N433QX

Part: PCU — INOPERATIVE (NR 1 PROPELLER) · airframe 24,729 hrs · 26,861 cycles

ON CLIMB OUT BOTH PILOTS OBSERVED AN ENGINE SURGING SOUND, ITT DEG. C ON ENGINE 1 NOTICED APPROX 100 LOWER IN COMPARISON TO ENGINE 2. FUEL FLOW ON ENGINE 1 WAS HIGHER THROUGHOUT THE FLIGHT. REMOVED FROM SERVICE. REMOVED AND REPLACED #1 PROPELLER CONTROL UNIT, OVERSPEED GOVERNOR, FEATHER PUMP AND CLEANED CONNECTORS ON #1 PEC. C/W POWER ASSURANCE RUNS ON #1 AND #2 ENGINES. POWER ASSURANCE CHECKS GOOD. ALL OPERATIONAL CHECKS GOOD. NO SURGING ON #1 ENGINE. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: GENERATOR — FAILED (NR 1 AC) · airframe 24,676 hrs · 26,806 cycles

AFTER TAKE-OFF PRIOR TO ACCELERATION HEIGHT, #1 AC GEN CAUTION ILLUMINATED, AND REMAINED SO AFTER RUNNING CHECKLIST. RETURNED TO FILED, LANDING UNEVENTFUL. REMOVED FROM SERVICE. REPLACED #1 AC GEN. C/W GROUND RUN OF #1 ENG., AC GEN. OPS CHECKS AND LEAK CHECKS GOOD. AC GEN CAUTION LIGHT DID NOT ILLUMINATE DURING THE 20 MINUTE GROUND IDLE RUN REQUIRED FOR THE #1 ENG. OIL LEAK CHECK. RETURNED TO SERVICE.

Part: PCU — INOPERATIVE (NR 2 ENGINE) · airframe 24,641 hrs · 26,768 cycles

AFTER SETTING T/O POWER OBSERVED NR 2 ENGINE TORQUE AT 104%. T/O ABORTED AT LESS THAN 65 KTS. ABORTED TAKE OFF. REMOVED FROM SERVICE. NR 2 ENGINE PCU REMOVED AND REPLACED. ALL LEAK CHECK AND OPS TEST GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ROLL PIN — NOT SEATED (SERVICE DOOR) · airframe 24,573 hrs · 26,697 cycles

AFT SERVICE DOOR DIFFICULT TO OPEN FROM INSIDE. OPENS NORMALLY USING EXTERIOR HANDLE. REMOVED FROM SERVICE. FOUND EXTERIOR "AFT""PUSH" LATCH FLAP DOOR SPRING ROLL PIN NOT FULLY ENGAGED. FULLY ENGAGED ROLL PIN PULLING "PUSH" FLAP DOOR INWARD AND NO LONGER BINDED ON EXTERIOR LOCK SENSOR BRACKET WHICH CAUSED "HARD TO OPEN" DOOR FROM INSIDE. CLEANED AND LUBED ALL EXTERIOR DOOR HANDLE PARTS. OPERATIONAL TEST PERFORMED SATISFACTORY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — SURGES · airframe 24,521 hrs · 26,638 cycles

ON VERY SHORT FINAL ONE ENGINE APPEARED TO SURGE 3-4 TIMES. NO CAUTION OR WARNING LIGHTS ILLUMINATED. ED INDICATIONS WERE NOT OBSERVED AS THE SURGES HAPPENED AT VERY LOW ALTITUDE. REMOVED FROM SERVICE. PERFORMED GVI INSPECTION OF ENGINES, PROPELLERS. NO DEFECTS NOTED. INTERROGATED CDS NO FAULT MESSAGES OR RECORDED. NO FURTHER DEFECTS NOTED. A/C OK FOR RETURN TO SERVICE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: GUARD — BROKEN (SERVICE DOOR) · airframe 23,976 hrs · 25,999 cycles

AFT SERVICE DOOR VERY HARD TO OPERATE. COCKPIT INDICATION IS CYCLING ON AND OFF. SENSOR TARGET GUARD BROKEN OFF DURING TROUBLESHOOTING. FERRIED FOR REPAIRS. REMOVED FROM SERVICE. REINSTALLED TARGET GUARD IAW Q400 SRM 51-42-05. CYCLED DOOR OPENED AND CLOSED, DOOR OPERATED NORMALLY WITH GREEN INDICATION IN COCKPIT. NO FURTHER DEFECTS NOTED AT THIS TIME. OK FOR CONTINUED SERVICE.

Part: DOOR — DETACHED (EXTERNAL POWER) · airframe 23,824 hrs · 25,818 cycles

EXTERNAL DC POWER DOOR DETACHED. ( EXTERNAL DC POWER DOOR (113BL). PLACED ON DMI. RETURNED TO SERVICE.

Part: STOP — DAMAGED (DOOR HANDLE) · airframe 23,714 hrs · 25,695 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN FROM INSIDE AND OUT. OUTSIDE HANDLE MISSALIGNED WITH THE DOOR HANDLE OPENING. REMOVED FROM SERVICE. REMOVED AND REPLACED RUBBER HANDLE STOP IAW AMM 52-11-00-820-003. DOOR OPS CHECKED GOOD IAW AMM 52-11-00-710-802. RETURNED TO SERVICE.

Part: WASHER — MISSING (PAX DOOR) · airframe 23,639 hrs · 25,610 cycles

MAIN CABIN DOOR EXTERNAL HANDLE IS RECESSED INTO THE FUSELAGE SKIN. FOUND WASHER ON TIP OF THE BUMPER STOP MISSING. APPLIED NEW WASHER TO THE BUMPER STOP NR 10 IAW AMM 52-11-11-400-801. CHECKED GOOD.

Part: SENSOR — OUT OF ADJUST (CARGO DOOR) · airframe 39,597 hrs · 41,422 cycles

AFTER TAKEOFF, RECEIVED A MASTER WARNING FUSELAGE DOOR SWITH LIGHT. RAN CHECK LIST, RETURNED TO FIELD. NO PRESSURE PROBLEMS NOTED. AFT CARGO DOOR RED LIGHT ON MFD ASSOCIATED WITH MASTER WARNING. REMOVED FROM SERVICE. PSEU INDICATES ABDRLK FAULT UNRSNABLE FAR IN FAULT HISTORY. ADJUSTED INDUCTANCE CHECK OF ABDRLK PROXIMITY SENSOR TO NOMINAL NEAR RIGGING GAP TOLERANCE IAW AMM 32-61-00-280-801, GAP M/H STARTED AT 8.164, ENDED AT 8.675. OPS TEST GOOD. RETURNED TO SERVICE.

Part: BUMPER — RECESSED (PAX DOOR) · airframe 23,055 hrs · 24,953 cycles

RAMP REPORTED MAIN CABIN DOOR UNABLE TO OPEN FROM OUTSIDE DUE TO DOOR HANDLE IS RECESSED. REMOVED FROM SERVICE. FERRIED FOR REPAIRS. MCD HANDLE RECESSED DUE TO DEFECTIVE BUMPER. REPLACED BUMPER, ALL CHECKS GOOD. RETURNED TO SERVICE.

Part: SENSOR — MALFUNCTIONED (FWD CARGO DOOR) · airframe 22,785 hrs · 24,684 cycles

MASTER WARNING, FUSELAGE DOORS WARNING AND FORWARD CARGO DOOR ON DOORS PAGE ILLUMINATE INTERMITTENTLY. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. R & R THE FWD CARGO DOOR LOCK SENSOR. AIRCRAFT RETURNED TO SERVICE.

Part: SEAL — PINCHED (AFT PAX DOOR) · airframe 22,741 hrs · 24,637 cycles

RAMP REPORTED THE AFT PAX DOOR HANDLE HARD TO TURN. DOOR DOES NOT OPEN. REMOVED FROM SERVICE. FOUND SMALL AREA OF DOOR SEAL PINCHED. DOOR SEAL NOT DAMAGED. LUBRICATED THE AFT PAX DOOR SEAL ONLY IAW AMM 1220-01-640-806. NO FURTHER DEFECTS NOTED. DOOR OPENS AND CLOSES NORMALLY. AIRCRAFT RETURNED TO SERVICE.

Part: BUSHING — DAMAGED (AFT SERVICE DOOR) · airframe 22,696 hrs · 24,581 cycles

AFT SERVICE DOOR EXTREMELY DIFFICULT TO OPEN FROM THE INSIDE. REMOVED & REPLACED BUSHINGS & BEARING IN AFT SERVICE DOOR HANDLE MECHANISM PIVOT ASSY. OP'S CHECKS GOOD. RETURNED TO SERVICE.

Part: HANDLE — BROKEN (ENTRY DOOR) · airframe 22,673 hrs · 24,557 cycles

GROUND CREW REPORTS THAT THE AFT ENTRY DOOR ASSIST HANDLE IS BROKEN. REMOVED FROM SERVICE. REMOVED & REPLACED AFT ENTRY DOOR ASSIST HANDLE AS NECESSARY. DOOR OPENS AND CLOSES NORMALLY. NO OTHER DEFECTS. RETURNED TO SERVICE.

Part: FITTING — CORRODED (BS 388) · airframe 22,616 hrs · 24,498 cycles

CORROSION ON STRINGER TO FRAME FITTING, BS 388, STRINGER 24R. REMOVED & REPLACED THE FITTING IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 22,616 hrs · 24,498 cycles

RIGHT INBD FWD SEAT TRACK CORRODED. REMOVED & REPLACED THE SEAT TRACK IAW SRM 51-42-05, 51-40-15, 51-40-07, AND 51-41-05.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 22,616 hrs · 24,498 cycles

SEAT TRACK, BS 39 TO 10.50 CORRODED BEYOND LIMITS. REMOVED & REPLACED THE SEAT TRACK IAW SRM 51-42-05, 51-40-07, AND 51-41-05.

Part: SHEAR WEB — CORRODED (AFT) · airframe 22,616 hrs · 24,498 cycles

AFT SHEAR WEB CORRODED. FABRICATED A NEW AFT SHEAR WEB AND REINFORCEMENT RINGS IAW RD84-53-8502.

Part: SEAT TRACK — CORRODED (BS 670-782) · airframe 22,616 hrs · 24,498 cycles

SEAT TRACK, BS 670 - 782 CORRODED BEYOND LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-40-15-02-01, 51-42-05-02-01, AND 51-41-05-00-01.

Part: STRINGER — CORRODED (BS 216) · airframe 22,616 hrs · 24,498 cycles

CORROSION ON STRINGER 25R, BS 216. DAMAGED PORTION OF THE STRINGER WAS CUT OUT IAW RD84-53-8492. NDT CARRIED OUT IAW NDTM 6, 51-00-08-250-801 M. REPAIRED THE STRINGER IAW RD84-53-8492.

Part: SHEAR WEB — CORRODED (BS 714-783) · airframe 22,616 hrs · 24,498 cycles

AFT CARGO BAY, AFT SHEAR WEB, BS 714 TO 783 CORRODED. REMOVED THE SHEAR WEB IAW SRM 51-42-05, AND 51-40-15. FOUND TO BE OUT OF LIMITS IAW SRM 53-40-43-02-01, AND 53-40-43-02-03.

Part: SKIN — GOUGED (BS 216-234) · airframe 22,616 hrs · 24,498 cycles

GOUGE IN THE FUSELAGE SKIN BETWEEN BS 216 AND 234.5, STRINGER 18 TO 19R. CUT OUT DAMAGE IAW SRM 53-20-00-02-03. NDT CARRIED OUT IAW NDTM 6, 51-00-08-250-801. REPAIRED THE SKIN IAW SRM 53-20-00-02-03.

Part: INDICATOR — MALFUNCTIONED (CABIN PRESSURE) · airframe 22,194 hrs · 24,064 cycles

AT 22000 FT CABIN DIFF AT 5.9 PSI. CABIN ALT 3800 FT. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INTERROGATED CDS AND FOUND CP CONTROLLER, INDICATION MOD AND CPC/OF VALVE DATA FAIL FAULTS. R/R AFT OUTFLOW VALVE IAW Q400 AMM 21-31-16-000/400-801. NO HELP. REMOVED & REPLACED CABIN INDICATION MODULE IAW Q400 AMM 21-31-11-000/400-801. ALL FAULTS CODES CLEARED & DID NOT RETURN. FUNCTIONAL TEST OF PRESSURIZATION CONTROL IS GOOD IAW Q400 AMM 21-31-00-720-801. PRESSURIZATION OF A/C IN MANUAL MODE IS GOOD IAW Q400 AMM 21-00-00-863-801/802. RETURNED TO SERVICE.

Part: HOOK — BROKEN (PAX DOOR) · airframe 21,473 hrs · 23,334 cycles

AFT PASSENGER DOOR IS HARD TO OPEN AND CLOSE. REPLACED BROKEN HOOK ASSEMBLY IN THE LATCHING MECHANISM. RETURNED TO SERVICE.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 22,889 hrs · 21,038 cycles

CLIMBING THROUGH APPROXIMATELY 12000 FT CABIN DEPRESSURIZED. AFTER ABOUT 20 SECONDS, THE AIRCRAFT BEGAN TO ONCE AGAIN PRESSURIZE. FA REPORTED LOUD NOISE & COLD AIR FROM AFT PAX DOOR. NO FAULT LIGHTS OR CAUTION OR DOOR WARNING LIGHTS OBSERVED. INTERROGATED CDS AND NO FAULTS NOTED. VERIFIED NO FAULT LIGHT ON CPCP. COMPLIED WITH A GVI OF AFT PAX. DOOR SEAL GVI OF ALL DOOR SEALS, CLEANED SEALS. BLOW OUT PANELS IN AFT CARGO BAY SECURE. COMPLIED WITH A PRESSURE CHECK TO 5 PSI IAW AMM 21-00-00-863-801/802. NO SQUEAL OR ABNORMAL NOISES NOTED. A/C OK FOR CONT. SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 20,775 hrs · 22,610 cycles

FA REPORTED A BURNED RUBBER ODOR IN MID CABIN AND FWD TO THE FRONT OF THE CABIN DURING DESCENT. COMPLIED WITH INSPECTION & TESTS IAW MCN 62172-01 ISSUE NO.2 STEP 1.A.-C. COULD NOT DUPLICATE ORIGINAL DISCREPANCY. NO ODORS WHILE RUNNING ACFT & CYCLING LIGHTS & SYSTEMS. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LINE — DAMAGED (HYD SYSTEM) · airframe 20,525 hrs · 22,361 cycles

NR 2 HYD ISOLATION VALVE CAUTION ILLUMINATED. HYD SYSTEM 2 PRESSURE WAS INDICATING NORMALLY BUT HYD SYSTEM 2 QUANTITY WAS NEAR 10%. LOST OUTBOARD SPOILERS, NOSEWHEEL STEERING, AND NORMAL GEAR EXTENSION. ALTERNATE EXTENSION PERFORMED. LANDING UNEVENTFUL. REMOVED AND REPLACED DAMAGED HYDRAULIC LINE FROM NR 1 MLG WHEEL WELL. OPS TESTED GOOD. NR 2 HYD ISOLATION VALVE CAUTION DID NOT RETURN. RETURNED TO SERVICE.

Part: DITCHING DAM — UNWANTED DEPLOY (PAX DOOR) · airframe 20,091 hrs · 21,870 cycles

DITCHING DAM ON THE MAIN CABIN DOOR DEPLOYED AFTER PASSENGER BUMPED THEIR HEAD ON IT. STOWED DITCHING DAM IAW AMM 25-62-01-400-801. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: FUEL SYS — MALFUNCTIONED (NR 1 ENGINE) · airframe 20,078 hrs · 21,853 cycles

AFTER STARTING THE NR 1 ENGINE WITH THE CONDITION LEVER IN THE START AND FEATHER POSITION, THE NR 1 ENGINE FUEL PRESSURE CAUTION ILLUMINATED AND AFTER A FEW SECONDS, THE ENGINE SHUTDOWN. AIRCRAFT CURRENTLY DOWN FOR REPAIRS.

Part: LIGHT — UNSECURE (CABIN FLOOR) · airframe 19,301 hrs · 21,039 cycles

EMERGENCY LIGHT STRIP AT ROW 2D LOOSE. SECURED THE LIGHT. CHECKED GOOD. RETURNED TO SERVICE.

Part: STRUT — BENT (PAX DOOR HANDLE) · airframe 19,101 hrs · 20,824 cycles

MAIN CABIN DOOR HARD TO OPEN AND CLOSE. HINGE ON RT SIDE BROKEN. PERFORMED GVI OF MAIN CABIN DOOR, FOUND UPPER HANDRAIL STRUT ASSY BENT AND LOWER CAM LINK ASSY BOLT SHEARED ON AFT HANDRAIL. REPLACED UPPER HANDRAIL STRUT ASSY AND LOWER CAM LINK HARDWARE. REF AMM TASK 52-11-21-000/400-801. NO FURTHER DEFECTS NOTED. PERFORMED OPS TEST OF FORWARD PASSENGER DOOR IAW AMM TASK 52-11-00-710-802. OPS CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (FLT CONTROLS) · airframe 18,681 hrs · 20,369 cycles

FCS ECU 1 CIRCUIT BREAKER POPPED DURING CLIMBOUT. RETURNED TO FIELD. LANDING UNEVENTFUL. ROLL SPOILER INBD GROUND, PITCH TRIM ELEVATOR FEEL CAUTIONS ILLUMINATED ELEVATOR ASYMMETRY CAUTION ILLUMINATED ON LANDING ROLL OUT. R & R FLIGHT CONTROL ELECTRONIC CONTROL UNIT AMM TASK 27-00-01-000-802 AND 27-00-01-400-802 OPS AND FUNCTIONAL TEST GOOD. COMPLETED FREEDOM OF MOVEMENT CHECK, ENSURED FULL TRAVEL AND VERIFIED PROPER DIRECTION OF MOVEMENT, NO DEFECTS NOTED IAW GPM 9.2, FREEDOM OF MOVEMENT CHECK, BREAKER REMAINED CLOSED GPM REF 9.2.2 FCECU WAS CHANGED AS A PRECAUTIONARY MEASURE. FAULT CODES FOUND. LT POWER FAIL/CCDL. PBIT NOT RUN.

Part: COVER — DETACHED (CABIN) · airframe 18,628 hrs · 20,315 cycles

EMERGENCY LIGHT COVER OFF. REPLACED EMERGENCY LIGHT COVER. RETURNED TO SERVICE.

Part: FADEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 17,676 hrs · 19,312 cycles

ON TAKEOFF NR 2 PROP DID NOT REACH 1020 RPM UNTIL 100 KNOTS, WAS ABOUT 1012 BEFORE THEN. REPLACED THE NR 2 ENGINE FADEC. OPS CHECKS GOOD. RETURNED TO SERVICE.

Part: PROPELLER — UNKNOWN (NR 2) · airframe 17,664 hrs · 19,296 cycles

DURING TAKEOFF, NR 2 PROPELLER DID NOT REACH 1020 TILL 100 KTS. NR 2 PROP INDICATED 1010 TILL 100 KTS. NR 2 PROP WAS A LITTLE SLOW TO COME OUT OF FEATHER AT START. PERFORMED ENGINE TREND DOWNLOAD FROM EMU MTC 6773101, PERFORMED OPS TEST OF THE PROPELLER OVERSPEED GOVERNOR IAW AMM 61-20-00-710-803, PERFORMED FUNCTIONAL CHECK OF THE PROPELLER TIME TO UNFEATHER IAW AMM 61-20-00-720-801, PERFORMED PROPELLER FORWARD CONSTANT SPEED IAW AMM 71-00-00-868-813 ALL TEST PASS, NO FAULT CODES FOUND. COULD NOT DUPLICATE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (MLG) · airframe 17,133 hrs · 18,725 cycles

LT DOOR AMBER LIGHT FLASHED ON AND OFF INTERMITTENTLY DURING CLIMB. IT WAS REGULAR AT APPROXIMATELY 30 SEC INTERVALS THROUGH 8000 FT. FERRIED FOR REPAIR. INTERROGATED PSEU RIGGING HISTORY, FOUND LANDING GEAR DOOR CLEAR, NEAR GAP TOO LARGE AND INDUCTANCE READING WAS AT THE NEAR/ FAR GAP LIMIT. ADJUSTED PROXIMITY SENSOR IAW AMM 32-61-06-830-801, NOW READS WITHIN NORMAL RANGE WITH HYD PRESSURE OFF. GVI OF DOOR MECHANISM, FOUND NO EXCESSIVE PLAY.

Part: SEAT TRACK — CORRODED (NR 10) · airframe 16,652 hrs · 18,181 cycles

SEAT TRACK, NR 10 REQUIRES REPLACEMENT DUE TO CORROSION. REMOVED BONDING WIRE BUNDLE FWD AT FS X-40.00 FROM SEAT TRACK NR 10 REF SRM 51-41-00 STRUCTURE IDENT -01 TO FOM. INSTALLED BONDING WIRE BUNDLE TO FWD SEAT TRACK NR 10 AT FS X-40.00, APPROXIMATELY REF SRM 51-41-00-00-01. REMOVED AFT SPLICE ON SEAT TRACK NR 10 COMMON TO SEAT TRACK NR 11 REF SRM 51-42-05, REPAIR 01 AND 51-40-15, REPAIR 01. INSTALLED AFT SPLICE OF SEAT TRACK NR 10, COMMON TO SEAT TRACK NR 11 IAW SRM 51-42-05 AND SRM 51-40-15 AND DWG 85328201. REMOVED SEAT TRACK NR 10 PN:85328210-121, REF SRM 51-40-15, REPAIR -01 AND 51-42-00 STRUCTURE IDENT -01. INSTALLED SEAT TRACK NR 10, PN:85328210-121 REF SRM 51-40-15, REPAIR -01, SRM 51-41-00-00-01 AND DWG 85328201 REV D, DATED 96/10/23. LOCATED AND DRILLED NEW SEAT TRACK NR 10, PN:85328210-121, REF SRM 51-40-01, REPAIR -01. PERFORMED BONDING CHECK OF SEAT TRACK NR 10 IAW AMM 51-80-00-760-830. BONDING CHECKED GOOD. SEALED BONDING WIRE AT SEAT TRACK NR 10 IAW AMM 51-23-00-390-801.

Part: DOUBLER — CORRODED (SERVICE PORT) · airframe 16,652 hrs · 18,181 cycles

LAV SERVICE PORT INTERNAL DOUBLER HAS CORROSION ON AFT SIDE. BLENDED CORROSION IAW SRM 52-42-10, REPAIR -01. DAMAGE DEPTH IS .043" AS MEASURED. DAMAGE IS NOT WITHIN SPECS LISTED IN REPAIR SCHEME B, 2 OF 1400, SRM 52-42-10, REPAIR 01. REMOVED INTERNAL DOUBLER, RIVETS REMOVED FROM EXTERNAL DOUBLER, PN:85307796 TO GAIN ACCESS TO INTERNAL DOUBLER, PN:85307789 IAW SRM 51-42-05. HINGE HALF REMOVED PN:85307797-001, REF SRM 51-42-05 STEP 4E. INSTALLED HINGE HALF TO LAV SERV DOOR OPENING REF SRM 51-42-05, REPAIR -01. EXTERNAL DOUBLER EPN:85307796-101, REF SRM 51-42-05, STEP 4E. INSTALLED EXT DOUBLER PN:85307796-101 TO LAV SERV DOOR CUT OUT REF Q400 SRM 51-42-05, REPAIR -01. INSTALLED INTERNAL DOUBLER, PN:85307789-101 TO LAV SERVICE DOOR CUTOUT REF SRM 51-42-05, REPAIR -01. LOCATED AND DRILLED NEW INTERNAL DOUBLER PN:85307789-101 REF SRM 51-40-07, REPAIR 01 AND DWG 85307789, REV.-- DATED 96/11/19. APPLIED FILLET SEAL AROUND EXTERNAL DOUBLER PN:85307796-101, REF SRM 51-23-00.

Part: SEAT TRACK — CORRODED (NR 11) · airframe 16,652 hrs · 18,181 cycles

SEAT TRACK NR 11 REQUIRES REPLACEMENT DUE TO CORROSION. REMOVED AFT SPLICE COMMON TO SEAT TRACKS NR 11 AND NR 12 REF SRM 51-40-15, REPAIR -01. INSTALLED AFT SPLICE COMMON TO SEAT TRACK NR 11 AND NR 12 REF SRM 51-42-05 AND 51-40-15. REMOVED DRIP TRAY ANGLE, PN: 85307495-117 FROM SEAT TRACKS NR 11 AND NR 12, REF SRM 51-42-05, REPAIR -01. INSTALLED DRIP TRAY ANGLE COMMON TO SEAT TRACK NR 11 AND NR 12 REF SRM 51-42-05. DISPLACED DRIP TRAY FROM 5 LOCATIONS ALONG SEAT TRACK NR 11 TO FOM REF SRM 51-41-00-00-01. INSTALLED DRIP TRAY AT 5 LOCATIONS ALONG SEAT TRACK NR 11 REF SRM 51-41-00 STRUCTURE IDENT-01. REMOVED SEAT TRACK NR 11 PN:85328210-115, REF SRM 51-42-05, REPAIR -01 AND SRM 51-40-07-02-01 AND SRM 51-41-00-00-01. INSTALLED NEW SEAT TRACK 11 PN:85328210-115 IAW DWG 85328201 AND SRM 51-42-05, SRM 51-40-15 AND SRM 51-41-00. REMOVED 7 EA WIRE BUNDLE STAND OFF CLIPS FROM SEAT TRACK NR 11 REF SRM 51-42-05, REPAIR -01. INSTALLED 7 EA WIRE BUNDLE STAND OFF CLIPS ON SEAT TRACK NR 11 IAW SRM 51-42-05. LOCATED AND DRILLED NEW SEAT TRACK, PN:85328210-115 SRM 51-40-07, REPAIR -01.

Part: SEAT TRACK — CORRODED (NR 7) · airframe 16,652 hrs · 18,181 cycles

SEAT TRACK NR 7 REQUIRES REPLACEMENT, PN 85361510-103, DUE TO CORROSION. REMOVED SEAT TRACK SPLICE ANGLES AT FS X229.5 BL Y-9.250 IAW SRM 51-40-15, PARA 6M, 51-42-05 PARA 4E. INSTALLED SEAT TRACK SPLICE ANGLES AT FS 229.5 BLY-9.250 REF DWG 85307071, REV A DATED 98/10/05. REMOVED SPLICE OF SEAT TRACK NR 8 COMMON TO SEAT TRACK NR 7 IAW SRM 51-42-05 AND SRM 51-40-15. INSTALLED SEAT TRACK SPLICE ANGLES TO FS 571.00, BLY-9.250 COMMON TO SEAT TRACK NR 8 REF DWG 8530771, REV A DATED 98/10/05. LOCATED AND DRILLED NEW SEAT TRACK NR 7, PN:85361510-103, PO:THORSTK-02/126 REF DWG 85307071, REV A DATED 98/10/05 AND DWG 85361501, REV E DATED 2013-02-12. INSTALLED SEAT TRACK NR 7 STA X321 TO X469 REF SRM 51-42-05, REPAIR 01 AND DWG 85361501, REV E 2013-02-12, SRM 51-41-00 AND DWT 85361501 AND 85307071.

Part: SEAT TRACK — CORRODED (NR 12) · airframe 16,652 hrs · 18,181 cycles

SEAT TRACK NR 12, PN 85338210-112 REQUIRES REPLACEMENT DUE TO CORROSION. REMOVED AFT SPLICE COMMON TO SEAT TRACK NR 12 AND NR 13 REF SRM 51-40-15 AND SRM 51-42-050. INSTALLED AFT SPLICE COMMON TO SEAT TRACK 12 AND 13 REF SRM 51-0-15 AND SRM 51-42-005. REMOVED SEAT TRACK NR 12 REF SRM 51-40-15 AND SRM 51-41-00. RECEIVED NEW SEAT TRACK, PN:85338210-112, LOCATED AND DRILLED NEW SEAT TRACK REF SRM 51-40-07. INSTALLED SEAT TRACK NR 12 IAW SRM 51-41-00.

Part: SEAT TRACK — CORRODED · airframe 16,652 hrs · 18,181 cycles

SEAT TRACK NR 13 CORRODED. REMOVED SEAT TRACK NR 13 IAW SRM 51-42-05 AND BY REMOVING BOLTS, NUTS AND WASHERS WITH HAND TOOLS. INSTALLED SEAT TRACK NR 13 SOLID RIVETS BETWEEN STA 321.00 TO STA 469.50 IAW DWG 85361501, REV E DATED 2013-07-02. REMOVED GROUNDING WIRE AT STA 290.0 BY REMOVING BOLT AND WASHERS WITH HAND TOOLS. ATTACHED WIRE BUNDLES WITH TIE WRAPS, REF Q400 WM 20-12-10. REMOVED QTY 4 STAND OFFS BTW STA 281.00 AND STA 301.00 AND QTY 1 AT STA 255.00 IAW Q400 SRM 51-42-05. INSTALLED QTY 4 STAND OFFS BTW STA 281.00 AND 301.00 AND QTY 1 AT STA 255.00 IAW Q400 SRM 51-42-05. RECEIVED NEW SEAT TRACK PN:85361510-104 LOCATED AND DRILLED SEAT TRACK REF Q400 SRM 51-40-07. REMOVED DRIP ANGLE AFT OF STA 297.00 REF Q400 SRM 51-42-05. INSTALLED DRIP TRAY ANGLE AFT OF STA 297, REF SRM 51-42-05. INSTALLED BOLTS, WASHERS, NUTS REF SRM 51-41-00.

Part: SEAT TRACK — CORRODED · airframe 16,652 hrs · 18,181 cycles

SEAT TRACK NR 8 HAS CORROSION. REMOVED SEAT TRACK NR 8 REF SRM 51-41-00, 51-42-05. REPAIR 01 AND 51-40-15 REPAIR 01. INSTALLED ALL RIVETS COMMON TO SEAT TRACK NR 8 AND VERTICAL WEB BETWEEN FS X644.5 AND X664.5 IAW SRM 51-42-05 AND DWG 85338201. LOCATED NEW SEAT TRACK, NR 8, PN:85338210-109 AND DRILLED IAW SRM 51-40-07. REMOVED INBD AND OTBD SPLICE OF SEAT TRACK NR 8 COMMON TO SEAT TRACK NR 9 IAW SRM 51-42-05 AND SRM 51-40-15. INSTALLED INBD AND OTBD SPLICE OF SEAT TRACK NR 8 COMMON TO SEAT TRACK NR 9 IAW SRM 51-42-05, SRM 51-40-15 AND DWG 85338201. REMOVED INBD AND OTBD SPLICE OF SEAT TRACK NR 8 COMMON TO TRACK NR 7 IAW SRM 51-42-05 AND SRM 51-40-15. INSTALLED INBD AND OTBD SPLICE OF SEAT TRACK NR 8 WITH FASTENER ONLY COMMON TO SEAT TRACK NR 8, FWD SPLICE IAW SRM 51-42-05. SRM 51-40-15 AND DWG 85307071. INSTALLED ALL BOLTS ON SEAT TRACK NR 8 IAW SRM 51-41-00 AND DWG 85338201.

Part: SEAT TRACK — CORRODED · airframe 16,652 hrs · 18,181 cycles

RIGHT INBD SEAT TRACK NR 6 HAS CORROSION. REMOVED DRIP TRAY ANGLE FROM FS X 49.8 TO FSX 174.0 APPROXIMATELY AT BL Y -9.250 COMMON TO SEAT TRACK NR 6 IAW SRM 51-42-05 PAR 4E. INSTALLED DRIP TRAY ANGLE FROM FS X 49.8 TO F.S. X 174.0 APPROXIMATELY AT BLY -9.250 COMMON TO SEAT TRACK NR 6 REF SRM 51-42-05 REPAIR-01. DISPLACED WIRE BUNDLE BRACKET COMMON TO FWD SPLICE OF SEAT TRACK NR 6 AT FSX 102.5 IAW SRM 51-42-05, PAR 4E. INSTALLED WIRE BUNDLE BRACKET AT FWD SPLICE OF SEAT TRACK NR 6 COMMON TO SEAT TRACK NR 5 REF SRM 51-42-05, REPAIR-01. REMOVED FWD SPLICE ANGLE AND SPLICE BOTTOM PLATE AT FSX 102.5 COMMON TO SEAT TRACK NR 6 AND SEAT TRACK NR 5 IAW SRM'S 51-42-05, PAR 4E, 51-40-15, PAR 6M. INSTALLED FWD SEAT TRACK SPLICE, ANGLES AND BOTTOM PLATE COMMON TO SEAT TRACK 5, REF SRM 51-42-05, REPAIR 01, AND 51-40-15 REPAIR 01. DISPLACED 12 WIRE BUNDLES COMMON TO SEAT TRACK NR 6 FOR FOM. RE-ATTACHED 12 EA WIRE BUNDLES ON SEAT TRACK NR 6 REF WM 20-12-10, PGS 201-210. REMOVED SEAT TRACK NR 6 PN 85328210-111 IAW SRM'S 51-42-05, PAR 4E, 51-40-15, PAR 6M, 51-41-00, PG 1. SEAT TRACK NR 6, PN 85328210-111, INSTALLED IAW SRM 51-42-05, 51-41-00, 51-40-15, DWG 85328201, REV E, 2013/10/19. 11 EA PLASTIC STAND OFFS INSALLED ON NEW SEAT TRACK NR 6, PN 85328210-111 IAW SRM 51-40-07, 51-42-05. LOCATED AND DRILLED NEW SEAT TRACK NR 6 REF SRM 51-40-07, REPAIR-01, PN 85328010-111.

Part: SEAT TRACK — CORRODED · airframe 16,652 hrs · 18,181 cycles

SEAT TRACK NR 14 CORRODED. REMOVED SPLICE COMMON TO SEAT TRACK NR 13 AND SEAT TRACK NR 14 REF SRM 51-40-15, SRM 51-42-05 AT STA 570. INSTALLED SPLICE COMMON TO SEAT TRACK NR 13 AND NR 14 AT STA 571.0, REF DWG 85307071, REV A 98/10/06, AND SRM 51-40-15 AND SRM 51-42-005. REMOVED SEAT TRACK NR 14 BETWEEN STA 570.00 AND STA 610.00, REF SRM 51-42-05 AND REMOVAL OF BOLTS, NUTS AND WASHERS BY HAND. INSTALLED SEAT TRACK NR 14, PN:85338210-113, REF DWG 85338201, REV C DATED 96/10/07 AND INSTALLATION OF BOLTS, NUTS AND WASHERS BY HAND. LOCATED AND DRILLED SEAT TRACK NR 14, PN:85338210-113, REF SRM 51-40-07, REPAIR 1. LOCATED AND DRILLED SEAT TRACK NR 14 AT SPLICE COMMON TO SEAT TRACK NR 15, REF SRM 51-40-07.

Part: SEAT TRACK — CORRODED · airframe 16,652 hrs · 18,181 cycles

LEFT OTBD SEAT TRACK HAS CORROSION. REMOVED SEAT TRACK NR 1, REF SRM 51-42-05 AND SRM 51-40-15. RECEIVED NEW SEAT TRACK, PN:85328261-107, LOCATED AND DRILLED REF SRM 51-40-07. REMOVED AFT SPLICE OF NR 1 SEAT TRACK COMMON TO SEAT TRACK NR 2. INSTALLED AFT SPLICE OF SEAT TRACK NR 1 COMMON TO SEAT TRACK NR 2 IAW SRM 51-40-15 AND DWG 85307071. INSTALLED FASTENERS, REF SRM 51-40-15, 51-42-45 AND DWG 85328251, REV A.

Part: SEAT TRACK — CORRODED (NR 15) · airframe 16,652 hrs · 18,181 cycles

SEAT TRACK NR 15, PN 85338210-115 REQUIRES REPLACEMENT DUE TO CORROSION. REMOVED SPLICE AT STA 670.00 COMMON TO SEAT TRACK NR 15 ONLY REF SRM 51-40-15 AND SRM 51-42-05. INSTALLED SPLICE TO SEAT TRACK NR 15 AT STA X670.00, REF SRM 51-40-15, REPAIR-01, SRM 51-42-05, REPAIR-01 & DWG 85338201, REV-C, DATED 96/10/07. REMOVED SPLICE AT STA 610.00 COMMON TO SEAT TRACK NR 14 AND NR 15, REF SRM 51-40-15 AND SRM 51-42-05. INSTALLED SPLICE AT STA 610.00 COMMON TO SEAT TRACK NR 14 AND NR 15 REF SRM 51-40-15 AND SRM 51-42-05. REMOVED SEAT TRACK NR 15 BETWEEN STA 670.00 AND STA 610.00, REF SRM 51-42-05 AND BY REMOVING BOLTS AND NUTS BY HAND. INSTALLED 30 PERCENT OF SEAT TRACK NR 15, REF SRM 51-42-05, REPAIR-01 & DWG 85338201, REV-C DATED 96/10/07. LOCATED AND DRILLED SEAT TRACK NR 15, PN 85338210-115. REF SRM 51-40-07, REPAIR-01. LOCATED AND DRILLED SEAT TRACK NR 15 AT SPLICE COMMON TO SEAT TRACK NR 14 REF SRM 51-40-07. COMPLETED INSTALLATION OF SEAT TRACK NR 15, PN 85338210-115, REF SRM 51-42-05, REPAIR 01 AND DWG 85338201, REV "C-" DATED 96/10/07. RESTORED FINISH ON SEAT TRACK NR 15, REF SRM 51-25-25, REPAIR 01 AND 51-25-10 REPAIR A. COMPLIED WITH FORM - M184 ON MWC 5421021, OP 166.

Part: SEAT TRACK — CORRODED (NR 2) · airframe 16,652 hrs · 18,181 cycles

LEFT OTBD SEAT TRACK NR 2 REQUIRES REPLACEMENT, PN 85361561-103 DUE TO CORROSION. SEAT TRACK NR 2, PN:85361561-103, REMOVED IAW SRM 51-42-05, 51-42-45, 51-40-07, 51-40-15. RADIUS SHIMS REMOVED IAW SRM 51-40-15, STEP 6 M AND N. INSTALLED RADIUS SHIMS ON SEAT TRACK NR 2 REF SRM 51-40-15-02-01, STEP 6 H2. LOCATED AND DRILLED NEW FROM STOCK SEAT TRACK NR 2 PN:85361561-103, REF SRM 51-40-07. LOCATED AND DRILLED ANGLE DADO SUPPORT TO SEAT TRACK NR 2 PN:85361561-103 IAW SRM 51-40-07, DWG 85361807, REV P 13/9/10. 18 EA AIR GRILLE SUPPORT BRACKETS INSTALLED ON SEAT TRACK NR 2 IAW SRM 51-40-07, 51-42-05, 51-42-45, DWG 85361807 REV A 13/9/10. COMPLETED INSTALLATION OF SEAT TRACK NR 2, PN:85361561-103 IAW SRM 51-42-05, 51-40-15, 51-42-45, 51-45-15, SWG 824637 REV G 3/7/11, DWG 85361551, REV B 5/3/10.

Part: SEAT TRACK — CORRODED · airframe 16,652 hrs · 18,181 cycles

LEFT OTBD SEAT TRACK HAS CORROSION. 5 EA MOUNTING PLATES REMOVED FROM SEAT TRACK NR 3 IAW SRM 51-42-05, STEP 4C. INSTALLED 5 EA MOUNTING PLATES TO SEAT TRACK NR 3 REF SRM 51-40-15, STEPS F-J AND SRM 51-42-05 STEPS B-D. SEAT TRACK 3, PN 85338261-101. REMOVED IAW SRM 51-42-05, STEP 4C & 51-40-07. INSTALLED NR 3 SEAT TRACK. REF SRM 51-42-05, STEP 5 AND SRM 51-40-15, STEPS 6B-6J. SEAT TRACK NR 3, PN 85338261-101, LOCATED & DRILL IAW SRM 51-40-07, DWG 85338251, REV -A 98/11/02, DWG 8Z4637 MARCH/7/2011. JOINT PLATE, PN 85361584-113. REMOVED IAW SRM 51-42-05, STEP 4C. JOINT PLATE INSTALLED IAW SRM 51-42-05, 51-40-15, DWG 8Z4637, REV G 3/7/2011. LOCATED AND DRILLED 3 EA DADO ATTACH ANGLES ON SEAT TRACK 3, REF SRM 51-40-07, STEP 5Q-5C. REMOVED 3 EA DADO PANEL ATTACH ANGLES FROM SEAT TRACK NR 3. INSTALLED 3 EA DADO PANEL ATTACH ANGLES ON SEAT TRACK NR 3, REF SRM 51-42-05, STEPS B-D AND SRM 51-42-45, STEPS E-G.

Part: SEAT TRACK — UNKNOWN · airframe 16,652 hrs · 18,181 cycles

RIGHT OTBD SEAT TRACK NR 20 REQUIRES REPLACEMENT, PN 85338261-102 DUE TO CORROSION. REMOVED 5 EA AIR GRILLES TO FOM REF AMM 21-22-17-000-801. LT AND RT RECIRCULATING AIR GRILLS INSTALLED ON 5421021/ 218. REMOVED OTBD SEAT TRACK NR 20 REF SRM 51-42-05 REPAIR -01. 51-40-15 REPAIR -01 AND 51-42-45, REPAIR -01. SEAT TRACK NR 20 INSTALLED IN ITEMS NR 8 AND NR 9 OF THIS NRI. REMOVED 6 EA AIR GRILL SUPPORT ANGLES REF SRM 51-42-05, REPAIR -01 AND 51-4-15, REPAIR 01. INSTALLED 5 EA RECIRCULATING AIR GRILLE SUPPORT ANGLES REF SRM 51-42-05, REPAIR -01 AND 51-40-15, REPAIR-01. REMOVED 3 EA SPLICE PLATES REF SRM 51-42-05, REPAIR -01 AND 51-40-15, REPAIR -01. INSTALLED 1EA SPLICE PLATE REF SRM 51-42-05, REPAIR -01. COMPLETED REMOVAL OF 3 DADO PANEL SUPPORT ANGLES COMMON TO SEAT TRACK NR 20 IAW SRM 51-42-05, PARA 4E. REINSTALLED 3 DADO PANEL SUPPORT ANGLES COMMON TO SEAT TRACK NR 20 IAW SRM 51-42-05 IAW PARA 4D. RECEIVED NEW SEAT TRACK NR 20 PN:85338261-1025P PO: TX-2375, LOCATED AND DRILLED NEW SEAT TRACK, NR 20, PN:85338261-102SP IAW SRM 51-40-7, PARA 5B. INSTALLED ALL HI-LITE FASTENERS COMMON TO SEAT TRACK NR 2 IAW SRM 51-40-15, PARA 6H, 6J AND DWG 85338251, REV A. INSTALLED ALL SOLID RIVETS COMMON TO SEAT TRACK NR 20 AND 1EA SPLICE PLATE REF SRM 51-42-05, REPAIR -01. INSTALLED 2 EA SPLICE PLATES AND 1 EA RECIRCULATION AIR GRILL SUPPORT ANGLE REF SRM 51-40-15-02-01, STEP 6 NR 2.

Part: BEAM — CORRODED · airframe 16,652 hrs · 18,181 cycles

INNER EDGE BEAM, CORRODED AND REQUIRES REPLACEMENT. LOCATED AND DRILLED NEW INNER EDGE BEAM IAW SRM 51-40-07, REPAIR-01. APPLIED ALUMIZIED TOP COAT ON NEW INNER EDGE BEAM REF SRM 51-25-25 REPAIR-01. COMPLIED WITH CPCP M-184 FORM .

Part: SEAT TRACK — UNKNOWN · airframe 16,652 hrs · 18,181 cycles

RIGHT OTBD SEAT TRACK, NR 19, REQUIRES REPLACEMENT, PN 85361561-104, DUE TO CORROSION. REMOVED SEAT TRACK NR 19, REF SRM 51-42-05 AND 51-40-15, REPAIR-01. LOCATED AND DRILLED HOLES ON NEW SEAT TRACK NR 19, PN: 85361561-104, PO: TX2326, REF SRM 51-40-07-02-01. LOCATED, DRILLED & DEBURRED SEAT TRACK NR 19, REF SRM 51-40-07, REPAIR-01. INSTALLED SEAT TRACK NR 19 REF SRM 51-42-05, SRM 51-40-15. REPAIR-01 & DWG 85361551, REV-B, DATED 96/08/13.

Part: SEAT TRACK — UNKNOWN · airframe 16,652 hrs · 18,181 cycles

SEAT TRACK, NR 18 REQUIRES REPLACEMENT, PN 85328261-105, DUE TO CORROSION. REMOVED AFT SPLICE COMMON TO SEAT TRACKS NR 18 & NR 19. REF SRM 51-40-15, REPAIR-01 & SRM 51-42-05 REPAIR-01. INSTALLED AFT SPLICE COMMON TO SEAT TRACKS NR 18 & NR 19, REF SRM 51-40-15 REPAIR-01 & SRM 51-42-05, REPAIR-01. REMOVED 8 EA RADIUS BLOCKS FROM SEAT TRACK NR 18 REF SRM 51-40-15, REPAIR-01. INSTALLED 8 EA RADIUS BLOCKS ON NEW SEAT TRACK NR 18 REF SRM 51-40-15-02-01, STEP 6H2. REMOVED 8 EA AIR GRILLE BRACKETS FROM SEAT TRACK NR 18, REF SRM 51-42-05, REPAIR-01. INSTALLED 8 EA AIR GRILLE BRACKETS COMMON TO SEAT TRACK NR 18 REF SRM 51-42-05, REPAIR-01. REMOVED SEAT TRACK 18, PN 85328261-105, REF SRM 51-42-05 REPAIR-01 AND SRM 51-40-07, REPAIR-01. INSTALLED 10 PERCENT OF FASTENER ON NEW SEAT TRACK NR 18, PN 85328261-105, REF SRM 51-42-05-02-01, STEP 4D, 3-10 AND SRM 51-40-015-02-01, STEP 6H2. REMOVED 3 EA DADO PANEL SUPPORT ANGLES FROM SEAT TRACK NR 18, REF SRM 51-42-05, REPAIR-01. INSTALLED 3EA DADO PANEL SUPPORT ANGLES TO SEAT TRACK NR 18, REF SRM 51-42-05, REPAIR-01. LOCATED DRILLED AND DEBURRED NEW SEAT TRACK NR 18, PN: 85328261-105, PO TX 2182, REF SRM 51-40-07-02-01. INSTALLED NEW SEAT TRACK, PN 85328261-105, REF SRM 51-42-05 REPAIR-01 & DWG 85328251, REV-A DATED 96/08/23.

Part: BEAM — CORRODED · airframe 16,652 hrs · 18,181 cycles

OUTER EDGE BEAM, CORRODED AND REQUIRES REPLACEMENT. LOCATED AND DRILLED NEW OUTER EDGE BEAM, IAW SRM 51-40-07, REPAIR 01. APPLIED ALUMINIZED TOP COAT TO NEW OUTER EDGE BEAM REF SRM 51-25-25, REPAIR-01. COMPLIED WITH FORM M-184.

Part: PROPELLER — MALFUNCTIONED (NR 2) · airframe 15,926 hrs · 17,379 cycles

TAKEOFF ABORTED DUE TO NR 2 PROPELLER ONLY REACHING 1010 RPM. ALL OTHER ENGINE INDICATIONS NORMAL. SPEED 97 KNOTS. CHECKED CDS FOR FAULT CODES, NOT FOUND. C/W POWER ASSURANCE ENGINE RUN FOR NR 2 ENGINE AND APPLICABLE ENGINE RUNS. COULD NOT DUPLICATE DISCREPANCY. R & R NR 2 OSG AS A PRECAUTION IAW AMM 61-20-26-000-801 AND 61-20-26-400-801. ALL CHECKED GOOD. RETURNED TO SERVICE.

Part: ACCESS PANEL — CORRODED (WING) · airframe 14,576 hrs · 15,979 cycles

NUMEROUS COUNTERSINKS ON FUEL PANEL 622BT HAS PITTING CORROSION. REMOVED CORROSION FROM COUNTERSINKS ON FUEL PANEL 622BT MEASURED FASTER HEAD AT .0195 BELOW FLUSH IAW TUC6161. PANEL OUT OF LIMITS, IAW SRM 57-10-35, REPAIR-03. PANEL INSTALLED.

Part: STOP FITTING — CORRODED (SERVICE DOOR) · airframe 14,576 hrs · 15,979 cycles

AFT SERVICE DOOR NR 9 AFT STOP FITTING NUT PLATE ARE CORRODED. REMOVED DAMAGED NUT PLATES ON AFT SERVICE DOOR STOP FITTING NR 9, LOCATIONS B AND D AND INSTALLED NUTS, IAW SRM 52-00-00 ALLOW DAMAGE.

Part: ACCESS PANEL — CORRODED (WING) · airframe 14,576 hrs · 15,979 cycles

NUMEROUS COUNTERSINKS ON FUEL PANEL 522BT HAVE PITTING CORROSION. REMOVED CORROSION FROM COUNTERSINKS ON FUEL PANEL 522BT MEASURED FASTENER HEAD AT .0175 BELOW FLUSH IAW TUC6161. PANEL OUT OF LIMITS IAW SRM 57-10-35, REPAIR-03. PANEL INSTALLATED.

Part: ACCESS PANEL — CORRODED (WING) · airframe 14,576 hrs · 15,979 cycles

NUMEROUS COUNTERSINKS ON FUEL PANEL 622CT HAVE PITTING CORROSION. REMOVED CORROSION FROM COUNTERSINKS ON FUEL PANEL 622CT MEASURED FASTENER HEAD AT .021 BELOW FLUSH IAW TUC6161. PANEL OUT OF LIMITS, REF SRM 57-10-35, REPAIR-03. PANEL INSTALLED.

Part: STOP FITTING — CORRODED (SERVICE DOOR) · airframe 14,576 hrs · 15,979 cycles

AFT SERVICE DOOR NR 7 AFT STOP FITTING ARE CORRODED. C/W FORM M-184 CORROSION REPORT. REMOVED DAMAGED NUT PLATES ON AFT SERVICE DOOR STOP FITTING NR 7 LOCATIONS B AND D AND INSTALLED NUTS, IAW SRM 52-00-00 ALLOW DAMAGE.

Part: STOP FITTING — CORRODED (SERVICE DOOR) · airframe 14,576 hrs · 15,979 cycles

AFT SERVICE DOOR NR 3 FWD STOP FITTING NUT PLATES ARE CORRODED. C/W FORM M-184 CORROSION REPORT. REMOVED DAMAGED NUT PLATES ON AFT SERVICE DOOR STOP FITTING NR 3 LOCATIONS B AND D AND INSTALLED NUTS, IAW SRM 52-00-00 ALLOW DAMAGE.

Part: ACCESS PANEL — CORRODED (WING) · airframe 14,576 hrs · 15,979 cycles

MULTIPLE COUNTERSINKS ON FUEL PANEL 623AT HAVE PITTING CORROSION. REMOVED CORROSION FROM COUNTERSINKS ON FUEL PANEL 623AT, MEASURED FASTENER HEAD AT .016 BELOW FLUSH IAW TUC6161. PANEL OUT OF LIMITS, IAW SRM 57-10-35. REPAIR -03. PANEL INSTALLED.

Part: STOP FITTING — CORRODED (SERVICE DOOR) · airframe 14,576 hrs · 15,979 cycles

AFT SERVICE DOOR NR 2 FWD STOP FITTING NUT PLATES ARE CORRODED. C/W FORM M-184 CORROSION REPORT. REMOVED DAMAGED NUT PLATES ON AFT SERVICE DOOR STOP FITTING NR 2 LOCATIONS B AND D AND INSTALLED NUTS, PN: MS21042L3 REF SRM 52-00-00 ALLOW DAMAGE.

Part: STOP FITTING — CORRODED (SERVICE DOOR) · airframe 14,576 hrs · 15,979 cycles

AFT SERVICE DOOR NR 8 AFT STOP FITTING NUT PLATES ARE CORRODED. C/W FORM M-184 CORROSION REPORT. REMOVED DAMAGED NUT PLATES ON AFT SERVICE DOOR STOP FITTING NR 8 LOCATIONS B AND D AND INSTALLED NUTS, IAW SRM 52-00-00 ALLOW DAMAGE.

Part: STOP FITTING — CORRODED (SERVICE DOOR) · airframe 14,576 hrs · 15,979 cycles

AFT SERVICE DOOR NR 4 FWD STOP FITTING NUT PLATES ARE CORRODED. C/W FORM M-184 CORROSION REPORT. REMOVED DAMAGED NUT PLATES ON AFT SERVICE DOOR STOP FITTING NR 4 LOCATIONS B AND D AND INSTALLED NUTS IAW SRM 52-00-00 ALLOW DAMAGE.

Part: ACCESS PANEL — CORRODED (WING) · airframe 14,576 hrs · 15,979 cycles

NUMEROUS COUNTERSINKS ON FUEL PANEL 523AT HAVE PITTING CORROSION. REMOVED CORROSION FROM COUNTERSINKS ON FUEL PANEL 523AT MEASURED FASTENER HEAD AT .0165 BELOW FLUSH IAW TUC6161. PANEL OUT OF LIMITS, IAW SRM 57-10-35, REPAIR -03. PANEL INSTALLED.

Part: ACCESS PANEL — CORRODED (WING) · airframe 14,576 hrs · 15,979 cycles

NUMEROUS COUNTERSINKS ON FUEL PANEL 522CT TO HAVE CORROSION. REMOVED CORROSION FROM COUNTERSINKS ON FUEL PANEL 522CT MEASURED FASTENER HEADS AT .0165 BELOW FLUSH IAW TUC6161. PANEL OUT OF LIMITS, IAW SRM 57-10-35, REPAIR-03. PANEL INSTALLED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,474 hrs · 15,858 cycles

F/A REPORTS THAT EMERGENCY LIGHTING "GREEN" LAMP NOT ILLUMINATED, REPLACED THE LAMP. OPS CHECKED NORMAL. RETURNED TO SERVICE.

Part: DOOR — BINDING (MAIN CABIN) · airframe 13,841 hrs · 15,183 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. ACFT DOWN FOR REPAIRS.

Part: UNKNOWN — ODOR (CABIN) · airframe 13,838 hrs · 15,180 cycles

MULTIPLE REPORTS OF ELECTRICAL BURNING ODOR FROM REAR OF ACFT. INITIALLY WAS UNABLE TO DETECT ANY ELECTRICAL BURNING. REMOVED GALLEY CONTROL PANEL IAW AMM 25-33-06-000-802. PERFORMED GVI OF ALL PLUGS WITH NO DEFECT OR BURNING ODOR NOTED. REINSTALLED GCP IAW 25-33-06-400-802. PERFORMED OPS TEST OF GCP IAW AMM 25-34-00-710-801. OPS TESTED GOOD. ALL LIGHTS AND COFFEE WARMER ON FOR AT LEAST 20 MIN WITH NO BURNING ODOR NOTED. CYCLED LIGHTS AND COFFEE WARMER FEW TIMES WITH NO DEFECTS NOTED. PERFORMED OPS TEST OF PSU IAW AMM 21-22-00-710-801. OPS CHECKED GOOD. RECIRCULATION FAN WORKS NORMAL. NO BURNING ODOR NOTED. PERFORMED OPS TEST OF PASSENGER COMPARTMENT LIGHTING IAW AMM 33-20-00-710-802. OPS CHECKED GOOD. DURING OPS CHECKED INSPECTED AFT CARGO LIGHTING WITH NO DEFECT & NO BURNING ODOR NOTICED. R & R CANTED BULHEAD IAW AMM 25-52-01-000/400-802 TO INSPECT OUTFLOW VALVE. NO BURING ODOR NOTED. RAMPERS REPORT BURING RUBBER ODOR FROM ANOTHER A/C LANDING. COULD NOT DUPLICATE. RETURNED TO SERVICE.

Part: WINDOW — ARCED (COCKPIT) · airframe 13,486 hrs · 14,824 cycles

OBSERVED ELECTRICAL SPARKS AT THE BASE OF SIDE WINDOW WHEN "PLT SIDE WDO HT" SWITCH WAS ON. SPARKING STOPS WHEN "PLT SIDE WDO/HT" SWITCH IS OFF. PERFORMED PILOT SIDE WINDOW HEAT OPS TEST AMM 30-41-00-710-802. CONFIRMED BASE OF WINDOW HEATING ELEMENT ARCING. REMOVED AND INSTALLED SERVICEABLE PILOT SIDE WINDOW IAW AMM 56-10-06-000-801 AND 56-10-06-400-801. OPS TEST GOOD. NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: SKIN — DENTED (BS 295) · airframe 13,264 hrs · 14,597 cycles

DENT AT BS 295, BELOW STRINGER 16R. PERFORMED HFEC NO CRACKS NOTED. WITHIN LIMITS FOR TEMP REPAIR IAW SRM 53-00-00, REPAIR 06.

Part: SKIN — DENTED (BS 321) · airframe 13,264 hrs · 14,597 cycles

DENT AT BS 321, BELOW STRINGER 16RT. PERFORMED HFEC NO CRACKS NOTED. WITHIN LIMITS FOR TEMP REPAIR IAW SRM 53-00-00, REPAIR 06.

Part: WARNING MESSAGE — FALSE ACTIVATION (HYD PUMP) · airframe 13,200 hrs · 14,529 cycles

AFTER TAKEOFF, DURING GEAR RETRACTION, NR 2 ENGINE HYD PUMP CAUTION ILLUMINATED, THEN WENT OUT AFTER GEAR RETRACTED. LT MAIN DOORS SLOW TO CLOSE. HEARD A STRANGE STRAINING HYD SOUND NEAR NOSE. REAR F/A ALSO HEARD A STRAINING SOUND IN REAR OF ACFT. RETURNED TO FIELD. LANDING UNEVENTFUL. JACKED ACFT, FUNCTIONAL TEST OF LANDING GEAR PRIMARY EXTENSION AND RETRACTION SYS. BLED NR 2 SYS HYD, GEAR RETRACTION IS NORMAL, GEAR DOORS OPERATED NORMAL, NO STRANGE HYD SOUNDS WERE IDENTIFIED. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: BOLT — MISSING (PAX DOOR) · airframe 12,578 hrs · 13,846 cycles

BOLT MISSING FROM MAIN CABIN DOOR. INSTALLED CORRECT BOLT IAW IPC REF 52-11-01 AND TORQUED BOLT IAW AMM 52-11-06-400-801 STEP 4 B (4) NO OTHER RETAINING HARDWARE REMOVED, NO ADJUSTMENTS MADE TO DOOR STOPS. RETURNED TO SERVICE.

Part: WARNING LIGHT — MULTIPLE FAIL (HYD SYSTEM) · airframe 11,766 hrs · 12,964 cycles

NR 2 HYD PRESSURE AT 0. NR 2 HYD ISO, ROLL SPOILER HYD SPOILER OTBD. NR 2 RUDDER HYD CAUTION LIGHTS ILLUMINATED, CIRCUIT BREAKERS ALL IN. COMPLIED WITH FIM TASK 29-10-00-810-804, STEPS 1 THRU 4A (1) FOUND LARGE AMOUNT OF AIR IN NR 2 HYD SYSTEM, BLEED HYD SYS IAW AMM TASK 29-10-00-870-802, STEPS 1 TO 4C CHECKS NORMAL. RETURNED TO SERVICE.

Part: HINGE — BROKEN (JUMPSEAT) · airframe 11,722 hrs · 12,919 cycles

DURING PREFLIGHT INSPECTION, FWD F/A REPORTS STORAGE COMPARTMENT DOOR UNDER FWD F/A JUMPSEAT DOES NOT RETRACT ON IT'S OWN. R & R DOOR HINGE ASSY. OPS CHECKS NORMAL. RETURNED TO SERVICE.

Part: STRUT — DIRTY (PAX DOOR) · airframe 10,908 hrs · 12,091 cycles

MAIN CABIN DOOR HARD TO OPEN FROM THE INSIDE. REMOVED HANDRAIL UPPER STRUT ASSY FWD AND AFT IAW AMM 52-11-21-000-801, PARA 4E (1), (2), (6), AND (7). CLEANED DIRT FROM FWD AND AFT HUB SHAFTS AND UPPER FWD AND AFT STRUT/NEWEL ASSY'S. REINSTALLED UPPER STRUT/NEWEL ASSY'S IAW AMM TASK 52-11-21-400-801, PARA 1-3, 4F (1), (2), (5), (6), AND (7). OPERATED DOOR FROM INSIDE AND OUTSIDE FOR SEVERAL CYCLES EACH. DOOR OPS CHECKED GOOD. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: SEAL — BINDING (PAX DOOR) · airframe 10,856 hrs · 12,033 cycles

AFT HANDRAIL OF THE MAIN CABIN DOOR RUBS AGAINST THE SIDEWALL AND MAKES THE DOOR HARD TO OPEN. FOUND SEAL ON FWD DRAFT BULKHEAD BINDING, PUSHING OUT BULKHEAD. LOOSENED TOP LATCH & RESET SEAL & RELATCHED FWD DRAFT BULKHEAD IAW AMM TASK 25-24-06-000-802, STEPS 1-3 & 4(A) 1&2. OPS CHECK GOOD IAW AMM TASK 52-11-00-710802, STEPS 1-3A. NO OTHER DEFECTS NOTED. NO PARTS REPLACED. RETURNED TO SERVICE.

Part: HINGE — LOOSE (COCKPIT DOOR) · airframe 10,809 hrs · 11,982 cycles

COCKPIT DOOR JAMMED IN FLIGHT. IT TOOK SEVERAL ATTEMPTS TO OPEN. DOOR AND CATCHIMG ON LAV DOOR- NOTED SCRAPE MARKS. REMOVED FLIGHT (DOOR) COMPARTMENT IAW 52-51-06-000-801, AND REINSPECTED FLIGHT COMPARTMENT DOOR, AND HINGES HARDWARE, FOUND TOP HINGE HARWARE LOOSE. RESECURED TOP HINGE HARDWARE WITH LOCTITE. REINSTALLLED FLIGHT COMPARTMENT DOOR IAW TASK 52-51-06-400-801 GAP WITH LIMITS. NO OTHER DEFECT NOTED. OPS TEST GOOD. NO JAMMING OF COCKPIT DOOR AND LAV DOOR NOTED. RETURNED TO SERVICE.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

FORWARD PAX DOOR THRESHOLD AND THRESHOLD SUPPORT ARE CORRODED. REMOVED FWD PAX DOOR THRESHOLD AND THRESHOLD SUPPORT CHANNEL IAW SRM 51-42-05-02-01. DRILLED NEW THRESHOLD AND THRESHOLD SUPPORT CHANNEL IAW SRM 51-40-07-02-01. INSTALLED THRESHOLD AND THRESHOLD SUPPORT CHANNEL IAW SRM 51-42-05-02-01. APPLIED SURFACE PROTECTION IAW SRM 51-25-10-02-01, 51-25-15-02-01 AND 51-21-10-02-01.

Part: SKIN — CHAFED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

FUSELAGE SKIN CHAFED. SMOOTHED OUT CHAFING DAMAGE IAW TC SB84-53-45. MIN NOTED THICKNESS .047" CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. MAPPED DAMAGE AND SUBMITTED TO ENGINEERING. REPAIRED CHAFE DAMAGE IAW RD 8/4-53-5052. FABRICATED SHIM IAW RD 8/4-53-5053. ACCOMPLIED TASK CARD SB84-53-45. COMPLIED WITH TC RD 8/4-53-5052.

Part: SKIN — GOUGED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

EXTERNAL SKIN HAS SMALL GOUGES AT FRAME 49.5 STR 30P. MEASURED DAMAGE AND FOUND IN LIMITS IAW RD 8/4-53-666. VERIFIED MIN THICKNESS REMAINING, MATERIAL LOSS FOUND IN LIMITS IAW SRM 53-20-31-01-02. VERIFIED AFFECTED AREA CRACK FREE USING HFEC REF NTM 51-00-01-250-801 PT 6. DAMAGE WITHIN LIMITS IAW RD 8/4-53-5025. ALODINED, PRIMED AND TOP COATED IAW RD 8/4-53-5025. APPLIED YELLOW DOT IAW GPM 10.11.3. COMPLIED WITH TC RD 8/4-53-5025.

Part: STRUCTURE — DAMAGED · airframe 10,790 hrs · 11,967 cycles

FWD LANDING STRIP ON 262AT MATING SURFACE HAS FRETTING. BLENDED OUT DAMAGE ON PANEL AND LANDING IAW SRM 53-75-06-02-01. MIN NOTED THICKNESS .063" CONFIRMED BLENDS CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. TREATED, PRIMED IAW SRM 53-75-06-02-01. ALODINED LANDING IAW SRM 51-21-10-02-01. REPLACED RIVETS AS REQUIRED IAW SRM 51-42-05-02-01. FILLED BLENDS FLUSH IAW SRM 51-22-20-02-01 AND APPLIED PRIMER IAW SRM 51-25-10-02-01. COMPLIED WITH TC RD 8/4-57-1980.

Part: SKIN — DENTED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

EXTERNAL SKIN HAS A DENT AT FRAME 32.4, STR 31S. DENT FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-666. BLENDED IAW RD 8/4-53-666. MIN NOTED THICKNESS .055", CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. DAMAGE IS IN LIMITS IAW RD 8/4-53-5025. ALODINED, PRIMED AND TOP COATED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01 AND 51-25-05-02-01. COMPLIED WITH TC RD 8/4-53-5025.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

FLOOR SUPPORT CORRODED AT THE AFT END OF THE FORWARD BAG DOOR. REMOVED CORROSION IAW SRM 51-21-00-00-02. VERIFIED AFFECTED AREA TO BE CRACK FREE USING HFEC REF NTM PT 1 51-00-06-910-801. ALODINE, PRIMED AND TOP COATED IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND 51-25-15-02-01. APPLIED CPC IAW AMM 51-25-01-390-801. ALL WORK PERFORMED IAW RD 8/4-53-5050. SUPPORT RAIL IS IN LIMITS OF RD 8/4-53-5050. MIN MATERIAL REMAINING .038" ORIGINAL THICKNESS WAS .040" IAW SRM 53-20-43-00-01. COMPLIED WITH TC RD 8/4-53-5050.

Part: SKIN — GOUGED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

EXTERNAL SKIN HAS SMALL GOUGES AT FRAME 49.5 STR 33. MEASURED AND FOUND OUT OF LIMITS IAW RD 8/4-53-666. REMOVED RIVETS FOM IAW RD 8/4-53-666. MIN REMAINING THICKNESS .046" CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. DAMAGE IS WITHIN LIMITS IAW RD 8/4-53-5025. INSTALLED RIVETS IAW IAW SRM 51-42-05-02-01. ALODINED, PRIMED, TOP COATED IAW RD 8/4-53-5025. APPLIED CPC IAW AMM 51-25-01-390-801. APPLIED YELLOW DOT IAW GPM 10.11.3.

Part: SKIN — GOUGED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

EXTERNAL SKIN HAS SMALL GOUGE AT FRAME 71.2 STR 33. MEASURE GOUGE AND FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-666. MIN REMAINING THICKNESS NOTE .052", CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. DAMAGE IS WITHIN LIMITS IAW RD 8/4-53-5025. ALODINED, PRIMED AND TOP COATED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01 AND 51-25-15-02-01. APPLIED YELLOW DOT IAW GPM 10.11.3. COMPLIED WITH TC RD 8/4-53-5025.

Part: STRINGER — CORRODED (BS 584.5 S24L) · airframe 10,790 hrs · 11,967 cycles

STRINGER 24P HAS CORROSION BS 584.5. REMOVED CORROSION IAW SRM 51-21-00-00-02. MIN THICKNESS REMAINING NOTED .044, REF NTM 51-00-04-910-801 PT 1. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. DAMAGE FOUND TO BE WITH IN LIMITS IAW RD 8/4-53-5040. APPLIED ALODINE, PRIMER, TOP COAT AND CPC IAW RD 8/4-53-5040. COMPLIED WITH TC RD 8/4-53-5040.

Part: THRESHOLD — CORRODED (EMERGENCY EXIT) · airframe 10,790 hrs · 11,967 cycles

EMERGENCY EXIT THRESHOLD IS CORRODED. REMOVED DOOR THRESHOLD IAW SRM 51-41-00-00-01. REMOVED DOOR SUPPORT Z CHANNEL IAW SRM 51-42-05-02-01. NO REPAIRS ALLOWED IN WORK AREA IAW SRM 53-20-21-00-01. MATCH DRILLED NEW PART IAW SRM 51-40-07-02-01. INSTALLED NUT PLATES IAW SRM 51-42-05-02-01. INSTALLED SUPPORT Z CHANNEL IAW SRM 51-42-05-02-01, 51-42-45-02-01. INSTALLED THRESHOLD IAW SRM 51-41-05-00-01. APPLIED PROTECTIVE SURFACE PAINT IAW SRM 51-25-15-02-01. APPLIED CPC IAW AMM 51-25-01-390-801. REINSTALLED THRESHOLD PLATE IAW SRM 51-41-05-00-01.

Part: SKIN — GOUGED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

EXTERNAL SKIN HAS SMALL GOUGE AT FRAME 32.4 STR 32S. BLENDED GOUGE IAW RD 8/4-53-666. MIN REMAINING THICKNESS NOTED .052", CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. DAMAGE IS IN LIMITS IAW RD 8/4-53-5025. ALODINED, PRIMED AND TOP COATED IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND 51-25-05-02-01. APPLIED YELLOW DOT IAW GPM 10.11.3. COMPLIED WITH RD 8/4-53-5025.

Part: STRUCTURE — DAMAGED · airframe 10,790 hrs · 11,967 cycles

FWD LANDING STRIP ON 262HT MATING SURFACE HAS FRETTING. BLENDED OUT DAMAGE. COMPLIED WITH TC RD 8/4-57-1980. SRM 53-75-46-02-01 MIN THICKNESS NOTED .065, CONFIRMED AFFECTED AREAS CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. TREATED, PRIMED IAW SRM 53-75-06-02-01. REPLACED RIVETS AS REQUIRED IAW SRM 51-42-05-02-01. ALODINED IAW SRM 51-21-10-02-01. FILLED BLENDS FLUSH IAW SRM 51-22-20-02-01 AND APPLIED PRIMER IAW SRM 51-25-10-02-01. APPLIED TEFLON TAPE IAW SRM 57-10-05-02-01. FOUND LANDING STRIP SURFACE CONDITION TO BE WITHIN LIMITS IAW RD 8/4-57-1980.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

SERVICE DOOR FWD FRAME HAS MULTIPLE AREAS OF MISSING SURFACE PROTECTION AND POSSIBLE CORROSION. BLENDED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. RESTORED SURFACE PROTECTION IAW SRM 51-25-10-02-01. APPLIED TOP COAT AND CPC IAW SRM 51-25-15-02-01 AND AMM 51-25-01-390-801. FOUND BLENDS TO BE WITHIN LIMITS IAW RD 8/4-52-867. COMPLIED WITH RD 8/4-52-867.

Part: SKIN — CORRODED (BS 547-567.5) · airframe 10,790 hrs · 11,967 cycles

SKIN STRAP OTBD OF STRINGER 32P IS CORRODED STA 547-564.5. REMOVED RIVETS IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW SRM 51-21-00-00-02. MIN THICKNESS.048" REF NTM 51-00-04-910-801, PT 1. VERIFIED AFFECTED AREA CRACK FREE USING HFEC REF NTM 51-00-01-250-801. FOUND TO BE IN LIMITS IAW RD 8/4-53-5041. INSTALLED NEW RIVETS IAW SRM 51-42-05-02-01. ALODINED, PRIMED, TOP COATED AND CPC'D IAW RD 8/4-53-5041 AND AMM 51-25-01-390-801. COMPLIED WITH RD 8/4-53-5041.

Part: SKIN — CORRODED (BS 116 S32L) · airframe 10,790 hrs · 11,967 cycles

SKIN STRAP SPLICE ON OTBD SIDE OF STRINGER 32P HAS CORROSION FWD OF STA 116. BLENDED OUT CORROSION IAW SRM 51-21-00-00-02. REMOVED RIVETS FOR ACCESS TO CORROSION IAW SRM 51-42-05-02-01. CONFIRMED BLENDED AREAS CRACK FREE USING HFEC REF NDTM PT 6 TASK 51-00-01-250-801. MIN REMAINING THICKNESS .047" REF NDTM PART 1 TASK 51-00-04-910-801. MATERIAL LOSS FOUND TO BE WITH IN LIMITS RD 8/4-53-5038. INSTALLED RIVETS IAW SRM 51-42-05-02-01 AND COMPLIED WITH RD 8/4-53-5038.

Part: FRAME — DAMAGED (BS 236) · airframe 10,790 hrs · 11,967 cycles

FRAME 236, FLANGE HAS TOOLING DAMAGE STRINGER 30P-31P. REMOVED FASTENER FOM IAW SRM 51-42-05-02-01. VERIFIED AFFECTED AREA TO BE CRACK FREE REF NTM 51-00-06-910-801 PT 1. FOUND CREASE DEPTH .008" OUT OF LIMITS IAW SRM 53-30-15-00-01. SMOOTHED OUT TOOLING DAMAGE ON FRAME 236 IAW SRM 51-14-00-02-01. MIN NOTED THICKNESS .029", CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. APPLIED ALODINE, PRIMER AND INSTALLED RIVETS IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND 51-42-05-02-01. APPLIED SURFACE PROTECTION IAW SRM 51-25-15-02-01. COMPLIED WITH RD 8/4-53-5053. COMPLIED WITH TC RD 8/4-53-5053.

Part: STRINGER — CORRODED (BS 564.5 - 584.5) · airframe 10,790 hrs · 11,967 cycles

STRINGER 24S IS CORRODED STA 584.5-564.5. CLEANED AFFECTED AREA AND BLENDED CORROSION WITH 100 PERCENT MATERIAL LOSS NOTED, REMOVED FASTENERS COMMON TO SKIN FOM REF 51-26-00-02-01, 51-42-05-02-01 AND 51-21-00-00-02. MIN NOTED THICKNESS NOTED .054" REF NTM 51-00-04-910-801 PT 1, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. REMOVED 3 STRINGER CLIPS FOM IAW SRM 51-42-05-02-01, CUT STRINGER IAW RD 8/4-53-5039. CONFIRMED STRINGER CUT LINES CRACK FREE REF NTM 51-00-06-910-801 PT 1. MATCH DRILLED STRINGER IAW RD 8/4-53-5039. FABRICATED PACKER IAW RD 8/4-53-5039.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

FWD LANDING ON 262FT MATING SURFACE HAS FRETTING. BLENDED OUT DAMAGE ON PANEL 262FT AND CORRESPONDING LANDING IAW SRM 53-75-06-02-01. CONFIRMED BLENDED AREAS CRACK FREE REF NTM 51-00-04-910-801 PT AND 51-00-06-910-801 PT 1. PANEL 262FT FOUND IN LIMTS IAW SRM 53-75-06-02-01. LANDING SURFACE FOUND IN LIMITS IAW SRM 57-10-02-01-01. TREATED, PRIMED PANEL IAW SRM 53-75-06-02-01. ALODINED PANEL LANDING IAW SRM 51-21-10-02-01. FILLED BLENDS FLUSH AND APPLIED PRIMER IAW RD 8/4-53-451.

Part: STRUCTURE — CORRODED (CENTER WING) · airframe 10,790 hrs · 11,967 cycles

UPPER CENTER WING DRY PANEL LANDING FOR PANEL 621BT HAS AREAS OF BARE METAL AND CORROSION. REMOVED CORROSION REF RD 8/4-57-441. REAMED 22 HOLES REF RD 8/4-57-879. COUNTERSUNK HOLES REF RD 8/4-57-441 AND 8/4-57-879. ALODINED REPAIR IAW RD 8/4-57-441. FILLED BLENDS FLUSH IAW RD 8/4-57-1969. INSTALLED BUSHINGS IAW RD 8/4-57-879. APPLIED ALODINE AND PRIMER IAW RD 8/4-57-441. COMPLIED WITH TC RD 8/4-57-1969.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 10,790 hrs · 11,967 cycles

SEAT TRACK 7 IS CORRODED. BLENDED AND FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED SEAT TRACK IAW SRM 51-42-05-02-01, 51-40-15-02-01 AND AMM 20-10-01-430-801. MATCH DRILLED NEW TRACK IAW SRM 51-40-07-02-01. INSTALLED SEAT TRACK IAW SRM 51-41-00-00-01, 51-40-15-02-01 AND 51-42-05-02-01. PRIMED AND TOP COATED IAW SRM 51-25-10-02-01.

Part: STANCHION — CORRODED (BS 236) · airframe 10,790 hrs · 11,967 cycles

STANCHION 31P IS CORRODED FRAME 236. STANCHION FOUND OUT OF LIMITS IAW SRM 53-30-43-00-01. REMOVED STANCHION IAW SRM 51-42-05-02-01. ALODINED PRIIMED IAW RD 8/4-53-2344. MATCH DRILLED NEW STANCHION IAW SRM 51-42-05-02-01. INSTALLED END FITTING AND FLOOR SUPPORT IAW SRM 51-42-05-02-01, 51-40-15-02-01, 51-23-00-00-01, 51-25-10-02-01 AND 51-25-15-02-01. ALODINED, PRIMED TOPCOATED AND CPC IAW SRM 51-21-10-02-01 AND 51-25-10-02-01 AND 51-20-00-00-01 AND AMM 51-25-01-390-801.

Part: WEB — CORRODED (ZONE 100) · airframe 10,790 hrs · 11,967 cycles

UNDER FLOOR WEB FOR FORWARD DRAFT BULKHEAD IS CORRODED STA 32.4. REMOVED WEB IAW SRM 51-42-45-02-01. MATCH DRILLED NEW FLOOR WEB TO AC IAW SRM 51-40-07-02-01. INSTALLED WEB IAW SRM 51-42-05-02-01 AND 51-42-45-02-01. APPLIED SURFACE PROTECTION T-FASTENERS IAW SRM 51-25-10-02-01.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 10,790 hrs · 11,967 cycles

SKIN 6.7 ATTACH ANGLE IS CORRODED STRINGER 25P-23P. REMOVED NECESSARY RIVETS IAW SRM 51-42-05-02-01. REMOVED ATTACH ANGLE IAW SRM 51-42-05-02-01. MATCH DRILLED NEW PART IAW SRM 51-40-07-02-01. INSTALLED ATTACH ANGLE IAW SRM 51-42-05-02-01. APPLIED SURFACE PROTECTION IAW SRM 51-25-10-02-01 AND 51-25-15-02-01.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 10,790 hrs · 11,967 cycles

SEAT TRACK 5 IS CORRODED. BLENDED OUT CORROSION IAW RD 8/4-53-884. FOUND TRACK OUT OF LIMITS IAW RD 8/4-53-884. REMOVED SPLICE AND SEAT TRACK NR 5 IAW SRM 51-42-45-0-2-01, 51-42-05-02-01 AND 51-40-15-02-01, AND 51-41-00-00-01. MATCH DRILLED NEW SEAT TRACK IAW SRM 51-40-07-02-01. INSTALLED SEAT TRACK NR 5 IAW SRM 51-42-05-02-01, 51-41-00-00-01 AND 51-40-15-02-01. INSTALLED SPLICE IAW SRM 51-42-05-02-01 AND 51-40-15-02-01.

Part: FRAME — CORRODED (ZONE 100) · airframe 10,790 hrs · 11,967 cycles

FRAME 116, FLANGES ARE CORRODED STRINGER 32P-30P. REMOVED RIVETS AND CORROSION IAW SRM 51-42-05-02-01 AND RD 8/4-53-2344. MIN NOTED THICKNESS .042, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801, PT 1. MATERIAL LOSS FOUND TO BE IN LIMITS IAW RD 8/4-53-2344 AND DWG 85328117. APLINED ALODINE, PRIMER AND ALUMINIZED PAINT IAW RD 8/4-53-2344. INSTALLED NEW RIVETS IAW SRM 51-42-05-02-01 AND COMPLIED WITH RD 8/4-53-2344.

Part: WEB — CORRODED (ZONE 100) · airframe 10,790 hrs · 11,967 cycles

WEB ATTACHED TO SEAT TRACK 5 IS CORRODED STA 1-19.4. NO REPAIRS ALLOWED IAW SRM 53-20-43-00-01. REMOVED WEB IAW SRM 51-42-05-02-01. MATCH DRILLED NEW WEB SRM 51-40-07-02-01. INSTALLED WEB ON SEAT TRACK IAW SRM 51-42-05-02-01. ALODINED, PRIMED AND TOP COATED IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND 51-20-00-00-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

FRAME 19.4, FLANGES ARE CORRODED, STRINGER 32P-29P. REMOVED RIVETS FOM AND REMOVED CORROSION IAW SRM 51-42-05-02-01 AND RD 8/4-53-2344. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1 AND NTM 51-00-04-910-801 PT 1. MATERIAL LOSS FOUND IN LIMITS IAW RD 8/4-53-2344. INSTALLED RIVETS IAW SRM 51-42-05-02-01. RESTORED EXTERIOR SURFACE PROTECTION AND ALODINED, PRIMED, TOP COATED AND CPC INTERIOR SURFACES IAW RD 8/4-53-2344.

Part: STRINGER CLIP — CORRODED (BS 301 S24R) · airframe 10,790 hrs · 11,967 cycles

STRINGER 24S CLIP IS CORRODED STA 301. REMOVED CORROSION PER RD 8/4-53-2344. NO LIMITS ALLOWED ON CLIP REMOVED DAMAGED CLIP AND MATCH DRILLED NEW CLIP IAW Q400 SRM 51-42-05-02-0`1, 51-40-07-02-01. INSTALLED CLIP, PRIMED AND PAINTED IAW Q400 SRM 51-42-05-02-01, 51-25-10-02-01 AND 51-25-15-02-01.

Part: CHANNEL — CORRODED (FUELAGE) · airframe 10,790 hrs · 11,967 cycles

STRINGER, Z CHANNEL 32P IS CORRODED FOWARD OF STA -18.25. REMOVED CORROSION IAW RD 8/4-53-2344. REMOVED Z SPLICE IAW SRM 51-42-05-02-01. DRILLED NEW Z SPLICE IAW SRM 51-40-07-02-01. INSTALLED Z CHANNEL IAW SRM 51-42-05-02-01. APPLIED SURFACE PROTECTION IAW SRM 51-21-10-02-01, 51-25-10-02-01, 51-25-15-02-01 AND AMM 51-25-01-390-801.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

STRINGER Z CHANNEL 30P IS CORRODED FOWARD OF STA -18.25. REMOVED CORROSION IAW RD 8/4-53-2344.REMOVED Z SPLICE IAW SRM 51-42-05-02-01. DRILLED NEW Z SPLICE IAW SRM 51-40-07-02-01. INSTALLED Z CHANNEL IAW SRM 51-42-05-02-01. APPLIED SURFACE PROTECTION IAW SRM 51-21-10-02-01, 51-25-10-02-01, 51-25-15-02-01 AND AMM 51-25-01-390-801.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 10,790 hrs · 11,967 cycles

SEAT TRACK 10 IS CORRODED. BLENDED CORROSION AND FOUND TRACK TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED SEAT TRACK IAW SRM 51-42-05-02-01 AND 51-41-00-00-01. REMOVED GROUND WIRE AND PILOT AFT BULKHEAD FOM IAW SRM 51-42-45-02-01 AND 51-40-00-00-01. MATCH DRILLED NEW SEAT TRACK IAW SRM 51-40-07-02-01, 51-21-10-02-01 AND 51-25-15-02-01. INSTALLED SEAT TRACK IAW SRM 51-42-05-02-01, 51-40-00-00-01 AND 51-40-15-02-01. REINSTALLED BULKHEAD AND GROUND WIRE IAW SRM 51-42-45-02-01 AND 51-41-05-00-01.

Part: FRAME — CORRODED (ZONE 100) · airframe 10,790 hrs · 11,967 cycles

FRAME 176, FLANGE REPAIR IS CORROSDED STRINGER 31P-32P. PREVIOUSLY REPAIRED FLANGE IS CORRODED BEYOND LIMITS IAW RD 8/4-53-2344. REMOVED NECESSSARY RIVETS AND REPAIR ANGLE IAW SRM 51-42-05-02-01. FABRICATED REPAIR ANGLE IAW RD 8/4-53-017. ALODINED ANGLE IAW SRM 51-21-10-02-01, CONFIRMED FRAME CUT LINE CRACK FREE REF NTM 51-00-06-910-801 PT 1. INSTALLED REPAIR FLANGE ANGLE IAW RD 8/4-53-017. TREATED AND PRIMED REPAIR AREA IAW RD 8/4-53-017.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

SEAT TRACK 11 IS CORRODED. BLENDED CORROSION AND FOUND SEAT TRACK TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED SEAT TRACK IAW SRM 51-42-05-02-01 AND 51-41-00-00-01. MATCH DRILLED NEW SEAT TRACK AND APPLIED FINISH IAW SRM 51-40-07-02-01 AND 51-21-10-02-01. INSTALLED SEAT TRACK IAW SRM 51-42-05-02-01, 51-41-05-00-01 AND 51-40-15-02-01. PRIMED AND PAINTED RIVETS IAW SRM 51-25-10-02-01 AND 51-25-15-02-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,790 hrs · 11,967 cycles

SEAT TRACK 25 IS CORRODED. REMOVED CORROSION IAW RD 8/4-53-884. MECHANICALLY MEASURED SEAT TRACK FOUND TO BE IN LIMITS, MAX MATERIAL LOSS TOP CLAW .063", FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-07-02-01. MATCH DRILLED AND INSTALLED NEW TRACK IAW SRM 51-40-07-02-01, 51-42-05-02-01 AND 51-42-45-02-01. APPLIED SURFACE PROTECTION IAW SRM 51-25-10-02-01.

Part: FRAME — CORRODED (ZONE 100) · airframe 10,790 hrs · 11,967 cycles

FRAME 32.4, FLANGES ARE CORRODED STRINGER 33-30S. REMOVED RIVETS AND CORROSION IAW SRM 51-42-05-02-01 AND RD 8/4-53-2344 MIN NOTED THICKNESS .035" REF NTM 51-00-04-910-801 PT 1. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. MATERIAL LOSS FOUND OUT OF LIMITS IAW RD 8/4-53-2344. REMOVED STANCHION IAW SRM 51-42-05-02-01. TRIMMED FRAME FLANGE IAW RD 8/4-53-017 VERIFIED TRIMMED FRAME EDGE CRACK FREE IAW NTM 51-00-06-910-801 PT 1. FABRICATED DRILLED LOCATED REPAIR ANGLE IAW RD 8/4-53-017. ALODINED, PRIMED REPAIR ANGLE IAW RD 8/4-53-017. INSTALLED ANGLE AND STANCHION IAW RD 8/4-53-017 AND SRM 51-42-05-02-01. APPLIED ALUMINIZED PAINT AND CPC IAW RD 8/4-53-017.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

ANGLE CONNECTING INTERCOSTAL 25P TO FLOOR SUPPORT WEB 26.7 CORRODED. REMOVED CLIP IAW SRM 51-42-05-02-01, 51-40-15-02-01. MATCH DRILLED NEW CLIP TO AC IAW SRM 51-40-07-02-01. INSTALLED NEW CLIP IAW SRM 51-42-05-02-01, 51-40-15-02-01. TREATED CLIP IAW SRM 51-25-15-02-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,790 hrs · 11,967 cycles

SEAT TRACK 15 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-00-00-02. MEASURED SEAT TRACK FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-15-02-01 AND 51-42-05-02-01. MATCH DRILLED AND INSTALLED NEW TRACK IAW SRM 51-40-07-02-01, 51-21-10-02-01 AND 51-25-15-02-01, 51-42-05-02-01 AND 51-41-00-00-01. APPLIED SURFACE FINISH IAW SRM 51-25-10-02-01.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

ATTACH ANGLE CONNECTING INTERCOSTAL 25P TO FLOOR SUPPORT WEB 6.7 CORRODED. REMOVED CLIP IAW SRM 51-42-05-02-01, 51-40-15-02-01. MATCH DRILLED NEW CLIP TO AC IAW SRM 51-40-07-02-01. INSTALLED NEW CLIP IAW SRM 51-42-05-02-01, 51-40-15-02-01. TREATED CLIP IAW SRM 51-25-15-02-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,970 hrs · 11,967 cycles

SEAT TRACK 9 IS CORRODED. REMOVED CORROSION ON TRACK 9, MEASURED SEAT TRACK FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED DAMAGED SEAT TRACK IAW SRM 51-42-05-02-01. MATCH DRILLED AND INSTALLED NEW TRACK IAW SRM 51-40-07-02-01, 51-21-10-02-01 AND 51-25-15-02-01, 51-42-05-02-01 AND 51-40-15-02-01. APPLIED SURFACE FINISH IAW SRM 51-25-10-02-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,790 hrs · 11,967 cycles

SEAT TRACK IS CORRODED. REMOVED CORROSION IAW SRM 51-21-00-00-02. MEASURED SEAT TRACK FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-15-02-01, 51-42-05-02-01 AND 51-41-00-00-01. MATCH DRILLED AND INSTALLED NEW TRACK IAW SRM 51-40-07-02-01, 51-41-00-00-01, 51-40-15-02-01, AND 51-42-00-00-02. APPLIED SURFACE FINISH IAW SRM 51-25-10-02-01.

Part: FRAME — CORRODED (ZONE 100) · airframe 10,790 hrs · 11,967 cycles

FRAME -18.25, FLANGE IS CORRODED STRINGER 31S-30S. REMOVED NECESSARY RIVETS AND CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .045" REF NTM 51-00-04-910-801 PT 1. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1. FLANGE FOUND IN LIMITS IAW RD 8/4-53-2344. ALODINED AND PRIMED IAW RD 8/4-53-2344. INSTALLED FASTENERS AND APPLIED ALUMINZIED TOP COAT REF RD 8/4-53-2344 AND SRM 51-21-10-02-01, 51-25-10-02-01, 51-25-05-02-01.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 10,790 hrs · 11,967 cycles

RT UPPER WING ACCESS PANEL 621BT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-425. MEASURED BLENDED AREAS BELOW MIN THICKNESS, MIN .215 ACTUAL .198 REF RD 8/4-57-425. PANEL OUT OF LIMITS, RECEIVED NEW PANEL FROM STOCK.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

FRAME 1, FLANGES ARE CORRODED STRINGER 32P-29P. REMOVED RIVET FOM. REMOVED CORROSION IAW RD 8/4-53-2344. CONFIRMED AREAS CRACK FREE REF NTM 51-00-06-910-801 PT 1 AND NTM 51-00-04-910-801 PT 1. NOMINAL THICKNESS .050". FLANGES FOUND TO BE IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED, INSTALLED RIVET AND TOP COATED IAW RD 8/4-53-2344. APPLIED CPC IAW AMM 51-25-01-390-801.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,790 hrs · 11,967 cycles

SEAT TRACK 12 IS CORRODED. REMOVED CORROSION IAW RD 8/4-53-884. MECHANICALLY MEASURED SEAT TRACK FOUND TO BE IN LIMITS, MAX MATERIAL LOSS IN CLAW .020" TOP CLAW .007" AS PER RD 8/4-53-884. VERIFIED BLENDED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. ALODINED SEAT TRACK IAW RD 8/4-53-884.

Part: THRESHOLD — CORRODED (EMERGENCY EXIT) · airframe 10,790 hrs · 11,967 cycles

EMERGENCY EXIT THRESHOLD IS CORRODED. REMOVED THRESHOLD AND EDGE BEAM IAW SRM 51-42-45-02-01 AND 51-42-05-02-01. EDGE BEAM FOUND BEYOND LIMITS IAW SRM 53-20-21-00-01. MATCH DRILLED NEW THRESHOLD EDGE BEAM IAW SRM 51-40-07-02-01. INSTALLED THRESHOLD EDGE BEAM IAW SRM 51-42-05-02-01 AND 51-42-45-02-01. PRIMED AND TOP COATED IAW SRM 51-25-10-02-01 AND 51-25-05-02-01.

Part: FRAME — CORRODED (ZONE 100) · airframe 10,790 hrs · 11,967 cycles

FRAME 19.4, FLANGE IS CORRODED STRINGER 33S-32S. REMOVED RIVETS FOM IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW RD 8/4-53-2344. MIN NOTED THICKNESS .038" CONFIRMED BLENDED AREAS CRACK FREE REF NTM 51-00-04-910-801 AND 51-00-06-910-801 PT 1. FOUND FLANGE TO BE WITHIN LIMITS IAW RD 8/4-53-2344. ALODINED AND PRIMED FRAME IAW RD 8/4-53-2344. INSTALLED RIVETS IAW RD 8/4-53-2344. APPLIED ALODINE PRIMER, TOP COAT AND CPC IAW IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND AMM 51-25-05-02-01 AND AMM 51-25-01-390-801.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 10,790 hrs · 11,967 cycles

SEAT TRACK 13 IS CORRODED. REMOVED CORROSION AS NOTED IAW RD 8/4-53-884. MAX REMOVED .013 FROM TOP CLAW AND .028" FROM CENTER CLAW. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-884. APPLIED ALODINE IAW RD 8/4-53-884.

Part: FRAME — CORRODED (ZONE 100) · airframe 10,790 hrs · 11,967 cycles

FRAME 281, FLANGE IS CORRODED, STRINGER 31P-32P. REMOVED RIVET FOM IAW SRM 51-42-05-02-01. BLENDED CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .044" REF NTM 51-00-04-910-801 PT 1. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1. MATERIAL LOSS FOUND OUT OF LIMITS IAW RD 8/4-53-2344. REMOVED STANCHION AND CROSS BRACE FOM IAW SRM 51-42-05-02-01 AND 51-41-00-00-01. TRIMMED OFF DAMAGE FLANGE, FABRICATED REPAIR ANGLE IAW RD 8/4-53-017. CONFIRMED WEB CUT LINE CRACK FREE REF NTM 51-00-06-910-801 PT 1. INSTALLED REPAIR IAW SRM 51-41-05-02-01 AND RD 8/4-53-017.

Part: FRAME — CORRODED (BS 624.5) · airframe 10,790 hrs · 11,967 cycles

FRAME 624.5, FLANGE IS CORRODED, STRINGER 32S-31S. BLENDED OUT CORROSION ON FRAME IAW SRM 51-21-00-00-02 MIN NOTED THICKNESS .054" REF NTM 51-00-04-910-801 PT 1, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. NOMINAL THICKNESS OF FRAME IS .050" FRAME FLANGES FOUND TO BE IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED IAW RD 8/4-53-2344. INSTALLED RIVETS IAW SRM 51-42-05-02-01. APPLIED TOP COAT IAW SRM 51-25-15-02-01, APPLIED CPC IAW AMM 51-25-01-390-801, APPLIED EXTERNAL TOP COAT IAW SRM 51-25-15-02-01.

Part: FRAME — CORRODED (ZONE 100) · airframe 10,790 hrs · 11,967 cycles

FRAME 449.5, FLANGES ARE CORRODED STRINGER 31P-33. REMOVED RIVETS IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW SRM 51-42-05-02-01 AND RD 8/4-53-2344. MIN NOTED THICKNESS .063" CONFIRMED BLENDED AREAS CRACK FREE REF NTM 51-00-04-910-801 AND 51-00-06-910-801 PT 1. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. ALODINED AND PRIMED FRAME IAW RD 8/4-53-2344. INSTALLED RIVETS IAW SRM 51-42-05-02-01. APPLIED PRIMER, TOP COAT AND CPC IAW SRM 51-25-10-02-01, 51-25-15-02-01 AND AMM 51-25-01-390-801.

Part: FRAME — CORRODED (ZONE 100) · airframe 10,790 hrs · 11,967 cycles

FRAME 624.5, FLANGE IS CORRODED, STRINGER 32P-31P. BLENDED CORROSION ON FRAME IAW SRM 51-21-00-00-02. MIN NOTED THICKNESS .057" REF NTM 51-00-04-910-801 CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801, PT 1. NOMINAL THICKNESS IS .050" FRAME FLANGES FOUND TO BE IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED IAW RD 8/4-53-2344. INSTALLED RIVETS IAW SRM 51-42-05-02-01. APPLIED TOP COAT TO FLANGE IAW SRM 51-25-15-02-01, APPLIED CPC TO FLANGE IAW AMM 51-25-01-390-801. APPLIED EXTERNAL TOPCOAT IAW SRM 51-25-15-02-01.

Part: ANGLE — CORRODED (ZONE 100) · airframe 10,790 hrs · 11,967 cycles

AFT CARGO DOOR LT FLOOR ATTACH ANGLE AT CARGO STEP UP HAS SURFACE CORROSION. REMOVED ATTACH ANGLE IAW SRM 51-42-05-02-01. NO REPAIRS ALLOWED IAW SRM 53-40-15-00-01. MATCH DRILLED NEW ANGLE IAW SRM 51-40-07-02-01. APPLIED ALODINE AND PIMER IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED ATTACH ANGLE IAW SRM 51-42-05-02-01.

Part: FRAME — CORRODED (BS 644.5) · airframe 10,790 hrs · 11,967 cycles

FRAME 644.5, FLANGES ARE CORRODED STRINGER 31P-33. REMOVED RIVET FOM IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW RD 8/4-53-2344. MIN THICKNESS .056", CONFIRMED BLENDED AREAS CRACK FREE REF NTM 51-00-06-910-801 PT 1 AND NTM 51-00-04-910-801 PT 1. FLANGES FOUND TO BE IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED, INSTALLED RIVET AND TOP COATED IAW RD 8/4-53-2344 AND SRM 51-42-05-02-01. APPLIED TOP COAT IAW SRM 51-25-15-02-01. APPLIED CPC IAW AMM 51-25-01-390-801.

Part: FRAME — CORRODED (BS 32.4) · airframe 10,790 hrs · 11,967 cycles

FRAME 32.4 FLANGES ARE CORRODED, STRINGER 32P-29P. REMOVED RIVET FO IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .039" REF NTM 51-00-04-910-801 PT 1. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1. MATERIAL LOSS FOUND IN LIMITS IAW RD 8/4-53-2344. ALODINED AND PRIMED IAW RD 8/4-53-2344. INSTALLED FASTENERS AND APPLIED ALUMINZIED TOP COAT REF RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: FRAME — CORRODED (BS 236) · airframe 10,790 hrs · 11,967 cycles

FRAME 236 FLANGES ARE CORRODED, STRINGER 31P-32P. REMOVED RIVET FOM IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW SRM 51-21-00-00-02 AND RD 8/4-53-2344. MIN REMAINING THICKNESS .046" REF NTM 51-00-04-910-801 PT 1. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1. MATERIAL LOSS FOUND IN LIMITS IAW RD 8/4-53-2344. ALODINED AND PRIMED IAW RD 8/4-53-2344. INSTALLED FASTENERS AND APPLIED ALUMINZIED TOP COAT REF RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: FRAME — CORRODED (BS 547) · airframe 10,790 hrs · 11,967 cycles

FRAME 547, FLANGE IS CORRODED, STRINGER 32P-31P. REMOVED RIVETS AS NECESSARY AND CORROSION IAW RD 8/4-53-2344. MIN NOTED THICKNESS .054 REF NTM 51-00-04-910-801 PT 1, VERIFIED AFFECTED AREA TO BE CRACK FREE REF NTM 51-00-06-910-801 PT 1. MATERIAL LOSS FOUND TO BE IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED AND INSTALLED RIVETS IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW RD 8/4-53-2344. ALODINED, PRIMED AND PAINTED EXTERIOR REPAIR AREA IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: FRAME — CORRODED (BS 301) · airframe 10,970 hrs · 11,967 cycles

FRAME 301, FLANGE IS CORRODED STRINGER 32P-30P. REMOVED FASTENERS FOM IAW SRM 51-42-05-02-01 AND BLENDED OUT CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .047" NTM 51-00-04-910-801 PT 1. VERIFIED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. MATERIAL LOSS FOUND IN LIMITS IAW RD 8/4-53-2344. NOMINAL THICKNESS IS .050 IAW DWG 85361313. ALODINED, PRIMED FLANGES AND INSTALLED FASTENERS, IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW AMM 51-25-31-370-801 AND AMM 51-25-01-390-801. ALODINED, PRIMED AND TOP COATED EXTERIOR AREA IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

FRAME 49.5, FLANGES ARE CORRODED STRINGER 32S-28S. REMOVED RIVETS AS NECESSARY AND CORROSION IAW SRM 51-42-05-02-01 AND 51-21-00-00-02 AND RD 8/4-53-2344. MIN NOTED THICKNESS .047 REF NTM 51-00-04-910-801 PT 1, VERIFIED AFFECTED AREA TO BE CRACK FREE REF NTM 51-00-06-910-801 PT 1. MATERIAL LOSS FOUND TO BE IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED AND INSTALLED RIVETS IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW RD 8/4-53-2344. ALODINED, PRIMED AND PAINTED EXTERIOR REPAIR AREA IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: FRAME — CORRODED (BS 156) · airframe 10,790 hrs · 11,967 cycles

FRAME BS 156 IS CORRODED, STRINGERS 31-32S. REMOVED CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .044" NTM 51-00-04-910-801 PT 1 CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. NOMINAL FRAME THICKNESS IS .040" FLANGES FOUND IN LIMITS RD 8/4-53-2344. INSTALLED FASTENER, ALODINED AND PRIMED IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW SRM 51-25-15-02-01 AND AMM 51-25-01-390-801. ALODINED, PRIMED AND TOP COATED EXTERIOR AREA IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: FRAME — CORRODED (BS 258.5) · airframe 10,790 hrs · 11,967 cycles

FRAME 258.5, FLANGE IS CORRODED, STRINGER 31P-32P. REMOVED FASTENERS FOM IAW SR 51-42-05-02-01. BLENDED CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .044" NTM 51-00-04-910-801 PT 1, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. NOMINAL THICKNESS IS .040" MATERIAL LOSS FOUND IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED INSTALLED FASTENERS, IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW SRM 51-25-3-370-801 AND AMM 51-25-01-390-801. ALODINED, PRIMED AND TOP COATED EXTERIOR AREA IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

FRAME 94.8, FLANGES ARE CORRODED, STRINGER 30P-32P. REMOVED RIVETS TO ACCESS CORROSION IAW SRM 51-42-05-02-01 AND RD 8/4-53-2344. MIN NOTED THICKNESS .042 REF NTM 51-00-04-910-801 PT 1, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. DAMAGE FOUND IN LIMITS IAW RD 8/4-53-2344. INSTALLED RIVETS, ALODINED, PRIMED FLANGES IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW SRM 51-25-15-02-01 AND AMM 51-25-01390-801. ALODINED, PRIMED AND PAINTED EXTERIOR REPAIR AREA IAW RD 8/4-53-2344 AMD SRM 51-25-05-02-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

FRAME BS 71.2, FLANGES ARE CORRODED STRINGER 30S-32S. REMOVED RIVETS AND CORROSION IAW RD 8/4-53-2344. MIN NOTED THICKNESS .039 REF NTM 51-00-04-910-801 PT 1, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. MATERIAL LOSS FOUND IN LIMITS IAW RD 8/4-53-2344. INSTALLED RIVETS, ALODINED, PRIMED FLANGES IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW SRM 51-25-15-02-01 AND AMM 51-25-01390-801. ALODINED, PRIMED AND PAINTED EXTERIOR REPAIR AREA IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: FRAME — CORRODED (BS 489.5) · airframe 10,790 hrs · 11,967 cycles

FRAME 489.5, FLANGES ARE CORRODED STRINGER 33-30P. REMOVED RIVETS TO ACCESS CORROSION IAW SRM 51-42-05-02-01. BLENDED CORROSION PER RD 8/4-53-2344. MIN NOTED THICKNESS .055 REF NTM 51-00-04-910-801 PT 1, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. MATERIAL LOSS FOUND TO BE IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED AND INSTALLED RIVETS IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT IAW AMM 51-25-31-370-801. APPLIED CPC ON FRAME FLANGES, STRINGERS IAW AMM 51-25-01-390-801. ALODINED, PRIMED AND PAINTED EXTERIOR REPAIR AREA IAW RD 8/4-53-2344 AMD SRM 51-25-05-02-01.

Part: WEB — CORRODED (CARGO DOOR) · airframe 10,790 hrs · 11,967 cycles

AFT CARGO DOOR FLOOR WEB JUST FWD OF LT STEP UP HAS SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-21-00-00-02. MIN REMAINING THICKNESS NOTED .047", CONFIRMED AFFECTED AREA OF WE CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. WEB FOUND IN LIMITS IAW SRM 53-40-43-02-01. NOMINAL THICKNESS .050, MATERIAL LOSS IS .003 WITHIN LIMITS IAW SRM 53-40-43-02-01. APPLIED ALODINE IAW SRM 51-21-10-02-01, PRIMED IAW SRM 51-25-10-02-01, APPLIED ALUMINIZED PAINT IAW SRM 51-25-15-02-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

FRAME 136, FLANGES ARE CORRODED STRINGER 30P-32P. REMOVED RIVETS AND CORROSION IAW SRM 51-42-05-02-01 AND RD 8/4-53-2344. MIN NOTED THICKNESS .043 REF NTM 51-00-04-910-801 PT 1, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. FLANGES FOUND IN LIMITS IAW RD 8/4-53-2344. INSTALLED RIVETS, ALODINED, PRIMED FLANGES IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW SRM 51-25-15-02-01 AND AMM 51-25-01390-801. ALODINED, PRIMED AND PAINTED EXTERIOR REPAIR AREA IAW RD 8/4-53-2344 AMD SRM 51-25-05-02-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

FRAME 469.5, FLANGE IS CORRODED STRINGER 32P-31P. REMOVED RIVETS AND CORROSION IAW SRM 51-42-05-02-01 AND RD 8/4-53-2344. MIN NOTED THICKNESS .055 REF NTM 51-00-04-910-801 PT 1, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. FLANGES FOUND TO BE IN LIMITS IAW RD 8/4-53-2344. INSTALLED RIVETS, ALODINED, PRIMED FLANGES IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW SRM 51-25-15-02-01 AND AMM 51-25-01390-801. ALODINED, PRIMED AND PAINTED EXTERIOR REPAIR AREA IAW RD 8/4-53-2344 AMD SRM 51-25-05-02-01.

Part: FRAME — CORRODED (BS 341) · airframe 10,790 hrs · 11,967 cycles

FRAME 341 FLANGE IS CORRODED, STRINGER 32S-31S. REMOVED FASTENER FOM IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .053" NTM 51-00-04-910-801 PT 1. VERIFIED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. NOMINAL FRAME THICKNESS IS .050" IAW DWG 85361315. MATERIAL LOSS FOUND IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED INSTALLED FASTENER, IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW RD 8/4-53-2344. ALODINED, PRIMED AND TOP COATED EXTERIOR AREA IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: FRAME — CORRODED (BS 321)

FRAME 321, FLANGE IS CORRODED STRINGER 32S-31S. REMOVED FASTENER FOM IAW SRM 51-42-05-02-01 AND BLENDED OUT CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .057" NTM 51-00-04-910-801 PT 1. VERIFIED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. NOMINAL FRAME THICKNESS IS .050" IAW DWG 853613141. MATERIAL LOSS FOUND IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED INSTALLED FASTENER, IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW AMM 51-25-31-370-801 AND AMM 51-25-01-390-801. ALODINED, PRIMED AND TOP COATED EXTERIOR AREA IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,790 hrs · 11,967 cycles

FRAME 136 FLANGE IS CORRODED STRINGER 30S-32S. REMOVED RIVETS AND CORROSION IAW RD 8/4-53-2344. MIN NOTED THICKNESS .043 REF NTM 51-00-04-910-801 PT 1, VERIFIED AFFECTED AREA TO BE CRACK FREE REF NTM 51-00-06-910-801 PT 1. FLANGES FOUND TO BE IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED AND INSTALLED RIVETS IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW SRM 51-25-15-02-01 AND AMM TASK 51-25-01-390-801. ALODINED, PRIMED AND PAINTED EXTERIOR REPAIR AREA IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: FRAME — CORRODED (BS 216) · airframe 10,790 hrs · 11,967 cycles

FRAME 216, FLANGE IS CORRODED STRINGER 33-29P. REMOVED FASTENERS AND CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .043" NTM 51-00-04-910-801 PT 1, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. NOMINAL FRAME THICKNESS IS .040" FLANGES FOUND IN LIMITS IAW RD 8/4-53-2344. INSTALLED FASTENERS, ALODINED AND PRIMED IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW SRM 51-25-15-02-01 AND AMM 51-25-01-390-801. ALODINED, PRIMED AND TOP COATED EXTERIOR AREA IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: FRAME — CORRODED (BS 321) · airframe 10,790 hrs · 11,967 cycles

FRAME 321, FLANGE IS CORRODED STRINGER 32P-31P. REMOVED FASTENER FOM IAW SRM 51-42-05-02-01 AND BLENDED OUT CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .054" NTM 51-00-04-910-801 PT 1. VERIFIED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. NOMINAL FRAME THICKNESS IS .050" IAW DWG 85361314. MATERIAL LOSS FOUND IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED INSTALLED FASTENER, IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW AMM 51-25-31-370-801 AND AMM 51-25-01-390-801. ALODINED, PRIMED AND TOP COATED EXTERIOR AREA IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: FRAME — CORRODED (BS 301) · airframe 10,790 hrs · 11,967 cycles

FRAME 301, FLANGE IS CORRODED STRINGER 31S-32S. REMOVED FASTENER FOM IAW SRM 51-42-05-02-01 AND BLENDED OUT CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .046" NTM 51-00-04-910-801 PT 1. VERIFIED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. NOMINAL FRAME THICKNESS IS .040" MATERIAL LOSS FOUND IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED INSTALLED FASTENER, IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW AMM 51-25-31-370-801 AND AMM 51-25-01-390-801. ALODINED, PRIMED AND TOP COATED EXTERIOR AREA IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: PANEL — CORRODED (LT WING) · airframe 10,790 hrs · 11,967 cycles

LT UPPER WING PANEL 522AT HAS AREAS OF CORROSION. REMOVED CORROSION FROM PANEL IAW RD 8/4-57-425. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801, PT 1. FOUND WORKED AREA TO BE IN LIMITS IAW RD 8/4-57-425. APPLIED ALODINE, PRIMERAN DEPT TAPE IAW RD 8/4-57-425.

Part: SKIN — CORRODED (LT WING) · airframe 10,790 hrs · 11,967 cycles

LT UPPER WING SKIN LANDING FOR ACCESS PANEL 624BT HAS AREAS OF CORROSION. BLENDED OUT CORROSION FROM LANDING IAW RD 8/4-57-445. MIN THICKNESS REMAINING .080" REF NTM 51-00-04-910-801 PT 1. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1. BLEND FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-445. ALODINED AND RESTORED PRIMER IAW RD 8/4-57-445.

Part: SKIN — CORRODED (LT WING) · airframe 10,790 hrs · 11,967 cycles

LT UPPER WING SKIN LANDING FOR ACCESS PANEL 524DT HAS AREAS OF CORROSION. REMOVED CORROSION FROM LANDING IAW RD 8/4-57-441. MIN THICKNESS REMAINING .075" REF NTM 51-00-04-910-801 PT 1. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1. REPAIR WITHIN LIMITS IAW RD 8/4-57-445. ALODINED AND RESTORED PRIMER IAW RD 8/4-57-445.

Part: NUT PLATE — CORRODED (SERVICE DOOR) · airframe 10,790 hrs · 11,967 cycles

RIGHT AFT SERVICE DOOR UPPER FWD LINER BRACKET HAS A CORRODED NUT PLATE. REMOVED CORRODED NUT PLATE IAW SRM 51-42-05-02-01. INSTALLED NEW NUT PLATE IAW SRM 51-42-05-02-01.

Part: SKIN — CORRODED (RT WING) · airframe 10,790 hrs · 11,967 cycles

RH UPPER WING SKIN LANDING FOR ACCESS PANEL 624AT HAS AREAS OF CORROSION. BLENDED OUT CORROSION FROM LANDING IAW RD 8/4-57-445. MIN THICKNESS REMAINING .079" REF NTM 51-00-04-910-801 PT 1. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1. BLEND FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-445. ALODINED AND RESTORED PRIMER IAW RD 8/4-57-445.

Part: FRAME — CORRODED (BS 49.5) · airframe 10,790 hrs · 11,967 cycles

FRAME 49.5, FLANGE IS CORRODED STRINGER 31P-30P. REMOVED CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .050" NTM 51-00-04-910-801 PT 1. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. MATERIAL LOSS FOUND TO BE IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW RD 8/4-53-2344.

Part: SKIN — CORRODED (LT WING) · airframe 10,790 hrs · 11,967 cycles

LT UPPER WING SKIN LANDING FOR ACCESS PANEL 524AT HAS AREAS OF CORROSION. REMOVED CORROSION FROM LANDING IAW RD 8/4-57-445. MIN THICKNESS REMAINING .079" REF NTM 51-00-04-910-801 PT 1. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1. FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-445. ALODINED AND RESTORED PRIMER IAW RD 8/4-57-445.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,790 hrs · 11,967 cycles

LT UPPER WING ACCESS PANEL 521AT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-425. MEASURED BLENDED AREAS MIN .215 ACTUAL .183, REF 8/4-57-425 PG 41. PANEL FOUND TO BE OUT OF LIMITS IAW RD 8/4-57-425. RECEIVED NEW PANEL FROM STOCK.

Part: FRAME — CORRODED (BS 509.5) · airframe 10,790 hrs · 11,967 cycles

FRAME 509.5, FLANGES ARE CORRODED STRINGER 33P-31P. REMOVED FASTENERS FOM IAW IAW RD 8/4-53-2344. BLENDED OUT CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .054" NTM 51-00-04-910-801 PT 1. VERIFIED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. NOMINAL THICKNESS IS .050 IAW DWG 85361326. MATERIAL LOSS FOUND TO BE IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED INSTALLED FASTENERS, IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW RD 8/4-53-2344. ALODINED, PRIMED AND TOP COATED EXTERIOR AREA IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: SKIN — CORRODED (LT WING) · airframe 10,790 hrs · 11,967 cycles

LT UPPER WING SKIN LANDING FOR ACCESS PANEL 524CT HAS AREAS OF CORROSION. REMOVED CORROSION FROM LANDING IAW RD 8/4-57-445. MIN THICKNESS REMAINING .080" REF NTM 51-00-04-910-801 PT 1. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1. FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-445. ALODINED AND RESTORED PRIMER IAW RD 8/4-57-445.

Part: FRAME — CORRODED (BS 71.2) · airframe 10,790 hrs · 11,967 cycles

FRAME 71.2, FLANGES ARE CORRODED, STRINGER 29P-32P. REMOVED FASTENERS FOM IAW IAW RD 8/4-53-2344. BLENDED OUT CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .039" NTM 51-00-04-910-801 PT 1. VERIFIED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. MATERIAL LOSS FOUND IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED INSTALLED FASTENERS, IAW RD 8/4-53-2344. APPLIED ALUMINIZED PAINT AND CPC IAW RD 8/4-53-2344. ALODINED, PRIMED AND TOP COATED EXTERIOR AREA IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: SKIN — CORRODED (LT WING) · airframe 10,790 hrs · 11,967 cycles

LT UPPER WING SKIN LANDING FOR ACCESS PANEL 524BT HAS AREAS OF CORROSION. REMOVED CORROSION FROM LANDING IAW RD 8/4-57-445. MIN THICKNESS REMAINING .080" REF NTM 51-00-04-910-801 PT 1. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1. FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-445. ALODINED AND RESTORED PRIMER IAW RD 8/4-57-445.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,790 hrs · 11,967 cycles

LT UPPER WING ACCESS PANEL 524CT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. MEASURED BLENDS AND FOUND TO BE IN LIMITS RD 8/4-57-442. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. APPLIED ALODINE, PRIMER, REIDENTIFIED PANEL AND INSTALLED OUTER SEAL IAW RD 8/4-57-442.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 10,790 hrs · 11,967 cycles

RT UPPER WING ACCESS PANEL 624AT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. MEASURED IAW RD 8/4-57-442. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. PANEL FOUND WITHIN LIMITS IAW RD 8/4-57-442. APPLIED ALODINED, PRIMER AND REIDENTIFIED PANEL IAW RD 8/4-57-442.

Part: FRAME — CORRODED (BS 449.5) · airframe 10,790 hrs · 11,967 cycles

FRAME BS 449.5, FLANGE IS CORRODED STRINGER 32S-31S. REMOVED RIVETS FOM IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW RD 8/4-53-2344. MIN NOTED THICKNESS .067" REF NTM 51-00-04-910-801 PT 1, VERIFIED AFFECTED AREA TO BE CRACK FREE USING HFEC REF NTM 51-00-06-910-801 PT 1. NO MATERIAL LOSS NOTED WITHIN LIMITS IAW RD 8/4-53-2344. NOMINAL THICKNESS IS .063" IAW DWG 85361323. ALODINED, PRIMED, INSTALLED RIVETS, PAINTED AND APPLIED CPC IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 10,790 hrs · 11,967 cycles

RT UPPER WING ACCESS PANEL 622AT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-425. CORRODED PANEL WAS FOUND TO BE OUT OF LIMITS AND REPLACED WITH NEW.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,790 hrs · 11,967 cycles

LT UPPER WING ACCESS PANEL 524AT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. MEASURED BLENDS AND FOUND TO BE IN LIMITS RD 8/4-57-442. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. APPLIED ALODINE, PRIMER, REIDENTIFIED PANEL AND INSTALLED OUTER SEAL IAW RD 8/4-57-442.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,790 hrs · 11,967 cycles

LT UPPER WING ACCESS PANEL 524DT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. MEASURED BLENDED AREAS FOUND WITHIN LIMITS IAW RD 8/4-57-442. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. ALODINED, PRIMED, REIDENTIFIED PANEL IAW AND INSTALLED OUTER SEAL RD 8/4-57-442.

Part: CHANNEL — CORRODED (WING) · airframe 10,790 hrs · 11,967 cycles

GANG CHANNEL ATTACHING RIVETS CORRODED FOR PANEL 524AT. REMOVED CORRODED GANG CHANNEL RIVETS AND INSTALLED NEW IAW SRM 51-42-05-02-01. APPLIED SEALANT TO RIVETS IAW SRM 51-23-20-02-01.

Part: CHANNEL — CORRODED (WING) · airframe 10,790 hrs · 11,967 cycles

GANG CHANNEL ATTACHING RIVETS CORRODED FOR PANEL 524CT. REMOVED CORRODED GANG CHANNEL RIVETS AND INSTALLED NEW IAW SRM 51-42-05-02-01. APPLIED SEALANT TO RIVETS IAW SRM 51-23-20-02-01.

Part: CHANNEL — CORRODED (WING) · airframe 10,790 hrs · 11,967 cycles

GANG CHANNEL ATTACHING RIVETS CORRODED FOR PANEL 525AT. UPON FURTHER INSPECTION CORROSION FOUND TO BE ON SURFACE ONLY. REMOVED SURFACE CORROSION IAW SRM 51-21-00-00-02. RESTORED SURFACE PROTECTION IAW SRM 51-21-00-00-02.

Part: FRAME — CORRODED (BS 341) · airframe 10,790 hrs · 11,967 cycles

FRAME BS 341, FLANGE IS CORRODED STRINGER 32P-31P. REMOVED RIVETS FOM IAW SRM 51-42-05-02-01. BLENDED CORROSION IAW RD 8/4-53-2344. MIN NOTED THICKNESS .053" REF NTM 51-00-4-910-801 PT 1, VERIFIED AFFECTED AREA TO BE CRACK FREE USING HFEC REF NTM 51-00-06-910-801 PT 1. NO MATERIAL LOSS NOTED NOMINAL IS .050 IAW DWG 85361315, FOUND TO BE IN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED, INSTALLED RIVETS AND PAINTED IAW RD 8/4-53-2344 AND SRM 51-25-05-02-01.

Part: CHANNEL — CORRODED (WING) · airframe 10,790 hrs · 11,967 cycles

GANG CHANNEL ATTACHING RIVETS CORRODED FOR PANEL 524DT. REMOVED CORRODED GANG CHANNEL ATTACHING RIVETS AND INSTALLED NEW IAW SRM 51-42-05-02-01. APPLIED SEALANT IAW SRM 51-23-20-02-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,790 hrs · 11,967 cycles

SEAT TRACK 6 IS CORRODED. REMOVED CORROSION ON SEAT TRACK IAW RD 8/4-53-884. INSPECTED BLENDS WITH HFEC, NO CRACKS NOTED REF NDTM PT 6 51-00-01-250-801. SEAT TRACK FOUND TO BE IN LIMITS IAW RD 8/4-53-884. RESTORED SURFACE PROTECTION IAW RD 8/4-53-884.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 10,790 hrs · 11,967 cycles

RT UPPER WING ACCESS PANEL 624BT HAS AREAS OF CORROSION. LOCALLY BLENDED CORROSION IAW RD 8/4-57-442.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,790 hrs · 11,967 cycles

SEAT TRACK 14 IS CORRODED. REMOVED CORROSION ON SEAT TRACK IAW 51-21-00-00-02. INSPECTED BLENDS WITH HFEC, NO CRACKS NOTED REF NDTM PT 6 51-00-01-250-801. SEAT TRACK FOUND TO BE IN LIMITS IAW RD 8/4-53-884. RESTORED SURFACE PROTECTION IAW RD 8/4-53-884.

Part: NUT PLATE — CORRODED (SERVICE DOOR) · airframe 10,790 hrs · 11,967 cycles

SERVICE DOOR FWD FRAME HAS A CORRODED NUT PLATE AT THE FOURTH FROM THE BOTTOM STOP FITTING. REMOVED RIVETS FOM IAW SRM 51-42-45-02-01. R & R CORRODED NUT PLATE FROM SERVICE DOOR FWD FRAME IAW RD 8/4-52-492.

Part: NUT PLATE — CORRODED (SERVICE DOOR) · airframe 10,790 hrs · 11,967 cycles

SERVICE DOOR AFT FRAME HAS CORRODED NUT PLATES AT THIRD FROM BOTTOM STOP FITTING. REPAIRED IAW RD 8/4-52-492. ALODINED AND PRIMED IAW RD 8/4-52-492.

Part: NUT PLATE — CORRODED (SERVICE DOOR) · airframe 10,790 hrs · 11,967 cycles

SERVICE DOOR FWD FRAME HAS CORRODED NUT PLATES AT THE THIRD FROM THE BOTTOM STOP FITTING. REMOVED CORRODED NUT PLATES AND MADE REPAIRS IAW RD 8/4-52-492.

Part: ANTENNA — MALFUNCTIONED (ZONE 100) · airframe 10,502 hrs · 11,653 cycles

NR 2 COMM RECEIVED SCRATCHY UNREADABLE ON 132.131.35, 130.72 DURING FLIGHT, RECEPTION IMPROVED WHEN ACFT WAS ON GROUND. DIVERTED. LANDING UNEVENTFUL. VERIFIED GOOD POWER OUT USING WATT METER, LOW VSWR READING. MEGGED COAX CABLE, CHECKED GOOD. FOUND HIGH RESISTENCE IN ANTENNA BONDING. CLEANED SURFACE OF ACFT AND R & R WITH NEW ANTENNA NR 2 COMM BOND, CHECKED GOOD. PERFORMED MX IAW AMM TASK 23-11-26-000-801, 23-11-26-400-801 AND OPS TESTED GOOD IAW TASK 23-11-00-710-801. ALL TESTED GOOD FOR NR 2 COMM AND ANTENNA. RETURNED TO SERVICE.

Part: GENERATOR — FAILED (NR 1) · airframe 9,995 hrs · 11,077 cycles

NR 1 AC GENERATOR WOULD NOT COME ONLINE. FOLLOWED THE EMERGENCY ACTION CHECKLIST. GENERATOR WOULD NOT RESET. REPLACED AC GENERATOR IAW MX 242101, CHECKS GOOD. RETURNED TO SERVICE.

Part: GENERATOR — FAILED (AC ELECTRICAL) · airframe 9,358 hrs · 10,383 cycles

NR 2 ACFT GENERATOR CAUTION LIGHT ILLUMINATED AT APPLICATION OF TAKEOFF POWER. ABORTED TAKEOFF, CLEARED RUNWAY, RAN NR 2 AC GEN CAUTION CHECKLIST, WAS ABLE TO CLEAR NR 2 AC GEN CAUTION LIGHT. REPLACED NR 2 AC GENERATOR IAW T/C 6242101. LEAK CHECKED GOOD. OPS CHECKED NORMAL. RETURNED TO SERVICE.

Part: SKIN — CORRODED (BS 225-227.5) · airframe 9,125 hrs · 10,135 cycles

LEFT FUSELAGE SKIN HAS FRETTING PITS FROM X225.0 TO X227.5 OVER STRINGER 17P. BLENDED AREA, HFEC INSPECTION INDICATED NO CRACKS. RESTORED TOP COAT.

Part: CONTROL PANEL — MALFUNCTIONED (MLG) · airframe 9,036 hrs · 10,051 cycles

NO NOSE GEAR GREEN LIGHT AFTER GEAR DOWN SELECTION. VERIFIED NOSE GEAR DOWN & LOCKED VIA CHECK LIST SECTION 10 IN EMERGENCY AND ABNORMAL CHECK LIST BINDER. PERFORMED ALTERNATE EXTENSION. LANDING UNEVENTFUL. INTEROGATED PSEU, NO NLG FAULTS NOTED. COMPLIED WITH GVI OF NLG FOR OBVIOUS DEFECTS, NONE NOTED. COMPLIED WITH MULTIPLE GEAR SWINGS, NO DEFECTS NOTED AND NO FAULTS FOUND IN PSEU. R & R LANDING GEAR CONTROL PANEL. FUNCTIONAL TESTED GOOD.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 8,297 hrs · 9,274 cycles

RT SIDE GALLEY SERVICE DOOR IS DIFFICULT TO OPEN FROM THE OUTSIDE. APPLIED LUBE TO THE AFT SERVICE DOOR OUTER HANDLE. DOOR OPERATES NORMALLY. NO FURTHER DEFECTS FOUND. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SEQUENCE VALVE — MALFUNCTIONED (MLG) · airframe 8,185 hrs · 9,164 cycles

LANDING GEAR AMBER NOSE DOOR & RED NOSE LIGHTS ILLUMINATED DURING INITIAL CLIMB. RETURNED TO THE FIELD. LANDING UNEVENTFUL. R & R THE FOLLOWING COMPONENTS, NLG SOLENOID SEQUENCE VALVE, MECHANICAL SEQUENCE VALVE (NLG), NLG DOOR ACTUATER NLG DOOR MECHANISM. REPAIRED ELONGATED MOUNTING HOLE FOR LINKAGE ASSY PN 47840. ALL TEST GOOD NO LEAKS NOTED , NO FAULT CODES LOGGED. DUE TO DAMAGE, LT FWD NLG DOOR REPLACED. RETURNED TO SERVICE.

Part: HAND RAIL — DIRTY (PAX DOOR) · airframe 7,378 hrs · 8,343 cycles

F/A REPORTS THE MAIN CABIN DOOR DIFFICULT TO OPEN. INSPECTED AND FOUND FWD HANDRAIL PIVOT PIN ON AIRFRAME BINDING CAUSING DOOR OPENING DIFFICULTY. DISASSEMBLED AND CLEANED DEBRIS FROM PHENOLIC PLATES ON HANDRAIL. REASSEMBLED AND CYCLED DOOR OPEN AND CLOSED SEVERAL TIMES. OPERATION AND INDICATION NORMAL. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 7,377 hrs · 8,342 cycles

F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN. CYCLED DOOR SEVERAL TIMES INSIDE AND OUTSIDE. LUBED DOOR MECHANISMS. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 7,217 hrs · 8,175 cycles

F/A REPORTS HARD TO OPEN AFTER FLIGHT & BEING PRESSURIZED. PERFORMED GVI OF MCD SEAL, HANDLE & MECHANISM W/ NO DEFECTS NOTED. PRESSURIZED A/C IAW AMM TASK 21-00-00-863-801. NOTED NO DIFFICULTY UPON OPENING MCD FROM INSIDE THE ACFT, UPON MX CTL REQUEST PERFORMED LUBRICATION OF FORWARD PASSENGER DOOR IAW AMM TASK 12-20-01-640-805. PERFORMED FUNCTION AL TEST OF FWD PAX DOOR IAW AMM TASK 52-11-00-720-802. FUNCTIONAL TEST GOOD IAW MX CONTROL REQUEST, F/A OPERATED FWD PAX DOOR OPEN/ CLOSE. DOOR OPERATION SATISFIED F/A. NO FURTHER DEFECTS. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: GENERATOR — FAILED (ZONE 400) · airframe 6,875 hrs · 7,823 cycles

NR 2 AC GEN CAUTION LIGHT ILLUMINATED. RETURNED TO THE FIELD. LANDING UNEVENTFUL. R & R NR 2 ACFT GEN IAW AMM TASKS 24-21-01-000-801 & 400-801. PERFORMED OPS TEST IAW AMM TASK 24-21-00-710-801. OPS TEST GOOD. ACFT GEN CAUTION LIGHT DID NOT COME ON. NO FURTHER DEFECTS NOTED. LEAK CHECK COMPLIED WITH. NO LEAKS FOUND. ENGINE INSP COMPLIED WITH IAW AMM TASK 05-53-00-210-819. NO EVIDENCE OF METAL FRAGMENTS FOUND, NO CODES POSTED. RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — NO TEST (NR 2) · airframe 6,554 hrs · 7,492 cycles

AUTOFEATHER TEST FOR THE DAILY FAILS. NR 2 ENGINE DOES NOT TEST AT ALL. NR 1 ENGINE DISPLAYS "A/F TEST ABORT" AFTER STARTING TEST. INSPECTED AND FOUND THE POWER LEVERS OUT OF THE "DISC" POSITION. PERFORMED THE AUTOFEATHER TEST IAW AMM TASK 61-20-00-710-801. CHECKS GOOD, NO DEFECTS. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: PROBE — FAILED (STATIC TEMP) · airframe 6,055 hrs · 6,947 cycles

"PROP DEICE" CAUTION LIGHT ILLUMINATED IN FLIGHT. DID CHECKLIST AND CAUTION LIGHT EXTINGUISHED, HOWEVER, PROP DEICE ADVISORY LIGHTS DID NOT ILLUMINATED. FLIGHT WAS GOING, BUT DIVERTED AND ACCOMPLISHED A UNEVENTFUL LANDING. REMOVED PANEL 263CL, REPLACED STATIC TEMP PROBE. REINSTALLED PANEL 263CL & SEALED. REPLACED PROBE IAW TASK 34-11-11-000-801 & 34-11-11-400-801. OPS CKS NORMAL IAW TK 34-11-11-710-801 & 30-61-00-720-801. CHECKS GOOD. RETURNED TO SERVICE.

Part: OIL CAP — MISSING (NR 1 ENGINE) · airframe 5,303 hrs · 6,077 cycles

NR 1 ENGINE OIL PRESSURE FLUCTUATES BETWEEN NORMAL & CAUTIONARY RANGES. MASTER WARNING TRIPLE CHIME SOUNDED (3) TIMES. CAUTION PANEL DARK WHEN CHECKED IN RESPONSE TO CHIMES. RETURNED TO DEPARTURE. LANDING UNEVENTFUL. FOUND NR 1 ENG OIL FILLER CAP MISSING. R & R OIL FILTER TUBE AND CHECK BALL ASSY AND REPLACED MISSING OIL CAP. SERVICED NR 1 ENG WITH OIL. CW ENGINE INSP AFTER LOW OIL PRESSURE IAW TASK 05-53-00-210-815. REMOVAL OF STARTER/GEN NOT REQUIRED, GEN COOLING FAN USED TO TORN HP ROTOR. NO OIL CONTAMINATION OR CHIP DETECTION NOTED. MAIN OIL PRESSURE DECREASED TO 44 PSID TO 01 PSID FOR A TOTAL OF 27 SECONDS. REF DAA2010-556-PW150A-FA0469 AND TC6-79-45. FOR CONTINUED SERVICEABILITY OF THE NR 1 ENGINE BEYOND 20 SECOND TRANSIENT PER DO. ALL OPS AND LEAK CHECKS GOOD. RETURNED TO SERVICE.

Part: FADEC — MALFUNCTIONED (ZONE 400) · airframe 5,254 hrs · 6,030 cycles

ENROUTE, RECEIVED A POWERPLANT MESSAGE. OVERFLEW LWS AND DIVERTED. R & R NR1 ENG FADEC IAW AMM 73-21-01,OPS CKD GOOD, POWER PLANT MESSAGE CLEARED. C/W HS 73-0026. RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 670) · airframe 4,854 hrs · 5,591 cycles

TOP FLANGE OF NR 15 SEAT TRACK AT FS 670 HAS CORROSION PITTING. BLENDED AREA OF CORROSION AND FOUND OUT OF LIMITS. REPLACED SEAT TRACK BY SPLICING IN NEW TRACK.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 4,854 hrs · 5,591 cycles

CHAFE ON THE UPPER SURFACE OF THE LT OTBD FLAP AT STA -263 TO -209. CHAFE FOUND TO NOT BE PAST THE CLAD LAYER OF THE MATERIAL. PRIMED AND PAINTED OK FOR SERVICE.

Part: DIAPHRAGM — CRACKED (LT NACELLE) · airframe 4,854 hrs · 5,591 cycles

LT NACELLE UPPER OTBD WING TO NACELLE SUPPORT DIAPHRAGM IS CRACKED. REPLACED DIAPHRAGM IAW SRM 51-42-05

Part: SEAT TRACK — CORRODED (BS 706-712) · airframe 4,854 hrs · 5,591 cycles

PDX - C1 CHECK - ON LT INBD SEAT TRACK NR 9 HAS VARIOUS AREA OF CORROSION ON INSIDE AND TOP OF CLAWS FROM APPROX STA X706 TO X712. BLENDED AND POLISHED REMOVING ALL CORROSION. MAX MATERIAL LOSS ON TOP OF TRACK WAS .007, INSIDE TRACK CLAWS WAS .010. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3167. ALODINED ALL BARE METAL PRIMER AND PAINT TO REQUIRED IN THIS AREA. HFEC IAW NDTM PART 6 51-00-01, NO CRACKS NOTED.

Part: SEAT TRACK — CORRODED (BS 481) · airframe 4,854 hrs · 5,591 cycles

C1 CHECK - RT INBD SEAT TRACK NR 13 HAS CORROSION ON TOP OF CLAWS AT APPROX STA X481. BLENDED AREA OF CORROSION TO REMOVE DAMAGE AND FOUND IT TO BE WITHIN LIMITS IAW RD 8/4-53-884 WITH .012" OF MATERIAL REMOVED FROM THE TOP SURFACE OF THE LUGS. ALODINED BARE AREA IAW SRM 51-21-10. HFEC IAW NDTM PART 6 51-00-01, NO CRACKS NOTED.

Part: SEAT TRACK — CORRODED (BS 783) · airframe 4,854 hrs · 5,591 cycles

C1 CHECK - LT SEAT RAIL HAS CORROSION AT STA X783.102 UNDER THE TIE DOWN. BLENDED CORROSION AND POLISHED SMOOTH IAW RD 8/4-53-2362. MAX MATERIAL REMOVED .038" FROM TOP OF CLAW AND .047" FROM INSIDE OF CLAW. TRACK FOUND TO REMAIN WITHIN LIMITS IAW R/D 8/4-53-2362. HFEC INSPECTED BLENDED AREAS FOR CRACKS IAW -8 NDTM PART 6 51-00-01, NO CRACKS NOTED. ALODINED ALL BARE METAL, PRIMER AND PAINT NOT REQUIRED IN THIS AREA.

Part: SEAT TRACK — CORRODED (BS 154-156) · airframe 4,854 hrs · 5,591 cycles

C1 CHECK - ON RT INBD SEAT TRACK NR 12 AT APPROX STA X154-X156 THERE IS CORROSION INSIDE THE TRACK. REMOVED CORROSION BY BLENDING AND POLISHING SMOOTH. MAX MATERIAL LOSS WAS .008. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-884. ALODINED ALL BARE METAL. HFEC IAW NDTM PART 6 51-00-01, NO CRACKS NOTED.

Part: SEAT TRACK — CORRODED (BS 373) · airframe 4,854 hrs · 5,591 cycles

C1 CHECK - ON RT INBD SEAT TRACK 13 AT APPROX STA X373.15 THERE IS CORROSION ON THE CLAWS AND INSIDE THE TRACK. REMOVED CORROSION BY BLENDING AND POLISHING SMOOTH. MAX MATERIAL LOSS WAS .012 INSIDE CLAW AND .005 ON TOP. FOUND IT TO BE WITHIN LIMITS IAW RD 8/4-53-884. ALODINED ALL BARE METAL. NO PRIMER OR PAINT REQUIRED IN THESE AREAS. HFEC IAW -8 400 NDTM PART 6 51-00-01, NO CRACKS NOTED.

Part: SEAT TRACK — CORRODED (BS 706-712) · airframe 4,854 hrs · 5,591 cycles

C1 CHECK - RT SEAT RAIL HAS PITTING AT STA X706 TO X712. REMOVED CORROSION IAW RD 8/4-53-2362 STEPS 1 AND 3. MAX MATERIAL REMOVED .015" FROM TOP OF CLAW AND .014" FROM INSIDE OF CLAW. TRACK FOUND TO REMAIN WITHIN LIMITS IAW R/D 8/4-53-2362. HFEC INSPECTED BLENDED AREAS FOR CRACKS IAW RD 8/4-53-2362 GENERAL NOTE 2 & -8 NDTM PART 6 51-00-01, NO CRACKS NOTED.

Part: SEAT TRACK — CORRODED (BS 720-743) · airframe 4,854 hrs · 5,591 cycles

C1 CHECK - RT AFT SEAT RAIL HAS PITTING AT STA X720 TO X743. REMOVED CORROSION IAW RD 8/4-53-2362 STEPS 1 AND 3. MAX MATERIAL REMOVED .010" FROM INSIDE CLAW. FOUND TO REMAIN WITHIN LIMITS IAW R/D 8/4-53-2362. HFEC INSPECTED BLENDED AREAS FOR CRACKS IAW RD 8/4-53-2362 GENERAL NOTE 2 & -8 NDTM PART 6 51-00-01, NO CRACKS NOTED.

Part: SEAT TRACK — CORRODED (BS 635) · airframe 4,854 hrs · 5,591 cycles

C1 CHECK - RT INBD SEAT TRACK NR15 HAS CORROSION ON THE INSIDE OF CLAWS AT APPROX STA X635. BLENDED AREA OF CORROSION TO REMOVE DAMAGE AND FOUND IT TO BE WITHIN LIMITS IAW RD 8/4-53-884 WITH .040" OF MATERIAL REMOVED FROM INSIDE OF CLAWS. ALODINED AREA IAW SRM 51-21-10. HFEC IAW -8 400 NDTM PART 6 51-00-01, NO CRACKS NOTED.

Part: SEAT TRACK — CORRODED (BS 111) · airframe 4,854 hrs · 5,591 cycles

C1 CHECK - ON RT INBD SEAT TRACK NR 12 AT APPROX STA X111 THERE IS CORROSION AT AFT INSIDE THE TRACK. REMOVED CORROSION BY BLENDING AND POLISHING SMOOTH. MAX MATERIAL LOSS WAS .006. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-884. ALODINED ALL BARE METAL. HFEC IAW NDTM PART 6 51-00-01, NO CRACKS NOTED.

Part: SEAT TRACK — CORRODED (BS 211-212) · airframe 4,854 hrs · 5,591 cycles

C1 CHECK - ON LT INBD SEAT TRACK NR6 AT APPROX STA X211-X212 THERE IS CORROSION INSIDE THE TRACK. REMOVED CORROSION BY BLENDING AND POLISHING SMOOTH. MAX MATERIAL LOSS WAS .006. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-884. ALODINED ALL BARE METAL. HFEC IAW NDTM PART 6 51-00-01, NO CRACKS NOTED.

Part: SEAT TRACK — CORRODED (BS 388-391) · airframe 4,854 hrs · 5,591 cycles

C1 CHECK - ON RT INBD SEAT TRACK NR 13 AT APPROX STA X388 TO X391 THERE IS CORROSION INSIDE THE TRACK. REMOVED CORROSION BY BLENDING AND POLISHING SMOOTH. MAX MATERIAL LOSS WAS .011. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-884. ALODINED ALL BARE METAL. NO PRIMER OR PAINT REQUIRED IN THESE AREAS. HFEC IAW -8 400 NDTM PART 6 51-00-01, NO CRACKS NOTED.

Part: SEAT TRACK — CORRODED (BS 391) · airframe 4,854 hrs · 5,591 cycles

C1 CHECK - ON RT INBD SEAT TRACK NR10 AT APPROX STA X3.0 TO X391 THERE IS A PIT OF CORROSION AT AFT MOUNT HOLE FOR THE LAV. REMOVED CORROSION BY BLENDING AND POLISHING SMOOTH. MAX MATERIAL LOSS WAS .022. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-884. ALODINED ALL BARE METAL. HFEC IAW NDTM PART 6 51-00-01, NO CRACKS NOTED.

Part: SEAT TRACK — CORRODED (BS 720-743) · airframe 4,854 hrs · 5,591 cycles

C1 CHECK - LT AFT SEAT RAIL HAS PITTING AT STA X720 TO X743. REMOVED CORROSION IAW RD 8/4-53-2362 STEPS 1 AND 3. MAX MATERIAL REMOVED .026" FROM INSIDE CLAW. HFEC INSPECTED BLENDED AREAS FOR CRACKS IAW RD 8/4-53-2362 GENERAL NOTE 2 & -8 NDTM PART 6 51-00-01, NO CRACKS NOTED.

Part: SEAT TRACK — CORRODED (BS 783) · airframe 4,854 hrs · 5,591 cycles

C1 CHECK - RT AFT SEAT RAIL HAS CORROSION AT STA X783.102 UNDER THE TIE DOWN. REMOVED CORROSION IAW RD 8/4-53-2362. MAX MATERIAL REMOVED .013" FROM TOP OF CLAW AND .024" FROM INSIDE OF CLAW. TRACK FOUND TO REMAIN WITHIN LIMITS IAW R/D 8/4-53-2362. HFEC INSPECTED BLENDED AREAS FOR CRACKS IAW RD 8/4-53-2362, GEN NOTE 2 & -8 NDTM PART 6 51-00-01, NO CRACKS NOTED.

Part: RUDDER CONTROL — LOCKED · airframe 4,485 hrs · 5,185 cycles

DESCENDING THRU 12000, F/O TRIED TO CTR RUDDER WITH RUDDER PEDALS. APPLIED HEAVY PRESSURE TO RT RUDDER. RUDDER BECAME FREE (BROKE FREE) AND ACFT YAWED WITH AP ON. AIRSPEED WAS AROUND 270KTS. THEN, WITH POWER BACK TO SLOW ACFT, NEEDED LT RUDDER. F/O SAID IT WAS LOCKED AGAIN. TOOK ACFT AND WITH AP OFF PUSHED ON THE LT RUDDER WITH HEAVY PRESSURE UNTIL IT CAME FREE (BROKE FREE) CAUSING THE ACFT TO YAW (DUE TO THE AMOUNT OF FORCE APPLIED TO FREE IT) THEN IT WORKED FINE. COULD MOVE THE RUDDER PEDALS NORMALLY WITH MY TOES. GAVE ACFT BACK TO F/O. SAID RUDDERS WERE FINE, THEN LATER SAID THEY ARE LOCKED AGAIN. COULD FREE THE RUDDER EACH TIME WITH A LITTLE YAW OF THE ACFT. CONFIRMED THE RUDDERS WERE LOCKED EACH TIME AND COULD FREE THEM. ALSO, BELIEVE THEY LOCKED 3-5 TIMES. PERFORMED GVI OF RUDDER CONTROL SYS, NO DEFECTS NOTED. PERFORMED OPS TEST OF RUDDER CONTROL SYS, NO DEFECTS NOTED. OPS TEST GOOD. COMPLETED FREEDOM OF MOVEMENT CHECK, ENSURED FULL TRAVEL AND VERIFIED PROPER DIRECTION OF MOVEMENT, NO DEFECTS NOTED IAW GPM 9.2.5. ACFT RETURNED TO SERVICE.

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 4,382 hrs · 5,054 cycles

SEA - CLIMBING OUT OF 16,000 "DOOR WARNING" MESSAGE. DOOR HANDLE POPPED. RETURNED TO THE FIELD. LANDING UNEVENTFUL. UPON AIRCRAFT ARRIVAL DISCOVERED AFT SERVICE DOOR EXTERNAL HANDLE NOT FLUSH. PERFORMED OPS TEST OF THE AFT SERVICE DOOR IAW AMM TASK 52-41-00-710-801. CYCLED DOOR NUMEROUS (MORE THAN 10) TIMES. NO DEFECTS NOTED. DOOR OPERATED SMOOTHLY AND CORRECTLY. PERFORMED GVI OF DOOR SURROUND AND STRUCTURE NO DEFECTS NOTED. A/C OK FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 3,931 hrs · 4,508 cycles

RECEIVED A FLAP POWER CAUTION MESSAGE. PERFORMED A ZERO FLAP LANDING WITHOUT INCIDENT. PERFORMED RESET PROCEDURE IAW DH8-400-SL-27-002A. NO DEFECTS NOTED. NO FAULTS NOTED IN CDS. SENT CDS INFO TO TECH FOR ANALYSIS. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: PROXIMITY SENSOR — MALFUNCTIONED (NLG) · airframe 3,723 hrs · 4,275 cycles

ON APPROACH AFTER DROPPING LANDING GEAR 3 GREEN LANDING GEAR LIGHTS ILLUMINATED BUT THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. LANDING UNEVENTFUL. REPLACED NG DRCL PROX SENSOR IAW AMM TASKS 32-61-06-000-802 AND 32-61-06-400-801, ALL CHECKS GOOD, NO DEFECTS NOTED.

Part: TRANSDUCER — OUT OF ADJUST (ELEVATOR SYS) · airframe 2,951 hrs · 3,342 cycles

PDX - DURING CRUISE FLIGHT AT 23,000 "ELEV ASYMMETRY" CAUTION ILLUM. C/W CHECKLIST. DIVERTED TO ALTERNATE AIRPORT PDX (30 MILES NORTH AT THE TIME). THE CAUTION LIGHT WENT OUT UPON LANDING. LANDING UNEVENTFUL. INSP ELEV ASYM IAW Q400 FIM 27-30-00-810-801 CAUTION LIGHT DID NOT RETURN. PERFORMED ASYM CHECK OF ELEV IAW Q400 AMM 27-31-00-750-801. NO DEFECTS. CHECKED VALUES OF ELEV LVDT'S THROUGH FDR AT ZERO, 20, 30 DEG WITHIN LIMITS PER AMM 27-31-61-830-801. INSP ELEV LT FWD QUADRANT AND RT QUADRANT TO RT AFT QUAD ELEV CABLE TENSIONS. TENSION WITHIN SPECS. INSP AND FOUND LEFT AND RIGHT LVDT'S OUT OF ADJUSTMENT BY APPROX 1.25 DEG FROM EACH OTHER. RIGGED IAW Q400 AMM 27-31-61-830-801, NO OTHER DEFECTS. CHECK FLIGHT OK. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: UNKNOWN — ODOR (CABIN) · airframe 2,847 hrs · 3,236 cycles

PDX - AFT F/A REPORTS AN UNUSUAL ODOR FROM ROW 17 TO THE AFT GALLEY. PLACED THE RECIRC FAN ON MEL 21-20-2. CLEARED MEL 7/28. PERFORMED OPERATIONAL TEST OF THE RECIRC FAN IAW Q400 AMM SUBTASK 21-22-16-710-001. OPS CHECK GOOD. NO UNUSUAL ODOR DETECTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: ELEVATOR SYSTEM — MALFUNCTIONED · airframe 2,581 hrs · 2,917 cycles

BOI - ELEVATOR ASYMMETRY CAUTION LIGHT ILLUMINATED IAS ABOVE 185 KTS. RETURNED TO THE FIELD. LANDING UNEVENTFUL. ON LANDING IN BOISE CAUTION LIGHT EXTINGUISHED. C/W FIM TASK 27-30-00-810-801 ELEVATOR ASYMMETRY CAUTION FAULT ISOLATION FOUND CODE ELEV ASSYM FAILURE STATUS MSG, CLEARED PER FIM. FAULT DID NOT RE-OCCUR. C/W OPERATIONAL TEST OF THE FCECU PER TASK 27-00-01-710-802, OPS CHECK GOOD. NO DEFECTS NOTED A/C OK'D FOR SERVICE. FAULTS DID NOT RE-OCCUR IN CDS. NO PARTS REPLACED.

Part: LIGHT — UNKNOWN (EMERGENCY) · airframe 2,117 hrs · 2,379 cycles

PDX - EMERGENCY LIGHTS DISARMED CAUTION LIGHT DOES NOT ILLUMINATE WHEN EMERGENCY LIGHT SWITCH PLACED OFF. BULB CHECKS GOOD. MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM FOUND NO DISCREPANCY IAW AMM TASK 33-51-00-710-801. OPS CHECK GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: PROXIMITY SENSOR — FROZEN (PAX DOOR) · airframe 1,311 hrs · 1,421 cycles

"CABIN DOORS" WARNING LIGHT ILLUMINATED CLIMBING THROUGH 5000'. DOORS PAGE REVEALED AFT PASSENGER DOOR AJAR. PRESSURIZATION SEEMED TO BE NORMAL. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. INSPECTED AFT PASSENGER DOOR HANDLES, ALL ARE FLUSH WITH DOOR. INSPECTED PROX SENSORS AND FOUND ICE ON DOOR PROX. CLEANED AND LUBED AND REMOVED ICE. SENSOR OPS CK GOOD. ACFT OK FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: HANDLE — STIFF (AIRSTAIR DOOR) · airframe 1,035 hrs · 1,120 cycles

SEA - FLIGHT ATTENDANT ADVISES INSIDE HANDLE ON MAIN CABIN DOOR IS EXTREMELY HARD TO LIFT WHEN OPENING DOOR. PERFORMED FUNCTIONAL CHECK OF AIRSTAIR DOOR IAW TASK NR 52-11-00-720-802. DOOR UNLOCKING LOAD FRONT INTERIOR HANDLE IS 45 LBS AFTER LUBING DOOR IAW TASK NR 52-11-00-640-801. NO DEFECTS NOTED, COULD NOT DUPLICATE. RETURNED TO SERVICE.