# Service difficulty reports: N908UP, cancelled Aug 23, 2006

A list on [N908UP, cancelled Aug 23, 2006](https://openairdocs.org/deregistered/N908UP-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 · 145 reports

- [SDR UPS02239857](https://openairdocs.org/sdr/UPS02239857.md): Cover · loose · Nov 4, 2002 · N908UP · Boeing 72727C · Emergency Lighting
  > INSPECTION TYPE:N/A MAIN ENTRY DOOR EMERGENCY LIGHT FELL OUT OF BRACKET DURING T/O. R&R MAIN ENTRY DOOR EMERGENCY LIGHT COVER OK FOR CONTINUED SERVICE.
- [SDR UPS01236690](https://openairdocs.org/sdr/UPS01236690.md): Stringer · cracked · Aug 16, 2001 · N908UP · Boeing 72727C · Wing Main, Frame Structure
  > INSPECTION TYPE:C SUSPECT CRACK IN CENTRE SECTION UPPER STRINGER S1 IN THE WING CENTRE TANK STRINGER REPAIRED IAW SRM 57-10-04 FIG 2
- [SDR UPS01236664](https://openairdocs.org/sdr/UPS01236664.md): Stringer · cracked · Aug 15, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C ON INSPECTION OF FUSELAGE STRINGERS AT BS 400 WHERE ACCESSABLE, S18R AT BS 400 FOUND TO BE CRACKED. STRINGER REPAIR CARRIED IAW SRM PROCEDURES
- [SDR UPS01236658](https://openairdocs.org/sdr/UPS01236658.md): Stringer · cracked · Aug 15, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C ON INSPECTION OF FUSELAGE STRINGERS AT BS 400 WHERE ACCESSABLE, STRI NGER 18R AT BS 400 FOUND TO BE CRACKED. STRINGER REPAIRED IAW SRM.
- [SDR UPS01236689](https://openairdocs.org/sdr/UPS01236689.md): Stiffener · corroded · Aug 13, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C WING CENTRE SECTION UPPER SKIN STIFFENER LWR CHORD IS CORRODED AT BS 870 RBL0. ***CPCP*** DAMAGED SECTION REMOVED AND NEW SECTION SPLICED IAW SRM
- [SDR UPS01236686](https://openairdocs.org/sdr/UPS01236686.md): Intercostal · cracked · Aug 13, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C SUSPECT CRACK AT R/H BS 1183 WL 230 OUTBD LWR CORNER OF INTERCOSTAL AT RBL 62.5 INTERCOSTAL REPLACED IAW DWG 65-16350
- [SDR UPS01236688](https://openairdocs.org/sdr/UPS01236688.md): Terminal · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Auxiliary Gear (Tail Skid)
  > INSPECTION TYPE:C L/H UPPER TENSION TIE CRACKED IN TAIL SKID BAY FABRICATED TERMINAL IAW DWG 65-85208, REMOVED / INSTALLED PER SRM
- [SDR UPS01236679](https://openairdocs.org/sdr/UPS01236679.md): Stringer · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON FURTHER INSPECTION S6L AT BS 400 FOUND TO BE CRACKED. DAMAGED STRINGER REPAIRED IAW SRM 53-10-3
- [SDR UPS01236678](https://openairdocs.org/sdr/UPS01236678.md): Stringer · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON FURTHER INSPECTION S3R FOUND CRACKED AT BS 400 REPAIRED PER SRM.
- [SDR UPS01236677](https://openairdocs.org/sdr/UPS01236677.md): Stringer · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON FURTHER INSPECTION S9R FOUND CRACKED AT BS 400 STRINGER REPAIRED IAW SRM.
- [SDR UPS01236676](https://openairdocs.org/sdr/UPS01236676.md): Stringer · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON FURTHER INSP FOR ACCESS S15R AT BS 400 FOUND TO BE CRACKED REPAIRED IAW SRM
- [SDR UPS01236675](https://openairdocs.org/sdr/UPS01236675.md): Stringer · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS S16R FOUND CRACKED AT BS 400 REPAIRED IAW SRM.
- [SDR UPS01236661](https://openairdocs.org/sdr/UPS01236661.md): Stringer · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS S15L FOUND CRACKED AT BS 400 REPAIRED IAW SRM
- [SDR UPS01236660](https://openairdocs.org/sdr/UPS01236660.md): Stringer · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS, S16L FOUND CRACKED AT BS 400 REPAIRED IAW SRM
- [SDR UPS01236657](https://openairdocs.org/sdr/UPS01236657.md): Stringer · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON FURTHER INSPECTION STRINGER S6R FOUND CRACKED AT BS 400 REPAIRED PER SRM
- [SDR UPS01236687](https://openairdocs.org/sdr/UPS01236687.md): Strap · cracked · Aug 10, 2001 · N908UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C ON NDT INSP, CRACK INDICATION FOUND IN REINFORCING STRAP OF MID GALLEY DOOR CUTOUT FWD UPPER CORNER. REPAIR CARRIED OUT PER UPS EO B727-5330-2695 APPENDIX 8.2
- [SDR UPS01236685](https://openairdocs.org/sdr/UPS01236685.md): Intercostal · cracked · Aug 10, 2001 · N908UP · Boeing 72727C · Standard Practices/Structures
  > INSPECTION TYPE:C INTERCOSTAL CRACKED ABOVE DRAG BRACE FITTING SUPPORT INTERCOSTAL REPLACED IAW DRWG 65-18417
- [SDR UPS01236666](https://openairdocs.org/sdr/UPS01236666.md): Frame · cracked · Aug 10, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C CRACK BS 930 R/H FLANGE I/B LOWER CORNER RADIUS REPAIRED PER SRM ADDENDUM B727-5310-2611B
- [SDR UPS01236684](https://openairdocs.org/sdr/UPS01236684.md): Skin · corroded · Aug 9, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C AREA OF LIGHT SURFACE CORROSION ON SKIN AT BS660 S19R ***CPCP*** AREA REPAIRED IAW APPENDIX 8.3 OF EO B727-5330-0509
- [SDR UPS01236681](https://openairdocs.org/sdr/UPS01236681.md): Skin · cracked · Aug 9, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SKIN CRACKS BS 400 BETWEEN S16R 15R REPAIRED IAW SRM
- [SDR UPS01236680](https://openairdocs.org/sdr/UPS01236680.md): Frame · corroded · Aug 9, 2001 · N908UP · Boeing 72727C · Aerodynamic Fairings
  > INSPECTION TYPE:C BODY FAIRING #3430 HAS CORRODED FRAME AT R/H GND FAN LOUVRE DOOR AFT CUTOUT. FRAME FABRICATED AND INSTALLED PER SRM
- [SDR UPS01236673](https://openairdocs.org/sdr/UPS01236673.md): Skin · cracked · Aug 9, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SKIN CRACKS BS 400 BETWEEN S16L AND 15L CRACKS REPAIRED IAW SRM
- [SDR UPS01235633](https://openairdocs.org/sdr/UPS01235633.md): Light · inoperative · Apr 18, 2001 · N908UP · Boeing 72727C · Emergency Lighting
  > EMERG EXIT LIGHT INOP. REPLACED BULB OP CHECKS GOOD
- [SDR UPS01235096](https://openairdocs.org/sdr/UPS01235096.md): Light · malfunctioned · Feb 27, 2001 · N908UP · Boeing 72727C · Emergency Lighting
  > INSPECTION TYPE:AS-E INFLIGHT, EMERGENCY EXIT LIGHTS ILLUMINATED FOR APPROX 2 MINUTES, THEN EXTINGUISHED. SWITCH WAS CHECKED TO BE IN ARMED THE ENTIRE TIME. UNABLE TO DUPLICATE PROBLEM. TESTED NORMAL PER MM 33-50-101.
- [SDR UPS01234802](https://openairdocs.org/sdr/UPS01234802.md): Skin · cracked · Jan 30, 2001 · N908UP · Boeing 72727C · Ailerons
  > INSPECTION TYPE:N/A, LT OUTBOARD AILERON HAS DELAMINATION AND.25 INCH CRACK AILERON REMOVED WD 66470 INSTALLED LT OUTBOARD AILERON TO STEP D (4) MM 27-10-31. OK FOR SERVICE.
- [SDR UPS01234586](https://openairdocs.org/sdr/UPS01234586.md): Battery · failed · Jan 3, 2001 · N908UP · Boeing 72727C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHT AT ENTRY DOOR INOP LIGHT SWITCH LEFT ON. REPLACED BATTERIES. OPS CK OK
- [SDR UPS00234560](https://openairdocs.org/sdr/UPS00234560.md): Transmitter · inoperative · Dec 21, 2000 · N908UP · Boeing 72727C · Trailing Flap Position Indicating System
  > INSPECTION TYPE:N/A DURING APPROACH INTO SDF FLAP EXTENSION OTBD FLAPS EXTENDED ASYMETRI CALLY RT AT APROX 1 DEG AND LT APROX 5 DEGS. RAN APPROPRIATE CK LIST AND LANDED. ***SUPPLEMENTAL*** REMOVED & REPLACED OTBD FLAP POS XMTR. CYCLED FLA P THRU FULL RANG
- [SDR UPS00232881](https://openairdocs.org/sdr/UPS00232881.md): Flap · malfunctioned · Jun 13, 2000 · N908UP · Boeing 72727C · Trailing Edge Flap Control System
  > INSPECTION TYPE:N/A, OUTBOARD FLAPS VERY SLOW TO RETRACT OUT OF CAE WOULD NOT EXTEND PAST 15 DEGREES AT ROA WITH NORMAL HYD FLAPS OPERATED NORMAL INTO CAE. A/C DID NOT LAND AT ROA, AIR TURNBACK TO CAE. REPAIRS IN PROGRESS AT CAE.
- [SDR UPS00231940](https://openairdocs.org/sdr/UPS00231940.md): Stringer · corroded · Feb 29, 2000 · N908UP · Boeing 72727C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C&SI, STR 24R BETWEEN BS 360 AND BS 259.5 IS CORRODED AT BS 277 AND END OF STRINGER AT BS 360 HAS CRACK FROM PREVIOUS STOP DRILL HOLE. STRINGER INSTALLED IAW BOEING DRG 65-18420.
- [SDR UPS00231974](https://openairdocs.org/sdr/UPS00231974.md): Skin · corroded · Feb 26, 2000 · N908UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C&SI, CORROSION ON SKIN BETWEEN BS 1080 AND BS 1183 STRINGER 4 RT TO STRINGER 10 RT. SKIN REMOVED IAW SRM 51-30-2. NEW SKIN DRILLED AND TRIMMED IAW SRM 51-30-2 AND DRG 65-18382. NEW SKIN INSTALLED IAW DRG 65-18382 AND SRM 51-30-2 AND 51-30-3
- [SDR UPS00231932](https://openairdocs.org/sdr/UPS00231932.md): Sill · corroded · Feb 24, 2000 · N908UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C&SI, CONTROL CABIN ENTRY DOOR SILL, STA 303.9, EVIDENCE OF CORROSION ON DOOR SILL BOTH UPPER AND LWR SURFACES AND BRACKET ON RT SIDE OF SILL CORRODED. CORROSION REMOVED IAW SRM 51-10-06, CORROSION FOUND TO BE WITHIN LIMITS OF SR 53-10-1 MAX D
- [SDR UPS00231949](https://openairdocs.org/sdr/UPS00231949.md): Lug · corroded · Feb 23, 2000 · N908UP · Boeing 72727C · Trailing Edge Flaps
  > INSPECTION TYPE:C&SI, CRACK ON ATTACH LUG OF FLAP POSITION TRANSMITTER HOUSING LEFT I/B FLAP CORRODED DRUM CRACKED HOUSING REPLACED IAW OHM 27-54-06.
- [SDR UPS00231880](https://openairdocs.org/sdr/UPS00231880.md): Flap Track · cracked · Feb 21, 2000 · N908UP · Boeing 72727C · Leading Edge Devices
  > INSPECTION TYPE:C&SI, NR 3 SLAT, O/B SLAT TRACK, O/B RIB ATTACH POINT HAS SUSPECT CRACK. REPAIR CARRIED OUT AS PER SRM 51-40-2.
- [SDR UPS00231879](https://openairdocs.org/sdr/UPS00231879.md): Bracket · cracked · Feb 18, 2000 · N908UP · Boeing 72727C · Nacelle/Pylon Structure
  > INSPECTION TYPE:C&SI, ENGINE NR 1 THROTTLE SHUT OFF CONTROL BRACKET ASSY IN FWD END OF PYLON IS CRACKED. BRACKET REPLACED IAW MM 76-11-21.
- [SDR UPS00231878](https://openairdocs.org/sdr/UPS00231878.md): Shear Tie · cracked · Feb 18, 2000 · N908UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C&SI, CRACK ON SHEAR TIE CLIP BETWEEN STIFEFNER AND UPPER CHORD AT FWD WALL OF CENTER TANK BS 740 AT LBL 45.61. CHANGED SHEAR TIE CLIP IAW EO B727-5710-4595.
- [SDR UPS00231976](https://openairdocs.org/sdr/UPS00231976.md): Lug · damaged · Feb 17, 2000 · N908UP · Boeing 72727C · Horizontal Stabilizer Structure
  > INSPECTION TYPE:C&SI, ULTRASONIC INSPECTION OF HORIZ STAB HINGE LUGS (ON VERT STAB) LT AND RT, I/B AND O/B DUE SUSPECT INDICATION FROM HFEC INSPECTION. ULTRASONIC INSPECTION CARRIED OUT BOTH LEFT AND RIGHT BORES REPAIRED IAW UPS EO B727-5510-2284.
- [SDR UPS00231975](https://openairdocs.org/sdr/UPS00231975.md): Lap Joint · corroded · Feb 16, 2000 · N908UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C&SI, SUSPECT CORROSION ON LAP JOINT AT BS 300 TO BS 320 STRINGER 24 RT. LAP REPAIRED IAW EO B727-5330-0509 AND SRM 53-30-15A.
- [SDR UPS00231939](https://openairdocs.org/sdr/UPS00231939.md): Stringer · crack · Feb 16, 2000 · N908UP · Boeing 72727C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C&SI, CRACK INDICATION FOUND AT BS 740 FWD LWR HOLE IN LINE WITH STR 16R. REPAIR CARRIED OUT IAW SMRO EO 2000-04-008 UPS ENGINEERING FILE NO 727-53-2231.
- [SDR UPS00231938](https://openairdocs.org/sdr/UPS00231938.md): Floorbeam · corroded · Feb 16, 2000 · N908UP · Boeing 72727C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C&SI, FWD CARGO LEFT FLOOR TRACK UPPER SURFACE CORRODED AT BS 482 ALSO CORROSION EVIDENT ADJACENT ANCHOR NUTS LWR SURFACE BS 480 - BS 540. FWD CARGO BAY LEFT FLOOR TRACK REPLACED FROM BS 480 TO 680 IAW SRM 51-30-2, 7 SRM 53-10-5 FIG 8.
- [SDR UPS00231936](https://openairdocs.org/sdr/UPS00231936.md): Skin · corroded · Feb 15, 2000 · N908UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C&SI, CORROSION ON WING CENTER SECTION UPPER SKIN AT BS 865 LBL 65.5. REPAIR CARRIED OUT IAW SMRO EO 200-004-004 UPS ENGINEERING FILE NR 727-57-2145.
- [SDR UPS00231935](https://openairdocs.org/sdr/UPS00231935.md): Mount · corroded · Feb 14, 2000 · N908UP · Boeing 72727C · Engine Mount Section
  > INSPECTION TYPE:C&SI, ON INSPECTION OF ENG NR 3 MOUNT HOLES CORROSION FOUND IN ALL HOLES. REPAIR CARRIED OUT IAW EO B727-5440-11592-A.
- [SDR UPS00231934](https://openairdocs.org/sdr/UPS00231934.md): Mount · corroded · Feb 14, 2000 · N908UP · Boeing 72727C · Engine Mount Section
  > INSPECTION TYPE:C&SI, ON INSPECTION OF ENG NR 1 MOUNT HOLES CORROSION FOUND IN ALL HOLES. REPAIR CARRIED OUT IAW EO B727-5440-11592-A.
- [SDR UPS00231995](https://openairdocs.org/sdr/UPS00231995.md): Flap Track · corroded · Feb 13, 2000 · N908UP · Boeing 72727C · Trailing Edge Flaps
  > INSPECTION TYPE:C&SI NR 4 FLAP TRACK CORROSION ON FACES OF FWD SUPPORT LUGS. REPAIR CARRIED OUT IAW SMRO EO 2000-004-10 UPS ENGINEERING FILE NR 727-57-2147.
- [SDR UPS00231876](https://openairdocs.org/sdr/UPS00231876.md): Seat Track · corroded · Feb 12, 2000 · N908UP · Boeing 72727C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C&SI, CORROSION ON SEAT TRACK UPPER FLANGE I/B AT BS 740 RBL 24.75. CORROSION REMOVED, LIMITS CHECKED AND FOUND OUTSIDE REF SRM 51-10-6. REPAIR CARRIED OUT IAW SRM 53-10-5.
- [SDR UPS00231931](https://openairdocs.org/sdr/UPS00231931.md): Carriage · corroded · Feb 11, 2000 · N908UP · Boeing 72727C · Wing, Control Surfaces
  > INSPECTION TYPE:C&SI, FLAP CARRIAGE NR 2 PITTING CORROSION IN BORE OF SPINDLE. CARRIAGE REPLACED IAW OHM 57-52-11..
- [SDR UPS00231875](https://openairdocs.org/sdr/UPS00231875.md): Flap Track · cracked · Feb 11, 2000 · N908UP · Boeing 72727C · Leading Edge Devices
  > INSPECTION TYPE:C&SI, NR 2 SLAT, I/B TRACK ATTACH POINT HAS SUSPECT CRACK. REPAIR CARRIED IAW SRM 51-40-2.
- [SDR UPS00231873](https://openairdocs.org/sdr/UPS00231873.md): Skin · corroded · Feb 11, 2000 · N908UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C&SI, SUSPECT CORROSION BETWEEN SKIN AND DOUBLER AT BS 1120 - BS 1140 BETWEEN STR 3R AND STR 4R. REPAIR CARRIED OUT IAW B727 NDM PT6 51-00-00 FIG 4 AND 5.
- [SDR UPS00231943](https://openairdocs.org/sdr/UPS00231943.md): Pin · corroded · Feb 10, 2000 · N908UP · Boeing 72727C · Wing Miscellaneous Structure
  > INSPECTION TYPE:C&SI, LEFT WING REAR SPAR TO BODY BOTTLE PIN HAS PITTING CORROSION ON FLANGE THAT SITS AGAINST SPAR TO BODY FITTING. BOTTLE PIN REPLACED IAW MM 57-41-01.
- [SDR UPS00231872](https://openairdocs.org/sdr/UPS00231872.md): Sill · cracked · Feb 10, 2000 · N908UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C&SI, SUSPECT CRACK ON MAIN CARGO DOOR SILL SKIN LWR SURFACE AT BS 488. MAIN CARGO DOOR SILL SKIN REPAIRED IAW SRM 51-40-2 FIG 1.
- [SDR UPS00231871](https://openairdocs.org/sdr/UPS00231871.md): Skin · corroded · Feb 10, 2000 · N908UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C&SI, SUSPECT CORROSION BETWEEN SKIN AND DOUBLER AT BS 1120 - BS 1140, BETWEEN STR 3R AND 4R. REPAIR CARRIED OUT IAW SRM 51-00-00.

Next page: https://openairdocs.org/deregistered/N908UP-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 = 'N908UP' AND deregistration_id = 'N908UP-2006-08-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N908UP-2006-08-23/reports

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