Pratt & Whitney JT3D-3

Service difficulty reports · 55

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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 engine_model_key = 'JT3D3'
  ORDER BY difficulty_date DESC"

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SDR U2RA485FLP5226Inu · inoperativeNR1, IMMEDIATELY AFTER ROTATION, NR 1 INU FAILED, CAPT INSTRUMENTS FLAGGED FAIL. NR 2, IMMEDIATELY AFTER ROTATION GPWS WENT INOP. NR 3, IMMEDIATELY AFTER ROTATION YAW DAMPER KICKED OFF AND A/P OR YAW DAMPER WOULD NOT ENGAGE FROM EITHER PILOTS A/P TRANSFER SWDec 14, 2010 · N155CA · Doug DC873F · Inertial Guidance SystemSDR IXXA10SMN069SLongeron · corrodedDURING ROUTINE C-CHECK INSP FOUND AFT ACCESSORY COMPARTMENT LONGERON L-23 RT INTERIOR CORRODED AT STA 1380-1400. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABERCATED SPLICES. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW Jun 19, 2010 · N71CX · Doug DC862F · Fuselage Main, Longeron/StringerSDR IXXA10SMN070SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND RT WING OTBD L/E OUTER SECTION LOWER SKIN CORRODED AT STA XFS 710.000 - 760.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSP. NO DISCREPANJun 19, 2010 · N71CX · Doug DC862F · Wing, Plate/SkinSDR IXXA10SMN071SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND THE LT WING OTBD FLAP UPPER SKIN DENTED AT STA XF 238.000 - 304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FJun 19, 2010 · N71CX · Doug DC862F · Trailing Edge FlapsSDR IXXA10SMN072SSkin · crackedDURING ROUTINE C-CHECK INSP FOUND RT WING NR 4 STUB WING LOWER SKIN CRACKED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, EXTERNAL DOUBLERS AND INTERNAL DOUBLERS. PERFJun 19, 2010 · N71CX · Doug DC862F · Wing, Plate/SkinSDR IXXA10SMN067SCargo Track · corrodedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 6 TRACK CORRODED AT STA 372.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED SPLICES. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW TRACK SEGMENT AND REJun 18, 2010 · N71CX · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA10SMN063SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT WING INBD L/E OUTER SECTION UPPER PART CORRODED AT STA XW 257.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER, AND FILLERS. Jun 17, 2010 · N71CX · Doug DC862F · Wing, Plate/SkinSDR IXXA10SMN065SAngle · corrodedDURING ROUTINE C-CHECK INSP, FOUND EMPENNAGE VERTICAL STABILIZER TO FUSELAGE LT JOINT ANGLE CORRODED AT STA 1640.382. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED ANGLE, FILLER AND TAPERED SHIMS. PERFORMED HEAT TREATMENT. CLEANED,Jun 17, 2010 · N71CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA10SMN066SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND LT HORIZ STABILIZER ELEVATOR LOWER SKIN CORRODED AT STA XE 195.313, 149.000, AND 132.750. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, FINGEJun 17, 2010 · N71CX · Doug DC862F · Elevator, Plate/SkinSDR IXXA10SMN064SFitting · corrodedDURING ROUTINE C-CHECK, INSP FOUND LT MLG WHEEL WELL FRAME FITTING CORRODED AT FS 879.000 LONGERON 24. REMOVED CORRODED FITTING. FABRICATED NEW FITTING, SPLICES AND DOUBLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FITTING AND REPAIR PARJun 16, 2010 · N71CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA10SMN061SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND LT WING UPPER PANEL EXTERNAL SKIN CORRODED AT STA XRS 204.000 STR 14. REMOVED CORROSION. FOUND OUT OF LIMITS. PERFORMED NDT INSP. NO DISCREPANCY FOUND. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED NEW SKIN AND Jun 16, 2010 · N71CX · Doug DC862F · Wing, Plate/SkinSDR IXXA100036OController · defectiveDURING CRUISE, CABIN RATE OF CLIMB RAISED QUICKLY TO 10,000 FT, FLIGHT ENGINEER RAN PNEUMATIC TO HIGH AND OPERATED THE PRESSURE CONTROL VALVE. THE CREW WAS PERMITTED PARTIAL CONTROL OF CABIN PRESSURE UNTIL ACFT DESCENDED BLOW FL200. THEY RETURNED TO DEPARTURE Jun 4, 2010 · N71CX · Doug DC862F · Cabin Pressure ControllerSDR IXXA100029SSkin · crackedDURING PREFLIGHT, FOUND VERTICAL STABILIZER L/E CRACKED AT STA ZFS 292 CTR LINE. REPLACED CRACKED L/E WITH INTERIM REPAIR IAW FVCI DWG NR 55-10165-1.May 1, 2010 · N71CX · Doug DC862F · Vertical Stabilizer, Plate/SkinSDR IXXA090065ORegulator · defectiveDURING CLIMB OUT FROM NR 2 ENG COMPRESSOR STALLED WITH GEAR UP, EPR 1.86 AND ANTI-ICE VALVE ON. THE CREW RETURNED TO WITHOUT FURTHER INCIDENT. MX REPLACED BOTH ANTI-ICE VALVE REGULATOR'S. OPS CHECK GOOD IAW MX MM 75-10-2. ACFT WAS RETURNED TO SERVICE.Nov 5, 2009 · N71CX · Doug DC862F · Compressor Bleed ValveSDR IXXA090038OAntenna · defectiveDURING CRUISE, WEATHER RADAR WILL NOT PAINT AND STABILIZATION INOP. THE CREW RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED WEATHER RADAR TRANSCEIVER AND RADAR ANTENNA. OPS CHECK GOOD IAW MM 34-41-1. ACFT WAS RETURNED TO SERVICE.Aug 5, 2009 · N71CX · Doug DC862F · Weather Radar SystemSDR IXX2008F00093Line · looseDURING TAKEOFF ROLL, NR (1) ENGINE WOULD NOT ACCELERATE PAST 78 PERCENT. NR 2 WITH CORRESPONDING LOW N1, FUEL FLOW AND EGT. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS. MAINT INSPECTED AND FOUND LOOSE PT2 LINE ON PRBC VALVE. MAINT RECONNECTED LINE. OPERSep 7, 2008 · N71CX · Doug DC862F · Engine (Turbine/Turboprop)SDR UPS08852685Structure · dentedDENT IN MAIN ENTRY DOOR AROUND AFT FRAME.Jul 8, 2008 · N868UP · Doug DC873F · Passenger/Crew DoorsSDR UPS08852664Frame · corrodedINSPECTION TYPE-C1, AREA OF CORROSION EXFOLIATON ON AFT SIDE OF STA 70 FRAME, A PIT, BETWEEN L29L AND L30L. REMOVED DAMAGE AND FABRICATED DOUBLER IAW SRM 53-02-05 FIG 008C.Jun 12, 2008 · N700UP · Doug DC871F · Fuselage Main, FrameSDR UPS07850577Starter · leakingINSPECTION TYPE:N/A IFSD - NR 1 ENG SHUTDOWN IN CLIMB PASSING 25000 DUE TO OIL QTY GOING TO ZERO. OIL PRESSURE WAS 12 PSI. SERVICED OIL, RAN ENGINE, FOUND OIL LEAKING FROM STARTER. REMOVED AND REPLACED NR 1 ENGINE STARTER IAW MM 80-10-01-2. OPS CHECK REQUISep 1, 2007 · N750UP · Doug DC871F · Engine CrankingSDR IXXA060453OEngine · leakingAPPROXIMATELY FIVE HOURS AFTER TAKEOFF FROM TAPA THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AND OIL PRESSURE DROPPED TO 20 PSI. THE ENGINE WAS SHUTDOWN AND CHECKLIST WAS COMPLIED WITH THE CREW RETURNED TO TAPA AND LANDED. MAINTENANCE FOUND THE OIL EJun 21, 2006 · N799AL · Doug DC862 · Turbine Engine Oil SystemSDR ARWA20051005Brake Assy · damagedLOG PAGE NR 117327. NR 2 MAIN WHEEL TIRE BLOWN; NR 2 BRAKE DAMAGED. REMOVED AND REPLACED NR 2 MAIN WHEEL IAW M/M 32-40-1; REMOVED AND REPLACED NR 2 BRAKE ASSEMBLY IAW MM 32-42-1, NO LEAKS NOTICE.Oct 20, 2005 · N661AV · Doug DC863F · BrakeSDR ABXA050090Indicator · defectiveON TAKEOFF AND CLIMB, NR 3 ENGINE OIL PRESSURE CLIMBED TO 75 - 80 PSI. TOOK THROTTLE TO IDLE, PRESSURE WENT TO 60 PSI. SECURED NR 3 ENGINE. AIR TURN BACK. AFTER SECURING THE ENGINE, THE PRESSURE READ 14 PSI STATIC ON TAXI. REPLACED NR 3 ENGINE OIL PRESSURApr 11, 2005 · N847AX · Doug DC861 · Engine Oil PressureSDR IXXA0400113OWarning Light · false activationDURING CRUISE AT FL 370 LOWER CARGO COMPARTMENT FIRE WARNING ILLUMINATED. DISCHARGED BOTH FIRE EXTINGUISHERS. CREW RETURNED AND LANDED WITHOUT INCIDENT. UPON LANDING MAINTENANCE INSPECTED ALL LOWER CARGO COMPARTMENTS AND FOUND NO EVIDENCE OF FIRE. REF DMI NROct 19, 2004 · N71CX · Doug DC862F · Fire DetectionSDR IXXA0400102OEngine · failedDURING CRUISE FROM KSUU TO PHIK, NR 4 ENGINE LOSS OF ALL OIL QUANTITY AND OIL PRESSURE OF 12PSI. ENGINE NR 4 OIL LIGHT CAME ON. CREW SHUT DOWN NR 4 ENGINE AND AFTER SHUT DOWN NR 4 ENGINE WINDMILLING OIL PRESSURE AT 5PSI. AIRCRAFT ARRIVED IN PHIK AND LANDED Aug 7, 2004 · N71CX · Doug DC862F · Engine Oil QuantitySDR UPS04842886Fitting · gougedINSPECTION TYPE: C3, C-1 DOOR AFT LOWER GUIDE PIN FITTING WORN GOUGED. REMOVED DAMAGED FITTING IAW UPS SRM 51-3-0. DAC DWG NR 5754075. FOUND TO BE OUT OF LIMITS IAW UPS SRM 53-2-0. RECEIVED NEW FITTINGS P/N NR SP 003923. LOCATED AND DRILLED AND DEBURRED FITJul 22, 2004 · N700UP · Doug DC871F · Cargo/Baggage DoorsSDR ARWA20040704Skin Panel · crackedDURING C-CHECK INSPECTION, RT WING BETWEEN XRS.428 AND XRS.463 AT STRINGER S-64 LOWER SKIN PANEL WITH CRACK, LENGTH 5.25 INCHES.Jul 19, 2004 · N661AV · Doug DC863F · Wing, Plate/SkinSDR UPS04842885Seat Track · crackedINSPECTION TYPE: C3 STA 65-75 RBL 36 SEAT TRACK LOBES OBLONGED. REMOVED FLOOR PANELS FS 70-170 FOM. REMOVED SEAT TRACK,DAMAGED OUT OF LIMITS IAW SRM 53-2-3. DRILLED NEW SEAT TRACK AND TRACK SPLICE TO FIT. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED FLOORJul 16, 2004 · N700UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS04842874Seat Track · wornINSPECTION TYPE: C3, STA 595-600 RBL 36 SEAT TRACK LOBES ELONGATED/OBLONGED. DAMAGE FOUND OUT OF LIMITS IAW SRM 53-2-3. REMOVED SEAT TRACK SECTION IAW SRM 51-3-0, DRILLED NEW SEAT TRACK SECTION TO FIT IAW SRM 51-1-24. INSTALLED IAW SRM 51-3-0 AND 51-3-1.Jul 2, 2004 · N700UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS04842876Floorboard · corrodedINSPECTION TYPE: C3, STA 280 RBL 1 FLOORBOARD CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED CORROSION SECTION OF FLOORBOARD FAB SPLICE PLATES. ALODINED AND PRIMED. INSTALLED SPLICE PLATES AND SECTION OF FLOORBOARD IAW SRM 51-3-0, 51-3-1, 5Jul 2, 2004 · N700UP · Doug DC871F · Fuselage Floor PanelSDR UPS04842877Floorboard · corrodedINSPECTION TYPE: C3, STA 235 RBL 8 FLOORBOARD CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED CORRODED FLOORBOARD. LOCATED NEW FLOORBOARD AND SPLICE PLATES. ALODINED AND PRIMED. INSTALLED FLOORBOARDS. ALL IAW SRM 51-3-0, 51-3-1, 51-1-8, AND 5Jul 2, 2004 · N700UP · Doug DC871F · Fuselage Floor PanelSDR UPS04842878Seat Track · gougedINSPECTION TYPE: C3, STA 1580 RBL 18 SEAT TRACK LOBES GOUGED AND OBLONGED. BLENDED OUT DAMAGED LOBES AND FOUND OUT OF LIMITS. REMOVED 4 HOLES SEAT TRACK PLUG P/N DC8-53B-007-002 PO NR SP0906208 AND INSTALLED IAW EO NR 5340-7779-B. ALL IAW SRM 53-2-0, 53-2-3, AJul 2, 2004 · N700UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS04842879Seat Track · wornINSPECTION TYPE: C3, SEAT TRACK (D) HAS WORN SCALLOPS AND LUGS BETWEEN FS 1560-1580 DOT NR D 973. BLENDED SEAT TRACK LUGS AND SCALLOPS, FOUND OUT OF LIMITS. OPEN FLOORBOARDS FROM FS 1495 TO 1690 LBL 16 TO LBL 32 IAW DC8 SRM 51-3-0 TO FOM, REMOVED SEAT TRACK Jul 2, 2004 · N700UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS04842880Seat Track · wornINSPECTION TYPE: C3 SEAT TRACK E HAS WORN SCALLOPS AND LUGS BETWEEN FS 1400 AND 1410. BLEND AREA IAW UPS SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW SRM 53-2-3, CUT OUT DAMAGE ON SEAT TRACK IAW EO 5340-7779B. ALODINED AND PRIMED CUT AREA, MAT ID PLUG SEAT TJul 2, 2004 · N700UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS04842881Longeron · crackedINSPECTION TYPE: C3, FUSELAGE INTERIOR L 17 RT CRACKED FROM FS 1770 TO FS 1774. REMOVED L17R AT STA 1766 IAW SRM 51-1-20D. RECIEVED NEW LONGERON PN 5 649327-43. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED LONGERON IAW SRM 51-1-21 AND 51-1-20D.Jul 1, 2004 · N700UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS04842882Frame · corrodedINSPECTION TYPE: C3, FLC BILGE FRAME HAS CORROSION AT FS 600 RBL 12. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. CUT PART OF FRAME WITH CORROSION FAB NEW FRAME SECTION IAW DWG 5750886. SECTION HEAT TREATED TO 17075+6 FAB SPLICES AND STAPS. SPLICES HEAT TREJun 30, 2004 · N700UP · Doug DC871F · Fuselage Main, FrameSDR UPS04842883Web · corrodedINSPECTION TYPE: C3, AFT PIT WEB CORRODED BETWEEN FS 1200 L35R. REMOVED WEB FROM STA 1160 TO 1220, MAT ID FOR WEB AND SPLICES 7075T6 .125 PO NR 424554.3 IAW DWG NR 3753772, FAB WEB AND SPLICES. ALODINED AND PRIMED IAW SRM 51-1-8, INSTALLED WEB FROM STA 1160Jun 30, 2004 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR ARWA20040602Indicator · erraticLOG PAGE NR 107344, AFTER ALL ENGINES SPOOLED AND TAKEOFF STARTED NR 1 EPR (ENGINE PRESSURE RATIO) ERRATIC; DISCONTINUED TAKEOFF AND TAXIED BACK TO RAMP. TRANSFERRED TO DMI NR 18568 IAW MM. AIRCRAFT RELEASED IAW MEL NR 77-1-2 CAT (A). REMOVED AND REPLACED NRJun 19, 2004 · N906R · Doug DC863F · Engine Pressure Ratio (EPR)SDR ARWA20040601Amplifier · malfunctionedDURING TAXI, NR 2 ENGINE FIRE WARNING INTERMITENTLY ILLUMINATED FIRE WARNING TEST INOPERATIVE, SHUT DOWN ENGINE; RETURNED TO RAMP. NO FIRE NOTED. CHECK FIRE WARNING SYSTEM AT RUNUP CONDITION. CHECK WIRING FOR CONDITION, ELEMENTS FOR CONDITION AT NR 2 ENGINJun 9, 2004 · N906R · Doug DC863F · Fire DetectionSDR 0375Frame · corrodedDURING CPCP TASK 5570-0551 FORWARD LOWER CARGO COMPARTMENT CIRCUMFERENTIAL FRAME LOWER LEG CORRODED AT FS 80 BETWEEN LONGERON 36R AND 35R AND IDENTIFIED AS LEVEL 2 CORROSION.Feb 17, 2004 · N865F · Doug DC863F · Fuselage Main, FrameSDR 0378Frame · crackedDURING CPCP TASK NR 5570-0551 FORWARD LOWER CARGO COMPARTMENT FORWARD FRAME FITTING CRACKED AT FS299 BETWEEN LONGERON 32R AND 33R.Feb 17, 2004 · N865F · Doug DC863F · Fuselage Main, FrameSDR U2R2004F00000Spar Cap · crackedDURING REPETIVE COMPLIANCE WITH AD AND SB, DETECTED 2 CRACKS AT RT WING FRONT SPAR LOWER CAP, REPAIRED IAW SB. REMAINING HOLES STRESS COINED TO CONDITION 1, OPTION 2.Oct 29, 2003 · N921R · Doug DC863F · Wing SparSDR IXXA0300059OValve · malfunctionedDURING CLIMB NR 4 ENG QTY DROPPED & OIL PRESS ROSE TO 60 PSI, TEMP INCREASED. POWER WAS REDUCED PARAMETERS REDUCED OIL PRESS, OIL TEMP REDUCED 20 DEGREES & OIL QTY INCREASED. OIL PRESS LIGHT NEVER ILLUM & OIL PRESS NEVER DROPPED BELOW 40 PSI. MX REMOVED & ISep 17, 2003 · N728PL · Doug DC862 · Turbine Engine Oil SystemSDR ARWA20030606Pin · damagedON WALK-AROUND FOUND LT MAIN LANDING GEAR EYEBOLT ACTUATOR WITH EXCESSIVE GAP AT PIN BOSS ATTACHMENT. REMOVED LT MAIN LANDING GEAR ROUTED TO SHOP FOR ACTUATOR PIN REPLACEMENT, REINSTALLED SERVICIABLE MAIN LANDING GEAR IAW MM 32-11-0, OPERATIONAL LEAK CHECK OKJun 25, 2003 · N661AV · Doug DC863F · Landing Gear Retraction/Extension SystemSDR UPS03840930Longeron · crackedINSPECTION TYPE: C LONGERON 17L AND FWD END FITTING CRACKED AT BS 1768 REMOVED LONGERON 17L AND END FITTING. LOCATED, DRILLED LONGERON AND END FITTING IAW SRM 51-1-24. REMOVED AND REINSTALLED HYDRAULIC CASE AND LINES AT STA 1768 IAW MM 20-12-00. INSJun 16, 2003 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03840931Door Frame · mislocatedINSPECTION TYPE: C, MAIN CABIN AT STA 1660-R2 DOOR JAMB WEB HAS DOUBLE DRILLED HOLES. REM FASTENERS FROM DOOR JAMB WEB. REM AIR GRILL AND R2 DOOR DRAIN PAN. TRIMMED OUT DAMAGE FOUND TO BE OUT OF LIMITS IAW DC8 DWG DC8-53A-01 0 AND UPS EO DC8-5310-11728-AJun 16, 2003 · N851UP · Doug DC873F · Fuselage Main, StructureSDR UPS03840908Longeron · crackedINSPECTION TYPE: C3 AFT PIT FS 1350, LONGERON 35L IS CRACKED. REMOVED CRACKED LONG 35L FS 1270 TO 1350 IAW SRM 51-1-20D. LOCATED AND DRILLED UP NEW LONG IAW SRM 51-1-24. INSTALLED NEW LONG 3 5L FS 1270-1350 IAW SRM 51-1-20D AND 51-3-0.Jun 6, 2003 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03840907Skin · crackedINSPECTION TYPE:C3 LOWER FUSELAGE CENTER SECTION AT FS 1350 LONGERON 34L FUSELAGE SKIN IS CRACKED. REMOVED 2 EA EXISTING REPAIR DOUBLERS, TRIMMED OUT CRACK FS 1350 LONG 34L FABBED REPAIR DOUBLER COMBINING 2 EA EXISTING REPAIR DOUBLERS, FABBED SKIN FILLERS ANJun 5, 2003 · N851UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03840906Longeron · crackedINSPECTION TYPE:C3 MAIN CABIN AT FS 1660, LONGERON 11R IS CRACKED. REMOVED OLD LONG 11RT TO FOM , LOCATED, DRILLED, DEBURRED AND INSTALLED NEW LONG 11RT IAW DC8 SRM 51-1-21.Jun 4, 2003 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03840932Angle · crackedINSPECTION TYPE: C, R/W/W KEEL BEAM INSIDE ACCESS DOVER STA 935, BEAM IS CRACKED REM MLG LT AND RT DOOR ACTUATORS, LT AND RT W/W WEBS TO FOM. LOC DRI LLED AND INSTALLED NEW SPLICE ANGLE IAW DAC DWG 5750371 P/N 5750042- 1N. FAB -51, -53, -55, -57 AND -59 RJun 3, 2003 · N851UP · Doug DC873F · Fuselage Main, KeelSDR ABXA020364Link · brokenRT WING INBOARD SPOILER WOULD NOT DEPLOY. REMOVED AND REPLACED BROKEN ACTUATOR CRANK LINKS IN THE INBOARD AND OUTBOARD POSITIONS FOR THE RT INBOARD SPOILER PANEL IAW MM. OPS CHECKED GOOD.Dec 18, 2002 · N842AX · Doug DC861 · Drag Control System
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