N614DL

Part: FIRE WARNING — FALSE INDICATION (CARGO BAY) · airframe 90,681 hrs · 41,900 cycles

FLIGHT DIVERTED DUE TO BOTH FORWARD AND AFT CARGO FIRE WARNINGS. NO EVIDENCE OF SMOKE/FIRE. R & R CARGO FIRE CARD M10427 AND CONTROL PANEL FOR APU AND CARGO FIRE TEST IAW AMM 26-10 AND 26-22. BOTH TESTED GOOD.

Part: GIRT BAR — DIRTY (R2 DOOR) · airframe 90,134 hrs · 41,695 cycles

R2 DOOR WILL NOT DISARM. ARMED AND DISARMED 2R DOOR MULTIPLE TIMES NO PROBLEMS NOTED. CLEANED GIRT BAR AND FITTINGS NO THER DEFECTS NOTED. REF AMM 25-66.

Part: CIRCUIT CARD — INOPERATIVE (FIRE DETECTION) · airframe 89,135 hrs · 41,377 cycles

ON APPROACH RECEIVED A FIRE WARNINGS IN BOTH FWD AND AFT CARGO BAYS SIMULTANEOUSLY. FOLLOWED QRH AND SHOT BOTH BOTTLES. NO INDICATIONS IN CABIN. INSPECTED CARGO BINS. NO EVIDENCE OF FIRE OR SMOKE. RAN APU BLEED AND AFT CARGO HEAT CKS. GOOD. INSPECTED CARGO FIRE DETECTION PANEL AND CONNECTORS NO TROUBLE FOUND. REPLACED CARD M10427 IAW AMM 26-10-01. REPLACED CARGO FIRE EXTINGUISHER BOTTLES IAW AMM 26-23-02. PERFORMED SYS TEST IAW AMM 26-23-00. CKS GOOD.

Part: STRUCTURE — DAMAGED (FWD CARGO DOOR) · airframe 88,974 hrs · 41,316 cycles

RAMP CREW REPORTS DENT OR NICK ON LOWER AFT EDGE OF FWD CARGO DOOR. INSPECTED AREA OF NICK AND SMOOTHED AS REQUIRED WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 52-30.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 88,936 hrs · 41,301 cycles

L2 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED LAMPS. OPS CHECKED GOOD.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 87,086 hrs · 40,680 cycles

L1 DOOR CUTOUT UPPER CORNER SKIN AND BEAR-STRAP CRACKED. REPAIRED IAW ERA 092195-14 AD REV ORIG.

Part: SWITCH — DAMAGED (L4 DOOR ASSIST) · airframe 85,846 hrs · 40,217 cycles

DURING A SCHEDULE INSPECTION OF THE L4 DOOR EMERGENCY POWER ASSIST, MAINTENANCE DISCOVERED THE L4 PASSENGER DOOR EMERGENCY POWER ASSIST TRIGGER BROKEN. REPLACED L4 DOOR ASSIST TRIGGER. NO OTHER DISCREPANCIES NOTED.

Part: BRACKET — DAMAGED (R2 DOOR) · airframe 83,457 hrs · 39,309 cycles

ERA 06-496024-14 REV A CLASSIFICATION WAS CHANGED FROM MINOR TO MAJOR REPAIR WHICH REQUIRES AN SDR TO BE SUMMITTED - BRACKET THICKNESS WAS CHANGED FROM .100" TO .060".

Part: SKIN — DENTED (BS 717) · airframe 81,581 hrs · 38,617 cycles

FUSELAGE HAS DENT BELOW LAP STA 717. COMPLIED WITH REPAIR PER ERA 490194-14AD REV O.

Part: SKIN — DENTED (BS 616 S16L) · airframe 81,581 hrs · 38,617 cycles

FUSELAGE DENT STA 616 ABOVE STR 16L. C/W REPAIR PER ERA 489481-14 REV O.

Part: UNKNOWN — ODOR (CABIN) · airframe 77,331 hrs · 37,146 cycles

DURING CRUISE, REPORTS OF ELECTRIC ODOR FROM ROWS 27-29ABC. TURNED OFF BOTH UTIL BUSSES AND LT REC FAN, ODOR DISSIPATED. RESTORED L RECIR - OK. RESTORED R AND L UTIL BUSS, ODOR RETURNED. IRO/ TURNED ON ALL LIGHTS AND IFE WITH UTIL SWITCHES. LT AND RT REC FANS ON. NO ELECTRICAL ODOR IN CABIN BETWEEN ROWS 27 THRU 29 ABC. INSPECTED WIRING UNDERNEATH SEATS. NO TROUBLE FOUND.

Part: BEAM — CORRODED (BS 730 LBL62) · airframe 76,111 hrs · 36,738 cycles

BOX BEAM CORRODED THRU OUT UPPER SURFACE STA. 730 LBL62 AND WL 208 CP53-231-01-02.051 / FABRICATED REPLACEMENT UPPER SECTION OF BOX BEAM IAW DWG 143N55-22 AND SRM 51-40-05 AND 51-30-01 DURING HMV4 AT SAA SAT ON N/R CARD 127156

Part: PLATE — CORRODED (STA 1712) · airframe 76,111 hrs · 36,738 cycles

MAIN CABIN DECK PLATE STA. 1712 LBL 35 REPAIR DOUBLER HAS CORROSION CP53-251-01-02.05I / REMOVED AND REPLACED DOUBLER DURING HMV4 AT SAA SAT ON N/R CARD 131960

Part: SKIN — DENTED (BS 1615 S23R) · airframe 76,111 hrs · 36,738 cycles

EXTERNAL DENTS WITH GOUGES NOT PROPERLY TAGGED ON FUSELAGE SKIN STA. 1615 BETWEEN S-23R AND S-24R / INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG 201 REPAIR 3 AND APPLIED ID TAG DURING HMV4 AT SAA SAT ON N/R CARD 131804

Part: SKIN — DENTED (BS 1623 S26R) · airframe 76,111 hrs · 36,738 cycles

PROTRUDING DENT ON LOWER EXTERNAL FUSELAGE AT STA. 1623 BETWEEN S26R AND S27R / ACCOMPLISHED ER/A 474939-14 REV ORIG AT SAA SAT DURING HMV ON N/R CARD 131803

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,252 hrs · 36,117 cycles

DURING AN AGING AIRCRAFT INSPECTION, CORROSION WAS FOUND ON THE INNER SURFACE OF THE GROUND AIR CONDITIONING CUTOUT AT STA 869. THE CORROSION DAMAGE WAS REPAIRED PER BOEING INSTRUCTIONS.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 74,252 hrs · 36,117 cycles

T-CLIP CRACKED IN RADIUS BS 800 LOWER BBL 0 COMMON TO FAIRING FORMER. REMOVED AND REPLACED FORMER.

Part: SUPPORT — CORRODED (FAIRING) · airframe 74,252 hrs · 36,117 cycles

WHILE WORKING CUSTOMER CARD 00068 FOUND FAIRING SUPPORT STRUCTURE CRACKED AT BS 780-800 BL 0. REMOVED AND REPLACED FAIRING SUPPORT STRUCTURE BS 780-800 BL 0 IAW SRM 51-40-02.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 74,252 hrs · 36,117 cycles

CORROSION AFT CARGO BAY AFT FLOOR PANEL FROM BS 1510 TO 1640 IS CORRODED ON BOTTOM SURFACE AT THE FASTENER HOLES. REMOVED AND REPLACED ACB FLOOR PANEL BS 1510-1640 IAW AMM 25, 50-04-004-001, AMM 25-50-04-404-004, SRM 51-40-02, 51-40-05, AND 51-40-08.

Part: FLOOR SUPPORT — CORRODED (BS 1510-1530) · airframe 74,252 hrs · 36,117 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 1510 THRU 1530 RT. REPLACED FLOOR SIDEWALL SUPPORT IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1523 LBL 3) · airframe 74,252 hrs · 36,117 cycles

CORROSION AROUND NUTPLATE HOLE BS 1523 LBL 3 FLOOR SUPPORT RAIL. REMOVED DAMAGED SECTION OF FLOOR SUPPORT RAIL BS 1523 LBL 3. FABRICATED REPAIR PARTS, ALODINED, PRIMED, AND INSTALLED WET WITH SEALANT. WORK DONE IAW SRM 53-60-53D FIG 206.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 74,252 hrs · 36,117 cycles

CORROSION AROUND NUTPLATE HOLE BS 1519 LBL 8 FLOOR SUPPORT RAIL. REMOVED DAMAGED SECTION OF FLOOR SUPPORT RAIL BS 1519 LBL 8. FABRICATED REPAIR PARTS, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH SEALANT. WORK DONE IAW SRM 53-60-53D FIG 206.

Part: SUPPORT BEAM — CORRODED (AFT CARGO BAY) · airframe 74,252 hrs · 36,117 cycles

CORROSION ON THE THRESHOLD SUPPORT BEAM IN THE AFT CARGO DOOR CUTOUT BS 1380-1440 RBL 21. SUPPORT BEAM WAS REPLACED ON CUST CARD 00126.

Part: FLOOR PANEL — CORRODED (BS 635-650) · airframe 74,252 hrs · 36,117 cycles

FWD CARGO BAY BILGE FIXED FLOOR PANEL UPPER SURFACE CORRODED AT STATION 635-650 AT RBL 19. REPAERED PER ERA 470940-14 REV ORG ON NR CARD 00063.

Part: FLOOR SUPPORT — CORRODED (BS 1510-1530) · airframe 74,252 hrs · 36,117 cycles

CORROSION ON FLOOR SIDEWALL SUPPORT BS 1510 TO BS 1530 LBL 19. REPAIRED ON NR 00042 PER 51-40.

Part: FLOOR PANEL — CORRODED (BS 635-650) · airframe 74,252 hrs · 36,117 cycles

FWD CARGO BAY BILGE FIXED FLOOR PANEL UPPER SURFACE CORROSION AT STATION 635 TO 650 LBL 19. REPAIRED ON NR 00065 PER DELTA ERA 470939-14 AND ATS ER 08 3281.

Part: WEB — CORRODED (BS 1500-1520) · airframe 74,252 hrs · 36,117 cycles

VERTICAL WEB AT 1520 TO 1500 IS CORRODED ON TOP OF WEB. REPAIRED PER 51-70-13 ON NR 00100.

Part: WEB — CORRODED (BS 1510) · airframe 74,252 hrs · 36,117 cycles

CORROSION ON LOWER SIDE OF FLOOR SUPPORT AT STATION 1510 RBL 12. REPAIRED ON NR 00044 PER 51-40-05.

Part: SKIN — CORRODED (BS 570-620) · airframe 74,252 hrs · 36,117 cycles

CORROSION FOUND AT STA 570 TO 620 AT RBL 21.5 IN FWD CARGO BAY. REPAIRED ON NR CARD 00062 PER 51-40-05.

Part: ANGLE — CRACKED (BS 660) · airframe 74,252 hrs · 36,117 cycles

ANGLE AT BS 660 RBL 45 CRACK. REPLACED ON NR CARD 00078 PER 51-40-05.

Part: ANGLE — CRACKED (BS 660) · airframe 74,252 hrs · 36,117 cycles

VERTICAL ATTACH ANGLE BS 660 CRACKED. REPAIRED ON NR 00083 PER 51-40-05.

Part: STRINGER CLIP — CORRODED (BS 1500 S29R) · airframe 74,252 hrs · 36,117 cycles

CORROSION ON SUPPORT CLIP AT STRINGER 1500 AND STRINGER 29R. REPAIRED ON ATS 00102 PER 51-40-02.

Part: SUPPORT — CORRODED (BS 1530) · airframe 74,252 hrs · 36,117 cycles

CORROSION ON SUPPORT STATION 1530 TO STATION 1560 RT. REPAIRED ON NR 00040 PER 53-00-02.

Part: FLOOR SUPPORT — CORRODED (BS 1530-1560) · airframe 74,252 hrs · 36,117 cycles

CORROSION ON FLOOR SUPPORT AT BS 1530 TO 1560 LT. REPAIRED ON ATS 00041 PER 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1460) · airframe 74,252 hrs · 36,117 cycles

FLOOR SUPPORT BRACKET AT BS 1460 RBL 11-15 IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT BRACKET IAW SRM 51-40-02, DWG 146N5458, SRM 51-30-01.

Part: CHANNEL — CORRODED (BS 1460-1480) · airframe 74,252 hrs · 36,117 cycles

WEB AT BS RBL CORRODED. REMOVED AND REPLACED WEB PN 146N5456-2, CHANNEL AT BS 1460 PN 146N5458-6, CHANNEL BS 1480 PN 146N5458-5 IAW SRM 51-40-02, SRM 51-30-01, DWG 146N5458.

Part: FLOORBEAM — CORRODED (BS 1480) · airframe 74,252 hrs · 36,117 cycles

FLOOR SUPPORT BRACKET AT BS 1480 RBL 11 CORRODED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-30-01, DWG 146N5458, SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1460 RBL 11) · airframe 74,252 hrs · 36,117 cycles

FLOOR SUPPORT BRACKET AT BS 1460 RBL 11 CORRODED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-02, SRM 51-30-01, DWG 146N5458.

Part: CHANNEL — CORRODED (BS 1440-1480) · airframe 74,252 hrs · 36,117 cycles

C CHANNEL BS 1440-1480 RBL 19 IN ACB IS CORRODED. REMOVED AND REPLACED CHANNEL IAW SRM 51-40-02.

Part: SUPPORT — CORRODED (BS 1440) · airframe 74,252 hrs · 36,117 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT THE AFT INBD CORNER OF THE ACB THRESHOLD BS 1440. REPLACED SUPPORT.

Part: FLOOR SUPPORT — CORRODED (BS 1540) · airframe 74,252 hrs · 36,117 cycles

CORROSION ON LOWER SURFACE OF FLOOR SUPPORT RAIL BS 1540 RBL 3 AT NUTPLATE LOCATION. REMOVED DAMAGED SECTION OF FLOOR SUPPORT RAIL BS 1540 RBL3. FABRICATED REPAIR PARTS, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH SEALANT. DONE IAW SRM 53-60-53D FIG 206.

Part: FLOOR SUPPORT — CORRODED (BS 1523) · airframe 74,252 hrs · 36,117 cycles

CORROSION AROUND NUTPLATE HOLE BS 1523 LBL3 FLOOR SUPPORT RAIL. REPAIRED SUPPORT IAW SRM 53-60-53 FIG 206.

Part: SPLICE — CORRODED (FLOOR PANEL) · airframe 74,252 hrs · 36,117 cycles

CORROSION ON FLOOR PANEL SPLICE BS 1510 LBL 19 THRU RBL 19. FLOOR PANEL SPLICE REPLACED.

Part: SKIN — GOUGED (FS 534 S27L) · airframe 70,474 hrs · 34,963 cycles

GOUGE BEYOND LIMITS, REPAIRED PER SRM 53-00-01. REPAIR 3 REF ERA 464376-14 REV ORIG FUSELAGE/SKIN/FS 534, S-27L/GOUGE.

Part: SKIN — DENTED (FS 495) · airframe 69,034 hrs · 34,552 cycles

REPAIR OF DENT AND GOUGE AT FS 495 AND STRINGER 28R. DAMAGE CUTOUT AND DOUBLER INSTALLED.

Part: REPAIR — MISINSTALLED (STA 1350, STR-1) · airframe 63,698 hrs · 32,745 cycles

FUSELAGE / SKIN / STA 1340-1360, STR 1-2R / SKY RADIO ANTENNA REPAIR. THE ORIGINAL REPAIR INSTALLED BY ER/A 385126-14 WAS REMOVED AND THE CUTOUT IN THE FUSELAGE SKIN WAS ENLARGED TO REMOVE KNIFE EDGED HOLES AND FASTENER HOLES WITH TOO TIGHT SPACING. AN ALUMINUM DOUBLER AND TRIPLER WERE INSTALLED EXTERNALLY OVER THE CUTOUT WITH SOLID ALUMINUM RIVETS.

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM) · airframe 57,051 hrs · 30,193 cycles

LT HYD QTY WENT TO 00-HAD PRESURE ON LT SIDE GOOD AT 3100. RETURNED TO CVG AFTER COORDINATING WITH MTC. EICAS MSGS LT HYD SYS PRESS, RUDDER RATIO, LT HYD QTY. REPLACED FLEX LINE AT LEFT SIDE ELECTRIC PUMP.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,424 hrs · 29,917 cycles

FUSELAGE, SKIN, FS 1723 STRINGER 19R, REPAIR OF DENT. A DENT WAS FOUND IN THE FUSELAGE SKIN AND CUTOUT. A REPAIR DOUBLER WAS INSTALLED WITH A MINIMUM OF THREE ROWS OF REPAIR FASTENERS. ERA 384755-14 REV B.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 56,424 hrs · 29,917 cycles

FUSELAGE / FS 680 AND STR 26L - REPAIR OF LIGHTNING STRIKE: DAL ER/A 385076-14 PROVIDES INSTRUCTIONS TO TRIM OUT THE DAMAGED SKIN AND INSTALL AN EXTERNAL DOUBLER AND STRUCTURAL FILLER. THE FUSELAGE SKIN IS M/F 2024-T3 CLAD ALUMINUM WITH A LOCAL THICKNESS OF 0.056 INCH AND 0.042 INCH IN THE TRIMMED AREA.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,061 hrs · 29,772 cycles

THE FUSELAGE SKIN WAS FOUND DENTED AT FS 405 NEAR STRINGER 22L. THE DENT WAS REMOVED WITH A 4 X 2 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS INSTALLED PER ER/A 384744-14.

Part: ENGINE — LEAKING (NR 1) · airframe 54,763 hrs · 29,161 cycles

ON APPROACH OIL PRESSURE STARTED TO FLUX IN YELLOW BAND. OIL PRESSURE WENT RED AND FLIGHT CREW SHUT ENGINE DOWN. FOUND NUMEROUS METAL ON NR 2 AND NR 3 BEARING CHIP DET AND ALSO MAIN OIL FILTER, REPLACED NR 1 ENG.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 52,432 hrs · 28,022 cycles

L-4 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED SAME. CHECKS OK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,988 hrs · 27,801 cycles

L-1 DOOR FLASHLIGHT BATTERY LOW. REPLACED FLASHLIGHT ASSY, OPS NORMAL.

Part: ENGINE — UNSERVICEABLE (#2 ENGINE) · airframe 51,629 hrs · 27,623 cycles

17,000 FT LOUD BANG AND BUFFET NBR 2 ENGINE ROLL BACK AND EGT WENT WELL INTO RED. SMOKE RECORDED IN CABIN._C/A REPLACE ENGING

Part: FAN — DEFECTIVE (CABIN) · airframe 51,476 hrs · 27,561 cycles

AFTER T/O FLT ATTENDANTS REPORT ELECTRICAL FUMES IN MID CABIN. FUMES SUBSIDED THEN RT RECIRC FAN MSG APPEARED ON EICAS. TURNED OFF RT RECIRC FAN ON OVERHEAD PANEL. NOTIFIED MCC. PULLED C/B P23. CONTRACT MTC REPLACED RT RECIRC FAN. FAINT ODOR FROM FAN.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 49,298 hrs · 26,529 cycles

CREW REPORTED TOTAL LOSS OF LEFT ENGINE OIL PRESS AND BUMPING NOISE. ENGINE SHUTDOWN. REPLACED ENGINE.

Part: MEDICAL KIT — UNSECURE (COCKPIT) · airframe 49,233 hrs · 26,497 cycles

FOUND MEDICAL KIT SEAL MISSING ON L/O. REPLACED MEDICAL KIT.

Part: PANEL — MALFUNCTIONED (COCKPIT) · airframe 48,274 hrs · 26,036 cycles

PRIOR TO T/O, STRONG ELECTRICAL SMELL AFTER EXT LIGHTS WERE TURNED ON. FOUND SOURCE OF SMELL TO BE LEFT RUNWAY TURNOFF LIGHT SWITCH. REPLACED COCKPIT OVERHEAD PANEL.

Part: CHARGER — INOPERATIVE (FWD E/E BAY) · airframe 47,975 hrs · 25,885 cycles

STATUS MSG ''MAIN BATTERY CHARGER'' INFLIGHT. CREW COULD NOT EXTINGUISH. REPLACED CHARGER.

Part: HYD PUMP — FAILED (NR 1 ENGINE)

06T CENTER NR 1 HYD PUMP LOW PRESS FOLLOWED BY PUMP OVHEAT BY LOSS OF CENTER HYD QTY. REPLACED NR 1 HYD PUMP, PUMP BORROWED FROM UAL. LEAK AND OPS CHK GOOD.

Part: DME — FAILED (AVIONICS COMPT)

FAILURE OF GROUND ELECTRICAL POWER, ACRID SMOKE IN COCKPIT AND GALLEY. LT DME C/B POPPED. REPLACED LT DME RECEIVER, OPS CK OK.

Part: FUEL CONTROL — FAILED (N1 ENGINE)

LEFT ENGINE VALVE CAUTION LIGHT CAME ON FOLLOWED BY THE ENGINE QUITTING. THROTTLES WERE AT IDLE DURING DESCENT THRU 22,000 FEET. REPLACED FUEL CONTROL UNIT.

Part: SWITCH — FAILED (RAT SYSTEM)

DURING INSPECTION, CONDUCTING RAM AIR TURBINE DEPLOYMENT TEST, TURBINE FAILED TO DEPLOY. REPLACED RAT DEPLOY PRESSURE SWITCH AND OPERATION NORMAL.

Part: CONTROL — BINDING (RT AILERON)

ON TAXI OUT FOR TAKEOFF DURING FLIGHT CONTROL CHECK, RIGHT AILERON BECAME STUCK IN FULL UP POSITION. RETURNED TO BLOCK, FOUND RT INBOARD PCA INPUT LEVER RESTRICTED. REPLACED UNIT, OPERATION NORMAL. SHOP INSPECTION OF PCA FOUND SPRING (P/N 1527725) MISSING. THIS ALLOWED THE WASHER (P/N 1527729) TO FALL OUT OF POSITION AND JAM THE SLIDE ASSEMBLY (P/N 1527721).

Part: SKIN — CRACKED (FS 1473)

DURING HMV INSPECTION, WHILE ACCOMPLISHING THE PERMANENT REPAIR FOR THE VHF ANTENNA MOUNT PER EO 6-59207-3, INTERFERENCE WAS FOUND WITH A DOUBLER PREVIOUSLY INSTALLED DUE TO CRACKING. TO ACCOMPLISH THE MODIFICATION, THE SKIN WILL BE REPAIRED BY EXTENDING THE DOUBLER AND TRIPLER REQUIRED BY EO 6-59207-3.

Part: SKIN — PUNCTURED (RT TE FLAP)

AT HMV, A SMALL HOLE WAS FOUND IN THE LWR SKIN APPROX 35 INCHES FROM THE I/B END AND 8 INCHES FROM THE T/E OF THE RT O/B AFT FLAP. THIS WAS REPAIRED AS PER SRM 57-53-01.

Part: TE WEDGE — DELAMINATED (TE 3 TE FLAP)

AT HMV, THE T/E WEDGE FOR NR 3 FLAP WAS FOUND TO BE DELAMINATED APPROX TWO FEET OF I/B END. THIS DAMAGED AREA WAS REPAIRED PER SRM 51-70-07.

Part: RADOME — DAMAGED (FWD FUS)

RADOME DAMAGED IN NOSE AREA. ON SHOP INSPECTION, FOUND OLD WETLAY UP AND MOISTURE ABOVE LIMITS 40 PERCENT OF SURFACE AREA. REBUILT RADOME FROM BASE RING UP PER S.R.M. 53-10-72 PAINTED AND TESTED, RETURN SERVICABLE UNIT TO STOCK.

Part: SKIN — WORN (RT WING)

AT HMV, FRETTING WEAR WAS FOUND AROUND OPENINGS FOR TANK PLATES 631 CB AND 641 AB. THIS WAS REMOVED PER SRM 57-20-01, ROTOPEENED PER PS 900-4 NR 5, TREATED AND PAINTED PER SRM 57-20-01.

Part: SKIN — CORRODED (LT WING)

AT HMV, FRETTING CORROSION WAS FOUND ON FUEL ACCESS OPENINGS 541 MB 541 LB AND 541 KB. THIS WAS CLEANED TREATED AND PAINTED PER SRM 57-20-01. ALSO, ROTOPEENED PER PS 900-4 NR 5.

Part: SKIN — CORRODED (LT WING)

AT HMV, FRETTING CORROSION WAS FOUND ON FUEL ACCESS OPENINGS 541 JB 541 HB AND 541 EB. THIS WAS CLEANED TREATED AND PAINTED PER SRM 57-20-01. ALSO, ROTOPEENED PER PS 900-4 NR 5.

Part: SKIN — CORRODED (LT WING)

AT HMV, FRETTING CORROSION WAS FOUND ON FUEL ACCESS OPENINGS 541 FB AND 541 EB. THIS WAS CLEANED TREATED AND PAINTED PER SRM 57-20-01. ALSO, ROTOPEENED PER PS 900-4 NR 5.

Part: SKIN — WORN (RT WING)

AT HMV, FRETTING WEAR WAS FOUND AROUND OPENINGS FOR TANK PLATES 631 AB AND 631 BB. THIS WAS REMOVED PER SRM 57-20-01, ROTOPEENED PER PS 900-4 NR 5, TREATED AND PAINTED PER SRM 57-20-01.

Part: SKIN — CORRODED (LT WING)

AT HMV, FRETTING CORROSION WAS FOUND ON FUEL ACCESS OPENING 531 BB. THIS WAS CLEANED AND TREATED PER SRM 57-20-01 AND ROTOPEENED PER PS 900-4 NR 5.

Part: SKIN — CORRODED (LT WING)

AT HMV, FRETTING CORROSION WAS FOUND ON FUEL ACCESS OPENINGS 541 CB 541 BB AND 541 AB. THIS WAS CLEANED AND TREATED PER SRM 57-20-01. ALSO, ROTOPEENED PER PS 900-4 NR 5.

Part: SKIN — CORRODED (LT WING)

AT HMV, FRETTING CORROSION WAS FOUND ON FUEL ACCESS OPENING 531 CB. THIS WAS CLEANED AND TREATED PER SRM 57-20-01 AND ROTOPEENED PER PS 900-4 NR 5.

Part: SKIN — CORRODED (LT WING)

AT HMV, FRETTING CORROSION WAS FOUND ON ACCESS PANEL 531 AB. THIS WAS CLEANED AND TREATED PER SRM 57-20-01 AND ROTOPEENED PER PS 900-4 NR 5.

Part: SKIN — CORRODED (LT WING)

AT HMV, FRETTING CORROSION WAS FOUND ON FUEL ACCESS OPENING 542 BB. THIS WAS CLEANED, TREATED AND PAINTED PER SRM 57-20-01. ALSO, ROTOPEENED PER PS 900-4 NR 5.

Part: SKIN — WORN (RT WING)

AT HMV, FRETTING WEAR WAS FOUND AROUND OPENINGS FOR TANK PLATES 641 BB AND 641 CB. THIS WAS REMOVED PER SRM 57-20-01, ROTOPEENED PER PS 900-4 NR 5, TREATED AND PAINTED PER SRM 57-20-01.

Part: SKIN — CORRODED (LT WING)

AT HMV, FRETTING CORROSION WAS FOUND ON THE FUEL ACCESS OPENING 542 CB. THIS WAS CLEANED PER SRM 57-20-01 TREATED AND PAINTED PER SAME AND ROTOPEENED PER PS 900-4 NR 5.

Part: FLOORBEAM — CORRODED (FS 1660)

AT HMV, THE CABIN FLOORBEAM AT STA 1660 WAS FOUND TO HAVE SEVERAL FASTENER HOLES CORRODED THE ENTIRE LENGTH OF THE BEAM. CORROSION WAS CLEANED PER SRM 51-10-00 AND FOUND WITHIN LIMITS, EXCEPT HOLE AT RBL 4. REPAIR WAS FABRICATED FOR RBL 4 PER SRM 53-10-51 AND INSTALLED PER SAME, AREA WAS TREATED AND PAINTED.

Part: AILERON — WORN (RT WING)

AT HMV, THE LWR O/B L/E OF THE RT AILERON WAS FOUND TO BE WORN. THE AILERON WAS REPAIRED PER SRM 51-70-03 REF FROM 57-60-01.

Part: T/E WEDGE — CHIPPED (LT T/E AFT FLAP)

AT HMV, THE LT I/B AFT FLAP WAS FOUND TO BE CHIPPED ON THE TRAILING EDGE. THIS WAS REPAIRED PER SRM 57-53-01 REF 51-70-17.

Part: LE SKIN — WORN (RT AILERON)

AT HMV, THE UPPER I/B L/E SURFACE OF THE RT AILERON WAS FOUND TO BE WORN. THIS WAS REPAIRED PER SRM 51-70-03 REF FROM 57-60-01.

Part: COWL — ERODED (NR 1 ENG)

AT HMV, THE NR 1 ENG NOSE COWL WAS FOUND ERODED ON THE COMPOSITE L/E. THIS WAS REPAIRED PER SRM 54-11-01 REF 51-70-03.

Part: SKIN — CRACKED (NR 1 PYLON)

AT HMV, THE NR 1 PYLON O/B SKIN WAS FOUND TO BE CRACKED ON TOP AFT CORNER OF CUTOUT FOR PANEL 433 AT INSIDE OF STRUT BOX. THE DAMAGE WAS CUT OUT, HFEC OF CUTOUT WAS OK. DOUBLER WAS DRILLED AND REAMED TO FINAL SIZE AND INSTALLED PER SRM 54-51-01.

Part: SKIN — CRACKED (NR 2 PYLON)

AT HMV, THE NR 2 PYLON O/B SKIN WAS FOUND CRACKED AT TOP FWD CORNER OF CUTOUT FOR PANEL 443 AR. THE CRACK WAS ROUTED OUT PER SRM 54-51-01 DYE PEN. INSP PER PS 900-6-3, NO CRACK FOUND. DOUBLER PER SRM 54-57-01 WAS FABRICATED AND INSTALLED.

Part: SKIN — CRACKED (NR 1 PYLON)

AT HMV, THE NR 1 PYLON I/B SKIN WAS FOUND CRACKED PAST STOP DRILL ON TOP FWD CORNER OF CUTOUT FOR PANEL 433 AR. THE DAMAGE WAS REMOVED AND AREA DYE PENETRANT INSP PER PS 900-6-3 NR 01, NO CRACK FOUND. HFEC INSP, NO CRACK FOUND. DRILLED AND INSTALLED DOUBLERS PER SRM 54-51-01.