N955DN

Part: UNKNOWN — FUMES (CABIN) · airframe 51,181 hrs · 28,973 cycles

DIVERTED TO TUL DUE TO SEVERAL PASSENGERS REPORTED LIGHT HEADINESS, DIZZINESS AND NAUSEA AT FL300. MAINTENANCE PERFORMED BORESCOPE INSPECTION OF STAGE 3 AND 4 HPC OF NR 1 AND 2 ENGINES. NO EVIDENCE OF OIL LEAKAGE FOUND. REMOVED AND REPLACED COALESCE BAGS. RAN BOTH ENGINES WITH FIRE DEPARTMENT ON BOARD. NO CO2 DETECTED. PERFORMED DUCT BURNOUT. AIRCRAFT OKAY FOR SERVICE. (LP# 8512746)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 51,013 hrs · 28,860 cycles

CREW REPORTED APU WOULD NOT START. MAINTENANCE FOUND EVIDENCE OF AN APU STARTER FIRE. NO FIRE EXTINGUISHER DISCHARGED. REPLACED APU, START RELAYS, ECU, SHIPS BATTERIES AND CHARGER. INSPECTING ALL START CIRCUIT CABLES AND CONNECTIONS FOR HIGH RESISTANCE, HEAT DAMAGE. ACFT OK FOR SERVICE.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 50,877 hrs · 28,776 cycles

CRACKED ANGLE FOUND ON INSIDE RT OF DORSAL FIN ATTACHMENT TO FUSELAGE. FABRICATED NEW ANGLE IAW DWG 5912188.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,432 hrs · 28,502 cycles

EMERGENCY EXIT IDENTIFIED IN FORWARD GALLEY ABOVE F/A SEAT FLASHES ON AND OFF. R & R BATTERY PACK. OPS CHECKS GOOD.

Part: BATTERY PACK — DISCONNECTED (EMERGENCY LIGHTS) · airframe 49,549 hrs · 27,973 cycles

LOWER EMERGENCY EXIT SIGNS INOPERATIVE AT LT AND RT AFT OVERWING EXITS AND AFT EXIT DOORS. FOUND BATTERY PACK DISCONNECTED AT ROW 37CDE. RECONNECTED BATTERY PACK. OPS CHECKS GOOD.

Part: FASTENER — LOOSE (VERTICAL STAB) · airframe 48,924 hrs · 27,581 cycles

VERTICAL STABILIZER L/E AT THE SPLICE, ZFS=52-237 HAS LOOSE FASTENERS. REPAIRED IAW PRI/ERA 538746-14AD AND DWGSG09550004, REV D.

Part: STRAP — CORRODED (BS 1231-1250) · airframe 48,924 hrs · 27,581 cycles

AFT CARGO CENTER BELLY STRAP CORRODED FROM LONGERONS 29L - 29R, BS 1231-1250. REPAIRED IAW ERA 538850-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,924 hrs · 27,581 cycles

FUSELAGE SKIN ABOVE MID CARGO DOOR, DAMAGE. REPAIRED IAW SRM 51-00-01.

Part: CUSP WEB — CHAFED (BS 902) · airframe 48,924 hrs · 27,581 cycles

OVERWING BS 902, CUSP WEB IS CHAFING ON FRAME. COMPLIED WITH ERA 531210-14MA, REV O.

Part: CABLE — MISROUTED (TAILCONE) · airframe 47,618 hrs · 26,799 cycles

DURING TAIL CONE SLIDE CHANGE NOTED TAILCONE NITROGEN PULL CABLE ROUTED INCORRECTLY. ROUTED CABLE CORRECTLY IAW AMM. OK FOR SERVICE.

Part: SILL — CORRODED (AFT CARGO BAY) · airframe 45,188 hrs · 25,239 cycles

AFT CARGO DOOR SILL HAS LIGHT CORROSION ALONG EDGE OF INNER ANGLE. REPAIRED IAW ERA 524124-14, REV O.

Part: BEAM — DAMAGED (BS 1212-1269) · airframe 45,454 hrs · 25,404 cycles

AFT CARGO C-3, LOWER BEAM, BS 1212-1269 DAMAGED. REPAIR WAS ACCOMPLISHED IAW NR 23 AND 127 DURING C-CHECK.

Part: SILL — DAMAGED (AFT CARGO BAY) · airframe 45,188 hrs · 25,239 cycles

FOUND FASTENER HOLE OUT OF TOLERANCE IN AFT CARGO DOOR SILL. ACCOMPLISHED REPAIR IAW ERA 524124-14, REV O.

Part: WEB — CRACKED (BS 1520) · airframe 45,176 hrs · 25,234 cycles

BS 1520 WEB CRACKED LBL 36, REPAIRED IAW ERA 524098-14.

Part: PIN — UNSECURE (ESCAPE SLIDE) · airframe 45,094 hrs · 25,194 cycles

DURING SERVICE CHECK, R1 DOOR SLIDE HAS LOWER PARACHUTE PIN NOT ENGAGED. R & R R1 SLIDE PACK IAW AMM.

Part: PAN — CRACKED (CARGO DOOR) · airframe 44,922 hrs · 25,086 cycles

MID CARGO DOOR PAN CRACKED. PERMANENT REPAIR COMPLIED WITH ERA 499926-14MA.

Part: GROUND WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 44,907 hrs · 25,078 cycles

DURING SERVICE CHECK, EMERGENCY LIGHT AT SEAT 21AB INOPERATIVE ON STANDBY POWER. TROUBLESHOT AND FOUND GROUND 5244 DISCONNECTED. TERMINATED IAW SWPM. OPS CHECKED NORMAL.

Part: LONGERON — CORRODED (BS 1258-1298) · airframe 40,655 hrs · 22,617 cycles

AFT CARGO COMPARTMENT L30, LOWER SIDE OF FLANGE, CORRODED AT FASTENER HOLES AND FASTENER AT SPLICE BS 1258-1298. REMOVED AND REPLACED NEW SECTION OF FRAME, BS 1205 THRU 1258, PER ERA 502680-14 REV O.

Part: SUPPORT FITTING — DAMAGED (LT MLG) · airframe 40,655 hrs · 22,617 cycles

LT MLG RETRACT ACTUATOR SUPPORT FITTING DAMAGED. REPLACED SUPPORT FITTING, BUSHINGS, AND BEARING PER EA 02-093855-03AD.

Part: SUPPORT FITTING — DAMAGED (RT MLG) · airframe 40,655 hrs · 22,617 cycles

RT MLG RETRACT ACTUATOR SUPPORT FITTING DAMAGED. REPLACED RT MLG RETRACT ACTUATOR SUPPORT FITTING, BUSHING, AND BEARING PER EA 02-093855-03AD REV A.

Part: CARGO TRACK — CORRODED (BS 500-693) · airframe 40,655 hrs · 22,617 cycles

CENTER CARGO BAY LEFT AND RIGHT CARGO TRACKS HAVE PAINT PEELING AND SURFACE CORROSION AROUND ATTACH HOLES. REMOVED AND REPLACED FROM BS 500-693 RT SIDE PER SRM 53-40-01 FIG 7 VOL II.

Part: FASTENER — WORN (LT PYLON) · airframe 40,655 hrs · 22,617 cycles

FASTENERS ON LT PYLON WORN, REMOVED AND REPLACED FASTENERS PER EA 02-476701-12AD REV E OPN 0101.

Part: SKIN — CORRODED (E & E DOOR) · airframe 40,655 hrs · 22,617 cycles

E & E DOOR HAS INNER SKIN WITH SURFACE CORROSION AROUND RIBNUTS. INSTALLED DOUBLER REPAIR AT E/E DOOR INNER SKIN PER MD90 SRM 52-01-01 FIG 6 VOL I.

Part: CARGO TRACK — CORRODED (BS 218-587) · airframe 40,655 hrs · 22,617 cycles

FWD CARGO TRACK LEFT AND RIGHT HAVE LIGHT CORROSION AROUND NUMEROUS ATTACHING SCREW HEADS. REMOVED AND REPLACED FWD CARGO COMPARTMENT TRACK FROM BS 218-522 LEFT SIDE AND BS 218-587 RIGHT SIDE PER SRM 53-40-01 VOL I AND SRM 51-30-00 VOL II.

Part: SKIN — CORRODED (BS 1145-1174) · airframe 40,655 hrs · 22,617 cycles

FUSELAGE SKIN CORRODED BS 1145-1174. REPAIRED IAW ERA 502654-14.

Part: SEAT TRACK — CORRODED (BS 1156 LBL 44) · airframe 40,655 hrs · 22,617 cycles

CORROSION FOUND ON OUTBOARD LBL 44 SEAT TRACK AT BS 1156 ON SPLICE. REMOVED AND REPLACED SEAT TRACK SECTION PER SRM 53-40-01 VOL I, 51-30-01 VOL II, 51-30-02 VOL II, AND 51-30-05 VOL II.

Part: FRAME — DAMAGED (BS 1520 L1R) · airframe 40,655 hrs · 22,617 cycles

HOLE DAMAGED AT AFT ACS COMPARTMENT BS 1520 FWD FACE 6 INCHES ABOVE LONGERON 1R. REPAIRED DAMAGE AT AFT ACCESSORY COMPARTMENT AT BS 1520 PER ERA 502687-14 REV O.

Part: LONGERON — CORRODED (BS 1258 L29L) · airframe 40,655 hrs · 22,617 cycles

CORROSION AT AFT CARGO COMPARTMENT L29L AT BS 1258 AROUND FASTENERS ON LOWER SIDE OF FLANGE. REMOVED DAMAGE AND REPAIRED PER SRM 53-10-01 VOL I.

Part: WEB — DAMAGED (BS 160 RBL 8) · airframe 40,655 hrs · 22,617 cycles

MAIN CABIN BS 160 RBL 8 FLOOR WEB IS DAMAGED AT FASTENER HOLE. INSTALLED WEB REPAIR PER MD90 SRM 51-11-01 FIG 1 VOL I.

Part: ATTACH ANGLE — CRACKED (MLG WW) · airframe 40,655 hrs · 22,617 cycles

WHEEL WELL RIGHT ATTACH ANGLE CRACKED INSIDE HYDRAULIC SERVICE COMP O/B AREA. REMOVED AND REPLACED PER SRM 51-30-02 VOL II AND 51-30-05 VOL II.

Part: SEAT TRACK — DAMAGED (BS 1288-1307) · airframe 40,655 hrs · 22,617 cycles

SEAT TRACK HAS SCRATCHES AT LBL 22 STA 1288 TO 1307. INSTALLED SEAT TRACK REPAIR PER SRM 53-40-01 VOL 1 FIG 6.

Part: FLOOR SKIN — CRACKED (BS 160 RBL 22) · airframe 40,655 hrs · 22,617 cycles

COCKPIT FLOOR WEB CRACKED UNDER F/O SEAT AT BS 160 RBL 22. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 VOL I.

Part: WEB — CRACKED (BS 200) · airframe 40,655 hrs · 22,617 cycles

FWD CABIN FLOOR WEB HAS SMALL CRACK BY R1 DOOR BS 200 RBL 52. INSTALLED REPAIR DOUBLER PER SRM 53-20-02 VOL I.

Part: SEAT TRACK — CORRODED (BS 237-256) · airframe 40,655 hrs · 22,617 cycles

FWD CABIN SEAT TRACK CORRODED AT RBL 22 STA 237 AND STA 256. REPLACED SEAT TRACK PER MD 90 SRM 53-40-01 VOL I FIG 6.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 40,655 hrs · 22,617 cycles

CRACK ON STR 20L, JUST BEHIND AND ABOVE LEFT W/W EXTERNAL FUSELAGE. INSTALLED REPAIR DOUBLER PER DRAWING SG09530021 BY STA 1060 AND REF MD 90 SRM 53-10-01.

Part: WEB — DAMAGED (L1 DOOR) · airframe 40,655 hrs · 22,617 cycles

L1 DOOR ENTRY WEB HAS A 4 BY 3 INCH HOLE AT APPROX BS 170 LBL 48. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 51-11-01 VOL I.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,655 hrs · 22,617 cycles

FWD CARGO RT SIDE AT STR 22RT AND 23RT 3 BAD RIVETS AT STA 332. INSTALLED PERMANENT FLUSH REPAIR PER MD 90 SRM 53-30-01 FIG 5 VOL I.

Part: DOUBLER — CORRODED (PRESS BULKHEAD) · airframe 40,655 hrs · 22,617 cycles

AFT PRESSURE BULKHEAD DOME T-CHORD DOUBLER LOWER SECTION HAS CORROSION. REMOVED AND FABRICATED NEW DOUBLER PER DWG PL5910130 AND INSTALLED.

Part: INTERCOSTAL — CRACKED (BS 1246-1288 L30) · airframe 40,655 hrs · 22,617 cycles

AFT CARGO COMPARTMENT BILGE AREA INTERCOSTAL BETWEEN BS 1246 - 1288 L30 FOUND CORRODED AND CRACKED. FABRICATED NEW AND INSTALLED PER DWG 5936071 AND SRM 51-30-05.

Part: DOOR FRAME — CORRODED (BS 1211-1269) · airframe 40,655 hrs · 22,617 cycles

CORROSION FOUND ON AFT CARGO DOOR JAMB BETWEEN 1211-1268. REPAIRED IAW SRM 53-60-02, 51-10-03, 51-10-04, AND 51-30-02.

Part: FRAME — CRACKED (BS 1520.225 L1R) · airframe 40,655 hrs · 22,617 cycles

AFT ACCESSORY COMPARTMENT CANTED FRAME 1520.225 FWD FACE AT STRINGER 1R FUSELAGE STRAP ATTACHED TO THE CANTED FRAME HAS A CRACK. REPAIRED DAMAGED AT CANTED FRAME STA 1520.225 FWD FACE L2R PER ERA 502687-14 REV O.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 40,655 hrs · 22,617 cycles

CUSP WEB CRACKED AT STA 1288 LBL 45 UNDER SEAT TRACK FLANGE. INSTALLED REPAIR DOUBLER PER MD 90 SRM 53-20-02 FIG 14.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 40,655 hrs · 22,617 cycles

CUSP WEB CRACKED AND WRONG RIVETS INSTALLED IN LEFT CUSP "T" AREA AT STA 880. INSTALLED REPAIR DOUBLER PER MD 90 SRM 53-20-02 FIG 7.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,655 hrs · 22,617 cycles

SEAT TRACK CORRODED OUT OF LIMITS AT STA 237 RBL 44. REPAIRED PER MD 90 SRM 53-40-01 VOL I.

Part: FLOOR SUPPORT — CORRODED (BS 1212-1269) · airframe 40,655 hrs · 22,617 cycles

AFT COMPARTMENT BILGE AREA FLOOR SUPPORT BETWEEN STA 1212-1269 UPPER SURFACE HAS CORROSION. FABRICATED AND REPLACED FLOOR SUPPORT PER DWG 5936660 AND SRM 53-20-01VOL III, 51-10-03 VOL II, AND 51-10-04 VOL II.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 40,655 hrs · 22,617 cycles

CUSP WEB CRACKED ON LEFT CUSP AREA AT STA 902 UNDER RIB CUTOUT DOUBLER. INSTALLED REPAIR DOUBLER PER MD 90 SRM 53-20-02 FIG 7.

Part: CUSP WEB — CORRODED (BS 691-757) · airframe 40,655 hrs · 22,617 cycles

CUSP WEB ON RT BS 691 TO 757 CORRODED OUT OF LIMITS. INSTALLED CUSP WEB REPAIR PER SRM 53-20-02 FIG 4.

Part: FRAME — CORRODED (BS 1344 L28-29R) · airframe 40,655 hrs · 22,617 cycles

CORROSION UNDER FRAME 1344 BETWEEN L28R AND L29R. CUTOUT DAMAGE AND REPAIRED PER SRM 53-10-02 VOL I.

Part: INTERCOSTAL — CORRODED (BS 1328 L30) · airframe 40,655 hrs · 22,617 cycles

CORROSION ON INTERCOSTAL AND TIE CLIPS AT L30 AND FRAME 1328. FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 51-30-02, 51-30-05, 51-30-03, 51-30-04 VOL II, 51-10-04, AND 51-10-02.

Part: SPAR — CRACKED (WING) · airframe 40,629 hrs · 22,611 cycles

WING REAR SPAR CRACKED. REPAIRED IAW AA 5710-01119.

Part: DOOR FRAME — CORRODED (AFT CARGO DOOWAY) · airframe 40,625 hrs · 22,609 cycles

AFT CARGO DOOR FRAME L28R CORRODED. REPAIRED IAW ERA 398119-14.