N948DN

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,462 hrs · 36,517 cycles

OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER AND PACK. OPERATION CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (L2 DOOR SLIDE) · airframe 43,461 hrs · 36,515 cycles

L2 DOOR SLIDE DISCHARGE BOTTLE GAUGE NEEDLE IN RED. REMOVED AND REPLACED SLIDE IAW MM. (LP# 2991305)

Part: ATTACH ANGLE — CRACKED (BS 1475) · airframe 43,461 hrs · 36,515 cycles

LONGERON TO FRAME ATTACH ANGLE IS CRACKED AT BS 1475 LONGERON 2L. REPLACED IAW SRM 51-30-05 AND DWG 9964460, REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,461 hrs · 36,515 cycles

FRAME, STA 924, RIGHT HAND SIDE, HAS A CRACK. REPAIRED.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,461 hrs · 36,515 cycles

CUSP WEB, STA 940, RBL 44 IS CRACKED AT FASTENER HOLE. REPAIRED IAW SRM 53-20-02.

Part: STRUCTURE — CORRODED (FUEL TANK) · airframe 43,461 hrs · 36,515 cycles

CORROSION, STA 912, RBL 56 CENTER WING TANK. REPAIRED IAW ERA 555238-14.

Part: HYDRAULIC SYSTEM — PRESSURE LOSS (RIGHT) · airframe 42,826 hrs · 36,181 cycles

AFTER TAKE-OFF. RIGHT HYDRAULIC PRESSURE 0. QUANTITY WAS NORMAL. AN ALTERNATE GEAR EXTENSION WAS PERFORMED DUE TO THE RIGHT HYDRAULIC PRESSURE LOSS. EMERGENCY DECLARED AND RETURNED TO DEPARTURE. MAINTENANCE REPLACED RIGHT EDP, HYDRAULIC SYSTEM FILTERS AND FLUSHED SYSTEM TWICE DUE TO CONTAMINATION IAW MM. DURING OPS CHECK RT EDP ONLY PUTS OUT 2000 PSI. REPLACED RT HYD. PRESSURE TRANSMITTER IAW AMM. LEAK AND FUNCTION CHECKS OK.

Part: FRAME — CRACKED (BS 1520) · airframe 42,358 hrs · 35,922 cycles

CANTED FRAME, BS 1520, WEB CRACKED AT UPPER LEFT CORNER AT LONGERON 1. COMPLIED WITH ERA 552506-14, REV O.

Part: ANGLE — CRACKED (BS 1520) · airframe 42,358 hrs · 35,922 cycles

ANGLE CRACKED FORWARD SIDE OF CANTED FRAME BS 1520 BETWEEN LONGERONS 17 - 18L. COMPLIED WITH PRI/ERA 552554-14.

Part: FRAME — CRACKED (BS 1520) · airframe 42,358 hrs · 35,922 cycles

CANTED FRAME, BS 1520, WEB CRACKED AT UPPER LEFT CORNER OF CUT OUT . REPAIRED IAW ERA 552506-14, REV O.

Part: FRAME — CRACKED (BS 1542) · airframe 42,358 hrs · 35,922 cycles

INBOARD FLANGE OF CANTED FRAME , BS 1542 AFT SIDE CRACKED. COMPLIED WITH SRM 53-10-03.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,722 hrs · 35,520 cycles

EMERGENCY LIGHTS AT FORWARD OVERWING ESCAPE HATCH INOPERATIVE. REPLACED BATTERY PACK AT SEAT 25D IAW MM. OPS CHECKED GOOD.

Part: CLEVIS — BROKEN (CATWALK CABLE) · airframe 41,021 hrs · 35,126 cycles

AFT FUSELAGE CATWALK LIFT CABLE END BROKEN. INSTALLED NEW CLEVIS ON CABLE IAW MM.

Part: BATTERY PACK — OVERHEATED (EMERGENCY LIGHTS) · airframe 40,824 hrs · 35,014 cycles

DURING PUSH BACK, CREW REPORTED A STRONG ELECTRICAL ODOR IN THE REAR OF THE CABIN. ACFT RETURNED TO GATE. MAINTENANCE TROUBLESHOT AND FOUND EMERGENCY LIGHT BATTERY PACK AT ROW 36CDE SIGNIFICANTLY OVERHEATING. REMOVED AND REPLACED SAME. OPERATION CHECKS GOOD.

Part: SKIN — DENTED (BS 168-175) · airframe 38,412 hrs · 33,615 cycles

DENT DAMAGE ON FUSELAGE SKIN AT BS 168.75 - 178, S6R TO S20R. ACCOMPLISHED PERMANENT REPAIR IAW ERA 521303-14, REV C.

Part: DOUBLER — WORN (BS 1437) · airframe 38,412 hrs · 33,615 cycles

TAIL INTERIOR B-FRAME WEB DOUBLER AND RIVET AT BS 1437 FORWARD SIDE ARE DEEPLY WORN, NEAR LONGERON 5L. REPAIRED IAW PRI 536163-14, REV O AND ERA 536163-14, REV O. LP 1961718.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 38,412 hrs · 33,615 cycles

VERTICAL FIN SKIN HAS ONE INCH LONG CRACK AT RIVET LINE NEAR BS 1475. REPAIRED IAW ERA 516509-14MA, REV A. LP 1960283.

Part: SHEAR TIE — CRACKED (BS 1508) · airframe 38,412 hrs · 33,615 cycles

TAIL INTERIOR CRACKED SHEAR TIE AT BS 1508, JUST INBD OF L2L. REPLACED SHEAR TIE IAW SRM 51-00-01.

Part: LONGERON — CRACKED (BS 1475) · airframe 38,394 hrs · 33,603 cycles

LONGERON 2L IS CRACKED AT BS 1475. SPLICED NEW SECTION IAW SRM 53-30-01.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 38,412 hrs · 33,615 cycles

VERTICAL FIN SKIN HAS A FOUR INCH LONG CRACK AT RIVET LINE NEAR BS 1475. REPAIRED IAW ERA 516509-14MA, REV A.

Part: SKIN — CRACKED (BS 1494) · airframe 38,412 hrs · 33,615 cycles

AIRCRAFT SKIN HAS 1.5" LONG CRACK NEAR BS 1494, OTBD OF LONGERON 3R. ANOTHER CRACK INBD OF LONGERON 4R. COMPLIED WITH PRI 536060-14, REV O AND ERA 536060-14, REV O.

Part: SKIN — CRACKED (BS 1475) · airframe 38,394 hrs · 33,603 cycles

SKIN CRACKED FROM FASTENER HOLE AT BS 1475 JUST INBD OF L1R. REPAIRED IAW SRM 53-30-01, FIG 16.

Part: STRUCTURE — CRACKED (VERTICAL STAB) · airframe 38,412 hrs · 33,615 cycles

CRACKED FLANGE ON VERTICAL FIN NEAR BS 1475. R & R FORMER AND DOUBLER IAW DWG 5910242.

Part: SKIN — CRACKED (BS 1494) · airframe 38,394 hrs · 33,603 cycles

AIRCRAFT SKIN HAS A CRACK NEAR BS 1494, OTBD OF LONGERON 3L. REPAIRED IAW SRM 53-00-01, FIG 6.

Part: SKIN — CRACKED (BS 1494) · airframe 38,394 hrs · 33,603 cycles

AIRCRAFT SKIN HAS TWO CRACKS NEAR BS 1494, OTBD OF LONGERON 3 AND INBD OF LONGERON 4. REPAIRED IAW ERA 536060-14.

Part: SKIN — CRACKED (BS 1494) · airframe 38,394 hrs · 33,603 cycles

ACFT HAS SKIN CRACKED, BS 1494, TWO INCHES OTBD OF LONGERON 3 AND 4. REPAIRED.

Part: STRUCTURE — DENTED (L1 DOOR) · airframe 34,934 hrs · 31,433 cycles

L1 DOOR HAS A DENT APPROXIMATELY 6 INCHES AT LOWER FWD EDGE. REPAIRED IAW SRM 52-01-01, PAGE 23-29. OK FOR SERVICE.

Part: LANYARD — MISINSTALLED (R1 DOOR GIRT BAR) · airframe 33,222 hrs · 30,413 cycles

DURING CHECK, R1 DOOR GIRT BAR LANYARD NOT INSTALLED CORRECTLY. INSTALLED R1 GIRT BAR LANYARD IAW MM.

Part: LANYARD — MISINSTALLED (L1 GIRT BAR) · airframe 33,222 hrs · 30,413 cycles

DURING CHECK, FOUND L1 DOOR GIRT BAR LANYARD NOT INSTALLED CORRECTLY. INSTALLED L1 DOOR SLIDE GIRT BAR LANYARD IAW MM.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 33,221 hrs · 30,412 cycles

DURING INSPECTION OF RT UPPER INBD HORIZONTAL STABILIZER PLANK, FOUND AN EXISTING TRIM OUT ON 01091 AND EM 5511-01023. COMPLETED REPAIR IAW PRI 513426-14AD. REPAIR COMPLETE AND FINAL ERA ISSUED 513426-14AD REV O.

Part: LANYARD — FRAYED (TAILCONE SLIDE) · airframe 33,221 hrs · 30,412 cycles

TAILCONE SLIDE LANYARD FRAYED. R & R TAILCONE SLIDE LANYARD IAW AMM.

Part: LANYARD — FRAYED (TAILCONE SLIDE) · airframe 33,221 hrs · 30,412 cycles

TAILCONE SLIDE LANYARD FRAYED. R & R TAILCONE SLIDE LANYARD IAW AMM.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 33,221 hrs · 30,412 cycles

A BONDED REPAIR DOUBLER WAS INSTALLED ON THE HORIZONTAL STABILIZER RT UPPER SKIN PANEL IAW ERA 513426-14AD, SECTION I. REPETITIVE INSPECTIONS AT 1,000 CYCLE INTERVALS AFT SECTION I, REPAIR AND SECTION III ONE TIME INSPECTION AFTER 3,000 CYCLES BUT BEFORE 5,000 CYCLES FROM SECTION I REPAIR INSTALLATION.

Part: SKIN — MISREPAIRED (BS 389) · airframe 33,221 hrs · 30,412 cycles

FUSELAGE SKIN REPAIR FS 389, LONGERON 16R IS NOT COMPLAINT WITH SRM. REMOVED PREVIOUS REPAIR. FABRICATED NEW REPAIR DOUBLER, FILLER AND FINGER DOUBLERS. INSTALLED REPAIR PARTS IAW SRM 51-30-02 AND ERA 513394-14, REV O.

Part: WEB — CORRODED (FUSELAGE) · airframe 33,221 hrs · 30,412 cycles

FOUND INTERIOR WEB CORRODED IN SEVERAL PLACES. REMOVED WEB. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. FABRICATED NEW WEB IAW SRM 51-30-05 AND DWG 9963260.

Part: SEAT TRACK — CRACKED (BS 401) · airframe 33,221 hrs · 30,412 cycles

CABIN SEAT TRACK BS 401 HAS TWO CRACKS AT SCALLOP. R & R SEAT TRACK IAW SRM 53-20-01 AND 51-30-01 AND DWG 5930547 AND SR09530115-7005.

Part: SKIN — DAMAGED (BS 826) · airframe 33,221 hrs · 30,412 cycles

EXTERNAL FUSELAGE SKIN DOUBLER AT BS 826, LONGERON 28R CORRODED AT DOME NUT HOLE. FABRICATED FILLER, DOUBLER AND TRIPLER IAW SRM 53-30-01 PRIMED AND INSTALLED REPAIR PARTS ON EXTERNAL FUSELAGE SKIN AT BS 826 L28R IAW SRM 53-30-01.