# Service difficulty reports: N943UP, cancelled May 10, 2007

A list on [N943UP, cancelled May 10, 2007](https://openairdocs.org/deregistered/N943UP-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 · 102 reports

- [SDR UPS02238317](https://openairdocs.org/sdr/UPS02238317.md): Intercostal · corroded · May 10, 2002 · N943UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C CORROAION ON INTERCOSTAL FROM BS 294.5 - BS 312 AT LBBL 40 APPROX INTERCOSTAL REPAIRED IAW SRM 51-40-3
- [SDR UPS02238306](https://openairdocs.org/sdr/UPS02238306.md): Flap Track · cracked · May 9, 2002 · N943UP · Boeing 72722C · Trailing Edge Flap Control System
  > INSPECTION TYPE:C RH WING #8 FLAP TRACK SAILBOAT FAIRING, O/B ROLLER GUIDE TRACK IS CR ACKED #8 FLAP TRACK FAIRING TRACK GUIDE REPLACED IAW SRM 51-30-02
- [SDR UPS02238319](https://openairdocs.org/sdr/UPS02238319.md): Skin · cracked · May 8, 2002 · N943UP · Boeing 72722C · Wing Structure
  > INSPECTION TYPE:C SUSPECT CRACK ON RH WING LE SKIN AT CUT OUT FOR NO 6 LE SLAT O/B SLA T HOOK REPAIR CARRIED OUT IAW 57-30-4 SRM
- [SDR UPS02238314](https://openairdocs.org/sdr/UPS02238314.md): Bracket · cracked · May 8, 2002 · N943UP · Boeing 72722C · Leading Edge Slat Actuator
  > INSPECTION TYPE:C, SUSPECT CRACKS ON NR 6 L/E FLAP ACTUATOR I/B & O/B ATTACH BRACKETS LWR FWD CORNERS. ATTACH BRACKETS FABRICATED IAW SRM 51-20-1 FIG 7, HEAT TREATMENT REF HT 02-27-03. BRACKETS INSTALLED IAW SRM 51-30-2 & DRAWING 65-16275.
- [SDR UPS02238313](https://openairdocs.org/sdr/UPS02238313.md): Hinge Fitting · cracked · May 7, 2002 · N943UP · Boeing 72722C · Aileron Control System
  > INSPECTION TYPE:C R/H O/B AILERON, 2ND HINGE FITTING FROM O/B HAS 2 SUSPECT CRACKS EMA NATING FROM BOTH UPPER FITTING FASTNER HOLES REPLACED R/H O/B AILERON FITTING IAW DRAWING 65-19259
- [SDR UPS02238289](https://openairdocs.org/sdr/UPS02238289.md): Bracket · cracked · May 7, 2002 · N943UP · Boeing 72722C · Elevator Control System
  > INSPECTION TYPE:C L/H ELEV. POSITION SENSOR LINKAGE ATTACHED TO FRONT SPAR OF ELEVATOR CRACKED. BRACKET OF POSITION SENSOR LINKAGE ATTACHED TO FRONT SPAR OF L/H ELE VATOR REPLACED IAW MM 20-80-01
- [SDR UPS02238318](https://openairdocs.org/sdr/UPS02238318.md): Rib · cracked · May 6, 2002 · N943UP · Boeing 72722C · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C, 3 SUPPORT RIBS CRACKED ON T/E PANEL BELOW NR 8 SPOILERS. RIBS REPLACED IAW SRM 51-30-2 & DRG 65-21656.
- [SDR UPS02238288](https://openairdocs.org/sdr/UPS02238288.md): Bracket · cracked · May 6, 2002 · N943UP · Boeing 72722C · Engine Thrust Reverser
  > INSPECTION TYPE:C #1 ENG. TR PRIMARY ACTUATOR FAIRING MID. ATTACH BRACKET CRACKED REPLACED BRACKET IAW SRM 51-30-02 & MM 20-80-01
- [SDR UPS02238287](https://openairdocs.org/sdr/UPS02238287.md): Bracket · cracked · May 6, 2002 · N943UP · Boeing 72722C · Engine Thrust Reverser
  > INSPECTION TYPE:C #3 ENG. TR PRIMARY ACTUATOR FAIRING MID ATTACH BRACKET CRACKED REPLACED BRACKET IAW SRM 51-30-02 & MM 20-80-01
- [SDR UPS02238304](https://openairdocs.org/sdr/UPS02238304.md): Beam · corroded · May 4, 2002 · N943UP · Boeing 72722C · Horizontal Stabilizer Structure
  > INSPECTION TYPE:C CORROSION ON RH STAB TE UPPER BEAM AT STAB STA. 115 TO 145 CORROSION REMOVED IAW SRM 51-10-06 FOUND TO BE OUTSIDE LIMITS HFEC C/O IAW B727 NDTM PT 6 51-00-00 - NDF BEAM REPAIRED IAW SMRO EO 2002-027-003 UPS ENGINEERING FILE NO. 727-53-200
- [SDR UPS02238292](https://openairdocs.org/sdr/UPS02238292.md): Beam · corroded · May 4, 2002 · N943UP · Boeing 72722C · Horizontal Stabilizer Miscellaneous Structure
  > INSPECTION TYPE:C, CORROSION ON LT STAB T/E UPPER BEAM AT STAB STA 155. CORROSION REMOVED IAW SRM 51-10-06 FOUND TO BE OUTSIDE LIMITS HFEC C/O IAW B727 NDTM PT 6 51-00-00 - NDF. REPAIR CARRIED OUT IAW SMRO EO 2002-027-008 UPS ENGINEERING FILE 727-55-20006.
- [SDR UPS02238291](https://openairdocs.org/sdr/UPS02238291.md): Beam · corroded · May 4, 2002 · N943UP · Boeing 72722C · Horizontal Stabilizer Miscellaneous Structure
  > INSPECTION TYPE:C CORROSION ON LT STAB T/E UPPER BEAM AT STAB STA 215. CORROSION REMOVED IAW SRM 51-10-06 FOUND TO BE OUTSIDE LIMITS HFEC C/O IAW B727 NDTM PT 6 51-00-00 - NDF. REPAIRED BEAM IAW EO 2002-027-006.
- [SDR UPS02238290](https://openairdocs.org/sdr/UPS02238290.md): Beam · corroded · May 4, 2002 · N943UP · Boeing 72722C · Horizontal Stabilizer Miscellaneous Structure
  > INSPECTION TYPE:C CORROSION ON RT STAB T/E BEAM (UPPER) AT STAB STA 205 AND STA 209. CORROSION REMOVED IAW SRM 51-10-06 & FOUND TO BE OUTSIDE LIMITS AFTER CORROSION REMOVAL HFEC CARRIED OUT IAW B727 NDT MANUAL PART 6, 51-00-00 - NDF. AREA ON RT STAB T/E BEA
- [SDR UPS02238321](https://openairdocs.org/sdr/UPS02238321.md): Lap Joint · corroded · May 2, 2002 · N943UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SUSPECT CORROSION AT LAP JOINT STR. 19R BS 650 REPAIR CARRIED OUT IAW SMRO EO 2002-027-002 UPS ENGINEERING FILE NO. 727-53-20053
- [SDR UPS02238316](https://openairdocs.org/sdr/UPS02238316.md): Tie · cracked · May 2, 2002 · N943UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C LWR BEAM TIE CRACKED IN E & E BAY BS 328 RBL 25. TYPICAL REPAIR CARRIED OUT IAW SRM 51-40-4.
- [SDR UPS02238315](https://openairdocs.org/sdr/UPS02238315.md): Tie · cracked · May 2, 2002 · N943UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C LWR BEAM TIE IN E&E BAY IS CRACKED BS 312 RBL 45. TYPICAL REPAIR CARRIED OUT IAW SRM 51-40-04.
- [SDR UPS02238312](https://openairdocs.org/sdr/UPS02238312.md): Trunnion · cracked · Apr 24, 2002 · N943UP · Boeing 72722C · Main Landing Gear Attach Section
  > INSPECTION TYPE:C SUSPECT CRACK RT MLG FWD TRUNNION FITTING AT I/B SUPPORT LEG O/B FLANGE FITTING. RT MLG FWD TRUNNION FITTING REPLACED IAW SMRO EO 2002-027-001R1 UPS ENGINEERING FILE 727-51-20054.
- [SDR UPS01236779](https://openairdocs.org/sdr/UPS01236779.md): Flap · corroded · Aug 27, 2001 · N943UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION TYPE:AD SUSPECT CORROSION BETWEEN SKIN MIDSPAR OF RT INBD MIDFLAP WBL130 APPROX. CORROSION FOUND TO BE OUT OF LIMITS, FLAP REPLACED IAW TC 1259
- [SDR UPS01236778](https://openairdocs.org/sdr/UPS01236778.md): Stop Fitting · cracked · Aug 25, 2001 · N943UP · Boeing 72722C · Cargo/Baggage Doors
  > INSPECTION TYPE:C CRACK FOUND ON DOOR STOP AT LWR AFT CORNER OF FWD PIT DOOR. REPLACED CRACKED FITTING IAW B727-5230-0032.
- [SDR UPS01234897](https://openairdocs.org/sdr/UPS01234897.md): Web · cracked · Jan 31, 2001 · N943UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, LT MLG WHEEL WELL, SUSPECT CRACKS IN KEEL BEAM WEB, AREA FWD OF APU CUTOUT COVERED BY REPAIR PLATE. REPAIR CARRIED OUT IAW EO B727-5330-1995-B.
- [SDR UPS01234895](https://openairdocs.org/sdr/UPS01234895.md): Stringer · corroded · Jan 31, 2001 · N943UP · Boeing 72722C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C, CORROSION ON STR 19 L AT BS 360 IN E & E BAY. STR 19L REPLACED IAW DRAWING 65-18420.
- [SDR UPS01234896](https://openairdocs.org/sdr/UPS01234896.md): Frame · cracked · Jan 29, 2001 · N943UP · Boeing 72722C · Fuselage Main, Frame
  > INSPECTION TYPE:C, RT MLG WHEEL WELL SUSPECT CRACK TO VERT CHORD AT BS 870 TO KEEL BEAM JOINT, 16.5 INCHES FROM BOTTOM OF CHORD. REPAIR CARRIED OUT IAW B727-5330-1995-B.
- [SDR UPS01234885](https://openairdocs.org/sdr/UPS01234885.md): Door Frame · cracked · Jan 29, 2001 · N943UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C, CRACK ON FWD LT CORNER OF FWD LWR NOSE ACCESS DOOR ON INNER LIP OF DOOR FRAME. REPAIR CARRIED OUT IAW SRM 51-40-3 FIG 1.
- [SDR UPS01234900](https://openairdocs.org/sdr/UPS01234900.md): Support Bracket · corroded · Jan 26, 2001 · N943UP · Boeing 72722C · Vertical Stabilizer
  > INSPECTION TYPE:C, VERT STAB, FAIRING SUPPORT AT JUNCTION OF TENSION TIE RIB AND VERT STAB FRONT SPAR IS WORN DUE TO FRETTING CORROSION LT. REPLACED FAIRING SUPPORT STRUCTURE IAW BOEING INST DRG 65-17485 & SRM 51-30-02.
- [SDR UPS01234903](https://openairdocs.org/sdr/UPS01234903.md): Jackscrew · corroded · Jan 25, 2001 · N943UP · Boeing 72722C · Trailing Edge Flap Control System
  > INSPECTION TYPE:C, NR 5 TRANSMISSION YOKE ASSY & JACKSCREW ARE BADLY CORRODED. JACKSCREW REPLACED IAW MM 27-51-41.
- [SDR UPS01234888](https://openairdocs.org/sdr/UPS01234888.md): Skin · cracked · Jan 25, 2001 · N943UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, CRACK IN FUSELAGE SKIN AT BS 243.7 LT. REPAIR CARRIED OUT IAW SRM 51-30-03.
- [SDR UPS01234887](https://openairdocs.org/sdr/UPS01234887.md): Stiffener · corroded · Jan 25, 2001 · N943UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, ON INSP HORIZ STIFFENER ON LWR BODY 740 FRAME FOUND CORRODED AT BBL 0. STIFFENER REMOVED IAW SRM 51-30-02, STIFFENER REPLACED IAW SRM 51-10-02.
- [SDR UPS01234886](https://openairdocs.org/sdr/UPS01234886.md): Flange · corroded · Jan 25, 2001 · N943UP · Boeing 72722C · Aerodynamic Fairings
  > INSPECTION TYPE:C, FAIRING 3608 AFT SUPPORT FRAME AFT FLANGE CORRODED. REPAIR CARRIED OUT IAW SRM 51-40-3 FIG 1.
- [SDR UPS01234894](https://openairdocs.org/sdr/UPS01234894.md): Frame · corroded · Jan 24, 2001 · N943UP · Boeing 72722C · Wing, Center Box
  > INSPECTION TYPE:C, RIVET POPPED AND EVIDENCE OF CORROSION ON WING CENTER SECTION REAR SPAR LWR CHORD BS 870. REPAIR CARRIED OUT IAW SRM 51-30-02 & SRM 51-20-4 AND DRAWING 65C215 66.
- [SDR UPS01234890](https://openairdocs.org/sdr/UPS01234890.md): Stringer · corroded · Jan 24, 2001 · N943UP · Boeing 72722C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C, CORROSION ON STR 18L AT BS 360. REPAIR CARRIED OUT IAW SRM 51-10-54 AND SRM 51-30-2.
- [SDR UPS01234884](https://openairdocs.org/sdr/UPS01234884.md): Structure · cracked · Jan 24, 2001 · N943UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C, SUSPECT CRACK IN UPPER LIGHTENING HOLE 6 O CLOCK POSITION BS 1300 LT. CRACK STOPPED DRILLED IAW SRM 51-10-1, CRACK FOUND TO BE WITHIN LIMITS.
- [SDR UPS01234893](https://openairdocs.org/sdr/UPS01234893.md): Structure · cracked · Jan 22, 2001 · N943UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, SUSPECT CRACK IN UPPER LIGHTENING HOLE 70 C POS BS 1243 LT AFT AIRSTAIRS AREA. REPAIR CARRIED OUT IAW SRM 51-10-1.
- [SDR UPS99230263](https://openairdocs.org/sdr/UPS99230263.md): Fairing · cracked · Jul 25, 1999 · N943UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION TYPE:C, NR 8 FLAP TRACK MID FAIRING INBOARD TRACK CRACKED. TRACK REPLACED IAW DRAWING 65-21796.
- [SDR UPS99230262](https://openairdocs.org/sdr/UPS99230262.md): Bracket · cracked · Jul 25, 1999 · N943UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION TYPE:C, NR 7 FLAP TRACK MID FAIRING AFT SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW DRAWING 65-21796.
- [SDR UPS99230261](https://openairdocs.org/sdr/UPS99230261.md): Fairing · cracked · Jul 25, 1999 · N943UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION TYPE:C, NR 7 FLAP TRACK MID FAIRING OUTBOARD TRACK CRACKED. TRACK REPLACED IAW DRAWING 65-21796.
- [SDR UPS99230260](https://openairdocs.org/sdr/UPS99230260.md): Bracket · cracked · Jul 25, 1999 · N943UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION TYPE:C, NR 1 FLAP TRACK MID FAIRING AFT SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-02 AND DRAWING 65-21796.
- [SDR UPS99230264](https://openairdocs.org/sdr/UPS99230264.md): Bracket · cracked · Jul 23, 1999 · N943UP · Boeing 72722C · Engine Thrust Reverser
  > INSPECTION TYPE:C, NR 3 ENGINE THRUST REVERSER FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-02 AND MM 78-30-00.
- [SDR UPS99230259](https://openairdocs.org/sdr/UPS99230259.md): Angle · cracked · Jul 22, 1999 · N943UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, CRACKED FRAME ANGLE AT FWD SIDE OF LATCH SUPPORT FITTING AT BS500 FWD CARGO BAY. FRAME ANGLE REPAIRED IAW SRM 53-10-4.
- [SDR UPS99230258](https://openairdocs.org/sdr/UPS99230258.md): Angle · cracked · Jul 22, 1999 · N943UP · Boeing 72722C · Wing Miscellaneous Structure
  > INSPECTION TYPE:C, RT WING TE PANEL OUTBOARD OF NR 7 FLAP TRACK, ATTACH ANGLE CRACKED. ANGLES REPLACED IAW SRM 51-30-2.
- [SDR UPS98225656](https://openairdocs.org/sdr/UPS98225656.md): Tee · cracked · Jan 30, 1998 · N943UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-D, CRACK ON ANGLE ABOVE NR 2 ENGINE HORIZONTAL FIREWALL AT STATION 1409 RT SIDE (NR 2 ENG AFT MOUNT SUPPORT RIB CHORD). SUPPORT RIB TEE CHORD REPLACED IAW DRAWING 65-22913 AND 65-17551.
- [SDR UPS98225654](https://openairdocs.org/sdr/UPS98225654.md): Skin · corroded · Jan 30, 1998 · N943UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE-D, SUSPECT CORROSION BETWEEN SKIN AND STRUCTURE AT BS 1115 BETWEEN S18R AND S19R. REPAIRED IAW SRS EO 98-01-025R1.
- [SDR UPS98225653](https://openairdocs.org/sdr/UPS98225653.md): Skin · corroded · Jan 30, 1998 · N943UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE-D, CORROSION BETWEEN INTERNAL STRUCTURE AND SKIN DOUBLER BS 1090 STR 18R. CORROSION REMOVED IAW SRM 51-10-6. REPAIR CARRIED OUT IAW SRS EO 98 -01-025 R1.
- [SDR UPS98225652](https://openairdocs.org/sdr/UPS98225652.md): Web · corroded · Jan 29, 1998 · N943UP · Boeing 72722C · Cargo/Baggage Doors
  > INSPECTION TYPE-D, ON FURTHER INSPECTION OF DAMAGED ANCHOR NUTS EXTRUSION WAS CORRODED AND WEB DAMAGED. REPLACED EXTRUSION WITH 65-24258-1 IAW DRAWING 65C33855.
- [SDR UPS98225650](https://openairdocs.org/sdr/UPS98225650.md): Casting · corroded · Jan 29, 1998 · N943UP · Boeing 72722C · Aileron Control System
  > INSPECTION TYPE-D, LT I/B AILERON TURNAROUND FITTING HAS CORROSION AROUND LOWER PULLEY MOUNT HOLE. CASTING REPLACED IAW SRM 51-10-1 AND MM 20-80-1.
- [SDR UPS98225636](https://openairdocs.org/sdr/UPS98225636.md): Bolt · corroded · Jan 29, 1998 · N943UP · Boeing 72722C · Cargo/Baggage Doors
  > INSPECTION TYPE-D, MAIN CARGO DOOR AFT HINGE BOLT ON PRESS RELIEF DOOR BADLY CORRODED. MAIN CARGO DOOR BOLT AND BUSHING REPLACED PER STANDARD PRACTICES 20- 50-01.
- [SDR UPS98225645](https://openairdocs.org/sdr/UPS98225645.md): Fitting · cracked · Jan 28, 1998 · N943UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-D, RT BS 740 FUSELAGE FITTING HAS NEW CRACK ON LOWER OUTBD WEB FLANGE (VERTICAL). FITTING REMOVED AND NEW FITTING INSTALLED PER UPS ENGINEERING ORDER B727-5310-7477C.
- [SDR UPS98225641](https://openairdocs.org/sdr/UPS98225641.md): Carriage · corroded · Jan 28, 1998 · N943UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION TYPE-D, NR 3 FLAP CARRIAGE IS CORRODED IN SPINDLE BORE AND AROUND LARGE BEARING. SEAT CARRIAGE REPLACED IAW OHM 57-58-01.
- [SDR UPS98225638](https://openairdocs.org/sdr/UPS98225638.md): Rear Spar · cracked · Jan 28, 1998 · N943UP · Boeing 72722C · Elevator Structure
  > INSPECTION TYPE-D, LT ELEVATOR HAS CRACKED REAR SPAR, CRACKED HINGE LUG, AND CRACKED LOWER SKIN. REPLACEMENT ELEVATOR INSTALLED IAW MM27-30-01.
- [SDR UPS98225629](https://openairdocs.org/sdr/UPS98225629.md): Tee · cracked · Jan 28, 1998 · N943UP · Boeing 72722C · Nacelle/Pylon Structure
  > INSPECTION TYPE-D, CRACK ON VERTICAL ANGLE ABOVE NR 2 ENGINE HORIZONTAL FIREWALL, LT SIDE AT STATION 1409 NR 2 ENGINE AFT MOUNT SUPPORT RIB CHORD. REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 98-01-012R1.
- [SDR UPS98225637](https://openairdocs.org/sdr/UPS98225637.md): Hinge Lug · cracked · Jan 27, 1998 · N943UP · Boeing 72722C · Elevator Structure
  > INSPECTION TYPE-D, RT ELEVATOR NR 3 HINGE LUG ES 66.50 CRACKED. HINGE LUG FITTING REPAIRED IAW SRS ENGINEERING ORDER 98-01-014.

Next page: https://openairdocs.org/deregistered/N943UP-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 = 'N943UP' AND deregistration_id = 'N943UP-2007-05-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N943UP-2007-05-10/reports

---
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