# Service difficulty reports: N910UP, cancelled Aug 23, 2006

A list on [N910UP, cancelled Aug 23, 2006](https://openairdocs.org/deregistered/N910UP-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 2 · 97 reports

- [SDR UPS02238614](https://openairdocs.org/sdr/UPS02238614.md): Slat · cracked · Jun 12, 2002 · N910UP · Boeing 72727C · Leading Edge Devices
  > INSPECTION TYPE:AS NR 5 SLAT CRACKED OUTBOARD OF FENCE JUST OUTBOARD OF UPSTOP. REMOVED AND REPLACED NR 5 SLAT PER MM 27-81-11, RIG AND OPS CHECK GOOD.
- [SDR UPS02237507](https://openairdocs.org/sdr/UPS02237507.md): Battery · discharged · Jan 23, 2002 · N910UP · Boeing 72727C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERIES NOT CHARGED OVER MAIN ENTRY DOOR, PARTS ON F/E'S DESK LIGHT ASSY 10-0067-9. INSTALLED NEW BATTERIES.
- [SDR UPS01236392](https://openairdocs.org/sdr/UPS01236392.md): Stringer · cracked · Jul 9, 2001 · N910UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C END OF STRINGER 15 @ BS 676 LH IS CRACKED. REPAIR CARRIED OUT IAW 51-30-2 & 53-10-3
- [SDR UPS01236388](https://openairdocs.org/sdr/UPS01236388.md): Pressure Panel · cracked · Jul 6, 2001 · N910UP · Boeing 72727C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C CRACKS FOUND AT 2 FASTENER HOLES AT PRESSURE DECK UPPER SURFACE AT BS 880 - 890 RBL 23. REPAIR CARRIED OUT IAW DRAWING 65-89360 & SRM 53-10-9 & SRM 51-30-2.
- [SDR UPS01236386](https://openairdocs.org/sdr/UPS01236386.md): Frame · cracked · Jul 5, 2001 · N910UP · Boeing 72727C · Landing Gear Doors
  > INSPECTION TYPE: C, LT MLG WING DOOR (OUTER HALF) O/B DOOR FRAME AFT CORNER CRACKED. REPAIR CARRIED OUT IAW SRM 51-20-2 & SRM 51-40-3
- [SDR UPS01236385](https://openairdocs.org/sdr/UPS01236385.md): Strap · corroded · Jul 4, 2001 · N910UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, DURING RECTIFICATION OF CORROSION BETWEEN TEAR STRAP SKIN AT BS 680 S6L INDICATIONS OF SUSPECT CORROSION ALSO FOUND AT BS 660 S4L TO S3L AT TEAR STRAP. NEW TEAR STRAP INSTALLED IAW SRM 53-30-4.
- [SDR UPS01236387](https://openairdocs.org/sdr/UPS01236387.md): Intercostal · cracked · Jul 3, 2001 · N910UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CRACK ON INTERCOSTAL AT STR 17R AT BS 830 INTERCOSTAL REPLACED IAW SRM 51-30-1
- [SDR UPS01236283](https://openairdocs.org/sdr/UPS01236283.md): Structure · cracked · Jul 3, 2001 · N910UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C, SUSPECT CRACK AT FASTENER HOLE BS 474 STR 5R. REPAIR CARRIED OUT IAW SRM 53-30-3.
- [SDR UPS01236390](https://openairdocs.org/sdr/UPS01236390.md): Pressure Panel · cracked · Jul 2, 2001 · N910UP · Boeing 72727C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C, DURING NDT INSP OF RT MLG WHEEL WELL PRESSURE WEB CRACK WAS FOUND ON WEB AT BS 940 RBL 33 APPROX. REPAIR CRACKED OUT IAW SRM 51-10-01, 51-30-2 & DRAWING 659360.
- [SDR UPS01236389](https://openairdocs.org/sdr/UPS01236389.md): Rib · cracked · Jul 2, 2001 · N910UP · Boeing 72727C · Leading Edge Slat Control System
  > INSPECTION TYPE:C SUSPECT CRACK IN #6 SLAT RIB, O/B OF SLAT ACTUATOR. DAMAGED RIB REPAIRED IAW SRM 57-30-3
- [SDR UPS01236373](https://openairdocs.org/sdr/UPS01236373.md): Web · corroded · Jul 2, 2001 · N910UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C CORROSION ON CABIN FLOOR WEB FWD OF BS 1183 BLK OF BBL 12R ***CPCP*** WEB REPLACED IAW SRM 51-10-01
- [SDR UPS01236372](https://openairdocs.org/sdr/UPS01236372.md): Web · corroded · Jul 2, 2001 · N910UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, CORROSION ON CABIN FLOOR WEB FWD OF BS 1183 BLK AT BBL 15L. REPAIR CARRIED OUT IAW SRM 51-40-2.
- [SDR UPS01236371](https://openairdocs.org/sdr/UPS01236371.md): Strap · corroded · Jul 2, 2001 · N910UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, SUSPECT CORROSION AT TEAR STRAP LOCATION BS 580 S4R TO S3R. REPAIR CARRIED OUT IAW SRM 51-10-6, SRM 32-30-3.
- [SDR UPS01236369](https://openairdocs.org/sdr/UPS01236369.md): Skin · corroded · Jul 2, 2001 · N910UP · Boeing 72727C · Horizontal Stabilizer Structure
  > INSPECTION TYPE:C CORROSION OF RH STAB SKIN UPPER SURFACE & RIVET PULLED @ STAB STA 80 APPX FWD OF REAR SPAR. ***CPCP*** REPAIR CARRIED OUT IAW SRM 55-10-3.
- [SDR UPS01236281](https://openairdocs.org/sdr/UPS01236281.md): Stiffener · cracked · Jul 2, 2001 · N910UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C VERTICAL STIFFENER LOCATED IN AIRSTAIRS MANUAL PUMP CAVITY HAS A SUS PECT CRACK REPAIR CARRIED OUT IAW SRM 51-10-1, 51-20-1, 51-40-4
- [SDR UPS01236391](https://openairdocs.org/sdr/UPS01236391.md): Support Bracket · cracked · Jul 1, 2001 · N910UP · Boeing 72727C · Landing Gear System
  > INSPECTION TYPE:C BS 910 FRAM FWD FLANGE LWR CORNER SUPPORT BRACKET CRACKED. REPAIR CARRIED OUT IAW SRM 51-20-01, 51-30-2
- [SDR UPS01236370](https://openairdocs.org/sdr/UPS01236370.md): Support · corroded · Jul 1, 2001 · N910UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, RT MLG SUPPORT ANGLE CORRODED AT PRESSURE DECK SURFACE 2 AREAS, RBL 23 BS 880 TO 882. RT MLG SUPPORT ANGLE REPLACED IAW SRM 51-40-4.
- [SDR UPS01236308](https://openairdocs.org/sdr/UPS01236308.md): Lap Joint · corroded · Jul 1, 2001 · N910UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SUSPECT CORROSION AT LAP JOINT STA 1110 TO 1165 STR4L DAMAGE REAPIRED IAW B727-5330-0509 APPENDIX 8.3
- [SDR UPS01236282](https://openairdocs.org/sdr/UPS01236282.md): Lap Joint · corroded · Jul 1, 2001 · N910UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SUSPECT CORROSION AT LAP JOINT BS 1115 TO 1175 S4R REPAIR CARRIED OUT IAW SRM 51-30-2 & UPS EO B727-5330-0509 APPENDIX 8.3
- [SDR UPS01236368](https://openairdocs.org/sdr/UPS01236368.md): Strap · corroded · Jun 29, 2001 · N910UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, SUSPECT CORROSION AT TEAR STRAP LOCATION BS 560 S4R TO S3R. REPAIR CARRIED OUT IAW SRM 51-30-2 & SRM 32-30-3.
- [SDR UPS01236310](https://openairdocs.org/sdr/UPS01236310.md): Strap · corroded · Jun 29, 2001 · N910UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, SUSPECT CORROSION AT TEAR STRAP LOCATION BS 680 BETWEEN S6L AND S5L. DAMAGE REPAIRED IAW SRM PROCEDURES.
- [SDR UPS01235813](https://openairdocs.org/sdr/UPS01235813.md): Elevator · binding · May 2, 2001 · N910UP · Boeing 72727C · Elevator Control System
  > INSPECTION TYPE:N/A ELEVATORS BINDING AND MAKING A LOUD NOISE ***SUPPLEMENTAL MRR*** LUBED RUB STRIPS OPS CHECK GOOD.
- [SDR UPS01234902](https://openairdocs.org/sdr/UPS01234902.md): Smoke Detector · failed · Feb 3, 2001 · N910UP · Boeing 72727C · Smoke Detection
  > INSPECTION TYPE:IN LOWER CARGO SMOKE M208340, ALERT H19221. REMOVED AND REPLACED SMOKE DETECTION SYSTEM CONFIGURATION MODULE PER MM 26-18-01 AND OPS CHECKED SYSTEM PER MM 26-18-00 SYSTEM OPS CHECKS GOOD THIS CLEARS M208340 PLACARD REMOVED.
- [SDR UPS01234775](https://openairdocs.org/sdr/UPS01234775.md): Pitot Tube · clogged · Jan 26, 2001 · N910UP · Boeing 72727C · Pitot/Static System
  > INSPECTION TYPE:IN, ELEVATORS REQUIRE EXCESSIVE FORCE IN FWD/AFT DIRECTION. CLEARED PITOT BLOCKAGE IN FEEL COMPUTER SYSTEM AND CHANGED FILTERS IN A-SYSTEM MODULAR PACKAGE. BREAKAWAY FORCE CHECKS NORMAL IAW MM 27-30-00.
- [SDR UPS00234212](https://openairdocs.org/sdr/UPS00234212.md): Light · inoperative · Oct 19, 2000 · N910UP · Boeing 72727C · Emergency Lighting
  > INSPECTION TYPE:N/A, FWD ENTRY DOOR EMERGENCY LIGHT WILL NOT EXTINGUISH AUTOMATICALLY AFTER TEST OR SHUTDOWN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY, TESTS GOOD.
- [SDR UPS00233920](https://openairdocs.org/sdr/UPS00233920.md): Switch · out of adj · Oct 10, 2000 · N910UP · Boeing 72727C · Door Warning System
  > INSPECTION TYPE:N/A, CREW DECLARED EMERGENCY DUE TO AFT AIRSTAIR LIGHT ILLUMINATED IN FLIGHT. ADJUSTED AND OPS CK AIRSTAIR SWITCH PER MM 52-70-01 & 52-62-01.
- [SDR UPS00231510](https://openairdocs.org/sdr/UPS00231510.md): Gimbal · cracked · Jan 28, 2000 · N910UP · Boeing 72727C · Trailing Edge Flap Control System
  > INSPECTION TYPE:C, RIGHT I/B TRAILING EDGE FLAP, GIMBAL ELECTRIC ASSY, CRACKED AT NR 5 FLAP TRANSMISSION ATTACH POINT. GIMBAL REPLACED IAW MM 27-51-251, ADJUST/TEST CARRIED OUT IAW MM 27-51-22.
- [SDR UPS00231508](https://openairdocs.org/sdr/UPS00231508.md): Skin · corroded · Jan 25, 2000 · N910UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, BS 470 AT STR 7L RIVET PULLED RIVET TAIL. REMOVED IAW SRM 51-30-2. EVIDENCE OF CORROSION BETWEEN SKIN AND INTERNAL DOUBLER. FUSELAGE SKIN REPAIRED BETWEEN BS 440 AND BS 507 STR 2L TO 7L IAW SMRO EO NR 2000-002-05. UPS ENGINEERING FILE NR
- [SDR UPS00231504](https://openairdocs.org/sdr/UPS00231504.md): Stop · cracked · Jan 25, 2000 · N910UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, NR 5 FWD STOP ON AFT CARGO DOOR FOUND CRACKED. PART REPLACED IAW B727-5230-0032.
- [SDR UPS00231509](https://openairdocs.org/sdr/UPS00231509.md): Rib · cracked · Jan 21, 2000 · N910UP · Boeing 72727C · Ailerons
  > INSPECTION TYPE:C, RIGHT O/B AILERON L/E NOSE RIB NR 2 I/B OF TAB ACTUATING MECHANISM CRACKED. REPAIR CARRIED OUT IAW SRM 51-40-3, FASTENERS INSTALLED IAW SRM 51-30-2.
- [SDR UPS00231503](https://openairdocs.org/sdr/UPS00231503.md): Stop · cracked · Jan 20, 2000 · N910UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, SUSPECT CRACK ON NR 4 STOP FORWARD ON AFT CARGO DOOR (INTERNAL). HFEC INSPECTION CARRIED OUT IAW B727 NDTM PT 6, 51-00-00 FIG 4, CRACK CONFIRMED. NR 4 STOP REPLACED IAW EO B727-5230-0032, APPENDIX C.
- [SDR UPS00231502](https://openairdocs.org/sdr/UPS00231502.md): Support · corroded · Jan 20, 2000 · N910UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, SURFACE CORROSION ON UPPER SIDE OF TOILET PARTITION SUPPORT BS 330 APPROX RBL 20. CORROSION ON THE TOILET PARTITION SUPPORT REMOVED AND FOUND MUCH DEEPER AND OUTSIDE LIMITS. PARTITION SUPPORT REPLACED. FABRICATED FROM EXTRUSION BAC 1510-3
- [SDR UPS00231467](https://openairdocs.org/sdr/UPS00231467.md): Skin · delaminated · Jan 20, 2000 · N910UP · Boeing 72727C · Ailerons
  > INSPECTION TYPE:C, LT O/B AILERON DELAM ON UPPER AND LWR SKIN AT T/E O/B OF TAB. REPAIRED IAW SRM 51-40-6 FIG 39.
- [SDR UPS00231466](https://openairdocs.org/sdr/UPS00231466.md): Bracket · cracked · Jan 19, 2000 · N910UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, SUSPECT CRACK ON NLG MANUAL GEAR EXTENSION JACKSCREW LWR SUPPORT BRACKET ON RT SIDE OF W/W. REPLACED NLG MANUAL EXTENSION JACKSCREW LWR SUPPORT BRACKET ON RT SIDE OF W/W IAW SRM 51-30-2 AND DRAWING NR 65-21947.
- [SDR UPS00231465](https://openairdocs.org/sdr/UPS00231465.md): Channel · cracked · Jan 19, 2000 · N910UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, NLG LOCK ACTUATOR BULKHEAD CHANNEL SUPPORT CRACKED. REPAIRED NLG LOCK ACTUATOR CHANNEL SUPPORT IAW SRM 51-30-2 AND DRAWING NR 69-18194.
- [SDR UPS99231049](https://openairdocs.org/sdr/UPS99231049.md): Light · inop · Oct 3, 1999 · N910UP · Boeing 72727C · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT AT ENTRY DOOR INOP. REMOVED AND REPLACED EXIT LIGHT ASSY IAW 33-50-00.
- [SDR UPS99229518](https://openairdocs.org/sdr/UPS99229518.md): Battery Pack · discharged · May 5, 1999 · N910UP · Boeing 72727C · Emergency Lighting
  > INSPECTION TYPE:N/A, COCKPIT AND CABIN ENTRY EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN BOTH PACKS. LIGHTS OPS CHECK NORMAL.
- [SDR UPS98225454](https://openairdocs.org/sdr/UPS98225454.md): Airspeed Ind · malfunctioned · Jan 13, 1998 · N910UP · Boeing 72727C · Airspeed/Mach Indicator
  > INSPECTION TYPE-N/A, ON CLIMBOUT CAPTAINS AIRSPEED INDICATOR BEGAN DECREASING, FO'S AIRSPEED CONTINUED TO INCREASE. STBY AIRSPEED INDICATED ZERO CAPTAINS ALTIMETER SHOWED 2800 FT/FOS SHOWED 4000. CONTINUED ERRONEOUS INDICATION FOUND STATIC LEAK AT STBY ALT/A
- [SDR UPS97222271](https://openairdocs.org/sdr/UPS97222271.md): Skin · corroded · Mar 9, 1997 · N910UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE-SI, CORROSION ON SKIN 620-630 LBL 38 WL 291-307. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-30-1 REPAIRED IAW EWO 97-2045 UPS ENG FILE NR 727-53-1865 AND NON ROUTINE 497979.
- [SDR UPS97222270](https://openairdocs.org/sdr/UPS97222270.md): Strap · cracked · Mar 9, 1997 · N910UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-SI, LFEC INSP OF BEAR STRAP, AT BS 620, EXHIBIT CRACK INDICATIONS AT 6 FASTENERS (MARKED) BETWEEN STR 14L AND 15 L. REQUIRE FASTENER REMOVAL TO FACILITATE INVESTIGATION INSP. REPAIRED PER EWO 97-2055 UPS ENG FILE NR727-53-1863.
- [SDR UPS97222273](https://openairdocs.org/sdr/UPS97222273.md): Doubler · corroded · Mar 8, 1997 · N910UP · Boeing 72727C · Trailing Edge Flaps
  > INSPECTION TYPE-SI, CORROSION ON LOWER SKIN SURFACE AT NR 2 FLAP TRACK AFT ATTACH POINT. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 57-30-01, REPAIRED PER EWO 97-2044 UPS ENG FILE NR 727-57-1796.
- [SDR UPS97222272](https://openairdocs.org/sdr/UPS97222272.md): Skin · corroded · Mar 8, 1997 · N910UP · Boeing 72727C · Wing, Plate/Skin
  > INSPECTION TYPE-SI, WHILE WORKING CUST CARD 497867, FOUND CORROSION ON TOP OF SKIN ON FUEL TANK, STA 850-870 WL 191 LBL 50-65 MARKED. FOUND CORROSION TO BE OUT OF LIMITS, REPAIRED IAW EWO 97-2059 UPS ENG FILE NR727-57-1797.
- [SDR UPS97222179](https://openairdocs.org/sdr/UPS97222179.md): Stringer · corroded · Feb 27, 1997 · N910UP · Boeing 72727C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE-SI, CORROSION ON STR 4 BS 310 TO 340 AND INTERCOSTAL ATTACH TO STRINGER. REMOVED CORROSION IAW SRM 51-10-6, REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED STR 4L AND INTERCOSTAL FROM STA 310 TO 340 IAW SRM 53-10-3, 53-10-4, 51-20-1, 51
- [SDR UPS97222178](https://openairdocs.org/sdr/UPS97222178.md): Chord · corroded · Feb 27, 1997 · N910UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CORROSION BS 740 UPPER CHORD SHOWS SIGNS OF CORROSION AT RBL 45 TO RBL 52 AND LBL 47 WL 200. CORROSION REMOVED REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPLACED UPPER CHORD FROM 32.75 TO 70.5 IAW TRAMCO EWO 97-2043 (UPS FILE B727-57-17
- [SDR UPS97222216](https://openairdocs.org/sdr/UPS97222216.md): Bearing Support · cracked · Feb 26, 1997 · N910UP · Boeing 72727C · Main Landing Gear Attach Section
  > INSPECTION TYPE:SI, NOTED CRACK INDICATION ON RT MLG FWD TRUNNION BEARING SUPPORT. REMOVED AND REPLACED RT MLG FWD TRUNNION BEARING SUPPORT IAW M/M 32-11-51.
- [SDR UPS97222274](https://openairdocs.org/sdr/UPS97222274.md): Spar Chord · corroded · Feb 25, 1997 · N910UP · Boeing 72727C · Wing Spar
  > INSPECTION TYPE-SI, WHILE WORKING CUST CARD 497867, FOUND LOWER CHORD BS 870, TO BE CORRODED. REMOVED CORRODED LOWER SPAR CHORD AT BS 870, INSTALLED A NEW SPAR CHORD IAW SRM 57-10-1, EWO 97-2050 UPS ENG FILE NR 727-57-1788.
- [SDR UPS97222177](https://openairdocs.org/sdr/UPS97222177.md): Spar Chord · corroded · Feb 25, 1997 · N910UP · Boeing 72727C · Wing Spar
  > INSPECTION TYPE-C, WHILE WORKING CUST CARD 497867 FOUND LOWER CHORD BS 870 TO BE CORRODED. REMOVED CORRODED LOWER SPAR CHORD AT BS 870 AND INSTALLED A NEW SPAR CHORD IAW SRM 57-10-1 AND EWO 97-2050.
- [SDR UPS97222138](https://openairdocs.org/sdr/UPS97222138.md): Stiffener · corroded · Feb 24, 1997 · N910UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-SI, CORROSION ON VERTICAL STIFFENER BS 259.5 WL 162 RBL 24. REMOVED CORROSION REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED VERTICAL STIFFENER AT BS 259.5 RBL 24 WL 162 IAW SRM 51-40-4.
- [SDR UPS97222137](https://openairdocs.org/sdr/UPS97222137.md): Beam · cracked · Feb 24, 1997 · N910UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-SI, WHILE WORKING NRC 497868 FOUND RBL 45 LONGITUDINAL BEAM LOWER CHORD CRACKED IN RADIUS STA 745 WL 204. REPLACED LONG BEAM LOWER CHORD AT RBL 45 STA 745 IAW SRM 51-10-1, 51-10-2, 51-30-2 AND BOEING DRAWING 65-34144.
- [SDR UPS97222103](https://openairdocs.org/sdr/UPS97222103.md): Skin · corroded · Feb 20, 1997 · N910UP · Boeing 72727C · Leading Edge Devices
  > INSPECTION SI-CHECK, NR 6 K-FLAP INNER SURFACE IS CORRODED UNDER FASTENER ON RIB 6 FROM OUTBOARD END. CORROSION REMOVED, REWORK OUT OF LIMITS IAW SRM 57-50-1. REMOVED AND REPLACED NR 6 K-FLAP IAW MM 27-81-01.

Next page: https://openairdocs.org/deregistered/N910UP-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 = 'N910UP' AND deregistration_id = 'N910UP-2006-08-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N910UP-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.