N222FE

Part: UNKNOWN — MALFUNCTIONED · airframe 54,988 hrs · 35,425 cycles

UPON RAISING GEAR HANDLE THE FOLLOWING LIGHTS ILLUMINATED, CAPT AND FO DECISION HEIGHT, SPEED BRAKE DO NOT ARM, SPEED BRAKE ARMED, ALL REVERSER OPERATING, RED AND GREEN GEAR AND DOOR LIGHTS, TAIL SKID, GREEN AND AMBER LE FLAPS, FO ALT.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 54,859 hrs · 35,331 cycles

DURING FLAP RETRACTION AFTER TAKEOFF OUTBOARD TRAILING EDGE FLAPS WENT ASYMETRIC AND LOCKED OUT AT 2 DEGREES. FOLLOWED QRH PROCEDURES. LANDING UNEVENTFUL. REMOVED AND REPLACED INDICATOR PER M/M 27-52-000-0 SYSTEM OPS CHECKS OK AT THIS TIME. PREMATURE REMOVAL/INSTALLATION OFF MFG 2061-12-1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,836 hrs · 35,305 cycles

MAIN ENTRY DOOR EXT SKIN AFT UPPER CORNER HAS 2 CRACKS. REPAIRED MAIN ENTRY DOOR AFT UPPER DOOR IAW SRM 52-00-. FABRICATED REPAIR DOUBLER FROM 2024 T-3 .063 C BATCH 986936, FILLER FROM 2024 T-3 .050C BATCH 1136567 TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR IAW SRM 51-30-2. REMOVED AND REPLACED UPPER GATE IAW SRM 51-3-2. PREPPED AND PAINTED REPAIRED AREA AND GATE IAW MM 51-20-151-7.

Part: FRAME — CRACKED (BS 1352) · airframe 54,836 hrs · 35,305 cycles

FRAME AT BS 1352 INNER STRUCTURE CRACKED AT 8:00 POSITION FOUND UPON REMOVAL OF OUTER CHORD. REPAIRED INNER STRUCTURE ON FRAME STA 1352 IAW SRM 51-40-3.

Part: SHIM — CORRODED (ZONE 500) · airframe 54,836 hrs · 35,305 cycles

LT NR 3 FLAP TRACK BEAM CENTER MOUNT TAPERED SHIM CORRODED REMOVED CORROSION FOUND OUT OF LIMITS, CORROSION EXFOLIATION IAW SRM 51-10-6 AND SRM57-10-1 FIG 1 DETAIL 1. FABRICATED NEW SHIM ON MAE TRAVLER T6/31804.

Part: SHIM — CORRODED (ZONE 500) · airframe 54,836 hrs · 35,305 cycles

LT NR2 FLAP TRACK AFT MOUNT TAPERED SHIM CORRODED REMOVED CORROSION FOUND OUT OF LIMITS REMOVED .035 FROM ORG MAT .045 REMAINING MAT .010 IAW SRM 57-10-6 AND 57-10-1 FIG 1 FABERICATED NEW SHIM ON MAE TRAVLER T6/ 631803.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 54,836 hrs · 35,305 cycles

LT NR 3 FLAP TRACK BEAM FWD MOUNT SUPPORT FITTING CORRODED. REMOVED AND REPLACED BUSHNG IAW SR 27-57-020 AND SOPM 20-50-03. REMOVED CORROSION FROM FITTING ORIGINAL MATERIAL .750 AFTER REWORK .740. FOUND TO BE WITHIN LIMITS IAW SRM 51-106 AND SR 27-51-020 TREATED AND PRIMED IAW SRM 51-10-2.

Part: DISPLAY — INOPERATIVE (WX RADAR) · airframe 53,719 hrs · 34,566 cycles

AFTER T/O, SWITCHING FROM TERRAIN TO WX MODE OR RADAR, LOST RANGE MARKER AND DATA DISPLAY. ACTUAL WX RETURNS WORKED. REMOVED AND REPLACED INDICATOR R/T AS PRECAUTIONARY. REF B727-200MM SEC 34-41-031-4 AND 34-41-041-4.

Part: TUBE — CHAFED (ZONE 500) · airframe 53,620 hrs · 34,509 cycles

HYD SYS A FAILED (W/FLAPS 15) WHILE CONFIGURING TO LAND AT MEM. REPLACED ENGINES NR 1 AND 2 ENGINE DRIVEN HYDRAULIC PUMPS, REF MM29-11-041-2. REPLACED BOTH CASE DRAIN FILTERS. REPLACED SYSTEM "A" HYDRAULIC RETURN FILTER, R/I. REMOVED AND REPLACED SYSTEM A HYDRAULIC PRESS FILTERS. REMOVED AND REPLACED SYSTEM A SPOILER 3 PRESS AND RET LINES IAW SMP. PERFORMED LEAK CK OF ALL CHANGED COMPONENTS. LK CKS GOOD. RAN 12 ENGINES PER JRH CHAP 5 AND PERFORMED OP AND LK CHK OF SYSTEM A ENG DRIVEN PUMPS. OPS AND LK CHECKS GOOD.

Part: MODULE — FAILED (MLG INDICATOR) · airframe 53,020 hrs · 34,161 cycles

WHEN GEAR HANDLE IS UP, RIGHT GEAR SAFE GREEN LIGHT WILL NOT TEST. REPLACED BULBS CYCLED CBS. SWAPPED RIGHT GEAR AND LEFT GEAR LIGHTS IN LEFT POSITION, RIGHT LIGHT WORKED IN RIGHT POSITION, LEFT LIGHT DID NOT WORK. CK'D CONTINUITY THROUGH WARN LIGHT PUSH TO TEST CIRCUIT. L808 FOR RT MLG. FOUND NO CONTINUITY. CK'D NEW PANEL ASSY. LIGHT L808 FOR CONTINUITY FOUND GOOD CONTINUITY. INSTALLED NEW L/G LIGHT MODULE, OPS CK GOOD. REF 727-200 WDM 32-64-01.

Part: ACTUATOR — MALFUNCTIONED (NLG DOWNLOCK) · airframe 52,548 hrs · 33,877 cycles

NOSE GEAR WOULD NOT EXTEND DURING APPROACH. RED NOSE LIGHT ILLUMINATED. UPON LEVEL OFF IE UNLOADING, THE A/C NOSE GEAR EXTENDED, NORMAL LANDING. REMOVED AND REPLACED NOSE LANDING GEAR DOWN LOCK ACT, IAW B727-200MM 32-33-011-4, ACFT STILL REQUIRES JACKING FOR OPS CK AND RII. JACKED ACFT AND PERFORMED RETRACTION TEST PER MM32-33-000-5. NO DEFECTS FOUND. NO LEAKS FOUND. OK FOR SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

FOUND FRAME BS 783 RT FASTENER HOLE CRACKED. REPAIR PER EO 7-5310-7-3367 PART 9. REPAIRED FRAME BS 783 RT PER EO 7-5310-7-3367 PART 9.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,108 hrs · 33,602 cycles

CORROSION ON FLOORBEAM, STA 760, LBL 66, WL 206. *S/D* CORROSION OUT OF LIMITS. REMOVED STUB FLOORBEAM BS 760 LT SIDE. DRILLED UP & INSTALLED NEW STUB FLOORBEAM WL 200 PER SRM 51-30-2, 51-30-5, 53-10-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,108 hrs · 33,602 cycles

CORROSION ON FLOORBEAM STRAP AT BS 950, LBL 9, WL 138.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,108 hrs · 33,602 cycles

CORROSION ON FLOORBEAM AT BS 950, RBL 27.5, WL 208 UPPER FLANGE.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

FWD CARGO BAY STA 680 FRAME DENTED STR 25 LT.

Part: STRUCTURE — CORRODED (CTR FUEL TANK) · airframe 52,108 hrs · 33,602 cycles

CORROSION AT LOWER SURFACE OF CTR FUEL TANK, BS 830, RBL 26, WL 160, JUST ABOVE RT PRIMARY HEAT EXCHANGER. CORROSION AT LOWER SURFACE OF CENTER FUEL TANK - BS 830, RBL 26, WL 160 ABOVE PRIMARY HEAT EXCHANGERS FOUND TO BE OUT OF LIMITS PER SRM 57-30-1. REPAIRED AREA PER SRM 57-30-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,108 hrs · 33,602 cycles

CORROSION ON FLOORBEAM AT BS 950 RBL 27.5 WL 208 UPPER FLANGE. REMOVED CORROSION ON FLOORBEAM IAW SRM 51-10-6 AND FED EX EA 7-5310-55308.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,108 hrs · 33,602 cycles

CORROSION (C53-224-04) ON FLOORBEAM AROUND NUT PLATE HOLES BS 1130, LBL 27 - LBL 43, WL 207. CORROSION OUT OF LIMITS. REPAIRED 1130 FLOORBEAM UPPER CHORD LBL 27-43 WL 207 IAW SRM 53-10-8 FIG 10.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

SIDE FRAME DENTED BS 460 RBL 65 STR 16R. FOUND DENT IN 460 FRAME, STR 16R TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3 AND FED EX EA 7-5310-70665A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

WHILE CLOSING MAIN CARGO FLOOR PANELS FOUND BS 1070, LBL 25 TO RBL 60, WL 200 LOWER FLOORBEAM FWD SIDE CORRODED. REPAIRED FLOOR BEAM BS 1070 PER FED EX EA 7-5310-55306.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

BS 990 FRAME LT PREVIOUS REPAIR CRACKED ON BOTTOM. FOUND DAMAGE TO BS 990 FRAME, STR 24 LT TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED AREA PER SRM 51-40-3 AND FED EX EA 7-5310-55307.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

FWD CARGO COMPARTMENT STA 520 WL 150 RBL 21 STR 26R STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP BS 520, WL 150, RBL 21, STR 26R. REMOVED DAMAGE 1 X 5 INCH FROM EDGE OF CLIP. ALODINED AND PRIMED BARE METAL IAW SRM 51-30-2, 51-10-01, 51-10-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,108 hrs · 33,602 cycles

WHILE CLOSING MAIN CARGO FLOOR PANELS FOUND BS 970 LBL 12 WL 200 LOWER FLOORBEAM CORRODED. CORROSION OUT OF LIMITS. REMOVED CORRODED FLOORBEAM LOWER CHORD 1 X 4.25 INCHES. FABRICATED & INSTALLED REPAIR ANGLES (2 EA) & FILLER, AND RESTORED ALL ACCESS PER SRM 53-10-1, 53-10-8 FIG 8.

Part: FAILSAFE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,108 hrs · 33,602 cycles

CORROSION (C53-224-01, 2) ON FRAME, STA 760, RBL 70, WL 207. FOUND CORROSION ON FRAME FAIL SAFE STRAP AT BS 760 RBL 70, WL 207 TO BE OUT OF LIMITS PER SRM 53-10-2. REMOVED DAMAGED SECTION OF FAIL SAFE STRAP. FABRICATED REPAIR SECTION OF STRAP AND DOUBLER PER SRM 51-10-4 FIGURE 1 AND INSTALLED PER SRM 51-30-2.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

FWD CARGO COMPARTMENT STA 560 WL 155 LBL 35 FLOOR FRAME DENTED. CUT OUT DAMAGE IN FRAME AT BS STA 560 WL 155 LBL 35 AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,108 hrs · 33,602 cycles

CORROSION (C53-224-01, 3) FLOORBEAM STA 1130 LWR CHORD FWD FLANGE UPPER SURFACES CORRODED LBL 1-45 WL 200 AROUND NUT PLATE. REMOVED CORROSION ON 1130 FLOORBEAM, LOWER CHORD, FWD FLANGE UPPER AND LOWER SURFACES LBL 1 - LBL 45, WL 200 AROUND FASTENER HOLES. ORIGINAL THICKNESS .163 INCH. REMAINING THICKNESS AFTER CORROSION REMOVAL FOUND TO BE .116 INCH AT LBL 16.5, .103 INCH AT LBL 19.5 AND .138 INCH AT LBL 34.5. FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1. REPLACED LOWER CHORD OF BS 1130 FLOORBEAM IAW EA 7-5310-55302.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

CORROSION (C53-224-01) FLOORBEAM UPPER FLANGE LWR SURFACE IS GOUGED AND CORROSION STA 400 LBL 2-8 WL 208. REPAIRED FLOORBEAM AT BS 400, LBL 2-8, WL 208 IAW SRM 53-10-8 FIG 3, 51-40-3, 51-10-3, FED EX MM 51-20-000-7, 51-20-021-7, SRM 51-30-2. ORIGINAL MATERIAL THICKNESS = .125 INCH. DEPTH OF DAMAGE = .080 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

FWD CARGO COMPARTMENT STA 520, WL 163, LBL 39 FRAME DENTED. REMOVED DAMAGE ON FRAME B.S. 520, WL 163, LBL 39 IN A 1 1/2 X 17 1/2 AREA. FABRICATED REPAIR DOUBLER USING 7075-T6 .050 LOT 553781. ALODINED, PRIMED AND INSTALLED IAW 727 SRM 51-30-2, 51-40-3 SH3 AND EA 7-5310-70665.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,108 hrs · 33,602 cycles

CORROSION (C53-224-01,3) FLOORBEAM STA 1110 WL 208 CORRODED UPPER CHORD. REMOVED CORROSION FROM BS 1110 FLOOR BEAM, FOUND TO BE OUT OF LIMITS PER SRM 53- 10-1. ACCESSED AREA, REPLACED UPPER CHORD PER FED EX EA 7-5310-77727, RESTORED ACCESS PER SRM 51-30-2 AND SOPM 20-50-1.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

CRACKED STRINGER CLIP, STA 950C, STRINGER 3L. REMOVED AND REPLACED STRINGER CLIP AT STA 950C, STR 3L IAW SRM 51-30-2.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

FRAME UPPER CHORD DENTED BS 1010, RBL 30 ABOVE STR 26R. CUT OUT DAMAGED AREA OF FRAME AT BS 1010, RBL 30 ABOVE STR 26R IN 1.75 X 1.5 DIAMETER AREA. FABRIATED TYPICAL FORMED SECTION REPAIR. ALODINED, PRIMERED AND INSTALLED IAW SRM 51-40-3 FIGURE 1, SRM 51-10-2 AND SRM 51-30-2.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

STA 600 FRAME DENTED BETWEEN STR 24 LT & 25 LT IN FWD CARGO BAY. FRAME AT BS 600 BETWEEN STR 24 LT & 25 LT IN FWD CARGO BAY DENT FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIR FRAME PER SRM 51-40-3 AND FED EX EA 7-5310-70665.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

FWD CARGO STA 680 FRAME DENTED AT STR 24 RT. CUT OUT DAMAGE ON FRAME INNER CHORD BS 680, STR 24 RT. DRILLED UP REPAIR DOUBLER AND INSTALLED PER SRM 51-40-3 FIG 1 AND FED EX EA 7-5310-70665.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

FWD CARGO COMPARTMENT STA 580, WL 155, LBL 35 FLOOR FRAME DENTED. FWD CARGO COMPARTMENT STA 580, WL 155, LBL 35 FRAME DENTED OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3 AND FED EX EA 7-5310-70665.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

FWD CARGO BAY STA 660 FRAME DENTED AT STR 24 LT. REPAIRED DENTED FRAME AT FWD CARGO BAY STA 660, STR 24L IAW EA 7-5310-70665 AND SRM 51-40-3.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

STRINGER CLIP CRACKED STA 950A STR 6R. REMOVED AND REPLACED STRINGER CLIP AT BS 950A, STR 6R IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,108 hrs · 33,602 cycles

FLOORBEAM TOP TEE CORRODED STA 1030 LBL 25 - RBL 25 WL 208. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED DAMGE AREA PER SRM 53-10-8.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

FWD CARGO STA 660 FRAME DENTED AT STR 24 RT. TRIMMED OUT DENT DAMAGE FROM FLANGE ON FRAME STA 660, STR 24R, LOCATED AND DRILLED FASTENER HOLES IN REPAIR DOUBLER PER SRM 51-40-3 PG 1-6 AND EA 7-5310-70665. ALODINED, PRIMERED AND INSTALLED FASTENERS PER SRM 51-20-1 AND 51-30-2. APPLIED BMS3-29 TO REPAIR AREA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,108 hrs · 33,602 cycles

CORROSION (C53-224-01), ON FLOORBEAM LWR FLANGE STA 600 RBL 49 TO 60 WL 201. REMOVED CORROSION ON LOWER FLANGE FLOORBEAM CHORD AT BS 600, RBL 49-60, WL 201. FOUND TO BE OUT OF LIMITS. ACCESSED AREA AND CUT LOWER CHORD FROM RBL 35 TO END OF FLOORBEAM. FABRICATED LOWER CHORD, (2) SUPPORT ANGLES, (2) REINFORCEMENT STRAPS, (4) SHIMS. ALODINED AND PRIMERED. INSTALLED ALL REPAIR PARTS AND FASTENERS THAT WERE REMOVED FOR ACCESS IAW SRM 53-10-1, 51-10-6, 53-10-8, 51-30-2 AND FED EX M/M 51-20-151-7.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

CRACKED STRINGER CLIP, STA 950C, STRINGER 3R. REMOVED AND REPLACED STRINGER CLIP AT STA 950C, STR 3R IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,108 hrs · 33,602 cycles

CORROSION (C53-224-01), ON FLOORBEAM BS 344 LBL 33 TO 60 WL 208 AROUND NUT PLATE HOLES. REMOVED CORROSION ON FLOORBEAM, BS 344. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1. REMOVED AND REPLACED FLOORBEAM UPPER CHORD BS 344, RBL 65 - LBL 65, WL 208. ALL WORK DONE PER SRM 53-10-8 FIG 9, 51-10-2, 51-30-2, 51-30-5, 51-30-8.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

CRACKED STRINGER CLIP, STA 950D, STRINGER 6R. REMOVED AND REPLACED STRINGER CLIP AT BS 950D, STR 6R IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

CORROSION (C53-224-01) ON FLOORBEAM UPPER SURFACE BS 380 RBL 25 TO 35 WL 208. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA RBL 25.75 TO 27.75 AND RBL 46 TO 48 AT BS 380, WL 208. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS, BOTH LOCATIONS, IAW SRM 53-10-1 AND 53-10-8 FIG 8.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,108 hrs · 33,602 cycles

FWD CARGO STR 26 RT STA 720B CORRODED. REMOVED DAMAGE AREA OF STRINGER AND STIN AT BS 720B. FABRICATED AND INSTALLED REPAIRS IAW SRM 53-30-3, 53-10-3.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,108 hrs · 33,602 cycles

CORROSION (C53-111-01, 2) FWD CARGO BAY SHEAR TIE ON FRAME 720 STR 26 LT IS CORRODED. REMOVED CORROSION ON SHEAR TIE ON FRAME STA 720, STR 26 LT, FWD CARGO BAY. REMOVED .017 3 X 1 INCH FROM .050, OUT OF LIMITS. REMOVED DAMAGED SHEAR TIE, LOCATED, DRILLED, INSTALLED NEW SHEAR TIE IAW SRM 53-10-1, 51-10-6, 51-30-02, FED EX MM 51-20-021-7, 51-20-151-7.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,108 hrs · 33,602 cycles

CORROSION ON STRINGER 27R BS 955. REMOVED AND REPLACED STR 27 RT IN ACCORDANCE WITH FED EX E.A #7-5310-55318.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,108 hrs · 33,602 cycles

FWD CARGO STA 629 FRAME DENTED LBL 6 STR 28. CUT OUT DAMAGED PORTION OF FRAME AT BS 720 LBL 6 STR 28 AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3.

Part: ACTUATOR — MALFUNCTIONED (NLG) · airframe 51,607 hrs · 33,296 cycles

NOSE GEAR DID NOT EXTEND ON 1ST TRY. RECYCLED GEAR AND IT CAME DOWN. JACKED NOSE GEAR PER 727-200 MM 07-11-000-2. REMOVED AND REPLACED NOSE GEAR ACTUATOR PER 727-200 MM 32-33-001-4. LUBRICATED ALL GEAR COMPONENTS. REMOVED AND REPLACED LANDING GEAR ACC WARNING UNIT. PERFORMED NOSE GEAR EXTENSION AND RETRACTION PER 727-200 MM 32-33-000-5. GROUND OPS CHECKS NORMAL. LEAK CHECKS GOOD. REMOVED MAIN GEAR PINS AND TAIL SKID. RETURNED A/C TO SERVICE.

Part: HOSE — LEAKING (NR 3 PYLON) · airframe 50,707 hrs · 32,808 cycles

APPROX 5 MIN AFTER TAKEOFF PASSING THROUGH 1000 FT, ENG. 3 STRUT LT ILLUMINATED. LT EXTINGUISHED ON ITS OWN BEFORE ANY QRH ITEMS WERE ACCOMPLISHED. FOLLOWED QRH TESTED SYSTEM-GOOD AND MONITORED. PARAMETERS: A/C WEIGHT 180.0 TAT +12 EPR 1.90,1.95,1.90 N1 95%. REMOVED NR 3 STRUT LOWER PANELS AND INSPECTED DETECTOR LOOP CKD GOOD. RAN ENGINE AND FOUND A PNEUMATIC FLEX LINE LEAKING WITH TELL TAILS HEADING TOWARDS HEAT DETECTOR. THIS WAS A REPEAT ITEM, NO ANOMALY HERE ! R & R T/R FLEX LINE PER SMP. RAN #3 ENGINE PER JRH NO MORE LEAKS FOUND.

Part: WARNING LIGHT — ILLUMINATED (WING/BODY OVHT) · airframe 50,683 hrs · 32,794 cycles

ON CLIMB OUT OF MAO APPROX 5,000 FT. NR 3 STRUT OVERHEAT LIGHT CAME ON. UPON RETARDING POWER APPROX. .20 EPR LIGHT WENT OUT. AFTER COMPLYING WITH QRH PROCEDURES, POWER WAS RESTORED TO NORMAL WITH NO FURTHER INDICATIONS. BASED ON CREW REPORT, AND VERBAL DEBRIEF UPON ARRIVAL IN MIA, AFTER THE ENGINE PWR WAS REDUCED AND THE LIGHT EXTING,THE PILOT RESTORED THE POWER SETTING TO NORM, AND THE STRUT OVERHEAT LIGHT STAYED OUT THE REMAINDER OF THE FLT, AFTER 5 HOURS NO REPEAT, I'LL TAKE AS AN ANOMALLY. RAN ENG AND PER JET RUN HANDBOOK, NO FAULTS NOTED,CHECKED SYSTEM IAW M/M 26-12-011-5 AND 26-14-001-2 ALL CHECKED OK. A/C OK FOR SERVICE.

Part: BRAKE — FIRE (MLG)

BRAKE FIRE ON NR 3 AND 4 RED. REMOVED AND REPLACED 3 & 4 BRACKET, AND MAIN WHEEL ASSY PER AMM 32-45-001-4, 32-42-001-5.

Part: ACCESSORY UNIT — FAILED (E/E BAY)

ATTEMPT TO RAISE GEAR LEVER, WOULD NOT GO BEYOND OFF POS. COMPLIED WITH CKLIST WITH NEGATIVE RESULTS. REPLACED LG ELECTRONIC MODULE PER MM 32-09-21-4. PERFORMED CONTROL HANDLE LOCK SYS TEST PER MM 32-31-011-5. SYS CK OK.

Part: DOOR — DAMAGED (L1 DOOR)

FWD ENTRY DOOR LIGHT ILLUM AT 18,000. LOUD BANG AT 3000 ON DEP I FRONT AREA OF A/C. *S/D* REMOVED AND REPLACED FWD ENTRY DOOR PER 727-200 MM 52-11-00-4. PERF RIG ADJUSTMENT TEST PER B727-200 MM 52-11-001-5. INSTALL DOOR LINER PER MM 52-11-001-5. REINSTALL ESCAPE SLIDE PER MM 25-60-015-2 AND PERF DOOR WARNING CHECK.

Part: CYLINDER — FAILED (HYD TRANSFER)

NOSE GEAR FAILED TO EXTEND NORMALLY ON FIRST ATTEMPT. OK WHEN CYCLED UP TO DOWN- REPEAT WRITE-UP. *S/D* REMOVED AND REPLACED NOSE GEAR HYDRAULIC TRANSFER CYLINDER AS PER MM 32-35-011-4. JACK AND LWR NOSE PER MM 07-11-000-2. ACCOMP EXT AND RETRACT PER 32-33-000-5, 32-61-001-5. CHECK OK.

Part: ACCESSORY UNIT — MALFUNCTIONED (E/E BAY)

NOSE GEAR UNSAFE. RECYCLE TWICE TO GET ALL DOWN. *S/D* REMOVED AND REPLACED PER MM 32-09-122-5, 32-33-000-5. JACKED AND LWR A/C PER MM 07-11-000-2.

Part: CONTROLLER — CONTAMINATED (DETECTION SYS)

ON T/O BOTH FIRE WARN BELL CUTOUT LIGHT ON GLARESHIELD CAME ON DIM. FOUND WATER LEAKING DOWN BEHIND FIRE WARN DETECTOR ONTO WIRING TERMINALS. NO WATER ON ANY BLACK BOXES. REMOVED AND REPLACED APU FIRE AND OVERHEAT DETECTOR PWR UNIT PER MM 26-15-0. CLEANED AND DRIED PLUG PER GENERAL MAINTENANCE PRACTICES.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE)

CABIN ALTITUDE CLIMBING THRU FL 180 WITH POSITIVE DIFFERENTIAL PRESSURE. COULD NOT DUPLICATE. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER PRECAUTIONARY MM 21-31-010-4 & MM 21-31-0. CHECK GOOD FOR SERVICE AT THIS TIME.

Part: PANEL — CORRODED (FUSELAGE) · airframe 46,961 hrs · 30,681 cycles

TRANSITION PANEL CORRODED ABOVE STR 26 RT AT BS 1030. REMOVED DAMAGE. FAB REPAIR IAW SRM 51-40-2. INSTALL IAW SRM 5 1-30-2.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 46,961 hrs · 30,681 cycles

HEAVY CORROSION ON FLOOR SUPPORT IN FWD BAG BIN BS 643, LBL 10 & LBL 14. CUT OUT DAMAGED AREA. FAB & INSTALL REPAI R ANGLES IAW SRM 51-40-4.

Part: CAP — CRACKED (NR 5 SLAT) · airframe 46,961 hrs · 30,681 cycles

NR 5 LEADING EDGE SLAT I/B END CRACKED. REMOVED AND REPLACED I/B END CAP ON NR 5 SLAT IAW SRM 51-30-2.

Part: ANGLE — CORRODED (CARGO BAY) · airframe 46,961 hrs · 30,681 cycles

FWD BAG BIN CENTER FLOOR PANEL RT SUPPORT CORRODED BS 643. R&R FAB IAW SRM 51-40-4.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 46,961 hrs · 30,681 cycles

MODERATE TO HEAVY CORROSION INSIDE OF DELTA KEEL BEAM ON ATTACH FITTINGS, LT & RT CHORDS, AND LOWER WEB. REMOVED FAB & INSTALL NEW ATTACH ANGLEA AT STA 750-840 IAW SRM 51-10-1 & SRM 51-30-2.

Part: WEB — CRACKED (FUSELAGE) · airframe 46,961 hrs · 30,681 cycles

AIRSTAIR AREA, RT SIDE WEB CRACKED AT LIGHTENING HOLE AT BS 1240. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-2 & SRM 51-30-2.

Part: WEB — CRACKED (AIRSTAIR) · airframe 46,961 hrs · 30,681 cycles

AIRSTAIR AREA, LT SIDE WEB CRACKED AT LIGHTENING HOLE AT BS 1260. STOP DRILLED CRACK, FABRICATED AND INSTALL REPAIR IAW SRM 51-40-2 & 51-30-2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,961 hrs · 30,681 cycles

FUSELAGE SKIN CRACKED AT FORWARD ENTRY DOOR LOWER HINGE CUTOUT.

Part: FITTING — CRACKED (LT MLG DOOR) · airframe 46,961 hrs · 30,681 cycles

LT MLG DOOR RIB FITTING CRACKED ABOVE THE ACTUATOR POINT. R&R LT MAIN LG DOOR IAW MM 32-12-1.

Part: WINDSHIELD — CRACKED (LT COCKPIT)

99-158 - DURING CLB L1 WIND STARTED ARCING AND A CRACK DEVELOPED. REMOVED AND REPLACED L1 WINDSHIELD AS PER MM 56/11/011/04 AND WINDOW HEAT CONTROL UNIT AS PER MM 30/41/042/5. OP CK GOOD.

Part: INDICATOR — ERRATIC (NR 2 EGT)

NR 2 ENGINE EGT GAUGE ERRATIC IN CRUISE, READ BETWEEN 350-100. SHUT DOWN NR 2 ENG. REMOVED AND REPLACED EGT IND PER MM 77-21-02, RAN UP ENGINE, FOUND OK.

Part: CADC — FAILED (NR 1)

99-105 - CAPT AIRSPEED, ALTIMETER AND VSI INSTR MALFUNCTION AFT T/O. REMOVED AND REPLACED NR 1 CADC AS PER MM 34-12-011-4, SYS OK FOR SERVICE.

Part: FIRE LOOP — FAILED (NR 1 ENGINE)

NR 1 ENG FIRE LIGHT AND BELL ON, SHUT DOWN ENGINE LIGHT AND BELL OUT. REPLACED NR 1 LOWER FIRE DETECTION ELEMENT.

Part: CAP — LOOSE (NR 1 ENGINE)

ALL POWER LEVERS AT IDLE, NR 1 ENG FIRE LIGHT ON, REMAINED OUT WITH NR 1 AT IDLE. INSPECTED ALL PNEUMATIC PLUMBING AND DUCTING, AIR LEAKAGE ON SURROUNDING SURFACES, TIGHTENED AND RESAFTIED CAP. CHECKS SATISFACTORILY.

Part: SHUTOFF VALVE — INOPERATIVE (NR 3 BLEED AIR)

REPEAT WRITE-UP FROM DISCREPANCY NR 01199454 ENGINE NR 3 STRUT OVERHEAT LIGHT ON. OVERHEAT LIGHT CAME ON PASSING FLIGHT LEVEL 250 AND APPROXIMATELY 20 MINUTES INTO FLIGHT. BOTH PACKS ON NR 1 BLEED OFF, NR 2 OPEN NR 3 OPEN CLIMB POWER WITHIN PARAMETERS. ADMINISTERED RED TABS CHECKLIST AND THE LIGHT WENT OUT. CONTINUED FLIGHT ON ONE PACK FOR REST OF FLIGHT. PULLED NR 3 STRUT PANELS AND RAN ENGINE TO CHECK FOR BLEED LEAKS. NO LEAKS FOUND BUT NR 3 BLEED AIR SHUTOFF VALVE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED NR 3 SHUTOFF VALVE AND OPERATIONAL CHECKED AND LEAK CHECKED NORMAL. RAN NR 3 ENGINE AT HIGH POWER AND STRUT OVERHEAT CHECKS NORMAL. REINSTALLED PANELS, OK FOR SERVICE.

Part: SPLICE — CORRODED (BS 720)

NR 0789 70C079-00, BS 720D - 720E, STR 21R IN SNAKE PIT AREA CORRODED. CUTOUT CORRODED AREA AND INSTALLED STR SPLICE PER SRM 53-10-3, PAGE 3.

Part: BEAM — CORRODED (BS 743)

A/C BAY, BS 743, RBL 8 HEAVY CORROSION ABOVE DELTA BEAM, LWR SURFACE OF PLATE AT FWD ROW OF FASTENERS. REMOVED CORROSION, TREATED, INSTALLED DOUBLER PER SRM 51-40-02 OVER DAMAGED AREA.

Part: SKIN — CORRODED (BS 660)

FUSE SKIN CORRODED AT BS 660 BETWEEN STR 28L TO W8R. REMOVED CORROSION. REMOVED SECTION OF FUSE SKIN I/B OF STR 28R. INSTALLED REPAIR DOUBLER PER SRM 53-30-3.

Part: BEAM — CORRODED (BS 750)

A/C BAY CORROSION ABOVE DELTA BEAM BS 750, RBL 6, AROUND ACCESS PLATE 3210. REMOVED CORROSION, TREATED, INSTALLED DOUBLER OVER AREA PER SRM 51-40-2.

Part: FRAME — DENTED (BS 540)

UPPER LOBE BS 540, RBL 65, BELL FRAME DENTED. REMOVED DAMAGED AREA OF BELL FRAME. INSTALLED DOUBLER PER EA 7531028295 AND SRM 53-40-30.

Part: FRAME — DENTED (BS 600)

UPPER LOBE, BS 600, RBL 65 BELL FRAME DENTED. REMOVED DAMAGED AREA OF BELL FRAME. INSTALLED DOUBLER PER EA 7531028295 AND SRM 53-40-3.

Part: FRAME — DENTED (BS 580)

UPPER LOBE BS 580, RBL 65 BELL FRAME DENTED. REMOVED DAMAGED AREA OF BELL FRAME. INSTALLED DOUBLER PER EA 7531028295 AND SRM 53-40-3.

Part: BEAM — CORRODED (BS 743)

A/C BAY, BS 743 CHORD ABOVE DELTA BEAM, UPPER SURFACE CORRODED LBL - RBL 12. REMOVED CHORD ANGLE AND REINSTALLED WITH NEW CHORD ANGLE PER SRM 51-30-2.

Part: FRAME — DENTED (BS 500)

UPPER LOBE BELTFRAME AT BS 500, RBL 65 DENTED OUT OF LIMITS PER EA 7531028295. REMOVED DAMAGE AT BELTFRAME BS 500, RBL 65 AND INSTALLED DOUBLER PER SRM 51-40-3 PG 1-6 AND EA 7531028295.

Part: FRAME — DENTED (BS 520)

UPPER LOBE, BELTFRAME AT BS 520, RBL 65 DENTED OUT OF LIMITS. REMOVED DAMAGE AT BELTFRAME BS 520, RBL 65 AND INSTALLED DOUBLER AS PER SRM 51-40-3 PG 1-6 AND EA 7531028295.

Part: ENGINE — FOD (NR 2 ENGINE)

ON CLIMBOUT AT ABOUT 4500 FT MSL (3000' AG) A LARGE BIRD FLEW RIGHT OVER COCKPIT AND INTO NR 2 ENGINE. AIRCRAFT HAD BAD VIBRATION, EVEN AT IDLE, SHUTDOWN NR 2 ENGINE. EGT DID NOT EXCEED LIMITS. NUMBER 2 ENGINE REPLACED PER FEDEX B727 ENGINE REPLACEMENT WORK CARD NUMBER 70T0002. ACCOMPLISHED ENGINE OPERATIONAL TEST PER JET RUN HANDBOOK B727 AND ALL WORK PROPERLY.

Part: CHORD — CORRODED (BS 1070)

CORROSION BS 1070, WL 201, LBL 45 - RBL 45 ON LOWER CHORD. *S/D* REPAIRED LOWER CHORD BS 1070, WL 201, LBL 45 - RBL 45 IAW FED-EX EA NR 7-5310-37461.

Part: CHORD — CORRODED (BS 1148)

CORROSION FOUND ON LOWER CHORD AT BS 1148, LBL 30 TO RBL 43, WL 201 FLOORBEAM. *S/D* REMOVED CORROSION BS 1148, LBL 30 TO RBL 43, WL 201. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-01. FABRICATED REPAIR PARTS, ALODINED AND PRIMED PARTS. INSTALLED ALL REPAIR PARTS PER FED-EX EA NR 7-5310-37464.

Part: CHORD — CORRODED (BS 1130)

NR 0025 006 CORROSION ON LOWER CHORD BS 1130, WL 201, LBL 25 TO RBL 25. REPAIRED LOWER CHORD AT BS 1130, WL 201, LBL 62 TO RBL 62. ALL WORK DONE IAW FED-EX EA NR 7-5310-37462.

Part: STRINGER — CRACKED (BS 1243)

NR 0029 003 WHILE WORKING 7-5450-7-3301L PT 11 FOUND CRACK IN STRINGER 14L AT BS 1243. REPAIRED STR 14L, BS 1233 TO BS 1253 IAW FED-EX SRM 53-10-3, 53-10-4.

Part: CHORD — CORRODED (BS 1050)

NR 0021 002, CORROSION LOWER CHORD BS 1050, WL 201, RBL 15. REMOVED DAMAGED AREA BS 1050, WL 201, RBL 13. FABRICATED REPAIR PARTS, ALODINED AND PRIMED. INSTALLED REPAIR PARTS PER FED-EX SRM 53-10-08 FIG 8.

Part: CHORD — CORRODED (BS 1030)

CORROSION UPPER CHORD BS 1030, WL 208, LBL 11 TO 21. *S/D* REMOVED CORROSION BS 1030, WL 208, LBL 11 TO 21. FOUND TO BE IN LIMITS PER FED-EX SRM 53-10-01. ALODINED AND PRIMED ALL EFFECTED AREA.

Part: FLOORBEAM — CORRODED (BS 1010)

NR 0023 001, CORROSION LOWER CHORD BS 1010, WL 201, LBL 24 TO 36. REMOVED CORROSION ON LOWER CHORD, BS 1010, WL 201, LBL 1 TO 45.5. REMOVED LOWER FLANGE OF LOWER CHORD. FABRICATED REPAIR PARTS AND INSTALLED IAW FED-EX SRM 53-10-8 FIG 2.

Part: INDICATOR — MALFUNCTIONED (TE FLAPS)

DURING TAKEOFF RETRACTING FLAPS FROM 15 DEGREES TO 5 DEGREES, OUTBOARD FLAPS LEFT AND RIGHT NEEDLES SPLIT BY 2 NEEDLE WIDTHS AND OUTBOARD FLAP INDICATOR STOPPED MOVING. COMPLIED WITH ASYMMETRICAL FLAP CHECKLIST. REPLACED OUTBOARD FLAP POSITION INDICATOR. CHECKED AND CLEANED LEFT OUTBOARD POSITION TRANSMITTER PLUG. FARED FLAPS WITH A HYD SYS AND SAFTIED ALTERNATE FLAP SWITCH OFF. PERFORMED SEVERAL FLAP CYCLES USING STANDARD PROCEDURE. OPS CK GOOD. NO DEFECT NOTED.

Part: OIL BYPASS SW — FAILED (NR 1 ENGINE)

NR 1 OIL BYPASS LIGHT ON IN FLT, OIL PRESS 50, TEMP 90, 3.5 GAL, ALL OK. IT STAYED ON AT IDLE PWR, SHUTDOWN NR 1. A/C RELEASED FOR SERVICE PER MEL 79-2 CAT B EXP 29JUL96. *S/D* REMOVED AND REPLACED NR 1 OIL BYPASS SWITCH. RAN AND OPS CHECK GOOD.

Part: STRINGER — CORRODED (BS 480-720)

CORROSION INSIDE UPPER LOBE AT STR 14R FROM STA 480 TO 720E AT SKIN LAP. REMOVED CORROSION OUT OF LIMITS, INSTALLED DOUBLER PER SRM 53-30-3 FIG 5.

Part: STRINGER — CRACKED (BS 640)

STA 640 STR 3R CRACKED IN RADIUS. REPAIRED STR PER SRM 53-10-3 FIG 3.

Part: SKIN — CORRODED (BS 680-685)

CORROSION BETWEEN SKIN LAP FROM STA 680 TO 685 AT STR 14R. CUT OUT CORRODED SKIN BEHIND LAPPED SKIN AND INSTALLED REPAIR PER SRM 53-30-03.

Part: FLOOR BEAM — CORRODED (BS 344)

MAIN CARGO STA 344 FLOOR BEAM UPPER CHORD CORRODED WL 208 FROM RBL 23 TO LBL 65. REMOVED DAMAGED SECTION OF UPPER CHORD. INSTALLED NEW UPPER CHORD SECTION, RBL 23 TO LBL 65, PER STANDARD REPAIR DRAWING NR SR 27-53-007, DATED 03-15-94.

Part: FRAME — CORRODED (BS 227.8)

NR0704, FRAME CORRODED AT STA 227.8 BELOW F/O'S SLIDING WINDOW NEAR FLOOR. *S/D* REMOVED AND REPLACED STA 227.8 RT FRAME WEB SRM 51-10-1.

Part: INTERCOSTAL — CORRODED (BS 259.5-277)

NR0710, FLT DECK FLOOR SUPPORT INTERCOSTAL CORRODED ON TOP SURFACE FROM STA 259.5 TO 277 LBL 18.

Part: FLOOR BEAM — CORRODED (BS 268)

NR0708, FLOOR BEAM BELOW F/E'S SEAT AFT TRACK CORRODED ON TOP SURFACE STA 268 LBL 5. *S/D* REMOVED CORROSION PER SRM 51-10-06, INSTALLED DOUBLER PER ESO 11782 AND EA 7-5300-28617.

Part: CHANNEL — GOUGED (BS 640)

NR0168, UPPER LOBE STA 640 STR 3R, 2 DEEP GOUGES IN CHANNEL AND FLANGE CUT. *S/D* INSTALLED STR REPAIR PER SRM 53-10-3.

Part: STRINGER — CRACKED (BS 430-450)

STR 3R CRACKED AND GOUGED BETWEEN STA 420 TO 440. *S/D* REPLACED STR FROM STA 430 TO 450 PER SRM 53-10-3.

Part: SKIN — CORRODED (BS 1160)

NR0198, SKIN BULGED FWD LWR CORNER OF AFT LAV SERVICE PANEL STA 1160 STR 22L. *S/D* REMOVED RIVETS AS MARKED PER SRM 51-30-2, NO EVIDENCE OF CORROSION. INSTALLED FASTENERS PER SRM 51-30-2.

Part: DNLOCK BUSHING — WORN (NLG)

LANDING AT MEM, PUT DOWN GEAR; MAINS GOOD BUT NOSE GEAR KEPT RED LIGHT AND NO GREEN LIGHT. RECYCLED GEAR, GOT GREEN MAINS AGAIN, AND RED NOSE GEAR LIGHT. ON GO AROUND, NOSE GEAR AND LIGHTS WENT GREEN APPROX 1 MINUTE AFTER RECYCLED GEAR. REPLACED BUSHING ON NOSE LANDING GEAR DOWNLOCK SWITCH. LUBED NOSE LANDING GEAR DOWNLOCK. CYCLED NOSE LANDING GEAR SEVERAL TIMES, OPS CHECK GOOD IAW MM 32-61-01.

Part: TRANSMITTER — FAILED (LT TE FLAP)

DURING FLAP RETRACTION ON T/O O/B FLAPS SHOWED AS ASYMMETRICAL. O/B FLAPS WERE LOCKED OUT. COMPLIED WITH EMERGENCY PROCEDURES AND RETURNED TO AIRPORT. LANDED WITH NO OTHER PROBLEMS. REPLACED LEFT O/B FLAP POSITION TRANSMITTER ASYMMETRICAL. CHECKS OK PER MM 27-52-13.

Part: SPRING — FROZEN (TE FLAPS)

AFTER TAKEOFF UPON FLAP RETRACTION, ASYMMETRIC OUTBOARD FLAPS, FLAPS IND DOESN'T MATCH DETENT, FLAP HANDLE IS DIFFICULT TO MOVE FROM 0 TO 2 DEGREES. FOUND LT OTBD FLAP TRANSMITTER RETRACT SPRING STIFF FROM COLD - FREED SPRING WITH HEAT - OPS CKS GOOD NOW.