N27213

Part: SKIN — CORRODED (ZON E100) · corrosion level 2 · airframe 83,484 hrs · 30,800 cycles

FOUND EXFOLIATED CORROSION AT STA 540 CENTER WING LOWER SKIN FROM SPAR BETWEEN S-22R & 23R. ACCOMPLISHED REPAIR AT WING CENTER SECTION LOWER SKIN BS 540 BETWEEN S22R AND 23R ESR-WI 3-13294 AND ECRA 5710-02953,

Part: SKIN — DAMAGED (ZONE 800) · airframe 83,484 hrs · 30,800 cycles

AS PER C/R REPLACE THE FWD CARGO DOOR INNER SKIN. REMOVED AND REPLACED FWD CARGO DOOR SKIN PER SRM 51-40-02-0G-0 AND DWG#143A6110

Part: UNKNOWN — ODOR (CABIN) · airframe 83,313 hrs · 30,724 cycles

STRONG WET SOCK SMELL IMMIDIATELY AFTER T/O INDICATION OF OIL BURN SMELL LEAKING INTO PACKS DEBRIEFED CREW, PILOT SAID ODOR DISAPATED QUICKLY AFTER TAKEOFF. ACFT HAS NO HISTORY OF ODORS FROM PACKS IN LAST 90 DAYS. OPS CHECKED PACKS, NO ODORS NOTED.

Part: GIRT BAR — NO DISCREPANCY (ZONE 800) · airframe 82,303 hrs · 30,271 cycles

DOOR SLIDE AT 1R. IS STARTING TO SAG AND INTERFERING WITH ARMIN G/DISARMING INSPECTED R1 DOOR SLIDE ASSY REF AMM 25-66-01. GIRT MATERIAL SHOWING WITHIN SERVICEABLE LIMITS. GIRT BAR STOWS/ENGAGES LOCKS NORMALLY. OPERATED DOOR OPEN/CLOSE, GIRT MATERIAL NOT TOUCHING DOOR FRAME. OK TO CONTINUE SERVICE.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 81,792 hrs · 30,041 cycles

AFT ENTRY DOOR 2R EXT EMERGENCY LIGHT INOP R&R AFT EMERGENCY LIGHT BATTERY ON POWER SUPPLY M1672 OPS CHECK NORMAL REF. AMM 33-51-00.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 81,747 hrs · 30,015 cycles

CREW DEBRIEF - ON ROTATION. FELT THUMP. ON CLIMB #2 ENGINE STALLED 3 TIMES. REDUCED POWER, ENGINE QUIT STALLING. ONCE LEVELED OUT.ACCOMPLISHED CHECKLIST. SHUT ENGINE DOWN. NO SEVER VIBRATION. AT ROTATION FLT CREW OBSERVED A RABBIT INGESTED #2 ENGINE, ENGINE STALLED 3 TIMES DURING CLIMBOUT. SLIGHT VIBRATION FELT AND INDICATED,, CREW LEVELED OFF AND ENGINE SHUTDOWN. PAX REPORTED FLASH FROM TAIL OF ENGINE. INSPECTION FOUND NO EVIDENCE OF FIRE, MISSING STATORS, MISSING FAN BLADES, INLET GUIDE VANES, NO DAMAGE OR MISSING TURBINE BLADES. SEE LOG PAGES, 453016, 4503910, 4502575, 4502233, 4499460, 4499436, 4499376 AND 4499336 FOR WORK ACCOMPLISHED. FAN BLADE AND PLATFORM CHANGE, BOROSCOPE INSPECTION, ENGINE RUNS AND DEBRIS CLEAN-UP. ADDING MATERIALS FOR BLADE SET PARTS INFO ADDED. BLADE SET REMOVED WAS SN 0653 ON 4-14

Part: DOOR — FOD (ZONE 200) · airframe 81,385 hrs · 29,853 cycles

LANDING GEAR MOULD NOT RETRACT AFTER TO RAN 2.140.10 OPS NORMAL CONTINUE DEBRIEFING THE CREW. THEY SAID THE PREVIOUS CREW SPILLED RICE ON FLIGHT DECK FLOOR BY THE MANUAL GEAR EXTENSION ACCESS DOOR. ONCE THEY CYCLED THE DOOR OPEN AND CLOSE. THE GEAR OPS NORMAL. FOUND MANUAL EXT ACCESS DOOR IN COCKPIT TO NOT BE SECURELY LATCHING AND ALLOWING THE DOOR TO LIFT UP RETENTION CLIPS ON FLOOR ARE NOT GRASPING THE DOOR CLIPS CLEANED ALL OF THE MANUAL EXT ACCESS DOOR AND FRAME AROUND DOOR AND IN THE RETENTION HOLES OF THE DOOR POSTS REF AMM 32-34-00-100-801-C1. DOOR IS NOW CLOSING AND LATCHING SECURED. PERFORMED ALTNERATE LANDING GEAR TEST REF AMM 32-31-51-400-801 ADD EMP:U409284 OPS CHECK GOOD. DUE TO PILOTS STATEMENT OF THE GEAR WOULD NOT RETRACT RECOMMEND A GEAR SWING. ALSO REF FIM 32-30-815 PARAGRAPH E 1A AND NEXT STEP IS TO JACK AIRPLANE AMD SWING GEAR CONTINUED FIM 32-30 TASK 815. GEAR SYSTEM SATISFACTORY PER FIM. ACCOMPLISHED A NLG AND MLG SWING AND OPERATION CHECK IN REF TO AMM 32-32-00 AND 32-33-00. GEAR OPS CHECK PASSED. NO DEFECTS NOTED.

Part: LAMP — INOPERATIVE (DOOR INDICATOR) · airframe 81,196 hrs · 29,761 cycles

EMER EXIT NOT ARMED LITE NEEDS REPLACED. RELAMPED, OPS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 80,936 hrs · 29,640 cycles

AIRCRAFT SMELLS LIKE BAD LAV THROUGH ENTIRE CABIN NOT A MAINTENANCE TASK. CONTACT OPS.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 80,618 hrs · 29,490 cycles

SEAT EMERGENCY LIGHTS INOP AT ROWS 15ABC 20ABC AND 21ABC REMOVED AND REPLCE BATTERY AND CHARGER IAW AMM 33-51-06 OPS CHECK GOOD.PARTS USED: 99-3351-3-0015, QTY :1 29-3351-3-0031,QTY :1

Part: COVER — FOD (MLG EXTEND) · airframe 78,696 hrs · 28,565 cycles

LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF INSP A/C FOUND ALTERNATE GEAR EXTENSION COVER HAS DEBRI OBSTRUCTING COVER FROM CLOSING. REMOVED SOME BUT NEEDS FURTHER CLEANING. REMOVED REMAINING DEBRIS FROM MANUAL EXTENSION COVER HINGE AND LATCHES, VERIFIED DOOR CLOSES ND ENGAGES DOOR POSITION SWITCH. REQUIRES GEAR SWING TO CONFIRM FIX PERFORMED LANDING GEAR EXTENSION AMD RETRACTION TEST REF AMM 32-32-00-710-801. OPS CK GOOD.

Part: FRAME — CORRODED (STA 300) · airframe 75,868 hrs · 27,247 cycles

CORROSION FOUND AT STA 300 APPROX S-8L ABOVE DOOR SILL DRAIN DIAPHRAM.(UNDER BLANKET411A4901-1349 TO "ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF ECRA 5310-08113 ON OR BEFORE FEBRUARY 6, 2025. PERFORMED PART 1 INTERIM REPAIR PER ECRA 5310-08113. REFERENCE BAM N/R#001177141 FOR ALL WORK ACCOMPLISHED. PLACED ON DTA DIP VEREFIED ECRA AND DIP LIMITS

Part: PROBE — FAULTY (NA) · airframe 72,626 hrs · 25,863 cycles

SUSPECT FUEL LEAK RIGHT IMBALANCE IN FLIGHT UNABLE TO STOP INDCA TION CHANGED ON GRD H TANK .AT LANDING (TURNED ON BOTH R/H BOOST PUMPS) CLOSED ( CROSSFEED) AND NOTICE A BIG JUMP ON R/H HAND TANK INDICATION .HE ALSO NOTICE WHAT IT APPEAR ERONEOUS INDICATION FROM LEFT TANK. PERFORMED FQIS BITE. LAST LEG FAULT SHOW TANK 1 & 2 DEGRAD ACC DEBRIEF CREW AT 10K FT ( L/H TANK READING ABOUT 8.5) ( R/H TANK SUMPED 4 BOTTLES FROM #1 AND #2 TANKS, NO WATER FOUND. FQIS COMPENSATOR DATA BAD. READING ABOUT 7) .TURNED OFF (R/H BOOST PUMPS) OPEN (CROSSFEED) GROUND TEST PASSED AND HAS NO CURRENT FAULTS. ADD FAULT: 28-41108 AND 28-411208 AND LEFT ON (L/H BOOST PUMPS ON) . AT 30 K FOR A LITTLE BIT IT APPEAR THE MISSBALANCE WAS BEING CORECTED BUT THEN CONTINUE TO HAVE WHAT IT APPEAR ERONEOUS QUANTITY INDICATION COMING FROM R/ FOR PARTS INFO FOR PARTS INFO FOR PARTS INFO FOR PARTS INFO ROTABLE PARTS CHANGE WAS INDICATED - TT # 1952992 SN OFF 0274 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1154639 SN OFF 0262 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1003520 SN OFF 0177 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1152759 SN OFF 0235 TT # 1931568 SN OFF 0317 TT # 1154301 SN OFF 0262 TT # 1927833 SN OFF 0283 TT # 1924167 SN OFF 0489 TT # 1925317 SN OFF 0265 TT # 1149295 SN OFF 1976 TT # 1954172 SN OFF 0255 TT # 1154639 SN OFF 0262 TT # 1003520 SN OFF 0177 TT # 1170353 SN OFF 0244 IPC REFERENCE # 28-41-21-04 IPC REFERENCE # 28-41-21-04 PROBE, FUEL, 73 OFF 29-2841-9-9010 0262 ON 29-284

Part: DOOR — MISSING (WASTE SERVICE) · airframe 71,779 hrs · 25,503 cycles

PDA 1 LAVATORY TOILET SERVICE DOOR MISSING FROM ACFT UPON ARRIVAL EXAMINED ACFT FOR DMG FROM PART DEPARTING ACFT. NO DAMAGE NOTED. NEEDS NEW DOOR AND HARDWARE. REFERENCE IPC 52-49-07-01 ITEMS 55, 60, 65, 70, 75 & 230. UPDATED MATERIALS LIST. PLACAED ON CDL 52D.

Part: LIGHT — DAMAGED (ROW 28 ABC) · airframe 70,970 hrs · 25,193 cycles

SEAT MOUNTED EMERGENCY LIGHT AT ROW 28ABC DAMAGED. REMOVED AND REPLACED LIGHT ASSY (WHITE) REF CONFIG DRAWING 3350DD14743 AND IFM 25-22-55. OPS CK OK.

Part: LIGHT — INOPERATIVE (SEAT 15 ABC) · airframe 69,184 hrs · 24,520 cycles

SEAT 15 ABC AREA EMERGENCY LIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (SEAT 14DEF) · airframe 69,184 hrs · 24,520 cycles

SEAT 14 DEF EMERGENCY LIGHT AREA INOPERATIVE.

Part: SIGN — INOPERATIVE (SEAT 15ABC) · airframe 69,184 hrs · 24,520 cycles

EXIT SIGN EMERGENCY NEAR ROW 15 ABC INOPERATIVE.

Part: LIGHT — INOPERATIVE (SEATS 22-28 ABC) · airframe 69,184 hrs · 24,520 cycles

EMERGENCY PROXIMITY LIGHTS INOPERATIVE AT SEAT ROW 20 ABC THRU 28 ABC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,184 hrs · 24,520 cycles

SEAT 8 ABC EMERGENCY LIGHT INOP SUPPORT TASK.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,184 hrs · 24,520 cycles

SHEAR FITTING AT STA 540 RBL 40.87 IS CRACKED, SUPPORT TASK. REMOVED IN REPLACED SHEAR FITTING AT STA 540 RBL 40.87 IAW SRM 57-40-02 AND DWG 111A2000 SSFR REPORT FORM 46-0024 ENTERED BY INSPECTION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,184 hrs · 24,520 cycles

SHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED, SUPPORT TASK. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 6.14 IAW SRM 51-40-02 AND DWG 111A2000 SSFR REPORT FORM 46-0024 ENTERED BY INSPECTION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,184 hrs · 24,520 cycles

SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED, SUPPORT TASK. REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 15.04 IAW SRM 51-40-02 AND DWG 111A2000 SSFR REPORT FORM 46-0024 ENTERED BY INSPECTION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,184 hrs · 24,520 cycles

SHEAR FITTING AT STA 540 LBL 32.40 IS CRACKED, SUPPORT TASK. REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 32.40 IAW SRM 51-40-02 AND DWG 111A2000 SSFR REPORT FORM 46-0024 ENTERED BY INSPECTION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,184 hrs · 24,520 cycles

SHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED, SUPPORT TASK. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 54.60 IAW SRM 51-40-02 AND DWG 111A2000 SSFR REPORT FORM 46-0024 ENTERED BY INSPECTION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,184 hrs · 24,520 cycles

SHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED, SUPPORT TASK. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 15.04 IAW SRM 51-40-02 AND DWG NR 111A2000 SSFR REPORT FORM 46-0024 ENTERED BY INSPECTION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,184 hrs · 24,520 cycles

SHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED, SUPPORT TASK. REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 40.87 IAW SRM 51-40-02 AND DWG 111A2000 SSFR REPORT FORM 46-0024 ENTERED BY INSPECTION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,184 hrs · 24,520 cycles

SHEAR FITTING AT STA 540 LBL 54.60 IS CRACKED, SUPPORT TASK. REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 54.60 IAW SRM 51-40-02 AND DWG 111A2000 SSFR REPORT FORM 46-0024 ENTERED BY INSPECTION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,184 hrs · 24,520 cycles

SHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED, SUPPORT TASK. REMOVED AND REPLACED SHEAR FITTING AT STA 540 LL 6.14 IAW SRM 51-40-02 AND DWG 111A2000 SSFR REPORT FORM 46-0024 ENTERED BY INSPECTION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,184 hrs · 24,520 cycles

SHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED, SUPPORT TASK. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 32.40 IAW SRM 51-40-02 AND DWG 111A2000 SSFR REPORT FORM 46-0024 ENTERED BY INSPECTION.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 69,076 hrs · 24,481 cycles

#1 FLIGHT COMPARTMENT WINDOW O/B POST CRACKED AT THE TOP CORNER. VERIFIED L-1 WINDOW POST CRACK. REF. FLEETCYCLE LOG PG. 9713223 SEE TASK 1,2,3. CRACK VERIFIED IAW AVO#213-19-11-29-01. L-1 WINDOW FRAME POST REPAIRED ON FLEETCYCLE LOG PAGE 9715068 ALSO IAW AVO#213-19-12-05-01 CONDITION 2. SFR REPORT NUMBER 1023218 CREATED FOR MAJOR REPAIR. FINAL ECRA 5311-02341 GENERATED. INITIATE A DTA DIP FOR THE L1 WINDOW FRAME REPAIRTO"ACCOMPLISH AN INITIAL INSP PER PART2, SECTION A ON OR BEFOREAIRCRAFT REACHI NG 50,000 TOTAL AIRCRAFT FLIGHT CYCLES. ACCOMPLISH REPETITIVE... ACCOMPLISH REPETITIVE INSPECTIOND PER PART 2, SECTION A AT INTER VALS NOT TO EXCEED 18,000 FLIGHT CYCLES THEREAFTER. A SECOND DIP REQUIRED FOR L1 WINDOW FRAME REPAIR. A DTA DIP FOR THE WINDOW FRAME REPAIR TO "ACCOMPLISH AN INITIAL INSPPER PART 2,SECTION B ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL AIRCRAFT FLIGHTCYCLES. ACCOMPLISH REPETITIVE .... PER PART 1 D. STEP 9 OF ECRA 5311-02341 PAGE 5. "INITIATE LS NOT TO EXCEED 36,000 FLIGHT CYCLES THEREAFTER." ACCOMPLISH REPETITIVE INSPECTIONS PER PART2 SECTION B AT INTERVA TOMC APPROVES DTA DIP FOR THE L1 WINDOW FRAME REPAIR TO ?ACCOMPLISH AN INITIAL INSPECTION PER PART 2, SECTION A ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL AIRCRAFT FLIGHT CYCLES. ACCOMPLISH REPETITIVE INSPECTIONS PER PART 2, SECTION A AT INTERVALS NOT TO EXCEED 18,000 FLIGHT CYCLES THEREAFTER.? PER ECRA 5311-02341 TOMC-APPROVAL FROM SC1ELBYC COMMENT THE SECOND DIP REQUIRED STATED ON THE LOG PAGE W

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 69,076 hrs · 24,481 cycles

C-SCAN ON LOWER SKIN OF THE RIGHT HORIZONTAL STAB. FOUND ONE CRACK INDICATION AT STAB STA 147.90 ABOUT 16" FROM THE AFT SPAR. (REF. F/C N/R 9713359). INITIATE DIP FOR INSPECTION REQUIREMENTS PER SRM 55-10-01 REPAIR 11 PAR. 5 TABLE 204. INITIATE DIP FOR INSPECTION REQUIREMENTS PER SRM 55-10-01 REPAIR 11 PAR. 5 TABLE 204 PG 223. INSPECTION THRESHOLD 56,000 TOTAL FLIGHT CYCLES. REPEAT INSPECTIONS- DETAILED VISUAL INSPECTION 9,000 FLIGHT CYCLES. LFEC INSPECTION 9,000 FLIGHT CYCLES. APPROVED TO LFEC INSPECTION AT AN INSPECTION THRESHOLD OF 56,000 TOTAL FLIGHT CYCLES AND REPEAT INSPECTIONS AT 9,000 FLIGHT CYCLES IN REFERENCE WITH SRM 55-10-01 REPAIR 11 PAGE 223 TABLE 204.

Part: SEAL — DAMAGED (BLEED AIR SYS) · airframe 66,636 hrs · 23,503 cycles

RT BLEED PRESS MAY BE 20 PSI MIN. R&R OF NR 2 PCCV KISS SEAL.

Part: WIRE HARNESS — FAULTY (CABIN PRESSURE) · airframe 62,705 hrs · 21,970 cycles

PRESSURIZATION CANNOT KEEP THE CORRECT CABIN PRESSURE. EMERGENCY DECLARED. CB 797(AIR CONDITIONING BLEED AIR VALVES RIGHT) ON P6 PANEL POPS. REF WDM 36-11-11 SHEET 2, ISOLATED #2 BAR BY REMOVING CONN DP1104 AT ENG 2 FIREWALL AND BREAKER DOES NOT TRIP. REMOVED AND REPLACED WIRING HARNESS MW0311 REF SSM 36-11-11 PAGE 2.1

Part: LINE — LEAKING (HYD SYSTEM) · airframe 62,405 hrs · 21,858 cycles

THE NR 1 LE SLAT TRANSIT LIGHT IS ON WITH OVERHEAD LE DEVICE PANEL SHOWING NORMAL. EMERGENCY DECLARED. REPLACED L/E SLAT, B SYSTEM PRESSURE LINE. SERVICED THE HYD SYS IAW MM 12-12-00. OPS CHECKED IAW MM 27-81-00. NO FAULTS NOTED. NO FURTHER LEAKS NOTED. OK FOR SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 62,405 hrs · 21,858 cycles

AISLE EMERGENCY LIGHT INOPERATIVE AT 26ABC. CRIMPED THE CONNECTOR ON ROW 26 ABC. OPS CHECKED GOOD,

Part: SIGN — DETACHED (SEAT 21F) · airframe 62,360 hrs · 21,836 cycles

EMERGENCY EXIT SIGN AT 21F DETACHED. INSTALLED THE SIGN.

Part: HOOK — DAMAGED (R2 DOOR GIRT BAR) · airframe 61,051 hrs · 21,318 cycles

GIRT BAR AT THE R2 DOOR WILL NOT REMAIN STOWED IN UNARMED POSITION. HOOKS ARE DAMAGED. ADJUSTED GIRT BAR HOOKS ,OK FOR SERVICE IAW MM 25-66-01-200-802.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 60,735 hrs · 21,201 cycles

ESCAPE SLIDE PACK BUSTLE LOOSE. REMOVED AND REPLACED R2 DOOR SLIDE IAW AMM 25-66-01 PAGEBLOCK 40 1 AND 25-66-01-400-801,ALL NORMAL.

Part: TRUNNION — CORRODED (LT MLG) · airframe 59,553 hrs · 20,757 cycles

LT MAIN LANDING GEAR FWD TRUNNION SUPPORT ASSEMBLY CORRODED. INSTALLED A NEW LT GEAR TRUNION FITTING IAW SRM 51-40-02, AND DRAWING 115A5002.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 58,121 hrs · 20,247 cycles

UPPER VAPOR BARRIER CRACKED IN LT WW. REPAIRED WING CTR SECTION REAR SPAR VERTICAL PRESS DECK WEB IAW SRM 57-10-10 REPAIR 3, ALTERNATIVE 2.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 54,634 hrs · 18,991 cycles

FOUND CRACK ON L ANGLE AT RBL 6.30, STATION 663.75. SEE ATTACHED 44.0008, REPAIRED L ANGLE IAW ECRA 5710-0244 8.

Part: ACOUSTIC PANEL — DEBONDED (THRUST REVERSER) · airframe 49,187 hrs · 17,129 cycles

IAW CMM 78-31-24 FIG 3 ITEM 670A. THE 315A2502-101 BOND PANEL, ACOUSTIC, HAS NUMEROUS AREAS OF DELAMINATION THAT MEASURES 75.0" X 57.0". ULTRASONIC INSPECTION IAW NDT MANUAL REVEALS SEVERAL AREAS OF DISBOND COMMON TO THE PERF SKIN. SUSPECT IMPROPER PERF SKIN PREPARATION DURING ORIGINAL BUILD.

Part: BOLT — MISSING (THRUST REVERSER)

INSPECTION OF THRUST REVERSER FOUND ONE LOOSE AND ONE MISSING BOLTS

Part: BULKHEAD — CRACKED (RT WHEEL WELL) · airframe 47,815 hrs · 16,666 cycles

RT MLG WW AT STA RBL 34 TO RBL 38-CRACK IN PRESS BULKHEAD AT APPROX S17R-S18R INSTALLED WEB REPAIR IN RT W/W REF SRM 57-10-10, REPAIR 3, ISSUED DIP TO INSPECT AREA AT INTERVAL OF 56,000 FLT CYCLES AND THEREAFTER AT 36,000 FLT CYCLES REF SRM 57-10-10. REPAIR 3 PARA 6 FOR INSP INTERVALS. ACCOMPLISH INSPECTION IAW SRM 57-10-10, REPAIR 3, PARAG 6 AT 56,000 FLT CYCLES AFTER REPAIR INSTALLATION AND EACH 36,000 FLT CYCLES THEREAFTER.

Part: RELAY — SHORTED (BOOST PUMP) · airframe 45,033 hrs · 15,720 cycles

NR 1 FUEL TANK FWD FUEL PUMP LOW PRESSURE LIGHT ILLUM IN CRUISE, GFI R19 FOUND BAD, R & R R19 IAW MM 28-22-18. R & R LT FWD BOOST PUMP AS PRECAUTION IAW MM 28-22-41-400-801. OPS AND LEAK CHECKED GOOD,

Part: SKIN — CORRODED (CARGO DOOR) · airframe 43,652 hrs · 15,210 cycles

AFT CARGO DOOR INNER SKIN CORRODED LOWER FWD CORNER, MARKED. REPAIRED AFT CARGO DOOR INNER SKIN AT LWR FWD CORNER REF ECRA 5232-01118.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

PERFORM REPAIR OF FLOOR SUPPORT INTERCOSTAL AT STA 907-927 ABOUT 10'' FROM LEFT WALL PER ECRA 5321-01778 REV A. REMOVED FASTENERS TO INITIATE REPAIR; PERFORMED HFEC ON HOLES, SPOT FACED DAMAGED AREA; FABRICATED ALL REPAIR PARTS; TREATED, PRIMED & INSTALLED REPAIR. SEE ATTACHED 44.0008 FOR WORK ACCOMPL ISHED.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 43,652 hrs · 15,210 cycles

FWD CARGO INNER DOOR SKIN CORRODED LOWER AFT CORNER. MARKED INSTALLED REPAIR DOUBLER (SEE 44.008 FOR PARTIAL WORK ACCOMPLISHED) REF EC/RA 5232-01119.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

SUPPORT TASK-INTERIOR SURFACE OF SKIN DAMAGED AT STA 386.5 AND STRINGER 27LT. REPAIR ACCOMPLISHED PER ECRA 5331-01576.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

FLOORBEAM HAS CORROSION STA 294 LBL 11 TO RBL 3 BLENDED OUT DAMAGE AND REPAIRED PER EC/RA 5321-01781 MAINTAINING 4-6 SPACING AS REQUIRED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

E&E COMPARTMENT STRINGER S27L BETWEEN STA 380-396 HAS CORROSION AROUND FASTENERS. INSTALLED STRINGER REPAIR REF ECRA 5311-01538 SEE BLOCK 38 AND ATTACHED FORMS 44.0008 FOR WORK ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

CORROSION ON FLOORBEAM STA 344 LBL 10 FWD END. REPAIR COMPLIED WITH PER ECRA 5321-01780.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

SUPPORT TASK E&E COMP S27L HAS CORROSION STA351 TO 363 B737-53-3-0712 INSTALLED STRINGER REPAIR SPLICE AND STRINGER SECTION STA336 TO 351 PER SRM53-00-03.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

E&E COMPARTMENT FUSELAGE FRAME STA 360 AND BETWEEN STRINGERS S26L-S28L HAS CORROSION (SHEAR TIE). REFERENCE LOG PAGE 9733518 N00603 REMOVED AND REPLACED SHEAR TIE AT STA 360 BETWEEN STR 26L AND 28L. REF SRM 51-40-02.

Part: STRAP — CORRODED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

E & E COMP FUSELAGE FRAME STA 360 HAS CORROSION BETWEEN S-26L AND S-28L ON UPPER SURFACE OF STRAP. PERFORM SPLICE STRAP CORROSION REPAIR PER ECRA 5331-01575.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

FLOORBEAM HAS CORROSION STA 312 LBL 11 TO LBL 22. REPAIRED FLOORBEAM STA 312 LBL 11 TO LBL 22 PER ECRA 5321-01779.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

E&E COMPARTMENT SUPPORT ANGLE BETWEEN STA 360 - 380 AND STRINGERS S27L-S26L HAS CORROSION. REMOVED AND REPLACED SUPPORT ANGLE BETWEEN STA 360-380 AND STRINGERS 27L 26L. REF-SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

E&E COMPARTMENT STRINGER 28L BETWEEN STATION 380 - 396 HAS CORROSION AROUND FASTENERS REPAIRED STRINGER 28L FROM STATION 360 TO STATION 414 REF ECRA 5311-01537 AND SRM 53-00-03 REPAIR 1.

Part: TIE DOWN — CRACKED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

A/B/B TIE DOWN RAIL CRACKED STA 767. INSTALLED REPAIR PER ECRA 5320-02039.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

SUPPORT TASK AFT CABIN FLOORBEAM AT STA 947.5 HAS HEAVY CORROSION AT LBL 48 AT AFT O/B LAV MOUNT. TRIMMED OUT DAMAGED SECTION AND INSTALLED REPAIR REF SRM 53-70-51 REPAIR 5.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

PAX CABIN HEAVY CORROSION AROUND AFT LAV O/B MOUNT ON FLOOR STRUCTURE INTERCOSTAL (MACHINED) BEWEEN STA 947.5 AND 4" FROM. REMOVED AND REPLACED INTERCOSTAL REF SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

SUPPORT TASK: FUSELAGE FRAME STA 480 RT BETWEEN STR 8R AND STR 9R CRACKED AT A/C OUTLET ASSY SUPPORT BRACKET FASTENER MOUNTING BRACKET. REPAIRED FRAME REF EA 5310-04716 REV C OP 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

SUPPORT TASK: FUSELAGE FRAME STA 400 RT BETWEEN STR 8RT & STR 9RT CRACKED AT A/C OUTLET ASSY SUPPORT BRACKET FASTENER MOUNTING HOLE. REPAIRED FRAME REF EA 5310-04716 REV C OP 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

SUPPORT TASK: FUSELAGE FRAME STA 400RT BETWEEN STR 8RT AND STR 9RT CRACKED AT A/C OUTLET ASSY SUPPORT BRACKET FASTENER MOUNTING HOLE. REPAIRED FRAME REF EA 5310-04716 REV C OP 2.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

FLOOR SUPPORT CRACKED STA 344-360 LBL 11. REMOVED AND REPLACED INTERCOSTAL STA 344-360 AT LBL 11 REF BOEING DRAWING 141A5400, SRM 51-40-2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

EA 5310-04716 OP2 FRAME 440L IS CRACKED BETWEEN STR 8 AND STR 9. REPAIRED CRACKED FRAME REF EA 5310-04716 OP 2 REV C.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

EA 5310--04716 OP 2; FRAME 827 L IS CRACKED BETWEEN STR 8 AND STR 9 REPAIR C/W EA 5310-04716 REV COP 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

EA 5310-04716 OP2 FRAME 480L IS CRACKED BETWEEN STR 8 AND STR 9. INSTALLED REPAIR REF ECRA 5310-04716 REV C OP2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

EA 5310-04716 OP2; FRAME 867L IS CRACKED BETWEEN STR 8 AND 9 INSTALLED REPAIR ANGLES REF EA 5310 -04716 REV C OP 2.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

FLOOR SUPPORT CRACKED STA 277 TO 294 BL 0. REMOVED AND REPLACED FLOOR SUPPORT REF SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

EA 5310-04716 OP2 FRAME 500 D LEFT IS CRACKED BETWEEN STR 8 AND STR 9. REPAIRED FRAME PER EA 5310-04716 REV C OP 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

EA 5310-04716 OP2 FRAME 500A LT IS CRACKED BETWEEN STR 8 AND STR 9. REPAIRED FRAME 500A LEFT BETWEEN STR 8 &9 PER EA 5310-04716 REV C OP2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

EA 5310-04716 OP 2; FRAME 400 L IS CRACKED BETWEEN STR 8 AND STR 9. INSTALLED REPAIR ANGLES.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

FLOOR SUPPORT CRACKED STA 328 TO 344 LBL 48. REMOVED AND REPLACED FLOOR SUPPORT AT STA 328 TO 344 LBL 48 REF SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

FLOOR SUPPORT CRACKED STA 312 - 328 RBL-32. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 43,652 hrs · 15,210 cycles

FLOOR SUPPORT CRACKED STA 312 TO 328 LBL 47. REMOVED AND REPLACED FLOOR SUPPORT AT STA 312 TO 328 LBL 47 REF SRM 51-40-02.

Part: SLIDE — TWISTED (L-1 DOOR) · airframe 23,795 hrs · 8,404 cycles

L-1 DOOR SLIDE DID NOT DEPLOY PROPERLY DURING AN EMERGENCY EVACUATION ON RUNWAY AFTER LANDING AT IAH. EVACUATION WAS PERFORMED DUE TO A HYD LEAK THAT CAUSED FORMATION OF HYD MIST AND FUMES IN CABIN ON LANDING AT IAH. SLIDE WAS DESCRIBED AS BEING UNUSEABLE DUE TO FACT THAT WHEN IT DEPLOYED IT BECAME "TWISTED"/WAS IN A COCKED POSITION (ONE SIDE WAS HIGHER THAN THE OTHER). L-I DOOR SLIDE WAS R/R`D IAW MM 25-66-01. ENGINEERING PERFORMED A DEPLOYMENT TEST WITH ANOTHER SLIDE AT L-I DOOR AND SLIDE DEPLOYED AND INFLATED W/O ANY PROBLEMS. SLIDE PACK CONTAINER AT L-1 DOOR WAS ALSO EXAMINED BY ENGINEERING AND NO ANOMALIES WERE FOUND. ANOTHER SLIDE WAS INSTALLED ON L-1 DOOR TO REPLACE TEST SLIDE. INVESTIGATION IS CONT

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 22,168 hrs · 7,804 cycles

INSPECTION FOUND SUPPORT BRACKET FOR BELLY PANEL RT SIDE OF A/C EXHAUST DUCT CORRODED AT STA 649.96. REPAIRED IAW ECRA 5336-01002 AND SRM 53-40-01.

Part: SPAR — CORRODED (LT WING) · airframe 22,168 hrs · 7,804 cycles

INSPECTION FOUND LT WING FRONT SPAR CORRODED AT LT NR 1 BOOST PUMP UPPER BONDING JUMPER STRAP CONTACT, WS 120-121. REPAIRED IAW ECRA 5711-01140.

Part: FRAME — CORRODED (THRESHOLD) · airframe 22,168 hrs · 7,804 cycles

INSPECTION FOUND R-1 DOOR FLOOR CUTOUT THRESHOLD FRAME CORRODED AT STA 290-300, RBL 48. THE THRESHOLD FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,168 hrs · 7,804 cycles

INSPECTION FOUND FLOORBEAM TEE CAP CORRODED AT STA 294.5, RBL 0 TO RBL 24. A REPAIR WAS INSTALLED IAW ECRA 5321-01231.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 22,168 hrs · 7,804 cycles

INSPECTION FOUND SUPPORT ANGLE CORRODED AT STA 1000, RBL 32. A NEW ANGLE WAS INSTALLED IAW DRAWING 147A5710, SRM 51-20-01, AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 22,168 hrs · 7,804 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AROUND NUT PLATE AT STA 986, LBL 43. REPAIRED IAW ECRA 5321-01230.

Part: ANGLE — CORRODED (STA) · airframe 22,168 hrs · 7,804 cycles

INSPECTION FOUND L-ANGLE CORRODED AT STA 1002, LBL 32. A NEW ANGLE WAS INSTALLED IAW DRAWING 147A5710, SRM 51-20-01, AND 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,168 hrs · 7,804 cycles

INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 380, LBL 18. A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 22,168 hrs · 7,804 cycles

INSPECTION FOUND FLOOR INTERCOSTAL CORRODED AT STA 957, RBL 48. THE FLOOR INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SKIN — GOUGED (FWD CARGO DR) · airframe 15,065 hrs · 5,168 cycles

INSPECTION FOUND A GOUGE AND DENT IN THE FORWARD CARGO DOOR EXTERNAL SKIN. THE GOUGE WAS APPROXIMATELY 6 INCHES IN LENGTH. THE DAMAGED AREA OF DOOR SKIN WAS REPAIRED IAW ECRA 5230-01709 AND SRM 52-00-01, REPAIR 3.