Douglas DC-8-73F

Service difficulty reports · 15,471

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC873F'
  ORDER BY difficulty_date DESC"

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SDR UPS08852444Structure · damagedINSPECTION TYPE:C2 MAIN CABIN, FLOORBOARD TIEDOWN BULGED AND FASTENERS PULLING STA 350 LBL 35. REMOVED, DAMAGED RECEPTICLE, FABBED AND INSTALLED REPAIR DOUBLER ON FLOOR PANEL, INSTALLED NEW RECEPTICLE IAW SRM 51-1-8, 53-2-3 FIG 1F, 51-1 -21A, 51-1-11.May 25, 2008 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS08852536Floorboard · crackedINSPECTION TYPE:C2 MAIN CABIN FLOORBOARD CRACKED, STA 45 RBL 47. FABBED AND INSTALLED REPAIR DOUBLER IAW, SRM. 53-2-00, 53-2-3, 510108, 51-1-26, 51-1-21.May 25, 2008 · N802UP · Doug DC873F · Fuselage Floor PanelSDR UPS08852606Fitting · crackedINSPECTION TYPE:C2 RIGHT WHEEL WELL AT UPPER FWD BULKHEAD, HYDRAULIC MANIFOLD PULLEY BRACKET IS CRACKED. REMOVED CRACKED FITTING, REPAIRED AND RE-INSTALLED FITTING IAW SRM 20-16-0, 51-1-8, DPS 4.706, DPS9.18.May 24, 2008 · N802UP · Doug DC873F · Main Landing GearSDR UPS08852433Seat Track · damagedINSPECTION TYPE:C2 COCKPIT, SECOND OBSERVER SEAT TRACKS SHOW ELONGATIONS. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-3-0, 51-1-2, 51-1-8.May 24, 2008 · N802UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS08852462Seat Track · wornINSPECTION TYPE:C2 COCKPIT SECOND OBSERVER SEAT TRACKS SHOWS ELONGATIONS. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-1-8, 51-3-0, 51-1-24.May 24, 2008 · N802UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS08852535Seat Track · wornINSPECTION TYPE:C2 PILOT REAR LT AND RT SEAT TRACKS SHOW ELONGATIONS REMOVED AND REPLACED 2 EACH SEAT TRACKS IAW SRM, 51-1-20D, 51-1-24.May 24, 2008 · N802UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS08852463Frame · chafedINSPECTION TYPE:C2 NR 2 PYLON UPPER PANEL FRAME, WORN BEYOND LIMITS, DEEP CHAFED DAMAGE BETWEEN PANELS 293A/B AND 294A/B. FABBED AND INSTALLED NEW PANEL FRAME IAW SRM, 51-1-8, 51-1-20D, 51-1-2 1, 54-3-3 FIG 7.May 23, 2008 · N802UP · Doug DC873F · Nacelle/Pylon, Frame/Spar/RibSDR UPS08852461Fitting · crackedINSPECTION TYPE:C2 MAIN CARGO COMP STA 980, L22R ATTACHING FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20, 51-1-20D, 51-1-8.May 22, 2008 · N802UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS08852579Flap · damagedINSPECTION TYPE:C2 INTERIM REPAIR TO RT INBOARD FLAP AT TRAILING EDGE XM-75. REMOVED INTERIM REPAIR, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-21A, 51-1-8, 51-1-9A.May 21, 2008 · N802UP · Doug DC873F · Trailing Edge FlapsSDR DHL2008807525Fitting · crackedFWD CARGO COMPT FITTING CRACKED STA 300.000 L-26L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-11, SRM 51-1-20D, SMay 19, 2008 · N807DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2008807526Stiffener · crackedKEEL BEAM TEE STIFFENER (EXTRUSION) HAS TWO CRACKS OF 0.250 INCH STA 896.000. REMOVED CRACKED TEE STIFFENER IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW STIFFENER IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE).May 14, 2008 · N807DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2008807530Skin · crackedFUSELAGE NOSE SECTION, MODIFICATION DOUBLER AT AFT UPPER CORNER OF RT PRIMARY HEAT EXCHANGER, STA -12.000 L-24R (0.500" SKIN CRACKED) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-30-08, EVA D853-00056 REV IR DATED 04-16-08, ASTAR DWG NR EMay 13, 2008 · N807DH · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS08852352Fitting · crackedINSPECTION TYPE:C3 STA 280, L36 FLANGE IS CRACKED ON FITTING. REMOVED AND REPLACED STA 280/L 36 FITTING IAW SRM 51-01-24-0 AND SRM 51-03-00-0.May 13, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR IXXA080021OLanding Gear · malfunctionedDURING TAKEOFF FROM GOOY, THE NOSE LANDING GEAR WOULD NOT RETRACT. THE CREW WAS ABLE TO RETRACT NOSE GEAR WITH HANDLE LATCH FLIGHT RELEASE. WHEN NOSE GEAR RETRACTED THE TAKEOFF WARNING HORN SOUNDED, THE CREW PULLED GROUND SHIFT BREAKERS, WHEN THE LEFT BREAKEMay 13, 2008 · N604BX · Doug DC873F · Landing Gear Retraction/Extension SystemSDR UPS08852235Engine · flamed outINSPECTION TYPE:N/A CLIMBING THROUGH FL360 THE NR 4 ENGINE FLAMED OUT. DESCENDED TO FL220 AFTER ACCOMPLISHING THE IN FLIGHT ENGINE FLAMEOUT CHECKLIST TO ATTEMPT A RESTART. FOLLOWED THE IN FLIGHT ENGINE START CHECKLIST AND ATTEMPTED 1 RESTART. AFTER DRY MOTOMay 13, 2008 · N805UP · Doug DC873F · Engine (Turbine/Turboprop)SDR DHL2008807528Skin · crackedLT ELEV UPPER SKIN CRACKED 2 INCHES AND SEVERAL FASTENERS LOOSE (STA XE 79.531) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-4-1 FIG 1 SHEET 1-2. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING AND FINGER DOUBLER BOTH FMay 11, 2008 · N807DH · Doug DC873F · Elevator, Plate/SkinSDR DHL2008807523Skin · canningRT RUDDER SKIN OIL CANNING (STA ZR 136.000 - 125.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING AND BONDED DOUBLER BOTH FROM AL2024T3 0.016" IAW SRM 55-6-1 FMay 9, 2008 · N807DH · Doug DC873F · Rudder StructureSDR DHL2008807513Stiffener · crackedRUDDER INTERNAL STRUCTURE STIFFENER CRACKED 1.500 INCH STA ZR 162.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW STIFFENER IAW SRM 51-1-21.May 9, 2008 · N807DH · Doug DC873F · Rudder StructureSDR DHL2008807512Stiffener · crackedRUDDER INTERNAL STRUCTURE STIFFENER CRACKED 1.500 INCH STA ZR 105.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW STIFFENER IAW SRM 51-1-21.May 9, 2008 · N807DH · Doug DC873F · Rudder StructureSDR DHL2008807521Fitting · crackedMAIN CARGO COMPT FRAME FITTING CRACKED 3 INCHES STA 857.125 L-19R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20DMay 9, 2008 · N807DH · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS08852233Skin · damagedA/C IS OOS DUE TO FUSELAGE DAMAGE CAUSED BY OTHER CARRIER'S BAGGAGE CART. REPAIRED PER UPS EO DC8-5330-29309-A.May 9, 2008 · N808UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2008807511Panel · delaminatedWING TO FUS LWR PANEL NR 732 INTERNAL SKIN DELAMINATED (STA 980.000 - 1050.000). REMOVED WING TO FUS LWR PANEL NR 732 IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL IAW SRM 51-3-0.May 9, 2008 · N807DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2008807527None · noneREMOVED AND REPLACED EXISTING REPAIR AT FUSELAGE STA 320 LT SIDE L-28L WITH PERMANENT TYPE REPAIR PER SRM. INDICATE TYPE OF REPAIR, RE-INSPECTION INTERVAL AND NEXT REQUIRED INSPECTION (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1,4. REMay 8, 2008 · N807DH · Doug DC873F · Standard Practices/StructuresSDR DHL2008807536Skin · corrodedFUSELAGE EXTERNAL SKIN CORRODED (STA 665.000 - 680.000, L-35L - L-36) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1-4. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. FABRICATED REPAIR DOUBLER (AL707May 8, 2008 · N807DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2008807532Cowl Door · dentedNR 3 ENG RT COWL DOORS EXTERIOR SHOWS TWO DENTS AT 5 O'CLOCK POS STA YN 160.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-2-8 PAR 17 FIG 8, TR NR 71-44 DATED 11-20-07. CUT OUT DAMAGED SECTION IAW SRM 71-2-8 PAR 17 PG 29 FIG 8 TR NR 71-44. FABRICATEDMay 8, 2008 · N807DH · Doug DC873F · Nacelle/Pylon, Main FrameSDR DHL2008807535Door Frame · cracked"D" CARGO DOOR AFT LWR JAMB CORNER WITH CRACKS ON IT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2005-18-07, S/B DC8 53-078, DOUGLAS DWG SR08530019, 5750776. REMOVED PARTS TO GAIN ACCESS IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED EDDY CURRENT INSP OF EXT SKMay 7, 2008 · N807DH · Doug DC873F · Fuselage Main, StructureSDR DHL2008807516Angle · crackedRT MLG W/W ZEE ANGLE CRACKED 1 INCH STA XCW -3.000. REMOVED CRACKED ZEE ANGLE IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ZEE ANGLE IAW SRM 51-1-21.May 7, 2008 · N807DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2008807534Door Frame · cracked"D" CARGO DOOR JAMB FWD LWR CORNERS CRACKED (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2005-18-07, S/B DC8 53-078, DOUGLAS DWG SR08530019, 5750776. REMOVED PARTS TO GIVE ACCESS IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED EDDY CURRENT INSPECTION OF EXT SKIN, IMay 7, 2008 · N807DH · Doug DC873F · Fuselage Main, StructureSDR IXXA080019OLanding Gear · malfunctionedDURING CLIMB-OUT FROM KTOL LANDING GEAR WOULD NOT RETRACT. THE CREW GOT A INFLIGHT INDICATION OF MECHANICAL AND ELECTRICAL GROUND SHIFT FAILURE. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE RAISED THE AIRCRAFT OFF THE GROUND AND PERFORMay 7, 2008 · N604BX · Doug DC873F · Landing Gear Retraction/Extension SystemSDR IXXA08SMN185SFloor Panel · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FLOOR PANEL WITH CORROSION AT STATION 1425.000 RIGHT BOTTOM LINE 50. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED DOMay 7, 2008 · N602AL · Doug DC873F · Fuselage Floor PanelSDR DHL2008807529Doubler · crackedFUS NOSE SECTION ACCESS DOOR NR 2 INTERNAL DOUBLER CRACKED AND BROKEN (STA -156.000 - -165.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-29-08, EVA D853-00071 REV IR DATED 05-02-08. REMOVED CRACKED INTERNAL DOUBLER IAW SRM 51-1-21. May 6, 2008 · N807DH · Doug DC873F · DoorsSDR DHL2008807514Fitting · crackedRT WING T/E FITTING CRACKED AT STA XRS 421.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE).May 6, 2008 · N807DH · Doug DC873F · Wing, Attach FittingsSDR DHL2008807531Floorbeam · damagedMAIN CARGO COMPT FLOORBEAM HAS A MISDRILLED HOLE, STA 980.000 RBL 32 1/4 INCHES (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 045-29-08, EVA D853-00070 REV IR DATED 05-01-08, DWG AF56-53-101 REV IR DATED 04-28-08. REMOVED FASTENERS IAW SRMMay 6, 2008 · N807DH · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2008807533Structure · misrepaired"A" CARGO DOOR FWD LWR JAMB CORNER REPAIR NOT IN ACCORDANCE WITH DRAWING NR SR08530019 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2005-18-07, S/B DC8 53-078, DOUGLAS DWG SR08530019 S750776. REMOVED REPAIR NOT ACCORDING TO DOUGLAS DWG SR08530019 IAW SRM 51-May 6, 2008 · N807DH · Doug DC873F · Cargo/Baggage DoorsSDR DHL2008807537Cowl Door · dentedNR 3 ENG RT COWL DOORS EXTERIOR SHOW 2 DENTS AT 5 O'CLOCK POS STA YN 192.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-2-8 PAR 16 FIG 6, TR NR 71-44 DATED 11-20-07. CUT OUT CORE AND DAMAGED EXTERNAL SKIN IAW SRM 71-2-8 PAR 16 FIG 6, TR NR 71-44. FABMay 6, 2008 · N807DH · Doug DC873F · Nacelle/Pylon, Main FrameSDR DHL2008807517Bracket · crackedNR 4 ALT TANK BOOSTER PUMP BRACKET CRACKED STA XW 415.000 S-59. REMOVED AND REPLACED CRACKED BOOSTER PUMP BRACKET AT NR 4 ALT TANK STA XW 415.000 S-59 IAW SRM 51-1-20D. REFER TO JC BZ5R28338 FOR LEAK CHECK.May 6, 2008 · N807DH · Doug DC873F · Wing, Attach FittingsSDR UPS08852248Angle · crackedINSPECTION TYPE:C3 NR 1 STUBWING INBOARD WEB "L" ANGLE CRACKED IN LOWER RADIUS. FABRICATED AND REPLACED NR 1 STUBWING INBOARD WEB L-ANGLE IAW SRM 51- 01-20D, SRM 51-03-00 AND SRM 51-1-21.May 6, 2008 · N894UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS08852177Battery · dischargedEMERGENCY EXIT LIGHTS DO NOT TEST. EMERGENCY EXIT LIGHTING BATTERY AND RELAY UNIT REPLACED AND TESTED SERVICEABLE IAW DC8 33-50-01-2-4.May 6, 2008 · N801UP · Doug DC873F · Emergency LightingSDR IXXA080018OMechanism · out of adjustDURING CLIMB-OUT FROM KTOL, THE CREW WAS UNABLE TO RAISE NOSE LANDING GEAR NORMALLY AFTER TAKEOFF. THE CREW ACCOMPLISHED COM PROCEDURE'S, USING THE HANDLE LATCH FLIGHT RELEASE THE NOSE GEAR CAME UP AND LOCKED. WHEN THE GEAR WAS BEING RAISED THE CREW HEARD A May 6, 2008 · N604BX · Doug DC873F · Landing Gear Door Retract SectionSDR DHL2008807515Door Frame · crackedLT MLG DOOR JAMB ZEE CRACKED STA 880.000. REMOVED CRACKED JAMB ZEE IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW JAMB ZEE IAW SRM 51-1-21.May 5, 2008 · N807DH · Doug DC873F · Fuselage Main, StructureSDR UPS08852249Fitting · crackedINSPECTION TYPE:C3 TAIL 62 COMPT POGO STICK FITTING CRACKED AT FWD END. REPLACED POGO STICK SUPPORT FITTING IN 62 COMPT IAW SRM 51-03-00, SRM 51-01-21, SRM 51-01-24-0 AND SRM 51-03-01-0.May 5, 2008 · N894UP · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2008807524Skin · misrepairedREMOVED AND REPLACED EXISTING REPAIR AT FUSELAGE STA 420 LT SIDE L-27L TO L-28L WITH PERMANENT TYPE REPAIR PER SRM, INDICATE TYPE OF REPAIR REINSPECTION INTERVAL AND NEXT REQUIRED INSPECTION (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1-May 4, 2008 · N807DH · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS08852164Door · bindingLT OVERWING EMERGENCY EXIT DOOR BINDING. LUBRICATED SEAL AND ALL MOVING PARTS IAW MM 12-80-00. OPS CHECK GOOD.May 3, 2008 · N805UP · Doug DC873F · Emergency ExitsSDR DHL2008807509Stringer Splice · crackedFWD CARGO COMPT SPLICE FITTING CRACKED 2 INCHES (STA 440.000 - 460.000, L-31R). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, May 2, 2008 · N807DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS08852167Slide · inoperativeWITH MAIN DOOR SHUT AND SLIDE ARMED, DOOR WAS OPENED AND SAFETY WIRE REMOVED FROM SLIDE HOUSING. REMOVED AND REINSTALLED MAIN CABIN DOOR ESCAPE SLIDE IAW AMM 25-60-01-2. INSTALLATION CHECK WAS GOOD.May 2, 2008 · N851UP · Doug DC873F · Escape SlideSDR DHL2008807522None · noneREMOVE AND REPLACE EXISTING REPAIR AT FUSELAGE STA 1260 LONGERON 31L TO 29L WITH A PERMANENT TYPE REPAIR PER SRM OR APPROVED DATA. INDICATE TYPE OF REPAIR, REINSPECTION INTERVAL AND NEXT REQUIRED INSPECTION (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2May 1, 2008 · N807DH · Doug DC873F · Standard Practices/StructuresSDR DHL2008807520Fitting · crackedMAIN CARGO COMPT FRAME FITTING CRACKED 1.250 INCH STA 834.500 L-18R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-2May 1, 2008 · N807DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2008807519Fitting · crackedMAIN CARGO COMPT FRAME FITTING CRACKED 2 INCH STA 759.000 L-18L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED FITTING IAW SRM 51-1-20D, SRM May 1, 2008 · N807DH · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS08852257Seat Track · corrodedINSPECTION TYPE:C3 CORROSION, MISSING BOLTS ON SEAT TRACK SPLICE IN A-PIT CEILING,STA 130, RBL 30. FABBED AND REPLACED SEAT TRACK SPLICE AT STA 130 AND RBL 30 IAW SRM 51 -03-00, SRM 53-02-00 FIG 1F, SRM 53-02-03 FIG 6A.May 1, 2008 · N894UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS08852178Battery Pack · dischargedEMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-00. OPS CHECKED OK.May 1, 2008 · N810UP · Doug DC873F · Emergency Lighting
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