N284KH, cancelled May 14, 2007

Service difficulty reports · 57

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 = 'N284KH' AND deregistration_id = 'N284KH-2007-05-14'
  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 GAIA06027OPShutoff Valve · closedDURING CLIMB THE NR 2 ENGINE OIL FILTER BYPASS/LOW PRESSURE LIGHT ILLUMINATED. THE OIL PRESSURE TEMPERATURE AND QUANTITY WERE NORMAL. THE NR 2 ENGINE FLAMED OUT SHORTLY AFTERWARD. THE FLIGHT CREW PERFORMED THE ENGINE FAILURE CHECKLIST AND RETURNED. THE AIRAug 25, 2006 · N284KH · Boeing 7272J0 · Fuel Selector/Shut-Off ValveSDR GAIA05019OPLight · illuminatedEMERGENCY EXIT DOOR LIGHT ON ALL THE TIME. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. AIRCRAFT RETURNED TO SERVICE. (K)Apr 4, 2005 · N284KH · Boeing 7272J0 · Emergency LightingSDR GAIA05016OPBattery Pack · dischargedDURING PREFLIGHT, FOUND L1 DOOR AND COCKPIT ENTRY DOOR EMERGENCY BATTERY PACKS DRAINED TO DIM ILLUMINATION. REPLACED BATTERY PACKS (2 EA). OPERATED EMERGENCY LIGHTS SYSTEM AND FOUND OPERATING NORMALLY. OK FOR SUBSEQUENT FLIGHT. AC WAS RETURNED TO SERVICE. Mar 25, 2005 · N284KH · Boeing 7272J0 · Emergency LightingSDR GAIA05002OPO-Ring · damagedDURING CRUISE THE FLIGHT CREW SHUT DOWN THE NR 2 ENGINE DUE TO LOSS OF OIL QUANTITY AND PRESSURE. THE AIRCRAFT DIVERTED, AND MADE AN UNEVENTFUL LANDING. REMOVED AND REINSTALLED NR 2 ENGINE FUEL PUMP, REPLACED FUEL PUMP GARLOC SEAL AND SHAFT O-RING PACKING. Jan 18, 2005 · N284KH · Boeing 7272J0 · Turbine Engine Oil SystemSDR GAIA04171OPGasket · blownDURING CLIMB, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED, WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND BLOWN GASKET AND LOOSE CLAMPS AND DUCT LEAKS. REMOVED AND REPLACED GASKET AND TIGHTENED CLAOct 19, 2004 · N284KH · Boeing 7272J0 · Engine Bleed Air SystemSDR GAIA04168OPSequence Valve · crackedFLT 715 - ELP-FWA - ON TAKEOFF DURING GEAR RETRACTION THE FLIGHT CREW NOTICED THE A-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ELP WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND LEFT MLG SEQUENCE VALVE LESep 30, 2004 · N284KH · Boeing 7272J0 · Landing Gear Retraction/Extension SystemSDR GAIA02051STStringer · crackedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT STRINGER 15 LEFT IS CRACKED AT BS 720B PLUS 5. ACCOMPLISHED STRINGER REPAIR AT BS 720B PLUS 5 STRINGER 15 LEFT IAW B727 SRM 53-10-3 FIG 5. (M)May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Main, Longeron/StringerSDR GAIA02052STStringer · crackedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT STRINGER 15 LEFT IS CRACKED AT BS 720B PLUS 15. ACCOMPLISHED STRINGER REPAIR AT BS 720B PLUS 15 STRINGER 15 LEFT IAW B727 SRM 53-10-3 FIG 5. (M)May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Main, Longeron/StringerSDR GAIA02053STSeat Track · damagedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE MAIN CABIN SEAT TRACK RBL 24.75 IS DAMAGED SEVERAL DIFFERENT PLACES FROM BS 480-530. ACCOMPLISHED SEAT TRACK REPAIR AT BS 480-530 RBL 24.75 IAW B727 SRM 53-10-5 FIG 1. (M)May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA02054STStiffener · crackedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE PRESSURE BULKHEAD BS 1183 VERTICAL BEAM LBL 36.9 CRACKED AT WL 245. ACCOMPLISHED BS 1183 VERTICAL BEAM REPAIR AT LBL 36.9 IAW S/B 727-53-0192. (M)May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Miscellaneous StructureSDR GAIA02055STSkin · crackedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE SKIN IS CRACKED AT THE FORWARD ENTRY DOOR LOWER HINGE CUT OUT. ACCOMPLISHED FUSELAGE SKIN REPAIR AT THE FORWARD ENTRY DOOR LOWER HINGE CUT OUT IAW S/B 727-53-0198. (M)May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Main, Plate/SkinSDR GAIA02056STWeb · corrodedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT STATION 1230 AFT FACE OF THE TAIL SKIN CAVITY BULKHEAD, CORROSION ON SUPPORT ANGLE AND WEB VISIBLE THROUGH AIRSTAIR CUT-OUT, AFT OF THE TAIL SKID. ACCOMPLISHED BS 1230 WEB AND T-ANGLE REPAIR IAW B727 SRM 51-May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Miscellaneous StructureSDR GAIA02057STWeb · crackedDURING A CHECK INSPECTION, IT WAS DISCOVERED THAT VENTRAL STAIR AREA STATION 1225 LBL 12, VERTICAL WEB HAS A CRACK AT THE LIGHTENING HOLE. ACCOMPLISHED BS 1225, LBL 12 WEB REPAIR IAW B727 SRM 51-40-2 FIG 1. (M)May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Miscellaneous StructureSDR GAIA02058STWeb · crackedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT VENTRAL STAIR AREA STATION 1232 LBL 14, VERTICAL WEB IS BUCKLED WITH A 3 INCH CRACK OUTBOARD OF 5TH STEP FROM TOP. ACCOMPLISHED BS 1232, LBL 14 CRACKED WEB ANGLE REPLACEMENT IAW B727 SRM 53-10-2 FIG 6. (M)May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Miscellaneous StructureSDR GAIA02059STWeb · crackedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE VENTRAL STAIR AREA STATION 1244 RBL 12 VERTICAL WEB HAS 1 CRACK AT THE LIGHTENING HOLE. ACCOMPLISHED TORQUE BOX WEB REPAIR IAW B727 SRM 51-40-2 FIG 1. (M)May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Miscellaneous StructureSDR GAIA02060STSpar · corrodedDURING A C-CHECK INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED LEFT WING FRONT SPAR LOWER CHORD IS CORRODED UNDER AND INBOARD OF EXISTING REPAIR INSIDE L/E COVE AREA AT LES 200-240. ACCOMPLISHED LEFT WING LEADING EDGE LOWER SKIN AND SPAR CHORD REPAIR IAW AVITASMay 17, 2002 · N284KH · Boeing 7272J0 · Wing SparSDR GAIA02061STSpar · corrodedDURING A C-CHECK INSPECTION AT FLIGHT STAR, IT WAS DISCOVERED LEFT WING FRONT SPAR UPPER SURFACE AT WS 410 IS CORRODED. ACCOMPLISHED LEFT WING FRONT SPAR LOWER CHORD UPPER SURFACE REPAIR IAW B727 SRM 57-30-4 FIG 6. (M)May 17, 2002 · N284KH · Boeing 7272J0 · Wing SparSDR GAIA02062STHinge · crackedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED THE MAIN CARGO DOOR HINGE AFT UPPER SECTION IS CRACKED. ACCOMPLISHED MAIN CARGO DOOR HINGE UPPER AFT SECTION REPLACEMENT IAW B727-200 MM AEI STC SA179SO. (M)May 17, 2002 · N284KH · Boeing 7272J0 · Cargo/Baggage DoorsSDR GAIA02063STIntercostal · crackedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED IN THE AFT CARGO COMPARTMENT BETWEEN BS 1030 AND 1050 AT STRINGER 25L, INTERCOSTAL IS CRACKED. ACCOMPLISHED INTERCOSTAL REPLACEMENT IAW B727 SRM 53-10-2 FIG 5. (M)May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Miscellaneous StructureSDR GAIA02064STIntercostal · crackedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED IN THE FORWARD CARGO COMPARTMENT, INTERCOSTAL IS CRACKED BETWEEN BS 950A-950B AT STRINGER 25L. ACCOMPLISHED INTERCOSTAL REPAIR IAW B727 SRM 51-40-3 FIG 1. (M)May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Miscellaneous StructureSDR GAIA02065STStringer · crackedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED STRINGER 18A RIGHT IS CRACKED AT BS 940 RUNNING AFT FROM RADIUS BLOCKS AT THE BASE OF THE HORIZONTAL LEG. ACCOMPLISHED STRINGER 18A REPAIR IAW BOEING DRAWING 65C27166. (M)May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Main, Longeron/StringerSDR GAIA02066STSkin · corrodedDURING A C-CHECK INSPECTION, IT WAS DISCOVERED DISHED FASTENERS ON FUSELAGE SKIN AT BS 351, BELOW STRINGER 26R. ACCOMPLISHED SKIN PANEL AND T-CHORD REPLACEMENT IAW B727 SRM 53-30-2, FIG 2 AND SRM 51-30-2. (M)May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Main, Plate/SkinSDR GAIA01126STDoubler · leakingDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING AT STATION 224.5 HAD A PREVIOUS DOUBLER REPAIR THAT WAS LEAKING FUEL FROM SEVERAL HI-LOCKS FASTENERS. REMOVED AND REPLACED DOUBLER IAW KHA EA B7-57-025. FLIGHT VEHICLES CONSULTING DRAWING 57-0Apr 13, 2001 · N284KH · Boeing 7272J0 · Wing, Plate/SkinSDR GAIA00795Switch · out of adjNR2 LEADING EDGE FLAP DEPLOYED IN FLIGHT. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT ANY FURTHER DIFFICULTIES.ADJUSTED NR2 LEADING EDGE FLAP SWITCH, ONE TURN AND RESAFETIED. OPS CHECKED GOOD ON GROUND. AIRCRAFT RETURNED TO SERVICE.Dec 22, 2000 · N284KH · Boeing 7272J0 · Leading Edge Slat Position Indicating SystemSDR GAIA00524Door · malfunctionedFLT 1729 - DEN-FWA - AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT GO PAST OFF, GEAR AND DOORS LIGHTS WERE ALL ILLUMINATED. CYCLED THE GEAR THREE TIMES AND THERE WAS NO CHARGE. THE AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. JACKED AIRCSep 20, 2000 · N284KH · Boeing 7272J0 · Landing Gear Door Retract SectionSDR GAIA0088Battery · dischargedDURING ROUTINE MAINTENANCE AT HNL, IT WAS DISCOVERED THAT THE EMERGENCY EXIT LIGHTS WOULD NOT RETAIN A CHARGE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BATTERIES. OPERATIONAL CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 14, 2000 · N284KH · Boeing 7272J0 · Emergency LightingSDR GAIA9974O-Ring · deterioratedDURING BOS-TOL - FLT 715 - DURING DESCENT AT FL280, THE FLIGHT CREW NOTICED THAT THE NR 1 ENGINE WOULD ONLY PRODUCE PARTIAL POWER. THE FLIGHT CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN ON THE NR 1 ENGINE AND DECLARED AN EMERGENCY. THE AIRCRAFT CONTINUED Jun 16, 1999 · N284KH · Boeing 7272J0 · Fuel Controlling SystemSDR GAIA9973Connector · dirtyFLT 504 - DURING CLIMB-OUT FROM TOL, THE NR 5 SLAT INDICATE AS NOT RETRACED WHILE ALL OTHER TRAILING AND LEADING EDGE DEVICES WERE RETRACTED. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO TOL. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. CLEANED NR 5 SJun 8, 1999 · N284KH · Boeing 7272J0 · Leading Edge Slat Position Indicating SystemSDR GAIA9997Pitot Tube · cloggedAFTER TAKEOFF FROM AUS TO STL, FLIGHT 721, HAD THE CO-PILOTS AIRSPEED INDICATOR DECREASE 40 TO 50 KNOTS FROM THE CAPTAINS AIRSPEED INDICATOR. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO AUS. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. FOUND AN OBSTRJun 7, 1999 · N284KH · Boeing 7272J0 · Pitot/Static SystemSDR GAIA9960APin · missingMCO - FLT 1726 - AFTER TAKEOFF, RETRACTED GEAR AND GEAR DOOR LIGHT REMAINED ON. RECYCLED GEAR AND LIGHT REMAINED ON. PROCEEDED TO MEM AND LANDING WAS SMOOTH. BRAKING WAS STARTED AT 80 KIS, RUMBLE WAS NOTICED IN THE AIRCRAFT. UNABLE TO STEER AIRCRAFT. AIRCMay 27, 1999 · N284KH · Boeing 7272J0 · Nose/Tail Landing GearSDR 98ZZZX2710B Nut · looseAIRCRAFT DIVERTED INTO KFLL DUE LOSS OF A-SYSTEM HYDRAULIC FLUID: FOUND B-NUT NR 1 ENGINE MAIN HYD LINE LOOSE. TIGHTENED B-NUT. CHECKED CASE DRAIN FITTINGS. PRESSURE CHECKED SYSTEM. RELEASED AIRCRAFT.Jul 2, 1998 · N284KH · Boeing 7272J0 · Hydraulic System, MainSDR 98ZZZX2546B-Nut · looseAIRCRAFT DIVERTED INTO KFLL. DUE LOSS OF A-SYSTEM HYDRAULIC FLUID, FOUND B-NUT NR 1 ENGINE MAIN HYDRAULIC LINE LOOSE. TIGHTENED B-NUT, CHECKED CASE DRAIN FITTINGS. PRESSURE CHECKED SYSTEM. RELEASE AIRCRAFT.Jul 2, 1998 · N284KH · Boeing 7272J0 · Hydraulic System, MainSDR B4MR97031Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND LFT WING, O/B MID FLAP, L/E LWR SURFACE, CORROSION ON TWO AREAS. (REFERENCE: O/B ATTACHED FAIRING FWD AREA). REPAIRED IAW ENGINEERING SKETCH NR AIA/E/2587, APPROVED BY FAA FORM 8110-3 DATED 7-21-97 PN=7075-T6 0.125IN. Sep 26, 1997 · N284KH · Boeing 7272J0 · Wing, Plate/SkinSDR B4MR97030Angle · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND LEFT MLG WW, AFT BULKHEAD LWR CENTER AREA, CORROSION ON T-ANGLE. REMOVED CORROSION ON T-ANGLE, FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. REMOVED DAMAGED AREA, REPAIRED T-ANGLE IAW B727 SRM 51-40-4, 51-30-2 AND MSep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage Miscellaneous StructureSDR B4MR97029Structure · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND LT WING L/E AREA, NR 2 L/E FLAP STA 212 HAS SUPPORT ANGLE WEB CORRODED AND CORROSION AROUND ANCHOR NUTS. FOUND CORROSION TO BE OUT OF LIMITS IAW B727 SRM 57-20-1. REMOVED AND REPLACED ACCESS WEBBING PANEL, TOP COVESep 26, 1997 · N284KH · Boeing 7272J0 · Wing Main, Frame StructureSDR B4MR97028Floorbeam · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND STA 328 FLOORBEAM AT LBL 3 HAS CORROSION. REPAIRED FLOORBEAM IAW B727 SRM 53-10-8 FIG 3. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 110399.Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage Main, Floor BeamSDR B4MR97027Seat Track · wornDURING ROUTINE CPCP CHECK INSPECTION, FOUND FE SEAT TRACK IS WORN. REPLACED FE SEAT TRACK IAW B727 BOEING MM CHAPTER 25-10-81. CORROSION TASK CARD NUMBER C53-221-01. NON-ROUTINE TASK CARD NUMBER 110442.Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach FittingsSDR B4MR97026Skin · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND TOP RT ELEVATOR ES92 AREA HAS SURFACE CORROSION OUT OF LIMITS. REPAIRED AND REPLACED A PIECE OF TOP SKIN IAW B727 SRM 55-20-3 FIG 2 PN=2024-T3 .032. CORROSION TASK CARD NUMBER C55-300-10. NON-ROUTINE TASK CARD NUMSep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage Main, Plate/SkinSDR B4MR97025Skin · corrosionDURING ROUTINE CPCP CHECK INSPECTION, FOUND FORWARD PIT FS 686 S26R TO 25R HAS SURFACE CORROSION ON INTERNAL SKIN. CORROSION OUT OF LIMITS IAW B727 SRM 53-30-1. REPAIRED IAW SRM 53-30-3 FIG 5 PN=2024-T3. CORROSION TASK CARD NUMBER C53-113-01. NON-ROUTINE TSep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage Main, Plate/SkinSDR B4MR97024Skin · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND RT MLG W/W OUTBD, ABOVE MLG BEAM, BETWEEN STA 930 AND 940 PRESSURE DECK SKIN AND FASTENERS HAVE CORROSION. REPAIRED AREA (CORROSION OUT OF LIMITS IAW B727 SRM 53-10-1) IAW SRM 53-10-9 FIG 4 PN=2024-T3. CORROSION TASep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage Main, Plate/SkinSDR B4MR97023Support · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND COCKPIT AREA, CO-PILOT SEAT BASE SUPPORT NEEDING ANTI CORROSION TREATMENT ON BOTH AFT ATTACH POINTS. REMOVED AND REPLACED CO-PILOT SEAT BASE SUPPORT IAW BOEING B727 MM CHAPTER 25-10-42. NEW BASE SUPPORT REQUIRED DUSep 26, 1997 · N284KH · Boeing 7272J0 · Flight Compartment EquipmentSDR B4MR97022Keel Beam · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND KEEL BEAM RT W/W UNDER APU ANGLE CORRODED TOP AND BOTTOM. OUT OF LIMITS PER SRM 53-10-1. REPAIRED PER SRM 51-40-4 PN=7075-T6 OR 2X2X.150. CORROSION TASK CARD NUMBER C53-132-01. NON-ROUTINE TASK CARD NUMBER 108224Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage Main, KeelSDR B4MR97021Seat Track · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND SEAT TRACK LBL 40 STA 1140 TO 1030 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 51-10-1 AND 51-30-2. CORROSION TASK CARD NUMBER C53-111-01. NON-ROUTINE TASK CARD NUMBER 108166.Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach FittingsSDR B4MR97020Seat Track · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND SEAT TRACK LBL 20 STA 1140 TO 1030 CORRODED. REPAIRED SEAT TRACK PER B727 SRM 53-10-5 CORROSION WAS FOUND TO BE OUT OF LIMITS PER SRM 51-10-2. CORROSION TASK CARD NUMBER C53-111-01. NON-ROUTINE TASK CARD NUMBER 108Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach FittingsSDR B4MR97019Seat Track · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND SEAT TRACK RBL 20 STA 1140 TO 1030 CORROSION. REPAIRED SEAT TRACK PER B727 SRM 53-10-5 CORROSION WAS FOUND TO BE OUT OF LIMITS PER SRM 51-10-2. CORROSION TASK CARD NUMBER C53-111-01. NON-ROUTINE TASK CARD NUMBER 1Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach FittingsSDR B4MR97018Seat Track · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND SEAT TRACK RBL 40 STA 1140 TO 1030 CORROSION. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 51-10-1 AND 51-30-2. CORROSION TASK CARD NUMBER C53-111-01. NON-ROUTINE TASK CARD NUMBER 108163.Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach FittingsSDR B4MR97017Seat Track · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND STA 1050 TO 1070 LBL 40 SEAT TRACK CORRODED (OLD REPAIR). REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 51-10-1 AND 51-30-2. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 107834.Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach FittingsSDR B4MR97016Seat Track · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND STA 1070 TO 1090 RBL 46 SEAT TRACK CORRODED AROUND NUT PLATE AND BETWEEN TRACK AND FLOORBEAM. REMOVED AND REPLACED SEAT TRACK IAW B727 51-10-1 AND 51-30-2. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CSep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach FittingsSDR B4MR97015Heat Plenem · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND HEAVY CORROSION LT HEAT EXCHANGER PLENEM TOP PLATE AFT END REPAIR PREVIOUSLY ACCOMPLISHED IS CORRODED. ALSO, REPAIRED DAMAGE AREA IAW BOEING REPORT KHC-ORD-97-0003RR DATED 9-JUL-97, APPROVED BY FAA FORM 8110-3 DATEDSep 26, 1997 · N284KH · Boeing 7272J0 · Heating SystemSDR B4MR97014Skin · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND STA 1090R FWD EDGE OF NR 3 CARGO DOOR OPENING HAS CORROSION UNDER LOWER END OF SKIN DOUBLER APPROX STR 25R. REMOVED AND REPLACED RT SKIN FROM STA 1010 TO 1090, STR 20 TO 26 IAW B727 SRM 51-10-1 AND 51-30-2 AND INSTASep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage Main, Plate/Skin
Back to N284KH, cancelled May 14, 2007