N221FE

Part: SWITCH — MALFUNCTIONED (E/E BAY DOOR) · airframe 58,395 hrs · 37,358 cycles

EQUIPMENT BAY ACCESS DOOR LIGHT ILLUMINATED DURING PUSH BACK. R & R ELECTRIC ACCESS LIMIT SWITCH (S114) IAW SWPM 20-30-00. PERFORMED DOOR WARNING TEST IAW AMM 52-70-001-5-1. ALL CHECKED GOOD, ACFT OK FOR SERVICE.

Part: TRIM SYSTEM — MALFUNCTIONED · airframe 57,847 hrs · 37,113 cycles

MAIN STAB TRIM (ON FINAL) DID NOT WORK, TRIED CAPT AND F/O TRIM BUTTONS ON YOKE LIGHT ON CENTER CONSOLE DID COME ON. DID NOT WORK TAXIING IN. AFTER SHUTDOWN OF ENGINES WORKED NORMALLY BOTH SIDES. ACCOMPLISHED THE STABILIZER TRIM SYS TEST IAW AMM 27-40-000-5. ALL THE SYS DID WORK PROPERLY DURING THE SYS TEST. FINAL CLOSED.

Part: ACTUATOR — FAILED (NR 1 SLAT) · airframe 57,764 hrs · 37,078 cycles

NR 1 SLAT FAILED TO RETRACT AFTER TAKEOFF. QRH COMPLIED WITH NO HELP. REPLACED L/E SLAT NR 1 ACTUATOR IAW TO AMM 27-81-000-2. TEST SEVERAL TIMES NO DISCREPANCIES FOUND.

Part: CONNECTOR — DIRTY (SLAT ACTUATOR) · airframe 57,708 hrs · 37,054 cycles

ON CLIMB OUT, FLAPS 15 ALL IS WELL. WHEN FLAP HANDLE RAISED FROM FLAPS 15 GOT AN ASSYMETRYCAL WARNING LIGHT. RUN QRH RETURNED TO DEPARTURE. FAULT CONTINUES ON GROUND OPERATION . VERIFIED SLAT ACTUATOR NR 1 DIDN`T RETRACT AT HANDLE AT 2 DEG POS. INSPECTED SLAT ACTUATOR SWITCH CONNECTOR DIRTY. CLEANED UP IAW AMM 27-82-011-4 AND CHECKED OPERATION NORMALLY SEVERAL TIMES ON GROUND.

Part: SKIN — GOUGED (BS 620) · airframe 57,583 hrs · 36,965 cycles

MCD INNER SURROUND SKIN GOUGED STA 620 STR 15 - 16L ACCOMPLISHED REPAIR AT MCD INNER SURROUND SKIN IAW EA 7-5310-123597.

Part: SKIN — DAMAGED (BS 540 S3L) · airframe 57,583 hrs · 36,965 cycles

INNER SKIN STA 540 STR 3L DOUBLE DRILLED HOLES. ACCOMPLISHED REPAIR AT BS 540 STR 3L INNER SKIN IAW EA 7-5310-123595.

Part: SUPPORT FITTING — DAMAGED (ZONE 200) · airframe 57,583 hrs · 36,965 cycles

MAIN CARGO DOOR BS 620 AFT O/B SUPPORT FITTING HAS ELONGATED FASTENER HOLES REMOVED DAMAGED BS 620 TENSION ANGLE (SUPPORT FITTING), FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-30-2, 51-10-2, AND DRAWING 53FX1286.

Part: FRAME — DAMAGED (ZONE 200) · airframe 57,583 hrs · 36,965 cycles

MAIN CARGO DOOR CUT-OUT BS 620 FRAME WEB HAS DOUBLE DRILLED FASTENERS REMOVED AND REPLACED BS 620 FRAME WEB IAW EA 7-5310-123595.

Part: FRAME — DAMAGED (BS 620) · airframe 57,583 hrs · 36,965 cycles

AFTER FRAME REMOVAL AND CLEAN UP FOUND DOUBLE DRILL HOLES STA 620 BETWEEN STR 10L TO STR 13L. CUTOUT DAMAGED AREAS (3) AT BS 620 STR 10L, STR 11L, AND STR 13L AND FABRICATED FILLERS (3). INSTALLED FILLERS (3) AND FABRICATED REPAIR DOUBLER AND REPAIR TRIPLER. INSTALLED REPAIR DOUBLER AND REPAIR TRIPLER AT BS 620 IAW B727 SRM 51-30- 2, FEDEX EA 7-5310-123595, SRM 51-10-2 AND EA 7-5310-123595.

Part: FRAME — DAMAGED (BS 620 S9L) · airframe 57,583 hrs · 36,965 cycles

DOUBLE DRILLED HOLES FOUND UPON REMOVAL OF INNER SKIN GOING THROUGH SHIM AND FRAME STA 620, STR 9L AT 2 EACH LOCATIONS.

Part: WEB — DAMAGED (BS 1183) · airframe 57,583 hrs · 36,965 cycles

BS 1183 HORIZONTAL CHORD & WEB WL 190 HAS FASTENERS WITH NO SPACING & DAMAGED FASTENER HOLES. ACCOMPLISHED REPAIR AT BS 1183 HORIZONTAL CHORD & WEB IAW EA 7-5310-123591.

Part: SKIN — DAMAGED (BS 590 S3L) · airframe 57,583 hrs · 36,965 cycles

SKIN STA. 590 STR 3L HAS DOUBLE DRILLED HOLES. ACCOMPLISHED REPAIR AT BS 590 STR 3L IAW EA 7-5310-123595.

Part: FRAME — DAMAGED (ZONE 200) · airframe 57,583 hrs · 36,965 cycles

BS 620 FRAME DOUBLER HAS FASTENER HOLES WITH NO ED. REMOVED AND REPLACED BS620 FRAME DOUBLER IAW EA 7-5310-123595.

Part: FRAME — DAMAGED (BS 620 S3-4L) · airframe 57,583 hrs · 36,965 cycles

AFTER REMOVAL OF FRAME AND CLEANUP FOUND DOUBLE DRILL HOLES STA. 620 BETWEEN STR 3L - 4L. REPAIRED BS 620 STRINGER 3-4L SKIN AND FRAME IAW EA 7-5310-123595.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 57,583 hrs · 36,965 cycles

UPON REMOVAL OF AFT LOWER RADIUS SEAL DEPRESSOR, FOUND C-2 DOOR SFT FRAME CORRODED AT LOWER STUB. CUTOUT DAMAGE ON C-2 DOOR LOWER AFT FRAME IAW FED EX B727 SRM REV 103, 51-10-1. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW FED EX EA# 7-5230-136757 AND B727 SRM 51-20-1 FIG 7 AND 51-30-2.

Part: RIB — CHAFED (NR 5 SLAT) · airframe 57,583 hrs · 36,965 cycles

NR 5 SLAT OTBD END WEB IS CHAFED. REMOVED RIB WEB, FORMED RIB WEB FROM 20240 .032 DIM 17.3" X 6.8", HEAT TREATED TO T4 CONDITION IAW FAS ENG REP. 2-37153-801 REV A & DWG. 65-17286, INSTALLED RIB WEB IAW SRM 51-30-2, 51-30-5, 51-10-2 AT NR 5 SLAT OUTBOARD END WEB.

Part: FLOORBEAM — DAMAGED (BS 783) · airframe 57,583 hrs · 36,965 cycles

DOUBLE DRILLED FLOORBEAM WEB MAIN CABIN STA 783, RBL 55. REMOVED SEAT TRACK, REMOVED DAMAGED WEB AT BS 783 RBL 55, CUTOUT DAMAGE AREA OF WEB, FABRICATED WEB REPAIR, INSTALLED WEB REPAIR AT BS 783 RBL 55, REINSTALLED SEAT TRACK SECTION AT RBL 65 BETWEEN BS 760 - BS 840 IAW B727 SRM 51-30-2, 51-10-1, 51- 40-2, 51-10-2 AND EA# 7-5310-136756.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 57,583 hrs · 36,965 cycles

C-2 DOOR INNER SKIN IS CRACKED AT RIVNUT, UPPER SECTION BTWN BS 950F - 970. CUT OUT DAMAGE ON C-2 DOOR INNER SKIN UPPER SECTION IAW SRM, REV 103, 52-30-2, FIG 3. FABRICATED DOUBLER AND SHIMS IAW SRM 52-30-2, FIG 3. INSTALLED FITTING, DOUBLER AND SHIMS IAW SRM 52-30-2 AND 52-00-3, FIG 3.

Part: FLOORBEAM — DAMAGED (BS 783) · airframe 57,583 hrs · 36,965 cycles

DOUBLE DRILLED FLOORBEAM WEB MAIN CABIN STA 783, RBL 55. REMOVED SEAT TRACK REMOVED DAMAGED WEB AT BS 783 RBL 55, CUTOUT DAMAGE AREA OF WEB, FABRICATED WEB, INSTALLED WEB REPAIR AT BS 783 RBL 55, AND REINSTALLED SEAT TRACK SECTION IAW SRM 51-30-2, 51-10-1, 51-40-2, 51-10-2, EA 7-5310-136756.

Part: SKIN — DAMAGED (BS 500 S3L) · airframe 57,583 hrs · 36,965 cycles

UPON REMOVAL OF MCD, FOUND FASTENER HOLE WITH ZERO EDGE MARGIN - FUSELAGE SKIN, STA 590 BENEATH STR 3L. REPAIRED FUSELAGE SKIN AT BS 500 STR 3L IAW EA 7-5310-123595.

Part: SKIN — DAMAGED (BS 520 S3L) · airframe 57,583 hrs · 36,965 cycles

BS 520 STR, 3L FOUND MISDRILLED HOLES IN THE OEM SKIN. ACCOMPLISHED REPAIR AT BS 520 STR 3L INNER SKIN IAW EA 7-5310-123595.

Part: SKIN — DAMAGED (BS 545 S3L) · airframe 57,583 hrs · 36,965 cycles

UPON REMOVAL OF MCD, FOUND FASTNER HOLE WITH ZERO EDGE MARGIN. FUSELAGE SKIN STA 545 BENEATH STR 3L. CUTOUT DAMAGED AREA, FABRICATED FILLER AND INSTALLED REPAIR PARTS IAW EA 7-5310-123595.

Part: SKIN — DAMAGED (BS 560 S3L) · airframe 57,583 hrs · 36,965 cycles

BS 560 STR 3L FOUND MISDRILLED HOLES IN THE EOM SKIN. ACCOMPLISHED REPAIR AT BS 560 STR 3L INNER SKIN IAW EA 7-5310-1235.

Part: SKIN — DAMAGED (BS 490) · airframe 57,583 hrs · 36,965 cycles

UPON REMOVAL OF MCD HEADER BEAM NOTED FASTENER HOLES WITH SHORT OFF CTR SPACING AT FS 490 BETWEEN STRINGERS 3 & 4 LT. ACCOMPLISHED REPAIR AT BS 490 STR 3L INNER SKIN IAW EA 7-5310-123595.

Part: SKIN — DAMAGED (BS 600-610) · airframe 57,583 hrs · 36,965 cycles

BS 610 - 600 STR 3L FOUND MISDRILLED HOLES IN THE OEM SKIN. ACCOMPLISHED REPAIR AT BS 610 - 600 STR 3L IAW EA 7-5130-123595.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 57,583 hrs · 36,965 cycles

ATTACH ANGLE CRACKED, APPROX 3" LONG CRACK, AT NLG RT TRUNNION FITTING. (NDT VERIFIED). REMOVED RT NLG TRUNNION FITTING SUPPORT IAW SRM REV 103, 51-30-2. DRILLED, DEBURRED SUPPORT ANGLE IAW SRM 51-30-5 AND 51-30-2. INSTALLED SUPPORT IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 1140-1150) · corrosion level 2 · airframe 57,583 hrs · 36,965 cycles

AFT MAIN CABIN CARGO DECK AT BS 1140 - BS 1150 RBL 25 INBD SEAT TRACK ATTACHMENT FLANGE HAS 2 EA LOCALIZED AREAS OF CORROSION. REMOVED DAMAGED SEAT TRACK SECTION AT RBL 25 FROM BS 1130 - BS 1175. FABRICATED NEW SEAT TRACK SECTION. INSTALLED NEW SEAT TRACK SECTION AT RBL 25 FROM BS 1130 - BS 1175 IAW B727 SRM 51-10-6, SRM 53-10-1 FIG 3, SRM 51-30-2, DRWING 53FX976, SRM 51-10-2, AND SRM 51-30-2.

Part: RIB — CRACKED (NR 3 SLAT) · airframe 57,583 hrs · 36,965 cycles

NR 3 SLAT OTBD END RIB IS CRACKED. REMOVED RIB ANGLE AT NR 3 SLAT OUTBD END, IAW SRM 51-30-2 FABRICATED NEW RIB ANGLE IAW SRM 51-20-4 FIG 2 AND DWG 65-17304, TREATED AND PRIMED NEW RIB ANGLE IAW SRM 51-10-2, INSTALLED NEW RIB ANGLE SECTION IAW SRM 51-30-2 HEAT TREATED TO T6 CONDITION IAW FAS ENG REPORT NR 2-37153-801 REV A.

Part: WINDOW FRAME — CORRODED (BS 950) · corrosion level 2 · airframe 57,583 hrs · 36,965 cycles

CORROSION WINDOW FRAME RT SIDE STA. 950 REMOVED CORROSION IAW SRM 51-10-6. MEASURED BLEND TO BE OUT OF LIMITS IAW SRM 56-20-1 FIG 1. FABRICATED DOUBLER REPAIR AND INSTALLED DOUBLE REPAIR IAW SRM 56-20-3 FIG 1.

Part: SILL — DAMAGED (BS 620) · airframe 57,583 hrs · 36,965 cycles

MCD CUTOUT INBD AFT UPPER SILL HAS DOUBLE DRILLED HOLE AT STA 620, STR 3L. ACCOMPLISHED REPAIR AT MAIN CARGO DOOR UPPER SILL IAW EA 7-5310-123588 AND EA 7-5310-123595.

Part: SILL — DAMAGED (BS 530-570) · airframe 57,583 hrs · 36,965 cycles

INBD CTR SILL HAS DOUBLE DRILLED HOLES STA 530-570, STRINGER 3L ACCOMPLISHED REPAIR AT MAIN CARGO DOOR SILL IAW EA 7-5310-123588 AND EA 7-5310-123595.

Part: STRINGER — CRACKED (BS 340 S5R) · airframe 57,583 hrs · 36,965 cycles

CRACK ON STR 5R, STA 340 AT 9G BULKHEAD FWD SIDE. CUTOUT DAMAGED STRINGER, FABRICATED REPAIR PARTS (FILLER AND SPLICE). INSTALLED NEW REPAIR PARTS AT STRINGER 5R, BS 340 IAW SRM 53-10-3, FIG 1.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 57,583 hrs · 36,965 cycles

REMOVED DOUBLER AND FILLER REPAIR AT MCD OUTER SKIN STA 560 STR 7L IAW EA 7-5230-136753. FABRICATED NEW DOUBLER AND FILLER REPAIR IAW E.A. 7-5230-136753. INSTALLED NEW DOUBLER AND FILLER REPAIR IAW E.A. 7-5230-136753.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 57,583 hrs · 36,965 cycles

LT ELEVATOR TOP SIDE AT TRIM TAB CTR BOB WEIGHT HAS 3 LIGHTING STRIKES. REMOVED DAMAGE ON LT ELEVATOR UPPER AFT SKIN IAW SRM REV 103, 51-10-1. FABRICATED FILLER AND DOUBLER IAW SRM 55-20-3, FIG 5, INSTALLED DOUBLER AND FILLER IAW SRM 51-40-20 AND 55-20-3, FIG 5.

Part: WEB — CRACKED (ZONE 100) · airframe 57,583 hrs · 36,965 cycles

AFT AIRSTAIR LT LOWER TORQUE BOX INBD WEB IS CRACKED AT LIGHTNING HOLE BETWEEN BS 1223 - 1233. CUT OUT DAMAGE 5/8" X 1" IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 & 51-40-2 FIG 1.

Part: WEB — CRACKED (ZONE 100) · airframe 57,583 hrs · 36,965 cycles

AFT AIRSTAIR RT LOWER TORQUE BOX INBD WEB IS CRACKED AT LIGHTNING HOLE BETWEEN BS 1293- 1303. CUT OUT DAMAGE 1/2" X 1" ON AFT AIRSTAIR RT LOWER TORQUE BOX WEB IAW SRM REV 103 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1. INSTALLED DOUBLER IAW SRM 51-40-2 FIG 1

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,583 hrs · 36,965 cycles

FWD PIT STR 26L IS CORRODED WITH EXFOLIATION FROM BS 720D- 720E. CUTOUT DAMAGED SECTION OF STRINGER IAW SRM 53-10-3 FIG 1 REV 103. FABRIATED HAT SECTION (2 EACH) AND SPLICE CHANNEL (3 EACH) IAW SRM 53-10-3 FIG 1 REV 103. INSTALLED STRINGER REPAIR PARTS IAW SRM 53-10-3 FIG 1 REV 103.

Part: SILL — DAMAGED (BS 502) · airframe 57,583 hrs · 36,965 cycles

MCD UPPER SILL BS 502 BETWEEN STR 3L AND 4L UPPER FLANGE HAS DOUBLE DRILLED FASTENER HOLE. ACCOMPLISHED UPPER SILL REPAIR IAW EA 7-5310-123588 AND EA 7-5310-123595.

Part: BULKHEAD — MISINSTALLED (BS 1183) · airframe 57,583 hrs · 36,965 cycles

LOCK FASTENER FOUND WITH NO EDGE DISTANCE STA 1183 FWD SIDE OF BULKHEAD WL 163, LBL 24 VERTICAL BEAM. ACCOMPLISHED REPAIR AT BS 1183 VERTICAL BEAM IAW EA 7-5310-123591.

Part: SWITCH — INOPERATIVE (LE FLAPS) · airframe 56,158 hrs · 36,321 cycles

ON CLIMBOUT RT INBD LED WOULD NOT RETRACT. RUN QRH, RTB, NO RESTRICTION NR 4 L/E FLAP HAS JUMPER CABLE INSTALLED IAW MM 27-82-000-1. REMOVED AND REPLACED AND CHECKED NR 4 L/E SWITCH IAW AMM 27-82-011-4, ALL SYS CHECKED GOOD AT THIS TIME. PREMATURE REMOVAL/INSTALLATION.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 55,637 hrs · 35,946 cycles

REPAIR AT STA 440 STR 10L NOT IAW SRM. REMOVED PREVIOUS REPAIR AND CUTOUT DAMAGED AREA DIMS 12" BY 9" IAW WITH EA 7-5330-126855 HFEC INSPECTED EDGE OF CUTOUT AND .040 INSURANCE CUT AND EXISTING HOLES FREE OF CRACK INDICATIONS IAW NDTM 51-00-00. FABRICATED DOUBLER REPAIR, TRIPLER, FILLER, & 3 EACH SHIMS. INSTALLED REPAIR PARTS IAW EA 7-5330-126885.

Part: SKIN — DAMAGED (ZONE 200) · airframe 55,637 hrs · 35,946 cycles

CABIN STA 440 STR 10L HAS MIS-DRILLED FASTENER HOLES. CUT OUT DAMAGED AREA DIMS 2 INCH BY 7/8 INCH. FABRICATED DOUBLER USING 2024-T3 .090 PO NR 9007561 DIMS 12 5/8 BY 9 1/2 INCH, FILLER USING 2024-T3 .190 PO NR 314676 DIMS 2 INCH BY 7/8 INCH, IAW B727 SRM 53-30-3 AND INSTALLED REPAIR PARTS IAW B727 SRM 53-30-3 FIG 6.

Part: STRUCTURE — CRACKED (RT WING TE FLAP) · airframe 55,637 hrs · 35,946 cycles

CRACK ON AFT STRUCTURE OF RT INBD FLAP WBL 114.2 FABRICATED AFT STRUCTURE REPAIR FILLER, ANGLE SPLICE, INSTALLED REPAIR SPLICE AND FILLER ON RT INBD FLAP IAW SRM 57-50-2, SRM 51-40-4, AND SRM 51-30-2.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,637 hrs · 35,946 cycles

CORROSION ON S29R AT BS 970-990. BLENDED OUT S29R FLANGE AS NECESSARY TO REMOVE CORROSION, REMAINING THICKNESS DIMENSIONS MAINTAIN A 20-1 BLENDOUT RATIO WITH A MIN 1.0: RADIUS PER MESSAGE 1-1013418906-2,3,4,5,6, AND ARE WITHIN LIMITS. ACCOMPLISHED HFEC AND SURFACE INSP PER NDTM 51-00-00, NO DEFECTS NOTED, FLAP PEENED AREA PER SOPM 20-10-03, FINISHED AREA AND APPLIED CORROSION INHIBITOR. ALL STEPS ACCOMPLISHED PER EA 7-5330-126853.

Part: LEVER — GOUGED (ZONE 700) · airframe 55,637 hrs · 35,946 cycles

LEFT AND RIGHT WHEEL WELL MLG DOOR RELEASE HANDLES ARE GOUGED. REWORKED GOUGED AREAS ON LH AND RH WHEEL WELL MLG DOOR REALEASE HANDLES IAW B727 SRM 51-10-1, PERFORMED DYE PENETRANT INSPECTION IAW SOPM 20-20-02 NO DEFECTS NOTED TREATED AND PRIMED AREAS. ALL STEPS ACCOMPLISHED IAW FEDEX EA 7- 3210-123502 "LANDING GEAR - L/H AND R/H MLG DOOR MANUAL RELEASE LEVER GOUGED - REPAIR"

Part: SPAR — CRACKED (WS 870) · airframe 55,637 hrs · 35,946 cycles

CRACK ON WING CENTER SECTION REAR SPAR WEB STA 870 LBL 13 TO 16.

Part: FRAME — CHAFED (ZONE 200) · airframe 55,637 hrs · 35,946 cycles

9G BULKHEAD CONTACTING FRAME AT STA 344 AND STR 5L. TRIMMED OUT FRAME AND FABRICATED FRAME REPAIR, INSTALLED FRAME REPAIR IAW B727 SRM 51-30-2, 53-10-2 FIG 3 AND SRM 53-10-4 FIG2.

Part: WEB — DAMAGED (ZONE 100) · airframe 55,637 hrs · 35,946 cycles

AFT AIRSTAIR AREA LT LOWER TORQUE BOX HAS IMPROPER REPAIR AT LIGHTNING HOLE BS 1240. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2, CUT OUT DAMAGED AREA ON WEB IAW SRM 51-40-2, FABRICATED DOUBLER REPAIR IAW SRM 51-30-5, 53-10-2 AND 51-40-2, INSTALLED REPAIR IAW SRM 51-40-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,637 hrs · 35,946 cycles

CORROSION ON SEAT TRACK STA 1060 TO 1090 RBL 45. FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED SEAT TRACK FROM BS 1040 TO 1130 RBL 45 IAW SRM 51-30-2, FABRICATED SECTION OF SEAT TRACK IAW SRM 53-10-5, INSTALLED NEW SEAT TRACK IAW SRM 53-10-5.

Part: SEAT TRACK — WORN (BS 1130) · airframe 55,637 hrs · 35,946 cycles

WORN SEAT TRACK RBL 45 STA 1130. REMOVED SEAT TRACK, 2 EACH DOUBLERS AND BEAM EXTENSION, FOUND DAMAGED AREA ON WEB, CUT OUT DAMAGED AREA ON WEB IAW SRM 51-30-2 AND 51-40-2 FABRICATED WEB FILLER, 2 STRAPS, BEAM EXTENSION, BEAM STRAP AND EXTENSION SUPPORT FILLER, FABRICATED NEW SEAT TRACK USING EXTRUDED ALUMINUM BAR AND 2 SIDE DOUBLERS IAW DRAWING 53FX939, INSTALLLED ALL PARTS IAW DRAWING 53FX939.

Part: STRUCTURE — CRACKED (LT WING TE FLAP) · airframe 55,637 hrs · 35,946 cycles

LEFT WING INBD MIDFLAP CRACKED 2 PLACES AT CUTOUTS. REMOVED DAMAGED AREA AND FABRICATED NEW ANGLES AND SPLICE REPAIR IAW SRM 57-50-2 AND 51-40-4. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 55,637 hrs · 35,946 cycles

CORROSION ON SEAT TRACK ON INBD VERTICAL SIDE FWD OF BS 1070 RBL 25. FOUND CORROSION OUT OF LIMITS, CUT OUT DAMAGED SEAT TRACK FROM BS 950 TO 1134 RBL 25, FABRICATED 2 SEAT TRACK SECTIONS, 4 ANGLE SPLICES, 2 STRAPS AND IAW SRM 53-10-5. INSTALLED REPAIR PARTS IAW SRM 53-10-5.

Part: SKIN — GOUGED (ZONE 100) · airframe 55,637 hrs · 35,946 cycles

SKIN GOUGED STA 700 STR 28R. CUT OUT DAMAGED SKIN AND FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER IAW SRM 53-30-3, 53-30-2 AND SRM 51-30-2.

Part: SKIN — GOUGED (ZONE 100) · airframe 55,637 hrs · 35,946 cycles

SKIN SCRATCHED BELOW COOLING BLOWER STATIC PORT RT FWD FUSELAGE BS 435 ABOVE S21R. BLENDED AREA AND FOUND MATERIAL LOSS OUT OF LIMITS, CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND REPAIR FILLERS IAW SRM 53-30-3, INSTALLED REPAIR PARTS IAW SRM 53-30-3.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 55,637 hrs · 35,946 cycles

CORROSION ON SEAT TRACK LBL 25 BS 560-720. FOUND CORROSION ON SEAT TRACK OUT OF LIMITS. REMOVED SEAT TRACK AND FABRICATED 2 SECTIONS, SPLICE ANGLELS AND 2 STRAPS IAW SRM 53-10-5. INSTALLED REPAIR PARTS IAW SRM 53-10-5.

Part: SKIN — MISALIGNED (ZONE 100) · airframe 55,637 hrs · 35,946 cycles

CARGO DOOR SKIN AT BS 650 S25L HAS 2 FASTENERS WITH NOT ENOUGH SPACING. CUT OUT DAMAGED STRINGER AT BS 650 AND S25L , FABRICATED STRINGER REPAIR SPLICE FABRICATED FILLER, CUT OUT DAMAGED EXT SKIN DIMS .755" FABRICATED FREEZE PLUG, FABRICATED EXT SKIN DOUBLER, FABRICATED REPAIR TRIPLER. INSTALLED REPAIR PARTS IAW SRM 53-10-3, 51-10-7 AND SRM 53-30-3.

Part: SKIN — GOUGED (ZONE 100) · airframe 55,637 hrs · 35,946 cycles

SKIN GOUGED BS 990 S24L. BLENDED OUT AREA AND FOUND MATERIAL LOSS OUT OF LIMITS. CUT OUT DAMAGED AREA IAW SRM 53-30-3, FABRICATED DOUBLER AND FILLER IAW SRM 53-30-3 AND 53-30-3. INSTALLED REPAIR PARTS IAW SRM 53-30-3 AND 51-30-2.

Part: CHECK VALVE — LEAKING (HYD SYSTEM) · airframe 55,285 hrs · 35,700 cycles

INSTANTANOUS LOSS OF HYD SYS A PRESSURE AND QUANTITY. ALL QRH PROCEDURES COMPLETED. NO RESTORATION. FOUND SYS "A" HYDRAULIC MODULAR PACKAGE WITH BLOWNOUT CHECK VALVE. REMOVAL/INSTALLATION OFF MFG 65-17821-14.

Part: RIB — CRACKED (NR 1 KRUEGER) · airframe 54,767 hrs · 35,289 cycles

LT WINGS, RIB UPPER CORD AT BL 70-5 FASTENER INSP. DURING "B" CHECK, CRACKED INDICATION WITNESSED BETWEEN BOTH HOLES AND BEYOND. HOLES SHOWN ON FIGURE 1 OF EO 7-5710-7-2308 PT1L . REPAIRED IAW EO 7-5710-7-2308 PT1 AND PT2 AND EA 7-5710-102035 REF WRI 57-10/0313.

Part: RIB — CRACKED (RT WING) · airframe 54,767 hrs · 35,289 cycles

RT WINGS, RIB AT BL 70-5 FASTENER INSP DURING "B" CHECK CRACK INDICATION WITNESSED BETWEEN BOTH HOLES AND BEYOND. HOLES SHOWN ON FIGURE 1 OF EO 7-5710-7-2308 PT1R. REPAIRED IAW EO 7-5710-7-2308 PT1 AND PT2 AND EA 7-5710-102035 REF WRI 57-10/0313.

Part: RIB — CRACKED (LT WING) · airframe 54,767 hrs · 35,289 cycles

COMPLY WITH EA 7-5710-102035 WINGS (AD 90-06-09 AND (94-07-08) MAIN FRAME -RIB REPAIR EO 7-5710-7-2308. COMPLIED WITH EA 7-5710-102035 WINGS (AD 90-06-09 AND AD 94-07-08)MAIN FRAME-RIB UPPER CHORD REPAIR EO 7-5710-7-2308 PART 2.

Part: RIB — DAMAGED (RT WING) · airframe 54,767 hrs · 35,289 cycles

COMPLY WITH E.A. 7-5710-110741-WING (AD 90-06-09:94- 87-08;98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS. COMPLIED WITH EA 7-5710-110741 WING (AD90-06-09-94-0 7-08, 98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS. COMPLIED WITH EA 5710-110741 WING AD 90-06-09, 94-07-08,98-11-03 RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS.

Part: REPAIR — MISINSTALLED (ZONE 100) · airframe 54,053 hrs · 34,714 cycles

IMPROPER REPAIR INSTALLED STA 430 - 436 STR 21R - 22R. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED FUSELAGE FLUSH REPAIR IAW FX SRM 53-30-3 FIG 2, 51-30-2 AND 51-10-2.

Part: CONNECTOR — DAMAGED (FIRE DETECTOR) · airframe 54,033 hrs · 34,694 cycles

FIRE INDICATION ON NR 1 ENGINE, SHUTDOWN IN FLIGHT. BOTH BOTTLES DISCHARGED. LIGHT EXTINGUISHED WHEN PWR REDUCED, CAME BACK ON WHEN PWR APPLIED. REPLACED AFT A-LOOP DETECTOR CONNECTOR IAW 727-200 WDM 26-11-01 AND OP CHECKED IAW 727-200 MM 26-11-002-5, WITH NO DEFECTS NOTED. A/C OK FOR SERVICE.

Part: TRANSMITTER — FAILED (NR 3 EPR) · airframe 53,831 hrs · 34,563 cycles

NUMBER 3 ENG EPR GAUGE FAILED TO REACH TAKEOFF EPR. UPON BLOCK IN NUMBER 3 EPR WAS SPINNING. RELEASED FOR SERVICE PER MEL/CDL: 77-01-01 CAT 'C' EXP: 31DEC05. NR 3 ENGINE EPR INDICATOR, INOP. REMOVED AND REPLACED NR 3 EPR TRANSMITTER PER 727-200 M/M 77-11-011-4. SYSTEM CHECKS NORMAL PER M/M 31-26-000-5.

Part: SWITCH — INOPERATIVE (ZONE 600) · airframe 53,278 hrs · 34,223 cycles

NR 7 SLAT FAILED TO RETRACT FROM FLAPS 2 DEGREE TO FLAPS UP. AIRCRAFT ROLLED LEFT DURING RETRACTION. PERFORMED QRH PROCEDURES. LED REMAINED OUT. OPERATED SLATS NUMEROUS TIMES - EXTEND AND RETRACT FUNCTION CK'S GOOD. FOUND NR 7 SLAT EXTEND SWITCH INOP. REPLACED PER MM 27-82-011-4. OPS CK GOOD.

Part: STRIKER — WORN (ZONE 800) · airframe 53,278 hrs · 34,223 cycles

AIR RETURN FOR AFT AIRSTAIR LIGHT ILLUMINATED WHEN AIRBORNE AFTER SECOND PACK WAS TURNED ON. INSPECTED AFT AIRSTAIR "UP LOCK" SWITCH AND STRIKER PLATE.FOUND STRIKER PLATE HAS A HOLE WORN THROUGH IT.APPLIED AERODYNAMIC TAPE TO AREA.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 51,465 hrs · 33,111 cycles

CAPT`S A/S INDICATOR FAILED AT 80 KNOTS. REJECTED THE T/O. ACCOMPLISHED RTO CHECK LIST ON TAXI BACK, CYCLED THE APP CIRCUIT BREAKER AND IT WORKED NORMALLY. REMOVED AND REPLACED CAPTAIN A/S INDICATOR AS PER 727-200 AMM 34-12-021-4. PERFORMED GROUND TEST AS PER 727-200 AMM 34-12-001-0. TEST ON GROUND OK. A/C OK FOR SERVICE.

Part: FRAME — GOUGED (MAIN CARGO DOOR) · airframe 51,261 hrs · 32,988 cycles

MAIN CARGO DOOR FWD SIDE FRAME GOUGED 52 INCHES FROM LOWER CORNER. GOUGE IN MAIN CARGO DOOR FWD FRAME 52 INCHES ABOVE LOWER CORNER FOUND TO BE OUT OF LIMITS IAW SRM 52-00-1. REPAIRED IAW FED EX EA 7-5230-70516.

Part: FRAME — GOUGED (MAIN CARGO DOOR) · airframe 51,261 hrs · 32,988 cycles

MAIN CARGO DOOR FWD SIDE FRAME GOUGED 12" FROM LWR CORNER .

Part: FRAME — GOUGED (MAIN CARGO DOOR) · airframe 51,261 hrs · 32,988 cycles

MAIN CARGO DOOR AFT SIDE FRAME GOUGED 12 INCHES FROM LOWER CORNER. REPAIRED GOUGED MAIN CARGO DOOR FRAME AFT SIDE 12 INCHES FROM LOWER CORNER IAW FED EX EA 7-5230-70516

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,261 hrs · 32,988 cycles

CORROSION / GOUGE ON FLOORBEAM BS 277, LBL 14 - LBL 10, WL 208. REPAIRED FLOORBEAM BS 277, LBL 10-14 PER EA 7-5310-54991.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,261 hrs · 32,988 cycles

CORROSION BS 1130, WL 201, LBL 38 - BL 0, IN AND AROUND NUTPLATE HOLES. REPAIRED BS 1130 FLOORBEAM LOWER CHORD, W.L 201, LBL 65 TO RBL 65. CORROSION ON FLOOR BEAM WAS FOUND TO BE OUT OF LIMITS. LOWER CHORD OF 1130 FLOOR BEAM WAS REMOVED AND REPLACED PER FED EX EA 7-5310-54974.

Part: FRAME — DENTED (FUSELAGE) · airframe 51,261 hrs · 32,988 cycles

FWD CARGO BAY FRAME DENTED BS 500, STR 24R. DENT OUT OF LIMITS. REPAIRED FRAME BS 500, STR 24R PER SRM 51-40-3 FIG 1 AND EA 7-5310-70515.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,261 hrs · 32,988 cycles

AFT FRAME DOOR CUTOUT, AFT FRAME CRACKED, LOWER CORNER, BS 990, RBL 26.

Part: DOOR FRAME — DENTED (FUSELAGE) · airframe 51,261 hrs · 32,988 cycles

LOWER FWD CARGO BAY FRAME IS DENTED AT STA 600 BETWEEN STR 24 AND 25, WL 160 **SD** COMING

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,261 hrs · 32,988 cycles

CORROSION ON FLOORBEAM BS 328 LBL 18 TO LBL 30 WL 208.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,261 hrs · 32,988 cycles

CORROSION ON STRAP LOWER SURFACE OF UPPER FLANGE OF BS 950 FLOORBEAM RBL 45 WL 208.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,261 hrs · 32,988 cycles

N1550 CRACKED STRINGER CLIP, BS 720, STR. 5R. REMOVED AND REPLACED CRACKED STRINGER CLIP, BS 720, STR. 5R PER SRM 51-30-02.

Part: STRINGER CLIP — CRACKED (BS 720F) · airframe 51,261 hrs · 32,988 cycles

CRACKED STRINGER CLIP, BS 720F, STR 4 RT. REMOVED AND REPLACED CRACKED STRINGER CLIP, BS 720F, STR 4R PER SRM 51-30-2.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,261 hrs · 32,988 cycles

CRACK IN STRINGER CLIP AT BS 720B, STRINGER 7 RT. REMOVED AND REPLACED CRACKED STRINGER CLIP AT BS 720B, STRINGER 7 RT.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 51,261 hrs · 32,988 cycles

STA 950F LBL 97 TO 54 WL 208 FLOORBEAM HAS DAMAGE ON UPPER FLANGE. TOOLING MARKS FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM PER SRM 51-30-5, 53- 10-1, & FED EX EA 7-5310-54997, BS 950F, LBL 35 - 65, WL 208.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,261 hrs · 32,988 cycles

CORROSION ON FLOORBEAM UPPER CHORD, STA 340, RBL 4 WL 208.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,261 hrs · 32,988 cycles

CORROSION ON FLOORBEAM BS 1030 RBL 25-0 WL 208 INSTALLED REPAIR PARTS PER/ UPPER CHORD PER SRM 53-10-8

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,261 hrs · 32,988 cycles

N01548 CRACKED STRINGER, BS 720B 4 STR 15R. REMOVED DAMAGED PORTION OF STR 15R AT BS 720B 4 IAW SRM 53-10-3 FIG 5. HFEC INSPECTION ON PERPHERY OF CUTOUT NO CRACKS NOTED. FABRICATED ALODINED, PRIMED AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-3 FIG 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,261 hrs · 32,988 cycles

CORROSION ON UPPER CHORD OF FLOORBEAM BS 1130 LBL 32 AND 37 WL 208. REMOVED DAMAGED AREA OF FLOORBEAM, FABRICATED REPAIR ALODINED, PRIMED, PAINTED & INSTALLED REPAIR IAW SRM 53-10-8 FIG 10 BS 1130 LBL 32-38 WL 208.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,261 hrs · 32,988 cycles

N01557 STR CRACKED B/S 720B 15 STR 15L. REPAIRED IAW SRM 53-10-3 FIG 5.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,261 hrs · 32,988 cycles

STA 950D, STRINGER 2L CLIP IS CRACKED. REMOVED AND REPLACED CRACKED STRINGER CLIP BS 950D, STR 2L PER SRM 51-30-2.

Part: FRAME — DENTED (FUSELAGE) · airframe 51,261 hrs · 32,988 cycles

AFT CARGO FRAME DENTED BS 950F AT STR 23L.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,261 hrs · 32,988 cycles

CORROSION ON FLOORBEAM UPR FLANGE UPR SURFACE STA. 1010 RBL 25-45 WL 208.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,261 hrs · 32,988 cycles

CORROSION ON FLOORBEAM UPPER FLANGE UPPER & LOWER SURFACE AT NUTCLIP HOLES STA 950D LBL 10 & 21 WL 208. CUT OUT FLOORBEAM & REPAIRED PER SRM 53-10-8.

Part: SKIN — DENTED (FUSELAGE) · airframe 51,261 hrs · 32,988 cycles

CREASED & DENTED SKIN , BS 620 TO BS 640 STR 21. CUT OUT DAMAGED SKIN BS 620 TO 640 STR 21 RT 4.3 X 19.7 AND INSTALLED REPAIR DOUBLER TRIPLER AND FILLER IAW FEDEX EA 7-5330-70507.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 51,261 hrs · 32,988 cycles

DAMAGED STRINGER BS 647 STR 21R. CUT OUT DAMAGE & REPAIRED PER SRM 51-10-3 FIG 1

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,261 hrs · 32,988 cycles

STR 15L CRACKED AT 720B 4. REPAIRED IAW SRM 53-10-3 FIG 5

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,261 hrs · 32,988 cycles

CORROSION ON FLOORBEAM LOWER CHORD UNDER NUTCLIP. REPAIRED IAW SRM 53-10-8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,261 hrs · 32,988 cycles

FRAME CRACKED BS 360 LBL 2 WL 155. CUT-OUT CRACK DAMAGE ON FRAME PER 727 SRM 51-10-1. FABRICATED REPAIR ANGLE FROM 7075T6 .050, LOT 508357 PER 727 SRM 51-40-3. LOCATED & DRILLED ANGLE PER 727 SRM 51- 40-3. ALODINED, PRIMED & PAINTED ANGLE PER 727 SRM 51-10-2. INSTALLED REPAIR ANGLE PER 727 SRM 51-30-2 AND 51-40-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,261 hrs · 32,988 cycles

CORROSION BS 1070, WL 201, LBL 25-45 AROUND AND IN NUT CLIP HOLES. CORROSION ON FLOORBEAM BS 1070, WL 201, LBL 25-45 AROUND END IN NUT CLIP HOLES FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED FLOOR BEAM IAW SRM 53-10-8.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,261 hrs · 32,988 cycles

N01551 CRACKED STRINGER BS 720 STR 5R. REMOVED AND REPLACED CRACKED STRINGER CLIP, BS 720 STR 5R PER SRM 51-30-02.

Part: WIRE — DAMAGED (NR 6 LE FLAP) · airframe 50,199 hrs · 32,406 cycles

ON CLIMBOUT, DURING FLAP RETRACT, MOVED HANDLE FROM FLAP 5 TO FLAP 2 AND 6. LEADING EDGE FLAP SHOWED IN TRANSIT ON S/O AUX PANEL WITH AMBER LEADING EDGE FLAP LIGHT ON FOWARD PANEL. INSTALLED JUMPER CABLE ON NR 6 LEADING EDGE FLAP IAW MM. MAINTENANCE AND OPERATIONAL CHECK GOOD. (CONTORL NUMBER 145201) AIRCRAFT OK FOR SERVICE AT THIS TIME.

Part: WINDOW — LOOSE (COCKPIT)

AFTER ROTATION F/O WINDOW POPPED AJAR WINDOW, OUT OF RIG. R/R R-2 SLIDING WINDOW PER MM 56-12-011-4.

Part: SOLENOID — INOPERATIVE (LG CONTROL LEVER)

1-386 AFT T/O LG HANDLE WOULD NOT RAISE PAST OFF POS. R&R LG CONTROL LEVER SOLENOID PER MM 32-31-016-4.

Part: FRAME — CRACKED (FUSELAGE)

WHILE WORKING N 199 FOUND FLANGE OF FRAME BS 1070, LBL 23, WL 156 CRACKED. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 51-40-3.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2

PILLOWING AROUND FASTENER IN CHANNEL OF STR 28L, BS 486 (C53-113-01,1). *S/D* REMOVED AND REPLACED STR PER IAW FED EX SRM 53-10-3.

Part: SKIN — DAMAGED (FUSELAGE)

DAMAGE ON EDGE OF EXTERNAL SKIN AT BS 1352, 3 AREAS FROM STR 20R-23R. *S/D* REMOVED AND REPLACED SKIN PER SRM 53-30-1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2

CORROSION ON SHEAR TIE BS 640, LBL 2, WL 146. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2

CORROSION ON FRAME SHEAR TIE BS 1166, RBL 3, WL 158. *S/D* REMOVED AND REPLACED PER IAW FEDEX EA 7-5310-57302.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2

CORROSION (C53-113-01,1) ON INNER SKIN BS 640, RBL 15, WL 148. *S/D* REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 3.

Part: DOOR — CRACKED (E/E BAY)

A/C FAIL TO PRESSURIZE, AFT GEAR RETRACTION EQUIP ACCESS DOOR LIGHT CAME ON. AVIONIC ACCESS DOOR CRACKED. CLOSED AND OPS CK PER MM 52-40-011-4, CK NORMAL.

Part: INTERCONN LINE — CRACKED (THRUST REVR APU)

99-173 - ENGINE 3 STRUT OH LIGHT ILLUM IN FLT. SYSTEM TEST UNSATISFACTORY WITH CRUISE PWR ON ENG 3. FOUND THRUST REVERSER APU INTERCONNECT LINE CRACKED AND LEAKING. REMOVED AND REPLACED LINE IN ACCORD WITH STANDARD MAINTENANCE PRACTICE. LEAK CK GOOD. OK FOR SERVICE.

Part: DOOR — NOT LATCHED (E & E COMPT)

AFT T/O, EQUIPMENT DOOR CAME OPEN AND A/C WOULD NOT PRESSURIZE. FOUND E & E DOOR UNLOCKED. LOCKED AND PRESSURIZED ON GROUND IN HRL.

Part: FIRE LOOP — WORN (NR 3 ENGINE)

CREW VERBALLY REPORTED, ENGINE NR 3 FIRE LOOP-B, WITH FAULT LIGHT ON AND BELL/FIRE LIGHTS INTERMITTENTLY ACTUATING DURING FLIGHT. TROUBLESHOT B-LOOP AND FOUND ON ENG NR 3 FIREWALL FIRE DETECTION ELEMENT FORWARD CONNECTOR (D1498) CERAMIC INSULATOR WORN, CAUSING FALSE INTERMITTENT FIRE DETECTION. DUE PARTS NOT IN STOCK AT GDL DEFERRED ENGINE NR 3 B-LOOP PER MINIMUM EQUIPMENT LIST 26-6B CONTROL NR 27935 EXPIRES 15 JAN 98. *S/D* REPLACED D-1498 ON FIREWALL FWD FIRE DETECTOR LOOP-B, CHECKS GOOD.

Part: SENSING ELEMENT — MALFUNCTION (AFT BODY)

97-0178 4 MINUTES 30 SECONDS AFTER SWITCHING BLEEDS AT FLIGHT LEVEL 180 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. BLEED SWITCHED BACK (NR 1 BACK ON, NR 2 OFF) AND LIGHT WENT OUT AFTER 4 MINUTES.RAN ALL 3 ENGINE PER JET RUN HANDBOOK AND COULD NOT DUPLICATE PROBLEM. CHECKED INTO SENSING ELEMENTS AND FOUND RIGHT AFT BODY OVERHEAT SENSING ELEMENT BAD. REMOVED AND REPLACED RIGHT AFT BODY ELEMENT PER MAINTENANCE MANUAL 26-14-1. OPERATIONAL CHECKS GOOD.

Part: DUCT — LEAKED (NR 2 ENG BLEED)

WITHIN 5 MINUTES OF SWITCHING OVER TO NR 2 ENGINE BLEED FOR NR 1 PACK LOWER AFT BODY OVERHEAT LIGHT CAME ON. LIGHT EXTINGUISHED WITHIN 30 SECONDS OF PLACING NR 2 BLEED SWITCH BACK OFF. RAN NR 1 AND NR 2 ENGINES TO POWER. COULD NOT DUPLICATE PROBLEM. LEAK CHECKED ALL DUCTS AND CLAMPS UNDER GIVEN CONDITIONS. NO LEAKS FOUND.

Part: CLAMP — FAILED (NR 1 BLEED)

ON CLIMBOUT, APPROXIMATELY 5 MINUTES AFTER CLOSING NR 1 BLEED AND OPENING NR 2 BLEED AT 18,000 FT LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. INITIATED CHECKLIST. AFTER SWITCHING TO NR 1 BLEED, LIGHT EXTINGUISHED. NOTED L-PACK AT 145 DEG C. PARTIALLY OPENED LEFT PACK COOLING DOOR, TEMPERATURE CAME ON TO 100, SWITCHED BACK TO 2 BLEED WITHOUT INCIDENT. FOUND AN AIR LEAK AT 8TH STAGE DUCT OF ENGINE 1 IN THE AFT AIRSTAIR AREA (CLAMP CRACKED). REMOVED AND REPLACED CLAMP, GROUND CHECK GOOD. NO FURTHER LEAK NOTED.

Part: OVERHEAT LIGHT — WRONG BULB (COCKPIT)

LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED 5 MINUTES AFTER SWITCHING LEFT AIR CONDITIONING PACK FROM NR 1 TO NR 2 ENGINE. CHECKLIST COMPLIED WITH LIGHT WENT OUT AFTER CLOSING NR 1 START LEVER. RAN ALL 3 ENGINES WITH ALL BLEEDS OPEN AND BOTH PACKS ON COULD NOT DUPLICATE. ENGS WERE AT 65 PERCENT N2. FOUND NO LEAKS IN AFT AIRSTAIR OR NR 1 PACK AREA. DETECTOR LOOPS OK, FOUND 1819 BULB IN LIGHT ON S/O PANEL. REPLACED WITH 1864, RAN ENGINES TO TAKEOFF POWER WITH BLEEDS OPEN AND PACKS ON, OPERATION OK.

Part: DUCT — LEAKING (AFT FUSELAGE)

LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED APPROX 5 MINS AFTER SWAPPING BLEEDS FROM NR 1 TO NR 2 ON THE ALTIMETERS CHECKLIST. RAN THE LOWER AFT BODY OVERHEAT LIGHT CHECKLIST AND THE LIGHT EXTINGUISHED AFTER SWAPPING BLEEDS BACK TO NR 1. CONTINUED FLIGHT WITH NR 1 BLEED FOR THE LEFT PACK, TESTED OK. REMOVED AND REPLACED PNEUMATIC DUCT FROM NR 2 ENGINE BLEED RUN ENGINE NR 2, LEAK TEST OK.

Part: FLOORBEAM — CORRODED (BS 720)

NR 0604 71C205 00, UPPER CARGO; CORROSION ON FLOORBEAM AT STA 720A, BL 0 TO 25 LBL. CORROSION REMOVED AND ANGLE REPAIR INSTALLED PER SRM/AARD10H 53-10-07-2 FIG 2.

Part: RETRACT MECH — MALFUNCTIONED (LANDING GEAR)

LANDING GEAR LEVER FAILED TO RAISE PAST THE OFF POSITION AFTER TAKEOFF. LANDING GEAR LEVER LATCH/LIGHT CIRCUIT BREAKER WAS PULLED AND RESET IN ACCORDANCE WITH RED TABS AND LANDING GEAR WAS NORMALLY RAISED AFTER. INSTALLED GEAR PINS, OPERATED GEAR HANDLE SEVERAL TIMES AND ALL OPERATION NORMAL. OK FOR SERVICE. GEAR PINS REMOVED AND STOWED, NO PREVIOUS HISTORY.

Part: BLEED SYST — ODOR (NR 1 ENGINE)

ON DESCENT WHEN NR 1 BLEED SELECTED STRONG BURNING ODOR UNTIL BLEED TURNED OFF. RAN ENGINE AND CHECKED OUT NR 1 BLEED SYS, NO STRONG BURNING ODORS WERE DETECTED. A/C OK FOR SERVICE.

Part: MAP LIGHT CONN — BURNED (COCKPIT)

IMMEDIATELY AFTER TURNING THE NR 1 ON, DURING THE START OF DESCENT A BURNING SMELL WAS NOTICEABLE IN THE COCKPIT. REPEAT WRITE UP, REF 522004. RAN NR 1 PACK, FOUND NO TRACE OF BURNING ODOR. OPENED NR 1 ENG, CHECKED DUCTING, FOUND OK. RAN ENGINE, STILL NO BURNING ODOR, INSPECTED DUCTING AT NR 1 PACK CHECKED OK. FOUND SECOND OFFICER'S LEFT MAP LIGHT TERMINAL BURNED. REPLACED TERMINAL, LIGHT CHECKED OK. C/N DUP ODOR PROBLEM.

Part: FIRE LOOP — OUT OF POSITION (NR 1 ENGINE)

NR 1 ENG STRUT O/H LIGHT CAME ON. BLEED AIR WAS BEING USED FOR PACK. OPS AFTER AIR WAS TURNED OFF, O/H LIGHT EXTINGUISHED, ACCOMP ENG STRUT O/H LIGHT ON CKLST. ESTABLISH PACK OPS USING NR 2 BLEED. OPENED NR 1 STRUT ACCESS PANELS, FOUND AFT UPPER LOOP IN CONTACT WITH LOWER LOOP BRACKET, REPOSITIONED. ALSO, FOUND LOOPS CONN LOOSE AT FUSELAGE, RE-TIGHTENED AND RE-SAFETIED. RAN ENG PER JRH A DIF POWER SETTING. NO LEAKS, NO LIGHT, GND OPS CK GOOD. RE-INSTALLED STRUT ACCESS PANELS.

Part: WINDOW POST — CRACKED (FLIGHT DECK)

NDT PLEASE C/W E.O. 7-5330-7-3354 ( AD 93-05-17) X-RAY INSPECTION THE E-N WINDOW POST. E.O. 7-5330-7-3354 PART II X-RAY INSP E-N WINDOW POST RT HAND. PILOTS SLIDING WINDOW CRACK INDICATION APPX 1.125 INCH LONG. ENGINEERING NOTIFIED. REFERENCE PART 4 AND PART 5 FOR E.O. 7-5330-7-3354 FOR REPAIRS.