N426FE

Part: ENGINE — FAILED (NR 1) · airframe 42,239 hrs · 28,580 cycles

DURING CLIMBOUT, NR 1 ENGINE OVERTEMPED. HEARD A LOUD POP WITH A YAW TO THE LEFT. ALL ENG INDICATIONS WERE NORMAL EXCEPT EGT WHICH WAS 700 DEGREES HIGHER THEN NR 2 EGT, NR 1 EGT STAYED BEWTEEN 600 TO 700 DEGREES. DURING RETURN, MAX EGT 1000 FT. REMOVED AND REPLACED NR 1 ENGINE. LEAK AND OPS CHECKED GOOD.

Part: SPAR — DAMAGED (ZONE 400) · airframe 42,135 hrs · 28,516 cycles

RT PYLON LWR SPAR BETWEEN RIBS 6 AND 7. REPAIRED IAW EA 6-5450-117917C, PART 2. COMPLIED WITH EA 6-5450-117917C PART2. REMOVED AND INSTALLED THE REPAIR DOUBLER FOR NDT INSPECTION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,135 hrs · 28,516 cycles

LT WING ROOT CENTER WING BOX BOTTOM SKIN LWR SURFACE FOUND CORRODED BETWEEN FR44-45. REMOVED CORROSION IAW SRM 51-74-10. REPAIRED EA 6-5710-T0301458.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,135 hrs · 28,516 cycles

BULK CARGO DOOR SILL FOUND CORROSION SURROUNDING FASTENER HOLES BETWEEN FR 68 & 69. REPLACED SILL IAW SRM 51-40-21.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,135 hrs · 28,516 cycles

MAIN DECK FR 12A-15A Y1456 FLOOR SUPPORT CORRODED. REPAIRED THE FLOOR SUPPORT IAW SRM 53-12-15/201, FIG 207.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,135 hrs · 28,516 cycles

MAIN DECK FR 14-14B, Y730, FLOOR SUPPORT CORRODED. REPAIRED FLOOR SUPPORT IAW SRM 53-12-15/201, FIG 207.

Part: BUFFER — BINDING (TE FLAP) · airframe 41,799 hrs · 28,297 cycles

DURING CLIMBOUT, FLAP VANE JAMMED. HANDLE WAS AT SLATS/FLAPS POS 15/0 . SLATS/FLAPS INDICATED 15/5. FLAPS SYS 1 AND SYS 2 FAULT LIGHTS ON. SLATS/FLAPS EXTENDED NORMALLY FOR LANDING. SFCC NR 1 AND SFCC NR 2 BOTH FAULTED " LT VANE OUT ". EFCU NR 1 FAULTS M1 , 3 , 7, EFCU NR 2, NO FAULTS. DURING VANE BINDING DETECTOR UNIT INSPECTION CHECK, FOUND LT EXTENDED DETECTOR UNIT 37CV "Y" GAP MEASUREMENT OUT OF TOLERANCE IAW MM 27-56-15-06. CONTINUING WITH VANE OPERATING MECHANISM INSPECTON CHECK IAW MM 27-50-16-06. FOUND THAT LT OTBD BUFFER ASSY WAS OUT OF LIMITS. R & R LT OTBD BUFFER ASSY AND SWITCH (37CV) IAW MM 27-56-15-04. INBD BUFFER ASSY CHECKED GOOD. VERIFIY THE RIG ON THE INBD BUFFER SWITCH (41CV). RIG CHECKED GOOD. VERIFIED RIG ON THE CENTER RETRACT SWITCH AND ASSY(39CV). CHECKED GOOD. RIG CHECK OF SWITCHES IAW MM 27-56-15-6. PREFORMED OP'S CHECK ON LT WING VANE EXTEND AND RETRACT SWITCHES IAW MM 27-56-15-05. SWITCHES OPS CHECKED GOOD.

Part: SWITCH — MALFUNCTIONED (TE FLAPS) · airframe 41,797 hrs · 28,295 cycles

DEPARTING & DURING FLAP RETRACTION, RECEIVED AN ECAM ALERT "FLAPS VANE JAM". COMPLIED WITH QRH, CYCLED THE FLAPS, AND UNABLE TO FIX PROBLEM. RETURNED TO DEPARTURE. FOUND BOTH NR 1 & NR 2 SFCC'S FAULTED "LT VANE IN 2" ON ARRIVAL. RESET BOTH SFCC'S & RETRACTED FLAPS. ALSO CYCLED FLAPS TO 40 & FULLY RETRACTED WITHOUT ANY FAULTS. TROUBLESHOT IAW TSM 27-50-16 CHECKED ADJUSTMENT OF FLAP VANE DETECTOR UNIT 39CV ALL CHECKED NORMAL. R & R VANE RETRACTED SWITCH 39 CV PRECAUTIONARY BECAUSE BOTH SFCC FAULTED SAME SWITCH IAW M/M 27-56-15-05. C/W OPERATIONAL TEST OF FLAPS IAW M/M 27-54-00-05 ALL OPS CHECKS NORMAL A/C OK FOR SERVICE.

Part: BRACKET — WORN (FUSELAGE) · airframe 40,377 hrs · 27,292 cycles

PERFORM W/C 47C0201 FOUND NLG MAIN DOOR RT SELECTOR VALVE FIXED BRACKET THREAD WORN OUT. REMOVED THE WORN OUT BRACKET, THEN INSTALLED A NEW ONE FOR REPLACEMENT IAW EA NR6-3220-150288 (LANDING GEARS, NOSE GEAR AND DOORS: SHAFT INSTALLATION, THREAD DAMAGE ON NLG HATCH UNLOCKING SUPORT, REPAIR). REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED MINOR.

Part: PANEL — MISREPAIRED (ZONE 100) · airframe 40,377 hrs · 27,292 cycles

DOUBLER HAD TO BE REMOVED. PERFORMED FUSELAGE, PLATES AND SKIN: RT FUSE SKIN PANEL, FR54, STR 44R, REDUNDANT FASTENER, PERMANENT REPAIR DURING PERFORMED 41 X 5141 ALI STEP ID. ONE FASTENER IS COVERED BY DOUBLER IAW EA NR 6-5330-1502 81.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 40,377 hrs · 27,292 cycles

MAIN DECK COMPT FLOOR AREA FOUND CROSSBEAM GOT A CRACK AT FR 42 LOCATION BETWEEN -Y450 AND -Y953. REMOVED THE NR 242RH. NR 242QJ, NR 242SH FLOOR PANELS FOR CROSSBEAM REPLACEMENT IAW AMM 53-10-25-4. R & R THE CROSSBEAM WITH CHECK OK FOR SERVICE IAW SRM 51-72-10. REINSTALLED THE NR 242RH, NR 242QJ, NR 242SH FLOOR PANELS TO NORMAL CONDITION IAW AMM 53-10-25-4.

Part: RIB — CRACKED (ZONE 100) · airframe 40,377 hrs · 27,292 cycles

REAR FUSELAGE INTERNAL FOUND 1 RIB CRACKED AT FR86 STR32R. REMOVED THE CRACKED RIB. FABRICATED A NEW RIB FOR REPLACEMENT IAW SRM 51-72-10 AND IAW DWG A53986743205.

Part: SKIN — CORRODED · airframe 40,377 hrs · 27,292 cycles

LT WING FOR SKIN GOT CORROSION AT STA 845 SURROUND GROUNDING STUD (RIB 13-14, STR7-8).

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 40,377 hrs · 27,292 cycles

UPPER SUPPORT CROSSBEAM GOT CORROSION AT FR86 STG R12L. REPLACED THE DAMAGED CROSSBEAM BY NEW ONE IAW SRM 51-40-21. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED MINOR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,377 hrs · 27,292 cycles

UPPER SUPPORT STRUCTURE GOT MINOR CORROSION AT FR86 STG 12R. REMOVED THE CORRODED CROSS BEAM. FABRICATED A NEW CROSS BEAM I.A.W. DRAWING NO.: A53988624201. INSTALLED THE NEW CROSS BEAM FOR REPLACING.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 40,377 hrs · 27,292 cycles

RIGHT WING UPPER SURFACE FOUND CORROSION POSITION AT O /B GROUND POINT ABOUT RIB 27-28 PERFORMED WINGS, SKIN AND PLATES: PERMANENT REPAIR REF. TO EA 6-5730-150286. PER GMM 6-2-100 CLASSIFIED MAJOR.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED (NR 2) · airframe 39,834 hrs · 26,880 cycles

ON TAKE OFF WITH ONLY NR 2 ATS OPERATIVE, THE NR 2 THROTTLE KEPT TRYING TO ADVANCE TO FIREWALL AFTER 90 KNOTS, EGT WENT UP TO 940, T/0 ABORTED AT 100 KIAS, BRAKES COOLED, AUTOTHROTTLE OFF TAKEOFF ACCOMPLISHED. PERFORMED CROSSLOAD FROM NR 1 FMC. ALSO PERFORMED AFS LAND TEST WITH NO FAULTS NOTED.

Part: SEQUENCE VALVE — MALFUNCTIONED (NLG) · airframe 38,615 hrs · 25,998 cycles

UNSAFE NOSE GEAR INDICATION/MANUAL CRANK DOWN. JACK ADAPTER AND TEST BOX SHIPPED FROM LAX, T/S TO SEQUENCE VALVE AND RT NOSE GEAR ACTUATOR. BOTH REPLACED PER 32-31-16-4 AND 32-31-18-4. OPS AND LEAK CHECKS GOOD PER 32-30-158. ALSO, PERFORMED FREE FALL ACTUATION PER 32-33-00-2. ALL ACTUATION NORMAL. RESTORED AIRCRAFT BACK TO NORMAL CONFIGURATION. A/C OK FOR SERVICE.

Part: FRAME — CRACKED (ZONE 200) · airframe 38,587 hrs · 25,973 cycles

FUSELAGE MAIN FRAME FRAME FOOT 45 RIGHT SIDE ,INSTALL 1ONE CADMIUM PLATED SHOULDERED BUSH MADE OF STAINLESS STEEL 17-4PH REQUESTED BY E.A 6-5310-123911. FABED BUSHING ON MAE TRAVELER T8/761893, INSTALLED PER E.A 6-5310-123911

Part: FRAME — CRACKED (ZONE 200) · airframe 38,587 hrs · 25,973 cycles

CENTER FUSELAGE ZONE 12 REINFORCE THE UPPER FRAME BASE TO ARCH STRUCTURE AT FRAME 45 FASTENER HOLE CRACKED ON FR4AME FOOT, RIGHT SIDE. COMPLIED WITH E.A 6-5310-123911.

Part: FRAME — CRACKED (ZONE 200) · corrosion level 3 · airframe 38,587 hrs · 25,973 cycles

MAIN DECK REINFORCE UPPER FRAME BASE TO ARCHES JUNCTIONS FRAME FOOT 46 LEFT, REWORK HOLES 23, 26, 27 BY E.A 6-5310-123911. REAMED HOLES 23, 26,& 27. TO .433. BUSHINGS FABED ON TRAVELER T8/762882, BUSHINGS INSTALLED IAW E.A 6-5310-123911

Part: FRAME — CRACKED (ZONE 200) · airframe 38,587 hrs · 25,973 cycles

CENTER FUSELAGE ZONE 20 REINFORCE THE UPPER FRAME BASE TO ARCH JUNCTION AT FRAME 44 FASTENER HOLE CRACKED ON FRAME FOOT FITTING. COMPLIED WITH E.A 6-5310-123911.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,587 hrs · 25,973 cycles

CENTER FUSELAGE ZONE 20 - REINFORCE THE UPPER FRAME JUNCTION AT FR 46 LT FASTENERS HOLES CRACKED ON FRAME FOOT FITTING. REMOVED FRAME FOOT IAW SRM 51-40-21. RE-INSTALLED FRAME FOOT PER EA 6-5310-123911 & SRM 51-40-21, INSTALLED BUSHINGS PER EA 6-5310-123911.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 38,587 hrs · 25,973 cycles

LEFT AFT PAX DOOR CUTOUT LOWER AFT DOOR STOP FITTING HAS CORROSION UNDER IT. REMOVED AND REPLACED THE LT AFT PAX DOOR CUTOUT AFT FRAME IAW SRM 51-40-21. PREPPED AND PAINTED IAW AMM 51-75-10-8, PERFORMED DOOR STOP ADJUSTMENT CHECK IAW AMM 52-10-11-5 CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,587 hrs · 25,973 cycles

LOWER FUSELAGE LT FR 18 TO FR 23 BETWEEN STR 37 AND STR 39 HAS 6 LIGHTNING STRIKES. REWORKED LIGHTNING STRIKES IAW SRM 51-40-21, 51-10-30, AND 51-10-10. TREATED AND PRIMED IAW 51-21-10, PAINTED IAW MM 51-75-10.

Part: SKIN — GOUGED (FUSELAGE) · airframe 38,587 hrs · 25,973 cycles

LOWER FUSELAGE FWD CARGO DOOR CUTOUT FWD LOWER EDGE BELOW REPAIR DOUBLER HAS SKIN GOUGES 5 INCH LONG. BLENDED AREA FOUND TO BE WITH IN LIMITS IAW SRM 53-10-12, AND 51-73-10 FIG 201. TREATED, PRIMED AND PAINTED IAW SRM 51-21-10, AND MM 51-75-10-8.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 38,587 hrs · 25,973 cycles

VERTICAL STABILIZER FWD RT LOWER CHORD ANGLE HAS A 6.5 INCH CRACK. REMOVED AND REPLACED CHORD ANGLE IAW SRM 51-40-21.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 38,587 hrs · 25,973 cycles

MAIN DECK RT SIDE BETWEEN FR 13 AND FR 13 A, ATTACH ANGLE ABOVE GALLEY SIDE FITTING HAS A CRACK. REMOVED AND REPLACED FRAME FITTING BETWEEN FR13 AND 13A IAW SRM 51-40-00 AND 51-40-21.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 38,587 hrs · 25,973 cycles

VERT STAB ATTACH FITTING CORROSION L AND R SIDE. COMPLIED WITH EA 6-5536-110931 RII:680053. COMPLIED WITH EA 6-5536-110931.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 38,587 hrs · 25,973 cycles

FUSELAGE CENTER SECTION ZONE 240 LT/SIDE EMERGENCY EXIT LOWER JAMB, AT FRAME 43 TOP ANGLE SUPPORT HAS CRACK. REMOVED AND INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-21.

Part: SUPPORT ANGLE — CRACKED · airframe 38,587 hrs · 25,973 cycles

FUSELAGE CENTER SECTION ZONE 240 RT/SIDE EMERGENCY EXIT LOWER JAMB AT FRAME 43,TOP ANGLE SUPPORT HAS CRACK. REMOVED AND INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-21.

Part: SENSOR — FAILED (AOA) · airframe 37,437 hrs · 25,193 cycles

RTO AT 100KTS , NAV ADC 1 FAILURE WITH ASSOCIATED WARNINGS. SWAPPED 1 ANGLE OF ATTACK AND NR 3 ANGLE OF ATTACK, PER AMM 34-11-19-4. PERFORMED ALPHA PROBE TEST AND AFS/ LAND TEST NO FAULT OR FAILURES. PER TSM 22-00-00. R/I FROM FACT SWAP COMPONENT POSITIONS FROM POSITION 3 TO POSITION 1 SWAPPED NR 1 AND NR 3 AOA SENSORS. PLACED NR 3 AOA ON MEL. REF WRI 34-18-8810.

Part: SYMBOL GENERATOR — FAILED (NR 1) · airframe 36,674 hrs · 24,743 cycles

ON TAKEOFF ROLL, NR 1 EFIS SGU FAILED. BOTH PFD AND ND HAD DIAGONAL LINES ON THE CAPTAINS SIDE "MEL 34-73-01: EFIS SGU (IDENTIFY 2 OR 3) NR 3 INOP." BY LGB MX. SWAPPED NR 1 AND 3. REMOVED AND REPLACED NR 3 EFIS SGU IAW M/M 34-73-34-4. ALL OPS CHECKS NORMAL A/C OK FOR SERVICE. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION.

Part: POWER CABLE — FAULTY (COCKPIT) · airframe 36,542 hrs · 24,676 cycles

PDIS 426 30-40 0008213 28JUL06 MEM, SMOKE IN COCKPIT DUE TO OVERHEAT OF RT WINDOW HEAT COILED POWER CORD. RAM AIR VALVE OPENED AND COURIER 02 MAN OVERRIDE SELECTED ON. COURIER 02 SYSTEM RESET AND RAM AIR DOOR CLOSED. ACN RELEASED FOR SERVICE IAW MEL/CDL: 30-42-01-01-A CATEGORY: C EXPIRATION: 07AUG06 (MEL 30-42-01-01-A: RT SIDE WINDOW HEAT - INOP.) UPDATED MPN E0385HH, CPN 5610228 QTY 1, CORD, MSN 998250, UPDATED MPN NSA935805-09, CPN 0117006 QTY 2, CONDUIT, MSN 998251.

Part: REPAIR — MISINSTALLED (TE FLAP) · airframe 36,207 hrs · 24,483 cycles

PREVIOUS REPAIR INSTALLED ON LT ELEVATOR STA 604/ER26 UPPER SURFACE T/E WEDGE UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION. NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 55-21-11. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: FLANGE — BENT (FUSLELAGE) · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. LOWER FLANGE AFT SIDE BEND FR 60 FR 3249, - Y214. PERFORMED PART 1 OF FEDEX EA 6-5310-97865, NO CRACKS FOUND. EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: REPAIR — UNKNOWN · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE ON RT AFT PIT CROSSBEAM AT FR 65 TO FR 65 FS 3514 TO FS 3514, AND -Y20 UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-15 FIG 207. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE ON RT MCD SEAT TRACK BETWEEN FR 62 TO FR 63 FS 3355 TO FS 3408, AT -145. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-16 FIG 202. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: STRUCTURE — DAMAGED (L/E SLAT) · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS BLEND REPAIR 3 EACH ON RT SIDE NR 2 L/E SLAT TRAILING EDGE UNABLE TO DETERMINE APPROVED REPAIR. DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED PER EA 6-5750-95703 FEDEX REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON FWD PIT CROSSBEAM AT FR 25 TO FR 25, FS 1711 TO FS 1711 AND Y72 TO Y72. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-15 FIG 201. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND AFT PIT CROSSBEAM AT FR 65 TO FR 65, FS 3514 TO FS 3514 AND Y 20. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-15 FIG 207. REPAIR EVALUATED PER GMM 6-2-100.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND MCD FLOORBEAM AT FR 37 TO FR 37, FS 2029 TO FS 2029 AND YE 57 TO YD 81. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM SUPPLEMENT 53-10-15 FIG 201 SHEET 2. REPAIR EVALUATED PER GMM 6 -2-100 AND CLASSIFIED AS MINOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND MCD FLOORBEAM AT FR 12A TO FR 13, FS 1091 TO FS 1128 AND YD 95.3. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-12-15 FIG 207. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON LEFT HAND MCD SEAT TRACK AT FR 54.3 TO FR 55/58, FS 3090 TO FS 3143, AT - YD95.3. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-16 FIG 202 SUPPLEMENT REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — UNKNOWN · airframe 36,207 hrs · 24,483 cycles

PREVIOUS REPAIR INSTALLED ON RIGHT HAND MCD FLOORBEAM AT FR 12A TO FR 13, FS 1091 TO FS 1125 AND -YC 145.6. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-12-15 FIG 207. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND MCD FLOORBEAM AT FR 14 TO FR 14C, FS 1204 TO FS 1232 AND YB 195.9. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED PER SRM 53-12-15 FIG 207. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND MCD FLOORBEAM AT FR 15A TO FR 16A, FS 1245 TO FS 1267 AND -YB 195.9. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRACK REPLACED PER SRM 51-72-10 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — UNKNOWN · airframe 36,207 hrs · 24,483 cycles

PREVIOUS REPAIR INSTALLED ON RIGHT HAND AFT PIT CROSSBEAM AT FR 64 TO FR 64, FS 3461 TO FS 3461 AND -Y 117. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPLACED PER SRM 51-40-21 AND 51-72-10 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 39 TO FR 39, FS 2227 TO FS 2265, STR 35 TO STR 35. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO EO FEDEX 6-5310-7-3315 P3. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — MISINSTALLED (FUSELAGE4) · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 63 TO FR 64, FS 3408 TO FS 3461, STR 39 TO STR 41, AND AFT OF AFT CARGO DOOR CUTOUT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED PER SRM 53-17-12 FIG 203 AND 51-40-21. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 80/82 TO FR 83, FS 4370 TO FS 4430, STR 32 TO STR 34. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-12 FIG 225 SHEET 2. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — UNKNOWN · airframe 36,207 hrs · 24,483 cycles

PREVIOUS REPAIR INSTALLED AT FUSELAGE CROWN LEFT HAND SIDE AT FR 40/41 TO FR 40/41, FS 2294 TO FS 2294, STR 2 TO STR 3. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED PER SRM 53-10-12 FIG. 225 SHT1 AND E.A. 6-5310-95709 FEDEX REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — UNKNOWN · airframe 36,207 hrs · 24,483 cycles

PREVIOUS REPAIR INSTALLED ON LT OUTBOARD FLAP LOWER SURFACE BETWEEN FLAP RIB 4 AND 5 AT WS 1010 TO WS 1030. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED INSTALLED ON LT OUTB FLAP E.A. 6-5750-90224 FEDEX REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 64 TO FR 64, FS 3451 TO FS 3471, STR 7 TO STR 8 AND AFT AND BELOW UPPER AFT ANTENNA. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-12 FIG 225 SHEET 3. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 12 TO FR 12A, FS 1067 TO FS 1091, AND LOCATED ON TOILET SERVICE PANEL. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 52-42-11 FIG 201. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 12A TO FR 12A, FS 1081 TO FS 1101, AND LOCATED ABOVE TOILET SERVICE PANEL. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-12-12 FIG 202. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: REPAIR — UNKNOWN · airframe 36,207 hrs · 24,483 cycles

PREVIOUS REPAIR INSTALLED ON LEFT HAND INBOARD FLAP UPPER TRAILING EDGE WEDGE, WS 40 TO WS 86. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGE WAS REPLACED PER SRM 51-72-10 AND 51-40-21,51-40-44 AND E.A. 6-5710-97864 FEDEX REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 73 TO FR 74, FS 3938 TO FS 3998, STR 29 TO STR 31 AND BELOW L2 DOOR. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-12 FIG 225 SHEET 1. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 73A TO FR 73A, FS 3964 TO FS 3964, STR 23 TO STR 24, AND FWD OF R2 DOOR CUTOUT LOWER FAIL SAFE RING. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-18-18 FIG 201. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

PREVIOUS REPAIR INSTALLED ON LEFT HAND INBOARD FLAP UPPER TRAILING EDGE WEDGE, WS 145 TO WS 177. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGE WAS REPLACED PER SRM 51-72-10 AND 51-40-21,51-40-44 AND E.A. 6-5710-97864 FEDEX REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 77 TO FR 77, FS 4181 TO FS 4181, STR 28 TO STR 29. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-12 FIG 225 SHEET 1. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON R2 DOOR AT FR 74 TO FR 74, FS 3998 TO FS 4024, STR 26 TO STR 27. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-12-00 FIG 204. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND MDC FLOORBEAM AT FR 12A/13, FS 1091/1125, AT YD953. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-12-15 FIG 207. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — UNKNOWN (TE FLAP) · airframe 36,207 hrs · 24,483 cycles

PREVIOUS REPAIR INSTALLED ON RIGHT INBOARD FLAP LOWER TRAILING EDGE WEDGE, WS 163 TO WS 189. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED & EVALUATED PER SRM 57-52-12 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND SIDE NUMBER THREE SLAT OUTBOARD END, WS 1868 TO WS 1868. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 57-44-11 FIG 201. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: REPAIR — UNKNOWN · airframe 36,207 hrs · 24,483 cycles

PREVIOUS REPAIR INSTALLED ON RIGHT HAND NUMBER TWO SPOILER UPPER OUTBOARD END AT WS 339 TO WS 359. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED AT NR 2 SPOILER (RT WING) PER SRM 57-70-00 FIG. 218 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 60 TO FR 60, FS 3249 TO FS 3249, STR 39 TO STR 41, AND FWD OF AFT CARGO DOOR CUTOUT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT. INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM PER SRM 53-17-12 FIG 201. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 67 TO FR 68, FS 3620 TO FS 3670, STR 47 TO STR 47 AND BELOW BULK CARGO DOOR. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO FEDEX EA 6-5300-86140 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 38.1 TO FR 38.2, FS 2135 TO FS 2188, STR 46 TO STR 47, ON CUTOUT OF POTABLE WATER SERVICE PANEL. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM PER SRM 53-14-12 FIG 202 SHEET 3. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 75A TO FR 75A, FS 4095 TO FS 4095, STR 23 TO STR 24, AND AFT OF R2 DOOR CUTOUT LOWER FAIL SAFE RING. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-18-18 FIG 201. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE CROWN RIGHT HAND SIDE AT FR 10 TO FR 10, FS 962 TO FS 982. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-11-12 FIG 202. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED ON RIGHT HAND SIDE OF LOWER WING SURFACE INBOARD OF WING TIP, RIB 31, WS 1868. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND PER FEDEX EA 6-5720-85-503. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 87 TO FR 87, FS 4625 TO FS 4645, STR 8 TO STR 8. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-13 FIG 225 SHEET 3. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — UNKNOWN · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR INSTALLED ON RIGHT OUTBOARD FLAP RIB 15 TO RIB 15, WS 925 TO WS 935. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED & EVALUATED PER SRM 57-32-12 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR"

Part: REPAIR — UNKNOWN · airframe 36,207 hrs · 24,483 cycles

PREVIOUS REPAIR INSTALLED ON LEFT HAND INBOARD FLAP LOWER TRAILING EDGE WEDGE, WS 140 TO WS 185. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGE WAS REPLACED PER SRM 51-72-10 AND 51-40-21,51-40-44 AND E.A. 6-5710-97864 FEDEX REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — UNKNOWN · airframe 36,207 hrs · 24,483 cycles

PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 20 TO FR 20, FS 1446 TO FS 1446, STR 36 TO STR 40, AND FWD LOWER SIDE OF FWD CARGO DOOR CUTOUT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED PER SRM 53-13-13 FIG. 201 SHEET 1 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — MISINSTALLED (FUSELAGE) · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE AT FR 9 TO FR 10, FS 949 TO FS 972, AND AFT OF LEFT HAND LOWER PITOT TUBE. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED PER SRM 53-11-12 FIG 202 SHEET 1 AND FEDEX EA 6-5310-95705. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 37 TO FR 38.2, FS 2029 TO FS 2082, STR 26 TO STR 26. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-12 FIG 225 SHEET 1. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE · airframe 36,207 hrs · 24,483 cycles

COMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 16A TO 16A, FS 1260 TO FS 1285 AND 150CM BELOW R1 DOOR. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED PER SRM 53-12-12 FIG 201 SHEET 1 & FEDEX EA 6-5310-95701. REPAIR EVALUATED PER GMM 6-2-10 AND CLASSIFIED AS MAJOR.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 33,324 hrs · 22,688 cycles

AT 23,000 FT WHILE ACCEL, FELT AIRFRAME VIB AND RETURNED. FOUND NR 1 VERT, LE, FIN ASSY DAMAGED. COAX ENDS PULLED FROM MOUNT, NUMEROUS FIBERGLASS SUPPORTS BROKEN, ANTENNA CONDUIT BENT AND STANDOFFS BROKEN. THIS INCLUDES ANTENNA ITSELF. FOUND STIFFENER 4.5 AND 5 BENT AND STIFFENER 5 CRACKED. STRAIGHTENED 4.5 STIFFENER AND AWAITING EA FOR STOP DRILL REPAIR OF NR 5 STIFFENER. FIN ASSY BUTT STRAP AND SUPPORT WEB BENT AND TORN. FIN ASSY UPPER EDGE FASTENER HOLES TORN THROUGH. REMOVED VERT STAB ACCESS PANELS, REMOVED DAMAGED FIN ASSY AND VERTICAL LE. DRILLED UP NEW FIN ASSY. INSTALLED DORSAL FIN ASSY. INSTALLED FWD, LEFT AND RIGHT VERTICAL STABILIZER SIDE FAIRINGS.

Part: SWITCH — FAILED (NLG) · airframe 33,102 hrs · 22,553 cycles

GO-AROUND DUE TO ONLY 2 GREEN LANDING GEAR LIGHT ON FORWARD LANDING GEAR PANEL, OVERHEAD LANDING PANEL 3 GREEN AS NORMAL. DURING GO-AROUND FORWARD GREEN NOSE GEAR LIGHT CAME ON. NORMAL LANDING ON SECOND PASS. LANDING GEAR INDICATING PANELS SYSTEM NR 1 NOSE GEAR DOWN LOCK INDICATOR INOPERATIVE. REMOVED AND REPLACED MICRO SWITCH 40GB IAW AMM. OPS CHECK NORMAL.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 31,839 hrs · 21,779 cycles

ON CLIMBOUT FWD BELLY CARGO DOOR WARNING CAME ON.

Part: WIRE — FAILED (ELECTRICAL) · airframe 30,817 hrs · 21,126 cycles

A/C WILL NOT ACCEPT EXTERNAL POWER. FOUND GPCU CB POPPED. FOUND WIRES BURNT THRU IN 101VU, BURNED A HOLE THROUGH BACK PANEL. CRIMPED NEW 2432-0025, 0026 AND 2432-0027 IN 101VU PNL TERMINAL PER MM 20-25-26.

Part: PMC — OVERLIMIT (NR 2 ENGINE)

DESTINATION THRU FL310 HAD ECAM MSG ENG 2 OVERLIMIT. IND WERE EVIDENT IN N1, EGT, N2 AND HI FF. PULLED THROTTLE TO IDLE & OVERLIMIT ABATED BUT NR 2 STILL MUCH HIGHER THAN ENG NR 1. DFDR VERIFICATION CONFIRMED OVERLIMIT (EGT, N1, N2). PERFORMED BORESCOPE PER MM NO LIMITING DEFECTS NOTED. REMOVED AND REPLACED NR 2 ENG PMC, PERFORMED TEST PER MM 73-23-00.

Part: ELECT UNIT — FAILED (NR 2 PITCH TRIM)

99-145 NR 2 PITCH TRIM LEVER WILL NOT REMAIN ENGAGED. NR 1 ATS LEVER WILL NOT REMAIN ENGAGED, NR 2 FD INOP. REMOVED AND REPLACED PROX ELEC UNIT IAW 32-31-71 SYS FND CK GOOD AND AFS TEST NORM IAW 22-00-00.

Part: VALVE — FAILED (E & E COMPT)

EQUIP COOLING OVBD VALVE FAILED TO CLOSE, COULD NOT PRESSURIZE CABIN. *S/D* REPLACED AIRFLOW SENSOR DET MM 21-23-00. REMOVED AND REPLACED COOLING OVBD EXTRACTION VALVE MM 21-23-13.

Part: DUCT — FAILED (NR 1 ENGINE)

CLIMBING THRU 10,000 FT GOT NR 1 ENG NACELLE TEMP ADVISORY, TEMP AT 95 CELSIUS. CLOSED BLEED, NO HELP. OPENED NR 1 BLEED AND RETARDED THROTTLE AND TEMP DECREASED. RESUMED CLIMB POWER AND TEMP AGAIN INCREASED TO 110C. FOUND HPT RECOUP DUCT BLOWN. REMOVED AND REPLACED DUCT. RAN ENGINE PER JRH. OPS CHECK OK.

Part: HYD LINE — LEAKING (GREEN HYD SYST)

GREEN HYDRAULIC SYSTEM LEAK INTO CAUTION ZONE. REPAIRED LEAKING GREEN SYSTEM PRESSURE LINE IN AFT SECTION OF NR 1 ENGINE PYLON PER E.A. 6-29 10-27643. SERVICED AND LEAK CHECKED OK.