N952FD

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 34,971 hrs · 24,368 cycles

RH PYLON BOLT HOLE #2 HAS DAMAGE INDICATION. CLEANED HOLE #2 BY REAMING TO .624 IAW SRM 51-40-05 AND EA # F-5730-T0368661 P1. PERFORMED ROTO-PROBE AT HOLE #2 IAW NTM 51-00-16. NO DAMAGE NOTED. WING- PLATES AND SKINS-RH WING, UPPER SKIN AND DRAG FITTING, HOLE 2 DAMAGE/ CORROSION REPAIR. ACCOMPLISHED STEPS 1-8 IAW EA F-5730-T0368661 P1. MAJOR REPAIR

Part: FRAME — CRACKED (ZONE 200) · airframe 34,971 hrs · 24,368 cycles

BS 1640 FUSELAGE FRAME WEB AT STRINGER S-14L HAS CRACK INDICATION NOTED, IN TOP INBOARD AND OUTBOARD HOLES AND BOTTOM OUTBOARD HOLE. COMPLIED WITH EA # F-5310-T0368467 P1 "FUSELAGE-MAINFRAME-FRAME 1640 AT S-14L HAS A CRACK INDICATIONS-REPAIR" MAJOR REPAIR

Part: SLIDE — INOPERATIVE (L1 DOOR) · airframe 33,787 hrs · 23,498 cycles

SLIDE RAFT DEPLOYED UPON GROUND OPENING L1 DOOR FROM THE OUTSIDE. REMOVED AND REPLACED L-1 DOOR SLIDE, IAW AMM 52-11-25-5. STILL REQUIRES GIRT BAR RIG/ADJUSTMENT AND OPERATIONS CHECK. REMOVED AND INSTALLED NEW GIRT BAR ASSEMBLY ON L1 DOOR SLIDE FOR BINDING WHILE DISENGAGING, REF 757 AMM 25-66-10-2. ACCOMPLISHED L1 GIRT BAR TEST, REF 757 AMM 52-11-25-5. VERIFIED EXTERNAL SLIDE DISENGAGMENT WITH EXTERIOR DOOR HANDLE, REF 757 AMM 52-11-00-6-0. AC OK FOR SERVICE.

Part: COMPRESSOR — CORRODED (NR 2 ENGINE) · corrosion level 3 · airframe 33,682 hrs · 23,413 cycles

`#2 ENGINE COMPRESSOR CASING FWD MOST FRAME FLANGE HAS AREAS OF CORROSION AROUND THE REMOVED #2 ENGINE REF WORK CARD # 7180260-02-01 SEQ #172 AND REPLACED ENGINE REF WORK CARD # 7180260-02-02 SEQ # 173

Part: SKIN — CRACKED (LE SLAT) · airframe 33,292 hrs · 23,140 cycles

R/H WING # 9 SLAT LOWER COVE PANEL SKIN HAS A CRACK AT WS 594. REMOVED AND REINSTALLED #9 LEADING EDGE SLAT IAW B757 AMM 27-81-02-4, FABRICATED AND INSTALLED LOWER COVE PANEL IAW B757 SRM 51-40-02-06 AND B, DWGS. 114N4003, REV. E AND REV. B, B DWG : 114N4076 REV. C. PERFORMED SATISFACTORY OPERATIONAL CHECK LEADING SLAT AND FLAPS IAW B757 AMM 27-81-005 AND 27-51-005

Part: SKIN — CRACKED (LE SLAT) · airframe 33,292 hrs · 23,140 cycles

R/H WING # 9 SLAT LOWER COVE PANEL SKIN HAS CRACK AT WS 594.

Part: FILLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,292 hrs · 23,140 cycles

CORROSION FORWARD WET AREA STA 375 LBL 20 FLOOR SUPPORT CORRIER AREA. REMOVED CORROSION FWD WET AREA STA 375 LBL 20 FILLER IAW B 757 SRM 51-10-02-OG ORIGINAL MATERIAL .071",MAT REM .058",MAT LOSS .013" FOUND TO BE OUT OF LIMITS IAW B 75 757 SRM 53-00-51-1A FIG 101 DET VI.REMOVED FILLER IAW B 757 SRM 51-40-02-OG,FABRICATED & INSTALLED FILLER PER VENTURA AEROSPACE DWG 3471 REV B AND 3470 REV B

Part: FILLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,292 hrs · 23,140 cycles

CORROSION FORWARD WET AREA STA 375 LBL 20 FLOOR SUPPORT CORRIER AREA. REMOVED CORROSION FWD WET AREA STA 375 LBL 20 FILLER IAW B 757 SRM 51-10-02-OG ORIGINAL MATERIAL .071",MAT REM .058",MAT LOSS .013" FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-51-1A FIG 101 DET VI.REMOVED FILLER IAW B 757 SRM 51-40-02-OG,FABRICATED & INSTALLED FILLER PER VENTURA AEROSPACE DWG 3471 REV B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,292 hrs · 23,140 cycles

FWD CARGO PIT-R/H SIDE,FRAME 846 AT STR 22 RT. CRACKED AT FASTENER HOLE. REMOVED,FABRICATED AND INSTALLED STANCHION STUB (FRAME) ON FWD CARGO PIT R/H SIDE AT STA 846 BETWEEN STR-21R TO STR-26R IAW B 757 SRM 51-40-02-OG AND B. DWG : 143N5811, REV : - , REV : - J AND B. DWG : 143N5800, REV : C.

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 32,536 hrs · 22,576 cycles

DURING POST FLIGHT MX WALKAROUND FOUND THE INTERIOR EMERGENCY EXIT LIGHT ABOVE THE L1 DOOR INOP. REPLACED BATTERY CHARGER CPN 3311913 AND BATTERY CPN 3301128 IN POS M731, EMERGENCY LIGHT ABOVE L1 DOOR OPERATES NORMALLY PER B757 AMM 33-51-07

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 32,536 hrs · 22,576 cycles

DURING POST FLIGHT MX WALKAROUND FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP AFT OF THE L1 DOOR . REPLACED BATTERY CHARGER CPN 3311913 AND BATTERY CPN 3301128 POS M731, EMERGENCY LIGHT AFT OF L1 DOOR OPERATES NORMALLY PER B757 AMM 33-51-07. SEE WRI 33-50/6156 FOR PART REMOVAL/INSTALL

Part: UNKNOWN — ODOR (COCKPIT) · airframe 32,438 hrs · 22,508 cycles

AT FL 340, AIRCREW SMELLED A STRONG PUNGENT ODOR COMING FROM VENTS. IT WAS STRONG BUT NOT QUITE STRONG ENOUGH TO GO ON OXYGEN. RAN PACKS FOR 30 MINUTES AT MAX HEAT. NO UNUSUAL ODORS NOTED THROUGHOUT MAIN CARGO COMPARTMENT AND IN FLIGHT DECK. RAN BOTH ENG AT MAX STATIC EPR PER JRH & FIM 21-00-01-3 AND 71-00-00-5-3, SUPPLYING PACKS WITH ENG AIR FOR 10 MINUTES, NO SMELL FROM EITHER PACK 1 OR 2. INSPECTED PACK BAYS FOR LEAKS NON FOUND. NO ENG FLUID LEAKS NOTED. UNABLE TO RECREATE ODOR. REF FIM IF THERE IS NO SMOKE OR FUMES AND IF THE PROBLEM DOES NOT OCCUR ON THE SUBSEQUENT FLIGHT, THEN THERE WAS AN INTERMITTENT PROBLEM. FIM 21-00-01-3 P8.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT PAX DOOR) · airframe 32,264 hrs · 22,382 cycles

PDIS 952 52-10 5943 05DEC18 MEM FACT U LOGPAGES:2924671 MOMENTARY LEFT FORWARD ENTRY DOOR EICAS DURING CRUISE AT FL 360 PRESURIZATION NORMAL. FACT 05DEC18 05:50 MEM U COMPLIED WITH FIM 52-11 FAULT TREE 802. NO VISUAL DEFECTS NOTED. OPERATED L1 DOOR THROUGH ALL CYCLES NO DEFECTS NOTED . A/C HAS NO HISTORY IN 90 DAYS. A/C OK FOR SERVICE.

Part: STATIC LINE — OUT OF POSITION (ARMING LIGHT) · airframe 32,199 hrs · 22,343 cycles

RIGHT DOOR DISARM LIGHT WILL NOT COME ON. IT INITIALLY CAME ON, BUT NOW IT STAYS OUT. DOOR DIDNT FEEL NORMAL DURING DISARM. REMOVED R1 DOOR SLIDE COVER. FOUND SLIDE STATIC LINE SQUARE KNOT INTERFERANCE WITH GIRT BAR HANDLING MECHANISM AT FORWARD GIRT BAR FLOOR FITTING. PROPERLY ROUTED STATIC LINE PER MM, REINSTALLED GIRT BAR AND SLIDE COVER. ALL WORK ACCOMPLISHED REF B757 MM 25-66-01-4. SLIDE ARM / DISARM MECHANISM AND SLIDE ARM INDICATION OPS CHECK NORMAL REF MM 52-11-00-6 AND 25-66-01-4.

Part: SKIN — DENTED (NR 8 SLAT) · airframe 31,693 hrs · 22,016 cycles

LARGE DENT ON TOP OF THE NR 8 SLAT WEDGE. REPAIRED THE SLAT WEDGE IAW SRM 57-43-02-2R, FIG 201, AND SRM 51-70-10-2R, REPAIR 3 AND 4, SRM 51-70-10-2R, PARAGRAPH 20, AND EA F-5750-T0339954 P1.

Part: TRANSMITTER — FAILED (FLAP POSITION) · airframe 31,630 hrs · 21,972 cycles

AT 13000 FT AND 220 KNOTS, CALLED FOR FLAPS 1. RECEIVED A TE FLAP ASYM ON EICAS. RECEIVED TRAILING EDGE LIGHT ON THE PANEL, FLAP ASYM OCCURRED BETWEEN FLAPS UP AND FLAPS 1 INDICATION. COMPLETED QRH AND CONTINUED TO LANDING. ACCOMPLISHED FIM 27-51 FAULT TREE 805, FIG 104B TROUBLESHOOTING PROCEDURE, AND FOUND A BAD LT FLAP POSITION TRANSMITTER, R & R THE TRANSMITTER IAW AMM 27-58-03-4. FLAP SYSTEM OPS TESTED GOOD IAW AMM 27-51-00-5. ACFT GOOD FOR SERVICE.

Part: ROPE — EXPOSED (L1 DOOR) · airframe 31,279 hrs · 21,738 cycles

DOOR L1 HAD A PIECE OF EQUIPMENT EXPOSED AFTER CLOSING. RAMP PERSONNEL HAD US RE-OPEN DOOR TO SECURE. CALLED MX. SECURED DOOR SLIDE ROPE AND SLIDE COVER REF MM CH. 25-66-01-4. OK TO CONTINUE. OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,233 hrs · 21,707 cycles

R1 INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE M730 POWER SUPPLY BATTERY PACK IAW AMM 33-51-07-2, OPS CHECKED GOOD.

Part: PLUG — DETACHED (ENGINE GEARBOX) · airframe 30,908 hrs · 21,484 cycles

AT FL 350, THE RT ENG OIL PRESSURE ALERT ACTIVATED. OIL QTY RAPIDLY DECREASED TO ZERO. WINDMILLED FOR 30 MINUTES. FOUND THE ENGINE CUP PLUG HAD FALLEN OUT OF THE HIGH SPEED GEARBOX REINSTALLED THE PLUG, SERVICED OIL TANK, INSPECTED CHIP DETECTORS, NO METAL FOUND. STARTED AMM PROCEEDURE FOR ENGINE STOP IN FLT. AMM 757 71-00-00-6 COMPLETED STEP 4. REMOVED, INSPECTED AND REPLACED THE NR 2 ENGINE OIL SCAVENGE PUMP FILTER IAW MM 79-21-08-4. NO DEFECTS NOTED. ALSO INSPECTED AND REPLACED THE OIL PRESSURE FILLER IAW MM 79-21-07-4. NO DEFECTS NOTED. R & R THE DAMAGED CORE PLUG AND CUP WASHER IAW MM 71-00-00-6, ITEM 4C AND SERVICE BULLETIN 211-72-9578. LEAK AND OPS CHECKED GOOD. ENGINE RAN IAW JRH. REMOVED, INSPECTED, AND REPLACED THE NR 2 ENGINE OIL SCAVENGE PUMP FILTER IAW MM 79-21-08-4, NO DEFECTS NOTED. REMOVED, INSPECTED, AND REPLACED THE OIL PRESSURE FILTER IAW MM 79-21-07-4. NO DEFECTS NOTED.

Part: GUARD — BROKEN (TEST SWITCH) · airframe 30,773 hrs · 21,389 cycles

L1 DOOR EMERGENCY LIGHT TEST SWITCH GUARD IS MISSING. TEST SWITCH OPS NORMAL. PLASTIC FLANGE ON SWITCH IS BROKEN AND WILL NOT REMAIN FASTENED IN PLACE. WHILE TESTING THE LIGHTS THE SWITCH FELL DOWN IN BEHIND THE SIDEWALL LINER. REMOVED AND REPLACED THE SWITCH AND INSTALLED IAW SWPM AND WDM 33-51-12. EMERGENCY LIGHTS OPS CHECKED NORMAL IAW MM 33-51-00-5. ACFT OK FOR SERVICE.

Part: COVER — DAMAGED (ESCAPE ROPE) · airframe 30,664 hrs · 21,303 cycles

CAPTAIN`S SIDE ESCAPE ROPE COVER IS BROKEN AND LOWER LATCH HAS COME OFF. REPLACED THE ACCESS COVER IAW MM 25-61-00-0-0 PARA 2A1.

Part: SENSOR — INOPERATIVE (ENTRY DOOR) · airframe 30,600 hrs · 21,263 cycles

SLIDE ARM LIGHTS INOP BOTH ENTRY DOORS. T/S PER FIM 25-66 TASK 802. R&R S10216 PROX SENSOR A AND S10217 PROX SENSOR B IAW AMM CH 25-66-11-2. BOTH R1 AND L1 SLIDE LIGHTS OPS CHECKS GOOD. MEL REMOVED.

Part: UNKNOWN — ODOR (CABIN) · airframe 30,479 hrs · 21,198 cycles

APPROXIMATELY 20 MINUTES BEFORE COMMENCING DESCENT, A FAIRLY STRONG SMOKE ODOR OCCURRED WHICH SEEMED ELECTRICAL IN NATURE. DONNED OXYGEN MASKS AND STARTED QRH SEARCH. DID A SNIFF TEST AFTER A COUPLE MINUTES AND THE ODOR HAD DISSIPATED. CONTINUED FLIGHT UNEVENTFULLY. SIMULATE ACFT IN THE AIR MODE IAW AMM32-09-02-2, OPEND OVERHEAD CIRCUIT BREAKER PANEL AND INSPECTED THE TERMINAL AND SPLICE NO BURNING TRACK FOUND, ALSO INSPECTED THE ELECTRICAL EQUIPMENT AND BUNDLE IN THE FWD EQUIPMENT CENTER AND MAIN EQUIPMENT CENTER WITH ACFT POWER ON FOR 4H, NO FUMES AND ELECTRICAL ODORS FOUND, PERFORM TROUBLESHOOTING IAW FIM21-00-01,EXAMINED THE RECIRCULATION FANS AND OPS TEST IAW AMM 21-25-00-5,NO ABNORMAL FOUND. PERFORMED BOTH ENG RUN PER JRH WITH BOTH PACKS ON, NO SMOKE OR FUMES DETECTED IN THE COCKPIT AND GALLEY AREA

Part: UNKNOWN — ODOR · airframe 30,395 hrs · 21,156 cycles

PASSING F360 NOTICED ELECTRICAL SMELL. PER CHECKLIST, SHUTOFF UTILITY BUSSES AND RESIRC FAN. SMELL DISAPPEARED AND PER CHECKLIST CONTINUED TO DESTINATION. PERFORMED EXAMINATION OF THE LT AIR RECIRCULATION FAN FILTERS NORMAL PER AMM 21-25-02-4. ALSO PERFORMED OPERATIONAL TEST OF THE LT RECIRCULATION FAN SYSTEM PER AMM 21-25-00-5, TEST NORMAL. THE LT AIR RECIRCULATION FAN AND THE RELATED WIRING NO GENERATED SMOKE. PRECAUTIONARY REMOVED AND REPLACED THE LT AIR RECIRCULATION FAN PER AMM 21-25-01-4. PERFORMED TEST OF THE LT RECIRCULATION FAN SYS PER AMM 21-25-00-5, TEST NORMAL. ALSO PERFORMED BOTH ENGS RUN PER JRH, PARAMETERS NORMAL, NO ELECTRICAL SMELL. A/C OK FOR SERVICE.

Part: BLOWER — FAILED (EVAS) · airframe 30,361 hrs · 21,139 cycles

F/O EVAS BLOWER MOTOR TEST FAILED IAW WC F-2560-E0323178 A, P2, STEP 2. RT EVAS UNIT TEST PROCEDURES, RELEASED FOR SERVICE IAW MEL: 25-60-01, CATEGORY: D, EXPIRATION: 02DEC16, MEL 25-60-01. F/O EVAS UNIT REPLACED PER AMM 25-62-00-4. PERFORMED BLOWER ND BATTERY CHECK PER AMM 25-62-00-6.

Part: LIFTER — BROKEN (ZONE 200) · airframe 30,303 hrs · 21,110 cycles

L1 DOOR VERY HARD TO DISARM AND ARM. ALSO DIFFICULT TO OPEN & CLOSE. FOUND THE GIRT BAR STRIKE BRACKET BROKEN. R & R THE BROKEN L1 DOOR GIRT BAR LIFTER, 140N2754-9 AND PERFORMED DOOR GIRT BAR MECHANISM TEST IAW AMM52-11-25-5, SATISFIED. DMI CLEARED AND STICKER, REMOVED. ACFT OK FOR SERVICE.

Part: PUMP — MALFUNCTIONED (RT ENGINE) · airframe 30,168 hrs · 21,039 cycles

FLIGHT TEST FTAM 4-66, RT ENG SHUTDOWN & RE-LIGHT FL 220 AIRSPEED 300KTS. AFTER THE NORMAL SHUTDOWN OF THE RT ENG, RELIGHT WAS ATTEMPTED. WHEN THE RT FUEL CONTROL SWITCH WAS POSITIONED FROM CUT OFF TO RUN THE SPAR, VLV OPEN & THE ENG VLV ON THE RT ENG DID NOT OPEN. THE ENG VLV, WITH THE COMMANDED OPEN POSITION. THERE WERE NO FUEL FLOW INDICATION. WHEN THE RT FUEL CONTROL SWITCH WAS MOVED FROM RUN TO CUT OFF, THE ENG VLV LIGHT WENT OUT INDICATING THE ENG VLV WAS IN AGREEMENT WITH THE COMMANDED CLOSED POSITION. R & R RT ENG LP & HP FUEL PUMPS IAW AMM 73-11-03-4 & 73-11-01-4. OPERATIONS & LEAK CHECKED GOOD IAW AMM 71-00-00-5-3. REMOVED HP FUEL PUMP.

Part: SPLICE PLATE — DAMAGED (RT ENGINE) · airframe 30,166 hrs · 21,038 cycles

RIGHT ENG PYLON AFT OTBD ENG MOUNT BRACKET HAS A DING. REMOVED RT ENGINE SPLICE PLATE IAW B757 SRM 51-40-02. FABRICATED NEW SPLICE PLATE IAW SRM 51-40-05 AND 51-40-08. INSTALLED NEW SPLICE PLATE IAW SRM 51-40-02. PART MARKED IWA GMM 7-0-1001-1 PAR 7

Part: LATCH — DEFECTIVE (COCKPIT) · airframe 295 hrs · 20,608 cycles

PARTS FELL OFF CAPTAIN`S ESCAPE ROPE HATCH DURING PREFLIGHT. REINSTALLED LATCH COMPONENTS, HATCH LOCKED INTO PLACE. OK FOR SERVICE. MM 25-61-00-4.

Part: COLLAR — WORN (ENTRY DOOR) · airframe 294 hrs · 20,521 cycles

YELLOW DOOR LOCK RELEASE ON LT ENTRY DOOR IS VERY HARD TO LIFT UP WHEN CLOSING DOOR. R & R OPEN LOCK COLLAR IAW AMM 52-11-08-8. OPERATIONS CHECKED GOOD.

Part: LIGHT — INTERMITTENT (ZONE 800) · airframe 29,191 hrs · 20,317 cycles

SLIDE LIGHT ON DOOR IR ILLUMINATED INTERMITTENTLY THROUGH FLIGHT. REPLACE BULBS IAW MM 33-16-02-2. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 29,154 hrs · 20,294 cycles

R1 DOOR SLIDE LIGHT INOPERATIVE. SUSPECT BAD BULB. RELAMPED LIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-13-00-2.

Part: RESERVOIR — UNKNOWN (L1 DOOR) · airframe 29,017 hrs · 20,200 cycles

L1 DOOR EMER POWER RESERVOIR ASSEMBLY NEEDS TO BE REPLACED. R & R L1 DOOR EMER POWER RESERVOIR IAW AMM 52-11-30-4.

Part: BOTTLE — OUT OF POSITION (R1 DOOR) · airframe 28,013 hrs · 19,385 cycles

DOOR ASSIST RESERVIOR GAUGE FACES IN THE UPWARD DIRECTION REQUIRING USE OF A MIRROR TO VIEW BOTTLE PRESSURE. R & R R1 EMERGENCY POWER RESERVOIR IAW AMM 52-11-30-4. ACFT OK FOR SERVICE.

Part: DOOR — OUT OF ADJUST (PAX DOOR) · airframe 27,848 hrs · 19,275 cycles

LEFT CREW ENTRY DOOR VERY HARD TO CLOSE. INSPECTED DOOR FOR ADJUSTMENT. DOOR OPERATES NORMAL IAW MM 52-11-00-5.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,245 hrs · 18,891 cycles

R1 DOOR SLIDE ILLUMINATION LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.

Part: SKIN — DENTED (ZONE 100) · airframe 27,193 hrs · 18,860 cycles

RIGHT SKIN DENTED AT BS 720 -740, STR 27. REPAIR CARRIED OUT AS PER EA F-5330-158041 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: STRAP — MISMANUFACTURED (ZONE 300) · corrosion level 2 · airframe 27,193 hrs · 18,860 cycles

HORIZONTAL STAB LEFT SIDE LOWER SURFACE PIVOT PIN RETAINING STRAP HAS CORROSION DUE WRONG MATERIAL USED. REWORKED STRAP. REMOVED AND FABRICATED NEW RETAINING STRAP IAW DWG 182N1608, SHEET 1 REV A AND INSTALLED IAW DWG 182N1601, SHEET 2, REV. REPAIR IS CLASSIFIED AS MAJOR.

Part: STRAP — MISMANUFACTURED (ZONE 300) · corrosion level 2 · airframe 27,193 hrs · 18,860 cycles

HORIZONTAL STAB RT SIDE LOWER SURFACE PIVOT PIN RETAINING STRAP HAS CORROSION DUE WRONG MATERIAL USED. REWORKED OF RETAING STRAP. STRAP REMOVED. NEW STRAP FABRICATED IAW DWG 182N1608, SHEET 1, REV A AND INSTALLED IAW DWG 182N1601, SHEET 2, REV. REPAIR IS CLASSIFIED AS MAJOR.

Part: SUPPORT — CHAFED (ZONE 300) · airframe 27,193 hrs · 18,860 cycles

FOUND KNIFE EDGE CHAFING ON LOWER END OF SUPPORT ON VERTICAL STAB. R & R WITH FAIRING SUPPORT FABRICIATED IAW DWG 173N1300-3, SHT 1, REV B AND INSTALLED IAW DWG 173N1300 SHT 1, REV B. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,193 hrs · 18,860 cycles

AFTER REMOVAL OF TCAS ANTENNA FOUND CORROSION ON SKIN AT BS 420-440 AT STRINGER 28L TO 28R. REPAIRED IAW DWG 143N3003-2, SHT 1, REV C AND DWG 143N3400, SHT 21, REV B. REPAIR IS CLASSIFIED AS MAJOR.

Part: FLOOR SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,193 hrs · 18,860 cycles

CABIN DECK PLATE AT BS 1717, RBL 14 TO RBL 14.5 CORRODED. REPAIR CARRIED OUT IAW SRM 53-60-51, REPAIR 2 FIG 201, REV 105. REPAIR IS CLASSIFIED MAJOR.

Part: ANGLE — CORRODED (RIGHT) · airframe 27,193 hrs · 18,860 cycles

RT SIDE APU DOOR CUT OUT AREA THE ANGLE THAT THE NUTPLATES ARE ATTACHED TO ALONG STRINGER 2R IS CORRODED. REMOVED, FABRICATED IAW DWG 148N3152-2, SHT 1, REV- AND INSTALLED IAW SRM 51-40-02, REV 105 AND DWG 148N3105, SHT 1, REV C. REPAIR IS CLASSIFIED AS MAJOR.

Part: STRAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 27,193 hrs · 18,860 cycles

RIGHT SIDE OF APU DOOR CUTOUT AREA, BS 1825 THE APU INLET STRAP CORRODED. CORRODED STRAP REMOVED. STRAP FABRICATED IAW DWG 148N3138-8000 SHT 1, REV C, AND INSTALLED IAW DWG 148N3105, SHT 1, REV C. REPAIR CLASSIFIED AS MAJOR.

Part: ATTACH ANGLE — CORRODED (ZONE 300) · airframe 27,193 hrs · 18,860 cycles

RT SIDE APU INLET CUTOUT, AFTER THE APU INLET REMOVAL FOUND THE INLET ATTACH ANGLE FROM STA 1793 -1825 HAS CORROSION AT STRINGER 6, RT. CORRODED RT APU INLET CUTOUT ATTACHMENT ANGLE REMOVED. REPLACED WITH ANGLE FABRICATED IAW DWG 148N3152-1, SHT 1, REV A AND INSTALLED IAW SRM 51-40-02, REV 105 AND DWG 148N3105, SHT 1, REV C. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — SCRATCHED (ZONE 100) · airframe 27,193 hrs · 18,860 cycles

FUSELAGE SKIN, UNDER SHORING BS 540 - 560 BETWEEN STR 26L - 26R HAS SCRATCHES. SKIN REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 16, REV 105. REPAIR IS CLASSIFIED AS MAJOR.

Part: SPLICE PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,193 hrs · 18,860 cycles

APU DOOR CUT OUT AREA, RT SIDE. NUTPLATES ALONG THE FWD EDGE ARE CORRODED JUST AFT OF BS 1787 BULKHEAD FRAME. CORRODED SPLICE PLATE R & R IAW SRM 51-40-02, REV 105 AND DWG 148N3105, SH 1REV C. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — SCRATCHED (ZONE 100) · airframe 27,193 hrs · 18,860 cycles

FUSELAGE SKIN UNDER SHORING BS 500 -520 BETWEEN STR 26L - 26R HAS SCRATCHES. DAMAGED SKIN REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 16, REV. 105. REPAIR IS CLASSIFIED AS MAJOR.

Part: RIB — CORRODED (LT WING TE FLAP) · airframe 27,193 hrs · 18,860 cycles

LEFT WING INBD T/E MAIN FLAP INBD TORQUE TUBE SUPPORT RIB LOWER AREA FOUND CORROSION. REPAIR CARRIED OUT IAW EA F-5750-158016. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — DENTED (ZONE 100) · airframe 27,193 hrs · 18,860 cycles

DENT ON EXTERIOR SKIN AT BS 1500-1520 BETWEEN STRINGER 24-25L. REPAIR CARRIED OUT IAW EA F-5330-158156, PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — DENTED (ZONE 100) · airframe 27,193 hrs · 18,860 cycles

DENT ON EXTERIOR SKIN AT BS 1480-1500 BETWEEN STRINGER 25-26L. REPAIR CARRIED OUT IAW EA F-5330-158156, PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — PUNCTURED (BS 700-720) · airframe 27,193 hrs · 18,860 cycles

EXTERIOR SKIN AT BS 700-720 AND STR 25-26 RT PUNCTURED. REPAIRED IAW EA F-5330-158160, PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: RIB — GOUGED (HORIZONTAL STAB) · airframe 27,193 hrs · 18,860 cycles

RT HORIZONTAL STABILIZER THE AFT AUX SPAR, FOUND ONE GOUGE AT STAB STATION 100. DAMAGED SUPPORT RIB REMOVED. SUPPORT RIB FABRICATED IAW DWG 183N1308 SH1, REV A AND INSTALLED IAW DWG 183N1302 SHT 1, REV C. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — SCRATCHED (ZONE 100) · airframe 27,193 hrs · 18,860 cycles

EXTERIOR SKIN BS 760-780 BETWEEN STR 27 - 30 LT THERE ARE NUMEROUS SMALL SCRATCHES. REPAIR CARRIED OUT IAW EA F-5310-155875. REPAIR IS CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (BS 700-760) · corrosion level 2 · airframe 27,193 hrs · 18,860 cycles

CABIN CREASE BEAM INNER STRUCTURE AT BS 700 TO 760, RBL 64 HAS CORROSION. R & R BETWEEN BS 660 AND 760 IAW SRM 51-40-02 REV 105. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — CRACKED (LT WING LE) · airframe 27,193 hrs · 18,860 cycles

LEFT WING L/E NOSE SKIN COVER AT NACELLE AT ISS 280 FOUND WITH A 3 INCH CRACK. CRACKED SKIN COVER REMOVED. COVER FABRICATED IAW DWG NR 114N1802, REV G AND INSTALLED IAW SRM 51-40-02, REV 105. REPAIR IS CLASSIFIED AS MINOR.

Part: SKIN — SCRATCHED (ZONE 100) · airframe 27,193 hrs · 18,860 cycles

FUSELAGE EXTERIOR SKIN AT BS 1710 BETWEEN STRINGER 19-20L THERE IS A SCRATCH. REPAIRED IAW SRM 53-00- 01 FIG.201, REPAIR 16, REV 105. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — SCRATCHED (ZONE 200) · airframe 27,193 hrs · 18,860 cycles

FUSELAGE EXTERIOR SKIN AT BS 1714 BETWEEN STRINGER 15-16L, SCRATCHED. REPAIR CARRIED OUT IAW EA F-5330-158020, PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,193 hrs · 18,860 cycles

CREASE BEAM AT DOOR 2L HAS CORROSION. CREASE BEAM R & R IAW SRM 51-40-02, REV 105. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 27,193 hrs · 18,860 cycles

FUSELAGE EXTERIOR SKIN AT BS 1670 BETWEEN STRINGER 19-20L THERE IS A SCRATCH. REPAIR CARRIED OUT IAW EA F-5330-158018, PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — SCRATCHED (ZONE 200) · airframe 27,193 hrs · 18,860 cycles

FUSELAGE EXTERIOR SKIN, BS 1698 BETWEEN STRINGER 14-15L. SCRATCHED. REPAIR CARRIED OUT IAW EA F-5330-158019, PART 1 . REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 27,193 hrs · 18,860 cycles

CABIN CREASE BEAM WEB AT BS 1360 TO 1380 CORRODED. R & R IAW SRM 51-40-02 REV 105. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 27,193 hrs · 18,860 cycles

DAMAGE ON SEAT TRACK CROWN AND CHANNEL AT STA 470-480, RBL 45.5. REPAIR CARRIED OUT ON SEAT TRACK IAW SRM 53-00-52 REPAIR 1, FIG 201, REV 105. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 27,193 hrs · 18,860 cycles

DAMAGE ON SEAT TRACK CROWN AND CHANNEL AT BS 490 - 510, RBL 45.5. DAMAGED SEAT TRACK TRIMMED AND CARRIED OUT SPLICE REPAIR IAW SRM 53-00-52, REPAIR 1, FIG 201, REV 105. REPAIR IS CLASSIFIED AS MAJOR.

Part: FLOOR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,193 hrs · 18,860 cycles

CABIN DECK PLATE AT BS 1717, LBL 58 TO RBL 58 HAS AREAS OF CORROSION. REPAIR CARRIED OUT IAW SRM 53-60-51, REPAIR 2, FIG 201, REV 105. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 27,193 hrs · 18,860 cycles

DAMAGE ON SEAT TRACK CROWN & CHANNEL AT BS 860-879, RBL 24.75. DAMAGED SEAT TRACK REMOVED, FABRICATED NEW IAW DWG 143N5106, SHT 1, REV A AND INSTALLED IAW SRM 51-40-02, REV 105. REPAIR IS CLASSIFIED AS MAJOR.

Part: STRAP — CORRODED (ZONE 300) · airframe 27,193 hrs · 18,860 cycles

HORIZONTAL STABILIZER LT SIDE-LOWER SURFACE PIVOT PIN RETAINING STRAP HAS CORROSION. CORRODED STRAP REMOVED. FABRICATED IAW DWG 182N1608, SH 1, REV A AND INSTALLED IAW SRM 51-40-02, REV 105 AND DWG 182N1601 SH 1, REV C. REPAIR IS CLASSIFIED AS MAJOR.

Part: STRAP — CORRODED (ZONE 800) · airframe 27,193 hrs · 18,860 cycles

HORIZONTAL STABILIZER RT SIDE-LOWER SURFACE PIVOT PIN RETAINING STRAP HAS CORROSION. CORROSION REMOVED. STRAP FABRICATED IAW DWG 182N1608, SHT 1, REV A, AND INSTALLED IAW SRM 51-40-02, REV 105 AND DWG 182N1601 SHT 1, REV C. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 27,193 hrs · 18,860 cycles

DAMAGE ON SEAT TRACK CROWN & CHANNEL AT BS 870 - 890, RBL 45.5. REMOVED SEAT TRACK, FABRICATED NEW IAW DWG 143N5106 SHT 1, REV A AND INSTALLED IAW SRM 51-40-02, REV 105. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — DAMAGED (ZONE 200) · airframe 27,193 hrs · 18,860 cycles

CABIN BS 1540, STR 3L TO STR 4L ELONGATED HOLE IN FRAME. FRAME R & R IAW SRM 53-00-07, REPAIR 3 FIG 201, REV 105. REPAIR IS CLASSIFIED AS MAJOR.