N956AT

Part: COVER — MISSING (EXIT SIGN) · airframe 49,156 hrs · 34,089 cycles

EMERGENCY EXIT SIGN COVER IS MISSING AT INTERIOR LOCATION 600. INSTALLED LENS. CHECKS GOOD.

Part: STRUCTURE — CRACKED (VERTICAL STAB) · airframe 48,146 hrs · 33,392 cycles

CRACK WAS INDICATED IN 6 LOCATIONS ON THE RIGHT VERTICAL STAB AREAS. REPAIRED PER PRI 567609-14AD. ER/A, 567609-14AD, MATCHES PRI.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,111 hrs · 32,766 cycles

DURING A SERVICE CHECK, FOUND THE CEILING MID-CABIN DIRECTIONAL EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IAW AMM 33-51 AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,736 hrs · 31,795 cycles

DURING A SERVICE CHECK, OVERWING EMERGENCY EXIT LIGHTS WOULD NOT STAY ILLUMINATED. R & R THE BATTERY PACK AT 22CDE IAW AMM 33-51. OPS CHECKED GOOD.

Part: BRACKET — BROKEN (FUSELAGE) · airframe 43,746 hrs · 30,297 cycles

LOUD VIBERATION UNDER SEAT 20B. FOUND SUPPORT BRACKET FOR OVERWING TO BODY FAIRING BROKEN BELOW AFT OVERWING EXIT DOOR. FABRICATED AND REPLACED THE BRACKET IAW DRAWING 5971068.

Part: BEAM — CRACKED (GALLEY DOORWAY) · airframe 43,165 hrs · 29,827 cycles

GALLEY DOOR BEAM IS CRACKED AT THE LOWER HINGE MOUNTING FLANGE, MARKED. REPLACED GALLEY DOOR BEAM AT THE LOWER HINGE MOUNTING FLANGE IAW SRM 51-41-00.

Part: FRAME — GOUGED (BS 1146) · airframe 43,165 hrs · 29,827 cycles

WHEN REMOVING PANEL FOR ACCESS, FOUND FRAME GOUGED AT BS 1146 ALSO 2 FWD BRACKETS CRACKED AT APPROXIMATELY 1106 IN WALKWAY. REPAIR IAW SRM. REPAIRED DAMAGED FRAME IAW ER/A 545664-14, REV O. ASSOCIATED ER/A 00-545664, ADDED FOR AC 9515.

Part: SKIN — CRACKED (BS 1133) · airframe 43,165 hrs · 29,827 cycles

FUSELAGE SKIN CRACKED, BS 1133 OTBD OF STR 2L AT SHEAR TIE FASTENER, HFEC VERIFIED. REPAIRED SKIN CRACK AT BS Y1133 OTBD OF STR SL IAW ER/A 544353-14AD. SEE NON-ROUTINE/ AMDS CONTINUATION SHEETS FOR WORK ACCOMPLISHED. ASSOCIATED ER/A 00-544353 ADDED FOR AC 9515.

Part: STRINGER — CRACKED · airframe 43,165 hrs · 29,827 cycles

THREE STRINGERS ARE CRACKED AT THE OTBD ENDS INTERNAL OF THE CANTED KEEL. RT BS 675, AND LT BS 675 AND 696. MARKED EXTERNALLY. REMOVED AND REINSTALLED WING TO BODY FAIRING SUPPORT IAW SRM 51-41-05. REMOVED AND REINSTALLED NOSE STEERING, SLAT EXTEND AND RETRACT LINES, AND HYD PRESSURE AND RETURN LIMITS AT BS 688 TO 726 IAW AMM 20-10-07. REMOVED AND INSTALLED SERVICEABLE FORMERS IAW SRM 51-41-02.

Part: FRAME — CORRODED (BS 908) · airframe 43,165 hrs · 29,827 cycles

FRAME CORRODED IN ALC BS 908 BL0. REPLACED FORMER FRAME SECTION IN C2 AT BS 908 BL0 IAW SRM 53-00-06, REPAIR 2, FIG 201. FORMER WAS FABRICATED AND HEAT TREATED TO T6 IAW DAL PSM 900-4-1, NR 1, PG 16, 12-20-10, PG 25 1/17/12 WO 66072-0026. REPAIR SPLICE MATERIAL WAS FABRICATED IAW 53-00-06, REPAIR 2, FIG 201.

Part: SKIN — CRACKED (BS 1133) · airframe 43,165 hrs · 29,827 cycles

FUSELAGE SKIN CRACKED, BS 1133, OTBD OF STR 2R AT SHEAR TIE FASTENER, HFEC VERIFIED. REPAIRED SKIN CRACK AT BS 1133 OTBD OF STR 2R IAW ER/A 544354-14AD, REV A. NON-ROUTINE/AMDS CONTINUATION FORMS FOR WORK ACCOMPLISHED. ASSOCIATED ER/A 00-544354 ADDED FOR AC 9515.

Part: FRAME — CORRODED (BS 927) · airframe 43,165 hrs · 29,827 cycles

FRAME CORRODED IN ALC BS 927, BL0. REPLACED FORMER SECTION OF FRAME IN AFT CARGO STA 927 BL0 IAW B717 SRM 53-00-06 REPAIR 2. FORMER WAS FABBED IAW B717 PL 9915524 AND HEAT TREATED TO 7075-T6 IAW DPS 900-4-1, NR 1, PG 16 12/20/10, PG 25 1/17/12. REPAIR SPLICE FABRICATED AND ALSO INSTALLED IAW SRM 53-00-06, REPAIR 2.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 43,165 hrs · 29,827 cycles

VERTICAL STABILIZER L/E ZFS 52.267, NUMEROUS FASTENERS LOOSE, SEVERAL FASTENERS PULLED THROUGH AND PARTIALLY PULLED THROUGH. REPAIRED VERTICAL STABILIZER L/W FASTENERS HOLES IAW SERVICE DWG SG 95550001, REPAIRED CRACK ON VERTICAL STABILIZER. FOUND DURING OPEN HOLE SCAN, LT SPAR CAP UPPER FLANGE AT BS ZFS52 IAW ER/A 544360-14 REV ORIGINAL, AND DWG SG95550005.

Part: FRAME — CORRODED (BS 974) · airframe 43,165 hrs · 29,827 cycles

BS 974 AT STRINGER 30 HAS APPROXIMATELY 6" OF CORROSION COMMON TO FRAME. BLENDED CORRODED AREA IAW SRM 53-00-00, FIG 103. FOUND OUT OF LIMITS IAW SRM 53-20-07. NEW FRAME FABRICATED AND HEAT TREATED IAW DPS 900-4-1 NR 1, PG 16 12-20-10, PG 25 1-17-12, INSTALLED IAW SRM 53-00-06, REPAIR 2, FIG 201.

Part: LONGERON — CORRODED (BS 908-960) · corrosion level 2 · airframe 43,165 hrs · 29,827 cycles

LONGERON 29L IN BS 908-960 IS CORRODED IN SEVERAL AREAS. REMOVED RIVETS ON STR 29L IAW SRM 51-41-02, INSTALLED NEW RIVETS ON STR 29L IAW SRM 51-41-02 BLENDED CORROSION ON STR 29L FROM BS 908-960 IAW SRM 53-00-05. REPAIR 3 C/W THICKNESS CHECK IAW MD/B NTSPM 04-00-07 ORIGINAL T .125 REMAINING T.088, BS 958 INSTALLED U CHANNEL REPAIR IAW SRM 53-00-05, FABRICATED U CHANNEL IAW SRM 51-30-01 AND 53-00-05 HEAT TREADED U CHANNEL IAW DPS 900-4-1, NR 1, PAGE 16, 12-20-10, PAGE 25-1-17-12.

Part: SEAT TRACK — CORRODED (BS 148-1053) · corrosion level 2 · airframe 43,165 hrs · 29,827 cycles

LT CTR SEAT TRACK BS 148-1053, X=44.5 HAS MULTIPLE DISCREPANCIES. BLENDED LBL 44.5 LT CTR SEAT TRACK, BS 140-STA 200, STA 246-STA 1053. SEAT TRACK IS WITHIN ALLOWABLE LIMITS IAW SRM 53-20-52. REPLACED SECTION OF SEAT THAT IS OUT OF LIMITS BS 200-BS 246 IAW SRM 51-40-2 AND 53-20-52, REPAIR 5, FIG 201.

Part: SKIN — CRACKED (BS 1087) · airframe 43,165 hrs · 29,827 cycles

FUSELAGE SKIN CRACKED, HFEC VERIFIED, BS 1087 ABOVE STR 14R AT SHEAR TIE FASTENER. REPAIRED FUSELAGE CRACKED SKIN IAW BS 1087, STR 14R IAW ER/A 544359-14.

Part: SKIN — CRACKED (BS 1087) · airframe 43,165 hrs · 29,827 cycles

FUSELAGE SKIN CRACKED, HFEC VERIFIED, BS 1087 ABOVE STR 14L SHEAR TIE FASTENER. REPAIRED FUSELAGE CRACKED SKIN IAW ER/A 544359-14.

Part: SUPPORT — CRACKED (SEAT TRACK) · airframe 43,165 hrs · 29,827 cycles

RIGHT SIDE OF CENTER TANK, RBL 45, SEAT TRACK SUPPORT IS CRACKED AT BOTTOM OF SUPPORT, MARKED. REPLACED SEAT TRACK SUPPORT IAW SRM 51-40-02 AND 53-20-51, FIG 1, SHEET 2 OF 3.

Part: CUSP WEB — CORRODED (BS 207) · airframe 43,165 hrs · 29,827 cycles

AREA OF CORROSION ON OUTER CUSP WEB NEAR S18R APPROXIMATELY BS 207. REPLACED CUSP WEB IAW SRM 51-41-02, PG 1-4, 51-41-05, PG 1.

Part: LONGERON — CORRODED (BS 908-960) · corrosion level 2 · airframe 43,165 hrs · 29,827 cycles

LONGERON 30 IN BS 908-960 HAS SEVERAL AREAS OF CORROSION. BLENDED CORROSION FROM BS 908-960, L30 IN AFT CARGO IAW SRM 53-00-05, REPAIR 3. THICKNESS CHECK PERFORMED IAW NTSPM 04-00-07, ORIGINAL THICKNESS .125, .093 LEG, REMAINING THICKNESS ON LEG AT BS 954 IS .061 BS 908-953 OF STR FOUND WITHIN LIMITS. BS 954-960 FOUND OUT OF LIMITS IAW SRM 53-00-05, REPAIR 3. A "U" CHANNEL WAS FABRICATED AND INSTALLED TO THE OUT OF LIMITS AREA IAW SRM 53-00-05 AND 51-03-07.

Part: PIN — DETACHED (L1 DOOR SLIDE) · airframe 41,413 hrs · 28,479 cycles

L1 DOOR SLIDE PINS WERE DETACHED. REPLACED L-1 DOOR SLIDE AND COMPLETED REQUIRED INSPECTION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,166 hrs · 28,293 cycles

DURING LINE CHECK, NOTED EMERGENCY LIGHTS IN AFT EXIT AND WALKWAY WERE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY AND FUNCTION CHECK WAS GOOD.

Part: CUSP WEB — CRACKED (BS 655) · airframe 40,509 hrs · 27,773 cycles

MAIN CABIN, CUSP WEB CRACKED AT BS 655, LBL 54. REPAIRED IAW SRM 53-00-55, REP 4, FIG 223 & DWG 9910151.

Part: CUSP WEB — CRACKED (BS 717) · airframe 40,509 hrs · 27,773 cycles

MAIN CABIN CUSP MEMBRANE CRACKED AT STA 717, LBL 49. DAMAGED SECTION REPLACED IAW SRM 53-00-55, REP 4, FIG 219 AND DWG 9910151, REV AL & CH.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 38,122 hrs · 25,835 cycles

FORMER ANGLE CRACKED AT BS 1050, LONGERON 26L. R & R ANGLE IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,728 hrs · 26,224 cycles

AFT LOWER EMERGENCY EXIT LIGHT BULB INOPERATIVE. RE-LAMPED BULB IAW MM.

Part: PAN — CORRODED (FUSELAGE) · airframe 38,782 hrs · 26,261 cycles

AFT CARGO DOOR CUT OUT LOWER PAN CORRODED BETWEEN BS 954 TO BS 970. REPAIRED PAN IAW SRM.

Part: MOUNT BRACKET — BROKEN (CABIN) · airframe 38,728 hrs · 26,224 cycles

CEILING EMERGENCY LIGHT AT ROW 1 MOUNTING BRACKET BROKEN. R & R LIGHT IAW MM.

Part: PAN — CORRODED (FUSELAGE) · airframe 38,122 hrs · 25,835 cycles

AFT CARGO DOOR LOWER JAMB PAN CORRODED BETWEEN BS 954 TO BS 970. REPAIRED JAMB PAN IAW SRM.

Part: SUPPORT — CRACKED (LT AILERON) · airframe 38,122 hrs · 25,835 cycles

LEFT AILERON NR 4 HINGE UPPER PANEL SUPPORT CRACKED. R & R SUPPORT IAW SRM.

Part: HINGE — CRACKED (FUSELAGE) · airframe 38,122 hrs · 25,835 cycles

EXTERNAL POWER DOOR HINGE CRACKED. R & R HINGE IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 38,122 hrs · 25,835 cycles

LEFT WING NR 5 SLAT CTR TRACK SKIN CUT OUT FIXED LE CRACKED. REPAIRED SKIN IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 38,122 hrs · 25,835 cycles

MAIN CABIN FLOOR PANEL 223GF DAMAGED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 38,122 hrs · 25,835 cycles

CENTER FLOOR PANEL 211ALF IN FLIGHT COMPARTMENT DELAMINATED. R & R PANEL IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 38,122 hrs · 25,835 cycles

AFT PRESS BULKHEAD FWD FACE BULKHEAD SKIN CORRODED AT FS 1053, BETWEEN LONGERON 30R TO LONGERON 29R. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (BS 200) · airframe 38,122 hrs · 25,835 cycles

WEB CRACKED AT BS 200, LBL 7. REPAIRED WEB IAW SRM & EA.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 38,122 hrs · 25,835 cycles

CUSP WEB DAMAGED AT BS 219, RBL 44.5. REPAIRED WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,122 hrs · 25,835 cycles

CABIN FLOOR SUPPORT BEAM CORRODED BETWEEN BS 160 TO BS 200, RBL 10. R & R BEAM IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,122 hrs · 25,835 cycles

CABIN FLOOR SUPPORT CORRODED AT BS 200, BETWEEN RBL 10 TO RBL 44. R & R SUPPORT IAW SRM & DRAWING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,122 hrs · 25,835 cycles

CABIN SEAT TRACK CORRODED AT BS 237, RBL 44. R & R SEAT TRACK IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,122 hrs · 25,835 cycles

CABIN FLOOR SUPPORT BEAM CORRODED AT STATION 160 TO STATION 200, LBL 7. R & R SUPPORT IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 38,122 hrs · 25,835 cycles

MAIN CABIN FLOOR PANEL 222DF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,122 hrs · 25,835 cycles

MAIN CABIN FLOORBOARD DELAMINATED 222BF. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 38,122 hrs · 25,835 cycles

MAIN CABIN FLOOR PANEL GF DELAMINATED. R & R PANEL IAW SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 38,122 hrs · 25,835 cycles

AFT FUSELAGE PRESS BULKHEAD FWD FACE CORRODED BETWEEN ROW 26L TO ROW 26R. R & R BULKHEAD IAW SRM & DWG.

Part: PAN — CORRODED (FUSELAGE) · airframe 38,122 hrs · 25,835 cycles

AFT CARGO DOOR LOWER JAMB PAN CORRODED BETWEEN BS 954 TO BS 970. REPAIRED PAN IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 38,122 hrs · 25,835 cycles

FORWARD CARGO DOOR LOWER JAMB CORRODED BETWEEN BS 417 TO BS 425. R & R PAN IAW SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 38,674 hrs · 26,191 cycles

EMERGENCY EXIT SIGN INOPERATIVE. RELAMPED SIGN IAW SIP.

Part: PIN — MISSING (EVAC SLIDE) · airframe 37,952 hrs · 25,717 cycles

L1 DOOR EMERGENCY EVAC SLIDE PINS MISSING. R & R SLIDE IAW MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 37,296 hrs · 25,301 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE BETWEEN ROWS 25 - ROW 31. R&R POWER SUPPLY UNIT IAW AMM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 36,628 hrs · 24,874 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 35,946 hrs · 24,447 cycles

FWD GALLEY DOOR SLIDE IN RED. REMOVED AND REPLACED R1 DOOR SLIDE REF AMM P/N VERIFIED 100561.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 34,952 hrs · 23,815 cycles

MOLDY OR MUSTY SMELL COMING FROM PACKS (AIR SYSTEM) DURING FLIGHT. REMOVED AND REPLACED RIGHT COALESCER BAG PER MM.

Part: COTTER PIN — MISSING (L2 DOOR) · airframe 28,270 hrs · 12,923 cycles

AFT ENTRY DOOR AFT COTTER PIN MISSING. INSTALLED PIN PER MM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 33,937 hrs · 23,157 cycles

EMERGENCY LIGHT INOP AT ROW 18 DEF. SECURED LIGHT CONNECTOR PER MM.

Part: COVER — OUT OF POSITION (CABIN)

EXIT LIGHT COVER FELL OFF. RE-SECURED EXIT LIGHT COVER REF AMM 25-20.

Part: LIGHT — INOPERATIVE (CABIN)

ONE BULB BURNT OUT BELOW 3D IN THE EMERGENCY LIGHT SYSTEM. RELAMPED, OPS CHECK GOOD, MM 33-51.

Part: ENGINE — FAILED (LEFT)

LEFT ENGINE FAILURE AT 22,000 FEET. REMOVED AND REPLACED NR 1 ENGINE ON W/O 247893, TASK CARD 603. OPS AND LEAK CHECK GOOD. AUTOLAND ACCOMPLISHED W/O 247893 TASK 625. ALL TESTS PASSED.

Part: COVER — MISSING (CABIN)

EPL COVER MISSING AT 26D. INSTALLED NEW COVER IAW AMM 33-51.

Part: COALESCER BAG — ODOR (AC BAY)

LEVEL AT 28K FLT ATTS CALLED AND REPORTED A BURNING SMELL IN THE VENT F/O SMELLED AS WELL AT GATE IN ATL AND ELECTRIC SMELL / WAS VERY EVIDENT AFTER COCKPIT DOOR OPENED. PERFORMED FIM TASK 21-22 808-810 AND SPECIAL INSPECTION FOR IRREGULAR ODOR. REMOVED AND REPLACED BOTH COALESCER BAGS REFER TO LOG BOOK PG 1708830 / ITM 3. ODOR INSPECTION PERFORMED ON LOG BOOK PG 1708831 ITM 1, GOOD FOR CONTINUED FLIGHT.

Part: LIGHT — INOPERATIVE (CABIN)

SEAT ROW 15 AND 29 EMERGENCY LIGHTS INOPERATIVE. RELAMPED EMERGENCY LIGHTS. OPS CHECK GOOD. REF MM 33-51.

Part: FRAME — DAMAGED (FUSELAGE)

AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 3. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2985.

Part: FRAME — DAMAGED (FUSELAGE)

AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 3. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2975.

Part: ATTACH FITTING — CORRODED (GIRT BAR)

GALLEY ENTRANCE, AFT GIRT BAR ATTACH FITTING, CORROSION. ACCOMPLISHED GIRT BAR ATTACH FITTING REPLACEMENT PER B717 SRM 51-41-01.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237, RBL 44.5, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F AND EA 17-53-02800IR.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F AND EA 17-53-02799IR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 237, BL 0, CRACKED AND CORRODED. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: STRUCTURE — CRACKED (PYLON)

LEFT PYLON APRON LOWER NR 4 HINGE CUTOUT AREA, CRACKED. ACCOMPLISHED NR 4 HINGE CUTOUT AREA DOUBLER REPAIR PER TRA 17-54-TR00129.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 194, LBL 1, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-41-02.

Part: STRUCTURE — CRACKED (LT MLG DOOR)

LEFT MLG DOOR, LOWER CORNER INNER FACE, CRACKED. ACCOMPLISHED INNER FACE DOUBLER REPAIR PER TRA 17-52-TR00139.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 5 TO RBL 25, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: DOOR FRAME — CRACKED (FUSELAGE)

PASSENGER ENTRANCE AREA DOOR JAMB WEB, STA 210, LONG L15L, CRACKED AND CORRODED. ACCOMPLISHED DOOR JAMB WEB DOUBLER REPAIR PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148, RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: SLIDE — UNSERVICEABLE (L1 DOOR)

L-1 GIRT BAR HANGS DOWN LOOSELY. NO DEFECTS NOTED ON GIRT BAR. REMOVED AND REPLACED L-1 EVACUATION SLIDE PER 25-61 DUE TO PINS DISCONNECTED.

Part: SLIDE — UNSERVICEABLE (L1 DOOR)

L-1 DOOR SLIDE PIN PULLED. REPLACED L-1 DOOR SLIDE ASSY PER AMM 25-61.

Part: ENGINE — MALFUNCTIONED (NR 1)

NR 1 ENGINE SURGE AND EGT RISE WITH LOUD BANG. EGT CLIMBED TO 1078 DEGREES, N1 WENT TO ZERO AND THE N2 WAS AT 20 PERCENT. THE FLIGHT CREW PERFORMED AN INFLIGHT SHUTDOWN.

Part: SKIN — DENTED (FUSELAGE)

FOUND 2 DENTS WITH GOUGES AT FS 266 ABOVE LONGERON 18L. REPAIRED PER B717 SRM 53-00-01, INSTALLED FLUSH REPAIR.

Part: DOOR — OPEN (NLG)

SEVERE VIBRATION AFTER TAKEOFF. DISCOVERED LEFT NOSE GEAR DOOR OPEN DURING INSPECTION (WALKAROUND). RELATCHED NOSE GEAR DOOR, NO DAMAGE NOTED. BOTH LEFT AND RIGHT NOSE GEAR DOORS LOCK NORMAL. REF TO AMM 32-20.

Part: PAN — CORRODED (CARGO DOORWAY)

AFT CARGO COMPT LOWER PAN CORRODED. INSTALLED LOWER JAMB PAN AND SPLICES AS PER B717 SRM 53-20-15 REPAIR 6.

Part: FRAME — CRACKED (BS 1178)

AFT ACCESSORY COMP CANTE FRAME CRACKED FS 1178 BELOW LONG 17 RT. INSTALLED FORMED ANGLE REPAIR PER SRM 51-70-11.

Part: PAN — CORRODED (CARGO DOORWAY)

FWD BAG BIN DOOR FRAME PAN HAS CORROSION BEYOND LIMITS. INSTALLED PAN SPLICE REPAIR PER SRM 53-20-15 REPAIR 6.

Part: FRAME — CRACKED (BS 1178)

AFT ACCESSORY COMP CANTE FRAME CRACKED, FS 1178 BELOW LONG 17 LT. INSTALLED FORMED ANGLE REPAIR PER SRM 51-70-11.

Part: FITTING — DAMAGED (NLG)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. NLG RETRACT ACTUATOR FITTING AND DETAILS COMMON TO STA 110.0 BULKHEAD DAMAGED. REPLACED NLG RETRACT ACTUATOR FITTING AND DETAILS COMMON TO STA 110.0 BULKHEAD PER MDC DRAWING 5911509 REV CC DATED 5/16/01.

Part: SKIN PANEL — DAMAGED (FUSELAGE)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LOWER SKIN PANEL AND HINGE DAMAGED. REPLACED LOWER SKIN PANEL AND HINGE INSTALLATION AT AFT NLG WHEEL WELL PER MDC DRAWING 5913421 REV W DATED 12/04/99.

Part: BUNGEE — DAMAGED (NLG)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. NLG COLLASPED (AFT DIRECTION) APPORX 18 INCHES EXPOSED (WHEEL ASSEMBLE). REMOVED AND REPLACED NLG ASSY AND RETRACT CYCLE AND BUNGEE PER JAC 717-5044-559532001-01 PER MDC DRAWING 5940760 REV T DATED 01/24/06.

Part: FRAME — CRACKED (BS 83)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LEFT SIDE FRAME AT STA 83.0 CRACKED AND BENT BEYOND REPAIR. REPLACED LEFT SIDE FRAME AT STA 83.0 PER MDC DRAWING 9911505 REV AN DATED 8/20/99.

Part: FRAME — DAMAGED (BS 120)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LOWER FRAME AT STA 120.0 DAMAGED. REPAIRED LOWER FRAME AT STA 120.0 PER MDC DRAWING 9911510 REV M DATED 7/13/00 AND PER BOEING ENGINEERING ROD/SKETCH NUMBER 06-12-10-004, 8100-9 APPROVED ON 01-07-07.

Part: SUPPORT — CRACKED (NLG DOOR)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. AFT SUPPORT OF THE FWD LEFT NLG DOOR CRACKED. REPLACED AFT SUPPORT OF THE FWD LEFT NLG DOOR PER MDC DRAWING 9957851 REV S DATED 01/26/00 AND DRAWING 9957852 REV Y DATED 01/26/00.

Part: RADOME — CRACKED (BS 37)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. RIGHT AND LEFT RADOME LATCH ASSEMBLIES AND FORWARD LOWER SKIN CRACKED AND BROKEN BEYOND REPAIR. REPLACED RIGHT AND LEFT RADOME LATCH ASSEMBLIES AND FORWARD LOWER SKIN AT STA 37.0 PER MDC DRAWING 5911400 REV CM DATED 05/03/01.

Part: SUPPORT — DAMAGED (FUSELAGE)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. GLIDE SLOPE ANTENNA SUPPORT AND SHIELD DENTED AND BENT BEYOND REPAIR. REPLACED GLIDE SLOPE ANTENNA SUPPORT AND SHIELD PER MDC DRAWING 9971488 REV (NEW) DATED 10-22-97.

Part: PANEL — CRACKED (FUSELAGE)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. DISCONNECT PANEL ASSEMBLY CRACKED. REMOVED AND REPLACED DISCONNECT PANEL ASSEMBLY AND DETAILS PER MDC DRAWING 5971435 REV F DATED 03/03/03 AND PER DRAWING 7970776 REV J DATED 01/24/06.

Part: SKIN PANEL — DAMAGED (BS 110-229)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LOWER SKIN PANEL FROM STA 110.0 TO STA 229.0 DAMAGED. REPLACED LOWER SKIN PANEL FROM STA 110.0 TO STA 229.0 PER MDC DRAWING 5911401 REV DW DATED 1/7/04.

Part: FRAME — CRACKED (BS 76)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LEFT SIDE FRAME AT STA 76.0 CRACKED AND BENT BEYOND REPAIR. REPLACED LEFT SIDE FRAME AT STA 76.0 PER 991 1504 REV L DATED 7/10/98.

Part: FRAME — CRACKED (BS 37)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. FORMER ANGLE, WEB AND SEAL CRACKED AND BROKEN BEYOND REPAIR. REPLACED STA 37.0 FORMER ANGLE, WEB AND SEAL PER MDC DRAWING 991 1500 REV DL DATED 4/24/01.

Part: DOOR — DAMAGED (NLG)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LEFT FWD AND AFT NOSE GEAR DOOR DAMAGED. REPLACED NLG FWD AND AFT DOORS PER MDC DRAWING 5910086 REV AF DATED 01/24/06.

Part: DRAIN MAST — DAMAGED (FWD)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. DRAIN MAST DAMAGED. REPLACED DRAIN MAST PER 717 AMM CHAPTER 30-72-02 REV 27 DATED 01/01/07.

Part: SUPPORT FITTING — CRACKED (NLG STEERING)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. NLG STEERING VALVE SUPPORT FITTING CRACKED. REPLACED NLG STEERING VALVE SUPPORT FITTING AT STA 83.5 PER MDC DRAWING 5910098 REV R DATED 01-24-06.

Part: HYDRAULIC LINE — CRACKED (NLG)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. NLG HYDRAULIC PIPING AND RELATED SUPPORTS CRACKED. REMOVED AND REPLACED NLG HYDRAULIC PIPING AND RELATED SUPPORTS PER MDC DRAWING 5963926 REV T DATED 06/28/00.

Part: ANTENNA — DAMAGED (NR 1 VHF COMM)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. NR 1 VHF COMMUNICATION ANTENNA DAMAGED. REPLACED NR 1 VHF COMMUNICATION ANTENNA PER 717 AMM CHAPTER 23-12-03 REV 27 DATED 01/01/07.

Part: SUPPORT BEAM — CRACKED (NLG)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. NLG LT AND RT SUPPORT BEAMS CRACKED AND BENT BEYOND REPAIR. REPLACED NLG LT AND RT SUPPORT BEAMS PER MDC DRAWING 9910088 REV CJ DATED 01/24/06.

Part: BULKHEAD — CRACKED (BS 110)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. BULKHEAD AT STA 110 CRACKED AND BENT BEYOND REPAIR. REPAIRED BULKHEAD AT STA 110 PER MDC DRAWING 9911509 REV L DATED 5/13/02 AND PER BOEING ENGINEERING ROD/SKETCH NUMBER 06-12-10-003-002, 8100-9 APPROVED ON 01-07-07.

Part: SWITCH — DAMAGED (NLG)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. GROUND SENSING INTERLOCK SWITCH DAMAGED. REPLACED GROUND SENSING INTERLOCK SWITCH PER MDC DRAWING 7940768 REV AP DATED 01/24/06.

Part: ANTENNA — DAMAGED (DME)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. DME ANTENNAS DAMAGED. REPLACED DME ANTENNAS PER 717 AMM CHAPTER 34-52-02 REV 27 DATED 01/01/07.

Part: ACCESS DOOR — DAMAGED (ACC BAY)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. ACCESSORY COMPARTMENT ACCESS DOOR DAMAGED. REPLACED ACCESSORY COMPARTMENT ACCESS DOOR PER MDC DRAWING 5910083 REV AY DATED 01/24/06.

Part: STRUCTURE — CRACKED (BS 110)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. TEE CAP AT STA 110 CRACKED AND BENT BEYOND REPAIR. REPAIRED TEE CAP AT STA 110 PER MDC DRAWING 9911509 REV L DATED 5/13/02 AND PER BOEING ENGINEERING ROD/SKETCH NUMBER 06-12-10-003-001, 8100-9 APPROVED ON 01-07-07.

Part: FRAME — CRACKED (BS 69)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LEFT SIDE FRAME AT STA 69.0 CRACKED AND BENT BEYOND REPAIR. REPLACED LEFT SIDE FRAME AT STA 69.0 PER MDC DRAWING 9911503 REV CT DATED 1/7/04.

Part: RADOME — DENTED (FUSELAGE)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. RADOME ASSEMBLY DENTED. REPLACED RADOME ASSEMBLY PER 717 AMM CHAPTER 53-51-01 REV 27 DATED 01/01/07.

Part: BATTERY BOX — DAMAGED (E&E BAY)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. MAIN BATTERY INSTALLATION STRUCTURE DAMAGED. REPLACED DAMAGED DETAILS OF MAIN BATTERY INSTALLATION STRUCTURE PER MDC DRAWING 9971381 REV Y DATED 0711 3/04 AND DRAWING 5971382 REV P DATED 09/16/02.

Part: FRAME — DAMAGED (BS 133)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LOWER FRAME AT STA 133.4 DAMAGED. REPLACED LOWER FRAME AT STA 133.4 PER MDC DRAWING 9911512 REV T DATED 09-01-99.

Part: SUPPORT — CRACKED (BS 110)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LEFT & RIGHT BUNGEE SUPPORT INSTALLATION AT STA 110.0 RIGHT CRACKED AND BENT BEYOND REPAIR. REPLACED LEFT & RIGHT BUNGEE SUPPORT INSTALLATION AT STA 110.0 RIGHT PER MDC DRAWING 9911599 REV Z DATED 02/03/99.

Part: DOOR FRAME — DAMAGED (ACCESSORY BAY)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. ACCESSORY COMPARTMENT DOOR JAMB DAMAGED. REPLACED ACCESSORY COMPARTMENT DOOR JAMB PER MDC DRAWING 5910343 REV AL DATED 01/24/06.

Part: WEB — CRACKED (NLG)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. NLG LEFT AND RIGHT SUPPORT WEB CRACKED AND BENT BEYOND REPAIR. REPLACED NLG LEFT AND RIGHT SUPPORT WEB AND DETAILS PER MDC DRAWING 9910088 REV CJ DATED 01/24/06.

Part: DOOR FRAME — DENTED (NLG)

AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. NLG FWD DOOR JAMB DENTED AND BENT BEYOND REPAIR. REPLACED NLG FWD DOOR JAMB PER MDC DRAWINGS 5912852 REV B DATED 06/27/81.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

SEAT 31D E PATH LIGHTS WILL NOT ILLUMINATE. SECURED LOOSE FLOOR TRACK TO SEAT HARNESS CONNECTOR AS REQUIRED. OPS CHECK GOOD.

Part: SKIN — DENTED (BS 237)

FUSELAGE SKIN HAS A DENT ON LEFT SIDE AT BS 237 NEXT TO CUSP LINE. INSTALLED DOUBLER REPAIR ON LEFT FUSELAGE SKIN AT STA 237 BETWEEN L-17L TO 18L AS PER B717 SRM 53-00-01 FIG 204. MATERIAL USED .032" 2024-T3. SIZE OF REPAIR 6.5 X 5.5 INCHES.

Part: SKIN — DENTED (BS 237)

FUSELAGE SKIN HAS A DENT ON LEFT SIDE AT BS 237 NEXT TO CUSP LINE. INSTALLED DOUBLER REPAIR ON LEFT FUSE SKIN AT STA 237 BETWEEN L-17L TO 18L AS PER B717 SRM 53-00-01 FIG 204. MATERIAL USED .032" 2024T3 SIZE OF REPAIR 6.5 X 5.5 INCH.