N918DH

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,374 hrs · 19,204 cycles

SEVERAL CABIN EMERGENCY LIGHT FAIL TEST. R&R EMERGENCY LIGHT BATTERY PACKS B5-235 AND B--236 IAW MDPO AMM 33-51, OPS CK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,429 hrs · 18,659 cycles

EMERGENCY EXIT LIGHT AT SEAT 30 ABC INOPERATIVE. REPLACED THE POWER SUPPLY. OPS CHECKED GOOD IAW AMM 33-51.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,341 hrs · 17,995 cycles

EMERGENCY POWER SUPPLY INOPERATIVE AT THE AFT EMERGENCY EXIT DOOR. REMOVED AND REPLACED THE POWER SUPPLY .

Part: SLIDE — LOOSE (TAILCONE) · airframe 35,449 hrs · 16,893 cycles

TAIL CONE COMPARTMENT SLIDE LOOSE. REPLACED THE SLIDE.

Part: PROBE — DAMAGED (PITOT/STATIC SYS) · airframe 35,306 hrs · 16,799 cycles

LIGHTNING STRIKE ON CLIMB OUT FROM ATL. INSPECTED. FOUND DAMAGE TO AUXILIARY PITOT PROBE, LEFT WING NAV LIGHT AND RIVETS ON CROWN OF FUSELAGE. NON- ROUTINES WRITTEN FOR DAMAGE.

Part: HOUSING — DAMAGED (EMERGENCY LIGHT) · airframe 34,780 hrs · 16,505 cycles

R1 EMERGENCY EXIT LIGHT LENS MISSING AND COVER MOUNT DAMAGED. REPLACED LIGHT BASE AND COVER IAW MM. OPERATION CHECKS GOOD. (LP# 9167692)

Part: RECEPTACLE — DAMAGED (CABIN) · airframe 33,749 hrs · 15,874 cycles

EMERGENCY LIGHT BATTERY PACK B5-234 RECEPTACLE DAMAGED. R & R SAME. OPERATION CHECKS GOOD.

Part: LOCK PIN — WORN (TAILCONE) · airframe 32,780 hrs · 15,291 cycles

TAILCONE RELEASE LOCK PIN AND RECEPTICAL WORN, LEFT UPPER. REPLACED THE LT UPPER TAILCONE LOCKPINE AND RECEPTICAL IAW MM. OPS CHECK OK.

Part: SLIDE — NO TEST (TAILCONE) · airframe 31,351 hrs · 14,436 cycles

TAIL CONE DROPPED AS REQUIRED, SLIDE DID NOT DEPLOY, FOUND EVIDENCE OF SLIDE EXPANSION INSIDE OF CONTAINER. REPLACED SLIDE.

Part: FUEL TANK — CORRODED · airframe 30,441 hrs · 13,882 cycles

CORROSION ON CENTER TANK UPPER SKIN LT SIDE STR 5 BETWEEN BS XCW42.00 AND 58.688. REPAIRED IAW ERA, REV O.

Part: FUEL TANK — CORRODED · airframe 30,441 hrs · 13,882 cycles

CORROSION ON CENTER FUEL TANK UPPER SKIN RT SIDE ON STR 9, BETWEEN XCW 58.688 AND XCW 42.00. COMPLIED WITH ERA 533302-14AD, REV O.

Part: FUEL TANK — CORRODED · airframe 30,441 hrs · 13,882 cycles

CORROSION ON CENTER FUEL TANK UPPER SKIN RT SIDE ON STRINGER 5, BETWEEN XCW 58.688 AND SCW 42.000. REPAIRED IAW ERA 533304-14, REV O.

Part: FUEL TANK — CORRODED · airframe 30,441 hrs · 13,882 cycles

CORROSION ON CENTER FUEL TANK UPPER SKIN RT SIDE ON STR 3, BETWEEN SCW 58.688 AND XCW 42.000. REPAIRED ERA 53305-14AD, REV O.

Part: FUEL TANK — CORRODED · airframe 30,441 hrs · 13,882 cycles

CORROSION ON CENTER FUEL TANK UPPER SKIN RT SIDE ON FRONT SPAR BETWEEN XCW 58.688 AND XCW 42.000. CORROSION COMPLIED WITH ERA 533301-14 AD, REV O.

Part: INTERCOSTAL — CRACKED (BS 1344-1364) · airframe 30,403 hrs · 13,860 cycles

SEVERAL CRACKS ON INTERCOSTAL BETWEEN FLOOR BEAMS STA 1344 TO 1364. REPLACED INTERCOSTAL IAW ERA 533320-14, REV O.

Part: FRAME — CRACKED (BS 1231) · airframe 30,403 hrs · 13,860 cycles

CRACK ON FRAME STA 1231, LONGERON 6L. R & R FRAME IAW ERA 495237-14, REV B.

Part: CARGO TRACK — CORRODED (BS 1091-1277) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON LT TIE TRACK BETWEEN, STA 1091 AND 1277. REPLACED TIE TRACK IAW SRM 51-30-01, 51-30-02, AND 51-10-05.

Part: DOUBLER — CRACKED (VERTICAL STAB) · airframe 30,403 hrs · 13,860 cycles

CRACKED INTERNAL DOUBLER ON VERTICAL STABILIZER ACCESS PLATE 370 BL CUTOUT. REPAIRED CRACK IAW SRM 5330-05, FIG 3.

Part: INTERCOSTAL — CRACKED (BS 994-997) · airframe 30,403 hrs · 13,860 cycles

CRACKED INTERCOSTAL BETWEEN RT X=-4 TO X=-6, STA 994 TO 997 AT KEEL BEAM AREA. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-30-05, DWG 9936368, REV AW.

Part: BEAM — CRACKED (BS 163-197) · airframe 30,403 hrs · 13,860 cycles

CRACK ON BEAM, NR 1 AT STA 163 AND STA 197 ON FORWARD PASSENGER DOOR STRUCTURE. R & R BEAM IAW SRM 51-30-00, 51-10-03, 51-10-04 AND ERA 533300-14, REV O.

Part: STRUCTURE — BENT (PAX DOOR) · airframe 30,403 hrs · 13,860 cycles

BENT ON PREVIOUSLY REPAIRED DOUBLER ON FORWARD PASSENGER ENTRANCE DOOR ON FORWARD LOWER CORNER. R & R DOUBLER IAW SRM 52-10-01, 51-30-00 AND 51-10-03.

Part: INTERCOSTAL — CRACKED (BS 1344-1364) · airframe 30,403 hrs · 13,860 cycles

CRACKS ON INTERCOSTAL BETWEEN FLOORBEAMS, STA 1344 TO 1364, X=0. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-30-02 AND SRM 51-30-05.

Part: SKIN — CORRODED (ELEVATOR) · airframe 34,688 hrs · 16,440 cycles

CORROSION ON UPPER AND LOWER ELEVATOR. REPLACED ELEVATOR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,403 hrs · 13,860 cycles

CRACK ON RT WHEEL WELL FORWARD FRAME, 6" OF INBD BELOW HD SERVICE PANEL. R & R CHANNEL IAW SRM 51-30-02 AND 51-30-05.

Part: SEAT TRACK — CORRODED (BS 207-243) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON SEAT TRACK FROM STA 207 - 243, X=-43, X=-44 AND X=-45. TASK 53-211-01. R & R SEAT TRACK IAW SRM 53-40-01 AND ERA 533308-14MA, REV O.

Part: SEAT TRACK — CORRODED (BS 200-220) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON SEAT TRACK, X=22, BS 200-220. TASK 53-211-01. R & R SEAT TRACK, STA 200 TO STA 230 IAW SRM 53-40-01, RIG 6 AND ERA 533308-14MA, REV O.

Part: SEAT TRACK — CORRODED (BS 207-237) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON SEAT TRACK, STA 207 TO 237, X=- 21, X=-22, X=-23. TASK 53-211-01. R & R SEAT TRACK, STA 200 - 260 IAW SRM 51-30-01, 51-30-02 AND 51-30-05 AND ERA 533308-14MA, REV O.

Part: BAR — CORRODED (TE FLAPS) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON LT FLAP FLEX JOINTS LOWER BAR AND LINK. TASK 57-051-03. REPLACED IAW AMM 27-51-07-420.

Part: SKIN — CORRODED (WING) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON SETTLEMENT ARE OF FUEL ACCESS DOOR CUTOUTS. COMPLIED WITH WORK ON NRC 61, ZONE 500.

Part: BAR — CORRODED (RT WING TE FLAP) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON LOWER BAR AT RT FLAP FLEX JOINT. TASK 27-05-03. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. NEW BAR INSTALLED.

Part: SKIN — CORRODED · airframe 30,403 hrs · 13,860 cycles

PREVIOUS BLEND OUT ON RT WING UPPER SKIN, STA 988 - 953, X=61, 67 AND 70. REMOVED CORROSION. FLAP PENNING IAW 95900-4. AREA TREATED AND PAINTED. FASTENER INSTALLED IAW SRM 51-30-03.

Part: CARGO TRACK — CORRODED (BS 1155-1212) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON RIGHT TIE TRACK BETWEEN, STA 1155-1212 AT C3. TASK 20-010-12. R & R TIE TRACK IAW SRM 51-30-02, 51-30-01, 51-10-05, AND 51-10-03. LP 1853329.

Part: ANGLE — CORRODED (BS 1210-1212) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON ANGLES BETWEEN RT LONGERON 28 AND 27, STA 1212-1210 AND 1268-1271, DOOR JAMB. TASK 53-123-02. ANGLES REPLACE IAW SRM 51-30-02. LP 1853601.

Part: SKIN — DENTED (BS 617-636) · airframe 30,403 hrs · 13,860 cycles

DENT ON FUSELAGE SKIN BETWEEN STA 617-636, LONGERON 24R-25R. EVALUATED AND FOUND DENT CONDITION 1B.

Part: CHANNEL — CRACKED (UNKNOWN) · airframe 30,403 hrs · 13,860 cycles

RT CHANNELS CRACKED. REPAIRED IAW SRM 53-20-03.

Part: SKIN — CORRODED (LT ELEVATOR) · airframe 34,677 hrs · 16,435 cycles

CORROSION ON LEFT HAND ELEVATOR UPPER AND LOWER SKIN TASK 53-300-03. REPLACED ELEVATOR ON CARD 2730-4139LH.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON BARREL NUT NR 21, XH=27 AT LT HORIZONTAL STABILIZER. FABRICATED AND INSTALLED BUSHING IAW SRM 55-10-03 AND DWG 5922576, REV 2.

Part: CHANNEL — WORN (RT MLG DOOR) · airframe 30,403 hrs · 13,860 cycles

WORN SPLICE ON AFT CHANNEL AT RT INBD MLG DOOR. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR ANGLE IAW EA 469617-14, REV AFC.

Part: BULKHEAD WEB — CRACKED · airframe 30,403 hrs · 13,860 cycles

CRACKED WEB, AFT BULKHEAD DOOR AT LT EDGE FORWARD MID SECTION. REPAIRED IAW SRM 52-00-01.

Part: CUSP WEB — CORRODED (BS 769-788) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON LT CUSP MEMBRANE, STA 769-788, X=55/60, TASK 53-211-01. DAMAGE REMOVED. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-02, FIG 12, 51-10-03 AND 51-30-01.

Part: CUSP WEB — CORRODED (BS 512) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON LT CUSP MEMBRANE UPPER AND LOWER SURFACE, BS 512 AND X=59, TASK 53-211-01. REMOVED CORROSION. FABRICATED AND INSTALLED NEW REPAIR PARTS IAW SRM 53-20-02, FIG 18.

Part: CUSP WEB — CORRODED (BS 512) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON LT CUSP WEB MEMBRANE UPPER AND LOWER SURFACE, BS 512, X=59, TASK 53-211-01. REPAIRED IAW SRM 53-20-02, FIG 11.

Part: SEAT TRACK — CORRODED (BS 424-427) · airframe 30,403 hrs · 13,860 cycles

CORROSION OUT OF LIMITS ON RT SEAT TRACK, X=-22, BS 424 TO 427, TASK 53-211-02. REMOVED DAMAGE. REPAIR PARTS INSTALLED IAW SRM 53-40-01, FIG 2.

Part: WEB — CRACKED (BS 1542) · airframe 30,403 hrs · 13,860 cycles

CRACKED WEB, STA 1542, LONGERON 5R. REMOVED WEB. FABRICATED AND INSTALLED DOUBLER IAW SRM 51-10-03, PARA 14 AND 21, AND 53-00-01.

Part: CHANNEL — CRACKED (RT MLG DOO) · airframe 30,403 hrs · 13,860 cycles

CRACKED LOWER CHANNEL, RT INBD MLG DOOR, AFT SECTION. REPAIRED IAW SRM 52-80-02, FIG 2.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,677 hrs · 16,435 cycles

CORROSION ON LEFT HAND CUSP WEB AND CRACK ON WEB AND REPAIR DOUBLER. REMOVED CORROSION AND REPAIRED IAW SRM 53-20-02.

Part: PAN — CRACKED (CARGO BAY) · airframe 30,403 hrs · 13,860 cycles

CRACKED ON OTBD PAN FORWARD SIDE BETWEEN BEAM NR 1 AND NR 2 AFT CARGO COMPARTMENT. REPAIRED IAW SRM 52-30-02, FIG 3.

Part: DOOR FRAME — CORRODED (BS 696-747) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON LOWER DOOR JAMB REPAIR SPACER BETWEEN RT LONGERON 29 AND 28, STA 696 TO 747, TASK 53-122-02. REMOVED, FABRICATED AND INSTALLED SPACER IAW SRM 51-30-05, 53-60-02, FIG 9 AND 51-10-03, PARA 14 AND 21.

Part: CUSP WEB — CORRODED (BS 915-918) · airframe 30,403 hrs · 13,860 cycles

RIGHT CUSP WEB CORRODED, STA 915-918, S=-54 TO X=-60, TASK 53-211-02. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-02, FIG 18.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON BARREL NUT 12 AND 22, STA XH=27.7 AT RT HORIZONTAL STABILIZER. REMOVED CORROSION. NR 22 FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR BUSHING AND REWORKED IAW ETI-90-15-004, REV O AND ERA 532546-14, REV O.

Part: CUSP WEB — CORRODED (BS 389-408) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON CUSP WEB, STA 389 TO 408, BETWEEN X=-54 AND X=-60, TASK 53-211-02. REPAIRED IAW SRM 53-20-02, FIG 29.

Part: CUSP WEB — CORRODED (BS 370-380) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON CUSP WEB, STA 370 TO 380, BETWEEN X=-54 TO X=-60, TASK 53-211-02. REPAIRED IAW SRM 53-20-02, FIG 29.

Part: CUSP WEB — CORRODED (BS 676-682) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON CUSP WEB LOWER SIDE OF STA 676 TO 682, X=-56 TO X=-59, TASK 53-100-18. REMOVED DAMAGE. FABRICATED AND INSTALLED NEW CUSP WEB AND RINGS IAW SRM 51-10-03 AND 53-20-02, FIG 20.

Part: CUSP WEB — CORRODED (BS 655-674) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON CUSP WEB, STA 655 TO 674, BETWEEN X=-54 TO X=-60, TASK 53-211-02. R & R CUSP WEB IAW SRM 53-10-02, FIG 5.

Part: BEAM — CORRODED (BS 186) · airframe 30,403 hrs · 13,860 cycles

CRACKED ANGLE ON BEAM 1, STA 186. R1 DOOR STRUCTURE. REMOVED DAMAGED ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW DWG 2913008, REV O AND SRM 51-30-05.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 30,403 hrs · 13,860 cycles

CORRROSION ON BARRELL NUT NR 21, STA XH=27.7 AT LT HORIZONTAL STABILIZER. REMOVED CORROSION, WITHIN LIMITS. HFEC, WITH NO FINDINGS. DRILLED IAW DWG 5922576, REV 2.

Part: SEAT TRACK — CORRODED (BS 200-220) · airframe 30,403 hrs · 13,860 cycles

SEVERAL CORROSION POINTS ON SEAT TRACK, STA 200 TO 220, TASK 53-211-01. R & R SEAT TRACK IAW SRM 53-40-01, FIG 6.

Part: CHANNEL — WORN (RT MLG DOOR) · airframe 30,403 hrs · 13,860 cycles

WORN PREVIOUS DOUBLER REPAIR ON AFT CHANNEL AT RT INBD MLG DOOR. REMOVED DOUBLER. FABRICATED AND INSTALLED NEW DOUBLER IAW SRM 52-80-02, FIG 8, 51-10-05, 51-10-03 AND 51-30-02.

Part: CUSP WEB — CRACKED (BS 633) · airframe 30,403 hrs · 13,860 cycles

RT CUSP WEB CRACKED BETWEEN X=-54 TO X=-60, STA 633. REMOVED CUSB WEB. FABRICATED AND INSTALLED NEW CUSP WEB AND CLIPS IAW SRM 51-10-05, 51-30-02 AND 51-10-03.

Part: CUSP WEB — CORRODED (BS 935-940) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON RT CUSP WEB, BS 935 TO 940, X=-54 TO X=-60, TASK 53-211-02. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-20-02, FIG 18 AND 53-10-03, PARA 38.

Part: ACCESS PANEL — CORRODED (UNKNOWN) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON COUNTERSINK, ON FUEL ACCESS DOOR 620 MB. REMOVED CORROSION. FABRICATED NEW BUSHING AND REWORKED AREA IAW SRM 57-00-04.

Part: SKIN — CRACKED (RT WING) · airframe 30,403 hrs · 13,860 cycles

RIGHT WING L/E, STA XRS=164, CRACKED SPLICE JUNCTION. REMOVED, FABRICATED AND INSTALLED NEW SPLICE IAW SRM 57-30-01, FIG 1, 51-30-02 AND 51-30-05.

Part: CUSP WEB — CORRODED (BS 682) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON LT CUSP WEB MEMBRANE, STA Y=682, BETWEEN X=55 AND X=59, TASK 53-211-01. REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-02, FIG 18 AND 51-10-03.

Part: BRACKET — BROKEN (SPOILER) · airframe 30,403 hrs · 13,860 cycles

BROKEN BRACKET ON INBD FLIGHT SPOILER TORSION BAR, STA XRS=209 AT LT WING. INSTALLED NEW BRACKET IAW AMM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,677 hrs · 16,435 cycles

CORROSION ON LEFT HAND CUSP MEMBRANE FROM STA 750 TO 767 BETWEEN X=55/60 TASK 53-211-01. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-02, 51-10-03 AND 51-30-02.

Part: SUPPORT FITTING — CORRODED (BS 198) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON SUPPORT FITTING, BS 198 AND X 44. SUPPORT REPLACED IAW SRM 53-10-01, FIG 10 AND 51-30-02.

Part: CUSP WEB — CORRODED (BS 929-940) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON RT CUSP WEB, X 54 TO X 60 BETWEEN BS 929 - 940. FOUND OUT OF LIMITS AND WAS REPAIRED.

Part: SKIN — CRACKED (BS 1376-1395) · airframe 30,403 hrs · 13,860 cycles

FUSELAGE SKIN, BS 1395-1376, LONGERON L10 - 11R CRACKED. REPAIRD IAW ERA 523447-14A.

Part: CUSP WEB — CORRODED (BS 767-807) · airframe 30,403 hrs · 13,860 cycles

CORROSION ON LT CUSP MEMBRANE, BS 767 - 807 BETWEEN X 55 AND X 60. AREA OUT OF LIMITS. CORROSION REMOVED IAW ERA 520318-14MA, REV O.

Part: WEB — CRACKED (BS 200) · airframe 30,403 hrs · 13,860 cycles

CRACK ON INTERNAL WEB AT BS 200, LONGERON 15L. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED A REPAIR IAW SRM 53-60-02, FIG 15 AND 51-10-03.

Part: CUSP WEB — CORRODED (BS 846-974) · airframe 30,403 hrs · 13,860 cycles

CORROSION FOUND ON LT CUSP WEB, BETWEEN BS 846-974. REMOVED CORROSION FOUND TO BE OUT OF LIMITS.

Part: BRACKET — MISSING (TAILCONE SLIDE) · airframe 30,007 hrs · 13,611 cycles

TAILCONE SLIDE COVER MISSING BRACKETS. INSTALLED BRACKETS.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 29,221 hrs · 13,111 cycles

FUSELAGE BULGED AT LAVATORY EXHAUST PORT. REMOVED SUPPORT BRACKET AND FOUND IT CORRODED. REPLACED SUPPORT BRACKET IAW DWG 5965766.

Part: SEAL — TORN (L1 DOOR) · airframe 29,217 hrs · 13,108 cycles

LARGE AIR LEAK FORWARD BOTTOM CORNER OF L1 DOOR DURING FLIGHT. DOOR SEAL TORN. REPAIRED IAW SRM 52-00-03 PRESSURIZED TO 4 PSI NO LEAKS.

Part: LONGERON — CRACKED · airframe 29,376 hrs · 13,196 cycles

LONGERON 11R CRACKED. REPAIRED IAW ERA 527345-14.

Part: SKIN — CRACKED (BS 1475) · airframe 29,376 hrs · 13,196 cycles

FUSELAGE SKIN CRACKED NEAR LONGERON LONGERON 2R, BS 1475. REPAIRED IAW ERA 527346-14.

Part: DOOR FRAME — CORRODED (AFT CARGO DOOR) · airframe 28,956 hrs · 12,960 cycles

AFT CARGO DOOR LOWER FRAME CORRODED. FABRICATED AND INSTALLED NEW THRESHOLD AND SPACER IAW SRM 53-60-02, FIG 9A.

Part: DOOR FRAME — CRACKED (LT MLW WW) · airframe 28,956 hrs · 12,960 cycles

LEFT WHEEL WELL OPENING CRACKED AT AFT OUTBOARD EDGE. DAMAGE CONTAINED. FABRICATED AND INSTALLED FRAME REPAIR IAW SRM 53-60-02, FIG 8.

Part: STARTER — OVERHEATED (APU) · airframe 28,578 hrs · 12,717 cycles

FLIGHT CREW REPORTED ELECTRICAL ODOR IN COCKPIT. MAINTENANCE TROUBLESHOT AND FOUND APU STARTER OVERHEATED. REPLACED RELAY 52-63 AS A PRECAUTION. R & R COALESCER BAGS. OPS CHECKED GOOD.

Part: FRAME — DAMAGED (BS 1379) · airframe 28,074 hrs · 12,423 cycles

A SECTION OF FRAME BS 1379, BETWEEN LONGERONS 10-11R DAMAGED. FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-02.

Part: SKIN — CRACKED (BS 1379) · airframe 28,074 hrs · 12,423 cycles

DURING LIGHTNING STRIKE INSPECTION, FOUND A 4.75 INCH LONG CRACK AT FRAME, BS 1379 AND SEVERAL SMALL CRACKS AT RIVETS ON LONGERONS 10 - 11R, JUST AFT OF BS 1379. REPAIRS COMPLIED WITH ON NON-ROUTINE CARDS.

Part: FRAME — CRACKED (BS 1374) · airframe 28,074 hrs · 12,423 cycles

FOUND CRACK, BS 1374, S7R UPPER FASTENER UNDER SHIM NEAR RADIUS. S9R, UPPER AND LOWER FASTENERS AT RADIUS AND S10R, UPPER FASTENER AT RADIUS. REMOVED FASTENERS AND SHIMS FROM STR 7, 9, 10 FRAME BS 1379. CUT OUT DAMAGE. FABRICATED AND INSTALLED FRAME REPAIR IAW SRM 53-10-02.

Part: APU — ODOR · airframe 27,682 hrs · 12,180 cycles

DURING INITIAL CLIMB, STRONG BURNING ODOR DETECTED IN FWD CABIN AND COCKPIT. NO SMOKE. DISSIPATED AFTER ABOUT ONE MINUTE. APU AUTO SHUTDOWN WITH CODE 87. HIGH OIL TEMP SEVERAL MINUTES AFTER SHUTDOWN. OIL TEMPRATURE STILL AT 150 C, 1 MIN PRIOR TO SHUTDOWN. BURNING ODOR NOTICED. R & R APU IAW AMM. OPS CHECKED NORMAL. PERFORMED DUCT BURNOUT IAW AMM. COALESCER BAGS REPLACED.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,376 hrs · 13,196 cycles

FUSELAGE SKIN DENTED. REPAIRED IAW ERA 493463-14.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,212 hrs · 10,719 cycles

DURING SERVICE CHECK, MX FOUND AFT CABIN EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK AT B5-107 IAW MM. OPERATION CHECKED GOOD.

Part: OXYGEN MASK — DAMAGED · airframe 24,848 hrs · 10,526 cycles

SHIP DIVERTED WITH CREW O2 PRESSURE READING 0 ALONG WITH OVERHEAD PANEL. MX PERFORMED LEAK CHECK OF O2 SYSTEM IAW AMM 3510. FOUND F/O'S MASK FERREL LOOSE. REPLACED MASK. UNABLETO LOCATE OR DUPLICATE ANY OTHER LEAKS OR FAULTS. REPLACED CREW O2 CYLINDER WITH SERVICABLE UNIT IAW AMM 35-10. SYS CHECKS GOOD.

Part: LIGHT — DISCONNECTED (TAILCONE) · airframe 24,676 hrs · 10,427 cycles

PILOT FOUND AFT STAIRWAY OVERHEAD EMERGENCY LIGHT DISCONNECTED. MX SECURED LIGHT, OPS CHECKED GOOD.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 24,616 hrs · 10,400 cycles

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

Part: LANYARD — BROKEN (R1 DOOR) · airframe 23,512 hrs · 9,773 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND R1 GIRT BAR LANYARD BROKEN. REMOVED AND REPLACED GIRT BAR LANYARD PER AMM.

Part: EPSU — INOPERATIVE (CABIN) · airframe 22,221 hrs · 9,160 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND AFT CABIN EXIT EMERGENCY LIGHT SIGN, 8 INCHES OFF THE FLOOR, INOPERATIVE. MAINTENANCE TROUBLESHOT L2-838 AND FOUND EPSU FAULTY B2-239. REMOVED AND REPLACED EPSU ASSEMBLY PER AMM. OPERATION CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: SPAR CAP — DAMAGED (VERTICAL STAB) · airframe 21,125 hrs · 8,589 cycles

VERTICAL STABILIZER, LEAD EDGE FRONT SPAR CAP DAMAGED. REPAIRED IAW AA 5530-01044.

Part: LUG — DAMAGED (STAB HINGE) · airframe 21,125 hrs · 8,589 cycles

HORIZONTAL STABILIZER HINGE RIB PIVOT BEARING LUG DAMAGE. REPAIRED IAW AA 5510-01083.

Part: SKIN — DAMAGED (BS 294) · airframe 21,123 hrs · 8,588 cycles

LIGHTNING STRIKE AT STA 294, LONGERON 4R. REPAIRED IAW SRM 53-31-02.

Part: FASTENER — DAMAGED (PYLON) · airframe 18,544 hrs · 7,519 cycles

PYLON AFT FITTING UPPER FASTENERS DAMAGED. REPLACED IAW AA 5440-01069.

Part: JACKSCREW — DAMAGED (HORIZONT STAB) · airframe 18,544 hrs · 7,519 cycles

HORIZONTAL STABILIZER JACKSCREW ASSY DAMAGED. REPAIRED IAW AA 2740-01071.

Part: STOP FITTING — DAMAGED (CARGO DOOR) · airframe 18,544 hrs · 7,519 cycles

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

Part: FRAME — DAMAGED (BS 883) · airframe 18,544 hrs · 7,519 cycles

BS 883 OVERWING FRAME DAMAGED. REPAIRED IAW AA 5310-01375.