N926DH

Part: THRUST REVERSER — DAMAGED (NR 2 ENGINE) · airframe 45,658 hrs · 29,982 cycles

DURING A MAINTENANCE CHECK, NR 2 ENGINE UPPER THRUST REVERSER HAS POSSIBLE HEAT DAMAGE DUE TO ENGINE FIRE. DRY CHEMICAL FIRE AGENT WAS USED TO EXTINGUISH FIRE FOLLOWED BY WATER. REPLACED THE THRUST REVERSER IAW AMDS CARDS 7830-4120 AND 7830-4372.

Part: WEDGE — NICKED (LT SPOILER) · airframe 45,658 hrs · 29,982 cycles

LT O/B FLIGHT SPOILER WEDGE HAS NICK ON T/E. COMPLETED REPAIR, REF ERA 581613-14 REV A. (LP#1286933)

Part: CRANK ASSY — WORN (RUDDER TAB) · airframe 45,658 hrs · 29,982 cycles

TAIL EXTERNAL: RUDDER TAB HAS EXCESSIVE PLAY AT CONTROL ROD, FWD END. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0248:5330-2171/016 00129. REPLACED WORN PARTS, CONTROL TAB UPPER CRANK. REF LONG BEACH DWG 5955542 AND AMM 27-21-02 PREFORMED RUDDER TRAVEL FUNCTIONAL TEST PER B AMM 27-20-01. CHECKS OK. (LP# 1283111)

Part: TAB — WORN (RT AILERON) · airframe 45,658 hrs · 29,982 cycles

RIGHT WING: PAINT WORN COMPOSITE FIBERS EXPOSED TOP OF AILERON CONTROL TAB. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0265:5700-2494/011 00086 REMOVED INSTALLED RT AILERON CONTROL TAB ON 2710-4536 -RT REPAIRED PER S/O PZ3311. (LP# 1280394)

Part: TAB — WORN (RT AILERON) · airframe 45,658 hrs · 29,982 cycles

RIGHT WING: PAINT WORN COMPOSITE FIBERS EXPOSED TOP OF AILERON CONTROL TAB. REMOVED RT AILERON CONTROL TAB PER MD90 AMDS 2710-4236. TAB, AILERON CO OFF 88-2710-9-0011 10211. RH AILERON CONTROL TAB INSTALLED ON LOG 1280394. (LP1272938)

Part: STRUT — DISCHARGED (NLG) · airframe 45,400 hrs · 29,817 cycles

PERF. INITIAL INSP UPON ARRIVAL TO GATE, FOUND NOSE STRUT FLAT. REMOVED PISTON AND CYLINDER ASSY, REF AMM 32-21-01. REPACKED NOSE GEAR PER CMM 32-21-1 REV 62 12 /11/2017. REINSTALLED CYLINDER AND PISTON ASSY, STEERING AND GEAR SWING CHECKED GOOD, REF MD90 AMM 32-21-01.

Part: UNKNOWN — ODOR (CABIN) · airframe 44,368 hrs · 29,139 cycles

SHIP 9226 -DIV- GPT. FA REPORTED A RUBBERY ELECTRIC BURNING SMELL ABOVE SEATS 16 A/B AND 17 A/B. CORRECTIVE ACTION: T/S PER FIM 21-22-00-810-811. INSPECTED AREA BETWEEN SEAT ROWS 15+18 WITH NTF. PERFORMED FULL DUCT BURNOUT AND REPLACED BOTH PACK COALESCER BAGS. LT AND RT PACKS OPERATIONAL CHECKS GOOD. NO SMELL OR ODORS NOTED. C/W NO-GO ODI PREVENTION PROGRAM WITH NO FAULTS. (LP# 5746586)

Part: UPLOCK SENSOR — FAILED (NLG) · airframe 42,930 hrs · 28,236 cycles

NLG UNSAFE INDICATION AFTER TAKEOFF WITH GEAR HANDLE UP. AFTER CYCLING NLG, ENCOUNTERED NG DOOR NOISE. LOWERED GEAR AND HAD ALL NORMAL INDICATIONS. RETURNED TO DEPARTURE, WITH HYDRAULIC PRESSURES NORMAL. FOUND THE UPLOCK SENSOR D1-31 IN POOR CONDITION. IMPEDANCE CHECKED. CONFIRMED FAILURE . REPLACED THE UPLOCK SENSOR D1-31. CLEANED THE CONNECTOR R5-1156, AND SERVICED NLG STRUT. SWUNG NLG SEVERAL TIMES. PERFORMED NO-GO ODI PREVENTION TASKS. OPS AND INDICATIONS ALL NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,760 hrs · 27,544 cycles

L2 DOOR SMALL EMERGENCY EXIT SIGN INOPERATIVE. REPLACED THE POWER SUPPLY & BATTERY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,139 hrs · 27,173 cycles

EMERGENCY LIGHT INOPERATIVE FORWARD OF L2 DOOR. CHANGED EMERGENCY POWER BATTERY. LIGHT OPERATION CHECKS GOOD.

Part: SKIN — DEBONDED (THRUST REVERSER) · airframe 40,674 hrs · 26,874 cycles

DISBOND SKIN ON LEFT THRUST REVERSE LOWER HALVE OTBD FWD SPAR AT 9 O`CLOCK POSITION AND REPAIRED IAW 599544-14.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON DOOR JAMB UNDER PREVIOUS REPAIR DOUBLER, STA 1212-1269 AFT CARGO. REPAIRED IAW SRM 53-60-02.

Part: CARGO TRACK — CORRODED (BS 1060-1212) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON RIGHT CARGO TRACK, BS 1060 - 1212, AFT CARGO BAY. REPLACED IAW SRM 51-30-01, 51-30-02 AND 51-10-06.

Part: LONGERON — CRACKED (BS 1475) · airframe 40,674 hrs · 26,874 cycles

CRACK ON LONGERON 2L, BS 1475. REPLACED IAW SRM 53-10-01.

Part: DOOR FRAME — CRACKED (RT MLG WW) · airframe 40,674 hrs · 26,874 cycles

CRACK AT FORWARD RIGHT MAIN LANDING GEAR DOOR FRAME CHANNEL. REPLACED IAW DWG 5930584-122, SRM 51-30-02 AND 51-30-05.

Part: STRAP — DAMAGED (BS 1250-1260) · airframe 40,674 hrs · 26,874 cycles

DAMAGED STRAP, OUT OF LIMITS FROM BS 1250 AND 1260. REPLACED IAW SRM 51-30-02, AND DWG 5936442.

Part: ANGLE — CRACKED (BS 1495) · airframe 40,674 hrs · 26,874 cycles

CRACKED ANGLE BS 1495 BETWEEN LONGERON 3L AND 3R AFT ACC COMPARTMENT. REPLACED IAW DWG 9953016.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON SCUFF PLAT SUPPORT STA 269 OVER DOOR JAMB WEB AFT LOWER CARGO COMPARTMENT. REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-05.

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 40,674 hrs · 26,874 cycles

CRACKED SKIN ON HANDLE HOUSING AT CENTER CARGO DOOR. REPAIRED HOUSING IAW ETI-90-17-071 AND ERA 559513-14.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON FRAME, STA 1437 BETWEEN PROJECTION OF LONGERONS 27R-29R. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 51-30-05 AND DWG 9912246.

Part: FLOOR PANEL — PUNCTURED (COCKPIT) · airframe 40,674 hrs · 26,874 cycles

PUNCTURE ON COCKPIT FLOOR PANEL 211BG. REPAIRED IAW SRM 53-00-01.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON DOUBLER ON STA 1395 AND PROJECTION OF LONGERON 30. REPLACED IAW SRM 51-30-02, 51-30-05 AND DWG 9915561.

Part: SPACER — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON PREVIOUS REPAIR SPACER AT LOWER DOOR JAMB STA 693-750. REPLACED IAW SRM 53-60-02.

Part: COVER — CRACKED (FLOOR PANEL) · airframe 40,674 hrs · 26,874 cycles

CRACKED METALLIC COVER JUST ABOVE FLOOR PANELS, STA 110 AT COCKPIT. REPAIRED IAW SRM 53-00-01.

Part: TRACK — DAMAGED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

TIE TRACK OUT OF LIMITS FROM STA 1264-1307. REPLACED IAW SRM 51-10-05 AND 53-20-01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON INTERCOSTAL, STA 826-845 BETWEEN LONGERONS 28-27 RIGHT HAND SIDES ALSO OVER LONGERON 30.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON FRAME STA 1344 JUST ABOVE LONGERON 28L AT AFT CARGO COMPARTMENT. REPAIRED IAW SRM 53-10-02.

Part: FITTING — WORN (VENTRAL DOOR) · airframe 40,674 hrs · 26,874 cycles

WEAR ON RIGHT HAND LOWER FITTING AT VENTRAL DOOR. REPLACED IAW SRM 51-30-05.

Part: FITTING — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION O FRAME CLIP, STA 1288 BETWEEN LONGERON 30 TO 29L. REPLACED IAW SRM 51-30-02 AND 51-30-05.

Part: FITTING — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON FRAME CLIP, STA 1344 BETWEEN LONGERON 27L TO 27R. REPAIRED IAW SRM 53-10-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CRACK ON FRAME CLIP, STA 1288 BETWEEN LONGERON 30 TO 29R AFT CARGO. REPLACED IAW SRM 51-30-05 AND 51-30-02.

Part: RETAINER — CORRODED (CARGO DOOR) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON LOWER RETAINER AT AFT CARGO DOOR BARRIER. REPLACED IAW SRM 51-30-01.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON CENTER CARGO COMPARTMENT DOOR BARRIER. DAMAGED CHANNEL REPLACED IAW SRM 51-30-01.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON FLOOR PANEL. REPLACED IAW SRM 51-30-02 AND DWG 9957828.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON FLOOR SUPPORT STA 218 BETWEEN LONGERON 28R TO 28L. REPLACED IAW SRM 53-10-01 AND 51-30-01.

Part: ACCESS PANEL — DAMAGED (WING) · airframe 40,674 hrs · 26,874 cycles

ELONGATED HOLES ON FUEL PANEL 520LB, 520EB, 520GB AND 520KB. OUT OF LIMITS. REPLACED.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CRACKED LONGERON STA 1495, 12L. REPAIRED IAW SRM 53-10-01.

Part: FITTING — CRACKED (TE FLAP) · airframe 40,674 hrs · 26,874 cycles

CRACK ON FITTING STA 1041, RIGHT HAND FLAP ACTUATOR MECHANISM. REPLACED FITTING IAW SRM 51-30-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CRACKED RIGHT HAND CUSP WEB, STA 764, 924 AND 962 BELOW PRODUCTION DOUBLER. REPAIRED IAW SRM 53-20-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON FLOOR SUPPORTS, STA 200, X=-45 TO X=-54 AND STA 200-215, X=-56. REPLACED IAW SRM 51-30-02, 51-30-05.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CRACKED LEFT HAND FLOOR BEAM, STA 984, X=56 AT WING BOX. REPLACED IAW SRM 51-30-01, 51-30-02, AND 51-30-05.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON FLOOR SUPPORTS FROM STA 160-196, X=44 AND X=54. REPLACED IAW SRM 51-30-02, 51-30-05 AND 53-10-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CRACK ON UPPER ANGLE OF VENTRAL STAIRWAY BULKHEAD FROM STA 1395, LONG 1. REPLACED IAW DWG9915562 AND SRM 51-30-02, 51-30-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON FLOOR SUPPORT STA 130-150, X=-55. REPLACED IAW SRM 515-10-01, 53-10-01 AND 51-10-05 AND DWG 9936533.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON FLOOR SUPPORT STA 185-193, X=52 AND STA 200, X=10. REPLACED IAW SRM 53-10-02, 51-10-05 AND 51-30-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON FLOOR SUPPORT STA 180, X=-2 TO X=-42. REPLACED IAW SRM 51-30-02 AND 51-30-05.

Part: SKIN — CORRODED (WING) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON SETTLEMENT AREA ON FUEL PANEL 620CT AND 620AT. FOUND OUT OF LIMITS. REPLACED IAW SRM 57-00-04.

Part: FITTING — CORRODED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON FITTINGS X=-45 AND X=-52, STA 160. REPLACED IAW SRM 51-30-05.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON FLOOR SUPPORT BS 160 - 200 LBL 5. REPLACED IAW SRM 51-30-01 AND 51-30-05.

Part: ACCESS PANEL — CORRODED (WING) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON COUNTERSINK OF FUEL PANEL 520DB. FOUND OUT OF LIMITS. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — DAMAGED (WING) · airframe 40,674 hrs · 26,874 cycles

ELONGATED HOLES ON ACCESS PANEL 620GB. REPAIRED WITH BUSHINGS IAW SRM 57-00-04.

Part: SEAT TRACK — CORRODED (BS 200-275) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON RIGHT SEAT TRACK, BS 200 TO 275, RBL 22. FOUND OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 53-40-01.

Part: ANGLE — CRACKED (BS 883-888) · airframe 40,674 hrs · 26,874 cycles

CRACKED RIGHT ANGLE BETWEEN BS 883 - 888 AND RBL 42 IN THE WING BOX. REPAIRED IAW ERA 498192-14.

Part: ANGLE — CRACKED (BS 883-888) · airframe 40,674 hrs · 26,874 cycles

CRACKED LEFT ANGLE BETWEEN BS 883 - 888 AND LBL 42. REPAIRED IAW ERA 498192.

Part: FLOOR SUPPORT — CORRODED (BS 1364-1402) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON FLOOR SUPPORT BS 1364 TO 1402, RBL 44. REPLACED IAW SRM 51-30-05.

Part: FLOOR SUPPORT — DAMAGED (BS 1196) · airframe 40,674 hrs · 26,874 cycles

FLOOR SUPPORT OUT OF LIMITS. BS 1196, LBL 60. REPLACED IAW SRM 51-30-05 AND DWG 5930490.

Part: LATCH — CORRODED (BS 166-195) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON SLIDE LATCH FITTINGS, BS 166 AND 195, RBL 53. REPLACED IAW SRM 51-30-01.

Part: FLOOR SUPPORT — CORRODED (BS 148-200) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON FLOOR SUPPORT FROM BS 148 - 200, RBL 6 TO 8. REPLACED IAW SRM 53-10-01 AND 51-30-01.

Part: CUSP WEB — CORRODED (BS 200-218) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON RIGHT HAND CUSP WEB BS 200 TO 218 X=-44 TO X=-60. REPAIRED IAW SRM 51-11-01.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 40,674 hrs · 26,874 cycles

CRACKED FITTING ON INNER LOWER EDGE BS 712 AT CENTER CARGO DOOR. REPLACED IAW SRM 51-30-02.

Part: INTERCOSTAL — CRACKED (BS 714) · airframe 40,674 hrs · 26,874 cycles

CRACKED INTERCOSTAL ON INNER LOWER EDGE BS 714 AT CENTER CARGO DOOR. REPLACED IAW SRM 551-30-02 AND 51-30-05. (LP# 0110626)

Part: BEAM — CRACKED (L1 DOOR) · airframe 40,674 hrs · 26,874 cycles

CRACKED NR 1 BEAM ON FORWARD & AFT EDGE AT L1 DOOR. REPAIRED IAW SRM 52-10-02.

Part: WEB — PUNCTURED (BS 148) · airframe 40,674 hrs · 26,874 cycles

PUNCTURE ON DIAPHRAGM BS 148, X=-30. REPAIRED IAW SRM 51-11-01.

Part: ACCESS PANEL — CORRODED (WING) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 520CT. FOUND OUT OF LIMITS. REPLACED.

Part: PANEL — CRACKED (NR 1 SLAT) · airframe 40,674 hrs · 26,874 cycles

CRACKED SLAT PANEL SKIN NR 1, XIS 136, LEFT WING. REPAIRED IAW SRM 57-00-01.

Part: PANEL — CRACKED (SLAT) · airframe 40,674 hrs · 26,874 cycles

CRACKED SLAT PANEL NR 2, XOS 240 LEFT WING. REPAIRED IAW SRM 51-00-01

Part: PAN — CRACKED (CARGO DOOR) · airframe 40,674 hrs · 26,874 cycles

CRACKED AFT EDGE ON INNER PAN AT FORWARD CARGO DOOR BETWEEN BEAM 1-2. REPAIRED IAW SRM 52-30-02.

Part: PAN — CRACKED (CARGO DOOR) · airframe 40,674 hrs · 26,874 cycles

CRACKED FORWARD EDGE ON INNER/OUTER PAN BETWEEN BEAMS 1-2 AT FORWARD CARGO DOOR. REPAIRED IAW SRM 52-30-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,674 hrs · 26,874 cycles

CRACKED FUSELAGE SKIN STA 1531.604 CANT BETWEEN LONGERONS 22R-23R. REPAIRED IAW SRM 53-00-01.

Part: PAN — CRACKED (CARGO DOOR) · airframe 40,674 hrs · 26,874 cycles

WORN LOWER EDGE ON INNER AND OUTER PAN AT CENTER CARGO DOOR. REPAIRED IAW ERA 413163-14.

Part: SUPPORT — CORRODED (CARGO DOOR) · airframe 40,674 hrs · 26,874 cycles

CORROSION ON CENTER CARGO COMPARTMENT DOOR BARRIER FORWARD/AFT STRAP SUPPORTS. REPLACED IAW SRM 51-30-01.

Part: PAN — WORN (FWD CARGO DOOR) · airframe 40,674 hrs · 26,874 cycles

WORN FORWARD & AFT LOWER EDGE ON INNER & OUTER PAN AT FORWARD CARGO DOOR. REPAIRED IAW ERA 413163-14.

Part: SLIDE — LOW PRESSURE (SERVICE DOOR) · airframe 39,888 hrs · 26,431 cycles

AFT SERVICE DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE IAW MM.

Part: RECEPTACLE — WORN (TAILCONE) · airframe 39,790 hrs · 26,376 cycles

TAILCONE HAS SEVERAL GUIDE PIN RECEPTACLES WORN OUT OF ROUND. REMOVED AND REPLACED IAW SRM 51-41-01.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 39,596 hrs · 26,274 cycles

DURING TAKEOFF, THE AMBER FLOW LIGHT ILLUMINATED ON THE CABIN PRESSURE CONTROL PANEL. BOTH PACKS INOPERATIVE USING LT AND RT ENGINE PNEUMATICS. PRESSURIZED AIRCRAFT WITH APU AIR. MAINTENANCE REMOVED AND REPLACED PSC IAW MM. OPERATIONAL CHECKED GOOD.

Part: SUPPORT FITTING — DAMAGED (RT MLG) · airframe 38,916 hrs · 25,857 cycles

RIGHT MLG SUPPORT FITTING BEARING BORE GROOVED. FABRICATED AND INSTALLED NEW BUSHING AND BEARING IN OVERSIZE BORES IAW ERA 551862-14AD, REV P.

Part: SUPPORT FITTING — DAMAGED (LT MLG) · airframe 38,916 hrs · 25,857 cycles

LEFT MLG SUPPORT FITTING BEARING BORE GROOVED. MACHINED BEARING BORE AND INSTALLED NEW BUSHING AND BEARING IAW ERA 551861-14AD, REV O.

Part: AIRSTAIR — CORRODED · airframe 38,916 hrs · 25,857 cycles

AFT AIR STAIR FORWARD SECTION HAS CORROSION. OUT OF LIMITS. REMOVED AND REPLACED AFT ENTRANCE DOOR STAIRWAY ASSEMBLY IAW MM AND ERA 551859-14, REV O. (LP# 2740635)

Part: FLOOR PANEL — CRACKED (BS 1519) · airframe 38,916 hrs · 25,857 cycles

AFT ACCESSORY COMPARTMENT BS 1519 UPPER FLOOR PANEL SKIN RBL 9 IS CRACKED. FABRICATED AND INSTALLED A REPAIR ON THE FLOOR PANEL.

Part: SKIN — CRACKED (L1 DOOR) · airframe 38,916 hrs · 25,857 cycles

L1 DOOR LOWER SKIN FORWARD AREA HAS CRACKED AND WAVED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 52-10-01.

Part: BEAM — CORRODED (AFT CARGO BAY) · airframe 38,916 hrs · 25,857 cycles

AFT CARGO LOWER DOOR FRAME OUTBOARD BEAM HAS VISIBLE CORROSION ABOVE AFT LOWER STOP FITTING APPROXIMATELY BS 1259. FOUND OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER SPACER IAW SRM 53-60-02.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 38,916 hrs · 25,857 cycles

L1 DOOR LOWER ANGLE IS CRACKED. REMOVED AND REPLACED LOWER ANGLE IAW SRM 51-30-02 AND DW 5910081, REV FD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,261 hrs · 24,899 cycles

EMERGENCY LIGHTS OUT AT ROWS 23-26. R & R BATTERY PACK IAW MM. OPS CHECK OK.

Part: LINE — LEAKING (THRUST REVERSER) · airframe 36,557 hrs · 24,476 cycles

ON DESCENT, FUMES, LIGHT SMOKE AND MIST REPORTED BY F/A IN AFT CABIN AREA. MAINTENANCE FOUND LT THRUST REVERSER STOW LINE LEAKING. REPAIRED LINE IAW AMM. OPERATION AND LEAK CHECKS OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,287 hrs · 24,282 cycles

CEILING EXIT SIGN DOES NOT ILLUMINATE. REPLACED BATTERY PACK. OK FOR SERVICE.

Part: UNKNOWN — ODOR (AFT CABIN) · airframe 35,736 hrs · 23,931 cycles

ELECTRICAL WIRE BURNING ODOR IN AFT PART OF CABIN DURING DESCENT. QRH GALLEY POWER AND SIDEWALL LIGHTS TURNED OFF. ODOR DISSIPATED. MAINTENANCE TROUBLESHOT. NO ODORS NOTED. REPLACED COALESCER BAGS AND RECIRICULATION FAN FILTER. COMPLETED DUCT BURN OUT. ALL CHECKS GOOD.

Part: STRUCTURE — HANDLER ERROR · airframe 34,498 hrs · 23,181 cycles

JETWAY DAMAGED, FUSELAGE AFT OF L1 DOOR. COMPLIED WITH EAR 533293-14, SECTION I AND ER 533293-14, SECTION II.

Part: STRUCTURE — DENTED (LT NOSE COWL) · airframe 33,773 hrs · 22,729 cycles

FOUND BIRD STRIKE DENT AT LT ENGINE NOSE COWL. INSPECTED DENT, FOUND OUT OF LIMITS. R & R LEFT ENGINE NOSE COWL IAW AMM.

Part: PIN — MIGRATED (L1 DOOR SLIDE) · airframe 33,656 hrs · 22,638 cycles

PARACHUTE PIN MIGRATING OUT OF RETENTION STUD. R & R FORWARD ENTRY L1 DOOR SLIDE IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,656 hrs · 22,638 cycles

ACFT SKIN HAS A TWO INCH CRACK AT ADJACENT FASTENER HOLES FORWARD OF TAIL CONE RELEASE HANDLE. REPAIRED IAW PRI 529909-14.

Part: FRAME — WORN (BS 1437) · airframe 33,656 hrs · 22,638 cycles

TAIL INTERIOR FRAME, BS 1437, WEB FORWARD SURFACE IS DEEPLY WORN NEAR, L5L. REPAIRED IAW SRM 53-00-01,

Part: FRAME — CRACKED (BS 1520) · airframe 33,656 hrs · 22,638 cycles

TAIL INTERIOR CANTED FRAME AFT WEB HAS A CRACK, BS 1520, 18 INCHES INBD OF L10 END FITTING. FABRICATED DOUBLER AND INSTALLED IAW SRM 51-11-01.

Part: ACM — OVERSERVICED (RIGHT) · airframe 32,407 hrs · 21,822 cycles

F/A REPORTED SMOKE & HAZE COMING FROM THE RT OVERHEAD BIN AREA AROUND THE EMERGENCY EXIT ROW. LASTED APPROXIMATELY THREE MINUTES, AT WHICH TIME BEGAN TO DISSIPATE. NO FURTHER ISSUES. TROUBLESHOT, FOUND RT ACM OVERSERVICED. PROPERLY SERVICED RIGHT ACM IAW AMM. REPLACED COALESCER BAGS AND PERFORMED DUCT BURNOUT. INSTALLED IAW MEL 21-51-01A. R & R RT COOLING TURBINE IAW AMM. OPS AND LEAK CHECKS GOOD. MCO/PLAC REMOVED.

Part: SKIN — PUNCTURED (BS 77) · airframe 31,771 hrs · 21,422 cycles

FUSELAGE, SKIN, BS 77, BELOW AOA VANE PUNCTURED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,393 hrs · 21,169 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND CABIN EMERGENCY STANDBY LIGHTS INOPERATIVE. REPLACED LAMP IAW AMM. OPS CHECKED GOOD.

Part: LATCH — MISINSTALLED (GIRT BAR) · airframe 31,114 hrs · 21,011 cycles

L2 DOOR GIRT BAR LATCH INSTALLED BACKWARDS AND UNABLE TO ARM GIRT BAR. REPOSITIONED LATCH. OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,751 hrs · 20,772 cycles

AFT EMERGENCY LIGHT FLASHING. R & R POWER SUPPLY B5-239. OPS CHECKED NORMAL.

Part: COFFEEMAKER — DIRTY (CABIN) · airframe 29,632 hrs · 20,142 cycles

EXPERIENCED SLIGHT HAZE AND ODOR IN R1 GALLEY APPROXIMATELY 40 MINUTES INTO FLIGHT. COFFEE POTS TURNED OFF AND CIRCUIT BREAKERS PULLED WITH NO EFFECT. COCKPIT GALLEY POWER WAS TURNED OFF AND HAZE/ODOR DISSIPATED. MX FOUND BURNED DEBRIS ON BOTTOM OF COFFEE POT AND COFFEEMAKER HOT PLATE. CLEANED COFFEE POT AND HOT PLATE. OPERATED PACKS WITH APU AND ENGINES. NO FURTHER HAZE OR ODOR NOTED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,171 hrs · 19,877 cycles

ACFT FUSELAGE DAMAGED RT SIDE 6" BELOW AOA VANE. INSTALLATION GOOD IAW PRI 510048-14, REV 3. FINAL ERA RECEIVED AND MATCHED QC1502.

Part: ANGLE — DAMAGED (COCKPIT) · airframe 29,171 hrs · 19,877 cycles

COCKPIT PRESSURE DECK ANGLE FS 77, RT SIDE HAS NICK IN RADIUS .023 DEEP BEFORE CLEANUP. DUE PRI510048-14, REV 3. COMPLIED WITH PRI 510048-14M, REV3 QC1503 FINAL ERA AND MATCHED.

Part: FRAME — BENT (FUELAGE) · airframe 29,171 hrs · 19,877 cycles

FRAME RT SIDE, STA 83.5 REMOVED FOR REPAIR (FRAME 4). FOUND FRAME BENT AT UPPER END. DRILLED UP NEW FRAME. OK TO INSTALL FRAM AT STA 83.5 QC4044. INSTALLED NEW FRAME IAW DWG 9911505.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 29,171 hrs · 19,877 cycles

TOOLING DAMAGE ON FRAME FS64, ABOVE RT PRESSURE DECK CHORD. REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER IAW SRM 51-70-01. OK TO INSTALL REPAIR DOUBLER. INSTALLED REPAIR IAW SRM 51-70-01.

Part: SLIDER — OUT OF RIG (TAIL CONE) · airframe 28,802 hrs · 19,671 cycles

TAILCONE UPPER SLIDER BLOCKS NOT RIGGED IN CORRECT POSITION. IMPROPER INSTALLATION LT AND RT UPPER SLIDING BLOCKS. ADJUSTED CLAMPS IAW AMM AND OPS CHECKED GOOD.

Part: CABLE — OUT OF TOLERANCE · airframe 28,765 hrs · 19,655 cycles

DURING INSPECTION AND RIG CHECK, MSU FOR VENTRAL STAIRWAY MOVEABLE CEILING, FOUND LT LIFT CABLE UNDER TENSION. RIGGED IAW MM. OPS CHECKED GOOD. OK FOR SERVICE.

Part: CABLE — FRAYED (JETTISON SYSTEM) · airframe 28,375 hrs · 19,427 cycles

WHILE PERFORMING TAIL CONE FUNCTIONAL CHECK, FOUND NITROGEN JETTISON BOTTLE ACTIVATION CABLE FRAYED. MAINTENANCE REMOVED AND REPLACED TAIL CONE NITROGEN JETTISON BOTTLE PULL CABLE PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,922 hrs · 19,189 cycles

DURING SERVICE CHECK, MAINTENANCE, FOUND WHEN EMERGENCY LIGHTS ARE TURNED ON, OVERHEAD AISLE AND LEFT AFT SERVICE DOOR LIGHTS ILLUMINATE THEN GO OFF. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 27,472 hrs · 18,934 cycles

EXPERIENCED ODOR IN THE CABIN ON APPROACH. MAINTENANCE PERFORMED BURNOUT PER AMM 21-53. OPS CHECKED NORMAL.

Part: FIRE LOOP — DAMAGED (NR 1 ENGINE) · airframe 27,089 hrs · 18,736 cycles

FLIGHT RETURNED TO MSP DUE TO NUMBER 1 ENGINE FIRE INDICATION CREW ACCOMPLISHED QRH PROCEDURES, PULLED FIRE HANDLE AND DISCHARGED FIRE BOTTLE (IFSD). AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND BURNT FERRELS ON LOWER CORE FIRE DETECTOR LOOP ASSEMBLY. REMOVED AND REPLACED DETECTOR LOOPS AND GROMMETS.

Part: CONTROL UNIT — ODOR (AIR CONDITIONING) · airframe 26,833 hrs · 18,600 cycles

ACFT EXPERIENCED HAZE AND FUMES IN THE CABIN DURING TOP OF DESCENT. MAINTENANCE OPERATED CABIN LIGHTING AND GALLEY ELECTRICAL POWER. NO TROUBLE FOUND. OPERATED BOTH PACKS WITH APU AIR AT HOT AND COLD. RAN ENGINES AT HIGH POWERSETTINGS WITH PACKS RUNNING. NO SMOKE NOTED. INSPECTED ACM INLETS AND OUTLETS FOR OIL CONTAMINATION. NONE FOUND. REPLACED COALESCER BAGS AND LEAK CHECKED OK. FOUND ELECTRICAL BURNING ODOR COMING FROM EPCU. REMOVED AND REPLACED EPCU.

Part: SKIN — DAMAGED (TE FLAP) · airframe 26,696 hrs · 18,533 cycles

FOUND HOLE IN LEFT WING FLAP LOWER SURFACE 5 3/8 INCHES FORWARD OF TRAILING EDGE - APPROXIMATELY 32 INCHES IN OF OUTBOARD. MAINTENANCE CUT AWAY DAMAGE 1 INCH DIAMETER PER ERA 499808-14. PERFORMED DVI NTF. HFEC PER MD90 NDT SPM 06-10-01, .001 DAMAGE REMOVED. FABRICATED DOUBLER FROM 2024-T3 .063. TREATED, PRIMED, PAINTED AND INSTALLED WITH CR3212-5.

Part: LIGHT — MISSING (EXIT SIGN) · airframe 26,243 hrs · 18,323 cycles

DURING LINE CHECK, MAINTENANCE FOUND 2 MISSING AND 1 BURNT OUT BULBS AT FORWARD 2L DOOR EMERGENCY EXIT SIGN. MAINTENANCE RELAMPED. OPERATION CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: COFFEEMAKER — OVERHEATED (GALLEY) · airframe 25,445 hrs · 17,935 cycles

FLIGHT ATTENDANTS REPORTED A BURNING SMELL IN THE CABIN DURING THE LAST 10 MINUTES OF FLIGHT. PASSENGERS COULD SMELL THE FUMES THROUGHOUT AIRCRAFT. MAINTENANCE FOUND THE FORWARD GALLEY COFFEEMAKER EXTREMELY HOT. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY COFFEEMAKER. OPERATION CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: ANGLE — CORRODED (AFT AIR STAIR) · airframe 25,175 hrs · 17,794 cycles

AFT AIR STAIR RT ANGLE, STA 1445, CORRODED. REPLACED ANGLE IAW SRM 51-30-01.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 25,174 hrs · 17,793 cycles

ACFT MODIFIED IAW ERA484704-14, REV A, STABILIZER, HORIZONTAL, RT, LOWER SKIN PANELS REPLACEMENT.