026](https://openairdocs.org/sdr/UPS01236026.md): Panel · cracked · May 31, 2001 · N905UP · Boeing 72751C · Wing, Plate/Skin
  > INSPECTION TYPE:C, 1 INCH CRACK ON PANEL, UPPER SURFACE OF WING, JUST FWD OF I/B AILERON ON RIGHT WING, I/B EDGE OF PANEL. REPAIRED PER SRM 51-40-2.
- [SDR UPS01236033](https://openairdocs.org/sdr/UPS01236033.md): Skin · cracked · May 30, 2001 · N905UP · Boeing 72751C · Spoilers
  > INSPECTION TYPE:C, CRACK FOUND IN TRAILING EDGE SKIN ADJACENT NR 3 SPOILER PANEL HINGE INBOARD HINGE. CRACK REPAIRED IAW SRM.
- [SDR UPS01235942](https://openairdocs.org/sdr/UPS01235942.md): Light · inoperative · May 21, 2001 · N905UP · Boeing 72751C · Emergency Lighting
  > INSPECTION TYPE:IN EMERGENCY LIGHTS UNARMED LIGHT INOP WHEN UNARMED AND PRESS TO TEST. RELAMPED AND FUNCTIONALLY CK GOOD AS PER 33-50.
- [SDR UPS00234515](https://openairdocs.org/sdr/UPS00234515.md): Skin · cracked · Nov 26, 2000 · N905UP · Boeing 72751C · Leading Edge Devices
  > INSPECTION TYPE:C FOUND R/H OUTBRD FOREFLAP WITH A 3/8 INCH CRACK AT HINGE CUTOUT. REPLACED R/H OUTBRD FOREFLAP IAW M/M 27-51-11. OK PER SAME
- [SDR UPS98227681](https://openairdocs.org/sdr/UPS98227681.md): Doubler · cracked · Sep 15, 1998 · N905UP · Boeing 72751C · Wing Miscellaneous Structure
  > INSPECTION TYPE-N/A, RIGHT WING AFT SPAR LOWER EDGE CORRIGATED DOUBLER CRACKED APROX 2 INCHES AT APROX WS 340 WBL 220. STOP DRILLED CRACK PER SRM 51-10-1 PG 6B.
- [SDR UPS98227517](https://openairdocs.org/sdr/UPS98227517.md): Rib · cracked · Aug 14, 1998 · N905UP · Boeing 72751C · Wing, Rib/Bulkhead
  > INSPECTION TYPE-D, ON REMOVAL OF NR 4 SLAT ACTUATOR EYE END BOLT FROM SLAT BOTH RIBS EITHER SIDE OF MOUNT POINT FOUND CRACKED. REPLACED RIBS IAW SRM AND DRAWING 657276, REINSTALLED NR 4 SLAT EYE BOLT IAW MM 27-81-32.
- [SDR UPS98227488](https://openairdocs.org/sdr/UPS98227488.md): Bottle Pin · corroded · Aug 13, 1998 · N905UP · Boeing 72751C · Wing, Fuselage Attach Fittings
  > INSPECTION TYPE:D LT BS 750 BOTTLE PIN FOUND WITH LIGHT PITTING CORROSION. PIN REPLACED IAW MM 57-41-00.
- [SDR UPS98227574](https://openairdocs.org/sdr/UPS98227574.md): Stringer · corroded · Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:D STRINGER ON TOP OF NOSE WHEEEL WELL AT BL 0, BS 260 TO 277 IS CORRODED. STRINGER SECTION REPAIRED IAW SRM 53-10-3.
- [SDR UPS98227572](https://openairdocs.org/sdr/UPS98227572.md): Stringer · cracked · Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:D SUSPECT CRACK ON STRINGER 23R AT STA 440. REPLACED PART WITH 69-14492-5 IAW SRM 51-30-2.
- [SDR UPS98227566](https://openairdocs.org/sdr/UPS98227566.md): Stringer · cracked · Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE-D, STRINGER 23L AT STATION 400 CRACKED AT FASTENER HOLE. STRINGER REPAIRED IAW SRM 53-10-3, FIG 1.
- [SDR UPS98227565](https://openairdocs.org/sdr/UPS98227565.md): Stringer · cracked · Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE-D, S21L HAS CRACK AT FASTENER HOLE AT STATION 380. STRINGER REPAIRED IAW SRM 53-10-3, FIG 1.
- [SDR UPS98227564](https://openairdocs.org/sdr/UPS98227564.md): Rib · cracked · Aug 12, 1998 · N905UP · Boeing 72751C · Wing, Rib/Bulkhead
  > INSPECTION TYPE-D, CRACK ON RIB ATTACH TAB ON NR 13 STRINGER AT WING STATION 656.5 RT. REPAIR CARRIED OUT IAW UPS B727-5710-0314.
- [SDR UPS98227561](https://openairdocs.org/sdr/UPS98227561.md): Rib · cracked · Aug 12, 1998 · N905UP · Boeing 72751C · Wing, Rib/Bulkhead
  > INSPECTION TYPE-D, CRACK ON RIB ATTACH TAB ON NR 10 STRINGER AT WING STATION 656.5 RT. REPAIR CARRIED OUT IAW UPS EO B727-5710-0314 FIG 13.
- [SDR UPS98227551](https://openairdocs.org/sdr/UPS98227551.md): Stringer · cracked · Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE-D, CRACK IN FASTENER HOLE AND FASTENER MISSING ON S21R AT BS 400. REPAIRED CRACK IAW SRM 51-10-3, FIG 2.
- [SDR UPS98227550](https://openairdocs.org/sdr/UPS98227550.md): Stringer · cracked · Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE-D, SUSPECT CRACK ON S22R FASTENER HOLE ST STA 380. REPAIRED CRACK IAW SRM 51-10-3 FIG 2.
- [SDR UPS98227549](https://openairdocs.org/sdr/UPS98227549.md): Stringer · cracked · Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE-D, CRACK AT FASTENER HOLE OF STRINGER 21R AT STATION 420. STRINGER REPAIRED IAW SRM 53-10-2, FIG 1, DETAIL 2.
- [SDR UPS98227548](https://openairdocs.org/sdr/UPS98227548.md): Stringer · broken · Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE-D, STRINGER 23R BROKEN AT STA 420. STRINGER REPAIRED IAW SRM 53-10-2, FIG 1 DETAIL 2.
- [SDR UPS98227496](https://openairdocs.org/sdr/UPS98227496.md): Stringer · cracked · Aug 12, 1998 · N905UP · Boeing 72751C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:D, SUSPECT CRACK ON STRINGER 23R AT STA 440. REPLACED PART WITH 69-14492-5 IAW SRM 51-30-2.
- [SDR UPS98227573](https://openairdocs.org/sdr/UPS98227573.md): Frame · cracked · Aug 11, 1998 · N905UP · Boeing 72751C · Fuselage Main, Frame
  > INSPECTION TYPE:D CRACK ON UPPER FLANGE OF FRAME AT BS 420, BL 0. REPAIR CARRIED OUT ON UPPER FLANGE IAW SRM 51-40-3, FIG 1.
- [SDR UPS98227518](https://openairdocs.org/sdr/UPS98227518.md): Frame · cracked · Aug 10, 1998 · N905UP · Boeing 72751C · Fuselage Main, Frame
  > INSPECTION TYPE-D, SLIDING FAIRING 2ND AFT FRAME HAS A CRACK AT THE UPPER SLIDING TRACK ATTACH POINT. CRACK STOP DRILLED PER SRM 51-10-1, REPAIRED FRAME IAW SRM 51-40-3 FIG 1.
- [SDR UPS98227571](https://openairdocs.org/sdr/UPS98227571.md): Strap · cracked · Aug 8, 1998 · N905UP · Boeing 72751C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:D ON ACCOMPLISHMENT OF EDDY CURRENT INSPECTION OF RT E-F WINDOW POST PER EO B727-5310-0012, CRACKS FOUND ON 3 HOLES COMMON TO REPAIR STRAP. REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 98-24-012, REF UPS ENGINEERING FILE NUMBER 727-5310-2066.
- [SDR UPS98227560](https://openairdocs.org/sdr/UPS98227560.md): Track · cracked · Aug 7, 1998 · N905UP · Boeing 72751C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-D, CARGO TRACK SECTION BS 1010 RT SIDE HAS SIZEABLE CRACK. RT FWD TRACK REPLACED IAW SRM 51-30-2.
- [SDR UPS98227529](https://openairdocs.org/sdr/UPS98227529.md): Web · cracked · Aug 7, 1998 · N905UP · Boeing 72751C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-D, CRACK ON VERTICAL WEB ABOVE KEEL BEAM RBL BS 885 APPROX. VERTICAL WEB ABOVE KEEL BEAM REPAIRED IAW SRM 51-40-02.
- [SDR UPS98227528](https://openairdocs.org/sdr/UPS98227528.md): Clip · cracked · Aug 7, 1998 · N905UP · Boeing 72751C · Wing Miscellaneous Structure
  > INSPECTION TYPE-D, WING CENTER SECTION FWD TANK FWD WALL SHEAR TIE CLIP CRACKED AT RBL 25. REPLACED SHEAR TIE CLIP IAW DRW 64-08333.
- [SDR UPS98227527](https://openairdocs.org/sdr/UPS98227527.md): Clip · cracked · Aug 7, 1998 · N905UP · Boeing 72751C · Wing Miscellaneous Structure
  > INSPECTION TYPE-D, WING CENTER SECTION FWD TANK FWD WALL SHEAR TIE CLIP CRACKED AT LBL 25. REPLACED SHEAR TIE CLIP IAW DRAWING 64-08333.
- [SDR UPS98227519](https://openairdocs.org/sdr/UPS98227519.md): Skin · corroded · Aug 7, 1998 · N905UP · Boeing 72751C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE-D, SUSPECT CORROSION BETWEEN SKIN AND CUSP ANGLE BS 1180 STR 17R. CORRODED SKIN AT BS 1180 STR 17R REPAIRED PER SRS EO 98-24-006 REF UPS ENGINEERING FILE NR 727-53-2063.
- [SDR UPS98227499](https://openairdocs.org/sdr/UPS98227499.md): Fitting · corroded · Aug 7, 1998 · N905UP · Boeing 72751C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:D, 9G BARRIER NET ATTACH FITTING ON FLOOR LBL 20 BETWEEN BS 360-380 HAS SEVERE CORROSION. 9G FITTING AT LBL 20 REPLACED IAW SRM 51-30-02.
- [SDR UPS98227495](https://openairdocs.org/sdr/UPS98227495.md): Web · corroded · Aug 7, 1998 · N905UP · Boeing 72751C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:D, COROSION ON WEB RBL 10 BS 830 APPROX. REPAIR CARRIED OUT IAW SRM 51-40-2.
- [SDR UPS98227533](https://openairdocs.org/sdr/UPS98227533.md): Spindle · corrosion · Aug 6, 1998 · N905UP · Boeing 72751C · Trailing Edge Flaps
  > INSPECTION TYPE-D, SURFACE CORROSION IN BORE OF SPINDLE OF NR 3 FLAP TRACK CARRIAGE. FLAP TRACK CARRIAGE REPLACED REF OHM 57-58-11.
- [SDR UPS98227492](https://openairdocs.org/sdr/UPS98227492.md): Web · cracked · Aug 6, 1998 · N905UP · Boeing 72751C · Engine Thrust Reverser
  > INSPECTION TYPE:D, ENGINE NR 1 THRUST REV AFT VERTICAL WEB SUSPECT CRACK AT 12 O'CLOCK POSITION AT HYD PIPE BRACKET ATTACH. REPAIR CARRIED OUT IAW SRM 51-40-2.
- [SDR UPS98227563](https://openairdocs.org/sdr/UPS98227563.md): Angle · corroded · Aug 5, 1998 · N905UP · Boeing 72751C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-D, CHORD ANGLE AT BS 740 LT (P/N 65-15940-24) HAS CORROSION ON O/B SECTION. CHORD REPAIRED IAW DRAWING 65C13724 AND SRS ENGINEERING ORDER 98-24- 004, REF UPS ENGINEERING FILE NUMBER 727-53-2064.
- [SDR UPS98227544](https://openairdocs.org/sdr/UPS98227544.md): Bolt · corroded · Aug 5, 1998 · N905UP · Boeing 72751C · Trailing Edge Flaps
  > INSPECTION TYPE-D, NR 5 FLAP TRACK ATTACH BOLT CORRODED. BOLT CHANGED IAW MM 27-51-31.
- [SDR UPS98227576](https://openairdocs.org/sdr/UPS98227576.md): Panel · corroded · Aug 4, 1998 · N905UP · Boeing 72751C · Wing, Plate/Skin
  > INSPECTION TYPE:D LT WING TANK FROMT SPAR ACCESS PANEL NR 1 CORRODED. PANEL REPLACED IAW MM 28-11-21.

Next page: https://openairdocs.org/deregistered/N905UP-2007-05-10/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 = 'N905UP' AND deregistration_id = 'N905UP-2007-05-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N905UP-2007-05-10/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.