N929DN

Part: FITTING — BROKEN (TAILCONE) · airframe 44,794 hrs · 30,748 cycles

INTERNAL RELEASE HANDLE CLIP BROKEN FOR TAIL CONE. CLIP REPLACED.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 44,794 hrs · 30,748 cycles

CORROSION AT MID CARGO DOOR THRESHOLD SILL AREA. REMOVED CORROSION AS REQ AND FOUND OUT OF LIMITS IAW SRM 53-60-02. INSTALLED DOUBLER AND SPACER PER SRM 53-60-02 PARA 11 FIG 9. INSTALLED FWD AND AFT SCUFF PLATE. INSTALLED STOP FITTINGS.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 43,741 hrs · 30,120 cycles

LAVATORY SMOKE MESSAGE ON OAP. PERFORMED OPERATION CHECKS IAW MM. OPERATION CHECKS GOOD.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 41,498 hrs · 28,807 cycles

RIGHT EXTERNAL OVERWING EMERGENCY ESCAPE LIGHT INOPERATIVE. FOUND OPEN WIRE L1598B18N. REPAIRED THE WIRE, OPS CHECKED GOOD.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 39,600 hrs · 27,667 cycles

L1 DOOR GIRT BAR WOULD NOT ENGAGE FORWARD END. ADJUSTED LATCH SHIMS. OPS CHECKS OK.

Part: KEELBEAM — CRACKED (BS 1003) · airframe 39,595 hrs · 27,663 cycles

CRACK ON FORMER FORWARD SIDE, BS 1003 X=-6 TO X=6, KEEL BEAM. REPLACED IAW SRM 51-10-03, 51-10-05, 51-30-02, 51-30-05 AND DWG 5930584, REV BY.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 39,628 hrs · 27,688 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 520AT LT WING. FOUND OUT OF LIMITS. REPLACED FUEL PANEL.

Part: KEELBEAM — CRACKED · airframe 39,595 hrs · 27,663 cycles

CRACK ON LT KEEL BEAM, NLG WHEEL WELL DOOR JAMB, BS 45 X=18. REPAIRED IAW SRM 53-90-01, FIG 6.

Part: ANGLE — CRACKED (BS 1007) · airframe 39,591 hrs · 27,661 cycles

CRACK ON LT & RT FORWARD ANGLES AT KEEL BEAM, BS 1007, X -6 AND X 6. REPLACED ANGLES IAW SRM 51-30-02 AND 51-30-05.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 39,591 hrs · 27,661 cycles

CORROSION ON PREVIOUS REPAIR LOWER BEAM AT AFT CARGO COMPARTMENT DOOR JAMB. REPAIRED IAW ERA 539880-14, REV O AND SRM 53-60-02, FIG 9.

Part: SKIN — DAMAGED (BS 693-712) · airframe 39,591 hrs · 27,661 cycles

LIGHTNING STRIKE ON LOWER FORWARD CORNER AND AFT EDGE WINDOW BETWEEN BETWEEN BS 693 AND 712, RT SIDE. REPAIRED IAW ETI-90-15-082, R1, REV AND ERA 539893-14, REV O.

Part: TAB — DAMAGED (LT ELEVATOR) · airframe 39,591 hrs · 27,661 cycles

EXPOSED MATERIAL COMPOUND ON LT ELEVATOR CONTROL TAB. REPAIRED IAW SRM 55-21-01, PAR 4B.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 39,628 hrs · 27,688 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 520EB LT WING. FOUND OUT OF LIMITS. REPLACED FUEL ACCES PANEL.

Part: INTERCOSTAL — CRACKED · airframe 39,591 hrs · 27,661 cycles

CRACKS ON INTERCOSTAL BETWEEN, BS 1542 AND 154 RT SIDE AT AFT ACC COMPARTMENT. R & R IAW DWG 9910087, REV 2 AND SRM 51-10-03, 51-30-02 AND 51-30-05.

Part: HOUSING — WORN (DOOR HANDLE) · airframe 39,591 hrs · 27,661 cycles

WEAR AT FORWARD CARGO DOOR HANDLE HOUSING. REPLACED IAW SRM 51-30-02 AND 51-30-05.

Part: INTERCOSTAL — CRACKED (BS 1555) · airframe 39,591 hrs · 27,661 cycles

CRACK ON CANT INTERCOSTAL, BS 1555 RT SIDE AFT ACC COMPARTMENT. REPLACED IAW DWG 9910087, REV AD AND SRM 51-30-02, 51-30-05 AND 51-10-03.

Part: INTERCOSTAL — CORRODED (BS 1364-1374) · airframe 39,591 hrs · 27,661 cycles

CORROSION ON INTERCOSTAL BETWEEN BS 1364 - 1374, LONGERON 26 TO 27. REPLACED IAW SRM 51-30-02, 51-10-03, PARA 14 -21 AND DWG 5936667, REV BZ.

Part: CUSP WEB — CRACKED (BS 864) · airframe 39,591 hrs · 27,661 cycles

CRACK UNDER CUSP WEB AT BS 864 BELOW SEAT TRACK RBL 54. REPAIRED IAW SRM 51-30-02 AND 51-10-03, PARA 14 ADN 21.

Part: FRAME — CORRODED (BS 1344) · airframe 39,591 hrs · 27,661 cycles

CORROSION ON FRAME ANGLE BS 1344 BETWEEN LONGERON 27 - 29R. REPAIRED IAW SRM 53-10-02.

Part: RIB SPLICE — CRACKED (RT WING) · airframe 39,591 hrs · 27,661 cycles

CRACKED SPLICE ON FIXED L/E, APPROXIMATELY XRS 164 LT WING. R & R THE RIBSPLICE, AND ANGLE IAW SRM 57-30-01, 51-10-03 AND 51-10-02.

Part: WIRE — BROKEN (L1 DOOR SLIDE) · airframe 39,591 hrs · 27,661 cycles

BROKEN WIRES ON LANYARD OF L1 DOOR. R & R LANYARD.

Part: SKIN — CORRODED (LT WING) · airframe 39,620 hrs · 27,682 cycles

CORROSION ON LT WING UPPER SKIN AT BS XRS 248, 295, 315, 353, AND 412. LOCATION XRS 315 IS OUT OF LIMITS. ROTO PEENING WAS APPLIED IAW SRM 57-30-01 AND 51-10-03.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 39,591 hrs · 27,661 cycles

CORROSION ON BARREL NUT HOLE NR 11 AT LT HORIZONTAL STABILIZER UPPER SURFACE, BS XH=7. REPAIRED IAW ETI-90-15-084, REV 1 AND ERA 539891-14, REV O.

Part: CUSP WEB — CORRODED (BS 218-237) · airframe 39,591 hrs · 27,661 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 218-237, X=-54 AND X=-60. R & R CUSP WEB AND RING DOUBLER IAW SRM 51-30-02, 53-20-02, FIG 18.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 39,628 hrs · 27,688 cycles

CORROSION ON SETTLEMENT AREA OF FUEL ACCESS PLATE NR 520 CT AND 620CT LT WING. FOUND OUT OF LIMITS. REPLACED PANEL.

Part: FRAME — CRACKED (BS 180) · airframe 39,591 hrs · 27,661 cycles

CRACKED FRAME IN BS 180 BETWEEN LONGERON 5L-4L. REMOVED, FABRICATED AND INSTALLED NEW FRAME IAW SRM 51-30-02, 51-30-05 AND 51-10-03, PARA 14 AND 21.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 39,591 hrs · 27,661 cycles

CORROSION ON FLOOR SUPPORT BS 160-200 BETWEEN X=54 AND 44 AND BS 148-200, X=7 TO-7. REPLACED IAW SRM 53-10-01, 51-10-03, 51-10-05, 51-30-05 AND 51-30-02.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 39,591 hrs · 27,661 cycles

CORROSION ON FLOOR SUPPORT AT BS 200 BETWEEN -7 TO 7. REPLACED FLOORBEAM IAW SRM 53-10-01 AND 51-10-03, 51-30-05 AND 51-30-02.

Part: FITTING — CORRODED (LT PYLON) · airframe 39,591 hrs · 27,661 cycles

CORROSION ON FORWARD/AFT FITTING BUSHING ON AFT CONEBOLT AT LEFT PYLON. NEW BUSHING INSTALLED IAW DWG 5965645, REV B.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 39,628 hrs · 27,688 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 520FT RT WING. FOUND OUT OF LIMITS. REPLACED FUEL ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 39,628 hrs · 27,688 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 620FT. FOUND OUT OF LIMITS. REPLACED FUEL ACCESS PANEL.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 39,628 hrs · 27,688 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREAS OF FUEL ACCESS PLANTE 620CB RT WING. FOUND OUT OF LIMITS. REPLACED FUEL ACCESS PANEL.

Part: DOUBLER — CORRODED (BS 1395 BULKHEAD) · airframe 39,591 hrs · 27,661 cycles

CORRODED PRODUCTION DOUBLER ON AFT PRESSURE BULKHEAD, BS 1395, LONGERON 29L-29R, AFT CARGO COMPARTMENT. REPLACED IAW DWG 5910130, REV ET AND SRM 51-30-02.

Part: SKIN — BENT (L1 DOOR) · airframe 39,591 hrs · 27,661 cycles

L1 DOOR EXTERNAL LOWER SKIN BENT. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER AND HINGE IAW SRM 51-10-03, PAR 14 AND 21, 52-10-01, FIG 4, 51-30-01 AND 51-30-02.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 39,628 hrs · 27,688 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 520CB LT WING. FOUND OUT OF LIMITS. REPLACED ACCESS PANEL.

Part: SKIN — CORRODED (BS 952-960) · airframe 42,268 hrs · 29,301 cycles

CORROSION ON SKIN , BS 952 - 960 BETWEEN X -48 AND X -54. REPAIRED IAW ERA 539882-14, REV O.

Part: DOOR FRAME — CRACKED (R1 DOORWAY) · airframe 39,591 hrs · 27,661 cycles

CRACK ON DRILL HOLE HITTING AT R1 FORWARD LOWER DOOR JAMB. REPAIRED IAW ERA 539892-14, REV O AND ETI-90-15-085.

Part: STIFFENER — CRACKED (PRESS BULKHEAD) · airframe 39,591 hrs · 27,661 cycles

CRACK ON STIFFENER AT P DOME, BS 1395. R & R STIFFENER IAW SRM 51-30-05 AND 51-30-02.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 39,591 hrs · 27,661 cycles

CRACK ON FORWARD CARGO COMPARTMENT DOOR AFT EDGE STOPS NR 6 AND NR 8. REPLACED STOPPED FITTING NR 3 IAW SRM 51-30-01 AND 51-30-05.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 39,628 hrs · 27,688 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620DT RT WING. FOUND OUT OF LIMITS. REPLACED ACCESS PLATE.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 39,628 hrs · 27,688 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 520DT AT LT WING. FOUND OUT OF LIMITS. REPLACED PANEL ON AMDS 5730-0433.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 39,628 hrs · 27,688 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 620 RT WING. FOUND OUT OF LIMITS. REPLACED ACCESS PLATE.

Part: BEAM — CRACKED (L1 DOOR) · airframe 39,591 hrs · 27,661 cycles

L1 DOOR BEAM CRACKED FORWARD/AFT ENDS. REPAIRED IAW SRM 51-30-02, 51-30-01, 52-10-02, FIG 5 AND 51-30-02.

Part: WEB — CORRODED (BS 617-636) · airframe 39,591 hrs · 27,661 cycles

CORROSION FOUND ON WEB, X-54 TO X-60 BETWEEN BS 617 - 636. REMOVED, FABRICATED AND REPLACED WEB IAW SRM 51-10-03.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 39,591 hrs · 27,661 cycles

CRACK ON MID CARGO COMPARTMENT DOOR STOP, NR 2 AT AFT EDGE. REPLACED IAW SRM 51-30-01 AND 51-30-05.

Part: LONGERON — DAMAGED (BS 1475) · airframe 38,898 hrs · 27,250 cycles

LONGERON L2L AND L2R, SPLICE REPAIR, BS 1475, REPAIRED IAW ERA 537329-14MA.

Part: COVER — WRONG PART (TAILCONE SLIDE) · airframe 37,676 hrs · 26,471 cycles

WRONG TAIL CONE SLIDE COVER INSTALLED. FABRICATED BRACKETS IAW DWG 5966532. INSTALLED IAW DWG 5966532.

Part: SLIDE — LOW PRESSURE (PAX DOOR) · airframe 37,676 hrs · 26,471 cycles

FORWARD MAIN DOOR ESCAPE SLIDE PRESSURE NOT IN GREEN BAND. R & R SLIDE IAW AMDS WC 2561-4641.

Part: SKIN — CRACKED (BS 1494) · airframe 37,670 hrs · 26,468 cycles

CROWN SKIN HAS A ONE INCH LONG CRACK FORWARD OF RIVET LINE AT APPROXIMATELY BS 1494, EIGHT INCHES LEFT OF VERTICAL FIN. REPAIRED IAW PRI 531704-14.

Part: SKIN — CRACKED (BS 1494) · airframe 37,670 hrs · 26,468 cycles

CROWN SKIN HAS A .6250 INCH LONG CRACK AT APPROXIMATELY BS 1494, EIGHT INCHES RIGHT OF VERTICAL FIN. REPAIRED IAW PRI 531706-14.

Part: PIN — DISENGAGED (DOOR SLIDE) · airframe 37,181 hrs · 26,146 cycles

FOUND BOTH PARACHUTE PINS DISENGAGED ON FORWARD ENTRY DOOR SLIDE. R & R FORWARD ENTRY DOOR ESCAPE SLIDE IAW AMDS 2561-4641.

Part: WEB — DAMAGED (FUSELAGE) · airframe 34,658 hrs · 24,603 cycles

FOUND DAMAGE ON WEB BY MID JACKSCREW AREA 1 X 1 1/2 HOLE. INSTALLED REPAIR IAW PRI ERA 520433-14 .

Part: SKIN — CRACKED (BS 1542 L22R) · airframe 33,252 hrs · 23,795 cycles

BS 1542 L22R FUSELAGE SKIN CRACKED, TAIL SECTION. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER IAW 53-00-01 FIG 6. INSTALLED, SEALED AND PAINTED.

Part: WINDOW FRAME — CRACKED · airframe 32,732 hrs · 23,499 cycles

PILOT WINDOW FRAME CRACKED. VERIFIED CRACK WITH HFEC. REMOVED INTERNAL DOUBLER. DRILLED, PRIMED, PAINTED AND INSTALLED DOUBLER.

Part: SLIDE — WRONG PART · airframe 32,732 hrs · 23,499 cycles

EVACUATION SLIDE ON L1 DOOR IMPROPER PART INSTALLED. DOES NOT MATCH EFFECTIVITY. R & R SLIDE IAW AMDS CARD 2500-4332.

Part: SLIDE — WRONG PART · airframe 32,732 hrs · 23,499 cycles

EVACUATION SLIDE INSTALLED ON R1 SERVICE DOOR DOES NOT MATCH EFFECTIVITY. IMPROPER PART INSTALLED. R & R IAW AMDS CARD 2500-4322.

Part: SLIDE — WRONG PART · airframe 32,732 hrs · 23,499 cycles

EVACUATION SLIDE ON 2L DOOR IMPROPER PART INSTALLED. DOES NOT MATCH EFFECTIVITY. R & R IAW CARD 2500-4332.

Part: CABLE — FRAYED (TAIL CONE) · airframe 32,484 hrs · 23,365 cycles

DURING FUNCTIONAL CHECK, FOUND TAILCONE NITROGEN BOTTLE ACTUATOR CABLE FRAYED. R & R IAW MM. REQUIRED INSPECTION COMPLETED.

Part: SKIN — DAMAGED (BS 655-674) · airframe 32,786 hrs · 23,527 cycles

WINDOW BELT LT SIDE HAS LIGHTNING STRIKES BS 655-674. ACCOMPLISHED ERA 501771-14, REV O, SECT III. NO CRACKS FOUND.

Part: SKIN — DAMAGED (BS 598-617) · airframe 32,786 hrs · 23,527 cycles

WINDOW BELT LT SIDE HAS LIGHTNING STRIKES, BS 598-617. ACCOMPLISHED ERA 501771-14, REV O. NO CRACKS FOUND.

Part: SKIN — DAMAGED (BS 560-579) · airframe 32,786 hrs · 23,527 cycles

WINDOW BELT, LIGHTNING STRIKES BS 560-579. ACCOMPLISHED ERA 501771-14, REV O, SECT III. NO CRACKS FOUND.

Part: SKIN — DAMAGED (BS 636-655) · airframe 32,793 hrs · 23,533 cycles

WINDOW BELT LT SIDE LIGHTNING STRIKES BS 636-655. ACCOMPLISHED ERA 501771-14 REV O, SECT III. NO CRACKS FOUND.

Part: SKIN — DAMAGED (BS 579-598) · airframe 32,786 hrs · 23,527 cycles

WINDOW BELT LT SIDE HAS LIGHTNING STRIKES BS 579-598. ACCOMPLISH ERA 501771-14 REV O, SECT III. NO CRACKS FOUND.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 31,819 hrs · 23,031 cycles

DURING SERVICE CHECK, MX FOUND EMERGENCY LIGHTS INOPERATIVE AFT TAIL CONE COMPARTMENT. FOUND SPLICE IN TAIL COMPARTMENT DISCONNECTED. RECONNECTED. OPERATION CHECKS GOOD. (LP 425862004)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,349 hrs · 22,234 cycles

WHILE IN MSP, A/C 9229 SUSTAINED LIGHTNING STRIKE DAMAGE AT STA 150 LONGERON 1. THE DAMAGE WAS BLENDED AND FOUND TO BE OUT OF SRM LIMITS. REPAIRED PER ER/A 501808-14.

Part: SKIN — DAMAGED (BS 560-6764) · airframe 32,786 hrs · 23,527 cycles

WINDOW BELT LIGHTNING STRIKES FS 560-6764.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,759 hrs · 21,951 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND LEFT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE RELAMPED SAME. OPERATIONAL CHECKS GOOD. AIRCRAFT IS OKAY FOR SERVICE.

Part: COOLING FAN — INOPERATIVE (AC BAY) · airframe 29,673 hrs · 21,915 cycles

SHIP 9229 FLIGHT CREW REPORTED VISIBLE SMOKE IN THE FORWARD CABIN AREA AND A LIGHT HAZE IN THE AFT CABIN UPON TAXI IN LAS. SMOKE AND ODOR HAD DISSIPATED BY THE TIME AIRCRAFT ARRIVED AT THE GATE. MAINTENANCE REMOVED AND REPLACED LEFT RADIO RACK COOLING FAN AND RIGHT AIR CONDITIONING RECIRCULATION FAN PER AMM. PERFORMED DUCT BURNOUT, LEAK AND OPERATION CHECKS GOOD.

Part: STIFFENER — CRACKED (NLG WW) · airframe 29,423 hrs · 21,792 cycles

FOUND DURING CONFORMITY CHECK, FAA FIND. AT STATION 44, IN THE NOSE WHEEL WELL, FORWARD OF LEFT NOSE GEAR DOOR, STIFFENER CRACKED ON BULKHEAD. MAINTENANCE REMOVED STIFFENER FABRICATED AND DRILLED STIFFENER PER MD90 DRAWING 9911500. TREATED AND PAINTED STIFFENER PER PS 900-2-4-1 NUMBER 2. INSTALLED STIFFENER PER MD90 SRM 51-00-0.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,407 hrs · 21,783 cycles

DUE AT BRIDGE CHECK - SRM 51-50-01 VOLUME II. INSPECT DENT ON FUSELAGE BETWEEN STA 1520.225 TO 1531.604. DURING PSV O VISIT, PERMANENT REPAIR INSTALLED PER MD90 SRM 53-30-01, FIGURE 1. ID PERMANENT REPAIR PER PS 900-5-1 NR 4.

Part: SUPPORT FITTING — CRACKED (RT MLG) · airframe 29,407 hrs · 21,783 cycles

DURING PSV/MOD FOUND RT MLG DOOR ACTUATOR SUPPORT FITTING ATTACH BRACKET IS CRACKED. LOCATION KEEL BEAM ABOVE ACTUATOR ATTACH POINT. REMOVED AND REPLACED RT MLG DOOR ACTUATOR SUPPORT FITTING BRACKET AS PER MD90 SRM 51-30-05.

Part: SUPPORT FITTING — CRACKED (LT MLG WW) · airframe 29,407 hrs · 21,783 cycles

DURING PSV FOUND LT MLG DOOR ACT SUPPORT FITTING ATTACH BRACKET CRACKED LOCATED ABOVE ACT ATTACH POINT. REMOVED AND REPLACED LT BRACKET SUPPORT P/N 3936361-1 REF 51-30-05.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 29,407 hrs · 21,783 cycles

DURING MAJOR REPAIR INSPECTION EA 02-49943-12 STRUCTURES/GENERAL/MAJOR-MINOR REPAIR DOCUMENT FOUND REPAIR ERN52 LT MLG INBD LOWER FRAME NON COMPLIANT TO SRM. REMOVED AND REPLACED CHANNEL P/N 5930584U121 IN REF WITH MD90 SRM 51-30-05 & 51-30-02.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,407 hrs · 21,783 cycles

PSV ZERO FUSELAGE SKIN DENT BETWEEN CANT STA 1520.225 AND 1531.604 LT LOWER SIDE. REPAIR PER MD90 SRM 53-30-01 FIG 1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,407 hrs · 21,783 cycles

PSV ZERO STA 258 LONG 5L INTERCOSTAL CRACKED. REPAIR PER MD90 SRM 53-40-01 FIG 1 VOL 2.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,407 hrs · 21,783 cycles

AFT FUSELAGE LT SIDE LOWER EXTERNAL SKIN CLOSE TOVENTRAL STAIR DOOR CUTOUT: BETWEEN CANTED FRAME 1520.225 TO CANTED FRAME 1531.604 HAS A DENT. INSTALLED DOUBLER REPAIR AT AFT FUSELAGE LT SIDE LOWER EXTERNAL SKIN PER SRM 53-30-1 FIG 1. IDENTIFIED REPAIR PER DELTA PS 900-5-1 NR 04.

Part: SUPPORT FITTING — NOT REPORTED (PYLON) · airframe 29,415 hrs · 21,787 cycles

PYLON AFT SUPPORT FITTING UPPER FASTENERS REPAIRED IAW AA 5440-01069.

Part: SPAR — CRACKED (WING) · airframe 29,415 hrs · 21,787 cycles

WING REAR SPAR CRACKING REPAIRED IAW AA 5710-01119.

Part: SUPPORT FITTING — NOT REPORTED (MLG ACTUATOR) · airframe 29,415 hrs · 21,787 cycles

REPLACED MLG RETRACT ACTUATOR SUPPORT FITTINGS IAW EA 02-093855-03.

Part: MOTOR — NOT REPORTED (HYD PUMP) · airframe 29,415 hrs · 21,787 cycles

HYD PUMP MOTOR REPAIRED IAW AA 2920-01077.

Part: JACKSCREW — NOT REPORTED (HORIZONTAL STAB) · airframe 29,415 hrs · 21,787 cycles

HORIZONTAL STABILIZER JACKSCREW ASSY REPAIRED IAW AA 2740-01071.

Part: STOP FITTING — NOT REPORTED (CARGO DOOR) · airframe 29,415 hrs · 21,787 cycles

CARGO DOOR STOP PAD FITTINGS REPAIRED IAW AA 5230-01136.

Part: SUPPORT FITTING — NOT REPORTED (MLG) · airframe 29,415 hrs · 21,787 cycles

MLG ACTUATOR SUPPORT FITTING. REPAIRED IAW AA 5740-01140.

Part: FRAME — NOT REPORTED (BS 883 - 962) · airframe 29,415 hrs · 21,787 cycles

BS 883- 962 OVERWING FRAMES REPAIRED IAW AA 5310-01375.

Part: SPAR CAP — NOT REPORTED (VERTICAL STAB) · airframe 29,415 hrs · 21,787 cycles

VERTICAL STABILIZER, L/E FRONT SPAR CAP REPAIRED IAW AA 5530-01044.

Part: HEATER — NOT REPORTED (STATIC PORT) · airframe 29,415 hrs · 21,787 cycles

STATIC PORT HEATING REPAIRED IAW AA 3032-01002.

Part: LUG — NOT REPORTED (HORIZONTAL STAB) · airframe 29,415 hrs · 21,787 cycles

HORIZONTAL STABILIZER HINGE RIB PIVOT BEARING LUG REPAIRED IAW AA5510-01083.

Part: SKIN — NOT REPORTED (HORIZONTAL STAB) · airframe 29,415 hrs · 21,787 cycles

HORIZONTAL STABILIZER UPPER CENTER SKIN PANEL REPAIRED IAW AA 5510-01085.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 29,415 hrs · 21,787 cycles

STA 1542 CANT, RT FUSELAGE TO VERTICAL STABILIZER DORSAL FIN REPAIRED IAW BAC TWX BNI-BNI-10-168-01C, DWG SR09530296 AND SERVICE BULLETIN MD90-53-027 R2__(TO 82).

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 29,415 hrs · 21,787 cycles

AFT CARGO DOOR JAMB REPAIRED IAW SRM 53-60-02 VOL I FIG 9.

Part: ANGLE — CRACKED (NACELLE) · airframe 29,415 hrs · 21,787 cycles

STA 1542 NESTED ANGLES REPAIRED IAW SRM 54-00-01 VOL I FIG 2 SHEET 2 AND THE ORIGINAL REPAIR BAC APPROVED BY A 8100-9 BAC TWX 1-201845718-2 AND BLUE 1 AIRLINES EOM 90-53-004.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,415 hrs · 21,787 cycles

STA 229-275 L10-16LT SKIN REPAIRED IAW BAC TWX BNI-BNI-10-0071-10B 8100-9 RECEIVED 09/28/2011 (TO 89).

Part: STRUCTURE — CRACKED (DORSAL FIN) · airframe 29,415 hrs · 21,787 cycles

STA 1475 L3LT-L3RT DORSAL FIN REPAIRED IAW BNI-BNI-10-0069-09B 8100-9 RECEIVED 09/23/2011___(TO 85.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 29,415 hrs · 21,787 cycles

STA 1344-1364 LT CUSP MEMBRANE REPAIRED IAW DWG SG09530019 SRM 53-20-02 VOL I PARA 6__(TO 86).

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,415 hrs · 21,787 cycles

STA 1379 L27-29RT AFT CARGO COMPARTMENT FRAME REPAIRED IAW SRM 53-10-02 VOL I FIGURE 2_(TO 80).

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 29,415 hrs · 21,787 cycles

STA 1542 CANT, DORSAL FIN ATTACH ANGLE REPAIRED IAW BAC TWX BNI-BNI-10-168-01C DWG SR09530296 S/B MD90-53-027 R2(TO 57).

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 29,415 hrs · 21,787 cycles

STA 1344-1364 RT CUSP MEMBRANE REPAIRED IAW PMT-PMT-10-0001-02B DWG SG09530019 SRM 53-20-02 VOL I, PARA 6__(TO 84).

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 29,415 hrs · 21,787 cycles

LT MLG FORWARD LOWER DOOR JAMB CHANNEL REPAIR IAW SRM 53-60-02 VOL I PARA 8 FIG 6 AREA REWORKED AND NEW REPAIR COMPLETED SRM 53-60-02.

Part: SKIN — CHAFED (FUSELAGE) · airframe 29,415 hrs · 21,787 cycles

STA 1458 L7LT REPAIR IAW SRM 53-10-02 VOL I FIG 4 AND BLUE 1 AIRLINES EOM90-53-002. (TO 16A).

Part: SKIN — CORRODED (FUSELAGE) · airframe 29,415 hrs · 21,787 cycles

STA 1364 L29-29RT REPAIRED IAW SRM 53-10-02 VOL I FIG 2.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 29,415 hrs · 21,787 cycles

STA 685-796 CUSP REPAIR IAW DWG SG09530019 SRM 53-20-02 VOL I PARA 6__(TO 87).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,415 hrs · 21,787 cycles

STA 200-237 MID SEAT TRACK GALLEY ATTACH POINTS SPLICE REPAIR IAW SRM 53-40-01 VOL I FIG 6_(TO 58).

Part: SKIN — CORRODED (FUSELAGE) · airframe 29,415 hrs · 21,787 cycles

STA 769-788 L28-29 RT SKIN REPAIR IAW SRM 53-30-01 VOL I FIG 9 PARA 11_(TO 79).