# Service difficulty reports: N906UP, cancelled May 10, 2007

A list on [N906UP, cancelled May 10, 2007](https://openairdocs.org/deregistered/N906UP-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 · 109 reports

- [SDR UPS03241659](https://openairdocs.org/sdr/UPS03241659.md): Light · inoperative · Dec 15, 2003 · N906UP · Boeing 72730C · Emergency Lighting
  > EMERGENCY EXIT LIGHT OVER FLIGHT DECK DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY, SYS GROUND CHECK GOOD.
- [SDR UPS02239970](https://openairdocs.org/sdr/UPS02239970.md): Angle · corroded · Dec 6, 2002 · N906UP · Boeing 72730C · Wing Miscellaneous Structure
  > INSPECTION TYPE:C SMALL AREA OF CORROSION NOTED IN R/H WING T/E STRUCTURE WS 383, ANGL E BETWEEN SUPPORT WEB & UPPER T/E SKIN REMOVED FASTNERS FROM CORRODED AREA AS PER SRM 51-30-02 & CUT AND TR IMMED ANGLE AS PER SRM 51-20-00. FABRICATED REPAIR PARTS IAW
- [SDR UPS02239964](https://openairdocs.org/sdr/UPS02239964.md): Skin · cracked · Dec 3, 2002 · N906UP · Boeing 72730C · Engine Thrust Reverser
  > INSPECTION TYPE:C ENGINE #1 THRUST REVERSER UPPER DOOR INNER SKIN CRACKED AT UPPER I/B CORNER OF LWR SKIN REPAIRED DAMAGED AREA IAW SRM 78-30-01 FIG 201
- [SDR UPS02239973](https://openairdocs.org/sdr/UPS02239973.md): Web · cracked · Dec 2, 2002 · N906UP · Boeing 72730C · Fuselage Main, Structure
  > INSPECTION TYPE:C SUSPECT CRACKS IN NOSE WHEEL WELL R/H WEB, JUST BELOW FWD END OF AFT PRESSURE PANEL REPAIR CARRIED OUT IAW SRM 51-40-2 & 51-30-2. REPAIR PARTS LEAK CEHC KED OK IAW MM 5-51-25
- [SDR UPS02239961](https://openairdocs.org/sdr/UPS02239961.md): Longeron · cracked · Dec 2, 2002 · N906UP · Boeing 72730C · Engine Cowl Flaps
  > INSPECTION TYPE:C ENG. #2 R/H FWD COWL CRACK ON UPPER LONGERON AT BS 1387 APPROX UNDER BLOCK(DOOR SHEAR) LONGERON REMOVED IAW SRM 51-30-02. NEW LONGERON FABRICATED IAW SRM 5 1-30-1 NEW LONGERON INSTALLED IAW SRM 51-30-02 & REPORTECTED IAW MM 51-20-01
- [SDR UPS02239960](https://openairdocs.org/sdr/UPS02239960.md): Longeron · cracked · Dec 2, 2002 · N906UP · Boeing 72730C · Nacelle/Pylon, Longeron/Stringer
  > INSPECTION TYPE: C, ENGINE NR 2, LT NACELLE. CRACK ON UPPER LONGERON AT BS 1387 APPROX UNDER BLOCK (DOOR SHEAR). LONGERON REMOVED IAW SRM 51-30-02. NEW LONGERON MANUFACTURED IAW SRM 51-20-1. NEW LOGERON INSTALLED IAW SRM 51-30-02 & RE-PROTECTED
- [SDR UPS02239965](https://openairdocs.org/sdr/UPS02239965.md): Skin · cracked · Nov 29, 2002 · N906UP · Boeing 72730C · Engine Thrust Reverser
  > INSPECTION TYPE:C ENG. #1 THRUST REVERSER, UPPER DOOR, INNER SKIN CRACKED AT I/B OF CE NTER OF LWR SKIN REPAIRED DAMAGED AREA IAW SRM 78-30-01 FIG 201
- [SDR UPS02239956](https://openairdocs.org/sdr/UPS02239956.md): Bracket · cracked · Nov 28, 2002 · N906UP · Boeing 72730C · Engine Thrust Reverser
  > INSPECTION TYPE: C, ENGINE NR 1 & 3 THRUST REVERSER OUTBOARD FAIRING MID SUPPORT BRACKETS CRACKED. REPLACED BRACKETS IAW MM 20-80-01
- [SDR UPS02239955](https://openairdocs.org/sdr/UPS02239955.md): Fitting · cracked · Nov 26, 2002 · N906UP · Boeing 72730C · Fuselage Main, Structure
  > INSPECTION TYPE:C L/H LWR TENSION TIE FITTING CRACKED AT O/B LUG IN TAILSKID COMPARTME NT INSTALLED NEW L/H LWR TENSION TIE FITTING IAW SRM 51-30-02 & DRAWING 65-25992
- [SDR UPS02239962](https://openairdocs.org/sdr/UPS02239962.md): Fitting · cracked · Nov 24, 2002 · N906UP · Boeing 72730C · Fuselage Main, Structure
  > INSPECTION TYPE:C TAILSKID BAY R/H UPPER TENSION TIE AFT FITTING CRACKED NEW R/H UPPER TENSION TIE AFT FITTING INSTALLED IAW SRM 51-30-02 AND DRAWING 65-25992
- [SDR UPS02239957](https://openairdocs.org/sdr/UPS02239957.md): Bulkhead · cracked · Nov 24, 2002 · N906UP · Boeing 72730C · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C, SUSPECT CRACKS IN NOSE WHEEL WELL BULKHEAD RT SIDE, BETWEEN FASTENER JUST UNDER CENTER OF FWD RT PRESSURE PANEL REPAIR CARRIED OUT IAW SRM 51-10-1 & SRM 51-40-2 FIG 2
- [SDR UPS02239954](https://openairdocs.org/sdr/UPS02239954.md): Fitting · cracked · Nov 24, 2002 · N906UP · Boeing 72730C · Fuselage Main, Structure
  > INSPECTION TYPE:C TAILSKID BAY L/H UPPER TENSION TIE AFT FITTING CRACKED L/H UPPER TENSION TIE REPLACED IAW SRM 51-30-02 & DRAWING 65-25992
- [SDR UPS02239953](https://openairdocs.org/sdr/UPS02239953.md): Fitting · cracked · Nov 24, 2002 · N906UP · Boeing 72730C · Fuselage Main, Structure
  > INSPECTION TYPE:C TAILSKID BAY RH LWR TENSION TIE AFT FITTING HAS EVIDENCE OF CRACK INSTALLED NEW R/H LWR TENSION TIE FITTING IAW SRM 51-30-02 & DRAWING 65-25992
- [SDR UPS02239974](https://openairdocs.org/sdr/UPS02239974.md): Structure · damaged · Nov 22, 2002 · N906UP · Boeing 72730C · Wing Main, Frame Structure
  > INSPECTION TYPE: C, RT LE, REMOVABLE SECTION, SOME SCREWS HAVE PULLED THROUGH ON UPPER SURFACE AT O/B END (INTERSECTION OF NR 6 KREUGER & NR 5 SLAT). REPAIR CARRIED OUT IAW SMRO EO 2002-057-003.
- [SDR UPS02239972](https://openairdocs.org/sdr/UPS02239972.md): Elevator · cracked · Nov 22, 2002 · N906UP · Boeing 72730C · Elevator Control System
  > INSPECTION TYPE:C X-RAY INSPECTION SHOWS A CRACK INDICATION ON THE LEFT ELEVATOR AT EL EV STA. 204, APPROX 5" FWD OF THE TRAILING EDGE REPAIR CARRIED OUT IAW SRM 51-30-02, 55-20-3, 51-40-5
- [SDR UPS02239971](https://openairdocs.org/sdr/UPS02239971.md): Pressure Panel · cracked · Nov 22, 2002 · N906UP · Boeing 72730C · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C, SUSPECT CRACKS ON RT VERTICAL WEB OF NOSE WHEEL WELL AT UPPER FWD EN D OF AFT PRESSURE PANEL. REPAIR CARRIED OUT IAW SRM 51-40-2
- [SDR UPS02239969](https://openairdocs.org/sdr/UPS02239969.md): Pressure Panel · cracked · Nov 22, 2002 · N906UP · Boeing 72730C · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C. SUSPECT CRACKS ON RT VERTICAL WEB OF NOSE WHEEL WELL IN AREA ADJACENT TO AFT LOWER CORNER OF AFT PRESS PANEL REPAIR PARTS FABRICATED IAW SRM 51-40-2 FIG 1. REPAIR PARTS PROTECTED AS PER SRM 51-10-02. REPAIR PARTS ASSEMBLED AND FASTNERS
- [SDR UPS02239963](https://openairdocs.org/sdr/UPS02239963.md): Elevator · cracked · Nov 22, 2002 · N906UP · Boeing 72730C · Elevator Control System
  > INSPECTION TYPE:C X-RAY INSP. SHOWS A CRACK INDICATION ON THE RIGHT ELEVATOR JUST I/B OF THE TAB AT ELEV. STA. 47, APPROX. REPAIR CARRIED OUT IAW SRM 51-30-2,51-10-1, 55-20-3, 51-40-5, 51-10- 2 & DRAWING 65-25638
- [SDR UPS02237691](https://openairdocs.org/sdr/UPS02237691.md): Light · unsecure · Feb 15, 2002 · N906UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:N/A L1 DOOR EMERGENCY EXIT LIGHT LENS COVER HANGING BY ONE END. FOUND FWD END OF EMERGENCY EXIT LIGHT ASSY NOT SECURED. SECURED LIGHT ASSY AND LENS. OPS CHECK GOOD.
- [SDR UPS02237393](https://openairdocs.org/sdr/UPS02237393.md): Lens · loose · Jan 5, 2002 · N906UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:AS PLASTIC LENS FOR ENTRY DOOR EMERGENCY EXIT LIGHT FALLS OFF. REPLACED LIGHT LENS.
- [SDR UPS02237389](https://openairdocs.org/sdr/UPS02237389.md): Battery · discharged · Jan 3, 2002 · N906UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:IN ENTRY DOOR EMERGENCY LIGHT INOP. INSTALLED NEW BATTERIES IN EMERGENCY EXIT LIGHT OVER ENTRY DOOR. OPS CHECK GOOD.
- [SDR UPS01236732](https://openairdocs.org/sdr/UPS01236732.md): Guard · inoperative · Aug 29, 2001 · N906UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:IN EMERGENCY EXIT LIGHTS SWITCH GUARD IS INOP; WHEN LIGHTS ARE TURNED ON TO TEST & GUARD IS CLOSED, LIGHTS REMAIN ON INSTEAD OF MOVING TO ARMED POSITION. R&R EMERGENCY EXIT LIGHT SWITCH GUARD. OPS CHECKS NORMAL. PERFORMED EMERGENCY EXIT LIGHT O
- [SDR UPS01235909](https://openairdocs.org/sdr/UPS01235909.md): Skin · cracked · May 15, 2001 · N906UP · Boeing 72730C · Leading Edge Devices
  > INSPECTION TYPE:C, CRACK ON ANTI-ICE SKIN NR 3 L/E FLAP I/B OF ACTUATOR ATTACH POINT. REPAIR CARRIED OUT IAW UPS EO B727-5750-3082.
- [SDR UPS01235978](https://openairdocs.org/sdr/UPS01235978.md): Web · cracked · May 11, 2001 · N906UP · Boeing 72730C · Leading Edge Devices
  > INSPECTION TYPE:C NR 3 SLAT ANTI ICE WEB IS CRACKED AT CUTOUT FOR ANTI ICE DUCT. REPAIRED IAW UPS AUTORIZATION B727-57-20028 AND SMRO EO 2001-016-006.
- [SDR UPS01235908](https://openairdocs.org/sdr/UPS01235908.md): Web · cracked · May 11, 2001 · N906UP · Boeing 72730C · Vertical Stabilizer
  > INSPECTION TYPE:C STRUCTURE ABOVE NR 2 ENGINE, WEB CRACKED AT BS 1388 APPROX RT SIDE. NEW WEB INSTALLED IAW SRM 51-30-02 & BOEING DRAWING 65-17555.
- [SDR UPS01235946](https://openairdocs.org/sdr/UPS01235946.md): Door Frame · cracked · May 10, 2001 · N906UP · Boeing 72730C · Cargo/Baggage Doors
  > INSPECTION TYPE:C, SUSPECT CRACK IN LWR AFT CORNER OF FWD CARGO DOOR FRAME. REPLACED LWR AFT CORNER OF FWD CARGO DOOR FRAME IAW DRAWING 65-18620.
- [SDR UPS01235979](https://openairdocs.org/sdr/UPS01235979.md): Fitting · cracked · May 9, 2001 · N906UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C NDI ON BS 950 RT FITTING CONFIRMED CRACK ON OUTBOARD FLANGE BETWEEN S9R AND 10R. RT 950 FRAME FITTING REPLACED IAW UPS EO B727-5310-3011.
- [SDR UPS01235975](https://openairdocs.org/sdr/UPS01235975.md): Beam · corroded · May 9, 2001 · N906UP · Boeing 72730C · Cargo/Baggage Doors
  > INSPECTION TYPE:C MCD UPPER BEAM AND UPPER BEAM DOUBLER CORRODED. DOOR REMOVED AND UPPER BEAM AND UPPER BEAM DOUBLER REPLACED.
- [SDR UPS01235968](https://openairdocs.org/sdr/UPS01235968.md): Strap · cracked · May 9, 2001 · N906UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CRACK INDICATIONS IN REINFORCING STRAP AT MID GALLEY DOOR FWD UPPER CORNER. REPAIR CARRIED OUT IAW UPS EO B727-5330-2685.
- [SDR UPS01235967](https://openairdocs.org/sdr/UPS01235967.md): Door Frame · cracked · May 9, 2001 · N906UP · Boeing 72730C · Service Doors
  > INSPECTION TYPE:C, CRACK ON AFT UPPER SECTION OF GALLEY DOOR FRAME. REPAIR CARRIED OUT IAW UPS EO B727-5240-4626.
- [SDR UPS01235953](https://openairdocs.org/sdr/UPS01235953.md): Stringer · corroded · May 8, 2001 · N906UP · Boeing 72730C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C, AREA OF SUSPECT CORROSION AT S4L BS 1185. REPAIR CARRIED OUT IAW SRM 51-30-2, 53-10-00, 51-30-4.
- [SDR UPS01235907](https://openairdocs.org/sdr/UPS01235907.md): Skin · damaged · May 8, 2001 · N906UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, FUSELAGE SKIN FOUND TO HAVE WEAR HOLE AT BS 1187 BETWEEN S24 LT & S26 LT SECT 48. REPAIR CARRIED OUT IAW SRM 53-30-3, 51-30-1, 51-20-00, 51-10-2.
- [SDR UPS01235877](https://openairdocs.org/sdr/UPS01235877.md): Bracket · cracked · May 7, 2001 · N906UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, WING TO BODY FAIRING ATTACH BRACKET BS 945 S18A LT CRACKED. NEW BRACKET FABRICATED
- [SDR UPS01235113](https://openairdocs.org/sdr/UPS01235113.md): Light · inoperative · Feb 28, 2001 · N906UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:PFLT, ON PREDEPT CK FOUND COCKPIT EMERGENCY EXIT ASSY INOP IN ARM OR ON. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSY, OPS CHECK OK.
- [SDR UPS01234996](https://openairdocs.org/sdr/UPS01234996.md): Light · inoperative · Feb 15, 2001 · N906UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:IN ON PREFLIGHT CHECK EMERGENCY EXIT LIGHT OVER COCKPIT DOOR WOULD NOT TEST WITH EMERGENCY EXIT LIGHT SWITCH ON O/H. LIGHTS WORK OK AT LIGHT ASSY W/SWITCH ON. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AT COCKPIT DOOR. OPS CHECK OK PER M
- [SDR UPS01234654](https://openairdocs.org/sdr/UPS01234654.md): Light · detached · Jan 19, 2001 · N906UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:PFLT CREW REPORTS MAIN ENTRY EMERGENCY EXIT LIGHT FELL OFF AT LANDING. REPLACED EMERGENCY EXIT LIGHT ASSY, OPS NORMAL.
- [SDR UPS00233348](https://openairdocs.org/sdr/UPS00233348.md): Generator · overheated · Jul 12, 2000 · N906UP · Boeing 72730C · Alternator-Generator Drive
  > INSPECTION TYPE:N/A, A/C DECLARED EMERGENCY WITH SMOKE IN THE COCKPIT WITH A CORRESPONDING TRIP ON THE NR 3 GENERATOR BREAKER. AIRCRAFT DIVERTED TO KMDT. MAINTENANCE FOUND THE NR 3 GENERATOR VOLTAGE REGULATOR VERY HOT AND A DOMINATE ELECTRICAL SMELL IN THE A
- [SDR UPS00232976](https://openairdocs.org/sdr/UPS00232976.md): Cartridge · out of adj · Jun 23, 2000 · N906UP · Boeing 72730C · Aileron Control System
  > INSPECTION TYPE:N/A ATB-AILERON BINDING T/S PER MM CHAPT 27-10-00 PG 102,106,AND 107 ADJUSTED AILERON SPRING CARTRIDGE PER MM 27-10-00 OPS CHECKS GOOD ***SUPPLEMENTAL MRR***
- [SDR UPS00231383](https://openairdocs.org/sdr/UPS00231383.md): Light · malfunctioned · Jan 21, 2000 · N906UP · Boeing 72730C · Emergency Lighting
  > L-1 DOOR EMERGENCY LIGHTS DIM. RESEATED L-1 DOOR EMERGENCY LIGHT PACK, LIGHT CHECKS NORMAL PER MM 3 3-50-01.
- [SDR UPS00231382](https://openairdocs.org/sdr/UPS00231382.md): Support · cracked · Jan 5, 2000 · N906UP · Boeing 72730C · Wing Miscellaneous Structure
  > INSPECTION TYPE:C LEFT WING FIXED LEADING EDGE CAVITY VERTICLE OUTBOARD SUPPORT IS CRACKED FOR THE NR 2 SLAT INBOARD TRACK, INBOARD SUPPORT RIB. REPLACED LEFT WING FIXED LEADING EDGE CAVITY VERTICAL OUTBOARD SUPPORT AS PER SRM 57-20-03 FIG 2. MATERIAL USED 7
- [SDR UPS99229358](https://openairdocs.org/sdr/UPS99229358.md): Engine · malfunctioned · Apr 15, 1999 · N906UP · Boeing 72730C · Engine (Turbine/Turboprop)
  > INSPECTION TYPE:N/A ON TEST FLIGHT, PERFORMED TEST EVENT SHUT DOWN OF NR 2 ENGINE. ENGINE NR 2 WAS THEN RESTARTED WITH ALL PARAMETERS NORMAL. MINUTES LATER AS NR 2 ENGINE WAS ADVANCED TO CRUISE SETTING, ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. PRECAUT
- [SDR UPS99228533](https://openairdocs.org/sdr/UPS99228533.md): Skin · corroded · Jan 22, 1999 · N906UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE-S, CORROSION BEYOND LIMITS FS 1080 STR 17R EXTERNAL FUSELAGE SKIN. REPAIRED IAW SRM 53-30-3.
- [SDR UPS99228322](https://openairdocs.org/sdr/UPS99228322.md): Light · inop · Jan 5, 1999 · N906UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT AT MAIN PAX DOOR INOP. RELAMPED, OPS CHECK GOOD.
- [SDR UPS98227289](https://openairdocs.org/sdr/UPS98227289.md): Floorbeam · corroded · Jul 31, 1998 · N906UP · Boeing 72730C · Fuselage Main, Floor Beam
  > INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON FLANGES OF LONGITUDINAL FLOORBEAM ON AND AT NUT PLATES BS 760 TO 848 LBL 45 WL 208. CORRODED PART OUT OF LIMITS. FABRICATED AND INSTALLED NEW REPAIR PARTS IAW SRM 51-30-2, 51-10-2, 51-20-21, 51-20-151, 51-3
- [SDR UPS98227283](https://openairdocs.org/sdr/UPS98227283.md): Bulkhead · corroded · Jul 31, 1998 · N906UP · Boeing 72730C · Fuselage Main, Bulkhead
  > INSPECTION TYPE-SI, CORROSION (C53-111-01.00-03) ON BS 1183 BULKHEAD RBL 15 WL 178. REMOVED CORROSION AND ACCOMPLISHED EO B727-5311-0635 WITH THE ADDITION OF EXTENDING THE RBL 8 BULKHEAD DOUBLER TO ENCOMPASS THE CORRODED AREA.
- [SDR UPS98227339](https://openairdocs.org/sdr/UPS98227339.md): Bracket · corroded · Jul 28, 1998 · N906UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SI, CORROSION AROUND EXPANSION LINK BRACKET. REPLACED BRACKET PER SRM 53-10-1.
- [SDR UPS98227337](https://openairdocs.org/sdr/UPS98227337.md): Seat Track · corroded · Jul 28, 1998 · N906UP · Boeing 72730C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:SI, SEAT TRACK CORRODED BS 760-785 RBL 25. REPLACED TRACK PER SRM 53-10-5.
- [SDR UPS98227284](https://openairdocs.org/sdr/UPS98227284.md): Skin · corroded · Jul 28, 1998 · N906UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE-SI, DISHED RIVETS AND PILLOWED SKIN STA 1120 TO 1150 LT 3 STR TO STR 4 LT AND 3 STR RT TO 4 STR RT. REPLACED SKIN PER EO 98-2608.
- [SDR UPS98227336](https://openairdocs.org/sdr/UPS98227336.md): Link · corroded · Jul 27, 1998 · N906UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SI, CORROSION ON EXPANSION LINK BS 870 RBL 25. REPLACED PER DRAWING 65-34144.
- [SDR UPS98227335](https://openairdocs.org/sdr/UPS98227335.md): Floorbeam · corroded · Jul 24, 1998 · N906UP · Boeing 72730C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:SI CORROSION ON FLANGES OF LONGITUDINAL FLOORBEAM. REPLACED PER DWG 65-34144.

Next page: https://openairdocs.org/deregistered/N906UP-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 = 'N906UP' AND deregistration_id = 'N906UP-2007-05-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N906UP-2007-05-10/reports

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