# Service difficulty reports: N925UP, cancelled Aug 23, 2006

A list on [N925UP, cancelled Aug 23, 2006](https://openairdocs.org/deregistered/N925UP-2006-08-23.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 · 105 reports

- [SDR UPS02239958](https://openairdocs.org/sdr/UPS02239958.md): Door · out of rig · Dec 4, 2002 · N925UP · Boeing 72731C · Landing Gear Door Retract Section
  > NOISE FROM NLG AREA DURING FLIGHT, WITH RED DOOR WARNING INDICATION. LEVEL AT FL260, MACH 0.82, 342 KIAS. HEARD LOUD THUMPING FROM FRONT OF AIRCRAFT WITH ASSCOCIATED RED 'DOORS' ANNUNCIATOR, SLOWED TO MACH 0.80 AND CONDITION WENT AWAY. PERFORMED NLG DOOR RI
- [SDR UPS02237879](https://openairdocs.org/sdr/UPS02237879.md): Fitting · cracked · Feb 28, 2002 · N925UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CRACK AND CORROSION INDICATIONS FROM FASTENER HOLES AT BS 870L STR 13L TO STR 12L.
- [SDR UPS02237819](https://openairdocs.org/sdr/UPS02237819.md): Stringer · cracked · Feb 26, 2002 · N925UP · Boeing 72731C · Fuselage Main, Structure
  > INSPECTION TYPE:C WHILE CARRYING OUT SKIN SPLICE AT L/H BS 740 FITTING STR 23L FOUND T O BE CRACKED STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03
- [SDR UPS02237872](https://openairdocs.org/sdr/UPS02237872.md): Support Fitting · cracked · Feb 25, 2002 · N925UP · Boeing 72731C · Elevator Structure
  > INSPECTION TYPE:C LH ELEVATOR, STA 46.50, ACTUATOR ATTACH SUPPORT FITTING, CRACK BETWE EN THREE FASTENER HOLES LH ELEVATOR REPLACED. REF. NRC 450554.
- [SDR UPS02237822](https://openairdocs.org/sdr/UPS02237822.md): Rib · cracked · Feb 25, 2002 · N925UP · Boeing 72731C · Leading Edge Devices
  > INSPECTION TYPE:C LT WING, NR 3 SLAT, CRACK IN O/B RIB AT O/B TRACK, FWD TRACK ATTACH AREA. CRACK STOP DRILLED IAW SRM 51-10-1, REPAIR CARRIED OUT IAW SRM 57-50-3.
- [SDR UPS02237821](https://openairdocs.org/sdr/UPS02237821.md): Link · corroded · Feb 25, 2002 · N925UP · Boeing 72731C · Main Landing Gear Attach Section
  > INSPECTION TYPE:C ON REMOVAL OF LT MLG TRUNNION LINK EXCESSIVE CORROSION WAS FOUND ON FWD SPLINED LOCKING SLEEVE. LT MLG TRUNNION LINK REPLACED IAW MM 32-11-01.
- [SDR UPS02237871](https://openairdocs.org/sdr/UPS02237871.md): Fitting · cracked · Feb 21, 2002 · N925UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C LT BS 740 FITTING CRACKED IN 2 PLACES IN O/B FLANGE LOWER END. REPLACED LT FITTING IAW EO B727-5310-7477-G.
- [SDR UPS02237869](https://openairdocs.org/sdr/UPS02237869.md): Keelbeam · cracked · Feb 21, 2002 · N925UP · Boeing 72731C · Fuselage Main, Keel
  > INSPECTION TYPE:C CRACK FOUND IN KEEL BEAM WEB FWD OF APU CUTOUT. CRACK REPAIRED IAW SRM ADDENDUM EO B727-5330-1995-B USING KIT P/N 65 -88832-2 AND BOEING DRG 65-88832 AND 65-22466.
- [SDR UPS01236156](https://openairdocs.org/sdr/UPS01236156.md): Uplock · failed · Jun 20, 2001 · N925UP · Boeing 72731C · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:N/A NOSE LANDING GEAR TOOK 4 CYCLES TO EXTEND MANUAL EXTENSION WAS NO HE LP. *S/D* REF WDM 32-64-01 REMOVED AND REPLACED WIRE BETWEEN S96 & S93. REMOVED AND ADJUSTED CORRECTLY. REMOVED AND REPLACED NLG LOCK ACT W/REF 32-33-11, PERFORMED NLG
- [SDR UPS00233659](https://openairdocs.org/sdr/UPS00233659.md): Stringer · corroded · Aug 22, 2000 · N925UP · Boeing 72731C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C, ON REMOVAL OF ATTACH BRACKET FASTENERS CORROSION FOUND ON STR 24L AT BS 740. STRINGER REPAIRED IAW SRM 53-10-3 FIG 1.
- [SDR UPS00233670](https://openairdocs.org/sdr/UPS00233670.md): Bolt · cracked · Aug 17, 2000 · N925UP · Boeing 72731C · Engine Mount Section
  > INSPECTION TYPE:C, ENG NR 2 LEFT ADAPTER FITTING SUSPENSION LINK UPPER ADAPTER FITTING DUE CRACK IN TREADS. REPLACED BOLT IAW MM 71-21-12.
- [SDR UPS00233669](https://openairdocs.org/sdr/UPS00233669.md): Bolt · cracked · Aug 17, 2000 · N925UP · Boeing 72731C · Engine Mount Section
  > INSPECTION TYPE:C, ENG NR 2 LEFT ADAPTER FITTING SWING LINK BOLT FAILED NDI DUE CRACK IN THREADS. REPLACED BOLT IAW MM 71-21-12.
- [SDR UPS00233668](https://openairdocs.org/sdr/UPS00233668.md): Bolt · cracked · Aug 17, 2000 · N925UP · Boeing 72731C · Engine Mount Section
  > INSPECTION TYPE:C, ENG NR 2 RIGHT ADAPTER FITTING CONE BOLT ATTACH BOLT FAILED NDI DUE CRACK IN THREADS. REPLACED BOLT IAW MM 71-21-22.
- [SDR UPS00233667](https://openairdocs.org/sdr/UPS00233667.md): Bolt · cracked · Aug 17, 2000 · N925UP · Boeing 72731C · Engine Mount Section
  > INSPECTION TYPE:C, ENG NR 3 AFT LOWER CRANE BEAM SHOULDER BOLT FAILED NDI DUE CRACK COMING FROM SPLIT PIN HOLE. ALSO, CAD PLATING DAMAGED. NR 3 ENG AFT CRANE BEAM LOWER SHOULDER BOLT REPLACED IAW MM 71-21-03.
- [SDR UPS00233666](https://openairdocs.org/sdr/UPS00233666.md): Bolt · cracked · Aug 17, 2000 · N925UP · Boeing 72731C · Engine Mount Section
  > INSPECTION TYPE:C, ENG NR 3 FWD LOWER CRANE BEAM SHOULDER BOLT FAILED NDI DUE CRACK COMING FROM SPLIT PIN HOLE. ALSO, CAD PLATING DAMAGED. NR 3 ENG FWD CRANE BEAM LOWER SHOULDER BOLT REPLACED IAW MM 71-21-03.
- [SDR UPS00233665](https://openairdocs.org/sdr/UPS00233665.md): Bolt · cracked · Aug 17, 2000 · N925UP · Boeing 72731C · Engine Mount Section
  > INSPECTION TYPE:C, ENG NR 1 FWD UPPER CRANE BEAM SHOULDER BOLT FAILED NDI DUE CRACK COMING FROM SPLIT PIN HOLE. ALSO, CAD PLATING DAMAGED. ENG NR 1 FWD CRANE BEAM UPPER SHOULDER BOLT REPLACED IAW MM 71-21-03.
- [SDR UPS00233664](https://openairdocs.org/sdr/UPS00233664.md): Bolt · cracked · Aug 17, 2000 · N925UP · Boeing 72731C · Engine Mount Section
  > INSPECTION TYPE:C, ENG NR 1 AFT LOWER CRANE BEAM SHOULDER BOLT FAILED NDI DUE CRACK COMING FROM SPLIT PIN HOLE. ALSO, CAD PLATING DAMAGED. NR 1 ENG AFT CRANE BEAM LOWER SHOULDER BOLT REPLACED IAW MM 71-21-03.
- [SDR UPS00233663](https://openairdocs.org/sdr/UPS00233663.md): Bolt · cracked · Aug 17, 2000 · N925UP · Boeing 72731C · Engine Mount Section
  > INSPECTION TYPE:C, ENG NR 1 AFT UPPER CRANE BEAM SHOULDER BOLT FAILED NDI DUE CRACK COMING FROM SPLIT PIN HOLE. ALSO, CAD PLATING DAMAGED. NR 1 ENG AFT CRANE BEAM UPPER SHOULDER BOLT REPLACED IAW MM 71-21-03.
- [SDR UPS00233662](https://openairdocs.org/sdr/UPS00233662.md): Web · cracked · Aug 17, 2000 · N925UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, AFT CARGO DOOR HINGE FWD WEB CRACKED AT INNER CORNER. FABRICATED WEB IAW DRW 69-19170. AFT CARGO DOOR FWD HINGE FWD WEB REPLACED IAW DRAWING 65-18625.
- [SDR UPS00233661](https://openairdocs.org/sdr/UPS00233661.md): Web · cracked · Aug 17, 2000 · N925UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, AFT CARGO DOOR AFT HINGE FWD WEB CRACKED AT UPPER CORNER. AFT CARGO DOOR AFT HINGE FWD WEB REPLACED IAW DRW 65-18625.
- [SDR UPS00233637](https://openairdocs.org/sdr/UPS00233637.md): Angle · corroded · Aug 17, 2000 · N925UP · Boeing 72731C · Wing Miscellaneous Structure
  > INSPECTION TYPE:C, CRACK ON ANGLE BETWEEN SKIN AND RIB IN RIGHT WING L/E CAVITY AT O/B END OF NR 6 L/E FLAP. REPLACED ANGLE AND INSTALLED FASTENERS IAW SRM 51-30-02 AND BOLTS IAW OHM 20-50-01.
- [SDR UPS00233658](https://openairdocs.org/sdr/UPS00233658.md): Bulkhead · corroded · Aug 16, 2000 · N925UP · Boeing 72731C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C EVIDENCE OF CORROSION UNDER RIVET HEAD ON BS 870 BULKHEAD I DOWN FROM PRES DECK, 42 INCHES RIGHT OF KEEL BEAM (RT WHEEL WELL). HFEC INSP OF THE CUTOUT PERIPHERY C/O NDF BULKHEAD REPAIRED IAW SRM 53-10-9 FIG 4.
- [SDR UPS00233660](https://openairdocs.org/sdr/UPS00233660.md): Rib · cracked · Aug 15, 2000 · N925UP · Boeing 72731C · Leading Edge Devices
  > INSPECTION TYPE:C, NR 4 L/E SLAT 2 RIBS CRACKED OUTBOARD OF OUTBOARD TRACK. RIBS REPAIRED IAW SRM 57-50-3 FIG 9 & SRM 51-30-2.
- [SDR UPS00233657](https://openairdocs.org/sdr/UPS00233657.md): Bolt · cracked · Aug 15, 2000 · N925UP · Boeing 72731C · Engine Mount Section
  > INSPECTION TYPE:C, ENG NR 2 FWD MOUNT CROSS STRUT AFT ATTACH BOLT FAILED NDI DUE BOLT CRACKED. NR 2 ENG FWD MOUNT CROSS STRUT AFT ATTACH BOLT REPLACED PER MM 71-21-1 2.
- [SDR UPS00233656](https://openairdocs.org/sdr/UPS00233656.md): Firewall · cracked · Aug 15, 2000 · N925UP · Boeing 72731C · Nacelle/Pylon, Bulkhead/Firewall
  > INSPECTION TYPE:C, SUSPECT CRACK ON WEB OVER ENGINE NR 2 HORIZONTAL FIRE WALL BS 1376 RT. HFEC C/O, CRACK CONFIRMED. FABRICATED AND INSTALLED WEB IAW DRAWING 657555.
- [SDR UPS00233655](https://openairdocs.org/sdr/UPS00233655.md): Bolt · cracked · Aug 15, 2000 · N925UP · Boeing 72731C · Engine Mount Section
  > INSPECTION TYPE:C, ENGINE NR 2 FWD LEFT CONE BOLT HOUSING ATTACHMENT BOLTS, AFT UPPER BOLT FAILED NDI DUE BOLT CRACKED. ENG NR 2 FWD LEFT CONE BOLT HOUSING ATTACH BOLTS AFT UPPER REPLACED IAW MM 71-21-12.
- [SDR UPS00233636](https://openairdocs.org/sdr/UPS00233636.md): Skin · corroded · Aug 14, 2000 · N925UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 1020 S17L. HFEC INSP C/O ON HOLES IN ABOVE AREA. NO DEFECT FOUND. CORROSION REMOVED IAW SRM 51-10-06 FROM SKIN AND FROM CUSP ANGLE SKIN CUTOUT BS 1020 S17L. REPAIRED AREA IAW SRM 5
- [SDR UPS00233635](https://openairdocs.org/sdr/UPS00233635.md): Skin · corroded · Aug 14, 2000 · N925UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, SUSPECT CORROSION BETWEEN SKIN AND STRUCTURE BS 1178 BETWEEN S7R & 9R. FASTENERS REMOVED, CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SKIN BETWEEN BS 1183 - 1165 RT S7R - S9R IAW SRM 53-30-3. NDT INSP C/O. NO DEFECT FOUND. REPA
- [SDR UPS00233365](https://openairdocs.org/sdr/UPS00233365.md): Apu · overserviced · Jul 12, 2000 · N925UP · Boeing 72731C · APU Cowling/Containment
  > INSPECTION TYPE:N/A, APU FIELD RELAY TRIPPED FLIGHT DECK FILLED WITH SMOKE. FOUND APU OVERSERVICED WITH OIL. RESERVICED APU PACKS, RUN ALL AND OPS CHECK NORMAL WITH NO SMOKE.
- [SDR UPS00231602](https://openairdocs.org/sdr/UPS00231602.md): Bulb · failed · Feb 11, 2000 · N925UP · Boeing 72731C · Emergency Lighting
  > DURING ASE, COCKPIT EMERGENCY EXIT IND ONE FILAMENT INOP. RELAMPED EMERGENCY EXIT LIGHT IN COCKPIT FROM AIRCRAFT SPARE STOWAGE.
- [SDR UPS99230638](https://openairdocs.org/sdr/UPS99230638.md): Spar · cracked · Sep 19, 1999 · N925UP · Boeing 72731C · Wing Spar
  > INSPECTION TYPE:N/A, LT WING AFT FALSE SPAR LWR. CAP CRACKED BELOW I/B GROUND SPOILER ACTUATOR SUPPORT BRACKET AT TERMINATING END. DAMAGE APROX 1.25 INCHES IN LENGTH. *S/D* REPAIRED CRACK PER UPS EO B727-5750-11867-A, PARA 6A. CRACK STOP DRILLED IAW SRM 5
- [SDR UPS99229832](https://openairdocs.org/sdr/UPS99229832.md): Light · loose · Jun 13, 1999 · N925UP · Boeing 72731C · Emergency Lighting
  > INSPECTION TYPE:N/A, DURING TAKEOFF THE FLIGHT DECK EMERGENCY LIGHT FELL OFF MOUNT. REINSTALLED EMERGENCY EXIT LIGHT ASSY, OPS CHECKS NORMAL.
- [SDR UPS99229608](https://openairdocs.org/sdr/UPS99229608.md): Out Flow Valve · stuck · May 14, 1999 · N925UP · Boeing 72731C · Pressure Regulator/Outflow Valve
  > INSPECTION TYPE:SI, AIR TURNBACK AT 1945UTC DUE TO UNSATISFACTORY AIRCRAFT PRESSURIZATION. WHEN CLIMB THRUST SET, CARGO HEAT O'FLOW VALVE CLOSED, FULL MANUAL INCRASE ON MANUAL CONTROLLER. AIRCRAFT WAS ONLY ABLE TO MAINTAIN A CABIN ALTITUDE OF 8,000 AND DIFFE
- [SDR UPS99229607](https://openairdocs.org/sdr/UPS99229607.md): Airstair · out of adjust · May 14, 1999 · N925UP · Boeing 72731C · Passenger/Crew Doors
  > INSPECTION TYPE:SI, AFT AIRSTAIR LIGHT ILLUMINATED IN FLT. VISUAL INSPECTION OF STAIR AREA SHOWED FLEXING OF DOOR ARMS INDICATIVE OF UNLOCK CONDITION. DOOR LIGHT WENT OUT WITH INITAIL FLAP SELECTION TO 2 DEGREES (POSSIBLE AIRFLOW CHANGE ON DOOR/STAIR AREA).
- [SDR UPS99229610](https://openairdocs.org/sdr/UPS99229610.md): Connector · dirty · May 13, 1999 · N925UP · Boeing 72731C · Landing Gear Position and Warning
  > INSPECTION TYPE:SI, AIR TURNBACK AT 0100 UTC UPON GEAR RETRACTION, GEAR LEVER WOULD NOT MOVE PAST OFF POSITION. ALSO, I/B ANTISKID RELEASE REMAINED ON IN FLIGHT WITH GEAR HANDLE IN DOWN/IN POSITION. REMOVED, CLEANED CONNECTOR AND RE-INSTALLED ANTISKID CONTRO
- [SDR UPS99229606](https://openairdocs.org/sdr/UPS99229606.md): Track · corroded · May 13, 1999 · N925UP · Boeing 72731C · Trailing Edge Flaps
  > INSPECTION TYPE:SI (CORROSION C57-581-06.00-04) ON NR 6 FLAP TRACK AT SPOILER BEAM PAD. CORROSION ON SPOILER BEAM PAD IS OUT OF LIMITS IAW SRM 57-40-02. FLAP TRACK WAS REPLACED ON CID 888728.
- [SDR UPS99229551](https://openairdocs.org/sdr/UPS99229551.md): Floorbeam · corroded · May 10, 1999 · N925UP · Boeing 72731C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:SI, CORROSION ON STRAP ON FLOORBEAM UPPER CHORD LOWER SIDE BS 312, BL 0, WL 208. REPAIR TO BE ACCOMPLISHED ON CUSTOMER ID 888989.
- [SDR UPS99229561](https://openairdocs.org/sdr/UPS99229561.md): Fitting · corroded · May 7, 1999 · N925UP · Boeing 72731C · Trailing Edge Flaps
  > INSPECTION TYPE:SI, CORROSION ON NR 7 FLAP TRACK FWD ATTACH FITTING. FITTING WAS REWORKED ON NRC NR 888956 AND REINSTALLED ON NRC NR 888744.
- [SDR UPS99229562](https://openairdocs.org/sdr/UPS99229562.md): Fitting · corroded · May 6, 1999 · N925UP · Boeing 72731C · Trailing Edge Flaps
  > INSPECTION TYPE:SI, CORROSION ON NR 8 FLAP TRACK FWD ATTACH FITTING. REWORKED FITTING PER ER 99-5226.
- [SDR UPS99229517](https://openairdocs.org/sdr/UPS99229517.md): Chord · corroded · May 3, 1999 · N925UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SI, 740 UPPER CHORD CORRODED RBL 65-70 WL 202. REMOVED AND REPLACED CHORD SEGMENT RBL 53-55 TO RIGHT O/B END.
- [SDR UPS99229515](https://openairdocs.org/sdr/UPS99229515.md): Skin · corroded · Apr 29, 1999 · N925UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SI, INTERIOR FUSELAGE SKIN AT STA 873-877 RT WL 261 ALONG EDGE OF 5-10R IS CORRODED. BLENDED CORROSION ON LOWER SKIN, HFEC FASTENER HOLES, FLAT PEENED THE BLENDED AREA. ALODINED AND PRIMED BLENDED AREA, FABRICATED REPAIR DOUBLER AND REPAIR FI
- [SDR UPS99229559](https://openairdocs.org/sdr/UPS99229559.md): Skin · corroded · Apr 27, 1999 · N925UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SI, CORROSION (C57-174-01-1B) ON INTERNAL 870 SKIN AT UPPER SPAR CHORD BS 870, RBL 61-64. REMOVED CORROSION PER SRM 57-30-1, FLAP PEENED AREA PER ER NR 99-5258, ALODINED AND PRIMED PER ER NR 99-5258.
- [SDR UPS99229283](https://openairdocs.org/sdr/UPS99229283.md): Floorbeam · corroded · Apr 11, 1999 · N925UP · Boeing 72731C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:SI CORROSION ON FLOORBEAM BS 312, LBL 3.5, WL 208. REMOVED AND REPLACED UPPER CHORD SEGMENT PER SRM 53-10-8 FIG 9.
- [SDR UPS99229375](https://openairdocs.org/sdr/UPS99229375.md): Stringer · corroded · Apr 9, 1999 · N925UP · Boeing 72731C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:SI BS 851 STR 2 RT FOUND TO BE OUT OF LIMITS. REPAIRED PER SRM 53-10-3 CPCP.
- [SDR UPS99229286](https://openairdocs.org/sdr/UPS99229286.md): Stringer · cracked · Apr 9, 1999 · N925UP · Boeing 72731C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:SI CRACKS AROUND UPPER AND LOWER FASTENERS IN STRINGER 15R COMMON TO BS 400 FRAME. REPAIRED PER SRM 53-10-3.
- [SDR UPS99229281](https://openairdocs.org/sdr/UPS99229281.md): Seat Track · corroded · Apr 9, 1999 · N925UP · Boeing 72731C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:SI CORROSION C53-224-01.05-01, ON FLANGE OF SEAT TRACK BS 740, LBL 25, WL 208, CUT OUT DAMAGED SECTION DUE TO THE EXTENT OF CORROSION. FABRICATED REPAIR PARTS (SEAT TRACK AND STRAPS). ALODINE, PRIMED AND INSTALLED REPAIR PARTS PER SRM 53-10-5
- [SDR UPS99229280](https://openairdocs.org/sdr/UPS99229280.md): Doubler · corroded · Apr 9, 1999 · N925UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SI WHILE WORKING NRC 888366 (FUSE 123) LT 870 ACCESS COVER (PANEL) DOUBLER RING IS CORRODED LBL 58, BS 870, WL 180. AFTER THE CORROSION REMOVAL, THE DOUBLER RING WENT BEYOND THE SRM LIMITS. REMOVED DOUBLER RING AND FABRICATED A NEW ONE. ALOD
- [SDR UPS99229278](https://openairdocs.org/sdr/UPS99229278.md): Stringer · corroded · Apr 9, 1999 · N925UP · Boeing 72731C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:SI, CORROSION AT BS 806 STR 2 FOUND TO BE OUT OF LIMITS. REPAIRED SRM 53-10-3.
- [SDR UPS99229274](https://openairdocs.org/sdr/UPS99229274.md): Shear Tie · cracked · Apr 9, 1999 · N925UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SI CRACKED SHEAR TIE AT BS 400 BETWEEN STR 14R AND STR 15R. REPLACED PER SRM 51-30-2.
- [SDR UPS99229273](https://openairdocs.org/sdr/UPS99229273.md): Stringer · cracked · Apr 9, 1999 · N925UP · Boeing 72731C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:SI CRACKS AROUND UPPER FASTENER ON STR 16R COMMON TO BS 500 FRAME. REPAIRED PER SRM 53-10-3.

Next page: https://openairdocs.org/deregistered/N925UP-2006-08-23/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 = 'N925UP' AND deregistration_id = 'N925UP-2006-08-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N925UP-2006-08-23/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.