N816FD

Part: CANISTER — LEAKING (FUEL CELL) · airframe 56,413 hrs · 11,551 cycles

RT WING SLAT JACKSCREW NR 3 CANISTER DRAIN PORT HAD FUEL SEEPAGE IAW EA 6-5710-149029. REMOVED FUEL PANEL 540BB, 540CB IAW AMM 28-11-22. RE-SEALED SCREWJACK CANISTER IAW EO 6-5710-7-3304C PT1. RE-INSTALLED FUEL PNL 540BB, 540CB IAW AMM 28-11-22. LEAK CHECKED RT WING SLAT JACKSCREW NR 3 AND MANHOLE COVER (540BB, 540CB) IAW AMM 28-11-00. NO LEAK FOUND . REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FUEL CELL — LEAKING (RT WING) · airframe 56,413 hrs · 11,551 cycles

RT WING FRONT SPAR HAD FUEL SEEPAGE AT RIB 18. REMOVED AND CLEANED THE DAMAGED SEALANT AREA. RE-APPLIED NEW SEALANT FOR REPAIRING IAW EO 6-5710-7-3304, PT3 AND EA 6-5710-149029. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FUEL CELL — LEAKING (RT WING) · airframe 56,413 hrs · 11,551 cycles

RT WING BOTTOM SKIN HAD FUEL SEEPAGE AT SLAT TRACK NR9 CANISTER DRAIN PORT FASTENER. REMOVED AND CLEANED THE DAMAGED SEALANT AREA. RE-APPLIED NEW SEALANT FOR REPAIRING IAW EO 6-5710-7-3304 PT3 AND EA 6-5710-149029 (FOR REPAIR OF FUEL TANK SEALING). THE REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: DOOR — GOUGED (COCKPIT) · airframe 56,413 hrs · 11,551 cycles

FOUND CREW DOOR GOUGED. REPAIRED IAW EA 6-52-50-149021 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — DENTED (TE FLAP) · airframe 56,413 hrs · 11,551 cycles

RT WING T/E OTBD FLAP UPPER SURFACE DENTED. REPAIRED IAW SRM 57-53-12 FIG 210. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED · airframe 56,413 hrs · 11,551 cycles

LEFT NOSE SECTION/ FR 12A STIFFENER FITTING WAS FOUND 1 EA CRACK ABOUT .7500" IN LENGTH . ON ZONE B,J AREA IAW NTM 51-10-08, PART 1. REMOVED STIFFENER FITTING AND JUNCTION FITTING. INSTALLED STIFFENER FITTING AND JUNCTION FITTING WITH NEW PART REFER TO EO 65340-7-5002P3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 56,413 hrs · 11,551 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 162AF HAS EDGE IMPACT DAMAGED. FOUND OUT OF LIMITS. REPLACED THE FLOOR PANEL BY FABRICATION OF A NEW PANEL WITH ADHESIVE AND INSERTS IAW SRM 53-10-20 & DWG A53279966. REPAIR MINOR PER GMM 6-2-100.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 56,330 hrs · 11,507 cycles

EMERGENCY LIGHTS WOULD NOT TEST PROPERLY. R & R EMERGENCY LIGHT POWER SUPPLY AND BATTERY IAW MM 33-51-14-04-09. OK FOR SERVICE.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 54,302 hrs · 10,203 cycles

LOWER AFT CORNER OF L - 1 DOOR HAS 3/16 INCH ARC CUT OUT DAMAGED AREA AND INSTALLED REPAIR OF OUTER SKIN IN CORNER AREA OF L-1 DOOR LOWER AFT CORNER,FR 17, STRINGER 25 LT IAW A310 SRM 52-11-00,FIG 206,PAGE 239/240

Part: SKIN — DENTED (ZONE 300) · airframe 54,302 hrs · 10,203 cycles

ON WALK AROUND FOUND DENT ON LOWER FUSELAGEAFT OF RADOME BETWEEN FRAME O AND FRAME 1 CUT OUT DAMAGED AREA IAW A310 SRM 53-11-12 FIG. 201. INSTALLED PERMANENT REPAIR IAW A310 SRM 53-11-12 FIG. 201. BETWEEN FRAME 0 AND FRAME 1 AT FUSELAGE LOWER CENTERLINE.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 53,234 hrs · 9,511 cycles

UPON CLIMB-OUT CABIN VERTICAL SPEED EXCEEDED 2000FPM, AT 15000 ALT CAB ALT EXCEEDED 10,000. OUTBOARD EXTRACT VALVE FAULTED, UNABLE TO MANUALLY CONTROL CABIN PRESS. REACTIVATED SYSTEM. FAILED OPS CHECKED AS PER AMM 21-23-00-5, VALVE NEVER MOVED. T/S AS PER WDM, R&R RELAY 69HR, NO HELP. R&R OVERBOARD EXTRACT VALVE AS PER AMM 21-23-13-4, OPS CHECKED GOOD, OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 52,523 hrs · 9,107 cycles

AFTER LIFT-OFF ACRID SMOKE ODOR AND EYES HAD BURNING SENSATION. LEVEL OFF AT 10,000 FT. NO CLEARING. OPENED RAM AIR ON DESCENT TO CLEAR AIR. SHUT OFF NR 2 PACK AS IT HAD A HIGH TEMP 55 DEG C. NO OTHER WARNINGS. REPLACED CHECK VALVES 291394,293388,291388,292388. CLEANED AND BLEW OUT BLEED AIR PRESSURE LINE STARTING AT 14TH STAGE RESTRICTOR 291392 ENDING AT CHECK VALVE 291378 PERFORMED POWER ASSURANCE CHECK PER JRH. RAN NR 1 PACK FULL HOT/FULL COLD DURING POWER ASSURANCE CHECK WITH NUMBER ONE ENGINE BLEED. UPON RETURN TO THE GATE, FOUND ONLY MOISTURE IN FILTER 291376, REF MM 29-14-00-0. CHANGED FILTER PER 29-14-00-0. NO HYDRAULIC FLUID ODOR IN CABIN/COCKPIT DURING RUN.

Part: B-NUT — LEAKING (HYD LINE) · airframe 52,526 hrs · 9,110 cycles

AFTER ENGINE START CREW REPORTED SMOKE IN THE COCKPIT COMING FROM THE CASPER VENTS. FOUND HYDRAULIC RETURN LINE B NUT LEAKING AT PYLON ON NR 1 ENGINE. SECURED AND OPERATED ENGINE WITH NO LEAKS REMOVED AND REPLACED NR 1 PACK COALESCER BAG PER MM 21-51-16-3. OPERATED PACKS USING ENGINE BLEED AIR WITH NO SKYDROL VAPOR. COMPLETED PROCEDURE FOR CLEARING CONTAMINATION FROM A/C PACKS PER AMM 21-50-00-3. CLEANED COALESCER BAGS PER AMM 21-51-16-3. OK FOR SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,242 hrs · 8,927 cycles

DEVIATION TO EO 6-5310-7-5020, SB A310-53-2124, AD 2006-02-06, CRACKS IN FRAME FEET , C45, C46 LT REPAIR PERFORMED BY CRACK REMOVING THRU OVERSIZING IAW EA 6-5315-106424 AND RAS 049395/047/2007 ISS A.

Part: FRAME — CRACKED (ZONE 100) · airframe 52,242 hrs · 8,927 cycles

DEVIATION TO EO 6-5310-7-5020-SB A310-53-2124- AD 2006-020-06, CRACKS IN FRAME FEET C43, C46 RT REPAIR PERFORMED BY REMOVING THE CRACKS THRU OVERSIZING IAW EA 6-5315-106424 AND RAS 049395/047/2007 ISS. A

Part: RIB — CRACKED (TE FLAP) · airframe 52,242 hrs · 8,927 cycles

FOUND OLD CRACK REPAIR ON INBOARD FLAP RT, RIB 21 (POCKET REPAIR). REPAIR WAS PERFORMED BY REPLACEMENT OF RIB 21 IAW SB A310-57-2055, APPROVED BY EA 6-5752-106443.

Part: FAIRING — CRACKED (ZONE 500) · airframe 52,242 hrs · 8,927 cycles

CRACKED SHIM PLATE AT INNER SIDE AFT AREA OF LT NR 3 FLAP TRACK FIXED FAIRING. REPAIR PERFORMED BY WET LAY-UP PER SRM 57-20-35 AND INSERT INSTALLATION, APPROVED BY EA 6-5720-106421 AND RAS/FOK/016/2007 ISS. A

Part: ATTACH FITTING — CORRODED (ZONE 400) · airframe 52,242 hrs · 8,927 cycles

FOUND CORROSION IN AFT PYLON ATTACH FITTING HOLE , PYLON NR 2, RIB 18 REPAIR PERFORMED WITH SB A31-52-2021, APPROVED BY EA 6-5450-106340.

Part: ATTACH FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 52,242 hrs · 8,927 cycles

CORROSION IN AFT PYLON ATTACH FITTING HOLE , PYLON NR 2, RIB 18 REPAIR PERFORMED WITH SB A31-52-2021, APPROVED BY EA 6-5450-106340.

Part: SKIN — DAMAGED (ZONE 100) · airframe 52,242 hrs · 8,927 cycles

OLD EXTERNAL DOUBLER REPAIR AT C38/38A, P44 RT REPAIR WAS PERFORMED IAW LHT SDR 0226/007536, APPROVED BY EA 6-5314-106414 AND RAS/DABRE/7005488/2005 ISS.A

Part: FAIRING — DAMAGED (ZONE 100) · airframe 52,242 hrs · 8,927 cycles

REPAIR DAMAGE TO FAIRING 577EL REPAIR WAS PERFORMED BY WET LAY-UP REPAIR IAW EA 6-5317-106416 AND RAS/DAHAM/4021689/2007 ISS.A

Part: FRAME — CRACKED (ZONE 100) · airframe 52,242 hrs · 8,927 cycles

MILLED FRAME CRACKED, C22, P26, RHS REPAIR PERFORMED BY REPLACEMENT OF FITTING IAW EA 6-5313-106374 AND RAS/DABRE/7007381/2007 ISS. A.

Part: SKIN PANEL — GOUGED (ZONE 100) · airframe 52,242 hrs · 8,927 cycles

TWO MISDRILLED HOLES THROUGH THE SKIN PANEL, INTERNAL DOUBLER, C17 FLANGE AND CONNECTING FITTINGS AT P44 LT. REPAIR PERFORMED BY REPLACING CONNECTING FITTINGS P44 BY NEW ONES; INSTALLING STEEL REPAIR BUSHES IN SKIN PANEL, INTERNAL DOUBLER C17 FLANGE AND C17 FLANGE USING NEW FASTENERS NSA5022-4 ALL IAW RAS/AS/0006/2007 ISS "A" AND EA 6-5312-106418.

Part: BULKHEAD — GOUGED (ZONE 100) · airframe 52,242 hrs · 8,927 cycles

SOME GOUGES FOUND AT BULKHEAD 54, APPROX Y-953 AND Z-957, REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-106419 AND RAS 049380/2007 ISS. A

Part: FRAME — CRACKED (ZONE 100) · airframe 52,242 hrs · 8,927 cycles

DEVIATIONS TO EO 6-5710-7-3322 (CRACKS IN HOLE 23 AND 62 LT). REPAIR PERFORMED BY OVERSIZING HOLE 23 AND 62 LT IAW EA 6-5710-106423 AND RAS/049817/013/2007 ISSUE "A".

Part: MOUNT — CHAFED (ZONE 400) · airframe 52,242 hrs · 8,927 cycles

OLD CHAFING MARK ON PYLON NR 1 FWD PYLON TO ENGINE MOUNT FITTING. REPAIR PERFORMED BY INSTALLATION OF AN PROTECTION ANGLE, APPROVED BY RAS 018876/027/2002 ISSUE "A" AND EA 6-5450-106441.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 52,242 hrs · 8,927 cycles

OLD SCRATCH REPAIR ON EXTERNAL SKIN BETWEEN C75/76, P27. REPAIR VERIFICATION, PERFORMED IAW SRM 53-18-12/FIG 102 EA FOR TRACKING: 6-5318-106413.

Part: FITTING — DAMAGED (ZONE 100) · airframe 52,242 hrs · 8,927 cycles

MISDRILLED HOLES IN C17 AT P44 LT. REPAIR WAS PERFORMED BY BUSHING REPAIR AND NEW FITTING INSTALLATION (P/N A536-10607-206-93, A536- 10607-207-93) IAW EA 6-5312-106418 AND RAS/AS/006/2007 ISSUE "A".

Part: SKIN — CHAFED (ZONE 200) · airframe 52,242 hrs · 8,927 cycles

CHAFE MARKS ON C38.1, P14-15 LT SIDE. REPAIR WAS PERFORMED BY BLEND OUT IAW EA 6-5314-106417 AND RAS/DATLS/0003560/2007 ISS. B

Part: SKIN — DAMAGED (ZONE 100) · airframe 52,242 hrs · 8,927 cycles

DOUBLE HOLE ON FUSELAGE SKIN AT C67, P35 RHS REPAIR WAS PERFORMED BY BUSH REPAIR IAW SRM 51-40-51, APPROVED BY EA 6-53176-106410 AND RAS/DAHAM/4021719/2007 ISS. A

Part: VANE — DAMAGED (ZONE 600) · airframe 52,242 hrs · 8,927 cycles

CHAFE MARK ON INBOARD FLAP VANE. REPAIR WAS PERFORMED.

Part: SKIN — CHAFED (ZONE 800) · airframe 52,242 hrs · 8,927 cycles

TWO OLD NICK/CHAFING MARKS AT THE INTERNAL SKIN OF FWD CARGO DOOR C20A-25A, LONGERON 4-5. REPAIR WAS PERFORMED BY INSTALLING A DOUBLER IAW LHT SDR.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,242 hrs · 8,927 cycles

CORROSION AT MAIN DECK FLOOR STRUCTURE PARTS C74-75, P26 LT/RT, CONNECTING SECTION P/N A539-80458-200-90, P/N A539-80464-200-51 AND P/N A539-80464-201-00. PARTS REPLACED IAW SRM 51-72-10.

Part: SKIN — CRACKED (ZONE 600) · airframe 52,242 hrs · 8,927 cycles

RT WING BOTTOM SKIN PANEL NR 2, AFT OF REAR SPAR INBOARD OF RIB 11 CRACKED. REPAIR WAS PERFORMED IAW REPAIR DRAWING R572-49152-001 AND SB A310-57-2066 (DOUBLER INSTALLED).

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,242 hrs · 8,927 cycles

AFT CARGO COMP FLOORBEAM AT C63 LT, Y 445 CORRODED. REPAIR WAS PERFORMED IAW SRM 53-10-15/FIG 207 BY LHT SDR.

Part: SHAFT — CHAFED (ZONE 800) · airframe 52,242 hrs · 8,927 cycles

OLD CHAFING MARK ON PAX DOOR NR 1 RT AT LOCKING CONTROL SHAFT. REPAIR WAS PERFORMED BY BLEND OUT IAW LHT SDR.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,242 hrs · 8,927 cycles

FOUND CORRODED STRINGER P52 AND P53, C65-66. REPAIR WAS PERFORMED IAW SRM 53-10-14.

Part: STRINGER — CHAFED (ZONE 100) · airframe 52,242 hrs · 8,927 cycles

OLD CHAFING MARKS BETWEEN C44-45, P45 LT. REPAIR PERFORMED BY BLEND OUT IAW LHT SDR.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,242 hrs · 8,927 cycles

FOUND CORROSION AT MAIN DECK FLOOR STRUCTURE PARTS C74-75, P26 LT/RT (CONNECTING SECTION P/N A539-80458-200-90, P/N A539-80464-200-51 AND P/N A539-80464-201-00). PARTS REPLACED IAW SRM 51-72-10.

Part: LONGERON — BENT (ZONE 800) · airframe 52,242 hrs · 8,927 cycles

APU ACCESS DOOR LT/RT LOWER LONGERON, OLD BENT REPAIR. REPAIR WAS PERFORMED BY CUT OUT AND INSTALLATION OF NEW LONGERON SECTION.

Part: STIFFENER — DAMAGED (ZONE 600) · airframe 52,242 hrs · 8,927 cycles

RT WING, SHROUD BOX F/S SPAR, DAMAGE BY MAIN BARREL PIN. REPAIR WAS RENEWED BY REPLACEMENT OF VERTICAL STIFFENER.

Part: DOOR FRAME — DAMAGED (ZONE 100) · airframe 52,242 hrs · 8,927 cycles

OLD MARKS ON FWD CARGO DOOR FRAME FWD LOWER CORNER. REPAIR WAS PERFORMED BY BLEND OUT WITH LHT SDR.

Part: ATTACH FITTING — CHAFED (ZONE 400) · airframe 52,242 hrs · 8,927 cycles

PYLON NR 2, CHAFING MARKS ON INBOARD SIDE OF PYLON-TO-ENGINE ATTACH FITTING. REPAIR WAS PERFORMED BY BLEND OUT AND RESTORE PROTECTION.

Part: ATTACH FITTING — DAMAGED (ZONE 300) · airframe 52,242 hrs · 8,927 cycles

V/S TAPERED ATTACH FITTINGS LT REAR, RT REAR AND RT CENTER BRONZE PLATING MISSING. PARTS REPLACED IAW AMM 55-30-11/401, P/N A555-72151-000-00 (1 EA.) AND P/N A555-72201-000- 00 (2 EA.)

Part: BEAM — DAMAGED (ZONE 100) · airframe 52,242 hrs · 8,927 cycles

TWO LONGITUDINAL BEAMS BETWEEN C64-65, -Y 525 AND Y 805 WITH WRONG EXISTING HOLES. PARTS REPLACED IAW SRM 51-72-10.

Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,242 hrs · 8,927 cycles

FOUND CORRODED CROSSBEAM AT C67, Y-1070-1115. PART REPLACED IAW SRM 51-72-10.

Part: WEB — CHAFED (ZONE 500) · airframe 52,242 hrs · 8,927 cycles

CHAFING MARK AT BACK WALL OF KRUEGER FLAP CHAMBER. REPAIR WAS PERFORMED BY BLEND OUT AND REPROTECT.

Part: RIB — CHAFED (ZONE 600) · airframe 52,242 hrs · 8,927 cycles

KRUEGER BOX RT, DAMAGED REPAIR, ABRASION IN AN SUPPORT FLANGE OF RIB 2B. REPAIR WAS PERFORMED BY BLEND OUT.

Part: SKIN — DENTED (ZONE 800) · airframe 52,242 hrs · 8,927 cycles

OLD DENT REPAIR ON BULK CARGO DOOR OUTER SKIN BETWEEN BEAM 1-2 AND BEAM 4-5. REPAIR WAS PERFORMED BY INSTALLING EXTERNAL DOUBLER BETWEEN BEAM 4-5 AND BLEND OUT BETWEEN BEAM 1-2 IAW LHT SDR.

Part: SKIN — DELAMINATED (ZONE 800) · airframe 52,242 hrs · 8,927 cycles

OLD REPAIR ON LT MLG DOOR, DELAMINATED SKIN. REPAIR WAS PERFORMED BY FILL OUT THE DELAMINATED AREA IAW LHT SDR.

Part: HINGE — MISINSTALLED (ZONE 800) · airframe 52,242 hrs · 8,927 cycles

RT MLG FITTING BUSH, WRONG INSTALLATION. REPAIR WAS PERFORMED IAW EA 6-5281-106381 AND RAS/CASA/5328/2007 ISSUE "A" AND RAS/AS/228/95 ISSUE "A".

Part: SKIN — DAMAGED (WING) · airframe 52,242 hrs · 8,927 cycles

ELONGATED HOLES IN LT BOTTOM WING SKIN AT PYLON SUPPORT BRACKET. REPAIR WAS PERFORMED IAW EA 6-5720-106422, DRAWING R572-49184 AND RAS/BAE/1004144/2007 ISSUE "A".