N968AT

Part: FRAME — CRACKED (BS 696) · airframe 47,526 hrs · 32,913 cycles

FRAME CRACKED AT BS 696. REPAIRED IAW AMDS CARD 5310-01436-03A.

Part: FRAME — CRACKED (BS 715) · airframe 47,526 hrs · 32,913 cycles

FRAME CRACKED AT BS 715. CONDITION 3, GREATER THAN .125 INCH. REPAIRED IAW AMDS CARD 5310-01436-03A.

Part: DOOR FRAME — CORRODED (AFT CARGO BY) · corrosion level 2 · airframe 47,526 hrs · 32,913 cycles

CORROSION FOUND ON THE AFT CARGO BAY THRESHOLD. SEVERAL PLACES. REPLACED THE DOOR FRAME IAW SRM 53-20-15-2R, PROC 7.

Part: APU — FAILED (APU BAY) · airframe 47,087 hrs · 32,600 cycles

UPON ARRIVAL AT GATE, AS PASSENGERS WERE DEPLANING , F/A NOTIFIED COCKPIT OF SMOKE AND FUMES IN THE CABIN. THE PASSENGERS CONTINUED TO EXIT NORMALLY. MIST SEEMED TO ORIGINATE FROM AFT CABIN AND WORK FORWARD. MAINTENANCE INSPECTED AND FOUND THE APU CAVITY OIL SOAKED. THE APU OIL QUANTITY WAS BELOW THE ADD LEVEL. SERVICED APU OIL AND WHEN STARTING THE APU, THE GEARBOX MADE CLANKING NOISES AND A STEADY STREAM OF OIL AND SLUDGE CAME FROM THE COMPRESSOR DRAIN AND GENERATOR PAD. THE APU GEARBOX CHIP DETECTOR HAS METAL PRESENT INDICATING APU GEARBOX FAILURE. APU WAS REPLACED PER WORKCARD 5352-4013 ON LP #4335907. PERFORMED PACK BURN OUT PER B-717 AMM 21-54-00. REPLACED BOTH COALESCE BAGS PER AMM 21-54-08. NO SMOKE OR FUMES NOTED. REFER TO LP 4335908 FOR VERIFICATION FLIGHT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,555 hrs · 31,467 cycles

FOUND THE OVERWING EMERGENCY LIGHTS INOPERATIVE, ALSO LIGHTS IN MID-CABIN INOPERATIVE. REPLACED THE BATTERY AND CHARGER ASSEMBLY IN AFT CARGO BAY. EMERGENCY LIGHTS CHECKED GOOD. REPLACED THE BATTERY PACK AT BS 1045 AND CABIN LIGHTS NOW CHECKED GOOD IAW AMM 33-51.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,807 hrs · 30,246 cycles

CABIN CEILING EMERGENCY LIGHTS ARE OUT. REPLACED THE POWER SUPPLY AND OPS CHECKED NORMAL IAW AMM 33-51.

Part: CIRCUIT BOARD — BURNED (POWER SUPPLY) · airframe 43,686 hrs · 30,183 cycles

OVERWING EMERGENCY LIGHT BATTERY POWER SUPPLY CIRCUIT BOARD BURNT. REPLACED OVERWING EMERGENCY LIGHT BATTERY POWER SUPPLY PER AMM 33-51-03 OPS CHECK GOOD. AC OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,703 hrs · 30,193 cycles

OVERWING EMERGENCY LIGHT BATTERY PACK INOPERATIVE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,592 hrs · 29,329 cycles

FUSELAGE SKIN CRACKED AT UPPER FASTENER IN FORMER 1152 BETWEEN L2-L3 LT LOCATION MARKED. REMOVED DAMAGE FROM FUSELAGE SKIN CRACKED AND REPAIRED IAW ER/A 549614-14. REPAIR REQUIRES REPETITIVE INSPECTIONS EVERY 3000 FLIGHT CYCLES.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,592 hrs · 29,329 cycles

CRACKS IN FUSELAGE SKIN AROUND RIVET HEAD ABOVE RT PYLON STA 1095.868, JUST ABOVE L14 RT LOCATION MARKED. SKIN CRACKS REMOVED AND REPAIRED IAW ER/A 549613-14 REQUIRES REPETITIVE INSPECTIONS EVERY 3000 FLIGHT CYCLES AFTER REPAIR.

Part: PANEL — DAMAGED (RT WING) · airframe 42,592 hrs · 29,329 cycles

RIGHT WING L/E PANEL 610RB HAS 2 EA ENLARGED SCREW HOLES WITH SURROUNDING CHAFED SURFACES AND 1 EA HOLES HAS TOOLING MARKS. FABRICATED REPAIR DOUBLER FOR 2 ENLARGE HOLES AND TOOLING MARK REPAIR IAW SRM 57-40-01, REPAIR 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,592 hrs · 29,329 cycles

UPPER FUSELAGE, AFT CABIN, STA 1037 FRAME 17R, CRACK, MARKED. REPAIRED CRACKED FRAME AT FS 1037 AT 17R BY REMOVED DAMAGE ON FRAME AND INSTALLING FILLERS, DOUBLERS IAW SRM 53-20-07. REPAIR 1, FIG 201, USING DOUBLERS MADE FROM 7075 T6 .063 AND FILLERS MADE FROM 7075 T6 .050 AND TRIMMED PYLON ANGLE TO ACCESS TRAPPED FASTENERS IAW PRI AND ER/A 549616-14.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,592 hrs · 29,329 cycles

UPPER CABIN RT CUSP WEB, STA 670 IS CRACKED OTBD OF BL 56R TRACK, MARKED. REMOVED DAMAGED CUSP WEB FROM STA 655-756, OTBD OF RBL 44 IAW SRM 51-41-02. INSTALLED REPLACEMENT CUSP WEB FROM STA 655-756, OTBD OF RBL 44 IAW SRM 51-41-02.

Part: SKIN — CORRODED (BS 737-745) · corrosion level 2 · airframe 42,833 hrs · 29,517 cycles

SKIN CORRODED AT BS 737-745 RBL 58. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM ALLOWABLE DAMAGE 1. REPAIRED IAW SRA 549615-14.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,592 hrs · 29,329 cycles

CENTER FLOOR PANEL SUPPORT AT STA 636 IS CRACKED. MARKED, PULLEY CLUSTER AT STA 636 REMOVED IAW SRM 51-41-01, PG 1. INTERCOSTAL REMOVED IAW SRM 51-41-02. MATERIAL VERIFICATION IS 7075-T6 .050 IAW MFG PROPRIETARY DWG 9936580, REV B. ALODINED AND PRIMED IAW SRM 51-22-01. HOLES LOCATED AND DRILLED IAW SRM 51-40-08, PAGE 1, STEP 3. INSTALLED NEW, L BRACKET IAW SRM 51-41-02, PG 1, STEP 4, 51-41-05, PG 1, STEP 3. INSTALLED PULLEY CLUSTER AT STA 636 IAW SRM 51-41-01. ROUTE AND RIG CHECK OK IAW AMM 28-22-24-830-801. FABRICATED L-ANGLE DOUBLER IAW SRM 53-00-00, FIG 201, REPAIR 1, PAGE 202, ITEM 3, TAG 2892.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,592 hrs · 29,329 cycles

CORROSION ALC STA 927 FRAME FORMER, BETWEEN STA 30 AND 29L FWD AND AFT. BLEND, CHECK LIMITS, REPAIR AS REQUIRED. BLENDED CORROSION AT STA 927, LONGERON 30-29L, LOWEST MEASURED THICKNESS WAS .038", FOUND TO BE OUT OF LIMITS. REPAIRED CORRODED FRAME FORMER IAW SRM 53-00-06 REPAIR 2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,592 hrs · 29,329 cycles

RIGHT IB SEAT TRACK HAS NUMEROUS AREAS CORRODED OUT OF LIMITS STA 200-588, RBL22. REPAIRED SEAT TRACKS SECTION RBL 22 BETWEEN STA 200-STA 588 FOR OUT OF LIMITS DUE TO CORROSION BLENDING WORK ACCOMPLISHED IAW SRM 53-20-52, REPAIR 5.

Part: STRUCTURE — WORN (NR 2 ENGINE) · airframe 42,592 hrs · 29,329 cycles

THE NR 2 ENGINE UPPER COWLING PRECOOLER OUTLET INTERNAL CONTACT SURFACE IS WORN. BLEND, CHECK LIMITS. BLENDED WORN AREA IAW SRM 54-20-00 FIG 101, .038 REMAINING FROM ORIGINAL .050, FOUND TO BE OUT OF LIMITS IAW SRM 54-20-00, FIG 101, GAUGE 6784. REPAIRED AREA IAW SRM 54-00-00, REPAIR 2, 2024-T3-.050, TAG 1681144.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,592 hrs · 29,329 cycles

LEFT CUSP WEB OTBD LIGHTNING HOLE IS CRACKED AT STA 360. REMOVED LT OTBD SEAT TRACK FROM STA 200 TO STA 445. REPAIRED CUSP WEB IAW SRM 53-00-55, REPAIR 4 AND REINSTALLED SEAT TRACK IAW SRM 51-41-01, PAR 6.

Part: PAN — CORRODED (FWD CARGO DOOR) · corrosion level 2 · airframe 42,592 hrs · 29,329 cycles

MULTIPLE SPOTS OF CORROSION ON FORWARD CARGO DOOR PAN. CLEANED UP CORROSION IAW SRM 53-00-00 FIG 103. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103). REPLACED THE PAN IAW SRM 51-41-02 SEC 4 AND 51-41-09.

Part: FLOOR PANEL — DAMAGED (UPPER CABIN) · airframe 42,592 hrs · 29,329 cycles

UPPER CABIN FLOOR PANEL 221CF AT BS 465, LBL 22 HAS DAMAGE ON UPPER SURFACE. FABRICATED A NEW FLOOR PANEL IAW SRM 53-20-50 REPAIR 3 AND INSTALLED.

Part: SHEAR TIE — CRACKED (BS 1022) · airframe 42,592 hrs · 29,329 cycles

SHEAR TIE CRACKED AT BS 1022 LONGERON 6R. REPLACED THE SHEAR TIE IAW SRM 53-20-07 AND DWG 9912243 AND SRM 51-41-05 PG 1.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 42,592 hrs · 29,329 cycles

PASSENGER CABIN FLOOR PANEL 222GF DELAMINATING. FABRICATED FLOOR PANEL IAW SRM 53-20-50 3 AND INSTALLED.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 42,592 hrs · 29,329 cycles

PASSENGER CABIN FLOOR PANEL 223FF IS DELAMINATING. FABRICATED A NEW FLOOR PANEL IAW SRM 53-20-50, AND INSTALLED.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 42,592 hrs · 29,329 cycles

PASSENGER CABIN FLOOR PANEL 222DF DELAMINATING. FABRICATED A NEW FLOOR PANEL IAW SRM 53-20-50 REPAIR 3 AND INSTALLED.

Part: BULKHEAD — CRACKED · airframe 42,592 hrs · 29,329 cycles

ENGINE PYLON SUPPORT BULKHEAD ON THE RIGHT SIDE AT LONGERON 7R IS CRACKED. REPAIRED BULKHEAD IAW SRM 53-20-07 REPAIR 1.

Part: FLOORBEAM — CORRODED (BS 135) · corrosion level 2 · airframe 42,592 hrs · 29,329 cycles

FLOORBEAM BS 135 R RBL 40 - 50 CORRODED. REPLACED THE FLOORBEAM IAW DWN S00074 AND SRM 51-41-02.

Part: PANEL — CRACKED (ELEVATOR) · airframe 42,592 hrs · 29,329 cycles

ELEVATOR LOWER SURFACE RT PANEL 340 KB IS CRACKED. THE PANEL IS ON THE UPPER TAIL DOCK. FABRICATED NEW PANEL 340KB IAW SRM 51-20-09 AND DWG NR 5910412, REV 05. PANEL 340KB TO BE INSTALLED ON JC 2040-0030.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 42,592 hrs · 29,329 cycles

SEAT TRACK CORRODED. FOUND BEYOND LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-01 PAR 6.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 42,592 hrs · 29,329 cycles

LEFT WING ACCESS PANEL 520GB CRACKED. REPLACED THE ACCESS PANEL IAW AMM 28-00-00-410.

Part: SEAT TRACK — DAMAGED (BS 520-598) · airframe 42,592 hrs · 29,329 cycles

UPPER CABIN SEAT TRACK LBL 22, BS 520 - 598 HAS TWO AREAS OF EXPOSED METAL. REPLACED THE SECTION OF SEAT TRACK IAW SRM 53-20-52 REPAIR 5. FABRICATED THE NEW SECTION IAW SRM 53-20-05 REPAIR 5.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 42,592 hrs · 29,329 cycles

LEFT WING ACCESS PANEL 520DB CRACKED. REPLACED THE ACCESS PANEL IAW AMM 28-00-00 410.

Part: PAN — GOUGED (CARGO DOOR) · airframe 42,592 hrs · 29,329 cycles

FORWARD CARGO DOOR PAN GOUGED ABOVE FORWARD DOOR HOLD OPEN HOOK. CLEANED UP GOUGES ON FORWARD CARGO DOOR PAN ABOVE FORWARD DOOR HOLD OPEN HOOK IAW SRM 52-00-00, FIG 103, 52-30-02, PG 1. REMOVED .014 OF .050 BEYOND ALLOWABLE LIMITS, TAG 2721. REPAIRED DOOR PAN IAW SRM 52-30-02, FIG 201, REPAIR 5.

Part: WIRE — BURNED · airframe 38,637 hrs · 26,134 cycles

DURING TAXI, RT ENGINE WOULD NOT SHUTDOWN. CIRCUIT BREAKER FOR RT ENGINE FUEL SWITCH TRIPPED. MAINTENANCE FOUND WIRES SHORTED RT SIDE OF ATC TRANSPONDER NR 1 AND FOUND BURNED WIRES ON TOP OF ATC NR 1. INSPECTED WIRES IAW SWPM 20-10-01, WIRES THAT ARE OUT OF LIMITS ARE N5201-1010-12A, N5201-1011-12B, N5201-1015-20, N5201-202-22. SPLICED WIRES N5201-1010-12A, N5201-1011-12B, N5201-1015-20 & N5201-202-22. RESET BREAKERS AND CHECKS NORMAL. REPLACED NR1 ATC TRANSPONDER IAW AMM 34-54-02 AND OPS WAS NORMAL. TIED AND ROUTED WIRE BUNDLE N5201. ENGINE RUNS NR 1 & NR 2 WERE NORMAL IAW AMM 71-00-04.

Part: CUSP WEB — CRACKED (BS 655) · airframe 38,545 hrs · 26,054 cycles

FORWARD CARGO BAY BS 655, RBL 54 AFT SIDE OF FRAME, CUSP WEB CRACKED. REPAIRED IAW SRM 53-00-55, REPAIR 4.

Part: COVER — CRACKED (EXIT SIGN) · airframe 37,729 hrs · 25,387 cycles

R1 DOOR EXIT SIGN COVER CRACKED. REMOVED COVER IAW AMM.

Part: LIGHT — CRACKED (CABIN) · airframe 37,729 hrs · 25,387 cycles

R1 DOOR EXIT SIGN MOUNTING LIGHT ASSEMBLY CRACKED. R & R LIGHT ASSEMBLY IAW AMM.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 37,729 hrs · 25,387 cycles

FORWARD EMER FLASHLIGHT MISSING. INSTALLED FLASHLIGHT IAW AMM.

Part: PANEL — CRACKED (CARGO BAY) · airframe 37,729 hrs · 25,387 cycles

SIDEWALL PANEL FWD PIT LT SIDE ACROSS FROM DOOR CRACKED IN LINER OVER FRAME. REPAIRED PANEL IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,314 hrs · 25,122 cycles

LEFT MAIN ENTRANCE EMER LIGHT FAILED AT BS 180. REMOVED & INSTALLED BATTERY PACK IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,314 hrs · 25,122 cycles

FORWARD OVERWING EXIT DOOR SIGN BATTERY INOPERATIVE. R & R BATTERY IAW AMM.

Part: WEB — CRACKED (LT WING) · airframe 37,314 hrs · 25,122 cycles

LEFT WING OTBD TE WEB JUST FWD OF AILERON CRACKED. R & R WEB IAW AMM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 37,314 hrs · 25,122 cycles

FORWARD CARGO COMPARTMENT SIDE WALL SUPPORT STRAP CRACKED AT BS 237, LBL 35. R & R STRAP IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 37,860 hrs · 25,476 cycles

AFT CARGO DOOR CUT OUT LOWER SKIN EDGE CORRODED BETWEEN SKIN LAYERS. REPAIRED SKIN IAW SRM.

Part: ATTACH FITTING — CRACKED (LT WING) · airframe 37,314 hrs · 25,122 cycles

LEFT WING OTBD AILERON ATTACH FITTING CRACKED. R & R FITTING IAW SRM.

Part: SKIN — CRACKED (ELEVATOR TAB) · airframe 37,314 hrs · 25,122 cycles

RIGHT ELEVATOR GEARED TAB LOWER SURFACE SKIN CRACKED AT INBD EDGE. REPAIRED TAB IAW AT EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,314 hrs · 25,122 cycles

SHEAR TIE CRACKED AT BS 1116, LONGERON 15L. R & R SHEAR TIE IAW DWG.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 36,937 hrs · 24,887 cycles

SKIN PANEL DOUBLER CORRODED BETWEEN BS 636 TO BS 655, BETWEEN LONGERON 29L TO LONGERON 29R. R & R DOUBLER IAW DRAWING & SRM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 34,941 hrs · 23,596 cycles

EMERGENCY LIGHTS ON COCKPIT OVERHEAD INOPERATIVE. RECONNECTED CONNECTOR IAW MM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

LONGERON CORRODED BETWEEN STATION 898 TO STATION 954, LONG 29L. R & R LONGERON IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

INTERCOSTAL CORRODED BETWEEN STATION 946 TO STATION 954, LONGERON 29R. R & R INTERCOSTAL IAW DRAWING.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 34,941 hrs · 23,596 cycles

MAIN CABIN FLOOR PANEL 221 XF CORRODED BETWEEN STATION 313 TO 389, RBL 44. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 34,941 hrs · 23,596 cycles

MAIN CABIN FLOOR PANEL 222 EF CORRODED BETWEEN STATION 389 TO STATION 465, RBL 44. R & R PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 34,941 hrs · 23,596 cycles

MAIN CABIN FLOOR PANEL 221 SF CORRODED BETWEEN STATION 256 TO STATION 313, RBL 44. R & R PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 34,941 hrs · 23,596 cycles

MAIN CABIN FLOOR PANEL 222 MF CORRODED BETWEEN STATION 465 TO STATION 541, RBL 44. R & R PANEL IAW SRM.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 34,941 hrs · 23,596 cycles

AFT CARGO DOOR CRACKED ON ANGLE AT AFT LATCH ASSEMBLY. REPAIRED DOUBLER IAW SRM.

Part: SUPPORT — CRACKED (VERTICAL STAB) · airframe 34,941 hrs · 23,596 cycles

FWD LOWER VERTICAL STABILIZER LE INTERNAL SUPPORT CRACKED AT STATION 113. R & R STRAP IAW SRM & DRAWING.

Part: WIRE — BROKEN (CABIN) · airframe 34,941 hrs · 23,596 cycles

RT EMERGENCY WIRE BROKEN ON FIRST CEILING PANEL AFT OF FORWARD LAVATORY PANEL 221HC. REPAIRED WIRE IAW SWPM & AMM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

FORMER CRACKED AT BS 1037, BETWEEN LONGERON 17R TO LONGERON 16R. REPAIRED FORMER IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

FORMER CRACKED AT BS 1022, BETWEEN LONGERON 13R TO LONGERON 14R. REPAIRED FORMER IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

FLOOR SUPPORT CORRODED AT BS 200, BETWEEN RBL 22 TO RBL 44. R & R SUPPORT IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,941 hrs · 23,596 cycles

MAIN CABIN BS 541-636 FLOOR PANEL 222RF DELAMINATED. R &R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 34,941 hrs · 23,596 cycles

MAIN CABIN FLOOR PANEL 222AGF DELAMINATED BETWEEN BS 737 TO BS 813. R & R FLOOR BOARD IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,941 hrs · 23,596 cycles

MAIN CABIN FLOOR PANEL 222 ABF DELAMINATED BETWEEN STATION 674 TO STATION 696. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,941 hrs · 23,596 cycles

MAIN CABIN FLOOR PANEL 222AAF DELAMINATED BETWEEN STATION 674 TO STATION 696. R & R PANEL IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,087 hrs · 24,332 cycles

FRAME CORRODED AT STATION 889, STRINGER 30R. REPAIRED FRAME IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,941 hrs · 23,596 cycles

MAIN CABIN BETWEEN BS 465 TO BS 541 FLOOR PANEL 222TF DELAMINATED. R & R PANEL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

FRAME CRACKED AT STATION 889, LONGERON 30. R & R FRAME IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,941 hrs · 23,596 cycles

MAIN CABIN FLOOR PANEL DELAMINATED BETWEEN STATION 889 TO STATION 954. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 34,941 hrs · 23,596 cycles

MAIN CABIN FLOOR PANEL 222DF DELAMINATED BETWEEN BS 954 TO BS 973. R & R FLOOR BOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 34,941 hrs · 23,596 cycles

MAIN CABIN BETWEEN BS 696 TO BS 737 FLOOR PANEL 222ACF DELAMINATED. R & R FLOOR BOARD IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,941 hrs · 23,596 cycles

MAIN CABIN FLOOR PANEL 222 FF DELAMINATED BETWEEN STATION 408 TO STATION 446. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 34,941 hrs · 23,596 cycles

MAIN CABIN FLOOR PANEL 222AHF DELAMINATED BETWEEN BS 737 TO BS 813. R & R FLOOR BOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 34,941 hrs · 23,596 cycles

MAIN CABIN FLOOR PANEL 222AEF DELAMINATED BETWEEN BS 696 TO BS 737. R & R FLOOR BOARD IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

SEAT TRACK CORRODED BETWEEN BS 645 TO BS 825 LBL 44. R & R SEAT TRACK IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

UNDER WING BARREL KEEL BEAM AREA, BS 715 RT SIDE CANTED KEEL AREA OTBD END OF FORMER CRACKED. R & R FORMER IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

UNDER WING BARREL KEEL BEAM AREA, BS 696 LT SIDE CANTED KEEL AREA OTBD END OF FORMER CRACKED. R & R FORMER IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,087 hrs · 24,332 cycles

FRAME CORRODED AT STATION 870. REPAIRED FRAME IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

SEAT TRACKS CORRODED BETWEEN BS 237 TO BS 589 RBL 22. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

SEAT TRACK CORRODED BETWEEN BS 589 TO BS 645. R & R SEAT TRACK IAW SRM.

Part: ATTACH ANGLE — CRACKED (CARGO BAY) · airframe 34,941 hrs · 23,596 cycles

AFT LOWER CARGO COMPARTMENT FWD BULKHEAD RT LINER ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: FORMER — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

LT UNDER WING BARREL KEEL BEAM AREA, BS 674 CANTED KEEL AREA OTBD END OF FORMER CRACKED. R & R FORMER IAW SRM & DRAWING.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 34,941 hrs · 23,596 cycles

LT VERTICAL STABILIZER SKIN CRACKED AT ACCESS PANEL 370BL. REPAIRED SKIN IAW SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

AFT BULKHEAD CORRODED AT STATION 1053, BETWEEN STRINGER 29L TO STRINGER 28R. R & R WEB IAW SRM & DRAWING.

Part: FORMER — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

RT UNDER WING BARREL KEEL BEAM AREA, BS 674 CANTED KEEL AREA OTBD END OF FORMER CRACKED. REPAIRED FORMER IAW SRM & DRAWING.

Part: FORMER — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

UNDER WING BARREL KEEL BEAM AREA, BS 696 RT SIDE CANTED KEEL AREA OTBD END OF FORMER CRACKED. R & R FORMER IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

UNDER WING BARREL KEEL BEAM AREA, BS 715 LT SIDE CANTED KEEL AREA OTBD END OF FORMER CRACKED. R & R FORMER IAW SRM & DRAWING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

SEAT TRACK CORRODED BETWEEN BS 645 TO BS 825, RBL 22. R & R SEAT TRACK IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

FRAME CORRODED AT STATION 870, BETWEEN LONGERON 28L TO LONGERON 28R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

LT SIDE OF EMPENNAGE CRACKED UPPER ANGLE INSIDE PANEL AT FS 1250, LONGERON 7L. R & R ANGLE IAW SRM & DRAWING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 237 TO BS 589, RBL 44. R & R SEAT TRACK IAW MM & SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

AFT BULKHEAD ANGLE CRACKED AT STATION 1053, BELOW STRINGER 18R. R &R SHEAR TIE IAW SRM & DRAWING.

Part: ATTACH ANGLE — CRACKED (CARGO BAY) · airframe 34,941 hrs · 23,596 cycles

AFT LOWER CARGO COMPARTMENT FWD BULKHEAD LINER ATTACH ANGLE CRACKED LT SIDE. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

RT CUSP WEB SUPPORT STRAP CORRODED BETWEEN BS 813 TO BS 820. R & R WEB IAW SRM.

Part: DOOR — CRACKED (LT WING) · airframe 34,941 hrs · 23,596 cycles

LT WING LOWER SURFACE INBD BUTTE DOOR CRACKED. R & R IAW DRAWING.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

RT CUSP WEB CORRODED BETWEEN BS 617 TO BS 636. R & R WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

RT CUSP WEB CORRODED BETWEEN BS 446 TO BS 465. REPAIRED WEB IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

AFT ACCESSORY COMPARTMENT AT CANT FRAME 1178 LT SIDE LOUVER SUPPORT BRACKET CRACKED. REPAIRED SUPPORT IAW SRM & DRAWING.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

LT CUSP WEB CORRODED BETWEEN BS 756 TO BS 737. REPAIRED WEB IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

SEAT TRACK VERTICAL FITTING SUPPORT CRACKED AT BS 735 LBL 44. R & R FITTING IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

RT CUSP WEB CORRODED BETWEEN BS 484 TO BS 803. REPAIRED WEB IAW MM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

LT CUSP WEB CORRODED BETWEEN BS 832 TO BS 813. R & R CUSP WEB IAW SRM.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

RT MAIN CABIN WINDOW PAN CRACKED AFT LOWER FLANGE BETWEEN BS 851 TO BS 870. REPAIRED ANGLE IAW DRAWING & SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

LT CUSP WEB CORRODED BETWEEN BS 465 TO BS 446. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

LT CUSP WEB PANEL CRACKED AT BS 655 BETWEEN LBL 44 TO LBL 54. REPAIRED WEB IAW SRM

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

RT CUSP WEB CORRODED BETWEEN BS 522 TO BS 541. R & R CUSP WEB IAW SRM.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

LT MAIN CABIN WINDOW PAN CRACKED AFT LOWER FLANGE BETWEEN BS 889 TO BS 908. REPAIRED ANGLE IAW DRAWING & SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

CUSP WEB CRACKED AT BS 676 RBL 44. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

RT CUSP WEB CORRODED BETWEEN BS 832 TO BS 851. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

RT CUSP WEB CORDED BETWEEN BS 427 TO BS 446. R &R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

LT CUSP WEB CORRODED BETWEEN BS 313 TO BS 294. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

LT CUSP WEB CORRODED BETWEEN BS 408 TO BS 389. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

RT CUSP WEB CORRODED BETWEEN BS 598 TO BS 617. R & R WEB IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

AFT SIDE OF FRAME CLIP CRACKED AT BS 1151, LONGERON 2R. R & R CLIP IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

AFT SIDE OF FRAME CLIP CRACKED AT BS 1151, LONGERON 2L. R &R CLIP IAW SRM & DRAWING.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

LONGERON CRACKED AT BS 1133, LONGERON 2L. REPAIRED LONGERON IAW SRM.

Part: PANEL — CRACKED (RT MLG WW) · airframe 34,941 hrs · 23,596 cycles

RT MLG WW AFT DOOR CUT OUT SHIELD PANEL CRACKED. R & R PANEL IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

LONGERON CRACKED AT BS 1133, LONGERON 2R. REPAIRED LONGERON IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

AFT CARGO, FWD BULKHEAD GILLINER ATTACHMENT STRAP CRACKED. REPAIRED STRAP IAW SRM & DRAWING.

Part: STRAP — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

LT WING TO BODY SUPPORT FAIRING CORRODED AT BS 851 LOWER SECTION. R & R STRAP IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

WING TO BODY SKIN CORRODED BETWEEN STATION 846 TO STATION 863, STRINGER 28L TO STRINGER 28R. R &R SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

RT NLG STRUT DOOR AFT HINGE CUT OUT CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

RT WING TO BODY LOWER SECTION OF SUPPORT FAIRING CORRODED AT BS 851. R & R STRAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,941 hrs · 23,596 cycles

LT NLG STRUT DOOR AFT HINGE CUTOUT CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: PIN — MISSING (EVAC SLIDE) · airframe 34,941 hrs · 23,596 cycles

R1 DOOR EMERGENCY EVAC SLIDE SAFETY PIN MISSING. INSTALLED PIN IAW AMM.

Part: SHIELD — CRACKED (RT MLG WW) · airframe 34,941 hrs · 23,596 cycles

RT MLG WW SURROUND STRUCTURE FRAME SHIELD CRACKED. REPAIRED SHIELD IAW EA.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 35,872 hrs · 24,196 cycles

FWD LOWER FLASHLIGHT INOPERATIVE. R&R BATTERY PACK IAW AMM.

Part: FIRE LOOP — FAULTY (E&E BAY) · airframe 35,384 hrs · 23,884 cycles

FIRE DETECTION LIGHT FAIL ILLUMINATED. R&R LOOP ASSEMBLY IAW MM.

Part: SIGN — MISSING (CABIN) · airframe 35,073 hrs · 23,688 cycles

EMERGENCY EXIT SIGN IN CEILING AT ROW 1 MISSING. INSTALLED SIGN PER AMM.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE) · airframe 34,620 hrs · 23,408 cycles

R1 DOOR EMERGENCY EVAC SLIDE LANYARD OUT OF POSITION. REPOSITIONED LANYARD PER AMM.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE) · airframe 34,620 hrs · 23,408 cycles

L1 DOOR EMERGENCY EVAC SLIDE LANYARD OUT OF POSITION. REPOSITIONED LANYARD PER AMM.

Part: ATTACH ANGLE — CRACKED (TE FLAP) · airframe 34,270 hrs · 23,191 cycles

LEFT WING NR 2 FLAP TRACK FWD FAIRING FWD ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW BAC DWG & SRM.

Part: BRACKET — BROKEN (R1 DOOR) · airframe 34,533 hrs · 23,358 cycles

R1 DOOR GIRT BAR STORAGE BRACKET BROKEN. REMOVED AND REPLACED COVER ASSY PER AMM.

Part: LANYARD — LOOSE (EVAC SLIDE) · airframe 34,419 hrs · 23,289 cycles

R1 DOOR EMERGENCY SLIDE LANYARD LOOSE. R-EINSTALLED R1 SLIDE LANYARD PER AMM.

Part: AILERON — DELAMINATED (RT WING) · airframe 33,655 hrs · 22,805 cycles

RIGHT WING OUTBOARD PORTION OF AILERON T/E DELAMINATED. REPAIRED AILERON PER MM.

Part: LANYARD — FRAYED (R2 DOOR) · airframe 33,116 hrs · 22,444 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR LANYARD FRAYED. REMOVED AND REPLACED LANYARD IAW AMM.

Part: SLIDE — UNSERVICEABLE (R1 DOOR)

R1 SLIDE PACK PRESSURE INDICATES OUTSIDE THE GREEN BAND. REMOVED AND REPLACED R1 DOOR SLIDE. REF B717 AMM 25-61.

Part: SLIDE — UNSERVICEABLE (TAILCONE)

TAIL CONE SLIDE UNABLE TO READ GAUGE. REMOVED AND REPLACED TAIL CONE SLIDE IAW B717 AMM 25-61-02.

Part: SLIDE — OUT OF POSITION (L1 DOOR)

L1 SLIDE PACK FELL TO JETWAY AS DOOR CAME OPENED. REMOVED & REPLACED L-1 SLIDE ASSY IAW MM 25-61.

Part: GUST LOCK — DIRTY (L1 DOOR)

L-1 DOOR GIRT BAR WILL NOT STAY LATCHED. REMOVED AND CLEANED GUST LOCK AND OPS CHECKED GOOD PER B717 AMM 25-61.

Part: SEAT TRACK — CORRODED (FUSELAGE)

MAIN CABIN RT INBOARD SEAT TRACK, STA 195 TO 200, CORROSION. ACCOMPLISHED SEAT TRACK REPLACEMENT PER B717 SRM 51-10-04, 53-00-00, 51-40-00, 51-30-08 AND 53-21-01 AND BOEING DWG SR09530095.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD GALLEY SERVICE DOOR JAMB FLOOR SUPPORT ANGLE, STA 195, RBL 58, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 53-00-00 AND 51-41-01 AND BOEING DWG SR09936534.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CLIP NUT HOLES, MAIN CABIN FLOOR SUPPORT, STA 195, RBL 9 TO RBL 48, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04 AND 51-22-01 AND BOEING DWG SR09936534.

Part: ANGLE — CRACKED (LT MLG DOOR)

LEFT MLG DOOR O/B FORWARD BODY ANGLE, CRACKED. ACCOMPLISHED BODY ANGLE DOUBLER REPAIR PER B717 SRM 52-82-02 AND 51-10-04 AND TRA 17-52-TR00139.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 195, LBL 5 TO RBL 5, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND 53-00-00 AND BOEING DWG SR09936534.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD GALLEY SERVICE DOOR JAMB FLOOR SUPPORT ANGLE, STA 157 TO 195, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-10-04, 51-41-02 AND 51-22-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CLIP NUT HOLES, MAIN CABIN FLOOR SUPPORT, STA 177, RBL 9 TO RBL 41, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND 53-00-00 AND BOEING DWG SR09936535.

Part: PAN — CORRODED (FUSELAGE)

FWD CARGO LOWER AFT DOOR JAMB PAN, CORROSION. ACCOMPLISHED DOOR JAMB PAN REPLACEMENT PER B717 SRM 53-20-15.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CLIP NUT HOLES, MAIN CABIN FLOOR SUPPORT, STA 157 TO 190, RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND 53-00-01 AND BOEING DWG SR09936536.

Part: ANGLE — CRACKED (RT MLG DOOR)

RIGHT MLG DOOR O/B FORWARD BODY ANGLE, CRACKED. ACCOMPLISHED BODY ANGLE DOUBLER REPAIR PER B717 SRM 52-82-03 AND 51-10-04 AND TRA 17-52-TR00139.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 192, LBL 13 TO LBL 40, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00 AND 51-42-02 AND BOEING DWG SR09936534.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 167 TO 195, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02 AND BOEING DWG SR09936534.

Part: STRUCTURE — CORRODED (GALLEY)

GALLEY COFFEEMAKER COMPARTMENTS 102, 103 AND 106 LOWER SURFACE, CORROSION. ACCOMPLISHED LOWER SURFACE REPLACEMENT PER B717 SRM 51-40-00, 51-40-02, 51-41-02, 51-20-05 AND EA 17-25-03115IR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 167 TO 195, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 157 TO 190, LBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00 AND B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 195 TO 255, LBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND BOEING DWG SR09936534.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 237, LBL 13 TO RBL 13, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 51-4105 AND BOEING DWG SR09936534.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 195, LBL 13, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND 51-30-08 AND BOEING DWG SR09936534.

Part: WIRE HARNESS — UNSECURE (CABIN)

EMERGENCY LIGHT HARNESS HANGING DOWN IN FRONT OF LIFEVEST POUCH AT SEAT 31D. CORRECTLY SECURED LIGHT HARNESS AT 31D AS REQUIRED.

Part: CIRCUIT BREAKER — POPPED (CABIN)

CIRCUIT BREAKERS B1-41, B1-42 POPPED. (EMERGENCY LIGHTING) PERFORMED CIRCUIT BREAKER RESET. REF MM 20-30. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY. OPS CHECK GOOD REG MM 33-51.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

CEILING EMERGENCY LIGHT IS NOT AT ROW 27 RT. REMOVED AND REPLACED POWER SUPPLY ASSY AT ROW 27 DEF OVERHEAD BIN.

Part: FRAME — CORRODED (FUSELAGE)

SURFACE CORROSION AT CIRCUMFERENTIAL FRAME LONG 29L-29R AFT CARGO BILGE STA 889. INSTALLED CIRCUMFERENTIAL FRAME REPAIR AS REQ LONG 19L-29R REFERENCE B717 SRM 51-10-04 AND 53-20-07.

Part: THRESHOLD — CORRODED (FUSELAGE)

AFT CARGO DOOR JAM THRESHOLD CORRODED BEYOND LIMIT. CUT OUT DAMAGED AREA AND REPLACED PER B717 SRM 53-20-15 REPAIR 7.

Part: FRAME — CRACKED (FUSELAGE)

AFT FUSELAGE COMPARTMENT AT STA 1178.225 BETWEEN LONG 16 AND 17 RIGHT HAND CANTED FRAME CRACK.

Part: FRAME — CRACKED (FUSELAGE)

AFT FUSELAGE COMP AT STA 1178.225 BETWEEN LONG'S 16L AND 17L, CANTED FRAME IS CRACKED. INSTALLED FORMED REPAIR AT CANTED FRAME ON STA 1178.225 LEFT HAND BETWEEN LONG 16 AND 17 PER SRM 51-20-11 FIG 201.

Part: SKIN — DAMAGED (FUSELAGE)

BAGGAGE CART COLLIDED WITH FORWARD CARGO BIN DOOR OPENING; DAMAGED SKIN OF A/C. INSTALLED DOULBER REPAIR AT FWD CARGO BIN DOOR AS PER AIRTRAN RES 06-0048 AND IAW B717 SRM 53-20-15 REPAIR 1. MATERIAL USED: FILLER REPAIR .050.2024-T3 X 1 5/8 X 3.0" AND .090.2024T-3 X 1 5/8 X 3.0", DOUBLER .071 2024-T3 X 16 3/4 X 181 1/4" AND TRIPLER REPAIR .090 2024 T3 X 13 3/8" X 12 1/2", AND INSTALLED FILLER SEAL DEPRESSOR REPAIR IAW RES 06-0048. MATERIAL USED 0.080 2024-T3 X 2.0" X 1.0".

Part: GEARBOX — FAILED (NR 1 ENGINE)

MASTER CAUTION ILLUMINATED. FOLLOW BY A/C YAW AT 33,000. LEFT ENGINE SHUT DOWN (AUTO) SUDDENLY. RED BOXED NUMBERS WERE VISIBLE. OIL PRESSURE AND OIL FILTER LEVEL 2 ALERTS WERE ALSO NOTED. CHECKLIST WERE ACCOMPLISHED FOR ENGINE FAILURE (FIRE BOTTLE WAS NOT DISCHARGED) AND THE A/C LANDED WITH LEFT ENGINE SHUTDOWN, WITH NO FURTHER PROBLEMS. (MX SAID IT WAS GEARBOX FAILURE.) CORRECTIVE ACTION: REMOVED AND REPLACED NR 1 ENGINE.