Douglas DC-8-71F

Service difficulty reports · 8,938

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC871F'
  ORDER BY difficulty_date DESC"

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SDR IXXA05SMN86SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, MLG W/W FITTING FRAME CORRODED, STA 879.375 AND L-24. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-0 FIG. 8, EO SEMAN NR 2005843 DATE 06-23-05. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17, 18. FOUND OUT OF LIMITS IAW DC-8 SJun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA05SMN85SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MLG W/W FITTING CRACKED 4 INCHES, STA 940.000, RBL 5 INCHES. REMOVED CRACKED FITTING IAW SRM 51-1-20D. FABRICATED NEW FITTING IAW DWG NR 3643758 (ALCLAD 7075 T6 51). PERFORMED HEAT TREATMENT IAW SRM 51-1-11. PERFORMED NDTJun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA05SMN84SFitting · corrodedDURING C CHECK INSPECT, MLG W/W FRAME FITTING CORRODED, STA 960.000 L-24. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-1-0 PG 1, DC-8 SRM 53-2-0 FIG. 8 (SHEET 1), EO SEMAN # 2005845 DATE 06-27-05. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PG 17, 18, FOUND OUT OF LIMITJun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA05SMN83SClip · crackedDURING ROUTINE C-CHECK INSPECTION, MLG W/W CLIP CRACKED 5 INCHES , STA 857.725 AND RBL 46 INCHES. REMOVED CRACKED FITTING IAW SRM 51-1-21 PAGE 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9.Jun 23, 2005 · N822BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA05SMN82SSkin · damagedDURING C CHECK INSPECTION, EXTERNAL DOUBLER LEFT AFT FUSELAGE BELOW L-2 DOOR. REPAIR FAILED ASSESSMENT DOUBLER NOT THICK ENOUGH, SIDES 2 UPPER AND 4 LOWER EXCEED AVERAGE RIVET SPACING SIDES 1 FWD, 2 UPPER, 3 AFT, 4 LOWER EXCEED MAX RIVET SPACING. UPGRADE REPAJun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN81SSkin · damagedDURING C CHECK INSPECT, EXTERNAL DOUBLER UAL DRAIN DOUBLER, RT AFT FUSELAGE SIDE. REPAIR MUST BE UPGRADED, REPAIR MUST HAVE 3 ROWS OF RIVETS STA FS 1693, L-30.5R (REF.- 822BX-R71). PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-1 FIG 7, EO SEMAN NR 2005871 DATE 06-Jun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN80SSkin · damagedDURING C CHECK INSPECT, EXTERNAL DOUBLER SKIN SPLICE FROM LONG 28 LT TO 28 RT; AFT EDGE RIVET SPACING EXCEEDS SRM LIMITS AFT SKIN SPLICE NON DOUG SRM UPGRADE REPAIR TO CONFORM TO DACO DC-8 SRM; FS 1696 L-36. (REF. 822BX-R68). PERFORMED MAJOR REPAIR IAW DC-8 SJun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN79SSkin · damagedDURING C CHECK INSPECT, EXT DOUBLER LT AFT FUSELAGE MUST BE UPGRADED REPAIR MUST HAVE THREE ROWS OF RIVETS, STA FS 1695.000 L-30.5L (REF. 822BX-R67). PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-1 FIG 7, EO SEMAN NR 2005872 DATE 06-13-05. REMOVED EXISTING REPAIR Jun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN78SDoor · wornDURING C CHECK INSPECT, EXTERNAL FUS "C" BELLY DOOR LWR PART WORN. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05283 DATE 07-06-05, SEMAN DWG ED 4002 DATE 07-01-05, EO SEMAN NR 2005971 DATE 07-06-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM Jun 23, 2005 · N822BX · Doug DC871F · Cargo/Baggage DoorsSDR IXXA05SMN77SSkin · crackedDURING C CHECK INSPECT, RT WING INBD OUTER L/E LWR SKIN CRACKED 1/2", XFS 591.250. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05270 DATE 06-29-05, SEMAN DWG ED 4017 DATE 06-28-05, EO SEMAN NR 2005969 DATE 06-29-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 PJun 23, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN76SSkin · inadequateDURING C CHECK INSPECT, EXTERNAL DOUBLER FWD FUSELAGE BELLY SKIN MUST BE UPGRADED, REPAIR MUST HAVE THREE ROWS OF RIVETS, STA FS 543.000 L-3.75R (REF. 822BX-R50). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05271 DATE 06-29-05, SEMAN DWG ED 3998 DATE 06-22-Jun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN75SSkin · damagedDURING C CHECK INSPECTION, EXTERNAL DOUBLER ON WINDOW BELT AREA ABOVE C-PIT BASKET DOOR OLD UNITED AIRLINES INSUFFICIENT SIZE OF LOWER EXTENSION UPGRADE DOUBLER TO CONFORM TO THE CURRENT DACO DC-8 SRM REQUIREMENTS (REF. 822BX-R59), STA FS 1400.000 L-15.5R. PEJun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN74SSkin · damagedDURING ROUTINE C CHECK INSPECTION, RT WING INBD L/E UPPER SKIN NON STANDARD REPAIR BETWEEN STA XFS 113.750 - XF 120.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG. 2J, EO SEMAN NR 2005970 DATE 06-23-05. REMOVED DAMAGED PLATING IAW DC-8 SRM 57-2-1 FIG. 2Jun 23, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN73SSkin · damagedDURING ROUTINE C CHECK INSPECTION, EXTERNAL DOUBLER ON FWD FUSELAGE BELLY SKIN, MUST BE UPGRADED, REPAIR MUST HAVE THREE ROWS OF RIVETS AT STA FS 1135.000 L-35.5R. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-1 FIG 7 EO SEMAN Nº 2005870 DATE 06-13-05. REMOVED EXIJun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN72SSkin · damagedDURING C CHECK INSPECTION, EXTERNAL DOUBLER ON FWD FUSELAGE BELLY SKIN MUST BE UPGRADED, REPAIR MUST HAVE THREE ROWS OF RIVETS, STA FS 543.000 L-3.75R (REF. 822BX-R50). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05271 DATE 06-29-05, SEMAN DWG ED 3998 DATE Jun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN71SSkin · damagedDURING ROUTINE C CHECK INSPECTION, EXTERNAL DOUBLER ON FWD FUSELAGE BELLY SKIN, MUST BE UPGRADED, REPAIR MUST HAVE THREE ROWS OF RIVETS AT STA FS 401.000 L-35.75 (REF. 822BX-R47). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05271 DATE 06-29-05, SEMAN DWG EDJun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN70SSkin · damagedDURING C CHECK INSPECT, EXT DOUBLER FWD LWR BASKET DOOR OPENING FWD EDGE REPAIR LACKS ENOUGH RIVETS ALL SIDES OF CUT OUT STA FS 279.000 L-31.5R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05270 DATE 06-29-05, SEMAN DWG ED 3995 DATE 06-25-05, EO SEMAN # 2005Jun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN69SSkin · damagedDURING C CHECK INSPECT, EXTERNAL DOUBLER LWR FUSELAGE, STA FS 238.000, L-31R REPAIR EXCEEDS MAX RIVETS SPACING ON SIDES 1 FWD, 2 UPPER AND 4 LOWER ADD ADDITIONAL RIVETS OR REWORK SIDES 1,2 AND 4 TO BRING INTO LIMITS PER SRM BELOW 1.400” SPACING (REF. 822BX-R35Jun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN68SSkin · damagedDURING C CHECK INSPECT, UAL DRAIN DOUBLER ON FWD LOWER FUSELAGE, STA FS 224.000, L-35.75R REPAIR MUST BE UPGRADED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05258 DATE 06-24-05, SEMAN DWG ED 3994 DATE 06-22-05, EO SEMAN NR 2005832 DATE 06-24-05. REMOVED EJun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN67SSkin · damagedDURING C CHECK INSPECT, EXTERNAL DOUBLER ON FWD LOWER FUSELAGE, STA FS 173, L-35.5R REPAIR MUST BE UPGRADED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05271 DATE 06-29-05, SEMAN DWG ED 3993 DATE 06-22-05, EO SEMAN NR 2005862 DATE 06-29-05. REMOVED EXISTINJun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN66SSkin · damagedDURING C CHECK INSPECT, EXTERNAL DOUBLER FWD LOWER FUSELAGE, STA FS 114.000, L-35.5L MUST BE UPGRADED. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-1 FIG. 7, EO SEMAN NR 2005869 DATE 06-13-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PAGE 1. TRIMMED OJun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN65SSkin · damagedDURING ROUTINE C CHECK INSPECT, UAL DRAIN DOUBLER AT FWD LWR FUSELAGE FS 77, L-35.5R MUST BE UPGRADED, REPAIR MUST HAVE THREE ROWS OF RIVETS (REF. 822BX-R29). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05258 DATE 06-24-05, SEMAN DWG ED 3992 DATE 06-21-05, Jun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN63SSkin · damagedDURING C CHECK INSPECT, EXTERNAL DOUBLER ON AFT LOWER FUSELAGE, STA FS 1540.000, L-35.5L REPAIR MUST BE UPGRADED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05271 DATE 06-29-05, SEMAN DWG ED 4001 DATE 06-22-05, EO SEMAN NR 2005903 DATE 06-29-05. REMOVED EXJun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN61SAntenna · deterioratedDURING C CHECK INSPECT, RT AFT FUS STA FS 1346.000, L-35.5R. ONLY 2 ROWS OF RIVETS IN OLD ANTENNA DOUBLER ADD 3RD ROWS OF RIVETS UTILIZING SRM RIVET SPACING OR UPGRADE REPAIR DOUBLER, STA 1346.000 L-35.5R (REF 822BX-R14). PERFORMED MAJOR REPAIR IAW DC-8 SRM 5Jun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN60SAntenna · deterioratedDURING C CHECK INSPECT, RT AFT FUS AFT FS 1290.000, L-35.5R; ONLY 2 ROWS OF RIVETS IN OLD OMEGA ANTENNA DOUBLER ADD THIRD ROW OF RIVETS UTILIZING SRM RIVET SPACING OR UPGRADE REPAIR DOUBLER (REF 822BX-R13). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05259 DJun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN59SSkin · deterioratedDURING C CHECK INSPECT, REPAIR ON UAL DRAIN DOUBLER MUST BE UPGRADED. REPAIR MUST HAVE 3 ROWS OF RIVETS STA 1270.000, L-35.5L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05259 DATE 06-24-05, SEMAN DWG ED 4000 DATE 06-20-05, EO SEMAN # 2005902 DATE 06-24-05.Jun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN58SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, EXTERNAL DOUBLER/TRIPLER FWD BASKET DOOR FWD LEFT UPPER CORNER. REPAIR DOES NOT CONFORM TO EVA 33-2614 USED FOR INSTALLATION. EVALUATE REPAIR FOR SRM CONFORMITY (53-2-0 FIG. 19, SHEET 1). PERFORMED MAJOR REPAIR IAW FAA FORM Jun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN57SSkin · corrodedDURING C CHECK INSPEC, LWR FWD FUS BELLY AFT NLG W/W SIDE 2 AND 4 EXCEED AVG PITCH, SIDE 2 AND 3 EXCEED MAX PITCH, STA 15.000 L-36. ADD RIVETS TO BRING AVG AND MAX PITCH INTO LIMITS PER SRM OR REWORK. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-1-0 PG 1, DC-8 SRM Jun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN56SDoubler · out of limitsDURING C CHECK INSPECT, LT FWD FUS ABOVE AND AFT TURBO COMPRESSOR, SIDE 1 (FWD) BELOW, MIN EDGE DISTANCE FOR RIVETS, REPAIR DOUBLER RATIO ABOVE LIMITS TO THICK, STA FS 116.000 L-21.5L. UPGRADE REPAIR BY REPLACING EXISTING DOUBLER WITH 0.071AND ENSURE MIN EDGE Jun 23, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR U2RAM83088Fitting · corrodedLONGERON END FITTING LOCATED AT FRAME 80 AFT, L27R FOUND CORRODED BEYOND LIMITS. CLASSIFIED AS LEVEL 2 CORROSION.Jun 21, 2005 · N872SJ · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05844803Longeron · crackedINSPECTION TYPE:C-2, LONGERON 24L CRACKED ON O/B FLANGE. REMOVED AND REPLACED LONGERON 24L IAW SRM 51-3-2, 51-1-8, AND 51-1-20D.Jun 20, 2005 · N705UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA0500078OHsi · malfunctionedON TAKEOFF, NR 1 COMPASS FAILED WITH OFF FLAG IN CAPTAIN HSI. CREW RETURNED AND LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED CAPTAIN HSI PER ALL APPLICABLE MAINTENANCE MANUALS. OPS CHECK GOOD. ACFT RETURNED TO SERVICE.Jun 9, 2005 · N820BX · Doug DC871F · Integrated Flight SystemSDR UPS05844682Doubler · delaminatedUNDER BELLY PANELS (4EA) DELAMINATED ON PREVIOUS REPAIR. LT WING TO BODY LOWER FILLET PANEL DELAMINATED. D303878 LT WING TO BODY FAIRING FILLET PANEL DELAMINATED D303879 LT WING TO BODY FAIRING FILLET PANEL DELAMINATED.Jun 9, 2005 · N708UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS05844771Fitting · crackedINSPECTION TYPE:C-2. BANANA FITTING CRACKED AT STA 340 L33R. REMOVED AND REPLACED BANANA FITTING AT STA 340 L33R IAW SRM 51-1-20D.Jun 8, 2005 · N705UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05844770Frame · corrodedINSPECTION TYPE:C-2. MAIN CARGO STA 1700 RBL 24 SEVERE CORROSION AT TOP OF FRAME ON UNDERSIDE AND CONTINUES OUTBD TO RBL48. CUT OUT DAMAGED AREA PER SRM 51-2-1 FIG 1, SHEET 7. FABRICATED REPAIR REPAIR DOUBLER AND REPAIR ANGLES IAW SRM 51-1-21 FIG 1, AND INSJun 8, 2005 · N705UP · Doug DC871F · Fuselage Main, FrameSDR UPS05844767Seat Track · corrodedINSPECTION TYPE:C-2. HEAVY CORROSION IN SEAT TRACK ALONG RBL 59 STA 375-420. REMOVED AND FABRICATED SEAT TRACK PER DWG S2400463. INSTALLED FABBED SEAT TRACK AT STA 375-420 PER SRM 53-2-3.Jun 8, 2005 · N705UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS05844766Fitting · corrodedINSPECTION TYPE:C-2. A-PIT AT STA 320 L33R, BATH TUB FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED BATH TUB FITTING AT A-PIT STA 320 L33R IAW SRM 53-2-0 FIG 1F, 51-1-20D, AND 51-1-21.Jun 8, 2005 · N705UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05844763Seat Track · corrodedC2 SEAT TRACK HEAVILY CORRODED AT STA 420 LBL 25. REMOVED AND REPLACED SEAT TRACK AT STA 360-560 LBL 25 IAW SRM 51-3-0, 51-3-2, 53B-003-501.Jun 8, 2005 · N705UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS05844761Seat Track · corrodedMAIN CABIN SEAT TRACK HAS HEAVY CORROSION, STA 1480 RBL 50. REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 1460-1580 RBL 50 IAW SRM 51-3-0.Jun 8, 2005 · N705UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS05844935Fitting · crackedINSPECTION TYPE: C2, B-PIT BETWEEN STA 460-440 L28R SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING IN B-PIT AT STA 460-440, L28R IAW SRM 51-1-21D AND SRM 51-1-21Jun 7, 2005 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS05844772Skin · damagedINSPECTION TYPE:C-2. UPPER PORTION OF RUDDER ON RT SIDE JUST ABOVE LOGO, OIL CANNING OF SKIN. REMOVED AND REPLACED SKIN ON RT SIDE OF RUDDER JUST ABOVE LOGO IAW DC8 DWG 5655077 AND SRM 51-1-8, AND 51-1-21A. NO WEIGHT AND BALANCE DUE TO 1FOR 1 SKIN CHANGE.Jun 7, 2005 · N705UP · Doug DC871F · Rudder, Plate/SkinSDR UPS05844768Floor Support · crackedINSPECTION TYPE:C-2. MAIN CABIN STA 759 LBL24 UNDER SEAT TRACK. SEAT TRACK FLOOR SUPPORT FITTING CRACKED. REMOVED AND REPLACED SUPPORT FITTING AT STA 759 LBL24 IAW 51-1-20D, AND 51-3-0.Jun 7, 2005 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS05844769Fitting · corrodedINSPECTION TYPE C-2, CORNER FITTING CRACKED AND HEAVILY CORRODED, RT W/W STA 980 CEILING O/B CORNER NEXT TO L24R. REMOVED FITTING IAW SRM 51-1-20D. FABRICATED DOUBLER, REPAIR ANGLE AND FILLERS IAW SRM 53-02-00-0, INSTALLED DOUBLER REPAIR ANGLE AND FILLERS IAJun 5, 2005 · N705UP · Doug DC871F · Fuselage, Landing Gear Attach FittingsSDR UPS05844765Skin · crackedINSPECTION TYPE:C-2. LT ELEVATOR CONTROL TAB SKIN AND DOUBLER CRACKED AT INBD EYEBOLT ACCESS HOLE LWR SKIN. REMOVED AND REPLACED LT ELEVATOR CONTROL TAB ASSY PER TASK CARD 3016 STEP 13.Jun 5, 2005 · N705UP · Doug DC871F · Elevator, Plate/SkinSDR UPS05844762Rib · crackedLT HORIZ STAB L/E 2ND INBD LWR RIB REPAIR HAS DOUBLER AND TRIPLER CRACKED. REMOVED, FABRICATED, AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW SRM 55-2-0, 51-1-21, AND SRM 55-2-0 FIG 2.Jun 5, 2005 · N705UP · Doug DC871F · Horizontal Stabilizer, Spar/RibSDR UPS05844764Longeron · corrodedINSPECTION TYPE C-2, CORROSION BETWEEN TOP OF L24L AND REPAIR DOUBLER STACK IN LT W/W NEAR STA 906. REMOVED CORROSION OUT OF LIMITS IAW SRM 51-1-8 AND 53-2-0 FIG 1F. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-02-02 FIG 005 SHEET 8.Jun 3, 2005 · N705UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS05844594Battery Pack · inoperativeEMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER 33-50-01.Jun 2, 2005 · N708UP · Doug DC871F · Emergency LightingSDR UPS05844571Windshield · failedF/O'S WINDSHIELD SHATTERED WHEN TURNED ON. APPLIED SEALANT TO F/O WINDSHIELD, REF MM 56-10-02-2. D303437 CLOSEDJun 1, 2005 · N718UP · Doug DC871F · Flight Compartment WindowsSDR U2RA3056Bellcrank · disconnectedDURING INSPECTION, RT ELEVATOR GEARED TAB OUTBOARD CRANK P/N 4710542-3 FOUND DISCONNECTED FROM LINK P/N 271442-501. NOTE: AIRCRAFT IS CURRENTLY CLASSIFIED PART 91.May 26, 2005 · N872SJ · Doug DC871F · Elevator Tab Control SystemSDR UPS05844467Oxygen Mask · leakingINSPECTION TYPE:N/A F/O'S OXYGEN MASK LEAKS. REMOVED AND REPLACED F/O'S REGULATOR AND MASK PER MM CHAPT 35-10-08-2 AND CHAPT 35-10-07-4. OPS LEAK CHECK GOOD.May 15, 2005 · N755UP · Doug DC871F · Crew Oxygen System
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