# Service difficulty reports: N922UP, cancelled Jan 8, 2008

A list on [N922UP, cancelled Jan 8, 2008](https://openairdocs.org/deregistered/N922UP-2008-01-08.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 4 · 173 reports

- [SDR UPS07249235](https://openairdocs.org/sdr/UPS07249235.md): Line · leaking · Feb 21, 2007 · N922UP · Boeing 72731C · Hydraulic System, Main
  > INSPECTION TYPE:N/A A-SYSTEM HYDRAULIC QUANTITY LOSS DURING FINAL APPROACH. NO EMERGENCY DECLARED. MX IS I/W REPLACING A LEAKING RETURN LINE. FOUND UNION LEAKING AT A SYSTEM PRESS LINE, REMOVED AND REPLACED UNION, LOCATED AND MARKED ON A AFT RIGHT STAIRWELL
- [SDR UPS07249102](https://openairdocs.org/sdr/UPS07249102.md): Light · inoperative · Feb 1, 2007 · N922UP · Boeing 72731C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. PERFORMED EMERGENCY LIGHT CHECK PER MM 33-50-01-5. NO DEFECT NOTED.
- [SDR UPS06247167](https://openairdocs.org/sdr/UPS06247167.md): Smoke Goggles · scratched · Jun 20, 2006 · N922UP · Boeing 72731C · Emergency Equipment
  > INSPECTION TYPE:N/A 2ND OBSERVER SMOKE GOGGLES BADLY SCRATCHED. REMOVED AND REPLACED 2ND OBSERVER SMOKE GOGGLES.
- [SDR UPS05245518](https://openairdocs.org/sdr/UPS05245518.md): Slat Track · corroded · Sep 13, 2005 · N922UP · Boeing 72731C · Leading Edge Devices
  > ON REMOVAL OF NR 6 SLAT I/B TRACK SKIN SUPPORT BRACKET, CORROSION ON TEE TRACK FOUND BENEATH BRACKET. NR 6 SLAT TRACK REPLACED IAW MM 27-81-11.
- [SDR UPS05245433](https://openairdocs.org/sdr/UPS05245433.md): Lap Joint · corroded · Sep 2, 2005 · N922UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C 2 BULGES FOUND ON LAP JOINT AT STRINGER 4R BS 1139. DAMAGED AREA CUT OUT IAW SRM 53-30-3 FIG 5 AND REPAIRED IAW SRM 53-30-3 FIG 5.
- [SDR UPS05245465](https://openairdocs.org/sdr/UPS05245465.md): Bushing · corroded · Sep 1, 2005 · N922UP · Boeing 72731C · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION TYPE:C NR 1 ENGINE FWD ENGINE MOUNT PITTING CORROSION IN BORE OF MOUNT HOLES (TW O/B HOLES). BUSHINGS REPLACED IAW SOPM 20-50-03 AND EO B727-5440-1592 APNDX-A.
- [SDR UPS05245466](https://openairdocs.org/sdr/UPS05245466.md): Rib · cracked · Aug 30, 2005 · N922UP · Boeing 72731C · Leading Edge Devices
  > INSPECTION TYPE:C-CRACK ON NR 8 SLAT O/B RIB AT I/B TRACK ATTACHMENT AREA. SLAT STOP DRILLED IAW AAAE EO 2005-081-004 REV 1 (UPS ENG FILE NR 727- 57-20133).
- [SDR UPS05245437](https://openairdocs.org/sdr/UPS05245437.md): Attach Fitting · cracked · Aug 28, 2005 · N922UP · Boeing 72731C · Wing, Attach Fittings
  > INSPECTION TYPE: C, CRACK IN ZEE SECTION ATTACHED TO FRAME AT BS 1050 LBL 21. Z-SECTION REPAIRED IAW SRM 51-40-4 FIG 2.
- [SDR UPS05245436](https://openairdocs.org/sdr/UPS05245436.md): Floorbeam · corroded · Aug 28, 2005 · N922UP · Boeing 72731C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C SURFACE CORRSION AT BS 1130 JOINT BETWEEN FLOORBEAM TOP AND CREASE WEB AT RBL 62. REPAIR PARTS FABRICATED IAW AAAE EO 2005-081-003 - UPS ENG FILE 72 7-53-20189. DOUBLER INSTALLED IAW SRM 51-30-02.
- [SDR UPS05245435](https://openairdocs.org/sdr/UPS05245435.md): Bulkhead · corroded · Aug 28, 2005 · N922UP · Boeing 72731C · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C, CORROSION ON LT WHEEL WELL BULKHEAD AT BS 870 - FWD FACE 25 INCH FROM O/B EDGE AND 20 INCH FROM BOTTOM EDGE. REPAIR CARRIED OUT IAW AAAE RO 2005-081-2 -UPS ENG FILE NUMBER 727-53 -20190.
- [SDR UPS05245442](https://openairdocs.org/sdr/UPS05245442.md): Shear Tie · cracked · Aug 27, 2005 · N922UP · Boeing 72731C · Wing Main, Frame Structure
  > INSPECTION TYPE:C SUSPECT CRACK IN CENTER TANK FRONT SPAR TO STIFFENER SHEAR TIE CLIP O/B AFT RADIUS LBL 25-08. SHEAR TIE CLIP REPLACED IAW 51-30-02.
- [SDR UPS05245470](https://openairdocs.org/sdr/UPS05245470.md): Flap Track · corroded · Aug 26, 2005 · N922UP · Boeing 72731C · Trailing Edge Flaps
  > INSPECTION TYPE:C-CORROSION ON NR 4 FLAP TRACK AFT MOUNT PAD CORROSION REMOVED IAW SOPM 20-10-01 P1 AND EO B727-5742-0651K & TEMPER ETCHED 2B (3) IAW SOPM 20-10-01. CAD PLATED IAW OHM 20-42-10.
- [SDR UPS05245469](https://openairdocs.org/sdr/UPS05245469.md): Flap Track · corroded · Aug 26, 2005 · N922UP · Boeing 72731C · Trailing Edge Flaps
  > INSPECTION TYPE:C-CORROSION FOUND ON FWD MOUNTING PAD OF NR 4 FLAP TRACK. CORROSION REMOVED IAW SOPM 20-10-01 P1 AND EO B727-5742-0651K. SURFACE TEMPER ETCHED 2B (3) IAW SOPM 20-10-01. CAD PLATED IAW OHM 20-42-10.
- [SDR UPS05245468](https://openairdocs.org/sdr/UPS05245468.md): Flap Track · corroded · Aug 26, 2005 · N922UP · Boeing 72731C · Trailing Edge Flaps
  > INSPECTION TYPE:C-CORROSION ON NR 4 FLAP TRACK FWD MOUNTING UPPER AND LWR, ALSO INNER RADIUS OF HOLES. CORROSION REMOVED IAW SOPM 20-10-01 P1 AND EO B727-5742-0651K AND TEMPER ETCHED IAW SOPM 20-10-01.
- [SDR UPS05245430](https://openairdocs.org/sdr/UPS05245430.md): Fitting · corroded · Aug 25, 2005 · N922UP · Boeing 72731C · Nose/Tail Landing Gear
  > INSPECTION TYPE:C CORROSION ON NLG TRUNNION FITTINGS LT AND RT. CORROSION REMOVED FROM LT & RT TRUNNION FITTINGS IAW SRM 53-40-01. NEW BUSHINGS FABRICATED AND INSTALLED IAW MM 53-40-01 AND 53-40-01 FIG 2.
- [SDR UPS05245467](https://openairdocs.org/sdr/UPS05245467.md): Stiffener · cracked · Aug 23, 2005 · N922UP · Boeing 72731C · Wing Miscellaneous Structure
  > INSPECTION TYPE:C-CRACK IN VERTICAL STIFFENER LT WING FRONT SPAR AT STA 557. STIFFENER REPLACED IAW SRM 51-30-2 AND DRW NR 65-16200.
- [SDR UPS05245431](https://openairdocs.org/sdr/UPS05245431.md): Channel · cracked · Aug 22, 2005 · N922UP · Boeing 72731C · Elevator Structure
  > INSPECTION TYPE:C SUPPORT CHANNEL CRACKED AT TOP END, JUST I/B OF RT ELEVATOR NR 1 HINGE BEAM, AFT OF ELEVATOR I/B INPUT ROD. CHANNEL FABRICATED IAW SRM 51-20-1 FIG 7. CHANNEL REPLACED IAW SRM 51-30-02.
- [SDR UPS05245434](https://openairdocs.org/sdr/UPS05245434.md): Stiffener · corroded · Aug 19, 2005 · N922UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C HORIZONTAL STIFFENER CORRODED IN CABIN AT BS 870 FWD SIDE, RBL 19. REPLACEMENT STIFFENER FABRICATE IAW SRM 51-20-10 AND DRAWING 65-23114. STIFFENER INSTALLED IAW SRM 51-30-02 AND DRAWING 65-16328.
- [SDR UPS05245526](https://openairdocs.org/sdr/UPS05245526.md): Fitting · leaking · Aug 17, 2005 · N922UP · Boeing 72731C · Aircraft Fuel Distribution System
  > INSPECTION TYPE: C+SI, FUEL LEAK FROM UNDERNEATH LT LANDING GEAR FWD TRUNNION SUPPORT SITTING SEEMS TO BE COMING FROM LWR LARGE BOLTS. LWR I/B FASTENERS (X2) REMOVED IAW TRUNNION REMOVED AND CORROSION FOUND SRM 51-30-02 AND BOTH HOLES REAMED TO 1ST OVERSIZE
- [SDR UPS03240253](https://openairdocs.org/sdr/UPS03240253.md): Structure · gouged · Mar 3, 2003 · N922UP · Boeing 72731C · Trailing Edge Flaps
  > INSPECTION TYPE: ASV, LEFT O/B TRAILING EDGE FLAP HAS A GOUGE AT LEADING EDGE O/B ATTACH POINT (I/B OF ATTACH POINT). INSTALLED REPAIR DOUBLER PER SRM 57-50-4 FIG 9. REMOVED AND REINSTALLED LEFT O/B TRAILING EDGE AFT FLAP TO FACILITATE REPAIR IAW MM 27-51-1
- [SDR UPS02238875](https://openairdocs.org/sdr/UPS02238875.md): Battery · discharged · Jul 22, 2002 · N922UP · Boeing 72731C · Emergency Lighting
  > INSPECTION TYPE:PFLT FORWARD ENTRY EMERGENCY EXIT LIGHT INOP. FORWARD ENTRY EMERGENCY EXIT LIGHT BATTERIES REPLACED. INSPECTED/TESTED SERVICEABLE IAW B727 MM 33-50-01.
- [SDR UPS02238038](https://openairdocs.org/sdr/UPS02238038.md): Trunnion · corroded · Apr 9, 2002 · N922UP · Boeing 72731C · Main Landing Gear Attach Section
  > INSPECTION TYPE:C LT MLG TRUNNION LINK FWD TRUNNION CORRODED. LT MLG TRUNNION LINK REPLACED IAW MM 32-11-01.
- [SDR UPS02238037](https://openairdocs.org/sdr/UPS02238037.md): Web · cracked · Apr 5, 2002 · N922UP · Boeing 72731C · Leading Edge Slat Control System
  > INSPECTION TYPE:C SUSPECT CRACK #4 SLAT RIB I/B OF ACTUATOR ROD END CARRIED OUT WEB REPAIR IAW SRM 51-40-2
- [SDR UPS02238036](https://openairdocs.org/sdr/UPS02238036.md): Flange · worn · Apr 4, 2002 · N922UP · Boeing 72731C · Fuselage Main, Structure
  > INSPECTION TYPE:C BS 1183 BULKHEAD THE AFT FLANGE OF HOIZ. STIFFENER P/N 65-16350-240 IS WORN AT LBL 32 APPROX DUE CHAFFING OFF HYDRAULIC PIPE FLANGE REPAIRED IAW SMRO EO 2002-015-001 UPS ENGINEERING FILE NO. 727-53-20048
- [SDR UPS02238048](https://openairdocs.org/sdr/UPS02238048.md): Skin · cracked · Apr 3, 2002 · N922UP · Boeing 72731C · Elevator Structure
  > INSPECTION TYPE:C R/H ELEVATOR SUSPECT CRACK IN ELEVATOR BEADED SKIN ELEV. STA. 130 AP PROX. REPAIR CARRIED OUT IAW SRM 51-30-2, 55-20-3, 51-40-5, 51-80-7
- [SDR UPS02238047](https://openairdocs.org/sdr/UPS02238047.md): Flap · cracked · Apr 3, 2002 · N922UP · Boeing 72731C · Leading Edge Devices
  > INSPECTION TYPE:C NR 5 L/E FLAP HAS CRACK AT I/B LOWER BONDING WIRE ATTACH POINT (BULLNOSE). REPAIR CARRIED OUT IAW SMRO EO 2002-015-002 UPS ENGINEERING FILE 727-57-20052.
- [SDR UPS02237744](https://openairdocs.org/sdr/UPS02237744.md): Engine · malfunctioned · Mar 1, 2002 · N922UP · Boeing 72731C · Engine (Turbine/Turboprop)
  > INSPECTION TYPE:N/A NR 3 ENGINE SHUT DOWN IN FLIGHT DUE TO LOW OIL PRESSURE (4 PSI). REPLACED ENGINE NR 3 IAW TC 1273 AND TC 1276. ENGINE RUN SATISFACTORY.
- [SDR UPS01237265](https://openairdocs.org/sdr/UPS01237265.md): Stop Fitting · cracked · Nov 10, 2001 · N922UP · Boeing 72731C · Cargo/Baggage Doors
  > INSPECTION TYPE:N/A AFT CARGO DOOR AFT NR 1 STOP FITTING CRACKED. AFT CARGO DOOR NR 1 STOP FITTING REPLACED IAW EO B727-5230-0032 APP C AND DRAWING 65-18625.
- [SDR UPS01235040](https://openairdocs.org/sdr/UPS01235040.md): Slide · out of position · Feb 23, 2001 · N922UP · Boeing 72731C · Emergency Equipment
  > INSPECTION TYPE:N/A, SLIDE FELL OUT OF CONTAINER. ITEM DEFFERRED IAW MEL 52-15, NOT REQUIRED FOR FLIGHT.
- [SDR UPS01235000](https://openairdocs.org/sdr/UPS01235000.md): Module · failed · Feb 13, 2001 · N922UP · Boeing 72731C · Hydraulic System, Main
  > INSPECTION TYPE:N/A ON CLIMBOUT OF WAW A-SYS HYD PRESS DROPPED TO ZERO. NO FLUID LOSS. INADVERTANT DEPLOYMENT OF NR 1 THRUST REVERSER ON TOUCH DOWN. REPLACED A-HYD SYS PRESSURE MODULE DEACTIVATED NR1 T-R PER MEL. SUSPECT OUT OF RIG.
- [SDR UPS01234619](https://openairdocs.org/sdr/UPS01234619.md): Battery · discharged · Jan 12, 2001 · N922UP · Boeing 72731C · Emergency Equipment
  > INSPECTION TYPE:N/A, FLASHLIGHT ON BULKHEAD AFT OF LAV NEEDS NEW BATTERIES. REMOVED AND REPLACED BATTERIES IN FLASHLIGHT REAR BULKHEAD TOILET COMPARTMENT. OPS CHECK SATISFACTORY.
- [SDR UPS01234600](https://openairdocs.org/sdr/UPS01234600.md): Light · inoperative · Jan 9, 2001 · N922UP · Boeing 72731C · Emergency Lighting
  > INSPECTION TYPE:N/A ON SHUTDOWN, DISCOVERED COCKPIT EMERGENCY EXIT LIGHT DOES NOT WORK- BULBS CHECK GOOD-EXTREMELY DIM WHEN SWITCHED TO ON POSITION - BATTERY APPEARS BAD R/R EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-50-00 OPS CHECK SATIS. PN/ OFF/ON 10-0067-
- [SDR UPS00233861](https://openairdocs.org/sdr/UPS00233861.md): Cargo Track · cracked · Sep 30, 2000 · N922UP · Boeing 72731C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C DURING 950 FITTING REPLACEMENT TIE DOWN ATTACH POINT AT FLOOR LEVEL ON BEAM AT BS 950 FOUND CRACKED. TIE DOWN REPLACED IAW SRM 51-30-2.
- [SDR UPS00233868](https://openairdocs.org/sdr/UPS00233868.md): Skin · corroded · Sep 28, 2000 · N922UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C ON REMOVAL OF S18A RT SECTION AND NR 1 INSP OF ALL ACCESSED FASTENER HOLES CORROSION AND SUSPECT CRACKS FOUND IN SKIN REPAIR CARRIED IAW SRM 51-10-6 AND SMRO EO 2000-036-003 UPS ENGINEERING FILE NR 727-53-2289.
- [SDR UPS00233867](https://openairdocs.org/sdr/UPS00233867.md): Stringer · corroded · Sep 28, 2000 · N922UP · Boeing 72731C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C, ON REMOVAL OF BODY FITTING 940 RT CORROSION FOUND ON LWR SURFACE OF STR 18 A AROUND FASTENER HOLES COMMON TO BS 940. REPAIR CARRIED OUT IAW SRM 51-30-2 UPS EO B727-5330-3815 & SMRO EO 2 000-036-003 UPS ENGINEERING FILE 727-53-2289.
- [SDR UPS00233865](https://openairdocs.org/sdr/UPS00233865.md): Stringer · cracked · Sep 27, 2000 · N922UP · Boeing 72731C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C, POSSIBLE CRACK INDICATION ON STR 15L, BS 1213 IN AFT AIRSTAIRS AREA. REPAIRED STRINGER IAW SRM 53-10-03 FIG 1.
- [SDR UPS00233862](https://openairdocs.org/sdr/UPS00233862.md): Casting · cracked · Sep 27, 2000 · N922UP · Boeing 72731C · Auxiliary Gear (Tail Skid)
  > INSPECTION TYPE:C TAIL SKID SUPPORT STRUCTURE IN TAIL SKID CAVITY AREA, UPPER CASTING TIE ROD, LEFT HAND SIDE, CASTING CRACKED BETWEEN TWO FASTENER HOLES. CASTING REPLACED IAW SRM 51-30-2.
- [SDR UPS00233860](https://openairdocs.org/sdr/UPS00233860.md): Rib · cracked · Sep 26, 2000 · N922UP · Boeing 72731C · Leading Edge Devices
  > INSPECTION TYPE:C SUSPECT CRACK NR 4 SLAT ACTUATOR O/B RIB PREVIOUS (AFT) RADIUS OF ANGLE. REPAIR CARRIED OUT IAW MM 27-81-32 SRM 51-40-02 & MM 27-81-32.
- [SDR UPS00233845](https://openairdocs.org/sdr/UPS00233845.md): Butt Joint · corroded · Sep 25, 2000 · N922UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, SUSPECT CORROSION AT BUTT JOINT BS 441, S5L. REPAIR CARRIED OUT IAW UPS EO B727-5310-1371 APPENDIX 8.5 AND BOEING DRAWING 69-62161.
- [SDR UPS00233837](https://openairdocs.org/sdr/UPS00233837.md): Fitting · corroded · Sep 25, 2000 · N922UP · Boeing 72731C · Nacelle/Pylon, Attach Fittings
  > INSPECTION TYPE:C, CORROSION EVIDENT IN NR 1 PYLON, ENG FWD MOUNT FITTING HOLES. REPAIR CARRIED OUT IAW UPS EO B727-5440-11592.
- [SDR UPS00233833](https://openairdocs.org/sdr/UPS00233833.md): Skin · cracked · Sep 25, 2000 · N922UP · Boeing 72731C · Leading Edge Devices
  > INSPECTION TYPE:C, NR 6 SLAT INNER SKIN CRACKED AROUND CTR FASTENER I/B OF ACTUATOR. REPAIRED INNER SKIN IAW UPS EO B727-5750-3082.
- [SDR UPS00233830](https://openairdocs.org/sdr/UPS00233830.md): Fitting · corroded · Sep 25, 2000 · N922UP · Boeing 72731C · Nacelle/Pylon, Attach Fittings
  > INSPECTION TYPE:C CORROSION EVIDENT IN NR 3 PYLON, ENG FWD MOUNT FITTING HOLES. REPAIR CARRIED OUT IAW EO B727-5440-11592
- [SDR UPS00233846](https://openairdocs.org/sdr/UPS00233846.md): Skin · corroded · Sep 22, 2000 · N922UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C ON INSP PER APPENDIX 8.2 SUSPECT MATERIAL LOSS OF 20 PERCENT AT BS 360 BETWEEN STR 23 & 24R. REPAIR CARRIED OUT IAW APPENDIX 8.5 UPS EO B727-5310-1371 AND DRAWING 69-62161.
- [SDR UPS00233831](https://openairdocs.org/sdr/UPS00233831.md): Frame · damaged · Sep 22, 2000 · N922UP · Boeing 72731C · Fuselage Main, Frame
  > INSPECTION TYPE:C ON INSP PER APPENDIX 8.2 SUSPECT MATERIAL LOSS OF 20 PERCENT AT BS 360 AND STR 21L. REPAIR CARRIED OUT IAW EO B727-5310-1371 APPENDIX 8.5.
- [SDR UPS00233834](https://openairdocs.org/sdr/UPS00233834.md): Beam · cracked · Sep 21, 2000 · N922UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, 3 CRACKS FOUND ON AFT PRESSURE BULKHEAD VERT BEAM BS 1183 RBL 26.83 AT WL 260 WEB. REPAIR CARRIED OUT IAW UPS EO B727-5311-0631 APPENDIX D.
- [SDR UPS00233832](https://openairdocs.org/sdr/UPS00233832.md): Beam · cracked · Sep 21, 2000 · N922UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CRACK FOUND ON AFT PRESSURE BULKHEAD VERTICAL BEAM BS 1183 LBL 26.83 AT WL 262 WEB. REPAIR CARRIED OUT IAW WITH UPS EO B727-5311-0631 APPENDIX D.
- [SDR UPS00233855](https://openairdocs.org/sdr/UPS00233855.md): Bolt · damaged · Sep 20, 2000 · N922UP · Boeing 72731C · Engine Mount Section
  > INSPECTION TYPE:C TO AID NDI REMOVE ENGINE NR 3 FWD AND AFT CRANE BEAM SHOULDER BOLTS. REPAIR CARRIED OUT IAW MM 71-21-03.
- [SDR UPS00233854](https://openairdocs.org/sdr/UPS00233854.md): Bolt · damaged · Sep 20, 2000 · N922UP · Boeing 72731C · Engine Mount Section
  > INSPECTION TYPE:C TO AID NDI REMOVE ENG NR 1 FWD & AFT CRANE BEAM SHOULDER BOLTS. REPAIR CARRIED OUT IAW MM 71-21-03.
- [SDR UPS00231260](https://openairdocs.org/sdr/UPS00231260.md): Light · inoperative · Jan 5, 2000 · N922UP · Boeing 72731C · Emergency Lighting
  > EMERGENCY EXIT LIGHT IN COCKPIT CAME LOOSE DURING TAXI.. REINSTALLED COCKPIT EMERGENCY EXIT LIGHT AND CHECKED LATCH SECURITY. TESTED PER MM 33-50-01, OPS CHECK GOOD.
- [SDR UPS99230277](https://openairdocs.org/sdr/UPS99230277.md): Retract Mech · inop · Aug 5, 1999 · N922UP · Boeing 72731C · Trailing Edge Flap Control System
  > FLAPS FAILED TO DEPLOY.

Next page: https://openairdocs.org/deregistered/N922UP-2008-01-08/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 = 'N922UP' AND deregistration_id = 'N922UP-2008-01-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N922UP-2008-01-08/reports

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