N961DN

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,306 hrs · 25,885 cycles

FWD LEFT AND RIGHT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. R & R BATTERY PACK IAW MM 33-51.

Part: MODULE — MALFUNCTIONED (THROTTLE) · airframe 49,208 hrs · 25,828 cycles

LANDING GEAR UNSAFE LIGHTS. THREE RED ILLUMINATED AT 10,000 AT 320KTS WITH THROTTLES ADVANCED. LIGHTS WENT OUT WHEN THROTTLES RETARDED. MAINTENANCE TROUBLESHOT. REMOVED AND REPLACED THROTTLE MODULE PER MM. OPERATION CHECKS OK.

Part: LANDING GEAR — MALFUNCTIONED · airframe 49,208 hrs · 25,828 cycles

PERFORMED AN AIR TURN BACK, DUE TO THREE RED GEAR UNSAFE INDICATIONS WITH GEAR HORN AFTER LIFT OFF. GEAR HANDLE WAS IN THE RAISED POSITION. COMPLIED WITH QRH 14.5. PLACED GEAR HANDLE DOWN NOSE GEAR INDICATION STAYED RED. INCREASED SPEED TO 250 KTS. NOSE GEAR RED UNSAFE LIGHT EXTINGUISHED. UNEVENTFUL LANDING. REMOVED, REPLACED AND ADJUSTED NLG LOCKED SWITCH, D1-32 AND GEAR HANDLE SWITCH, S1-89. PERFORMED GEAR SWING PER AMM. ALL INDICATIONS AND OPERATIONS NORMAL. NLG STRUT SERVICE CHECKED GOOD PER AMM. AIRCRAFT OKAY FOR SERVICE. (LP#8869798)

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 50,530 hrs · 26,601 cycles

CORROSION RIGHT SERVICE DOOR GIRT BAR FITTING INSERTS. INSTALLED A NEW ATTACH FITTING IAW DWG 3936190.

Part: BEAM — CRACKED (L1 DOOR) · airframe 48,342 hrs · 25,322 cycles

L1 DOOR INTERIOR NR 1 BEAM CRACKED AT THE AFT END. INSTALLED NEW BEAM IAW SRM 53-30-05 AND DWG 9955752.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,152 hrs · 24,571 cycles

EMERGENCY LIGHTS AT ROWS 24-26 INOPERATIVE. R & R BATTERY PACK IAW AMM. OPERATION CHECKS OK.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 46,365 hrs · 24,108 cycles

F/A REPORTED A BURNING ACRID ODOR NEAR EXIT ROW AFTER TAKEOFF. MAINTENANCE FOUND EMERGENCY LIGHT BATTERY OVERCHARGED AND HOT OVER EXIT DOOR. R & R POWER SUPPLY AND BATTERY PACK IAW AMM. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,905 hrs · 23,841 cycles

EMERGENCY CEILING LIGHT INOPERATIVE BETWEEN ROWS 23 AND 26. R & R EMERGENCY BATTERY ASSY IAW AMM. OPERATION CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,750 hrs · 23,750 cycles

EXIT SIGNS OVER EMERGENCY WING EXITS INOPERATIVE. REPLACED THE BATTERY PACK. OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,173 hrs · 23,384 cycles

CEILING EMERGENCY LIGHTS INOPERATIVE AT SEATS 23, 24 AND 26 RT SIDE. R & R BATTERY AND POWER SUPPLY IAW AMM. OPS CHECKED NORMAL.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 44,328 hrs · 22,822 cycles

AFT DOOR AND STAIRS EMERGENCY LIGHTS INOPERATIVE. R & R POWER SUPPLY IN CARGO BIN FORWARD OF LAVATORY IAW AMM. OPERATION CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,990 hrs · 21,979 cycles

OVERWING EMERGENCY LIGHTS NOT ILLUMINATING. R & R POWER SUPPLY.

Part: FRAME — CRACKED (BS 1520) · airframe 42,990 hrs · 21,979 cycles

CANTED FRAME BS 1520, AFT WEB CRACKED INSIDE LT VENT BOX. REPAIRED IAW PRI 525053-14, REV 1.

Part: SKIN — CORRODED (BS 1531) · airframe 42,990 hrs · 21,979 cycles

TAILCONE LT SIDE OUTER SURFACE SKIN CRACKED AT STA 1531, APPROX 12 INCHES ABOVE VENTRAL STAIR DOOR CUTOUT. CUT OUT DAMAGE IAW SRM. FABRICATED AND INSTALLED NEW DOUBLER AND FILLER IAW SRM 53-00-01.

Part: DOOR FRAME — CRACKED (RT MLG DOOR) · airframe 40,636 hrs · 20,510 cycles

RT MLG DOOR FRAME HAS A CRACK 2.5" LOCATED 4" BELOW DOOR SENSOR. REMOVED FRAME. DRILLED NEW DOOR FRAME AND INSTALLED.

Part: SKIN — DAMAGED (BS 424-514) · airframe 38,168 hrs · 19,147 cycles

RT ALTERNATE STATIC PORT HAS MANY AREAS IN CRITICAL SEMI CRITICAL AND CONTROLLED AREAS THAT ARE OUT OF WAVINESS TOLERANCE. REMOVED AND REPLACED SECTION OF FUSELAGE SKIN BETWEEN STA 424 TO 514 FROM L26R AND BETWEEN L24R AND L25. REINSTALLED REPAIR REFERENCES USED MD90 SUM 51-30-02, 51-30-05, 51-10-03 AND 51-10-05 VOLE II, 53-30-01 FIG 5 VOLE AND DELTA ERR/A 502685-14.

Part: SKIN — DAMAGED (FS 394-488.5) · airframe 38,168 hrs · 19,147 cycles

LT ALTERNATE STATIC PORT HAS SPOTS IN RVSM CONTROLLED AREA THAT ARE OUT OF WAVINESS TOLERANCES. REMOVED AND REPLACED SECTION OF FUSELAGE SKIN BETWEEN STA 394 TO 488.5 FROM L26L TO BETWEEN L24L AND L25L AND INSTALLED REPAIR REFERENCES USED MD90 SRM 51-30-02, 51-10-03, 51-30-05, 51-10-05 VOL II 53-30-01 FIG 5 VOLI DRW NR 5920323 AND ER/A 502684-14.

Part: FRAME — CORRODED (BS 446 L29-30L) · airframe 38,168 hrs · 19,147 cycles

FWD CARGO COMPT BILGE AREA STA 446 BETWEEN L29L-L30 WITH CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IN REF SRM 53-00-01. CUT FRAME SECTION STA 446 BETWEEN L26L AND L26R IN REF SRM 53-10-02 VOL II. LOCATED AND DRILLED NEW SECTION OF FRAME IN REF SRM 51-10-05. FABRICATED SPLICES IN REF SRM 53-10-01 VOL I. TREATED AND PRIMED FRAME AND SPLICE IN REF MD90 SRM 51-10-3 VOL II. INSTALLED FRAME AND SPLICE AT STA 446 BETWEEN L26L AND L26R IN REF SRM 51-30-02 AND 51-30-05 VOL I AND 51-10-02 FIG 2.

Part: LONGERON — GOUGED (BS 439 L26R) · airframe 38,168 hrs · 19,147 cycles

FWD CARGO L26R STA 439 HAS GOUGES. CUT-OUT DAMAGED SECTION OF L26R IN FWD CARGO FROM F/S 434-475. REPLACED LONGERON AND INSTALLED REPAIR, REF USED SRM 51-30-00, 51-30-02, 51-30-05 VOL II, 53-10-01 FIG 7 VOL I AND ER/A 501337-14. COMPARED PRI AND ER/A AND NO DIFFERENCES NOTED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

SKIN WAVY AT ROW OF RIVETS BELOW LEFT ALTERNATE STATIC PORT. REMOVED AND REPLACED SECTION OF FUSELAGE SKIN FROM BS 401.5 TO 500 AND BETWEEN L26L TO L26R AND INSTALLED REPAIR PER ERA 501337-14 REV O.

Part: LONGERON — CORRODED (BS 455-494 L29L) · airframe 38,168 hrs · 19,147 cycles

AT FWD CARGO COMPARTMENT LONGERON 29L HAS CORROSION FROM STA 455 TO 494. REMOVED DAMAGED SECTION OF L29L IN FWD CARGO FROM FS 455 TO 494. REPLACED LONGERON AND INSTALLED REPAIR, REFERENCES USED SRM 51-30-00, 51-30-02, 51-30-05 VOL II, 53-10-01 FIG VOL I, AND DELTA ER/A 501337-14. COMPARED PRI AND ER/A AND NO DIFFERENCES NOTED.

Part: SKIN — MISREPAIRED (BS 229-248) · airframe 38,168 hrs · 19,147 cycles

RIGHT SKIN SPLICE AFT OF R1 DOOR BS 229 TO 248 L15 TO 18R DAMAGED IN AREA AND MISSING SHIMS, OUTWARD DENT, SEVERAL FASTENERS BAD, AND SKIN BULGED. REPAIRED PER ERA 498686-14 REV 0.

Part: SHEAR TIE — DAMAGED (BS 446) · airframe 38,168 hrs · 19,147 cycles

AT FWD CARGO COMPARTMENT BS 446 FROM L26R TO L26L SHEAR TIE HAS ILLEGAL REPAIR AND DAMAGED HOLES. REMOVED AND REPLACED SHEAR TIE PER SRM 51-30-03, 51-30-02, AND 51-30-05.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 38,168 hrs · 19,147 cycles

RT MLG RETRACT SUPPORT FITTING BUSHING BORE HAS CORROSION, PITTING ON SURFACE. MACHINED RT RETRACT BUSHING BORE TO 2.381 AND REMOVED .068 FROM BUSHING BORE INNER FACE. EXCEEDED LIMITS OF EA 02-093855-03 REV A. FABRICATED OVERSIZED BUSHING PER ERA 487463-14AD AND INSTALLED PER EA 02-093855-03 REV A.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 38,168 hrs · 19,147 cycles

LEFT MLG RETRACT CYL BUSHING BORE HAS CORROSION ON SURFACE. MACHINED RETRACT BUSHING BORE TO 2.378 AND REMOVED .083 FROM BUSHING BORE INNER FACE AND EXCEEDS LIMITS. FABRICATED OVERSIZED BUSHING AND BEARING PER ERA 487467-14AD AND INSTALLED PER EA 02-093855-03AD REV A.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 38,168 hrs · 19,147 cycles

RT MLG RETRACT CYL BEARING BORE HAS VERY LIGHT SURFACE CORRSION AND BARE METAL. MACHINED RT RETRACT BEARING BORE TO 1.536 TO REMOVE CORROSION. FABRICATED AND INSTALLED OVERSIZED BEARING PER ERA 487463-14AD AND EA 02-093855-03AD REV A.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

AFT CARGO COMPT BILGE TIE DOWN CLIP CORRODED OUT OF LIMITS AT STA 1231 RBL 3. FABRICATED NEW SHEAR CLIP AND INSTALLED PER MD 90 SRM 51-30-02, 51-10-03, 53-00-01, 51-10-01, 51-10-05, AND DWG 9936073.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

MID CARGO BILGE ANTENNA CUTOUT CORRODED OUT OF LIMITS. REMOVED AND REPLACED ANTENNA CUTOUT INNER DOUBLER PER MD 90 SRM 51-30-02 AND 51-30-05.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

MID CARGO STA 742 BETWEEN L29L AND L30 INTERNAL DOUBLER CORRODED. REPAIRED PER ERA 491775-14 REV 0.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

ELONGATED HOLES L16LT FS 230-255. INSTALLED NEW LONGERON SECTION FROM FS 230-265 L16LT PER SRM 53-10-01 FIG 7, 51-30-02 AND 51-30-05.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

L17L FROM STA 230 TO STA 255 WITH ELONGATED HOLES. REMOVED AND REPLACED SECTION AND SPLICE REPAIR PER MD 90 SRM 53-10-01 VOL I FIG 7.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

L17LT FS 230-255 HAS ELONGATED HOLES. SPLICED IN NEW SECTION OF LONGERON FROM FS 230-285 PER SRM MD90 51-30-02, 51-30-05 AND 53-10-01 FIG 7.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

L16R BETWEEN STA 229 TO 250 HAS ELONGATED HOLES. REPLACED SECTION OF LONGERON PER SRM 53 10 01 V1.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

L17R BETWEEN STA 229 TO 260 HAS ELONGATED HOLES. REPLACED LONGERON SECTION PER SRM 513002 VOL II REF (NR 920089).

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

CENTER CARGO COMP BILGE AREA LONGERON SLICE BETWEEN STA 579 TO STA 598 ON L-29-L CORRODED. REMOVED AND REPLACED LONGERON SPLICE PER MD 90 SRM 51-30-05 VOL II.

Part: LONGERON SPLICE — CORRODED (BS 579-598 L28L) · airframe 38,168 hrs · 19,147 cycles

LONGERON 28 LEFT SPLICE BETWEEN BS 579 - 598 CORRODED. REPLACED SPLICE AND RADIUS FILLER PER SRM 51-10-05 VOL I, 51-10-03 VOL II, AND 51-30-05 VOL II.

Part: LONGERON SPLICE — CORRODED (BS 218-229 L28R) · airframe 38,168 hrs · 19,147 cycles

FWD CARGO BAY BILGE AREA BETWEEN BS 218 - 229 L28R LONGERON SPLICE CORRODED. REPLACED SPLICE PER SRM 51-10-03 VOL II.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 38,168 hrs · 19,147 cycles

DORSAL FIN FWD LOWER PANEL CUTOUT UPPER CORNER CRACKED. INSTALLED DOUBLER REPAIR PER SRM 51-70-01 VOL I.

Part: INTERCOSTAL — CORRODED (BS 1205-1212) · airframe 38,168 hrs · 19,147 cycles

CORROSION ON INTERCOSTAL AT AFT CARGO STA 1205 THRU 1212 L30-L29R. FABRICATED NEW INTERCOSTAL PER DWG 5936071 AND INSTALLED PER MD 90 SRM 51-30-02.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

FS 1375 DENTED L25R & L24R INTERNAL SKIN DOUBLER DEFORMED. INSTALLED NEW DOUBLER AND FILLER PER SRM MD90 53-31-02.

Part: SHEAR TIE — DAMAGED (BS 465 L26L/R) · airframe 38,168 hrs · 19,147 cycles

AT FWD CARGO COMPARTMENT STA 465 FROM L26L TO L26R SHEAR TIE MISREPAIRED AND DAMAGED HOLES. REMOVED AND INSTALLED NEW SHEAR TIE PER SRM 51-30-05 AND 51-30-02 VOL II.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

EXTERNAL DOUBLER REPAIR INSTALLED AT TOP OF FUSELAGE APPROX STA 351 HAS INTERNAL FINGER DOUBLER BULGING, TOOL MARKS, AND OVER 50 PERCENT OF THE FASTENERS IMPROPERLY INSTALLED. REMOVED EXISTING REPAIR AND INSTALLED NEW REPAIR PER MD 90 SRM 53-31-03 FIG 8 VOL I.

Part: WEB — CRACKED (BS 160-200) · airframe 38,168 hrs · 19,147 cycles

CABIN WEB AT BS 200 AND 160 LT CRACKED. INSTALLED WEB REPAIR PER SRM 51-11-01 FIG 2 VOL I.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

SEAT TRACK CORRODED OUT OF LIMITS AT STA 1250 - STA1269 LBL 22. REPLACED SEAT TRACK PER MD 90 SRM 53-40-01 FIG 6.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

AFT CARGO COMPT AFT BULKHEAD AFT FACE LOWER LOBE CORRODED OUT OF LIMITS AT STA 1395 RBL 2-10. FABRICATED NEW WEB AND WEB SPLICE AND INSTALLED PER MD 90 SRM 51-30-00.

Part: WEB — CORRODED (BS 685-757) · airframe 38,168 hrs · 19,147 cycles

MID CARGO BAY WEB BETWEEN BS 685 THRU 757 AND BETWEEN L26 THRU 30R CORRODED OUT OF LIMITS. REPLACED WEB PER SRM 51-30-02 AND 51-30-05 VOL II.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

AFT CARGO PRESSURE BULKHEAD DOME "T" EXTRUSION AT LONGERON 30 CORRODED. FABRICATED AND INSTALLED "T" EXTRUSION PER DWG 5910130.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

LEFT SKIN SPLICE AFT OF L-1 DOOR STA 229 -STA 248, LONGERON17L TO 18L, HAS TOOLING MARKS IN AREA. MISSING SHIMS AND STRAP, OUTBOARD DENTS, SEVERAL FASTENERS BAD, AND SKIN BULGES. REMOVED EXISTING SKIN REPAIR AND DAMAGE. INSTALLED FLUSH PANEL REPAIR PER MD 90 SRM 53-30-01 FIG 5.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

AFT CARGO COMP BILGE AREA, FUSELAGE SPLICE BETWEEN FRAME STA 1231 AND STA 1250 AND BETWEEN STR'S 29L AND 30 CORRODED. FABRICATED NEW SPLICE STRAP AND INSTALLED PER DWG 593667.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

SEAT TRACK CORRODED AT STA 200-STA 285 RBL 22. INSTALLED SEAT TRACK REPAIR SPLICE AND TRACK PER MD 90 SRM 53-40-01 VOL I FIG 6.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

CORROSION ON CUSP WEB FS 1231-1250 RBL 58. DAMAGED REMOVED AND REPAIR DOUBLER INSTALLED REF SRM MD90 53-20-02 FIG 16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

CABIN FLOOR RT CUSP WEB HAS CORROSION BETWEEN FRAME STA 1231 TO 1250 RBL 58 REF NR 1000-0261 SERIAL 919174. REPAIRED PER SRM 53-20-02 FIG 11. (NR 1000-0261).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

SEAT TRACK FLANGE CORRODED OUT OF LIMITS BETWEEN STA 200 TO STA 256 RBL 44. INSTALLED SEAT TRACK SPLICE PER MD 90 SRM 53-40-01 FIG 6.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

SEAT TRACK FLANGE CORRODED OUT OF LIMITS AT STA 200 AND 256 LBL 22. INSTALLED SEAT TRACK SPLICE REPAIR FROM STA 200 TO STA 265 IN REF WITH MD 90 SRM 53-40-01 FIG 6 SHEET 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,168 hrs · 19,147 cycles

SEAT TRACK FLANGE CORRODED FROM STA 200 TO STA 304 LBL 44 AND OUT OF LIMITS. INSTALLED SEAT TRACK SPLICE REPAIR PER MD 90 SRM 53-40-01 FIG 6.

Part: PAN — CORRODED (BS 370-427) · airframe 38,168 hrs · 19,147 cycles

FWD CARGO COMPARTMENT DOOR JAMB FROM STA 370 TO 427 WITH CORROSION. REPAIRED LWR DOOR PAN PER SRM 53-60-02 FIG 11 VOL I.

Part: SHEAR TIE — CORRODED (BS 750 S29-30R) · airframe 38,168 hrs · 19,147 cycles

MID CARGO COMPT STA 750 BETWEEN STR L30-29R INTERCOSTAL SHEAR TIE CORRODED. REPLACED INTERCOSTAL SHEAR TIE PER MD 90 SRM 51-30-05 AND 51-30-02 VOL II.

Part: FRAME — CORRODED (BS 465) · airframe 38,168 hrs · 19,147 cycles

FWD CARGO COMPARTMENT STA 465 FRAME AFT SIDE BETWEEN L20L TO L30 HAS CORROSION OUT OF LIMITS. REMOVED CORRODED FRAME SECTION AND REPLACED PER SRM 53-10-02 FIG 2 VOL I.

Part: CUSP WEB — CORRODED (BS 503-522) · airframe 38,168 hrs · 19,147 cycles

CORROSION ON LEFT CUSP WEB BS 503-522 OUT OF LIMITS. REPAIRED PER SRM 53-20-02 FIG 11 VOL I.