N773NC

Part: GROUND WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 76,140 hrs · 73,280 cycles

ON SERVICE CHECK, FOUND SEAT ROWS 1-4 EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE FOUND EMERGENCY LIGHT BATTERIES DEAD. REPLACED BATTERIES WITH SPARE ONE. LIGHTS WOULD NOT EXTINGUISH AFTER TEST. FOUND GROUND WIRE PINCHED BETWEEN ROW 1 AND ROW 2. REPAIRED WIRE AND LIGHTS NOW TEST GOOD. AIRCRAFT OK FOR SERVICE.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,140 hrs · 73,280 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEATS 1 THRU 4 AND SERVICE DOOR TO BE INOPERATIVE. MAINTENANCE REPLACED THE FUSE AT THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,105 hrs · 73,236 cycles

WHILE ACCOMPLISHING AD RELATED TASK CARD 5330-01142-02 EDDY CURRENT INSPECTION, FWD PASSENGER DOOR JAMB SKIN CORNERS AND DOOR STOPS SECTION 02 1. CRACK INDICATION ON SKIN WAS DETECTED EMANATING FROM NR 7 DOOR STOP. REMOVED DAMAGE ON DOOR STOP SKIN NR 7 AFT, CUT OUT DIMENSION TO FAB REPAIR DOUBLER AND FILLER, FABRICATED LOCATED AND DRILLED REPAIR. TREATED AND PRIMED REPAIR, FABRICATED ID TAG AND INSTALLED ID TAG ON DOUBLER REPAIR AND CONICAL SPACER WASHERS ON FUSELAGE SKIN FWD PASSENGER NR 7 AFT DOOR STOP.

Part: STRAP — CORRODED (FUSELAGE) · airframe 76,105 hrs · 73,236 cycles

UPON CLEANING OF AREA ON N/R 2 ZONE 1E IN AFT CARGO PIT FOUND STRAP TO BE CORRODED. DOUBLER STRAP WAS REMOVED AND REPLACED PER DC9 SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 76,105 hrs · 73,236 cycles

UPON CLEANING OF AREA ON NR 2 ZONE 1 FOUND AFT CARGO AFT BULKHEAD AREA STA 1167 BL0 T-ANGLE TO HAVE CORROSION. T-ANGLE EXFOLIATED AND CRACKED FOUND TO BE OUT OF LIMITS. REMOVED ON NRC NR 2 ZONE 1E AFT CARGO PIT AFT BULKHEAD AREA STA 1167 BL-0 TEE ANGLE. LOCATED AND DRILLED NEW TEE ANGLE. INSTALLED ON AFT CARGO PIT AFT BULKHEAD AND APPLIED TOP COAT.

Part: CABLE — BINDING (AIRSTAIR) · airframe 75,756 hrs · 72,829 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE CATWALK STUCK IN THE LOWERED POSITION WITH THE AFT AIRSTAIRS LOWERED. ON INSPECTION, MAINTENANCE FOUND THE RIGHT RETRACT CABLE JAMMED. MAINTENANCE REPLACED THE FITTING CRANK ASSEMBLY AND RETRACT CABLE AND RETURNED THE AIRCRAFT TO SERVICE AFTER A SUCCESSFUL FUNCTIONAL CHECK OF THE SYSTEM.

Part: PANEL — DELAMINATED (RT WING) · airframe 73,440 hrs · 70,600 cycles

RT WING T/E FIXED PANEL INBD OF AILERON IS DELAMINATED. APPROX 36 SQ INCHES. R & R PANEL IAW SRM 51-30-01 AND 51-30-2. REPAIRED UPPER T/E SPAR IAW ERA 488339-147. REQUIRED INSP COMPLETED.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 73,440 hrs · 70,600 cycles

MAIN CABIN FLOOR PANEL 19 FASTENER HOLES ELONGATED IN FLOOR PANEL RACK. FABRICATED FLOOR PANEL 19 IAW DOUGLAS DRAWING 9957823 AND ER/A 488722-14. REQUIRED INSPECTION COMPLETED.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 73,440 hrs · 70,600 cycles

MAIN CABIN LT SIDE BETWEEN STA 693-712 BATHTUB FITTING LBL 55 UNDER FLOOR CUSP WEB HAS CORROSION. REMOVED FITTING MATCH DRILLED AND INSTALLED 2EA FREEZE PLUGS ON TRAVELER 2311N01993. INSTALLED FITTING PER ERA 487368-14. REQUIRED INSPECTION COMPLETED.

Part: SKIN — DENTED (FUSELAGE) · airframe 73,440 hrs · 70,600 cycles

FUSELAGE EXTERIOR STA 238 APPROX 3" BELOW L18L SKIN HAS DENT. CUT OUT SECTION OF SKIN 4"X 5"; NO DAMAGE PER NDT SPM 06-10-01. FABRICATED AND INSTALLED NEW SECTION OF SKIN .050 AND FINGER DOUBLERS .025 IAW DC-9 SRM 53-04 FIG 12C P-226. REQUIRED INSPECTION COMPLETED.

Part: WEB — CRACKED (STA 1130 RBL 47) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN STA 1130 RBL 47 REPAIR DOUBLER IS CRACKED. REMOVED DAMAGED DOUBLER IAW SRM 51-30-2, IAW DWG 5609530019 AND SRM 51-10-4. INSTALLED MEMBRANE REPAIR IAW SRM 51-30-2 AND 51-30-5. P-127 REQUIRED INSPECTION COMPLETED.

Part: BULKHEAD — CRACKED (BS 851 RBL 58) · airframe 73,440 hrs · 70,600 cycles

RT MLG, STA 851, BULKHEAD RBL 58, 3 INCHES FROM TOP WEB IS CRACKED. CUT OUT DAMAGE SECTION 2.5" X 3". DAMAGE CONTAINED IAW NDT SPM 06-10-01, .001. FABRICATED AND INSTALLED FILLER .050 DOUBLER .032 AND SPLICE DOUBLER .071 IAW ERA 488374-14, P-226, Q-953, 186938. REQUIRED INSP COMPLETED.

Part: PAN — DAMAGED (BS 427) · airframe 73,440 hrs · 70,600 cycles

FWD CARGO COMPARTMENT, STA 427, LOWER DOOR PAN SPLICE FASTENER HOLES ELONGATED IN FRAME. GAINED ACCESS IAW SRM51-30-2. REMOVED FRAME IAW SRM 51-30-5 AND 51-30-2. RECEIVED NEW FRAME, INSTALLED AND RESTORED ACCESS IAW DWG 9912453. R & R DOOR PAN IAW SRM 53-05, FIG 44, 51-30-5 AND 51-30-2.P-117 25 JAN 11. REQUIRED INSPECTION COMPLETED.

Part: FRAME — CRACKED (BS 674) · airframe 73,440 hrs · 70,600 cycles

FWD CARGO COMPT STA 674, LONG 29 LT FRAME IS CRACKED. REMOVED DAMAGED FRAME AT STA 674, L25L TO L25R IAW SRM 51-30-05. LOCATED, DRILLED & DEBURRED FRAME IAW SRM 51-10-4. TREATED AND PRIMED NEW FRAME IAW SRM 51-10-3. INSTALLED FRAME IAW SRM 51-30-02 & SRM 51-30-05. REQUIRED INSP COMPLETED.

Part: PAN — CORRODED (CARGO DOOR FRAME) · airframe 73,440 hrs · 70,600 cycles

FWD PIT-CARGO DOOR JAMB PAN HAS CORROSION 375-421 AROUND CORENUTS AND UNDER 2 EA STOP FITTINGS. REMOVED CORROSION .5" X 4" FROM PAN IAW SRM 51-10-3. ORIG MAT .050 IAW SRM 53-13-2, .038. FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1. R & R PAN IAW SRM 53-13-2, 51-30-2, 51-30-5. REQUIRED INSP COMPLETED.

Part: FLOOR SUPPORT — CRACKED (BS 636) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN STA 636, LBL 8, FLOOR SUPPORT CRACKED. REMOVED FLOOR SUPPORT AT STA 636 THAT WAS CRACKED IAW SRM 51-30-5. FORMED, TRIMMED, DRILLED, DEBURRED NEW FLOOR SUPPORT APPLIED ALODINE TREATMENT AND PRIMED IAW SRM 51-10-3. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-30-5. REQUIRED INSPECTION COMPLETED.

Part: CUSP WEB — CRACKED (BS 229) · airframe 73,440 hrs · 70,600 cycles

MAIN PAX CABIN RT SIDE CUSP WEB HAS 1 EA CRACK AND ELONGATED HOLES UNDERNEATH OF OTBD SEAT TRACK AT STA 229, RBL 46. REMOVED DAMAGED CUSP WEB. FABRICATED NEW CUSP WEB IAW DWG09530019 IAW SRM 53-13-2. CUT OUT ADDITIONAL DAMAGE AT STA 237. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-10-4, 51-30-2 & 3 RP DC9-A-53-10-16-801-663A-A IAW SRM 51-30-2 AND SRP. REQUIRED INSPECTION COMPLETED.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 73,440 hrs · 47,775 cycles

CABIN FLOOR PANEL NR 29, 1 EA CRACK. 31 IN AFT TOP. FABRICATED NEW PANEL IAW DWG 995720 AND ERA 488344-14, REV ORIG STENCILED AND IDENTIFIED IAW PS 900-5-1, NR4 P-117 25 JAN 11. CORRECTED..

Part: FLOOR PANEL — CRACKED (MAI CABIN) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN PANEL NR61 TOP SKIN CRACKED TRIMMED OUT DAMAGED AREA 3 .2500" X 2.5". FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 53-01, FIG 4 SHEET 1, 51-10-4 AND 51-10-3. REQUIRED INSPECTION COMPLETED.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 73,440 hrs · 70,600 cycles

MAIN CABIN FLOOR PANEL, 30 HOLES BROKE OUT AND ELONGATED IN FLOOR PANEL RACK. FABRICATED NEW NR 30 FLOOR PANEL IAW DWG 9957915. INSTALLED 5 EA HAT CHANNELS IAW SRM 51-30-7. TAGGED REPAIR IAW DPS 900-5-1 AND IAW ERA 488746-14. REQUIRED INSPECTION COMPLETED.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 73,440 hrs · 70,600 cycles

MAIN CABIN FLOOR PANEL NR105 CRACKED TOP SIDE IN FLOOR PANEL RACK. MFG FLOOR PNL NR105 IAW DWG 9915532, REV ORIGINAL AND ER/A 488724-14 REV ORIGINAL. CORRECTED. REQUIRED INSPECTION COMPLETED.

Part: FLOOR PANEL — CORRODED (BS 148-160) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN STA 148-160, FLOOR PANEL 14B HAS CORROSION. MFG FLOOR PNL NR14 IAW DWG 9957826, REV ORIGINAL AND ER/A 488341-14 REV ORIGINAL. STENCILED AND IDENTIFIED PANEL IAW PS 900-5-1, NR 04 P-117 25 JAN 11. REQUIRED INSP COMPLETED.

Part: LONGERON — DAMAGED (STA 674 L29L) · airframe 73,440 hrs · 70,600 cycles

FWD CARGO COMPT STA 674, L29L BOTTOM SIDE OF TOP LEG DAMAGE. REMOVED DAMAGE FROM STA 674, L29L, ORIG MAT .080, LOSS MAT .050, REMAINING .030. FOUND TO BE OUT OF LIMITS IAW SRM 53-01. REMOVED L29 FROM STA 647 TO 698 IAW SRM 51-30-5, 51-30-2,51-30-1. INSTALLED L29L IAW SRM 51-30-5, 51-30-2, 51-30-1. REQUIRED INSPECTION COMPLETED.

Part: FLOOR PANEL — CORRODED (BS 148-160) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN STA 148-160, FLOOR PANEL NR15 HAS CORROSION. MFG FLOOR PANEL NR15 IAW DWG 9957825, REV ORIGINAL AND ER/A 488340-14 REV ORIGINAL. STENCILED AND IDENTIFIED PANEL IAW PS900-5-1, NR 04, P-117. CORRECTED. REQUIRED INSPECTION COMPLETED.

Part: DOOR FRAME — CORRODED (BS 370-427) · airframe 73,440 hrs · 70,600 cycles

FWD CARGO DOOR JAMB WEB STA 370-427 HAS CORROSION AT CORENUTS. REMOVED CORROSION ORG MAT .040. REMOVED .013, REMAINING .027 FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. R & R WEB IAW SRM 51-30-2 AND 51-30-5. REQUIRED INSP COMPLETED.

Part: WEB — CORRODED (FUSELAGE) · airframe 73,440 hrs · 70,600 cycles

DURING M-CK, CORROSION WAS FOUND ON THE WEB AT STA 1108 BETWEEN L24R & L26R. ONCE BLENDED OUT, THE PART DAMAGE WAS OUT OF SRM LIMITS. WORK IAW ER/A 488329-14 AS FOLLOWS: SECT I, SECT II - ON OR BEFORE 3,000 CYCLES AFTER SECTION I, SECT III - WITHIN EVERY 3,000 CYCLES AFTER SECTION II.

Part: FLOOR PANEL — CHAFED (MAIN CABIN) · airframe 73,440 hrs · 70,600 cycles

MAIN CABIN FLOOR PNL 62 FASTENER HOLES ELONGATED, CHAFED AND BROKE OUT. ORIG MATERIAL THICKNESS .025 IAW SRM 53-23-0. MATERIAL LOSS MAXIMUM .009 MATERIAL REMAINING .016 IAW SRM 53-01, FIG 1. RECEIVED MATERIAL FOR WEB AND HAT CHANNEL IAW DWG 9957919. DRILLED WEB AND CHANNELS IAW SRM 51-10-2 AND 51-10-4. INSTALLED LOCATED WEB AND CHANNELS IAW DWG 9957919 & ER/A 488723-14 REV ORIGINAL. REQUIRED INSP COMPLETED BY Q948.

Part: SKIN — DAMAGED (BS 522-541 L24R) · airframe 73,440 hrs · 70,600 cycles

FWD CARGO BS 522-541, L24R, FUSELAGE SKIN HAS 3EA FASTENER HOLES KNIFE EDGED. CUT SECTION OUT FOR SKIN REPAIR STA 516-550. RT STATIC PORT IAW SRM 53-04, FIG 12C FABRICATED NEW SECTION, TREATED & PRIMED IAW SRM 53-04 FIG.12C, 51-10-3 FABRICATED FINGER DOUBLER TREATED & PRIMED IAW SRM 53-04, FIG 12C & 51-10-3. FABRICATED 10EA SPLICES TREATED & PRIMED IAW SRM 53-04, FIG 12C & 51-10-3. INSTALLED DOUBLER SKIN SPLICES IAW SRM 51-30-2, 51-30-5, & 53-04 FIG 12C. REQUIRED INSPECTION COMPLETED.

Part: WEB — CORRODED (BS 1106-1116) · airframe 73,440 hrs · 70,600 cycles

AFT CARGO STA 1106 TO 1116 BETWEEN L24R AND L26R WEB HAS CORROSION. REPAIRED WEB IAW ERA 488337-14 WEIGHT OF DOUBLER IAW 30-10-7 IS 63 GRAMS TOOL NR 9513 INSTALLED & EDGE SEALED, ID TAG IAW DPS 900-5-1. CUTOUT DAMAGE 7." X 15.5 CORRECTED BY LOVE 490448. REQUIRED INSPECTION COMPLETED.

Part: ATTACH ANGLE — CRACKED (NR 2 NACELLE) · airframe 73,440 hrs · 70,600 cycles

NR 2 ENG PYLON FWD LOWER ATTACH ANGLE FOR PANEL 8220NW HAS APPROX 1 IN CRACK AT FWD END. REMOVED & FABRICATED NEW ANGLE IAW SRM 54-04, FIG 10 PRIMED IAW SRM 51-10-3 INSTALLED IAW SRM 51-30-5 & 54-04 FIG 10 & 51-30-2. REQUIRED INSP COMPLETED.

Part: THRESHOLD — DAMAGED (FS 427-370) · airframe 73,440 hrs · 47,775 cycles

FWD CARGO COMPARTMENT FS 427 TO 370 STEEL THRESHOLD HAS 31EA (PREVIOUS REPAIR) DRILLED OUT HOLES. REMOVED THRESHOLD & CLIP. RECEIVED NEW PART. LOCATED AND INSTALLED IAW SRM51-10-4-51-30-2 AND 51-30-5, 53-13, 53-05. REQUIRED INSPECTION COMPLETED.

Part: LONGERON — DAMAGED (BS 522-541 L24R) · airframe 73,440 hrs · 70,600 cycles

FWD CARGO COMPT BETWEEN STA 522-541 RT SIDE LONGERON 24 HAS 2EA CUTOUTS IN TOP LEG OF LONGERON. REMOVED SECTION OF LONGERON 24 RT SIDE FROM STA 491 TO STA 569. NDT NO CRACKS NOTED. REPLACED WITH NEW SECTION OF LONGERON LOCATED, DRILL AND INSTALLED IAW SRM 53-02, FIG 18, 51-30-02, 51-30-05, 51-10-3, 51-10-01, 51-10-4, 51-10-02. NDT SPM 06-10-01.001. REQUIRED INSPECTION COMPLETED.

Part: FLOOR SUPPORT — CORRODED (STA 1151-1167) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN BETWEEN STA 1151-1167, RBL 18 FLOOR SUPPORT CORRODED. REMOVED CORROSION AND FABRICATED NEW SUPPORT. HEAT TREATED ON TRAVELER 2311NO2233. INSTALLED SUPPORT IAW SRM 51-30-1 AND 51-01,P-226, REQUIRED INSPECTION COMPLETED.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 73,440 hrs · 70,600 cycles

CABIN FLOOR PANEL NR 75 CRACKED AND PUNCTURED AT AFT INBD SIDE. CUT OUT DAMAGE 2EA PLACES 1" X 2". NO DEFECTS IAW NDT SPM 06-10-01. FABRICATED AND REINSTALLED 2EA FILLERS AND 1EA DOUBLER FROM .025, 7075-T6 PO 1120034 IAW SRM 53-01, FIG 4, SHEET 4.

Part: INTERCOSTAL — DAMAGED (DOOR FRAME) · airframe 73,440 hrs · 47,775 cycles

FWD CARGO DOOR JAMB, 5 EA INTERCOSTALS HOLES ELONGATED. REMOVED AND INSTALLED (5EA) INTERCOSTALS IAW SRM 51-30-05. REQUIRED INSPECTION COMPLETED.

Part: FLOOR SUPPORT — DAMAGED (STA 1151-1167) · airframe 73,440 hrs · 70,600 cycles

DURING REPAIR ON SUPPORT STA 1151-1167, RBL 18, NR 6C/230, FOUND SUPPORT CHANNEL WITH MULTIPLE DOUBLE DRILLED HOLES AND ELONGATED HOLES. FABRICATED NEW SUPPORT FROM .050. HEAT TREATED ON TRAVELER 2311 NR 02266. INSTALLED SUPPORT IAW SRM 51-01 AND 51-30-1.P-226. REQUIRED INSPECTION COMPLETED BY Q-987 284650.

Part: FRAME — CRACKED (BS 1136) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN STA 1136 OTBD BETWEEN LONGERON FRAME CLIP IS CRACKED. R & R FRAME CLIPS IAW SRM51-30-5. REMOVED AND INSTALLED FASTENERS FOR ACCESS IAW SRM 51-30-5. CLEANED UP MINOR SCRATCHES ON SURROUNDING AREA IAW SRM 53-01 & SRM 51-10-3 AND FABRICATED & INSTALLED NEW ATTACHING SPRING CLIP IAW DWG35911427 AND ANGLE IAW DWG 9957739-121. REQUIRED INSP COMPLETED.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 73,440 hrs · 70,600 cycles

AFT ACCESORY COMPARTMENT STA 1258 VERTICAL STAB. RT SIDE FITTING CRACKED. RECEIVED NEW FITTING IAW TRAVELER 2311NO21922, OK TO TREAT HOLES. TREATED AND PRIMED HOLES IAW SRM 51-10-3. INSTALLED NEW FITTING IAW SRM 51-30-1 AND SRM 51-30-5. REQUIRED INSPECTION COMPLETED.

Part: DOUBLER — CRACKED (BS 237 LBL 55) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN STA 237, LBL 55 DOUBLER CRACKED. GAINED ACCESS & REMOVED EXISTING PREVIOUSLY REPAIRED CUSP WEB AT FS218 TO 237, LBL 44-55 IAW SRM 51-10-4,51-30-2 & 51-30-5. FABRICATED NEW WEB IAW DWG 9910699 REV M IAW SRM 51-10-2 & 51-10-4. HFEC INSP IAW NDT SPM 06-10-01.001. NO CRACKS NOTED. INSTALLED NEW WEB & RESTORED AREA IAW SRM 51-30-2 & 51-30-5. REQUIRED INSP COMPLETED.

Part: INTERCOSTAL — CRACKED (BS 712) · airframe 73,440 hrs · 70,600 cycles

LT FWD OVERWING EMERGENCY EXIT DOOR PAN FWD SIDE AT FS712, L12 INTERCOSTAL CLIP IS CRACKED. REMOVED CLIP IAW SRM 51-30-2 AND DWG 5910537-18. FABRICATED AND TRIMMED, PICKED HOLES IAW SRM 51-10-2 AND DWG 5910537-18. INSTALLED NEW CLIP IAW SRM 51-30-05. REQUIRED INSP COMPLETED.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 73,440 hrs · 70,600 cycles

FLOOR PANEL NR 68, 1 EA CRACK ON FASTENER HOLE. REMOVED CRACK IAW SRM 53-01, FIGURE 2. FABRICATED DOUBLER AND FILLER IAW SRM 53-01, FIG 2. INSTALLED DOUBLER AND FILLER IAW SRM 51-30-2. REQUIRED INSP COMPLETED.

Part: BRACE — DAMAGED (BS 218-237) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN BETWEEN STA 218-237, LBL 55, 2EA FASTENERS MISSING IN BRACES. REMOVED REMAINING FASTENERS IAW SRM 51-30-2. FABRICATED RADIUS FILLERS IAW EO 94FS481230. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED FASTENERS, FILLERS, AND BRACES IAW SRM 51-30-5. REQUIRED INSPECTION COMPLETED.

Part: WEB — CHAFED (EMERGENCY EXIT) · airframe 73,440 hrs · 70,600 cycles

RT AFT OVER WING EMERGENCY EXIT ABOVE DOOR LOCK WEB IS CHAFED. CHAFED OUT OF LIMITS. CUT OUT 1" X 2" IAW SRM 09-00-01. FABRICATED AND DRILLED IAW SRM 51-70-4. DAMAGE CONTAINED IAW NDT SPM 06-10-01.001. INSTALLED IAW SRM 51-30-5. REQUIRED INSPECTION COMPLETED.

Part: WEB — CRACKED (BS 712 L12L) · airframe 73,440 hrs · 70,600 cycles

MAIN CABIN-STA 712, L12L CLOSEOUT WEB CRACKED AT TOP FASTENERHOLE. GAINED ACCESS STA 712 CABIN WINDOW NR26. REMOVED FRAME AND DAMAGED CLOSEOUT WEB. LOCATED, DRILLED, DEBURRED, ALODINED. PRIMED AND INSTALLED NEW CLOSEOUT WEB IAW SRM 51-10-2, 51-10-4, 51-30-02 AND 51-30-05. REINSTALLED FRAME AND REINSTALLED ALL ACCESS THAT WAS REMOVED IAW SRM 51-30-02, 51-30-05. LEAK CHECK TO BE ACCOMPLISHED ON CABIN VESSEL LEAK CHECK CARD 2130-8077M. REQUIRED INSP COMPLETED.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 73,440 hrs · 47,775 cycles

MAIN CABIN FLOOR PANEL 21 CORRODED IN FLOOR PANEL RACK. RECEIVED NEW FLOOR PANEL NR 21. TO BE INSTALLED ON JOB CARD 0590-4010-8M. LOCATED AND DRILLED, LOCATED AND DEBURRED FLOORPANEL NR 21 IAW SRM 51-10-4 TO BE INSTALLED ON WORK CARD 2311R68.

Part: FLOOR SUPPORT — CRACKED (STA 313 LBL 1) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN STA 313, LBL 1, FLOOR SUPPORT, Z-ANGLE CRACKED. REMOVED FLOOR SUPPORT IAW SRM 51-30-2. FABRICATED & INSTALLED FLOOR SUPPORT IAW SRM 51-30-5. REQUIRED INSP COMPETED.

Part: ATTACH FITTING — CRACKED (STA 1136) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN STA 1136 OTBD BETWEEN LONG 14-15L, FRAME CLIP IS CRACKED. REMOVED AND INSTALLED NEW FRAME CLIP IAW SRM 51-30-2 AND 51-30-5. RESTORED ACCESS. REQUIRED INSP COMPLETED.

Part: SHEAR TIE — CRACKED (BS 1116 L14) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN STA 1116 BELOW LONG 14 FRAME NEAR TIE IS CRACKED. REMOVED, FABRICATED, & INSTALLED SHEAR TIE IAW SRM 51-30-2, SRM 51-30-5 & DWG 9957739. REQUIRED INSP COMPLETED.

Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 73,440 hrs · 70,600 cycles

PARTS RACK 777B/ MAIN CABIN FLOOR PANEL NR 60C BROKEN AT CORNER AROUND FAST HOLE. REPAIRED PANEL IAW SRM 51-30-2 & SRP A-53-22-01-501-663A-A, REPAIR NR3 SRM 51-90-0, PARA 5 & 6. WORK ACCOMPLISHED ON TRAVELER NR 2269.

Part: STRUCTURE — CRACKED (BS 1151-1167) · airframe 73,440 hrs · 70,600 cycles

LAVATORY AREA BETWEEN STA 1151-1167, RT SIDE BETWEEN LONG 14 AND 16 SKIN IS CRACKED. REMOVED EXISTING DOUBLER. CUT OUT DAMAGED SECTION AND NDT FOR CRACK CONTAINMENT. NO CRACKS NOTED IAW NDT SPM 06-10-01.001. FABRICATED AND INSTALLED NEW REPAIR IAW SRM 53-04, FIG 41. REQUIRED INSP COMPLETED.

Part: STOP FITTING — CRACKED (LAV DOOR) · airframe 73,440 hrs · 70,600 cycles

LAVATORY AREA RT SIDE CTR DOOR STOP FITTING IS CRACKED. R & R FITTING. R & R 2 EA STRIPS IAW SRM 51-30-5.

Part: SUPPORT CHANNEL — CRACKED (BS 106 L28R) · airframe 73,440 hrs · 70,600 cycles

NLG STA 106, R28L SUPPORT CHANNEL CRACKED APPROX 1.5 INCHES. REMOVED 6 EA FASTENERS. TRIMMED OUT DAMAGED AREA HFEC INSPECTED NDT SPM 06-10-01.001. FAB & INSTALLED REPAIR ANGLE IAW SRM 51-30-2,51-30-5. REQUIRED INSP COMPLETED.

Part: DOOR — CRACKED (MLG) · airframe 73,440 hrs · 70,600 cycles

RT MLG WHEEL WELL, MAIN GEAR DOOR CRACKED AT FWD UPPER END. R & R RT MLG WHEEL WELL DOOR IAW AMM 32-12-01. REPAIR OF DOOR INITIATED BUT DUE TO TIME CONSTRAINTS DOOR WAS REPLACED. FIT AND FAIR OF DOOR TO BE ACCOMPLISHED ON JOB CARD 3211-7584M-RT P-129 Q-967 000449, CORRECTED.

Part: SKIN — CRACKED (BS 1266 L2-3L) · airframe 73,440 hrs · 70,600 cycles

FUSELAGE EXTERIOR STA 1266, BETWEEN L2L AND L3L SKIN CRACKED. REMOVED DAMAGED SECTION OF SKIN IAW SRM 51-10-4 NDT FORE CRACK REMOVED NO DAMAGE REMAINING IAW 06-10-01-001. FABRICATED & INSTALLED REPAIR DOUBLER IAW SRM 51-30-5, 53-01, FIG 4 SHEET 4. REQUIRED INSPECTION COMPLETED.

Part: DOUBLER — CORRODED (BS 229-279) · airframe 73,440 hrs · 70,600 cycles

CORROSION FOUND ON INTERNAL DOUBLER STA 229 TO 279, LONGERON 19-21. REMOVED CORROSION, OUT OF LIMITS. FABRICATED NEW DOUBLER IAW DWG NR 5911410. MILLED DOUBLER ON TRAVELER 2311NO2287 IAW DWG NR5911410.P-226. REQUIRED INSP COMPLETED.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN FLOOR PANEL NR46 TOP SKIN HAS HOLE. REPAIRED MAIN PASSENGER CABIN FLOOR PANEL NR46 TOP SKIN IAW SRM 51-70-4, FIG 1.E.CASTELLO AP 3107610. REQUIRED INSP COMPLETED.

Part: FLOOR SUPPORT — CORRODED (BS 1167 L24-27R) · airframe 73,440 hrs · 70,600 cycles

AFT CARGO STA 1167, FLOOR SUPPORT ANGLE BETWEEN L24R AND L27R HAS CORROSION SEVERAL PLACES. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 53-01 FIG 1. REMOVED DAMAGED SECTION OF ANGLE. FABRICATED NEW SECTION OF ANGLE INSTALLED NEW ANGLE AND SPLICE IAW SRM 51-30-5. REQUIRED INSP COMPLETED.

Part: SKIN — CRACKED (BS 108 L27R) · airframe 73,440 hrs · 70,600 cycles

FUSELAGE SKIN BS 108, LONGERON 27R EXTERIOR SKIN CRACKED AT FASTENER LOCATION. TRIMMED OUT DAMAGED SKIN NDT VERIFIED NO CRACKS NOTED. LOCATED HOLES PRIMED, DEBURRED, COUNTERSUNK, ALODINED & PRIMED NEW REPAIR DOUBLER & FILLER. INSTALLED REPAIR DOUBLER & FILLER IAW SRM 53-01, FIG 4, PS 900-5-1, NR 4 P. PAZ 073401, P-224 REQUIRED INSP COMPLETED.

Part: CUSP WEB — CRACKED (BS 1135) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN STA 1135 BETWEEN LBL 44-55 CUSP WEB IS CRACKED 2EA PLACES. REMOVED DAMAGED AREA IAW SRM 51-30-2. NDT COMPLETED IAW N/R FORM 6C/247. FABRICATED DOUBLER IAW SRM 51-10-2. INSTALLED DOUBLER IAW SRM 51-30-5. REQUIRED INSPECTION COMPLETED.

Part: CUSP WEB — DAMAGED (BS 674) · airframe 73,440 hrs · 70,600 cycles

MAIN CABIN LT CUSP WEB AT STA 674 HAS A HOLE. CUT OUT DAMAGE IAW DC-9-A-53-10-16-801. NDT VERIFIED DAMAGE CONTAINED IAW NDT SPM 06-10-01.001 H2700. FABRICATED DOUBLER AND FILLER IAW DPS 900-5-1, H9573 1.102. INSTALLED PARTS IAW DC-9-A-53-10-16-801 PART MARKED IAW DPS 900-5-1. REQUIRED INSPECTION COMPLETED.

Part: FLOOR PANEL — CORRODED (BS 218-310 BL 0) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN STA 218-310 BL 0 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 53-01 FIG 1. ORIGINAL THICKNESS .060 IAW SRM 53-13-01, OUT OF LIMITS. FABRICATED FLOOR SUPPORT IAW SRM 51-10-2. FABRICATED & INSTALLED CLIPS IAW SRM 53-05, FIG 1 & INSTALLED FLOOR SUPPORT IAW SRM 51-30-5. P-127 REQUIRED INSPECTION COMPLETED..

Part: SKIN — DAMAGED (BS 256 L22-23L) · airframe 73,440 hrs · 70,600 cycles

FUSELAGE EXTERIOR, STA 256 BETWEEN L22L AND L23L FORMER HAS .2500" HOLE. CUT OUT DAMAGE AREA 4.5 IN BY 1.5 IN FABRICATED & INSTALLED REPAIR ANGLE IAW SRM 53-03, FIG 7, P109 485797 G, FUNK 116102 07JAN11. REQUIRED INSP COMPLETED Q912.

Part: CUSP WEB — CRACKED (1100 LBL 49) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN STA 1100, LBL 49, CUSP WEB IS CRACKED UNDER EXISTING REPAIR. REMOVED EXISTING DOUBLER IAW SRM 51-30-02. STOP DRILLED CRACK IAW SRM 51-01. FABRICATED NEW DOUBLER IAW DC-9 A-53-10-16-801-663A-A, FIG 1. ALODINED & PRIMED IAW SRM 51-10-3. INSTALLED DOUBLER IAW A-53-10-16-801-663A-A, FIG 1. NDT OK IAW SPM 06-10-01.001, NR 1. REQUIRED INSPECTION COMPLETED.

Part: SEAT TRACK — CORRODED (BS 200-285) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN STA 200-285, RBL 44, SEAT TRACK HAS CORROSION. REMOVED CORROSION ON SEAT TRACK IAW SRM 51-10-3. REMOVED .052 ORIGINAL MATERIAL .090. REMAINING MATERIAL. .038 FOUND TO BE OUT OF LIMITS IAW SRM 51-10-01 FIG 4B. REMOVED OLD SEAT TRACK IAW SRM 51-30-5, 51-30-1. LOCATED DRILLED AND DEBURRED IAW SRM 51-10-4. INSTALLED NEW SEAT TRACK IAW SRM 51-30-5, 51-30-1. REQUIRED INSP COMPLETED.

Part: LONGERON — CORRODED (BS 200-211 L29R) · airframe 73,440 hrs · 70,600 cycles

E AND E COMPT UNDER FR 200 TO STA 211 HAS CORROSION AROUND RIVET TAILS FOR LONGERON 29R. REMOVED CORROSION IAW SRM 53-01, FIG 1. MATERIAL REMOVED .012 MAT REMAINS .038. FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. R & R L29R FROM STA 160-STA 229.57" IAW SRM 51-10-4. REQUIRED INSP COMPLETED.

Part: MOUNT — CRACKED (NR 1 ENGINE) · airframe 73,440 hrs · 70,600 cycles

NR1 ENGINE PYLON APRON LOWER FRAME JUST AFT OF FWD MOUNT CRACKED. REMOVED FASTENERS AND SEVERAL PARTS TO GAIN ACCESS. CUT-OUT SECTION OF FRAME THAT WAS CRACKED. NDT TO VERIFY THAT DAMAGED WAS REMOVED. FABRICATED FORMER AND SPLICES IAW SRM 51-70-5. INSTALLED IAW SRM 51-70-5. REQUIRED INSP COMPLETED.

Part: LONGERON — CRACKED (STA 160 L3L) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN STA 160, LONGERON 3L IS CRACKED AT FRAME ATTACHMENT. REMOVED DAMAGED SECTION OF LONGERON. FABRICATED AND INSTALLED NEW SECTION IAW SRM 53-02, FIG 18. REQUIRED INSPECTION COMPLETED.

Part: ANGLE — GOUGED (BS 693-712) · airframe 73,440 hrs · 70,600 cycles

MAIN PAX CABIN LT SIDE BETWEEN BS 712 AND BS 693 BATHTUB FITTING ENCOMPASS ANGLE, HAS GOUGES. FABRICATED NEW ANGLE. HEAT TREATED ANGLE ON TRAVELER 2311NO2247 IAW AMS 2770. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-10-4.

Part: FLOORBEAM — DAMAGED (BS 160) · airframe 73,440 hrs · 70,600 cycles

COCKPIT FLOORBEAM UPPER CAP HAS SEVERAL ELONGATED AND DOUBLE DRILL FASTENER HOLES AT BS 160 FROM BL 0 TO RBL 57. REMOVED 51 INCHES FLOORBEAM UPPER CAP IAW SRM 53-05, FIG 20B. REMOVED PULLEY BRACKET IAW SRM 51-30-1. REINSTALLED PULLEY BRACKET IAW SRM 51-30-1. FABRICATED, DRILLED SPLICES. MACHINE TAPERED AND INSTALLED IAW SRM 53-05, FIG 20B, P-224. REQUIRED INSP COMPLETED .

Part: LONGERON — DAMAGED (BS 285) · airframe 73,440 hrs · 70,600 cycles

DAMAGE FOUND ON LONG 22 WHILE WORKING SKIN REPAIR AT STA 285. DAMAGE REMOVED, HFEC INSPECTED, DAMAGE REMOVED, REPLACED WITH NEW SECTION OF LONGERON IAW S/PM (06-710-0-6001) AND SRM 53-02, FIG18. REQUIRED INSP COMPLETED.

Part: LONGERON — CRACKED (STA 160 L4L) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN STA 160, LONGERON 4L IS CRACKED AT FRAME ATTACHMENT. REMOVED DAMAGED SECTION OF LONGERON IAW SRM 53-02, FIG 18, P-239. REQUIRED INSPECTION COMPLETED.

Part: FRAME — CRACKED (BS 1339 RT) · airframe 73,440 hrs · 70,600 cycles

AFT ACCESSORY COMPARTMENT STA 1339 RT SIDE AT ALIGNMENT PIN FRAME IS CRACKED. REMOVED OLD FRAME IAW SRM 51-30-2, 51-30-1. RECEIVED NEW FRAME LOCATED DRILLED AND DEBURRED NEW FRAME IAW SRM 51-30-1,51-30-2. INSTALLED NEW FRAME AT STA 1339 RT SIDE IAW SRM 51-30-1,51-30-2. RECEIVED LOWER SEAL INSTALLED LOWER SEAL IAW AMM.

Part: WEB — CRACKED (BS 1128) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN STA 1128 BETWEEN LBL44-55 CUSP WEB IS CRACKED. REMOVED EXISTING CUSP WEB IAW SRM 51-30-2. NDT VERIFIED CRACK IAW REPAIR DWG 5609530019. INSTALLED IAW DC-9-A53-10-16-801-663A-A. REQUIRED INSP COMPLETED BY Q948.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 73,440 hrs · 70,600 cycles

NLG STA 37, RBL 12 PREVIOUS REPAIR ANGLE CRACKED. REMOVED REPAIR DOUBLER AT STA 37, RBL 12 NOT NECCESARY TO REINSTALL WEB BEING REPLACED IAW SRM 51-30-5.

Part: INTERCOSTAL — CRACKED (BS 148-160) · airframe 73,440 hrs · 70,600 cycles

MAIN PASSENGER CABIN BETWEEN STA 148-160 RT INTERCOSTAL IS CRACKED. TAGGED REPAIR DOUBLER IAW DPS 900-5-1. HFEC INSPECTED IAW NDT SPM 06-10-01.001 TO LOCATE CRACK IN INTERCOSTAL. INSTALLED IAW SRM 51-10-4, 51-10-3, 53-05 FIG 100, 53-30-0. REQUIRED INSP COMPLETED.

Part: HINGE BRACKET — CRACKED (LT WING TE FLAP) · airframe 73,440 hrs · 70,600 cycles

LT WING T/E FLAP NR4 HINGE BRACKET CRACKED INBD AT MOUNT HOLE FLAP SIDE. REMOVED ANGLES FROM INBD SIDE OF FITTING IAW SRM 51-30-2 AND DWG 5910134-0. NEW HINGE BRACKET LOCATED AND DRILLED IAW SRM 51-10-4. INSTALLED ANGLES AND HINGE BRACKET IAW SRM 51-30-2 AND DWG 5910134-0. REMAINING FASTENERS THAT JOIN INBD AND OTBD BRACKET INSTALLATION.

Part: WEDGE — CRACKED (LT WING TE FLAP) · airframe 73,440 hrs · 70,600 cycles

LT WING FLAP T/E WEDGE CRACKED ON INBD RIB CAP AT T/E. CUTOUT DAMAGED AREA IAW SRM 51-70-05. FABRICATED 2EA REPAIR ANGLES. FABRICATED FILLER IAW SRM 51-70-05. LOCATED AND DRILLED IAW SRM 51-10-4. TREATED AND PRIMED IAW 51-10-3. INSTALLED ANGLES AND FILLER IAW SRM 51-30-2 AND 51-30-5 TOPCOATED IAW SRM 51-10-3. INSTALLED ID TAG IAW DPS 900-5-1 NO 4.

Part: HINGE BRACKET — CRACKED (LT WING TE FLAP) · airframe 73,440 hrs · 70,600 cycles

LT WING T/E FLAP NR4 HINGE BRACKET CRACKED AT MOUNT HOLE FLAP SIDE. REMOVED L/E PANEL, T/E FLAP LT WING FLAP T/E PANEL 1548A, OTBD HINGE BRACKET, NR 4 FLAP HINGE FITTING AND 2 EA ANGLES IAW SRM 51-30-1,51-30-2. RECEIVED OTBD HINGE BRACKET LOCATED, DRILLED AND DEBURRED IAW SRM 51-10-4. INSTALLED NEW OTBD HINGE BRACKET, 2EA ANGLES, NR4 FLAP HINGE IAW SRM 51-30-1, 51-30-2.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 73,440 hrs · 70,600 cycles

MAIN CABIN FLOOR PANEL NR70 CORRODED SEVERAL PLACES IN FLOOR PANEL RACK. REMOVED CORROSION IAW SRM 51-10-3. NDT VERIFIED DAMAGED CONTAINED IAW NDT SPM 06-10-01.001. MATERIAL FOUND TO OUT OF LIMITS IAW SRM 51-10-3. FABRICATED DOUBLER IAW SRM 51-70-4, FIG 38, 1EA FILLER. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED REPAIR IAW SRM 51-70-4.

Part: FLOOR SUPPORT — CRACKED (BS 775) · airframe 73,440 hrs · 70,600 cycles

MAIN CABIN RT AT BS 775 RBL 43 SUPPORT ANGLE FOR FLOOR FRAME CRACKED AT BOTTOM. REMOVED SUPPORT ANGLE AT STA 775, RBL 43 IAW SRM 51-30-5. RECEIVED NEW PART LOCATED, DRILLED AND DEBURRED IAW SRM 51-10-4. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-30-5 AND 51-30-1.

Part: SKIN — DENTED (BS 77 L19-L20R) · airframe 73,440 hrs · 70,600 cycles

FUSELAGE EXTERIOR STA 77 BETWEEN LONGERON L19R AND L20R SKIN HAS PROTRUDING DENT. COLD WORKED DENT BACK TO CONTOUR IAW SRM 53-04, FIG 38. FABRICATED NEW DOUBLER IAW SRM 53-04, FIG 38. INSTALLED DOUBLER IAW SRM 53-04, FIG 38. NDT VERIFIED DAMAGE CONTAINED IAW NDT SPM 06-10-01.001.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

REMOVED FLOOR SUPPORT IAW SRM 51-30-02. REMOVED CORROSION IAW SRM 53-13-1, FIG 11 OUT OF LIMITS IAW SRM 53-01, FIG 1. FABRICATED AND INSTALLED FLOOR SUPPORT IAW SRM 51-10-4 AND 51-30-05.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND HOLE IN MAIN CABIN FLOOR PANEL 32. CUTOUT DAMAGE IAW 53-01, FIG 4. NDT VERIFIED DAMAGE WAS CONTAINED IAW NDT SPM 06-10-01.001. FABRICATED DOUBLER AND FILLER IAW SRM 53-01, FIG 4. TREATED AND PRIMED DOUBLER AND FILLER IAW SRM 51-10-3. INSTALLED DOUBLER AND FILLER IAW 53-01, FIG 4.

Part: FLOOR SUPPORT — CORRODED (BS 200-218) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PASSENGER CABIN BETWEEN STA 200-218, RBL 18 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED FLOOR PANEL SUPPORT IAW SRM 51-30-0. REMOVED CORROSION IAW SRM 51-10-3. OUT OF LIMITS IAW SRM 53-01, FIG 1. RECEIVED IEA RAW MATERIAL IAW SRM 51-10-2 LOCATED, DRILLED, DEBURRED IAW SRM 51-10-4. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED FLOOR SUPPORT FOR PANEL IAW SRM 51-30-5.

Part: BRACKET — CHAFED (BS 389) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND LOWER FUSELAGE FWD CARGO COMPARTMENT OVERHEAD BS 389, BRACKET CHAFED. FABRICATED, LOCATED, DRILLED THE HOLES, ALODINED AND PRIMED R & R IAW 53-05, FIG 86, 51-30-5 51-10-3, 51-10-4.

Part: CHANNEL — CRACKED (FUSLEAGE) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND NLG STA 37, RBL-6 CHANNEL CRACKED IN 2 PLACES. REMOVED CHANNEL NLG STA 37, RBL 6 IAW SRM 51-30-5. FABRICATED LOCATED, DRILLED NEW CHANNEL IAW SRM 51-10-2, 51-10-4. ALODINED AND PRIMED NEW CHANNEL IAW SRM 51-10-3. INSTALLED NEW CHANNEL IAW SRM 51-30-5.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PASSENGER CABIN FLOOR PANEL NR20 CORRODED OUT OF LIMITS. LOCATED AND DRILLED NEW FLOOR PANEL. INSTALLED NUTPLATES. R & R G-1 GALLEY DRAIN PAN IAW SRM 51-10-4,51-30-2.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 73,440 hrs · 70,600 cycles

DURING M”-CHECK, FOUND MAIN CABIN FLOOR PANEL NR74 HAS CRACK ON END. CUTOUT DAMAGED AREA IAW SRM 51-70-4. FABRICATED AND INSTALLED FILLER FABRICATED DOUBLER IAW SRM 51-70-4. INSTALLED FILLER AND DOUBLER IAW SRM 51-30-2, 51-70-4.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN CABIN FLOOR PANEL 78 HAS CORROSION AROUND FASTENER HOLES. REMOVED CORROSION IAW SRM 51-10-3, MAT LOSS FOUND TO BE OUT OF LIMITS. FABRICATED DOUBLER IAW SRM 51-70-4, 2 EA HOLES. REMOVED CORROSION ON 8 OF 10 HOLES FOUND TO BE WITHIN LIMITS IAW SRM 51-10-2.

Part: INTERCOSTAL — MISINSTALLED (BS 1116 L28R) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND AFT CARGO HAS DOUBLE DRILLED HOLE IN INTERCOSTAL AT BS 1116 L28R. R & R INTERCOSTAL IAW SRM 51-30-5,53-13-3, FIG 3.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 73,440 hrs · 70,600 cycles

AFT ACCESSORY COMPARTMENT, STA 1258, VERTICAL STABILIZER, CTR FITTING IS CRACKED AT LOWER END CORNER. REMOVED CTR FITTING IN AFT ACC COMP STA 1258 IAW SRM 51-30-5. RECEIVED NEW MATERIAL IAW DWG 9911840-115. HEAT TREATED NEW FITTING TRAVELER NR2311N02296 TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED NEW FITTING IAW SRM 51-30-5. REQUIRED INSPECTION COMPLETED.

Part: FLOORBEAM — CHAFED (BS 237) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 237 BL 0- LBL 22 FLOORBEAM IS CHAFED, BLENDED CHAFE. REMAINING WAS OUT OF LIMITS IAW SRM 53-01, FIG 1, FABRICATED PARTS AND COMPLETED REPAIRS IAW SRM 53-05, FIG 20A AND SRM 51-30-5.

Part: TIE DOWN — CRACKED (BS 294) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND FWD CARGO COMPARTMENT, STA 294 RT TIE DOWN RACK CRACKED. REMOVED TIE DOWN TRACK IAW SRM 51-30-1. FABRICATED THE SHAPE FUSELAGE TIE DOWN TRACK DRILLED IAW SRM 51-10-4. SCALLOPED TIE TRAVELER 2311N0251. TREATED, PRIMED IAW SRM 51-10-3. REMOVED CORROSION ON INTERCOSTAL IAW SRM 53-01, FIG 1 TREATED & PRIMED & IAW SRM 51-10-3 INSTALLED IAW SRM 51-30-1.

Part: WEB — MISMANUFACTURED (BS 693-712) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PASSENGER CABIN LT SIDE BETWEEN BS 712 AND BS 693 BATH TUB FITTING ENCOMPASS WEB HAS SEVERAL DOUBLE DRILLED FASTENER HOLES. FABRICATED WEB IAW DWG 9923410-3 AND MATCH DRILLED IAW SRM 51-10-4.

Part: PAN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND AFT CARGO COMPT DOOR CUT OUT LOWER PAN CORRODED. REMOVED CORROSION IAW SRM 51-10-3. MATERIAL LOSS OUT OF LIMITS IAW SRM 53-01, FIG 1. R & R DOOR JAMB PAN IAW SRM 51-30-2, 51-30-5, 51-30-4, 53-05 FIG 44. REINSTALLED ALL PARTS IAW SRM 51-30-2, 51-30-4, 51-30-5.

Part: INTERCOSTAL — CRACKED (BS 1339) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND AFT ACC COMPARTMENT STA 1339, LT LOWER INTERCOSTAL AT TAILCONE CABLES CRACKED AND BENT. REMOVED CRACKED INTERCOSTAL IAW SRM 51-30-5. FABRICATED NEW INTERCOSTAL IAW DWG NR 9917701-3. TREATED AND PRIMED IAW SRM 51-30-5 & 51-30-2.

Part: FLOOR SUPPORT — CORRODED (BS 1139) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND LAVATORY, STA 1139, RBL 22 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED FLOOR PANEL SUPPORT IN LAV AREA STA 1139, RBL 22 IAW SRM 51-30-2. FABRICATED NEW FLOOR PANEL SUPPORT IAW DWG 94FS481223 TREATED, PRIMED AND TOPCOATED IAW SRM 51-10-3, INSTALLED FLOOR PANEL SUPPORT IAW SRM 51-10-4, 51-10-5.

Part: CUSP WEB — DENTED (BS 237-284) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PAX CABIN RT SIDE CUSP WEB HAS 1EA DENT AT LIGHTNING HOLE AND SEVERAL ELONGATED HOLES UNDERNEATH OF OTBD SEAT TRACK FROM BS 237 TO BS 254 RBL 46. CUTOUT DAMAGED SECTION OF CUSP WEB IAW SRM 51-10-4 & SRP DC9-A-53-10-16-801-663A-A. LOCATED DRILLED DEBURRED & PRIMED IAW SRM 53-13-20, 51-10-4 & SRP 53-10-16-801-663A-A. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 & SRP 53-10-16-801-663A-A.

Part: CUSP WEB — CRACKED (CABIN) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PAX CABIN RT SIDE CUSP WEB HAS 1EA CRACK AND SEVERAL ELONGATED HOLES UNDERNEATH OF OTBD SEAT TRACK AT STA 258, RBL 46. CUTOUT DAMAGED SECTION OF CUSP WEB IAW SRM 51-10-4 & SRM 53-10-16-801-663A-A. LOCATED DRILLED DEBURRED & PRIMED TO FIT REPAIR DOUBLER FROM IAW SRM 53-13-20, 51-10-4 & SRP 53-10-16-801-663A-A. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2, & SRP 53-10-16-801-663A-A.

Part: FLOORBOARD — CHAFED (CABIN) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND CABIN FLOORBOARD 89 CHAFING MARKS FROM FASTNERS AT EXISTING HOLES. REMOVED DAMAGED AREA HFEC NDT SPM 06-10-01.001. REPAIRED PANEL IAW SRM 51-70-4. INSTALLED IAW SRM 51-30-2 AND SRM 51-70-4, FIG 1.

Part: SKIN — TORN (VERTICAL STAB) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND VERTICAL STABILIZER RUDDER TOP END, RT SIDE SKIN TORN AT EDGE. REMOVED DAMAGED AREA ON VERTICAL STAB RUDDER IAW SRM 51-70-06, FIG 2, SHT 1. HFEC INSP NO OTHER DAMAGE NOTED NDT SPM 06-10-01.001. FABRICATED AND DRILLED DOUBLER AND FILLER IAW SRM 51-10-04. TREATED, PRIMED AND TOPCOATED DOUBLER AND FILLER IAW SRM 51-10-3. INSTALLED REPAIR IAW SRM 51-70-06, FIG 2, SHT 1.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN CABIN FLOOR PANEL NR 102B HAS CORROSION AROUND FASTENER HOLES. RECEIVED NEW FLOOR PANEL TO BE INSTALLED ON JOB CARD 0590-4020-8M P177.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN CABIN FLOOR PANEL 103 AROUND FASTENER HOLES CORRODED. RECEIVED NEW MAIN CABIN FLOOR PANEL, TO BE INSTALLED ON JOB CARD 0590-4020-8M. LOCATED IAW SRM 51-10-4A.

Part: FLOOR PANEL — GOUGED (MAIN CABIN) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN CABIN FLOOR PANEL NR32 GOUGED 2 PLACES IN FLOOR PANEL. BLENDED GOUGES IAW SRM 53-01, FIG 1. MATERIAL FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1 CUTOUT DAMAGED SECTION OF CHANNEL IAW SRM 53-05, FIG 1. FABBED 2EA CHANNELS IAW SRM 53-05, FIG 1. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED 2EA CHANNEL IAW 51-30-2.

Part: SEAT TRACK — CORRODED (BS 237) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 237, LBL 22 SEAT TRACK HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-3, FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. REMOVED SEAT TRACK IAW SRM 51-30-1 AND 51-30-5. LOCATED, DRILLED IAW SRM 51-10-4 ALODINED AND PRIMED SEAT TRACK IAW 51-10-3. INSTALLED IAW SRM 51-30-5.

Part: FLOOR SUPPORT — CORRODED (BS 310-313) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 310-313, BL 0, FLOOR PANEL SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-3 LOSS OUT OF LIMITS IAW SRM 53-01 FIG 1, CUTOUT SECTION BS 310-348, BL 0 FLOOR SUPPORT REPAIR ANGLES TAPERED 4EA ANGLES ON TRAVELER 2311N02124. INSTALLED IAW A53-10-03-801-663A

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND AFT LT PANEL NR 73, CORROSION AROUND FASTENER HOLES. RECEIVED NEW MAIN CABIN FLOOR PANEL 73 TO BE INSTALLED ON JOB CARD 0590-4020-8M. LOCATED IAW SRM 51-10-4.

Part: GUSSET — CORRODED (BS 1108) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND AFT CARGO STA 1108 GUSSET HAS CORROSION FRONT AND BACK SIDE. LOWER AFT CARGO JAMB CORNER. REMOVED CORROSION IAW SRM 51-10-3 FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1. R & R GUSSET IAW SRM 51-30-2, 51-30-5.

Part: CUSP WEB — CRACKED (BS 280) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PAX CABIN RT SIDE CUSP WEB HAS 1EA CRACK UNDERNEATH OF OTBD SEAT TRACK AT FS280, RBL 46. CUTOUT DAMAGED SECTION OF CUSP WEB, FS 280 RBL 46 IAW SRM 51-10-4 AND SRP DC-9-A-53-10-16-801-663A-A. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRP DC9-A-53-10-16-801-663A-A.

Part: INTERCOSTAL — CORRODED (BS 1116 L27-28R) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND AFT CARGO STA 1116 BETWEEN L27R AND L28R INTERCOSTAL HAS CORROSION. REMOVED CORROSION ON INTERCOSTAL OUT OF LIMITS. REMOVED INTERCOSTAL, INSTALLED GUSSET AND STRAP IAW SRM 53-01, FIG 1,51-30-2 51-30-5.

Part: PAN — CORRODED (BS 1068-1106) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND AFT CARGO STA 1068 TO 1106 LOWER PAN AT DOOR CUTOUT HAS CORROSION SEVERAL PLACES. REMOVED CORROSION IAW SRM 51-10-3. MATERIAL LOSS OUT OF LIMITS IAW SRM 53-01, FIG 1. R & R WEB IAW SRM 51-30-2, 51-30-5, 51-30-4, 53-13-3.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND NOSE WHEEL WELL THROUGH ACCESS HOLE STA 69, LBL 12 BULKHEAD WEB IS CRACKED APPROX .5". STOP DRILLED CRACK IAW SRM 53-01, FIG 2. HFEC INSP IAW NDT SPM 06-10-01 VERIFIED CRACK CONTAINED. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-01, FIG 2.

Part: CUSP WEB — CRACKED (BS 579) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN CABIN RT CUSP WEB IS CRACKED OVER FLOOR SUPPORT STA 579, ABOVE OTBD RIVET EXTENDING 1" FWD AND .2500" AFT OF SUPPORT. REMOVED FLOOR PANEL IAW SRM 51-30-1. REMOVED FLOOR SUPPORT IAW SRM 51-30-2. CUT OUT CRACKED SECTION OF WEB IAW SRM 51-10-2. HFEC INSP IAW NDT SPM 06-10-01. VERIFIED CRACK, REMOVED. FABRICATED REPAIR DOUBLER IAW DC9A-53-10-16-801-663A-A INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-2.

Part: SUPPORT ANGLE — CRACKED (BS 160-200) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND MAIN PASSENGER CABIN STA 160-200 LBL 55 Z ANGLE SUPPORT IS CRACKED. REMOVED Z-ANGLE FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-30-1.

Part: FITTING — BROKEN (TORSION BAR) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND RT WING OTBD FLIGHT SPOILER TORSION BAR INBD FITTING IS BROKEN AT WING AFT SPAR. R & R OTBD SPOILER INBD FITTING IAW SRM 51-30-2 51-30-5.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND NOSE WHEEL WELL LT TUNNEL STA 105, LBL 35 PRESSURE DECK WEB IS CRACKED. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-30-05, 51-20-0 AND DELTA DC-9-A-53-10-02-801-663A-A.

Part: FLOOR SUPPORT — DEBONDED (BS 160-200) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND MAIN PASSENGER CABIN STA 160-200, RBL 55 FLOOR PANEL SUPPORT HAS EXISTING REPAIR DISBONDED AND FASTENER ATTACHMENTS PULLED THROUGH. REMOVED FLOOR SUPPORT. REPAIRED IAW SRM 51-70-1, FIG 3.

Part: FLOOR SUPPORT — MISMANUFACTURED (BS 160) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND MAIN PASSENGER CABIN STA 160, LBL 55 FLOOR PANEL SUPPORT HAS A DOUBLE DRILLED HOLE. REMOVED CLOSEOUT PANEL AND FLOOR SUPPORT IAW SRM 51-30-02 AND 51-30-05. FABRICATED NEW SUPPORT IAW SRM 51-10-2 AND 51-10-4. INSTALLED NEW FLOOR SUPPORT AND CLOSEOUT PANEL IAW SRM 51-30-02 AND 51-30-05.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN CABIN FLOOR PANEL 77, SKIN AND RIB CRACKED. CUTOUT DAMAGED SECTION OF HAT CHANNEL IAW SRM 53-05, FIG 1 FABRICATED DOUBLER AND 2EA HAT CHANNELS, TREATED AND PRIMED IAW SRM 51-10-3.

Part: FLOORBEAM — CHAFED (BS 237) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND MAIN PASSENGER CABIN STA 237 BETWEEN BL 0-LBL 22 FLOOR SUPPORT CHAFED. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-01-1. REMOVED FLOOR SUPPORT IAW SRM 51-30-05. FABRICATED AND DRILLED HOLES IAW SRM 51-10-4 AND DWG 5914617. INSTALLED FLOOR SUPPORT IAW SRM 51-30-05.

Part: FLOORBEAM — CORRODED (BS 196) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND MAIN PASSENGER CABIN STA 196, LBL 44-55 FLOOR SUPPORT PANEL HAS CORROSION. REMOVED FLOOR SUPPORT IAW SRM 51-30-5. FABRICATED AND PICKED UP HOLES IAW SRM 51-10-2 & 51-10-4. INSTALLED FLOOR SUPPORT IAW SRM 51-30-5.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN CABIN FLOOR PANEL 60, SEVERAL RIBS CHAFED, CRACKED AND BROKEN. FABRICATED NEW SKIN AND 5EA RIBS IAW SRM 53-23-0, 53-05, FIG 1. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED SKIN AND RIBS IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND MAIN PASSENGER CABIN STA 200, RBL 44 - 55 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED CORROSION ON FLOOR SUPPORT STA 200, RBL 40-55 IAW SRM 53-01, FIG 1. FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. REMOVED FLOOR SUPPORT IAW SRM 51-30-5. FABRICATED NEW FLOOR SUPPORT LOCATED AND DRILLED IAW SRM 51-10-4, ALODINED AND PRIMED IAW SRM 51-10-3, INSTALLED FLOOR SUPPORT IAW SRM 51-30-5.

Part: SHEAR TIE — CRACKED (BS 832) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND MAIN CABIN CTR WING SECTION AREA STA 832, LBL15, RIVET PULLING THROUGH AT SHEAR TIE. REMOVED FASTENER FOUND CRACK IN SPLICE. REMOVED SPLICE IAW SRM 51-30-2 FORMED SPLICE IAW TRAVELER 2311NG1920. INSTALLED SPLICE AND FASTENER IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 693-851) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN CABIN RT SIDE OTBD SEAT TRACK AT STA 693 TO 851, RBL 44 TOP SURFACE CORRODED AND CHAFING INSIDE TRACK AREA. CUT AND REMOVED CORRODED SEAT TRACK STA 851-775, RBL 44 IAW SRM 51-30-01. INSTALLED NEW TRACK AND SPLICE IAW SRM 53-05, FIG 4.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 200, RBL22-44 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 53-01, FIG 1 FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1. FABRICATED NEW FLOOR SUPPORT INSTALLED NEW FLOOR SUPPORT IAW SRM 51-10-5.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 200, LBL 44-LBL22 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-01, FIG 1. REMOVED SUPPORT, FABRICATED NEW SUPPORT USING INSTALLED SUPPORT IAW SRM 51-30-5.

Part: LONGERON — CRACKED (BS 237 L17L) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN CABIN FS 237, LONG 17L IS CRACKED AT FRAME ATTACH FASTENER. REMOVED SECTION OF LONGERON 17L FROM STA 231-285 IAW SRM 53-13-2 FIG 3. INSTALLED NEW LONGERON SECTION IAW SRM 51-10-2,-4,-3 AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 160-200, LBL 44 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-01, FIG 1. REMOVED SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED SUPPORT IAW SRM 51-30-5.

Part: FLOOR SUPPORT — CORRODED (BS 160-218) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PASSENGER STA 160-218, BL0 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED CORROSION FROM FLOOR SUPPORT IAW SRM 53-01, FIG 1. FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. R & R FLOOR SUPPORT IAW SRM 51-30-5.

Part: SEAT TRACK — DAMAGED (BS 598-617) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND FWD CARGO COMPARTMENT BETWEEN STA 598-STA 617 BETWEEN L27L-L28L SEAT TRACK INSTALLED IMPROPERLY. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-01. FABRICATED NEW TRACK IAW SRM 51-10-02. PICKED UP HOLES IAW SRM 51-10-04. ALODINED AND PRIMED IAW SRM 51-10-03. INSTALLED TRACK IAW SRM 51-30-05.

Part: SHEAR TIE — CRACKED (BS 1151 L14R) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND LAVATORY RT AFT STA 1151 BELOW LONGERON 14 FRAME SHEAR TIE IS CRACKED. REMOVED SHEAR TIE AT RT AFT LAV RECEIVED NEW PART. PICKED UP HOLES IAW SRM 51-10-4. INSTALLED FASTENERS AT SHEAR TIE IAW SRM 51-10-05.

Part: SPLICE — CRACKED (BS 832) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN CABIN CTR WING SECTION AREA BS 832 LBL 7 SPLICE CRACKED. REMOVED SPLICE IAW SRM 51-30-2. FORMED SPLICE IAW SRM 51-10-2, 55-13-3. HEAT TREATED SPLICE 7075-T6. ALODINED & PRIMED IAW SRM 51-10-3. INSTALLED IAW SRM 51-30-2.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND AFT CARGO COMPARTMENT FROM FWD BULKHEAD TO STA 1003 LT CARGO TIE DOWN TRACK CORRODED AROUND FASTENER HOLES AND TRACK GROOVE. REMOVED CORROSION STA 993-1003, SRM 51-10-3. REPLACED TIE DOWN TRACK FROM FWD BULKHEAD TO STA 993 IAW SRM 51-10-4, 51-10-2 & 51-30-5.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 200, LBL 22-BL 0 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED CORROSION FROM FLOOR SUPPORT. FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1. FABRICATED NEW FLOOR SUPPORT AND INSTALLED IAW SRM 51-30-5.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND MAIN CABIN FLOOR PANEL NR59 FASTENER HOLES ELONGATED AND BROKEN OUT. CUT AWAY DAMAGE IAW 51-70-4 NDT VERIFIED DAMAGE. REMOVED IAW NDT SPM 06-10-01. FABBED DOUBLER AND FILLER INSTALLED REPAIR IAW SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 200, BLO-RBL22 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED CORROSION MATERIAL, REMOVED, FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG1, REMOVED FLOOR SUPPORT IAW SRM 51-30-5 FABRICATED NEW FLOOR SUPPORT LOCATED AND DRILLED, TRIMMED NEW FLOOR SUPPORT SRM 51-30-4. ALODINED AND PRIMED IAW SRM51-10-3 INSTALLED IAW SRM 51-30-5.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND MAIN PASSENGER STA 148-170 RBL 55 FLOOR PANEL SUPPORT HAD DOUBLED DRILLED HOLE. REMOVED FLOOR SUPPORT IAW SRM 51-30-5 FABRICATED, TRIMMED, DRILLED, NEW FLOOR SUPPORT IAW SRM 53-13-3, FIG 11. ALODINED AND PRIMED IAW SRM 51-10-3. INSTALLED IAW SRM 51-10-5.

Part: SKIN — CORRODED (BS 1151 L29R) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND FUSELAGE EXTERIOR, REPAIR DOUBLER HAS CORROSION AT FUSELAGE STA 1151 BELOW LONGERON 29R. REMOVED EXTERIOR DOUBLER, FINGER DOUBLER, FILLER, REPLACED WITH NEW ONES, SEALED, IDENTIFIED IAW DWG NR SG09530001 REV REISSUED, NOT VALID AFTER 01-10-2011) AND DELTA PS 900-5-1 NR4.

Part: SHEAR TIE — CHAFED (BS 794) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND MAIN CABIN CTR WING SECTION, STA 794, LBL15 SHEAR TIE TO FRAME IS CHAFED. REMOVED CHAFE FROM SHEAR TIE ORIG MAT .032", LOSS .022" FOUND TO BE OUT OF LIMITS IAW SRM 53-01. FABBRICATED NEW SHEAR TIE IAW SRM 51-10-2, INSTALLED NEW SHEAR TIE IAW SRM 51-30-2. P109.

Part: FRAME — CRACKED (BS 712) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND LT MAIN WHEEL WELL, KEEL AREA BS 712 PREVIOUS FRAME REPAIR IS CRACKED. REMOVED OLD REPAIR DOUBLER AND FABRICATED NEW DOUBLER. INSTALLED REPAIR DOUBLER IAW SRM 51-30-5.

Part: SHEAR TIE — BROKEN (BS 794) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN CABIN CTR WING SECTION/ STA 794, LGL7 SHEAR TIE TO FRAME BROKEN. REMOVED DAMAGED PART IAW SRM 51-30-08 FABBED NEW PART INSTALLED IAW SRM 51-30-08.

Part: SKIN — CHAFED (FUSELAGE) · airframe 73,440 hrs · 70,600 cycles

LT MLG SKIN BETWEEN GEAR DOORS CHAFED AT PANEL NR 5502NW. CHAFED AREA WAS FOUND OUT OF LIMITS. SUPPORT ANGLES FOUND CORRODED OUT OF LIMITS IAW SRM 57-01 FIG 1, FABRICATED RT AND LT SUPPORT IAW SRM 51-30-2.

Part: FLOOR SUPPORT — BROKEN (BS 832) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN CABIN RT STA 832 OTBD FLOOR PANEL ZEE ANGLE SUPPORT BROKEN ON END. REMOVED 26" SECTION OF ZEE ANGLE. FABRICATED 1EA ZEE ANGLE SPLICE IAW SRM 53-13-3 FIG 13, SHEET 1 & 2, 51-10-1 FIG 1, SHEET 2 AND 51-10-2. INSTALLED ZEE ANGLE AND SPLICE IAW SRM 51-10-4, 51-30-2, AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 160-200, RBL 44, FLOOR PANEL SUPPORT HAD CORROSION. REMOVED CORROSION ON FLOOR SUPPORT MAIN CABIN STA 160-200, RBL 44 IAW SRM 53-01, FIG 1, ORIGINAL THICKNESS .060 IAW SRM 51-13-1. MATERIAL REMOVED .030 MATERIAL REMAINING .030 FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. FABRICATED NEW FLOOR SUPPORT IAW SRM 53-13-1. TRIMMED DRILLED DEBURRED NEW FLOOR SUPPORT IAW SRM 51-10-4. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED FLOOR SUPPORT IAW SRM 51-30-5.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN CABIN FLOOR PANEL 26 RIBS PREVIOUS REPAIR CORRODED. REMOVED OLD FILLER AND MADE NEW FILLER IAW SRM 51-70-4, FIG1 NEW FILLER MATERIAL IAW SRM 53-23-0, FIG 4 TREATED AND PRIMED IAW SRM 51-10-3, INSTALLED NEW FILLER IAW SRM 51-70-4, FIG 1.

Part: SUPPORT SPLICE — BROKEN (BS 627 S27-28R) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND FWD CARGO COMPARTMENT STA 627, BETWEEN LONGERON 27R TO L28R SEAT TRACK SUPPORT SPLICE IS BROKEN. REMOVED EXISTING SPLICE.FABRICATED,HEAT TREATED, DRILLED AND INSTALLED NEW SPLICE IAW SRM 51-72-01-801-663A-A.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND MAIN CABIN METAL FLOOR PANEL NR39C HAS DENT. CUT OUT DAMAGED AREA 2"X 2" FABRICATED NEW FILLER AND DOUBLER IAW SRM 53-05, FIG 1. TREATED & PRIMED FILLER & DOUBLER IAW SRM 51-10-3, VERIFIED NO CRACK EXISTS. INSTALLED FILLER AND DOUBLER IAW SRM 53-05, FIG 1.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN CABIN METAL FLOOR PNL NR38C, 1 EA FASTENER PULLING THROUGH FWD END MATERIAL CUT AWAY FOR ORIGINAL REPAIR CRACK FOUND. CUT AWAY DAMAGE. NDT VERIFIED CRACKS ALODINED AND PRIMED. DOUBLER INSTALLED IAW SRM 53-01 FIG 4C.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND MAIN CABIN METAL FLOOR PANEL NR37 CORROSION OTBD EDGE ALONG FASTENERS. WHILE REMOVING CORROSION FOUND CRACK, CUT AWAY DAMAGE CRACKS. REMOVED DOUBLER AND FILLER FABRICATED. INSTALLED REPAIR IAW SRM 53-01, FIG 4.C.

Part: CUSP WEB — CRACKED (BS 706) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN CABIN AT LT STA 706, CUSP WEB HAS EXISTING REPAIR THAT IS CRACKED IN SEVERAL PLACES. REMOVED DOUBLER FABRICATED NEW DOUBLER, PRIMED & INSTALLED IAW SRM 51-30-02 & 53-10-16.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND MAIN PASSENGER CABIN FLOOR PANEL 32 HOLE IN TOP SKIN. FABBED DOUBLER AND FILLER AND INSTALLED ON CABIN FLOOR PANEL 32 ON TOP IAW DC9/MD80 SRM 51-30-2.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 73,440 hrs · 70,600 cycles

AFT CARGO CTR FLOOR PANEL NR 3 HAS A CRACK IN RADIUS OF DOOR CUTOUT AREA. REMOVED CRACK BY TRIMMING AREA. NDT VERIFIED NO CRACK EXIST IAW NDT SPM 06-10-01. FABRICATED DOUBLER SEALED & INSTALLED REPAIR PARTS. ALL WORK ACCOMPLISHED IAW EA98-201837 & SRM (51-10-3) (51-10-4) (51-30-1) (51-30-2) (51-20-00).

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND MAIN CABIN METAL FLOOR PANEL 56 DISBONDED FORWARD CENTER. REMOVED AND REPAIRED FLOOR PANEL IAW DC-9/MD-80 SRM 51-30-1 AND DC-9/MD-80 51-70-1. INSTALLED FLOOR PANEL IAW DC-9-A-53-20-01-201-925A-A.P-177.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,440 hrs · 70,600 cycles

DURING M-CHECK FOUND MAIN PASSENGER CABIN STA 237 BL 0-RBL 22 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED & FABBED 2 ANGLES AT STA 237 RBL 22 BL 0 FLOOR. INSTALLED Z-ANGLE AT STA 237 RBL 22 TO BL 0 FLOOR IAW DC-9/MD80 SRM 51-30-5.

Part: SKIN — CHAFED (BS 1314-1326) · airframe 73,440 hrs · 70,600 cycles

AFT ACCESSORY BETWEEN CANTED FRAME 1314 AND 1326 SKIN IS CHAFED BELOW RT SIDE OF VENTRAL STAIRWAY CROSSFRAME SUPPORT. BLENDED AREA OUT OF LIMITS. FABRICATED DOUBLER CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 53-01, FIG 4, 53-33-0 FIG 5, 51-10-4, 51-10-3, 51-20-0 & 51-30-2.

Part: LONGERON — DAMAGED (FS 168 L18R) · airframe 73,440 hrs · 47,775 cycles

MAIN CABIN FS 168, LONGERON 18R FRAME FITTING DAMAGED, REQUIRES REPLACEMENT. REMOVED DAMAGED FITTING AT FS 163, L18R IAW SRM 51-30-1 AND 51-30-5 FITTING LOCATED, DRILLED, TREATED PRIMED AND INSTALLED IAW SRM 51-10-4,51-10-3,51-30-1, AND 51-30- 5.

Part: CARGO TRACK — CORRODED (BS 427-503) · airframe 73,440 hrs · 70,600 cycles

LOWER FUSELAGE FWD CARGO COMPARTMENT STA 427 TO STA 503, RT TIE DOWN TRACK BOTTOM SCREW HOLES HAVE CORROSION AROUND THEM. REMOVED CORROSION ON TIE DOWN TRACK IAW SRM 51-10-3 WITH AN ORIGINAL THICKNESS OF .060 IAW SRM 53-23-0, FIG 9 AND A MATERIAL LOSS OF .033 LEAVING A REMAINING THICKNESS OF.027 FOUND OUT OF LIMITS IAW SRM 53-01. R & R TIE DOWN TRACK IAW SRM 51-30-1, 459577, P109. REQUIRED INSPECTION COMPLETED.

Part: CARGO TRACK — CORRODED (BS 1106-1167) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND AFT CARGO STA 1106 TO 1167 RT TIE DOWN TRACK HAS CORROSION IN SEVERAL PLACES. REMOVED CORROSION ON TIE DOWN TRACK, STA 1167, RT SIDE IAW SRM 51-10-3, FOUND TO BE OUT OF LIMITS IAW SRM 53-01, REMOVED TIE DOWN TRACK IAW SRM 51-30-2. RECIEVED CUSTOMER PART TRIMMED AND DRILLED IAW SRM 51-10-4. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED IAW SRM 51-30-7.

Part: BULKHEAD — CRACKED (BS 69) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND NOSE WHEEL WELL THROUGH ACCESS HOLE, STA 69, RBL 12 BULKHEAD IS CRACKED APPROX .5 INCH. STOP DRILLED CRACK WITH A .250" HOLE ON WEB IN NOSE WHEEL WELL THROUGH ACCESS HOLE STA 69 RBL 12 BULKHEAD WEB, CRACK CONTAINED. FABRICATED DOUBLER IAW SRM 53-01, FIG 2, SHEET 3 INSTALLED DOUBLER IAW SRM 53-01, FIG 2, SHEET 3. IDENTIFIED REPAIR IAW PROCESS STANDARD 900-5-1 NR 4 F.

Part: SKIN — DAMAGED (BS 450) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND FWD CARGO COMPARTMENT, DURING INSPECTION, MATERIAL THINNING INDICATION BETWEEN OUTER SKIN AND INNER DOUBLER AT DME ANTENNA STA 450 MIN. REMAINING MATERIAL .042. DEFER TO ENGINEERING. R & R DOUBLER AND FINGER DOUBLER PN 09-5300-3-14 AND PN 09-5300-3-15 IAW SRM 51-30-2 AND 51-30-05 P177.

Part: SKIN — DAMAGED (BS 340) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND FWD CARGO COMPARTMENT, DURING INSPECTION, MATERIAL THINNING INDICATION BETWEEN OUTER SKIN AND INNER DOUBLER AT DME ANTENNA STA 340 MIN. REMAINING MATERIAL .041 DEFER TO ENGINEERING. R & R DOUBLER AND FINGER DOUBLER PN 09-5300-3-0014 AND PN 09-5300-3-0015 IAW DWG 5925992 IAW SRM 51-30-2 AND 51-30-5 P177.

Part: SKIN — DAMAGED (BS 395) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND FWD CARGO COMPARTMENT, DURING INSP MATERIAL THINNING INDICATION BETWEEN OUTER SKIN AND INNER DOUBLER AT DME ANTENNA STA 395 MIN. REMAINING MATERIAL .045. DEFER TO ENGINEERING. R & R DOUBLER AND FINGER DOUBLER PN 09-5300-3-14 AND PN 09-5300-3-0015 IAW SRM 51-30-2 AND 51-30-5 P177.

Part: SKIN — DAMAGED (BS 508) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND FWD CARGO COMPARTMENT DURING INSP, MATERIAL THINNING INDICATION BETWEEN OUTER SKIN AND INNER DOUBLER AT DME ANTENNA STA 508 MIN. REMAINING MATERIAL .042 DEFER TO ENGINEERING FOR REVIEW. R & R DOUBLER AND FINGER DOUBLER PN 09-5300-3-14 AND PN 09-5300-3-0015 IAW SRM 51-30-02 AND 51-30-05. P177.

Part: SEAT TRACK — CORRODED (BS 200-303) · corrosion level 2 · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 200-303, RBL 22 SEAT TRACK HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 51-10-3 & 53-05. REMOVED SEAT TRACK IAW SRM 51-30-1. FABRICATED SEAT TRACK IAW SRM 53-23-0, FIG 4 & LOCATED, DRILLED IAW SRM 51-10-4, TREATED & PRIMED IAW SRM 51-10-3. INSTALLED SEAT TRACK IAW SRM 51-30-1.

Part: FLOOR PANEL — DENTED (CABIN) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND MAIN CABIN METAL FLOOR PANEL 71 HAS DENT. CUT OUT DAMAGE PER DC9 SRM 53-01. ALODINED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED DOUBLER AND FILLER IAW DC9 SRM 53-01 FIG 4.

Part: FRAME — GOUGED (BS 598) · airframe 73,440 hrs · 70,600 cycles

DURING M-CHECK FOUND FWD CARGO, TOP OF FWD SIDE OF FR 598, BOTTOM OF LT SIDEWALL LOWER ATTACH SUPPORT IS GOUGING THROUGH FRAME DOUBLER. BLENDED GOUGE IAW SRM 53-01, FIG 1 OUT OF LIMITS. FORMED AND FABRICATED DOUBLER IAW SRM 53-01, 51-10-4, 51-10-3. INSTALLED DOUBLER IAW SRM 51-30-5.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,678 hrs · 69,050 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE RIGHT EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHT RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING THE PREFLIGHT CHECK, IT WAS DISCOVERED THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT AND ALL OF THE OVERWING EXITS WERE INOPERATIVE. MAINTENANCE REPLACED EACH OF THE APPLICABLE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 68,917 hrs · 66,641 cycles

JUST AS THE AIRCRAFT TOOK OFF, THE COCKPIT CREW DETECTED SMOKE AND FWD LAVATORY SMOKE DETECTOR ACTIVATED. CREW REPORTED "EXTREME HEAT" AND SMOKE FILLED CABIN AREA. RED-BORDER COM PROCEDURES WERE COMPLIED WITH AND ACFT RETURNED TO CMH WITH CFR STANDING-BY. CREW PERFORMED AN OVER-WEIGHT LANDING AND BRAKES FUSED UPON STOPPING. PAX DID NOT EVACUATE BUT WERE DEPLANED THROUGH AFT STAIRS. NO FIRE OR EVIDENCE OF BURNING WAS FOUND. MAINTENANCE REPLACED THE RT PACK TEMPERATURE CONTROLLER FOR FAILING TO RUN COLD, EXECUTED THE PACK BURN-OUT PROCEDURES BECAUSE OF SMOKE, REPLACED THE COALESCER BAGS, LEAK CHECKED AND FUNCTIONALLY CHECKED ALL APPLICABLE SYSTEMS AND RETURNED THE AIRCRAFT TO SERVICE. (A)

Part: FRAME — CRACKED (BS 1209 L8L) · airframe 67,801 hrs · 65,650 cycles

DURING "H" CHECK, FOUND CRACK IN FRAME INNER CHORD AT BS 1209 L8L. REPAIRED PER EA 98-211041.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 67,225 hrs · 65,135 cycles

SHORTLY AFTER TAKEOFF, THE FLIGHT ATTENDANT REPORTED VERY HOT TEMPERATURES AND SMOKE IN THE CABIN. THE FLIGHT CREW COULD SMELL SMOKE AND OIL FUMES ALSO. NO MENTION OF COM COMPLIANCE BUT CREW DID SAY THAT ALL PACK INDICATIONS WERE NORMAL. THE FLIGHT RETURNED TO A SUCCESSFUL BUT OVERWEIGHT LANDING BACK AT LAN AND WAS ABLE TO TAXI TO THE GATE UNDER ITS OWN POWER. MAINTENANCE DID FIND OIL RESIDUE IN THE LEFT COALESCER BAG AND REPLACED IT. SOURCE OF OIL WAS NOT IDENTIFIED. COMPLETE PACK BURNOUT PROCEDURES WERE ACCOMPLISHED AND THE COCKPIT TEMPERATURE CONTROLLER WAS REPLACED. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: BOOT — SEPARATED (LT PACK) · airframe 64,545 hrs · 62,773 cycles

DURING CRUISE FLIGHT AT FL350 WITH ANTI-ICE ACTIVATED THE CABIN ALTITUDE STARTED CLIMBING. COM PROCEDURE COMPLIANCE COULD NOT CORRECT THE CABIN RATE OF CLIMB. THE RED -CABIN PRESS- WARNING LIGHT ALONG WITH THE -MASTER CAUTION- LIGHT ILLUMINATED SO A RAPID DESCENT WAS INITIATED. CREW WAS NOT ABLE TO REGAIN CONTROL OF THE CABIN UNTIL 12,000 MSL AND ABOUT THAT TIME THE -FWD ACCESSORY COMP DOOR- WARNING LIGHT ILLUMINATED. FLIGHT DIVERTED TO JAN AND LANDED UNEVENTFULLY. MAINTENANCE FOUND A RUBBER BOOT BLOWN OFF AFT OF THE LEFT WATER SEPARATOR AND MEL'D THE LEFT PACK SYSTEM.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,377 hrs · 60,805 cycles

DURING H-CHECK FOUND LT ACCESS KIDNEY PANEL BELOW LEADING EDGE WING TO BODY FAIRING HAS CORROSION ON SKIN INNER DOUBLER AT INBOARD CORNER SURFACE. REPAIRED PER EA 98-201833.

Part: ACM — SMOKE (LEFT) · airframe 62,221 hrs · 60,666 cycles

DURING TAKEOFF ROLL, A STRONG ODOR AND VISIBLE SMOKE ENTERED THE FLIGHT DECK. SMOKE WAS ALSO REPORTED IN THE CAIBN COMING FROM THE GASPER VALVES. THE TAKEOFF WAS SAFELY ABORTED AT ABOUT 120 KTS AND THE CREW PERFOMRED COM PROCEDURES FOR SMOKE REMOVAL PRIOR TO RETURNING TO THE GATE. MAINTENANCE REPLACED THE LEFT AIR CYCLE MACHINE, BOTH THE LEFT AND RIGHT COALESCER BAGS, AND THEN RAN THE ENGINE AT TAKEOFF POWER FOR FIVE MINUTES. NO SMOKE WAS GENERATED IN THE CABIN OR COCKPIT. THE AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,723 hrs · 55,624 cycles

DURING MCK AT ATL, CORROSION WAS FOUND ON THE CENTER LINE FLOOR SUPPORT CAP BETWEEN STATIONS 237 AND 294. REPAIRED PER EA 98-185352.

Part: PRESSURE PANEL — CRACKED · airframe 56,723 hrs · 55,624 cycles

During M ck in ATL, cracks were found in the flight compartment horizontal pressure panel at sta 105. Located at x=25 .5"long and x=35 .5"long. Repaired per EA 98-185344. Material .040" 2024-t3 AL.

Part: BRACKET — CRACKED · airframe 56,723 hrs · 55,624 cycles

During Mck in ATL, a .25" crack was found to the RHS bracket 9957860-6. Material 7075-t6 AL. Repaired per EA 98-185364

Part: SKIN — CRACKED · airframe 56,313 hrs · 55,261 cycles

During CK in MSP, A skin crack was found near the aft cargo door cutout in the skin at the lower aft corner. Skin is .063 2024-t3. Repaired per EA 99-183545.

Part: SKIN — CRACKED · airframe 56,313 hrs · 55,261 cycles

During overnight in MSP, a skin crack was found near the aft cargo door cut out in the skin at the lower aft corner. Repaired per EA 99-183545.

Part: FUSE — BLOWN (CABIN)

DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY ESCAPE PATH AND FORWARD GALLEY EXIT SIGN LIGHTS INOPERATIVE. REPLACED FUSE, OPERATIONAL CHECK NORMAL.

Part: LIGHT — MALFUNCTIONED (NLG)

DURING APPROACH INTO MSY, THE NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW UTILIZED EMERGENCY GEAR EXTENSION PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED GEAR SIX TIMES AND NO PROBLEMS WERE FOUND.

Part: CYLINDER — INOPERATIVE (RT MLG)

DURING CLIMBOUT, THE RIGHT MAIN LANDING GEAR RED WARNING AND DOOR OPEN INDICATIONS REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR BUNGEE CYLINDER, OPERATIONAL CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING INSPECTION, THE OVERHEAD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERATIONAL CHECK OK.

Part: SWITCH — INOPERATIVE (TAIL)

DURING CRUISE FLIGHT, TAIL ANTI-ICE PRESSURE ABNORMAL ANNUNCIATOR LIGHT CAME ON. FLIGHT CREW FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, DIVERTED FLIGHT TO ORD, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ICE PROTECTION AIR PRESSURE SWITCH, OPERATIONAL CHECK OK.

Part: BATTERIES — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND EMERGENCY OVERHEAD CABIN LIGHTS INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY FORWARD OF OVERWING EXITS. OPERATIONAL CHECK OK.

Part: CONNECTOR — BROKEN (CABIN)

DURING INSPECTION, FOUND EMERGENCY ESCAPE FLOOR LIGHTS INOPERATIVE AT SEATS 19-22. MAINTENANCE REPAIRED PIN IN CONNECTOR PLUG.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE CHECK, FOUND SEAT ROWS 19, 20, 21 AND 22 EMERGENCY PROXIMITY FLOOR LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY, OPERATIONAL CHECK GOOD.

Part: PAN — CRACKED (CARGO DOOR)

DURING L CHECK, FOUND CRACK IN FORWARD CARGO DOOR PAN. REPLACED PER EA 98-113030.

Part: BATTERIES — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND ONE SECTION OF CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK OK.

Part: BATTERIES — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND THE TWO EMERGENCY LIGHTS BY THE OBSERVER'S OXYGEN REGULATOR INOPERATIVE. REPLACED BATTERIES IN POWER PACK B5-23, OPERATIONAL CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND BOTH EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED LEFT AND RIGHT BATTERY PACKS, SYSTEM OPERATIONAL CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND AFT SECTION OF CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN BATTERY PACKS, OPERATIONAL CHECK OK.

Part: CONTROL VALVE — MALFUNCTIONED (LT TE FLAP)

ON TAKEOFF ROLL, TAKEOFF WARNING HORN SOUNDED WITH ALL FLIGHT CONTROLS IN NORMAL POSITION. ABORTED TAKEOFF. MAINTENANCE REPLACED LEFT FLAP CONTROL VALVE, OPERATIONAL CHECK OK.

Part: FUEL CONTROL — WATER CONTAM (NR 2 ENGINE)

DURING TAKEOFF ROLL, THE NR 2 ENGINE EPR AND N1 INDICATIONS BEGAN FLUCTUATING. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE DRAINED FUEL CONTROL MOISTURE TRAP AND RAN ENGINE TO TAKEOFF POWER. ACCELERATION AND OPERATIONAL CHECK OK.

Part: CROSSFEED VALVE — LEAKING (TAIL COMPT)

ON TAKEOFF JUST AFTER ROTATION, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. PERFORMED COM PROCEDURE BUT LIGHT REMAINED ON. FLIGHT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND LEFT PNEUMATIC CROSSFEED VALVE LEAKING. REPLACED CROSSFEED VALVE, OPERATIONAL CHECK OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT ROW 23 INOPERATIVE. REPLACED POWER SUPPLY FOR AFT SECTION OF FLOOR EMERGENCY LIGHTS. OPERATIONAL CHECK NORMAL.

Part: WIRE — CHAFED (CABIN)

DURING LINE MAINTENANCE INSPECTION, FOUND AFT SECTION OF FLOOR PROXIMITY EMERGENCY LIGHT WIRING CHAFER AT SIDEWALL. REPAIRED WIRING AND OPERATIONAL CHECK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY AND EMERGENCY EXIT SIGN LIGHTS INOPERATIVE, AFT OF ROW 22. REPLACED POWER SUPPLIES AND BATTERIES. OPERATIONAL CHECK NORMAL.

Part: FITTING — CORRODED (FS 1167)

DURING H-CHECK, FOUND CORROSION IN THE LONGERON 22R END FITTING AT FS 1167. REPLACED FITTING PER SRM 51-30-2.

Part: BLKHD WEB — OIL CANNED (FS 1136)

DURING H-CHECK, FOUND OIL CANNING IN THE FS 1136 PYLON BULKHEAD WEB, LEFT AND RIGHT SIDES. REPAIRED WEBS (P/N 9912243-81, -4, -3) PER EA 98-103301.

Part: INTERCOSTAL — CRACKED (FS 140)

DURING H-CHECK, FOUND A CRACK IN THE INTERCOSTAL BETWEEN THE SERVICE DOOR JAMB AND COCKPIT LOWER SILL FS 140. REPAIRED INTERCOSTAL (P/N 9911557-3), PER EA 98-101990.

Part: FITTINGS — CORRODED (FS 1167)

DURING H-CHECK, FOUND CORROSION IN THE LONGERON 19R TO 20R END FITTINGS AT FS 1167. REPLACED FITTINGS PER SRM 51-10-3.

Part: CABLE — FRAYED (TAIL CONE)

DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR HANDLE FROM THE CLIPS AND DROP THE TAIL CONE. ALSO, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE EXTERIOR HANDLE FROM THE CLIPS AND THAT CABLE RUN 301A WAS FRAYED. ADJUSTED THE CLIPS/RELEASE SYSTEM AND REPLACED THE CABLE, CHECKED OK.

Part: BLOCK/LATCH — WORN (TAILCONE)

DURING L-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAILCONE HANDLE FROM THE CLIPS AND SUBSEQUENTLY DROP THE TAILCONE. ALSO, FOUND THE UPPER LEFT CABLE BLOCK WORN AND THE LOWER LEFT LATCH WITH EXCESSIVE PLAY. REPLACED BLOCK, LATCH, ADJUSTED THE RELEASE SYSTEM AND HANDLE CLIPS, CHECKED OK.

Part: ACM DUCT — BLOWN (LEFT SIDE)

TAIL COMPARTMENT TEMPERATURE HIGH AND MASTER WARNING LIGHTS ILLUMINATED DURING CLIMBOUT FROM RDU. LIGHTS STAYED ON FOR APPROXIMATELY THREE SECONDS THEN EXTINGUISHED. AFTER A FEW MINUTES, AGENT 2 LOW LIGHT ILLUMINATED AND REMAINED ON. FLIGHT CONTINUED TO DESTINATION (DTW) AND LANDED WITHOUT INCIDENT. FOUND LEFT ACM DUCT BLOWN AND NR 2 FIRE AGENT BOTTLE HAD DISCHARGED. REPLACED DUCT AND NR 2 FIRE AGENT BOTTLE. AIRCRAFT RETURNED TO SERVICE.