N919DN

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,621 hrs · 22,653 cycles

ROW 25 EMERGENCY LIGHT OUT C/A R/R BATTERY ASSY PER MD90 AMM 33-51. OPS CHECK IS GOOD AT THIS TIME. (6615064)

Part: UNKNOWN — ODOR (CABIN) · airframe 46,419 hrs · 22,515 cycles

WHILE PULLING INTO THE GATE. AFTER LANDING IN SYRACUSE WE ACTIVATED APU AIR. THE FA IN THE AFT CABIN CHIMED THE COCKPIT TO REPORT FUMES THAT SMELLED LIKE RUBBER. AS PASSENGERS DEPLANED THE FORWARD FA'S REPORTED FUMES. I WALKED OUTSIDE TO SEE IF THE FUMES WERE OUTSIDE THE AIRCRAFT. THEY WERE NOT. WHEN I RE-ENTERED THE AIRCRAFT THE FUMES WERE GONE. THE APU AIR WAS STILL ACTIVE(ON). ABOUT 10 MINUTES LATER FA'S REPORT TO FO MORE FUMES. (CAPT WAS NOT ON BOARD). FO TURNS OFF APU AIR AND FUMES ABATE. COCKPIT AND CABIN HAVE NO FUMES . THEN. FO TRIES APU AIR AND FUMES IMMEDIATELY RETURN. FO TURNS OFF APU AIR. WE SECURE EXTERNAL POWER AND SHUT DOEN APU. T/S PER MD90 FIM 21-22. FOUND APU BLEED AIR WITH BURNING ACRID SMELL. MCC NOTIFIED. C/W BURNOUT OF PNEU. HIGH PRESS DUCTING PER MD90 AMM 21-53. NO ODORS PRESENT WITH ENGINE AIR. APU AIR INOP ON LOG 6612981. C/W MD90 NO GO ODI PREVENTION ATA 2172. OK FOR SERVICE. (6612978)

Part: CABLE — FRAYED (TAILCONE) · airframe 45,896 hrs · 22,186 cycles

AFT TAILCONE DISPLACEMENT NITROGEN CYLINDER PULL CABLE FRAYED THROUGH. REMOVED AND REPLACED CABLE PER AS REQUIRED PER AMM 53-52. SERVICED NITROGEN CYL PER AMM 12-16. LEAK CHECK GOOD. (LP# 4623321)

Part: BATTERY — THERMAL RUNAWAY (MAIN) · airframe 44,290 hrs · 21,119 cycles

FOUND BOTH SHIP BATTERIES THERMAL RUNAWAY & BATT CABLES INSULATION MELTED. BATTERIES REMOVED FROM A/C. ROUTED BATT WIRES P48B2 AND P49B2. TERMINATED AND INSTALLED ENDS AT LEFT AND RIGHT BATTERIES. TERMINATED CENTER BATTERY CONNECTOR PER SWPM 20-00-16 & WDM 24-31-00. WIRES REPLACED WITH BMS13-58T1C1G2 AS ENGINEERING APPROVED REPAIR BY ERA 575010 PER PS 900-5-1, NR 04. REMOVED AND REPLACED A/C BATTERY SET AND TEST OK PER AMM 24-34-01/401. OK FOR SERVICE.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 44,269 hrs · 21,106 cycles

DURING REPLACEMENT OF RH ATTACH ANGLE WAS FOUND A CRACK ON VERTICAL STABILIZER SKIN STA ZFS= -26.8. VERTICAL STABILIZER SKIN STA ZFS= -26.8 WAS REPAIRED (PERMANENT REPAIR) PER ERA 574733-14AD REV ORIGINAL AND ETI-90-19-03 REV 1. REPAIR APPROVAL IS LIMITED TO 60,000 TOTAL CYCLES ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. REF : FAA AC 120-93. PER ERA 574733-14 AD REV ORIGINAL. (LP# 0914321)

Part: PUSHROD — CORRODED (RUDDER) · airframe 44,269 hrs · 21,106 cycles

CORROSION ON RUDDER LIMITER PUSHROD P/N NAS354-4-270. RUDDER LIMITER PUSHROD P/N NAS354-4-270 WAS REPLACED PER AMM 27-23-02-420-801 AND WAS ADJUSTED PER AMM 27-26-01-820-801. (LP# 0912831)

Part: SEAL — MISSING (LE SLAT) · airframe 44,269 hrs · 21,106 cycles

APPROX 15 IN OF SPANWISE SLAT LOWER TRAILING EDGE SEAL MISSING FROM RT WING. NEW SEAL WAS INSTALLED PER VOL.II SRM 51-30-05 AND VOL.II SRM 51-30-02. (LP# 3897134)

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,269 hrs · 21,106 cycles

CRACK ON EXTERNAL FUSELAGE SKIN AT STA Y=1494 BTW LONGERONS 3R AND 4R. PERMANENT REPAIR WAS PERFORMED SECTION I ON EXTERNAL FUSELAGE SKIN AT STA Y=1494 BTW LONGERONS 3R AND 4R. WAS REPAIRED PER ER/A 574627-14 REV ORIGINAL AND ETI-90-19-02 REV. 2. PERFORM A GENERAL VISUAL INSPECTION EVERY 3000 FLIGHT CYCLES REF. SRM VOL II 51-10-11. IN REF ER/A NO 574627-14 REV. ORIGINAL SEC. II, AND FOLLOWED WILL BE ACCOMPLISHED UNDER LOG PAGE 0905261. (LP# 0907046)

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 44,269 hrs · 21,106 cycles

CRACKED RT INTERNAL VERTICAL STABILIZER ATTACH ANGLE ON STA. Y= 1475. RT INTERNAL VERTICAL STABILIZER ATTACH ANGLE ON STA. Y= 1475 WAS REPLACED PER SRM 51-30-02 AND 51-30- 05VOL.II. (LP# 0907778)

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 44,269 hrs · 21,106 cycles

CRACKED LT INTERNAL VERTICAL STABILIZER ATTACH ANGLE ON STA. Y= 1475. LT INTERNAL VERTICAL STABILIZER ATTACH ANGLE ON STA. Y= 1475 WAS REPLACED PER SRM 51-30-02 AND 51-30-05 VOL.II. (LP# 0907775)

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 44,269 hrs · 21,106 cycles

CRACK ON FWD DOOR JAMB STA Y=1012 X=57. FWD DOOR JAMB STA Y=1012 X=57 WAS REPLACED. (LP# 0904201)

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,269 hrs · 21,106 cycles

AWR HIDDEN DAMAGE IN REF MON/9219/045-MON, 92 L/L, 0566067 INSP. CORROSION ON FWD AND AFT LATCH FITTINGS OVER X=-54 WAS FOUND DURING REMOTION FLOOR PANEL 221KF (W1). LEVEL CORROSION 2; FWD AND AFT LATCH FITTINGS OVER X=-54 WERE REPLACED PER VOL. II SRM 51-30-01. (LP# 0900999)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,942 hrs · 19,690 cycles

EXIT LIGHTS ABOVE WING EXIT DOORS AT ROW 27 INOP. R&R BATTERY PACK AT ROW 27 PER AMM 33-51 CKS GOOD.

Part: SIGN — MISSING (CABIN) · airframe 40,834 hrs · 18,983 cycles

L2 DOOR EXIT SIGN MISSING. INSTALLED. OPERATION CHECKS GOOD.

Part: RECEPTACLE — WORN (TAILCONE) · airframe 40,340 hrs · 18,713 cycles

SEVERAL TAIL CONE GUIDE PIN RECEPTACLES FOUND WORN. REPLACED IAW SRM 51-30-00.

Part: OUTFLOW VALVE — OBSTRUCTED (CABIN PRESSURE) · airframe 40,340 hrs · 18,713 cycles

AT FL280, AUTO PRESSURIZATION ERRATIC. THE AUTO - MANUAL CONTROL SWITCH WAS UNABLE TO SELECT THE MANUAL MODE. CABIN ALTITUDE BEGAN TO RAPIDLY CLIMB. THE OXYGEN MASKS AUTOMATICALLY DEPLOYED DURING RAPID DECENT. TROUBLESHOT IAW FIM 21-30-00-801-802. FOUND THE AC MOTOR FAULTS ON BOTH 1 & 2 PRESSURE CONTROLLERS. ON FURTHER INVESTIGATION, A SCREW WAS FOUND IN THE OUTFLOW VALVE PEDESTAL TRACK RESULTING IN A BINDING OF THE PRESSURIZATION MANUAL CONTROL WHEEL. HARDWARE IN PEDESTAL REMOVED. REPLACED NOZZLE VALVE DRIVE ASSY. PERFORMED RIGGING OF THE NOZZLE VALVE DRIVE ASSEMBLY. OPERATIONAL CHECKED OK IN AUTO AND MANUAL MODE.

Part: SCREW — SHEARED (CARGO DOOR) · airframe 39,190 hrs · 18,102 cycles

CENTER CARGO DOOR JAMB HAS 1 SHEARED DOOR STOP ADJUSTMENT SCREW AFT EDGE. REMOVED AND REPLACED CENTER CARGO DOOR JAMB DOOR STOP AND SET SCREW IAW MM 52-31-01.

Part: SCREW — SHEARED (CARGO DOOR) · airframe 39,190 hrs · 18,102 cycles

AFT CARGO DOOR JAM HAS SHEARED DOOR STOP ADJUSTMENT SCREW AT EDGE. REMOVED AND REPLACED AFT CARGO DOOR JAMB IAW MM 52-31-01.

Part: FLOOR SUPPORT — NOT REPORTED (BS 180) · airframe 39,175 hrs · 18,092 cycles

MAIN CABIN FLOOR SUPPORT CRACKED, BS 180, LBL 2 IN E/E COMPARTMENT. REPAIRED IAW SRM 53-00-01.

Part: FRAME — CRACKED (BS 180) · airframe 39,175 hrs · 18,092 cycles

CRACKED FRAME ANGLE, BS 180, RBL 0. REMOVED AND REPLACED ANGLE IAW SRM 51-30-02 AND DWG 9936534 AND 9923484.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,453 hrs · 17,072 cycles

BOTH AFT OVERWIND EXIT SIGNS BY FLOOR INOPERATIVE, LT AND RT OVERWING HATCHES. REMOVED AND INSTALLED NEW BATTERY IAW MM. OPS CHECKS GOOD.

Part: CABLE — BROKEN (TAILCONE JET) · airframe 37,141 hrs · 16,907 cycles

TAILCONE JETTISON BOTTLE CABLE BROKEN. INSTALLED NEW CABLE ASSEMBLY.

Part: CHARGER — MALFUNCTIONED (MASTER BATTERY) · airframe 36,628 hrs · 16,592 cycles

BATTERY CHARGER FAIL MESSAGE ON OAP. FOUND ALL 3 BATTERIES VERY HOT. R & R BATTERIES, CHARGER, BATTERY RECEPTACLE PLUGS, AND STARTER RELAY IAW AMM.

Part: ATTACH BRACKET — CORRODED (TAIL CONE) · airframe 33,991 hrs · 14,958 cycles

CORROSION AROUND RIVETS OF D-RING ATTACH BRACKETS, TWO ON TAILCONES SLIDE VALISE. R & R THE ATTACH BRACKETS IAW SRM 51-30-02.

Part: FRAME — CORRODED (BS 1520) · airframe 33,991 hrs · 14,958 cycles

AFT ACCESSORY COMPARTMENT, FRAME BS 1520 BETWEEN LONGERONS 1 - 24L, LOWER END OF FRAME HAS SEVERAL SPOTS WITH CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED A REPAIR IAW DWG 9911839, REV DP, SRM 51-30-02 AND 51-30-03.

Part: ANGLE — CORRODED (BS 1463-1480) · airframe 33,991 hrs · 14,958 cycles

CORROSION ON ANGLE AND INTERNAL FUSELAGE SKIN AT LT SIDE OF VENTRAL STAIRS CUTOUT BS 1463-1480. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-30-02 AND DWG 9911991, REV K.

Part: CARGO TRACK — CORRODED (BS 1160-1307) · airframe 33,995 hrs · 14,961 cycles

AFT CARGO BAY CARGO TRACK BETWEEN BS 1160-1307 CORRODED. FOUND TO BE OUT OF LIMITS. R & R THE CARGO TRACK IAW SRM 53-40-01, FIG 5. AND FIG 7.

Part: BAR — CORRODED (LT WING TE FLAP) · airframe 33,991 hrs · 14,958 cycles

LEFT FLAP FLEX JOINT LOWER BAR HAS CORRODED. SEVERAL COUNTER SUNK HOLES. REMOVED CORROSION. REPAIRED IAW ERA 531458-14.

Part: SKIN — CORRODED (BS 1463-1480) · airframe 33,991 hrs · 14,958 cycles

CORROSION ON ANGLE AND INTERNAL FUSELAGE SKIN ON RT SIDE OF VENTRAL STAIR CUTOUT, BS 1463 - 1480. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 51-10-03, 51-30-02 AND DWG 9911991, REV K.

Part: CARGO TRACK — CORRODED (BS 522-845) · airframe 33,991 hrs · 14,958 cycles

CENTER CARGO BAY LT SIDE CARGO TRACK BETWEEN BS 522-845 HAS CORROSION AROUND FASTENERS, NUT PLATES AND FLANGES. REMOVED THE CORROSION AND FOUND THE FLANGES TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW CARGO TRACK IAW SRM 53-40-01, FIG 7.

Part: LANYARD — TORN (L1 DOOR SLIDE) · airframe 33,991 hrs · 14,958 cycles

L1 DOOR EVACUATION SLIDE LANYARD TORN. REMOVED AND INSTALLED NEW LANYARD IAW AMDS 2561-4641.

Part: FRAME — CRACKED (BS 1494) · airframe 33,991 hrs · 14,958 cycles

AFT ACCESSORY COMPARTMENT BS 1494, LONGERON 2R FRAME CRACKED. REMOVED CRACKED FRAME ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-10-05, FIG 1 AND DWG 9911860, REV L.

Part: FRAME — CRACKED (BS 1494) · airframe 33,991 hrs · 14,958 cycles

AFT ACCESSORY COMPARTMENT FRAME CRACKED AT LONGERON 2R, BS 1494. REMOVED CRACKED FRAME. FABRICATED AND INSTALLED NEW FRAME IAW DWG 9911860, REV L AND SRM 51-30-02.

Part: FINGER DOUBLER — DAMAGED (BS 1542) · airframe 33,991 hrs · 14,958 cycles

AFT ACCESSORY COMPARTMENT CANTED FRAME FINGER DOUBLER AT BS 1542 DAMAGED. REMOVED DAMAGED FRAME SECTION. FABRICATED AND INSTALLED NEW FINGER DOUBLER IAW DWG 9918558 AND DWG 5910228.

Part: FITTING — CORRODED (TAILCONE SLIDE) · airframe 33,991 hrs · 14,958 cycles

TWO TAILCONE SLIDE HOLD DOWN STRAP FITTINGS CORRODED. REMOVED AND INSTALLED TAILCONE SLIDE FORWARD HOLD DOWN STRAPS.

Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 33,991 hrs · 14,958 cycles

AFT CARGO DOOR FRAME CORRODED. FOUND CORROSION ON REPAIR SPACER. FABRICATED AND INSTALLED NEW SPACER IAW SRM 53-60-02, FIG 9A.

Part: LANYARD — TORN (L2 DOOR SLIDE) · airframe 33,991 hrs · 14,958 cycles

L2 DOOR EVACUATION SLIDE LANYARD CABLE ASSEMBLY IS TORN. REMOVED AND INSTALLED NEW SLIDE LANYARD IAW AMDS 2561-4642.

Part: ANGLE — CRACKED (BS 1475) · airframe 33,991 hrs · 14,958 cycles

CRACKED ANGLE AT FRAME 1475, LONGERON 2R, REMOVED AND REPLACED IAW DWG 5911432, REV CE AND SRM 51-30-05.

Part: ANGLE — CRACKED (BS 1475) · airframe 33,991 hrs · 14,958 cycles

CRACKED ANGLE AT FRAME 1475, LONGERON 2L, REMOVED AND REPLACED IAW DWG 5911432.

Part: ANGLE — CRACKED (BS 1475) · airframe 33,991 hrs · 14,958 cycles

CRACKED ANGLE AT BS 1475, LONGERON 2R. REMOVED AND REPLACED IAW DWG 9964461, REV W.

Part: ANGLE — CRACKED (BS 1475) · airframe 33,991 hrs · 14,958 cycles

ANGLE CRACKED AT BS 1475, LONGERON 2L, AFT SIDE. REMOVED AND REPLACED IAW DWG 9964461, REV W.

Part: RUB STRIP — CORRODED (WING) · airframe 38,705 hrs · 17,793 cycles

FUEL PANEL 620CT RUBSTRIP CORRODED. REMOVED AND REPLACED RUBSTRIP IAW SRM 57-00-04.

Part: RUB STRIP — CORRODED (WING) · airframe 38,705 hrs · 17,793 cycles

FUEL PANEL RUBSTRIP CORRODED. REMOVED AND REPLACED RUBSTRIP IAW SRM 57-00-04.

Part: RUB STRIP — CORRODED (WING) · airframe 38,705 hrs · 17,793 cycles

FUEL PANEL 520DT RUBSTRIP CORRODED. REMOVED AND REPLACED RUBSTRIP IAW SRM 57-00-04.

Part: FLOOR SUPPORT — CORRODED (BS 148-200) · airframe 33,991 hrs · 14,958 cycles

FLOOR SUPPORT IN FORWARD WET AREA, BS 148-200 HAS CORROSION, LBL 10. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW DWG 9936534.

Part: FRAME — DAMAGED (BS 1003) · airframe 33,991 hrs · 14,958 cycles

BS 1003 FRAME LBL 50 HAS TWO .2500" HOLES DRILLED WITHOUT APPROPRIATE SPACING. FABRICATED A STANDARD REPAIR IAW SRM 51-31-01 AND ERA 504723-14, REV O. (LP 1771814)

Part: STRAP — CORRODED (TAILCONE) · airframe 38,705 hrs · 17,793 cycles

CORROSION ON TAILCONE STRAPS. REMOVED AND REPLACED STRAP IAW AMM.

Part: INTERCOSTAL — CRACKED (BS 826-845) · airframe 33,991 hrs · 14,958 cycles

MAIN CABIN, INTERCOSTAL BETWEEN BS 826-845 AT BL 0 HAS TWO CRACKS ON TOP ISDE. R & R INTERCOSTAL IAW SRM 51-30-02, 51-30-05 AND DWG 9936580, REV BW.

Part: CUSP WEB — CORRODED (BS 712-731) · airframe 33,991 hrs · 14,958 cycles

RIGHT SIDE CUSP WEB BETWEEN BS 731-712 SHOWS EVIDENCE OF CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. INSTALLED A NEW CUSP WEB IAW DWG 9940443, REV D AND SRM 51-30-05, 51-30-02.

Part: LOCK — WORN (TAILCONE) · airframe 33,991 hrs · 14,958 cycles

FOUR TAILCONE LOCK FITTINGS ARE WORN. R & R THE TAIL CONE LOCK HOUSING IAW SRM 51-30-01 AND AMM.

Part: SEAT TRACK — CORRODED (BS 408) · airframe 33,991 hrs · 14,958 cycles

SEAT TRACK, RBL 44.5, BS 408 CORRODED. REMOVED SEAT TRACK, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED A NEW SEAT TRACK IAW SRM 53-40-01, FIG 6 AND DWG 5930547.

Part: SEAT TRACK — CORRODED (BS 854-971) · airframe 33,991 hrs · 14,958 cycles

SEAT TRACK, RBL 22, CORRODED. REMOVED SEAT TRACK SECTION FROM BS 854-971, RBL 22. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SPLICE AND SEAT TRACK SECTION IAW 53-40-01, 51-10-05 AND 51-30-01.

Part: CUSP WEB — CORRODED (BS 924-943) · airframe 33,991 hrs · 14,958 cycles

LEFT SIDE CUSP WEB BETWEEN BS 943-924 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED AND INSTALLED NEW CUSP WEB.

Part: CUSP WEB — CORRODED (BS 984-962) · airframe 33,991 hrs · 14,958 cycles

LT CUSP WEB, BETWEEN BS 984-962, CORRODED. FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED AND INSTALLED NEW CUSP WEB IAW SRM 51-30-01, 51-30-02, 51-30-05 AND DWG 9910151, REV CH.

Part: CUSP WEB — CRACKED (BS 883-864) · airframe 33,991 hrs · 14,958 cycles

CUSP WEB CRACKED BETWEEN BS 883-864. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED A DOUBLER REPAIR IAW SRM 53-20-02, FIG 6.

Part: SEAT TRACK — CORRODED (BS 420) · airframe 33,991 hrs · 14,958 cycles

MAIN CABIN, RBL 54, SEAT TRACK AT BS 420 CORRODED. CUTOUT DAMAGED SECTION OF SEAT TRACK, . LOCATED, DRILLED AND INSTALLED NEW SEAT TRACK , SPLICES AND STRAPS IAW SRM 53-40-01, FIG 6.

Part: PLATE — GOUGED (BEARING SUPPORT) · airframe 33,991 hrs · 14,958 cycles

RUDDER MAIN BEARING SUPPORT PLATE GOUGED. R & R IAW SRM 51-10-30 AND DWG 5913121, REV D.

Part: CUSP WEB — CORRODED (BS 541-560) · airframe 33,991 hrs · 14,958 cycles

LEFT CUSP WEB BETWEEN BS 541-560 HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED A DOUBLER IAW SRM 53-20-02 AND ERA 520318-14.

Part: CUSP WEB — CORRODED (BS 484-500) · airframe 33,991 hrs · 14,958 cycles

LEFT CUSP WEB BETWEEN BS 484-500 HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED A DOUBLER IAW SRM 53-20-02 AND ERA 520318-14MA.

Part: FRAME — CRACKED (BS 1542) · airframe 33,991 hrs · 14,958 cycles

AFT ACCESSORY COMPARTMENT ON CANTED FRAME BS 1542, RT SIDE LOWER END CRACKED. COMPLIED WITH ERA 531455.

Part: TOGGLE — MISINSTALLED (TAILCONE) · airframe 32,963 hrs · 14,291 cycles

TAIL CONE SLIDE TOGGLES INSTALLED INCORRECTLY. INSTALLED TAIL CONE TOGGELS PER AMDS 5352-4491.

Part: BULKHEAD WEB — CRACKED (BS 1531) · airframe 32,963 hrs · 14,291 cycles

CANTED BULKHEAD, BS 1531, AFT WEB CRACKED, RBL 20. COMPLIED WITH ERA 527163-14, REV O.

Part: LONGERON — DAMAGED (7 LEFT) · airframe 32,918 hrs · 14,268 cycles

FOUND DAMAGE ON LONGERON 7L, APPROXIMATELY AFT OF APB. BLENDED DAMAGE. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-10-01.

Part: FRAME — WORN (FUSELAGE) · airframe 32,918 hrs · 14,268 cycles

FUSELAGE FRAME IS WORN AT LT SIDE 10:00 POSITION APPROXIMATELY 48 INCHES AFT OF AFT PRESSURE BULKHEAD. REPAIRED IAW SRM 53-10-02, FIG 2.

Part: DOOR FRAME — CRACKED (LT MLG) · airframe 32,918 hrs · 14,268 cycles

LEFT WHEEL WELL, AFT DOOR FRAME CRACKED AT OTBD END. REPAIR COMPLETED IAW SRM 53-60-02, FIG 8 AND ERA 520684-14MA, REV O.

Part: LANYARD — FRAYED (TAILCONE) · airframe 32,918 hrs · 14,268 cycles

TAIL CONE JETTISON BOTTLE LANYARD FRAYED. REPLACED PULL CABLES IAW AMDS 5350-4491.

Part: SKIN — CRACKED (BS 1542) · airframe 33,712 hrs · 14,765 cycles

FUSELAGE SKIN CRACKED AT BS 1542 JUST ABOVE STAIRWAY C/O RT SIDE. REMOVED DAMAGE AND HFEC IAW NDT SPM 06-10-01.001 DAMAGE CONTAINED. INSTALLED LOCK FASTENER IAW SRM 53-31-02, VOL I AND SRM 51-30-08, VOL II.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,918 hrs · 14,268 cycles

FUSELAGE SKIN CRACKED AT NOSE WHEEL WELL LEFT AFT DOOR AFT HINGE. R & R IAW ERA 527126-14, REV O.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,187 hrs · 13,794 cycles

DURING SERVICE CHECK, FOUND AFT STAIRWELL EMERGENCY LIGHTS INOPERATIVE. R & R AFT EMERGENCY POWER SUPPLY IAW AMM. OPS CHECKED GOOD.

Part: STRUCTURE — OUT OF POSITION (TAILCONE) · airframe 31,143 hrs · 13,127 cycles

DURING TAXI OUT, F/A HEARD A LOUD THUD IN TAILCONE. RETURNED TO GATE. FOUND AFT VENTRAL STAIRS CATWALK OUT OF RIG. FOUND CATWALK CATCHING ON LOOSE TRIM. SECURED TRIM. OPS CHECKED GOOD.

Part: SPRING — FAILED (TAILCONE LATCH) · airframe 31,117 hrs · 13,107 cycles

TAILCONE LATCH, RT UPPER, DOESN'T SPRING CLOSED. R & R SPRING IAW CMM. OPS CHECKED ON AMDS 1200-6647.

Part: SPRING — FAILED (TAILCONE LATCH) · airframe 31,117 hrs · 13,107 cycles

TAILCONE LATCH, LT UPPER, DOESN'T SPRING CLOSED. R & R SPRING IAW CMM. OPS CHECKED ON AMDS 1200-6647.

Part: SPRING — FAILED (TAILCONE LATCH) · airframe 31,117 hrs · 13,107 cycles

TAILCONE LATCH, LT LOWER, IS SPRING LOADED TO OPEN. R & R SPRING IAW CMM. OPERATIONS CHECKED ON AMDS 1200-6647.

Part: SPRING — FAILED (TAILCONE LATCH) · airframe 31,117 hrs · 13,107 cycles

TAILCONE LATCH, RT LOWER, IS SPRING LOADED TO OPEN. R & R SPRING IAW CMM. OPS CHECKED ON AMDS 1200-6647.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,805 hrs · 12,933 cycles

EMERGENCY LIGHTS INOPERATIVE FROM SEAT ROW 24 TO 27. R & R BATTERY PACK IAW AMM. OPS CHECKED GOOD.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 30,654 hrs · 12,840 cycles

RT HORIZONTAL STABILIZER UPPER AFT SKIN INBD CORNER CRACKED. COMPLETED SECTION I OF ERA 517327-14AD.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 30,647 hrs · 12,834 cycles

WHILE PERFORMING INSPECTION OF HORIZONTAL STABILIZER RT UPPER SKIN, FOUND CRACK INDICATION ON SCAN3 - LOW FREQ - APPROX 1 INCH LONG.

Part: HINGE FITTING — UNKNOWN (FLAP) · airframe 28,077 hrs · 11,408 cycles

REPLACED THE OTBD FLAP IDLER HINGE FITTING IAW EA 02-087116-03, ME01-7-02.

Part: SLIDE — WRONG PART (TAILCONE) · airframe 27,637 hrs · 11,155 cycles

TAILCONE SLIDE FOUND TO BE INCORRECT, REMOVED AND REPLACED TAILCONE SLIDE PER OPN 7008.

Part: CABLE — BROKEN (TAILCONE) · airframe 27,119 hrs · 10,844 cycles

DURING SCHEDULED SLIDE DEPLOYMENT, CABLE BROKE ON TAIL CONE NITROGEN ASSIST BOTTLE. INSTALLED NEW NITROGEN ASSIST BOTTLE PER MM AND ALUMINUM WASHERS PER REPAIR ORDER 842417.

Part: UNKNOWN — SMOKE (CABIN) · airframe 19,950 hrs · 8,097 cycles

DURING FLIGHT, PASSENGER INFORMED CREW OF SMOKE BEING EMITTED AT 24C OVERHEAD. MX INSPECTED ROW 24 AREA AND FOUND NO BURNING OR OVERHEAT INDICATIONS. LIGHT CHECKS GOOD AND OK FOR SERVICE.

Part: ATTACH FITTING — UNKNOWN (GALLEY) · airframe 22,474 hrs · 8,767 cycles

FWD GALLEY AND LAV UPPER ATTACH STRUCURE REPAIRED IAW EA 02-477514-03, ME 01 & 05.

Part: BRAKE SYS — UNKNOWN (MLG) · airframe 22,474 hrs · 8,767 cycles

BRAKE SYSTEM REPAIRED IAW EA 02-476765-03, ME01.

Part: STRUCTURE — UNKNOWN (GALLEY) · airframe 22,474 hrs · 8,767 cycles

FWD GALLEY FLOOR STRUCTURE REPAIRED IAW EA 02-477513-03, ME 01 & 04.