N920DN

Part: EXTENSION — MISSING (SPOILER) · airframe 49,309 hrs · 32,694 cycles

SPOILER TRAILING EDGE EXTENSION MISSING LEFT WING. REPLACED LT SPOILER T/E EXTENSION PER SRM 51-30 SEC CHECK GOOD. (LP# 3739778)

Part: TEE FITTING — MISSING (RT SPOILER) · airframe 49,309 hrs · 32,694 cycles

RT WING SPOILER TRAILING EDGE TEE MISSING. REPLACED RT MIDDLE SPOILER T/E EXTENSION PER SRM 51-30 SEC CHECK GOOD THIS CLEARS CDL. (LP# 4383670)

Part: TIRE — FAILED (LT MLG OTBD) · airframe 49,356 hrs · 32,726 cycles

SHIP 9220 *****TIRE**** MSP- BDL. ON LANDING INTO BDL LT OB MAIN LANDING TIRE BLEW ON LANDING. CORRECTIVE ACTION: REPLACED LO AND LI MLG TIRE ASSEMBLIES. PERFORMED AACU BITE. RESULTS OF BITE SHOWS FAULT DATA - ANTISKID SOV RELAY / ANTI SKID SOV RHYD AND LHYD. THE S10-130 PARKING BRAKE SWITCH, POWER SOURCE AND THE AS SOV RELAY WERE REPLACED. REPLACED LT MLG DOOR AS FOUND MISSING. REPLACED LT OB SPRAY DEFLECTOR AS FOUND DAMAGED. REPAIRED DAMAGED LT BODY FAIRING PANELS AS PER ENGINEERING INSTRUCTIONS AND TOPP 40-60-05. REPAIRED DAMAGED FORMER PER MD90 SRM 51-70-01. (LP# 4383672, 0841198, 0839831, 4383673, 0838855)

Part: DOOR — MISSING (LT MLG) · airframe 49,295 hrs · 32,684 cycles

RH MLG OUTBOARD DOOR REMOVED FOR FERRY FLIGHT AND LT MLG DOOR MISSING DUE TO TIRE BLOWM. REINSTALLED R/H MLG OUTBD DOOR PER MD90 AMM TASK 32-10-01-402-801. INSTALLED SERVICEABLE LT MLG DOOR ASSY PER MD90 AMM 32-10 AND ADJUSTED BOTH L/H & R/H MLG DOORS. ALL CHECKS GOOD. (LP# 0839831)

Part: FORMER — DAMAGED (NOT REPORTED) · airframe 49,295 hrs · 32,684 cycles

REMOVED DAMAGE FORMER FOR REPAIR P/N 9951285-403. REPAIRED FORMER PER MD90 SRM 51-70-01 FIG 1 REINSTALLED FORMER. (LP#0838855)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 48,893 hrs · 32,426 cycles

CUSP WEB CRACKED STA 903 RT.

Part: DOOR FRAME — CRACKED (RT MLG WW) · airframe 48,893 hrs · 32,426 cycles

RT MLG DOOR CUTOUT FORWARD FRAME CRACKED. REPAIRED FRAME PER SRM 53-60-02 PARA 8 FIG 6.

Part: STRUCTURE — CRACKED (VERTICAL STAB) · airframe 48,450 hrs · 32,160 cycles

WHILE PERFORMING VISUAL INSPECTION PER SRM 55-30-04 P 4, FOUND CRACK TO GO EXCEEDED PAST STOP DRILLS AND TO BE PAST MAX TOLERANCE. PERFORMED FPI INSPECTION OF SUBJECT AREA TO MARK ENDS OF CRACKS PER SRM 55-30-05. COMPLETED PERM REPAIR PER SRM 55-30-05 PAR 5.

Part: CABLE — UNSECURE (CATWALK) · airframe 46,118 hrs · 30,773 cycles

LEFT CATWALK CABLE BROKEN. SECURED CABLE. NO DAMAGE FOUND.

Part: CABLE — BROKEN (CATWALK) · airframe 46,118 hrs · 30,773 cycles

CATWALK CABLE LEFT SIDE BROKEN. REMOVED AND REPLACED CEILING CABLE OPERATION CHECKS GOOD.

Part: LENS — MISSING (CABIN) · airframe 45,989 hrs · 30,703 cycles

CEILING EMERGENCY LIGHT LENS ASSEMBLY MISSING. REPLACED IAW MM. OPERATION CHECKS GOOD.

Part: BOTTLE — LEAKING (EVAC SLIDE) · airframe 45,953 hrs · 30,681 cycles

TAIL SLIDE INFLATION BOTTLE LEAKING FROM BALL VALVE ASSEMBLY. REPLACED IAW MM 53-52-03.

Part: GIRT BAR — DETACHED (CABIN) · airframe 45,838 hrs · 30,617 cycles

GIRT BAR NOT ATTACHED TO AIRCRAFT. REINSTALLED GIRT BAR TO DOOR. OPERATION CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,755 hrs · 30,568 cycles

CATWALK EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPERATION CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 45,204 hrs · 30,282 cycles

AFT OVERHEAD EXIT SIGN AND EXIT SIGN IN TAIL CONE IS FLASHING. REMOVED AND REPLACED BATTERY PACK CHARGER B5-239. OPERATION CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,535 hrs · 29,917 cycles

EMERGENCY EXIT LIGHT OVER ATTENDANT REMAINS ILLUMINATED AFTER THE LIGHT SWITCH IS IN THE ARMED POSITION, WITH FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH IN OFF. REPLACED THE BATTERY PACK. OPS CHECKED OKAY.

Part: FAN — SEIZED (LAVATORY) · airframe 43,921 hrs · 29,555 cycles

FLIGHT ATTENDANT REPORTED A WARM ELECTRICAL ODOR IN GALLEY. SHUT ALL POWER TO GALLEY. ODOR DISSIPATED. MAINTENANCE FOUND M1-83 IN FIRST CLASS LAVATORY FAN SEIZED. REPLACED THE FAN. OPERATION CHECKED GOOD.

Part: CATWALK — OUT OF ADJUST · airframe 43,749 hrs · 29,440 cycles

CATWALK HARD TO EXTEND. ADJUSTED IAW MM.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON LOWER DOOR JAMB WEB BETWEEN STA 1203-1276 AND LONGERON 29L-27R, TASK 53-302-07. REPLACED WEB IAW SRM 51-30-05 AND 51-30-02.

Part: HINGE FITTING — WORN (LT SPOILER) · airframe 43,747 hrs · 29,439 cycles

WEAR ON LT WING INBD FLIGHT SPOILER HINGE FITTING. REPLACED FITTING IAW CMM 57-40-04.

Part: FRAME — CRACKED (BS 1542) · airframe 43,747 hrs · 29,439 cycles

CRACK ON FRAME, BS 1542 CANT BETWEEN DOOR FRAME AND LONGERON 24R IN AFT ACCESSORY COMPARTMENT. TWO CRACKS FOUND DURING HFEC. REPAIRED IAW SRM 53-10-02.

Part: CARGO TRACK — CORRODED (BS 1269-1307) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON CARGO TRACKS BETWEEN BS 1269-1307. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED A NEW CARGO TRACK IAW SRM 51-10-03 AND 51-30-01.

Part: SKIN — CORRODED (BS 1369) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON INTERNAL FUSELAGE SKIN, BS 1369 BETWEEN LONGERS 29 -30L IN AFT CARGO COMPARTMENT. REPAIRED IAW SRM 53-31-02.

Part: TRACK — CORRODED (FUSELAGE) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON TIE TRACK, STA 1060-1212 BETWEEN LONGERON 28R AND 27R. OUT OF LIMITS. REPLACED TRACK IAW SRM 51-30-01 AND 51-30-02.

Part: WEB — CORRODED · airframe 43,747 hrs · 29,439 cycles

CORROSION ON LEFT AND RIGHT LATERAL WEBS, VENTRAL STAIRWAY MOVABLE STRUCTURE. REPAIRED ETA 90-16-038, REV 2 AND ERA 549268-14, REV O.

Part: HINGE — DAMAGED (CARGO DOOR) · airframe 43,747 hrs · 29,439 cycles

ELONGATED HOLE IN FORWARD AND AFT HINGES OF AFT CARGO DOOR. OUT OF LIMITS. HINGES WERE REPLACED IAW MM AND ERA 521061-10.

Part: CARGO TRACK — CORRODED (BS 1060-1307) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON LEFT CARGO TRACK BETWEEN BS 1060-1307. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 51-10-05 AND 51-30-01.

Part: FRAME — CORRODED (BS 1307) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON FRAME, BS 1307 BETWEEN LONGERONS 27L - 27R, IN THE AFT CARGO COMPARTMENT. REMOVED AND REPLACED THE FRAME IAW SRM 53-10-02.

Part: REPAIR — CORRODED (FUSELAGE) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON PREVIOUS REPAIR OF FRAME IN STA Y=1344 BETWEEN LONG 29LT-28RT AT AFT CARGO COMPARTMENT. PREVIOUS REPAIR WAS REPLACED IAW SRM 53-10-02, FIG 2.

Part: DOUBLER — DAMAGED (LT ELEVATOR) · airframe 43,747 hrs · 29,439 cycles

LIGHTING STRIKE ON LT ELEVATOR T/E OUTER STATIC DISCHARGE AND BASE OF STATIC DISCHARGE, PREVIOUS DOUBLER REPAIR. DOUBLER WAS REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · airframe 44,042 hrs · 29,633 cycles

CORROSION ON SEATING AREA AND COUNTERSINK OF FUEL PANEL ACCESS PLATE 620DT. REPLACED PANEL.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 43,747 hrs · 29,439 cycles

CRACKED LOWER DORSAL ATTACH FITTING AT STA Y=1494 AND LONGERON PROJECTION 3 LT IN AFT ACCESSORY COMPARTMENT. FITTING WAS REPLACED IAW DWG 9953016, REV AU AND SRM 51-30-05.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 44,042 hrs · 29,633 cycles

CORROSION ON FILLET FAIRING SUPPORT, STA 807. FABRICATED AND INSTALLED REPAIR PARTS IAW ERA 549283-14, REV O.

Part: ACCESS PANEL — CORRODED (WING) · airframe 44,042 hrs · 29,633 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL PANEL 620AT. REPLACED PANEL.

Part: SUPPORT — BROKEN (FUSELAGE) · airframe 44,042 hrs · 29,633 cycles

BROKEN SLANT SUPPORT, STA 1118 LEFT HAND SIDE CARGO COMPARTMENT. REPLACED IAW ERA 412247-14MA, REV D.

Part: SUPPORT — BROKEN (FUSELAGE) · airframe 44,042 hrs · 29,633 cycles

BROKEN SPLICE SUPPORT STA 136 BETWEEN LONGERON 27L AND 24L, C3. REPLACED SLANT IAW ERA 412247-14MA, REV D.

Part: ACCESS PANEL — CORRODED (WING) · airframe 44,042 hrs · 29,633 cycles

CORROSION ON SEATING AREA AND COUNTERSINK OF FUEL PANEL 520 FT. FOUND OUT OF LIMITS. REPLACED PANEL.

Part: BEAM — CORRODED (FUSELAGE) · airframe 44,042 hrs · 29,633 cycles

CORROSION ON BEAM BETWEEN STA 1197-1238 LONGERON 29R AFT COMPARTMENT. CORROSION ATTENDED IAW ERA 549247-14, REV O AND ETI-90-16-031, REV 1.

Part: DOUBLER — CORRODED (BS 205-218) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON INNER FUSELAGE SKIN DOUBLER, LONGERONS 28 - 29R, BS 205 - 218. DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-02.

Part: FLOOR SUPPORT — CRACKED (BS 1328-1344) · airframe 43,747 hrs · 29,439 cycles

CRACKED FLOOR SUPPORT BS 1328 - 1344 , X 3. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-02.

Part: ANGLE — CRACKED (BS 1520) · airframe 43,747 hrs · 29,439 cycles

CRACKED AND LOOSE FASTENERS ON LT DOOR SILL ANGLE BS 1520. REPAIRED PER ER/A 549245-14.

Part: SKIN — CRACKED (FLOOR PANEL) · airframe 43,747 hrs · 29,439 cycles

CRACK ON SKIN AND CHANNEL OF FLOOR PANEL 222FG. REPAIRED IAW SRM 53-20-03.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 43,747 hrs · 29,439 cycles

CRACK AND BEND ON CHANNEL AT VARIOUS FLOOR PANELS. REPAIRED IAW SRM 53-20-03.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON FUEL ACCESS PANEL 620CT. REPLACED THE ACCESS PANEL. (LP# 2647779)

Part: PAN — CRACKED (OVERWING DOOR) · airframe 43,747 hrs · 29,439 cycles

CRACK FOUND ON PAN LOWER FWD EDGE OF OVERWING EXIT DOOR. PAN WAS REPAIRED PER ER/A 549256-14.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON SEATING AREA AND COUNTERSINK OF FUEL ACCESS PLATE 520DT. REPLACED THE ACCESS PANEL.

Part: FRAME — CORRODED (BS 1307) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON PREVIOUS REPAIR OF FRAME, BS 1307 BETWEEN LONGERON 29 - 30R AFT CARGO COMPARTMENT. REPLACED THE REPAIR IAW SRM 53-10-02.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON SEATING AREA AND COUNTERSINK OF FUEL ACCESS PANEL, 620FT. REPLACED THE ACCESS PANEL.

Part: CUSP WEB — CORRODED (BS 389-490) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON RIGHT CUSP WEB, BS 389, - 490. REPAIRED IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 764) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON RIGHT CUSP WEB, BS 764. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-20-02.

Part: DOUBLER — CORRODED (FUSELAGE SKIN) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON FUSELAGE SKIN DOUBLER BETWEEN LONGERONS 29 AND 30L. FOUND TO BE OUT OF LIMITS. REPLACED THE DOUBLER IAW SRM 51-30-02.

Part: SKIN — CRACKED (BS 1494) · airframe 43,747 hrs · 29,439 cycles

CRACK ON EXTERNAL FUSELAGE SKIN, BS 1494 BETWEEN LONGERON 3L AND 4L. REPAIRED IAW ERA 549236-14, REV O. (LP# 2643887)

Part: LONGERON SPLICE — CORRODED (BS 160-175) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON LONGERON SPLICE 30 BETWEEN, BS 160-175. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 51-30-02 AND DWG 5911401, REV C.

Part: SKIN — CORRODED (BS 541) · airframe 43,747 hrs · 29,439 cycles

CORROSION ON INNER FUSELAGE SKIN AT BS 541 LONGERON 30, MID CARGO COMPARTMENT. REPAIRED IAW SRM 53-31-02.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 44,042 hrs · 29,633 cycles

CORROSION OUT OF LIMITS AT STA 389 X-58, STA 389, X=-49 AND STA 764. COMPLIED WITH SRM 53-20-01 AND ERA 511165-14MA REV C.

Part: ACCESS PANEL — CORRODED · airframe 43,747 hrs · 29,439 cycles

CORROSION ON SEATING AREA OF FUEL PANEL 520CT. REPLACED IAW SRM 57-00-04.

Part: DOOR FRAME — CRACKED (BS 208) · airframe 43,747 hrs · 29,439 cycles

L1 DOOR FRAME WEB, BS 208, LONGERON 15L CRACKED. REPAIRED IAW SRM 53-60-02.

Part: CUSP WEB — CRACKED (BS 878) · airframe 43,747 hrs · 29,439 cycles

LEFT CUSP WEB, BS 878, X 56 CRACKED. REPAIRED IAW SRM 53-20-02, FIG 6.

Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 43,747 hrs · 29,439 cycles

LOWER AREA OF MID CARGO COMPARTMENT DOOR FRAME CORRODED. REMOVED AND REPLACED IAW SRM 53-60-02 AND ERA 39754-14.

Part: LONGERON — CRACKED (BS 524) · airframe 43,747 hrs · 29,439 cycles

CRACK ON LONGERON 4L, BS 524. REMOVED DAMAGED. FABRICATED A NEW SECTION OF THE LONGERON IAW SRM 51-30-02 AND 51-30-05.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 43,747 hrs · 29,439 cycles

FORWARD GALLEY SERVICE DOOR FORWARD END OF BEAM NR 4 CRACKED. REPLACED IAW SRM 51-30-02 AND 51-30-05.

Part: DOOR FRAME — CRACKED (NLG WW) · airframe 43,747 hrs · 29,439 cycles

NOSE LANDING GEAR WHEEL WELL LEFT DOOR FRAME CRACKED, X=46. REPAIRED IAW SRM 53-90-01.

Part: FRAME — CRACKED (BS 1231) · airframe 43,747 hrs · 29,439 cycles

CRACKED FRAME, BS 1231 BETWEEN LONGERONS 5 - 6L. REPAIRED IAW ERA495237-14, REV B.

Part: LONGERON — CRACKED (BS 524) · airframe 43,747 hrs · 29,439 cycles

CRACK ON LONGERON 4R, BS 524. REPAIRED IAW SRM 53-10-01.

Part: BEAM — CRACKED (L1 DOOR) · airframe 43,747 hrs · 29,439 cycles

L1 DOOR FORWARD AND AFT NR 1 BEAM CRACKED. REPAIRED IAW SRM 52-10-02, FIG 5.

Part: DIAPHRAGM — CRACKED (BS 171) · airframe 43,747 hrs · 29,439 cycles

CRACK ON DIAPHRAGM BS 171, X 50. PLUG WAS INSTALLED SRM 51-30-02.

Part: PAN — CRACKED (BS 1003-1288) · airframe 43,747 hrs · 29,439 cycles

CRACK ON FORWARD UPPER RING PAN, BETWEEN BS 1003 - 1288 RIGHT SIDE. REPAIRED IAW SRM 56-20-02, 51-30-02 AND 51-30-05.

Part: PAN — CRACKED (BS 1041-1250) · airframe 43,747 hrs · 29,439 cycles

CRACK ON FORWARD LOWER RING PAN BETWEEN, BS 1041, 1227 AND 1250. REPAIRED IAW SRM 51-10-03 AND 56-20-02.

Part: SKIN — DENTED (BS 207-218) · airframe 43,747 hrs · 29,439 cycles

DENT ON EXTERNAL FUSELAGE SKIN BETWEEN, BS 207 - 218, LONGERONS 16 - 17L. HFEC NO DISCREPANCIES FOUND.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,131 hrs · 29,069 cycles

F/A REPORTED AN ODOR OF PROPANE IN CRUISE AND AGAIN DURING DESCENT AROUND 18000 FT. MAINTENANCE RAN BOTH ENGINES AT VARIOUS POWER SETTINGS. NO ODOR PRESENT. PERFORMED DUCT BURNOUT.

Part: CABLE — LOOSE (GIRT BAR) · airframe 43,067 hrs · 29,030 cycles

FORWARD ENTRY DOOR GIRT BAR CABLE LOOSE. R & R GIRT BAR CABLE ASSEMBLY IAW AMM.

Part: ATTACH FITTING — CRACKED (BS 1567) · airframe 38,457 hrs · 26,159 cycles

TAIL INTERIOR, RUDDER ACTUATOR OUTBOARD ATTACH INTERCOSTAL CRACKED AT CANTED STA 1567. R & R INTERCOSTAL IAW DWG 9911875.

Part: SKIN — CRACKED (BS 1475) · airframe 38,457 hrs · 26,159 cycles

CRACK FOUND ON SKIN BS 1475. REPAIRED IAW ERA 527787-14.

Part: DOUBLER — CORRODED (BS 1231) · airframe 38,457 hrs · 26,159 cycles

AFT CARGO BEAM INNER DOUBLER, BS 1231 CORRODED. REPAIRED IAW ERA 527788-14, REV O.

Part: FRAME — CRACKED (BS 1458) · airframe 38,454 hrs · 26,156 cycles

FRAME IS CRACKED AT FASTENER, BS 1458. INSTALLED REPAIR IAW SRM 51-70-01.

Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 38,454 hrs · 26,156 cycles

AFT CARGO DOOR LOWER FRAME CORRODED AND PAINT CHIPPED. REPAIRED IAW SRM 53-60-02, FIG 9. RII QC1981.

Part: SKATE ANGLE — CRACKED (VERTICAL STAB) · airframe 38,454 hrs · 26,156 cycles

RIGHT SIDE VERTICAL STABILIZER INNER SKATE ANGLE CRACKED, STA 1475. R & R ANGLE IAW DWG 5912188.

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 38,454 hrs · 26,156 cycles

L1 DOOR SLIDE FOUND UNSERVICEABLE. R & R L1 DOOR SLIDE ON AMDS 2561-4641.

Part: CLEVIS — BROKEN (CATWALK) · airframe 38,139 hrs · 25,965 cycles

FOUND CATWALK DOWN AND CABLE ON LT SIDE OF CATWALK LOOSE. FOUND LT CABLE AFT CLEVIS SNAPPED. R & R CLEVIS AND RIGGED IAW AMM.

Part: HANDLE — DISLODGED (COCKPIT DOOR) · airframe 37,697 hrs · 25,684 cycles

LOWER QUICK RELEASE HANDLE CAME OUT OF DOOR ON CENTER CONSOLE. SECURED COCKPIT DOOR LOWER HINGE RELEASE WIRE AND HANDLE. DOOR OPS CHECKS GOOD.

Part: FLANGE — BENT (L1 DOOR) · airframe 37,296 hrs · 25,465 cycles

FORWARD CABIN L1 DOOR IS BENT ON BOTTOM EDGE. REPAIRED L1 DOOR FLANGE IAW SRM 52-01-01, PARA 8.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 36,588 hrs · 24,975 cycles

RT HORIZONTAL STABILIZER UPPER SPAR CAP, CRACKED. REPAIRED IAW PRI 519463-14, REV 2. C/W FINAL ERA 519463-14AD, REV ORG.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 36,588 hrs · 24,975 cycles

RT HORIZONTAL STABILIZER UPPER SPAR CAP CRACKED. REPAIRED IAW PRI ERA 519463-14, REV 0 AND PRI ERA 519463-14 REV 2.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 36,588 hrs · 24,975 cycles

AFT UPPER SKIN CRACKED ON HORIZONTAL STABILIZER. REPAIRED IAW ERA 519495-14, REV ORIG.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 36,588 hrs · 24,975 cycles

RIGHT HORIZONTAL STABILIZER HINGE PIVOT FITTING CRACKED. CRACK EXCEEDS LIMITS. REPAIRED IAW ERA 519756-14AD ORIG.

Part: PIN — GALLED (HORIZONTAL STAB) · airframe 36,588 hrs · 24,975 cycles

HORIZONTAL STABILIZER PIVOT PIN GALLED. NEW PIN INSTALLED ON PRI 519756-14.

Part: PIN — GALLED (HORIZONTAL STAB) · airframe 36,588 hrs · 24,975 cycles

HORIZONTAL STABILIZER PIVOT PIN GALLED. INSTALLED NEW PIN ON PRI 519756-14.

Part: STRUCTURE — CORRODED · airframe 36,588 hrs · 24,975 cycles

UPPER AFT HOLE ON CENTER SECTION, RT SIDE, CORRODED. OPENED HOLE. REMOVED CORROSION. NO CRACKS FOUND. FABRICATED AND INSTALLED BUSHING IAW PRI 519682-14, REV 4.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 36,588 hrs · 24,975 cycles

RIGHT HORIZONTAL STABILIZER, UPPER AFT SPAR INBD FORWARD ATTACH HOLE BORE IS CORRODED. BURNISHED OUT CORROSION. FABRICATED AND INSTALLED BUSHING IAW ERA 519683-14.

Part: FITTING — DAMAGED · airframe 36,588 hrs · 24,975 cycles

DAMAGE AT UPPER SECOND FROM AFT HOLE ON CENTER SECTION, FITTING. REMOVED DAMAGE. INSTALLED BUSHINGS IAW SRM 55-10-03.

Part: FITTING — DAMAGED (UNKNOWN) · airframe 36,588 hrs · 24,975 cycles

DAMAGE AT UPPER AFT HOLE ON CENTER SECTION FITTING. REAMED AND REMOVED DAMAGE IAW SRM 55-10-03 HFEC. INSTALLED BUSHING. REPAIR COMPLETE IAW ERA 519682-14.

Part: HINGE FITTING — CORRODED (HORIZONTAL STAB) · airframe 36,588 hrs · 24,975 cycles

EVIDENCE OF FRETTING ON LT OUTER LUG FACE, LEFT HORIZONTAL STABILIZER HINGE FITTING ON VERTICAL STABILIZER. CORROSION REMOVED/REWORKED IAW SRM 55-30-05.

Part: HINGE FITTING — CORRODED (HORIZONTAL STAB) · airframe 36,588 hrs · 24,975 cycles

EVIDENCE OF FRETTING ON RIGHT OUTER LUG FACE, RT HORIZONTAL STABILIZER HINGE FITTING. REMOVED CORROSION IAW SRM 55-30-05.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 35,725 hrs · 24,467 cycles

DURING SERVICE CHECK, TAIL COMPARTMENT EXIT LIGHT ASSEMBLY FOUND INOPERATIVE. WIRES PULLED OUT OF SOCKET. MX RESEATED WIRES IN SOCKET. OPERATION CHECKS GOOD.

Part: CABLE — OUT OF ADJUST (AIR STAIR) · airframe 34,305 hrs · 23,719 cycles

CHECKED TENSION ON STAIRWING CEILING LIFT CABLES AND FOUND TO BE LOW, READJUSTED IAW AMM. OK FOR SERVICE.

Part: CABLE — BROKEN (COCKPIT DOOR) · airframe 32,177 hrs · 22,557 cycles

DURING SERVICE CHECK, FOUND COCKPIT DOOR EMERGENCY EGRESS LOWER CABLE BROKEN. MAINTENANCE INSTALLED NEW RELEASE CABLE. STOWED HINGE RELEASE HANDLE. OKAY FOR SERVICE.

Part: LONGERON — CORRODED (BS 1344-1355) · airframe 30,435 hrs · 21,676 cycles

LONGERON 29R CORRODED AT STA 1344-1355. REPAIRED IAW SRM 53-10-01 VOL 1.

Part: STRINGER — CORRODED (BS 1211 S29R) · airframe 30,435 hrs · 21,676 cycles

CORROSION AFT PIT STA 1211 LONGERON BEAM 29R. INSTALLED STRAP REPAIR IAW ERA 489830-14 ORIG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,435 hrs · 21,676 cycles

SKIN CORRODED UNDER VHF ANTENNA AFT CARGO PIT REPAIRED SKIN PER ERA 487590-14 ORIG.

Part: ANGLE — CORRODED (BS 427-465) · airframe 30,435 hrs · 21,676 cycles

FWD CARGO COMPARTMENT FLOOR SUPPORT Z ANGLE CORRODED BOTTOM SIDE AROUND FASTENER HOLES STA 427- 465. REPLACED Z ANGLE IAW SRM 53-40-01 VOL I FIG 7.

Part: SKIN — CORRODED (BS 588 L28-29L) · airframe 30,435 hrs · 21,676 cycles

LOWER FUSELAGE SKIN CORRODED AT BS 588 BETWEEN L282L AND L29L AREA REPAIRED IAW ERA 488948-14 ORIG.

Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 30,435 hrs · 21,676 cycles

MID CARGO FUSELAGE CUTOUT JAMB CORRODED REPAIR IAW SRM53-60-02

Part: LONGERON — CORRODED (BS 1134-1155) · airframe 30,435 hrs · 21,676 cycles

LONGERON 30 SPLICE AT STA 1134-1155 CORRODED. FABRICATED NEW SPLICE IAW DRAWING 3914677 PRI 4888951-14.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,435 hrs · 21,676 cycles

MID CARGO BAY LOWER DOOR SIL IS CORRODED AT SCUFF PLATE REPAIRED IAW EA02-397542-14MA REVB.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,433 hrs · 21,674 cycles

DURING DELTA HMV MTC VISIT PRODUCTION PERSONAL REPORTED CORROSION TO THE FUSELAGE SKIN PANEL 145AB P/N 5936371-3 COMPLETELY THROUGH. PART WAS BLENDED AND AMOUNT OF MATERIAL REMOVED EXCEEDED SRM 53-30-01.

Part: FRAME — CORRODED (BS 1443) · airframe 30,433 hrs · 21,674 cycles

HMV STA 1443 LOWER FRAME CORRODED. REMOVED AND REPLACED FRAME IAW SRM 51-10-05 AND SRM 51-30-00.

Part: INTERCOSTAL — CORRODED (BS 1203-1212) · airframe 30,433 hrs · 21,674 cycles

HMV SURFACE CORROSION ON INTERCOSTAL FS 1212-1203 LGN 30. REMOVED AND REPLACED CLIPS AND INTERCOASTAL IAW SRM 51-30-02.

Part: SHEAR TIE — CORRODED (BS 1212 L29-30L) · airframe 30,433 hrs · 21,674 cycles

HMV FOUND SHEAR TIE AT STA 1212 L30-29L CORRODED. FABRICATED NEW SHEAR TIE AND INSTALLED IAW 51-30-02.

Part: LONGERON — CORRODED (BS 1250-1269) · airframe 30,433 hrs · 21,674 cycles

HMV LONGERON 29L STA 1269-1250 CORRODED. REPAIRED IAW SRM 53-10-01 VOL 1.

Part: SILL — CORRODED (AFT CARGO BAY) · airframe 30,433 hrs · 21,674 cycles

HMV AFT CARGO BAY LOWER DOOR SILL CORRODED REPAIRED IAW SRM 53-60-02 VOL 1.

Part: LONGERON — CORRODED (BS 1298 L30) · airframe 30,433 hrs · 21,674 cycles

HMV LONGERON 30 STA 1293 CORRODED. REPAIRED IAW SRM 53-10-01 VOL 1.

Part: CARGO TRACK — CORRODED (BS 532-865) · airframe 30,433 hrs · 21,674 cycles

MID CARGO PIT LT STA 532-865 CARGO TRACK CORRODED BEYOND ALLOWABLE LIMITS CARGO TRACK. REMOVED AND REPAIRED IAW 53-40-01 FIG 1.

Part: LONGERON — CORRODED (BS 1345 L29L) · airframe 30,433 hrs · 21,674 cycles

AFT CARGO COMPARTMENT LONGERON 29L AT BS 1345 ON LOWER SIDE EXFOLIATED. REMOVED DAMAGE SECTION OF LONGERON AND SPLICED NEW SECTION IN IAW SRM 53-10-01 FIG 7 FROM STA 1317 TO 1354 LONGERON 29L.

Part: FLOORBEAM — CORRODED (FORWARD CARGO) · airframe 30,433 hrs · 21,674 cycles

FORWARD CARGO BAY FLOOR SUPPORT AT BS 218, LONGERON 28L TO 28R LEVEL 1 CORROSION. REPLACED IAW SRM 51-30-02, VOL II, PAGE 11, PN 9936719-169. NR 19838.

Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 30,433 hrs · 21,674 cycles

AFT CARGO BAY FUSELAGE CUTOUT DOOR JAMB HAS SURFACE CORROSION LEVEL 2 AT LOWER CENTER OF DOOR JAMB OUT OF LIMITS. REPAIRED IAW SRM 53-60-02, VOL 1, PARA 11.

Part: FRAME — CORRODED (BS 807) · airframe 30,433 hrs · 21,674 cycles

CENTER CARGO STA 807 FRAME CORRODED. REPAIRED FRAME IAW ERA 487594-14 REVISION ORIG.

Part: ANGLE — CORRODED (FWD CARGO BAY) · airframe 30,433 hrs · 21,674 cycles

FWD CARGO COMPARTMENT FLOOR SUPPORT Z ANGLE IS CORRODED ON BOTTOM SIDE AROUND FASTENER HOLES STA 427 THRU 446 X15 TO X18. REMOVED AND REPLACED Z ANGLE FROM STA 427 TO 446 IAW SRM 53-40-01 VOL 1 FIG 7.

Part: FLOORBEAM — CORRODED (BS 1212) · airframe 30,433 hrs · 21,674 cycles

AFT COMPARTMENT CARGO SURFACE CORRSION ON FLOORBOARD SUPPORT STA 1212 LGN 28L-28R. REMOVED CORROSION ON FLOOR SUPPORT ORIG THICKNESS .063 AFTER BLENDING .50 REMAINS .013 MAT LOSS OUT OF LIMITS PER SRM 53-00-01 PG 9. REPLACED FLOOR SUPPORT.

Part: SKIN — CORRODED (BS 1344) · airframe 30,433 hrs · 21,674 cycles

AFT CARGO COMPT SURFACE CORROSION AROUND DRAIN VALVE SKIN FASTENERS L30 FS 1344. REPAIRED SKIN WITH 0.071 DOUBLER AND INTERNAL FINGER DOUBLER IAW SRM 53-30-01 FIG 1 VOL1.

Part: SUPPORT ANGLE — CORRODED (BS 655 FRAME) · airframe 30,433 hrs · 21,674 cycles

CENTER CARGO BILGE BS 655 SUPPORT ANGLE ON FRAME IS CORRODED, LEVEL 2 FROM LONGERON 28R TO 28L. REPLACED SUPPORT ANGLE IAW ERA 487593-14 AND SRM 51-30-02, FIG 2, PG 4, FIG 3, PG 5, AND FIG 7, PG 11.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 25,352 hrs · 17,932 cycles

FWD LOWER CARGO DOOR JAMB PAN CORROSION REPAIR FWD CORNER TO AFT CORNER.

Part: SKIN — CORRODED (BS 1079 L29) · airframe 25,352 hrs · 17,932 cycles

SKIN CORROSION L29 AT STA 1079 OF AFT CARGO COMPARTMENT.

Part: SEAT TRACK — CORRODED (BS 1155-1296) · airframe 25,352 hrs · 17,932 cycles

CORROSION ON THE LT SECOND SEAT TRACK OF AFT CABIN AT STA 1155-1296.

Part: SPLICE — CORRODED (BS 1241) · airframe 25,352 hrs · 17,932 cycles

CORROSION ON SPLICE BAR AT STA 1241 OF AFT CARGO COMPARTMENT SRM 53-30-01, FIG 3.

Part: FITTING — CORRODED (BS 522-541) · airframe 25,352 hrs · 17,932 cycles

CORROSION ON LT TRACK FITTING AT STA 522-541 OF MID CARGO COMPARTMENT SRM 53-40-01, FIG 7.

Part: FITTING — CORRODED (BS 579-598) · airframe 25,352 hrs · 27,932 cycles

CORROSION ON LT TRACK FITTING AT STA 579-598 OF MID CARGO COMPARTMENT.

Part: SEAT TRACK — CORRODED (BS 1155-1296) · airframe 25,352 hrs · 17,932 cycles

CORROSION ON THE LT FIRST SEAT TRACK OF AFT CABIN AT STA 1155-1296.

Part: SKIN — DENTED (BS 229-256) · airframe 25,352 hrs · 17,932 cycles

DENT DAMAGE ON LT FUSELAGE SKIN AT STA 229-256, L16-18L.