N219FE

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 54,431 hrs · 30,381 cycles

AFT PIT ALONG LEFT SIDE OF S-29L FROM STA 950F-970 HAS SURFACE CORROSION REMOVED FLOOR SUPPORT FOR ACCESS IAW SRM 51-30-2. REMOVED CORROSION IAW SRM 51-10-6. AREA FOUND WITHIN LIMITS FOR STRAP REPAIR IAW SRM 27-53-023. FABBED STRAP IAW SR 27-53-023, MATERIAL USED TO MAKE STRAP IS 7075-T6-.071, BATCH NR 1119665. LOCATED AND DRILLED IAW SRM 51-30-5. TREATED AND PRIMED AREA IAW SRM 51-10-2. INSTALLED STRAP IAW SR 27-53-023.

Part: STRINGER — CORRODED (BS 600) · airframe 54,431 hrs · 30,381 cycles

FWD PIT 3" FWD OF STA 600, STR 27L EXFOLIATED REPAIRED STR 27L AT STA 600 IAW SRM 53-10-3 PG4 FIG1 SHEET 2,TABLE I.

Part: CARGO — LEAKING (CARGO BAY) · airframe 53,449 hrs · 29,665 cycles

FUMES IN COCKPIT STRONG ODOR, EMERGENCY EVACUATED ON TAXIWAY. DEPLOYED SLIDE. HAZMAT TEAM DETERMINED THE FUMES AND ODOR WERE COMING FROM THE HAZMAT CAN. HAZMAT TEAM DOWNLOADED HAZMAT CAN AND FOUND ONE DRUM LEAKING UN1993 (TERDODECIL MERCAPTANO). CLEANED UP HAZMAT CAN. NO LEAKS FOUND INSIDE A/C OR CARGO AREA. MX INSPECTED A/C THROUGHOUT CARGO AREA, COCKPIT, E/E COMPARTMENT, FWD AND AFT BELLY CARGO BINS AND AFT AIRSTAIR AREA. NO FURTHER FUMES OR SMELL NOTED IN A/C. FOUND NORMAL. OK FOR SERVICE.

Part: WARNING HORN — ACTIVATED (CABIN PRESSURE) · airframe 53,369 hrs · 29,623 cycles

PASSING THRU FL250 CABIN ALTITUDE WARNING HORN CAME ON AND CABIN WAS AT 10,000FT. BOTH PACKS ON, ENGINE BLEED NR 1 AND NR 3 OPEN. NO OTHER ABNORMAL INDICATIONS (OUTFLOW VALVE CLOSED AND ALL DOES CLOSED). EMERGENY DECLARED AND NO FUEL DUMP REQUIRED.

Part: CLAMP — LOOSE (BLEED AIR) · airframe 53,329 hrs · 29,597 cycles

CRUISE POWER SETTING , NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. RAN QRH AND LIGHT WENT OUT GOOD SYST TEST, RETURNED TO KMIA. INSPECTED ALL DUCTS, CLAMPS AND SENSE LINES. FOUND NUMEROUS CLAMPS LOOSE AT NR 1 PRECOOLER AND NR 1 BLEED VALVE. TIGHTEN CLAMPS IAW MM 36-00-001-2. RAN ENG AT IDLE PER JRH NO LEAKS NOTED. FOUND CLAMPS ON NR 1 ENG BLEED VALVE WORN REPLACED SAME, RAN A/C TO HIGH POWER, NO MORE LEAKS NOTED, A/C OK FOR SERVICE. FOUND NR 1 ENG BLEED VALVE CLAMPS WORN REPLACED SAME, RAN A/C AT HIGH POWER NO LEAKS FOUND. CLOSED ALL PANELS ON NR 1 ENG STUB WING.

Part: ACTUATOR — MALFUNCTIONED (NR 1 SLAT) · airframe 52,113 hrs · 28,848 cycles

NR 1 SLAT LED FAILED TO RETRACT AND INDICATING AMBER ON FLAP RETRACTION TO FLAPS 2 IN FLIGHT. REMOVED AND REPLACED NR 1 SLAT ACTUATOR AS PER M/M 27-81-03-4, OP CKS NORM.

Part: OIL COOLER — FAULTY (CSD) · airframe 49,487 hrs · 27,333 cycles

DURING CLIMBOUT NR 1 CSD AND NR 3 CSD OVERHEATED (NR 1 REPEAT), NR 1 WAS 130C & NR 3 125C WITH NR 2 105C (IN LIMITS). IAW QRH NR 1 GEN BREAKER WAS TRIPPED AND WAS STILL OVER 120C AFTER 3 MIN. DISCONNECTED NR 1 CSD. NR 3 GEN WAS TRIPPED AND WAS OVER 120C AFTER 3 MIN. DISCONNECTED NR 3 CSD. NR 2 CSD NEVER WENT ABOVE 110C. INSPECTED NR 01 AND 03 CSD OIL LEVEL AND MAGNETIC FILTERS, FOUND OK. REMOVED AND REPLACED NR 01 & 03 -IN- TEMP SENSORS (IPC 24- 10-02-01ZZ). REMOVED AND REPLACED NR 01 CSD OIL COOLER PER MM 24-10-061-4. RECONNECTED BOTH NR 01 AND 03 CSD'S, RAN THE ENGINES TO TAKEOFF POWER DURING 5 MINUTES PER 727 JRH, SYS WORKED PROPERLY IAW MM 24-10-001-0.

Part: MOTOR — LEAKING (T/E FLAP)

INBOARD FLAP DRIVE HYD MOTOR LEAKING IN LT WHEEL WELL. REMOVED AND REPLACED MOTOR PER 727 200 MM 27-51-062-4. LEAK CHECK GOOD.

Part: RADAR — FAULTY (WEATHER RADAR)

AT 14000 MSL WITH A/C STRAIGHT AND LEVEL RADAR TILT AT +2.5 DEG.R&R RADAR ANTENNA DRIVE UNIT PER AMM 34-41-021-4. R&R RADAR T/R PER AMM 34-41-041-4. TEST NORM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,777 hrs · 26,511 cycles

LWR CARGO COMPT PERF HFEC INSP FOUND 1 CRACK APPROX 1.5 INCH AT BS 600 JUST ABOVE S-20L AT I/B RADIUS SUB FRAME UNDER CARGO DOOR SPOOL FITTING. ** S/D ** R&R & FAB PER FDW DWG 53FX1349. PER SRM 51-10-01 & FDX DFWG 53FX1371.

Part: FRAME — CORRODED (AUX FUEL TANK)

ON THE AFT AUX FUEL TANK THE LOWER, AFT STRAP CORRODED IN MULTIPLE PLACES THE LENGTH OF STRAP ON LOWER FACE. *S/D* REMOVED AND REPLACED PER IAW DRAWING 65-80689 & FEDEX SRM 51-30-2, 51-30-5.

Part: FLOORBEAM — CORRODED (CABIN)

CORROSION (C53-111-01 ,3) AROUND NUT PLATE HOLE, LWR CHORD OF BS 1148 FLOORBEAM, RBL 22, WL 201. *S/D* REMOVED AND REPLACED FEDEX EA 7-5310-52128 & SRM 53-10-8.

Part: FLOORBEAM — MISDRILLED (CABIN)

WHILE INSP NRC 0901 (INT 194) FINAL BAY OFF FOUND DOUBLE DRILLED HOLE AT BS 360, LBL 23, WL 208. *S/D* DAMAGE OUT OF LIMITS IAW FEDEX SRM 53-10-1 AND REPAIRED PER IAW FEDEX SRM 57-10-8 FIG 8.

Part: STRINGER — CRACKED (FUSELAGE)

TWO INCH CRACK IN STRINGER, BS 740, STR 24R, UNDER I/B HAT. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 53-10-3.

Part: SHEAR TIE — CORRODED (FUSELAGE FRAME)

CORROSION (C53-111-01) ON BS 950E, STR 26L SHEAR TIE AND TWO FASTENERS RUSTED OFF. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 51-10-6 PG 5, 51-20-5.

Part: DOOR FRAME — CORRODED (FUSELAGE)

CORROSION (C53-111-02, 2) NR 3 CARGO DOORWAY FWD FRAME AT BS 1090, RBL 33, WL 150. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-10-6, 53-10-1, EA 7-5310-52146.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION (C53-111-01, 3) ON LOWER CHORD BS 1148 FLOORBEAM LBL 1 - 3, 10, 21, 29, WL 200. *S/D* ACCOMPLISHED PER FEDEX EA 7-5310-52128. OUT OF LIMITS PER FEDEX 53-10-1.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION (C53-111-01, 3) ON LOWER CHORD BS 1130 FLOORBEAM, LBL 43 - RBL 50, WL 208. *S/D* REMOVED AND REPLACED PER FEDEX 51-30-2, 51-20-4.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON FLOOR SUPPORT UPPER FLANGE LOWER FWD, AND AFT SIDE AT BS 720A, LBL 10, WL 208. *S/D* REMOVED AND REPLACED CORROSION PER IAW FEDEX SRM 51-10-6, 53-10-1. ALODINED, PRIMED, INSTALLED PARTS AND SEAT TRACK PER IAW FEDEX SRM 53-10-9, 51-20-021, 51-20-151.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION (C53-224-01,3) AROUND NUT PLATE HOLES UPPER CHORD, BS 1030 FLOORBEAM, RBL 21, RBL 28, RBL 35, WL 208. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-8.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION (C53-224-01,1) ON FLOORBEAM BS 344, LBL 38, WL 208. *S/D* REMOVED AND REPLACED CORROSION PER IAW FEDEX SRM 53-10-4, 51-30-2 & SR 27-53-007.

Part: FLOORBEAM — CORRODED (CABIN)

CORROSION (C53-224-01, 1) ON FLOORBEAM AT BS 328, LBL 44, WL 208. *S/D* REMOVED AND REPLACED PER FEDEX DRAWING SR 27-53-017.

Part: KEELBEAM — CRACKED (FUSELAGE)

LT KEEL BEAM IS CRACKED AT BS 873 ON UPPER FLANGE UNDER APU I/B. *S/D* REPAIRED PER FEDEX EA NR 7-5310-52126.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION (C53-224-01, 3) AROUND NUT PLATE HOLES UPPER CHORD BS 1110 FLOORBEAM, RBL 15, LBL 15, LBL 21, LBL 41 - 44, WL 208. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-1, 53-10-8 & FEDEX EA NR 7-5310-52116.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION (C53-224-01, 3) ON UPPER CHORD BS 950D FLOORBEAM RBL 10, 2, LBL 10, 21, WL 208. *S/D* BLENDED CORROSION IAW FEDEX SRM 51-10-6. REMOVED AND REPLACED RBL 10 PER FEDEX SRM 53-10-8.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION (C53-111-01, 3) ON LOWER CHORD BS 1030 FLOORBEAM LBL 10 - 12, 18, 40 RBL 34, WL 200. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-1, 53-10-8.

Part: SKIN — GOUGED (FUSELAGE)

NUMEROUS NICKS AND GOUGES IN SKIN FROM BS 480 - 520 BETWEEN STR 27L AND 26R. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-30-3 FIG 3.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION (C53-111-01, 3) ON LOWER CHORD BS 1070 FLOORBEAM LBL 27 - 43, RBL 40, WL 200. *S/D* REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED NEW REPAIR ANGLES AND FILLERS PER IAW FEDEX SRM 53-10-1 FIG 4 AND FEDEX SRM 53-10-8 FIG 8.

Part: KEELBEAM — CRACKED (FUSELAGE)

RT KEEL BEAM IS CRACKED AT BS 873 ON UPPER FLANGE UNDER APU I/B. *S/D* REPAIRED PER FEDEX EA NR 7-5310-52126.

Part: STRINGER — CRACKED (FUSELAGE)

STRINGER 4 LT IS CRACKED AT BS 640. *S/D* REPAIRED PER FEDEX SRM 53-10-3.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

HDG COMPARATOR LIGHT REPEATEDLY ILLUM. *S/D* REPLACED SPLICES AS PER MM 20-30-12, REPAIRED WIRES AS PER SMP & REPLACED NR 1 & 2 COMPASS RACKS & DIRECTIAL GYROS AS PER MM 34-21-071-4.

Part: AMPLIFIER — INOPERATIVE (NR 1 COMPASS)

DURING CLIMBOUT INOP HEADING FLAGS WERE OBSERVED ON CAPT RMI & FOS HSI. HDG INSTRUMENT COMPARATOR LIGHT ALSO ILLUM. REMOVED AND REPLACED NR 1 COMPASS AMP RACK AS PER SMP AND NR 1 DG AS PER MM 34-21-071-4. PERFORMED OPER TEST OK.

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

WHEN LANDING GEAR EXTENDED, BOTH GROUND AND RED IND LIGHTS WERE PRESENT ON FRONT IND. REMOVED AND REPLACED LANDING GEAR ASSY UNIT AND CLEANED ELECTRICAL CONNECTORS ON THE RACK WITH CONTACT CLEANER MM 32-01-122, TEST OK ON GROUND.

Part: ACCESSORY UNIT — INOP (MLG)

DURING GEAR EXT, 3 GRN LIGHT+3 RED GEAR LIGHT+TAILSKID LIGHT WERE ILLUMINATED. REMOVED AND REPLACED L/G ACCESSORY UNIT PER MM 32-09-122 & TEST OK.

Part: RELAY — INOP (LANDING GEAR)

99-172 LANDING GEAR LEVER FAILED TO RAISE AFTER TAKEOFF. WING ANTI-ICE WAS TESTED AND DID NOT OPEN. REMOVED AND REPLACED R-92 RELAY, OPER CK WAS NORM PER MM 32-31-011-1 THROUGH 5. CLEANED PROXIMITY SWITCHES.

Part: ACCESSORY UNIT — FAILED (LANDING GEAR)

99-180 - LAND GEAR LEVER UNABLE TO RAISE AFT T/O. LAND GEAR LEVER LATCH LIGHTS CIRCUIT BREAKER WAS CK IN. NO CHG. FLAPS RAISED TO 2 AND NO WARN HORN. WING ANTI-ICE TEST AND DID NOT OPEN. NOSE GEAR STEER HANDLE ALIGNMENT MARKS WERE ALIGNED. REMOVED AND REPLACED LAND GEAR ACCESSORY UNIT PER MM 32-09-121. OPS CK GOOD PER MM 32-09-122.

Part: AIR DIST — ODOR (CABIN)

AN ODOR WAS NOTICED IN THE ENTRYWAY. INSPECTED UPPER DECK AREA, E & E COMP, LWR CARGO AREAS AND AFT AIRSTAIR AREA, RUN ENGINES AND OPERATED PACKS PER JET RUN HANDBOOK. COULD NOT DUPLICATE ODOR. OK TO CONTINUE.

Part: FLOORBEAM — CORRODED (BS 1110)

CORROSION ON TOP FLANGE AND BOTTOM OF TOP FLANGE ON FLOORBEAM BS 1110, LBL 65. REPAIRED FLOORBEAM AT BS 1110, LBL 65 PER SRM 53-10-8 AND EA 7-5310-29647.

Part: BELLFRAME — BENT (BS 560)

NR 1755 UPR LOBE BENT BELLFRAME AT BS 560, RBL 65 5 APPROX ABOVE FLOORBEAM. CUT OUT DAMAGE AREA FAB DOUBLER, ALODINED, PRIMED & INSTALLED DOUBLER PER SRM 51-40-3.

Part: SEAT TRACK — CORRODED (BS 1050)

NR 975 CORROSION ON SEAT TRACK & FLOORBEAM AT BS 1050 AT LBL 25 FROM C/L. SEAT/TRACK CORROSION REMOVED & NOW OUT OF LIMITS. INSTALL FLOORBEAM UPPER CHORD BY ACCORD WITH SRM 53-10-8 FIG 1 & EA 7-5310-29647 DATED 9/30/98.

Part: FLOORBEAM — CORRODED (BS 1130)

CORROSION ON FLOORBEAM BS 1130, LBL 35 AND LBL 42. REPAIRED IAW EA NR 7-5310-29637B.

Part: FLOORBEAM — CORRODED (BS 1130)

CORROSION ON FWD FLANGE OF FLOORBEAM BS 1130, RBL 45. INSTALLED DOUBLER ON FWD SIDE OF FLOORBEAM BS 1130, RBL 38 TO RBL 70 PER EA 7-5310-29637A DATED 9-4-98.

Part: FLOORBEAM — CORRODED (BS 720)

HEAVY AREA OF CORROSION ON TOP OF FLOORBEAM BS 720A, RBL 4 AT NUT PLATE HOLE (2 PLACES). REMOVED CORROSION ON FLOORBEAM, INSTALLED FLOORBEAM REPAIR PER AARD 53-10-7-2 FIG 2 IAW EA 7-5310-29647.

Part: BELTFRAME — DAMAGED (BS 520)

BELTFRAME DAMAGED BS 520, RT SIDE 6 INCHES ABOVE FLOORBEAM. TRIMMED OUT DAMAGE. INSTALLED TYPICAL FORMED SECTION REPAIR PER SRM 51-40-3.

Part: FLOORBEAM — DAMAGED (BS 1030)

BS 1030 BL 0, FLOORBEAM REPAIR NOT PER SRM ON I/B AIRCRAFT. REMOVED PREVIOUS REPAIR AND INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8, FIG 3.

Part: FITTING — CORRODED (BS 870)

BS 870 FLOORBEAM FITTING AT CENTER EXPANSION TRACK BELOW FLOOR LWR FITTING HAS CORROSION BOTH SIDES. REMOVED AND REPLACED CORROSION PER EA 7-5310-29647 AND REINSTALLED EXPANSION TRACK.

Part: FLOORBEAM — DAMAGED (BS 950)

ACCOMPLISH REPAIR TO BS 950D, BL 0 AS PER SRM 53-10-8 FIG 8 PG 44 REF AARD 51-20-1-05. INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8 FIG 8 AND EA 7-5310-29647.

Part: FLOORBEAM — CORRODED (BS1050)

CORROSION BETWEEN FLOORBEAM AND SEAT TRACK BS 1050, RBL 25. REMOVED CORROSION AND CUT OUT DAMAGE. INSTALLED REPAIR DOUBLERS PER SRM 53-10-8.

Part: BELL FRAME — CRUSHED (BS 580)

LWR FWD CARGO COMP BS 580 BELL FRAME CRUSHED IN SEVERAL AREAS BETWEEN STR 26 AND 23 LEFT. REPAIRED BELL FRAME AT BS 580 BETWEEN STR 26L AND 23L PER SRM 51-40-3.

Part: FLOORBEAM — CORRODED (BS 950)

BS 950D RBL 25 TO LBL 25, 8 FLOORBOARD FASTENER HOLES CORRODED AT FLOORBEAM. REMOVED CORROSION AREA AT RBL 10, BS 950D OUT OF LIMITS. INSTALLED FLOORBEAM REPAIR PER AARD 53-10-07-2 IAW EA 7-5310-29647.

Part: FLOORBEAM — CORRODED (BS 1130)

UPPER LOBE FLOORBEAM BS 1130, LBL 65 FIG 8 HAVE IN UPPER FLANGE AND LIGHT CORROSION UNDER FLANGE. REMOVED AND REPLACED CORROSION ON FLOORBEAM WITH FREEZE PLUG SRM 51-10-7. TREATED AND PRIMED AREA PER MM 51-20-0.

Part: BELL FRAME — CRUSHED (BS 600)

LWR FWD CARGO COMP BS 600 BELL FRAME CRUSHED IN SEVERAL AREAS BETWEEN STR 26L AND 23L. REPAIRED BELL FRAME AT BS 600 BETWEEN STR 26L AND 23L PER SRM 51-40-3.

Part: FLOORBEAM — CORRODED (BS 1130)

CORROSION ON THE BOTTOM O/B SEAT TRACK BOLTS BS 1130, RBL 65 O/B. INSTALLED DOUBLER ON FWD SIDE OF FLOORBEAM BS 1130, RBL 30 TO RBL 70 PER EA 7-5310-29637A DATED 9-4-98.

Part: FLOORBEAM — CORRODED (BS 1130)

CORROSION UNDER NUT PLATE ON FLOORBEAM BS 130, RBL 43. INSTALLED DOUBLER ON FWD SIDE OF FLOORBEAM BS 1130, RBL 38 TO RBL 70 PER EA 7-5310-29637A DATED 9/4/98.

Part: FLOORBEAM — CORRODED (BS 870)

BS 870 FLOORBEAM AT BL 0 TO RBL 25 CORROSION ON FLOORBEAM AND IN FASTENER HOLES. REMOVED CORROSION AND INSTALLED FREEZE PLUG PER EA 7-5310-2964.

Part: FLOORBEAM — CORRODED (BS 580)

NR 1120, OVERSIZED HOLES NOT IN USE IN FLOORBEAM AT BS 580 BLO. INSTALLED REPAIR PER AARD 53-10-07-2 PG 1,2,3 AND FIG 1.

Part: FLOORBEAM — CORRODED (BS 620)

NR 0380, UPPER LUBE CORROSION FLOORBEAM BS 620, BL O TO RBL 25. REPAIRED FLOORBEAM PER SRM 53-10-8.

Part: FLOORBEAM — CORRODED (BS 1010)

NR 0811 - CORROSION ON FLOORBEAM LWR FLANGE SEEN FROM LWR AFT CARGO BS 1010, RBL 45 TO LBL 45. CUT OUT CORROSION REMOVED BEYOND LIMITS AT LBL 12 AND LBL 20 TO LBL 45. INSTALLED DOUBLER REPAIR PER SRM 53-10-8 PG 44 THROUGH PG 48.

Part: FLOORBEAM — DAMAGED (BS 560)

NR 1119 - DAMAGE TO FLOORBEAM OVERSIZED HOLES NOT IN USE AT BS 560 BLO. INSTALLED REPAIR PER AARD 53-10-07-2 PG 1,2,3 AND FIG 1.

Part: O-RING — MISSING (NR 1 ENGINE)

98-210 - NR 1 ENG PRIOR TO PUSH HAD OIL QTY OF 4 PLUS GAL AND GAUGE NORM. DURING T/O ROLL PRIOR TO 80 KTS, ALL 3 OIL QTY GAUGE READ 3.5 GAL AFT ROTATION NR 1 OIL QTY WAS 2.5 CONT TO DROP 1.5. TEST NORM. FOUND OIL SERV CAP O-RING DISPLACED. REINSTALLED O-RING ON CAP. SERV ENG TO PROPER LIMITS. INSP TAIL PIPE AND ENG NO DEFECT. REF PRATT AND WHITNEY M/M 70-00 PAGE 203.

Part: ACTUATOR — FAILED (NR 8 LE SLAT)

98-0058 AFTER TAKEOFF WITH GEAR AND FLAPS UP, LEADING EDGE DEVICE INDICATIONS WERE NORMAL. SYSTEM 'A' LOST ALL QUANTITY. DURING HYDRAULIC LOSS CHECK LIST, LEADING EDGE DEVICE MALFUNCTION, LIGHT ON SLAT NR 8 WAS AMBER. AFTER AIRCRAFT TOW IN, FOUND NR 8 SLAT ACTUATOR BLOWN. REMOVED AND REPLACED PER MAINTENANCE MANUAL 27-81-32. REMOVED AND REPLACED SYSTEM FILTERS. TEST, BLED AND LEAK CHECK SYSTEM. NO LEAK, ALL FUNCTION NORMAL. RAN ENGINES 1 AND 2 PER JET RUN HANDBOOK AND TESTED PER CHAPTER 5A AND 9. GROUND CHECK NORMAL. SERVICED SYSTEM AS REQUIRED.

Part: LINE — FAILED (A-HYD SYST)

HYDRAULIC LOSS SYSTEM-A UPON GEAR RETRACTION. PRESSURE 0 ENGINE LOW PRESSURE LIGHT INITIALLY ILLUMINATED, ONLY PRESSURE WAS 3000. HYDRAULIC QUANTITY WENT FROM 0 TO 1.2, ENGINE 1 PUMP LOW PRESSURE LIGHT EXTINGUISHED FOR 10 SEC THEN HYDRAULIC QUANTITY WENT TO 0, PRESSURE 0 ENGINE 1 LOW PRESSURE LIGHT ILLUMINATED AGAIN. A SYSTEM RUDDER LIGHTS ILLUMINATED, THEN NR 2 LOW LIGHT ILLUMINATED. REPLACED A-SYSTEM HYDRAULIC PRESSURE LINE TO TRANSMITTER. SERVICED HYDRAULIC. BLEED ALL SYSTEMS LEAK CHECKED OK.

Part: HYD DRIVE MOTOR — LEAKING (TE FLAPS)

AFTER TAKE OFF DURING RETRACTION, THE INBOARD FLAPS REMAINED AT 2 DEGREES (SPLIT FLAP CONDITION). WHILE FOLLOWING THE CHECK LIST WE LOST SYSTEM A HYDRAULICS. PERFORM SYSTEM A LOSS CHECKLIST AND LANDED UNEVENTFULLY. LANDED HARD (FIRM). REMOVED AND REPLACED INBOARD FLAP DRIVE HYDRAULIC MOTOR. OPERATIONAL CHECK AND LEAK CHECKED GOOD PER 27-50 MAINTENANCE MANUAL. VISUAL INSPECTION FOR HARD LANDING. NO DEFECTS NOTED. OK FOR SERVICE.

Part: STRINGER — CRACKED (BS 390)

NR 0511 AND 011. CRACK IN STR 23L BETWEEN STR 380 AND STR 400. ****S/D***** COMING.

Part: FLOOR BEAM — CORRODED (BS 1148)

NR0054 AND 012, CORROSION (C53-111-01, -3) ON BOTTOM OF FLOOR BEAM BS 1148 RBL 10.

Part: CLIP — CRACKED (BS 680)

NR 0471 AND 010. STRINGER CLIP IS CRACKED AT BS 680 STR 3L. ***S/D***** COMING.

Part: FRAME — DENTED (BS 580)

NR0469 AND 006. DENTS IN FRAME AT BS 580 BETWEEN STR 16-17R. REPAIRED DAMAGED FRAME AT BS 580 BETWEEN STR 16-17R PER FEDEX SRM 51-40-3.

Part: FLOOR BEAM — CORROSION (BS 1050)

NR0465 AND 088. CORROSION C53-224-04 ON FLOOR BEAM OUT OF LIMITS BS 1050 RBL 35 WL 208.1. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLES (2 EA), AND REPLACED FILLER ON FLOOR BEAM AT BS 1050 RBL 35 WL 208.1 AND TREATED IAW FEDEX SRM 53-10-8.

Part: FRAME — DENTED (BS 660)

NR0042 AND 007. DENTS IN FRAME BS 660 STR 23-25L. DENT IN FRAME AT BS 660 BETWEEN STR 24-25L FOUND TO BE WITHIN LIMITS PER FEDEX SRM 53-10-1. DENT IN FRAME AT BS 660 BETWEEN 23-24L FOUND OUT OF LIMITS (CRACKED). REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR CAP PER FEDEX SRM 51-40-3.

Part: FRAME — DENTS (BS 500)

NR0470 & 004 DENT IN FRAME AT BS00 BETWEEN STR 15-16R. ****S/D***** REPAIRED DAMAGED FRAME AT BS 500 STR 15-16R AS PER FEDEX SRM 51-40-3.

Part: SHEAR WEB — CORRODED (BS 1170- 1176)

NR 0467 AND 005. CORROSION C53-224-04 ON BOTTOM SIDE OF WEB BS 1170-1176 RBL - LBL 2 WL 207. REMOVED WEB BS 1170-1176 RBL - LBL 2 WL 207. FABRICATED AND INSTALLED NEW WEB. REMOVED SEAT TRACK BS 1130 - 1183 BL ZERO WL 207. FABRICATED AND INSTALLED NEW TRACK. ALL PER FEDEX SRM 51-20-1, 51-10-1.

Part: FLOOR BEAM — CORROSION (BS 1110)

NR0466 & 003 CORROSION C53-224-04 ON FLOOR BEAM AROUND CLIP NOT HOLE BS 1110 LBL 16 WL 207.9 *****S/D**** REMOVED DAMAGED AREA & FABRICATED REPAIR ANGLES (2 EA) & REPAIR FILLER, INSTALLED & TREATED ON FLOOR BEAM AT BS 1110 LBL 16 WL 207.9 IAW FEDEX SRM 53-10-8.

Part: FRAME SPLICE — DENTED (BS 520)

NR0041 & 002 DENT IN FRAME SPLICE BS 520 STR 25L. ****S/D***** REMOVED FRAME CAP FROM BS 520 STR 25L FABRICATED & INSTALLED FRAME CAP IAW FEDEX SRM 51-20-1 ALODINED & PRIMED.

Part: STRINGER — CORRODED (BS 720)

NR0328 AND 001, CORROSION (C53-111-01, -2) ON STR 27L BS 720A PLUS 10 WL 150 LBL 15. *S/D* REMOVED DAMAGED SECTION FROM 720A PLUS 7 TO 720A PLUS 10. REPAIRED STR SECTION PER FEDEX SRM 53-10-1, 53-10-3 FIG 1.

Part: FLOOR BEAM — CORRODED (BS 1070)

NR0265 AND 009, CORROSION ON BOTTOM OF FLOOR BEAM BS 1070 LBL 55 TO RBL 65. *S/D* REPAIRED FLOOR BEAM AT 1070 LBL 47 TO RBL 65 IAW FEDEX SRM 53-10-8.

Part: DRIVE MOTOR — LEAKING (FLAP SYST)

LOSS OF SYSTEM-A OCCURRED 30 MINUTE AFTER TAKEOFF. RAN CHECK LIST VERIFIED SYSTEM-A LEAK. SHUT-OFF BOTH SYSTEM-A FLUID SHUT-OFF SWITCHES. LEAK/FLUID LOSS STOPPED WITH LESS THAN 1 GALLON. REMOVED 40 DEGREE FLAP STOP, REMOVED AND REPLACED HYDRAULIC FLAP DRIVE MOTOR AND SERVICED A-SYSTEM HYDRAULIC. REMOVED AND REPLACED A-SYSTEM CASE DRAIN FILTERS ON NR 1 AND NR 2 MOTORS. REMOVED AND REPLACED A-SYSTEM PRESSURE FILTER ON A-SYSTEM MODULAR UNIT PER MM 29-11-62 PG 301. NO METAL FOUND, CHECKS GOOD, INTALLED FLAP STOP.