N201FE

Part: LANDING GEAR — UNKNOWN (NOSE) · airframe 32,820 hrs · 18,921 cycles

WHEN CONFIGURING FOR LANDING, NOSE GEAR STAYED UP. GO AROUND INITIATED AND NOSE GEAR EXTENDED BEFORE QRH STARTED. HYD PRESSURE NORMAL THROUGH-OUT. WHEN NOSE GEAR DID EXTEND, DOOR LIGHT CAME ON FOR ABOUT 20 SECS BEFORE GEAR CAME DOWN. INSP NLG, WHEEL WELL AND DOORS. NO DEFECTS NOTED. LUBRICATED NLG AND DOORS PER M/M 12-21-011-2. JACKED A/C NLG PER MM 07-11-000-2. PERFORMED NLG EXTENSION AND RETRACTION TEST PER MM 32-33-000-5. CYCLED GEAR HANDLE 5 T0 6 CYCLES EACH GEAR RETRACT TIME 7 SEC (MAX TIME IS 10 SEC). NOSE GEAR EXTEND TIME 10 SEC EACH CYCLE.

Part: UNKNOWN — ODOR (CABIN) · airframe 31,955 hrs · 18,384 cycles

UPON T/O, SMELLED UNKNOWN ODOR. DURING CLIMB, IT DISSIPATED AND CAME BACK A FEW TIMES. AT FL 260, DECLARED A PRECAUTIONARY EMERGENCY. WHEN POWER CAME BACK DESCENDED, THE FUMES WENT AWAY AND DID NOT RETURN. ALL THE WAY PACK TO EWR, IT SEEMS TO COME AND GO W/THROTTLES. RAN ENGINES AT VARIOUS POWER SETTINGS UP TO TAKEOFF. POWER EPR IAW B727 JRH CH 4 AND 7-15 WITH BLEEDS ISOLATED AND ALL OPEN, CYCLING PACKS HOT/COLD. NO NOTICEABLE ODORS IN COCKPIT AT THIS TIME. CHECKED GASPER FAN, OPS NORMAL, NO ODORS. CHECKED MDC COMPARTMENT FOR POSSIBLE SPILLS, NONE.

Part: RIB — DAMAGED (WING) · airframe 31,913 hrs · 18,343 cycles

RT RIB UPPER CHORD AT BL 70.5 FASTENER HOLE REWORK AND REPAIR. COMPLIED WITH EO 7-5710-7-2038 PART 2.

Part: LATCH — GOUGED (CARGO DOOR) · airframe 31,913 hrs · 18,343 cycles

FOUND MAIN CARGO DOOR LATCH AT BS 500, GOUGED. REPAIRED MAIN CARGO DOOR LATCH IAW EA 7-5230-7-4348.

Part: SPINDLE — DAMAGED (RT MLG) · airframe 31,913 hrs · 18,343 cycles

RT MLG HAS EXCESSIVE MOVEMENT AT SPINDLE. REPAIRED RT MLG SPINDLE BORE IAW EA 7-5230-100580.

Part: FLOORBEAM — UNKNOWN (BS 870) · airframe 31,913 hrs · 18,343 cycles

FOUND BS 870 FLOORBEAM UPPER TEE HOLE LBL 54 WL 208. REPAIRED BS 870 FLOOR BEAM UPPER CHORD HOLE LBL 54 WL 208 IAW FED EX EA 7-5310- 100578.

Part: SKIN — CHAFED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

THE RT HORIZONTAL NR 5 BALANCE BAY UPPER SKIN PANEL IS CHAFED AT THE TE OF THE STIFFENER OB END. REMOVED AND REPLACED SKIN PANEL PER FED EX EA 7-5510-100575.

Part: FLOORBEAM — GOUGED (BS 328) · airframe 31,913 hrs · 18,343 cycles

FUSELAGE INTERIOR FLOOR STRUCTURE, BS 328 LBL 45 WL 208, FLOORBEAM GOUGED. REPAIRED DAMAGED FLOOR BEAM PER FED EX EA 7-5310-100573.

Part: SUPPORT FITTING — GOUGED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

GOUGES IN MAIN CARGO DOOR FORWARD ACTUATOR SUPPORT FITTING JUST BELOW UPPER ATTACH POINT OF AFT REACTION LINK. REPAIRED DAMAGED ACTUATOR SUPPORT FITTING PER FEDEX EA 7-5230-100572.

Part: FLOORBEAM — GOUGED (BS 1110) · airframe 31,913 hrs · 18,343 cycles

N01216 FUSELAGE INTERIOR FLOOR STRUCTURE BS 1110 RBL 2 TO 22 WL 208 FLOORBEAM UPPER SURFACE GOUGED. REPARIED FLOOR BEAM PER FED EX EA 7-5310-100571.

Part: PLATE — MISDRILLED (BS 720D) · airframe 31,913 hrs · 18,343 cycles

N01369 FUSELAGE INTERIOR FLOOR STRUCTURE BS 720D LBL 21 TOP SURFACE OF FLOORBEAM NUT PLATE HOLES MISDRILLED. REPARIED MISS DRILLED HOLES PER FED EX EA 7-5310-100570.

Part: SUPPORT BEAM — CRACKED (RT WING) · airframe 31,913 hrs · 18,343 cycles

RIGHT WING - UPPER I/B MOST FIXED T/E PANEL/HUD LINE SUPPORT BEAM (RUNNING ALONG THE FWD SIDE OF THE MLG BEAM) CRACKED AT I/B END LOWER CHORD, APROX 26 INCHES I/B OF FWD MLG TRUNNION BEARING. REPAIRED RT WING UPPER I/B MOST FIXED T/E PANEL HYD LINE SUPPORT BEAM PER FED EX EA 7-5710-100566.

Part: BUSHING — GALLED (FLAP TRACK) · airframe 31,913 hrs · 18,343 cycles

N01113, NR 2 FLAP TRACK, BUSHING GALLED IN IB BOLT HOLE AT FWD ATTACH POINT IN REAR SPAR. REPAIRED BUSHING NR2 FLAP TRACK IB BOLT HOLE AT FWD ATTACH POINT IN REAR SPAR IAW EA 7-5710-100565.

Part: STRINGER CLIP — CORRODED (BS 720A S4R) · airframe 31,913 hrs · 18,343 cycles

WHILE ACCOMPLISHING NR N01259 FOUND SURFACE CORROSION ON STRINGER CLIP AT BS 720A, STR 4R. REMOVED AND REPLACED STRINGER CLIP AT BS 720A STR 4R IAW SRM 51-30-2.

Part: DOOR — DENTED (FWD ENTRY) · airframe 31,913 hrs · 18,343 cycles

N00870 DENT ON FWD ENTRY DOOR ON IB WEB LIGHTNING HOLE AT BS 335 STR 14L ** SD ** COMING. REPAIRED DENT ON FWD ENTRY DOOR ON IB WEB LIGHTING HOLE AT BS 335, STER 14L IAW, SRM 51-40-2.

Part: STRINGER CLIP — CORRODED (BS 720A S3R) · airframe 31,913 hrs · 18,343 cycles

WHILE ACCOMPLISHING NR N01259, FOUND SURFACE CORROSION ON STRINGER CLIP, AT BS 720A, STR 3R. REMOVED AND REPLACED STRINGER CLIP AT BS 720A STR 3R IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720A S2R) · airframe 31,913 hrs · 18,343 cycles

WHILE ACCOMPLISHING NR N01259, FOUND SURFACE CORROSION ON STRINGER CLIP, AT BS 720A, STR 2R. REMOVED AND REPLACED STRINGER CLIP AT BS 720A STR 2R IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 950) · airframe 31,913 hrs · 18,343 cycles

CORROSION (C53-224-01(2) BS 950 FLOORBEAM UPPER TEE EMANATING FROM UNDER NUTPLATES RBL10 AND 27 WL 208. REPARIED CORROSION ON BS 950 FLOORBEAM RBL 10 AND 27 WL 208 PER FED EX EA 7-5310- 100568.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

EXTERIOR SKIN HAS DENT JUST BELOW FWD ENTRY DOOR UPR HINGE CUTOUT. REPAIRED DENT IN EXTERIOR SKIN JUST BELOW FWD ENTRY DOOR UPPER HINGE CUTOUT IAW EA NR 7-5330-100564.

Part: DOOR — DENTED (FWD ENTRY) · airframe 31,913 hrs · 18,343 cycles

DENT ON FWD ENTRY DOOR ON IB WEB AFT EDGE AT 346 STR 13L. REPAIRED DENT ON FWD ENTRY DOOR ON IB WEB AFT EDGE AT 346 STR 13L IAW SRM 51-40-2.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

N01429 WHILE ACCOMPLISHING NR N01259, FOUND SURFACE CORROSION ON STINGER CLIP, AT BS 720A, STR 1. REMOVED AND REPLACED STRINGER CLIP AT BS 720A STR 1 IAW SRM 51-30-2 AND 51-30-5.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

EXISTING FLOORBEAM REPAIR AT STA 344 ON MAIN CARGO DECK LBL 40 TO RBL 15. REPAIR REQURIES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED UPPER FLOORBEAM CHORD IAW SRM 53-10-1, 53-30-2, 51-30-5, 51-10-2 AND SR 27-53-007.

Part: SKIN — UNKNOWN · airframe 31,913 hrs · 18,343 cycles

N01454 EXISTING EXTERNAL DOUBLER REPAIR APPROX. 9.50 INCHES X 14.50 INCHES AT STA. 494 LT STRINGER NR 19 (DOT NR 16) REQURIES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR AND INSTALLED NEW REPAIR IAW FED EX EA 7-5330-100569.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

CORROSION (C53-224-01(2) BS 740 FLOORBEAM UPPER CHORD EMANATING FROM UNDER NUT PLATE RBL 5 WL 208. FLOORBEAM BS 740 UPPER CHORD WAS BLENDED IN AN AREA 4 X 1.5 INCHES RBL 5 WL 208 WITH REMAINING THICKNESS OF .115 FLAP PEENED BLENDED AREA, ALODINED AND PRIMED IAW FED EX EA 7-5310-100563.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

STRINGER DAMAGED AT BS 1090 STR 7R. REPAIRED DAMAGED STRINGER PER SRM 53-10-3.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

STRINGER CLIP CRACKED STA 1090 STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-02.

Part: SKIN — DENTED (BS 361) · airframe 31,913 hrs · 18,343 cycles

DENT IN SKIN AT BS 361 JUST BELOW STR 17L CUT OUT & REMOVED DAMAGE IN SKIN BS 361 BELOW STR 17L. FABRICATED & INSTALLED REPAIR IAW FED EX EA 7-5330-100574. REPAIR IS CONSIDERED A MAJOR REPAIR.

Part: STRINGER CLIP — CRACKED (BS 1070 S7R) · airframe 31,913 hrs · 18,343 cycles

STRINGER CLIP CRACKED AT STA 1070 STR 7R. REMOVED AND REPLACED STRINGER CLIP AT STA 1070, STR 7R IAW SRM 51-30-2 AND 51-30-5.

Part: STRINGER CLIP — CRACKED (BS 950D S7R) · airframe 31,913 hrs · 18,343 cycles

STRINGER CLIP CRACKED AT STA 950D STR 7R. REMOVED AND REPLACED STRINGER CLIP AT STA 950D, STR 7R IAW SRM 51-30-2 AND 51-30-5.

Part: STRINGER CLIP — CRACKED (BS 970 S9R) · airframe 31,913 hrs · 18,343 cycles

STRINGER CLIP CRACKED AT STA 970 STR 9R. REMOVED AND REPLACED STRINGER CLIP BS 970 STR 9R IAW SRM 51-30-2.

Part: STRINGER CLIP — CRACKED (BS 950D S7L) · airframe 31,913 hrs · 18,343 cycles

STRINGER CLIP CRACKED AT STA 950D STR 7L. REMOVED AND REPLACED STRINGER CLIP AT STA 950D, STR 7L IAW SRM 51-30-2 AND 51-30-5.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

STRINGER CLIP CRACKED AT STA 1090, STR 7L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2 AND 51-30-5.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

STRINGER CLIP CRACKED AT STA 990, STR 7L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2 AND 51-30-5.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

STRINGER CLIP CRACKED AT STA 950F, STR 7L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2 AND 51-30-5.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

STRINGER CLIP CRACKED AT STA 1030, STR 7L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2 AND 51-30-5.

Part: FRAME — DENTED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

FUSELAGE UPPER LOBE, FRAME IS DENTED, BS 500, 5 INCHES ABOVE STR 17R. REPAIRED UPPER LOBE FRAME AT SB 500 5 INCHES ABOVE STR 17R IAW SRM 51-40-3.

Part: FRAME — CORRODED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

FUSELAGE UPPER LOBE, CORROSION ON FRAME INNER AND OUTER FLANGE, AT BS 720A BETWEEN STR 1 TO STR 4 RT. REPAIRED FRAME PER SRM 53-10-4.

Part: FRAME — DENTED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

FUSELAGE UPPER LOBE, FRAME IS DENTED, BS 520, 5 INCHES ABOVE STR 17R. REPAIRED FUSELAGE UPPER LOBE FRAME AT BS 520 5 INCHES ABOVE STR 17R IAW SRM 51-40-3.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

STRINGER CLIP CRACKED AT STA 950B, STR 7L. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-2.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

STRINGER CLIP CRACKED AT STA 950E, STRL 7L. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-2.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

STRINGER CLIP CRACKED AT STA 950C, STR 7L. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-2.

Part: SKIN — CHAFED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

EXTERNAL SKIN IS CHAFED, AT BS 950E, STR 26R. REPAIRED PER FED EX EA 7-5330-100567.

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 31,913 hrs · 18,343 cycles

EXISTING EXTERNAL DOUBLER REPAIR APPROX 2 X 2 INCHES ON RT HORIZONTAL STABILIZER UPPER SURFACE T/E AREA, ELEVATOR STA 99.79 NR 2 BALANCE BAY UPPER PANEL. REPAIR REQUIRES EVALAUTION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED FABRICATED NEW, BONDED AND INSTALLED REPAIR DOUBLER IAW SRM 55-20-3.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

EXISTING EXTERNAL DOUBLER REPAIR APPROX 18 X 12 INCHES AT STA 1185 RT STRINGER NR 5 ON UPPER FUSELAGE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR DOUBLER AT STA 1185 RT STR 5. FABRICATED NEW DOUBLER FORM 2024T3 .063 LOT 678274. ALODINE, PRIMED, INSTALLED REPAIR EDGE PAINTED. REPAIR PER SRM 53-30-3 FIG 1, 51-30-2, 51-30-5, 51-30-8, FEDEX MM 51-20-021, 51-20-151. MAJOR REPAIR.

Part: SKIN — CHAFED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

EXTERNAL SKIN CHAFED, AT RT WING L/E AND UNDER WING TO BODY FAIRING FWD, WRAP AROUND PANEL, BS 720D 13, STR 19R. REMOVED DAMAGE, AND REPIAR IAW SRM 53-30-3, 53-30-1 AND M/M 51-20-021, 51-20-151.

Part: FRAME — DENTED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

FUSELAGE UPPER LOBE FRAME IS DENTED AT BS 600 5" ABOVE STR 17. REMOVED DAMAGED FRAME, REPAIRED FRAME IAW SRM 53-10-2, 51-20-1, 51-30-5, 51-10-2, 51-40-3, 53-10-4, AND 51-30-2.

Part: FRAME — DENTED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

FUSELAGE UPPER LOBE, FRAME IS DENTED, BS 580, 5 INCHES ABOVE STR 17R. REMOVED DAMAGE AND REPAIRED FRAME IAW SRM 53-10-2, 51-20-1, 51-40-3, 53-10-4, 51-30-5 AND 51-30-2.

Part: FRAME — DENTED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

N01255 FUSELAGE UPPER LOBE, FRAME IS DENTED, BS 540, 5 INCHES ABOVE STR 17R. REMOVED DAMAGE AND REPAIRED IAW SRM 53-10-2, 51-20-1, 51-30-5, 51-10-2, 51-40-3, 53-10-4 AND 51-30-2.

Part: FRAME — DENTED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

FRAME DENTED BETWEEN STR 23 AND 24 RT, STA 680. CUT OUT DAMAGE AND FABRICATED REPAIR IAW SRM 51-40-3 FIG 1.

Part: FRAME — DENTED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

FRAME DENTED BETWEEN STR 23 AND 24 LT, STA 520. CUT OUT DAMAGE AND FABRICATED REPAIR IAW SRM 51-10-3 FIG 1.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

FOUND FASTENER HOLE ELONGATED ON UPPER SURFACE OF FLOORBEAM STA 400 RBL 12 WL 208. CUT OUT DAMAGE ON FLOOR BEAM B/S 400 RBL 12 W/L 208. FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-8 FIG 8.

Part: RIB — DAMAGED (WING) · airframe 31,913 hrs · 18,343 cycles

FOUND RIB AT BL 70.5 FASTENER HOLE REWORK AND REPAIR. COMPLIED WITH WRI 57-10/0252 EO. 7-5710-7-2308I PART 2.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

FOUND FUSELAGE INTERIOR FLOOR STRUCTURE BS 312 LBL 30 WL 208 FLOORBEAM GOUGED. REPAIRED FLOOR BEAM PER SRM 53-10-8.

Part: SKIN — CHAFED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

FOUND EXTERNAL SKIN, IS CHAFED AT BS 950E PLUS 9, 4" BELOW STR 18R. REPAIRED PER FED EX EA 7-5330-100577.

Part: REPAIR — MISINSTALLED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

EXISTING EXTERNAL CIRCULAR DOUBLER REPAIR APPROX 6 INCHES AT STA 950C PLUS 15 INCHES RT STRINGER NR 23. REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING EXTERIOR REPAIR DOUBLER BS 950C PLUS 15, RT STR 23. DOES NOT COMPLY WITH APPROVED FAA REPAIR DATA. REMOVED PREVIOUSLY INSTALLED REPAIR PER SRM 51-30-2. TRIMMED OUT SKIN IN A 7.6 X 6 INCHES AREA. FABRICATED REPAIR DOUBLER FROM 2024T3 X 0.112. INSTALLED REPAIR BS 950C PLUS 3 TO 950D PLUS 1 STR 23-24 RT, ALL WORK PER SRM 53-30-3 FIG 1 FOUND TO BE A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 312) · airframe 31,913 hrs · 18,343 cycles

FUSELAGE INTERIOR FLOOR STRUCTURE, BS 312 LBL 19 WL 208, FLOORBEAM CORRODED. REPAIRED FLOOR BEAM IAW SRM 53-10-1.

Part: FRAME — DENTED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

DENTED FRAME AT BS 1148 STRINGER 25R. REMOVED DAMAGED AND REPAIR FRAME PER SRM 51-40-3.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 31,913 hrs · 18,343 cycles

CORROSION (C53-224-01) BS 720, STR CLIP 4L. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720C S2L) · airframe 31,913 hrs · 18,343 cycles

CORROSION BS 720C, STR 2L CLIP. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-2.

Part: SKIN — BENT (E/E BAY DOOR) · airframe 31,913 hrs · 18,343 cycles

E&E COMPARTMENT DOOR EXTERNAL SKIN BENT AT CTR FWD. REMOVED AND REPLACED E & E COMPARTMENT DOOR IAW SRM 52-00-2.

Part: SWITCH — DAMAGED (K FLAPS) · airframe 30,731 hrs · 17,627 cycles

AFTER T/O DURING FLAP RETRACTION FROM 5 DEG TO 2 DEG AMBER LED LIGHT REMAINED ILLUMINATED S/O AUX PAN INDICATED NR 5 REMAINED EXT. PERFORMED QRH PROC AND LIGHT REMAINED ILLUM. RET TO LAND. REMOVED AND REPLACED NR 5 KRUEGER FLAP SWITCH AND STRAIGHTENED SWITCH ARM. REF M/M 27-82-001-4 OPERATES NORMAL.

Part: BEARING — LOOSE (ZONE 500) · airframe 28,550 hrs · 16,356 cycles

INBOARD FLAPS INDICATE ASYMMETRIC BETWEEN 2 DEG & 5 DEG ON RETRACTION AFTER LANDING. REMOVED AND REPLACED NR 4 FLAP TRANSMISSION IAW MM 7-51-041-4, LEAK AND OPS CHECKS GOOD IAW MM 27-51-00 0-5.

Part: CYLINDER — CRACKED (ZONE 700) · airframe 28,424 hrs · 16,289 cycles

NOSE GEAR OUTER CYLINDER IS CRACKED INBOARD OF LEFT TRUNNION. C/W WITH W/C 32T2501 NOSE LANDING GEAR AND DRAG BRACE REMOVAL/INSTALL. COMPLIED WITH W/C 32T2501 REMOVED AND REPLACED NOSE LANDING GEAR ASSY AND DRAG BRACE.

Part: CSD — FAULTY (NR 2) · airframe 26,330 hrs · 15,209 cycles

LEVEL AT FL 310 IN SMOOTH CONDITIONS, EXPERIENCED A THREE LIGHT TRIP. RAN QRH PROCEDURES, UNABLE TO RECOVER BTB, G/B OR FIELD. FREQS/VOLTS ON NR 2 GEN WERE ZERO (OFF SCALE LEFT). NO LIGHTS ON ELEC FAULT PANEL ILLUMINATED. NR 2 CSD WAS DISCONNECTED. AIR TURNBACK. UNABLE TO POWER NR 2 AC BUS. REMOVED AND REPLACED NR 2 CSD IAW 727-200 M/M 24-10-011-4 AND REMOVED AND REPLACED NR 2 GEN IAW 24-20-001-4 OP AND LEAK CHECKED GOOD.

Part: SKIN — GOUGED (FUSELAGE)

GOUGE AND DENT IN FUSELAGE SKIN AT BS 1310, STR 23L. REMOVED AND REPLACED REPAIR DOUBLER PER SRM 53-30-3 FIG 1.

Part: FRAME — DENTED (FUSELAGE)

SHARP DENT IN FRAME UPPER FLANGE BS 680, STR 24L. REMOVED AND REPLACED FRAME PER SRM 51-40-3.

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

CORROSION ON FWD ENTRY DOOR MOP SILL BS 344-328, LBL 55, WL 208. REMOVED AND REPLACED MOPSILL LT PER SRM 51-30-2.

Part: SPAR — CHAFED (VERTICAL STAB)

LEFT HAND VERTICAL STABILIZER MID SPAR CHORD CHAFED AT FIN STA 229. REMOVED AND REPLACED PER SRM 55-30-6 FIG 3.

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

CORROSION BS 344, FLOORBEAM UPPER CHORD RBL 17 - LBL 55, WL 208. REMOVED AND REPLACED CHORD PER SRM 51-10-2, 51-10-6, 53-10-1, & 53-10-8.

Part: FRAME — DENTED (FUSELAGE)

DENT IN FRAME UPPER FLANGE BS 500, STR 24L. REMOVED AND REPLACED FRAME PER SRM 51-40-3, 51-40-2, 53-30-5 & EA 7-5310-60591.

Part: SHEAR TIE — CRACKED (FUSELAGE)

WHILE WORKING N296 FOUND CRACK IN SHEAR TIE BS 720, RBL 11, WL 150. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4, 51-10-3.

Part: SUPPORT — CORRODED (FUSELAGE)

CORROSION (C53-111-01, 2) ON CENTER CEILING SUPPORT BEAM AROUND NUT PLATES BS 720+10 TO 720C+3, BL 0, WL 200. REMOVED AND EPLACED CHORD PER SRM 51-40-4.

Part: FRAME — CRACKED (FUSELAGE)

FRAME CRACKED AT BS 783, RBL 66, WL 193 AFT SIDE. REMOVED AND REPLACED FRAME PER EA 7-5310-7-3367.

Part: SWITCH — INOPERATIVE (L/E FLAP)

NR 4 LEADING EDGE DEVICE MALFUNCTION DURING FLAP RETRACTION. REMOVED AND REPLACED FLAP SWITCH PER MM 27-82-001-4.

Part: SKIN — LIGHTNING STRIKE (BS 1088-1097)

NR 240 - 3 LIGHTNING STRIKES IN EXTERNAL SKIN AT BS 1088-1097, STR 30. INSTALL PATCH AND INSTALL FILLER WITH SOLID RIVETS IAW FEDEX SRM 53-30-3 AND EA NR 7-5330-46963, BS 1088-1097, STR 30.

Part: SKIN — LIGHTNING STRIKE (BS 1072-1083)

NR 239 - 4 LIGHTNING STRIKES IN EXTERNAL SKIN BETWEEN BS 1072-1083 AT STR 30. REPAIRED DAMAGED SKIN AT BS 1072.5, STR 30 PER FEDEX 7-5330-46963.

Part: SKIN — LIGHTNING STRIKE (BS 1059-1067)

NR 238 - 3 LIGHTNING STRIKES BETWEEN BS 1059 AND 1067 AT STR 30. REPAIRED DAMAGED SKIN PER FEDEX EA 7-5330-46963.

Part: ENGINE — FAILED (NR 2)

WHEN SWITCH FROM BLD NR 1 TO BLD NR 2 AT 18000 FT, THE ENG NR 2 BLD HIGH TEMP LIGHT ILLUM. AFT SWITCH BACK TO NR 1 BLD. THE HIGH TEMP LIGHT WENT OUT APPROX 30 SEC TO 1 MIN LATER. NR 2 ENG PWR SET WAS 2.08 EPR. *S/D* CHGD NR 3 ENG EPR TRANSMITTER, PRECAUTION B/B 77-11-11. REMOVED AND REPLACED NR 2 ENGINE PER WORK CARD 70T0002 AND 70T0301. CK GOOD NO LEAKS NOTED.

Part: FIRE WARN BELL — MALFUNCTIONED (COCKPIT)

97-0211 - AFTER TAKEOFF, 2000FT FIRE WARNING BELL SOUNDED AND GLARE SHIELD LIGHT CAME ON FOR 1-2 SECONDS. NO OTHER INDICATION ALL ENGINE INSTRUMENTS NORMAL. OPERATIONAL CHECK ALL SYSTEM CHECK NORMAL COULD NOT DUPLICATE. OK FOR SERVICE.

Part: ACCESSORY UNIT — MALFUNCTIONED (RT MLG)

ON GEAR EXTENSION GEAR DOOR LIGHTS CYCLED CORRECTLY. NOSE AND LEFT GEAR LIGHTS INDICATED NORMAL EXTENSION. THE RIGHT RED GEAR LIGHT STAYED LIT. THE RIGHT GREEN GEAR LIGHT DID NOT COME ON, LIGHTS TESTED GOOD. RAN CHECKLIST, CYCLED GEAR, RED LIGHT STAYED ON, NO GREEN LIGHT. REMOVED AND REPLACED ACCESSORY UNIT LANDING GEAR POSITION LIGHT PER M/M 32-09-122 PAGE 505 SYSTEM CHECKS OK. REMOVED LANDING GEAR PINS.

Part: ACCESS PANEL — MISSING (LT NAV LIGHT)

UPPER ACCESS PANEL MISSING ON LT NAVIGATION LIGHT. INSTALLED PANEL.

Part: LIGHT — FAILED (FE PANEL)

SMOKE COMING FROM ENGINEERS FLUORESCENT LIGHT, THIS IS A REPEAT WRITE UP. FOUND FLT ENGINEER'S RT AFT TABLE LIGHT BAD, WITH A BURNT ODOR FROM LIGHT. REMOVED AND REPLACED SAME. OPS CHECKS NORMAL AS PER MM 33-10.

Part: LIGHT — SMOKING (FE TABLE)

SMOKE WAS COMING FROM FLUORESCENT LIGHT AND RIGHT TABLE LIGHT AREA. PULLED C/B FOR F/E TABLE FLUORESCENT LIGHT FIXTURE. NO FURTHER SMOKE, TIGHTENED LOOSE WIRE.