N918UP, cancelled Nov 21, 2007

Service difficulty reports · 135

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 = 'N918UP' AND deregistration_id = 'N918UP-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 UPS06247834Light · no testINSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED C/P PORTABLE EMERGENCY LIGHT ASSY IAW MM 33-50-67-2. SYS OPS CKS OK.Aug 29, 2006 · N918UP · Boeing 72730C · Emergency LightingSDR UPS06247826Lamp · failedINSPECTION TYPE:NA EMERGENCY LIGHT ABOVE CREW ENTRY DOOR DIM, RELAMPED. OPS CK NORMAL IAW 25 60 00.Aug 28, 2006 · N918UP · Boeing 72730C · Emergency LightingSDR UPS06246793Light · inoperativeEMERGENCY EXIT LIGHT CAME OUT OF SOCKET. REINSTALLED ASSEMBLY. OPS CK GOOD PER AMM 33-50-01-5.May 4, 2006 · N918UP · Boeing 72730C · Emergency LightingSDR 2006FA0000645Control Valve · failedNR 2 ENGINE FIRE EXTINGUISHING SELECTOR CONTROL VALVE FAILED TO OPEN DURING ROUTINE TESTING IAW UPS ROUTINE TASK CARD TC 2-221-12. THE VALVE SOLENOID HOUSING WAS NOTED AS BEING CORRODED. (K)Nov 8, 2005 · N918UP · Boeing 72730C · Extinguishing SystemSDR UPS05245823Stringer · corrodedINSPECTION TYPE:C STRINGER 24 RT FOUND CORRODED AT BS 725. PLEASE INVESTIGATE DAMAGE FOUND TO BE BEYOND LIMITS IAW SRM 53-10-3. DAMAGED SECTION OF STRINGER 24R CUT OUT AND REMOVED. AREA REPAIRED IAW 53-10-3 FIG 1 DETAIL 1 PAGE 4B.Nov 1, 2005 · N918UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR UPS05245859Skin · crackedINSPECTION TYPE:C AFT CARGO DOOR CRACK ON INNER SKIN SECOND INSPECTION HOLE FWD EDGE AT BOTTOM. REMOVE FASTENER AND CHECK DEPTH OF CRACK TO DETERMINE REPAIR. HFEC CARRIED OUT AND CRACK FOUND CONTAINED WITHIN FASTENER HOLE. REPAIRED IAW SRM 51-40-02.Oct 25, 2005 · N918UP · Boeing 72730C · Cargo/Baggage DoorsSDR UPS05245826Intercostal · crackedINSPECTION TYPE:C STA 660, ST 29R REPAIR TO INTERCOSTAL IS CRACKED. PLEASE REPAIR IAW SRM. REPAIR BRACKET FABRICATED IAW SRM 51-20-071 FIG 7. REPAIR BRACKET REPLACED IAW SRM 51-30-02.Oct 24, 2005 · N918UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS05245861Link · crackedINSPECTION TYPE:C RT MLG UPLOCK FWD SUPPORT LINKS CRACKED. REPLACE LINKS. RT MLG UPLOCK FWD SUPPORT LINKS REPLACED IAW MM 20-80-01.Oct 18, 2005 · N918UP · Boeing 72730C · Main Landing GearSDR UPS05245851Spar · corrodedAREA OF SUSPECT CORROSION ON WING CENTER SECTION REAR SPAR LWR CHORD BS 870 RBL36 DUE TO 2 POPPED FASTENER HEADS. PLEASE INVESTIGATE AND RECTIFY AS NECESSARY. AS PER BOEING INSTRUCTIONS THE LWR CHORD WAS REPLACED. NEW CHORD WAS CUT AT RBL 9.5. REPAIR SPLICEOct 16, 2005 · N918UP · Boeing 72730C · Wing SparSDR UPS05245832Skin · corrodedEVIDENCE OF CORROSION AT BS 360 STR 22L AT FWD END OF STR AT AFT FACE OF FRAME. PLEASE INVESTIGATE AND RECTIFY. CORROSION BLENDED OUT IAW SRM 51-10-06. CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-1. REPAIR STRAP FABRICATED IAW SRM 51-20-1 FIG 7. MOct 16, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS05245821Skin · corrodedINSPECTION TYPE:C NDT INSPECTION HAS INDICATION OF MATERIAL LOSS AT BS 441 FWD OF CENTER LINE AT STR 8L, INVESTIGATE. CORROSION FOUND BETWEEN SKIN AND DOUBLER. CORROSION REMOVED AND FOUND BE WITHIN LIMITS, AREA REPROTECTED IAW SRM 51-30-02.Oct 16, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS05245836Trunnion · crackedRT TRUNNION ATTACH FITTING HAS CRACK AT OB FLANGE HOLE E RUNNING UP APPROX 2.5 INCHES. REMOVE AND REPLACE FITTING. RT TRUNNION FITTING FOUND CRACKED OUTSIDE REPAIRABLE LIMITS IN UPS EO B727-5740-20666C. REPLACED IAW UPS AUTHORIZATION B727-5740-23046-B.Oct 15, 2005 · N918UP · Boeing 72730C · Fuselage, Landing Gear Attach FittingsSDR UPS05245831Skin · corrodedSURFACE CORROSION ON LAP JOINT BETWEEN S-4L AND 5L AT LOCATIONS BETWEEN BS 852 AND 1011. CORROSION REMOVED IAW SRM 51-10-2 (.002") AND FOUND WITHIN LIMITS IAW SRM 51-20-4.Oct 14, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS05245824Support · corrodedINSPECTION TYPE:C RT MLG TRUNNION BUTTERFLY FITTING HAS CORROSION. PLS REPLACE. SUPPORT REPLACED IAW DRW 65-19296.Oct 14, 2005 · N918UP · Boeing 72730C · Fuselage, Landing Gear Attach FittingsSDR UPS05245860Bushing · crackedINSPECTION TYPE:C ENGINE NR 3 AFT MOUNT FITTING HAS CORROSION ON INNER SURFACE OF UPPER USHING. REPLACE BUSHING. REPLACED BUSHING IAW OHM 20-50-03.Oct 13, 2005 · N918UP · Boeing 72730C · Engine Mount SectionSDR UPS05245827Mount · corrodedINSPECTION TYPE:C ENGINE NR 3 FWD MOUNT FITTING HAS PITTING CORROSION ON BOTH OUTBOARD HOLES. REPAIR. REPAIRED IAW EO B727-5540-11592-A.Oct 13, 2005 · N918UP · Boeing 72730C · Engine Mount SectionSDR UPS05245833Skin · corrodedAREA OF SUSPECT CORROSION ON CROWN SKIN BS 521 TO BS 515 BETWEEN STR 2L AND 3L. PLEASE PAINT STRIP AREA, REMOVE FASTENERS IF REQUIRED, REINSPECT AND RECTIFY AS NECESSARY. REPAIRED IAW UPS AUTHORIZATION B727-5330-23323-AOct 12, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS05245822Support Fitting · crackedRT WING FRONT SPAR TO BODY FITTING HAS SUSPECT CRACK ON OUTBD SIDE OF BOTTLE PIN. FITTING REPLACED IAW DWG 65C13724 AND UPS EO B727-5310-7477.Oct 12, 2005 · N918UP · Boeing 72730C · Wing, Attach FittingsSDR UPS05245835Trunnion · crackedLT MLG SUPPORT FITTING HAS CRACK INDICATION IN HOLE B & C ON INB FLANGE AND HOLES E IN COUNTERSINKS. REPAIR AND REPLACE FITTING LT MLG TRUNNION REMOVED AND FOUND CRACKED OUTSIDE REPAIRABLE LIMITS IN UPS EO B727-5740-20666C. TRUNNION REPAIRED IAW UPS AUTHORIZOct 11, 2005 · N918UP · Boeing 72730C · Fuselage, Landing Gear Attach FittingsSDR UPS05245829Skin · crackedINSPECTION TYPE:C NDT INDICATES 2 CRACKS EMINATING FROM FASTENERS " BS235.8 STR16L-17L. PLEASE REPAIR IAW SRM 53-30-3 FIG 3. FASTENERS REMOVED FROM AFFECTED AREA IAW SRM 51-80-02. AFFECTED AREA CUTOUT IAW SRM 53-30-3. HFEC CARRIED OUT AROUND CUTOUT AND ON Oct 11, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS05245828Skin · crackedINSPECTION TYPE:C SUSPECT SKIN CRACKS AT UPPER FWD CORNER OF FWD ENTRY DOOR CUT OUT BETWEEN STR 7L AND 8L. PLEASE CARRY OUT NDI AND RECTIFY AS NECESSARY IAW SRM ADDENDUM. HFEC CARRIED OUT IAW NDTM 51-00-00 PT6 FIG 4. TWO CRACKS FOUND. DAMAGE REMOVED IAW EOOct 11, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS05245834Skin · crackedFOUND SKIN CRACK AT FASTENER HOLE IN MID GALLEY DOOR CUT OUT, UPPER FWD CORNER. PLEASE CONFIRM WITH NDI AND RECTIFY AS NECESSARY HFEC CARRIED OUT ON FASTENER HOLES COMMON TO REPAIR IAW 727NDTM 51-00- 00 PT6 FIG 16. THREE CRACKS FOUND. REPAIR CARRIED OUT IAWOct 9, 2005 · N918UP · Boeing 72730C · Service DoorsSDR UPS04241790Light · inoperativeBOTH EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REPLACED BATTERIES, OPS CHECK'S NORMAL.Jan 29, 2004 · N918UP · Boeing 72730C · Emergency LightingSDR UPS03241453Warning Light · illuminatedINSPECTION TYPE:N/A LOWER CARGO MX LIGHT ILLUMINATED INFLIGHT, MAINT. CODES DISPLAYED; A3398. SYSTEM TEST NORMAL PER MM 26-18-00. TESTED SEVERAL TIMES DURING LAYOVER PERIOD WITH NO DEFECTS NOTED AT THIS TIME DI 268782 CLOSEDOct 21, 2003 · N918UP · Boeing 72730C · Smoke DetectionSDR UPS03241350Light · inoperativeEVACUATION SLIDE ILLUMINATION LIGHT IS INOPERATIVE. REF TO WDM 33-50-02, EVACUATION SLIDE ILLUMINATION LIGHT IS ONLY A PROVISION.Oct 6, 2003 · N918UP · Boeing 72730C · Emergency LightingSDR UPS01236693Control Unit · malfunctionedWITH RUDDER TRIMMED TO ZERO 12 DEGREE LEFT AILERON REQUIRED TO HOLD WINGS LEVEL DEPLOYING SPEED BRAKE SLIGHTLY FIXES PROBLEM. INSPECTED SPOILERS NO DEFECTS FOUND INSPECTED FLIGHT CONTROLS GEN MX PRACTICES 27-00-00 PAGE 201, 203 NO DEFECT FOUND HOWEVER SUSAug 23, 2001 · N918UP · Boeing 72730C · Rudder Control SystemSDR UPS01236443Battery · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS EXTINGUISH SHORTLY AFTER TURNED ON. REPLACED BATT IN FWD AFT EMERG LIGHT ASSY OPS CHECKS GOOD.Jul 28, 2001 · N918UP · Boeing 72730C · Emergency LightingSDR UPS01235624Stringer · corrodedINSPECTION TYPE: C, FWD CARGO COMPT BETWEEN STA 680 AND 660, LT SIDE STRINGER 24, CORROSION. CUT OUT SECTION AT BAD STRINGER AREA STA 680 TO STA 660 LT STRINGER 24 INSTALLED REPAIR AS PER B727 SRM 53-10-3 FIG 1 SIDE OF STRINGER DOUBLER REPAIR 11 1/4 INCHESMar 29, 2001 · N918UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR UPS01235625Keelbeam · crackedINSPECTION TYPE:C, RT SIDE OF KEELBEAM APU CUT OUT FWD END HAS A DOUBLER CRACKED AT BS 874 NEXT TO HORIZONTAL STIFFENER. REMOVED OLD DOUBLER REPAIR OF KEEL BEAM AREA AND INSTALLED NEW DOUBLER REPAIR AT SAME AREA BS 874 AS PER B727 SRM 51-10-01.Mar 28, 2001 · N918UP · Boeing 72730C · Fuselage Main, KeelSDR UPS01235623Web · crackedINSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION APROX 770 AND LBL 13 WEB IS CORRODED. REMOVED WEB AT LOWER FUSELAGE CENTER SECTION AT BS 770 AND LBL13 WEB AS PER B727 SRM 51-30-02. REPLACED DAMAGE WEB LOWER CENTER WING AT BS 770 AND LBL 13 WEB AS PER B 7Mar 27, 2001 · N918UP · Boeing 72730C · Wing, Center BoxSDR UPS01235622Web · crackedINSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION APROX BETWEEN BS 800 TO 810 AND LBL 13 WEB IS CORRODED. REMOVE WEB AT LWR FUSELAGE CENTER SECTION BETWEEN BS 800 TO BS 810 LBL 13 WEB AS PER B727 SRM 51-30-2. REPLACED DAMAGED WEB LOWER CENTER WING AT BSMar 27, 2001 · N918UP · Boeing 72730C · Wing, Center BoxSDR UPS01235621Web · crackedINSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION BETWEEN BS 775 TO BS 800 AND RBL 13 WEBS CRACKED AND CORRODED. REMOVE WEB AT LWR FUSELAGE CENTER SECTION BETWEEN 767 TO 830 RBL13 AS PER B727 SRM 51-30-02 REMEOVED AND REPLACED DAMAGE WEB LOWER CENTER WING Mar 27, 2001 · N918UP · Boeing 72730C · Wing, Center BoxSDR UPS01235628Seat Track · gougedINSPECTION TYPE: C, MAIN CARGO DECK FUSELAGE STATION 1130 LBL 45 SEAT TRACK TONGUES ARE NICKED AND GOUGED REPLACED DAMAGED SECTION OF SEAT TRACK FROM BS 1110 TO STA 1130 LBL 45Mar 26, 2001 · N918UP · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR UPS01235626Pressure Panel · crackedINSPECTION TYPE: C, NOSE WHEEL WELL RT SIDE CRACKED AT BS 286.5 TO BS 294.5 WL 160 LOOKING FROM INSIDE TUNNEL. CUT OUT DAMAGE AREA, NDT CUT OUT, AND INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-40-2 FIG.1Mar 26, 2001 · N918UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS00234210Pulley · wornINSPECTION TYPE:N/A, ATB DURING FLAP RETRACTION OUTBOARD FLAPS WENT TO 2 DEGREES, MATCHED FL AND LE, INBOARD FLAPS JAMMED AT R-5 DEGREES L-15 DEGREES. REMOVED AND REPLACED LEFT INBOARD FLAP TRANSMITTER CABLE AND PULLEY PER MM 27-52-02. OPS CK NORMAL.Oct 20, 2000 · N918UP · Boeing 72730C · Trailing Edge Flap Control SystemSDR UPS00233553Light · inoperativeINSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLE AND BATTERIES OPS CK GOOD.Aug 9, 2000 · N918UP · Boeing 72730C · Emergency LightingSDR UPS00233240Battery Pack · inoperativeEMERGENCY LIGHT FWD ENTRY DOOR INOPERATIVE. R/R EMERGENCY LIGHT AND BATTERY PACK. OPS CHECKED GOOD. P/N 10-00067 -9 SN ON 1315 SN OFF 900Jul 6, 2000 · N918UP · Boeing 72730C · Emergency LightingSDR UPS00232107Light · inoperativeEMERGENCY LIGHT AT MAIN ENTRANCE DOOR IS INOPRATIVE. R/R EXIT LIGHT BATTERY ALL OPS CHECKS GOODMar 29, 2000 · N918UP · Boeing 72730C · Emergency LightingSDR UPS99231178Light · failedINSPECTION TYPE:N/A, REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY (P/N 10-0067-7) (S/N 20261) OFF, REF IPC 33-50-00-20-15. REMOVED EMERGENCY EXIT LIGHT ASSY, OPS CHECK GOOD.Dec 7, 1999 · N918UP · Boeing 72730C · Emergency LightingSDR UPS99231181Light · inopINSPECTION TYPE:N/A, BORROWED PART INSTALLED IN EMERGENCY EXIT LIGHT L1 POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IN L1 POSITION (P/N 10-0067-9) ON, (P/N 10- 0067-7) OFF, (S/N 2151) ON, (S/N 20261) OFF.Dec 6, 1999 · N918UP · Boeing 72730C · Emergency LightingSDR UPS99229619Battery Pack · dischargedINSPECTION TYPE:N/A, COCKPIT EMERGENCY LIGHTS ABOVE DOOR INOP, FAILED TO TEST. REMOVED UNIT FROM A/C, PUT BATTERIES ON CHARGE, REINSTALLED BATTS IN A/C AND OPS OK.May 17, 1999 · N918UP · Boeing 72730C · Emergency LightingSDR UPS98227171Light · inoperativeINSPECTION TYPE-N/A, EMER EXIT LIGHT OVER FLIGHT DECK DOOR WILL NOT STAY IN IT'S ELECTRICAL SOCKET CAUSING IT TO STAY ON IN FLIGHT. REINSTALLED EMER EXIT LIGHT PROPERLY UNTILL LATCHES ENGAGED, EMER EXIT LIGHT, OPS CHECK GOOD.Jul 15, 1998 · N918UP · Boeing 72730C · Emergency LightingSDR UPS98227164Batteries · dischargedINSPECTION TYPE-N/A, EMER EXIT LIGHT OVER FLIGHT DECK DOOR INOP. REPLACED WITH NEW BATTERIES, LIGHT OPS CHECKED OK.Jul 14, 1998 · N918UP · Boeing 72730C · Emergency LightingSDR UPS97222408Light · inoperativeINSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS DO NOT TURN ON WITH SWITCH IN ON POSITION. REPLACED BATT ON EMERGENCY EXIT LIGHT, OPS CKS NORMAL.Mar 18, 1997 · N918UP · Boeing 72730C · Emergency LightingSDR UPS97221862Light · inoperativeEMERGENCY EXIT LIGHT IN COCKPIT IS NOT SECURE AND CAME ON DURING LANDING ROLL OUT. RESECURED, OPS CHECKED GOOD.Jan 28, 1997 · N918UP · Boeing 72730C · Emergency LightingSDR UPS97221835Shear Web · corrodedINSPECTION TYPE-C, SHEAR WEB STA 1131 RBL 62 WL 208 HAS CORROSION AT NUTPLATE HOLE. CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED ALL WORK DONE IAW EO NR 727-53-1851 AND TRAMCO EWO 97-2020.Jan 21, 1997 · N918UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS97221834Support Fitting · crackedINSPECTION TYPE-C, NR 3 SPOILER SUPPORT FITTING ATTACH ANGLE IS CRACKED AT LOWER I/B ATTACH BOLT HOLE. REMOVED CRACKED NR 3 SPOILER SUPPORT FITTING ATTACH ANGLE. REPLACED PER SRM 51-30-2, MM 27-61-81, 27-61-0.Jan 20, 1997 · N918UP · Boeing 72730C · Drag Control SystemSDR UPS97221841Skin · crackedINSPECTION TYPE-C, LT WING I/B FOREFLAP L/E SKIN CRACKED FWD OF DEFLECTOR DOOR I/B END. REMOVED AND INSTALLED SERVICEABLE FOREFLAP, WORK DONE IAW MM 27-51-01.Jan 15, 1997 · N918UP · Boeing 72730C · Trailing Edge FlapsSDR UPS97221833Angle · corrodedINSPECTION TYPE-C, CORROSION FOUND ON RT LOWER L-ANGLE RBL 24 BS 178 WL 207. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED L-ANGLE PER SRM 51-40-4, 53-10-2, 51-10-1, 51-10-6, 51-30-2.Jan 12, 1997 · N918UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS97221840Hinge · corrodedINSPECTION TYPE-C, NR 5 K-FLAP CENTER HINGE FITTING HAS SEVERAL SPOTS OF CORROSION. REMOVED AND INSTALLED NEW HINGE ASSY, WORK DONE IAW SRM 51-30-2, 51-30-5, 51-30-8, 51-10-2, 51-20-04, MM 27-87-01.Jan 11, 1997 · N918UP · Boeing 72730C · Leading Edge Devices
Back to N918UP, cancelled Nov 21, 2007