N922UP, cancelled Jan 8, 2008

Service difficulty reports · 173

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UPS07249235Line · leakingINSPECTION 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 STAIRWELLFeb 21, 2007 · N922UP · Boeing 72731C · Hydraulic System, MainSDR UPS07249102Light · inoperativeINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. PERFORMED EMERGENCY LIGHT CHECK PER MM 33-50-01-5. NO DEFECT NOTED.Feb 1, 2007 · N922UP · Boeing 72731C · Emergency LightingSDR UPS06247167Smoke Goggles · scratchedINSPECTION TYPE:N/A 2ND OBSERVER SMOKE GOGGLES BADLY SCRATCHED. REMOVED AND REPLACED 2ND OBSERVER SMOKE GOGGLES.Jun 20, 2006 · N922UP · Boeing 72731C · Emergency EquipmentSDR UPS05245518Slat Track · corrodedON 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.Sep 13, 2005 · N922UP · Boeing 72731C · Leading Edge DevicesSDR UPS05245433Lap Joint · corrodedINSPECTION 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.Sep 2, 2005 · N922UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS05245465Bushing · corrodedINSPECTION 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.Sep 1, 2005 · N922UP · Boeing 72731C · Nacelle/Pylon Miscellaneous StructureSDR UPS05245466Rib · crackedINSPECTION 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).Aug 30, 2005 · N922UP · Boeing 72731C · Leading Edge DevicesSDR UPS05245437Attach Fitting · crackedINSPECTION TYPE: C, CRACK IN ZEE SECTION ATTACHED TO FRAME AT BS 1050 LBL 21. Z-SECTION REPAIRED IAW SRM 51-40-4 FIG 2.Aug 28, 2005 · N922UP · Boeing 72731C · Wing, Attach FittingsSDR UPS05245436Floorbeam · corrodedINSPECTION 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.Aug 28, 2005 · N922UP · Boeing 72731C · Fuselage Main, Floor BeamSDR UPS05245435Bulkhead · corrodedINSPECTION 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.Aug 28, 2005 · N922UP · Boeing 72731C · Fuselage Main, BulkheadSDR UPS05245442Shear Tie · crackedINSPECTION 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.Aug 27, 2005 · N922UP · Boeing 72731C · Wing Main, Frame StructureSDR UPS05245470Flap Track · corrodedINSPECTION 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.Aug 26, 2005 · N922UP · Boeing 72731C · Trailing Edge FlapsSDR UPS05245469Flap Track · corrodedINSPECTION 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.Aug 26, 2005 · N922UP · Boeing 72731C · Trailing Edge FlapsSDR UPS05245468Flap Track · corrodedINSPECTION 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.Aug 26, 2005 · N922UP · Boeing 72731C · Trailing Edge FlapsSDR UPS05245430Fitting · corrodedINSPECTION 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.Aug 25, 2005 · N922UP · Boeing 72731C · Nose/Tail Landing GearSDR UPS05245467Stiffener · crackedINSPECTION 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.Aug 23, 2005 · N922UP · Boeing 72731C · Wing Miscellaneous StructureSDR UPS05245431Channel · crackedINSPECTION 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.Aug 22, 2005 · N922UP · Boeing 72731C · Elevator StructureSDR UPS05245434Stiffener · corrodedINSPECTION 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.Aug 19, 2005 · N922UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS05245526Fitting · leakingINSPECTION 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 Aug 17, 2005 · N922UP · Boeing 72731C · Aircraft Fuel Distribution SystemSDR UPS03240253Structure · gougedINSPECTION 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 27-51-1Mar 3, 2003 · N922UP · Boeing 72731C · Trailing Edge FlapsSDR UPS02238875Battery · dischargedINSPECTION TYPE:PFLT FORWARD ENTRY EMERGENCY EXIT LIGHT INOP. FORWARD ENTRY EMERGENCY EXIT LIGHT BATTERIES REPLACED. INSPECTED/TESTED SERVICEABLE IAW B727 MM 33-50-01.Jul 22, 2002 · N922UP · Boeing 72731C · Emergency LightingSDR UPS02238038Trunnion · corrodedINSPECTION TYPE:C LT MLG TRUNNION LINK FWD TRUNNION CORRODED. LT MLG TRUNNION LINK REPLACED IAW MM 32-11-01.Apr 9, 2002 · N922UP · Boeing 72731C · Main Landing Gear Attach SectionSDR UPS02238037Web · crackedINSPECTION TYPE:C SUSPECT CRACK #4 SLAT RIB I/B OF ACTUATOR ROD END CARRIED OUT WEB REPAIR IAW SRM 51-40-2Apr 5, 2002 · N922UP · Boeing 72731C · Leading Edge Slat Control SystemSDR UPS02238036Flange · wornINSPECTION 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. 727-53-20048Apr 4, 2002 · N922UP · Boeing 72731C · Fuselage Main, StructureSDR UPS02238048Skin · crackedINSPECTION 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, 51-80-7Apr 3, 2002 · N922UP · Boeing 72731C · Elevator StructureSDR UPS02238047Flap · crackedINSPECTION 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.Apr 3, 2002 · N922UP · Boeing 72731C · Leading Edge DevicesSDR UPS02237744Engine · malfunctionedINSPECTION 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.Mar 1, 2002 · N922UP · Boeing 72731C · Engine (Turbine/Turboprop)SDR UPS01237265Stop Fitting · crackedINSPECTION 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.Nov 10, 2001 · N922UP · Boeing 72731C · Cargo/Baggage DoorsSDR UPS01235040Slide · out of positionINSPECTION TYPE:N/A, SLIDE FELL OUT OF CONTAINER. ITEM DEFFERRED IAW MEL 52-15, NOT REQUIRED FOR FLIGHT.Feb 23, 2001 · N922UP · Boeing 72731C · Emergency EquipmentSDR UPS01235000Module · failedINSPECTION 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.Feb 13, 2001 · N922UP · Boeing 72731C · Hydraulic System, MainSDR UPS01234619Battery · dischargedINSPECTION 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.Jan 12, 2001 · N922UP · Boeing 72731C · Emergency EquipmentSDR UPS01234600Light · inoperativeINSPECTION 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-Jan 9, 2001 · N922UP · Boeing 72731C · Emergency LightingSDR UPS00233861Cargo Track · crackedINSPECTION 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.Sep 30, 2000 · N922UP · Boeing 72731C · Fuselage, Seat/Cargo Attach FittingsSDR UPS00233868Skin · corrodedINSPECTION 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.Sep 28, 2000 · N922UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS00233867Stringer · corrodedINSPECTION 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.Sep 28, 2000 · N922UP · Boeing 72731C · Fuselage Main, Longeron/StringerSDR UPS00233865Stringer · crackedINSPECTION TYPE:C, POSSIBLE CRACK INDICATION ON STR 15L, BS 1213 IN AFT AIRSTAIRS AREA. REPAIRED STRINGER IAW SRM 53-10-03 FIG 1.Sep 27, 2000 · N922UP · Boeing 72731C · Fuselage Main, Longeron/StringerSDR UPS00233862Casting · crackedINSPECTION 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.Sep 27, 2000 · N922UP · Boeing 72731C · Auxiliary Gear (Tail Skid)SDR UPS00233860Rib · crackedINSPECTION 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.Sep 26, 2000 · N922UP · Boeing 72731C · Leading Edge DevicesSDR UPS00233845Butt Joint · corrodedINSPECTION 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.Sep 25, 2000 · N922UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS00233837Fitting · corrodedINSPECTION TYPE:C, CORROSION EVIDENT IN NR 1 PYLON, ENG FWD MOUNT FITTING HOLES. REPAIR CARRIED OUT IAW UPS EO B727-5440-11592.Sep 25, 2000 · N922UP · Boeing 72731C · Nacelle/Pylon, Attach FittingsSDR UPS00233833Skin · crackedINSPECTION TYPE:C, NR 6 SLAT INNER SKIN CRACKED AROUND CTR FASTENER I/B OF ACTUATOR. REPAIRED INNER SKIN IAW UPS EO B727-5750-3082.Sep 25, 2000 · N922UP · Boeing 72731C · Leading Edge DevicesSDR UPS00233830Fitting · corrodedINSPECTION TYPE:C CORROSION EVIDENT IN NR 3 PYLON, ENG FWD MOUNT FITTING HOLES. REPAIR CARRIED OUT IAW EO B727-5440-11592Sep 25, 2000 · N922UP · Boeing 72731C · Nacelle/Pylon, Attach FittingsSDR UPS00233846Skin · corrodedINSPECTION 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.Sep 22, 2000 · N922UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS00233831Frame · damagedINSPECTION 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.Sep 22, 2000 · N922UP · Boeing 72731C · Fuselage Main, FrameSDR UPS00233834Beam · crackedINSPECTION 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.Sep 21, 2000 · N922UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS00233832Beam · crackedINSPECTION 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.Sep 21, 2000 · N922UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS00233855Bolt · damagedINSPECTION TYPE:C TO AID NDI REMOVE ENGINE NR 3 FWD AND AFT CRANE BEAM SHOULDER BOLTS. REPAIR CARRIED OUT IAW MM 71-21-03.Sep 20, 2000 · N922UP · Boeing 72731C · Engine Mount SectionSDR UPS00233854Bolt · damagedINSPECTION TYPE:C TO AID NDI REMOVE ENG NR 1 FWD & AFT CRANE BEAM SHOULDER BOLTS. REPAIR CARRIED OUT IAW MM 71-21-03.Sep 20, 2000 · N922UP · Boeing 72731C · Engine Mount SectionSDR UPS00231260Light · inoperativeEMERGENCY 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.Jan 5, 2000 · N922UP · Boeing 72731C · Emergency LightingSDR UPS99230277Retract Mech · inopFLAPS FAILED TO DEPLOY.Aug 5, 1999 · N922UP · Boeing 72731C · Trailing Edge Flap Control System
Back to N922UP, cancelled Jan 8, 2008