N930UP, cancelled Nov 21, 2007

Service difficulty reports · 175

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 = 'N930UP' AND deregistration_id = 'N930UP-2007-11-21'
  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 UPS06248609Battery · dischargedFOUND EMERGENCY EXIT LIGHT OVER ENTRY DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES PER MM 35-50-67. OPS CHECK GOOD.Nov 12, 2006 · N930UP · Boeing 72722C · Emergency LightingSDR UPS06246477Door · damagedFOUND LT AC PACK DOOR CAME OFF IN FLIGHT AND DAMAGING FUSELAGE AFT OF PACK. RT DOOR IS HANGING BY AFT HINGE AND IS BEYOND REPAIR.Mar 21, 2006 · N930UP · Boeing 72722C · Air Conditioning DoorsSDR UPS06246446Wire · looseEMERGENCY EXIT LIGHTS INOP. FOUND BOTTOM C/B PANEL LIGHTING INOP ON LEFT SIDE OF COCKPIT. FOUND POWER WIRE LOOSE. TIGHTENED LOOSE POWER WIRE. OPS CK GOOD.Mar 15, 2006 · N930UP · Boeing 72722C · Light System WiringSDR UPS06246517Battery · inoperativeON PREDEPARTURE CK, FOUND EMERGENCY EXIT LIGHT SWITCH IN ON POSITION. REMOVED AND REPLACED BATTERIES IAW MM 33-50-11-2. OPS CKS NORMAL.Mar 14, 2006 · N930UP · Boeing 72722C · Emergency LightingSDR UPS06246393Skin · dentedINSPECTION TYPE:SP REF DMI D-320435, DENT AT FS 1163 AT STR 20R INCOMING MEASUREMENT (APPROX) OF 3.0"DIA X .200 DEEP AND GOUGED 2.0" X .005"DEEP. CUT OUT DAMAGE AT FS 1163, STR 20R IAW SRM 53-30-03 FIG 5. FABRICATED AND INSTALLED REPAIR FILLERS (2EA), AND REFeb 28, 2006 · N930UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS05245314Skin · crackedSUSPECT SKIN CRACK AT BS 364 STR 3 LT. DAMAGED AREA CUT OUT AND REPAIRED IAW SRM 53030-3 FIG 3A.Aug 30, 2005 · N930UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS05245313Clip · crackedRT BODY FAIRING 3427 HAS SMALL CRACK AT FWD ATTACHING END CLIP. ATTACHING END CLIP REPLACED IAW SRM 51-20-04.Aug 29, 2005 · N930UP · Boeing 72722C · Aerodynamic FairingsSDR UPS05245312Frame · corrodedBODY FAIRING 3608 AFT FRAME AT ATTACHING ANGLE IS CORRODED AT BS 1010 ADJACENT TO STR 26R. FRAME REPLACED IAW SRM 51-20-1 FIG 7.Aug 29, 2005 · N930UP · Boeing 72722C · Aerodynamic FairingsSDR UPS05245357Skin · crackedSUSPECT SKIN CRACK AT UPPER FWD ENTRY DOOR CUT OUT BETWEEN STR 5 AND 6 L. PLEASE CARRY OUT NDI AND RECIFITY. REPAIR CARRIED OUT IAW SRM ADDENDUM EO B727-5330-1460-D OPT 1.Aug 25, 2005 · N930UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS05245372Web · crackedINSPECTION TYPE: C, NLG W/W CEILING AT BS 290 LBL 0 HAS SUSPECT CRACKS AT FASTENER HEADS. WEB REPLACED IAW SRM 51-20-1 AND DWG 65-18416.Aug 23, 2005 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS05245356Door · corrodedNLG FWD LT DOOR HAS CORROSION UNDER SEAL AT I/B END. CORRODED SECTION REPLACED WITH FABRICATED SECTION IAW SRM 51-20-1 AND DWG 65-17563.Aug 23, 2005 · N930UP · Boeing 72722C · Landing Gear DoorsSDR UPS05245317Stringer · corrodedAREA OF SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE AT BS 295 STR22R. CORROSION FOUND TO BE ON STRINGER 22R BETWEEN BS 204-316. STRINGER SECTION REPLACED BETWEEN BS 304 AND 320 IAW SRM 53-10-3 FIG 1.Aug 22, 2005 · N930UP · Boeing 72722C · Fuselage Main, Longeron/StringerSDR UPS05245316Skin · scratchedLIGHT SURFACE SCRATCHES FOUND ON SKIN AT BS 1263 BETWEEN S5L AND 6L. DAMAGED AREA FOUND OUT OF LIMITS, REPAIRED IAW SRM 53-30-3 FIG 13.Aug 22, 2005 · N930UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS04243231Panel · delaminatedINSPECTION TYPE:N/A NR 8 GROUND SPOILER CENTER HINGE BOTTOM S/M PANEL DELAMINATED. REMOVED AND REPLACED NR 8 GROUND SPOILER PER MM 27-62-01. OPS CHECK NORMAL.Sep 29, 2004 · N930UP · Boeing 72722C · SpoilersSDR UPS04242321Support · crackedINSPECTION TYPE:C CRACK ON SUPPORT STRUCTURE IN NWW RT FWD AREA. SUPPORT STRUCTURE REMOVED REF NRC NR 748078, SUPPORT STRUCTURE FABRICATE D IAW SRM 51-20-1, SUPPORT STRUCTURE INSTALLED IAW SRM 51-30-02.Apr 27, 2004 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS04242344Frame · crackedINSPECTION TYPE: C, VERT STAB JACKSCREW CUTOUT LT, FWD FRAME CRACKED AT FW STA 128 APPROX. CRACKED FRAME REMOVED IAW SRM 51-30-02. NEW FRAME INSTALLED IAW SRM 51-30-02Apr 26, 2004 · N930UP · Boeing 72722C · Vertical StabilizerSDR UPS04242316Pulley Bracket · crackedINSPECTION TYPE:C SUSPECT CRACKS ON RUDDER TRIM CABLE PULLEY BRACKET IN AIRSTAIRS AREA BS 1203 RT HFEC C/W, DERIVETED BRACKET, FAB BRACKET IAW SRM 51-20-01, BRACKET INSTALLED.Apr 26, 2004 · N930UP · Boeing 72722C · Rudder Control SystemSDR UPS04242343Skin · crackedINSPECTION TYPE: C, ENGINE NR 1 THRUST REV. UPPER DOOR INNER RAMP SKIN CRACKED. DYE PENETRANT INSP. CARRIED OUT ON THE ABOVE AREA IAW MIL-STD-6866. CRACKS FOUND AND ENDS MARKED. STOP DRILLED CRACKS IAW MM 78-30-01. DYE PENETRANT INSP. CARRIED OUT AROUND STOApr 24, 2004 · N930UP · Boeing 72722C · Engine Thrust ReverserSDR UPS04242341Skin · chafedINSPECTION TYPE:C CHAFING UNDER FAIRING AT BS1050 AND BS1070 JUST BELOW STR26L. AT BS1050 DAMAGE REMOVED AND FOUND TO BE WITHIN LIMITS IAW SRM 53-30-1. AREA REPROTECTED IAW SRM51-10-02. AT BS1070 DAMAGE OUT OF LIMITS IAW SRM 53-30-1. REPAIR CARRIED OUT IAWApr 16, 2004 · N930UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS04242358Rib · crackedINSPECTION TYPE: C, MID GALLEY DOOR UPPER GATE HINGE RIB CRACKED AT FWD CORNER. HINGE RIB REPLACED IAW DWG 65-16720 AND SRM 51-30-02Apr 15, 2004 · N930UP · Boeing 72722C · Service DoorsSDR UPS04242356Retainer · corrodedINSPECTION TYPE: C, SEAL RETAINER ON NWW CUTOUT FWD LHS CORRODED SEAL RETAINER REPLACED IAW SRM 51-20-01 AND AMM 20-80-01Apr 15, 2004 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS04242342Cargo Track · corrodedINSPECTION TYPE: C, SECTION OF TIE DOWN RAIL IS CORRODED FROM BS530 TO BS480 IN LOWER FWD CARGO COMPARTMENT. CORRODED SECTION OF TIE DOWN RAIL REMOVED IAW SRM 51-30-2. TIE DOWN RAIL FABRICATED IAW DRG. NO.:66-01573 INSTALLED NEW TIE DOWN RAIL IAW SRM 51-30-2Apr 15, 2004 · N930UP · Boeing 72722C · Fuselage, Seat/Cargo Attach FittingsSDR UPS04242355Retainer · corrodedINSPECTION TYPE: C, FWD RT SEAT RETAINER ON NLG WW CUTOUT CORRODED SEAL RETAINER REMOVED, SEAL RETAINER FABRICATED IAW SRM 51-20-1, SEAL RETAINER INSTALLED MM 20-80-01Apr 14, 2004 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS04242320Pressure Panel · crackedINSPECTION TYPE:C AIR LEAK FROM CRACK ON NWW WEB LHS BS 287. PAINT STRIPPED, HFEC INSPECTION C/O CRACKS CONFIRMED, CRACKED AREA CUT OUT, HFEC C/O AROUND CUT OUT AREA NDF, REMOVED SUPPORT STRUCTURE TO GAIN ACCESS, FABRICATED REPAIR PARTS, INSTALLED FABRICATED Apr 14, 2004 · N930UP · Boeing 72722C · Fuselage Main, BulkheadSDR UPS04242318Doubler · corrodedINSPECTION TYPE:C OLD REPAIR DOUBLER HAS SIGNS OF INTERGRANULAR CORROSION IN LOWER NOSE COMPT, DOUBLER LOCATED ON VERTICAL INTERNAL STRUCTURE OF NWW RBL 14.6 B STA 314. REMOVED OLD REPAIR. HFEC CW NDF. NEW DOUBLER INSTALLED IAW SRM 51-10-02 AND 51-30-02.Apr 14, 2004 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS04242357Web · crackedINSPECTION TYPE: C, 5 FLAP ACTUATOR TRUNNION SUPPORT BOX I/B WEB CRACKED. K FLAP ACTUATOR REMOVED, TRUNNION SUPPORT BOX I/B WEB REMOVED. WEB FABRICATED IAW DWG 65-16263. NEW K FLAP ACTUATOR TRUNNION SUPPORT BOX I/B WEB FITTED IAW SRM 51-30-02Apr 13, 2004 · N930UP · Boeing 72722C · Leading Edge DevicesSDR UPS03240913Skin · crackedINSPECTION TYPE: ASV, SKIN PANEL BELOW L1 AND R1 CENTER WINDOW POST HAS .375 INCH CRACK FROM EDGE TO RIVET. CONFIRMED BY DYE PENETRANT INSP. REPLACED SKIN PANEL AS PER SRM ADDENDUM EO B727-5330-5128A.Jun 26, 2003 · N930UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS02239758Hinge · crackedUPPER HINGE ARM OF AFT ENTRY DOOR CRACKED. HINGE REPLACED. FUNCTION AND OPERATION CHECK CARRIED OUT IAW MM 52-13-02 AND 52-13-00.Oct 10, 2002 · N930UP · Boeing 72722C · Passenger/Crew DoorsSDR UPS02239609Shear Tie · crackedINSPECTION TYPE:C+SI STR.SHEAR TIE CRACKED AT STR.5 R/H BS1050. SHEAR TIE REMOVED IAW SRM 51-30-2 SHEAR TIE REPLACED IAW 51-20-1+51-40-3Oct 4, 2002 · N930UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02239769Spar · corrodedDURING PREPARATION FOR CENTER SECTION REAR SPAR WEB SPLICE REPAIR, ADDITIONAL CORROSION WAS NOTED ON UPPER CHORD INBOARD OF LBL 34.20. WEB, CHORD, SPLICE AND STIFFENERS FABRICATED IAW DRG NR 65C21531 REPAIR COMPLETED IAW SMRO EO 2002-052-013. UPS ENG FILE NROct 3, 2002 · N930UP · Boeing 72722C · Wing SparSDR UPS02239767Beam · corrodedDURING REMOVAL OF T/E PANEL ATTACHED TO LOWER SURFACE OF RT MLG SUPPORT BEAM, CORROSION NOTED AROUND MLG SUPPORT BEAM FASTENER HOLE. CORROSION REMOVED AROUND HOLE IAW SRM 51-10-06. HFEC C/O ON FASTENER HOLE AND COUNTER BORE IN THE ABOVE AREA IAW B727 N DTM PSep 30, 2002 · N930UP · Boeing 72722C · Wing, Landing Gear Attach FittingsSDR UPS02239741Frame · damagedINSPECTION TYPE:C&SI DURING REPAIR OF FRAME BS 560 STR. 7R DAMAGE WAS FOUND ON EXISTING R EPAIR ABOVE AT S5R - 6R REPAIR TO FRAME CARRIED OUT IAW SRM 53-10-4 FIG 2Sep 30, 2002 · N930UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02239740Pressure Panel · damagedPRESS WEB AT BS 740 BULKHEAD DAMAGED AT LWR END WHERE IT ATTACHS TO 740 RT FITTING. DAMAGE BLENDED OUT AND REPAIRED PER SRM 53-10-9 FIG 4.Sep 30, 2002 · N930UP · Boeing 72722C · Fuselage Main, BulkheadSDR UPS02239774Riser · corrodedINSPECTION TYPE:C+SI CORROSION ON RISER #5 FOUND TO BE OUTSIDE LIMITS- REF NRC 480122.(AI RSTAIR DOOR) RISER REPLACED IAW SRM ADDENDIUM EO B727-5260-1551-A.Sep 24, 2002 · N930UP · Boeing 72722C · Entrance StairsSDR UPS02239773Hinge Pin · corrodedHORIZONTAL STAB HINGE LEFT OUTER PIN HAS EVIDENCE OF PITTING CORROSION ADJACENT TO RELIEF RADIUS. HORIZONTAL STABILIZER HINGE PIN LEFT OUTER REPLACED IAW MM 55-10-01 STEPS 3 AND 4.Sep 24, 2002 · N930UP · Boeing 72722C · Horizontal Stabilizer Miscellaneous StructureSDR UPS02239719Riser · corrodedINSPECTION TYPE:C&SI CORROSION ON RISER #6 ON AFT AIRSTAIRS FOUND TO BE OUTSIDE LIMITS RE F. NRC 480122 #6 RISER REPLACED IAW SRM ADDENDUM B727-5260-7551-ASep 24, 2002 · N930UP · Boeing 72722C · Entrance StairsSDR UPS02239718Riser · corrodedINSPECTION TYPE:C&SI CORROSION ON RISER #8 ON AFT AIRSTAIRS DOOR FOUND TO BE OUTSIDE LIMI TS REF. NRC 480122 RISER REPLACED IAW SRM ADDENDUM B727-5260-7551-ASep 24, 2002 · N930UP · Boeing 72722C · Entrance StairsSDR UPS02239716Panel · crackedINSPECTION TYPE:C&SI CRACK ON NLG WHEEL WELL PANEL RH SIDE ALONG ROW OF FASTNERS BELOW FW D RH PRESSURE PANEL BS 239 FASTENERS REMOVED IAW SRM 51-30-02. CRACK CUT OUT IAW SRM 51-40-2. REPAIRS TO CRACKED AREA CARRIED OUT IAW SRM 51-40-2 & SRM 51-30-2Sep 24, 2002 · N930UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02239715Panel · crackedINSPECTION TYPE:C&SI CRACK ON NLG WHEEL WELL SIDE PANEL RH SIDE ALONG ROW OF FASTENERS AF T OF FWD RH PANEL BS 250 FASTNERS REMOVED IAW SRM 51-30-02. CRACK CUT OUT IAW SRM 51-40-02. REPAIRS TO CRACKED AREA CARRIED OUT IAW SRM 51-40-2Sep 24, 2002 · N930UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02239557Pin · corrodedINSPECTION TYPE:C&SI HORIZ. STAB. HINGE R/H OUTER PIN HAS EVIDENCE OF PITTING CORROSION A DJACENT TO RELIEF RADIUS HORIZ. STAB HINGE R/H O/B PIN REPLACED IAW MM 55-10-01Sep 24, 2002 · N930UP · Boeing 72722C · Horizontal Stabilizer StructureSDR UPS02239768Keelbeam · crackedCRACKS RT KEEL BEAM VERTICAL WEB FWD OF APU CUT OUT. REPAIR IAW EO B727-5330-1995-B.Sep 23, 2002 · N930UP · Boeing 72722C · Fuselage Main, KeelSDR UPS02239717Frame · corrodedBS 740 BULKHEAD LWR CHORD FOUND CORRODED DURING REMOVAL TO FACILITATE FITTING REPLACEMENT. SECTION OF CHORD REPLACED IAW DRAWING 65C13724.Sep 23, 2002 · N930UP · Boeing 72722C · Fuselage Main, FrameSDR UPS02239558Intercostal · crackedINSPECTION TYPE:C&SI COCKPIT FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 294 & 284 LBL 5 REMOVED INTERCOSTAL IAW SRM 51-30-2 FABRICATED INTERCOSTAL IAW SRM 53-10-2 & SRM 51-20-4 INSTALLED INTERCOSTAL IAW SRM 51-30-2Sep 23, 2002 · N930UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02239607Rib · crackedINSPECTION TYPE:C+SI SUSPECT CRACK AT RIB BS 519 AT LWR. STR. ATTACH POINT AFT OF ACCESS PNL. STOP DRILLED CRACK IAW 51-10-1. PAGE 12.Sep 22, 2002 · N930UP · Boeing 72722C · Wing Main, Frame StructureSDR UPS02239714Seat Track · corrodedCORROSION AROUND NUT BS 380 LBL 45.5 ON SEAT TRACK. REMOVED DAMAGED SECTION IAW SRM 51-30-2, REPAIRED IAW SRM 53-10-5.Sep 20, 2002 · N930UP · Boeing 72722C · Fuselage, Seat/Cargo Attach FittingsSDR UPS02239639Frame · dentedINSPECTION TYPE:C+SI DENT IN FRAME BS 560 STR7 R/H REPAIRED IAW SRM 53-10-4 FIG 1Sep 20, 2002 · N930UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02239766Support Fitting · corrodedINSPECTION TYPE:C+SI CORROSION ON INNER FACE OF RH MLG TRUNNION SUPPORT FITTING. RH MLG TRUNNION SUPPORT FITTING REPLACED.Sep 19, 2002 · N930UP · Boeing 72722C · Main Landing GearSDR UPS02239756Stiffener · corrodedBULGING EVIDENT ON WING CENTER SECTION REAR SPAR WEB AT BS 870, 3RD VERTICAL STIFFENER FROM LEFT SIDE. CORROSION FOUND ON VERTICAL STIFFENER AT LBL 24.70. STIFFENER REPLACED IAW SRM 51-30-2 AND DRAWING 65-16202.Sep 19, 2002 · N930UP · Boeing 72722C · Wing, Center BoxSDR UPS02239745Frame · crackedINSPECTION TYPE:C&SI CRACK ON LWR AFT FLANGE OF FRAME BS 930 R/H AT MLG PRESS. WEB REPAIRS TO S15 & S16 CARRIED OUT IAW SRM 53-10-3. FRAME REPAIR BS 9 20 SPLICE FABRICATED IAW SRM 51-10-3 NEW 930 FITTING INSTALLED IAW D RG 65-16336 &65-18383 SRM 51-30-3 &Sep 19, 2002 · N930UP · Boeing 72722C · Fuselage Main, StructureSDR UPS02239721Frame · crackedINSPECTION TYPE:C&SI LWR AFT CARGO BAY, FRAME (BS1030)TO FUSELAGE SKIN ATTACH POINT IS CR ACKED IN BEND RADIUS BETWEEN STR 25 AND STR. 26L/H FRAME REPAIRED IAW SRM 53-10-4 FIG 11Sep 19, 2002 · N930UP · Boeing 72722C · Fuselage Main, Structure
Back to N930UP, cancelled Nov 21, 2007