N462FE

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,098 hrs · 29,628 cycles

"EMERGENCY EXIT LIGHTS BATTERIES ARE DEAD. LIGHTS WON'T TEST." REPLACED BATTERIES IN BOTH PORTABLE EMERGENCY LIGHT ASSY IAW AMM 33-50-101-2-0. (CLOSED)

Part: ACTUATOR — FAILED (NR 2 SLAT) · airframe 41,268 hrs · 28,948 cycles

FLIGHT TEST-THE NR 2 LED FAILED TO RETRACT AFTER TAKEOFF. NR 2 SLAT ASSY FOUND TO BE RETRACTED WITH ACFT INBOUND AND NR 2 SLAT INTRANSIT AMBER LIGHT ILLUM IN COCKPIT ON FWD PNL AND S/O IND PNL. T/S NR 2 SLAT INDICATION IAW MM 27-82-000-1 AND FOUND TO BE FAULTY NR 2 SLAT ACTUATOR RETRACT SWITCH. REMOVED AND REPLACED NR 2 SLAT ACTUATOR ASSY IAW MM 27-81-032-4. OPS LEAK CK GOOD IAW MM 27-81-032-4. OPEN

Part: SKIN — GOUGED (BS 620 S5-8L) · airframe 41,261 hrs · 28,935 cycles

PREVIOUS REPAIR AT BS 620 BETWEEN STR 5L AND STR 8L GOUGED. CUT-OUT DAMAGED AREA. FABRICATED FILLER REPAIR, AND DOUBLER IAW SRM 53-10-2 FIG 3A AND 51-40-2 FIG 1, TREATED AND PRIMED PARTS & AREA IAW SRM 51-10-2, INSTALLED DOUBLER, FILLER REPAIR IAW SRM 51-40-2 FIG 1.

Part: SKIN — DAMAGED (BS 620 S11-12L) · airframe 41,261 hrs · 28,935 cycles

PREVIOUS REPAIR AT BS 620 BETWEEN STR 11L AND STR 12L IS GOUGED TRIMMED AREA, FABRICATED FILLER AND DOUBLER REPAIR IAW SRM 53-10-2 FIG 3A AND 51-40-2 FIG 1. TREATED AND PRIMED DOUBLER, FILLER AND AREA IAW SRM 51-10-2, INSTALLED DOUBLER & FILLER REPAIR IAW SRM 51-40-2 FIG 1.

Part: RIB — CRACKED (ZONE 600) · airframe 41,261 hrs · 28,935 cycles

NR 6 SLAT RIB IS CRACKED, OTBD SIDE OF ACTUATOR FWD ATTACHMENT. REMOVED CRACKED RIB AT NR 6 SLAT OUTBD SIDE OF ACTUATOR IAW SRM 51-30-2 FABRICATED NEW SLAT RIB, HEAT TREATED RIB TO T6 IAW FAS ENGINEERING REPORT 2-37153-801 REV A VERIFIED HARDNESS IAW NDTM PT 6 51-00-00 FIG 20, LOCATED, DRILLED AND DE-BURRED NEW SLAT RIB IAW SRM 51-30-5 TREATED AND PRIMED RIB IAW SRM 51-10-2 INSTALLED NEW RIB IAW SRM 51-30-2.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 41,261 hrs · 28,935 cycles

AFT AIRSTAIR AREA, RT LWR TORQUE BOX UPPER SUPPORT ANGLE IS CRACKED AT BS 1263. FABRICATED NEW SUPPORT ANGLE IAW SRM 53-10-2, 51-30-5 AND 51-30-6 INSTALLED NEW SUPPORT ANGLE LOWER TORQUE BOX IAW SRM 51-30-2.

Part: DOUBLER — CRACKED (ZONE 100) · airframe 41,261 hrs · 28,935 cycles

AFT AIRSTAIR AREA, LT LWR TORQUE BOX LIGHTNING HOLE HAS CRACK BS 1243 ROUTED OUT CRACKED AREA AT AFT AIRSTAIR AREA LT LWR TORQUE BOX LIGHTNING HOLE BS 1243 IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1 AND 51-30-5. TREATED AND PRIMED DOUBLER IAW SRM 51-10-2 INSTALLED. REPAIR DOUBLER IAW SRM 51-30-2.

Part: FRAME — CRACKED (BS 560) · airframe 41,261 hrs · 28,935 cycles

FORWARD CARGO, STA 560, STR 21L - 22L, STUB FRAME EXTENSION CRACKED IN RADIUS. REMOVED CRACKED STUB FRAME EXTENSION AT FWD CARGO STA 560 S21-22L IAW SRM 51-30-2. HEAT TREATED STUB FRAME IAW FAS ENG REPORT 2-37153-801 REV A CW CONDUCTIVITY MEASUREMENT IAW NDTM DT 6 51-00-00 FIG 20 IACS 33.1%. FABRICATED NEW STUB FRAME IAW SRM 51-30-5 DWG 53FX1350 REV A. TREATED & PRIMED IAW SRM 51-10-2. INSTALLED IAW SRM 51-30-2.

Part: SPAR — DAMAGED (RT WING) · airframe 41,261 hrs · 28,935 cycles

RT WING T/E FALSE SPAR INBD REPAIR HAS LOOSE FASTENER IN THE UPPER SECTION WBL 118. FABRICATED REPAIR PARTS , NEW LOWER CHORD, ANGLE REPAIR , HEAT TREATED 7075 'O' TO T6 CONDITION IAW FAS ER 2-37153-801 REV A, NEW STRAP, TWO RADIUS FILLERS & NEW DOUBLER IAW DRAWING SR27-57-038, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2, INSTALLED REPAIR PARTS IAW DRAWING SR27-57-038 AND SRM 51-30 -2.

Part: SPAR — CRACKED (ZONE 500) · airframe 41,261 hrs · 28,935 cycles

CRACK ANGLE LT WING FALSE SPAR AT NR 7 SPOILER ATTACH FITTING. CUT ANGLE AT LT WING FALSE SPAR IAW FX DWG SR 27-57-038 REV C. FABRICATED 2 ANGLES. HEAT TREATED ANGLES FROM 'O' TO T6 IAW FAS ENG REPORT NR 2-37153-801 REV A, FABRICATED DOUBLER, WEB, LOWER ANGLE, STRAP IAW DWG NR SR 27-57-038 REV C, TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED ALL PARTS IAW DWG NR 27-57-038 REV C.

Part: TRANSCEIVER — FAILED (WX RADAR SYSTEM) · airframe 40,492 hrs · 28,344 cycles

(AIR-TURN-BACK), WX RADAR PAINTS INTERMITTENT FALSE RETURNS ONE SIDE THEN THE OTHER, STABILIZED OR UNSTABILIZED. WHEN UNSTABILIZED, RADAR PAINTS A SINGLE SPOKE AT THE 11 -12 O'CLOCK POSITION. GOING BACK TO STABILIZED, IT PAINTS A DOUBLE SPOKE. VERIFIED OLD RADAR RT PAINTING FALSE IMAGES EVEN ON GND. REMOVED AND REPLACED RADAR RT AND ALL FUNCTIONAL CHECKS GOOD PER M/M 34-41-000-5 PARA 1A-5J. A/C OK FOR SERVICE.

Part: CARRIAGE — DAMAGED (TE FLAPS) · airframe 40,024 hrs · 27,986 cycles

SPLIT FLAPS OUTBOARD ON DEPARTURE. COMPLIED WITH QRH FLAPS WOULD NOT RETRACT VIA ALTERNATE METHOD. CREW DEBRIEFED OUTBD FLAPS STAYED AT 5 DEG WHILE INBD FLAPS CAME TO 2 DEG AS COMMAMDED. L/E VALVE C/B ON P6 PANEL PULLED BY CREW AS PART OF QRH. REF WRI 27-50/9927. FOUND LT O/B FLAP, I/B SEQUENCING CARRIAGE, (ON TOP OF FLAP CARRIAGE) HAS ROLLERS MISSING. NO DAMAGE NOTED ON FLAP TRACK, OR TO THE SEQUENCING CARRIAGE CASTING. COMPLETED INSTALLATION OF LT WING, O/B FLAP, I/B TRACK TOGGLE LINK CARRIAGE PER 727-200 M/M 27-51-014-2.

Part: ROD — UNKNOWN (NLG) · airframe 39,752 hrs · 27,762 cycles

AFTER TAKE OFF FROM MEM, GEAR WAS RET AND THE FWD RED GEAR DOORS LT REMAINED ILLUM WITH ASSOC NOSE GEAR DOOR LT ILLUM ON S/O'S PANEL. C/W QRH, RECYCLED GEAR AND IND REMAINED. CONT'D FLT WITH APPROPRIATE RESTRICTIONS. UPON LDG IN ICT WITH NORM TOUCHDOWN, THE NOSE GEAR BEGAN TO SHAKE VIOLENTLY AT ABOUT 120KTS. NOSE WHEEL STEERING WAS NOT AVAIL. STOPPED A/C ON THE RWY AND HAD NOSE GEAR PINNED AND TOWED IN. REMOVED AND REPLACED NOSE GEAR PISTON POS ROD, APEX PIN PER M/M. REMOVED AND REPLACED RT AFT NOSE GEAR DOOR PER M/M. REMOVED AND REPLACED LOWER NOSE GEAR TORSION LINK PER M/M. REMOVED AND REPLACED NOSE GEAR POS SW PER M/M AND OP'S CK'D PER MM. OP'S CK GOOD. PERF'D NOSE GEAR EXT/RET PER M/M AND CK'D NOS

Part: FITTING — CORRODED (FUSELAGE) · airframe 39,637 hrs · 27,669 cycles

LOWER AFT SUPPORT TEE HAS CORROSION ON UPPER SURFACE AT FWD END OF LOWER BODY PANEL NR 3218 (INST AFT OF BEACON LIGHT). REMOVED STROBE LIGHT ASSY MOUNT IAW SRM 53-10-01. CHECK ALLOWABLE DAMAGE LIMITS IAW FOUND TO BE OUT OF LIMITS. FABRICATED T-CHORD AND STIFFENER ON THE MAE TRAVELER T7/667682 AND T7/667683. FABRICATED NEW U-CHANNEL ASSY ON MAE TRAVELER T7/667684. DRILLED AND LOCATED T-CHORD, STIFFENER, U-CHANNEL IAW SRM 51-30-2. INSTALLED T-CHORD, STIFFENER AND U-CHANNEL IAW SRM 51-30-2.

Part: SHROUD — CRACKED (L2 DOOR) · airframe 39,637 hrs · 27,669 cycles

LT AFT SERVICE DOOR FWD UPPER END SHROUD HAS CRACKS 2 PLACES APPROX 8 IN AND 6 IN FROM FWD UPPER CORNER. CONTAINED CRACK IN SHROUD BY STOP DRILLING IAW SRM 51-10-1 PARA 10. TREATED AND PRIMED AREA IAW SRM 51-10-1. RESEALED AREA IAW DWG 65-56992 AND MM 51-30-001-1. PREPPED AND PAINTED IAW MM 51-20-151-7.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 39,637 hrs · 27,669 cycles

MCD DOOR EXTERNAL SKIN AT AFT LOWER EDGE HAS DISTORTED AND CRACKED SKIN. BLENDED AREA IAW SRM 51-10-1 AND 52-00-2, ORIG MAT'L .063IN AFTER REWORK .061IN. WITHIN LIMITS IAW SRM 52-00-2, FIG NR 1. REMOVED DAMAGED ON SKIN EDGE AMOUNT OF MAT'L. REMOVED WAS 0.003 WITHIN LIMITS IAW SRM 52-00-2 FIG NR 1. HFEC IAW NTM 51-00-00 PT6. NO CRACK NOTED. TREATED AND PRIMED IAW SRM 51-10-2. PREPPED AND PAINTED AREA IAW MM 51- 20-151-7. CLASSIFIED AS MINOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,637 hrs · 27,669 cycles

CABIN FLOOR SUPPORT (BEAM ) HAS CORROSION FS 620, LBL 35. FABRICATED REPAIR ANGLES PER DWG SR27-53-033 AND MAE TRAVELER T7/669736 CUT OUT DAMAGED AREA IAW DWG SR27-53-033. TREATED AND PRIMED CUT OUT DAMAGE IAW SRM 51-10- 2. FABRICATED FILLER FROM 7075-T6 .125C BATCH NR 1046555 IAW DWG SR27-53-033. INSTALLED ANGLES AND FILLER REPAIR IAW SRM 51-30-2.

Part: BRACKET — CRACKED (NLG WW) · airframe 39,637 hrs · 27,669 cycles

NLG W/W CEILING THRU LT ACCESS PNL LT SUPPORT HAS CRACKS ON BOTH ENDS FS 259.50. REMOVED SEAT TRACK FOR ACCESS IAW SRM 51-30-2. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-30-2. REINSTALLED SEAT TRACK IAW SRM 51-30-2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,637 hrs · 27,669 cycles

CABIN FWD RT GALLEY DOOR EXT UPPER HINGE CUT OUT DOOR SKIN HAS A CRACK. STOPPED DRILLED CRACK IAW SRM IAW SRM 52-00-3 FIG 3. FABRICATED REPAIR DOUBLER FROM 2024 T-3 .080C. INSTALLED REPAIR IAW SRM 52-00-3 FIG 3. REPAIR CLASSIFIED AS A MAJOR REPAIR.

Part: BULKHEAD — CORRODED (BS 720D) · airframe 39,637 hrs · 27,669 cycles

FOUND FWD CARGO STA 720D LWR BULKHEAD BEAM HAS CORROSION AT LBL25. REMOVED AND REPLACED ANGLE IAW SRM 51-30-2.

Part: SUPPORT BRACKET — CRACKED (NR 2 FLAP TRACK) · airframe 39,637 hrs · 27,669 cycles

NR 2 FLAP TRACK AFT SUPPORT BRACKET IS CRACKED OTBD AFT END. REMOVED AND REPLACED BRACKET IAW SRM 51-30-2.

Part: FRAME — UNKNOWN · airframe 39,637 hrs · 27,669 cycles

FOUND AFT PIT FRAME REPAIR, STA 970, ABOVE S23L TO S24L. COMPLY WITH ATTACHMENT "B" OF EO 7- 5100-7-5005 PT2. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.

Part: TORQUE BOX — UNKNOWN (BS 1227) · airframe 39,637 hrs · 27,669 cycles

EXTERNAL DOUBLER SECTION 48, RT LOWER TORQUE BOX, ATA 1227.5,RBL 20, WL 190. COMPLY WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.

Part: STRINGER — UNKNOWN (BS 1050-1070) · airframe 39,637 hrs · 27,669 cycles

AFT PIT FUSE STRINGER REPAIR, STA 1050- 1070,S20R. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.

Part: SKIN — UNKNOWN · airframe 39,637 hrs · 27,669 cycles

THE MAIN CARGO DOOR HAS 4 EXTERNAL DOUBLERS ON ITS INTERNAL SKIN ALONG THE TOP EDGE AT STATIONS 520, 540, 560, AND 580. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.

Part: STRINGER — UNKNOWN · airframe 39,637 hrs · 27,669 cycles

AFT PIT, FUSE STRINGER REPAIR STA 1130- 1166,S29. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.

Part: TORQUE BOX — UNKNOWN (BS 1237) · airframe 39,637 hrs · 27,669 cycles

FOUND EXTERNAL DOUBLER, SECTION 48, RT LOWER TORQUE BOX STA 1237, RBL 20, WL 189. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.

Part: STRINGER — UNKNOWN · airframe 39,637 hrs · 27,669 cycles

AFT PIT, FUSE STRINGER REPAIR, STA 1070- 1090,S20R. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.

Part: TORQUE BOX — UNKNOWN (BS 1238) · airframe 39,637 hrs · 27,669 cycles

FOUND EXTERNAL DOUBLER, SECTION 48, RT LOWER TORQUE BOX STA 1238, RBL20, WL 183. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2.

Part: FRAME — UNKNOWN · airframe 39,637 hrs · 27,669 cycles

FOUND AFT PIT FRAME REPAIR STA 950, ABOVE S24L TO S25L. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.

Part: FLOOR SKIN — CORRODED (BS 435) · airframe 39,637 hrs · 27,669 cycles

E/E COMPT RT O/B FLOOR PNL WEB HAS CORROSION FS - 435, REMOVED AND REPLACED DAMAGED WEB AT STA 435 IAW SRM 51-30-2. NEW WEB MADE ON TRAVELER T7/665341.

Part: SEAT TRACK — CORRODED (740-840) · airframe 39,637 hrs · 27,669 cycles

FOUND MAIN DECK SEAT TRACK STA 740-850 RBL-45 HAS AREA OF BARE METAL AND CORROSION. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 620-720F) · airframe 39,637 hrs · 27,669 cycles

CABIN SEAT TRACK HAS CORROSION SPOTS FS 620-720F LBL 45, REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 620-700) · airframe 39,637 hrs · 27,669 cycles

CABIN SEAT TRACK HAS CORROSION SPOTS FS 620 - 700 RBL 24. REMOVED AND REPLACED SEAT TRACK FS 620 - 700 RBL 24 IAW SRM 51-30-2.

Part: APU — FIRE · airframe 38,947 hrs · 27,120 cycles

DURING MTC WALKAROUND, FOUND FLAMES COMING FROM FLOW MULT FRESH AIR INLET. IMMEDIATELY SHUTDOWN APU, AND EXTINGUISHED FIRE, FIRED APU FIRED PERFORMED APU START USING ALT FIRE PROT, WITH NO DEFECTS. TURNED ON ENG NR 2 BLEED AIR AND WITHIN 30 SEC. BLEED AIR TRIPS OFF WITH ASSOC LIGHT DUE TO FIRE. IN FLOW MULT SUSPECT POSSIBLE O'HEAT SENSOR. REMOVED FLOW MULT IAW MM. REMOVED AND REPLACED APU FIRE EXT BOTTLE IAW AMM. REMOVED AND REPLACED LEFT AND RIGHT COALESCER BAG. REPLACED FLOW MULT IAW MM. RAN APU AND LT AND RT A/C PACKS WITH ALL SYS OPS NORM. PERFORMED MX ENG RUN AND RAN A/C PACKS TO CLEAR ALL DUCTS AND ACM. A/C OK FOR SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 38,335 hrs · 26,631 cycles

CORROSION ON SEAT TRACK FLANGE BETWEEN STA 560 AND 600 AT LBL 24. REMOVED AND REPLACED SEAT TRACK FROM STA 480 TO 630 AT LBL, 24 IAW FX B727 SRM 53-10-5 FIG 1, 51-10-2 AND 51-30-2.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 38,335 hrs · 26,631 cycles

UPPER CHORD FLOORBEAM AT FS 344 LBL 22.5 TO RBL 22.5 CORRODED. REMOVED, FABRICATED AND INSTALLED CHORD AND HAT-CHANNEL IAW FED-EX DRAWING SR-27-53-007 AND B727 SRM 51-30-2.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 38,335 hrs · 26,631 cycles

CORROSION ON FLOORBEAM UPPER SURFACE STA 560 LBL 24-62. REMOVED, FABRICATED, AND REPLACED T-CAP, WEB AND STIFFENER IAW B727 SRM 53-10-8 FIG 3, 51-10-2 AND 51-30-2.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,416 hrs · 25,897 cycles

CORROSION EXT SKIN, BS 470 WL 148 CORROSION WHERE MOD S ANT MOUNTS. *S/D* REPAIRED PER SRM 53-30-1 AND 53-30-3.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 37,416 hrs · 25,897 cycles

RT MLG WHEEL WELL VERTICAL L-ANGLE CRACKED BS 870 RBL 6 FWD OF APU LWR CORNER . REMOVED AND REPLACED RT WHEEL WELL VERTICAL L-ANGLE BS 870 RBL 6 IAW SRM 51-30-5, 51-30-2, AND 51-10-2.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,416 hrs · 25,897 cycles

CORROSION ON STR 28R, AROUND FASTENER HOLES ATTACHING KEELBEAM, STA 722, FWD CARGO BAY. CORROSION ON STR NR 28 RT AROUND FASTENERS HOLES ATTACHING KEELBEAM STA 727 FWD CARGO BAY. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED DAMAGE AREA PER SRM 53-10-3 & SRM 51-30-2.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,416 hrs · 25,897 cycles

WHILE REMOVING CORROSION ON SHEAR TIE AT BS 1148 BETWEEN STRINGERS 28L AND 28R CORROSION WAS FOUND TO BE .100 PERCENT THROUGH THE FRAME. ALL WORK DONE PER E.A. 7-5310-55378

Part: DOOR — CORRODED (EMERGENCY EXIT) · airframe 37,416 hrs · 25,897 cycles

CORROSION LT FWD OVERWING ESCAPE HATCH, ALONG LWR EDGE UNDER PRESSURE SEAL. BLENDED CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1 & REPAIRED PER SRM 51-30-5 & 51-30-2.

Part: BRAKE ASSY — FIRE (MLG) · airframe 35,456 hrs · 24,358 cycles

FIRE IN RIGHT MAIN LANDING GEAR BRAKE AFTER SHUTDOWN CLEARED TO LAND ON 19R AT ICT. WINDS 020/8. TOOK LONGER THEN NORMAL TO SLOW DOWN TO TAXI SPEED. EVERYTHING ELSE WAS OTHERWISE NORMAL. FIRE STARTED AFTER BLOCK IN. FIRE WAS AT NR 3 BRAKE ASSEMBLY. INSPECTED RIGHT MAIN GEAR ASSEMBLY PER M/M 05-51- 121-2 AND REMOVED & REPLACED NR 3 BRAKE AND TIRE PER M/M 32-41-032-4 & 32-45-001-4. NO DAMAGE WAS NOTED TO RIGHT GEAR STRUT ASSEMBLY.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,294 hrs · 24,218 cycles

CORROSION ON FLOORBEAM BS 900, LBL 43. REMOVED AND REPLACED FLOORBEAM PER EA 7- 5310-64924.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 35,294 hrs · 24,218 cycles

MECHANICAL DAMAGE TO FRAME AT BS 720, STR 4L AND CEILING SUPPORT. REMOVED AND REPLACED FRAME PER SRM 53-10-4.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,294 hrs · 24,218 cycles

SHEAR WEB BULGING AROUND FASTENERS BS 1147, LBL 53-61, WL 208. REMOVED AND REPLACED WEB & FLOORBEAM PER SRM 51-40-2 FIG 1 & 53-10-8 FIG 3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,294 hrs · 24,218 cycles

WHILE WORKING FOUND FRAME CRACKED AT BS 720, LBL 2, WL 154. REMOVED AND REPLACED FRAME PER SRM 51-40-3 & EA 7-5310-64910.

Part: FRAME — DENTED (FUSELAGE) · airframe 35,294 hrs · 24,218 cycles

FRAME 600 DENTED AT OPEN HOLES 5R. REMOVED AND REPLACED FRAME PER SRM 53-10-4 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,294 hrs · 24,218 cycles

CORROSION ON LOWER SURFACE OF FLOORBEAM FWD FLANGE AT BS 360, LBL 3.1, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 3.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,294 hrs · 24,218 cycles

CORROSION ON STR 27L, BS 657 LOWER LOBE (C53-111-01-2). REMOVED AND REPLACED STRINGER PER SRM 53-10-1, 51-20-2, 53-10-2, 53-10-3.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 35,294 hrs · 24,218 cycles

HOLES IN SHEAR TIE AND SKIN AT BS 600 BETWEEN STR 27 & 28 L. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4, 51-30-2 & EA 7-5330-54321.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,294 hrs · 24,218 cycles

SKIN DENTED AT BS 1130 3 INCHES BELOW STR 23 R. REMOVED AND REPLACED SKIN PER SRM 53-30-1 & 53-30-3 FIG 3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,294 hrs · 24,218 cycles

CORROSION ON FLOORBEAM UPPER FLANGE BS 312, LBL 27, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 51-10-1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,294 hrs · 24,218 cycles

HOLES IN SHEAR TIE AND SKIN AT BS 580 BETWEEN STR 27 & 28L. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4, 51-30-2 & EA 7-5330-54321.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,294 hrs · 24,218 cycles

SKIN DENTED AT BS 1130 2 INCHES ABOVE STR 25 R.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,294 hrs · 24,218 cycles

CORROSION ON FLOORBEAM UPPER SURFACE BS 348, LBL 25-50, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,294 hrs · 24,218 cycles

EXTERIOR SKIN DAMAGED JUST AFT OF FWD E BAY DOOR AT BS 226, RBL 5. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 1.

Part: SKIN — GOUGED (FUSELAGE) · airframe 35,294 hrs · 24,218 cycles

GOUGE IN EXTERNAL SKIN AT STR 17L, BS 400. REMOVED AND REPLACED SKIN PER SRM 53-30-3 & EA 7-5330-54245.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,294 hrs · 24,218 cycles

CORROSION ON SKIN BS 720D+16, STR 26L. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 5 & EA 7-5330-64102.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,294 hrs · 24,218 cycles

CORROSION ON KEEL BEAM AT BS 950E+9, WL 139, LBL 6.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 35,294 hrs · 24,218 cycles

HOLES IN FRAME AT BS 870, STR 9 RT. REMOVED AND REPLACED FRAME PER EA 7-5310-64105.

Part: FRAME — DENTED (FUSELAGE) · airframe 35,294 hrs · 24,218 cycles

N 329 FRAME DENTED AT BS 950F BETWEEN STR 26 & 25 LT. R&R FRAME IAW SRM 51-40-03 FIG 1.

Part: FRAME — DENTED (FUSELAGE) · airframe 35,294 hrs · 24,218 cycles

N 653 FRAME DENTED AT BS 990 AT STR 26 LT. R&R FRAME PER SRM 51-40-3 & 51-10-2.

Part: FRAME — DENTED (FUSELAGE) · airframe 35,294 hrs · 24,218 cycles

FRAME DENTED AT BS 970 BETWEEN STR 25 & 26 LT. REMOVED AND REPLACED FRAME PER SRM 51-40-3 & EA 7-5310-64087.

Part: PLUNGER — STUCK (MLG DOOR SWITCH)

AMBER NOSE GEAR DOOR LIGHT ILLUM ON 2ND OFF PNL AFT GEAR EXT. RED DOOR LIGHT ALSO ILLUM ON FWD PNL. LEFT NOSE LANDING GEAR DOOR SWITCH PLUNGER STICKING. CLEANED AND LUBED PER MM 32-62-011-5. OPS CHECK NORMAL.

Part: VALVE — LEAKING (NR 3 ENGINE)

ON CLIMBOUT, ENGINE NR 3 STRUT OVERHEAT LIGHT CAME ON. COMPLETION OF RED TABS EXTINGUISHED LIGHT. OPERATED NR 3 ENGINE WITH NO FURTHER ILLUMINATION OF LIGHT. NR 3 BLEED AND NR 2 PACK TURNED OFF AND LEFT OFF PER RED TABS. REMOVED PYLON PANELS 5501-5502 FROM RIGHT SIDE FOUND 8TH STAGE BLEED CHECK VALVE LEAKING DOWN STEAM SIDE OF VALVE. INSTALLED 2 NEW GASKETS IN BLEED CHECK VALVE LEAK CHECKS GOOD RAN NR 3 ENGINE PER JET RUN HANDBOOK OPERATIONAL CHECKS GOOD.

Part: CLAMP — LOOSE (NR 3 ENGINE)

ON CLIMBOUT PASSING APPROXIMATELY FLIGHT LEVEL 270, ENGINE NR 3 STRUT OVERHEAT LIGHT CAME ON. LIGHT WENT OUT WHEN NR 3 POWER LEVER PULLED TO IDLE. RESTORED POWER AND LIGHT DID NOT COME BACK ON. FOUND ONE CLAMP LEAKING AT CHECK VALVE GOING TO AIR CLEANER. REPOSITIONED CLAMP AND TIGHTENED UP LEAK CHECKED GOOD. NOT IN LOG BOOK BUT LEAK AT CLAMP GOING TO PERCOOLER, NOT AIR CLEANER ON 8TH STAGE BLEED AIR LINE.

Part: CLAMP — INOPERATIVE (NR 3 ENGINE)

ON CLIMBOUT WITH AIRCRAFT CLEAN AND CLIMB POWER SET AT APPROXIMATELY 7,000 FEET THE ENGINE NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. COMPLIED WITH RED TAB PROCEDURE AND LIGHT WENT OUT AND STAYED OUT FOR REMAINING 30 MINUTE OF FLIGHT. FOUND 6TH STAGE DUCT LEAKING AT CLAMP DOWNSTREAM OF CHECK VALVE. REMOVED AND REPLACED CLAMP, OPERATIONAL AND LEAK CHECK GOOD.

Part: DUCT — CRACKED (NR 3 ENGINE)

IMMEDIATELY AFTER TAKEOFF, FIRE WARNING AND STRUT OVERHEAT NR 3 AND A NR 3 FIRE DETECTOR LIGHT ILLUMINATED. RED TABS PROCEDURES FOLLOWED. STRUT OVERHEAT LIGHT WENT OUT AFTER ONE MINUTE AT IDLE POWER. ENGINE NR 3 EPR DROPPED .2 EPR BELOW OTHER ENGINES. *S/D* INSTALLED 8TH STAGE AIR DUCT OPERATIONAL. CHECKED GOOD ON THE GROUND NORMAL.

Part: SPAR CAP — GOUGED (HORIZ STAB)

NR 0568 73C031-03 HORZ STAB REAR SPAR UPPER CAP, RT AND LT SIDES. ABOVE HINGE BEARINGS, HAVE GROOVES WORN FROM FAIRING CONTACT/CHAFFING. BLENDED AND HFEC REWORKED AREAS PER EA 7-5510-29145, DATED JULY 21, 1997.

Part: FLOORBEAM — GOUGE (BS 1110)

GOUGE IN TOP OF FLOORBEAM BS 1110, LBL 5. BLENDED GOUGE AREA, WHICH MADE FLOORBEAM OUT OF LIMITS. OUT OF LIMIT AREA WAS REMOVED PER SRM 53-10-8, DOUBLER REPAIR WAS INSTALLED ON FLOORBEAM PER SRM 53-10-8 PG 18 -23, AND SRM 53-10-2 PG 44E.

Part: FLOORBEAM — CORRODED (BS 1183)

BETWEEN FLOORBEAMS AT STA 1183 TO STA 1166 AT LBL 33 UNDERSIDE OF FLOORPAN (ACCESSED THRU AFT CARGO) HAS EXFOLIATION CORROSION MARKED. REMOVED CORROSION, CUT OUT PIECE OF FLOOR (SEE NR 0922) FABRICATED REPAIR DOUBLER AND INSTALL REPAIR AS PER SRM AND EA 7-5310-29144 DATED 7/18/97.

Part: ANGLE — CRACKED (BS 1183)

ANGLE CRACKED AT BS 1183, LBL 48 TO LBL 52 AT FLOOR. INSTALLED REPAIR ON CRACKED ANGLE PER SRM 51-40-3.

Part: FLOORBEAM — CORRODED (BS 1050)

NR 0396 72C237-02 UPPER LOBE BS 1050, LBL 35. CORROSION ON FLOORBEAM TOP AND BOTTOM SIDE AROUND SCREW HOLE. CLEANED CORROSION AND INSTALLED DOUBLER PER AARD 53-10-07-02.

Part: FLOORBEAM — CORRODED (BS 1110)

NR 0364 72C237-02 CORROSION ON FLOORBEAM BS 1110, RBL 12 - 24. REMOVED CORROSION PER SRM 51-10-6. INSTALLED DOUBLER PER AARD 53-10-07-2.

Part: CIRCUIT BREAKER — TRIPPED (MAIN)

DURING CLIMBOUT PASSING FLT LVL 260 MCD WARNING LIGHT CAME ON AND CABIN PRESSURIZATION STARTED CLIMBING AT APPROX 500 TO 800 FRM LEVELED OFF, THEN STARTED DESCENDING WHILE ACCOMP RED-TAB PROCEDURES. ACCOMP MANUAL DEPRESSURIZATION WITH MANUAL DC OUTFLOW VALVE. LANDED AT PIA UNEVENTFUAL. AFTER S/D FOUND CARGO DOOR WARNING C/B POPPED. NOTE: HEAVY RAIN ENCOUNTERED ON GRD PRIOR TO THIS FLT. RESET CARGO DOOR WARNING C/B, CYCLED CARGO DOOR SEVERAL TIMES AND CK'D GOOD. PRESSURIZED A/C TO 2.2 PSI, PRESSURE HELD GOOD. LEAK CK'D, MCD CK'D GOOD. VISUALLY CK'D MCD LOCK, OK FOR SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)

INTERMITTENT MAIN CARGO SMOKE INDICATION. INDICATOR LIGHT NR 5 WAS ON FOR 2 SECONDS AND THEN WENT OUT. TESTED SYS ANDCHECKED GOOD. CHECKED M/CARGO SMOKE DETECTORS 5 TIMES. NOINDICATIONS OF A PROBLEM, OK FOR SERVICE.