Boeing 727-30C

Service difficulty reports · 931

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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 aircraft_model_key = '72730C'
  ORDER BY difficulty_date DESC"

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SDR UPS01234654Light · detachedINSPECTION TYPE:PFLT CREW REPORTS MAIN ENTRY EMERGENCY EXIT LIGHT FELL OFF AT LANDING. REPLACED EMERGENCY EXIT LIGHT ASSY, OPS NORMAL.Jan 19, 2001 · N906UP · Boeing 72730C · Emergency LightingSDR DHL2001702001Warning System · activatedRTO BECAUSE OF FALSE T/O WARNING HORN-RECYCLED FLAPS, WARNING DID NOT SOUND WHEN T/L ADVANCED. PREFORMED T/O WARNING TEST,FOUND NORMAL OPS PER M/M 34-00 AND 31-00Jan 6, 2001 · N702DH · Boeing 72730C · Central WarningSDR UPS00234565Light · inoperativeINSPECTION TYPE:PFLT EMER. EXIT LITE INOP. REPLACED COCKPIT EMER. LIGHT ASSY. OPS NORMAL.Dec 22, 2000 · N919UP · Boeing 72730C · Emergency LightingSDR DHL2000703007Reservoir · lowDURING TAXI WITH FLAPS EXTENDED "A" HYD SYS QUANTITY DECREASED TO 1.9 GALLONS, ON RETURN TAXI QUANTITY INCREASED TO 2.4 GALS WITH FLAPS RETRACTED. C/W A VISUAL INSP OF THE WING FLAP SYS (NO EXTERNAL LEAKS NOTED) FOUND RESERVOIR QUANTITY LOW. SERVICED RESERVDec 19, 2000 · N703DH · Boeing 72730C · Hydraulic Reservoir, MainSDR DHL2000701008Window · leakingPRESSURIZATION LEAK OUT OF R-1 WINDOW. RETORQUED SCREWS ON R-1 WINDOW PER M/M 56-11-11. GROUND RAN A/C AND PRESSURIZED TO 4 PSI, NO LEAKS NOTED.Nov 22, 2000 · N701DH · Boeing 72730C · Flight Compartment WindowsSDR DHL2000701007Indicator · malfunctionedNR 2 EGT HIGH AFTER T/O. CLIMB THRUST SET, HAD TO PULL BACK THRUST LEVER ENGINE NR 2 TO KEEP EGT FROM EXCEEDING LIMITS. ENG NR 2 THRUST REDUCED TO EPR 1.58, N1 82.2, EGT 505, N2 87.8, F/F 4500 LBS. REMOVED AND REPLACED NR 2 EGT INDICATOR WITH SERVICEABLE EGNov 8, 2000 · N701DH · Boeing 72730C · Engine Temperature Indicating SystemSDR DHL2000703006Tire · failedO/B LEFT MAIN TIRE BLOWN. REPLACED LEFT MAIN O/B AND I/B TIRES PER M/M 32-40.Oct 31, 2000 · N703DH · Boeing 72730C · TireSDR 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 DHL2000702003Transmitter · stuckNR 3 ENGINE OIL PRESSURE INDICATION STUCK AT 10 PSI. REMOVED AND REPLACED NR 3 ENGINE OIL PRESSURE TRANSMITTER IAW M/M 79-32-1.Oct 19, 2000 · N702DH · Boeing 72730C · Engine Oil Indicating SystemSDR DHL2000703005Adc · intermittentINTERMITTENT GYRO FLAG ON CAPTAINS ADI AND FLIGHT DIRECTOR FLAGS ON BOTH CAPTAINS AND F/OS. REMOVED AND REPLACED FLIGHT DIRECTOR COMPUTER.Oct 6, 2000 · N703DH · Boeing 72730C · Air Data ComputerSDR DHL2000703004Gyro · failedINTERMITTENT GYRO FLAG AND FLIGHT DIRECTOR FLAG. REMOVED AND REPLACED VERTICAL GYRO AND FLIGHT INSTRUMENT AMPLIFIER.Oct 6, 2000 · N703DH · Boeing 72730C · Attitude Gyro and Indicating SystemSDR DHL2000701006Fairing · missingRT FWD WING TO BODY FAIRING MISSING FROM A/C ON ARRIVAL AT CVG.Oct 2, 2000 · N701DH · Boeing 72730C · Aerodynamic FairingsSDR DHL2000703003Brake · malfunctionedAFTER ROTATION PRIOR TO GEAR RETRACTION THE LEFT I/B AND RIGHT O/B ANTI SKID RELEASE LIGHTS ILLUMINATED. PLACED ANTI SKID SYS ON DMI 2456 PER MEL 32-5. TROUBLESHOT SYS PER M/M 32-42-0, SYS CHKS OK. SWAPPED TRANSDUCERS FOR T/S. TEST OK PER M/M 32-42-0.Sep 29, 2000 · N703DH · Boeing 72730C · Brake Anti-Skid SectionSDR DHL2000701005Structure · corrodedFWD E&E COMPT-NOSE W/W RBL 146 WL 169 EXTRUSION OR CHORD HAS SPOTS OF CORROSION BETWEEN BS 328 AND BS 360.0 (RT WEB OF WALKWAY). REMOVED WALKWAY WL STA 294.5 TO STA 351 PER SRM 51-30-2. REMOVED FASTENERS AND VERT STIFFENERS FOR ACCSESS TO REMOVE CHORD ANGLE Sep 24, 2000 · N701DH · Boeing 72730C · Fuselage Main, StructureSDR DHL2000701004Screw · looseIN FLIGHT A/C MOMENTARILY PULLS TO THE LEFT. WHEN CORRECTION APPLIED A/C RETURNS TO LEVEL. THIS IS INTERMITTENT AND AT ALL SPEEDS AND FLAP CONFIGURATIONS. ABOVE 250 KTS AIRFRAME HAS A VERY LOUD RUMBLE. PULLED SPEED BRAKE WITH NO CHANGE. WHEN SLOWED BELOW 2Sep 23, 2000 · N701DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR DHL2000703002Bullet · contaminatedNR 3 ENGINE EPR READS HIGH N1 AND N2 LOW NR 3 THROTTLE 3 & 1/2 BEHIND NR 1 AND NR 2. BLEW DEBRIS FROM NR 3 BULLET. PERFORMED ENGINE RUN. OPS CHECK GOOD.Sep 12, 2000 · N703DH · Boeing 72730C · Engine Pressure Ratio (EPR)SDR DHLA200070301Stringer · corrodedFOUND LOCALIZED CORROSION AT STATION 650 STRINGER 18R IN LAP JOINT. INSTALLED FLUSH DOUBLER REPAIR ON LAP SEAM AT STR 18 RIGHT FROM BS 615 TO BS 621. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 53-30-3 FIG 15A. MATERIAL USED 7075-T6 0.080 SIZED 14 X 4 INCHESAug 18, 2000 · N703DH · Boeing 72730C · Fuselage Main, Longeron/StringerSDR 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 DHL2000701003Structure · vibrationTAKEOFF REJECTED BECAUSE OF AIRCRAFT SHAKING AND VIBRATING AT 40-50 KTS. INSPECTED NOSE GEAR AND TIRES, NO DEFECTS. INSPECTED MLG AND TIRES, NO DEFECTS. CREW PERFORMED HIGH SPEED TAXI, CHKD OK PER M/M 32-45-0. A/C OK FOR SERVICE.Aug 2, 2000 · N701DH · Boeing 72730C · Aircraft StructuresSDR DHL2000701002Connector · looseON INITAL GEAR EXTENSION NOSE GEAR AGREE LIGHT DID NOT ILLUMINATE. WARNING HORN SOUNDED AT FLAPS 30. NORMAL INDICATION UPON COMPLETION OF ABNORMAL PROCEDURES. MOMENTARY SOUNDING OF WARNING HORN UPON NLG TOUCHDOWN ON LANDING. FOUND NLG DOWNLOCK SWITCH CONNEJul 27, 2000 · N701DH · Boeing 72730C · Landing Gear Position and WarningSDR UPS00233393Unknown · odorINSPECTION TYPE:N/A, BRIEF ACRID SMELL DURING CLIMB. RAN ALL ENGS AND OPERATED PACKS. LOADED ELECTRICAL SYSTEM INCLUDING INTERIOR LIGHTING. COULD NOT FIND ANY ABNORMAL SMELL/ODOR.Jul 20, 2000 · N917UP · Boeing 72730C · Air Distribution SystemSDR UPS00233348Generator · overheatedINSPECTION TYPE:N/A, A/C DECLARED EMERGENCY WITH SMOKE IN THE COCKPIT WITH A CORRESPONDING TRIP ON THE NR 3 GENERATOR BREAKER. AIRCRAFT DIVERTED TO KMDT. MAINTENANCE FOUND THE NR 3 GENERATOR VOLTAGE REGULATOR VERY HOT AND A DOMINATE ELECTRICAL SMELL IN THE AJul 12, 2000 · N906UP · Boeing 72730C · Alternator-Generator DriveSDR 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 UPS00232976Cartridge · out of adjINSPECTION TYPE:N/A ATB-AILERON BINDING T/S PER MM CHAPT 27-10-00 PG 102,106,AND 107 ADJUSTED AILERON SPRING CARTRIDGE PER MM 27-10-00 OPS CHECKS GOOD ***SUPPLEMENTAL MRR***Jun 23, 2000 · N906UP · Boeing 72730C · Aileron Control SystemSDR UPS00233384Stringer · crackedINSPECTION TYPE:C, IN FORWARD LWR CARGO COMPARTMENT STA 670, STR 22R, THE STRINGER HAS A CORROSION CRACK. CUT OUT DAMAGED STRINGER SECTION AND INSTALLED REPAIR IAW SRM 53-10-3 FIG 1. MATERIAL USED (P/N BAC1498-142), DOUBLER 20 INCHES.Jun 17, 2000 · N917UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR UPS00233388Fitting · corrodedINSPECTION TYPE:C, EVIDENCE OF CORROSION IN PREVIOUS BLEND OUTS AT RIGHT SIDE BOTTLE PIN FITTING REAR LUG IN BUSHING BORE (FOUND AFTER BUSHING REMOVED). ACCOMPLISHED REPAIR IAW UPS ENGINEERING ORDER B727-5310-3056 AND BOEING DWG 65C23231, SH 1, 2 & 3.Jun 12, 2000 · N917UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS00233383Stringer · crackedINSPECTION TYPE:C, STRINGER 16 RIGHT CRACKED AT BS 480 AND BS 500. INSTALLED REPAIR AT STR 16R, BS 480 & BS 500 IAW SRM 53-10-3 FIG 1. MATERIAL USED (P/N BAC1498-140), SPLICE (P/N BAC1498-132).Jun 12, 2000 · N917UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR UPS00233387Angle · missingINSPECTION TYPE:N/A, VIEW FROM LEFT WHEEL WELL INSIDE KEEL BEAM, THE CENTER CHORD ANGLE HAS TWO AREAS OF MATERIAL MISSING. INSTALLED NEW CHORD ANGLE IAW BOEING DRAWING 65-18636 AND SRM 51-30- 2. MATERIAL USED 2024T3511, 50 INCHES.Jun 10, 2000 · N917UP · Boeing 72730C · Fuselage Main, Attach FittingsSDR UPS00233385Pin · corrodedINSPECTION TYPE:C, RIGHT WING FRONT SPAR WING-TO-BODY FITTING BOTTLE PIN CORRODED. RIGHT WING FRONT SPAR WING-TO-BODY FITTING BOTTLE PIN REPLACED IAW B727 MM 57-41-01.Jun 10, 2000 · N917UP · Boeing 72730C · Wing, Attach FittingsSDR UPS00233382Seat Track · wornINSPECTION TYPE:C, SEAT TRACK WORN BETWEEN BS 500 AND BS 520 AT RBL 24.75. REPLACED SECTION OF SEAT TRACK FROM STA 500 TO STA 520 AT RBL 24.75 IAW SRM 53-10-5 FIG 7. MATERIAL USED (P/N BAC1520-1432).Jun 10, 2000 · N917UP · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR UPS00233381Seat Track · damagedINSPECTION TYPE:C, SEAT TRACK DAMAGED AT FRAME STA 500 AND BL RIGHT 0.5. REPLACED SEAT TRACK FROM BS 500 TO BS 550, RBL 0.5 IAW SRM 53-10-5 FIG 7. MATERIAL USED (P/N BAC1520-1331).Jun 10, 2000 · N917UP · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR UPS00233380Seat Track · wornINSPECTION TYPE:C, SEAT TRACK WORN AT BS 1130 AND LBL 45.5. REPLACED SEAT TRACK FROM BS 1110 - 1130, LBL 45.5. MATERIAL USED (P/N BAC1520251) IAW B727 SRM 53-10-5 PG 5.Jun 10, 2000 · N917UP · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR UPS00233386Skin · corrodedINSPECTION TYPE:C AT FS 680, STR 19L HAS BULGE AREA ON SKIN. PERFORMED LFEC, SKIN LOSS 30 PERCENT. INSTALLED REPAIR DOUBLER IAW SRM 53-3 0-3 & DRAWING 69-61590 SHEET 12. MATERIAL USED 2024-T3, 0.063, 6 INCHES X 12 INCHES.Jun 7, 2000 · N917UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR 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 UPS00231947Slat · malfunctionedATB - NR 6 SLAT FAILED TO RETRACT RETURNED TO BFI. REPLACED NR 5, NR 6 AND NR 7 SLAT AND ADJUSTED PER M/M27-81-11 PAGE 401 NR 6 P/N ON 65-16222-92, OFF 65-16222-2, S/N ON BN81, OFF 319.Mar 10, 2000 · N919UP · Boeing 72730C · Leading Edge Slat Control SystemSDR DHL2000702002Cam · crackedMAIN CARGO DOOR SUPPORT CENTERING CAM CRACKED. INSTALLED CAM PER 53-30-0.Feb 18, 2000 · N702DH · Boeing 72730C · Cargo/Baggage DoorsSDR DHL2000701001Cam · crackedMAIN CARGO DOOR SUPPORT CENTERING CAM CRACKED. INSTALLED CAM PER 53-30-0.Feb 18, 2000 · N702DH · Boeing 72730C · Cargo/Baggage DoorsSDR DHL20007020Pin · installedAFTER TAKEOFF, GEAR WOULD NOT RETRACT. RETURNED FOR LANDING AND FOUND GEAR PINS INSTALLEDFeb 4, 2000 · N702DH · Boeing 72730C · Landing Gear Retraction/Extension SystemSDR DHL2000702001Pin · installedAFTER TAKEOFF, GEAR WOULD NOT RETRACT. RETURNED FOR LANDING AND FOUND GEAR PINS INSTALLED.Feb 4, 2000 · N702DH · Boeing 72730C · Landing Gear Retraction/Extension SystemSDR UPS00231383Light · malfunctionedL-1 DOOR EMERGENCY LIGHTS DIM. RESEATED L-1 DOOR EMERGENCY LIGHT PACK, LIGHT CHECKS NORMAL PER MM 3 3-50-01.Jan 21, 2000 · N906UP · Boeing 72730C · Emergency LightingSDR UPS00231382Support · crackedINSPECTION TYPE:C LEFT WING FIXED LEADING EDGE CAVITY VERTICLE OUTBOARD SUPPORT IS CRACKED FOR THE NR 2 SLAT INBOARD TRACK, INBOARD SUPPORT RIB. REPLACED LEFT WING FIXED LEADING EDGE CAVITY VERTICAL OUTBOARD SUPPORT AS PER SRM 57-20-03 FIG 2. MATERIAL USED 7Jan 5, 2000 · N906UP · Boeing 72730C · Wing Miscellaneous StructureSDR 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 DHL99702001Bolt · looseWHEN SELECTING FLAP 2 DEGREE UPON FLAP RETRACTION, AMBER L/E LIGHT FAILED TO EXTINGUSH. NO AMBER L/E LIGHTS ON S/O AUX PANEL WERE ILLUMINATED. FOUND AND SECURED 1 THROUGH BOLT ON FLAP DETENT SWITCH. CHECKED ADJUSTMENT AND OPS CHECK GOOD.Aug 31, 1999 · N702DH · Boeing 72730C · Leading Edge Slat Control SystemSDR DHL9970101AWeb · crackedAT A CHECK, 3.5 INCH CRACK NOSE WHEEL WELL 15 AFT OF FWD BULKHEAD LEFT SIDE. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER PER SRM 41-40-2.Aug 29, 1999 · N701DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR DHL9970334CTrack · crackedAT C CHECK, NR 3 FLAP TRACK MOVABLE FAIRING O/B TRACK CRACKED. REMOVED AND REPLACED TRACK PER SRM 51-30-2, N/R 5107.Aug 6, 1999 · N703DH · Boeing 72730C · Trailing Edge FlapsSDR DHL9970342CHinge Fitting · crackedAT C CHECK, RT TAIL SKID DOOR HINGE FITTING CRACKED. REMOVED AND REPLACED RT TAIL SKID DOOR HINGE FITTING PER SRM 51-30-2, N/R 3198.Jul 30, 1999 · N703DH · Boeing 72730C · Auxiliary Gear (Tail Skid)SDR DHL9970341CHinge Fitting · crackedAT C-CHECK, LEFT TAIL SKID DOOR HINGE FITTING CRACKED. REMOVED AND REPLACED LEFT TAIL SKID DOOR HINGE FITTING AS PER SRM 51-30-2, N/R 3197.Jul 30, 1999 · N703DH · Boeing 72730C · Auxiliary Gear (Tail Skid)SDR DHL9970336CBulkhead Skin · crackedAT C CHECK, CRACK AT BS 1183 BULKHEAD SKIN AFT CARGO COMPT WL 182 LBL 15. REMOVED FASTENERS AND STOP DRILLED CRACK PER SRM 51-30-2, AND 51-10-1 PG NR 7. PERFOMRED HFEC INSPECT. NO CRACK IND PAST STOP DRILLS. CUT OUT DAMAGED AREA PER SB 727-53-0175. REMOVEJul 30, 1999 · N703DH · Boeing 72730C · Fuselage Main, BulkheadSDR DHL9970335CBulkhead Skin · crackedC-CK, CRACK BS 1183 BULKHEAD SKIN, AFT BAG COMPT WL 182 RBL 15. OVERSIZED HOLE BY .015625 TO REMOVE INDAT WL190 RBL 15.5 AND ACCOMP PER SRM 51-10-1, VERIFIED CRACK NOT VISIBLE NDT PROCEDURE HFEC B727, PER NDT MANUAL PART 6510000 FIG 4. NO CRACK IND. DRILLEDJul 30, 1999 · N703DH · Boeing 72730C · Fuselage Main, Bulkhead
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