Boeing 727-2J0

Service difficulty reports · 220

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '7272J0'
  ORDER BY difficulty_date DESC"

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SDR 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 RIVA020308Beam · corrodedMQY - FOUND RIGHT HORIZONTAL STAB UPPER TRAILING EDGE BEAM AT REAR SPAR STATION 151.81 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW B727 SRM 55=10-1, FIG 1. REMOVED AND REPLACED TRAILING EDGE BEAM IAW B727 SRM 51-30-5 AND B727SRM 51-30-2. PART REPLACED WITHMar 8, 2002 · N362PA · Boeing 7272J0 · Horizontal Stabilizer Miscellaneous StructureSDR RIVA020308ASkin · brokenMQY - FOUND LEFT WING INBOARD FLAP INBOARD END OF FORE FLAP UPPER SURFACE SKIN IS WORN AND HAS PIECES BROKEN OFF WS 220. REMOVED DAMAGED SECTION. FABRICATED FILLER DOUBLER AND INSTALLED PER EO NR 01-298 WITH APPROVED 8110-3. APPRECIABLE WEIGHT ADDED BY THISMar 8, 2002 · N362PA · Boeing 7272J0 · Leading Edge DevicesSDR RIVA020308BDoor Frame · crackedMQY - FOUND R-1 DOOR LOWER FORWARD CORNER WEB CRACKED 2.5 INCHES LENGTH STATION 380, STRINGER 17R. CUT OUT DAMAGED SECTION. FABRICATED NEW SECTION AND SPLICES AND INSTALLED PER EO NR 01-298 WITH APPROVED 8110-3. APPRECIABLE WEIGHT ADDED BY THIS REPAIR IS .6Mar 8, 2002 · N362PA · Boeing 7272J0 · Fuselage Main, StructureSDR RIVA020308CDoor Frame · corrodedMQY - FOUND R-1 DOOR AFT JAMB HAS CORROSION AT UPPER CAM FITTING STATION 420. CUT OUT DAMAGED AREA. FABRICATED FILLER/REPAIR ANGLE AND INSTALLED PER EO NR 01-298 WITH APPROVED 8110-3. APPRECIABLE WEIGHT ADDED BY THIS REPAIR IS .55 LB STATION 420. (M)Mar 8, 2002 · N362PA · Boeing 7272J0 · Fuselage Main, StructureSDR RIVA020308EFloorbeam · corrodedMQY - FOUND FLOORBEAM CORRODED AT STATION 1110 FROM LBL 45 INCHES TO RBL 20 INCHES HAS BEEN BLENDED TO LIMITS IAW B727 SRM 53-10-1, FIG 4. CORROSION STILL EXISTS IN AREA. REMOVED AND REPLACED UPPER T-CHORD AT STATION 1110 LBL 69 TO RBL 34.5 IAW B727 SRM 53-1Mar 8, 2002 · N362PA · Boeing 7272J0 · Fuselage Main, Floor BeamSDR RIVA020308FFloorbeam · corrodedMQY - FOUND STATION 344 FLOORBEAM CORROSION REMOVED TO MAX LIMITS PER SRM. CORROSION STILL EXISTS RBL 25 INCHES - LBL 25 INCHES. REMOVED DAMAGED SECTION AND REPLACED WITH NEW T-CAP AND SPLICES IAW B727 SRM 53-10-8, 51-30-2 AND 51-10-2. NEW REPLACEMENTS PARTMar 8, 2002 · N362PA · Boeing 7272J0 · Fuselage Main, Floor BeamSDR RIVA020308GFloorbeam · corrodedFOUND STATION 380 FLOORBEAM CORROSION. REMOVED TO MAX LIMITS PER SRM. CORROSION STILL EXISTS RBL 13 INCHES - 33 INCHES RBL. REMOVED EXISTING REPAIR T-CAP. FABRICATED NEW SECTION AND INSTALLED IAW B727 SRM 53-10-8, FIG 3 AND 51-10-2, 51-30-2. NEW REPLACEMEMar 8, 2002 · N362PA · Boeing 7272J0 · Fuselage Main, Floor BeamSDR RIVA020308HFloorbeam · corrodedMQY - FOUND STATION 400 FLOORBEAM CORROSION REMOVED TO MAX LIMITS PER SRM. CORROSION STILL EXISTS LBL 18 INCH - RBL 15 INCH. REMOVED AND INSTALLED REPAIR SECTION T-EXTRUSION IAW B727 SRM 53-10-8, FIG 3 AND 51-10-2. NEW REPLACEMENT PARTS USED. NO CHANGE IN WMar 8, 2002 · N362PA · Boeing 7272J0 · Fuselage Main, Floor BeamSDR RIVA0203081Rib · puncturedMQY - FOUND RIGHT ELEVATOR UPPER SKIN STATION 173 LOWER RIB PUNCTURED 3 PLACES. FABRICATED REPAIR DOUBLER IAW B727 SRM 55-20-3. TREATED AND PRIMED IAW B727 51-10-2. INSTALLED DOUBLER IAW B727 SRM 51-30-2. APPRECIABLE WEIGHT ADDED BY THIS REPAIR .120 LB AT Mar 8, 2002 · N362PA · Boeing 7272J0 · Elevator, Spar/RibSDR RIVA020308JFloorbeam · corrodedMQY - FOUND FLOORBEAM STATION 420 RBL 3 INCH CORROSION BLEND TO LIMITS IAW B727 SRM 53-10-1, FIG 4 CORROSION STILL EXISTS. CUT OUT CORRODED AREA PER B727 SRM 53-10-8, FIG 8. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED FILLER AND REPAIR ANGLES PER SRM 53-1Mar 8, 2002 · N362PA · Boeing 7272J0 · Fuselage Main, Floor BeamSDR RIVA020308KFloorbeam · corrodedMQY - FOUND FLOORBEAM STATION 328 UPPER FLANGE CORRODED BEYOND LIMITS LBL 30 INCHES AND RBL 13 INCHES UPPER AND LOWER SURFACES. REMOVED DAMAGED SECTION IAW B727 SRM 53-10-8. FABRICATED REPAIR SECTION AND SPLICES IAW B727 SRM 53-10-8. TREATED, PRIMED AND INSMar 8, 2002 · N362PA · Boeing 7272J0 · Fuselage Main, Floor BeamSDR RIVA020308LSkin · damagedMQY - FOUND LEFT OUTBOARD FORE FLAP TRAILING EDGE DAMAGE APPROX 2 INCH BY 5 INCH AT WS 491. CUT OUT DAMAGED AREA. FILLED VOID AREA. FABRICATED UPPER AND LOWER SKIN DOUBLERS. TREATED PRIMED PER EO NR 01-298 WITH APPROVED 8110-3. APPRECIABLE WEIGHT ADDED BYMar 8, 2002 · N362PA · Boeing 7272J0 · Trailing Edge FlapsSDR RIVA011218Skin · corrodedNR 6 SPOILER UPPER SKIN CORRODED. FABRICATED FILLER AND DOUBLER IAW BOEING SRM 51-40-20 FIG 5 AND 14. BONDED AND SEALED REPAIR PARTS IAW BOEING SRM 51-40-20 FIG 5, 14 AND SRM 51-20-4. (M)Dec 18, 2001 · N362PA · Boeing 7272J0 · SpoilersSDR RIVA011217Tab · delaminatedRIGHT ELEVATOR TAB DELAMINATED AT AFT OUTBOARD END. REMOVED DELAMINATED AREA OF SKIN .75 INCH BY .75 INCH IAW BOEING SRM 51-40-20 FIG 20. FABRICATED AND INSTALLED DOUBLER IAW BOEING SRM 51-40-20 FIG 20. (M)Dec 17, 2001 · N362PA · Boeing 7272J0 · Elevator, Tab StructureSDR GAIA01318STFrame · crackedDURING TROUBLESHOOTING FOR A PRESSURIZATION PROBLEM A 2 INCH CRACK WAS FOUND ON A FRAME ON THE FORWARD SIDE OF THE NR 3 AFT CARGO DOOR ASSEMBLY. REMOVED AND REPLACED THE NR 3 LOWER AFT CARGO DOOR ASSEMBLY. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNEDec 11, 2001 · N281KH · Boeing 7272J0 · Cargo/Baggage DoorsSDR 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 GAIA01078OPTransmission · bindsFLT 281 - JAX - DURING APPROACH, THE INBOARD TRAILING EDGE FLAP INDICATOR WILL NOT MOVE PAST FOUR DEGREES IN FLIGHT. PERFORMED ABNORMAL PROCEDURE. DECLARED AN EMERGENCY WITH APPROACH CONTROL. THE AIRCRAFT LANDED WITHOUT ANY FURTHER DIFFICULTIES. REMOVED ANDFeb 28, 2001 · N281KH · Boeing 7272J0 · Trailing Edge Flap Control SystemSDR GAIA01068STSkin · crackedDURNG A LTC INSPECTION OF FLIGHTSTAR JAX, FOUND RIGHT WING L/E HAS A CRACK AT WS 464. ACCOMPLISHED RIGHT WING FIXED L/E SKIN REPAIR WS 464 IAW B727 SRM 57-30-4 FIG 4. MATERIAL FILLER 2024-T3 .040 PO NR 9812. DIM''S 2.330 INCH BY 3 INCH. DOUBLER 2024-T3 .05Feb 28, 2001 · N281KH · Boeing 7272J0 · Wing, Plate/SkinSDR GAIA01067STSpar · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND LEFT WING STATION 431.5 CORROSION ON FRONT SPAR WEB AT LOWER CHORD. ACCOMPLISHED LEFT WING FRONT SPAR WEB REPAIR WS 431.5 IAW B727 SRM 57-10-6 FIG 1 MATERIAL 2024-T3 .250 PO NR 20093117. DIM''S 12 INCH BY 14 IFeb 28, 2001 · N281KH · Boeing 7272J0 · Wing SparSDR GAIA01066STStiffener · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND LEFT WING FRONT SPAR HYDRAULIC LINE SUPPORT ANGLE (VERTICAL STIFFENER) AT FSS 386 IS CORRODED. ACCOMPLISHED VERTICAL STIFFENER REMOVAL AND REPLACEMENT FSS LEFT 386 IAW B727 SRM 51-30-2 AND 51-30-5. P/N 65-17209Feb 28, 2001 · N281KH · Boeing 7272J0 · Wing Miscellaneous StructureSDR GAIA01065STStiffener · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND LEFT WING FRONT SPAR HYD LINE SUPPORT ANGLE (VERTICAL STIFFENER) AT FSS 396 IS CORRODED. ACCOMPLISHED VERTICAL STIFFENER REMOVAL AND REPLACEMENT FSS LEFT 396 YAW B727 SRM 51-30-2 AND 51-30-5 P/N 65-17210-27. TFeb 28, 2001 · N281KH · Boeing 7272J0 · Wing Miscellaneous StructureSDR GAIA01064STStiffener · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND LEFT WING L/E WS 390 HAS CORROSION ON FORWARD SPAR STIFFENER. ACCOMPLISHED VERTICAL STIFFENER REMOVAL AND REPLACEMENT FSS LEFT 390 LEFT 390 IAW B727 SRM 57-10-2 FIG 3 AND 51-30-2. MATERIAL STIFFENER BAC 1517-1Feb 28, 2001 · N281KH · Boeing 7272J0 · Wing Miscellaneous StructureSDR GAIA01063STSkin · gougedDURING A TLC INSPECTION AT FLIGHTSTAR JAX, FOUND SEVERAL DENT''S AND GOUGES ON FUSELAGE SKIN BS 1050-1055 AT STRINGER 23-25R. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 1050-1055 BETWEEN STRINGER 23R AND 25R IAW B727 SRM 53-30-3 FIG 3. MATERIALS FILLER 2024-T3 .06Feb 28, 2001 · N281KH · Boeing 7272J0 · Fuselage Main, Plate/SkinSDR GAIA01062STSkin · canningDURING LTC INSPECTION AT FLIGHTSTAR JAX, FOUND SKIN OIL CANNED AT BS 196R AREA IS MARKED. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 196 R IAW B727 SRM 53-30-3 FIG 1 MATERIAL 2024-T3 .050 PO NR 991266. DIM''S 10.400 INCH BY 8.5 INCH. THE AIRCRAFT WAS RETURNED TO Feb 28, 2001 · N281KH · Boeing 7272J0 · Fuselage Main, Plate/SkinSDR GAIA01061STSkin · dentedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND DENT IN FUSELAGE SKIN AT BS 1153 BETWEEN STRINGER 21-22 RIGHT. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 1153 BETWEEN STRINGER 21R AND 22R IAW B727 SRM 53-30-3 FIG 1. MATERIALS 2024-T3 .100 PO NR 2006763. DIM''S 1Feb 28, 2001 · N281KH · Boeing 7272J0 · Fuselage Main, Plate/SkinSDR GAIA01060STSkin · dentedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND OUTWARD FACING DENT AT BS 720A PLUS 10 INCHES ABOVE STRINGER 18 RT. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 720A PLUS 10 INCHES ABOVE STRINGER 18RT IAW B727 SRM 53-30-3 FIG 1. MATERIAL 2024-T3 .063 PO NR 991420. Feb 28, 2001 · N281KH · Boeing 7272J0 · Fuselage Main, Plate/SkinSDR GAIA01059STFrame · dentedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, IT WAS DISCOVERED THAT THE AFT CARGO FRAME BS 1070 HAS A DENT BELOW STRINGER 26L. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 1070 AT STRINGER 26L IAW B727 SRM 51-40-3 FIG 1. MATERIALS FILLER 7075-T6 .100 PO NR 9991-1117.Feb 28, 2001 · N281KH · Boeing 7272J0 · Fuselage Main, FrameSDR GAIA01057STSkin · bulgedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, BULGING SKIN ALONG STRINGER 4L SKIN LAP BS 1130-1166. ACCOMPLISHED FUSELAGE SKIN LAP REPAIR BS 1130-1166 AT STRINGER 4L IAW B727 SRM 53-30-3 FIG 5. MATERIAL DOUBLER 2024-T3 .071 PO NR 20029. DIM''S 30 INCH 32.75 INFeb 28, 2001 · N281KH · Boeing 7272J0 · Fuselage Main, Plate/SkinSDR GAIA01056STSkin · gougedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, DENT IN FUSELAGE SKIN AT BS 1090 BETWEEN STRINGER 17L AND 18L. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 1090 BETWEEN STRINGER 17L AND 18L IAW B727 SRM 53-30-3 FIG 1. MATERIAL DOUBLER 2024-T3 .063 PO NR 991578. DIM''S 1Feb 28, 2001 · N281KH · Boeing 7272J0 · Fuselage Main, Plate/SkinSDR GAIA01054STSkin · dentedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, DENT IN FUSELAGE SKIN AT BS 675 1 INCH ABOVE STRINGER 26R. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 675 1 INCH ABOVE STRINGER 26R IAW B727 SRM 53-30-3 FIG 1. MATERIAL DOUBLER 2024-T3 .063 PO NR 991420. DIM''S 13.750 INFeb 28, 2001 · N281KH · Boeing 7272J0 · Fuselage Main, Plate/SkinSDR GAIA01053STSkin · damagedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, MECHANICAL/TOOLING MARKS ON FUSELAGE SKIN BS 440-460 ABOVE STRINGER 7L. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 440-460 ABOVE STRINGER 7L IAW B727 SRM 53-30-3 FIG 1. MATERIAL DOUBLER 2024-T3 .050 PO NR 991378. DIM''S Feb 28, 2001 · N281KH · Boeing 7272J0 · Fuselage Main, Plate/SkinSDR GAIA01052STFitting · crackedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, IT WAS DISCOVERED THAT THE NOSE LANDING GEAR DOWNLOCK ACTUATOR MOUNT FITTING CRACKED BS 351. ACCOMPLISHED REMOVAL AND REPLACEMENT OF NOSE LANDING GEAR DOWN LOCK ACTUATOR FITTING P/N 69-191122-2 IAW B727 SRM 51-30-2. Feb 28, 2001 · N281KH · Boeing 7272J0 · Fuselage Miscellaneous StructureSDR GAIA01051STGusset · crackedDURING A TLC INSPECTION AT FLIGHT STAR JAX, IT WAS DISCOVERED HAT THE GUSSET AT BS 825.95 RIGHT FRAME WAS CRACKED AT WL 198. ACCOMPLISHED BS 825.95 GUSSET REMOVAL AND REPLACEMENT IAW B727 SERVICE BULLETIN 727-53-0197 PART 2 FIG P/N 69-45596-4. THE AIRCRAFT WFeb 28, 2001 · N281KH · Boeing 7272J0 · Fuselage Miscellaneous StructureSDR GAIA01050STGusset · crackedDURING AT LTC INSPECTION AT FLIGHTSTAR JAX, IT WAS DISCOVERED THAT THE GUSSET AT BS 825.95 LEFT FRAME WAS CRACKED AT WL 198. ACCOMPLISHED BS 825.95 LEFT GUSSETT REMOVAL AND REPLACEMENT IAW B727 SERVICE BULLETIN 727-53-0197. PART 2 FIG 2, P/N 69-45596-3. THEFeb 28, 2001 · N281KH · Boeing 7272J0 · Fuselage Miscellaneous StructureSDR GAIA01049STWeb · crackedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, IT WAS DISCOVERED THAT THE WEB AT BS 1283R WAS CRACKED AT A LIGHTING HOLE, RIGHT AFT AIRSTAIR. ACCOMPLISHED TYPICAL WEB REPAIR IAW B727 SRM 51-40-0. MATERIALS 2024-T3 .032 PO NR 9812 DIM''S 2 INCH BY 4 INCH. THE AIFeb 28, 2001 · N281KH · Boeing 7272J0 · Fuselage Miscellaneous StructureSDR GAIA01048STSkin · crackedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, THE RIGHT VERTICAL STAB ROOT AT BS 1342 SKIN CRACKED AT STRINGER 10R. ACCOMPLISHED DOUBLER REPAIR IAW B727 SERVICE BULLETIN 727-55-82 FIG 2 AND FIG 3 MATERIAL 2024 T3 .063 PO NR 9812 DIM''S 10 INCH BY 5.5 INCH. THE Feb 28, 2001 · N281KH · Boeing 7272J0 · Vertical Stabilizer, Plate/SkinSDR GAIA01058STSeat Track · corrodedDURING A LTC INSPECTION OF FLIGHTSTAR JAX, CABIN SEAT TRACK AT LBL 45.50 FROM BS 690-480 EXFOLIATED ON ATTACH FLANGE AT BS 577. ACCOMPLISHED SEAT TRACK REMOVAL AND REPLACEMENT BS 550-630 LBL 45.50 IAW B727 SRM 53-10-5 FIG 1 AND VAI DWG NR 2902. MATERIALS TRAFeb 22, 2001 · N281KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA01055STSkin · gougedDURING TLC INSPECTION AT FLIGHTSTAR, GOUGE IN FUSELAGE SKIN AT BS 1150-1160 BETWEEN STRINGER 22L AND 23L. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 1150-1160 BETWEEN STRINGER 22L AND 23L IAW B727 SRM 53-30-3 FIG 1. MATERIAL DOUBLER 2024-T3 .080 PO NR 9818. DIM''Feb 1, 2001 · N281KH · Boeing 7272J0 · Fuselage Main, Plate/SkinSDR GAIA01009OPBrake · fireFLT 718 - TOL-ELP - AFTER LANDING AND COMING TO REST AT THE PARKING SPOT AT ELP, THE RIGHT GEAR BRAKES CAUGHT FIRE. GROUND CREWS IMMEDIATELY EXTINGUISHED THE BRAKES FIRES. NR 1 BRAKE OVERTEMPED BUT DID NOT CATCH ON FIRE. APPROXIMATELY 20 MINUTES LATER, NR 1Jan 11, 2001 · N281KH · Boeing 7272J0 · BrakeSDR 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 System
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