N904UP, cancelled May 10, 2007

Service difficulty reports · 98

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 = 'N904UP' AND deregistration_id = 'N904UP-2007-05-10'
  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 UPS03241123Battery · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS BOTH NOT WORKING. REMOVED AND REPLACED BATTERIES. OPS CK GOOD.Aug 19, 2003 · N904UP · Boeing 72751C · Emergency LightingSDR UPS01236244Light · dischargedINSPECTION TYPE:PFLT COCKPIT EMERGENCY LIGHT ABOVE DOOR VERY DIM. REMOVED AND REPLACED BATTERIES, OPS CHECK OK AS PER MM 33-50-01.Jul 5, 2001 · N904UP · Boeing 72751C · Emergency LightingSDR UPS01235785Warning System · inoperativeCOMPT SHOWS-TD DELAY FOR FIRE WARNING BELL INDICATOR INOP COCKPIT FIRE BELL WILL NOT SOUND WITH THE ENG FIRE DETECTION PANEL TEST SWITCH IN A,B,OR A/B THIS APPLIES TO ACTUATING EITHER THE ENG TEST SWITCH OR WHEEL WELL TEST SWITCH. CLEANED AND RESECURED WIRMay 2, 2001 · N904UP · Boeing 72751C · Detection SystemSDR UPS01235220Strap · unserviceableINSPECTION TYPE:IN FWD ENTRY DOOR HANDLE STRAP IS NOT LONG ENOUGH TO ENGAGE VELCRO PAD WHEN LOOPED AROUND THE DOOR HANDLE. REMOVED FWD ENTRY DOOR HANDLE STRAP AS PER EO B727-2560-12064. OK FOR SERVICE.Mar 6, 2001 · N904UP · Boeing 72751C · Passenger/Crew DoorsSDR UPS01235105Switch · out of adjINSPECTION TYPE:N/A ATB-AIR/GROUND SAFETY SENSOR FAILED IN GROUND ILLEG BUT LANDING GEAR RETRACTED NORMALLY. REPOSITION MAIN GEAR SAFETY SWITCH ILLEG AND PERFORMED SWITCH OPS CHECK AS PER B727 M/M 32-0211. NO DEFECTS NOTED.Feb 26, 2001 · N904UP · Boeing 72751C · Landing Gear Position and WarningSDR UPS01235205Panel · crackedINSPECTION TYPE:C, NOSE WHEEL WELL LT SIDEWALL LOWER CHORD COVER PANEL SHOWS CRACK INDICATION 2 AROUND RIVET HEADS. REMOVED PANEL AND MADE NEW PER SAMPLE AND INSTALLED AS PER B727 SRM 51-30-2.Feb 19, 2001 · N904UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS01235203Pressure Panel · crackedINSPECTION TYPE:C, NOSE WHEEL WELL BS 227.8 FWD WALL BL 0 CRACK INDICATION AROUND ROW OF FASTENER HEADS. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2 & 51-10-1, INSTALLED DOUBLER REPAIR AS PER B727 51-40-2.Feb 19, 2001 · N904UP · Boeing 72751C · Fuselage Main, StructureSDR UPS01235202Pressure Panel · crackedINSPECTION TYPE:C, NOSE WHEEL WELL RT SIDEWALL BS 248 LWR OF FWD ACCESS DOOR CRACK INDICATION AROUND FASTENER HEAD. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2 & 51-10-1. INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-40-2.Feb 19, 2001 · N904UP · Boeing 72751C · Fuselage Main, StructureSDR UPS01235201Pressure Panel · crackedINSPECTION TYPE:C, NOSE WHEEL WELL RT SIDEWALL BS 264.3 WL 154 LWR OF AFT ACCESS DOOR CRACK INDICATION ALONG ROW OF RIVET HEADS. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2 & 51-10-1. INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-40-2 MAT USED 2024-T3.050 30, Feb 19, 2001 · N904UP · Boeing 72751C · Fuselage Main, StructureSDR UPS01235199Pressure Panel · crackedINSPECTION TYPE:C, NOSE WHEEL WELL RT SIDE WALL BS 259.5 FWD OF AFT ACCESS DOOR CRACK INDICATION ALONG ROW OF RIVET HEADS. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2, INSTALLED DOUBLER. REPAIR PER SRM 51-40-20.Feb 19, 2001 · N904UP · Boeing 72751C · Fuselage Main, StructureSDR UPS01235200Angle · corrodedINSPECTION TYPE:C-CK, AFT AIRSTAIR SUPPORT ANGLE CORROSION UNDER 4TH STEP FROM TOP. REMOVED AND REPLACED CHORD SUPPORT ANGLE ON AFT AIRSTAIRS.Feb 14, 2001 · N904UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS01235208Bracket · crackedINSPECTION TYPE:C-CK, TAIL SKID COMPT, 2 UPPER SUPPORT RODS AFT ATTACH BRACKETS, LT AND RT CRACKED. REMOVED AND REPLACED BOTH LT AND RT ATTACH BRACKETS FOR TAIL SKID UPPER SUPPORT RODS.Feb 13, 2001 · N904UP · Boeing 72751C · Fuselage Main, Attach FittingsSDR UPS01235198Attach Angle · crackedINSPECTION TYPE:C-CK RT MLG W/W UPPER O/B SIDE, FS 910, MLG UPLOCK SUPPORT FRAME FWD O/B ATTACH ANGLE CRACKED IN THE O/B RADIUS APPROX 6 INCHES BELOW PRESSURE DECK. REPAIRED RIGHT MLG W/W UPPER O/B SIDE FS 910 MLG UPLOCK SUPPORT FRAME.Feb 12, 2001 · N904UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS01235207Pressure Panel · crackedINSPECTION TYPE:C-CK, NOSE W/W LT SIDEWALL CRACK INDICATION ALONG ROW OF RIVETS HEADS. CUT OUT DAMAGE AREA AND INSTALLED DOUBLER.Feb 11, 2001 · N904UP · Boeing 72751C · Fuselage Main, StructureSDR UPS01235206Pressure Panel · crackedINSPECTION TYPE:C-CK, NOSE W/W LT SIDEWALL, CRACK INDICATION ALONG VERTICAL ROW OF RIVETS HEADS. CUT OUT DAMAGE AREA AND INSTALLED DOUBLER.Feb 11, 2001 · N904UP · Boeing 72751C · Fuselage Main, StructureSDR UPS01235204Panel · crackedINSPECTION TYPE:C-CK, RT WING T/E TOP PANEL HAS 2 CRACKS BY NR 10 SPOILER O/B HINGE. STOP DRILLED CRACKS AT RT WING T/E PANEL, ACCOMPLISHED HFEC INSP. NO CRACKS EXTENDED BEYOND STOP DRILLED HOLES. REMOVED NR 10 SPOILER O/B SUPPORT BRACKET. REMOVED AND REPLFeb 10, 2001 · N904UP · Boeing 72751C · Wing, Plate/SkinSDR UPS00233786Fire Detector · malfunctionedINSPECTION TYPE:N/A P-WRITE UP, LOWER CARGO FIRE DETECTOR AMBER LIGHT. *S/D* GROUND CKS SATISFACTORY AT THIS TIME IAW MM 26-18-01.Sep 21, 2000 · N904UP · Boeing 72751C · Fire DetectionSDR UPS00233377Light · malfunctionedINSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT AT REAR OF COCKPIT ILLUMINATED DURING CLIMB AND WOULD NOT TURN OFF. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSY, TEST GOOD.Jul 14, 2000 · N904UP · Boeing 72751C · Emergency LightingSDR UPS00231265Seal · brokenFWD LAV AVIOX OXYGEN GENERATOR HAS INCORRECT EQUIPMENT DUE STICKER. STICKER INDICATES DUE AT 'C' OR 'D' CHECK SHOULD BE A MONTH AND YEAR. FURTHER INSPECTION REVEALED TRIGGERING MECHANISM FOR GENERATOR ACTUATED, HOWEVER GENERATOR CANISTER WAS NOT BREACHED. IJan 11, 2000 · N904UP · Boeing 72751C · Portable Oxygen SystemSDR UPS99231093Battery Pack · dischargedFWD ENTRY DOOR EMERGENCY LIGHT DOES NOT ILLUMINATE. REPLACED BATTERY PACK ON EMERGENCY LIGHT. OPS CHECK GOOD.Nov 12, 1999 · N904UP · Boeing 72751C · Emergency LightingSDR UPS98225876Quadrant · corrodedINSPECTION TYPE-SI, AFT RUDDER CONTROL QUADRANT AREAS OF CORROSION AROUND FASTENERS. CORROSION REWORK OUT OF LIMITS. REMOVED OVER .75 OF THICKNESS. REMOVED AND REPLACED AFT RUDDER QUADRANT IAW MM 27-20-71.Feb 21, 1998 · N904UP · Boeing 72751C · Rudder Control SystemSDR UPS98225856Rib · crackedINSPECTION TYPE-SI, WHILE WORKING CARD NR 465869 FOUND L/W NR 3 SLAT O/B TRACK O/B TRACK RIB CRACKED. INSTALLED NEW RIB AT O/B TRACK STATION PER 727 SRM 51-30-2.Feb 20, 1998 · N904UP · Boeing 72751C · Leading Edge DevicesSDR UPS98225860Beam · corrodedINSPECTION TYPE-SI, CORROSION ON LONGITUDINAL BEAM LBL 25, WL 208, BS 765 TO 825. REMOVED AND REPLACED UPPER CHORD OF LONGITUDINAL BEAM IAW SRM 51-30-2, 51-20-1, 51-30-5.Feb 19, 1998 · N904UP · Boeing 72751C · Fuselage Main, Longeron/StringerSDR UPS98225859Seat Track · corrodedINSPECTION TYPE-SI, CORROSION ON CARGO TRACK IN WELL OF TRACK AT BS 675 TO 680, WL 155, RBL 15. REMOVED DAMAGED SECTION OF CARGO TRACK, FABRICATED AND INSTALLED REPLACEMENT SECTION IAW SRM 53-10-5.Feb 19, 1998 · N904UP · Boeing 72751C · Fuselage, Seat/Cargo Attach FittingsSDR UPS98225858Bulkhead Skin · crackedINSPECTION TYPE-SI, BS 178 BULKHEAD IS CRACKED AROUND FASTENERS AT BS 10, WL 235. REMOVED DAMAGED AREA .5 X 3 ENCOMPASSING 3 CRACKS. REPAIRED BS 178 AT LBL 10, WL 235, PER 727 SRM 53-10-9 AND SRM 51-30-2.Feb 19, 1998 · N904UP · Boeing 72751C · Fuselage Main, BulkheadSDR UPS98225857Fitting · corrodedINSPECTION TYPE-SI, NR 1 FLAP TRACK FWD FITTING IS CORRODED AROUND MOUNT HOLE. REPLACED FITTING PER SRM 51-10-1, NEW FITTING SETUP AND MACHINED PER BOEING DRAWING 65-17357.Feb 19, 1998 · N904UP · Boeing 72751C · Wing, Control Surface Attach FittingsSDR UPS98225855Seat Track · corrodedINSPECTION TYPE-SI, CORROSION AROUND NUT PLATES BS 861, RBL 24, WL 208. REMOVED AND REPLACED SECTION OF SEAT TRACK AND EXPANSION LINK IAW SRM 51-30-2.Feb 18, 1998 · N904UP · Boeing 72751C · Fuselage, Seat/Cargo Attach FittingsSDR UPS98225854Seat Track · corrodedINSPECTION TYPE-SI, WHILE WORKING CUST ID 2-224-22B FOUND CORROSION ON SEAT TRACK INBD FLANGE STA 730, LBL 65, WL 208. REMOVED DAMAGED SECTION OF SEAT TACK AND SPLICED IN NEW SECTION IAW SRM 53-10-5.Feb 18, 1998 · N904UP · Boeing 72751C · Fuselage, Seat/Cargo Attach FittingsSDR UPS98225853Stringer · crackedINSPECTION TYPE-SI, CRACKED STRINGER 24 RT BS 485, WL 165, RBL 35. STOP DRILLED ENDS AT CRACK AND INSTALLED REPAIR DOUBLERS OVER DAMAGED SECTION IAW SRM 53-10-3.Feb 18, 1998 · N904UP · Boeing 72751C · Fuselage Main, Longeron/StringerSDR UPS98225852Support · corrodedINSPECTION TYPE-SI, CORROSION ON FLOOR SUPPORT BS 328 TO 344, LBL 29, WL 208. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-2.Feb 18, 1998 · N904UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS98225851Beam · crackedINSPECTION TYPE-SI, FORWARD CARGO DOOR NR 3 BEAM IS CRACKED IN OUTBD RADIUS 12 INCHES AFT FROM FORWARD EDGE OF DOOR, 16 INCHES DOWN FROM TOP EDGE OF DOOR. REMOVED AND REPLACED DOOR IAW MM ON SEPARATE NRC NR 465118.Feb 18, 1998 · N904UP · Boeing 72751C · Cargo/Baggage DoorsSDR UPS98225848Core · corrosionINSPECTION TYPE-SI, WATER ENTRAPMENT NOTED IN LT WING NR 7 SPOILER I/B END FROM LEADING EDGE AFT 12 INCHES (X-RAY FILM VIEW NR 8). FURTHER INVESTIGATION REQUIRED. REMOVED 24 X 9 OF LOWER SURFACE SKIN AND 5 X 11.8 DAMAGED CORE CLEANED, DRIED AND REPAIRED IAW Feb 17, 1998 · N904UP · Boeing 72751C · SpoilersSDR UPS98225847Stringer · crackedINSPECTION TYPE-SI, CRACK AT STR 14 LT BS 887 LBL 70 WL 229. REPAIRED CRACKED STR 14 LT AT STA 887, LBL 70, WL 229 IAW SRM 51-40-4.Feb 17, 1998 · N904UP · Boeing 72751C · Fuselage Main, Longeron/StringerSDR UPS98225861Bullnose · corrodedINSPECTION TYPE-SI, L/W NR 2 K-FLAP BULLNOSE I/B MOUNT LUG CORRODED AROUND I/B FASTENER. REMOVED CORRODED BULLNOSE, CORROSION OUT OF LIMITS, INSTALLED SERVICABLE BULLNOSE IAW MM 27-81-01.Feb 16, 1998 · N904UP · Boeing 72751C · Leading Edge DevicesSDR UPS98225786Web · corrodedINSPECTION TYPE-SI, CORROSION ON VERTICAL WEB OF DOGHOUSE BS 307 TO 314, LBL 13.5, WL 157 TO 161. CUT OUT DAMAGED AREA OF WEB AND INSTALLED DOUBLER IAW SRM 53-10-9, 51-40-2.Feb 16, 1998 · N904UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS98225785Fitting · corrodedINSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON STRINGER TIE OF STR 26 LT BS 365. REMOVED AND REPLACED STRINGER TIE IAW SRM 51-30-2, 53-10-1, 51-30-4.Feb 16, 1998 · N904UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS98225782Frame · corrodedINSPECTION TYPE-SI, CORROSION BS 680 FRAME LBL 24 WL 154 UPPER FLANGE. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER PER SRM 51-40-3, HEAT TREATED AND THEN INSTALLED PER SRM 51-20-04 SRM 53-10-2 AND SRM 51-40-3.Feb 16, 1998 · N904UP · Boeing 72751C · Fuselage Main, FrameSDR UPS98225781Rib · crackedINSPECTION TYPE-SI ,RWS 629 RIB IS CRACKED IN RADIUS AT S-11 LOWER ATTACH BOLT HOLE. REPAIRED 629 RIB (RWS) IAW UPS EO B727-5710-1325H.Feb 16, 1998 · N904UP · Boeing 72751C · Wing, Rib/BulkheadSDR UPS98225780Stringer · crackedINSPECTION TYPE-SI, WHILE WORKING NRC 465706 WINGS 329, FOUND STRINGER 14 TAB TO BE CRACKED AT R/W STA 629.0. REPAIRED STR 14 AT RWS 629.0 IAW UPS EO B727-5710-0314F.Feb 16, 1998 · N904UP · Boeing 72751C · Wing, Longeron/StringerSDR UPS98225735Fitting · corrodedINSPECTION TYPE:SI, I/B CENTER HINGE FITTING ON AILERON SIDE IS CORRODED ON O/B AILERON L/W. REMOVED AND REPLACED L/W O/B AILERON CENTER HINGE FITTING AILERON SIDE IAW SRM 51-30-2 AND 51-30-5.Feb 13, 1998 · N904UP · Boeing 72751C · AileronsSDR UPS98225738Angle · corrodedINSPECTION TYPE:SI, CORROSION ON OUTBD SIDE OF INBD EXPANSION LINK STA 868, LBL 35, WL 161. REMOVED AND REPLACED EXPANSION LINK ATTACH ANGLES IAW SRM 51-30-2.Feb 12, 1998 · N904UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS98225737Stringer · corrodedINSPECTION TYPE:SI, CORROSION ON STRINGER 23L BS 730 TO 735 WL 155. REMOVED FASTENERS AND CUT STRINGER AT BS 712. INSTALLED STRINGER REPAIR PER SRM 53-10-3 FROM BS 712 TO 726, 726 TO 740 CORROSION FOUND WITHIN LIMITS.Feb 12, 1998 · N904UP · Boeing 72751C · Fuselage Main, Longeron/StringerSDR UPS98225874Rib · crackedINSPECTION TYPE-SI, WHILE WORKING CARD NR 465720 FOUND CRACKED RIB ON L/W NR 3 SLAT AT SLAT STA 128 TO 950. REMOVED CRACKED RIB, REPLACED WITH NEW RIB IAW SRM 51-30-2.Feb 10, 1998 · N904UP · Boeing 72751C · Leading Edge DevicesSDR UPS98225742Web · corrodedINSPECTION TYPE:S, CORROSION (C53-111-01.00-01) ON NOSE WHEELWELL PRESSURE WEB BS 243-251, LBL 235, WL 168-172 (AREA MARKED). REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 51-10-02. REPAIRED PER SRM 53-10-9, 51-10-02.Feb 10, 1998 · N904UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS98225741Stringer · corrodedINSPECTION TYPE:SI, CORROSION ON STR 21 RT, BS 575, WL 178. REMOVED DAMAGED SECTION OF STRINGER AND SPLICED IN REPAIR SECTION IAW SRM 53-10-3.Feb 10, 1998 · N904UP · Boeing 72751C · Fuselage Main, Longeron/StringerSDR UPS98225740Stiffener · corrodedINSPECTION TYPE:SI, CORROSION ON VERTICAL STIFFENER AT STA 294, RBL 5, WL 193 ON STIFFENER STRAP. REMOVED AND REPLACED STRAP ON STIFFENER IAW SRM 51-30-2.Feb 10, 1998 · N904UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS98225739Frame · corrodedINSPECTION TYPE:SI, CORROSION (C53-111-01.00-01) AROUND FASTENERS ON FRAME BS 243, RBL 25, WL 166. CORROSION OUT OF LIMITS. REMOVED CORROSION, FABRICATED FILLER AND DOUBLER, INSTALLED IAW SRM 51-40-2, 51-10-2, 51-20-151.Feb 10, 1998 · N904UP · Boeing 72751C · Fuselage Main, FrameSDR UPS98225877Intercostal · corrodedINSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON INTERCOSTAL BS 211.8 TO 219.8, LBL 25, WL 176. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPLACED INTERCOSTAL STA 211.8 TO 219.8, LBL 25, WL 176 IAW SRM 51-20-1, 51-30-2, 51-10-3.Feb 8, 1998 · N904UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS98225879Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AND BARE METAL ON FLOORBEAM BS 480, LBL 45 TO 59, WL 208. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. COMPLETED STANDARD UPPER CHORD SPLICE PER SRM 53-10-8, FIG 5, SRM 51-30-2 AND MM 51-20-21.Feb 4, 1998 · N904UP · Boeing 72751C · Fuselage Main, Floor BeamSDR UPS98225878Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON FLOORBEAM BS 400, LBL 25, WL 208, UPPER FLANGE. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 51-10-1. COMPLETED STANDARD T-CHORD REPAIR PER SRM 53-10-8, SRM 51-30-2 AND MM 51-20-31.Feb 4, 1998 · N904UP · Boeing 72751C · Fuselage Main, Floor Beam
Back to N904UP, cancelled May 10, 2007