# Service difficulty reports: N928UP, cancelled Mar 26, 2013

A list on [N928UP, cancelled Mar 26, 2013](https://openairdocs.org/deregistered/N928UP-2013-03-26.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 · 128 reports

- [SDR UPS02239022](https://openairdocs.org/sdr/UPS02239022.md): Stringer · corroded · Aug 8, 2002 · N928UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C MATERIAL LOSS INDICATION AT BS 259.5 AT STR.19 R/H. REMOVED FASTENERS IAW SRM 51-30-2. CORR NOT FOUND TO BE WITHIN LIMIT S IAW SRM 53-30-01. REPAIR CARRIED OUT AS REQUIRED IAW EO-B727-5310-1371 APPDX. E.
- [SDR UPS02238980](https://openairdocs.org/sdr/UPS02238980.md): Yoke · corroded · Jul 31, 2002 · N928UP · Boeing 72722C · Main Landing Gear
  > INSPECTION TYPE:C, LT BS 940 SWING LINK REMOVAL YOKE ASSY FOUND TO BE CORRODED. YOKE ASSY REPLACED IAW MM 57-15-01.
- [SDR UPS02239016](https://openairdocs.org/sdr/UPS02239016.md): Frame · corroded · Jul 30, 2002 · N928UP · Boeing 72722C · Aerodynamic Fairings
  > INSPECTION TYPE:C CORROSION ON FAIRING # 3334 ON FRAME AT L/H FAN INLET DOOR AFT AREA FRAME REPAIR CARRIED OUT IAW SRM 51-40-4 L/H FAN INLET DOOR REPLACED IAW MM 21-52-51 & DOOR ACTUATING ROD REP LACED IAW MM 21-52-51
- [SDR UPS02239021](https://openairdocs.org/sdr/UPS02239021.md): Link · damaged · Jul 26, 2002 · N928UP · Boeing 72722C · Main Landing Gear
  > INSPECTION TYPE:C, LEFT MLG BEAM SWING LINK BOLT HOLE HAS MECHANICAL DAMAGE. REPAIR CARRIED OUT IAW SMRO EO 2002-040-004 UPS ENGINEERING FILE 727-57-20059.
- [SDR UPS02239018](https://openairdocs.org/sdr/UPS02239018.md): Panel · delaminated · Jul 25, 2002 · N928UP · Boeing 72722C · Nacelle/Pylon, Plate/Skin
  > INSPECTION TYPE:C, ENGINE NR 3 PYLON PANEL 5508 IS DELAMINATED, INNER SURFACE FWD END. REPAIRED IAW SRM 51-40-5.
- [SDR UPS02239017](https://openairdocs.org/sdr/UPS02239017.md): Panel · delaminated · Jul 25, 2002 · N928UP · Boeing 72722C · Nacelle/Pylon, Plate/Skin
  > INSPECTION TYPE:C, ENGINE NR 1 PYLON PANEL 5408 IS DELAMINATED INNER, SURFACE FWD END. REPAIRED IAW SRM 51-40-5.
- [SDR UPS02238984](https://openairdocs.org/sdr/UPS02238984.md): Strap · cracked · Jul 24, 2002 · N928UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, FLOORBOARD SUPPORT STRAP CRACKED BS 850 LBL 45.5. FLOORBOARD SUPPORT STRAP REPLACED BS 850 LBL 45.5 IAW SRM 53-20-2.
- [SDR UPS02239025](https://openairdocs.org/sdr/UPS02239025.md): Fitting · cracked · Jul 23, 2002 · N928UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C LH WHEEL WELL BS 940 FORGING HAS A SUSPECT CRACK @ BASE OF PREVIOUS BLENDOUT FITTING REPLACED IAW UPS EO B727-5310-4501
- [SDR UPS02239011](https://openairdocs.org/sdr/UPS02239011.md): Channel · cracked · Jul 23, 2002 · N928UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C CRACK ON CHANNEL SECTION IN LWR AFT CARGO HOLD AT BS 1060 BBL 8L REPAIRED IAW SRM 53-10-5 FIG 4
- [SDR UPS02239010](https://openairdocs.org/sdr/UPS02239010.md): Frame · cracked · Jul 23, 2002 · N928UP · Boeing 72722C · Fuselage Main, Frame
  > INSPECTION TYPE:C, LEFT WHEEL WELL, BS 930 FRAME IS CRACKED ON INNER FLANGE UPPER HOLE. REPAIR CARRIED OUT IAW UPS EO B727-5310-2611-B.
- [SDR UPS02239009](https://openairdocs.org/sdr/UPS02239009.md): Stiffener · cracked · Jul 23, 2002 · N928UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, MAIN CARGO DECK COMPARTMENT BS 1183 STIFFENER TIE CRACKED AT RBL 361 UPPER TIE BETWEEN VERT BEAM AT RBL 26.83 & RBL 36.83. NEW STIFFENER INSTALLED IAW SRM 51-30-2.
- [SDR UPS02239029](https://openairdocs.org/sdr/UPS02239029.md): Skin · corroded · Jul 22, 2002 · N928UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, 15 TO 20 PERCENT MATERIAL LOSS INDICATION AT BS 1080 STR 4R. REPAIR CARRIED OUT IAW UPS EO B727-5330-1177 & SMRO EO 2002-040-005 UPS ENGINEERING FILE B727-5330-17277.
- [SDR UPS02239023](https://openairdocs.org/sdr/UPS02239023.md): Skin · corroded · Jul 22, 2002 · N928UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, MATERIAL LOSS INDICATIONS AT BS 521 AFT SKIN FROM STR 1 TO STR 2 OF 15 - 20 PERCENT AND FROM STR 3R TO STR 4R OF 20 PERCENT AND ON FWD SKIN AT BS 521 BETWEEN STR 3R AND STR 4R OF 15 PERCENT. AREA INSP AND CORROSION FOUND ON SKIN AND TEAR ST
- [SDR UPS02239020](https://openairdocs.org/sdr/UPS02239020.md): Doubler · cracked · Jul 22, 2002 · N928UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C CRACK ON R/H WINDOW POST BETWEEN R1 & R2 WINDOWS AT UPPER CORNER REPAIR DOUBLER FABRICATED IAW SRM 53-30-3 REPAIR DOUBLER INSTALLED IAW SRM 53-30-3 FIG 8 REPAIR 2
- [SDR UPS02239012](https://openairdocs.org/sdr/UPS02239012.md): Window Post · cracked · Jul 22, 2002 · N928UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C CRACKS ON CENTER WINDOW POST ON LWR LHS & RHS COCKPIT CENTER WINDOW POST REPAIRED IAW UPS EO B727-5330-5128
- [SDR UPS02239013](https://openairdocs.org/sdr/UPS02239013.md): Structure · cracked · Jun 26, 2002 · N928UP · Boeing 72722C · Leading Edge Devices
  > INSPECTION TYPE:C PLS CARRY OUT PERMANENT REPAIR TO NR 2 L/E SLAT DENT (APPROX 1.5 FT O/B OF ACTUATOR). PERMANENT REPAIR CARRIED OUT ON NR 2 L/E SLAT IAW SRM 57-50-03 FIG 1.
- [SDR UPS01236010](https://openairdocs.org/sdr/UPS01236010.md): Pressure Panel · cracked · May 26, 2001 · N928UP · Boeing 72722C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:N/A, RT WHEEL WELL CRACKS. *S/D* REPAIRED PER SRM 51-1-9A.
- [SDR UPS01235658](https://openairdocs.org/sdr/UPS01235658.md): Control Rod · lack of lube · Apr 21, 2001 · N928UP · Boeing 72722C · Aileron Control System
  > INSPECTION TYPE:IN AILERON STIFF IN LEFT TURNS AILERON SPRING CARTRIDGE FOUND OUT OF RIG. RE-ADJUSTED I.A.W. B727 M.M.27-61-21. SPRING CARTRIDGE OPS CHECKS SERV. CONTROL WHEEL INPUTS (FORCE) THE SAME LEFT AND RIGHT NOTE: MIXER CONTROL ROD AND SPD BRK INPU
- [SDR UPS01234776](https://openairdocs.org/sdr/UPS01234776.md): Pitot Tube · damaged · Jan 26, 2001 · N928UP · Boeing 72722C · Pitot/Static System
  > INSPECTION TYPE:IN AT FL 33.0 CAPTS ALT 33,000 FT F/OS ALT 32820 FT CAPTS A/S 296 KNOTS F/OS A/S 294.5. STANDBY ALT 33,200. TESTED CAPT AND FO ALT PER MM 34-12-05. TESTS GOOD. TESTED CAPT AND FO MACH A/S PER MM 34-12-06. TESTS GOOD F/OS PITOT TUBE DAMAGED
- [SDR UPS01234762](https://openairdocs.org/sdr/UPS01234762.md): Heat Exchanger · leaking · Jan 17, 2001 · N928UP · Boeing 72722C · Hydraulic System, Main
  > INSPECTION TYPE:C, RT WING HYDRAULIC HEAT EXCHANGER LEAKING HYD FLUID INTO NR 3 TANK. ACCOMPLISHED RIGHT WING HYDRAULIC COOLER ANTI-ROTATION PLATE REPLACEMENT IAW AVITAS ENGINEERING REPAIR ORDER AVHM-187RO-1.
- [SDR UPS01234765](https://openairdocs.org/sdr/UPS01234765.md): Frame · cracked · Jan 11, 2001 · N928UP · Boeing 72722C · Fuselage Main, Frame
  > INSPECTION TYPE:C, LEFT WHEEL WELL CASTING FRAME BS 930 SHOWS CRACK TO LOWER END STR 18L. INSTALLED REPAIR AT BS 930 CASTING FRAME IAW UPS EO B727-5310-2611B.
- [SDR UPS01234770](https://openairdocs.org/sdr/UPS01234770.md): Angle · cracked · Jan 3, 2001 · N928UP · Boeing 72722C · Leading Edge Devices
  > INSPECTION TYPE:C, RT WING NR 6 LE SLAT, I/B TRACK RECESS CUTOUT 2 ANGLES CRACKED, I/B AND O/B AT LWR END OF ANGLE. REMOVED AND REPLACED 2 ANGLES IAW SRM 57-10-2.
- [SDR UPS01234767](https://openairdocs.org/sdr/UPS01234767.md): Angle · cracked · Jan 3, 2001 · N928UP · Boeing 72722C · Leading Edge Devices
  > INSPECTION TYPE:C, RT WING NR 6 LE SLAT, O/B TRACK RECESS CUTOUT, I/B VERT ANGLE CRACKED AT LWR END. REMOVED AND REPLACED I/B VERT ANGLE IAW SRM 51-30-2.
- [SDR UPS01234764](https://openairdocs.org/sdr/UPS01234764.md): Skin · bulged · Jan 3, 2001 · N928UP · Boeing 72722C · Cargo/Baggage Doors
  > INSPECTION TYPE:C, MAIN CARGO DOOR OUTER SKIN BULGING AT BS 610, STR 4L. INSTALLED DOUBLER REPAIR IAW 52-30-01.
- [SDR UPS01234763](https://openairdocs.org/sdr/UPS01234763.md): Skin · bulged · Jan 3, 2001 · N928UP · Boeing 72722C · Cargo/Baggage Doors
  > INSPECTION TYPE:C, MAIN CARGO DOOR OUTER SKIN BULGED AT BS 490, STR 4 LEFT. INSTALLED REPAIR AT MAIN CARGO DOOR SKIN IAW SRM 52-30-01.
- [SDR UPS01234772](https://openairdocs.org/sdr/UPS01234772.md): Skin · bulged · Jan 2, 2001 · N928UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, SKIN BULGING AT STR 2L, STA 441. ACCOMPLISHED REPAIR IAW UPS EO B727-5310-1371E.
- [SDR UPS01234771](https://openairdocs.org/sdr/UPS01234771.md): Skin · cracked · Jan 2, 2001 · N928UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, NOSE LANDING GEAR WHEEL WELL TOP CEILING BS 272, LBL 15 SHOWS CRACK RUNNING BETWEEN RIVETS, ABOUT 2.5 INCHES LONG. INSTALLED DOUBLER REPAIR IAW SRM 51-40-2.
- [SDR UPS01234766](https://openairdocs.org/sdr/UPS01234766.md): Skin · bulged · Jan 2, 2001 · N928UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, SKIN BULGING BETWEEN STR 5R AND STR 6R AT STA 481. INSTALLED REPAIR DOUBLER IAW UPS EO B727-5310-1371E.
- [SDR UPS01234759](https://openairdocs.org/sdr/UPS01234759.md): Pressure Panel · cracked · Jan 2, 2001 · N928UP · Boeing 72722C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C CK, NLG W/W RIGHT SIDEWALL BS272 LWR OF AFT ACCESS DOOR CRACK INDICATION RUNNING BETWEEN FASTENER ROW, 1.5 INCH LONG. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 51-40-2.
- [SDR UPS01234758](https://openairdocs.org/sdr/UPS01234758.md): Pressure Panel · cracked · Jan 2, 2001 · N928UP · Boeing 72722C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C CK, NLG W/W LT SIDEWALL BS 243 TO LWR SHOWED CRACK AROUND FASTENER, ABOU T 1 INCH LONG. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 51-40-2.
- [SDR UPS01234757](https://openairdocs.org/sdr/UPS01234757.md): Pressure Panel · cracked · Jan 2, 2001 · N928UP · Boeing 72722C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C CK, NLG W/W TOP CEILING RBL 15 AND BS 272 CRACK INDICATION ALONG FASTENER ROW ABOUT 2.5 INCHES LONG. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 51-40-2.
- [SDR UPS01234756](https://openairdocs.org/sdr/UPS01234756.md): Pressure Panel · cracked · Jan 2, 2001 · N928UP · Boeing 72722C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C CK, NLG W/W RIGHT SIDEWALL BS 251 AFT OF FWD ACCESS DOOR, CRACK INDICATION ALONG FASTENERS ROW, ABOUT 4.5 INCHES. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 51-40-2.
- [SDR UPS01234755](https://openairdocs.org/sdr/UPS01234755.md): Pressure Panel · cracked · Jan 2, 2001 · N928UP · Boeing 72722C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C CK, NOSE LANDING GEAR WHEEL WELL SIDEWALL RIGHT BS 290 TO LWR HAS CRACK INDICATION MIGRATING FROM PREVIOUS REPAIR ABOUT 1 INCH LONG. INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH SRM 51-40-2.
- [SDR UPS01234761](https://openairdocs.org/sdr/UPS01234761.md): Skin · bulged · Dec 31, 2000 · N928UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, BULGE IN SKIN AT STA 260 LEFT WL 270. REPAIRED PER UPS EO B727-5310-1371E.
- [SDR UPS01234753](https://openairdocs.org/sdr/UPS01234753.md): Support Bracket · cracked · Dec 29, 2000 · N928UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CK, LEFT WHEEL WELL STA 913 UPLOCK SUPPORT ASSY, CRACK AT AFT SUPPORT FRAME. CRACK VERIFIED BY NDT. REPAIRED STA 913 SUPPORT FRAME IN ACCORDANCE WITH UPS EO B727-5310- 1896B, KIT INSTALLED. (P/N 65C-27194-25).
- [SDR UPS01234760](https://openairdocs.org/sdr/UPS01234760.md): Skin · bulged · Dec 26, 2000 · N928UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C CK, FUSELAGE AFT RIGHT BS 1333 STR 8R TO STR 10R, SKIN BULGE AND FASTENERS PULLING THROUGH. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 54-30-3 FIG 7.
- [SDR UPS00232079](https://openairdocs.org/sdr/UPS00232079.md): Light · inoperative · Mar 22, 2000 · N928UP · Boeing 72722C · Emergency Lighting
  > EXIT LIGHT OVER COCKPIT DOOR INOPERATIVE. CANIBALIZED EMERGENCY LIGHT ASSY FROM AIRCRAFT 907 OPS CHECKED GOOD.
- [SDR UPS99231048](https://openairdocs.org/sdr/UPS99231048.md): Light · missing · Nov 4, 1999 · N928UP · Boeing 72722C · Emergency Lighting
  > INSPECTION TYPE:N/A, FWD ENTRY DOOR EMERGENCY EXIT LIGHT ROBBED FOR ACFT 910. INSTALLED FWD ENTRY DOOR EMERGENCY EXIT LIGHT, OPS CHECK GOOD.
- [SDR UPS99230117](https://openairdocs.org/sdr/UPS99230117.md): Duct · cracked · Jul 9, 1999 · N928UP · Boeing 72722C · Engine Anti-Icing System
  > INSPECTION TYPE:C, ENGINE NR 3 ANTI-ICE DUCT CRACKED AT BRACKET NEAR ANTI-ICE VALVE. DUCT REPAIRED PER SMRO EO 99-17-005 (UPS ENGINEERING FILE NR 727-30- 0009).
- [SDR UPS99230116](https://openairdocs.org/sdr/UPS99230116.md): Skin · delaminated · Jul 9, 1999 · N928UP · Boeing 72722C · Rudder, Tab Structure
  > INSPECTION TYPE:C, RUDDER LOWER TAB DELAMINATED AT UPPER T/E LEFT SIDE PREVIOUS REPAIR. REPAIRED IAW SRM 51-40-10 FIG 3.
- [SDR UPS99230107](https://openairdocs.org/sdr/UPS99230107.md): Clevis · cracked · Jul 9, 1999 · N928UP · Boeing 72722C · Nacelle/Pylon Structure
  > INSPECTION TYPE:C, ENGINE NR 2 STRUTS ABOVE NR 2 HORIZONTAL FIRE WALL, CLEVIS CRACKED ON LOWER END OF LOWER STRUT. CLEVIS REPLACED IAW DWG 65-17553.
- [SDR UPS99230120](https://openairdocs.org/sdr/UPS99230120.md): Balance Panel · corroded · Jul 8, 1999 · N928UP · Boeing 72722C · Elevator Structure
  > INSPECTION TYPE:C, NR 5 ELEVATOR BALANCE PANEL RT HAS EVIDENCE OF CORROSION ON PANEL TO HINGE ATTACH RACK. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-6. BALANCE PANEL REPLACED AND INSTALLED IAW MM 27-30-21.
- [SDR UPS99230106](https://openairdocs.org/sdr/UPS99230106.md): Web · corroded · Jul 8, 1999 · N928UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, CORROSION ON SHEAR WEB LBL 24.75 STA 1130-1183. WEB REPAIRED IAW SRM 51-40-2.
- [SDR UPS99230124](https://openairdocs.org/sdr/UPS99230124.md): Angle · cracked · Jul 7, 1999 · N928UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, FLOOR SUPPORT CRACKED BS 850 LBL 45.5. FLOOR SUPPORT ANGLE REPAIRED IAW SRM 57-20-1.
- [SDR UPS99230119](https://openairdocs.org/sdr/UPS99230119.md): Mount · corroded · Jul 7, 1999 · N928UP · Boeing 72722C · Engine Mount Section
  > INSPECTION TYPE:C, CORROSION FOUND ON NR 1 ENG, FWD MOUNT HOLE AFT I/B HOLE ONLY (PITTING CORROSION). INVESTIGATED AND REPAIRED IAW SMRO EO 99-17-002 UPS ENGINEERING FILE NR 727-54-0088.
- [SDR UPS99230118](https://openairdocs.org/sdr/UPS99230118.md): Mount · corroded · Jul 7, 1999 · N928UP · Boeing 72722C · Engine Mount Section
  > INSPECTION TYPE:C, CORROSION FOUND ON NR 3 ENG FWD MOUNT HOLES AT TRUNNION FITTING ATTACH (PITTING CORROSION). REPAIRED IAW SRMO EO 99-17-003 (UPS ENGINEERING FILE NR 727-54-0089).
- [SDR UPS99230103](https://openairdocs.org/sdr/UPS99230103.md): Rib · cracked · Jul 7, 1999 · N928UP · Boeing 72722C · Leading Edge Devices
  > INSPECTION TYPE:C, NR 6 SLAT RIB AT IB SIDE OF ACTUATOR HAS SMALL CRACK IN FWD LOWER RADIUS. RIB REPAIRED IAW SRM 57-50-3.
- [SDR UPS99230121](https://openairdocs.org/sdr/UPS99230121.md): Firewall Web · cracked · Jul 6, 1999 · N928UP · Boeing 72722C · Nacelle/Pylon, Bulkhead/Firewall
  > INSPECTION TYPE:C, STRUCTURE OVER NR 2 ENGINE HORIZ FIREWALL LEFT AND RIGHT WEBS AT BS 1376 ARE CRACKED. FABRICATED AND INSTALLED WEBS IAW DRG NR 65-17555.
- [SDR UPS99230110](https://openairdocs.org/sdr/UPS99230110.md): Stiffener · cracked · Jul 6, 1999 · N928UP · Boeing 72722C · Spoilers
  > INSPECTION TYPE:C, NR 4 SPOILER IB ATTACH VERTICAL LEG CRACKED VERTICAL STIFFENER. REPLACED IAW DWG 69-16201.
- [SDR UPS99230105](https://openairdocs.org/sdr/UPS99230105.md): Support · corroded · Jul 6, 1999 · N928UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, CORROSION FOUND ON AFT LT LAVATORY PARTITION SUPPORT ON FLOOR STRUCTURE BS 1140 LBL 24.75-LBL60. TOP HAT SECTION REPLACED IAW SRM 51-10-1.

Next page: https://openairdocs.org/deregistered/N928UP-2013-03-26/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 = 'N928UP' AND deregistration_id = 'N928UP-2013-03-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N928UP-2013-03-26/reports

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