N620FE
Registered owner: FEDERAL EXPRESS CORP, TN (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
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1279, X= -47.5" FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1279, X = - 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES BS 1249 TO 1311, X = - 47.5 IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100
CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 979, X= -27.5 FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 979, X = - 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 969 TO STATION 1029, X = - 27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON SPLICE FITTING FOUND CRACK BETWEEN STATION 1801-1821 LONGERON 46 RIGHT. CRACKED LONGERON SPLICE FITTING AT LOWER CENTER CARGO COMPARTMENT BILGE AREA BETWEEN STATION 1801-1821, LONGERON - 46 RIGHT REMOVED AND REPLACED WITH FABRICATED LONGERON SPLICE FITTING PER MD11 SRM 51-33-01-0G. LONGERON SPLICE FITTING FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AFA 7225 REVISION J. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 755, X= -27.5" FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 755, X = - 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT STATION 805 TO EXISTING SPLICE STATION 745, X = - 27.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 47.5" FOUND CROWN WORN. THE SEAT TRACK BS 6-10, X = 47.5 WAS EVALUATED & FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BS 6-60 - EXISTING SPLICE BS 6-0/1129, X = 47.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1279, X= -27.5" FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK BS 1279, X = - 27.5 WORN CROWN EVALUATED & FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT BS 1229 TO 1331, X = - 27.5 IAW SRM 53-00-52-2R, FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 5-10, X= -8.5" FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 5-10, X = - 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES BS 5-83 TO 5-0/1531, X = - 8.5 IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 5-10, X= -27.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT BS 5-63 TO EXISTING SPLICE BS 5-0/1531, X = - 27.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= -8.5" FOUND CROWN WORN. THE SEAT TRACK BS 6-10, X = - 8.5 WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT STATION 6-60 TO EXISTING SPLICE STATION 6-0/1129, X = - 8.5 IAW SRM 53-00-52-2R, FIGURE 201. REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK AT STATION 1541, X= -47.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT BS 1571 TO EXISTING SPLICE STATION 5-123/1531, X = - 47.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1541, X= 27.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 8.5" FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 6-10, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT BS 6-60 TO EXISTING SPLICE STATION 6-0/1129, X = 8.5 IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 27.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= -47.5 FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1079, X= -47.5 FOUND CROWN WORN. THE SEAT TRACK BS 1079, X = - 47.5 WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES BS 1069 TO 1129/6-0, X = - 47.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1009, X= 27.5 FOUND CROWN WORN. THE SEAT TRACK STATION 1009, X = 27.5 WAS EVALUATED & FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT BS 989 TO EXISTING SPLICE BS 1049, X = 27.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1009, X= -47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT, AT SEAT TRACK STATION 1009, X = - 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 989 TO EXISTING SPLICE STATION 1069, X = - 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK AT STATION 879, X= 27.5 FOUND CROWN WORN. THE SEAT TRACK BS 879, X = 27.5 WAS EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BS 869 TO 909, X = 27.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 806, X= -8.5 FOUND CROWN WORN. SEAT TRACK STATION 810, X = - 8.5 CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES BS 805 TO 869, X = - 8.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REFER TO SNRM N00299 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 879, X= -27.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 879, X = - 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT BS 869 TO 909, X = - 27.5 IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 839, X= -8.5 FOUND CROWN WORN. THE SEAT TRACK STATION 839, X = - 8.5 EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES BS 805 TO 869, X = - 8.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 806, X= 8.5 FOUND CROWN WORN. EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101 ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES BS 745 TO 806, X = 8.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
UNABLE TO RAISE LANDING GEAR HANDLE ON TAKEOFF. COMPLIED WITH QRH. STILL COULD NOT RAISE GEAR. FOUND MLG TRIM INTERLOCK CYLINDER NOT MOVING WITH HYDS ON, STOPPING MOVEMENT OF GEAR SELECTOR QUADRANT & VALVE. R & R TRIM CYLINDER INTERLOCK FUSE IAW AMM 32-37-06-4. LEAK & OPS CHKD OK. PRESSURE RESTORED TO INTERLOCK CYLINDER & TRUCK POSITIONER SYS, REVEALED SWIVEL GLAND ON RT MLG BROKEN & LEAKING. R & R TRUCK BEAM TRIM CYLINDER SWIVEL GLAND IAW AMM 32-37-02-4. ALL LEAK & OPS CHKD OK. GEAR SWING CHK OK, HANDLE MOVES AS REQUIRED & GEAR RETRACTS & EXTENDS NORMALLY.
HYD 3 FAIL ON DESCENT. EMERGENCY DECLARED. SYSTEM 3 FOUND EMPTY AT COCKPIT INDICATION AT BLOCK IN. OPENED #3 ENGINE FOR POSSIBLE LEAKS AND WHILE DRY MOTORING PER JRH CHAPTER 5 SAW LARGE AMOUNT OF HYDRAULIC FLUID EXITING THE RIGHT FLUID DISCONNECT PANEL SCUPPER DRAIN. INSPECTED PANEL AND FOUND PUMP CASE DRAIN LINE FINGER TIGHT AND WET, TIGHTENED CASE DRAIN LINE PER AMM 20-40-01-2-0 AND DRY MOTORED AGAIN, LEAK STOPPED AND HYDRAULIC QUANTITY DID NOT DECREASE AS IT DID THE FIRST DRY MOTOR.
PILOTS WERE INFORMED AT BLOCK IN THAT #9 WHEEL WAS MISSING. NO PHYSICAL INDICATION ON EITHER TO OR LANDING. INSTALLED NEW.
NOSE GEAR INDICATOR LIGHT OUT. SECONDARY GEAR INDICATOR (CONFIG PAGE) INDICATED ALL DOWN AND LOCKED. EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. EMERGENCY DECLARED AMM 33-11-17-2 AMM 32-61-00-5 PER CREW DEBRIEF PRIMARY LIGHTS WERE INOP BUT CONFIG SYNOPTIC PAGE DISPLAYED ALL 4 GEAR GREEN. NOSE GEAR PIN WENT IN SMOOTH WITH NO BINDING. REPLAMPED NOSE GEAR INDICATOR LAMPS REF ABOVE. LIGHTS WORK PROPERLY. PERFORMED LIGHTS TEST ALL LIGHTS FOR ALL 4 GEAR ILLUMINATED. PULLED LANDING GEAR CONTROL HANDLE OUT OF DOWN DETNET. ALL GEAR SAFE AND UNSAFE LIGHTS ILLUMINATED. OK FOR SERVICE.
ON POST FLIGHT WALK AROUND FOUND R1 DOOR SLIDE TEST LIGHT INOP WITH RELAMP UNSUCCESSFUL. RELAMPED WITH 368 BLUBS OPS CKS GOOD.
LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 AND EA#1-5750-T0326149 B P3 STEP 2A AND STEP 2B. TITLE: WINGS-FLIGHT SURFACES-LEFT HAND WING- INBOARD FLAP-OUTBOARD FORWARD HINGE (WING SIDE) BRACKET ASSEMBLY- PSE 57.55.01.1. INSPECTION-ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100. (WRI:57509427 FOR DETAILS)
RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 AND EA#1-5750-T0326146 B P3 STEP 2A AND STEP 2B. TITLE: WINGS-FLIGHT SURFACES-RIGHT HAND WING- INBOARD FLAP-OUTBOARD FORWARD HINGE (WING SIDE) BRACKET ASSEMBLY- PSE 57.55.01.1. INSPECTION-ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100. (WRI:57509428 FOR DETAILS)
RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-07. REPAIR EVALUATED AND FOUND RIGHT HAND INBOARD FLAP FORWARD OUTBOARD HINGE PIVOT BORE SPOTFACE REMAINING THICKNESS IS CORRECT AS PER EA#1-5750-T0326146 B P3 STEP 1 FIGURE 1. TITLE: WINGS-FLIGHT SURFACES-RIGHT HAND WING- INBOARD FLAP-OUTBOARD FORWARD HINGE (WING SIDE) BRACKET ASSEMBLY- PSE 57.55.01.1. INSPECTION-ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.(WRI:57509428 FOR DETAILS)
RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 AND EA#1-5750-T0326146 B P3 STEP 2A AND STEP 2B. TITLE: WINGS-FLIGHT SURFACES-RIGHT HAND WING- INBOARD FLAP-OUTBOARD FORWARD HINGE (WING SIDE) BRACKET ASSEMBLY- PSE 57.55.01.1. INSPECTION-ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100. (WRI:57509428 FOR DETAILS)
RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 AND EA#1-5750-T0326146 B P3 STEP 2A AND STEP 2B. TITLE: WINGS-FLIGHT SURFACES-RIGHT HAND WING- INBOARD FLAP- OUTBOARD FORWARD HINGE (WING SIDE) BRACKET ASSEMBLY- PSE 57.55.01.1. INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.(WRI:57509428 FOR DETAILS)
LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 AND EA#1-5750-T0326149 B P3 STEP 2A AND STEP 2B. TITLE: WINGS-FLIGHT SURFACES-LEFT HAND WING- INBOARD FLAP- OUTBOARD FORWARD HINGE (WING SIDE) BRACKET ASSEMBLY- PSE 57.55.01.1. INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.(WRI:57509427 FOR DETAILS)
LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 AND EA#1-5750-T0326149 B P3 STEP 2A AND STEP 2B. TITLE: WINGS-FLIGHT SURFACES-LEFT HAND WING- INBOARD FLAP-OUTBOARD FORWARD HINGE (WING SIDE) BRACKET ASSEMBLY- PSE 57.55.01.1. INSPECTION-ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100. (WRI:57509427 FOR DETAILS)
RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-52-03 AND EA#1-5750- 71783G P6 STEP 2A AND STEP 2B. TITLE: WINGS-RIGHT INBOARD TRAILING EDGE FLAP-HINGE BRACKETS CORRODED PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100. (WRI:57109426 FOR DETAILS)
RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. REPAIR EVALUATED AND FOUND RIGHT HAND INBOARD FLAP AFT OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE SURFACE REMAINING THICKNESS IS CORRECT AS PER EA#1-5750-71783G P6 STEP 1 FIGURE 1.. TITLE: WINGS-RIGHT INBOARD TRAILING EDGE FLAP-HINGE BRACKETS CORRODED PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.(WRI:57109426 FOR DETAILS)
RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-52-03 AND EA#1-5750- 71783G P6 STEP 2A AND STEP 2B. TITLE: WINGS-RIGHT INBOARD TRAILING EDGE FLAP-HINGE BRACKETS CORRODED PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100. (WRI:57109426 FOR DETAILS)
LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. REPAIR EVALUATED AND FOUND LEFT HAND INBOARD FLAP AFT OUTBOARD HINGE PIVOT BORE INBOARD LUG HOLE SURFACE REMAINING THICKNESS IS CORRECT AS PER EA#1-5750-71784 I P6 STEP 1 FIGURE 1. TITLE: TITLE: WINGS-LEFT INBOARD TRAILING EDGE FLAP-HINGE BRACKETS CORRODED (FLAP SIDE) PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100. (WRI:57509425 FOR DETAILS)
LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-52-03 AND EA#1-5750- 71784 I P6 STEP 2A AND STEP 2B. TITLE: TITLE: WINGS-LEFT INBOARD TRAILING EDGE FLAP-HINGE BRACKETS CORRODED (FLAP SIDE) PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM6-2- 100.(WRI:57509425 FOR DETAILS)
LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-52-03 AND EA#1-5750- 71784 I P6 STEP 2A AND STEP 2B. TITLE: TITLE: WINGS-LEFT INBOARD TRAILING EDGE FLAP-HINGE BRACKETS CORRODED (FLAP SIDE) PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM6-2- 100.(WRI:57509425 FOR DETAILS)
CABIN - LEFT HAND FLOOR PANEL #271EF VIEW PORT CUTOUT HOLE FOUND DAMAGE AT STATION 1381, X = 50. CABIN - DAMAGED LEFT HAND FLOOR PANEL #271EF AT STATION 1381, X = 50 REMOVED AND REPLACED AS PER MD-11 AMM 53-21-04-4. LEFT HAND FLOOR PANEL #271EF FABRICATED AS PER FEDEX DRAWING SRZ 25-005 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - RIGHT HAND FLOOR PANEL #272EF VIEW PORT CUTOUT HOLE FOUND DAMAGE AT STATION 1381, X = - 50. CABIN - DAMAGED RIGHT HAND FLOOR PANEL #272EF AT STATION 1381, X = - 50 REMOVED AND REPLACED AS PER MD-11 AMM 53-21-04-4. RIGHT HAND FLOOR PANEL #272EF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
UPPER AUX TANK STRINGER 47 AT STATION XCW -46.5 FOUND CRACK. UPPER AUXILLARY TANK STRINGER 47 AT STAION XCW - 46.5 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.
UPPER AUX TANK STRINGER 47 AT STATION XCW 17 FOUND CRACK. UPPER AUXILLARY TANK STRINGER 47 AT STATION XCW 17 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.
RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 654 FOUND CRACK ABOUT 0.4 INCH. RT WING FIXED LEADING EDGE AT XOS 654 CRACKED BEADED DOUBLER REPAIR CARRIED OUT IAW MD-11 SRM 57-40-02-2R, REPAIR 15, FIGURE 203. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
CABIN SEAT TRACK RIGHT HAND STATION 1179, X = - 8.5 FOUND CROWN DAMAGE. CABIN - AT RIGHT HAND SEAT TRACK STATION 1179, X = - 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1189 TO EXISTING SPLICE STATION 6-100/1129, X = - 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN SEAT TRACK LEFT HAND STATION 1179, X = 8.5 FOUND CROWN DAMAGE. AT LEFT HAND SEAT TRACK STATION 1179, X = 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1129/6-100 TO STATION 1269, X = 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN SEAT TRACK LEFT HAND STATION 1219, X = 8.5 FOUND CROWN DAMAGE. AT LEFT HAND SEAT TRACK STATION 1219, X = 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1129/6-100 TO STATION 1269, X = 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SNRM N00506 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN SEAT TRACK RIGHT HAND STATION 1341, X = -8.5 FOUND CROWN DAMAGE. AT RIGHT HAND SEAT TRACK STATION 1341, X = - 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1311 TO STATION 1451, X = - 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SNRM N00510 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN SEAT TRACK LEFT HAND STATION 1381, X = 8.5 FOUND CROWN DAMAGE. AT LEFT HAND SEAT TRACK STATION 1381, X = 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1311 TO STATION 1411, X = 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN SEAT TRACK RIGHT HAND STATION 1421, X = -8.5 FOUND CROWN DAMAGE. AT RIGHT HAND SEAT TRACK STATION 1421, X = - 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1311 TO STATION 1451, X = - 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN SEAT TRACK RIGHT HAND STATION 1541, X = -8.5 FOUND CROWN DAMAGE. AT RIGHT HAND SEAT TRACK STATION 1541, X = - 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1531/5-123 TO STATION 1571, X = - 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING FIXED LEADING EDGE FORMER AT XOS 584 FOUND CRACK ABOUT 2 INCHES. RT WING FIXED LEADING EDGE AT XOS 584 CRACKED FORMER REMOVED AND REPLACED IAW MD-11 SRM 51-31-01-OG. FORMER FABRICATED IAW DRAWING ARB 2931 REVISION H. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 906 FOUND CRACK ABOUT 1 INCH. LEFT WING FIXED LEADING EDGE AT XOS 906 CRACKED RIB DOUBLER REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-OG. RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB 3954 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 582 FOUND CRACK ABOUT 0.8 INCH. LT WING FIXED LEADING EDGE AT XOS 582 CRACKED BEADED DOUBLER REPAIR CARRIED OUT IAW MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN SEAT TRACK LEFT HAND STATION 839, X = 8.5 FOUND CROWN DAMAGE. CABIN - AT LEFT HAND SEAT TRACK STATION 839, X = 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 860 TO EXISTING SPLICE STATION 805, X = 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
R1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INDICATOR LIGHT DOES NOT ILLUMINATE WHEN PRESSED. RELAMPED REMOTE PRESSURE INDICATOR PTT BUTTON, IAW AMM 25-61-04-4. OPS CHECK NORMAL IAW AMM 25-61-04-5. OK TO CONTINUE.
AT 3:55 INTO FLIGHT GOT TIRE PRESS LO ALERT. NOSE TIRE PRESSURES 132/161. THE LEFT SLOWLY DECAYED TO 119. ON LANDING, PRESSURES WENT TO 135/182. DECLARED EMERGENCY WITH APPROACH & TOWER. LT NOSE TIRE WITHIN LIMITS IAW SERVICE CHECK. TIRE SERVICED TO CORRECT PRESSURE, 195 PSI.
NUMBER 3 ENGINE LOST OIL QUANTITY (ALL OIL GONE) AS WE WERE IN THE CLIMB-OUT PASSING ABOUT 6,500 FEET, FOLLOWED BY AN OIL PRESSURE ALERT ABOUT A MINUTE LATER. RAN QRH FOR LOSS OF OIL QUANTITY (ENGINE OIL PRESS LOW) AND SHUT NUMBER 3 ENGINE DOWN IN FLIGHT WITH THE FUEL LEVER, USING ENGINE SHUTDOWN IN FLIGHT CHECKLIST. DECLARED AN EMERGENCY AND LANDED ON KMEM RUNWAY 18C. NO FUEL DUMP WAS NEEDED. FIRE VEHICLES CONFIRMED LEAKING OIL FROM NO. 3 ENGINE AND INSISTED WE BE TOWED IN. I ESTIMATE THE TIME FROM NOTICING OIL LOSS TO ENGINE SHUTDOWN WAS PROBABLY ABOUT FOUR MINUTES AS WE RAN CHECKLISTS AND COORDINATED WITH ATC, BUT I HAD REDUCED THE THRUST TO IDLE AS SOON AS I NOTICED THE LOW OIL ALERT. ***EMERGENCY DECLARED*** COMPLETED #3 ENG INSTALL REF WORK CARD 71T0903-PW. LEAKS AND OPS CHECKS GOOD OK FOR SVC
FORWARD CARGO - STATION 1119 TO STATION 6-10 LONGERON 44 LEFT SPLICE CORROSION. FORWARD CARGO - STATION 1119 TO STATION 6-10 LONGERON 44 LEFT LONGERON SPLICE CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND EXCEED LIMIT AS PER SRM 53- 00-00-2R FIGURE 205 REPAIR GENERAL. SPLICE REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01-0G. SPLICE FABRICATED AS PER DOUGLAS DRAWING : ADA8424 REVISION : A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO DOOR CUTOUT, UPPER SILL ATTACHED HINGE FITTING NUMBER 1 (ACA7223- 513) LOBES 1 AND 2, AND 12-17 FOUND OUT-OF-TOLERANCE. MAIN DECK CARGO DOOR CUTOUT, UPPER SILL ATTACHED HINGE FITTING NUMBER 1(ACA7223- 513) LOBES 1 AND 2, 12 TO 17 REWORKED AND FOUND LOBES 1 AND 2 EXCEED LIMIT AS PER MD-11 SRM 52-30-16-1A ALLOWABLE DAMAGE 2 FIGURE 101 SHEET 3. OVERSIZED REPAIR BUSHINGS (08EACH) FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 52-34-04 REPAIR-GENERAL, PARAGRAPH 2.Y AND EA # 1-5310-T0368724 PART 1 STEP 2 AND STEP 5, TITLE: FUSELAGE - MAINFRAME - MAIN DECK CARGO JAMB FORWARD SUPPORT HINGE (FUSELAGE SIDE) - WORN HINGE LOBE BORES. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
RIGHT HAND WING - FINGER DOUBLERS AT TRAILING EDGE COMPARTMENT BETWEEN STATION XW 375 AND XW 387 FOUND DISBONDED. RIGHT HAND WING FINGER DOUBLERS AT TARILING EDGE COMPARTMENT BETWEEN STATION XW 375 AND XW 387 REPAIR CARRIED OUT AS PER SRM 57-50-01-2R REPAIR 6 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING - FINGER DOUBLERS AT TRAILING EDGE COMPARTMENT BETWEEN STATION XW 375 AND XW 387 FOUND DISBONDED. LEFT HAND WING FINGER DOUBLER AT TRAILING EDGE COMPARTMENT BETWEEN STATION XW 375 AND XW 387 REPAIR CARRIED OUT AS PER SRM 57-50-01-2R REPAIR 6 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT RIGHT HAND SIDE , DENT FOUND AT STATION 1701 RIGHT HAND FRAME LONGERON 12 RIGHT. MAIN DECK CARGO COMPARTMENT RIGHT HAND SIDE AT STATION 1701 LONGERON 12 RIGHT FRAME FLANGE DENTED REPAIRED AS PER SRM 53-00-07-2R REPAIR 2 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL HIGH FREQUENCY EDDY CURRENT INSPECTION TO BE CARRY OUT AT 14,500 FLIGHT CYCLES FROM TIME OF REPAIR AND REPETITIVE INSPECTION TO BE CARRY OUT AT EVERY 9,500 FLIGHT CYCLES PER SRM 53-00-07- 2R TABLE 201 / REPAIR 2 REQUIREMENT.
EXISTING REPAIR AT FUSELAGE SKIN - FORWARD CARGO DOOR CUTOUT - FORWARD JAMB SKIN EXTERIOR STATION 895, LONGERON 39 RIGHT HAND TO 41 RIGHT HAND. EXISTING REPAIR AT FUSELAGE SKIN - FORWARD CARGO DOOR CUTOUT - FORWARD JAMB SKIN EXTERIOR STATION 895, LONGERON 39 RIGHT HAND TO 41 RIGHT HAND EVALUATED FOUND REPAIR DOUBLERS CRACKED. REPAIR CARRIED OUT AT FORWARD CARGO DOOR CUTOUT FORWARD JAMB SKIN EXTERIOR STATION 895, LONGERON 39 RIGHT HAND TO 41 RIGHT HAND IN ACCORDANCE WITH SRM 53-00-15-2R REPAIR 8 FIGURE 202. EO 1-5100-7-5001 B7 PART1, TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
EMPENNAGE - AFT FUSELAGE SKIN RIGHT HAND SIDE AT APPROXIMATE STATION 2160 LONGERON 33 RIGHT TO LONGERON 35 RIGHT AREA FOUND CORROSION. EMPENNAGE - AFT FUSELAGE RIGHT HAND SIDE AT APPROXIMATE STATION 2160 LONGERON 33 RIGHT TO LONGERON 35 RIGHT SKIN CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-01-2R FIGURE 201 SHEET 3 REPAIR 3. REPAIR CARRIED OUT AS PER SRM 53-70-01-2R FIGURE 201 REPAIR 3. REPAIR DOUBLER AND FILLER FABRICATED AS PER SRM 53- 70-01-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
FORWARD CARGO - STATION 1119 TO STATION 6-10 LONGERON 51 LEFT SPLICE SUSPECT CRACK. FORWARD CARGO - STATION 1119 TO STATION 6-10 LONGERON 51 LEFT CRACKED LONGERON SPLICE REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33- 01-0G. SPLICE FABRICATED AS PER DOUGLAS DRAWING : ADA8424 REVISION : A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
FORWARD CARGO - STATION 1119 TO STATION 6-10 LONGERON 52 SPLICE FOUND CORROSION. FORWARD CARGO - STATION 1119 TO STATION 6-10 LONGERON 52 SPLICE CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 REPAIR GENERAL. SPLICE REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01-0G. SPLICE FABRICATED AS PER DOUGLAS DRAWING : ADA8424 REVISION : A REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK X= 8.5 STATION 625 TO 645 LEFT HAND. EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK X= 8.5 STATION 625 TO 645 LEFT HAND EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201. EO 1-5100-7-5001 B7 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - SEAT TRACK AT STATION 715 X = -27.5 FOUND CRACKED. CABIN CRACKED SEAT TRACK AT STATION 715 X = -27.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 705 TO EXISTING SPLICE STATION 745 X = -27.5 AS PER SRM 53- 00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AGING AIRCRAFT - EXISTING REPAIR AT FUSELAGE SKIN EXTERIOR STATION 595 TO 615, LONGERON 27 LEFT TO 29 LEFT. EXISTING REPAIR AT FUSELAGE SKIN EXTERIOR STATION 595 TO 615, LONGERON 27 LEFT TO 29 LEFT EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 53-00-01-2R REPAIR 1 FIGURE 201 CLASS II SHEET 9-12. EA 1-5330-T0368767 PART1, TITLE: FUSELAGE - PLATES & SKINS - EXISTING EXTERNAL DOUBLER REPAIR ON FUSELAGE SKIN BETWEEN STA595 - STA615 AND LONGERONS 27L-29L, ACCOMPLISHED. EO 1-5100-7-5001 B7 PART1, TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707, ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
HIGH FREQUENCY EDDY CURRENT INSPECTION FOUND CRACK INDICATION APPROXIMATE 0.30" IN LENGTH AT RIGHT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT AT CORNER NUMBER 13 SLAT TRACK #10 CUTOUT AFT INBOARD CORNER AT APPROXIMATE XOS 659.717.
EMPENNAGE - AFT FUSELAGE AT STATION 2164 BULKHEAD LOWEST STIFFENER RIGHT HAND CORNER FOUND CRACK LENGTH 0.3 INCH
LEFT HAND WING FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 669. LEFT HAND WING FIXED LEADING EDGE SKIN INTERNAL DOUBLER AT STATION XOS 669 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 791. LEFT HAND WING FIXED LEADING EDGE SKIN INTERNAL DOUBLER AT STATION XOS 791 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 613.
RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 733.
RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 764.
PDIS 620 27-50 7107 23MAR22 EWR OPEN U FLAP DISAG ON FINAL APPROACH. LEFT OUTBOARD FLAP WAS CYCLING IN AND OUT OF TOLERANCE (FLAP DISAG ALERT) AT ALL FLAP SETTINGS (15, 28, 35). WENT AROUND AND DECLARED EMERGENCY. RAN FLAP DISAG QRH. SECOND APPROACH PUT FLAPS OUT AT LOWER SPEEDS. NEVER GOT ALERT. LEFT OUTBOARD STOPPED AT 30 DEGREES FOR FLAPS 35 SETTING. NO ADVERSE HANDLING CHARACTERISTICS NOTED. MEL 23MAR22 04:16 EWR U RELEASED FOR SERVICE PER MEL : 27-54-01 CATEGORY : C EXPIRATION : 02APR22 "MEL 27-54-01: FLAP POSITION INDICATOR - INOP. VERIFY SYMMETRICAL FLAP MOVEMENT PRIOR TO TAXI FOR EACH BLOCKOUT." -INSTALLED JUMPER ON LOB FLAP TRANSMITTER. PER THIS MEL. C/7309895
FUEL QTY/ USED CHK ILLUMINATED IN FLIGHT. UPON LANDING CFR STATED FUEL COULD BE SEEN LEAKING FROM ENGINE NACELLE #3 INSTALLED FUEL LINE CONNECTION WITH NEW PACKINGS IPC 28-24-01-01 AND INSTALLED FUEL SHROUD COUPLING. T- FITTING, ORING AND JAM NUT INSTALLED AND LEAK CHECKED NO LEAKS FOUND AFTER ENGINE RUNS. REF JRH, MD 11 MM 28-00-00-04, AND E.A.#:1-2802-T0367669. A/C OK FOR SERVICE.
PDIS 620 21-30 7092 19MAR22 MEM FACT U ON DEPARTURE OUT OF KMEM AT APPROX 2000 FT AS WE BEGAN OUR CLIMB WE GOT A LEVEL 1 CABIN RATE ALERT. OUTFLOW VALVE WAS CLOSED AND AVIONICS FAN WENT TO OVERRIDE. AS WE CONTINUED TO CLIMB THE CABIN ALT CONTINUED TO CLIMB. WE LEVELED OFF AT 10000 FT WITH A CABIN ALT OF 8800 FT. RTB TO KMEM. SHGN 20MAR22 00:08 MEM U UPON BLOCK IN OF A/C FOUND MAIN CARGO DOOR VENT DOOR OPEN. SUSPECT DOOR TO BE AT FAULT FOR PRESSURE ISSUE. CLOSED CARGO VENT DOOR PER SMP. DOOR INDICATION ISSUE STILL REMAINS AND NEEDS TO BE WORKED. INFO 20MAR22 00:28 MEM ********************MOCC UPDATE******************** PLEASE WORK IN CONJUNCTION WITH TSI: 21-30/7091 *************THANKS MOCC TECH SERVICES************* 20MAR22 06:58 MEM R OLD DISCREPANCY : 620 / 52-30 / 0007090 SHGN 20MAR22 07:04 MEM U REF WRI 52-70/7093 FOR MAIN CARGO DOOR INDICATION ISSUE. FACT 20MAR22 08:09 MEM U PRESSURIZED A/C REF. MD11 AMM 21-00-00-2. OPS CHECK WAS GOOD. NO FAULTS OR DEFECTS FOUND.
AFTER TO AT APPROX 6000 FT, WE GOT ALT DISAGREE WARNING ON BOTH PFDS. INITIALLY BOTH ALT TAPES WERE AT MOST 20 FT OFF FROM EACH OTHER. AS WE CONTINUED TO CLIMB UP TO 16000 FT, THE DISAGREEMENT BETWEEN THE TWO TAPES CONTINUED TO INCREASE TO A MAXIMUM OF 160 FT. AS WE RETURNED TO KMEM, DESCENDING TO 5000 FT THE ALT DISAGREE WARNING WENT AWAY. DURING T/S, MOCC NOTIFIED US THAT #2 ADC HAD NUMEROUS AHM FAULTS. REPLACED #2 ADC REF AMM 34-16-01-4. DURING OPS CHECKS, FOUND F/O ALT STATIC SOURCE SWITCH IN "ALTN" POSITION.
#10 BRAKE OVERHEAT LEVEL 2 AFTER TAKEOFF FROM KEWR. MAX TEMP 720, COMPLIED WITH QRH. TEMP DECREASED AND ALERT WENT AWAY. LANDING IN MEMPHIS, ALL BRAKE TEMPS WERE APPROXIMATELY THE SAME. #10 BRAKE MATCHED OTHER BRAKE TEMPERATURES.
#10 BRAKE OVERHEAT LEVEL 2 AFTER TAKEOFF FROM KEWR. MAX TEMP 720, COMPLIED WITH QRH. TEMP DECREASED AND ALERT WENT AWAY. LANDING IN MEMPHIS, ALL BRAKE TEMPS WERE APPROXIMATELY THE SAME. #10 BRAKE MATCHED OTHER BRAKE TEMPERATURES. NO. 10 BRAKE WAS HARD TO SPIN BY HAND AND WAS MAKING A RACHETING NOISE. REMOVED AND REPLACED NO. 10 BRAKE IAW MD11MM 32-43-20-4. OPS AND LEAK CHECK
DURING PREFLIGHT CHECK, SMELT BAD ODOR IN COCKPIT WHEN USING APU BLEED AIR. R & R ALL 3 PACK WATER SEPARATOR COALESCERS, RAN NR 1 & NR 2 ENGINE. PERFORMED ALL 3 PACK TEST, ALL TEST PASSED. NO MORE ODOR IN COCKPIT. A/C OK FOR SERVICE.
APU SMOKE IN COCKPIT AND COMING OUT OF THE PACKS OUTSIDE ON APU START. RAN APU, REF JRH WITH ALL THREE PACKS OPERATING AT MULTIPLE TEMP SETTINGS WITH NO ABNORMAL ODORS IN COCKPIT OR CABIN. INSPECTED APU AREA AND PACK BAYS. NO DEFECTS NOTED. MEL REMOVED, A/C OK FOR SERVICE.
CABIN, FOUND SEAT TRACK STATION 615, X = - 8.5 CROWN DAMAGED. CABIN, DAMAGED CROWN AT SEAT TRACK STATION 615 X = - 8.5, EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 605 TO STATION 625 X = - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231EF TOP SURFACE DAMAGED AT STATION 495 TO STATION 595 LEFT HAND SIDE. DAMAGED FLOOR PANEL REMOVED AS PER AMM 53-21-04. FLOOR PANEL 231EF FABRICATED AS PER DWG SRZ-25-005 REV R. FABRICATED FLOOR PANEL 231EF INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231 HF TOP SURFACE DAMAGED AT STATION 595 TO STATION 675 LEFT HAND SIDE. DAMAGED FLOOR PANEL 231 HF AT CABIN STATION 595 - STATION 675 (LT) REMOVED AS PER AMM 53-21-04. FLOOR PANEL 231 HF FABRICATED AS PER DWG SRZ -25-005 REV R. FABRICATED FLOOR PANEL 231 HF INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
CENTER CARGO COMPARTMENT DOOR SIDE HINGE MOST AFT 2 EACH HOLES FOUND EXCEEDED MAXIMUM DIAMETER LIMIT. CENTER CARGO COMPARTMENT DOOR SIDE HINGE MOST AFT 2 EACH HOLES REWORKED AS PER SRM 52-30-16-1A FIGURE 101 SHEET 1 AND FOUND HOLES EXCEEDED LIMIT. REPAIR BUSHINGS 02 EACH FABRICATED BY MACHINING AND WET INSTALLED AS PER CMM 52-32-07 REPAIR 1-1, PARAGRAPH G AND EA 1-5230-T0354384 PART 1 STEPS 2 AND 5 TITLE: DOORS - CARGO DOOR/HYD SYS - CENTER LOWER CARGO DOOR ASSY - ELONGATED HOLES ON AFT SUPPORT HINGE LOBE. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
CENTER CARGO COMPARTMENT DOOR FORWARD LOWER CORNER DOOR STATION 1640 FOUND CHAFING. CHAFING DAMAGE REPAIRED AS PER ENGINEERING AUTHORIZATION 1-5230-T0354334 PART 1 TITLE " DOORS - CARGO DOOR / HYD SYS - CENTER CARGO DOOR - DAMAGES FOUND ON OUTER SKIN AND INNER PAN AT LOWER FWD CORNER WORK INSTRUCTIONS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AFT CARGO COMPARTMENT DOOR AFT JAMB STATION 1959 FOUND CORRODED. AFT CARGO COMPARTMENT DOOR AFT JAMB CORRODED FRAME AT STATION 1959 REMOVED AND REPLACED WITH NEW FRAME AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
CENTER CARGO COMPARTMENT, UPON REMOVAL OF LONGERON ACCESS LONGERON SPLICE AT STATION 1531 LONGERON 39 RIGHT HAND FOUND CRACK. LONGERON SPLCE REMOVED AND REPLACED AS PER SRM 51-33-01-0G. LONGERON SPLICE FABRICATED AS PER DRAWING A5A7114 , REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER CARGO COMPARTMENT LONGERON SPLICE AT STATION 1539 LONGERON 38 RIGHT HAND FOUND WITH SUSPECTED CRACK. CENTER CARGO COMPARTMENT CRACKED LONGERON SPLICE AT STATION 1539, LONGERON 38 RIGHT HAND REMOVED AND REPLACED AS PER SRM 51-33-01-0G. LONGERON SPLICE FABRICATED AS PER DRAWING A5A7114 , REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AFT CARGO COMPARTMENT SEAT TRACK FLANGE AT 1962 X = 21 LEFT HAND FOUND CORRODED AFT CARGO COMPARTMENT CORRODED. SEAT TRACK REMOVED AND REPLACED AS PER AMM 20-50-02. SEAT TRACK REWORKED AS PER DRAWING AGA3855, REVISION N. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER CARGO COMPARTMENT LONGERON AT STATION 1581 - 1601 LONGERON 38 RIGHT HAND FOUND CRACK. CENTER CARGO COMPARTMENT CRACKED LONGERON AT STATION 1581 - 1601 LONGERON 38 RIGHT HAND REPAIR CARRIED OUT FROM STATION 1531 TO STATION 1620 END OF PART LONGERON AS PER SRM 53-00-05-2R REPAIR 1 FIGURE 201 AND FIGURE 202. REFER TO SPECIAL NONROUTINE MAINTENANCE FORM N00667 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER CARGO COMPARTMENT LONGERON AT STATION 1561 - 1581 LONGERON 38 RIGHT HAND FOUND CRACK. CENTER CARGO COMPARTMENT CRACKED LONGERON AT STATION 1561 - 1581 LONGERON 38 RIGHT HAND REPAIR CARRIED OUT FROM STATION 1531 TO STATION 1620 END OF PART LONGERON AS PER SRM 53-00-05-2R REPAIR 1 FIGURE 201 AND FIGURE 202. REFER TO SPECIAL NONROUTINE MAINTENANCE FORM N00667 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER CARGO COMPARTMENT/ LONGERON AT STATION 1539 LONGERON 38 RIGHT HAND FOUND CRACK. CENTER CARGO COMPARTMENT CRACKED LONGERON AT STATION 1539 LONGERON 38 RIGHT HAND REPAIR CARRIED OUT FROM STATION 1531 TO STATION 1620 END OF PART LONGERON AS PER SRM 53-00-05-2R REPAIR 1 FIGURE 201 AND FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER CARGO COMPARTMENT LONGERON AT STATION 1541 - 1561 LONGERON 38 RIGHT HAND FOUND CRACK CENTER CARGO COMPARTMENT CRACKED LONGERON AT STATION 1541 - 1561 LONGERON 38 RIGHT HAND REPAIR CARRIED OUT FROM STATION 1531 TO STATION 1620 END OF PART LONGERON AS PER SRM 53-00-05-2R REPAIR 1 FIGURE 201 AND FIGURE 202. REFER TO SPECIAL NONROUTINE MAINTENANCE FORM N00667 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING - BEADED DOUBLER AT STATION XOS 635 FOUND CRACK. REPAIR CARRIED OUT AT RIGHT HAND WING DOUBLER AT STATION XOS 635 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
DURING HFEC INSPECTION ON NOSE LANDING GEAR LEFT HAND TRUNNION FITTING TRIM OUT AREA AT STATION Y = 595 FOUND CRACK AT LONGERON 49 LEFT HAND. NOSE LANDING GEAR LEFT HAND TRUNNION FITTING AREA AT STATION Y = 595, CRACKED LONGERON 49 LEFT HAND REMOVED AND REPLACED AS PER SRM 51-33-01-0G. LONGERON 49 LEFT HAND FABRICATED AS PER DRAWING ACA 3796 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
AFT CARGO COMPARTMENT / SEAT TRACK TRACK FLANGE AT 1962 X = 21 ( LEFT HAND ) FOUND CORRODED AFT CARGO COMPARTMENT CORRODED SEAT TRACK AT STATION 1962, X = 21 LEFT HAND. REMOVED AND REPLACED AS PER AMM 20-50-02. SEAT TRACK REWORKED AS PER DRAWING AGA3855, REVISION N. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER CARGO COMPARTMENT LONGERON AT STATION 1581 TO 1601 LONGERON 38 RIGHT HAND FOUND CRACK.
CENTER CARGO COMPARTMENT LONGERON AT STATION 1561 TO 1581 LONGERON 38 RIGHT HAND FOUND CRACK.
CENTER CARGO COMPARTMENT LONGERON AT STATION 1539 LONGERON 38 RIGHT HAND FOUND CRACK.
CENTER CARGO COMPARTMENT LONGERON AT STATION 1541 TO 1561 LONGERON 38 RIGHT HAND FOUND CRACK.
CENTER CARGO COMPARTMENT / LONGERON SPLICE AT STATION 1537 LONGERON 44 RIGHT HAND FOUND CRACK. CENTER CARGO COMPARTMENT CRACKED LONGERON SPLCE AT STATION 1537 LONGERON 44 RIGHT HAND, REMOVED AND REPLACED AS PER SRM 51-33-01-0G. LONGERON SPLICE FABRICATED AS PER DRAWING A5A7114 , REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER CARGO COMPARTMENT / LONGERON SPLICE AT STATION 5-125 LONGERON 46 LEFT HAND FOUND CRACK. CENTER CARGO COMPARTMENT CRACKED LONGERON SPLICE AT STATION 5-125, LONGERON 46 LEFT HAND SIDE REMOVED AND REPLACED WITH NEW LONGERON SPLICE AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
LEFT HAND WING - BEADED DOUBLER AT STATION XOS 696 FOUND CRACK. REPAIR CARRIED OUT AT LEFT HAND WING DOUBLER AT STATION XOS 696 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING - BEADED DOUBLER AT STATION XOS 448 FOUND CRACK. REPAIR CARRIED OUT AT RIGHT HAND WING DOUBLER AT STATION XOS 448 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT AT STATION 1096 X = 27.5 SEAT TRACK FLANGE FOUND CORROSION. MAIN DECK CARGO COMPARTMENT AT STATION 1096 X = 27.5 SEAT TRACK FLANGE, CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1049 TO EXISTING SPLICE STATION 1129 X = 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT AT STATION 1111 X = 8.5 SEAT TRACK FLANGE FOUND CORROSION. MAIN DECK CARGO COMPARTMENT STATION 1111 X = 8.5 AT SEAT TRACK FLANGE CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1089 TO EXISTING SPLICE STATION 1129 X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - SEAT TRACK CROWN AREA DAMAGED AT STATION 5-05, X = -47.5. SEAT TRACK DAMAGE CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1, DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1531/5-0 TO STATION 5-15 X = - 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN SEAT TRACK CROWN AREA DAMAGED AT STATION 1289, X = 8.5. SEAT TRACK CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1269 TO STATION 1311 X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - SEAT TRACK CROWN AREA DAMAGED AT STATION 5-83, X = 8.5. CABIN - AT SEAT TRACK STATION 5-83 X = 8.5, DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REMOVED AND REPLACED AT EXISTING SPLICES STATION 1531/5-0 TO STATION 1531/5-123 X = 8.5 AS PER SRM 51-31-01-0G. SEAT TRACK SEGMENT REWORKED AS PER DRAWING A5A7082 REVISION B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - SEAT TRACK TOP SURFACE CORROSION AT STATION 5-43, X = 8.5. CABIN - AT SEAT TRACK TOP SURFACE STATION 5-43 X = 8.5, CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REMOVED AND REPLACED AT EXISTING SPLICES STATION 1531/5-0 TO STATION 1531/5-123 X = 8.5 AS PER SRM 51-31-01-0G. SEAT TRACK SEGMENT REWORKED AS PER DRAWING A5A7082 REVISION B. REFER TO SNRM N00788 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
NOSE LANDING GEAR LEFT HAND TRUNNION FITTING SUSPECTED CRACKED AT STATION Y = 595 CRACKED NOSE LANDING GEAR LEFT HAND TRUNNION FITTING AT STATION Y = 595 REPAIRED AS PER SRM 53-10-14-2R FIGURE 202 REPAIR 2. INITIAL INSPECTION TO BE CARRIED OUT AT 1500 FLIGHT CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 1500 FLIGHT CYCLES AS PER SRM 53-10-14-2R FIGURE 202 REPAIR 2 TABLE 201 REQUIREMENTS. METHOD BY HIGH FREQUENCY EDDY CURRENT OR LIQUID PENETRANT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
PDIS 620 33-50 3316 10MAY19 MEM FACT U LOGPAGES:2999948 DURING PREFLIGHT EMER LT TEST LEVEL 1. "EMER LT BAT 1 LO" ALERT DISPLAYED. FACT 10MAY19 19:42 MEM U ACCOMPISHED "EMERGENCY LIGHT TEST" AS PER AMM 24-34-00-5, TEST PASSED, OK FOR SERVICE.
PDIS 620 30-20 3106 20FEB19 DTW OPEN U LOGPAGES:2198834 ENG ANTI-ICE SELECTED INFLIGHT. GOT A ENG 2 ANTI-ICE OFF SHGN 20FEB19 16:18 DTW AS PERCAUTION REMOVED AND REPLACED THE NR 2 ENGINE ANTI ICE DET UNIT PER MM 30-22-10-4. OPS CHECKS GOOD.
REMOVED LOCK S 1287 DUE TO SEAT TRACK DAMAGED AT POSITION 8L, RESTRAINT NUMBER ..S 1287. REMOVED CARGO LOADING SYSTEM AND 4 FLOOR BOARDS REF AMM 53-21-01-4 @ POS 8L TO FOM SHGN 27JAN19 06:44 MEM U FABRICATED REPAIR SECTION OF SEAT TRACK FROM MPN 60-4508 PO #MP5624962. OK TO IN STALL. REF SRM 53-21-01-4 STRP 27JAN19 06:44 MEM U SHGN 27JAN19 06:56 MEM U REPAIR INSTALLED OK AT NOTED LOCATION REF SRM 53-21-01-4 STRP 27JAN19 06:56 MEM U STRP 27JAN19 07:45 MEM U FACT 27JAN19 07:45 MEM U REINSTALLED CARGO LOADING SYSTEM AND FLOORBOARDS IRW AMM 53-21-1-4 AND 25-59-00-1-1.
MDIS 620 52-10 2903 25DEC18 OAK FACT U NOTICED R1 DOOR EXTERNAL HANDLE IN EMERGENCY POSITION AND BOTTLE BLOWN. FACT 25DEC18 19:20 OAK U RE-POSITIONED R1 DOOR HANDLE & SERVICED R1 DOOR PNEUMATIC STORAGE BOTTLE REF M/M 12-25-04-3. A/C OK FOR SERVICE. FACT 25DEC18 19:20 OAK U RE-POSITIONED R1 DOOR HANDLE & SERVICED R1 DOOR PNEUMATIC STORAGE BOTTLE REF M/M 12-25-04-3. A/C OK FOR SERVICE.
GOT SLAT DISAG ALERT AFTER TAKEOFF FROM KIX, ALERT CAME ON IMMEDIATELY AFTER TAKEOFF. NO ADVERSE ROLL MOMENT NOTED. RAN QRH AND ALERT WENT AWAY WHEN SLATS WERE RETRACTED. WHEN CONFIGURING FOR APPROACH AT PEK. SLAT DISAG ALERT CAME ON AGAIN. NO ADVERSE ROLL MOMENT. RAN QRH AND DID 28/RET APPROACH AND LANDING. T/S PER FIM 31-71-07-00. FOUND SENSOR LT ON WITH CODE 01. R&R LT NR 4 SLAT POSITION SENSOR A. P/N 8-614-02 IAW AMM 27-84-03-4. OPS TEST SLAT GOOD PER AMM 27-80-00-2. PSEU TEST SATIS PER AMM 31-71-01-2. A/C OK FOR SVC.
CREW REPORTED , CAPTS SEAT HAS MISSING LIFE PRESERVER. LIFE VEST, P/N 63600-105 C/7147186. INSTALLED NEW LIFE VEST PER MM 25-64-01-2.
ATTEMPTED TAKEOFF ON SIN RW 20C AND FOUND RUDDER PEDALS NOT CONNECTED TO STEERING. REJECTED AT LESS THAN 60 KTS AND RETURN TO GATE. TROUBLESHOOT FOUND STEERING FOLLOW UP CABLE OUT OF RIG, CARRIED OUT TENSION ADJUSTMENT OF STEERING FOLLOW UP CABLES PER AMM 32-50-00-5. PERFORMED STEERING COLLAR RANGE OF MOVEMENT AND STEERING RESPONSE TIME PER AMM 32-50-00-5 ALL FOUND WITHIN LIMITS.
LEFT WING, INBOARD FLAP VANE LOWER SURFACE WAS FOUND DELAMINATED. REPAIRED IAW EA 1-5750-T0340230A, PT 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.
MAIN DECK AFT FLOOR SUPPORT AT BS 1887 - 2007, LBL 2 WAS FOUND CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, DWG AGA 7081, REV M . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK AFT FLOOR SUPPORT AT BS 1914 - 2007, RBL 22, FOUND CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, AND DWG AGA 7088, REV B. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED ABOUT 8 X 26 INCHES. THE FLAP VANE LOWER SURFACE WAS REPAIRED IAW EA 1-5750-T0340230A, PT 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
MAIN DECK AFT FLOOR SUPPORT BETWEEN BS 1887 - 2007, RBL 2 WAS FOUND CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, AND DWG AGA 7080, REV S. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK AFT FLOOR SUPPORT AT BS 1887 - 2007, RBL 25 WAS FOUND CRACKED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, AND DWG AGA 7087, REV M. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK AFT FLOOR SUPPORT AT BS 1887 - 2007, RBL 57, FOUND CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, DWG AGA 7551, REV G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
FRAME AT BS 535, LONGERON 23L FOUND WITH A REPAIR ANGLE DAMAGED. REPAIRED IAW SRM 53-20-07-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK SEAT TRACK AT BS 635, LBL 47.5 FOUND CRACKED. REPLACED FROM EXISTING SPLICES BS 625 TO 705 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
MAIN DECK SEAT TRACK AT BS 880, RBL 8.5, FOUND THE CROWN DAMAGED. REPLACED FROM BS 869 TO 909, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK SEAT TRACK AT BS 1014, RBL 8.5, FOUND THE CROWN DAMAGED. REPLACED FROM BS 989 TO 1069, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 613 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
LEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 646 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED MAJOR IAW GMM 6-2-100.
LEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 664 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
LEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 701 FOUND CRACKED. REPAIRED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
MAIN DECK R3 DOOR AFT FRAME LOWER BOX AT BS 1305.42, LONGERON 26R - L27R FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK SEAT TRACK AT BS 775, X= 75.25, FOUND THE CROWN DAMAGED. REPLACED THE SEAT TRACK FROM EXISTING SPLICES BS 765 TO 816, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK SEAT TRACK AT BS 1285, LBL 47.5, FOUND TO CROWN DAMAGED. REPLACED THE SEAT TRACK FROM BS 1248 TO 1312, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK SEAT TRACK CROWN AT BS 1421, LBL 47.5 DAMAGED. REPLACED THE SEAT TRACK FROM BS 1390 TO 1431 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK AT STA 1285, X= -8.5 FOUND CROWN DAMAGED AS MARKED. REPLACED THE SEAT TRACK FROM BS 1264 TO 1312, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK SEAT TRACK AT BS 1431, RBL 8.5 WAS FOUND CORRODED. THE CORROSION WAS FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK FROM BS 1391 TO EXISTING SPLICE AT BS 1451 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK SEAT TRACK CROWN AT BS 1421, RBL 47.5 WAS FOUND DAMAGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK FROM BS 1390 TO 1431 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK SEAT TRACK AT BS 1471, LBL 8.5 WAS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK FROM BS 1411 TO EXISTING SPLICE AT BS 5-0 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK SEAT TRACK AT BS 5-43, RBL 8.5 WAS FOUND CORRODED. FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK FROM EXISTING SPLICE BS 5-0 TO 5-83 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK SEAT TRACK CROWN AT BS 5-113, RBL 47.5 FOUND GOUGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK FROM BS 5-83 TO EXISTING SPLICE AT BS 5-123 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING OUTBOARD FLAP TRAILING EDGE CENTER WEDGE UPPER SURFACE FOUND DELAMINATED, ABOUT 5 X 17 INCHES. REPAIRED THE FLAP IAW SRM 57-50-80, REPAIR 1, PARA 4A, 1B. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.
LEFT WING LEADING EDGE, NR 1 PYLON LT SIDE ADJACENT AREA LOWER SUPPORT PLATE FOUND CRACKED. THE SKIN WAS REMOVED IAW SRM 51-35-01-0G, AND FABRICATED A NEW SKIN IAW DRAWING ARB2363, REV C, AND INSTALLED IAW SRM 51-35-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK SEAT TRACK CRACKED AT BS 635, RBL 8.5. REPLACED THE SEAT TRACK FROM EXISTING SPLICES AT BS 625 TO 645 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK SEAT TRACK CRACKED AT BS 635, RBL 27.5. REPLACED THE SEAT TRACK FROM EXISTING SPLICES BS 625 TO 645 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK CRACKED AT BS 695, RBL 27.5. REPLACED THE SEAT TRACK FROM EXISTING SPLICES BS 625 TO 745 IAW SRM 53-00- 52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK SEAT TRACK CRACKED AT BS 635, RBL 47.5. REPLACED THE SEAT TRACK FROM EXISTING SPLICES BS 625 TO 665 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
COCKPIT RT OBSERVER`S SEAT FLOOR SUPPORT CUTOUT WEB FOUND CRACKED AT BS 365, RBL 3.5. THE WEB WAS REPAIRED IAW SRM 53-10-51-2R, FIG 202, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT XOS 906 WAS FOUND CRACKED. THE DOUBLER WAS REMOVED AND AND A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB3954, REV K. INSTALLED THE DOUBLER IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LEADING EDGE COMPARTMENT DOUBLER WAS FOUND CRACKED AT XOS 789. THE DOUBLER WAS REMOVED AND REPLACED IAW DRAWING ARB3954, REV K.AND SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LEADING EDGE COMPARTMENT STIFFENER AT XOS 542 WAS FOUND CRACKED. THE STIFFINER WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, DRAWING ARB2918, REV G. AND SRM 51-33-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LEADING EDGE COMPARTMENT XOS 547 PANEL CUTOUT WAS FOUND CRACKED. REPAIRED IAW SRM 51-31-01-06, DRAWING ARB2933, REV AJ, AND SRM 51-35-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 700 WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 668 WAS CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK AFT FLOOR SUPPORT, BS 1887 - 2007, LBL 25 WAS FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01-0G, DWG AGA7078, REV M, AND SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK AFT FLOOR SUPPORT AT BS 1887 - 2007, LBL 57 WAS FOUND CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-31-01-0G, DWG AGA7551, REV G, AND SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK AFT FLOOR SUPPORT BETWEEN BS 1914 - 2007, LBL 22 WAS FOUND CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-31-01-0G, DWG AGA 7088, REV B, AND SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING, LOWER FUEL TANK ACCESS PANEL 538AB CUTOUT FOUND DAMAGED. REPAIRED IAW SRM 57-20-02-2R, FIG 201, REPAIR 5. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
ONE CRACK INDICATION APPROX 1/4 INCH IN LENGTH, FOUND DURING AN X-RAY INSPECTION AT BS 5-123, ON THE LONGERON SPLICE 3R. THE LONGERON SPLICE WAS REMOVED AND REPLACED IAW SRM 51-33-01-0G, DWG A5A7111, REV C, AND SRM 51-33-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
DURING A PREFLIGHT CHECK OF EMERGENCY LIGHTS, EMERGENCY LIGHT BATTERY 1 LOW MESSAGE DISPLAYED.
AFTER DEPARTURE, RECEIVED SLAT DISAGREE AND STICK SHAKER AT 200 FT. AIRCRAFT DID NOT ROLL, MAINTAINED LEVEL FLIGHT AND CONTINURED DEPARTURE. RETRACTED FLAPS AND SLATS WITH NO ISSUES. WENT INTO HOLDING FOR ATC WITH SLATS EXTENDED SPEED 210. NO ISSUE IN HOLDING. ON FINAL WITH SLATS EXTENDED, FLAPS 28, SPEED 180KIAS, RECEIVED SLAT DISAGREE, STICK SHAKER AND PERFORMED MISSED APPROACH. RETURENED TO DEPARTURE AND PERFORMED A LANDING WITH NO ISSUES. FOLLOWED FIM 31-71-07-00, PERFORMED PSEU SELF TEST AND TARGET 01 TEST. TEST PASSED. R & R THE NR 4A SLAT POSITION SENSOR AND PSEU TARGET, TESTED OK IAW AMM 27-84-03-4. OK FOR SERVICE.
L1 PRESS TO TEST DOOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED REMOTE PRESSURE INDICATOR ASSEMBLY IAW AMM 25-61-04-4-0. OPS CHECKED OK. GOOD FOR SERVICE.
ON PRE-FLIGHT WITH APU RUNNING SMOKE ENTERED FLIGHT DECK AND ALL AIR CONDITIONING DUCTS. SPARKS WERE SEEN EXITING APU EXHAUST AREA. APU FIRE HANDLE WAS PULLED AND BOTH FIRE BOTTLES WERE DISCHARGED. INSTALLED APU PER W/C 49T1901, APU OPS CHECKED GOOD WITH NO DEFECTS AT THIS TIME.
RIGHT WING OTBD FLAP VANE HORN FITTING-D, FWD HOLE CORROSION. CORROSION FOUND TO EXCEED LIMIT IAW SRM 57-50-02, REPAIR 5, FIGURE 201. EXISTING SLOT: 0.890", LENGTH, 0.625", WIDTH. FINAL SLOT: 0.965", LENGTH, 0.662", WIDTH. MAXIMUM ALLOWABLE: 0.940", LENGTH, 0.670" WIDTH. REPAIR BUSHING, SLOT, FABRICATED BY MACHINING IAW EA 1-5750-T0326035, PART 1, STEP 2A WINGS, FLIGHT SURFACES, EO1-5750-7-5002. BUSHING INSTALLED IAW AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
LT WING OTBD FLAP, INBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEED LIMIT IAW CMM 57-52-04. EXISTING HOLE DIA 1.148", FINAL HOLE DIA 1.162", MAXIMUM ALLOWABLE DIA 1.150". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325946, PART 1, STEP 1-A WINGS-FLIGHT SURFACES EO1-5750-7-5002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
LEFT WING INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE SURFACE CORROSION. CORROSION FOUND EXCEEDED LIMIT AS CMM 57-52-03, EXISTING THICKNESS: 0.260", MATERIAL REMOVED: 0.074", REMAINING THICKNESS: 0.186", MINIMUM ALLOWABLE THICKNESS: 0.205". STRAP REMOVED IAW EA 1-5750-71784E-PT5, STEP 1. NEW REPLACEMENT OTBD STRAP MACHINED IAW EA 1-5750-71784E-PT5 STEP 2 AND INSTALLED IAW STEP 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK FLANGE FOUND CORRODED AT BS 1621- BS 1641, X= 75, INBD. SEAT TRACK REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
1EA FASTENER HOLE FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN BS XORS =683.4 AND XORS =713.6. REPAIR BUSHING CARRIED OUT AT RT WING LOWER SKIN ACCESS DOOR CUTOUT IAW SRM 57-20-02-2R, FIG 201, REPAIR 5, 01 EA, AT HOLE NR 8. INITIAL INSPECTION TO BE CARRIED OUT AT 2000 FC, REPETITIVE INSPECTION AT EVERY 2000 FC IAW SRM 57-20-02-2R, TABLE 201, FIG 202, REPAIR 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
6 EA FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA, XORS =683.4 AND XORS =713.6. REPAIR BUSHING CARRIED OUT AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=683.4 AND STA XORS=713.6 IAW SRM 57-20-02-2R, FIG 201, REPAIR 5, 6 EA, AT HOLES NR 6, 10, 11, 13, 32 AND 33. INITIAL INSPECTION TO BE CARRIED OUT AT 2000 FC, REPETITIVE INSPECTION AT EVERY 2000 FC IAW SRM 57-20-02-2R, TABLE 201, FIG 202 REPAIR 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO SEAT TRACK FLANGE FOUND CORRODED AT BS 1601- BS 1621, X= 8.0, OTBD. SEAT TRACK REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA 0.594", FINAL HOLE DIA 0.705", MAXIMUM ALLOWABLE DIA: 0.667". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325943, PART 1, STEP 1B WINGS-FLIGHT SURFACES EO1-5750-7-5002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER MOUNT OTBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE, DIA: 0.582" FINAL HOLE, DIA: 0.598" MAXIMUM ALLOWABLE DIA: 0.584". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325889, PT1 STEP 1A, WINGS-FLT SURFACES-EO 1-5750-7-5002, LT WING-OTBD FLAP, OTBD HINGE ASSY WING SIDE CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.324" FINAL HOLE DIA: 0.406" MAXIMUM ALLOWABLE DIA: 0.391". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325889, PT1, STEP 1B. WINGS, FLT SURFACES-EO 1-5750-7-5002, LT WING-OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE, DIA: 0.579" FINAL HOLE DIA: 0.598" MAXIMUM ALLOWABLE DIA: 0.584". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325889 PT1 STEP 1A. WINGS, FLT SURFACES-EO 1-5750-7-5002 , LT WING-OTBD FLAP OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
LEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, PIVOT HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDING LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 2.306", FINAL HOLE DIA: 2.3290", MAXIMUM ALLOWABLE DIA: 2.3135". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325892, PART 1, STEP 1A WINGS, FLIGHT SURFACES-EO1-5750-7-5002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA, 0.325" FINAL HOLE DIA: 0.406" MAXIMUM ALLOWABLE DIA: 0.391". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325889 PT1 STEP 1B WINGS-FLT SURFACES-EO 1-5750-7-5002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
RT WING OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA 0.644", FINAL HOLE DIA 0.713", MAXIMUM ALLOWABLE DIA 0.709". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325890, PART 1, STEP 1A WINGS, FLIGHT SURFACES-EO1-5750-7-5002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
LEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.643", FINAL HOLE DIA: 0.716", MAXIMUM ALLOWABLE DIA: 0.709". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325892, PART 1, STEP 1B WINGS-FLIGHT SURFACES EO1-5750-7-5002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
LT WING INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA 1.251", FINAL HOLE DIA 1.283", MAXIMUM ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED IAW EA 1-5750-71784E, PT5, STEP 4B AND INSTALLED IAW STEP 4E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REF TO WRI 57509184 FOR WORK DETAILS.
LEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA 1.251", FINAL HOLE DIA 1.375", MAXIMUM ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED IAW EA 1-5750-71784E, PT5, STEP 4A AND INSTALLED IAW STEP 4D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REF TO WRI: 57509184 FOR WORK DETAILS.
RIGHT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA 1.253", FINAL HOLE DIA 1.283", MAXIMUM ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED IAW EA 1-5750-71783, C PART, 5 STEP 1A AND INSTALLED IAW STEP 1C AND 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REF TO WRI: 57509183 FOR WORK DETAILS.
RIGHT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE BORE CORROSION. CORROSION FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA 1.286", FINAL HOLE DIA 1.290", MAXIMUM ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED IAW EA 1-5750-71783C, PART 5 AND INSTALLED IAW STEP 1C AND 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
CABIN - MAIN DECK CARGO COMPARTMENT DENTED FRAME AT RT BS 5-53, LONGERON 12R. FRAME REPAIRED IAW SRM 53-00-07-2R, FIG 201, REPAIR 2. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14500 FLT CYCLES AND REPETITIVE INSPECTION AT 9500 FLT CYCLES TO BE CARRIED OUT IAW SRM 53-00-07-2R, TABLE 201, REPAIR 2, INSPECTION METHOD HFEC. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA 1.214", FINAL DIA 1.224", MAX ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325892, PT1 STEP 1C WINGS, FLT SURFACES, EO 1-5750-7-5002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
AGING AIRCRAFT, EXISTING REPAIR ON FRAME AT MAIN DECK CARGO COMPARTMENT, STA 1661, LONGERON L12R. EXISTING REPAIR ON FRAME AT MAIN CARGO COMPARTMENT STA 1661, LONGERON L12R EVALUATED AND FOUND DAMAGED. REPAIR CARRIED OUT AT FRAME AT MAIN CARGO COMPARTMENT, STA 1661, L12R IAW SRM 53-00-07-2R, FIG 201, REPAIR 2. EO 1-5100-7-5001, B6, P1. TITLE: STRUCTURES REPAIR CATALOG, REPAIR ID AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100. TO CARRY OUT INITIAL INSPECTION AT 14,500 FC AND REPETITIVE INSPECTION AS EVERY 9,500 FC IAW SRM 53-00-07-2R, TABLE 201, REPAIR 2. INSPECTION METHOD: HFEC.
CABIN, MAIN DECK CARGO COMPARTMENT L3 DOOR AFT LOWER FUSELAGE JAMB WEB CRACKED AT LT BS 1310 BETWEEN LONGERON 26L-27L. WEB REPAIRED IAW 53-40-15-2R, FIG 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
AGING AIRCRAFT, EXISTING SKIN REPAIR DOUBLER FOUND AT FWD CARGO DOOR CUTOUT FWD JAMB AT STA 895, LONGERON L39R-L41R EXISTING REPAIR AT FWD CARGO DOOR CUTOUT FWD JAMB AT STA 895, L39R-L41R EVALUATED AND FOUND CRACK. REPAIR CARRIED OUT AT FWD CARGO DOOR CUTOUT FWD JAMB AT STA 895, L39R-L41R IAW SRM 53-00-15-2R, FIG 202, REPAIR 8. EO 1-5100-7-5001, B6, PT1, SRM REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14, CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. INITIAL INSPECTION CARRIED OUT AT CURRENT CHECK. REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 6,300 FLT CYCLES IAW ALI 53.10.06.01.
CABIN, MAIN DECK CARGO COMPARTMENT FRAME CHAFED AT RT BS 535, LONGERON 19R. DAMAGED FRAME REPAIRED IAW SRM 53-20-07-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
CABIN, MAIN DECK CARGO COMPARTMENT FRAME CHAFED AT RT BS 535, LONGERON 24R. FRAME REPAIRED IAW SRM 53-20-07-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
CABIN, MAIN DECK CARGO COMPARTMENT L3 DOOR FWD LOWER FUSELAGE JAMB WEB CRACKED AT LT BS 1256 BETWEEN LONGERON 26L-27L. CRACKED WEB REPAIRED IAW 53-40-15-2R, FIG 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LE ANTI-ICE TELESCOPIC DUCT INNER SKIN BEADED AT STATION XOS 464, SURFACE FOUND DAMAGED. REPAIR CARRIED OUT PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
IN CRUISE FLIGHT, 3.5 HOURS INTO FLIGHT HAD HYD 3 FAIL ALERT WITH HYD 3 INDICATING 0.0 QTY.
BEGINNING DESCENT, RECEIVED ENG 2 ANTI-ICE OFF, ALERT WHEN ENG ANTI-ICE SELECTED ON.
SLAT DISAG ON ROTATION ON TAKEOFF. AT SLAT RETRACTION SPEED DURING CLIMB SLAT DISAG EXTINGUISHED. 30 SECONDS LATER SLAT DISAG LIGHT CAME ON. LIGHT STAYED ON UNTIL SLATS EXTENDED FOR LANDING, THEN LIGHT EXTINGUISHED, NORMAL LANDING. TROUBLE SHOT IAW FIM 31-71-07-00 NO FAULT NOTED. CHECKED PSEU FAULT AS LT WING SLAT PROX NR 4B SENSOR. CARRIED OUT WIRING CON & SHORT TO GND CHECK FROM PSEU RACK R5-1036B PINS 53 & 54 TO LT WING SLAT NR 4B PROX SENSOR TERMINAL BLOCK S3-458 PINS 4 & 5 IAW WDM 27-84-01 SHEET 2, PG 5 NO FAULT FOUND. REMOVED & INSTALLED NR 4B SLAT POSITION SENSOR IAW MM 27-84-03-4 & PSEU IAW MM 31-71-01-2. PSEU FUNTIONAL TEST IAW MM 31-71-01-2 ALL TEST PASSED. PERFORMED SLAT POSITION INDICATION TEST IAW MM 27-84-00 TEST PASSED. PERFORMED FCC NR 1 & 2 RT OF SLAT SYS IAW MM 27-80-01-5 ALL TEST PASSED.
CABIN RT STATION 1229, XCW = 105 CTR WING UPPER PANEL FOUND CORROSION. REPAIRED AS PER EA 1-5730-T0309294 PART 1, TITLE: WINGS - PLATES AND SKINS - CENTER WING UPPER SKIN CORROSION REMOVAL BEYOND SRM LIMITS. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 122.
SIX EACH FASTENER HOLES 5, 10, 17, 29, 30 & 31 FOUND CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STATION XORS =690 & XORS=700. LOWER SKIN ACCESS DOOR CUTOUT REPAIRED AS PER SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 55. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122.
FIVE EACH FASTENER HOLES 08, 28, 29, 30 & 31 FOUND CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STATION XORS =690 & XORS=700. SKIN ACCESS DOOR CUTOUT REPAIRED AS PER SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 55. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122.
LEFT WING LE SKIN AT OTBD OF SLAT TRACK 10 AT XOS 667 FOUND CRACKED. REPAIRED IAW SRM 57-40-01 FIGURE 201 REPAIR 9 REVISION 55. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.
LOST CPDLC CONTACT. HAD CPDLC "NO COMM" ATTEMPTED TO LOGON WITH NO RESULTS. SAW ACARS DISPLAYED "NO COMM" AND SATCOM MENU SHOWED "NOT AVAILABLE". AIRTURN BACK TO DEPARTURE. RESET FMC 1 AND FMC 2 CIRCUIT BREAKERS REF 34-63-09-05 AND CYCLED SATCOM CIRCUIT BREAKER. RAN SATCOM FANS ADJUSTMENT AND TESTED IAW AMM 23-26-01-5, TEST PASSED. SATCOM OPERATES NORMALLY.
ON ROLLOUT F/O RT RUDDER PEDAL WENT FULL FORWARD. CAPT SIDE NORMAL, THEN ON TAXI IN CAPT SIDE WENT FULL FORWARD BUT OPPOSITE OF F/O'S. F/O'S LT SIDE FULL FWD/CAPT RT SIDE FWD. ACCESSED AVIONICS COMPT & INSPECTED RUDDER PEDAL TORQUE TUBE. FOUND BROKEN IN HALF ON PILOTS SIDE. ACCOMPLISHED WC EO 9-2720-7-5000, PART 4.
RAISED GEAR HANDLE ALL FOUR GEAR INDICATED UNSAFE "RED" ON ALL PRIMARY AND SECONDARY INDICATIONS. CHECKED GEAR HANDLE AND FOUND TO BE OPERATIONAL BUT SLIDING HANDLE WAS GUMMED UP AND WOULD INTERMITTENTLY SLIDE INTO EITHER UP OR DOWN LOCKING POSITION. REMOVED DISPLAY UNITS NR 3 & NR 4 IAW AMM 31-61-03-2. VACUUMED AND BRUSHED LINT AND CLEANED DIRT FROM GEAR HANDLE ASSY; LUBED SLIDING HANDLE IAW AMM 32-31-00-7. COCKPIT LANDING GEAR POSITION INDICATION GOOD IAW AMM 32-61-00-5. REINSTALLED AND TESTED DISPLAY UNITS 3 & 4 IAW AMM 31-61-03-2. MEM U JACKED ACFT IAW AMM 07-11-00-2. SWUNG GEAR IAW AMM 32-31-00-5; HANDLE OPERATES NORMALLY AND ALL INDICATIONS GOOD. MEM U DOWN JACKED ACFT IAW AMM 07-11-00-2.
MAIN DECK BS 1761 - 1801, X=8.5 , SEAT TRACK FLANGE FOUND CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.
MAIN DECK BS 1877, X= 8.5 , SEAT TRACK FLANGE FOUND WITH CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.
MAIN DECK BS 1801 - 1821, X= 8.5 , SEAT TRACK FLANGE FOUND CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.
MAIN DECK BS 1801- 1821, X=-8.5 , SEAT TRACK FLANGE FOUND CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115
MAIN DECK BS 1761 - 1801, X=-8.5 , SEAT TRACK FLANGE FOUND CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115
MAIN DECK CARGO TRACK AT BS 1880, X=-8.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA.1751 TO STA..1887 , X= -8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.
MAIN DECK CARGO SEAT TRACK AT BS 1581, X=-8.5, FOUND WITH CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA.1571 TO STA..1691 , X= -8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER GMM 6- 2-100 REVISION 115.
MAIN DECK CARGO TRACK AT BS 997, X= 75 , FOUND CROWN CHIPPED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM BS 989 TO 1049 , X=75 AS PER SRM 53-00- 52 FIGURE 201 REPAIR 1 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.
RIGHT WING RIB NR 16 AT FIXED L/E AREA (INBD SIDE) FOUND CRACKED. RIB REMOVED AS PER SRM 51-31-01 REV. 50 AND REPLACED WITH NEW RIB 16 AS PER DWG ARB7565 REV. C REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.
MAIN DECK CARGO TRACK AT BS 1689, X=-8.5 , FOUND WITH CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM BS 1571 TO 1691 , X= -8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50 REFER TO SNRM N00262 FOR WORK DETAILS. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.
FSS DISCHARGE 7L AND 7R TEMP READS 451 ON FSS PANEL BUT NO OTHER FIRE INDICATIONS. FSS PANEL SHOWED TEMP OF 451 DEGREES. EMERGENCY DECLARED, DIVERTED. COMPLIED WITH EA 1-2624-160811A. REACTIVATED MAIN DECK FIRE SUPPRESSION SYS.
L1 "EXIT SIGN" FELL OFF IN FLIGHT. REINSTALLED L1 EXIT SIGN LIGHT COVER IAW SMP.
UPON REMOVAL OF MAIN DECK CARGO FLOOR PANEL NR245BF FOR SEAT TRACK REPAIR ACCESS, SEAT TRACK X=-8 INBD FLANGE AT STA 799 WAS FOUND CORRODED. SPLICE REPAIR CARRIED OUT ON CORRODED SEAT TRACK BETWEEN STATION 745 AND STATION 800 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REV.44. (MAJOR REPAIR)
MAIN DECK CARGO COMPARTMENT CARGO TRACK RBL 8.5 AT STATION 755 FOUND WITH DAMAGED CROWN. SPLICE REPAIR CARRIED OUT ON DAMAGED SEAT TRACK BETWEEN STATION 745 AND STATION 800 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REV. 44. (MAJOR REPAIR).
MAIN DECK CARGO, RT INTERIOR FUSELAGE FRAME STA 1661 L-11R FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 53-00-07, FIGURE 201, REPAIR 2, REVISION 44. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.
LEVEL 1 A-ICE FAIL AFTER TAKEOFF. COMPLIED WITH QRH PROCEDURES. NO CHANGE. RETURNED TO PEN. RELEASED FOR SERVICE IAW MEL: 36-10-01 CATEGORY: C EXPIRATION: 10NOV09 "MEL 36-10-01: PNEUMATIC SYS CONTROLLER NR 2-INOP. OPERATE AIR SYS CONTROL PANEL IN AUTO. " PSC SWAPPED IAW AMM 36-10-02-4. ACFT OK FOR SERVICE. REMOVED AND REPLACED THE PSC2 CONTROLLER WTH R-T-S ALL PASSED AND CHECK O.K FOR SERVICE IAW AMM 36-10-02-4 & 36-10-02-5.
CABIN, RT STA 5-113 TO STA 5-120 X= -8 SEAT TRACK FOUND CORROSION. REPAIRED AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
AFT FUSELAGE COMPARTMENT CROWN CLIP AT APPROX STA 2046 FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.
CABIN, RT STA 735 LONGERON, 12 FRAME FOUND DENT. REPAIRED AS PER SRM 53-30-00 FIG. I VOL I REV 40. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG I VOL I REV 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
RT STA 1531 - STA 1561 X= -8 SEAT TRACK FOUND CORRODED. REPAIRED AS PER SRM 53-70-00 FIG. I REV 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
LT STA 1545 TO STA 1551 X= 8 SEAT TRACK FOUND CORRODED. REPAIRED PER SRM 53-70-00 FIG. I REV 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
CABIN, LT STA 1731 X= 107 SEAT TRACK FOUND CORROSION. SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG. 6 VOL.I REV. 40. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
RT STA 1471 X= -8 SEAT TRACK FOUND CORRODED. REPAIRED AS PER SRM 53-70-00 FIG I VOL I REV 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-10 REV 107.
LT WING NR 16 SLAT TRACK INBD RIB SUPPORT FOUND CRACKED. REMOVED AND REPLACED AS PER DRAWING ARB7565 AND SRM 51-33-01 VOL. II REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.
AFT FUSELAGE COMPARTMENT CROWN CLIP AT STA 2093 FOUND WITH CRACK. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV 107.
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLES C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLE D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLE C. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLE D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLE C. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLE C. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
LT WING INBD FLAP LOWER SURFACE LOWER OUTBD SEGMENT FOUND SEVERAL DENTS AT XIFH 243 TO XIFH 255 EXCEED LIMIT. REPAIRED AS PER SRM 57-10-00 FIG. 3 VOL. I REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.
CABIN, LT STA 1741 LONGERON 12 FRAME FOUND DENT. REPAIRED AS PER SRM 53-30-00 FIG. I VOL. I REV 40. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
CABIN, RT STA 1641 LONGERON 12 FRAME FOUND DENT. REPAIRED AS PER SRM 53-30-00 FIG. I VOL. I REV 40. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES A, B, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II REV. 40. REPAIR BUSHINGS INSTALLED FOR THE 1ST AND 2ND LAYER WEB PER SRM 53-50-00 FIG 10 VOL I REV 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 107.
DURING ILS APPROACH TO SFS, IN LIGHT TO MODERATE PRECIP, AT'S AND AP DISCONNECTED, ALSO HAD IAS COMPARATOR WARNING, W/ 5 TO 15 KTS DIFFERENCE. ALSO LEVEL 2 SEL ELEV FEEL MANUAL, LSAS ALL FAIL AND TWO OR MORE MOMENTARY LEVEL 2 ALERTS OCCURRED. ON GO AROUND, ALL ALERTS BEGAN TO EXTINGUISHED, ATTEMPTED 2ND ILS APPROACH, ALL AS ABOVE RE-OCCURRED AGAIN. CFDS CURRENT FAULTS, NIL. FRONT FACE INSPECTION FOR FAULT BALL ON ALL 3 ADC'S, REVEALED NONE. PER RECOMMENDATION FROM MOCC, ADJUSTMENT TEST PER AMM 34-16-01-5 CARRIED OUT, ALL R-T-S TEST PASSED ON ALL 3 ADC'S, ADDITIONAL VISUAL INSPECTION ON ALL PITOT TUBES, NIL OBSTRUCTION, ACFT OK FOR SVC.
NOSE SKIN LOWER PANEL INSTALLATION, REPAIR OF SKIN DENT AT BS.421.5 BETWEEN X=0 AND X=-21. REFERENCE WRI NR 53-30/5861. LOWER FUSELAGE SKIN AT STA 421.5, BETWEEN X = 0 AND X = -21 CARRIED OUT REPAIR AS PER EA NR1-5330-121688. REPAIR OF SKIN DENT AT BS 421.5 BETWEEN X = 0 AND X = -21. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
UPON LOWER NOSE SKIN OPEN-UP FOUND ADJACENT FRAME AT STA 421.507, X=-20 CRACKED. FRAME AT STA 421.507, X = -21.25 CARRIED OUT REPAIR AS PER FEDEX EA NR 1-5310-123101 PT1, TITLE: FUSELAGE, MAINFRAME BS 421.5 FRAME, X = -21.25 - FLANGE CRACK REPAIR. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
UPON LOWER NOSE SKIN OPEN-UP FOUND ADJACENT INTERCOSTAL AT STA 410 CRACKED. INTERCOSTAL AT STA 410, X = -1.750 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. FABRICATED INTERCOSTAL AS PER DOUGLAS DRAWING ABA8678. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
T/O ROLL NR 4 DU BLANKED, NR 1 FMS DISP "TIMEOUT RESELECT" NR 3 MCDU BLANKED, OCCURRED PRIOR TO V, CONTINUED T/O. AT 180 NM FROM HNL RECEIVED MANY LVL 1 AND LVL 2. ALERTS MOST SIGNIFICANT LVL 1 "BUS AC 1 OFF" AND LVL2 FUEL QTY FAULT", LVL 2 SELECT FADEC ALTN". AUX IRU WENT TO "BATT" AND FAILED 20 MINUTES LATER. NR 1 FMS WENT TO STBY. DUMPED 120K FUEL. RETURNED TO HNL. NR 1 AC BUS REPOWERED ITSELF PRIOR TO APPROACH AND ALL DU CONTINUED TO FLICKER OFF/ON DURING APPROACH. AVIONICS RACK FAN C/B POPPED AND CAC FAN C/B. REMOVED AND REPLACED SENSE RELAY R2-5071, NO JOY. REMOVED AND REPLACED NR 1 GCU. OPS CHECK GOOD. REMOVED AND REPLACED NR 1 APR AND RAN ENGINES. EPCU CURRENT FAULTS SENSE RELAY STILL THERE. REMOVED AND REPLACED RCCB B1-174, OPS CHECK GOOD AND FAULT GONE. RAN ENGINES, CHECK GOOD.
DURING CLIMB FROM FL320 TO FL340 NOTICED A/C DETERIORATION. NR 2 ENG EPR READ .40 LESS THAN NR 1 AND NR 3. N1 READING 20 PERCENT LESS THAN 1 AND 3, N2 20 PERCENT LESS AS WELL. ENG 2 THROTTLE, MOVEMENTS RESULTED IN SLUGGISH RESPONSE W/MAX EPR OUTPUT OF 1.08 AND AT 80 PERCENT N1. SECONDARY ENG PARAMETER READINGS NORMAL FF NR 2 AT 1.00 EPR, N1 76.5, EGT 370, N2 86 WAS 4000LB/HR FL 310 OAT-32 DEG C TARGET EPR WAS 1.27 M.830 IAS 309 KTS TAT +1 DEG C. DIVERTED TO SIN. FOUND 9 FAN BLADES DAMAGED ON ENGINE NR 2. REMOVED AND REPLACED FAN BLADES IN PAIR TOTAL 18EA. REMOVED AND REPLACED FUEL METERING UNIT. REMOVED AND REPLACED NR 2 ENG EEC. 01-2008 REPLACED NR 2 ENGINE.
RIGHT MAIN LANDING GEAR FLIPPER DOOR FOUND CRACKED PASS THROUGH STOP DRILL. 10-30-07 REMOVED AND REPLACED AS PER AMM 32-14-10-4. OPERATION CHECK CARRIED OUT AS PER AMM 32-31 -00-700-803. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
CRACK FOUND DURING HFEC OPEN HOLE INSPECTION ON THE MOST OUTBOARD, LOWER FASTENER HOLE COMMON TO THE ARC4008 AND ARC4009 RIGHT WING OUTBOARD FLAP SUPPORT FITTING. 10-30-07 REMOVED AND REPLACED AS PER MD11 CMM 57-52-04. FLAP ADJUSTMENT TEST CARRIED OUT AS PER AMM 27-50-00-830-805. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
CRACK FOUND DURING HFEC OPEN HOLE INSPECTION ON THE MOST OUTBOARD, LOWER FASTENER HOLE COMMON TO THE ARC4008 AND ARC4009 LEFT OUTBOARD FLAP SUPPORT FITTING. 10-30-07 REMOVED AND REPLACED AS PER MD11 CMM 57-52-04. FLAP ADJUSTMENT TEST CARRIED OUT AS PER AMM 27-50-00-830-805. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
ONE FASTENER HOLE FOUND CRACK AT 3 AND 9 O'CLOCK POSITION AT RIGHT SIDE TRUNNION FITTING LOWER LONGERON. 10-30-07 REMOVED AS PER SRM 51-31-01 VOLUME II. LONGERON FABRICATED AS PER FEDEX EA 1-5310-116497, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AFT FUSELAGE INTERIOR FOUND DOG HOUSE LOCATION WITH FRAME CLIP QUANTITY 01 EACH CRACKED AT STATION Y2069. 10-30-07 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT RIGHT FLOOR SEAT TRACK AT STATION 635, X = -47.5, FOUND CRACKED APPROXIMATELY 3 INCHES. 10-30-07 REPAIRED BY REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT RIGHT FLOOR SEAT TRACK AT STATION 755, X = -8.5, FOUND CRACKED APPROXIMATELY 3 INCHES. 10-30-07 REPAIRED BY REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING LEADING EDGE CAVITY RIB DOUBLER AT STATION XOS 789 (XORS 683) FOUND CRACKED. 10-29-07 REMOVED CRACKED RIB DOUBLER AS PER SRM 51-31-01 VOLUME II AND FABRICATED RIB DOUBLER AS PER DOUGLAS DRAWING ARB3954 AND INSTALLED AT RIGHT HAND WING LEADING EDGE CAVITY AT XOS 789 AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT LEFT FLOOR SEAT TRACK AT STATION 635, X = 27.5 FOUND CRACKED APPROXIMATELY 3 INCHES. 10-30-07 REPAIRED BY REPLACEMENT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT LEFT FLOOR SEAT TRACK AT STATION 635, X = 47.5 FOUND CRACKED APPROXIMATELY 3 INCHES. 10-30-07 REPAIRED BY REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING LEADING EDGE CAVITY AREA RIB ANGLE AT STATION XOS 584 FOUND CRACKED. 10-29-07 REMOVED CRACKED RIB ANGLE (FORMER) AS PER SRM 51-31-01 VOLUME II AND FABRICATED FORMER AS PER DOUGLAS DRAWING ARB2931 AND INSTALLED FORMER AT LEFT HAND WING LEADING EDGE CAVITY AREA AT XOS 584 AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
NOSE LANDING GEAR RT TRUNNION FITTING CRACKED. CARRIED OUT REPAIR AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
LT WING INBOARD FLAP LOWER SURFACE FOUND DENTED. 10-29-07 REPAIR CARRIED OUT AT LT WING INBOARD FLAP LOWER SURFACE AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
DURING CLIMB, SELECTED ALL ANTI-ICE TO ON. GOT IMMEDIATE LEVEL 1 "ENG 2 A-ICE OFF" ALERT COMBINED WITH ENG 2 ANTI-ICE VALVE DISAGREE LIGHT ON ENG 2 A/I SWITCH. DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ANTI-ICE VALVE AND PRESSURE SWITCH, PER MM 30-22-04-4 -2 AND 30-22-00-5 2, OPS CHECK NORMAL. RAN NR 2 ENGINE TO PERFORM OPS CHECK OF ANTI-ICE VALVE PER JRH AND MM 30-22-00-5 2. OPS CHECK NORMAL.
CENTER LANDING GEAR WHEEL WELL, FOUND LEFT HAND TRUNNION ALIGNMENT HOLE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL BORE DIAMETER = 1.502", FINAL BORE DIAMETER = 1.6766", MAXIMUM ALLOWABLE DIAMETER = 1.680" AND FOUND WITHIN LIMIT AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REWORKED ALIGNMENT HOLE REPROTECTED AS PER SRM 51-21-01 VOLUME II. SLEEVE BUSHING FABRICATED AND INSTALLED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER LANDING GEAR WHEEL WELL, FOUND RT TRUNNION MATING SURFACE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL THICKNESS = 2.500", TOP SPOTFACE MATERIAL REMOVED = 0.007" (FWD), TOP SPOTFACE MATERIAL REMOVED = 0.0125" (AFT), LOWER MATING SURFACE MATERIAL REMOVED = 0.0375". FINAL THICKNESS REMAINED = 2.4555" (FWD) AND 2.450" (AFT), MINIMUM ALLOWABLE THICKNESS = 2.430" AND FOUND WITHIN LIMIT AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REWORKED AREA REPROTECTED AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER LANDING GEAR WHEEL WELL, FOUND RIGHT HAND TRUNNION ALIGNMENT PIN HOLE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL HOLE DIAMETER = 1.502", FINAL HOLE DIAMETER = 1.6502", MAXIMUM ALLOWABLE LIMIT DIAMETER = 1.680" AND FOUND WITHIN LIMIT AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REWORKED ALIGNMNET HOLE REPROTECTED AS PER SRM 51-21-01 VOLUME II. REPAIR SLEEVE BUSHING FABRICATED AND INSTALLED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER LANDING GEAR WHEEL WELL, FOUND RIGHT HAND TRUNNION AFT MOUNTING HOLE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL HOLE DIAMETER = 1.280", FINAL HOLE DIAMETER = 1.3776", MAXIMUM ALLOWABLE DIAMETER = 1.385" AND FOUND WITHIN LIMIT AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REWORKED MOUNTING HOLE REPROTECTED AS PER SRM 51-21-01 VOLUME II. REPAIR BUSHING FABRICATED AND INSTALLED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER LANDING GEAR WHEEL WELL, FOUND RIGHT HAND TRUNNION FORWARD MOUNTING HOLE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL HOLE DIAMETER = 1.280", REWORKED HOLE DIAMETER = 1.3768", MAXIMUM ALLOWABLE DIAMETER = 1.385" AND FOUND WITHIN LIMIT AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REWORKED FORWARD MOUNTING HOLE REPROTECTED AS PER SRM 51-21-01 VOLUME II. REPAIR BUSHING FABRICATED AND INSTALLED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER LANDING GEAR WHEEL WELL, FOUND LEFT HAND TRUNNION MATING SURFACE CORRODED. REWORKED AS PER FEDEX E.A. 1-5340-99703, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER LANDING GEAR WHEEL WELL, FOUND LEFT HAND TRUNNION AFT MOUNT HOLE CORRODED. TRUNNION REWORKED AS PER FEDEX EA 1-5340-99703, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER LANDING GEAR WHEEL WELL, FOUND LEFT HAND TRUNNION FORWARD HOLE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL BORE DIAMETER = 1.281", FINAL BORE DIAMETER = 1.3685", MAXIMUM BORE DIAMETER = 1.385" AND FOUND WITHIN LIMIT AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REWORKED FORWARD HOLE REPROTECTED AS PER SRM 51-21-01 VOLUME II. REPAIR BUSHING FABRICATED AND INSTALLED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
M/D CARGO SEAT TRACK (STA 1059, LT X=47.5) FOUND EDGE DAMAGED. TRIMMED OUT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. NEW SEAT TRACK AND SPLICE REWORKED AND INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
CARGO SEAT TRACK (STA 1059, LT X=47.5) FOUND EDGE DAMAGED. CRACKED BEADED DOUBLER ON LT WING FIXED LEADING EDGE BETWEEN STA XOS 629 REPAIRED AS PER FEDEX EA 1-5730-99698.
RIGHT WING FIXED LEADING EDGE ANTI ICE TELESCOPING DUCT CUTOUT INBOARD AND OUTBOARD CORNER FOUND CRACKED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-99697.
LEFT WING FIXED LEADING EDGE ANTI ICE TELESCOPING DUCT CUTOUT INBOARD AND OUTBOARD CORNER FOUND CRACKED. CRACKED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-99696. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
LT WING FIXED LEADING EDGE DOUBLER BETWEEN STA XOS 625 AND STA 629 FOUND CRACKED. REPAIRED AS PER FEDEX EA 1-5730-99698. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
HFEC INSPECTION FOUND CRACK ON RIGHT WING OUTBOARD END WING STRINGER S-11R AT XORS 704. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
HFEC INSPECTION FOUND CRACK ON LEFT WING TANK AT THE END OF STRINGER 49. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
HFEC INSPECTION FOUND CRACK ON RIGHT WING TANK AT THE END OF STRINGER 49. REPAIR CARRIED OUT AT RH WING TANK END OF STRINGER 49 CRACKED AREA AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
HFEC INSPECTION FOUND CRACK ON LEFT WING TANK AT THE END OF STRINGER 10 XORS 760. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
HFEC INSPECTION FOUND CRACK ON LEFT WING TANK AT THE END OF STRINGER 13 XORS 577. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
HFEC INSPECTION FOUND CRACK ON RIGHT WING OUTBOARD END UPPER WING STRINGER S-14R AT XORS 521. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
RIGHT WING I/B FLAP O/B SEGMENT LOWER SURFACE FOUND DENTS. REPAIRED AS PER SRM 57 -10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
BARREL NUT BORE NR 34R CORROSION REMOVAL FOUND EXCEEDED LIMITS. CORROSION REMOVED AND REPAIRED PER FEDEX EA 1-5510-81726.
BARREL NUT BORE NR 1R CORROSION REMOVAL FOUND EXCEEDED LIMITS. CORROSION REMOVED AND REPAIRED PER FEDEX EA 1-5510-81726
BARREL NUT BORE NR 3L CORROSION REMOVAL FOUND EXCEEDED LIMITS. REMOVED AND REPAIRED PER FEDEX EA 1-5510-81726,
BARREL NUT BORE NR 15R CORROSION REMOVAL FOUND EXCEEDED LIMITS. CORROSION REMOVED AND REPAIRED PER FEDEX EA 1-5510-81726.
BARREL NUT BORE NR 26L CORROSION REMOVAL FOUND EXCEEDED LIMITS. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II.
BARREL NUT BORE NR 14R CORROSION REMOVAL FOUND EXCEEDED LIMITS. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II.
RIGHT HAND WING, OUTBOARD FLAP STOP FITTING FOUND CRACKED. STOP FITTING REMOVED AND REPLACED PER DRAWING 4125 AND SRM 51-33-01 VOLUME II.
BARREL NUT BORE NR 25L CORROSION REMOVAL FOUND EXCEEDED LIMITS. CORROSION REMOVED AND REPAIRED PER FEDEX EA# 1-5510-81726.
BARREL NUT BORE NR 30R CORROSION REMOVAL FOUND EXCEEDED LIMITS. CORROSION REMOVED AND REPAIRED PER FEDEX EA 1-5510-81726.
MAIN DECK - DENT MARKS AT RIGHT HAND FRAME AT STA Y= 1681 LONGERON 12. LONGERON 12 REPAIRED PER SRM 53-30-00 VOLUME I, FIGURE 1.
DENT MARK FOUND AT RIGHT HAND FRAME STA Y= 1641 LONGERON 12. LONGERON 12 REPAIRED PER SRM 53-30-00 VOLUME I, FIGURE 1.
DENT MARKS FOUND AT LEFT HAND FRAME STA Y= 1681 LONGERON 14. LONGERON 14 REPAIRED PER SRM 53-30-00 VOLUME I, FIGURE 1.
SEAT TRACK CROWN AREA AT APPROXIMATE STA Y= 1701, X= 27.5 FOUND WORN. SMOOTHENED, MATERIAL REMOVED= 0.006", ORIGINAL THICKNESS= 0.414", REMAINING THICKNESS= 0.408" WITHIN PER SRM 53-10-00 VOLUME I, FIGURE 3.
MAIN DECK - SEAT TRACK CROWN AREA AT APPROXIMATE STA Y= 715, X= 47.5 FOUND WORN. MAIN DECK - SEAT TRACK CROWN AREA AT APPROXIMATE STA Y= 715, X= 47.5 REPAIR PARTS FABRICATED AND INSTALLED AS PER SRM 53-70-00 VOLUME I, FIGURE 1.
MAIN DECK - LEFT HAND SIDE FRAME G-NET ATTACHED YOKE ASSEMBLY AT STA Y=535 TOP AND BOTTOM REPAIR ANGLE FOUND WITH CHAFED MARK. MAIN DECK - LEFT HAND SIDE FRAME G-NET ATTACHED YOKE ASSEMBLY, CHAFED EXISTING REPAIR ANGLE AT STA Y=535, REMOVED PER SRM 51-31-01 VOLUME II. NEW REPAIR ANGLE FABRICATED AND INSTALLED PER FEDEX DRAWING SRM-53-503.
MAIN DECK - RIGHT HAND SIDE FRAME G-NET ATTACHED YOKE ASSEMBLY AT STA Y=535 TOP AND BOTTOM PART FOUND WITH CHAFED MARK. MAIN DECK - RIGHT HAND SIDE FRAME G-NET ATTACHED YOKE ASSEMBLY AT STA Y=535, CHAFED MARK REMOVED PER SRM 53-00-01 VOLUME I, FIGURE 3. MATERIAL REMOVED= 0.005; ORIGINAL MATERIAL THICKNESS= 0.140 INCH, REMAINING MATERIAL THICKNESS= 0.135 INCH. ALLOWABLE LIMIT= 0.20T.
LEFT HAND WING, OUTBOARD FLAP STOP FITTING FOUND CRACKED. REMOVED AND REPLACED PER DRAWING ARC4102 AND SRM 51-33-01 VOLUME II.
MAIN DECK, SEAT TRACK CROWN AREA AT APPROXIMATE STA Y= 1092 TO Y= 1095, X= -47.5 FOUND WORN. SEAT TRACK REMOVED FROM EXISTING SPLICE AT STA Y= 1129 AND CUT AT Y= 1159, X= -47.5 PER SRM 53-70-00 VOLUME I, FIGURE 1. NEW SEAT TRACK AND REPAIR PARTS FABRICATED AND INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1.
MAIN DECK - SEAT TRACK CROWN AREA AT APPROXIMATE STA Y= 1049, X= -8.5 FOUND WORN. SEAT TRACK CUT AND REMOVED FROM EXISTING SPLICE AT STA Y= 1069 AND Y= 1129, X= -8.5 PER SRM 53-70-00 VOLUME I, FIGURE 1. NEW SET TRACK AND REPAIR PARTS FABRICATED AND INSTALLED PER PER SRM 53-70-00 VOLUME I, FIGURE 1.
MAIN DECK, SEAT TRACK CROWN AREA AT APPROXIMATE STA Y= 1238 TO Y= 1286, X= -47.5 FOUND WORN. CUT AND REMOVED PER SRM 53-70-00 VOLUME I, FIGURE 1. NEW SEAT TRACK AND REPAIR PARTS FABRICATED AND INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1.
MAIN DECK - SEAT TRACK CROWN AREA AT APPROXIMATE STA Y= 1304, X= - 75.5 FOUND WORN. CUT AND REMOVED PER SRM 53-70-00 VOLUME I, FIGURE 1. NEW SEAT TRACK AND REPAIR PARTS FABRICATED AND INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1.
ON TAKEOFF, POSSIBLE LIGHTING STRIKE. SHORTLY AFTER RECEIVED (EPGS FAULT) AND (EMERG PWR ON) ALERTS. ALL BUSSES POWERED, ALL GENERATORS OUTPUT NORMAL. REFD QRH AT SAME TIME CAPT'S NO DEFECTS DISPLAYED (MAP FAIL ALERT. SELECTED CAPT ON FMS2 AND CONTINUED ON (OPERATION WITH A SINGLE FMS) IAW QRH. RECEIVED BUSS L EMERGY AC OFF) ALERT SELECTED (EMERG PWR OFF) AND REGAINED FLIGHT DISPLAY DATA. DEVERTED TO KPDX AND DECLARED AN EMERGENCY PERFORMED LIGHTING STRIKE INSPECTION IAW MM 05-53-01-6. NO DEFECTS NOTED. REMOVED AND REPLACED LT EMERGENCY SENCE RELAY AND RESET EPGS FAULTS IAW 24-20-00.FIG 101 AND PERFORMED RTS OF EPCU. TEST PASSED A/C OK FOR SERVICE.
DURING CLIMBOUT IN VMC NR 2 ENG (LOUD NOISE) FROM TAIL AREA. NEXT HIGH EGT (RED) AND VIBRATION. REF QRH SHUT NR 2 ENG DOWN. LANDED RPLL. CREW DEBRIEF AT CLIMBOUT 19,000 FT ENCOUNTERED LOUD NOISE FROM TAIL AREA AND VIBRATION, PERFORMED WALK-AROUND INSPECTION ON TAIL AREA NO DAMAGED FOUND EXTERNALLY. ON EAD NR 2 ENG AMBER 662 DEG CELSIUS. MX UPON INSPECTION OF THE EXHAUST FOUND METAL IN THE TAILPIPE. POWERPLANT ENGINEER TREVOR STEDKE HAS APPROVED THIS ENGINE FOR CHANGE..
MAINDECK - SEAT TRACK AT STA 1701, LBL 47 FOUND WORN. MAINDECK - SEAT TRACK AREA SMOOTHEN BY HAND CLEAN AS PER SRM 51-21- 01 VOL. 2 FOUND WITH IN LIMIT AS PER SRM 53-70-00 VOL. 1.
LT WING O/B FLAP VANE STOP NOSE RIB SUPPORT ISLAND CRACKED.
LT WING: O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR I/B LUG HOLE CORRODED. WORK ACCOMPLISHED AS PER FEDEX EA 1-5740-71779. WINGS - LEFT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.
RT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) O/B PIVOT LUG HOLE CORRODED.
RT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) I/B PIVOT LUG HOLE CORRODED.
RT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) I/B PIVOT LUG O/B SIDE SURFACE CORRODED.
LT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) I/B ACTUATOR LUG HOLE CORRODED.
LT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) ACTUATOR MOUNT O/B LUG HOLE CORRODED.
LT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT POINT I/B LUG HOLE CORRODED.
RT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) O/B ACTUATOR LUG HOLE CORRODED.
RT WING I/B FLAP I/B DRIVE ARM ATTACHMENT BORE (FLAP SIDE) CORRODED.
LT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) PIVOT POINT I/B LUG I/B SIDE SURFACE CORRODED.
LT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) PIVOT POINT I/B LUG O/B SIDE SURFACE CORRODED.
LT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) PIVOT POINT I/B LUG CORRODED.
LT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) ACTUATOR MOUNT O/B LUG CORRODED.
LT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) ACTUATOR MOUNT I/B LUG CORRODED.
LT WING - I/B FLAP O/B HINGE PIVOT LUG HOLE CORRODED. WORK ACCOMPLISHED AS PER FEDEX EA 1-5750-71784, TITLE - WINGS - LEFT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED.
LT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT POINT I/B LUG O/B SIDE SURFACE CORRODED.
LT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT POINT O/B LUG HOLE CORRODED.
RT WING - I/B FLAP O/B HINGE PIVOT I/B LUG HOLE CORRODED. WORK ACCOMPLISHED AS PER FEDEX EA 1-5750-71783, TITLE - WINGS - RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED.
RT WING - I/B FLAP O/B HINGE PIVOT O/B LUG I/B SIDE SURFACE CORRODED. WORK ACCOMPLISHED AS PER FEDEX EA 1-5750-71783. WINGS - RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED.
RT WING - I/B FLAP O/B HINGE PIVOT O/B LUG HOLE CORRODED. WORK ACCOMPLISHED AS PER FEDEX EA 1-5750-71783, TITLE - WINGS - RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED.
RT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) I/B ACTUATOR LUG HOLE CORRODED.
RT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) I/B PIVOT LUG O/B SIDE SURFACE CORRODED.
RT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) O/B PIVOT LUG HOLE CORRODED.
RT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) I/B PIVOT LUG HOLE CORRODED.
MAIN DECK - SEAT TRACK AT STA 755, LBL 8 FOUND CROWN AREA DAMAGED. CORRECTIVE ACTION : SNRM N0379 : MAIN DECK - SEAT TRACK AT STA 755 CARRIED OUT REPAIR IAW SRM 53-70-00 VOL. 1.
MAIN DECK - SEAT TRACK AT STA 1169 AND 1205, RBL 47 FOUND CROWN AREA DAMAGED. CORRECTIVE ACTION : SNRM N0375 : MAIN DECK - SEAT TRACK AT STA 1169 AND 1205 CARRIED OUT REPAIR IAW SRM 53-70-00 VOL. 1.
MAIN DECK - SEAT TRACK AT STA 755, LBL 47 FOUND CROWN AREA WORN. DAMAGE SEAT TRACK AT STA 755, LBL 47 REMOVED & REPLACED WITH NEW SEAT TRACK AT STA 765 - 800 LBL AS PER SRM 53-70-00 VOL. 1.
LT WING I/B FLAP O/B HINGE PIVOT I/B LUG HOLE CORRODED. WORK ACCOMPLISHED AS PER FEDEX EA 1-5750-71784.
LT WING I/B FLAP I/B DRIVE ARM ATTACHMENT BORE (FLAP SIDE) CORRODED.
LT WING O/B FLAP O/B AFT HINGE (FLAP SIDE) PIVOT POINT O/B LUG CORRODED.
AFTER GEAR RETRACTION DURING CLIMB OUT OF NRT, GOT LVL 1 TIRE PRESS LO ALERT AND OBSERVED NR 1 MAIN LANDING GEAR LOOSING PRESSURE UNTILL TIRE FAIL ALERT ILLUMINATED. DIVERED TO TPE AND LANDING UNEVENTFULY WITY O PSI IN NR 1 MAIN LANDING GEAR. REMOVED AND REPLACED NR 1 AND NR 2 MAIN TIRE ASSY IAW MM 32-41-01-4. TIRE PRESSURE SERVICED AND LEAK CHECK PASSED. INSP GEAR STRUT, BRAKE ASSY, AND OTHER TIRE ASSY, ALL CONDITIONS NORMAL. OK FOR CONTINUE SERVICE.
TWO WIRES FOUND BURNT & BROKEN ABOVE AVIONICS RACK IN CAC. REMOVED AND REPLACED WIRES PER C901-836-16C. OPS CHECK BOOST PUMP CARRIED OUT AS PER WC E1-2821-7-5000-03 PART 3 & 4.
DURING CLIMBOUT REC'D LEVEL 3 NR 2 ENG ANTI-ICE DUCT ALERT, SHUTDOWN ENG. R&R RELAYS R2-5229 & R2-5527. R&R NR 2 ENG MANIFOLD FAILURE SENSING COMPONENTS. R&R ANTI-ICE & REGULATING VALVE PER MM 30-22-04.
SNRM N 202 MAIN DECK CARGO COMPT SEAT TRACK AT BS 635, RH X=8.5 FND CRACKED APPROX 4" LONG. R&R SEAT TRACK PER SRM 53-70-00, VOL I.
RT WING LEAD/EDGE PNEU DUCT BLANKET FOUND WITH BURN (CHARRED) MARK, JUST AFT NR 3 ENGINE FIRE BOTTLES. REMOVED AND REPLACED BLANKET.
SNRM N 201 MAIN DECK CARGO COMPT SEAT TRACK AT BS 635 RH X=8.5 FND CRACKED APPROX 4" LONG. ** S/D ** R&R SEAT TRACK PER SRM 53-70-00 VOL I.
ON GEAR RETRACTION RT MG IND SHOW RED CONFIG PAGE SHOW RED ALSO. FOLLOW CKLIST RECYCLED GEAR, NO HELP. DOWN IND, ALL NML.
ON DESCENT GOT A STRONG ELECTRICAL ODOR, NO ALERTS WERE DISPLAY. PERFORMED BATTERY CHARGING TEST PER AMM 24-34-03-5. AC OK FOR SERVICE.
NR 3 ENGINE HIGH PRESSURE FRONT CASE ATTACHMENT BOLT AT 9 O CLOCK (1 OFF) AND 3 O CLOCK (2 OFF) SHEARED OFF. *S/D* REMOVED AND REPLACED PER MM 70-10-03.
UPON GEAR EXT HAD 4 RED LIGHTS ON MG PNL. RECYCLED GEAR AND SAME RESULTS.
UPON GEAR EXT HAD 4 RED LIGHTS ON MG PNL. RECYCLED GEAR AND SAME RESULTS. CLEANED AND LUBED GEAR HANDLE PER SMP PER MM 32-31-00-5.
99-101 - GEAR LWR AT 2300 ABOVE GROUND LEVEL. ALL GEAR UNSAFE POS. REMOVED AND REPLACED LANDING GEAR POSITION SWITCH PER MM 32-61-04-4. OPS CK NORM.