N574FE
Registered owner: FEDERAL EXPRESS CORP, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| FEDERAL EXPRESS CORP | Operator | 2010-09-18 – 2010-09-18 | Operator named in NTSB report |
| FEDERAL EXPRESS CORPORATION (FDEA) | Operator | 2010-09-18 – 2010-09-18 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
NR 3 ENGINE PYLON AFT BULKHEAD LUG BORE HOLE FOUND WITH CORROSION AFTER SPHERICAL BEARING REMOVED.
NR 1 ENGINE PYLON AFT BULKHEAD LUG BORE HOLE FOUND WITH EXISTING DAMAGE AND CORROSION AFTER SPHERICAL BEARING REMOVED.
TAIL ENGINE INTAKE DUCT LEADING EDGE FOUND MULTIPLE CRACKS. #2 ENGINE NOSE COWL REMOVED AND REPLACED AS PER AMM 54-22-01-04, CARRIED OUT NOSE COWL ANTI-ICE SYSTEM FUNCTIONAL TEST AS PER AMM 30-22-00-700-804, FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. COMPLIED EA NO. 1-5451-T0385073P1 TITLE: PYLON STRUCTURE - TAIL PYLON/STRUT - NO 2 ENGINE INLET LEDIING EDGE ASSY REWORK PER DRAWING -MPN RE-IDENTIFICATION.
VERTICAL STABILIZER CENTER SPAR UPON TRIM OUT OF STIFFENER FOUND CORROSION AT STATION 2122 X= -18.65 5 O'CLOCK AREA (REFERENCE SPECIAL/NONROUTINE MAINTENANCE FORM N00474). CORROSION ON STIFFENER AT EMPENNAGE VERTICAL STABILIZER REAR CENTER SPAR AT BS 2122 X= -18.65 5 O'CLOCK AREA EVALUATED AND FOUND EXFOLIATION CORROSION OUT OF LIMITS AS PER MD-11 SRM 55-00-00-2R FIGURE 202 REPAIR GENERAL. CORRODED STIFFENER AT EMPENNAGE VERTICAL STABILIZER REAR CENTER SPAR AT STATION 2122 X= -18.65 5 O'CLOCK AREA REPAIRED AS PER EA# 1-5530-T0385238 P1 TITLE: STABILIZERS - VERTICAL STABILIZER - LOWER VERTICAL STABILIZER INLET DUCT SKIN INSTL- STIFFENER CRACK REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
VERTICAL STABILIZER REAR CENTER SPAR STIFFENER CRACKED AT STATION 2122 5 O' CLOCK AREA. CRACKED STIFFENER AT EMPENNAGE VERTICAL STABILIZER REAR CENTER SPAR AT STATION 2122 5 O' CLOCK AREA REPAIRED AS PER EA# 1-5530-T0385238 P1 TITLE: STABILIZERS - VERTICAL STABILIZER - LOWER VERTICAL STABILIZER INLET DUCT SKIN INSTLN- STIFFENER CRACK REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
UPON REMOVAL OF R3 DOOR UPPER FORWARD DOOR BEAM FOUND WITH CRACK APPROXIMATELY 1.0". AT R3 DOOR, CRACKED UPPER FORWARD DOOR BEAM REMOVED AND REPLACED AS PER MD-11 SRM 51-35-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRY OUT ON THE FUSELAGE SKIN EDGE AT THE SECOND COAX PENETRATION HOLES OF INMARSAT SATCOM, BETWEEN STATION 939 AND STATION 959, FOUND CRACK INDICATION ON THE EDGE OF THE SKIN. CRACK ON THE FUSELAGE SKIN EDGE AT THE SECOND COAX PENETRATION HOLES OF INMARST SATCOM, BETWEEN STATION 939 AND STATION 959 REPAIRED AS PER EA# 1-5330-T0385062 P1 TITLE: FUSELAGE - PLATES & SKINS -SKIN PANEL CUTOUT C/T AREO - I SATCOM ANTENNA INSTALLATION- CRACK REPAIR BETWEEN STA939.00 - STA 959.00 AND LONGERON 1L -1R* THIS EA DEVIATES FROM EO 1-2328-E0365946.REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LOWER CENTER CARGO BAY BILGE AREA LONGERON 52 EXISTING REPAIR SPLICE FITTING FOUND WITH CORROSION AT BS 1691. CORROSION ON LONGERON 52, BS 1701 AND EXISTING REPAIR SPLICE FITTING AT BS 1691, LONGERON-52 AT LOWER CENTER CARGO COMPARTMENT BILGE AREA EVALUATED & FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-05-2R, REPAIR 1 FIGURE 203. CORRODED LONGERON 52, BS 1701 AND EXISTING REPAIR SPLICE FITTING STATION 1691 REPAIRED IAW SRM 53-00-05-2R, REPAIR 1 FIGURE 202. CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM N00586 FOR WORK DETAILS.
LOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 50RIGHT EXISTING REPAIR SPLICE FITTING FOUND WITH CORROSION AT STATION 1691. CORROSION ON LONGERON 50RIGHT STATION 1701 AND SPLICE FITTING AT STATION 1691, LONGERON - 50RIGHT AT LOWER CENTER CARGO COMPARTMENT BILGE AREA EVALUATED AND FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-05-2R, REPAIR 1 FIGURE 203. CORRODED LONGERON 50RIGHT STATION 1701 AND SPLICE FITTING STATION 1691 REPAIRED AS PER MD-11 SRM 53-00-05-2R, REPAIR 1 FIGURE 202. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2- 100. REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00585 FOR WORK DETATILS.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-06, X = - 47.5" CROWN FOUND WORN. SEAT TRACK STATION 5-06, 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 5-63 TO EXISTNG SPLICE STATION 1531/5-0, X = - 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND SIDE OVERWING FLOORBEAM UPPER FLANGE AT STATION Y = 1275.25. X = - 104.25 FOUND CRACK INDICATION APPROX X 0.8". CABIN - CRACK AT RIGHT HAND OVERWING FLOOR BEAM UPPER FLANGE STATION Y = 1275.25, X= - 104.25 REPAIR CARRIED OUT AS PER E.A. # 1-5310-T0385309 P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND AIR-CONDITION COMPARTMENT AFT BULKHEAD APPROXIMATE STATION 595 LONGERON 46LEFT X= 42, DOUBLER FOUND CRACKED. CRACKED DOUBLER AT LEFT HAND AIR-CONDITION COMPARTMENT AFT BULKHEAD APPROXIMATE STATION 595 LONGERON 46LEFT X= 42 AREA REPAIRED AS PER EA# 1-5310-T0385104 P1 TITLE: FUSELAGE - MAINFRAME - STA 595 AFT PRESSURE BULKHEAD - CRACK FOUND ON NCA6244-3 DOUBLER LAYER AT X = 42, ADJACENT TO SIDE LOAD FITTING AND EA# 1-0700-T0385102 PART 1 AND PART 2 TITLE: JACKING - JACKING AND SHORING - STA 595 AFT PRESSURE BULKHEAD WEB CRACK REPAIR - JACK AND SHORE REQUIREMENTS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CAC COMPARTMENT APPROXIMATE BS 1159, LONGERON 47LT SPLICE, SUSPECT CRACK. CRACKED SPLICE AT BS 1159 TO BS 1129/6-100, L47L REMOVED IAW SRM 51-31-01-0G. SPLICE FABRICATED IAW DRAWING A6A7115 REVISION J. FABRICATED SPLICE INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
CAC COMPARTMENT APPROXIMATE BS 1159, LONGERON 46LEFT, SPLICE SUSPECT CRACK. CRACKED SPLICE AT BS 1159 TO STATION 1129/6-100, LONGERON 46L REMOVED IAW SRM 51-31-01-0G. SPLICE FABRICATED IAW DRAWING A6A7115 REVISION J. FABRICATED SPLICE INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LOWER CENTER CARGO COMPARTMENT BILGE AREA AFTER REMOVAL OF LONGERON SPLICE FITTING FOUND LONGERON 52 FASTENER HOLE ELONGATED AT STATION 1691. DAMAGED LONGERON 52 SECTION STATION 1691 AT LOWER CENTER CARGO BILGE AREA REPAIRED AS PER MD-11 SRM 53-00-0-2R, REPAIR 1 FIGURE 201 AND MD-11 SRM 53-00-05-2R, REPAIR 1 FIGURE 202. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
FUSELAGE: RAMP REPORTED DENT 24 INCH FORWARD OF BULK CARGO DOOR AT AFT FUSELAGE ON SKIN BETWEEN STATION 1887 - STATION 1902 LONGERON 40LEFT - LONGERON 41LEFT, REQUIRED TO PERFORM TERMINATING REPAIR, (REFERANCE: WRI: 53304011). DENT AT 24 INCH FORWARD OF BULK CARGO DOOR AT AFT FUSELAGE ON SKIN BETWEEN STATION 1887 - STATION 1902 LONGERON 40LEFT - LONGERON 41LEFT AREA REPAIRED AS PER MD-11 SRM 53-00-01-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
UPON REMOVAL OF R3 DOOR AFT DOOR JAMB LOWER WEB BOX CUT OUT FOUND CRACKED AT BS 1310. R3 DOOR AFT DOOR JAMB, CRACK AT BS 1310 LOWER WEB BOX CUTOUT REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 630. X = - 27.5" CROWN FOUND WORN. SEAT TRACK STATION 630, 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 625 TO EXISTING SPLICE STATION 675, 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.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1130. X = 75.25" CROWN FOUND WORN. SEAT TRACK STATION 1130, X = 75.25 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 1168 TO EXISTING SPLICE STATION 6-100/1129, X = 75.25 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10, X = - 8.5" CROWN FOUND WORN. SEAT TRACK STATION 5-10, 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 EXISTING SPLICES STATION 1531/5-0 TO STATION 5-63, X= -8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM N00171 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-33, X = - 8.5" CROWN FOUND WORN. SEAT TRACK STATION 5-33, 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 EXISTING SPLICES STATION 1531/5-0 TO STATION 5-63, 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.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1045. X = - 8.5" CROWN FOUND WORN. SEAT TRACK STATION 1045, 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 STATION 989 TO EXISTING SPLICE STATION 1129/6-0, X = - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SNRM N00181 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1019. X = 8.5" CROWN FOUND WORN. CABIN - AT SEAT TRACK STATION 1019, 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 STATION 989 TO STATION 1069, X = 8.5 IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SNRM N00186 FOR WORK DETAILS, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1045. X = 8.5" CROWN FOUND WORN. CABIN - AT SEAT TRACK STATION 1045, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMITS IAW 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 STATION 1069, 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
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1009. X = - 27.5" CROWN FOUND WORN. CABIN - AT SEAT TRACK STATION 1009, 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 989 TO STATION 1049, 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.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1019. X = - 27.5" CROWN FOUND WORN. CABIN - AT SEAT TRACK STATION 1019, 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 989 TO STATION 1049, 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.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1299. X = 47.5" CROWN FOUND WORN. SEAT TRACK STATION 1299, 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 EXISTING SPLICES STATION 1249 TO STATION 1331, X = 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 5-10. X = 47.5" CROWN FOUND WORN. SEAT TRACK CROWN 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 STATION 5-15, X = 27.5" CROWN FOUND WORN. SEAT TRACK CROWN EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES BS 1531 TO 1531, 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 1481. X = 27.5" CROWN FOUND WORN. SEAT TRACK CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT BS 1471 TO EXISTING SPLICE BS 1531, X=27.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
01 EACH FASTENER HOLE #15 FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS= 683.4 AND STATION XORS= 713.6. REPAIR CARRIED OUT AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS= 683.4 AND STATION XORS= 713.6 01 EACH CRACKED FASTENER HOLE #15 AS PER MD-11 SRM 57-20-02-2R REPAIR 5 FIGURE 201. INITIAL INSPECTION TO BE CARRIED OUT AT 2000 FLIGHT CYCLES AND REPETITIVE INSPECTIONS TO BE CARRIED OUT AT EVERY 2000 FLIGHT CYCLES BY HIGH FREQUENCY EDDY CURRENT AND ULTRASONIC INSPECTION PER MD-11 SRM 57- 20-02-2R FIGURE 202/REPAIR 5 TABLE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1009, X = - 8.5" CROWN FOUND WORN. SEAT TRACK BS 1009, X = - 8.5 CROWN EVALUATED & FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT BS 989 TO EXISTING SPLICE BS 1129/6-0, 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 1199, X = - 8.5" CROWN FOUND WORN. SEAT TRACK STATION 1199, X = - 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT BS 1189 - 1299, 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 1685, X = - 27.5" CROWN FOUND WORN. CABIN - AT SEAT TRACK BS 1685, 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 BS 1671 TO BS 1711, X = - 27.5 IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
DURING ACCOMPLISHING W/C: 57.20.0.1, FOUND CRACK ON UPPER AUXILLIARY TANK LOWER STRINGER 47, ALONG XCW -46.5 (RIGHT SIDE). CRACKED STRINGER S-47 ALONG XCW -46.5 (RIGHT SIDE) ON UPPER AUXILLIARY TANK LOWER AREA REPAIRED AS PER MD-11 SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
DURING ACCOMPLISHING W/C: 57.20.0.1, FOUND CRACK ON UPPER AUXILLIARY TANK LOWER STRINGER 47, ALONG XCW 17 (LEFT SIDE). CRACKED STRINGER S-47 ALONG XCW 17 (LEFT SIDE) ON UPPER AUXILLIARY TANK LOWER AREA REPAIRED AS PER MD-11 SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
DURING ACCOMPLISHING W/C: 57.20.0.1, FOUND CRACK ON UPPER AUXILLIARY TANK LOWER STRINGER 48, ALONG XCW -46.5 (RIGHT SIDE). CRACKED STRINGER S-48 ALONG XCW -46.5 (RIGHT SIDE) ON UPPER AUXILLIARY TANK LOWER AREA REPAIRED AS PER MD-11 SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 51RIGHT STATION 1701 FOUND WITH CORROSION. CORROSION ON LONGERON 51RIGHT, STATION 1701 AT LOWER CENTER CARGO COMPARTMENT BILGE AREA EVALUATED AND FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53-00- 05-2R REPAIR 1 FIGURE 203. CORRODED LONGERON 51RIGHT, STATION 1701 REPAIRED AS PER MD-11 SRM 53-00-05-2R REPAIR 1 FIGURE 201 AND MD-11 SRM 53-00-05-2R REPAIR 1 FIGURE 202. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
DURING HIGH FREQUENCY EDDY CURRENT INSPETION ON THE LEFT HAND NOSE LANDING GEAR TRUNNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGE FITTING SLOT OUT AREA FOUND 01 EACH CRACKS WITH LENGTH APPROXIMATE 0.3" AT STATION 590. REPAIRED IAW EA 1-5310-T0385087 P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-65. X = - 8.5" CROWN FOUND WORN. CABIN - AT SEAT TRACK STATION 6-65, 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 STATION 6-40 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.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1545, X = - 8.5" CROWN FOUND WORN. SEAT TRACK STATION 1545, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT BS 1571 TO EXISTING SPLICE BS 5-123/1531, X= -8.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1601. X = 8.5" CROWN FOUND WORN. CABIN - AT SEAT TRACK STATION 1601, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1611 TO EXISTING SPLICE STATION 1571, 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.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1470. X = 8.5" CROWN FOUND WORN. THE SEAT TRACK CROWN 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 STATION 5-10, X = - 27.5" CROWN FOUND WORN. SEAT TRACK STATION 5-10, 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 5-63 TO EXISTING SPLICE STATION 5-0/1531, 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.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1299. X = - 47.5" CROWN FOUND WORN. SEAT TRACK STATION 1299, 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 EXISTING SPLICES STATION 1249 TO STATION 1331, X = - 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 960. X = 27.5" CROWN FOUND WORN. SEAT TRACK STATION 960, 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 929 TO STATION 969, X = 27.5 AS PER MD-11 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 775, X = - 47.5" CROWN FOUND WORN. SEAT TRACK STATION 775, X = - 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 783 TO EXISTING SPLICE STATION 726, X= - 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1210, X = 8.5" CROWN FOUND WORN. SEAT TRACK STATION 1210, 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 STATION 1229 TO EXISTING SPLICE STATION 1189, 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
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1199, X = 8.5" CROWN FOUND WORN. SEAT TRACK STATION 1199, 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 STATION 1229 TO EXISTING SPLICE STATION 1189, 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.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1305, X = 8.5" CROWN FOUND WORN. SEAT TRACK STATION 1305, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1269 TO EXISTING SPLICE STATION 1331, X = 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SNRM N00245 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1299, X = 8.5" CROWN FOUND WORN. SEAT TRACK STATION 1299, 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 STATION 1269 TO EXISTING SPLICE STATION 1331, 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.
LEFT HAND FRAME STATION 1721 LONGERON 12LT, DENTED. EXISTING REPAIR ANGLE WITH DENT REMOVED IAW SRM 51-33-01-0G AND REPAIR CARRIED OUT IAW SRM 53- 00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSPECTIONS REQUIRED - INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER MD-11 SRM 53-00-07- 2R TABLE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
STATION 1701 LONGERON 12 LEFT, FRAME FOUND WITH DENT. REMOVED AS PER MD-11 SRM 51-33-01-0G AND REPAIR CARRIED OUT AS PER MD-11 SRM 53- 00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYLES TO BE CARRIED OUT AS PER MD-11 SRM 53-00-07-2R TABLE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
STATION 1661 LONGERON 12 LEFT HAND FRAME FOUND WITH DENT. DENT AT LEFT HAND FRAME STATION 1661 LONGERON 12 LEFT REPAIRED AS PER MD-11 SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND AT 9,500 CYCLES REPETITIVE INSPECTION TO BE CARRIED OUT AS PER MD-11 SRM 53-00-07-2R TABLE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
STATION 1761 LONGERON 12 LEFT HAND FRAME FOUND WITH DENTED. DENT AT LEFT HAND FRAME STATION 1761 LONGERON 12 LEFT REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER MD-11 SRM 53-00-07-2R TABLE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING - UPPER SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER FOUND DEEP EXISTING BLEND - OUT AND CORROSION ALONG XORS = 264.00 LEFT HAND WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER STATION XORS = 264.00 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 57-20- 01-1A ALLOWABLE DAMADE 1. REPAIR CARRIED OUT AS PER BOEING REPAIR DRAWING SG11570014 REVISION -. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 52 STATION 1701 FOUND WITH CORROSION. CORROSION ON LONGERON 52, STATION 1701 AND EXISTING REPAIR SPLICE FITTING AT BS 1691, LONGERON-52 AT LOWER CENTER CARGO COMPARTMENT BILGE AREA EVALUATED AND FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-05-2R, REPAIR 1 FIGURE 203. CORRODED LONGERON 52, STATION 1701 AND EXISTING REPAIR SPLICE FITTING STATION 1691 REPAIRED AS PER MD-11 SRM 53-00-05-2R, REPAIR 1 FIGURE 202. REPAIR CLASSIFIED REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
LOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 50RIGHT STATION 1701 FOUND WITH CORROSION. CORROSION ON LONGERON 50RIGHT STATION 1701 AND SPLICE FITTING AT STATION 1691, LONGERON - 50RT AT LOWER CENTER CARGO COMPARTMENT BILGE AREA EVALUATED AND FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-05-2R, REPAIR 1 FIGURE 203. CORRODED LONGERON 50RIGHT STATION 1701 AND SPLICE FITTING STATION 1691 REPAIRED AS PER MD-11 SRM 53-00-05-2R, REPAIR 1 FIGURE 202. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.
NR 1 AIR-CON RAM AIR EXHAUST CUTOUT SUSPECT CRACK AT SKIN LEFT HAND STATION Y= 587. CRACKED SKIN AT NR 1 AIR-CON RAM AIR EXHAUST CUTOUT AT LT BS 587 AREA. REPAIRED IAW SRM 53-20-15-2R REPAIR 3, FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. INITIAL INSPECTION TO BE CARRIED OUT AT 4000 CYCLES AND REPETITIVE INSPECTIONS TO BE CARRIED OUT AT EVERY 4000 CYCLES AS PER MD-11 SRM 53-20- 15-2R TABLE 201/REPAIR 3 REQUIREMENTS. METHOD BY EXTERNAL VISUAL INSPECTION.
NR 1 AIRCON RAM AIR EXHAUST ASSEMBLY CUTOUT PRODUCTION DOUBLER FOUND CRACKED AT LEFT HAND STATION 561.667. CRACKED DOUBLER AT FUSELAGE #1 AIRCON RAM AIR EXHAUST ASSEMBLY CUTOUT AT LEFT HAND STATION 561.667 REMOVED AND REPLACED WITH FABRICATED DOUBLER AS PER MD-11 SRM 51-35-01-0G. DOUBLER FABRICATED AS PER DRAWING ACA3850 REVISION AA. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
EMPENNAGE- AFT ACCESSORY COMPARTMENT AFT BULKHEAD STATION 2164 MOST LOWER STIFFENER FOUND CRACKED. ENPENNAGE - AFT ACCESSORY COMPARTMENT AFT BULKHEAD STATION 2164 MOST LOWER AREA CRACKED STIFFENER REMOVED AND REPLACED WITH REWORKED STIFFENER AS PER MD-11 SRM 51-33-01-0G. STIFFENER REWORKED AS PER DOUGLAS DRAWING AJC 7001 REVISION DT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING DROOPED LEADING EDGE OUTBOARD SIDE EXISTING DOUBLER FOUND CHAFFED AT STATION XDLE 329.775. REPAIR CARRIED OUT AT RIGHT HAND WING DROOPED LEADING EDGE OUTBOARD SIDE STATION XDLE 329.775 AS PER MD-11 SRM 57-40-01-2R REPAIR 15 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 51LEFT STATION 1701 FOUND WITH CORROSION. CORROSION ON LONGERON 51LEFT STATION 1701 AT LOWER CENTER CARGO COMPARTMENT BILGE AREA EVALUATED AND FOUND EXFOLIATED AND OUT OF LIMIT AS PER MD-11 SRM 53-00-05- 2R REPAIR 1 FIGURE 203. CORRODED LONGERON 51LEFT AT STATION 1701 REPAIRED AS PER MD- 11 SRM 53-00-05-2R REPAIR 1 FIGURE 201 AND MD-11 SRM 53-00-05-2R REPIR 1 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING DROOPED LEADING EDGE INBOARD EXISTING DOUBLER FOUND CHAFFED AT STATION XDLE 309.934. REPAIR CARRIED OUT AT RIGHT HAND WING DROOPED LEADING EDGE INBOARD STATION XDLE 309.934 AS PER MD-11 SRM 57-40-01-2R REPAIR 15 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CHECK FOUND LH DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST SWITCH LT INOP. RELEASED FOR SERVICE PER MEL : 25-61-02 REPLACED BATTERIES AT L1 DOOR SLIDE REMOTE PRESS INDICATOR, IAW MD11 AMM 25-61-04-4. OPS CHECK GOOD,
RH WING REAR SPAR UPPER CAP - CORROSION AT STA XORS 783 (AREA MARKED) REPAIRED RIGHT WING REAR SPAR UPPER CAP AT STA XORS 783 REF EA# 1-5710-T0376494 TITLED: WINGS - BASIC WING STRUCTURE - RH WING REAR SPAR UPPER CAP AFT LEG - REWORK. MAJOR REPAIR.
CREW REPORTS R1 DOOR EVAC SLIDE PREMOTE PRESSURE PRESS-TO-TEST INDICATION INOP. OPS CHECK OF R1 DOOR SLIDE REMOTE PRESSURE INDICATOR GOOD IAW AMM 25-61-04-5. ALL OPS NORMAL. NO HISTORY. ACFT OK FOR SERVICE.
R1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN AND WILL NOT STAY IN PLACE. REMOVED AND REPLACED ITEM# 160 REF INCLUDED MANUAL EXIT COVER REPLACED AND OKAY TO CONTINUE.
MAIN CARGO - OVER WING - FLOOR BOARD - HAS DAMAGED & MISSING INSERTS - PANEL #262GF STA 1159, RBL 48. FABRICATED NEW MAIN CARGO DECK FLOOR PANEL 262GF AT STA 1159 PER FEDEX DRAWING SRZ-25-005 AND MD11 SRM 53-00-50-2R PARAGRAPH 4. STEPS E-G.
MAIN CARGO- OVER WING- FLOOR BOARD- HAS DAMAGED AND MISSING INSERTS- PANEL # 271JF STA 1481 TO 5-32 LBL 75-107. FACRICATED NEW MAIN CARGO DECK FLOOR PANEL 271JF PER FEDEX DRAWING SRZ-25-005 AND MD11 SRM 53-00-50-2R PARAGRAPH 4. STEPS E-G.
MAIN CARGO FLOORBOARD 262NF HAS DAMAGED AND MISSING INSERTS. AFTER FURTHER INSPECTION FOUND FLOORBOARD 262DF DELAMINATED, FABRICATED FLOORBOARD REF FEDEX DWG SRZ-25-005 MAJOR REPAIR .
RIGHT WING OUTBOARD OF MAIN LANDING GEAR ABOVE PANEL 641BB HAS CORROSION. AREA IS AROUND INBOARD SIDE OF FASTENER RETAINING RING ABOVE GROSS WEIGHT DOUBLER. PERFORMED STRAP AND FILLER REPAIR OF AREA THAT WAS BLENED REF. EA# 1-5730-T0376395 "MAJOR REPAIR"
R/H WING O/B FLAP I/B HINGE, AREA ABOVE FLAP, FLAP VANE BOTTOM SIDE HAS A DEEP GOUGE WITH SCREW IMBEDDED INSIDE SKIN. REPAIRED R/H WING O/B FLAP I/B HINGE, AREA ABOVE FLAP, FLAP VANE BOTTOM SIDE GOUGE PER SRM 57-50-80-2R, PG.25-26, REPAIR INSTRUTION 4, FIG. 201 SHT.4
MAIN CARGO FLOORBOARD 263QF HAS DAMAGED AND MISSING INSERTS. AFTER FURTHER INSPECTION FOUND FLOORBOARD 263QF DELAMINATED. FABRICATED FLOORBOARD REF FEDEX DWG SRZ-25-005 MAJOR REPAIR.
CAC LOOKING FWD, FOUND CENTER LINE LONGERON 52 BELLFRAME "J" ANGLE WITH HEAVY CORROSION. (MKD) APPROX. FIVE INCHES IN LENGHT STA 1129 (6-70) LOCATION TRIMMED OUT CORRODED SECTION OF J-CHANNEL (P/N ADA0112-11) AND APPLIED FILLER AND DOUBLER REPAIR PER SRM 53-00-00-2R FIG 210
MAIN CARGO FLOORBOARD 262KF HAS DAMAGED MISSING INSERTS. AFTER CLEANING FLOORBOARD FOUND LARGE HOLE. FABRICATED FLOORBOARD 262KF REF FEDEX DWG SRZ-25-005 MAJOR REPAIR.
RH WING, SUPPORT BRACKET P/N ARB0068-2 REQUIRES FABRICATION 0005108155 : SHERWIN, SAMUEL M - 18-OCT-2023 03:57 FABRICATED SUPPORT BRACKET P/N ARB0068-2 REF DAC DWG ARB0068, EA# 1-5710-T0376494 BUY BACK FABRICATED SUPPORT BRACKET P/N ARB0068-2 REF DAC DWG ARB0068, EA# 1-5710-T0376494 TITLED WINGS - BASIC WING STRUCTURE - RH WING REAR SPAR UPPER CAP AFT LEG - REWORK MAJOR REPAIR
FORWARD CARGO COMPARTMENT; STA. 735 RIGHTHAND TUNNEL HAS BURNT INSULATION BLANKET. FABRICATED AND INSTALLED INSULATION BLANKETS REF. AMM 25-85-01-4.
CENTER CARGO COMPARTMENT FLOOR PANEL 183EG HAS SEVERAL DAMAGED INSERTS CENTER CARGO FLOORBOARD 183EG, AFTER FURTHER INSPECTION FOUND FLOORBOARD DELAMINATED. FABRICATED FLOORBOARD REF FEDEX DWG SRZ-25-005 MAJOR REPAIR
RH WING REAR SPAR UPPER CAP - CORROSION AT STA XORS 783. (AREA MARKED) 0005108155 : 28-OCT-2023 02:13 REPAIRED RH WING REAR SPAR UPPER CAP AT STA XORS 783 REF EA# 1-5710-T0376494 TITLED: WINGS - BASIC WING STRUCTURE - RH WING REAR SPAR UPPER CAP AFT LEG - REWORK MAJOR REPAIR
L.H WING O/B FLAP I/B HINGE I/B SIDE, SUPPORT STRUCTURE FOR PANEL 535BR HAS A 3 INCH CRACK. REPLACED BEAM ARC0553-2. REF SRM 51-31-01-0G
#2 ACM BAY AT STA Y=535 X=24 AT NOSE GEAR WEB HAS EXFOLIATION CORROSION. (JUST AFT OF #2 ACM). REMOVED, FABERCATED, INSTALLED NCA5055-33 REINFORCEMENT AND NCA6050-63 STRIP IAW SRM SRM 51-33-01-0G AND DWG NCA6050
CENTER CARGO FLOORBOARD 183GB DAMAGED FABRICATED FLOORBOARD 183GB REF FEDEX DWG SRZ-25-005
MAIN CARGO - OVER WING - FLOOR BOARD - HAS DAMAGED & MISSING INSERTS - PANEL #261KF STA 1305 - STA 1361, RBL 78 AFTER FURTHER INSPECTION FOUND FLOORBOARD 261KF DELAMINATED. FABRICATED FLOORBOARD REF FEDEX DWG SRZ-25-005 MAJOR REPAIR
MAIN CARGO - CTR WING FWD UPPER SKIN PANEL - CORRISION FOUND AT S17, RBL 80-105, DIMENSIONS 13" X 4". COMPLIED WITH EA 958 "WING-PLATES AND SKINS- CENTER WING UPPER FORWARD SKIN - CORROSION REWORK" WORK CARD T 1-5730-T0376479 P1 "MAJOR REPAIR"
MAIN CARGO - OVER WING - FLOOR BOARD - HAS DAMAGED & MISSING INSERTS - PANEL #263DF STA 1321 - STA 1381, LBL 8 MAIN CARGO FLOOR BOARD DELAMINATED (263DF), FABRICATED FLOORBOARD REF FEDEX DWG SRZ-25-005 MAJOR REPAIR
LEFT WING OUTBOARD OF MAIN LANDING GEAR ABOVE PANEL 541BB HAS CORROSION. AREA IS AROUND INBOARD SIDE OF FASTENER RETAINING RING ABOVE GROSS WEIGHT DOUBLER. REMOVED CORROSION ON LH MLG SUPPORT LOWER DOUBLER (UPPER EXPOSED SURFACE) PER SRM 51-21-04-0G. BLENDED AND ACCEPTED AS IS PER EA T 1-5330-T0376395 "WINGS PLATES AND SKINS - MAIN LANDING GEAR SUPPORT LOWER DOUBLER REWORK - REPAIR MAJOR REPAIR
LH MLG GEARWELL DOOR - AFT CORNER INBD OF OUTER DOOR - GOUGED. REMOVED AND REPLACED DOOR INNER PAN CORNER IAW DWG NNB6086
FOUND DAMAGE TO THE A/C SKIN ON THE LH SIDE, BEHIND THE STATIC PORT/RVSM CONTROLLED AREA, AND BELOW THE OUTFLOW VALVE. INSTALLED ALL REPAIR PART ON AIRCRAFT IAW SRM 53-00-01-2R.
EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST LIGHT INOP. RELEASED FOR SERVICE PER MEL : 25-61-02 EVAC SLIDE SYS PRESS ADEQAUTE ONCE EACH FLIGHT DAY. SLIDE PRESSURE VERIFIED TO BE SERVICEABLE. REPLACED R1 DOOR REMOTE PRESSURE INDICATOR PTT SWITCH I.A.W AMM 25-61-04-4. PERFORMED OPS CHECKED SERVICEABLE. A/C OK FOR SERVICE. CLEAR MEL.
WHEN RETRACTING GEAR RECEIVED LEVEL 2 HYD 3 FAIL. DECLARED EMERGENCY. COMPLIED WITH CHECKLIST. ALTERNATE GEAR EXTENSION. DUE TO HSC MANUAL, EDP PUMPS RAN FOR APPROX 30 MINUTES WITH NO HYDRAULIC FLUID IN SYSTEM 3. EDP PUMPS SELECTED OFF AFTER LANDING. REMOVED AND REPLACED #3 ENGINE LOWER EDP PRESSURE LINE AND RIGHT HAND LANDING GEAR ACTUATOR LINE. OPERATIONAL AND LEAK CHECKS GOOD
MDIS 574 52-20 2983 28JAN23 IND OPEN U L1 DOOR SLIDE FELL OUT WHILE ATTEMPTING TO DISARM DOOR. MEL: 52-10-03-03 INSTALLED 10 MAN PORTABLE LIFE RAFT FOR MEL 52-10-03-03 IN CREW LUGGAGE NET, WEIGHT AND BALANCE CHANGES ARE AS FOLLOWS: (MPN:5A3210-40621) (WEIGHT (LBS) = 59.00) (ARM = 375.00 INCHES) (MOMENT = 22,125.00 INCH LBS AMM 25-61-15-4 REMOVED L1 DOOR SLIDE IAW MD11 AMM15-61-15-4 R/I 29JAN23 01:44 IND U REASON CODE : REMOVAL FROM A/C ONLY **NO INSTALLATION** OFF MPN: AWD9830-507L-FX POS: LH SRL: 0140 UPDT 29JAN23 01:44 IND U AMM 25-61-15-4 RELEASED FOR SERVICE PER MEL : 52-10-03-03 CATEGORY : C EXPIRATION : 07FEB23 "MEL 52-10-03-03: L1 CABIN ENTRY (IDENTIFY DOOR OR SLIDE/RAFT)SLIDE - REMOVED - EXTENDED OVERWATER OPS REQ UIRES TWO SLIDE/RAFTS AND/OR PORTABLE RAFTS." REMOVED AWD9830-507L-FX SLIDE FACT 07FEB23 23:07 MEM AMM: 25-61-01-4 INSTALLED SERVICEABLE L1 SLIDE REF AMM 25-61-01-4. INDICATION CHECK GOOD. PART INFO PART NAME: L1 DOOR SLIDE MANUFACTURE: THORNTON TECHNOLOGY CORPORATION PART NUMBER: AWD9830-507L SERIAL NUMBER: 0385TH
L1 DOOR SLIDE FELL OUT WHILE ATTEMPTING TO DISARM DOOR. INSTALLED 10 MAN PORTABLE LIFE RAFT FOR MEL 52-10-03-03 IN CREW LUGGAGE NET. REMOVED L1 DOOR SLIDE IAW AMM 15-61-15-4 RELEASED FOR SERVICE IAW MEL 52-10-03-03. L1 CABIN ENTRY (IDENTIFY DOOR OR SLIDE/RAFT)SLIDE - REMOVED - EXTENDED OVERWATER OPS REQ UIRES TWO SLIDE/RAFTS AND/OR PORTABLE RAFTS." REMOVED AWD9830-507L-FX SLIDE
DURING CLIMB OUT APPROX FL230 ACFT EXPERIENCED A LOUD POP WHICH SEEMED COME FROM BELOW COCKPIT IN E/E BAY. A MOMENTARY CLIMB INDICATED IN CAVING RATE OF CLIMB TO 700 FPM THEN RETURNED TO 300 FPM. SOUND OF AIR RUSHING THROUGH COCKPIT CONSTANT AFTER INITIAL POP. A SECOND POP OCCURRED APPROX 5 MINS LATER AT FL 280. OPENING AVIONICS FLOOR ACCESS THERE WAS A DEFINITE INCREASE IN A NOISE. NO SUCTION OR DIFFICULTY OPENING FLOOR ACCESS. LVL 1 AVIONICS FAN OVERRIDE ON & AS LVL 1 CABIN INFLOW LOW. RETURNED TO MEM. FOUND AVIONICS COMPARTMENT DOOR SEAL MISSING FORWARD SIDE. REPLACED SEAL IAW AMM 52-00-00-4.
PASSING 20,000 FEET ON DEPARTURE, SMOKE IN THE COCKPIT. DECLARED EMERGENCY. COMPLIED WITH QRH. RTB. ONCE WE DEPRESSURIZED THE COCKPIT, SMOKE WENT AWAY. FIRE DET 1 FAULT ALERT UNDER MAINTENANCE MENU. ***EMERGENCY DECLARED*** PERFORMED PACK BURN OUT PER AMM 21-53-00-7 AND REPLACED COALESCE BAGS FOR ALL 3 PACKS, REFERENCE WRI 21-50/2149.
MAIN DECK CARGO PLUG DOOR 3R , CUTOUT FORWARD JAMB UPPER WEB CORNER INNER SKIN , STATION 1250 - 1256 LONGERON 15 RIGHT - LONGERON 16 RIGHT FOUND CRACKED. MAIN DECK CARGO AT R3 PLUG DOOR CUTOUT FORWARD JAMB UPPER WEB CORNER CRACKED INNER SKIN , STATION 1250 TO STATION 1256 LONGERON 15 RIGHT TO LONGERON 16 RIGHT REPAIRED AS PER E.A. #: 1-5310-T0365926 P1 , TITLE: FUSELAGE - MAINFRAME - CRACK REPAIR FOR R3 CENTER FUS PAX DOOR JAMB FWD INNER SKIN , STA 1250 - 1256 , L - 15R TO L - 16R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.# 1-5750-87635 H PART 3 STEP 3A AND STEP 3B, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI : 57501397 FOR DETAILS)
LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.# 1-5750-87635 H PART 3 STEP 3A AND STEP 3B, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI : 57501397 FOR DETAILS)
RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.# 1-5750-87636 I PART 3 STEP 3A AND STEP 3B, TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI : 57501410 FOR DETAILS)
RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.# 1-5750-87636 I PART 3 STEP 3A AND STEP 3B, TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI : 57501410 FOR DETAILS)
LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-08 AND FOUND BARREL NUT WALL THICKNESS UPPER AND LOWER SURFACE EXCEED LIMIT BASED THE DIFFERENCE BETWEEN DRAWING LIMITS AND CMM MAXIMUM REWORK LIMITS. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# 1-5750-T0365867 PART 1 STEP 1E AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP INBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00400 ATTACHED E.A.# 1-5750-T0365867 PART 1 FOR DETAILS.
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-09 AND FOUND BARREL NUT WALL THICKNESS UPPER AND LOWER SURFACE EXCEED LIMIT BASED THE DIFFERENCE BETWEEN DRAWING AND CMM MAXIMUM REWORK LIMITS. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# 1-5750-T0365888 PART 1 STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00439 ATTACHED E.A.# 1-5750-T0365888 PART 1 FOR DETAILS.
MAIN DECK CARGO DOOR ASSEMBLY , HINGE FITTING NUMBER 1 [PART NUMBER ACA7332-1] FOUND WITH LOBES NUMBER 1 TO NUMBER 9 (ALL) OUT OF TOLERANCE. MAIN DECK CARGO DOOR ASSEMBLY , HINGE FITTING NUMBER 1 (PART NUMBER ACA7332-1) LOBES NUMBER 1 TO NUMBER 9 REWORDED AS PER MD-11 CMM 52-34-04 GENERAL REPAIR PARAGRAPH 2.Y. OVERSIZED REPIR BUSHINGS 09EA FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 52-34-04. REPAIR - GENERAL. PARAGRAPH 2.Y AND E.A #1-5230- T0365869 PART 1 STEP 2 AND STEP 5. TITLE: DOORS - CARGO DOOR/HYD SYS - MAIN DECK CARGO DOOR - FORWARD MOST SUPPORT (DOOR SIDE) - HINGE LOBE BORE FOUND WORN. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
LEFT HAND WING OUTBOARD FLAP VANE # 3 TEE FITTING TRACK ATTACH HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE # 3 TEE FITTING TRACK ATTACH HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.# 1-5750-T0365938 PART 1 STEP 1A, TITLE: WINGS- FLIGHT SURFACES- LH WING- OUTBD FLAP VANE ASSY- TRACK SUPPORT FITTING SLOT HOLES CORROSION REPAIR, AND INSTALLED AS PER AMM 27-50-32-020-034. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
LEFT HAND WING OUTBOARD FLAP VANE # 2 TEE FITTING TRACK ATTACH HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE # 2 TEE FITTING TRACK ATTACH HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.# 1-5750-T0365938 PART 1 STEP 1A, TITLE: WINGS- FLIGHT SURFACES- LH WING- OUTBD FLAP VANE ASSY- TRACK SUPPORT FITTING SLOT HOLES CORROSION REPAIR, AND INSTALLED AS PER AMM 27-50-32-020-034. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00727 ATTACHED E.A.# 1- 5750-T0365938 PART 1 FOR DETAILS.
LEFT HAND WING OUTBOARD FLAP VANE # 1 TEE FITTING TRACK ATTACH HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE # 1 TEE FITTING TRACK ATTACH HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.# 1-5750-T0365938 PART 1 STEP 1A, TITLE: WINGS- FLIGHT SURFACES- LH WING- OUTBD FLAP VANE ASSY- TRACK SUPPORT FITTING SLOT HOLES CORROSION REPAIR, AND INSTALLED AS PER AMM 27-50-32-020-034. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00727 ATTACHED E.A.# 1- 5750-T0365938 PART 1 FOR DETAILS.
LEFT HAND WING OUTBOARD FLAP VANE # 4 TEE FITTING TRACK ATTACH HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE # 4 TEE FITTING TRACK ATTACH HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.# 1-5750-T0365938 PART 1 STEP 1A, TITLE: WINGS- FLIGHT SURFACES- LH WING- OUTBD FLAP VANE ASSY- TRACK SUPPORT FITTING SLOT HOLES CORROSION REPAIR, AND INSTALLED AS PER AMM 27-50-32-020-034. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00727 ATTACHED E.A.# 1- 5750-T0365938 PART 1 FOR DETAILS.
MAIN DECK CARGO DOOR CUTOUT (AIRCRAFT SIDE) HINGE FITTING NUMBER 1 (PART NUMBER ACA 7223-513) FOUND WITH LOBES NUMBER 1 AND NUMBER 8 TO NUMBER 17 OUT OF TOLERANCE. MAIN DECK CARGO DOOR CUTOUT (AIRCRAFT SIDE) HINGE FITTING NUMBER 1 (PART NUMBER ACA 7223-513) LOBES NUMBER 1 AND NUMBER 8 TO NUMBER 17 REWORKED AND FOUND NUMBER 1 LOBE EXCEED LIMIT AS PER MD-11 SRM 52-30-16-1A FIGURE 101 SHEET 3. OVERSIZE REPAIR BUSHINGS 11EA FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 52-34- 04 AND E.A. #1-5310-T0335958A PART 2 STEP 5 AND STEP 2. TITLE: FUSELAGE - MAIN DECK CARGO DOOR JAMB - WORN HOLES ON MAIN DECK CARGO DOOR FORWARD SUPPORT HINGE LOBE (FUSELAGE DOOR JAMB SIDE). REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. # 1-5750-87633 G PART 4 STEP 2A AND STEP 2B, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION-PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57501391 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 (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.# 1- 5750-87635 H PART 3 STEP 3A AND STEP 3B, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI : 57501397 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 (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.# 1- 5750-87636 I PART 3 STEP 3A AND STEP 3B, TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI : 57501410 FOR DETAILS)
LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED AND FOUND ACCEPTED AS PER E.A.# 1-5750-87635 H PART 3 STEP 2 AND FIGURE 1, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI : 57501397 FOR DETAILS)
RIGHT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-04 AND E.A.# 1- 5750-87632 A PART 2 STEP 2 AND STEP 1, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- RH OUTBD FLAP/ INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# 1-5750-T0365960 PART 1 STEP 2A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE)- CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# 1-5750-T0365960 PART 1 STEP 2A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE)- CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00466 ATTACHED E.A.# 1-5750-T0365960 PART 1 FOR DETAILS.
RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 08. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# 1-5750- T0365960 PART 1 STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE)- CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00466 ATTACHED E.A.# 1-5750-T0365960 PART 1 FOR DETAILS.
RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# 1-5750- T0365960 PART 1 STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE)- CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00466 ATTACHED E.A.# 1-5750-T0365960 PART 1 FOR DETAILS.
RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# 1-5750-T0365960 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE)- CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00466 ATTACHED E.A.# 1-5750-T0365960 PART 1 FOR DETAILS.
RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-08 AND E.A.# 1-5750-T0365960 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE)- CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00466 ATTACHED E.A.# 1-5750-T0365960 PART 1 FOR DETAILS.
RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# 1- 5750-T0365960 PART 1 STEP 2A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7- 5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE)- CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00466 ATTACHED E.A.# 1- 5750-T0365960 PART 1 FOR DETAILS.
RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. # 1-5750-87634 I PART 6 STEP 2A AND STEP 2B, TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION-PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57501374 FOR DETAILS)
RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 52-03 AND E.A. # 1-5750-87634 I PART 6 STEP 2A AND STEP 2B, TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION-PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57501374 FOR DETAILS)
RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. REPAIR EVALUATED AND FOUND ACCEPTED AS PER E.A. # 1-5750-87634 I PART 6 STEP 2 AND FIGURE 2, TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION-PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57501374 FOR DETAILS)
LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. # 1-5750-87633 G PART 4 STEP 2A AND STEP 2B, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION-PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57501391 FOR DETAILS)
LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE SURFACE FOUND CORROSION CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. REPAIR EVALUATED AND FOUND ACCEPTED AS PER E.A. # 1-5750-87633 G PART 4 STEP 2 AND FIGURE 2, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION-PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57501391 FOR DETAILS)
LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. REPAIR EVALUATED AND FOUND ACCEPTED AS PER E.A. # 1-5750-87633 G PART 4 STEP 2 AND FIGURE 2, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION-PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57501391 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 CMM 57-44-07. REPAIR EVALUATED AND FOUND ACCEPTED AS PER E.A.# 1-5750-87636 I PART 3 STEP 2 AND FIGURE 1, TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI : 57501410 FOR DETAILS)
CENTER CARGO COMPARTMENT , STATION 5-113 TO STATION 1541 LONGERON SPLICE LONGERON 45 LEFT FOUND CRACKED. CENTER CARGO COMPARTMENT STATION 5-113 TO STATION 1541 CRACKED LONGERON SPLICE LONGERON 45 LEFT REMOVED AND REPLACED WITH FABRICATED MACHINED LONGERON SPLICE AS PER SRM 51-33-01-0G. LONGERON SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWING : A5A7116 REVISION : D. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.
CENTER CARGO COMPARTMENT , STATION 5-113 TO STATION 1541 LONGERON SPLICE LONGERON 43 LEFT FOUND CRACKED. CENTER CARGO COMPARTMENT STATION 5-113 TO STATION 1541 CRACKED LONGERON SPLICE LONGERON 43 LEFT REMOVED AND REPLACED WITH FABRICATED MACHINED LONGERON SPLICE AS PER SRM 51-33-01-0G. LONGERON SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWING : A5A7116 REVISION : D. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.
AFT CARGO - WEB STATION 1841 X = - 44 FOUND CRACKED. AFT CARGO CRACKED WEB STATION 1841 X = - 60 TO X = 0.0 REMOVED AND REPLACED WITH FABRICATED WEB AS PER SRM 51-31-01-0G. WEB FABRICATED AS PER DOUGLAS DRAWING : AGA7170 REVISION : R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER CARGO - FLOOR SUPPORT STATION 1841 X = - 24 FOUND CORROSION. CENTER CARGO - FLOOR SUPPORT STATION 1841 X = - 24 DAMAGED SUPPORT REMOVED AND REPLACED WITH REWORKED SUPPORT AS PER SRM 51-35-01-0G. SUPPORT REWORKED AS PER DOUGLAS DRAWING : AGA7170 REVISION : T. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.
LEFT HAND WING FIXED LEADING EDGE DOUBLER AT APPROXIMATE STATION XOS 995 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE DOUBLER AT APPROXIMATE STATION XOS 995 CRACKED AREA REPAIRED AS PER EA # 1-5730-T0365952 PART 1 TITLE : WINGS - PLATES AND SKINS - REPAIR FOR LH WING L.E SKIN P/N ARB2891-503 AND LOWER STRINGER DOUBLER P/N ARB2933-13 BETWEEN XOS 993.238 AND XOS 1013.179. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI # 57301755 FOR DETATILS.
RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT APPROXIMATE STATION XOS 990 FOUND CRACK. RIGHT HAND WING FIXED LEADING EDGE CRACKED DOUBLER AT APPROXIMATE STATION XOS 990 REPAIRED AS PER SRM 57-40-01-2R REPAIR 9 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO SPECIAL / NONROUTINE MAINTENANCE FORM # N00959 FOR WORK DETAILS.
CENTER CARGO COMPARTMENT , STATION 5-113 TO STATION 1541 LONGERON SPLICE LONGERON 50 LEFT FOUND CRACKED. CENTER CARGO COMPARTMENT STATION 5-113 TO STATION 1541 CRACKED LONGERON SPLICE LONGERON 50 LEFT REMOVED AND REPLACED WITH FABRICATED MACHINED LONGERON SPLICE AS PER SRM 51-33-01-0G. LONGERON SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWING : A5A7114 REVISION : E. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.
CENTER CARGO COMPARTMENT , BETWEEN STATION 5-113 AND STATION 1541 LONGERON SPLICE LONGERON 39 RIGHT FOUND CRACKED. CENTER CARGO COMPARTMENT BETWEEN STATION 5-113 AND STATION 1541 CRACKED LONGERON SPLICE LONGERON 39 RIGHT REMOVED AND REPLACED WITH FABRICATED MACHINED LONGERON SPLICE AS PER SRM 51-33-01-0G. LONGERON SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWING : A5A7114 REVISION : E. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER CARGO COMPARTMENT , STATION 5-113 TO STATION 1541 LONGERON SPLICE LONGERON 49 RIGHT FOUND CRACKED. CENTER CARGO COMPARTMENT STATION 5-113 TO STATION 1541 CRACKED LONGERON SPLICE LONGERON 49 RIGHT REMOVED AND REPLACED WITH FABRICATED MACHINED LONGERON SPLICE AS PER SRM 51-33-01-0G. LONGERON SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWING : A5A7114 REVISION : E. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.
CENTER CARGO COMPARTMENT , STATION 5-113 TO STATION 1541 LONGERON SPLICE LONGERON 52 FOUND CRACKED. CENTER CARGO COMPARTMENT STATION 5-113 TO STATION 1541 CRACKED LONGERON SPLICE LONGERON 52 REMOVED AND REPLACED WITH FABRICATED MACHINED LONGERON SPLICE AS PER SRM 51-33-01-0G. LONGERON SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWING : A5A7114 REVISION : E. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CENTER CARGO COMPARTMENT , STATION 5-113 TO STATION 1541 LONGERON SPLICE LONGERON 51 LEFT FOUND CRACKED. CENTER CARGO COMPARTMENT STATION 5-113 TO STATION 1541 CRACKED LONGERON SPLICE LONGERON 51 LEFT REMOVED AND REPLACED WITH FABRICATED MACHINED LONGERON SPLICE AS PER SRM 51-33-01-0G. LONGERON SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWING : A5A7114 REVISION : E. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.
CENTER CARGO COMPARTMENT , STATION 5-113 TO STATION 1541 LONGERON SPLICE LONGERON 44 LEFT FOUND CRACKED. CENTER CARGO COMPARTMENT STATION 5-113 TO STATION 1541 CRACKED LONGERON SPLICE LONGERON 44 LEFT REMOVED AND REPLACED WITH FABRICATED MACHINED LONGERON SPLICE AS PER SRM 51-33-01-0G. LONGERON SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWING : A5A7116 REVISION : D. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.
CENTER CARGO COMPARTMENT , STATION 5-113 TO STATION 1541 LONGERON SPLICE LONGERON 46 RIGHT FOUND CRACKED. CENTER CARGO COMPARTMENT STATION 5-113 TO STATION 1541 CRACKED LONGERON SPLICE LONGERON 46 RIGHT REMOVED AND REPLACED WITH FABRICATED MACHINED LONGERON SPLICE AS PER SRM 51-33-01-0G. LONGERON SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWING : A5A7116 REVISION : D. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# 1-5750-T0305236 C PART 2 STEP 3 AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- FLIGHT SURFACES- 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00363 ATTACHED E.A.# 1-5750-T0305236 C PART 2 FOR DETAILS.
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# 1-5750-T0305236 C PART 2 STEP 3 AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- FLIGHT SURFACES- 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE (#10 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# 1-5750-T0305236 C PART 2 STEP 3 AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- FLIGHT SURFACES- 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00363 ATTACHED E.A.# 1-5750-T0305236 C PART 2 FOR DETAILS.
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44- 09 AND E.A.# 1-5750-T0305236 C PART 2 STEP 3 AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- FLIGHT SURFACES- 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00363 ATTACHED E.A.# 1-5750-T0305236 C PART 2 FOR DETAILS.
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# 1-5750-T0305236 C PART 2 STEP 3 AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- FLIGHT SURFACES- 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00363 ATTACHED E.A.# 1-5750-T0305236 C PART 2 FOR DETAILS.
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# 1-5750-T0305236 C PART 2 STEP 1, TITLE: WINGS- FLIGHT SURFACES- FLIGHT SURFACES- 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00363 ATTACHED E.A.# 1-5750-T0305236 C PART 2 FOR DETAILS.
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-09 AND E.A.# 1-5750-T0305236 C PART 2 STEP 2 AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- FLIGHT SURFACES- 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00363 ATTACHED E.A.# 1-5750-T0305236 C PART 2 FOR DETAILS.
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# 1-5750-T0305236 C PART 2 STEP 2 AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- FLIGHT SURFACES- 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00363 ATTACHED E.A.# 1-5750-T0305236 C PART 2 FOR DETAILS.
FLIGHT COMPARTMENT LEFT HAND FLOOR PANEL #215DF , AT STATION 340-366 FOUND WITH DELAMINATION. DELAMINATED FLIGHT COMPARTMENT LEFT HAND FLOOR PANEL #215DF AT STATION 340 - STATION 366 REMOVED AS PER AMM 53-21-02-4. FLOOR PANEL #215DF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #215DF INSTALLED AS PER AMM 53-21- 02-4. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT APPROXIMATE STATION XOS 667 FOUND CRACK. CRACKED DOUBLER REMOVED AND FABRICATED DOUBLER AS PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FABRICATED DOUBLER AT RIGHT HAND WING FIXED LEADING EDGE AT APPROXIMATE STATION XOS 667 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING FIXED LEADING EDGE SKIN AT APPROXIMATE STATION 995 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE SKIN AT APPROXIMATE STATION XOS 995 CRACKED AREA REPAIRED AS PER EA # 1-5730-T0365952 PART 1 TITLE : WINGS - PLATES AND SKINS - REPAIR FOR LH WING L.E SKIN P/N ARB2891-503 AND LOWER STRINGER DOUBLER P/N ARB2933-13 BETWEEN XOS 993.238 AND XOS 1013.179. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING FIXED LEADING EDGE PANEL SUPPORT DOUBLER AT APPROXIMATE STATION XOS 787 FOUND CRACK. RIGHT HAND WING FIXED LEADING EDGE PANEL SUPPORT DOUBLER AT APPROXIMATE STATION XOS 787 REPAIR CARRIED OUT AS PER SRM 57-40-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING FIXED LEADING EDGE SKIN AT APPROXIMATE STATION XOS 990 FOUND CRACK. RIGHT HAND WING FIXED LEADING EDGE SKIN AT APPROXIMATE STATION XOS 990 REPAIR CARRIED OUT AS PER SRM 57-40-01-2R REPAIR 9 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
FLIGHT COMPARTMENT - LEFT HAND FLOOR PANEL #215BF AT STATION 330 FOUND WITH DELAMINATION. DELAMINATED FLIGHT COMPARTMENT LEFT HAND FLOOR PANEL #215BF AT STATION 330 REMOVED AS PER AMM 53-21-02-4. FLOOR PANEL #215BF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL INSTALLED AS PER AMM 53-21-02-4. REPAIR CLASSIFFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE (#10 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# 1-5750-T0365888 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00439 ATTACHED E.A.# 1-5750-T0365888 PART 1 FOR DETAILS.
MAIN DECK CARGO COMPARTMENT , LEFT HAND SEAT TRACK ALONG , X = 8.50 FLANGE FOUND WITH CORROSION BETWEEN STATION 1531 AND STATION 1541. MAIN DECK CARGO COMPARTMENT AT LEFT HAND SEAT TRACK FLANGE STATION 1531 AND STATION 1541 , X = 8.5 CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1571 TO EXISTING SPLICE STATION 1531/5-123 , X = 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT , RIGHT HAND SEAT TRACK ALONG X = - 8.5 FOUND WITH CORROSION ON FLANGE AT STATION 5-73 AND STATION 5-93. MAIN DECK CARGO COMPARTMENT AT RIGHT HAND SEAT TRACK FLANGE STATION 5-73 AND STATION 5-93 X = - 8.5 , CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 5-63 TO EXISTING SPLICE STATION 5- 123/1531 , X = - 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# 1-5750-T0365888 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# 1-5750-T0365888 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00439 ATTACHED E.A.# 1-5750-T0365888 PART 1 FOR DETAILS.
MAIN DECK CARGO COMPARTMENT , LEFT HAND SEAT TRACK ALONG X = 8.50 FLANGE FOUND WITH CORROSION BETWEEN STATION 5-53 AND STATION 5-103. MAIN DECK CARGO COMPARTMENT , AT SEAT TRACK FLANGE BETWEEN STATION 5-53 AND STATION 5-103 X = 8.5 , CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES FROM STATION 1531/5-0 TO STATION 1531/5-123 , X = 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-09 AND E.A.# 1-5750-T0365888 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00439 ATTACHED E.A.# 1-5750-T0365888 PART 1 FOR DETAILS.
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44- 09 AND E.A.# 1-5750-T0365888 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00439 ATTACHED E.A.# 1-5750-T0365888 PART 1 FOR DETAILS.
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 09. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# 1-5750- T0365888 PART 1 STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00439 ATTACHED E.A.# 1-5750-T0365888 PART 1 FOR DETAILS.
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# 1-5750-T0365888 PART 1 STEP 2A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00439 ATTACHED E.A.# 1-5750-T0365888 PART 1 FOR DETAILS.
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-09 AND E.A.# 1-5750-T0365888 PART 1 STEP 2A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00439 ATTACHED E.A.# 1-5750-T0365888 PART 1 FOR DETAILS.
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# 1-5750-T0365888 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00439 ATTACHED E.A.# 1-5750-T0365888 PART 1 FOR DETAILS.
LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-08. REPAIR EVALUATED AND FOUND ACCEPTED AS PER E.A.# 1-5750-T0365867 PART 1 STEP 1 AND FIGURE 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP INBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00400 ATTACHED E.A.# 1-5750-T0365867 PART 1 FOR DETAILS.
LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# 1-5750-T0365867 PART 1 STEP 1D AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP INBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00400 ATTACHED E.A.# 1-5750-T0365867 PART 1 FOR DETAILS.
LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# 1-5750-T0365867 PART 1 STEP 1D AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP INBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-08 AND E.A.# 1-5750-T0365867 PART 1 STEP 1C AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP INBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00400 ATTACHED E.A.# 1- 5750-T0365867 PART 1 FOR DETAILS.
LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# 1-5750-T0365867 PART 1 STEP 1C AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1- 5750-7-5002- LH WING- OUTBD FLAP INBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00400 ATTACHED E.A.# 1- 5750-T0365867 PART 1 FOR DETAILS.
LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# 1-5750- T0365867 PART 1 STEP 1A AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP INBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00400 ATTACHED E.A.# 1-5750-T0365867 PART 1 FOR DETAILS.
RIGHT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT APPROXIMATE STATION XOS 669 FOUND CRACK. RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT APPROXIMATE 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 BEADED DOUBLER AT APPROXIMATE STATION XOS 544 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE DOUBLER AT APPROXIMATE STATION XOS 544 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 BEADED DOUBLER AT APPROXIMATE STATION XOS 709 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE DOUBLER AT APPROXIMATE STATION XOS 709 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 BEADED DOUBLER AT APPROXIMATE STATION XOS 696 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE DOUBLER AT APPROXIMATE STATION XOS 696 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 BEADED DOUBLER AT APPROXIMATE STATION XOS 640 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE DOUBLER AT APPROXIMATE STATION XOS 640 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 BEADED DOUBLER AT APPROXIMATE STATION XOS 990 FOUND CRACK. RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT APPROXIMATE STATION XOS 990 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 BEADED DOUBLER AT APPROXIMATE STATION XOS 791 FOUND CRACK. RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT APPROXIMATE 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 BEADED DOUBLER AT APPROXIMATE STATION XOS 760 FOUND CRACK. RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT APPROXIMATE STATION XOS 760 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 BEADED DOUBLER AT APPROXIMATE STATION XOS 697 FOUND CRACK. RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT APPROXIMATE STATION XOS 697 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 BEADED DOUBLER AT APPROXIMATE STATION XOS 665 FOUND CRACK. RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT APPROXIMATE STATION XOS 665 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 BEADED DOUBLER AT APPROXIMATE STATION XOS 637 FOUND CRACK. RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT APPROXIMATE STATION XOS 637 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AIR TURN BACK DUE TO LEVEL 1, SEL LSAS ROB OFF, PASSING F320 DURING DEPARTURE. BOTH AUTOPILOTS WOULD NOT ENGAGE. FOUND BOTH RAM AND MOD LVDT AT UPPER LIMITS OF OHM READING FOR ROB ELEVATOR ACTUATOR . OHMED AND MEGGED WIRING TO GROUND WITH NO FAULTS FOUND. REF. FIM. 22-11. REMOVED AND REPLACED RH OUTBOARD ELEVATOR ACTUATOR UP TO AND INCLUDING 3G STEP 9 OF AMM 27-33-30-4, LEAK CHECK GOOD.
MAIN CARGO DECK, STA1341 RBL104 CORROSION ON ANGLE AT BASE OF OVERWING FUEL TANK, 2020-01-14] AREA REPAIRED PER EA 1-5710-T0351898.
RH WING TRAILING EDGE OUTBD ISLAND P/N ARC7203-13 DELAMINATED REPAIRED IAW SRM 57-50-80-2R PAR 2 (2) WET LAY UP.
UPPER CARGO COMPARTMENT; X=100 Y=1211 UNDER FLOOR UPPER INTERNAL STRUCTURE HAS LEVEL 2/3 CORROSION 1" X 1". DOT #2 REMOVED FASTENERS, BLENDED THE CORROSION WHICH WENT OUT OF LIMITS IN REF TO SRM 57-10-01, FIG 101 SHEETS 1-2. DOUBLER WAS FABRICATED & INSTALLED OVER ENTIRE AREA OF THE BLENDOUT PER EA # 1-5710-T0351335, PART # 1 TITLE: WINGS - CENTER WING UPPER SKIN - BETWEEN XCW=46 AND 118 AND BETWEEN STRINGER 15 AND 19 - CORROSION DAMAGE. AREA WAS TREATED, PRIMED, FASTENERS WERE RE-INSTALLED & THE VAPOR BARRIER WAS RE-APPLIED.
MAIN CARGO DECK, STA1231 LBL105, CORROSION ON CENTER WING UPPER PANEL BY OVERWING FUEL TANK (MARKED) REMOVED FASTENERS, REMOVED THE CORROSION, NDT CHECKED FOR MATERIAL LOSS, FOUND TO BE WITHIN ALLOWABLE LIMITS IN REF TO SRM 57-10-01 FIG 101 PAGES 1-2, AREA WAS TREATED, PRIMED, FASTENERS WERE RE-INSTALLED, AREA WAS PAINTED & VAPOR BARRIER WAS RE-APPLIED.
UPPER CARGO COMPARTMENT; X=98-106 Y=1225-1231 UNDER FLOOR UPPER INTERNAL STRUCTURE HAS LEVEL 2/3 CORROSION 5" X 7". REMOVED FASTENERS, REMOVED THE CORROSION, NDT CHECKED FOR MATERIAL LOSS AFTER BLENDING, HOLES WERE ALSO CHECKED WITH NO DEFECTS NOTED, AREA WAS TREATED, PRIMED, FASTENERS WERE RE-INSTALLED, AREA WAS PAINTED & VAPOR BARRIER WAS RE-APPLIED.
MAIN CARGO DECK, STA1219 LBL98, CENTER WING UPPER PANEL HAS CORROSION (MARKED) REMOVED FASTENER, REMOVED CORROSION, NDT CHECKED FOR REMAINING MATERIAL THICKNESS & CHECKED THE OPENED HOLE FOR ANY INDICATIONS WITH NO DEFECTS NOTED IN REF TO: EA # 1-5730-T0351160 REV (A) AND SRM 57-10-01 FIG 101 PAGES 1-2, AREA WAS TREATED, PRIMED, FASTENER RE-INSTALLED, PAINTED AND VAPOR BARRIER WAS APPLIED.
UPPER CARGO COMPARTMENT; X=58 Y=1227 UNDER FLOOR UPPER INTERNAL STRUCTURE HAS LEVEL 2/3 CORROSION 1" X 1". DOT #5 REMOVED FASTENERS, REMOVED CORROSION, NDT CHECKED FOR THE REMAINING MATERIAL THICKNESS, OPEN HOLES WAS ALSO CHECKED WITH NO DEFECTS NOTED, AREA WAS TREATED, PRIMED, FASTENERS WERE RE-INSTALLED, MAREA WAS PAINTED & THE VAPOR BARRIER WAS RE-APPLIED.
UPPER CARGO COMPARTMENT; X=86 Y=1228 UNDER FLOOR UPPER INTERNAL STRUCTURE HAS LEVEL 2/3 CORROSION 1" X 1". DOT #3 REMOVED FASTENERS, REMOVED CORROSION, NDT CHECKED FOR THE REMAINING MATERIAL THICKNESS, OPEN HOLES WAS ALSO CHECKED WITH NO INDICATIONS NOTED, AREA WAS TREATED, PRIMED, FASTENERS WERE RE-INSTALLED, AREA WAS PAINTED AND THE VAPOR BARRIER WAS RE-APPLIED.
MAIN CARGO DECK, STA1200 LBL106 CORROSION AROUND THE FASTENER (MARKED) REMOVED FASTENER, REMOVED THE CORROSION, NDT CHECKED THE REMAINING MATERIAL THICKNESS AND ALSO CHECKED THE OPENED HOLE FOR ANY INDICATIONS, FOUND NO DEFECTS, AREA WAS TREATED, PRIMED, FASTENER WAS RE-INSTALLED, AREA WAS PAINTED AND VAPOR BARRIER WAS APPLIED.
MAIN CARGO DECK, STA1319 LBL105, CENTER WING UPPER PANEL ANGLE TO FUEL TANK HAS CORROSION (MARKED) REMOVED FASTENERS, REMOVED CORROSION, NDT CHECKED THE MATERIAL LOSS AND FOUND THE ALL AREAS WERE WITHIN ALLOWABLE LIMITS PER SRM 57-10-01-1A FIG 101, HOLES WERE ALSO CHECKED WITH NO DEFECTS NOTED, AREA WAS TREATED, PRIMED, FASTENERS WERE RE-INSTALLED AND VAPOR BARRIER APPLIED.
MAIN CARGO DECK, STA1346 LBL108, CENTER WING UPPER PANEL HAS CORROSION (MARKED) REMOVED FASTENERS, REMOVED CORROSION, NDT WAS CALLED OUT TO DO A REMAINING THICKNESS CHECK, FOUND AREA TO BE WITHIN ALLOWABLE LIMITS OF SRM 57-10-01-1A FIG 101 & INSPECTED ALL OPEN HOLES WITH NO DEFECTS NOTED, AREA WAS TREATED, PRIMED, FASTENERS WERE RE-INSTALLED AND VAPOR BARRIER WAS APPLIED.
MAIN CARGO DECK, STA1361 LBL107, CENTER WING UPPER PANEL HAS CORROSION (MARKED) REMOVED FASTENERS, REMOVED CORROSION, NDT CHECKED FOR REMAINING MATERIAL THICKNESS AND FOUND AREA TO BE WITHIN ALLOWABLE LIMITS PER SRM 57-10-01-1A FIG 101, OPEN HOLES WERE ALSO CHECKED WITH NO DEFECTS NOTED, AREA WAS TREATED, PRIMED, FASTENERS WERE RE-INSTALLED AND VAPOR BARRIER WAS APPLIED.
MAIN CARGO DECK, STA1321 LBL108, CENTER WING UPPER PANEL HAS CORROSION (MARKED) REMOVED FASTENERS, REMOVED CORROSION, NDT CHECKED FOR THE REMAINING THICKNESS, FOUND TO BE WITHIN ALLOWABLE LIMITS, HOLES WERE ALSO CHECKED AND NO DEFECT WERE NOTED. AREA WAS TREATED, PRIMED, FASTENERS WERE RE-INSTALLED AND THE VAPOR BARRIER WAS APPLIED.
MAIN CARGO DECK, STA1393 LBL105 TO LBL111, CENTER WING UPPER PANEL HAS CORROSION (MARKED) CORRECTION: STA # IS: STA 1299LBL105 TO LBL 111 - REMOVED FASTENERS, REMOVED CORROSION, NDT CHECKED FOR MATERIAL LOSS AND FOUND TO BE WITHIN ALLOWABLE LIMITS PER SRM 57-10-01-1A FIG 101, HOLES WERE ALSO CHECKED BY NDT WITH NO DEFECTS NOTED, AREA WAS TREATED, PRIMED, FASTENERS WERE RE-INSTALLED AND VAPOR BARRIER WAS RE-APPLIED.
MAIN CARGO DECK, STA1890 LBL110, CENTER WING UPPER PANEL HAS CORROSION (MARKED) CORRECTION: STA # IS: STA 1296 @ LBL110 - REMOVED FASTENERS, REMOVED CORROSION, NDT CHECKED FOR MATERIAL LOSS AND FOUND AREA TO BE WITHIN ALLOWABLE LIMITS PER SRM 57-10-01-1A FIG 101, OPEN HOLES WERE ALSO CHECKED BY NDT WITH NO DEFECTS NOTED, AREA WAS TREATED, PRIMED, FASTENERS WERE RE-INSTALLED AND VAPOR BARRIER WAS RE-APPLIED.
MAIN CARGO DECK, STA1335 LBL105 TO LBL113, CENTER WING UPPER PANEL HAS CORROSION (MARKED) REMOVED FASTENERS, REMOVED CORROSION, NDT CHECK FOR MATERIAL LOSS, FOUND AREA TO BE WITHIN ALLOWABLE LIMITS PER SRM 57-10-01-1A FIG 101 & EA # 1-5710- T03511416, PART 1. TREATED, PRIMED, RE-INSTALLED FASTENERS AND VAPOR BARRIER APPLIED.
CTR CARGO - STA 1800 RBL 51 FLOOR SUPPORT SHOWS CORROSION MARKED DOT #3. REPLACED FLOOR SUPPORT PER DWG AFA7299. REMOVED CORRODED FLOOR SUPPORT SRM 51-31-0G-0 INSTALLED NEW FLOOR SUPPORT PER DWG AFA7299 & SRM 51-31-0G., MATERIAL VERIFIED S2929841 PER DWG AFA7299., FABRICATED PART PER DWG AFA7299.TREATED AND PAINTED FLOOR SUPPORT PER SRM 51-23-01-0G-0.
AFT CARGO COMPT - STA 1964 AT L46 SHOWS CORROSION ON FRAME. REPAIRED NOTED AREA OF CORROSION I.A.W. SRM 53-00-07-2R FIG 202 SHT 1.
R/H O/B FLAP TRAILING EDGE DAMAGED REMOVED AND REPLACED R/H O/B FLAP I/B SECTION TRAILING EDGE PER DWG NRC6753
L/E SKIN CORRODED ON R/H HORIZONTAL L/E SECTION 341BT...(MRK) 5121818: CONSIGNADO, FREDERICK J - 17-DEC-2019 22:02 REMOVED DAMAGED ON L/E, R/H HORIZ @ APPROX XFS 97. INSTALLED REPAIR PER SRM 55-10-02-2R REPAIR 1 FIG 201 SEE ATTACHMENTS NR 1274 AMT# RRB 828605, QC# 5063193, 12/14/19
CTR CARGO STA 1781 LBL 28 CARGO COMPARTMENT CONVEYOR CHANNEL UNDER LATCH ASSY IS CORRODED OUT OF LIMITS REMOVED AND REPLACE CHANNEL ASSY P/N# AFJ7014-507 REF DOUGLAS DWG AFJ7014A AND SRM 51-31-01-0G.
RH WING, AFT TOP WING SPAR HAS CORROSION AROUND FASTENER HOLE AT LOCATION APPROX STA XORS 903.0 REPAIRED PER E.A. 1-5710-T0351527 P1
R/H WING, UPPER REAR SPAR, STATION XORS 793 HAS SURFACE CORROSION. PERFORMED STRAP/ANGLE REPAIR PER EA T 1-5710-T0352042 P1
RH WING, AFT TOP WING SPAR HAS CORROSION AROUND FASTENER HOLE AT LOCATION APPROX XORS 846.3 REMOVED CORROSION PER SRM 51-21-01-0G. REF EA T 1-5710-T0351527 P1 "BASIC WING STRUCTURE - RH WING REAR SPAR UPPER CAP AFT LEG - REWORK." REWORKED AREA ACCEPTABLE AS IS.
RH WING, AFT TOP WING SPAR HAS CORROSION AROUND FASTENER HOLE AT LOCATION APPROX STA XORS 992.5 THRU XORS 1001.5 REPAIRED PER EA T 1-5710-T0351527
RH WING, AFT TOP WING SPAR HAS CORROSION AROUND FASTENER HOLE AT LOCATION APPROX STA XORS 1037.0 THRU XORS 1044.8 WORKED ACCOMPLISHED ON N/R 1206 AND 507 PER EA. 1-5710-T0351904
RH WING, AFT TOP WING SPAR HAS CORROSION AROUND FASTENER HOLE AT LOCATION APPROX STA XORS 983.5 THRU 989.0 REMOVED CORROSION PER SRM 51-21-01-0G. REF EA T 1-5710-T0351527 P1 "BASIC WING STRUCTURE - RH WING REAR SPAR UPPER CAP AFT LEG - REWORK." REWORKED AREA ACCEPTABLE AS IS.
RH WING UPPER REAR SPAR, STATION XORS 785 HAS SURFACE CORROSION. REPAIRED WITH STRAP/ANGLE PER EA T 1-5710-T0352042
RH WING UPPER REAR SPAR, STATION XORS 789 HAS SURFACE CORROSION. PERFORMED STRAP ANGLE REPAIR PER EA T 1-5710-T0352042
#1 ENGINE: RIGHT SIDE OF PYLON INSIDE ACCESS PANEL 438DR, PNEUMATIC DUCT SUPPORT. LOWER BRACKET HAS LOOSE ATTACH SCREWS/ELONGATED HOLES BRACKET REPAIR COMPLIED WITH I.A.W. E.A. 1-5450-T0351554 PT, REF JPF STEP ITEM 12. TITLE: NACELLES/PYLON - WING PYLON/STRUT - NO 1 PYLON BULKHEAD WEB ELONGATED HOLES AT YWN = 315.500 ELONGATED HOLES - REPAIR.
RH WING UPPER, REAR SPAR CORROSION AT WING STATION XORS 684. REPAIRED PER EA T 1-5710-T0351924 P1
MAIN DECK, CORROSION ON SEAT TRACK, APPROX. STA 1159 LBL 9. (MARKED) REMOVED & REPLACED SECTION OF SEAT TRACK BETWEEN STATIONS 1149 TO STATION 1189 IN REF TO DWG # SR10-53-002 AND SRM 53-00-52 REPAIR # 1, FIG 201
RT AFT FUSELAGE BELOW APU COMP COOLING AIR OUTLET, EXFOLIATION CORROSION AROUND FASTENER HOLE FOR PNL 347DF. REPAIRED AREA BELOW APU COMP COOLING AIR OUTLET REF SRM 53-70-01 FIG 201 SH 1 MAJOR REPAIR.
R/H AFT FUSELAGE BELOW HORZ. STAB CUT-OUT, NUMEROUS SURFACE CORROSIONS AROUND FASTENER HOLES FOR PNL 348BF AND 347DF REPAIRED AFT FUSELAGE SURFACE AT HORIZONTAL TAB CUTOUT IAW SRM 53-70-01-00 REPAIR #3 FIG 201 PG 202 AND JPF ITEMS.
#1 PYLON UPR PNL SUPPORT BRACKET BETWEEN PNLS 437CL AND 437DL WORN FROM PNL CHAFING. REPLACED BRACKET PER DWG AUB7564-29 AND SRM 51-31-01-0G.
MAIN CARGO DECK, STA1346 RBL105 CORROSION (MARKED) WORKED ACOMPLISHED ON N/R 664 AND 884 PER EA. 1-5710-T0351898
RT WING: DROOP L/E, INBD EDGE OF DROOP L/E REPAIR DOUBLER SKIN HAS WEAR MARK WORN INTO SKIN (MARKED AND DOT 36) REPAIRED PER SRM 57-40-01 2R
RT WING: OUTBD EDGE OF DROOP L/E REPAIR DOUBLER SKIN IS WORN THRU. INSTALLED REPAIR PER SRM 57-40-01-2R INSTALLED DROOP L.E IAW MM 27-80-10-4 OPS CK GOOD
RH WING UPPER SURFACE - XORS 248 LANDING GEAR DOUBLER - CORROSION AROUND THREE (3) FASTENERS. REPAIRED PER EA 1-5710-T0351593
FWD AVIONICS COMPT: APPROX STA 457, THE FRAME UNDER #1 PACK INLET DUCT. THE DUCT BOOT MOUNT FASTENERS HAVE WORN THRU THE UPPER PART OF THE FRAME. (UNDER THE DUCT BOOT). MARKED. REPAIR IS COMPLIED WITH E.A.#:1-5300-T0351624 PART 1, TITLE: MD-11 N574FE-FUSELAGE - FUSELAGE FRAME - EAR DAMAGE ON FUSELAGE FRAME INBD CHORD RETURN TAB AT STA 469.
CENTER CARGO COMPT: APPROX STA 1741 , CENTERLINE CARGO STOP. UNDER THE CARGO STOP THE FLOOR BEAM IS CRACKED.(UNDERSIDE OF STOP) REMOVED DAMAGED FLOOR BEAM IN CTR CARGO AT STA 1741. INSTALLED NEW FLOOR BEAM SECTION AND REPAIR PARTS PER SRM 51-31-01-0G.
MAIN CARGO DECK, STA1321 RBL48 UNDER SEAT TRACK, CORROSION BY FASTENER (MARKED) REMOVED AND REPLACED BRACKET PER APB7244
MAIN CARGO DECK, STA1341 RBL104 CORROSION ON ANGLE AT BASE OF OVERWING FUEL TANK (MARKED) WORK ACOMPLISHED ON N/R 664 AND 884 PER EA. 1-5710-T0351898 A P1
CENTER CARGO COMPT: APPROX STA 1721, X=-91.25. O/B CARGO RAIL HAS AN O/B FLOOR BOARD FASTNENER ATTACH EAR CRACKED TWO PLACES. MARKED. PROCESSED NEW CHANNEL PER DWG AJF7011-519, REMOVED AND INSTALLED NEW CHANNEL IN CTR CARGO AT STA 1721, X=-47.25 PER SRM 51-33-01-0G.
LT LWR VERTICAL STAB FAIRING SKIN AT STA 2160 HAS A .300 IN CRACK PROPAGATING OUT OF THE FASTENER HOLE. BELOW PYLON CARRY THROUGH CAP, REPAIRED SKIN FAIRING PER SRM 55-00-00-2R FIG 204 DWG AJC7582-17.
RIGHT WING T/E REAR SPAR UPPER CAP, LOWER FLANGE IS CORRODED AT STA. XORS 685. BLENDED AND REMOVED CORROSION IAW SRM 57-00-00-2R REFERENCE EA 1-5710-T0350918P1REMOVED FASTENERS THROUGH UPPER SPAR T-CAP LOWER FLANGE FROM XORS 680-690 IAW SRM 51-33-01-0G. REINSTALLED FASTENERS AS REQ'D IAW SRM 51-33- 01-0G. CORRODED AREA REQUIRES BLENDING. BLENDED CORRODED AREA IAW SRM 57-00-00-2R. PERFORMED NDT THICKNESS MEASUREMENT PER NDT SPM, TP-MDC-93K0393 MAXIMUM THICKNESS IS .351" MINIMUM THICKNESS MEASURED IS .300" PERFORMED HFEC HOLE PROBE INSP PER NDT SPM TP-MDC-93K0393 NO DISCONTINUITY INDICATION FOUND.
PERFORMED DETAIL VISUAL INSP. OF THE OUTER WING, UPPER SPAR CAP (P/N ARB7413-2) FROM STATIONS XORS-1041.500 THROUGH XORS-1044.000 PER FOLLOW UP E.A. 1-5720-87643 AND W/C SEQ. #000806, W/C #T-1-5720-87643 P2. FOUND CORROSION BETWEEN AREAS X0RS- 1035.500 THROUGH X0RS-1044.000. 5121818: CONSIGNADO, FREDERICK J - 12-FEB-2020 18:10 REF E.A 1-5710-T0351904 " WINGS - BASIC WING STRUCTURE - RH WING REAR SPAR UPPER GAP AFT LEG - REWORK" REMOVED CORROSION AND REPAIRED TOP WING SPAR PER EA T1-5710-Y0351904. WORKED ACCOMPLISHED ON N/R 1206 & N/R 507 "MAJOR REPAIR" AMT# EA 5082867, RII: QC# 5156615, 02/11/20 JPF ITEM 1: EMP: NMS 911637, RII: RII, OPEN WORK ITEM; CORROSION IN INDICATED AREA RE REQUIRES BLEEDING CORRECTIVE ACTION: BLENDED CORROSION IAW SRM 57-00-00-2R., MECH: NMS 911637, INSP: QC# 97952, 11/06/20 ITEM 2: EMP: NMS 911637, RII: RII, OPEN WORK ITEM: REQUEST NDT CHECK BLENDED AREA FO FOR REMAINING MATERIAL THICKNESS CORRECTIVE ACTION: PERFORMED UT THICKNESS MEASUREMENT PER NDTSPM TP-MDC- 93K0393 MINIMUM THICKNESS MEASURED IS .035 INCH MAXIMUM THICKNESS MEASURED I IS .115 INCH. MECH: N/A QC 97952, INSP; QC# 97952, 11/07/19
RH WING UPPER SURFACE - APPROX XORS 288 AFT SECTION OF LANDING GEAR DOUBLER - CORROSION AROUND FASTENER.
RT WING LWR FIXED L/E SKIN WORN FROM SLAT CONTACT. O/B OF SLAT TRACK NR 10 PERFORMED WING FIXED LEADING EGDE REPAIR IAW SRM 57-40-02-2R FIG 201 REP 5.
NUMEROUS AREAS OF SURFACE CORROSION ON L/H WING UPPER SURFACE XORS-93.00 TO XORS-96.00 STR.17.5 TO STRINGER-19.5...(MRK) REMOVED CORROSION ON L/H WING UPPER SURGACE REF SRM 57-00-01-1A & E.A. #: 1-5730- T0351592 "TITLE: WING - PLATES AND SKINS - LH OUTER WING UPPER PANEL PNS ARB7404-1/7406-1 - REWORK"
AFT CARGO TUNNEL:EXFOLIATION AT R/H STA 1960 STRINGER 40 DOT NO 3. REMOVED CORRODED SECTION OF LONGERON AS REQUIRED IAW SRM 53-00-05-2R FIG 202 REPAIR 1 PG 1-8.
AFT CARGO WASTE COMPT:EXFOLIATION AT R/H APX STA 1960 BETWEEN STRINGER 50-51 DOT NO 6. REMOVED AND REPLACED TEE CLIP P/N AGA8002-19 AT STA 1975 BETWEEN R/H L49 AND L/H49 REF SRM 51-35-01, SRM 51-33-01 AND DOUGLAS AGA8002.
NUMEROUS AREAS OF SURFACE CORROSION ON L/H WING UPPER SURFACE BETWEEN STA XORS-340.00 TO XORS-393.00 / STR-5.5 TO STR. 2...(MRK) REMOVED CORROSION ON L/H WING UPPER SURFACE BETWEEN STA XORS=345.75 TO XORS=298.501 STR 07 TO AFT SPAR REF EA#: 1-5730-T0351592 TITLE: WING PLATES AND SKINS L/H OUTER WING UPPER PANEL P/N ARB7404-1H406-1 REWORK & SRM 57-00-01-1A.
AFT CARGO COMPT:CORROSION AT R/H STA 1957 LONGERON 43R DOT NO 4. REMOVED AND REPLACED 48" LONG SECTION OF LONGERON 43 R/H FROM STSA 1948 TO 1997 IAW SRM 53-00-05-2R FIG 201, 202 SHEET 1-3, PG 1-8 DAC DWGS AGA7073, NGA6313.
NUMEROUS AREAS OF SURFACE CORROSION ON L/H WING UPPER SURFACE BETWEEN STA XORS-141.00 TO XORS-166.80 STR.22 TO STR-19....(MRK) REMOVED CORROSION ON L/H WING UPPER SURFACE BETWEEN STA XORS=130.40 TO XORS=163.80 FRONT SPAR TO STR 16 REF SRM 57-00-01-1A & E.A. #: 1-5730-T0351592 "TITLE: WING - PLATES AND SKINS - LH OUTER WING UPPER PANEL PNS ARB7404-1/7406-1 - REWORK"
NUMEROUS AREAS 0F SURFACE CORROSION ON L/H WING UPPER SURFACE BETWEEN STA XORS-166.80 TO XORS-201.00/FRONT STR-14 TO STR-19.5....(MRK) REWORKED CORROSION MD-11 SRM 57-00-01-1A SHEET 6
L/H LWR WING SKIN AT #12 SLAT TRACK CUT OUT AFT O/B CORNER HAS A .300 IN. CRACK. (MARKED) REPAIRED NOTED SKIN CRACK AT SLAT TRACK #12 PER SRM 57-40-02-2R REPAIR 7 FIG 201.
R/H NLG WHEEL WELL WEB AT STA. 495 HAS A .200 IN. CRACK AT FASTENER HOLE ABOVE HORIZONTAL STIFFENER. (MARKED) REPAIRED RH NLG WHEEL WELL WEB AT STA 495 REF SRM 53-10-13 FIG 201 SH. 8
L/H LWR WING SKIN AT #16 SLAT TRACK CUT OUT AFT I/B CORNER HAS A .400 IN. CRACK. (MARKED) REPAIR NOTED SKIN CRACK AT SLAT #16 PER SRM 57-40-02-2R REPAIR 7 FIG 201
L/H NLG WHEEL WELL WEB AT STA. 495 HAS A .200 IN. CRACK AT FASTENER HOLE ABOVE HORIZONTAL STIFFENER. (MARKED) REPAIRED LH NLG WHEEL WELL WEB @ STA 495 REF SRM 53-10-13 FIG 201 SH. 8 'MAJOR REPAIR' JPF
R/H NLG TRUNNION FITTING WEB AT STA. 590 HAS A .900 IN. CRACK. (MARKED) REPAIRED AS REQUIRED R/H NLG TRUNNION FITTING WEB AT STA 590, PER MD-11 SRM 53-10- 14-2R, FIGURE 202, REPAIR 2, PG 8-10.
RH WING UPPER SURFACE - APPROX XORS 288 AFT SECTION OF LANDING GEAR DOUBLER - CORROSION AROUND FASTENER. REPAIRED PER EA 1-5730-T0350758
FLT LVL 360 STARTED NOTICING THE NR 2 OIL QTY DECREASE. AFTER REFERENCING QRH, CAPTAIN DECIDED TO SHUTDOWN THE NR 2 ENGINE. NO ABNORMAL INDICATION ON OIL PRESS OR OIL TEMP. NO OTHER ISSUES AFTER SHUTDOWN. LOWEST QTY SEEN WAS 3. AFTER INSTALLATION OF NR 2 ENG IAW W/C 71T0902, PERFORMED LEAK CHK AND ALL FOUND NORMAL. CARRIED OUT NR 2 ENG 40% AND 83% HIGH POWER RUN IAW AMM 71-00-00-5-1. ALL PARAMETERS WERE NORMAL. ACFT OK FOR SERVICE.
PASSING THROUGH 2000' DEPARTING ZSPD WITH LANDING GEAR RETRACTED, LEVEL 2 " BRAKE OVERHEAT" ILLUMINATED.COMPLIED WITH QRH AND EXTENDED LANDING GEAR. OVERHEATED BRAKE WAS ON #7 WHEEL W/MAX TEMPERATURE OBSERVED OF 568 DEG WHILE ALL OTHER BRAKES WERE LESS THAN 200 DEG. GEAR WAS RETRACTED W/IN SPEED LIMITS AFTER #7 BRAKE COOLED. PRECAUTIONARY REMOVED AND REPLACED #7 BRAKE TEMPERATURE SENSOR PER AMM32-46-01-4, ALL BRAKE TEMPERATURE WERE NORMAL. A/C OK FOR SERVICE.
PDIS 574 79-32 8368 08JAN19 LAX OPEN U LOGPAGES:3074658 ON CLIMBOUT PASSING FL 300, NOTICED NR 3 ENG OIL PRESSURE LOW, IN YELLOW, 22 PSI. NR 1 PSI WAS 55, NR 2 WS 54. TALKED TO MOCC & GOCC & DECIDEDTO RETURN TO LAX. RAN NR 1 AND NR 3 ENGINES AT DIFFERENT POWER SETTINGS, NR 3 CONSISTENTLY LAGGED NR 1 ENGINE 4-8 PSI. REMOVED AND REPLACED NR 3 OIL PRESSURE TRANSMITTER IAW AMM 79-33-01-4-1, LEAKS AND OPÿ½S CHECK GOOD. RAN ENGINE A DIFFERENT POWER SETTING, OIL PRESSURE WITHIN NORMAL OIL PRESSURE ENVELOPE PER JRH CHAPT 4.
UPON ARRIVAL FOUND L GEAR NR 6 BRAKE AREA ON FIRE, FOUND EVIDENCE OF HYD LEAK FROM NR 6 BRAKE PISTON. ALL TIRES PRESSURE ARE NORMAL, BRAKES TEMP ARE NORMAL ALSO. REMOVED AND REPLACED NR 6 BRAKE AS PER AMM 32-43-20-4 AND TESTED NORMAL PER AMM 32-46-00-5, NO LEAK. INSPECTED LEFT LANDING GEAR AND STRUT, NO OTHER DAMAGE FOUND
LEVEL 2 WING ANTI ICE DISAGREE DURING CLIMB OUT AT 3,000 FT MSL. RETURNED TO DEPARTURE, INSTALLED A NEW ANTI-ICE DUCT SEALS AT SLATS 3 - 4 AND 5 - 6 IAW MM 30-11-03-2. RT WING DECAY CHECKED GOOD MM 36-00-01-5. WING ANTI-ICE CHECKED GOOD IAW MM 30-11-00-5.
LEFT FWD WING SIDE INBD FLAP FWD OTBD HINGE PIVOT BORE WORN. FOUND THE INDB & OTBD FACE OUT OF LIMITS IAW CMM 57-44-07. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-87635F, P2, STEP 1F (1) AND STEP 1F (3). THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM6-2-100.
LEFT MLG DOOR CENTER UPPER FRAME FOUND TWO CRACKS. REPAIRED IAW EA 1-5280-T0336029 P1, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
UPPER CARGO DOOR, FWD HINGE LOBES ON AIRCRAFT, FOUND INSIDE DIAMETER WORN, EXCEEDED MAXIMUM PERMITTED LIMITS. FOUND THE NR 1 HOLE EXCEED LIMITS IAW SRM 52-30-16-1A. REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5310-T0335958, PART 1, STEP 2 AND 5,
LEFT WING TELESCOPIC DUCT DOOR CUTOUT INBD AND OUTBD BRACKET WORN XOS 464-470. REMOVED IAW SRM 51-31-01-0G AND FABRICATED A NEW CAP IAW DWG ARB1284, REV AC. INSTALLED THE NEW CAPS IAW SRM 51-35-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT NR 3 SLAT LOWER AFT SKIN EDGE INBD AND OTBD OF TELESCOPIC DUCT CUTOUT DOOR FOUND CHAFING MARKS. REPAIRED.
RIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 643 - 648 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING DROOP LEADING EDGE, INBD EDGE, CHAFED AT XDLE 309. REPAIRED IAW SRM 57-40-01-2R, FIG 202, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 610 - 615 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 625 - 627 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
DURING HFEC INSPECTION ON LEFT WING FIXED LEADING EDGE SLAT TRACK CUTOUT, AFT INBOARD CORNER CRACKED, 1/8 INCH IN LENGTH AT XOS 655. REPAIRED THE SKIN IAW SRM 57-40-02-2R, FIGURE 201, REPAIR 7. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING LEADING EDGE RIB DOUBLER AT XOS 789, FOUND CRACKED. THE DOUBLER WAS REMOVED IAW SRM 51-31-01-0G, FABRICATED A NEW DOUBLER IAW DRAWING ARB3954, REV K. INSTALLED THE DOUBLER IAW SRM 51-33-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING LEADING EDGE BEADED DOUBLER AT XOS 729 - 734 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM6-2-100.
LEFT WING LEADING EDGE BEADED DOUBLER AT XOS 692 - 698 FOUND 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 CARGO TRACK CROWN DAMAGED AT BS 1289, RBL 47.5. FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED FROM BS 1248 TO 1331 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO TRACK CROWN DAMAGED AT BS 1269, LBL 47.5. THE CARGO TRACK WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 201, ALLOWABLE DAMAGE 1. THE CARGO TRACK WAS REPLACED FROM BS 6-100 TO 1170 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM6-2-100.
LEFT WING LEADING EDGE CAVITY FRAME FOUND CRACKED AT XOS 801. THE FRAME WAS REMOVED IAW SRM 51-31-01-0G. FABRICATED A NEW FRAME IAW DRAWING ARB2922, REV B. INSTALLED THE NEW FRAME AIW SRM 51-35-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING LEADING EDGE BEADED DOUBLER AT XOS 629 - 633 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
DURING GEAR RETRACTION WE GOT A RIGHT MAIN UNSAFE GEAR UP INDICATION. RAN QRH PROCEDURE AND OBTAINED A GOOD GEAR UP INDICATION. DURING TROUBLESHOOTING FOUND RIGHT MAIN GEAR DOOR FELL OPEN WITH NO HYDRAULIC PRESSURE AND DOOR HANDLE IN THE UP POSITION. INSPECTED THE RIGHT MAIN GEAR DOOR IAW FIM 32-30-03, BLOCK 4. FOUND THE RIGHT GEAR DOOR UPLATCH ROLLER LINK VERY STIFF AND BINDING, CAUSING THE TARGET TO MISALIGN WITH THE SENSOR. CLEANED AND LUBRICATED THE DOOR LATCH ROLLER LINK IAW AMM 12-21-02-3, ACTUATED DOOR OBSERVED AS DOOR CLOSED AND POSITIVELY LATCHES UPLOCK. CHECKED DOOR AFTER 30 MINUTES, DOOR IS STILL UP AND LOCKED WITH NO HYDRAULIC PRESSURE.
RIGHT WING OUTBOARD NR 8 SLAT HAS A BROKEN DRIVE CABLE. REPLACED THE SLAT CABLES 84E & 84F IAW AMM 20-20-06-2. PERFORMED TENSION ADJUSTMENT OF THE DRIVE CABLE.
AFTER TAKE OFF WITH AIR MANUAL AND ICING ANTICIPATED, ENGINE & WING ANTI-ICE WAS ON & ARMED. WHEN THE WING ANTI-ICE VALVE ATTEMPTED TO OPEN LEVEL 2 WING ANTI-ICE DISAGREE ILLUMINATED. NO LONGER IN ICING CONDITIONS, DESELECTED WING ANTI-ICE AND ALERT EXTINGUISHED. BACK INTO ICING CONDITIONS AND SAME SCENARIO RESULTED. THIS TIME NOTICED NR 3 BLEED CLOSED AND OPENED IT THINKING THAT WAS PROBLEM, WHICH WAS FOLLOWED BY LEVEL 3 AIR MANIFOLD 3 FAIL WHICH IMMEDIATELY EXTINGUISHED WHEN NR 3 BLEED WAS CLOSED. DESELECTED WING ANTI-ICE AND NR 3 BLEED RETURNED TO NORMAL OPEN.NO FURTHER ALERTS. PSC-1 AND 2 SHOWED BOTH RT WING MANIFOLD FAIL LAST FLIGHT LEG, ESC SHOWED RT WING ANTI-ICE MANIFOLD FAIL ON FL-17. FOUND HEAVY BLEED LEAK ON CLAMP UPSTREAM NR 3 FLOW CONTROL VALVE, REPOSITIONED THE CLAMP PROPERLY IAW MM 21-51-01-02. COMPLIED WITH THE NR 3 PNEUMATIC DECAY TEST, PASSED IAW MM 36-00-01-05.
WHILE INSTALLING THE RT WING NR 4 L/E SLAT, FOUND THE SLAT DRIVE CABLE HAS A BROKEN BRACKET HOLDING THE PULLEY. JUST I/B OF DRIVE SLAT TRACK. , INSTALLED A NEW RT NR 4 SLAT RETRACT PULLEY AND BRACKET. TORQUED BOLTS TO BRACKET AND PULLEY IAW AMM 20-50-02-2. INSTALLED A NEW RT NR 4 SLAT RETRACT CABLE. CABLE RUN IS ROUTED AND CONNECTED IAW AMM 27-80-00-5. ADJUSTED CABLE TENSIONS FOR SLAT EXTEND AND RETRACT CABLES 6,7, & 8 AND SAFTIED ALL TURNBARRELS IAW AMM 11-27-80-00-5.
INFLIGHT AT FL 320 DEU'S 4 - 6 & MCDU 2 WENT BLANK & IMMEDIATELY GOT LEVEL 1 BUSS RT EMERGENCY AC OFF ALERT. ALSO OFF LIGHT RT EMERGENCY AC ON OVERHEAD & ELECTRICAL DISPLAY, MANY ASSOCIATED ALERTS, SELECT FADEC ALTERNATE, SINGLE LAND, ATC TRANSPONDER 2 FAIL, GPWS FAULT, IRU 2 ON BATTERY, PITOT HEAT FO, INDEPENDENT OPERATION ON MCDU, NO COMPARE ON PFD, TANK 2L AFT PUMP LOW. DUMPED 25K FUEL. INTERROGATED EPCU & FOUND REAC SENSE RELAY & INTERFACE UNDER CURRENT FAULTS. R & R RT EMERGENCY SENSE RELAY, R2-5157, IAW MM 24-25-01-00. ALL LISTED FAULTS CLEARED IAW FIM 24-25-01-00. REPLACED THE RT EMERGENCY AC BUSS FEED RCCB. RAN ALL ENGINES IAW JRH, TOOK APU & EXTERNAL POWER OFF LINE. ACFT OPERATES NORMAL. ACFT OK FOR SERVICE.
LOCKING LATCH FOR L1 DOOR, DISARM LEVER BROKEN OFF. R & R THE L1 DOOR ARMING LEVER. OPERATIONS CHECKED NORMAL IAW AMM 52-11-02-4. ACFT OK TO CONTINUE.
APPROXIMATELY 2 HRS INTO FLIGHT FUEL TOTAL & ALL 3 MAIN TANKS SHOWED FLUCTUATION OF 5000 LBS. QRH FUEL QTY ABNORMAL INDICATION COMPLIED WITH. RELEASED FOR SERVICE IAW MEL 28-01-01-02 CATEGORY AN EXPIRATION 16 MAY 16. TANK NR 2 FUEL TANK SYNOPTIC QTY DISPLAY INOPERATIVE. FUEL TO KNOWN QTY & AFTER REFUELING, VERIFY TANK NR 2 QTY WITH FUEL LEVEL STICKS & RECORD IN THE AML & EAML. OPERATE FSC IN MANUAL. TAIL FUEL MGMT INOPERATIVE. FQBU STORED T2 REF L P P SHORTED PROBE AT LAST LEG, NEED TO REPLACE LT COMPENSATOR IAW FIM 28-41-07-00. R&R MJP IN NR 2 TANK IAW AMM 28-41-40-4. R&R PROBE NR 1 IN NR 2 TANK IAW AMM 28-41-01-4. R&R TAIL TANK COMP PROBE IAW AMM 28-41-37-4. R&R TAIL TANK MJP IAW AMM 28-41-40-4. PERFORMED TEST IAW AMM 28-41-00-5. TEST PASSED.
RIGHT WING FIXED LEADING EDGE SKIN LOWER EDGE FOUND CHAFFED JUST OUTBOARD OF DROOP LEADING EDGE. REPAIRED IAW EA 1-5730-T0321987 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK CARGO LT LONGERON 15L, AT STATION 5-0, FOUND LONGERON END SPLICE CRACKED. REMOVED IAW SRM 51-33-01-0G. LONGERON SPLICE FABRICATED BY MACHINING IAW DWG AEA7654 REV C & INSTALLED IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
CENTER CARGO COMPARTMENT BILGE AREA LONGERON 51L , STATION 1601, FOUND WITH CORROSION. REPAIRED IAW EA 1-5310-T0322006A PT 1. WORK INSTRUCTION REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100. REFER TO WRI 53103463 FOR WORK DETAILS.
LEFT WING, NR 14 LE SLAT TRACK LOWER CUT OUT SKIN, FOUND CRACK AT STATION XOS 891. CRACKED AREA TRIM OUT & CARRIED OUT REPAIR IAW SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
CENTER CARGO COMPARTMENT BILGE AREA AT STATION 1701, LONGERON 48R, FOUND CORROSION. REPAIRED IAW EA 1-5310-T0321985 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 53103462 FOR WORK DETAILS.
LEFT WING, FIXED LE BEADED DOUBLER AT XOS 613, FOUND CRACK DURING OTBD SLAT DRIVE CABLE INSPECTION. CARRIED OUT INNER SKIN DOUBLER REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING, FIXED LE BEADED DOUBLER AT XOS 646, FOUND CRACK DURING OTBD SLAT DRIVE CABLE INSPECTION. CARRIED OUT DOUBLER REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING INBD AILERON, LOWER LE SKIN FOUND WORN AT APPROX STATION XIA 524.456. REMOVED IAW SRM 51-31-01-0G. NEW SKIN FABRICATED IAW DWG ARC 1250 REV D. NEW FABRICATED SKIN INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 57503433 & EA 1-5750-T0321909 PT 1, WINGS FLIGHT SURFACES, RT INBD AILERON, LOWER FWD SKIN, PN ARC 1250-2, WORN, FABRICATE REPLACEMENT FOR DETAILS.
TO CARRY OUT PERMANENT REPAIR ON LT WING LEADING SKIN AT NR 8 SLAT TRACK CUT OUT AT STATION XOS 547.588 IAW EA 1-5730-T0309161 PART 3 WORK INSTRUCTIONS. REPAIRED IAW EA 1-5730-T0309161A PT 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 57303453 FOR WORK DETAILS.
MAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX AT BS 1305.25 - 1315.42, LONGERON 26 - 27L, FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK L3 DOOR FWD JAMB LOWER WEB BOX AT BS 1250.75 - 1256.75, LONGERON 26L - 27L, FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED IAW GMM 6-2-100.
MAIN DECK R3 DOOR FWD JAMB LOWER WEB BOX AT BS 1250.75 - 1256.75, LONGERON 26 - 27R, FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK AT STATION 695, X= -27.5, FOUND CRACKED AS MARKED. SECTIONAL REPAIR CARRIED OUT ON SEAT TRACK AT MAIN DECK FLOOR STATION 685 - 745, X= -27.5 AREA IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK AT STATION 695, X= 8.5, FOUND CRACKED AS MARKED. SECTIONAL REPAIR CARRIED OUT ON SEAT TRACK AT MAIN DECK FLOOR STATION 685 - 745, X=8.5 AREA IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK, LT FRAME AT BS 1681, LONGERON 12L, FOUND REPAIR DOUBLER DAMAGED. REPAIRED IAW SRM 53-00-07-2R FIG 201 REPAIR 2. MAJOR REPAIR IAW GMM 6-2-100.
RIGHT WING TE LOWER CHORD STRAP SILL FOUND CRACK AT WING STATION XORS 402. REMOVED IAW SRM 51-31-01-0G. NEW STRAP SILL FABRICATED BY MACHINING IAW DWG ARC7008 REV C. NEW FABRICATED STRAP SILL INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
ANTI-SKID FAIL ON APPROACH. REPLACED WIRE HARNESS (AES9301-501), REF SWP 20-10-10.
WE HAD A RAPID DEPRESSURIZATION. PAIR HEARD THUMP, BUMP ON RT SIDE OF ACFT FLIGHT 370 1000Z ACFT STOPPED AT TAXIWAY FOR GVI EXTERIOR & NO DAMAGE FOUND. ACFT ON BLOCK IAW AMM 21-00-00-5. PERFORMED FUSELAGE PRESS DECAY TEST & PRESSURIZED CABIN PRESS TO 8 PSI & DECAY TEST PASSED. DURING PRESSURIZATION CABIN PRESS CHECK, ALL AIR CONDITIONED BAYS, TWO AIR CONDITIONED FLAPPER CHECK VLVS, ALL CARGO DOOR SEAL AREAS, ALL EXTERIOR DOOR SEALS, OFV AREA, AFT COMPARTMENT, FUSELAGE DRAIN VLVS & WW AREAS FOR LEAKAGE. ALL CHECKS ARE NORMAL WITHOUT LEAKING. R & R NR 1 CPC AS PRECAUTION IAW MM 21-31-04. NR 1 CPC FUNCTIONAL TEST NORMAL IAW MM 21-31-00-5.
NUMBER 1 ENG OIL PRESS DISPLAYED AN AMBER BOX, 15 MIN AFTER DEPARTURE, CLIMB POWER FL335 TO FL350. AT CRUISE, PRESS WENT INTO GREEN. AMBER BOX APPEARED AGAIN WITH A LOSS OF 3 QTS OIL, 20 INTO FLIGHT. PRECAUTIONARY SHUTDOWN INFLIGHT, WIND MILLED FROM 1422Z - 1446Z, QTY WAS AT 12 QTS AT SHUTDOWN. FOUND OIL CAP OPEN, SERVICED ENG WITH 6 QTS OIL. CLEANED COWLS, COMPLIED WITH WINDMILL MX IAW MM 72-00-05-6-1 STEP 11. CREW RAN ENG FOR 5 MIN, NO DEFECTS NOTED ALL ENG INDICATIONS WERE NORMAL. ACFT OK FOR SERVICE.
DURING PREFLIGHT CHECK FOUND, EMERGENCY POWER TEST FAIL. R & R BATTERY CHARGER IAW MM 24-34-03-4. PERFORMED OPERATIONS TEST OF THE BATTERY CHARGER IAW MM 24-34-03-5. TESTED OK. CHECKED EMER POWER TESTED GOOD.
DURING FCD ON LT WING FOUND POSSIBLE CRACK ON NR 8 SLAT TRACK. PERFORMED HFEC INSPECTION IAW NTSPM 06-10-01001. VERIFIED CRACK, COMPLIED WITH EA
RT WING FUEL PANEL DOOR INBD POSSIBLE CRACK. PERFORMED HFEC INSPECTION ON SUSPECTED CRACK IAW NDTSPM 06-10-01. CRACK RUNS PAST RIVET, FUELING DOOR REMOVED & ADJUSTED PANEL INBD TO FACILITATE REPAIR. REMOVED FASTENERS TO BE INCLUDED IN REPAIR. CUT OUT DAMAGED AREA IAW SRM 57-40-02. NEED NDT TO COME OUT & VERIFY CRACK REMOVED. PERFORMED HFEC, VERIFIED CRACK REMOVAL IAW NTSPM 06-10-01 010. FABRICATED FILLER WITH 7075-T6 090 MATERIAL ID MP1643962 IAW SRM 57-40-02 FIG 202. ROUGH CUT REPAIR DOUBLER WITH 6AL4V 063 TITANIUM MATERIAL ID MA2861790.
WHILE LEVEL AT FL370, RECEIVE A LEVEL 2, NR 3 ENGINE OIL FILTER ALERT. COMPLIED WITH QRH DIRECTIVE & SHUTDOWN NR 3 ENGINE. ALL OTHER ENGINE INDICATIONS WERE NORMAL. REMOVED MAIN CHIP DETECTOR & FOUND LARGE QTY OF LARGE METAL PARTICLES. REMOVED OIL FILTER & FOUND NO VISIBLE PARTICLES. REMOVED AND REPLACED NR 3 ENGINE IAW 71T0003 AND 71T0903. PERFORMED ENGINE RUN PER JRH. GROUND OPS CHECKED NORMAL.
RIGHT WING OTBD FLAP, INBD FWD HINGE OTBD ACTUATOR HOLE. WORN BUSHING ON OTBD ACTUATOR HOLE AT RT WING OTBD FLAP INBD FWD HINGE. REMOVED IAW MD11 CMM 20-20-07 REV 78. NEW BUSHING & WASHER FABRICATED IAW EA 1-5750-87638C PART 2 TITLE, WINGS - TE & TE DEVICES. RT OTBD FLAP INBD HINGE BRACKET REPAIR STEP 2, STEP 2 B 1, STEP 2 B 2 & STEP 3.
RIGHT WING OTBD FLAP, OTBD FWD HINGE OTBD ACTUATOR BUSHING WORN. DAMAGE REMOVED IAW CMM 20-20-07 REV 78. BUSHING FABRICATED & INSTALLED IAW EA 1-5750-87641C PT2 STEP 2 & 3.
RIGHT WING OTBD FLAP, OTBD FWD HINGE INBD ACTUATOR BUSHING WORN. DAMAGE REMOVED IAW CMM 20-20-07 REV 78. . BUSHING & WASHER FABRICATED & INSTALLED IAW EA 1-5750-87641C PT2 STEP 2, 2B, 3, 4 & 5.
RIGHT WING OTBD FLAP, INBD FWD HINGE INBD ACTUATOR HOLE. WORN BUSHING ON INBD ACTUATOR HOLE AT RT WING OTBD FLAP INBD FWD HINGE. REMOVED IAW MD11 CMM 20-20-07 REV 78. NEW BUSHING & WASHER FABRICATED & INSTALLED IAW 1-5750-87638C PART 2 TITLE, WINGS - TE & TE DEVICES. RT OTBD FLAP INBD HINGE BRACKET REPAIR STEP 2, STEP 2 B 1, STEP 2 B 2 & STEP 3.
RIGHT WING OTBD FLAP, OTBD FWD HINGE SIDE LOAD FITTING SPOT FACE FOUND CORRODED. REWORKED IAW CMM 57-44-09 REVISION 78. NEW SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.
LEFT WING OTBD FLAP, INBD FWD HINGE SIDE LOAD FITTING SPOT FACE FOUND CORRODED. REWORKED IAW CMM 57-44-08 REV 78. NEW SHIM FABRICATED AND INSTALLED IAW CMM 57-44-08 REV 78. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.
DURING FPI ACCOMPLISHMENT, RT WING OTBD FLAP OTBD FWD HINGE OTBD ACTUATOR MOUNT FOUND CORRODED IN BORE. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REV 78. REPAIRED IAW EA 1-5750-87641C PT2 STEP 2, 3, & 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.
DURING FPI ACCOMPLISHMENT, RT WING OTBD FLAP OTBD FWD HINGE INBD ACTUATOR MOUNT FOUND CORRODED IN BORE. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REV 78. REPAIRED IAW EA 1-5750-87641C PT2 STEP 2,2B, 3, 4 & 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.
DURING FPI ACCOMPLISHMENT, RT WING OTBD FLAP INBD FWD HINGE OTBD ACTUATOR MOUNT FOUND CORRODED IN BORE. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-87638C PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 119.
DURING FPI ACCOMPLISHMENT, RT WING OTBD FLAP INBD FWD HINGE INBD ACTUATOR MOUNT FOUND CORRODED IN BORE. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. BUSHING AND WASHER FABRICATED AND INSTALLED IAW EA 1-5750-87638C PART 2 STEPS 2,2B1, 2B2 & 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.
LEFT WING INBD FLAP OTBD AFT HINGE INBD PIVOT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03 REV 78. REPAIRED IAW EA 1-5750-87633A P2 STEP 2,3 & 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.
RIGHT WING INBD FLAP OTBD AFT HINGE INBD PIVOT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03 REV 78. REPAIRED IAW EA 1-5750-87634B P2 STEP 2,3 & 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.
RIGHT WING INBD FLAP OTBD AFT HINGE OTBD PIVOT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03 REV 78. REPAIRED IAW EA 1-5750-87634B P2 STEP 2, 3 & 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.
L1 DOOR AREA, FOUND FLOOR PANEL 227AF SPONGY. FLOOR PANEL REMOVED IAW AMM 53-21-04 REVISION 78. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION K AND INSTALLED IAW AMM 53-21-04 REVISION 78. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.
RIGHT WING OTBD FLAP INBD FWD HINGE PIVOT FOUND CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-87638C PART 2, STEP 2 AND STEP 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.
RIGHT WING OTBD FLAP OTBD FWD HINGE SIDE LOAD FITTING UPPER HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW EA 1-5750-87641 REV C PART 2 STEP 2,3 &4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.
RIGHT WING OTBD FLAP OTBD FWD HINGE SIDE LOAD FITTING FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW EA 1-5750-87641 REV C STEP 2, 3 AND 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.
RIGHT WING OTBD FLAP OTBD FWD HINGE SIDE LOAD FITTING BARREL NUT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW EA 1-5750-87641 REV C P2 STEP 2, 3 AND 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.
RIGHT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT & AFT SPOT FACE FOUND CORRODED. REWORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-09 REVISION 77. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 REV. 77. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REVISION 119.
RIGHT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-09 REVISION 77. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 REV 77. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REVISION 119.
RIGHT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW EA 1-5750-87641 REV C STEP 2,2A, 3 AND 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.
RIGHT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW EA 1-5750-87641 REV C STEP 2A, 3 AND 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.
RIGHT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. REPAIRED IAW CMM 57-44-08 REV 78 AND EA 1-5750-87638C PART 2 FIGURE 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.
RIGHT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-87638C PART 2 STEPS 2 & 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.
RIGHT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-87638C PART 2 STEPS 2 & 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.
RIGHT WING OTBD FLAP OTBD FWD HINGE PIVOT HOLE DIAMETER FOUND OUT OF LIMITS AFTER REPAIR BUSHING REMOVAL. HINGE PIVOT BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-87641C PT2 STEP 2 & 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.
RIGHT WING FIXED LE LOWER, FOUND CRACKED AT SLAT TRACK NR 11, CUTOUT AREA SKIN. REPAIRED IAW SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.
CRACK INDICATION FOUND APPROXIMATELY 0.3 INCHES IN LENGTH ON FUSELAGE SKIN DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT BS 695 LONGERON 50L. REPAIRED IAW SRM 53-00-01 FIGURE 201 REPAIR 1 REVISION 53 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 119
CENTER CARGO BAY BETWEEN BS 1661 & 1681, LONGERON SPLICE 29 RT CRACKED. NEW SPLICE FABRICATED IAW DRAWING AFA7830. DAMAGED LONGERON SPLICE REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.
LEFT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT SPOT FACES FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REV 78. SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 REV 78. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.
MAIN DECK CARGO DOOR LOWER FRAME SUPPORT FITTING DAMAGED. NR 1 HOLE REAMED TO 0.562 INCHES. HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED FOUND CRACK INDICATION STILL EXIST, APPROXIMATELY 0.040 INCH. SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 53. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 119
LEFT WING OTBD FLAP, INBD TE WEDGE FOUND DELAMINATED AT XOFH 458.74 TO XOFH 465.24. REPAIRED IAW EA 1-5750-T0305303 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119
PASSING FL 220, HEARD A LOUD BANG AND AIR OUT FLOW IN AVIONICS BAY. CABIN PRESSURE CONTINUED A SLOW CLIMB. AIR TURN BACK. ACFT UNABLE TO HOLD PRESSURE. LANDED WITHOUT INCIDENT. FOUND AVIONICS DOOR SEAL HANGING OUT. SEATED DOOR SEAL AND OPS CHECKED DOOR CLOSING AND OPENING, IAW AMM 52-41-01-5. ACFT STILL NEEDS DURING REINSPECT, FOUND DAMAGE TO THE AVIONICS DOOR SEAL. R & R SEAL, REF AMM 52-00-00-4. LEAK CHECK REQUIRED. ACCOMPLISHED LEAK CHECK OF AVIONICS EQUIPMENT DOOR. LEAK CHECKS GOOD. ACCOMPLISHED FUSELAGE PRESSURE DECAY CHECK IAW AMM 21-00-00-5. ACFT LEAK CHECKS GOOD. ACFT OK FOR SERVICE.
DURING SERVICE CHECK, FOUND THE EMERGENCY LIGHTS TEST WILL NOT PASS. REPLACED EMERGENCY LIGHT POWER SUPPLY REF MM 33-51-01-4 , TESTED NORMAL.
DURING PRE-FLIGHT EMERGENCY LIGHT TEST, RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY ONE LOW WARNING. PERFORMED ADJUSTMENT AND TEST OF EMERGENCY LIGHTS, EMERGENCY LIGHTS TEST PASS, AND OPERATE NORMALLY. ACFT OK TO CONTINUE.
DURING PRE-FLIGHT EMERGENCY LIGHT TEST, RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY ONE LOW WARNING. PERFORMED ADJUSTMENT AND TEST OF EMERGENCY LIGHTS, EMERGENCY LIGHTS TEST PASS, AND OPERATE NORMALLY. ACFT OK TO CONTINUE.
AFTER TAKE OFF "ICE DET SINGLE" LEVEL 1 ALERT FOLLOWED BY "AIR SYS 1 OFF" LVL 1 AND LVL 3 MANIFOLD FAIL FOR SYS 1. NO ANTI ICE WING OR ENG WAS ON. LEVEL 3 MANIFOLD FAIL WENT OUT AS AS THROTTLE WAS RETARDED. REPLACED DUCT.
DURING CLIMBOUT, WE WERE INSTRUCTED TO RETURN TO DEPARTURE DUE TO POSSIBLE DAMAGE DURING PUSHBACK. LEFT UPPER WINGLET MISSING STATIC WICKS. REPAIRED L/H UPPER WINGLET CAP PER PART 2 OF EA 1-5720-162680. INSTALLED UPPER WINGLET CAP IAW MM 57-31-01-4 A/C OK FOR SERVICE.
AFT CARGO DOOR AFT CUTOUT ANGLE FOUND WITH SURFACE CORROSIONS. ANGLE REPAIRED AS PER SRM 53-00-15 FIGURE 202 REPAIR 1 REVISION 48. INITIAL INSPECTION AT 18300 FC AND REPEAT INSPECTION AT 1250 FC PER ALI 53-10-06 REVISION 15. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.
UPON REMOVAL OF R3 DOOR SILL PLATE FOR REPAIR ACCESS FORWARD LOWER DOOR CUTOUT INTERIOR SKIN FOUND CORRODED.
AFTER REMOVAL OF APU EXHAUST DOOR RT FUSELAGE SKIN AT STA 2120 BENEATH APU EXHAUST DOOR FOUND CORROSION.
FORWARD CARGO DOOR FRAME, BS 897 BETWEEN LONGERON 38 AND LONGERON 40R MISREPAIRED. CARRIED OUT REPAIR AS PER SRM 53-00-15 FIGURE 202 REPAIR 1 REVISION 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.
LEFT STA 421, X= 28 FLOOR SUPPORT STRUCTURE FOUND CORRODED. FLOOR SUPPORT FABRICATED AS PER DRAWING ABA8303 REVISION A. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.
REMOVAL OF FLOOR PANEL LT STATION 5-103, X= 8.5, SEAT TRACK FOUND CORRODED. REPAIRED AS PER 53-00-52 FIGURE 201 REVISION 48. SEAT TRACK REWORKED AS PER DRAWING SP11530506 REVISION NEW. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.
RT MLG DOOR CENTER HINGE CRACKED. HINGE REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 48. R/H MAIN GEARWELL DOOR REMOVED AND REINSTALLED AS PER AMM 32-14-20-4 REVION 70.1. OPERATION CHECK CARRIED OUT SATISFACTOTY AS PER AMM 32- 14-20-220-801 REVISION 70.1 AND AMM 32-34-05-700-801 REVISION 70.1. REPAIR CLASSIFIED AS PER MAJOR AS PER GMM 6-2-100 REVISION 114.
AFT LOWER RUDDER SKIN FORWARD LOWER CORNER FOUND DAMAGED. REPAIRED IAW SRM 55-40-01, FIGURE 201, REV 48. EA 1-5540-156837. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
LT WING FIX L/E LOWER SKIN AT XW 344 MISREPAIRED. REPAIRED IAW DWG ARB1230, REV CEO E1-5100-7-5001B PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
DURING HIGH FREQUENCY EDDY CURRENT INSPECTION, FOUND A CRACK AT TRANSVERSE SKIN SPLICE, STATION 5-0, LONGERON 4LT ON THE CENTER ROW FASTENER NR 4 TOWARD NR 5 FASTENER APPROX .5" LONG COUNT FROM FORWARD. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 48. SPLICE MACHINED AS PER DRAWING AEA7634 REVISION D. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.
RIGHT BS 1299, LONGERON 27, FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 REVISION 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.
RIGHT STA 1541 X= -8.5 SEAT TRACK FOUND CORROSION. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REVISION 48. SEAT TRACK REWORKED AS PER DRAWING SP11530506 REVISION NEW. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.
CENTER CARGO COMPARTMENT BEAM JUST BELOW DOOR ACTUATOR MOUNTING FOUND CRACKED ON STA 1748 X= -108. REPAIRED IAW EA 1-5310-156830. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
CENTER CARGO COMPARTMENT BILGE AREA, LONGERON SPLICE BETWEEN STA 1681 AND 1701, LONGERON 50RT FOUND CRACKED. NEW LONGERON SPLICE FABRICATED AS PER SRM 53-00-05 REVISION 48. SPLICE REMOVED AND REPAIR AS PER SRM 51-31-01 REVISION 48. AND SRM 51-33-01 REVISION 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.
CENTER CARGO COMPARTMENT - LONGERON SPLICE AT STA 1531/ 5-123 LONGERON 30RH FOUND CRACKED. REMOVED AND REPLACED WITH NEW FABRICATED LONGERON SPLICE AS PER DRAWING A5A7112 REVISION D AND INSTALLED AS PER SRM 51-33-01 REVISION 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.
LEFT BS 1721, LONGERON 11, FRAME FOUND DENTED. R & R IAW SRM 51-31-01, REV 48. REPAIR DOUBLER FABRICATED IAW SRM 53-00-07, FIG 201, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
CENTER CARGO COMPARTMENT BILGE AREA. LONGERON SPLICE BETWEEN STA 5-112 AND 1541, LONGERON 46 LT FOUND CRACKED. R & R WITH NEW FABRICATED LONGERON SPLICE IAW DWG A5A7114 REV J AND INSTALLED IAW SRM 51-33-01, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
CENTER CARGO COMPARTMENT BILGE AREA LONGERON SPLICE AT STATION 1531 / 5-123, LONGERON 49 RT FOUND CORRODED. R & R WITH NEW FABRICATED LONGERON SPLICE IAW DWG A5A7114, REV J AND INSTALLED IAW SRM 51-33-01, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
CENTER CARGO COMPARTMENT BILGE AREA LONGERON SPLICE AT STA 1531/ 5-123 LONGERON 47 RT FOUND CRACKED. R & R WITH NEW FABRICATED LONGERON SPLICE IAW DWG A5A7116, REV D AND INSTALLED IAW SRM 51-33-01, REVISION 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
CENTER CARGO COMPARTMENT BILGE AREA LONGERON SPLICE BETWEEN STA 5-112 AND 1541, LONGERON 50 RT FOUND CRACKED. R & R WITH NEW FABRICATED LONGERON SPLICE IAW DWG A5A7114, REV J AND INSTALLED IAW SRM 51-33-01, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
CENTER CARGO COMPARTMENT BILGE AREA LONGERON SPLICE BETWEEN STATION 5-112 AND 1541, LONGERON 47LT FOUND CRACKED. R & R WITH NEW FABRICATED LONGERON SPLICE IAW DWG A5A7114, REVISION J AND INSTALLED IAW SRM 51-33-01, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.
RIGHT BS 555 X= -8.5 SEAT TRACK FOUND CORRODED. R & R IAW SRM 51-31-01, REV 48. SEAT TRACK REWORKED IAW DWG SP11530302 REV A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
RIGHT BS 540 X=-8.5 SEAT TRACK FOUND CORRODED. R & R SRM 51-31-01, REV 48. SEAT TRACK REWORKED IAW DWG SP11530302, REV A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.
LEFT BS 1659-1677 X= 8.5 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201, REV 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 113.
ON TAKEOFF, GEAR DID NOT RETRACT COMPLETELY. CREW MOVED THE GEAR HANDLE UPWARD TO THE TOP OF THE DETENT AND RED LIGHTS EXTINGUISHED. SPEED MOMENTARILY 240KTS. REDUCED TO BELOW 230 WHILE PROBLEM WAS WORKED. NO ADVERSE YAW NOTED. LANDED OK, WITHOUT INCIDENT. CHECKED LANDING GEAR CONTROL VALVE INPUT RODS FOR FROZEN ROD ENDS. SEVERAL FOUND AND FLAGS ATTACHED. REPLACED ROD ENDS ON P AND N. REPLACED ROD ASSY N. ADJUSTED P AND N PER 32-31-00-5. RIG CHECK GOOD. JACKED & SWUNG GEAR IAW AMM 07-11-00-2-0, PERFORMED SWING THREE TIMES WITH NO NOTED PROBLEMS. PERFORMED OPS CHECK PER 32-31-00-5. EXTENSION & RETRACT CYCLE TIMES GOOD. ACFT OK FOR SERVICE.
LEVEL 1 "FIRE DET 3 FAIL" ILLUMINATED 5:30 INTO FLIGHT, AT FIRST ALERT WAS INTERMITTENT FOR 15 MINUTES THEN REMAINED STEADY FOR REMAINDER OF FLIGHT. ACCESSED FDCU 3 THROUGH CFDS SHOWED UPPER RT LOOP B FAULT. ADJUSTED ROUTING OF LOOP, RESECURED RESPONDER. PERFORMED R-T-S PASSED. NORMAL OPS IAW MM 26-11-03-4. OK FOR SERVICE. FINAL CLOSED.
APU SMOKE (BOTTLE DISCHARGED, IAW SMF THERE IS OIL LEAKING FROM APU AND APU OIL QTY IS ZERO. IAW FLIGHT CREW DISCHARGED BOTTLE, NO FIRE WARNING INDICATION WAS PRESENT. NOTIFIED BY MX POSSIBLE APU FIRE. DISCHARGED ON BOTTLE. REMOVED AND REPLACED OUTBD. FIRE BOTTLE, REMOVED AND REPLACED AGENT NR 1 DISCHARGE CARTRIDGE. APU FIRE EXTINGUISHING SYSTEM OPS. CHECKED GOOD. APU R & R ON 26JAN11.
RTO AT 70 KTS DUE TO LEVEL 1 "FIRE DET 3 FAIL" INDICATION. INSPECTED NR 3 ENG FIRE LOOP HARNESS . FOUND WIRE AT CONNECTOR (TB2) ,WIRE (A) BROKEN AT TERMINAL END. PERFORMED RESISTANCE CHECKS FOR (B) LOOP FIRE DETECTORS, FOUND BROKEN RESPONDER AT UPPER LT(B) LOOP (DH22). ALL OTHER UPPER AND LOWER (B) LOOPS READING WITHIN NORMAL RANGE. RETERMINATED TERMINAL AT TB2. RELEASED FOR SERVICE IAW MEL: 26-11-01 OPS CKS ARE GOOD ALL CONNECTORS ARE REINSTALLED. RESPONDER LT ABOUT 9'CLOCK POSITION OF THE NR3 ENG .2500 IN. STUD PULLED FROM RESPONDER. RETERMINATED TERMINAL AT TB2. RELEASED FOR SERVICE PER MEL: 26-11-01. FOUND NR 3 ENG LOOP 'B' D22 RESPONDER AT FAULT,ALSO FOUND HARNESS DH22C TERMINAL BROKEN, R & R NR 3 FIRE LOOP 'B' RESPONDER & HARNESS PER AMM 26-11-03-4-0, FDCU3 R-T-S TEST PASSED PER AMM 26-11-02-5-0, CLOSED & LATCHED NR 3 ENG COWLING PER AMM 71-10-00-2.
AFTER T/O COULD NOT RAISE GEAR. RUN QRH AND RETURN. PULLED GEAR HANDLE UP TENSION FELT LOOSE, ALSO ALL 4 LIGHT BOTH PRI AND SECONDARY WERE EITHER ALL RED, WITH HANDLE UP OR ALL GREEN WITH HANDLE DOWN.
MAIN DECK CARGO - UPON REMOVAL OF CTR TANK FLOOR PANEL FOR THRUST REVERSER MODIFICATION FOUND CTR TANK AFT UPPER SURFACE AT APPROX STA 1219 X = 107 WITH SURFACE CORROSION. COMPLIED WITH E.A. 1-5710-132333, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 109.
MAIN DECK CARGO - UPON REMOVAL OF CTR TANK FLOOR PANEL FOR THRUST REVERSER MODIFICATION FOUND CTR TANK FWD UPPER SURFACE AT APPROX STA 1219 X = 107 WITH SURFACE CORROSION. REPAIR CARRIED OUT IAW EA NR 1-5710-132333, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 109.
MAIN DECK CARGO, LT STA 535 FRAME ADJACENT TO 9-G NET LOWER SUPPORT YOKE FITTING FOUND CHAFED. REPAIR CARRIED OUT AS EA NR 1-5310-132334, THIS REPAIR IS CLASSIFIED AS MAJOR, IAW GMM 6-2-100 REVISION 109.
DURING HFEC OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA XORS 690 AND STA XORS 700, 07 EACH FASTENER HOLES FOUND CRACKED INDICATION. REPAIR IAW EA1-5710-132338.
CABIN, FUSELAGE FRAME EXISTING REPAIR DOUBLER AT STA 1701 LONGERON 12 LT FOUND DEFORMED. REPAIR IAW SRM 53-00-07 FIG 201 REPAIR 2 REV 42 (MAJOR REPAIR).
RT OVER WING BODY FAIRING ENCLOSED AREA BELOW R3 DOOR, APPROX AT STA 1249 LONGERON 28 RT FOUND CORRODED. REPAIR IAW SRM 51-33-01, REV42.
DURING HFEC OPEN HOLE INSP AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA XORS 690 AND STA XORS 700, 05 EACH FASTENER HOLES FOUND CRACKED INDICATION. REPAIR IAW EA1-5710-132339.
CTR LANDING GEAR WHEEL WELL, FWD BULKHEAD DOUBLER FOUND CRACKED. R & R IAW SRM 51-31-01 REVISION 42. NEW DOUBLER FABRICATED IAW DWG AE A0526 REVISION NC AND EA NR 1-5310-132336, REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 109.
RT WING OTBD AILERON T/E LOWER SURFACE FOUND DELAMINATED. RT WING OTBD AILERON R & R IAW AMM 27-10-30-4 REVISION 64. OPS TEST OF THE AILERON NEUTRAL AND RANGE OF MOVEMENT CARRIED OUT IAW AMM 27-10-00-710-802 REVISION 64. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REVISION 109.
RT WING NR 3 SPOILER TOP SURFACE FOUND CRACKED. RT WING NR 3 SPOILER R & R IAW AMM 27-60-30-4 REVISION 64. FUNCTIONAL TEST OF THE SPOILER LATERAL CONTROLS CARRIED OUT IAW AMM 27-61-00-730-801 REVISION 64. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 109.
RT WING NR 4 SPOILER TOP SURFACE FOUND DENTED. DENTED AREA FOUND CRACKED AFTER REPAIR IAW SRM 51-21-01 REV 42. CRACKED SKIN REPAIRED IAW SRM 51-71-00, PARAGRAPH 19 REV 2.
AT FL320 APPROX 40 MIN INTO FLT A/P 2 EXECUTED A SLOW UNCOMMANDED CLIMB TO FL 325. PRIOR TO PUSHBACK HAD LVL 2 FCC 2A & 2B DATA FAULT. STN MX RESET C/BS & ALERTS WENT AWAY. SWITCHED TO A/P 1 FOR REMAINDER OF FLT WITH NO FURTHER PROBLEMS. ADDITIONAL INFO ON PRE FLT THERE WAS A WATER LEAK IN GALLEY WITH A SUBSTANTIAL AMOUNT OF WATER LEAKING UNDER FLOOR CONTINUED ON LOG SHT 1550574. FURTHER INFO LATER IN FLT RETRIED A/P 2 AT FL 360 HELD ALT FOR APPROX 10 MIN THEN STARTED 100 FPM DESCENT. ARRESTED DESCENT APPROX 200 FT LOW & REENGAGED A/P 1 INSPECTED E&E COMPT FOR WATER NONE PRESENT. CHKD LAST FLT FAULTS NO FAULTS FOR NR 2 FCC. PERF FC C RTS REF AMM 22-00-00-5 NO FAULTS. STATUS DOWNGRADED TO CAT 2/CK 2.
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLES C AND D. MAIN CARGO DOOR LOWER JAMB NO. 3 AT HOLES C AND D CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLE C. MAIN CARGO LOWER JAMB NO. 1 FITTING AT HOLE C CARRIED OUT BUSHING REPAIR AS PER SRM 53-50 -00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLE A. MAIN CARGO DOOR LOWER JAMB NO. 2 FITTING CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOLUME I AT HOLE A. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
CENTER CARGO STA 1541 TO STA 1561 LONGERON 52 FOUND CORRODED. CENTER CARGO STA 1541 TO STA 1561 LONGERON 52 REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK FRAME AT LEFT STA 1741 APPROXIMATELY LONGERON 11 TO LONGERON 12 FOUND WITH DENT. CARRIED OUT REPAIR AS PER SRM 53-30-00, FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION TO BE CARRIED OUT AT 14,000 CYCLES AND THEREAFTER REPETITIVE INSPECTIONS AT EVERY 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK SEAT TRACK AT STA 610, X = -8 FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES B AND D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLES A, B, C AND D. MAIN CARGO DOOR JAMB NR 6 SUPPORT FITTING REMOVE AND REPLACED AS PER SRM 51-31-01 VOL II. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
RIGHT WING, TRAILING EDGE SPAR UPPER CAP AT STA XORS 675 FOUND 01 EACH FASTENER HOLE ELONGATED. REPAIR CARRIED OUT AS PER E.A. 1-5710-122430, THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING, TRAILING EDGE REAR SPAR UPPER CAP AT STA XORS 746 FOUND 01 EACH FOUND FASTENER HOLE ELONGATED. REPAIRED AS PER E.A. 1-5710-122430, THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING, TRAILING EDGE REAR SPAR UPPER CAP AT STA XORS 897 FOUND 01 EACH FASTENER HOLE ELONGATED. FASTENER HOLE REPAIR CARRIED OUT AS PER EA 1-5710-122430, THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK SEAT TRACK CROWN AT STA 885, X = -8 FOUND CHAFED. MAIN DECK SEAT TRACK AT STA 849 TO STA 909, X = -8 CARRIED OUT REPAIR AS PER SRM 53- 70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
EMPENNAGE, AFT ACCESSORY COMPARTMENT INTERIOR RIGHT FUSELAGE SKIN AT AROUND BS 2154, (BELOW FIRE EXTINGUISHER BOTTLES) 01 LOCATION FOUND WITH CORROSION. REPAIRED AS PER SRM 53-20-00 FIGURE 13 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT FUSELAGE EXTERNAL LONGERON END FITTING AT STA 1521.000 LONGERON 29 FOUND WITH CRACK. HFEC INSPECTION CARRIED OUT PER DAC NDT SPM REVISION 13.06-06-10-01.001, CRACK IS APPROXIMATELY 1 INCH LONG. CRACKED SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. NEW SPLICE REWORKED AS PER DRAWING AEA7643. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT MAIN LANDING GEAR TORQUE LINK SHEARED DURING PUSH-BACK.
LEFT MAIN LANDING GEAR TORQUE LINK SHEARED DURING PUSH-BACK.
LEFT MAIN LANDING GEAR TORQUE LINK SHEARED DURING PUSH-BACK. COMPLETED TORQUE LINK INSTALLATION IAW MD-11 MM 32-11-12-4
RIGHT WING, REAR SPAR UPPER CAP AT ABOUT STA XORS 1044 FOUND WITH CORROSION REFER TO SNRM NO.: N00247 (SDR TRACKING NO.: 07-1605). COMPLIED WITH FEDEX EA NR 1-5710-109869, WINGS, RIGHT REAR SPAR UPPER CAP CORROSION COMMON TO STATIONS XORS = 1039 THROUGH XORS = 1047 REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CRACKED. LT WING OUTBD FLAP ASSY REMOVED AND REPLACED AS PER MD11 CMM 57-52-04. LT OUTBD FLAP ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-830-805, FOUND SATIS.
RIGHT WING OUTBOARD FLAP INBOARD WEDGE TRAILING EDGE UPPER SURFACE FOUND DELAMINATED RIGHT WING OUTBOARD FLAP INBOARD WEDGE REMOVED AND REPLACED AS PER AMM 20-50-02, P/N ON: ARC4363-2, S/N ON: 177679-9.
RIGHT WING OUTBOARD FLAP CENTER TRAILING EDGE LOWER SURFACE FOUND DELAMINATED 4" BY 4" (LENGTH X WIDTH). [SUP 05-15-07] REMOVED AND REPLACED AS PER AMM 20-50-02.
LEFT WING OUTBOARD FLAP INBOARD AFT HINGE FORWARD FITTING INBOARD CENTER HOLE FOUND WITH CORROSION DURING ACCOMPLISHMENT OF EO 1-5750-7-5008. ORIGINAL HOLE DIAMETER = 0.580"; FINAL HOLE DIAMETER = 0.656". [SUP 05-14-07] COMPLIED WITH FEDEX EA 1-5750-109875, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.
TAIL CONE COMPARTMENT, LT HINGE FITTING FOUND CRACKED, VIEWED FROM AFT ACCESSORY COMPARTMENT. [SUP 05-14-07] REMOVED & REPLACED AS PER DAC DWG AJC7346 AND SRM 51-31-01 VOL.II. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.
LEFT WING OUTBOARD FLAP INBOARD AFT HINGE FORWARD FITTING INBOARD CENTER HOLE FOUND WITH CORROSION DURING ACCOMPLISHMENT OF EO 1-5750-7-5008. ORIGINAL HOLE DIAMETER = 0.580"; FINAL HOLE DIAMETER = 0.657". [SUP 05-14-07] COMPLIED WITH FEDEX EA 1-5750-109875, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.
FOUND LEFT MAIN FRAME STA 535 AT 9G NET SUPPORT YOKE AREA FOUND CHAFFED AT LONGERON 23L. [SUP 05-10-07] REPAIR CARRIED OUT AS PER FEDEX AIRCRAFT ENGINEERING STANDARD REWORK DRAWING NR: SRZ 53-503. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING, OUTBOARD FLAP INBOARD TRAILING EDGE UPPER SURFACE FOUND DELAMINATED 5" BY 7" (LENGTH X WIDTH). REMOVED AND REPLACED AS PER AMM 20-50-02. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
LEFT WING, CRACK INDICATIONS (APPROX 0.0156 INCH DEPTH ) REVEALED IN FIVE (5) EACH FASTENER HOLES TOWARDS THE EDGE OF ACCESS CUTOUT LOWER SKIN ACCESS DOOR (BETWEEN XOR=683.4 AND XOR=713.6). REPAIRED AS PER FEDEX EA 1-5710-109878, REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.
LEFT WING LEADING EDGE CAVITY STIFFENER FOUND WITH APPROX 0.25 INCH CRACK AT XOS 667. [SUP 05-15-07] REPAIRED AS PER FEDEX EA 1-5720-109874, WINGS - LEADING EDGE STRINGER - CRACK REPAIR. REPAIR CLASSIFIED AS MINOR PER GMMM 6-2-100.
RIGHT WING, CRACK INDICATIONS (APPROX 0.0156 INCH DEPTH) REVEALED IN SIX (6) EACH FASTENER HOLES TOWARDS THE EDGE OF ACCESS DOOR CUTOUT LOWER SKIN (BETWEEN XOR=683.4 AND XOR=713.6). [SUP 05-14-07] REPAIRED AS PER FEDEX EA 1-5710-109877, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING, LEADING EDGE CAVITY AT ABOUT XOS 774 STRIP ANGLE FOUND WITH APPROX 0.3124 INCH CRACKED. [SUP 05-14-07] RT FIXED LEADING EDGE STRINGER, CRACK REPAIR. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100.
CENTER LANDING GEAR, WHEEL WELL BRACKET LOCK LINK CHAMPER FOUND WORN. [SUP 05-04-07] REPAIRED AS PER SRM 53-40-00 VOLUME I, FIGURE 10. REPAIR CALSSIFIED AS MINOR PER GMM 6-2-100.
RIGHT WING, LEADING EDGE CAVITY AT ABOUT XOS 659 STRIP ANGLE FOUND WITH APPROX 0.5 INCH CRACKED. [SUP 05-14-2007] FIXED LEADING EDGE STRINGER, CRACK REPAIR. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.
RIGHT WING, REAR SPAR LOWER CAP AT ABOUT STA XORS 1046-1050 FOUND WITH CORROSION. [SUP 05-14-07] REMOVED AS PER SRM 51-21-01 VOLUME II. MATERIAL REMOVED= 0.064", ORIGINAL THICKNESS= 0.108", REMAINING THICKNESS= 0.044", AND EXCEEDED LIMITS AS PER SRM 57-20-00 VOLUME I, FIGURE 16. REPAIR CARRIED OUT ON REWORKED AREA AS PER FEDEX EA 1-5710-109870. REPAIR CLASSIFIED AS MAJOR PER GMMM 6-2-100.
RIGHT WING LEADING EDGE PERFORMANCE FILLET OUTBOARD RIB FOUND CRACKED. [SUP 05-16-07] RIB REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING, NR 1 SLAT INBOARD RIB FOUND WITH 0.05 INCH CRACKED. [SUP 05-14-07] RIB REMOVED & REPLACED ON RT WING, NR 1 SLAT INBOARD AS PER SRM 51-35-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1721 AT LONGERON 12L FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1721 AT LONGERON 12R FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1701 AT LONGERON 12L FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1701 AT LONGERON 12R FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1681 AT LONGERON 12L FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1681 AT LONGERON 12R FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING, REAR SPAR UPPER CAP AT ABOUT STA XORS 1042 FOUND WITH CORROSION. [SUP 05-14-07] REMOVED AS PER SRM 57-21-01 VOLUME II. MATERIAL REMOVED =0.043" ORIGINAL THICKNESS =0.136", REMAINING THICKNESS =0.093" AND FOUND EXCEEDED LIMITS AS PER 57- 20-00 VOLUME I FIGURE 16. REPAIR CARRIED OUT AS PER FEDEX EA 15710-109869.
LEFT WING, REAR SPAR UPPER CAP SURFACE AT ABOUT STA XORS 1046 FOUND WITH CORROSION. [SUP 05-14-07] REPAIRED AS PER FEDEX EA 1-5710-109868, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING, LEADING EDGE SLAT NR 3 TRAILING EDGE LOWER SURFACE FOUND WITH GOUGE MARK. [SUP 05-16-07] SURFACE SMOOTHENED OFF AND REPROTECTED AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
LEFT WING NR 1 SLAT INBOARD RIB ATTACHED TO THE PERFORMANCE FAIRING FOUND WITH ONE (1) INCH CRACK AT THE LOWEST STUD AREA. [SUP 05-14-07] REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.
RIGHT WING, INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED. [SUP 05-15-07] REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-22-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
LEFT WING, INBOARD FLAP VANE LOWER SURFACE FOUND WITH EXISTING REPAIR WHICH IS NOT COVERED BY SRM. [SUP 05-16-07] REMOVED AND REPLACED AS PER AMM 27-50-22-04. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-22-05. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
LEFT MAINFRAME STA 535 AT 9G NET SUPPORT YOKE AREA FOUND CHAFED. [SUP 05-10-07] REPAIR CARRIED OUT AS PER FEDEX AIRCRAFT ENGINEERING STANDARD REWORK DRAWING NR: SRZ 53-503. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING, TELESCOPIC DUCT CUT-OUT FOUND WITH 0.4375 INCH CRACK. [SUP 05-14-07] REPAIRED AS PER SRM 57-10-00 VOLUME I (T.R.), FIGURE 42. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING, TELESCOPIC DUCT CUT-OUT FOUND WITH 0.5 INCH CRACK. [SUP 05-14-07] REPAIRED AS PER SRM 57-10-00 VOLUME I (T.R.) FIGURE 42. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
RIGHT WING, LEADING EDGE SLAT TRACK NR 14 CUT-OUT FOUND WITH 0.4375 INCH CRACK. [SUP 05-16-07] CUTOUT CRACKED AREA TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING, LEADING EDGE SLAT TRACK NR 12 CUT OUT FOUND WITH 1.5 INCH CRACK. [SUP 05-14-07] TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
NOSE LANDING GEAR, LEFT TRUNNION FITTING WITH 1.25 INCH CRACKED. [SUP 05-14-07] REPAIRED PER SRM 53-40-00 VOLUME I, FIGURE 23 OPTION 2. COMPLIED WITH FEDEX EA 1-5310-109864. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.
PASSING 18,000 AFTER TURNING WINSHIELD ANTI ICE ON GET ACRID, ELECTRICAL SMELL AND FUMES. LWR R/L 1/4 OF FRONT WINDSCREENS FOGGED OVER. SMELL SOON DISSIPATED. VISUALLY INSPECTED WINDSHIELDS AND ASSOCIATED WIRING, NO DEFECTS FOUND. PERFORMED ADJUSTMENT AND TEST OF WINDSHIELD ANTI ICE PER MM 30-41-00-5, OPS CHECKED NORMAL. HEAT FELT ON WINDOW SURFACES WAS CORRECT FOR BOTH NORMAL AND HIGH POSITIONS. COULD NOT DUPLICATE. OK FOR SERVICE.
CLIMBING THROUGH 10,000 FEET & LOUD HIGH PITCH NOISE FOLLOWED BY STRONG ELECTRIC ODOR. RETURNED TO KIX. NOISE STOPPED IN DESCENT. ODOR RETURNED IN DESCENT. ACN RELEASED FOR SERVICE PER MEL/CDL: 21-26-06-B CATEGORY: C EXPIRATION: 02MAY06 MEL 21-26-06-B: NR 3 AVIONICS RACK COOLING FAN INOP. PER CREW DEBRIEF, NOISE CAME FROM UNDER THE FLOOR, DID NOT FIND SMOKE. T/S AND FOUND AVIONICS RACK FAN 3 C/B TRIPPED. TRIED TO RESET BUT IT TRIPS IMMEDIATELY AFTER RESET. REMOVED AVIONICS RACK FAN-3 AND FOUND MOTOR BURNED OUT WHICH CAUSED STRONG ELECTRIC ODOR, NEEDS TO BE REPLACED. PER MOCC INSTRUCTION, RAN APU AND CHECKED ODOR FOR PACKS OUTLET AIR, NO SMELL CAME OUT FROM ALL THREE PACKS.
CENTER CARGO BAY, STA 1841 LOWER FRAME SKIN FOUND DAMAGED. CENTER CARGO COMPT STA 1841 LOWER FRAME DAMAGE WEB REMOVED AND NEW WEB INSTALLED AS PER DRAWING AGA 7170, SRM 51-33-01 VOL II AND SRM 51-35-01, VOL II. NEW WEB P/N FX AGA 7170-3 LT AND FX AGA 7170-4 RT FABRICATED PER DRAWING AGA 7170. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.
FOUND RHW IN SPAR UPPER SKIN AT APPROX XORS 280 STRINGER 13 FOUND WITH SKIN BULGE. CARRIED OUT REPAIR AS PER EA 1-5720-87644.
CRACK FOUND ON RT AFT CTR FASTENER HOLE AT BANJO NR 4 FTG FAYING SURFACE. VIEW LOOKING I/B AT 2 O'CLOCK DIRECTION. CRACK LENGTH FROM THE EDGE OF THE BANJO NR 4 FTG APPROX 1/8 INCH LONG. CORRECTIVE ACTION: SNRM N1614: BANJO FTG R/H NO.4 AFT CENTER FASTENER CRACK HOLE REPAIRED AS PER SRM 55-20-00 FIG. 3 VOL.I. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.
FOUND CENTER CARGO COMP AFTER REMOVAL OF CRACKED LONGERON SPLICE AT STA 1641 TO 1661 LONGERON 44R FOR REPLACEMENT, LONGERON 44R FOUND CRACK AT STA 1646 TO 1651. REPAIRED AS PER SRM 53-10-00.
FOUND CENTER CARGO COMP, AFTER REMOVAL OF CRACKED LONGERON SPLICE AT STA 1641 TO 1661 LONGERON 44R FOR REPLACEMENT, LONGERON 44R FOUND CRACK AT STA 1652 TO 1658. REPAIRED AS PER SRM 53-10-01.
RT WING DROOP L/E UPPER SKIN FOUND WITH CRACK. RT WING DROOP L/E UPPER SKIN CRACK CARRIED OUT REPAIR AS PER SRM 57- 10-00 FIG.26 VOL.I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
AFT CABIN STA 2007 RBL 103 TO 107, Z=-18, AFT PRESSURE BULKHEAD T-CHORD FOUND REPAIR PATCH . SNRM N0845: WORK ACCOMPLISHED AS PER EA#1-5310-87647 TITLE: FUSELAGE- MAIN FRAME- PRESSURE BULKHEAD BODY STA. Y = 2007.000, TEE CHORD REPAIR. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100.
CENTER CARGO COMPT STA 1841 RT LOWER FRAME ASSY CORNER FOUND CRACK DURING REMOVAL. REPAIRED PER SRM 53-00-00 FIG.3 VOL.I. NEW ANGLE P/N FX AGA 7171-20 FABRICATED PER DRAWING AGA 7171. MAJOR REPAIR PER GMM 6-2-100.
AFT INTERMEDIATE FUSELAGE, FLOORBEAM LOWER CAP FOUND CRACK AT STA 1801 LBL 8 TO RBL 8. REPAIRED AS PER EA 1-5310-87655. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.
HORIZ STAB RT BARREL NUT BORE NR 8 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 24. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB RT BARREL NUT BORE NR 10 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 25. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
FWD CARGO COMPT AT STA 6-30 LT LOWER INTERCOSTAL ASSY BETWEEN LONGERON 42 TO LONGERON 43 FOUND CORRODED DURING REMOVAL.
FWD CARGO COMPT AT STA 6-30 RT LOWER FRAME ASSY BETWEEN LONGERON 42 TO LONGERON 43 FOUND CORRODED DURING REMOVAL. FRAME REMOVED AS PER SRM 51-35-01 VOL.II. NEW FRAME FABRICATED AS PER DWG ACA 7049 AND NEW FRAME INSTALLED AS PER SRM 51-35-01 VOL.II. MINOR REPAIR PER GMM 6-2-100.
HORIZONTAL STAB RT BARREL NUT BORE NR 35 FOUND WITH CORROSION. HOR. STAB. BARREL NUT BORE 35 RT REPAIRED IAW STABILIZERS-HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08 EA1-5510-87628, ATTACHMENT 45. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZONTAL STAB LT BARREL NUT BORE NR 35 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 39. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZONTAL STAB LT BARREL NUT BORE NR 4 FOUND WITH CORROSION. HORIZONTAL STAB BARREL NUT BORE NR 4 LT REPAIRED IAW STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 43. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
FWD CARGO COMPT ALONG STA 6-50 BETWEEN L51L AND L51R, FRAME CHORD CORRODED. CORROSION REMOVED, FOUND OUT OF LIMITS IAW SRM 53-00-01 AND REPAIRED IAW SRM 53-00-01. MAJOR REPAIR PER GMM 6-2-100.
LT WING NR 8 SLAT INNER SURFACE FOUND CRACKED AT SLAT TRACK NR 18 AREA. CARRIED OUT REPAIRED AS PER SRM 57-10-00 FIG 10, VOL I. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.
RT HORIZ STAB BARREL NUT BORE NR 2 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 33. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
RT HORIZ STAB BARREL NUT BORE NR 18 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 35. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
RT HORIZ STAB BARREL NUT BORE NR 20 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 37. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
RT HORIZ STAB BARREL NUT BORE NR 28 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 40. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
RT HORIZ STAB BARREL NUT BORE NR 30 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 41. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
RT HORIZ STAB BARREL NUT BORE NR 32 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 42. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
RT HORIZ STAB BARREL NUT BORE NR 34 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 44. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
LEFT HORIZ STAB BARREL NUT BORE NR 19 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 36. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
LEFT HORIZ STAB BARREL NUT BORE NR 17 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 34. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
LEFT HORIZ STAB BARREL NUT BORE NR 3 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 38. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB RT BARREL NUT BORE NR 4 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 23. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
LOWER FUSELAGE, AIRCON COMP 1 AT STA 535 TO 547 LONG 32-33 FOUND EDGE CRACK. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. MAJOR REPAIR PER GMM 6-2-100.
RT WING O/B FLAP MOUNTED L/E UP-STOP FITTING SUSPECTED CRACKED. RT WING O/B FLAP MOUNTED L/E UP-STOP FITTING CRACKED REMOVED AND REPLACED AS PER SRM 51-35-01 AND SRM 51-33-01 VOL.II. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
LTW O/B FLAP MOUNTED L/E UP, STOP FITTING SUSPECTED CRACKED. LT WING O/B FLAP MOUNTED L/E UPSTOP FITTING CRACKED. REMOVED AND NEW FITTING, REPLACED AS PER SRM 51-31-01 VOL II. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
HOR STAB RT BARREL NUT BORE NR 26 FOUND WITH CORROSION. SPLICE FITTING AT BARREL NUT BORE NR 26R REMOVED AND NEW FITTING INSTALLED IAW SRM 51-32-01 VOL.II, SRM 51-38-01 VOL.II, SRM 51-33-01 VOL.II AND E1-5510-7-5000 D1 PT1. MINOR REPAIR I.A.W FEDEX GMM 6-2-100.
HORIZ STAB RT BARREL NUT BORE NR 24 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 30. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB RT BARREL NUT BORE NR 14 FOUND WITH CORROSION. REMOVED AND NEW FITTING INSTALLED IAW SRM 51-32-01 VOL.II, SRM 51-38-01 VOL.II, SRM 51-33-01 VOL.II AND E1-5510-7-5000 D1 PT1. MINOR REPAIR I.A.W FEDEX GMM 6-2-100.
HORIZ STAB LT BARREL NUT BORE NR 3 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 26. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB LT BARREL NUT BORE NR 7 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 27. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB LT BARREL NUT BORE NR 15 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 31. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB LT BARREL NUT BORE NR 27 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 32. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB RT BARREL NUT BORE NR 16 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 28. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB RT BARREL NUT BORE NR 22 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 29. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
MID CABIN- CENTER AUX TANK UPPER SURFACE AT STA 1199 TO 1219 Z=-31 FOUND EXISTING PATCH REPAIR. CENTER AUX TANK UPPER SURFACE AT STA 1199 TO 1219 Z=-31 EXISTING PATCH. REPAIR EVALUATED AND CARRIED OUT AS PER EA NR 1-5720-93203 TITLE: WINGS, PLATES AND SKINS, CENTER WING/AUX TANK UPPER SKIN PANEL ASSEMBLY EXISTING REPAIR. PREVIOUSLY REPAIRED AREA CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.
FWD CARGO COMPT, ALONG STA 879 BETWEEN L52R AND L50L, FRAME ATTACHED CHORD WEB CORRODED. REPAIRED AS PER SRM 53-00-01 FIG.9 VOL.I. MAJOR REPAIR PER GMM 6-2-100.
LOWER FX: DENT ON FX EXTERIOR SKIN AREA ALONG STA 695, ALONG L-50L. REPAIRED PER SRM 53-20-00 FIG.6 VOL I, EO 1-5100-7-5001.
DENT ON FX EXTERIOR SKIN AREA ALONG STA 635, ALONG L-49L. REPAIRED PER SRM 53-20-00 FIG.6 VOL I, EO 1-5100-7-5001.
LOWER FX, DENT ON FX EXTERIOR SKIN AREA ALONG STA 1019, BETWEEN L-49L AND L-50L. REPAIR CARRIED OUT PER SRM 53-20-00 FIG.6 VOL I, EO 1-5100-7-5001.
DENT ON FX EXTERIOR SKIN AREA BETWEEN STA 700 AND STA 702, ALONG L-50L. REPAIRED PER SRM 53-20-00 FIG.6 VOL.I, EO 1-5100-7-5001.
HORIZ STAB RT BARREL NUT BORE NR 27 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA1-5510-87628, ATTACHMENT 19. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB LT BARREL NUT BORE NR 30 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 17. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB RT BARREL NUT BORE NR 33 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 22. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB LT BARREL NUT BORE NR 24 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 16. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB LT BARREL NUT BORE NR 34 FOUND WITH CORROSION. SNRM N2606: DUPLICATE CARD. REFER TO SNRM N2663 WITH SDR TRACKING NO.05-3103 FOR REPAIR DETAILS.
HORIZ STAB RT BARREL NUT BORE NR 29 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 20. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB RT BARREL NUT BORE NR 29 FOUND WITH CORROSION. SNRM N2607: DUPLICATE CARD. REFER TO SNRM N2659 WITH SDR TRACKING NO.05-3099 FOR REPAIR DETAILS.
HORIZ STAB LT BARREL NUT BORE NR 34 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 18. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB LT BARREL NUT BORE NR 30 FOUND WITH CORROSION. DUPLICATE CARD. REFER TO SNRM N2662 WITH SDR TRACKING NO.05-3102 FOR REPAIR DETAILS.
HORIZ STAB RT BARREL NUT BORE NR 33 FOUND WITH CORROSION. SNRM N2609: DUPLICATE CARD. REFER TO SNRM N2661 WITH SDR TRACKING NO.05-3101 FOR REPAIR DETAILS.
HORIZ STAB LT BARREL NUT BORE NR 2 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 13. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB LT BARREL NUT BORE NR 18 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 - EA 1-5510-87628 ATTACHMENT 14. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB LT BARREL NUT BORE NR 22 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 15. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB RT BARREL NUT BORE NR 31 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 21. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
LT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT AFT BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-87640.
L WING, O/B FLAP I/B HINGE (WING SIDE), FWD ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORRECTIVE ACTION: SNRM N1225: LH WING- O/B FLAP I/B HINGE (WING SIDE), FWD ATTACHMENT O/B HOLE SPOT FACE CORROSION REPAIR CARRIED OUT AS PER EA#1-5750-87637 TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- L/H OUTBD FLAP INBD HINGE BRACKET REPAIR. ORIGINAL THK 0.374" REMAINING THK 0.371" MATERIAL REMOVED 0.003". MAJOR REPAIR AS PER GMM 6-2-100.
LT WING, O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. REPAIR CARRIED OUT AS PER CMM 57-44-08 AND FOUND WITHIN LIMIT AS PER DAC DWG ARC 0502. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
LT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT FWD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87640.
LEFT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87640.
LEFT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-87640.
LEFT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09. REPAIR CARRIED OUT AS PER EA 1-5750-87640.
LT WING, O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08.
LT WING, O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87637.
HFEC CARRIED OUT AND CRACK FOUND ON LT WING AT S-40 STRINGER END WITH LENGTH OF APPROX 7 1/2" BY ACCESS FROM FUEL TANK CUTOUT 537AB. REPAIRED AS PER SRM 57-20-00 FIG.10 VOL I. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.
ALONG STA 6-90, LONGERON 44L, LONGERON SPLICE FITTING CORRODED. CAC COMPT. ALONG STA 6-90 LONGERON 44L LONGERON CORROSION SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER SRM 51-31-01 VOL.II, SRM 51-33-01 VOL.II, SRM 51-35-01 VOL.II AND DRAWING AGA 7115. NEW SPLICE FABRICATED PER DRAWING AGA 7115 P/N FX AGA 7116- 511. MAJOR REPAIR PER GMM 6-2-100.
MAIN DECK, AFT CABIN AT STA 1900 LT INTERCOSTAL AT LONGERON 13L FOUND CRACKED FROM FASTENER HOLES. REMOVED AND FABRICATED FROM 7075.0.0.063" AS PER DRAWING NFA 6374. FABRICATED INTERCOSTAL REPROTECTED, PART MARK AND INSTALLED AS PER SRM 51-33-01 VOL.II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.
LOWER FUSELAGE, LT AIRCON COMPT NR 1 INTERIOR FUSELAGE FRAME AT STA 577 LT LONGERON 44-48L, FOUND DENTED. DENTED FRAME REMOVED & NEW FRAME INSTALLED AS PER SRM 51-35-01 VOL.II. NEW FRAME FABRICATED AS PER DRAWING ACA 3352 P/N FX ACA 3352-3. MINOR REPAIR PER GMM 6-2-100.
LT WING UPPER STRINGER NR 13 FOUND CRACK (APPROX. 11.5" LONG) ON THE STRINGER OUTBOARD END RADIUS AREA. SNRM N1427: LH WING UPPER STRINGER #13 ON THE STRINGER OUTBOARD END RADIUS CRACK. STRINGER REPAIRED AS PER SRM 57-20-00 FIG.10 VOL.I. MAJOR REPAIR PER GMM 6-2-100. CLIP REPLACED IAW EA#1-5720-87702 TITLE: WINGS- OUTER WING- STRINGER REPAIR/CLIP FABRICATION.
CAC COMPT BETWEEN STA 6-90 AND STA 1139, NR L-44L LONGERON CORRODED. SNRM N1168: CAC COMPT BETWEEN STA 6-90 AND STA 1139 L-44L LONGERON CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL.II. MATERIAL ORIGINAL THK 0.071" REMOVED 0.006" X L=3" REMAIN 0.065 FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG.1A VOL.I. MINOR REPAIR PER GMM 6-2-100.
CRACK FOUND ON RT WING UPPER STRINGER ENDS S-10 APPROX 12 INCHES (ACCESS FROM LOWER WING FUEL TANK PANEL NR 636CB). SNRM N0950: RH WING UPPER STRINGER END S-10 APPROX. 12 INCHES CRACK, ACCESS FROM LOWER WING FUEL TANK PANEL NO. 636CB, CARRIED OUT REPAIRED AS PER SRM 57-20-00 FIG. 10 VOL.I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
CRACK FOUND ON RT WING UPPER STRINGER ENDS S-11 APPROX 7.5 INCHES (ACCESS FROM LOWER WING FUEL TANK PANEL NR 636AB). SNRM N0949: RH WING STRINGER END S-11 APPROX. 7.5 INCHES CRACK, ACCESS FROM LOWER WING FUEL TANK PANEL NO. 636AB CARRIED OUT REPAIRED AS PER SRM 57-20-00 FIG. 10 VOL.I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
HFEC CARRIED OUT AND CRACK FOUND ON LT WING AT S-11 STRINGER END WITH LENGTH OF APPROX 11" BY ACCESS FROM FUEL TANK CUTOUT 536AB. LT WING FUEL TANK 537AB CUTOUT AT S-11 CRACK STRINGER REPAIRED AS PER SRM 57-20-00 FIG.10 VOL.I. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.
CAC COMPT BETWEEN STA 1139 AND STA 1159, LONGERON 51L CORRODED. REMOVED AND NEW SPLICE INSTALLED AS PER SRM 51-31-01 VOL.II, SRM 51-33-01 VOL.II SRM 51-35-01 VOL.II AND DRAWING AAA 7086. NEW SPLICE PART. NR AAA 7086-1 FABRICATED PER DRAWING AAA 7086. MINOR REPAIR PER GMM 6-2-100.
RIGHT WING - O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. REPAIR CARRIED OUT AS PER CMM 57-44-08 AND FOUND WITHIN LIMIT AS PER DAC DWG ARC 0502. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
RIGHT WING - O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08.
RIGHT WING - O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87638.
RIGHT WING - O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87638.
O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87638.
HORIZ STAB LT NR 36 BARREL NUT BORE AREAS CORRODED. REWORK/REPAIR AD 2003-22-08- EA 1-5510-87628 ATTACHMENT 12. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZONTAL STAB LT NR 26 BARREL NUT BORE AREA CORRODED. CORRODED SPLICE FITTING REMOVED AND NEW FITTING INSTALLED PER SRM 51-32-01, VOL II, SRM 51-38-01 VOL II, SRM 51-33-01 VOL II. MINOR REPAIR IAW FEDEX GMM 6-2-100.
RT WING, O/B FLAP O/B HINGE (WING SIDE), LWR ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87641.
RT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT LWR AFT BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87641.
RT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT BARREL NUT BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87641.
RT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT UPPER FWD BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87641.
RT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87641.
RT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87641.
RT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87641.
RT WING, O/B FLAP O/B HINGE (WING SIDE) PIVOT BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87641.
HORIZ STAB RT NR 1 BARREL NUT BORE AREAS CORRODED. HORIZ STAB BARREL NUT BORE NR 1 RT REPAIRED IAW STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE REWORK/REPAIR AD 2003-22-08 - EA NR 1-5510-87628 ATTACHMENT 11. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100.
RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87634.
RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87634.
RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRRIED OUT AS PER EA 1-5750-87634.
HORIZONTAL STAB RT BARREL NUT BORE NR 15 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 8. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZONTAL STAB RT BARREL NUT BORE NR 19 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08- EA 1-5510-87628 ATTACHMENT 10. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB RT BARREL NUT BORE NR 23 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 9. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
CENTER CARGO COMPT, RT STA 5-123 LONGERON SPLICE 45R FOUND CRACKED. SNRM N1594: CENTER CARGO COMPT. R/H STA 5-123 LONGERON 45R CRACK SPLICE REMOVED AND NEW SPLICE P/N FXA5A 7116-503 INSTALLED AS PER DRAWING A5A 7116 AND SRM 51-33-01 VOL.II. NEW SPLICE P/N FX A5A 7117-503 FABRICATED PER DRAWING A5A 7116. CLASSIFIED MINOR REPAIR PER GMM 6-2-100.
CENTER CARGO COMPT, RT STA 1641 LONGERON 43R FOUND WITH HAIR LINE CRACK. REPAIRED AS PER SRM 53-10-00 FIG.2 VOL.I. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.
CENTER CARGO COMPT, RT STA 1661 LONGERON SPLICE 46R FOUND CRACKED. REMOVED AND REPLACED AS PER DRAWING AFA 7113 AND SRM 51-31-01 VOL.II. CLASSIFIED AS MINOR REPAIR PER FEDEX GMM 6-2-100.
CENTER CARGO COMPT, RT STA 1641 LONGERON SPLICE 44R FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. MINOR REPAIR PER GMM 6-2-100.
AFT CABIN, STA 1828 TO 1829 RBL 107 FOUND SEAT TRACK CROWN WORN. SNRM N1611: AFT CABIN STA 1771 TO STA 1831 RBL 107 CROWN WORN SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG.1 VOL.I. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.
CENTER CARGO COMPT, RT STA 1801 LONGERON 46 FOUND WITH CORROSION CRACKED. ONGERON REMOVED AND NEW LONGERON INSTALLED AS PER SRM 51-31-01 VOL.II, SRM 51-33-01 VOL.II AND SRM 51-35-01 VOL.II. MAJOR REPAIR PER GMM 6-2-100.
FWD CABIN, ENTRY DOOR NR 1 RT UPPER EDGE FOUND EXISTING DOUBLER UPPER EDGE BENT AND SEPARATED FROM DOOR. FWD CABIN ENTRY DOOR 1 R/H UPPER EDGE SKIN REPAIRED AS PER SRM 52-10- 00 FIG.4 VOL.I SHT.1. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.
LT WING, I/B FLAP O/B HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87635.
RT WING, I/B FLAP O/B HINGE (WING SIDE), PIVOT BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87636.
RT WING, I/B FLAP O/B HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87636.
LT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87631.
HORIZONTAL STAB RT BARREL NUT BORE NR 7 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 - EA 1-5510-87628 ATTACHMENT 7. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB RT BARREL NUT BORE NR 5 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 - EA 1-5510-87628 ATTACHMENT 4. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100.
LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87631.
LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87631.
LT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87633.
LT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87631.
HORIZONTAL STAB LT BARREL NUT BORE NR 1 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 - EA 1-5510-87628 ATTACHMENT 2. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100.
LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87631.
LT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87631.
LT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87633.
HORIZ STAB RT BARREL NUT BORE NR 36 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 - EA 1-5510-87628 ATTACHMENT 1. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB RT BARREL NUT BORE NR 13 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 6. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. ORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87631.
HORIZ STAB RT BARREL NUT BORE NR 3 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08. EA 1-5510-87628, ATTACHMENT 3. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
HORIZ STAB RT BARREL NUT BORE NR 11 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 - EA 1-5510-87628 ATTACHMENT 5. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100.
LT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87631.
LT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87629.
CAC COMPT BETWEEN STA 1139 AND STA 1159, LONGERON 51R CRACKED. SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER SRM 51-31-01 VOL.II, SRM 51-33-01 VOL.II, SRM 51-35-01 VOL.II AND DRAWING AAA 7086. NEW SPLICE PART. NR FXAAA 7086-1 FABRICATED AS PER DRAWING AAA 7086. MINOR REPAIR PER GMM 6-2-100.
RIGHT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87632.
RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87632.
RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA 1-5750-87630 AND CLASSIFIED AS MINOR PER GMM 6-2-100.
RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA 1-5750-87630.
RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87630.
RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-87630.
RIGHT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AND CARRIED OUT AS PER EA 1-5750-87630.
RIGHT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87630.
RIGHT WING - O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-87630.
RIGHT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-87630.
LEFT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87629.
LEFT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87629.
LEFT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87629.
LEFT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87629.
RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87632.
RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87632.
RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87632.
RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87632.
RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87632.
RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87632.
LEFT WING - O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87629.
LEFT WING - O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87629.
LEFT WING - O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87629.
MID CABIN AT STA 872 RBL 75 FOUND SEAT TRACK CROWN INBOARD SIDE CORROSION AS MARKED. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG.I VOL.I. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100.
EXISTNG REPAIR DOUBLER FOUND AT RT WING IB FLAP IB T/E SECTION UPPER SKIN BETWEEN XIFH 195.300 AND XIFH 201.300. EXISTING REPAIR DOUBLER AT RT WING IB FLAP IB T/E SECTION UPPER SKIN BETWEEN XIFH 195.300 AND XIFH 201.300 REPAIRED IAW SRM 57-10-00 FIG.34 VOL.I. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
EXISTING REPAIR DOUBLER FOUND AT RT WING IB FLAP, IB T/E SECTION UPPER SKIN, BETWEEN XIFH 165.300 AND XIFH 171.300. REPAIRED IAW SRM 57-10-00 FIG.34 VOL.I. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
FWD CABIN DOOR 1 RIGHT AFT SEAL RETAINER FOUND DENTED AS MARKED. FWD CABIN DOOR 1 R/H AFT DENT PAN SEGMENT REMOVED AND NEW PAN INSTALLED AS PER SRM 51-31-01 VOL.II, SRM 51-33-01 VOL.II AND SRM 51-35-01 VOL.II. MINOR REPAIR PER GMM 6-2-100.
FWD CARGO COMPT, BETWEEN STA 1119 AND STA 6-10 ALONG L-52L, LONGERON SPLICE CORRODED. CORRODED SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER DRAWING ADA8424 AND SRM 51-33-01.
FWD CARGO COMPT, BETWEEN LBL 3 AND LBL 22, ALONG STA 6-70, FLOORBEAM CRACKED AND CORRODED. CORRECTIVE ACTION: SNRM N1070: FWD CARGO STA 6-70 FLOOR PANEL BEAM CRACK AND CORROSION SUPPORT REMOVED AND NEW SUPPORT INSTALLED AS PER DRAWING ADA 7667, SRM 51-33-01 VOL.II AND SRM 51-35-01 VOL.II. FABRICATE NEW SUPPORT P/N FX ADA 7667-31 PER DRAWING ADA 7667. MINOR REPAIR PER GMM 6-2-100.
AFT CABIN, AFTER REMOVAL OF CORRODED SEAT TRACK, FLOORBEAM WEB UPPER CHORD AT STA 1828 LBL 27.5, FOUND EXTRA HOLE CLOSE TO EDGE AS MARKED. REMOVED AND REPLACED FROM S1464579-7075T6511 AS PER DRAWING AGA 7070.
AFT CABIN SEAT TRACK CORROSION AT CROWN, BASE AND FLANGES AT STA 1861 TO 1887 LBL 65.5. REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG.3 VOL.I. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG.1 VOL.I ON DISCREPANT SEAT TRACK. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100.
AFT CABIN INTERCOSTAL AT STA 1741 RT LONGERON 7 FOUND CRACK. REMOVED AND FABRICATED AS PER DRAWING AFA 7761. INSTALLED AS PER SRM 51-35-01 VOL.II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.
AFT CABIN INTERCOSTAL AT STA 1621 RT LONGERON 7 FOUND CRACK. INTERCOSTAL REMOVED AND FABRICATED FROM 7075-0-0.032 AS PER DRAWING AFA 7761. CARRIED OUT HEAT TREATMENT ON FABRICATED PART, PAINTED AND INSTALLED AS PER SRM 51-35-01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.
AFT CABIN - SEAT TRACK BASE AND CROWN CORRODED AT STA 1321 TO STA 1352 RT RBL 75. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG.3 VOL I. CARRIED OUT REPAIR AS PER SRM 53-70-00.
AFT CABIN INTERCOSTAL AT STA 1701 RT LONGERON 7 FOUND CRACK. REMOVED AND FABRICATED AS PER DRAWING AFA 7761. INSTALLED AS PER SRM 51-35-01 VOL.II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.
AFT CABIN SEAT TRACK CROWN AT STA 1349.5 TO 1353.5 RBL 107 FOUND CORROSION. CORRECTIVE ACTION: SNRM N0807: DISCREPANT SEAT TRACK CARRY OUT REPAIR AS PER SRM 53-70-00 FIG.1 VOL.I. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100.
AFT CABIN SEAT TRACK CORROSION FOUND ON CROWN, FLANGES AND BASE AT STA 1811 TO 1880 LBL 8.5. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG.3 VOL.I. CARRIED OUT REPAIR ON DISCREPANT SEAT TRACK AS PER SRM 53-70-00 FIG.1 VOL.I. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100.
AFT CABIN SEAT TRACK CORROSION ON FLANGES, CROWN AND BASE AT STA 1811 TO STA 1880 RBL 8.5 AT VARIOUS LOCATION. SEAT TRACK REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG.3 VOL.I. CARRY OUT REPAIR ON DISCREPANT SEAT TRACK AS PER SRM 53-70-00 FIG.1 VOL.I. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100.
AFT CABIN SEAT TRACK CORROSION ON FLANGES, CROWN AND BASE AT STA 1811 TO 1880 LBL 27.5. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I. CARRIED OUT REPAIR ON DISCREPANT SEAT TRACK AS PER SRM 53-70-00 FIG 1 VOL I. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100.
AFT CABIN SEAT TRACK CORROSION ON FLANGE, CROWN AND BASE AT STA 1811 TO 1880 RBL 27.5. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I. CARRIED OUT REPAIR ON DISCREPANT SEAT TRACK AS PER SRM 53-70-00 FIG 1 VOL I. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100.
AFT CABIN CURVED SEAT TRACK CORROSION ON FLANGES, CROWN AND BASE AT STA 1964 TO 1966 RBL 107. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG.1 VOL.I. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100.
LHW L/E UPPER SURFACE AFT OF NR 1 AND NR 2 SLAT AREA AT APPROX XORS 150 FOUND WITH EXISTING DOUBLER REPAIR. LT WING L/E UPPER SURFACE AFT OF NR 1 AND NR 2 SLAT AREA AT APPROX XORS 150. CARRIED OUT REPAIR AS PER SRM 57-10-00 FIG 24 VOL I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
EXISTING REPAIR DOUBLER FOUND AT FWD CARGO DOOR JAMB FWD EDGE AT STA 899 L-37R. FWD CARGO JAMB FWD EDGE STA 899 L-37R SKIN REPAIRED AS PER SRM 53-50-00 FIG 16 VOL I. MAJOR REPAIR PER GMM 6-2-100.
EXISTING REPAIR DOUBLER FOUND AT FWD CARGO DOOR JAMB AFT EDGE AT STA 999 L-41R. FWD CARGO DOOR JAMB AFT EDGE STA 999 L-41R SKIN REPAIRED AS PER SRM 53-50-00 FIG 16 VOL I. MAJOR REPAIR PER GMM 6-2-100.
RIGHT L/E UPPER SURFACE AFT OF NR 1 AND NR 2 SLAT AREA AT APPROX XORS 150 FOUND WITH EXISTING DOUBLER REPAIR. RIGHT WING L/E UPPER SURFACE AFT OF NR 1 AND NR 2 SLAT AREA AT APPROX XORS 150. CARRIED OUT REPAIR AS PER SRM 57-00-01 FIG 24 VOL I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
EXISTING REPAIR DOUBLER FOUND AT STA 392 TO STA 401 L26 LT. EXISTING REPAIR AT STA 392 TO STA 401 L26 LT EVALUATED AND FOUND CARRIED OUT AS PER SRM 53-40-00 FIG 5 VOL I EO 1-5100-7-5001, TITLE, STRUCTURES, REPAIR CATALOG MD-11 REPAIR CLASSIFICATION AND TRACKING REQUIREMENTS 14CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.