N118RW
Registered owner: CITATION N118RK LLC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
103 reports on file, 1998-05-28 – 2002-11-16.
Part: CHECK VALVE — INOPERATIVE (FUSELAGE) · airframe 61,015 hrs · 29,901 cycles
DURING CLIMB OUT, THE FLIGHT CREW NOTED AN ILLUMINATED WING/BODY OVERHEAT LIGHT WHICH WOULD NOT EXTINGUISH WHEN QUICK REFERENCE HANDBOOK ITEMS WERE ACCOMPLISHED. THE AIRCRAFT RETURNED TO THE DEPARTURE AIRPORT.MAINTENANCE REMOVED AND REPLACED THE START MANIFOLD CONNECTION CHECK VALVE IN ACCORDANCE WITH THE REQUIREMENTS OF MM 21-21-15.
Part: HYDRAULIC LINE — DAMAGED (RIGHT WHEEL WELL) · airframe 60,938 hrs · 29,845 cycles
DURING FLIGHT, A SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO FOLLOWED BY THE FAILURE OF THE NUMBER 2 ENGINE, ENGINE DRIVEN HYDRAULIC PUMP. A SYSTEM PRESSURE REMIAINED NORMAL. ON FINAL APPROACH TO DIVERSION SITY AIRPORT, A SYSTEM PRESSURE DROPPED TO ZERO. STANDBY SYSTEM CARRIED THE LOAD THROUGH THE LANDING.VISUAL INSPECTION OF THE WHEEL WELLS AND LANDING GEAR AREAS REVEALED A FRACTURED HYDRAULIC LINE IN THE RIGHT WHEEL WELL, FORWARD AREA OF THE WELL. INSTALLED A TEMPORARY HYDRAULIC LINE IN ACCORDANCE WITH THE REQUIREMENTS OF MM 20-10-51. REMOVED, INSPECTED AND REPLACED RETURN FILTERS IN THE A SYSTEM. TRACE AMOUNTS OF METAL WERE FOUND IN THE NUMBER 2 ENGINE CASE DRAIN FILTER. MAINTENANCE REMOVED AND REPL
Part: A/C PACK — MALFUNCTIONED (A/C BAY) · airframe 60,659 hrs · 29,658 cycles
AIR TURN BACK. FLIGHT CREW REPORTED SMOKE IN CABIN, LT WING/BODY OVERHEAT ILLUMINATED AND RT PACK TRIPPED OFF. DECLARED AN EMERGENCY AND RETURNED TO DEN. AIRCRAFT LANDED WITHOUT INCIDENT. ON APPROACH, AILERONS WERE DIFFICULT TO MOVE AND HAD A SHUDDER BELOW 180 KNOTS. REPOSITIONED DETECTION LINE FOUND TOUCHING BLEED DUCT IN FWD LT AFT CARGO COMPARTMENT. PLACARDED RT PACK PER MEL 21-1. PERFORMED A FLIGHT CONTROL MOVEMENT CHECK WITH NO DISCREPANCIES NOTED. PERFORMED VISUAL INSPECTION OF AILERON CONTROL SYSTEM, WITH NO DEFECTS NOTED. COMPLIED WITH FLAP MOVEMENT CHECK, WITH NO DEFECTS NOTED.
Part: ODOR — DETECTED (CABIN) · airframe 60,550 hrs · 29,580 cycles
AIR TURNBACK. FLIGHT CREW REPORTED FWD LAVATORY SMOKE ALARM ACTIVATED WHILE CLIMBING THROUGH 8000 FT. PASSENGERS IN ROW 2 NOTED DISTINCT SMELL/ODOR OR SMOKE (OVEN/ELECTRICAL) DURING FLIGHT. NR 2 PACK TRIP OFF LIGHT ILLUMINATED IMMEDIATELY BEFORE SMOKE ALARM ACTIVATED. PERFORMED OPERATIONAL CHECK OF LAVATORY SMOKE DETECTOR SYSTEM, WITH NO DISCREPANCIES NOTED. PERFORMED OPERATIONAL CHECK OF FWD GALLEY OVEN FOR 30 MIN ON HIGH, WITH NO DISCREPANCIES NOTED. PERFORMED OPERATIONAL CHECK OF RT PACK SYSTEM FOR SEVERAL HOURS, WITH NO DISCREPANCIES NOTED. REPLACED NR 2 PACK WATER SEPARATOR BAG AS PRECAUTIONARY.
Part: OVERHEAT LOOP — OUT OF POSITION (CARGO BAY)
DURING CLIMBOUT, THE FLIGHT CREW DISCOVERED A WIND/BODY OVERHEAT LIGHT ON. QRH ITEMS ACCOMPLISHED AND LIGHT EXTINGUISHED. AIR TURNBACK ACCOMPLISHED. UPON INSPECTION BY MAINTENANCE, AFT CARGO PIT HAD TWO AREAS WHERE THE OVERHEAT DETECTOR WAS TOUCHING THE BLEED DUCT. MAINTENANCE CORRECTED THE PROBLEM AND THE SYSTEM CHECKED NORMAL. CORRECTIONS MADE IN ACCORDANCE WITH MM 26-18-0, PAGE 501.
Part: FIRE DETECTOR — FALSE ACTIVATION (NR 1 ENGINE) · airframe 59,626 hrs · 28,948 cycles
UPON ARRIVAL AT GATE, FLIGHT CREW REPORTED THE FIRE BELL SOUNDED AND THE NR 1 ENGINE FIRE HANDLE WAS ILLUMINATED. PULLED NR 1 FIRE HANDLE AND DISCHARGED THE LEFT BOTTLE INTO THE NR 1 ENGINE. INSPECTED NR 1 ENGINE FOR EVIDENCE OF FIRE, NONE FOUND. INSPECTED FIRE DETECTION SYSTEM FOR DEFECTS PER MM 26-11-0. NO DEFECTS NOTED. INSPECTED FIRE LOOP. NO DEFECTS NOTED. REPLACED FIRE DETECTION UNIT, FIRE CONTROL MODULE AND NR 1 ENGINE FIRE BOTTLE, RAN ENGINE FOR SEVERAL MINUTES AND NO DEFECTS WERE NOTED.
Part: PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION AT SCREW HOLES ON TRANSITION PANEL AT STA 500-520. FABRICATED AND INSTALLED REPLACEMENT TRANSITION PANEL PER SRM 51-21-41.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON WEB AT STA 797 BETWEEN STR 22-R AND 24-R. REPLACED WEB PER SRM 51-30-2 AND 51-10-1.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED VERTICAL WEB CORRODED FROM STA 352 TO STA 360. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-20-01 AND 51-30-2.
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SIDEWALL ATTACH ANGLE AT STA 947.5, STR 21R TO 24R. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER BOEING DRAWING 65-55726 AND SRM 51-40-3.
Part: CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CLIP AT FWD FRAME, STA 360. FABRICATED AND INSTALLED CHANNEL TIE PER SRM 51-20-01 AND 51-30-2.
Part: COWLING — CRACKED (NR 2 ENGINE) · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CRACK ON AFT LOWER CORNER OF NR 2 ENGINE OUTBOARD FIXED COWL NEXT TO FIRE SEAL. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3 AND 51-30-2.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED STIFFENER ANGLE CRACKED AT STA 298 - STA 304. FABRICATED AND INSTALLED REPLACEMENT CLIP PER SRM 51-10-2 AND 51-30-2.
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SIDEWALL PANEL ATTACH ANGLE AT STA 727, LBL 21 TO LBL 25.
Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CRACK IN RADIUS UPPER SURFACE 28 INCHES FWD OF AFT EDGE OF WEB THRESHOLD C-2 DOOR AT STR 25-R, STA 794-847. REMOVED DAMAGED AREA AND INSTALLED DOUBLER AND FILLER ON WEB PER SRM 51-40-3.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY FLOOR WEB CORRODED, STA 1016, AT DRAIN TO LBL 30.
Part: SKIN PANEL — DAMAGED (STA. 326) · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED MISSED DRILLED RIVET HOLE IN FWD LT. CORNER OF AFT E&E DOOR CUTOUT AT STA. 326. FABRICATED DOUBLER, TRIPLER AND FILLER PER EA 57-737-157. TREATED AND PRIMED REPAIR PARTS PER SOPM 20-41-02. INSTALLED FASTENERS PER 51-30-2.
Part: ANGLE — CORRODED (STA. 727) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT PANEL ATTACH ANGLE AT STA. 727, RBL 21 TO RBL 25. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-30-2, 51-10-2 51-30-3 AND BOEING DRAWING 65-55726.
Part: SKIN — CRACKED (FUSELAGE) · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR CUTOUT CRACKED AT FWD LOWER CORNER OUTER SKIN APPROXIMATELY 1 INCH FROM RIVET TO DOOR CORNER. REPAIRED DAMAGE PER SRM 53-30-3.
Part: COWLING — DAMAGED (NR 1 ENGINE) · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED NR 1 ENGINE LT OUTBOARD COWL TOP EDGE DAMAGED BETWEEN SECOND AND LAST HINGE. REMOVED DAMAGE PER SRM 51-40-3. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-2, 51-40-3 AND 51-30-2.
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED BEAM IN FWD BULKHEAD, AFT CARGO COMPARTMENT, CORRODED AT NUT PLATE ATTACHMENT POINT FOR LOWER DUCT SHROUD BRACKETS AT LBL 20 AND WL 160. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 51-40-4.
Part: MOUNT BRACKET — CORRODED (SPOILER) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED LT WING REAR SPAR MOUNT TEE FOR NR 4 SPOILER OUTBOARD ACTUATOR MOUNT BRACKET CORRODED. REPLACED BRACKET AND BUSHING PER SRM 51-30-5, BOEING OHM 20-50-03 AND BOEING SOPM 20-50-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED FRAME AT STA 82.7, RBL 10, CRACKED AT SHEAR TIE ATTACH FASTENERS IN AFT CARGO COMPARTMENT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-4.
Part: BELTFRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON BELT FRAME AT STA 827, RBL 10. REMOVED DAMAGE, FABRICATED AND INSTALLED PER SRM 53-10-4.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 967 CORRODED. FABRICATED AND INSTALLED REPLACEMENT FLOORBEAM CAP PER SRM 51-30-2.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CHORD AT STA 352, STR 28L. REPLACED DAMAGED CHORD PER SRM 51-10-2 AND SRM 51-30-2.
Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CLOSING PANEL AROUND NUT PLATE AT STA 789, RBL 27 TO RBL 34. REPLACED CLOSING PANEL PER SRM 51-10-1.
Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CLOSING PANEL AROUND NUT PLATES AT STA 789, RBL 39 TO RBL 46. REPLACED CLOSING PANEL PER SRM 51-10-1.
Part: SKIN — CRACKED (FUSELAGE) · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED FUSELAGE SKIN RUBBED BY BELT 2 INCHES BELOW L-1 DOOR TOP SPIGOT (INTERIOR). PERFORMED EDDY CURRENT INSPECTION OF L-1 DOOR TOP SPIGOT INTERIOR BONDED DOUBLER AND FOUND 2 CRACKS. REPAIRED DAMAGED AREA PER EA 53-737-160.
Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY FLOOR WEB STRAP CORRODED AT STA 1006 TO STA 1016. FABRICATED AND INSTALLED REPLACEMENT WEB STRAP PER SRM 51-30-2.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 986 TO STA 1006, RBL 3, CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-30-2 AND EA 53-737-158.
Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED STRAP ALONG THE BOTTOM OF PRODUCTION BREAK AT STA 1016, STR 23-L TO 23-R CORRODED. REPLACED STRAP PER SRM 51-30-2 AND BOEING DRAWING 65-46568.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND EDGES OF AFT FLOOR PANEL IN FWD CARGO COMPARTMENT. REMOVED CORROSION AROUND EDGES OF AFT FLOOR PANEL PER SRM 51-10-06. FABRICATED AND INSTALLED REPLACEMENT RETAINER STRAP PER SRM 51-10-01, 51-10-02 AND SOPM 20-41-02.
Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUT PLATE HOLE AT STA 727, RBL 12, VERTICAL STIFFENER. CUT OUT DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND INSTALLED PER EO 51-00-737-001 AND SRM 51-40-4.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED WEB AT STA 996 TO STA 1016, RBL 40, NEXT TO R2 DOOR CORRODED. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-30-2.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED FLOOR SUPPORT AT STA 957, LBL 16 TO LBL 42, CORRODED. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 53-10-2 AND 51-30-2.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED TOP SURFACE OF FLOORBEAM AT STA 986 CORRODED. REPLACED FLOORBEAM CAP PER SRM 53-10-9.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT STA 847, BL 16-R. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER BOEING DRAWING 65-47957, SRM 51-10-2 AND SRM 51-30-2.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 794, STR 27-R CORRODED. FABRICATED AND REPLACED INTERCOSTAL PER SRM 51-30-2 AND 51-20-1.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 986 CORRODED AT BOTTOM SURFACE AT FASTENERS THROUGH FLOORBOARDS. ALSO SHOWS EVIDENCE OF CORROSION ON TOP OF BEAM FROM BL 0 TO RBL 54 AS VIEWED FROM BELOW. REPLACED FLOORBEAM CAP AT STA 986 PER SRM 53-10-9.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED FLOOR INTERCOSTAL IN AFT GALLEY ENTRY CORRODED STA 957, BL 16L TO BL 42L. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 53-10-2 AND 51-30-2.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CIRCUMFERENTIAL AT APPROX STA 350 BETWEEN STR 24-L AND 24-R CORRODED ON BOTH FWD AND AFT SIDES. FABRICATED REPLACEMENT SHEAR TIE AND INSTALLED PER SRM 53-10-4, FIG 9, 51-30-2 AND SOPM 20-41-02.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 500A - 500B, STR 26-R CORRODED AT NUT PLATE HOLES. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-10-1 AND 51-20-1.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY SUPPORT PARTITION FRAME CORRODED AT STA 998, 14 LBL. FABRICATED AND INSTALLED REPLACEMENT FRAME SUPPORT PER SRM 51-10-2.
Part: GUSSET — WORN (NR 1 COWLING) · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED NR 1 ENGINE RT EXHAUST COWL INSIDE FLANGE ON BOTTOM OF THIRD RIB FROM FRONT WORN. REMOVED DAMAGED GUSSET FROM NR 1 ENGINE RT EXHAUST COWL. FABRICATED AND INSTALLED REPLACEMENT GUSSET PER SRM 51-21-171 AND 51-30-2.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED WEB AT STA 1016, STR 20-L, BEHIND L-2 DOOR. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-30-2 AND BOEING DRAWING 65-46812.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED AFT FLOORBEAM AT STA 967 CORRODED ON TOP SURFACE. FABRICATED AND REPLACED FLOORBEAM CAP PER SRM 51-30-2.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED INTERCOSTALS BETWEEN STA 787 AND 794, STR 16R TO 26R, CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTALS PER SRM 51-30-2.
Part: MOUNT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CARGO NET ATTACH CLEAT MOUNT PLATE AT STA 847 ABOVE STR 22-L. FABRICATED AND INSTALLED NEW MOUNT PLATE PER SRM 51-10-2 AND 51-21-171.
Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FWD DOOR FRAME AT STA 803, STR 24-R, CRACKED AND CORRODED. REPLACED AFT CARGO COMPARTMENT DOOR FRAME PER SRM 57-10-1 AND 51-30-2.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY TRANSVERSE BEAM CORRODED AT STA 1006 TO STA 1016, LBL 6. REPLACED TRANSVERSE FRAME PER SRM 51-30-2.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED TOP OF FLOORBEAM CORRODED AT STA 1016, FROM CENTER TO 30 LBL. FABRICATED AND INSTALLED REPLACEMENT FLOORBEAM TOP CAP PER SRM 51-30-02.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INTERCOSTAL CORRODED FROM STA 1006 TO STA 1016, BL 0. FABRICATED AND REPLACED INTERCOSTAL PER SRM 53-10-2 AND 51-30-2.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED FWD CARGO BAY AFT BULKHEAD SUPPORT ANGLE AT STA 520, STR 26-L TO 19-L, CORRODED. REPLACED ANGLE PER SRM 51-10-1.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY TRANSVERSE FLOORBEAM CORRODED AT STA 986 TO STA 1006, LBL 10. REPLACED DAMAGED TRANSVERSE FRAME TOP CAP PER SRM 51-30-2 AND 51-10-2.
Part: PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED TRANSITION PANEL AT STA 520, STR 26-L, CORRODED AT NUT PLATE LOCATION. FABRICATED AND INSTALLED REPLACEMENT PANEL PER SRM 51-10-1.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT, LOWER FWD CORNER, AT STA 790. REPAIRED DAMAGED SECTION PER SRM 53-30-3.
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED BEAM IN FWD BULKHEAD AT BL 20, WL 160, CORRODED AT NUT PLATE ATTACHMENT POINT FOR LWR DUCT SHROUD BRACKETS. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-40-4.
Part: NUT PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUT PLATE HOLE AT STA 727, BL 12R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPLACEMENT PARTS PER EO 51-00-737-001 AND SRM 51-40-4, FIGURE I, DETAIL 3.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON TOP OF FLOORBEAM AT STA 294.5. REPLACED TOP CHORD OF 294.5 FLOORBEAM FROM LBL 28 TO RBL 65 PER SRM.
Part: SKIN — DELAMINATED (FOREFLAP) · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED UPPER SURFACE OF LT OUTBOARD FOREFLAP DELAMINATED, STA 325. REPAIRED PER SRM 51-40-2 AND F9 MAINTENANCE FORM 5034-2.
Part: BELTFRAME — CRACKED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED BELT FRAME CORRODED AND CRACKED AT STA 807, BL 0. REPAIRED FRAME SHEAR TIE PER SRM 53-10-2.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON TOP OF FLOORBEAM AT STA 294.5. REPLACED TOP CHORD OF FLOORBEAM AT STA 294.5, LBL 28 TO RBL 65, PER SRM 53-10-9, 51-30-2, 51-10-1, 53-10-2 AND SOPM 20-41-02.
Part: ATTACH FITTING — CRACKED (THRUST REVERSER) · airframe 58,984 hrs · 28,541 cycles
DURING C-3 CHECK, INSPECTION REPORTED NR 1 ENGINE BOTTOM OUTBOARD THRUST REVERSER ATTACH POINT DAMAGED AND CRACKED IN 2 PLACES. REPAIRED CRACKS AND DAMAGED AREA PER SRM 51-30-6.
Earlier reports · 1998–2001 · 39 reports
2001
Part: SLIDE — DISCHARGED (R1 DOOR) · airframe 58,542 hrs · 28,267 cycles
DURING SERVICE CHECK, MAINTENANCE REPORTED R-1 DOOR SLIDE PRESSURE LOW. AIRCRAFT WILL BE FERRIED TO DEN FOR REPLACEMENT OF SLIDE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,476 hrs · 28,216 cycles
DURING SERVICE CHECK, MAINTENANCE REPORTED EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN ROWS 6 AND 11 INOPERATIVE. FERRIED AIRCRAFT TO DEN FOR REPAIR. REPLACED EMERGENCY FLOOR PATH LIGHTING STRIP BETWEEN ROWS 6 AND 11 AND SYSTEM CHECKED OKAY.
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 57,763 hrs · 27,785 cycles
DURING SERVICE CHECK, MAINTENANCE REPORTED FLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSY. AND CHECKED OKAY.
Part: TRANSMITTER — READS LOW (NR 1 ENGINE) · airframe 56,562 hrs · 27,004 cycles
AIR TURNBACK. FLIGHT CREW REPORTED NR 1 ENGINE ANTI-ICE VALVES INDICATED OPEN ON OVERHEAD PANEL. AT CLIMB POWER, NR 1 ENGINE EPR AT APPROXIMATELY 87 PERCENT AND NR 2 ENGINE EPR AT 90 PERCENT. REPLACED NR 1 ENGINE EPR TRANSMITTER PER MM 77-11-21. PERFORMED ENGINE RUN PER MM 71-09-236, PAGE 206, AND FOUND TO BE WITHIN LIMITS.
Part: LINE — DAMAGED (NR 1 ENGINE) · airframe 56,563 hrs · 27,005 cycles
AIR TURNBACK. FLIGHT CREW REPORTED ON CLIMBOUT WITH EPR SET AT 2.20, THE NR 1 ENGINE N1 WAS APPROXIMATELY .7 LOW. NR 1 EGT WAS APPROXIMATELY 40 LOW, N2 APPROXIMATELY .5 LOW AND FUEL FLOW 800LB LOW. WHEN THROTTLES WERE MATCHED AND ALL OTHER ENGINE GAUGES MATCHED, THE NR 1 EPR WAS HIGH. PERFORMED EPR SYSTEM TEST PER MM 77-11-00 AND FOUND DAMAGED PT2 SENSE LINE. REPLACED PT2 SENSE LINE PER MM 20-10-51. PERFORMED ANOTHER EPR SYSTEM TEST PER MM 77-11-00 AND SYSTEM CHECKED GOOD. PERFORMED RIG CHECK OF THRUST REVERSERS AND THROTTLES PER MM 76-11-00 AND CHECKED OK. PERFORMED ENGINE RUN TRIM CHECK PER MM 71-00-00 AND CHECKED TO STATED VALUES. ALSO REPAIRED DAMAGED WIRING TO NR 1 ENGINE FWD BOOST PUMP PER.
2000
Part: FAN — FAILED (CABIN) · airframe 55,602 hrs · 26,344 cycles
AFTER LANDING, FLIGHT CREW REPORTED BURNING ELECTRICAL ODOR IN COCKPIT. REQUESTED EMERGENCY EQUIPMENT ESCORT. MAINTENANCE REPLACED CABIN CONTROL AUGMENTATION FAN.
Part: GALLEY TRACK — CORRODED (FUSELAGE)
DEN - DURING C-3 CHECK INSPECTION, REPORTED CORROSION ON NR 1 GALLEY TRACK, HORIZONTAL FLANGE, STATION 290, BL 18R. MAINTENANCE REMOVED CORROSION PER SRM 53-10-1. FABRICATED NEW TRACK PER SRM 51-20-2, TREATED AND PRIMED PER SRM 51-10-2 AND INSTALLED PER SRM 51-30-2. (M)
Part: GALLEY TRACK — CORRODED (FUSELAGE)
DEN - DURING C-3 CHECK INSPECTION, REPORTED CORROSION ON NR 1 GALLEY OUTBOARD TRACK STATION 294, RBL 42. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT TRACK PER SRM 53-10-5, FIG 5. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
DEN - DURING C-3 CHECK INSPECTION, REPORTED FLOOR TRACK CORRODED, STATION 344, BL 22L. MAINTENANCE REMOVED CORRODED SECTION OF TRACK AND FABRICATED AND INSTALLED REPLACEMENT TRACK PER SRM 51-30. (M)
Part: SUPPORT BRACKET — CRACKED (GLIDE SLOPE)
DEN - DURING C-3 CHECK INSPECTION, FOUND CRACK IN LOWER CENTER SUPPORT FOR GLIDE SLOPE ANTENNA ON FORWARD PRESSURE BULKHEAD. MAINTENANCE FABRICATED REPAIR ANGLE AND TREATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-40-03. REINSTALLED GLIDE SLOPE ANTENNA BRACKET PER EO 53-10-737-014, PAGES 80, 81 AND 82. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
DEN - DURING C-3 CHECK INSPECTION, FOUND CORROSION ON INTERCOSTAL FROM STATION 284 TO STATION 294, BL 12L AT FORWARD LAVATORY THRESHOLD. MAINTENANCE FABRICATED REPLACEMENT INTERCOSTAL, TREATED AND PRIMED PER SRM 51-10-02 AND INSTALLED PER 51-30-00 AND EA 53-737-085. (M)
Part: PLATE — CRACKED (CARGO DOORWAY)
DEN - DURING C-3 CHECK INSPECTION, FOUND REPORTED 16 CRACKS IN FORWARD CARGO DOOR SCUFF PLATE. MAINTENANCE INSTALLED NEW SCUFF PLATE. (M)
Part: BULKHEAD — CRACKED (FUSELAGE)
DEN - DURING C-3 CHECK INSPECTION, FOUND CRACK IN FORWARD PRESSURE BULKHEAD HORIZONTAL WEB AT STATION 178, WL 195, RBL 20. MAINTENANCE FABRICATED AND INSTALLED HORIZONTAL WEB PER EO 53-10-737-014 AND SRM 53-10-11. (M)
Part: BULKHEAD — CRACKED (FUSELAGE)
DEN -DURING C-3 CHECK INSPECTION, FOUND STATION 178 FORWARD PRESSURE BULKHEAD HORIZONTAL WEB CRACKED AT LBL 20, WL 195. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT HORIZONTAL WEB PER EO 53-10-737-014 FIGURE 46 AND SRM 53-10-11. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DEN - DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM UPPER CHORD CORRODED FROM RBL 20 TO LBL 49. MAINTENANCE FABRICATED REPAIR PARTS PER SRM 53-10-02 AND INSTALLED PER SRM 51-30-0. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
DEN - DURING C-3 CHECK INSPECTION REPORTED CORROSION ON INTERCOSTAL AND IN AND AROUND CLIP NUT HOLES OF INTERCOSTAL STATION 277 TO 294. MAINTENANCE REMOVED DAMAGED INTERCOSTAL, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-30-00, 51-10-2, 51-10-6 AND 53-10-1 AND EA 53-737-085. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
DEN - DURING C-3 CHECK INSPECTION REPORTED CORROSION IN CLIP NUT HOLES OF INTERCOSTAL, STATION 294.5 TO 312, BL 12L, FORWARD CABIN FLOOR STRUCTURE. MAINTENANCE REMOVED DAMAGED INTERCOSTAL. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-30-00. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
DEN - FOUND DURING C-3 CHECK INSPECTION, CORROSION ON INTERCOSTAL, STATION 312-328, BL 32R, FORWARD CABIN FLOOR STRUCTURE. MAINTENANCE REMOVED FLOOR SUPPORT. FABRICATED NEW SHIM AND INSTALLED REPLACEMENT SHIN AND FLOOR SUPPORT PER EA 53-737-085 AND SRM 51-10-2 AND 51-30-0. (M)
Part: FLOORBEAM — CORRODED (CABIN)
DEN - DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN AND AROUND FLOORBEAM CLIP NUT HOLES, STATION 294, BL 8R TO BL 44R. MAINTENANCE REMOVED CORROSION PER MM 51-31-31, FABRICATED REPLACEMENT PARTS AND INSTALLED PER 51-10-2, 53-10-2, AND 53-10-9, FIG 5. (M)
Part: INTERCOSTAL — CORRODED (CABIN)
DEN - DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT STATION 312, BETWEEN LBL 40 AND RBL 40. MAINTENANCE REMOVED CORROSION FROM UPPER CHORD, FABRICATED AND INSTALLED REPLACEMENT UPPER CHORD PER SRM 51-10-1, FIG 1 AND SRM 53-10-9 FIG 5. (M)
Part: FLOORBEAM — CORRODED (CABIN)
DEN - DURING C-3 CHECK INSPECTION REPORTED CORROSION IN AND AROUND FLOORBEAM CLIP NUT HOLES, STATION 294, BL 8R TO BL 44R. MAINTENANCE REMOVED CORROSION PER MM 51-31-31. FABRICATED REPLACEMENT PARTS AND INSTALLED PER 51-10-2, 53-10-2, AND 53-10-9 FIG 5. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DEN - DURING C-3 CHECK INSPECTION, FOUND FLOORBEAM UPPER CHORD AT STATION 277 CORRODED FROM LBL 17 TO LBL 49. MAINTENANCE FABRICATED REPLACEMENT UPPER CHORD PER SRM 53-10-02 AND INSTALLED PER SRM 51-30-0. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DEN - DURING C-3 CHECK INSPECTION REPORTED CORROSION ON FLOORBEAM AT STATION 294.5 UNDER FORWARD GALLEY, INBOARD OF R-1 DOOR. MAINTENANCE REPLACED FLOORBEAM PER SRM 51-21-31. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DEN - DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE, STATION 294 BL 0, FORWARD CABIN FLOORBEAM CAP. MAINTENANCE REPLACED FLOORBEAM PER SRM 51-21-31. (M)
Part: PLATE — CORRODED (SERVICE DOOR)
DEN - DURING C-3 CHECK INSPECTION REPORTED PITTING AND CORROSION ON L-2 DOOR UPPER AND LOWER GUIDE PLATES. MAINTENANCE REPLACED UPPER AND LOWER GUIDE PLATES (P/N 69391832, 69446521) WITH BEARINGS PER MM 53-41-0. (M)
Part: STRINGER — CRACKED (FUSELAGE)
DEN - DURING C-3 CHECK INSPECTION REPORTED STRINGER SUPPORT AT STATION 272B, STRINGER 4R, CRACKED. MAINTENANCE REMOVED CRACKED BRACKET. FABRICATED AND INSTALLED REPLACEMENT BRACKET PER SRM 51-10-01. (M)
Part: FLANGE — CORRODED (LAV DUMP VALVE)
DEN - DURING C-3 CHECK INSPECTION, FOUND CORROSION ON DUMP VALVE HOUSING MOUNT FLANGE. MAINTENANCE FABRICATED REPLACEMENT LAVATORY PAN DOUBLERS, HEAT TREATED, TREATED, PRIMED AND INSTALLED PER SRM 51-10-03 AND 51-30-0. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DEN - FOUND DURING C-3 CHECK INSPECTION REPORTED TOP CHORD OF FLOORBEAM CORRODED AT STATION 328 BETWEEN LBL 40 AND RBL 40. MAINTENANCE REMOVED DAMAGED SECTION OF TOP CHORD. FABRICATED AND INSTALLED REPLACEMENT SECTION PER SRM 51-30-00. (M)
Part: STRINGER CLIP — CRACKED (FUSELAGE)
DEN - DURING C-3 CHECK INSPECTION, REPORTED STRINGER FRAME TIE CLIP CRACKED .75 INCH, STRINGER 7L, STATION 747L. MAINTENANCE REMOVED CRACKED TIE CLIP. FABRICATED AND INSTALLED NEW TIE CLIP PER SRM 51-30-02 AND 53-10-02. (M)
Part: STRINGER CLIP — CRACKED (FUSELAGE)
DEN - DURING C-3 CHECK INSPECTION, REPORTED STRINGER FRAME TIE CLIP CRACKED .25 INCH, STRINGER 6R, STATION 887. MAINTENANCE REMOVED CRACKED TIE CLIP. FABRICATED AND INSTALLED NEW TIE CLIP PER SRM 51-30-02 AND 53-10-02. (M)
Part: STRINGER CLIP — CRACKED (FUSELAGE)
DEN - DURING C-3 CHECK INSPECTION REPORTED STRINGER FRAME TIE CLIP CRACKED .25 INCH, STRINGER 6R, STATION 727B. MAINTENANCE REMOVED CRACKED TIE CLIP. FABRICATED AND INSTALLED NEW TIE CLIP PER SRM 51-30-02 AND 53-10-02. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
DEN - DURING C-3 CHECK INSPECTION, REPORTED FLOOR SUPPORT SHIM FROM STATION 277 TO STATION 294 CORRODED. MAINTENANCE FABRICATED NEW SHIM PER EA 53-737-085, TREATED AND PRIMED PER SRM 51-10-02 AND INSTALLED SHIM. (M)
Part: STRUCTURE — WORN (NR 2 INTAKE)
DEN - DURING C-3 CHECK, FOUND NR 2 ENGINE INLET TRAILING EDGE MATING SURFACE FOR ENGINE COWL AT 6:00 POSITION WORN VERY THIN. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED TWO REPAIR ANGLES AND FILLERS PER SRM 54-10-03 AND TREATED AND PRIMED PER SRM 51-10-02. INSTALLED PER SRM 54-10-03. (M)
Part: RIB — DAMAGED (NACELLE)
DURING C-3 CHECK INSPECTION, FOUND 6TH RIB FROM REAR OF NR 2 ENGINE RT OUTBOARD COWL DAMAGED THROUGHOUT ENTIRE LENGTH. MAINTENANCE INSTALLED NEW RIB PER SRM 51-30-0. (M)
Part: FITTING — CORRODED (RT MLG BEAM)
DEN - DURING C-3 CHECK INSPECTION, REPORTED INTERGRANULAR CORROSION ON ATTACH FITTING ON RIGHT MLG SUPPORT BEAM AT NR 5 GROUND SPOILER INBOARD ACTUATOR BRACKET. MAINTENANCE REPLACED ATTACH FITTING PER MM 27-62-12 AND SRM 51-10-02. (M)
Part: BATTERY PACK — INOPERATIVE (CABIN)
DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED AFT DOOR EMERGENCY EXIT LIGHTS WOULD NOT TEST OF LIGHT. MAINTENANCE REPLACED BATTERY PACK AND POWER SUPPLY. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED AFT DOOR EMERGENCY EXIT LIGHTS WOULD NOT TEST OR LIGHT. MAINTENANCE REPLACED BATTERY PACK AND POWER SUPPLY. REF F3LA00032. (M)
1998
Part: YAW COUPLER — FAILED (RUDDER)
EWR - FLT 1606 - DURING TAKEOFF ROLL AT 90 KNOTS, AIRCRAFT VEERED SIGNIFICANTLY TO THE LEFT TWICE. ABORTED TAKEOFF. INSPECTED AND FOUND YAW DAMPENER FAILED HARD LEFT. REMOVED AND REPLACED YAW DAMPENER COUPLER PER MM 22-11-141. GROUND TESTS SHOW OPS NORMAL. (X)
Part: CONTROL CABLE — FRAYED (LT AILERON)
EKO - FLT 9988 - AILERON BUS CABLE FRAYED. CABLE ROUTED WRONG AROUND CABLE GUARD. REMOVED AND REPLACED CABLE. ROUTED PROPERLY IAW MM 27-11-11, 27-11-101, AND 27-11-71. AILERON FUNCTIONALLY CHECKED GOOD. AIRCRAFT REUTRNED TO SERVICE. (X)