N464FE
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
225 reports on file, 1995-09-28 – 2010-06-18.
Part: LINE — LEAKING (HYD SYSTEM) · airframe 53,737 hrs · 38,428 cycles
LOST "A" SYSTEM HYDRAULICS AT FL 250. ENG 1 & 2 FLUID SHUTOFF CLOSED FOR 30 MINUTES WITH ENGINE NR 1 & 2 OPERATING. FOUND SPOILER HYD FLUID RETURN LINE NEAR WING STATION 546.5 BROKEN REPLACED SPOILER RETURN LINE PER SPM. LEAK CK`S NORMAL. SYSTEM A PRESSURE FILTERS AND NR 1 ENGINE PUMP CASE DRAIN FILTERS CHECKED AND REPLACED WITH NO CONTAIMINATION FOUND. SEE WRI 29-10/1917 FOR FILTER REPLACEMENT. SERVICED A,B AND STBY RESERVIORS PER AMM 12-12-000-2-0.
Part: RIB — CRACKED (NR 3 SLAT) · airframe 53,658 hrs · 38,344 cycles
NR 3 SLAT 2ND FROM INBD RIB IS CRACKED AT SLAT STA 128. REMOVED CRACKED RIB, FABRICATED NEW RIB USING 7075-O .032 DIMS 18" X 6", HEAT TREATED TO T6 CONDITION IAW ENG REPORT 2-37153-801 REV A, LOCATED, DRILLED AND INSTALLED RIB IAW SRM 51-30-2, 51-20-1, AND 51-10-2.
Part: STRINGER — DAMAGED (BS 960-1010) · airframe 53,658 hrs · 38,344 cycles
AFT PIT STRINGER HAS DOUBLE DRILLED HOLES STA 970 STR 28L REMOVED PREVIOUS REPAIR SPLICE AND PRODUCTION SPLICE, REMOVED DAMAGED STRINGER SECTION, LOCATED AND DRILLED NEW STRINGER SECTION USING BAC1498-145 7075T-6 PO 29057141 DIMS 43.1250" AND INSTALLED NEW STRINGER SECTION AND EXISTING REPAIR SPLICE AND PRODUCTION SPLICE IAW SRM 53-10-2, 51-30-5, 53-10-3 AND 51-30-2.
Part: SKIN — GOUGED (BS 970) · airframe 53,658 hrs · 38,344 cycles
UPON REMOVAL OF INTERCOSTAL FOUND GOUGE IN FUSELAGE SKIN FWD OF BS 970 BTWN STR 30 AND STR 29R. REMOVED GOUGE AND CORROSION AND FOUND OUT OF LIMITS, REMOVED PREVIOUS REPAIR IAW SRM 51-30-2, CUT OUT DAMAGED AREAS DIMS 2.3750" X 4", 2 3/8" X 5.3125" AND 1" X 3" IAW EA 7-5330-135534, FABRICATED DOUBLER USING 2024T-3 .080 DIMS 26" X 29", TRIPLER USING 2024T-3 .080 DIMS 26.2500" X 15.6250", STRUCTURAL FILLER USING 2024T-3 .063 DIMS 27.2500" X 32", 3 EACH FILLERS USING 2024T-3 .125 DIMS 5.3750" X 2.1250" AND 2.1250" X 2.1250" AND 2024T-3 .100 DIMS 2.7500" X .8750" AND INSTALLED ALL REPAIR PARTS IAW EA 7-5330-135534.
Part: SKIN — DAMAGED (BS 650-665) · airframe 53,658 hrs · 38,344 cycles
MAIN CARGO AREA STA 660 BETWEEN STR 3L AND 4L NO EDGE DISTANCE ON FASTENERS. CUT OUT DAMAGED AREA DIMS 3" X 3.4", FABRICATED TRIPLER USING 2024T-3 .100 PO 9009120 DIMS 10 7/8" X 11 3/8", FABRICATED DOUBLER USING 2024T-3 .080 PO 9009327 DIMS 11 5/8" X 13 1/2", FABRICATED FILLER USING 2024T-3 .090 PO 9009093 DIMS 17" X 9 1/2", FABRICATED TEAR STRAP USING 2024T-3 .063 PO 9009362 DIMS 9 1/4" X 3 3/8", FABRICATED REPAIR AREA FILLER USING 7075T-6 .160 PO 5070342 DIMS 3 1/4" X 3" AND INSTALLED ALL REPAIR PARTS IAW P-F SRM 53-30-4, P-F SRM 53-30-3 AND SRM 51-30-2.
Part: FLOORBEAM — DAMAGED (BS 1166) · airframe 53,658 hrs · 38,344 cycles
STA 1166 FLOORBEAM HAS DOUBLE DRILLED HOLES LBL 25. CUT OUT DAMAGED AREA, FABRICATED NEW UPPER CHORD USING BAC1505-100617 7075T-73 PO 29103139 DIMS 11 5/8" X 2", FABRICATED 2 EACH SUPPORT ANGLES USING BAC1490-2831 7075T-62 PO 9006081 DIMS 11 1/2" X 3" AND BAC1490-2785 7075-T62 PO 29118113 DIMS 9 1/2" X 2 1/2", FABRICATED 1 REINFORCEMENT STRAP USING BAC1512-3353-7075T-6 PO 29067580 DIMS 11" X 3/4", FABRICATED 1 REINFORCEMENT STRAP USING BAC1512-3396 PO 9007927 DIMS 10 7/8" X 3/4" AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-8, 51-10-2 AND 51-30-2.
Part: SKIN — DAMAGED (RT WING FLAP) · airframe 53,658 hrs · 38,344 cycles
RT WING OTBD FORE FLAP, INBD L/E WBL 309 TO WBL 314 HAS 2 DEEP GOUGES FROM CONTACT WITH SPOILER PULLEY BOLTS. GOUGES OUT OF LIMITS IAW SRM 57-50-2 ,CUT OUT 2 DAMAGED AREAS DIMS .5" EACH IAW SRM 57-50-4, FABRICATED DOUBLER REPAIR USING 2024T-3 .050 DIMS 7" X 4.25" IAW SRM 57-50-4 AND INSTALLED REPAIR IAW SRM 57-50-4.
Part: SILL — DAMAGED (BS 970) · airframe 53,658 hrs · 38,344 cycles
C-2 DOOR CUT-OUT LOWER SILL HAS PILLOWING AT BS 970. REMOVED PREVIOUS REPAIR, REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED CHORD IAW SRM 51-30-2, LOCATED AND DRILLED NEW CHORD PN 65-56129Y10 IAW SRM 51-30-5 AND INSTALLED CHORD IAW SRM 51-30-2.
Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,658 hrs · 38,344 cycles
CORROSION ON NOSE WHEEL WELL RT MID-CHORD, REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED CHORD, LOCATED AND DRILLED NEW CHORD PN 65-19862-20 PO 20017288 AND INSTALLED IAW SRM 51-30-5, 53-10-1 AND 51-30-2.
Part: SKIN — CORRODED (BS 580-600) · airframe 53,658 hrs · 38,344 cycles
CORROSION ON SKIN FROM STA 580 TO 600 BETWEEN STR 27L AND 28L. THIS NR WAS INCOPORATED IN REPAIR.
Part: SKIN — CRACKED (L1 DOOR) · airframe 53,658 hrs · 38,344 cycles
L-1 DOOR LOWER LIGHTNING HOLE INNER DOOR SKIN HAS UNREPAIRED CRACK, STOP DRILLED. ROUTED OUT DAMAGE AT L-1 DOOR LOWER LIGHTNING HOLE INNER DOOR SKIN DIM 3/4" X 3/4" IAW SRM 51-10-1 REV 102 FABRICATED REPAIR DOUBLER OUT OF 2024 T3 .040" PO NR 9009253 DIM 2.7500 X 1.5 " IAW SRM 51-40-2 FIG 1 AND 52-10-1 FIG 1 INSTALLED REPAIR DOUBLER AT L-1 DOOR INNER SKIN AT LIGHTNING HOLE IAW IAW SRM 51-30-2 AND SRM 51-40-2, FIG 1.
Part: SKIN — CRACKED (L1 DOOR) · airframe 53,658 hrs · 38,344 cycles
L-1 DOOR LOWER LIGHTNING HOLE INNER DOOR SKIN IS CRACKED. ROUTED OUT DAMAGE ON L-1 DOOR INNER SKIN LIGHTNING HOLE DIM .1250" IAW SRM 51-10-1 FABRICATED REPAIR DOUBLER OUT OF 2024 T3 .040" PO 9009253 DIM 1" X 3.7500" IAW SRM 51-40-2, FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND 51-40-2, FIG 1 REV 102.
Part: FRAME — CORRODED (BS 990) · corrosion level 2 · airframe 53,658 hrs · 38,344 cycles
C-2 DOOR CUTOUT AFT FRAME BS 990, UPPER FLANGE IS CORRODED WITH EXFOLIATION ON LOWER SURFACE BTWN STR. 26R-25R. REMOVED CORROSION AND FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA DIMS 1.5" X 1", FABRICATED REPAIR ANGLE USING 15-5PH .080 DIMS 28" X 3", 2 FILLERS USING 7075T-6 .160 DIMS 1.5" X 1.1250" AND 1.5" X 1", FABRICATED 1 AFT FITTING USING 65-56126-37 AND 1 USING 7075T-6 .080 DIMS 6" X 4" AND INSTALLED ALL REPAIR PARTS IAW EA 7-5310-135531.
Part: SKIN — DAMAGED (L1 DOOR) · airframe 53,658 hrs · 38,344 cycles
L-1 DOOR LOWER LIGHTNING HOLE INNER SKIN IS DAMAGED. ROUTED OUT DAMAGE ON L-1 DOOR INNER SKIN LIGHTNING HOLE, DIM .1250" IAW SRM 51-10-1, FABRICATED REPAIR DOUBLER OUT OF 2024 T3 .040" PO NR 9009253, DIM 1" X 3.2500" IAW SRM 51-40-2 FIG 1 AND 52-10-1, FIG 1 INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND 51-40-2, FIG 1, REV 102.
Part: SKIN — MISREPAIRED (BS 1223 S23R) · airframe 53,658 hrs · 38,344 cycles
PREVIOUS REPAIR LOCATED AT STA 1223 STR 23R REQUIRES EVALUATION IAW EO 7-5100-7-5005 PH. REPAIR HAS BLIND FASTENERS INSTALLED. REMOVED BLIND FASTENERS AND INSTALLED SOLID FASTENERS IAW SRM 53-30-3.
Part: SKIN — DAMAGED (CARGO DOOR) · airframe 53,658 hrs · 38,344 cycles
C-2 DOOR EXTERIOR SKIN HAS ROUTE OUT GREATER THAN .100" AT FWD LOWER CORNER. CUT OUT DAMAGED AREA DIM 3 1/2" X 1 1/2" ON C-2 DOOR FWD LOWER CORNER OF SKIN IAW SRM 51-10-1 AND 52-00-3 FIG 3 FABRICATED REPAIR DOUBLER FROM 2024 T3 .080" PO 9009327 DIM 21 3/8" X 5 1/2" AND 2 EACH FILLERS FROM 2024 T3 .071" PO 9009068 DIM 3" X 1 1/2" AND 2" 1 1/2" IAW SRM 52-30-1 FIG 8 AND 52 00-3 FIG 3 INSTALLED REPAIR DOUBLER AND FILLERS IAW SRM 51-30-2, 52-00-3 FIG 3 AND 51-20-4
Part: STRINGER — CORRODED (BS 705 S27R) · corrosion level 2 · airframe 53,658 hrs · 38,344 cycles
FWD PIT- CORROSION AROUND DOME NUT IN STRINGER 27R AT BS 705. CORROSION OUT OF LIMITS, REMOVED DAMAGED STRINGER, FABRICATED FILLER USING BAC1498-144 7075T-6 PO 29067266 DIMS 9" X 3", FABRICATED 2 SPLICES USING BAC1498-132 7075T-6 PO 20017112 AND INSTALLED IAW SRM 51-10-6, 53-10-1, 53-10-2 AND 51-30-02.
Part: WEB — CRACKED (BS 620 S24-25R) · airframe 53,658 hrs · 38,344 cycles
FWD CARGO CUTOUT, STA 620, BETWEEN STR 24R AND 25R, CRACKED WEB. CUT OUT DAMAGED SECTION OF WEB, FABRICATED NEW FILLER USING 7075T-6 .071 PO 9009353 DIMS 6" X 4", FABRICATED 2 EACH DOUBLERS USING 7075T-6 .080 PO 9008389 DIMS 4" X 4" AND 4" X 3" AND INSTALLED IAW SRM 51-40-2, 51-10-2 AND 51-30-2.
Part: SKIN — DAMAGED (ZONE 200) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING STA 440 STR 10L. CUT OUT DAMAGED AREA DIMS 11" X 9.4", FABRICATED 3 FILLERS USING 2024T-3 .063 DIMS 11" X 6.75", 9.75" X 11" AND 17.75" X 4.30", FABRICATED DOUBLER AND TRIPLER USING 2024T-3 .071 AND 2024T-3 .090 DIMS 22.50" X 26" AND 24" X 20", FABRICATED FILLER REPAIR USING 2024T- 3 .063 DIMS 28.50" X 17.75" AND INSTALLED ALL REPAIR PARTS IAW EA 7-5330-135530.
Part: SHEAR TIE — CORRODED (BS 720 S28L/R) · corrosion level 2 · airframe 53,658 hrs · 38,344 cycles
FWD PIT- CORROSION ON SHEAR TIE AT BS 720, AFT SIDE, BETWEEN STRINGERS 28R AND 28L. CORRSION OUT OF LIMITS, REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE USING 2024T-3 .040 PO 9009253 DIMS 11" X 2" AND INSTALLED IAW SRM 51-30-2, 53-10-2 AND 51- 10-6.
Part: SUPPORT — CRACKED (RT ELEVATOR) · airframe 53,658 hrs · 38,344 cycles
CRACK ON SUPPORT ANGLE INSIDE RT ELEVATOR PANEL 9405. REMOVED CRACKED ZEE STIFFENER, FABRICATED NEW ZEE STIFFENER USING 2024T-3 .032 PO NR 9009378 DIMS 18 INCH BY 2.5 INCH, LOCATED, DRILLED AND INSTALLED IAW BOEING 727 SERVICE BULLETIN 55-26 AND SRM 51-30-02.
Part: SHEAR TIE — CORRODED (BS 720C) · corrosion level 2 · airframe 53,658 hrs · 38,344 cycles
CORROSION ON SHEAR TIE AT STA 720C STR'S 28R AND 27R. CORROSION OUT OF LIMITS, REMOVED SHEAR TIE, FABRICATED NEW SHEAR TIE USING 2024T-3 .040 PO NR 9009253 DIMS 5 INCH BY 2 INCH AND INSTALLED IAW SRM 53-10-1, 53-10-2 AND 51-30-2.
Part: STRINGER — CORRODED (BS 534 S26L) · corrosion level 2 · airframe 53,658 hrs · 38,344 cycles
FWD PIT STA 564 STRINGER 26L CORRODED. CUT OUT DAMAGED STRINGER DIMS 19" X 3" IAW SRM 53-10-3, FABRICATED FILLER USING BAC1498-140 7075T-6 PO 2910023 DIMS 19" X 3" IAW SRM 53-10-3. FABRICATED 2 EACH SPLICES USING BAC1498-132 7075T-6 PO 29067380 DIMS 14" X 3" AND 13" X 3" IAW SRM 53-10-3 AND INSTALLED IAW SRM 51-30-2.
Part: SHEAR TIE — CORRODED (BS 585 S26-27R)
FWD PIT - CORROSION ON SHEAR TIE AT BS 585, BETWEEN STRINGERS 27R AND 26R - MARKED. REMOVED FRAME TO BS 585 BETWEEN STR 27R AND 26R IAW SRM 51-30-2 FABRICATED NEW FRAME MATERIAL USED 7075 - 0 .063" PO NR 9009527 DIM 10" X 6.5" IAW SRM 51-20-1, FIG 7 AND 51-10-3 HEAT TREATED PART FROM 7075-0 TO 7075-T6 IAW ENGINEERING REPORT NR 2-37153-801, REV A. INSTALLED NEW FRAME IAW SRM 51-30-2 INSTALLED FLOOR SUPPORT IAW SRM 51-30-2.
Part: STRINGER — CORRODED (BS 740 S27R) · corrosion level 2 · airframe 53,658 hrs · 38,344 cycles
FWD PIT BS 740 STR 27R IS CORRODED AT AFT END. CORROSION OUT OF LIMITS, CUT OUT DAMAGED STRINGER SECTION, FABRICATED NEW STRINGER SECTION USING BAC1498-147 7075T-6 PO 20017342 DIMS 8" AND SPLICE USING BAC1498-131 PO 9009232 DIMS 10", FABRICATED SHIMS USING 2024T-3 .032 PO 9009134 DIMS 10" AND INSTALLED IAW SRM 51-10-6, 53-10-3 AND 51-30-02.
Part: SHEAR TIE — CORRODED (BS 720A S25-26R) · airframe 53,658 hrs · 38,344 cycles
FWD PIT - CORROSION ON SHEAR TIE AT BS 720A, FWD SIDE, BETWEEN STRINGERS 26R AND 25R. CORROSION OUT OF LIMITS, REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE USING BAC1505-100155 7075 PO NR 20013256 AND INSTALLED IAW SRM 53-10-1, 53-10-2 AND 51-30-02.
Part: SHEAR TIE — CORRODED (BS 720B S27-28L) · corrosion level 2 · airframe 53,658 hrs · 38,344 cycles
FWD PIT- CORROSION ON SHEAR TIE AT BS 720B, BETWEEN STRINGERS 28L AND 27L. REMOVED CORROSION ON SHEAR TIE BS 720B BETWEEN STR 28L AND 27L. ORIGINAL THICKNESS .063", MATERIAL LOSS .008" MATERIAL REMAINING .055" FOUND OUT OF LIMITS IAW SRM 51-10-6 AND SRM 53-10-1 FIG 1 REV 102. CUT OUT DAMAGED (DIM 5 3/4" X 7/8") SHEAR TIE IAW SRM 53-10-4 FIG 15. FABRICATED REPAIR OUT OF 7075-O .071" PO 2908670, DIM 4" X 8" IAW SRM 53-10-2 FIG 3 AND SRM 53-10-4 FIG 15. HEAT TREATED FROM 7075-O TO 7075 T6 IAW ER 2-37153-801 REV A. LOCATED, DRILLED AND DEBURRED REPAIR (DIM 3" X 6") IAW SRM 51-30-5 AND SRM 53-10-4 FIG 15. INSTALLED REPAIR AT BS 720B FWD CARGO BETWEEN STRINGERS 28L AND 27L IAW SRM 51-30-2.
Part: SHEAR TIE — CORRODED (BS 720A S27-28L) · airframe 53,658 hrs · 38,344 cycles
FWD PIT- CORROSION ON SHEAR TIE AT BS 720A (FWD SIDE) BETWEEN STRINGERS 28L AND 27L. REMOVED CORROSION ON SHEAR TIE, FWD SIDE BS 720A BETWEEN STRINGERS 28L AND 27L. ORIGINAL THICKNESS .063" MATERIAL LOSS .017" MATERIAL REMAINING .046" FOUND OUT OF LIMITS IAW SRM 51-10-6 AND SRM 53-10-1 FIG 1. REMOVED REPAIR AT FWD SIDE BS 720A BETWEEN STRINGERS 28L AND 27L IAW SRM 51-30-2 FABRICATED NEW REPAIR OUT OF 7075 -O .063" PO 9009327 DIM 3 1/4" X 6" IAW SRM 53-10-4 FIG 11 AND SRM 53-10-2 FIG 3 HEAT TREATED FROM 7075-O TO 7075 T6 IAW ER2-37153-801 REV A LOCATED, DRILLED AND DEBURRED NEW REPAIR DIM 3" X 6" IAW SRM 51-30-5 INSTALLED REPAIR AT FWD SIDE OF BS 720A BETWEEN STR 28L AND 27L IAW 51-30-2 AND 53-10-4 FIG 11 REV 102.
Part: WEB — GOUGED (CARGO DOORWAY)
MCD CUTOUT INNER WEB IS GOUGED IN SEVERAL SPOTS FROM BS 620 - 640 BTWN STR 4L-5L. REMOVED INNER SKIN AND 2 EACH SPLICER TO MAIN CARGO DOOR AFT UPPER AREA IAW SRM 51-30-2. FABRICATED NEW INNER SKIN MATERIAL USED 2024 T3 .125" DIM. 80" X 48" IAW SRM 53-10-2 FIG 3A AND STC DWG NR 53FX1551. INSTALLED NEW WEB AND SPLICER IAW 51-30-2, REV 102.
Part: STRINGER — CORRODED (BS 740 S26R) · corrosion level 2 · airframe 53,658 hrs · 38,344 cycles
FWD PIT- STRINGER 26R IS CORRODED AT BS 740. CORROSION OUT OF LIMITS, CUT OUT DAMAGED STRINGER SECTION, FABRICATED NEW STRINGER SECTION USING BAC1498-147 7075T-6 PO 20017342 DIMS 8 1/2" AND SPLICE USING BAC1498-131 PO 9009232 DIMS 10 1/4", FABRICATED SHIMS USING 2024T-3 .032 PO 9009134 DIMS 10" AND INSTALLED IAW SRM 51-10-6, 53-10-3 AND 51-30-02.
Part: ANGLE — CRACKED (LT WING) · airframe 53,658 hrs · 38,344 cycles
LT WING T/E FALSE SPAR CHORD ANGLE CRACKED WBL 118. TRIMMED OUT DAMAGE, FABRICATED NEW INBD WEB SECTION USING 7075T-6 .032 PO NR 9009201 DIMS 12 1/8 INCH BY 9 1/2 INCH, FABRICATED NEW LWR CHORD SECTION USING BAC1514-1437 7075T-6 PO NR 2911884, FABRICATED 2 ANGLES USING 7075-O .071 PO NR 2908670 DIMS 2 1/4 INCH BY 3 INCH AND 14 3/4 INCH BY 3 INCH, HEAT TREATED PARTS TO T6 CONDITION IAW FAS ENG REPORT 2-37153-801 REV A, FABRICATED STRAP, TWO RADIUS FILLERS, NEW DOUBLER AND INSTALLED IAW DWG NR SR-27- 57-038 REV C.
Part: FLANGE — CORRODED (BS 351) · corrosion level 2 · airframe 53,658 hrs · 38,344 cycles
SURFACE CORROSION ON FUSELAGE STRUCTURE FLANGE AND MONTING BRACKETS FOR FUSELAGE PANEL AFT OF NWW STA 351. CORROSION OUT OF LIMITS, REMOVED, LOCATED AND DRILLED AND INSTALLED NEW CHORD PART NUMBER 65-19861-8 PO# 79014451 IAW SRM 51-30-02 AND 51-30-5.
Part: ANGLE — CORRODED (BS 740 S27-28R) · corrosion level 2 · airframe 53,658 hrs · 38,344 cycles
FWD PIT- 740 BULKHEAD LOWER CHORD ANGLE IS CORRODED BETWEEN STRINGERS 28R AND 27R. REMOVED DAMAGED ANGLE SUPPORT IAW SRM 51-30-2, FABRICATED ANGLE SUPPORT USING 7075-O .190 DIMS 10.7" X 12" IAW DWG 69-64841, HEAT TREATED TO T6 CONDITION IAW FASI ENG REPORT 2-37153-801 REV A, AND INSTALLED REPAIR PART IAW SRM 51-30-2.
Part: STRUCTURE — CORRODED (BS 950) · corrosion level 2 · airframe 53,658 hrs · 38,344 cycles
AFT CARGO BS 950 LOWER CHORD ANGLE IS CORRODED WITH EXFOLIATION BTWN STR 29L- STR 28L. CORROSION OUT OF LIMITS, REMOVED CHORD, LOCATED AND DRILLED NEW CHORD PART NUMBER 65-16338-11 PO 20017118 AND INSTALLED IAW SRM 53-10-1, 51-30-5 AND 51-30-2.
Part: SKIN — DAMAGED (BS 420-450) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING STA 440, STRINGER 19L. CUT OUT DAMAGED AREA, HFEC INSPECTED CUT OUT AND EXISTING HOLES WITH NO DEFECTS NOTED IAW NDTM 51-00-00. FABRICATED REPAIR STRAP USING 2024T-3 .063 PO NR 9009353 DIMS 12 .5" X 4.2500", REPAIR DOUBLER USING 2024T-3 .080 PO NR 9009253 DIMS 19" X 13.2500", REPAIR TRIPLER USING 2024T-3 .125 PO NR 9009286 DIMS 16" X 10.2500", REPAIR FILLER USING 2024T-3 .100 PO NR 9009120 DIMS 7" X 6", REPAIR FILLER USING 2024T-3 .063 PO NR 9009353 DIMS 14.5" X 4.5" AND STRUCTURAL FILLER USING 2024T-3 .250 PO NR 9008186 DIMS 9.5" X 2.6250", STRINGER SPLICE USING BAC1498-132 7075T-6 PO NR 2904957 DIMS 21.5", 2 EACH REPAIR FILLERS USING BAC1498-142 7075T-6 PO NR 9009068 DIMS 14.5" AND 4.75", REPAIR "U" CHANNEL USING BAC1493-412 7075T-6 PO NR 290435 AND ZEE REPAIR "J" ANGLES USING BAC1493-513 7075T-6 PO 7332258 DIMS 7.25" EACH AND INSTALLED ALL PARTS IAW P-F SRM 53-30-3, SRM 51-30-2, SRM 53-10-3 AND SRM 53-10-2.
Part: SKIN — MISREPAIRED (BS 540 S27L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD PIT STA 540, STR 27L CUT OUT DAMAGED AREA THRU SKIN MCD STA 540 STR 27L IAW SRM 53-30-3, FIG 1B FABRICATED STRUCTURAL FILLER, DOUBLER AND TRIPLER IAW SRM 53-30-3 FIG 1B CUT OUT DAMAGED SHEAR TIE IAW SRM 53-10-4, FIG 15 FABRICATED SHEAR TIE IAW SRM 53-10-4 FIG 15, INSTALLED REPAIR SKIN PARTS IAW SRM 51-30-2 REV 102, INSTALLED SHEAR TIE REPAIR IAW SRM 53-10-4 FIG 15
Part: SEAT TRACK — CORRODED (BS 1142-1165) · airframe 53,658 hrs · 38,344 cycles
SEAT TRACK CORRODED BS 1142-1165 BL0. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION USING 7075T6510, DIMS 44.7500 INCHES LONG IAW P-F SRM 53-10-2 AND INSTALLED IAW SRM 51-30-2.
Part: STRINGER — CORRODED (BS 1005-1010) · airframe 53,658 hrs · 38,344 cycles
AFT PIT- CORROSION IN STRINGER 27L FROM BS 1005 TO 1010.
Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 53,658 hrs · 38,344 cycles
LT OTBD FOREFLAP, CARRIAGE ATTACH FITTING WBL 348 AREA, CUTOUT, SKIN FWD OF FITTING CRACKED. TRIMMED OUT DAMAGED AREA (DIM: .2500"X.2500") IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024-T3, .063", PO NR 9009353, DIM: 6"X4" IAW SRM 57-50-2, FIG 4. TREATED AND PRIMED REPAIR DOUBLER IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND 57-50-2 FIG 7, REV 102.
Part: SKIN — MISMANUFACTURED (BS 595 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD PIT SKIN STA 595 STR 25L. (2 LOCATIONS)
Part: SKIN — MISMANUFACTURED (BS 540 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD SKIN PIT STA 540 BELOW STR 25L.
Part: SKIN — MISMANUFACTURED (BS 500 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD PIT STA 500 BELOW STR 25L.
Part: SKIN — MISMANUFACTURED (BS 510 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD PIT STA 510 BELOW STR 25L.
Part: TRIPLER — MISMANUFACTURED (BS 460 S22-24L) · airframe 53,658 hrs · 38,344 cycles
MCD TRIPLER HAS NUMEROUS FASTENERS WITH IMPROPER SPACING STA 460 STR'S 22L TO 24L. CUT OUT DAMAGED AREAS DIM (13.6250 X 2.7500") AND (2.2500" X 1.7500") IAW PF SRM 53-30-3, FIG 1, CW HFEC INSPECTION IAW B727 NDTM PT 6 51-00-00 FIG 23 & FIG 16, NO CRACKS NOTED, FABRICATED STRUCTURAL FILLER 2 EACH 2024 T3 .125" DIM (13.6250" X 2.7500") (2.2500" X 1.2500") 1 EACH FILLER 2024 T3 .125" DIM 36" X 11") 1 EACH DOUBLER 2024 T3 .080" DIM 37" X 17") 1 EACH TRIPLER 2024 T3 .125" DIM (34" X 15") IAW PF SRM 53-30-2 FIG 1B INSTALLED SKIN REPAIR IAW SRM 51-30-2, REV 102
Part: SKIN — MISMANUFACTURED (BS 490 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD PIT STA 490 BELOW STR 25L. CUT OUT DAMAGED AREAS, FABRICATED FILLER USING 2024T-3 .125 DIMS 63.75" X 7.40", DOUBLER USING 2024T-3 .080 DIMS 62" X 13", TRIPLER USING 2024T-3 .125 DIMS 60" X 9.30", 3 SHEAR TIES USING BAC1505-100155 7075T-6 DIMS 6" EACH AND INSTALLED REPAIR PARTS IAW SRM 53-10-2, P-F SRM 53-30-3 AND SRM 51-30-2
Part: SKIN — MISMANUFACTURED (BS 520 S27L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING SKIN FWD PIT STA 520 STR 27L. CUT OUT DAMAGED AREA THRU SKIN IAW SRM 53-30-3 FIG 1B, FABRICATED STRUCTURAL FILLER, DOUBLER AND TRIPLER IAW PF SRM 53-30-3 FIG 1B, CUT OUT DAMAGED SHEAR TIE IAW SRM 53-10-4, FIG 15, FABRICATED SHEAR TIE IAW SRM 53-10-4, FIG 15, INSTALLED REPAIR SKIN IAW PF SRM 53-30-3, FIG 1B INSTALLED SHEAR TIE REPAIR IAW SRM 51-30-2 REV 102.
Part: SKIN — MISMANUFACTURED (BS 580 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING, SKIN FWD PIT STA 580, BELOW STR 25L.
Part: SEAT TRACK — CORRODED (BS 783-804) · airframe 53,658 hrs · 38,344 cycles
SEAT TRACK CORRODED STA 783-804 RBL 45.
Part: SKIN — MISMANUFACTURED (BS 620 S27L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD PIT STA 620 STR 27L. CUT OUT DAMAGED AREAS, FABRICATED REPAIR DOUBLER USING 2024T-3 .080 DIMS 89" X 29.5", TRIPLER USING 2024T-3, .125 DIMS 87" X 27.5", 2 STRUCTURAL FILLERS USING 2024T-3 .125 DIMS 90" X 25.5" AND 2024T-3 .063 DIMS 19" X 7.75", CUT OUT FILLERS USING USING 2024T-3 .125 DIMS 6.5" X 4.3750" AND 1.6250" X 5.6250", SHEAR TIES USING BAC1505-1001557075T6 DIMS 6", SHEAR TIES USING 7075-O .063 DIMS 7" X 3", HEAT TREATED PARTS TO T6 CONDITION IAW ENG REPORT 2-37153-801, REV A AND INSTALLED ALL PARTS IAW P-F SRM 53-30-3, SRM 53-10-4 AND SRM 51-30-2.
Part: SEAT TRACK — CORRODED (BS 720A-720D) · corrosion level 2 · airframe 53,658 hrs · 38,344 cycles
UPON REMOVAL OF FLOORBOARD, FOUND SEAT TRACK CORRODED BETWEEN BS 720A- 720D AT RBL 45. REMOVED SEAT TRACK (OUT OF LIMITS) AT STA 690-740 RBL 45 MAIN CABIN IAW SRM 51-30-2, REV 102 FABRICATED SEAT TRACKS OUT OF BAC 1520-792 7178 T6511, PO NR (1) 9006020, DIM 80", PO NR (2) 9009249, DIM 92", SPLICE ANGLES (2 EACH) OUT OF BAC1503-100122 7178 T6511, PO NR 9009327 & 9029168, DIM (1) 14.1250" X 2.5" AND 14" X 2.5", AND SPLICE PLATE OUT OF 7075-T6 .250", PO NR 9008117, DIM 7.1250" X 2" IAW SRM 53-10-2 FIG 7, SRM 51-30-5, AND 53-10-5 FIG 1 INSTALLED SEAT TRACKS AND REPAIR PARTS BS 690-740, RBL 45 MAIN CABIN IAW SRM 51-30-2.
Part: SKIN — MISMANUFACTURED (BS 640 S27L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD PIT STA 640 STR 27L. CUT OUT DAMAGE AREA TO SKIN STA 640 STR 27L. FABRICATED STRUCTURAL FILLER, DOUBLER AND TRIPLER IAW SRM 53-30-3 FIG 1B CUT OUT DAMAGE SHEAR TIE IAW SRM 53-10-4, FIG 15. FABRICATED SHEAR TIE IAW SRM 53-10-4 FIG 15. INSTALLED SKIN REPAIR PARTS FILLER, DOUBLER AND TRIPLER IAW SRM 53-30-3, FIG 1B AND INSTALLED SHEAR TIE IAW SRM 51-30-2.
Part: STRINGER — PUNCTURED (BS 520 S21L) · airframe 53,658 hrs · 38,344 cycles
FWD CARGO AREA, BS 520, STR 21L, STRINGER HAS PUNCTURE. CUT OUT DAMAGED STRINGER DIMS 14" X 3", FABRICATED FILLER USING BAC1498-140 7075T-6. PO NR 2910023 DIMS 14" X 3", FABRICATED 2 SPLICES USING BAC1498-132 7075T-6 PO NR 2001711 DIMS 11" X 3" AND 10" X 3" AND INSTALLED IAW SRM 53-10-3, 51-10-2 AND 51-30-02.
Part: ATTACH FITTING — CRACKED (RWS 224) · airframe 53,658 hrs · 38,344 cycles
RT INBD FOREFLAP, CARRIAGE ATTACH FITTING WBL 224, SKIN FWD OF FITTING CRACKED.
Part: ANGLE — CRACKED (NR 7 SLAT) · airframe 53,658 hrs · 38,344 cycles
NR 7 SLAT LOWER T/E CHORD ANGLE REPAIR DOUBLER AT INBD UPSTOP PAD IS CRACKED. REMOVED NR 7 SLAT T/E CHORD IAW SRM 57-30-2. LOCATED AND DRILLED NEW T/E CHORD. BAC 1514-1559-2024 T3511 PO 2001728 DIM. 113.7500" IN LENGTH IAW SRM 57-30-5 AND 57-50-2, FIG 2. INSTALLED NEW CHORD IAW SRM 51-30-2 REV 102.
Part: SKIN — MISMANUFACTURED (BS 585 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD PIT STA 585 STR 25L.
Part: STRINGER — DAMAGED (BS 600 S21L) · airframe 53,658 hrs · 38,344 cycles
FWD CARGO AREA, BS 600, STR 21L, STRINGER HAS DOUBLE DRILLED HOLE. CUT OUT DAMAGED STRINGER DIMS 13" X 3", FABRICATED FILLER USING BAC1498-140 7075T-6 PO NR 2910023 DIMS 13" X 3", FABRICATED 2 SPLICES USING BAC1498-132 7075T-6 PO NR 20017112, DIMS 12" X 3" AND 12" X 3" AND INSTALLED IAW SRM 53-10-3, 51-10-2 AND 51-30-02.
Part: SKIN — MISMANUFACTURED (BS 560 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD SKIN PIT STA 560 BELOW STR 25L.
Part: SKIN — MISMANUFACTURED (BS 518 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD PIT SKIN STA 518 BELOW STR 25L.
Part: SKIN — MISMANUFACTURED (BS 575 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD SKIN PIT STA 575 STR 25L.
Part: SKIN — MISREPAIRED (BS 390 S25L) · airframe 53,658 hrs · 38,344 cycles
PREVIOUS REPAIR LOCATED AT STA 390 STR 25L REQUIRES EVALUATION IAW EO 7-5100-7-5005 PT1. EVALUATION DETERMINED THE EXISTING REPAIR REQUIRES REPLACEMENT. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR DOUBLER USING 2024T-3 .056, PO 7178367 DIMS 13.5" X 11", FABRICATED STRAP REPAIR USING 2024T-3 .040 PO NR 9009035 DIMS 11" X 1" AND INSTALLED IAW SRM 51-30-2, 53-30-3 AND 51-10-2.
Part: SKIN — MISMANUFACTURED (BS 680 S22L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH ZERO ED FWD PIT STA 680 STR 22L.
Part: SKIN — MISMANUFACTURED (BS 600 S27L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING SKIN FWD PIT STA 600 STR 27L. CUT OUT DAMAGE AREA THRU SKIN STA 600 STR 27L-28L IAW B727 PF 53-30-3 FIG 1B. FABRICATED REPAIR PARTS FILLER, STRUCTURAL FILLER DOUBLER AND TRIPLER IAW PF 53-30-3 FIG 1B. CUT OUT DAMAGE SHEAR TIE IAW SRM 53-10-4 FIG 4. FAB SHEAR TIE REPAIR IAW SRM 53-10-4 FIG 15. INSTALLED REPAIR SKIN PARTS IAW SRM 51-30-2 AND INSTALLED SHEAR TIE IAW SRM 51-30-2, REV 102.
Part: SKIN — MISMANUFACTURED (BS 557 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD SKIN PIT STA 557 BELOW STR 25L.
Part: SKIN — MISMANUFACTURED (BS 530 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD SKIN PIT STA 530 BELOW STR 25L.
Part: SPAR — CRACKED (RWS 118) · airframe 53,658 hrs · 38,344 cycles
RT WING LOWER T/E, FALSE SPAR INBD END IS CRACKED AT WBL 118. TRIMMED OUT DAMAGE, FABRICATED NEW INBD WEB USING 7075T-6 .032 DIMS 12.1250" X 9.5" PO 9009201, FABRICATED NEW INBD LWR CHORD SECTION USING BAC1514-1437 7075T-6 PO 2911884 DIMS 20.5" X 3", FABRICATED 2 ANGLES USING 7075-O .071 PO 2908670 DIMS 14.7500" X 2.7500" AND 12.5" X 2.7500", HEAT TREATED MATERIAL TO T6 CONDITION IAW FASI ENG REPORT 2-37153-801, REV A, FABRICATED STRAP USING 7075T-6 .090 PO 9008486 DIMS 12" X 1.6250", FABRICATED 2 RADIUS FILLERS USING 7075T-6 .160 PO 5070342 DIMS 2" X 1" EACH , FABRICATED NEW DOUBLER USING 2024T-3 .050 PO 9009134 DIMS 12.5" X 8.3750" AND INSTALLED ALL REPAIR PARTS IAW DWG SR27-57-038 REV C.
Part: SKIN — MISMANUFACTURED (BS 605 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD PIT SKIN STA 605 STR 25L.
Part: STRUCTURE — CRACKED (TORQUE BOX) · airframe 53,658 hrs · 38,344 cycles
AFT A/S LOWER TORQUE BOX LIGHTENING HOLE CRACKED LT SIDE BS 1326.
Part: SKIN — MISMANUFACTURED (BS 675 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD PIT STA 675 STR 25L. CUT OUT DAMAGE AREA THRU SKIN TO STA 675 STR 25L IAW SRM 51-10-1. FABRICATED REPAIR PARTS STRUCTURAL FILLER, DOUBLER AND TRIPLER IAW PF SRM 53-3-3 FIG 1B. CUT OUT DAMAGE SHEAR TIE TO STA 660 STR 27L IAW SRM 53-10-4 FIG 15. FABRICATED SHEAR TIE REPAIR IAW SRM 53-10-4 FIG 15. INSTALLED STRUCTURAL FILLER, DOUBLER AND TRIPLER IAW SRM 51-30-2. INSTALLED SHEAR TIE REPAIR IAW SRM 51-30-2 REV 102.
Part: SKIN — MISMANUFACTURED (BS 600 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD SKIN PIT STA 600 BELOW STR 25L.
Part: SKIN — MISMANUFACTURED (BS 615 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD PIT STA 615 STR 25L.
Part: SKIN — MISMANUFACTURED (BS 660 S27L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD PIT STA 660 STR 27L. THIS NR WAS INCORPORATED IN REPAIR ON N00896.
Part: SKIN — MISMANUFACTURED (BS 565 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING SKIN FWD PIT STA 565 STR 25L.
Part: SKIN — MISMANUFACTURED (BS 635 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD SKIN PIT STA 635 BELOW STR 25L.
Part: SKIN — MISMANUFACTURED (BS 520 S25L) · airframe 53,658 hrs · 38,344 cycles
FASTENERS WITH IMPROPER SPACING FWD SKIN PIT STA 520 BELOW STR 25L.
Earlier reports · 1995–2008 · 151 reports
2008
Part: SWITCH — MISALIGNED (LE FLAPS) · airframe 52,911 hrs · 37,750 cycles
NR 2 LED/FLAP DID NOT RETRACT. FOUND SWITCH INTERNALLY BINDING. REPLACED SWITCH PER 27-82-001-4, OP CHECKS NORMAL, GOOD FOR SERVICE. PREMATURE REMOVAL/INSTALLATION. REMOVED AND REPLACED NR 2 LEADING EDGE FLAP SWITCH AMM 27-82-001-4
Part: SWITCH — MISALIGNED (LE FLAP) · airframe 52,911 hrs · 37,750 cycles
NR 2 LED/FLAP DID NOT RETRACT. FOUND SWITCH INTERNALLY BINDING. REPLACED SWITCH PER 27-82-001-4, OP CHECKS NORMAL, GOOD FOR SERVICE. REMOVED AND REPLACED NR 2 LEADING EDGE FLAP SWITCH AMM 27-82-001-4.
Part: SWITCH — FAILED (LE FLAPS) · airframe 52,884 hrs · 37,730 cycles
ON DEPARTURE WHEN FLAPS RAISED FROM 5 TO O GOT AN LED DISAGREE LIGHT WITH NR 2 LE FLAP LED INDICATING NOT IN PROPER POSITION. REMOVED NR 2 LE FLAP SWITCH AND PIGGY BACKED ONTO NR 1 LE FLAP POSITION AND PROBLEM FOLLOWED. REINSTALLED CONNECTOR ON ORIGINAL NR 1 SWITCH. REPLACED NR 2 LE FLAP SWITH AND CYCLED FLAPS SEVERAL TIMES PER MM 27-82-001-4, OPS CHECK GOOD.
Part: BYPASS VALVE — LEAKING (HYD SYSTEM) · airframe 52,885 hrs · 37,731 cycles
DURING DESCENT A HYDRAULIC SYSTEM LOST ALL QTY. COMPLIED WITH QRH LOSS OF ALL HYDRAULIC SYSTEM A ALT FLAPS AND MANUAL GEAR EXT SYST A ENG 1 AND 2 FLAP SHUTOFF SWITCHES CLOSED FOR MORE THAN 5 MIN WITH ENGINES RUNNING. REMOVED AND REPLACED RT FLAP BYPASS VALVE PER MM 27-51-151-4. ALSO, REPLACED A SYS CASE DRAIN FILTERS PER MM 29-11-041-2.
Part: VALVE — LEAKING (HYD SYSTEM) · airframe 52,885 hrs · 37,731 cycles
DURING DESCENT A HYDRAULIC SYSTEM LOST ALL QTY. COMPLIED WITH QRH LOSS OF ALL HYDRAULIC SYSTEM A. ALT FLAPS AND MANUAL GEAR EXT SYST A ENG 1 AND 2 FLAP SHUTOFF SWITCHES CLOSED FOR MORE THAN 5 MIN WITH ENGINES RUNNING. REMOVED AND REPLACED RT FLAP BYPASS VALVE PER MM 27-51-151-4. ALSO REPLACED A SYS. CASE DRAIN FILTERS PER MM 29-11-041-2
2007
Part: STRINGER — CRACKED (ZONE 200) · airframe 52,271 hrs · 37,220 cycles
RT EXT FUSELAGE SKIN STRINGER IS CRACKED, BS 940-946, STR 18A R REMOVED DAMAGE SECTION OF STR 18A RT. DRILLED UP REPAIR ANGLES, RADIUS FILLERS AND AND SHIMS, AND NEW STR SECTION. INSTALLED ALL REPAIR PARTS AND INSTALLED W/B PLN NR 3118 AND 3116. REF FED EX EA NR 7-5310-113120, SRM 51-30-02, BOEING DWG 65C29069. THIS IS CLASSIFIED AS A MAJOR REPAIR.
Part: BRACKET — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
AFT LOWER CARGO DOOR, LOWER AFT CORNER WEB CORRODED INSTALLED NEW BRACKET PER DWG 65-57204 AND APPLIED LEVELING COMPOUND TO THE LOWER AREA AROUND BRACKET PER BOHM 52-36-22 PG 407.
Part: PAN — CRACKED (FUSELAGE) · airframe 52,271 hrs · 37,220 cycles
DITCHING PAN IS CRACKED, LOCATED AT STA 1183, WL 20/8, LBL 27. REMOVED DITCHING PAN, STA 1183, LBL 27 REF SRM 51-30-02. FABRICATED DITCHING PAN REF BOEING DRAWING 65-29567-5 DITCHING PAN. HEAT TREATED REF BOEING DRAWING 65-29567-5. TREATED AND PRIMED DITCHING PAN REF SRM 51-10-2. IDENTIFIED DITCHING PAN WITH FX65-29567-5, REF FED EX GMM 7-0-1001. INSTALLED DITCHING PAN AT STA 1183 LBL27 REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,271 hrs · 37,220 cycles
AFT CARGO BS 970 LOWER FRAME ANGLE CRACKED BETWEEN STR 26L-27L REMOVED LOWER FRAME ANGLE. FABRICATED REPAIR ANGLE AND REINSTALLED LOWER FRAME REPAIR AND INSTALLED LOWER REPAIR ANGLE. REF SRM 51-40-3/ FIG NR 1/ PAGES 1-6 AND SRM 51-30-02. REPAIR IS CLASSIFIED AS A MAJOR REPAIR.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
RT FUSELAGE SKIN UNDER WING TO BODY TO FAIRING 3442 HAS CORROSION AROUND NUTPLATE HOLES AND FRETTING ALONG MATING SURFACE REMOVED CORROSION REF SRM 51-10-6, ORIGINAL MATERIAL THICKNESS "T" .060" AFTER BLENDING, REMAINING MATERIAL THICKNESS IS .043" AND IS OUT OF LIMITS REF 53-30-3 FIG 5. INSTALLED REPAIR REF SRM 53-30-3 FIG 5. THIS IS CLASSIFIED AS A MINOR REPAIR.
Part: PAN — CRACKED (FUSELAGE) · airframe 52,271 hrs · 37,220 cycles
DITCHING PAN AT STA 1183 BETWEEN RBL46 TO 49, WL 208 IS CRACKED, ALONG WITH AFT SUPPORT CLIP. REMOVED GILLINER SUPPORT PLUS DITCHING PAN SRM 51-30-20 PG 16. FABBED NEW DITCHING PAN REF DWG 65-29567. TREATED AND PRIMED REPAIR PARTS 51-10-02 PG 7. INSTALLED REPAIR PARTS SRM 51-40-3 PG 1-6. INSTALLED DITCHING PANS SRM 51-30-2 PG 1- 16. INSTALLED GILLINER SUPPORT SRM 51-30-2.
Part: FRAME — CRACKED (FUSELAGE) · airframe 52,271 hrs · 37,220 cycles
FWD PIT, PREVIOUS UNREPAIRED DAMAGE FRAME CRACKED AT BS 720, STR 19R REPAIRED FRAME 720 BTW STR 18R AND 19R REF FED EX EA 7-5310-113119, SRM 51-40-3 FIG 1 SRM 51-30-2 PG 2 51-30-5 PG 1 BOEING DWG 65-82614-12, 65-17664-50. TREATED AND PRIMED REF SRM 51-10-2 PG 7 PG 6. IDENTIFIED PART AS FX 65-82614-12 REF GMM 7-0-1001 PG 1. HFEC FOR DAMAGE REMOVAL, IAW 727 NDT MAN PART 6 51-00-00 FIG 23 TOOL NR IDM -0031 CAL DATE DUE 11-30-07. NO DEFECTS NOTED, THIS IS CLASSIFIED AS A MAJOR REPAIR.
Part: FRAME — CRACKED (FUSELAGE) · airframe 52,271 hrs · 37,220 cycles
AFT PIT BODY FRAME WEB IS CRACKED AT TOOLING HOLE BS 970, STR 26L - 27L REMOVED ASSOCIATED PARTS TO FRAME 970 SECTION, REMOVED DAMAGE SECTION OF FRAME FROM STR 27R TO STR 24L AND 25L. FABRICATED NEW FRAME SECTION, HEAT TREATED, ALODINED AND PRIMED, PAINTED AND INSTALLED. INSTALLED REMOVED ASSOCIATED PARTS TO FRAME REF BOEING DOCUMENT NUMBER 65-16339 AND SRM 51-30-02. REPAIR IS CLASSIFIED AS A MAJOR REPAIR.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
FWD PIT FLR SPPT Z-CHANNEL IS CORRODED BS 720B TO 720C PLUS 10, LBL 20, WL 156 BLENDED CORROSION ON FLOOR SUPPORT. MATERIAL OF .025" OF .063' ORIG "T" FOUND TO BE OUT OF LIMITS REF 53-10-1 PG 2. FABRICATED NEW FLOOR SUPPORT Z-CHANNEL FROM EXTRUSION BAC1517-1508 7075-T6. FABRICATED REPAIR SPLICE AT BS 720 PLUS 8 REF SRM 51-40-4 PG 1-9. INSTALLED Z-CHANNEL FLOOR SUPPORT FROM BS 720 PLUS 8 TO BS 720D, LBL 20, REF 51-30-2, SRM 51-40-4, 51-10-2.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 52,271 hrs · 37,220 cycles
2" CRACK THROUGH FASTENER ON ANGLE BRACKET, FS 1303, LBL 20, WL 273, ON FWD SIDE OF BULKHEAD, ABOVE S-DUCT, BRACKET CONNECTS BULKHEAD TO FUSELAGE SKIN. REMOVED AND INSTALLED NEW BRACKET AT FS 1303, LBL 20, WL 273 ON FWD SIDE OF BULKHEAD ABOVE S-DUCT REF 51-30-02 PG 1-12. LEAK CHECKED TAI DUCT REF W/C 73C015-00. LEAK CHECK GOOD. THIS IS CLASSIFIED AS A MINOR REPAIR.
Part: PAN — CRACKED (FUSELAGE) · airframe 52,271 hrs · 37,220 cycles
DITCHING PAN IS CRACKED LOCATED AT RBL 27 STA 1183, WL 208 REMOVED GILL LINER SUPPORT PLUS DITCHING PAN REF SRM51-30-2 PG 1-16. FABRICATED NEW DITCHING PAN REF DWG 65-29567. TREATED AND PRIMED DITCHING PAN SRM 51-30-02. REMOVED FLAPPER VALVE SRM 51-30-2. INSTALLED NEW FLAPPER VALVE.
Part: FRAME — CRACKED (FUSELAGE) · airframe 52,271 hrs · 37,220 cycles
FWD PIT, PREVIOUS UNREPAIRED DAMAGE FRAME CRACKED AT BS 700 AND BETWEEN STR 18R AND 19R REPAIRED FRAME 700 AT STRINGER 18 TO19 RT REF FED EX EA NR 7-5310-113118 AND BOEING DWG 65-15938, 65-82614-9, 65-17664-50. TREATED AND PRIMED PARTS REF SRM 51-10-2. IDENTIFIED PARTS FX 65-82614-9 REF FED EX GMM 7-0-1001 PG 1 SEC 7B. HFEC INSP FOR CRACK REMOVAL REF 727 NDT MAN, PART 6, 51-00-00 FIG 23. NO DEFECTS NOTED. THIS IS CLASSIFIED AS A MAJOR REPAIR.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
FWD PIT FLOOR SUPPORT PNL IS CORRODED BS 480-720D, LBL 20-26, WL 157. BLENDED CORROSION AT BS 480 TO 720C +10. MAX MATERIAL LOSS OF 16 PERCENT OF .050 ORIG "T". WITHIN LIMITS REF SRM 53-10-1 PG 31. BLENDED CORROSION AT BS 720C+10 TO BS 720D. MATERIAL LOSS OF 30 PERCENT OF .050" ORIG "T" FOUND TO BE OUT OF LIMITS REF SRM 53-10-1. FABRICATED AND REPLACED Z- ANGLE PANEL AT BS 720C+10 TO 720D, REF 51-30-2, 51-10-2 AND BOEING DWG 69-46373 THIS IS CLASSIFIED AS A MINOR REPAIR.
Part: FRAME — CRACKED (FUSELAGE) · airframe 52,271 hrs · 37,220 cycles
FWD PIT BODY FRAME, UPPER CHORD ANGLE, DOUBLER IS CRACKED, BS 720B, STR 26L-27L. REMOVED DAMAGE, FORMED REPAIR ANGLE AND FILLER, HEAT TREATED TO T-6 CONDITION, DRILLED AND TRIMMED REPAIR PARTS, ALODINED AND PRIMED. INSTALLED REPAIR REF SRM 51-40-3, 51-20-021, 8130-3 TRACKING NR 2007-11-087. REPAIR IS CLASSIFIED AS A MAJOR REPAIR.
Part: FRAME — CORRODED (FAIRING) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
BODY FAIRING FRAME LOCATED BETWEEN PANELS 3358 AND 3458, FORWARD END HAS CORROSION. REPLACED FAIRING FRAME, REF BOEING DWG 65-59318 AND SRM 51-30-2, TREATED AND PRIMED REF MM 51-20-021-7, THIS IS CLASSIFIED AS A MINOR REPAIR.
Part: TENSION TIE — CRACKED (ZONE 200) · airframe 52,271 hrs · 37,220 cycles
FOUND CLIP CRACKED AT FS 480 AND STR 2. REMOVED FASTENERS IN LOWER WEB. REMOVED CRACKED TENSION CLIP, FABRICATED NEW TENSION CLIP AND INSTALLED NEW TENSION CLIP AND FASTENERS IN LOWER WEB. REFERENCE DRAWING NR 53FX1285 AND SRM 51-30-02 CLASSIFIED AS A MAJOR REPAIR.
Part: SUPPORT — CORRODED (BS 720C) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
BODY FAIRING FRAME SUPPORT LOCATED RIGHT OF AIR CONDITION HOOK UP IS CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, ORIGINAL .040". REMOVED .023", REMAINING .014 IAW 53-101, TOOL AAR 10274 CAL DUE 12-27-07. REMOVED FAIRING AND BRACE. FABRICATED, DRILLED, AND TREATED AND PRIMED NEW BRACE. REINSTALLED FAIRING AND BRACE IAW SRM 51-30-2, 51-10-2, AND BOEING DRAWING 65-22579. THIS IS CLASSIFIED AS A MINOR REPAIR.
Part: CASTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
MAIN DECK 1L DR CUT OUT LWR HINGE UPPER STOP PLATE SUPPORT CASTING IS CORRODED AT FASTENER HOLE, BS 307, STR 13R, WL 238. REMOVED FITTING RER SRM 51-30-2, SENT TO HAVE NEW CASTING MATCHED DRILLED UP FOR BEARING PLATED AND INTO PLACE PER SRM 51-30-5 PG 1,2. INSTALLED FITTING PER SRM 51-30-2.
Part: FLANGE — DELAMINATED (NR 1 NACELLE) · airframe 52,271 hrs · 37,220 cycles
NR 1 ENGINE UPPER COWL T/E FLANGE IS CHIPPED AND DISBONDED REMOVED NR 1 ENGINE UPPER COWL T/E FLANGE, LOCATED AND DRILLED NEW FLANGE. INSTALLED NEW FLANGE, REF SRM 51-30-2 PG 1-4 REF DWG 65-19508.
Part: BULKHEAD — GOUGED (ZONE 100) · airframe 52,271 hrs · 37,220 cycles
FUSELAGE STA 178 FORWARD SIDE OF PRESSURE BULHEAD, SKIN HAS A GOUGE 2.5" IN FROM OUTER EDGE AT LEFT SIDE, 4TH RADOME ATTACH NUTPLATE FITTING DOWN BLENDED GOUGE, ORIGINAL MATERIAL IS .030" BONDED TO .056", MATERIAL REMOVED IS .008" MATERIAL REMAINING IS .022. HFEC DAMAGE. ALODINED AND PRIMED, REF FED EX EA 7-5330- 13117, THIS IS CLASSIFIED AS A MINOR REPAIR.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
AFT PIT BILGE SKIN CORRODED OB SIDE OF STR 28L, STA 1045-1048, LBL 16-17. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA OF SKIN. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND FR PRIMED. INSTALLED EXTERNAL REPAIR REF SRM 53-30-3 FIG 3. THIS IS CLASSIFIED AS A MAJOR REPAIR.
Part: SKIN — GOUGED (ZONE 100) · airframe 52,271 hrs · 37,220 cycles
FUSELAGE SKIN JUST FWD OF LANDING LIGHT IS GOUGED REMOVED INBD LT LEADING EDGE REF SRM 51-30-2 MANUFACTURED REPAIR DOUBLER AND FILLER REF SRM 53-30-3. TREATED AND PRIMED REPAIR DOUBLER AND FILLER, REF SRM 51-10-2. INSTALLED REPAIR DOUBLER AND FILLER REF SRM 53-30-3. INSTALLED LEADING EDGE REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.
Part: FRAME — CORRODED (BODY FAIRING) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
BODY FAIRING FRAME HAS CORROSION LOCATED FORWARD END OF PANEL 3455R. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, ORIGINAL .050'. REMOVED .025", REMAINING .025", IAW SRM 53-10-1. TOOL AAR23841 CAL DATE .
Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
UPPER FUSELAGE STATION 720D FRAME, AFT EDGE IS CORRODED AT STRINGER 4 RIGHT AREA REMOVED CORROSION AT UPPER FUSELAGE STA 720D FRAME AFT EDGE AT STR 4 RIGHT AREA REF SRM 51-10-6 ORIGINAL MATERIAL .064", MATERIAL REMAINING .048" MATERIAL LOSS .016". FOUND TO BE OUT OF LIMITS REF SRM 53-10-1 FIG 1. FABRICATED REPAIR DOUBLER REF SRM 51-40-3 FIG 1, MATERIAL USED 7075-0, .063" HEAT TREATED TO T-6, TRACKING NR 2007- 11-015 W/O N00740. TREATED AND PRIMED DOUBLER AND INSTALLED REF SRM 51-10-2, 51-30- 2. THIS IS CLASSIFIED AS A MAJOR REPAIR.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
AFT PIT STR 28L HAS CORROSION BET STA 1053 TO STA 1054 CORROSION FOUND DURING REPAIR ON N00489 AFTER SKIN WAS REMOVED CUT OUT DAMAGED STRINGER. FABRICATED REPAIR PARTS TREATED AND FR PRIMED. INSTALLED STRINGER REPAIR REF SRM 53-10-3 FIG 1. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.
Part: STRINGER — CRACKED (ZONE 100) · airframe 52,271 hrs · 37,220 cycles
AFT PIT STR 27R, END FITTING IS CRACKED AT BS 1056, REMOVED END FITTING, P/N 65-56185-1. INSTALLED PN 65-56185-2, IAW SRM 51-30-1 AND DWG 65-56185.
Part: BATTERY BOX — CRACKED (ZONE 100) · airframe 52,271 hrs · 37,220 cycles
E/E COMPARTMENT CRADLE (TRAY ASSY) IS CRACKED AT FWD RT CORNER REMOVED AND REPLACED BATTERY TRAY ASSY REF SRM 51-30-2, THIS IS CLASSIFIED AS A MINOR REPAIR.
Part: ANGLE — CRACKED (ZONE 500) · airframe 52,271 hrs · 37,220 cycles
LT OTBD AILERON BAY BAFFLE SEAL IS CRACKED AT INBD ANGLE (MKD) TO FASTENER HOLE REMOVED AND REPLACED AILERON BAY BAFFLE ANGLE REF DWG 65-19289 AND SRM 51-30-2. APPLIED PN FX 65-19289-17 REF FED EX GMM 7-0-1001.
Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
MAIN DECK FLOOR SUPPORT IS CORRODED, BS 328-344, LBL 29, WL 208. REMOVED CORROSION IAW SRM 51-10-6, FOUND TO BE OUT OF LIMITS ORIGINAL .080'. REMOVED .025" (DEEPEST POINT ) REMAINING .055', IAW SRM 53-10-01, TOOL AAR IND -0213, CAL DUE 10-15-08. REMOVED FLOOR SUPPORT, FABRICATED, TREATED AND PRIMED, AND INSTALLED FLOOR SUPPORT, AND FILLER IAW SRM 51-30-2, 51-10-2, 51-20-1, AND BOEING DWG, 65-17593. THIS IS CLASSIFIED AS A MINOR REPAIR.
Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
UPPER FUSELAGE STATION 720D FRAME, AFT EDGE IS CORRODED AT STRINGER 4 RIGHT REMOVED CORROSION AT UPPER FUSELAGE STA 720D FRAME AFT EDGE AT STR 4 RIGHT AREA REF SRM 51-10-6 ORIGINAL MATERIAL .064", MATERIAL REMAINING .048", MATERIAL LOSS .016'. FOUND TO BE OUT OF LIMITS REF, SRM 53-10-1 FIG 1. FABRICATED REPAIR DOUBLER, REF SRM 51-40-3 FIG 1, MATERIAL USED 7075-0 .063, HEAT TREATED TO T-6. TRACKING NR 2007-11-015. TREATED AND PRIMED DOUBLER AND INSTALLED REF 51-10-2, 51-30-2 THIS IS CLASSIFIED AS A MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
MAIN CARGO COMP STA 480 RBL 10" FLOORBEAM LOWER SURFACE CORRODED REMOVED CORROSION IAW SRM 53-10-1 PG1, ORIGINAL .135", REMOVED .035' REMAINING .096". FOUND TO BE OUT OF LIMITS AAR TOOL NR 280087 CAL DATE 4-27-08. REPAIRED IAW SRM 53-10-8 FIG 8. TREATED AND PRIMED IAW SRM 51-10-2. REMOVED AND REINSTALLED CABLE GUIDE IAW 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
AFT CABIN CENTER SEAT TRACK RIGHT FLANGE UPPER SURFACE CORRODED BETWEEN BS 1100-1110 REMOVED CORROSION VERIFIED REMOVAL TO BE OUT OF LIMITS ORIG THICKNESS .0947 REMAINING .0536 REMOVED .0411. FABRICATED SEAT TRACK AND REPAIR STRAP AND ANGLES. INSTALLED REPAIR AND SEAT TRACK. REF SRM 53-10-5 FIG 1, SRM 53-10-1 FIG 3 THIS IS CLASSIFIED AS A MAJOR REPAIR.
Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
LOWER FUSELAGE STATION 742, RBL 1 TO RBL 4, KEEL BEAM LOWER WEB CORRODED, REMOVED CORROSION IN REF TO SRM 51-10-1 PG 1, ORIG MAT'L .080, MAT'L REMAINING .045', OUT OF LIMITS. REMOVED DAMAGE AREA OF KEEL BEAM WEB 51-10-2 PG 10. FABRICATED DOUBLER AND FILLER IN REF TO SRM 51-40-2 FIG 1. TREAT AND PRIMED DOUBLER AND FILLER AND INSTALLED REF MM 51-20-021-07, MM 51-20-031-07.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 52,271 hrs · 37,220 cycles
MAIN DECK FLOORBEAM UPPER FLANGE IS CRACKED AT FLOOR PANEL FASTENER HOLE, BS 328 FWD, LBL 19, WL 208. CUT OUT DAMAGE AT BS 328, LBL 18.25 TO LBL 21. FABRICATED AND DRILLED REPAIR PARTS. TREATED AND PRIMED AND TOP COATED REPAIR PARTS. INSTALLED REPAIR TOP COATED UPPER SURFACE OF FLOORBEAM AT REPAIR AREA. APPLIED 1 COAT OF LPS TO REPAIR AREA. REF SRM 53-10-8 FIG 9, THIS IS CLASSIFIED AS A MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,271 hrs · 37,220 cycles
MAIN DECK FLOORBEAM UPPER FLG IS FRETTED/CORRODED AT FASTENER HOLE BS 312, LBL 4, WL 208. REMOVED CORROSION, FOUND OUT OF LIMITS, IAW SRM 51-10-6, 53-10-1 53-10-2 FIG 7 SHT 1, ITEM 18, ORIGINAL MAT. .080" REMOVED .026" REMAINING .064" TOOL AAR IN17-0213 CAL DATE 10-15-08. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 7. REMOVED AND REINSTALLED PULLEY BRACKET IAW SRM 51-30-2, THIS IS CLASSIFIED AS A MAJOR REPAIR.
Part: DUCT — DAMAGED (8TH STAGE) · airframe 52,153 hrs · 37,130 cycles
NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. PERFORMED QRH PROCEDURE AND LIGHT EXTINGUISHED. AFTER LIGHT EXTINGUISHED, NORMAL POWER SETTINGS USED, LIGHT NEVER CAME BACK ON. REMOVED AND REPLACED 8TH STAGE DUCT DUE TO FLANGE AND NUT LEAKING. GROUND RAN NR 1 ENGINE PER JRH. ALL NORMAL, OK TO CONTINUE.
2005
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 50,653 hrs · 35,889 cycles
FOUND SEAT TRACK SUPPORT CORRODED BS 760-848 LBL45. REMOVED AND REPLACED UPPER CHORD SUPPORT BEAM AND SEAT TRACK IAW BAC DWG 65-16279 AND FX B727 SRM 53-10-5 FIG 2. ALODINED AND PRIMED IAW FX B727 SRM 51-10-2.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 50,653 hrs · 35,889 cycles
FOUND CORROSION ON FLOORBEAM STA 344,BL0-LBL30. REMOVED, FABRICATED, ALODINED. PRIMED AND PAINTED FLOORBEAM REPAIR AT STA 344 AT BL0-LBL30 ALL IAW FX SRZ 27-53007 AND B727 SRM'S 51-30-2,53-10-2 FIG 7 AND 51-20-151.
Part: SKIN — TORN (ZONE 500) · airframe 50,574 hrs · 35,813 cycles
LEFT WING OUTBORD FORE FLAP UPPER SKIN SECTION MISSING (HONEYCOMB EXPOSED) REFERENCE FEDEX NSRM N00007. ORDERED AND RECEIVED LEFT OUTBORD FORE FLAP. INSTALLATION, ADJUSTMENT AND OPERATIONAL CHECK WAS ACCOMPLISHED ON FEDEX NSRM N00079 IAW B727-200 MM 27-51-011-4.
Part: DOUBLER — CORRODED (ZONE 100) · airframe 50,574 hrs · 35,813 cycles
CORRSION FWD PIT BETWEEN STA 720D AND STA 720E INTERIOR SKIN BETWEEN STR 29L AND STR 29R. REMOVED CORROSION ORIG MAT .100 MAT REM .053 FAB PARTS, LOCATED AND DRILL ALODINE AND PRIME PARTS IAW B727 SRM 53-30-1, 51-10-6, 53-30-3, 53-30-2, 51-10-2, 51-20-1, FIG 2.
Part: DOUBLER — CORRODED (ZONE 100) · airframe 50,574 hrs · 35,813 cycles
CORRSION FWD PIT BETWEEN STA 720D AND STA720E INTERIOR SKIN BETWEEN STR 29L AND STR 29R. REMOVED CORROSION ORIG MAT .100 MAT REM .053 FAB PARTS, LOCATED AND DRILL ALODINE AND PRIME PARTS IAW B727 SRM 53-30-1, 51-10-6, 53-30-3, 53-30-2, 51-10-2, 51-20-1, FIG 2.
Part: STRINGER — MISREPAIRED (ZONE 200) · airframe 50,574 hrs · 35,813 cycles
IMPROPER STRINGER SPLICE AT STR 23R BETWEEN STA 680 TO 720. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED STRINGER REPAIR AT STA 680 TO 720 ON STRINGER 23R ALL IAW FX B727 SRM 53-10-3, 51-30-2 AND 51-10-2.
Part: DOUBLER — CORRODED (ZONE 100) · airframe 50,574 hrs · 35,813 cycles
CORROSION FWD PIT BETWEEN STA 720E AND STA 720F INTERIOR SKIN BETWEEN STRINGER 29R AND STRINGER 28R. REMOVED CORROSION FOUND OUT OF LIMITS ORIG MAT .100 MAT. REMAINING .038, REMOVED DAMAGE, FABBED REPAIR DBLR. LOCATED AND DRILLED, ALODINED, PRIMED, INSTALLED DOUBLER IAW B727 SRM 53-30-1, SRM 51-10-6, SRM 53-30-3 FIG 1, SRM 53-30-2, SRM 53-30-2.
Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 50,574 hrs · 35,813 cycles
AFT PIT INTERCOSTAL AT STA 950B STRINGER 28R IS CRACKED. REMOVED AND REPLACED INTERCOSTAL AT FS 950B, STRINGER 28R, IAW B727 SRM 51-30-2, IAW B727 MM 51-20-013-7.
Part: SKIN — MISREPAIRED (ZONE 100) · airframe 50,574 hrs · 35,813 cycles
EXTERNAL SKIN DOUBLER AT STA 950B STRINGER 28R REQUIRES EVALUATION. REMOVED IMPROPERLY INSTALLED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER IAW B727 SRM 53-30-3, 51-10-2, 51-30-2, 53-30-2.
Part: SKIN — MISREPAIRED (ZONE 100) · airframe 50,574 hrs · 35,813 cycles
EXTERNAL SKIN DOUBLER AT STA 715-720A AND STRINGER 28R REQUIRES EVALUATION. DOUBLER FOUND TO NOT CONFORM TO SRM STANDARDS. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED NEW DOUBLER AT STA 715 TO 720A BEWEEN STRINGERS 27R AND 28R ALL C/W IAW FX B727 SRM 53-30-3,51-30-2 AND 51-10-2.
Part: FAIRING — CORRODED (ZONE 100) · airframe 50,574 hrs · 35,813 cycles
RIGHT WING TO BODY FAIRING NR 3437 HAS CORROSION (EXFOLIATED). REMOVED ANGLE IAW B727 SRM 51-30-2. FABRICATED ANGLE IAW BAC DRAWING 65-25582. ALODINED AND PRIMED ANGLE IAW B727 SRM 51-10-2. INSTALLED ANGLE IAW B727 SRM 51-30-2. REMOVED TEE CHORD IAW B727 SRM 51-30-2. FABRICATED CHORD IAW BAC DRAWING 65-25582. ALODINED AND PRIMED TEE CHORD IAW B727 SRM 51-10-2. INSTALLED TEE CHORD IAW B727 SRM 51-30-2.
Part: STRINGER CLIP — CORRODED (ZONE 100) · airframe 50,574 hrs · 35,813 cycles
CORROSION FWD PIT A/C PLENUM AREA FRAME STA 720E BILGE AREA BETWEEN STRINGER 29R AND STRINGER 28R. REMOVED CORROSION IAW FX B727 SRM 51-10-6. FOUND BEYOND LIMITS IAW FX B727 SRM 53-10-1. REMOVED DAMAGED SECTION IAW FX B727 SRM 51-40-3. FAB REPAIR ANGLE IAW FX B727 SRM 53-10-4F15. ALODINED AND PRIMED IAW FX B727 SRM 51-10-2. PAINTED IAW FX B727 MM 51-20-001-17. INSTALLED REPAIR ANGLE IAW FX B727 SRM 51-30-2.
Part: SKIN — DENTED (ZONE 200) · airframe 50,574 hrs · 35,813 cycles
FUSELAGE SKIN DENTED BS 370 BETWEEN STR 3-R AND STR 6-R.
Part: STRINGER — DENTED (ZONE 100) · airframe 50,574 hrs · 35,813 cycles
FABRICATE AND INSTALL STRINGER REPAIR AT BODY STATION 500 AND S21R. REMOVED, FABRICATED AND INSTALLED STRINGER CHANNEL IAW FX B727-200 SRM 53-10-3. ALODINED AND PRIMED IAW FX B727-200 SRM 51-10-2.
Part: STRINGER — PUNCTURED (ZONE 500) · airframe 50,574 hrs · 35,813 cycles
STA 480 SR20R HAS PUNCTURE ON LOWER SIDE. REMOVED DAMAGE ON STRINGER/DYE PENETRANT INSPECTION IAW B727 SRM 53-10-3 FIG 2, NO CRACKS NOTED. FABRICATED AND INSTALLED 3 EACH STRINGER TIES IAW B727 SRM 51-30-2 AND BAC DRAWING NR 66-11809. REMOVED AND REINSTALLED BRACKET, SUPPORT ANGLE, AND STIFFENER IAW B727 SRM 51-30-2.
Part: SKIN — CRACKED (ZONE 100) · airframe 50,574 hrs · 35,813 cycles
PREVIOUS REPAIR,SKIN CUT-OUT APPEARS TO HAVE CRACK STA 500 S20R AND S21R. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLERS IAW B727 SRM 51-30-2, 53-30-30 FIG 3.
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 50,574 hrs · 35,813 cycles
L1 DOOR CUT-OUT UPPER HINGE CAVITY, FRAME IS CRACKED AROUND HOLE.
Part: SKIN — TORN (FORE FLAP) · airframe 50,574 hrs · 12,794 cycles
LEFT WING OUTBORD FORE FLAP UPPER SKIN SECTION MISSING (HONEYCOMB EXPOSED). REMOVED AND REPLACED LEFT WING OUTBORD FORE FLAP ASSEMBLY ON FEDEX SNRM N00079. REFERENCE NON ROUTINE N00007.
2003
Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
WHILE WORKING MAIN CARGO CLOSE CARD, FOUND CORROSION EMANATING FROM UNDERNEATH PLASTIC STRIP BS 825, RBL 15, WL 196
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON 950 FLOORBEAM UPPER AND LOWER SURFACE OF UPPER FLANGE AT NUT PLATE HOLE LBL 23 WL 208. REMOVED CORROSION ON BS 950 FLOORBEAM AT LBL 23 WL 208 OUT OF LIMITS IAW SRM 53- 10-1 FIG 5 REMOVED DAMAGED PORTION OF FLOORBEAM, FABRICATED AND INSTALLED REPAIR PARTS IAW FED EX EA 7-5310-69433.
Part: FRAME — DENTED (FUSELAGE) · airframe 48,346 hrs · 34,031 cycles
DENTED FRAME BS 1030 LBL 28 WL 150. REPAIRED DENTED FRAME IAW EA 7-5310-69419.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON FLOOR SUPPORT UNDER NUTPLATE BS 1165-1166, LBL 7, WL 155. REMOVED CORROSION ON FLOOR SUPPORT UNDER NUT PLATE BS 1165-1166, LBL 7, WL 155. AN AREA OF 1 X 2 INCHES. ORIGINAL THICKNESS .063 INCH. REMAINING .050 INCH OUT OF LIMITS PER SRM 53- 10-1. REMOVED FLOOR SUPPORT BS 1166-1155. FABRICATED REPAIR PARTS PER SRM 53-10- 5 & SR 27-53-039. ALODINED & PRIMED PER SRM 51-10-2. INSTALLED PARTS PER SRM 51-30-2.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON TOP OF UPPER LOBE FLOORBEAM AT BS 320 LBL 46. FOUND UPPER LOBE OF FLOOR BEAM AT BS 320 LBL-46 TO BE OUT OF LIMITS. REPAIRED FLOOR BEAM AT BS 320 LBL-46 IAW FED EX E.A. 7-5310-69427A.
Part: FRAME — DENTED (FUSELAGE) · airframe 48,346 hrs · 34,031 cycles
DENTED FRAME BS 950E, LBL 31, WL 150. DENT IN FRAME AT B.S. 950E, LBL 31, WL 150 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED FABRICATED U CHANNEL IAW EA 7-5310-69418 AND ER 03-1450 .
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON 950D FLOORBEAM UPPER FLANGE UPPER AND LOWER SURFACES RBL 25, LBL 25, WL 208. REMOVED CORROSION FROM FLOORBEAM BS 950D, RBL 10.5, FOUND OUT OF LIMITS IAW SRM 53-10-1. CUT OUT DAMAGED SECTION OF UPPER CHORD BS 950D LBL 37-RBL 37. FABRICATED REPAIR PARTS, INSTALLED IAW SRM 53-10-8 FIG 3, SRM 51-30-2 PG 13 &14.
Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION (C55-224-01) ON TOP OF FCD CREASE BEAM BS 325-40 LBL 60. REMOVED CORROSION ON TOP OF CREASE BEAM BS 325-340, OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED CREASE BEAM PER SRM 51-30-2, 51-10-2, 51-30-5.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON STRINGER CLIP, BS 720C STR 26R. REMOVED STRINGER CLIP BS 720C STR 26R, REMOVED CORROSION ON CLIP IN A 1 INCH X 1 INCH AREA. BLENDED 0.020 INCH FROM 0.040 INCH OUT OF LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED REPLACEMENT STR CLIP FROM 7075 T6 X 0.040 INCH NR 472905 IAW SRM 51-30-1 AND REINSTALLED AT BS 720C STR 26R IAW SRM 51-30-2.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION (C53-224-011) ON TOP OF UPPER LOBE FLOORBEAM AT BS 620, RBL 3, TO RBL 23. CORROSION AT BS 620, WL 208, RBL 3 TO RBL 23 DETERMINED TO BE OUT OF LIMITS IAW B727, SRM 53-10-1 FIG 4. REMOVED UPPER CHORD OF BEAM FROM LBL 32 TO RBL 36.5. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS. ALL WORK ACCOMPLISHED IAW B727 SRM 53-10-1, 53-10-8, 51-10-2 & 51-20-4.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON SHEAR TIE, BS 720 NEXT TO STR 26R. REMOVED CORROSION ON SHEAR TIE, BS 720 BETWEEN STR 26-27 RIGHT, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED, ALODINED AND PRIMED REPAIR PARTS. INSTALLED REPAIR, ALL WORK ACCOMPLISHED IAW SRM 51-10-3, 51-30-2, 51-30-5, 53-10-4 FIG 11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON FLOOR SUPPORT UNDER NUT PLATE BS 1165 - 1166, RBL 16, WL 155. REMOVED FLOOR SUPPORT BS 1166-1120, RBL 16, WL 155. FABRICATED REPAIR PARTS IAW SRM 53-10-5 AND SR 27-53-039. ALODINED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED IAW SRM 51-30-2.
Part: SKIN — DENTED (FUSELAGE) · airframe 48,346 hrs · 34,031 cycles
LT AFT FUSELAGE SEC 48, SKIN HAS A CREASED DENT AT BS. 1349, WL 196 APPROX 8 O'CLOCK POS. LEFT AFT FUSE, SEC 48, SKIN CREASE DENT AT B.S 1349, WL 196, REMOVED DAMAGE, FOUND TO GO THROUGH BONDED SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER IAW E.A 7-5450-69416.
Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 48,346 hrs · 34,031 cycles
COMPLY WITH EO 7-5210-7-2302 EOCN L1, PART 2 DUE TO CRACKS FOUND DURING INSPECTION PER PART 1ON FWD ENTRY DOOR. ALL WORK ACCOMPLISHED IAW FED EX E.O. 7-5210-7-2302 EOCN L1 PART 2
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON REINFORCEMENT FRAME, BS 1176.9, RBL 45 TO RBL 59, WL 208. REMOVED CORROSION ON REINFORCEMENT FRAME, BS 1176.9 RBL 45-59 WL 208. DETERMINED TO BE OUT OF LIMITS IAW 53-10-1. REMOVED AND REPLACED CHORD IAW SRM 51-30-2.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON FLOORBEAM LOWER FRAME AROUND NUT PLATE HOLES, B.S.720, LBL 16 TO LBL 21, W.L. 200 AT PREVIOUS REPAIR.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON FLOORBEAM REPAIR STRAP BS 1130, RBL 30-RBL 36, WL 200. REMOVED CORROSION ON FLOORBEAM REPAIR STRAP BS 1130, FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED STRAP, FABRICATED AND INSTALLED NEW STRAP IAW SRM 51-10-2, 51-10-3, 51-30-2, AND 51-30-5.
Part: PRESSURE PANEL — GOUGED (NLG WW) · airframe 48,346 hrs · 34,031 cycles
GOUGED AREA AT NLW UPPER WEB AT LT PRESSURE PANEL CUT OUT INBOARD SIDE, B.S 242. REMOVED DAMAGE AND REPAIRED IAW SRM 51-40-2. GOUGE WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1.
Part: WEB — GOUGED (RT WHEEL WELL) · airframe 48,346 hrs · 34,031 cycles
RT WHEEL WELL HAS GOUGE IN WEB. DAMAGE ON RT WHEEL WELL WEB COMMON TO K-BEAM AREA, BS 872, RBL 5.5, WL 150, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER FROM 7075-T6 .040 INCH, LOT NR 472905. ALODINED, PRIMED, PAINTED, AND INSTALLED IAW 53-10-1, 51-10-1, 51-40-2.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION WHILE WORKING CARD N00544 FOUND CORROSION ON FRAME BS 720C, STR-26R. REPAIRED FRAME IAW EA 7-5310-69431.
Part: FRAME — CORRODED (CARGO BAY LWR) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION FORWARD CARGO BAY ON LOWER FRAME AT STA 660, STR 28L TO 28R.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON WEB, STA 1174, RBL 18, WL 208. REMOVED CORROSION AT STA 1174. WEB FOUND OUT OF LIMITS. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-1Q0-1, 51-40-2.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 48,346 hrs · 34,031 cycles
WHILE WORKING N00939, FOUND CRACKED SHEAR TIE AT BS 328, STR 26-27 LEFT. REPAIRED SHEAR TIE BS 328, STR. 26-27 LEFT, IAW SRM 53-10-4 FIG. 15.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON FLOORBEAM REPAIR FILLER B.S. 1070, RBL 42 TO LBL 36. REMOVED CORROSION ON FLOORBEAM REPAIR FILLER BS 1070. FOUND TO BE OUT OF LIMITS. REMOVED FILLER, FABRICATED REPLACEMENT AND INSTALLED IAW SRM 53-10-1, 53-10-8.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,346 hrs · 34,031 cycles
CORROSION ON FLOORBEAM, UPPER FLANGE AT BS 680 RBL 11, DAMAGED ON REPAIR DOUBLER, NO DAMAGE LIMITS ON REPAIR DOUBLER, REPAIRED FLOORBEAM AT BS 680, WL 208, RBL 11, IAW SRM 53-10-8 FIG 3.
Part: SKIN — DENTED (FUSELAGE) · airframe 48,346 hrs · 34,031 cycles
SKIN DENT, BS 720B+3, JUST BELOW STR 17R, REWORKED SKIN DENT, BS 720B+3 BELOW STR 17R. A=1.8 Y=.062 A/Y=12.9 AND OIL CANNED. OUT OF LIMITS IAW 53-30-01. REMOVED DAMAGED AREA 2.3 X 2.9. FABRICATED, ALODINED, PRIMED AND PAINTED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION FWD CARGO BAY ON SKIN STA 640 STR 28L TO 28R WL 149. CORROSION FWD CARGO BAY ON SKIN STA 640, STR 28L TO 28R, WL 149, FOUND TO BE OUT OF LIMITS. REPAIRED AREA PER SRM 53-30-1, 53-30-3, 51-30-2.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON TOP OF UPPER LOBE FLOORBEAM AT BS 344, LBL 3, TO LBL 60. REMOVED CORROSION ON UPPER LOBE OF FLOORBEAM AT 344, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED, TREATED AND INSTALLED REPAIR UPPER LOBE IAW SRM 53-10-8, SR 27-53-007, 53-10-1.
Part: SKIN — DENTED (FUSELAGE) · airframe 48,346 hrs · 34,031 cycles
DENT IN SKIN BS 460-480 BETWEEN 14.15R
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
WHILE WORKING CARD FOUND LOWER NOSE FRAME LT SIDE TO BE CORRODED AT BS 296 LBL 20. FOUND LOWER NOSE FRAME LT SIDE TO BE OUT OF LIMITS AT BS 296, LBL 70. REMOVED AND REPLACED LT FRAME IAW SRM 51-20-1, 51-30-7, 51-30-5.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON FLOORBEAM UPR FLANGE BS 1110, RBL 57 TO LBL 57, WL 208.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON STR 28R, BS 480-484, WL 150, INBOARD SIDE. REMOVED CORROSION FROM STR 28R AT B.S 480+4 INCH, FOUND TO BE OUT OF LIMITS. FABRICATED, ALODINED AND PRIMED REPAIR PARTS, AND INSTALLED IAW SRM 51-10-4, 53-10-1, 53-10-3, 51- 30-2 AND MM 51-20-151-7.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON STR 24L AT BS 312. CORROSION ON STR 24 LT AT B.S 312, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. STRINGER 24 LT REPAIRED PER SRM 53-10-3 FIG 1.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON 950F FLOORBEAM UPPER FLANGE UPPER AND LOWER SURFACE FROM LBL 55 TO RBL 55, WL 208.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION IN SEVERAL AREAS IN STRINGER 26R FROM BS 620 TO 720A. REMOVED AND REPLACED STRINGER SECTION AT BS 675 - 720+10 IAW SRM 53-10-3.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON SKIN AT BS 702, RBL 20, WL 150, BETWEEN STR 26R AND 27R.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON TOP OF UPPER LOBE FLOORBEAM AT BS 560, RBL 3 TO RBL 23. CORROSION ON TOP OF FLOORBEAM AT BS 560, RBL 3 TO 13, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED, LOCATED, DRILLED, ALODINED, PRIMED, SEALED, AND INSTALLED REPAIR CHORD IAW SRM 51-30-2, 53-10-1, 53-10-8, 51-10-2.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON SHEAR TIE BS 720C NEXT TO STR 26R. REMOVED CORROSION ON SHEAR TIE AT BS 720C NEXT TO STR 26R. FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED FASTENER HOLES IN NEW SHEAR TIE AND INSTALLED IAW SRM 53-10-1, 51-30-2 PART #69-43683-3.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,346 hrs · 34,031 cycles
CORROSION ON FLANGES OF LONGITUDINAL FLOORBEAM BS 760-848, LBL 25, WL 208. REMOVED DAMAGE LONGITUDINAL BEAM, BS 760-848, LBL 25, WL 208, FABRICATED, ALODINED, PRIMED, AND INSTALLED REPLACEMENT LONGITUDINAL BEAM IAW SRM 51-30-2, 51- 30-5, 53-10-2, 51-10-2, 51-30-2.
2000
Part: SUPPORT FITTING — CRACKED (RT WING TE FLAP) · airframe 46,496 hrs · 32,503 cycles
DURING ROUTINE INSP RIGHT WING NR 2 FLAP TRACK FWD ATTACH FITTING FOUND CRACKED. REMOVED AND REPLACED PER IAW BAC SRM 51-30-2.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,496 hrs · 32,503 cycles
DURING ROUTINE INSP SHEAR TIE AT BS 950E AT STR 29L FOUND CORRODED. REMOVED, REPLACED AND FAB PER IAW BAC SRM 53-10-4.
Part: SUPPORT BRACKET — CRACKED (RT MLG WW) · airframe 46,496 hrs · 32,503 cycles
DURING ROUTINE INSP SUPPORT ANGLE IN RT WHEEL WELL AT THE BOTTOM OF THE BS 870 FITTING FOUND CRACKED. REMOVED, REPLACED AND FAB PER IAW BAC SRM 51-20-1, 51-30-2.
Part: FLOORBEAM — CORRODED (CABIN) · airframe 46,496 hrs · 32,503 cycles
DURING ROUTINE INSP LWR CHORD OF FLOORBEAM BS 720, BL 0 FOUND CORRODED. REMOVED, REPLACED AND FAB PER IAW BAC SRM 53-10-8.
Part: ATTACH FITTING — SHEARED (SLATS) · airframe 46,496 hrs · 32,503 cycles
DURING ROUTINE INSP THE NR 2 LEAD EDGE SLAT INBOARD LWR ATTACH FITTING FOUND SHEARED. REMOVED, REPLACED AND FAB PER IAW BAC SRM 51-10-1, 51-30-2.
Part: SUPPORT BRACKET — CRACKED (LT AILERON) · airframe 46,498 hrs · 32,503 cycles
DURING ROUTINE INSP LEFT I/B AILERON FOUND CRACKED AT LEAD EDGE SUPPORT BRACKET. REMOVED, REPLACED AND FAB PER IAW BAC SRM 51-20-1, 51-30-2.
Part: ATTACH FITTING — CRACKED (NLG WW) · airframe 46,496 hrs · 32,503 cycles
DURING ROUTINE INSP NOSE LANDING GEAR BAY, AFT BULKHEAD, ATTACH FITTING FOR ACTUATOR FOUND CRACKED. REMOVED AND REPLACED PER IAW BAC SRM 51-30-2.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,496 hrs · 32,503 cycles
DURING ROUTINE INSP NR 2 MAIN CABIN SEAT TRACK FOUND CORRODED AT BS 772. REMOVED, REPLACED AND FAB PER IAW BAC SRM 53-10-5.
Part: SKIN — CORRODED (FUSELAGE) · airframe 46,496 hrs · 32,503 cycles
DURING ROUTINE INSP FUSELAGE SKIN AT NR 1 ADF LOOP ANTENNA FOUND CORRODED. REMOVED, REPLACED AND FAB PER IAW BAC SRM 51-40-3.
Part: DUCT — UNSECURE (ACM BAY)
ON CLIMBOUT, AUTO FAIL & STBY LIGHT CAME ON. FOUND DUCT UNSECURED. SECURED DUCT ASSY USING SMP AS PRECAUTION PERF PRESS ADJ/TEST PER 727 MM 21-30-00-5. AC OK FOR SERVICE.
1998
Part: LOOP — OUT OF POSITION (NR 2)
98-244 WITH RT PACK ON, RT NR 2 BLD OPEN, LT PK OFF AND ALL OTHER BLDS CLOSED. THE LWR AFT BODY O/H LIGHT CAME ON PER RED TABS. LIGHT WENT OUT WHEN NR 1 ENG BLD AND LT PK WERE OPEN/TURN ON RESPECTIVELY. FOUND LOOP PUSH DOWN CLOSE TO RT DUCT WORK. REPOSITION LOOP AND ATTACH POINT. OPER RT PK WITH DESCRIBE BLD SET AS ABOVE. OPER CK NORM. NO LEAKS DETECT.
Part: STRINGER — WORN (BS 485)
LWR FWD CARGO GROOVE WORN INTO INSIDE OF STR 26L STA 485. BLENDED DAMAGE, INSIDE STR, INSTALLED STR SPLICE PER SRM 53-10-3.
Part: TRUNNION — CORRODED (LT MLG)
L/MLG FWD TRUNNION CASTING CORRODED AROUND LWR I/B BUSHING. REMOVED CORROSION, REAMED HOLES, RESURFACED BUSHINGS, FLAP PEENED AND ALODINED, PRIMED, PER FEDEX EA 7-5140-29514.
Part: STRAP — DAMAGED (BS 1176)
NR1276 MAIN CARGO 2 EA LARGE HOLES IN FLOOR STRAP LBL 4 STA 1176. INSTALLED FREEZE PLUGS AND NEW STRAP PER EA 7-5310-29491.
Part: STRAP — DAMAGED (BS 1176)
NR1277 - MAIN CARGO COMPT HAS 3 EA ELONGATED FASTENERS HOLES IN PREVIOUS STRAP REPAIR STA 1176 LBL 30 WL 212. INSTALLED FREEZE PLUGS AND NEW STRAP PER EA 7-5310-29491.
Part: FLOORBEAM — CORRODED (BS 1130)
AFT LOWER CARGO COMP CEILING, FLOORBEAM AT FS 1130 IS HEAVILY CORRODED IN AND AROUND CENTER CEILING SUPPORT STRAP BL 0. FABRICATED AND INSTALLED DOUBLER PER EA 7-5310-29488 DATED APRIL 23, 1988.
Part: BELLFRAME — DENTED (BS 520)
LWR FWD CARGO, DENT IN BELLFRAME BS 520, STR 23L TO 24L WEB DEFORMED. REPAIRED BELLFRAME AT BS 520, STR 23L TO 24L PER SRM 51-40-3.
Part: STRINGER — CRACKED (BS 520)
CRACK IN STRINGER 24L STATION 520. REPAIRED STRINGER PER SRM 53-10-3 AT STR 24L BS 520.
Part: SPAR CHORD — CORRODED (WS 207)
CORROSION ON RT WING REAR SPAR LOWER CHORD, WS 207. CORROSION WAS REMOVED AREA APPROX 7 WIDE, HEIGHT .625, .25 DEPTH. REPAIRED PER SRM 57-10-6, FIG 2, SHEET 4 AREA WAS NOT CHECKED AND NO CRACKS FOUND.
Part: SKIN — CORRODED (BS 685-690)
NR 0616, 71-C209-02, CORROSION ON BELLY SKIN BS 685-690 BLO IN FWD LOWER CARGO. CUTOUT CORROSION AND INSTALLED .080 2024T3 DOUBLER PER 53-30-3 FIG 1 PG 8.
Part: FRAME — DENTED (BS 600)
NR 0220, DENTS IN BELLFRAME (6 TOTAL) BS 600, STR 23L TO 25L DEFORMING WEB. CUT OUT DAMAGE AND INSTALLED TYP BELL FRAME REPAIR 51-40-3 W/EXCEPTION OF EA 7-5310-29458.
Part: SKIN — CORRODED (BS 660-668)
NR 0504, CORROSION ON BELLY SKIN IN LWR FWD CARGO BS 660 TO 668, STR 28R TO STR 28L. CUTOUT SKIN AND INSTALLED .080 2024T3 DOUBLER PER 53-30-3.
Part: FLOORBEAM — CORRODED (BS 620)
CORROSION ON FLOORBEAM BS 620, BL O LBL 24. CORROSION REMOVAL OUT OF LIMITS AT LBL 4. REPAIRED FLOORBEAM PER SRM 53-10-8. REPAIRED FLOORBEAM PER SRM 53-10-8.
Part: FLOORBEAM — CORRODED (BS 720)
NR 0980, 72-C235-02, UPPER LOBE, BS 720D, LBL 5, CORROSION ON FLOORBEAM AT FASTENER HOLES. REMOVED CORROSION. INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8.
Part: STRUCTURE — CORRODED (BS 720)
NR 1175 - 71-C209-02, HEAVY CORROSION UNDER SEALER AND STRINGER IN AREA OF STATION 720 TO 720A, TOP SIDE AFT OF CENTER BAY TO STA 720A. REMOVED CORRODED SECTION OF STRINGER AND SKIN. INSTALLED EXTERNAL SKIN DOUBLER SRM 53-30-3 AND STRINGER AND STRINGER SPLICE PER SRM 53-10-3.
Part: FLOORBEAM — CORRODED (BS 560)
NR 0894, 72-C235-02, UPPER LOBE, CORROSION ON FLOORBEAM, BS 560, BLO - RBL 24. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED PER SRM 53-10-8, 51-20-4, AND 51-30-2.
Part: FLOORBEAM — CORRODED (BS 680)
NR 0902, 72-C235-02, UPPER LOBE CORROSION ON FLOORBEAM BS 680, BLO - RBL 24. REMOVED CORROSION OUT OF LIMITS. INSTALLED REPAIR PER SRM 53-10-8. TREATED AND PRIMED.
1997
Part: SENSOR — FAILED (LT MLG)
LANDING GEAR FAILED TO RAISE AFTER TAKEOFF. CONDUCTED CHECKLIST, GOT TAKEOFF WARNING HORN WHEN FLAPS WENT TO 2. WING ANTI-ICE WOULD NOT GROUND TEST, CSD OIL COOLER SWITCH AUTO WENT TO NORMAL AT ROTATION. DUMPED FUEL, NORMAL LANDING. REMOVED AND REPLACED AIR SENSING SENSOR (M831) PER MAINTENANCE MANUAL 32-00, OPERATIONAL CHECK NORMAL.
Part: SENSOR — FAILED (NR 1 ENGINE)
TEN MINUTES AFTER TAKEOFF, THE GLARESHIELD FIRE WARNING LIGHTS AND WARNING BELL ACTIVATED WITH NO LIGHTS IN FIRE HANDLES OR LIGHTS ON CARGO SMOKE INDICATOR. DURING ENGINE AND WHEEL WELL FIRE TEST THE NR 1 ENGINE WOULD NOT TEST, ALL THREE ENGINES TESTED OK DURING FIREWALL TEST. WITHOUT ANY OTHER INDICATION OF FIRE NR 1 WAS BROUGHT BACK TO IDLE AND LEFT THERE FOR REMAINDER OF FLIGHT. ADD'L WHEN THE FIRE WARNING BELL WAS 1ST SILENCED THE GLARESHIELD FIRE WARN LIGHTS WENT OUT AND NEVER RE-ILLUM. ALL ENGINE INSTRUMENTS APPEARED NORMAL THROUGHOUT FLIGHT. FOUND ENG FIRE SENSOR INOP. REPLACED ENGINE FIRE LOOP SENSOR, RAN ENGINE AT POWER, SYSTEM TEST GOOD.
Part: RELAY — INOPERATIVE (P4 PANEL)
ON TAKEOFF PASSING 7,000 FT, FIRE BELL WENT OFF WITH FIRE LIGHTS ON GLARESHIELD. NO FIRE HANDLES ILLUMINATED, REPEAT GRIPE. FOUND DEFECTIVE RELAY R198. REMOVED AND REPLACED SAME, OPERATIONAL CHECKED GOOD. RAN ENGINES ON GROUND, ALL OPERATIONAL CHECKS GOOD. NO MASTER WARNINGS LIGHTS AND NO BELLS.
1996
Part: DUCT ASSY — LEAKING (NR 1 PYLON)
SECOND FLT OF DAY ON DEPARTURE, MAXIMUM POWER ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. LIGHT WENT OUT UPON RETARDING THROTTLES. RETURNED FOR UNEVENTFUL LANDING. FOUND LEAKS AT BALL NUT CONNECTION TO 8TH STAGE CHECK VALVE, FLEX LINE FROM 13TH STAGE TO THRUST REV T-CONNECTION. REMOVED AND REPLACED 8TH STAGE DUCT ASSEMBLY, HP VALVE FLEX LINE, HOSE ASSEMBLY AND RAN ENGINE, LEAK CHECK GOOD.
Part: OVERHEAT LIGHT — ILLUMINATED (NR 1 ENG STRUT)
DISCREPANCY: (MOCC 96-137) NR 1 ENGINE STRUT OVERHEAT ILLUMINATED MOMENTARILY ON TAKEOFF. EXTINGUISHED WHEN POWER WAS REDUCED TO QUIET EPR. SYSTEM TESTED OK. CORRECTIVE ACTION: INSPECTED NR 1 ENGINE STUB WING DUCTING FOR LEAKS, NO DEFECTS NOTED, OK FOR SERVICE.
Part: CLAMP — LOOSE (NR 1 ENGINE)
DISCREPANCY: SHORTLY AFTER TAKEOFF (APPROXIMATELY 5 MINUTES) ENGINE NR 1 STRUT OVERHEAT LIGHT CAME ON FOR ABOUT 1 MINUTE THEN WENT OUT. COMPLIED WITH RED TABS, TESTED SATISFACTORY. CORRETIVE ACTION: FOUND LOOSE CLAMP BY SENSOR AND WAS BLOWING ON IT, TIGHTEN CLAMP, NO LEAKS NOTED ON SENSOR. OK FOR SERVICE THIS STATION..
1995
Part: STRINGER — CORRODED (BS 530)
CORROSION ON STRINGER AT BS 530 LBL 23 WL 151. REMOVED DAMAGE, FABRICATED SPLICE, FILLER AND INSTALLED PER SRM 53-10-3.
Part: STRINGER — CORRODED (BS 740)
CORROSION ON STR AT BS 740 LBL 23 WL 150. CORROSION ON STR AT BS 740 LBL 23 WL 150 OUT OF LIMITS PER FEDEX SRM 53-10-1. CUT OUT DAMAGED AREA AND REPAIRED PER FEDEX SRM 53-10-3.
Part: SHEAR TIE — CORRODED (BS 1166)
AFT CARGO BAY, THERE IS CORROSION ON SHEAR TIES ON AFT SIDE OF FRAME AT BS 1166 RBL 4 LBL 18 WL 150. REMOVED AND REPLACED CORROSION ON SHEAR TIES BS 1166 RBL 4 LBL 18 WL 150, PER FEDEX SRM 53-10-1.
Part: SKIN — LIGHTNING STRIKE (CARGO DOOR)
LOWER FWD CARGO DOOR HAS MULTIPLE LIGHTNING STRIKES ALONG LOWER OUTER SKIN. REPAIRED 10 AREAS OF LIGHTNING STRIKES ALONG OUTER SKIN OF FWD CARGO DOOR LOWER, BS 560 TO 620 3.23 INCHES UP FROM BOTTOM OF DOOR, PER FEDEX SRM 52-00-2, 52-00-3 AND 53-30-3.
Part: BEAM — CORRODED (BS 264)
CORROSION ON 25G BEAM, BS 264 LBL 4 WL 208. REMOVED FLOOR PANELS FOR ACCESS, REMOVED AND REPLACED CORRODED 25G BEAM, BS 264 LBL 4 WL 208. INSTALLED NEW 25G BEAM BS 204 LBL 4 WL 208. REINSTALLED FLOOR PANELS.
Part: BEAM — CORRODED (RT HORIZ STAB)
CORROSION (73C032-03), ON THE T/E AFT UPPER CHORD AT STAB STA 206 AND STA 161 RIGHT HORZ STAB. REMOVED AND REPLACED T/E AFT UPPER CHORD ON RIGHT HORZ STAB, ALL WORK DONE IAW.
Part: SKIN — CORRODED (BS 481)
CORROSION ON SKIN UNDER LEVELING COMPOUND AT BS 481, BL 0 WL 150 (C53-113-0161). REPAIRED CORRODED AREA PER FEDEX EA 7-5310-25902 AND SRM 53-10-4.
Part: TORQUE BOX — CRACKED (RIGHT)
THE RT TORQUE BOX IS CRACKED BEYOND THE DOUBLER IN THE FWD RADIUS OF THE SUPPORT ANGLE, JUST BELOW THE VERTICAL ACTUATOR SUPPORT, TEMP REPAIR INSTALLED AND LOGBOOK ENTRY REQ. REPAIRED RT TORQUE BOX PER EA 7-5310-25836.
Part: FRAME — CRACKED (BS 1090)
THE UPPER FLANGE OF FRAME IS CRACKED AT BS 1090 STA 27R. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND REPAIRED UPPER FLANGE OF FRAME AT BS 1090 STR 27R PER FEDEX SRM 51-40-3.
Part: FRAME — PUNCTURED (BS 1050)
IN THE AFT CARGO BAY, THE UPPER FLANGE OF FRAME IS PUNCTURED AND HAS A DOUBLE HOLE AT BS 1050, RBL 19, WL 148. REPAIRED UPPER FLANGE OF FRAME AT BS 1050, RBL 19, WL 148 PER FEDEX SRM 51-40-3.
Part: FRAME — CRACKED (BS 312)
CRACKED FRAME AT BS 312 LBL 45 WL 173 NEAR STR 22L. REMOVED CRACKED FRAME AT BS 312 LBL 45 WL 173 AND INSTALLED NEW FRAME.
Part: FRAME — CRACKED (BS 700)
FRAME DENTED AT BS 700 RBL 32 WL 160 AND CRACKED. REMOVED DAMAGED AREA, FABRICATED REPAIR PART, ALODINED, PRIMED, INSTALLED AND PAINTED REPAIR PART PER FEDEX SRM 51-40-3.
Part: STRINGER — CORRODED (BS 525/528/530)
CORROSION ON STR 3 PLACES, BS 525, 528 AND 530 LBL 15 WL 150. MECHANICALLY REMOVED CORROSION ON STR 27 BS 525 TO 530 LBL 15 WL 150, FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1 AND 53-10-0. REPAIRED STR 7 AT BS 525 TO 530 LBL 15 WL 150 PER FEDEX SRM 53-10-3.
Part: FRAME — DAMAGED (BS 1190)
AFT CARGO BAY, THERE IS MECHANCIAL DAMAGE ON UPPER FLANGE OF FRAME AT BS 1190 RBL 20 WL 151. REPAIRED FLANGE OF FRAME PER SRM 53-10-1.
Part: FRAME — DAMAGED (BS 1110)
AFT CARGO BAY, THE UPPER FLANGE OF FRAME HAS MECHANICAL DAMAGE AT BS 1110 LBL 20 WL 150. REPAIRED FLANGE OF FRAME PER SRM 53-10-1.
Part: FRAME — PUNCTURED (BS 1090)
AFT CARGO BAY, THE UPPER FLANGE OF FRAME IS PUNCTURED AT BS 1090 RBL 20 WL 148. REPAIRED FLANGE OF FRAME PER SRM 53-10-1.
Part: FRAME — PUNCTURED (BS 1010)
AFT CARGO BAY, THE UPPER FLANGE OF FRAME IS PUNCTURED AT BS 1010 RBL 24 WL 146. REPAIRED FLANGE OF FRAME PER SRM 53-10-1. REPAIRED FLANGE OF FRAME PER SRM 53-10-1.
Part: FRAME — DAMAGE (BS 1110)
AFT CARGO BAY, THE UPPER FLANGE OF FRAME HAS MECHANICAL DAMAGE AT BS 1110 RBL 20 WL 150. REPAIRED FLANGE OF FRAME PER SRM 53-10-1.
Part: FRAME — PUNCTURED (BS 1090)
AFT CARGO BAY, THE UPPER FLANGE OF FRAME IS PUNCTURED AT BS 1090 LBL 22 WL 149. REPAIRED FLANGE OF FRAME PER SRM 53-10-1.
Part: FRAME — PUNCTURED (BS 1090)
AFT CARGO BAY, THE UPPER FLANGE OF FRAME IS PUNCTURED AT BS 1090 LBL 20 WL 148. REPAIRED FLANGE OF FRAME PER SRM 53-10-1.