N107FE

Part: AOA — FAILED (ZONE 100) · airframe 20,724 hrs · 8,275 cycles

PASSING FL 200 THE ALT DISAGREE EICAS MESSAGE ALONG WITH THE AURAL ALERT ACTIVATED MOMENTARILY AND THE AGAIN PASSING FL 220. FOLLOWED QRH. EICAS MESSAGE EXTINGUISHED. THE CAPTAINS ALTIMETER WAS 200 FEET DIFFERENT FROM THE F/O AND THE STANDBY ALTIMETERS. REF WRI 34-10/1543 L ADRU HAS BEEN PLACED ON MEL 34-26-01-01 IN FRA FOR THE SAME REASON AFTER ANALYSIS OF EVENT AND FOLLOWING FIM, SUSPECTED L AOA TO BE THE ROOT CAUSE OF THE ALTITUDE DISCREPANCY. IT WAS REPLACED UNDER WRI 34-10/1550. PRESSURISED THE CAPT STATIC SYSTEM IAW AMM 34-11-00-2 UP TO 25,000 FT USING AIR DATA TEST SET. THE DIFFERENCE OF ALTITUDE BETWEEN CAPT PFD AND AIR DATA TEST SET WAS LESS THAN 10 FEET AND MAINTAINED THIS FOR OVER ONE MINUTE. TEST SATISFACTORY.

Part: CIRCUIT CARD — FAILED (FIRE DETECTION) · airframe 19,817 hrs · 7,977 cycles

FIRE WARNING BELL CAME ON AT ROTATION. NO OTHER INDICATIONS. BELL WILL NOT SILENCE EVEN AFTER BLOCK IN AND ENGINES SHUTDOWN. MDIS 31-50 1103. REF. FIM 31-51 TASK 801, DID A WEU BITE & RESET.TEST NORMAL IAW AMM 31-51-00-5, PERFORMED FIRE BELL WARNING SIGNALS TEST. TEST NORMAL INSPECTED BELL/CHIME MODULE M1000 IN P51. PAID ATTENTION TO CONDITION OF CONNECTORS & PINS. MADE SURE CARD WAS PROPERLY SEATED IAW AMM 31-51-04. INSPECTED NORMAL. REPLACED BELL/CHIME MODULE M1000 IAW AMM 31-51-04-4. MADE SURE THE CARD IS PROPERLY SEATED IAW AMM 31-51-04-4. PERFORMED BELL/CHIME AURAL WARNING CARD MODULE TEST, TESTED NORMAL IAW AMM 26-14-00-5. PERFORMED MDCC SMOKE DETECTOR SAMPLING TUBES & SAMPLING TRUNK TUBE ORIFICES OPS TEST, TESTED NORMAL. REF AMM26-21-02-2 REPLACED THE ENGINE FIRE CONTROL PANEL. REF AMM26-21-01-716-001 DID ENGINE FIRE SWITCH OPS CHECK, RESULT :TEST NORMAL. REF AMM26-21-02-2 DID ENGINE FIRE CONTROL PANEL INSTALLATION TEST, RESULT :TEST NORMAL REF AMM26-11-01-4. REPLACED THE FIRE/OVERHEAT TEST PANEL. REF AMM26-11-01-4. DID INSTALLATION TEST, TESTED NORMAL. REF AMM31-51-04-4 REPLACED THE T/O CONFIGURATION WARNING MODULE IAW AMM31-51-04-4. DID TEST , TEST NORMAL. REF AMM32-09-02-2. REPLACED THE RELAY K219, TEST NORMAL. RESTORE AC TO SERVICE. ORIGINAL SUBMISSION DATE: 7/16/2024

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 15,930 hrs · 6,393 cycles

MAIN DECK FLOOR SEAT TRACK DAMAGED AT STA610 10, RBL11. REPAIRED THE MAIN DECK DAMAGED FLOOR SEAT TRACK PER B767 SRM53-00-52-2R REPAIR 9 & EA H-5310-T0368785 P1. TITLE: FUSELAGE - MAINFRAME - DAMAGE ON MAIN DECK FLOOR SEAT TRACK AT RBL11 STA610 10 - SRM REPAIR WITH MINOR DEVIATIONS. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: CONNECTOR — DIRTY (HYD PRESSURE) · airframe 12,071 hrs · 4,758 cycles

PDIS 107, 29-11, 6407, 09SEP20, PEN, FACT, U. WHEN LEVELING AT FL 240 C HYD SYS PRESS LIGHT ILLUMINATED, COMPLIED WITH QRH PROCEDURE. FACT 09SEP20 14:00 PEN U. A/C BLOCKED IN WITH PRESSURE 2970 AT CENTER R HYD SYS WITH SWITCH PUMPS IN OFF POSITION. RECYCLED C/B C1 ELEC PUMP NIL HELP, PRESS IS STILL ONLINE C HYD SYS. T/S PER FIM FAULT CODE 29 90 15 43, CHECK PRESSURE TX M342 CONNECTOR REMOVED, CLEANED, AND RESECURED PER AMM 29-31-01-4. CENTER HYD SYS INDICATION RETURN TO NORMAL. C/O C HYD SYS ADJ/TEST, PER AMM 29-11-00-5. C/O ADJ AND TEST HORIZ STAB TRIM CTRL SYS, AS PER AMM 27-41-00-5 FOUND SATIS. CONSULTED MOCC AND RELEASED A/C FOR SERVICE. CHECK PRESSURE TX M342 CONNECTOR, CLEANED, AND RESECURED PER AMM 29-31-01-4. CENTER HYD SYS INDICATION RETURN TO NORMAL. C HYD SYS ADJ/TEST, PER AMM 29-11-00-5. HORIZ STAB TRIM CONTROL SYS ADJ/TEST, PER AMM 27-41-00-5 FOUND SATIS.

Part: SKIN — GOUGED (ZONE 100) · airframe 12,063 hrs · 4,755 cycles

FUSELAGE, FWD LOWER FUSELAGE SKIN AT STATION 773 STRINGER 36 LT FOUND WITH EXISTING BLEND OUT WITH GOUGE MARK. FWD LOWER FUSELAGE SKIN AT STATION 773 STRINGER 36 LT EXISTING BLEND OUT WITH GOUGE MARK, EVALUATED AND FOUND EXCEED LIMIT PER B767 SRM 53-00-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 DETAIL II. DAMAGED FUSELAGE SKIN AREA AT STATION 773 STRINGER 36 LT CUT OUT AND REPAIRED, AS PER B767 SRM 53-00-01-2R REPAIR 12 FIGURE 201. CATEGORY B REPAIR WHICH REQUIRES SUPPLEMENTAL INSPECTIONS AS GIVEN IN TABLE 202. INSPECTION THRESHOLD: 30,000 FLIGHT CYCLES AFTER AIRPLANE DELIVERY, REPEAT INSPECTIONS: ALTERNATIVE I, METHOD: INTERNAL-HIGH FREQUENCY EDDY CURRENT INSPECTION AND EXTERNAL DETAILED VISUAL, INTERVALS: 9,000 FLIGHT CYCLES, REFERENCE: NON DESTRUCTIVE TEST PART 6, 51-00-01. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (ZONE 100) · airframe 12,063 hrs · 4,755 cycles

FUSELAGE, FWD LOWER FUSELAGE AT STATION 325, STRINGER 34 LT FOUND WITH EXISTING BLENDOUT. FWD LOWER FUSELAGE SKIN AT STATION 325 STRINGER 34 LT EXISTING BLENDOUT EXCEED LIMIT AS PER B767 SRM 53-00-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 DETAIL II. DAMAGED SKIN AREA CUT-OUT AND REPAIRED PER B767 SRM 53-00-01-2R REPAIR 29 FIGURE 201. CATEGORY B REPAIR, WHICH REQUIRES SUPPLEMENTAL INSPECTIONS PER TABLE V. INSPECTION THRESHOLD: 30,000 FLIGHT CYCLES AFTER AIRPLANE DELIVERY, REPEAT INSPECTION: ALTERNATIVE II, METHOD: EXTERNAL-LOW FREQUENCY EDDY CURRENT INSPECTION AND EXTERNAL DETAIL INSPECTION, INTERVAL: 3,000 FLIGHT CYCLES, REFERENCE: NON DESTRUCTIVE TEST PART 6, 53-00-06. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (ZONE 100) · airframe 12,063 hrs · 4,755 cycles

FUSELAGE - RIGHT HAND LOWER FUSELAGE AT STATION 390, BETWEEN STRINGER 29 RIGHT TO 30 RIGHT FOUND WITH EXISTING BLEND OUT. RIGHT HAND LOWER FUSELAGE SKIN AT STATION 390 BETWEEN STRINGER 29 RIGHT - STRINGER 30 RIGHT EXISTING BLEND OUT EXCEED LIMIT PER B767 SRM 53-00-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 DETAIL II. DAMAGED SKIN AREA CUT-OUT AND REPAIRED AS PER B767 SRM 53-00-01-2R REPAIR 29 FIGURE 201 CATEGORY B REPAIR WHICH REQUIRES SUPPLEMENTAL INSPECTIONS PER TABLE V. INSPECTION THRESHOLD: 30,000 FLIGHT CYCLES AFTER AIRPLANE DELIVERY, REPEAT INSPECTION: ALTERNATIVE II, METHOD : EXTERNAL- LOW FREQUENCY EDDY CURRENT INSPECTION AND EXTERNAL DETAIL INSPECTION, REFERENCE : NON DESTRUCTIVE TEST PART 6 53-00-06. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (ZONE 100) · airframe 12,063 hrs · 4,755 cycles

FUSELAGE, FORWARD LOWER FUSELAGE SKIN AT STATION 478, STRINGER 35 LEFT FOUND WITH EXISTING BLEND OUT. FWD LOWER FUSELAGE SKIN AT STATION 478 STRINGER 35 LEFT EXISTING BLEND OUT AREA. REPAIRED AS PER E.A NR: H-5330-T0356108 PART 1 TITLE: FUSELAGE-PLATES & SKINS-ONE GOUGE DAMAGE C/T EXISTING BLENDOUT ON FUSELAGE SKIN PANEL AT STA478, BETWEEN S-34L AND S-35L. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: WARNING MESSAGE — FALSE ACTIVATION (FLAP SYSTEM) · airframe 10,451 hrs · 4,087 cycles

PDIS 107 27-50 5327 20NOV19 CRK FACT U LOGPAGES:3138465 AFTER SELECTING FLAPS 30 TE FLAP ASSYM ON EICAS, COMPLIED WITH QRH. FACT 20NOV19 23:26 CRK U FOLLOW FIM 27-51-00-815-811, FSEU BITE PERFORMED FOUND FAULT CODE " LE DISAG" , MSG NO. 27-81042, " LE SLATS NO HYD". CYCLE CB FSEU . RETRACT FLAP THRU ALT, THEN PERFORMED OOPS TEST LE AND TE, BY HYDRAULICS SOURCE. SATIS. NO FAULT ON EICAS. ALSO PERFORMED VISUAL INSPECTION TE FLAP TORQUE TUBES IN EACH WING AND FGLAP POWER DRIVE UNIT. NO DEFECT NOTED . AND PERFORMED INSPECTION COMPONENT DRIVE LE SLAT QUADRANT AND EACH PDU AND LINKAGE, SATIS. ALSO PERFORMED FIM 21-51 FT 809 FSEU BITE NO FAULT AFTER OPS CHK. A/C OK FOR SVC. FOLLOWING FIM 27-51 F/T 809 & 811, MSG CLEARED. PERFORMED THE VISUAL INSPECTION LE & TE SATISFACTORY. FSEU BITE TEST NO FAULT NOTED.

Part: CARABINER — MISSING (COCKPIT) · airframe 8,397 hrs · 3,284 cycles

ON SVC CHK FOUND RIGHT AND CENTER JUMP/SUPERNUMERARY SEAT MISSING CARABINERS 4 EA. A/C OK FOR SVC. JUMPSEAT ESCAPE HARNESS OBS MPN A657C30 CPN 2526711 QTY 4 CARABINER. INSTALLED 4 EA CARABINERS.

Part: CHANNEL — CRACKED (RT WING) · airframe 53,613 hrs · 39,663 cycles

RIGHT WING TRAILING EDGE AT AFT SPAR AREA 3 EA CLOSE OUT PANEL SUPPORTS ARE CRACKED LOCATED UNDER NR 12 & 13 SPOILER PANELS. REMOVED AND REPLACED 3 EACH CHANNEL SUPPORTS IAW SRM 51-30-2.

Part: RIB — CRACKED (ZONE 300) · airframe 53,341 hrs · 39,461 cycles

STABILIZER-ELEVATOR HINGE SUPPORT RIB INSPEC - S/B 727-55A0091 R1 COMPLY WITH EO 7-5510-7-5001. FOUND CRACK IN RIB AT ELEVATOR STA 50.50 DURING INSPECTION IAW EO 7-5510-5001. REMOVED AND REPLACED RIB IAW EO 7-5510-5001.

Part: STIFFENER — CORRODED (LT WHEEL WELL) · corrosion level 2 · airframe 52,953 hrs · 39,011 cycles

LEFT WHEEL WELL BULKHEAD STA 950 LOWER -TEE CHORD IS CORRODED. REMOVED AND REPLACED CHORD IAW SRM 51-30-2 ON N/R N00126 WO 24581 AT MAE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,953 hrs · 39,011 cycles

FUSELAGE SKIN BULGE AT STA 1163 STRINGER 18L & 19L. REMOVED CORROSION IAW SRM 51-10-6, FABRICATED & INSTALLED REPAIR DOUBLER IAW EA 7-5330-73867A.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 52,953 hrs · 39,011 cycles

AFT PIT BS 1080 TO 1050 AT STR 26R INTERCOSTAL DAMAGED AND HOLES ELONGATED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-30-2. NEW INTERCOSTAL FABRICATED ON TRAVELER NR T4/398010.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 52,953 hrs · 39,011 cycles

AFT LOWER PIT BS 970 TO 990 BETWEEN STR 29 AND LT KEEL BEAM CRACKED FLOOR SUPPORT AND CORRODED NUT PLATES. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 53-10-5 AT MAE ON N/R NOO419.

Part: WEB — CRACKED (MAIN CARGO DOOR) · airframe 52,953 hrs · 39,011 cycles

UPPER DECK, CARGO DOOR UPPER BOX WEB FINGERS ARE CRACKED AT STA 490 AND 500 STR 2L. REMOVED DAMAGED WEB AND INSTALLED NEW WEB IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,953 hrs · 39,011 cycles

MAIN CABIN SEAT TRACK AT APPROX RBL 24 FS 1140 TO 1183 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 AT MAE ON N/R N00448.

Part: SUPPORT ANGLE — CRACKED (LWR NOSE BAY) · airframe 52,953 hrs · 39,011 cycles

LOWER NOSE COMPT DOOR CUTOUT SUPPORT ANGLE IS CRACKED AT FS 203 RBL 11. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-30-2 AT MAE ON N/R N00687.

Part: COUPLER — FAILED (YAW DAMPER) · airframe 52,934 hrs · 38,998 cycles

LOWER YAW DAMPER RUNAWAY - LT AND RT AFTER TAKEOFF - LYD SWITCH TURNED OFF. REMOVED AND REPLACED LOWER YAW DAMP COUPLER IAW 727-100 MM CH 22-11-131-4. OPS CHECKS NORMAL ON GROUND. A/C OK FOR SERVICE.

Part: SWITCH — FALSE INDICATION (NLG) · airframe 52,787 hrs · 38,874 cycles

NOSE GEAR DID NOT INDICATE SAFE AFTER PLACING LANDING GEAR HANDLE DOWN. CYCLED LANDING GEAR LEVER. NOSE GEAR INDICATED SAFE AFTER APPROX 10 - 15 SEC. RED UNSAFE WAS NOT ILLUMINATED. REMOVED AND REPLACED SWITCHES S93 AND S96 IAW M/M 32-61-021-4. OPS CK GOOD.

Part: COALESCER BAG — CONTAMINATED (ZONE 100) · airframe 52,547 hrs · 38,696 cycles

AFTER GEAR RETRACTION, CREW BECAME AWARE OF AN ACRID ODOR WHICH INTENSIFIED. INITIAL ODOR WAS OF BURNING RUBBER OR A SMOLDERING WIRE BUNDLE. CREW WENT ON OXYGEN AND RETURNED TO IND. PERFORMED FIRE, SMOKE, FUMES AND ODOR CHECKLIST. REPLACED BOTH WATER SEPARATOR SOCKS. FOUND LT SOCK EXTREMELY DIRTY AND SMELLED OF DE-ICE FLUID. CHECKED ACM OIL LEVELS, FOUND NORMAL. RAN ALL 3 ENGINES IAW JRH. RUN WAS NORMAL. NO ODOR PRESENT. REF. M/M 21-51-032.

Part: ACTUATOR — FAILED (L/E SLAT) · airframe 52,331 hrs · 38,541 cycles

DURING FLAP RETRACTION NR 2 SLAT ON RIGHT WING REMAINED EXTENDED WITH FLAP LEVER IN UP POSITION. QRH PROCEDURES WERE FOLLOWED AND FLAPS WERE CYCLED BACK TO 5 ON SCHEDULE FLAPS RETRACTED AGAIN AND PROBLEM CONTINUED. REMOVED AND REPLACED NR 2 SLAT ACTUATOR AS PER B727 M/M 27-81-032-4, OPS AND LEAK CHECKED GOOD. A/C RETURNED TO SERVICE.

Part: OIL FILTER — DAMAGED (NR 1 ENGINE) · airframe 52,236 hrs · 38,455 cycles

NR 1 ENGINE, HIGH OIL TEMP (OFF SCALE HIGH) FOUND BAD CONNECTION AT OIL TEMP SENSOR. PER CREW INFO WINDMILLING WAS LESS THAN 30 MIN. FOUND BROKEN WIRE AT C/P ON NR 1 ENG OIL TEMP BULB. REMOVED AND REPLACED C/P D530 IAW SWPM. PERFORMED ENGINE WINDMILLING INSPECTION IAW M/M. NO DEFECTS FOUND. REPLACED NR 1 ENGINE MAIN OIL FILTER P/N AC-9806F-65, LEAK CKS GOOD. NR 1 ENG OIL TEMPERATURE INDICATOR, OPS CHECK GOOD IAW JRH.

Part: SKIN — CORRODED (BS 425-440) · airframe 51,663 hrs · 37,914 cycles

N 371 DUR ROUTINE INSP FUSELAGE SKIN FND CORRODED FROM BS 425-440 BETWEEN STR 3L AND 4L. R&R & FAB SKIN PER IAW BAC 727 SRM 53-30-3.

Part: FITTING — CORRODED (BS 227.8) · airframe 51,863 hrs · 37,914 cycles

N 773 DUR ROUTINE INSP, NLG DOOR UPR LINK FITTING BS 227.8 FND CORRODED. R&R FITTING IAW BAC 727 SRM 51-30-2.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 51,663 hrs · 37,914 cycles

DURING ROUTINE INSP THE NR 1 SEAT TRACK SUPPORT AT BS 860 FOUND CRACKED. *S/D* REMOVED AND REPLACED SUPPORT PER IAW BAC 727 SRM 51-30-2.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,663 hrs · 37,914 cycles

DURING ROUTINE INSP FLT DECK FLOORBEAM WEB AT BS 299, LBL 6 FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB WEB PER IAW BAC 727 SRM 51-20-1, SRM 51-30-2.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,663 hrs · 37,914 cycles

DURING ROUTINE INSP, STR TIE CLIP AT BS 312, STR 4R FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,663 hrs · 37,914 cycles

DURING ROUTINE INSP, HFEC IND TWO CRACKS IN BS 1183 BULKHEAD WEB AT WL 283. *S/D* REMOVED AND REPLACED WEB PER IAW FEDEX EO 7-5310-7-5000 PARTS 2 & 4.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,663 hrs · 37,914 cycles

DURING ROUTINE INSP, LT SIDE WEB IN AIRSTAIR COMPT FOUND CRACKED AT LIGHTENING HOLE AT BS 1263. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-40-2, 51-30-2.

Part: FITTING — CRACKED (ELEVATOR TAB) · airframe 51,663 hrs · 37,914 cycles

DURING ROUTINE INSP, RT ELEVATOR TAB ROD FITTING FOUND CRACKED. *S/D* REMOVED AND REPLACED RIGHT ELEVATOR TAB PER IAW BAC 727 MM 27-30-011-2.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,663 hrs · 37,914 cycles

DURING ROUTINE INSP, STR TIE CLIP AT BS 328, STR 14R FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,663 hrs · 37,914 cycles

DURING ROUTINE INSP BS 1183 BULKHEAD VERTICAL BEAM AT LBL 27 FOUND CRACKED AT WL 263. *S/D* REMOVED AND REPLACED PER VERTICAL BEAM PER IAW FEDEX EO 7-5310-7-2346 PART 2.

Part: SKIN — CRACKED (EXIT HATCH) · airframe 51,663 hrs · 37,914 cycles

DURING ROUTINE INSP, LT FWD EMERGENCY EXIT HATCH UPPER INNER SKIN FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 52-00-3, 51-30-2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,663 hrs · 37,914 cycles

DURING ROUTINE INSP, HFEC IND CRACK IN FASTENER HOLES IN ROW 3, LT BS 870 FITTING AT STR 9L. *S/D* HFEC IND NO CRACKS PER IAW BAC 727 NDT MANUAL PART 6.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 51,663 hrs · 37,914 cycles

DURING ROUTINE INSP THE NR 1 SEAT TRACK SUPT AT BS 840 FOUND CRACKED.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,663 hrs · 37,914 cycles

DURING ROUTINE INSP, RT SIDE WEB IN AFT AIRSTAIR AREA FOUND CRACKED AT BS 1283. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 BAC 727 SRM 51-40-2, 51-30-2.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 51,663 hrs · 37,914 cycles

DURING ROUTINE INSP LT SIDE WEB IN NOSE WHEEL WELL WAS FOUND CRACKED AT BS 1260. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.

Part: RIB — CRACKED (RUDDER) · airframe 51,663 hrs · 37,914 cycles

DURING ROUTINE INSP LWR RUDDER, LWR THRUST HINGE RIB FOUND CRACKED AT FASTENER COMMON TO FIN REAR SPAR. *S/D* HFEC IND CRACK TERMINATED. REMOVED, REPLACED AND FAB PER IAW FEDEX DRAWING SRM 27-55-005, SRM 51-30-2.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,663 hrs · 37,914 cycles

DURING ROUTINE INSP, HFEC IND CRACK IN BS 1183 BULKHEAD WEB AT WL 283, RBL 17.8. *S/D* REMOVED AND REPLACED PER IAW FEDEX EO 7-5310-7-5000 PARTS 3 & 5.

Part: BATTERY — DISCHARGED (CABIN)

ENTRY DOOR EMERGENCY LIGHT BURNED OUT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ON FORWARD ENTRY DOOR. SYS OPER CK GOOD IAW FEDEX MM 33-50-0.

Part: PUMP — FAILED (NR 2 ENGINE)

DURING CLIMBOUT, NR 2 LOW OIL PRESS/FILTER BYPASS LIGHT CAME ON. OIL PRESS DROPPED TO ZERO, TEMP WAS OK. SHUTDOWN ENG PER RED TABS WITHIN 4 TO 5 MIN. *S/D* REMOVED AND REPLACED NR 2 ENG OIL PUMP.

Part: HYD LINE — CRACKED (NR 12 SPOILER)

IN-FLIGHT AT FL 280, NR 1 ENGINE HYDRAULIC PUMP LIGHT STARTED BLINKING WITH FLUCTUATION IN PRESSURE. TWO SECONDS LATER, NR 2 ENGINE HYD PRESS LIGHT BLINKED, THEN BOTH LIGHTS CAME ON STEADY WITH RAPID LOSS OF ALL A-SYSTEM HYD FLUID. PUMPS WERE OPERATED WITHOUT FLUID FOR ABOUT THIRTY MINUTES. QUANTITY WENT TO ZERO ALMOST IMMEDIATELY WITH ILLUMINATION OF PUMP LIGHTS. FOUND HYD RETURN LINE BY NR 12 SPOILER CRACKED. REMOVED AND REPLACED LINE. CHANGED BOTH A-SYSTEM PRESSURE FILTERS AND RETURN FILTER. SERVICED SYSTEM. REMOVED AND REPLACED NR 2 HYD PUMP AND CASE DRAIN FILTERS. LEAK CK GOOD.

Part: TRACK — CORRODED (BS 840)

CORROSION ON O/B OF TRACK STA 840 RBL 48. INSTALLED DOUBLER PER EA 7531-0-28823 AND 51-10-1.

Part: INTEGRAL RIB — CRACKED (BS 870)

LT 870 INTEGRAL RIB FWD CRACK FROM O/B HOLE TO EDGE. INSTALLED BATHTUB FITTING PER EA NR 7-5310-28832.

Part: SKIN — CORRODED (BS 850-856)

UPPER SURFACE CENTER WING SECTION, CENTER WING SKIN HAS HEAVY CORROSION AT LT AFT CORNER SECTION UNDER PRESS. SEAL TRACK APPROX 6 INCH AREA, THREE PLACES FS 850 TO 856. CORROSION REMOVED, DIGITAL THICKNESS CHECKED BY NDT, ORIG 184 TAKEN DOWN TO .068. REPAIR DOUBLER INSTALLED PER ESO 11782 DATED 8/7/96 AND EA NR 7571028845 DATED 8/15/96.

Part: ANGLE — CORRODED (BS 344)

FLOOR BOARD SUPPORT ANGLE CORRODED AT STA 344 26 TO 45 LBL FLOOR BEAM. REMOVED CORROSION AND INSTALLED CAP STRIP REPAIR PER SRM 51-10-1.

Part: SPLICE PLATE — CORRODED (BS 870)

CORROSION UNDER WING TO FUSE SPLICE PLATE LT SIDE AFT CORNER OF TANK BS 870 LBL 70.5. CUT OUT CORROSION, INSTALLED REPAIR PER EA 7-5710-28845.

Part: ANGLE — CORRODED (BS 1176)

CABIN INTERIOR, FS 1176 REINFORCEMENT CHORD ANGLE HAS HEAVY TO SEVERE CORROSION. FLOOR LEVEL BETWEEN BL 44 TO 46 LT. REMOVED DAMAGED PORTION OF CHORD ANGLE, INSTALLED NEW SECTION AND SPLICE DOUBLER PER E/A NR 7531028817.

Part: SEAT TRACK — CORRODED (BS 840)

CORROSION ON O/B OF TRACK STA 840 RBL 48. INSTALLED DOUBLER PER EA 7531028823.

Part: DOUBLER — CRACKED (PAX DR CUTOUT)

FOUND CRACK AT FWD ENTRY DOOR CUT OUT FRAME UPPER HINGE AREA. INSTALLED DOUBLER AS PER SRM 53-10-4 FIG 2.

Part: FLANGE — CORROSION (BS 1148-1166)

NR0176, MAIN CARGO HAS CORR ON STR 5L STA 1148 TO 1166. REMOVED CORR SRM 51-10-6 OUT OF LIMITS, CUT REPAIR PARTS FOR INSIDE FLANGE REPAIR PER SRM 53-10-3.

Part: DOUBLER — CRACKED (BS 870)

RT 870 INTERGRAL RIB FWD CRACKED FROM O/B HOLE TO EDGE. THE 2ND CRACK O/B OF O/B HOLE CRACKED FROM EDGE THROUGH RADIUS INTO AFT LWR HOLE OF O/B FLANGE. INSTALLED DOUBLER PER EZ 7-5310-28831.

Part: STRINGER — CORRODED (BS 720)

FORWARD CARGO BS 720 STR 23R HEAVY CORROSION INSIDE STRINGER ON LOWER LEG. REMOVED CORROSION AND INSTALLED STRINGER REPAIR PER SRM 53-10-3.

Part: FLOOR BEAM — CORROSION (BS 312)

MAIN CARGO CORROSION ON FLOOR BEAM AT STA 312 LBL 19. INSTALLED AND COMPLETED FLOOR BEAM REPAIR STA 312 LBL 19 PER SRM 53-10-8.

Part: WINDOW POST — CRACKED (NR 1 WINDOW)

CRACK AT F/O'S NR 1 WINDOW O/B POST AT UPPER CORNER. CRACK LENGTH VERIFIED BY NDT HFEC, CRACK WAS STOP DRILLED AND VERIFIED BY NDT HFEC REPAIR DOUBLER INSTALLED PER SRM 53-30-3.

Part: STRINGER — CORROSION (BS 720)

NR0440, FWD CARGO BS 720 STR 23R HEAVY CORROSION INSIDE STR ON LOWER LEG. *S/D* REMOVED CORROSION AND INSTALLED STRINGER REPAIR PER 53-10-3.

Part: FLOOR BEAM — CORROSION (BS 600)

NR0436, FWD CARGO BS 600 BL 0 TO RBL 24 HEAVY CORROSION ON LOWER SIDE OF LOWER LEG OF MAIN CARGO FLOOR BEAM. *S/D* INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8.

Part: FITTING — CRACKED (BS 740)

STR END FITTING CRACKED STA 740 STR 5R. REMOVED AND REPLACED STR END FITTING PER 51-10-01.

Part: SPLICE BOLTS — CORRODED (BS 360)

NR0879 STA 360 STR 26 LT AND RT SEVERAL SPLICE BOLTS ARE HEAVILY CORRODED AND NUTS FOR THE BOLTS ALSO CORRODED.

Part: SPAR WEB — CORRODED (WS 870)

CTR FUEL TANK BAY 3, AFT SPAR WEB AT STA 870 BULGED, CRACKED AND CORRODED WITH POPPED RIVETS AT APPROX LBL 40 NEAR UPPER CHORD ANGLE. UPPER CHORD ANGLE HAS POPPED RIVETS IN THIS AREA ALSO.

Part: SKATE ANGLE — CORROSION (BS 294-312)

NR0875 AND 0949, STA 294 TO 312 LT SIDE OF DOGHOUSE NOSE W/W BELOW FLOOR PANEL HAS CORROSION ON SKATE ANGLE LWR I/B SECTION OF TORQUE BOX NR0875. LT SKATE ANGLE AT STA 294.5 TO 298 HEAVY CORROSION ON VERTICAL SIDE OF SKATE ANGLE NR0949.

Part: SKATE ANGLE — CORROSION (BS 294)

NR0867 AND 0868, STA 294 RT SIDE OF DOGHOUSE BELOW FLOOR PANEL CORROSION IN LWR FWD CORNER BELOW NUT AND BEHIND SEALANT - NR0867 STA 294 R/H SIDE OF DOGHOUSE, BELOW FLOOR PANEL CORROSION ON ANGLE THAT ATTACHS TO DOGHOUSE LWR FWD AREA SKATE ANGLE NR0868. *S/D* FOR NR0868 REMOVED AND REPLACED SKATE ANGLE WITH NEW SKATE ANGLE PER SRM 53-10-04.

Part: INDICATOR — MALFUNCTIONED (NLG DOWN)

CYCLED THE GEAR 3 TIMES BEFORE NOSE GEAR IND DOWN. REMOVED AND REPLACED NLG POS PER MM 32-61-21, CYCLED GEAR PER 7-11-0 AND ALL IND NORMAL.