Boeing 767-34AF

Service difficulty reports · 6,321

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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 = '76734AF'
  ORDER BY difficulty_date DESC"

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SDR IPXA10658199Floor Panel · damagedINSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 372 TO 412, LBL 55 TO LBL 77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658198Floor Panel · damagedINSPECTION TYPE:7C, MCD FLOOR PANEL FPIMD DAMAGED AT STN 654+22 TO 690, R11 TO R33. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658197Floor Panel · damagedINSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 833 TO 930, L11 TO L33. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658196Floor Panel · damagedINSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 654+22 TO 690, L33 TO L55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658159Stiffener · crackedINSPECTION TYPE:C, AV COMPT STA 246 FWD RBL 10" CABIN FLOOR STIFFENER FOUND CRACKED. AV COMPT STA 246 FWD RBL 10" CABIN FLOOR STIFFENER REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 45.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA10658157Stiffener · crackedINSPECTION TYPE: 7C, AV COMPT STA 246 AFT LBL 50 CABIN FLOOR STIFFENER FOUND CRACKED. AV COMPT STA 246 AFT LBL 50" CABIN FLOOR STIFFENER REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 45.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA10658126Floor Support · crackedSTA 246 CABIN FLOOR STRUCTURE ATT CLIP FOUND CRACKED JUST AT RBL10". AV COMPT STA 246 CABIN FLOOR STRUCTURE ATTACH CLIP AT RBL10" REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 45.Jan 9, 2010 · N314UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA10658113Skin · misrepairedSURVEY SEQUENCE NR 314-F1-06 BULK CARGO DOOR FWD LWR STA1423.5 TO 1431 THE EXISTING REPAIR DOES NOT CORRELATED TO A SRM DUE NO CUTOUT FOUND. FX SURVEY SEQUENCE NR 314-F1-06 BULK CARGO DOOR FWD LWR EDGE AT STA 1423.5 TO 1431 AREA SKIN REPAIRED IAW RS R52-36-36Jan 9, 2010 · N314UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA10658112Skin · misrepairedFX - SURVEY SEQUENCE NR 314-F1-04 STA382 TO 398 BETWEEN STR33L TO 35L THE EXISTING REPAIR NOT CORRELATE TO SRM DUE TOO CLOSE OF 314-F1-03 EXISTING REPAIR DOUBLER. FX SURVEY SEQUENCE NR 314-F1-04 STA382 TO 398 BTN STR33L-35L SKIN REPAIRED IAW RS R53-11-36575 OJan 9, 2010 · N314UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA10658111Skin · misrepairedSURVEY SEQUENCE NR 314-F1-03 STA 362 TO 374 BETWEEN STR31L AND 33L EXISTING REPAIR NOT CORRELATED TO SRM DUE TOO CLOSE OF 314-F1-04 EXISTING REPAIR DOUBLER. FX SURVEY SEQUENCE NR 314-F1-03 STA362 TO 374 BTN STR31L-33L SKIN REPAIRED IAW RS R53-11-36575 ORG MATJan 9, 2010 · N314UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA10658110Latch · faultedCLIMBING THRU 1000 FT ON DEPARTURE FWD CARGO EICAS MSG WITH LIGHT ON OVERHEAD PANEL ILLUMINATED. TS IAW FIM 52-71-00 PG 1. PSEU CHECK OF FWD BITE SHOWED DOOR LATCHED FAULT OF SWITCH 893. TARGET TESTS GOOD, CHECK PROX SENSOR GAP IAW MM 52-71-02-2, CK NORMAL. OJan 8, 2010 · N334UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA10658109Spar · crackedRT WING L/E LES675 FIXED FAIRING SUPPORT RIB AFT FRONT SPAR ANGLE FOUND CRACKED. RT WING L/E LES675 FIXED FAIRING SUPPORT RIB AFT FRONT SPAR ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 45.Jan 8, 2010 · N314UP · Boeing 76734AF · Wing SparSDR IPXA10658082Skin · delaminatedINSPECTION TYPE:SPV-RT WING INBD AFT FLAP LOWER SURFACE INBD T/E FOUND DELAMINATED ON THE EXISTING REPAIR PATCH OTBD EDGE. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10 REPAIR 4, FIG 202, SHEET 1 REV 45.Jan 7, 2010 · N314UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10658081Support Fitting · crackedINSPECTION TYPE:SPV-RT WING INBD MAIN FLAP, INBD AFT FLAP SUPPORT FITTING FOUND CRACKED. RT INBD MAIN FLAP AFT FLAP SUPPORT FITTING REPAIRED IAW SRM 57-53-02-2R1 FIG201, REV45. INBD FLANGE CRACK LENGTH 1.25". OTBD FLANGE CRACK LENGTH 1.5" BOTH INBD & OTBD CUJan 7, 2010 · N314UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10658074Attach Fitting · crackedINSPECTION TYPE:C-AFT CARGO STA 1087 FWD PARTITION BELOW FLOOR LBL 25 CLIP FOUND CRACKED. AFT CARGO STA 1087 LBL 25 FWD PARTITION BELOW FLOOR ATTACH CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV45.Jan 6, 2010 · N314UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA10658073Attach Fitting · crackedINSPECTION TYPE:SPV AFT CARGO STA 1087 FWD PARTITION BELOW FLOOR RBL 25 CLIP FOUND CRACKED. AFT CARGO STA 1087 RBL 25 FWD PARTITION BELOW FLOOR ATTACH CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV45.Jan 6, 2010 · N314UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA10658072Skin · crackedINSPECTION TYPE:C-RT WING NR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED RT WING NR 9 SLAT INBD AREA AT OSS573.125 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201, REV45. CRACK LENGTH IS 0.125" DAMAGED CUTOUT IS 9" X 7.125" THIS REPAIR IS CLASSIFIED AS Jan 6, 2010 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658071Skin · crackedINSPECTION TYPE:SPV-LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT OTBD AREA AT OSS641.5 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201, REV 45. CRACK LENGTH IS 0.125" DAMAGED CUTOUT IS 8.875" X 7.5" THIS REPAIR IS CLASSIFIED ASJan 6, 2010 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658070Skin · crackedINSPECTION TYPE:SPV-LT WING NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT INBD AREA AT OSS573.25 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201 REV 45. CRACK LENGTH IS 0.25" DAMAGED CUTOUT IS 8.875" X 7.25" THIS REPAIR IS CLASSIFIEDJan 6, 2010 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658069Skin · crackedINSPECTION TYPE:SPV-LT WING NR 3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT O/B AREA AT OSS792.1 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, REV 45. CRACK LENGTH IS 0.090" DAMAGED CUTOUT IS 8.875" X 7.25" THIS REPAIR IS CLASSIFIED AJan 6, 2010 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658068Skin · crackedINSP TYPE:SPV-LT WING NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT INBD AREA AT OSS724.61 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201 REV45. CRACK LENGTH IS 0.125" DAMAGED CUTOUT IS 8.875" X 7.125" THIS REPAIR IS CLASSIFIED AS A MAJan 6, 2010 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658067Skin · crackedINSPECTION TYPE:SPV-RT WING NR 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT OTBD AREA AT OSS792.1 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG201, REV45. CRACK LENGTH IS 0.100" DAMAGED CUTOUT IS 8.875" X 7.25" THIS REPAIR IS CLASSIFIED AJan 6, 2010 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658066Skin · crackedINSP TYPE:SPV- RT WING NR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT OTBD AREA AT OSS641.6 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201 REV 45. CRACK LENGTH IS 0.160" DAMAGED CUTOUT IS 8.875" X 7.25" THIS REPAIR IS CLASSIFIED AS A MAJJan 6, 2010 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658065Skin · crackedINSPECTION TYPE:C - RT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED RT NR 10 SLAT INBD AREA AT OSS724.35 NOSE SKIN REPAIRED AS IAW SRM 57-43-01-2R2 FIG201 REV45 ORG MATL IS CLAD7075T6-0.063" CRACK LENGTH IS 0.125" DAMAGED CUTOUT IS 8.875" X 7.12Jan 6, 2010 · N314UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658061Structure · damagedNR4 L/E SLAT HAS T/E DAMAGE APPROX. 1"X1". REPAIRED IAW EO B767-5750-36154-A.Jan 3, 2010 · N309UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658064Sensing Element · malfunctionedDIV - RT BLEED DUCT LEAK LIGHT, EICAS MESSAGE IN FLIGHT. R & R ELEMENT (TS216) IAW MM 26-18-01-4. ADJ/TEST IAW MM 26-18-01-5.Dec 31, 2009 · N327UP · Boeing 76734AF · Overheat DetectionSDR IPXA10658089Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL AT STN 873-932 R77 TO R88 FOUND DAMAGED. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 30, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658094Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STN 1370-1480 R33 TO R55. FLOOR PANEL FABRICATED EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 29, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658093Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL AT STN 1480-1598 L11 TO R11 FOUND DAMAGED. FLOOR PANEL FABRICATED, EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 29, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658092Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL AT STN 1480-1598 L33 TO L55 FOUND DAMAGED. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 29, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658091Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STN 1480-1598 R33 TO R55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 29, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658090Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STN 412-540 L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 29, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658088Floor Panel · damagedINSPECTION TYPE: 7C, MCD FLOOR PANEL FOUND DAMAGE AT STN 1197+22 - 1207 L55 TO L77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 29, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658087Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGED AT STN 1197+22 - 1207, R55 TO R77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 29, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658086Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGED AT STN 1114 TO 1197+22 R55 TO R77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 29, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658085Floorboard · puncturedINSPECTION TYPE:7C DMI NR D415075 POSITION 5 HAS A 1/2" HOLE IN THE CENTER FLOORBOARD. FLOORBOARD FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 27, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658084Floor Panel · puncturedINSPECTION TYPE:7C DMI NR D415072 POSITION 11R MCD FLOOR HAS A 3/16" HOLE. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 27, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658083Floor Panel · puncturedINSPECTION TYPE:7C DMI NR D415073 POSITION 7R MCD HAS 2 HOLES, ONE 3/16" AND THE OTHER 1/2". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Dec 27, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09658017Cover · tornCREW ENTRY DOOR IS DIFFICULT TO OPEN. FOUND INGRESS/RE ENTRY ROPE COVER TORN FROM CHANNEL CAUSING DOOR TO BIND. ACCOMP EO B767-2520-35992. SECURED DOOR INGRESS ROPE COVER IAW EO DEFERRED FOR PERM REPAIR.Dec 15, 2009 · N329UP · Boeing 76734AF · Emergency EquipmentSDR IPXA09658005Socket · inoperativeEXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED SOCKET ASSY IAW 33-51-16-2. OPS CKS GOOD.Dec 13, 2009 · N332UP · Boeing 76734AF · Emergency LightingSDR IPXA09657984Escape Rope · tornESCAPE ROPE JAMMED IN L1 DOOR ROLLERS. MX PERFORMED TEMP REPAIR ON THE ROPE COVER PER AN EO D414512 ASSIGNED. L1 DOOR ESCAPE ROPE COVER REPLACED IAW MM 25-20-00-2.Dec 6, 2009 · N329UP · Boeing 76734AF · Emergency EquipmentSDR IPXA09657961Floor Panel · damagedINSPECTION TYPE:N/A FLOOR PANEL AT POS 10/11 CENTER DAMAGED. FABRICATED FLOOR PANEL IAW EO B767-5320-9693-F.Nov 30, 2009 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657960Floor Panel · damagedINSPECTION TYPE:N/A DAMAGE TO FLOOR PANEL AT 7 RT REF D412512 EDGE BAND DAMAGE. REPLACED FLOOR PANEL PER EO B767-5320-9693-F.Nov 29, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657964Control Panel · defectiveINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED & REPLACED OVERHEAD EMERGENCY LIGHT CONTROL PANEL. OPS CHECKED GOOD PER MM 33-54-08-4.Nov 26, 2009 · N314UP · Boeing 76734AF · Emergency LightingSDR IPXA10659479Floor Panel · crackedREF D413411, 4 IN CRACK/ DENT IN MAIN CARGO FLOOR POSITION 8R OTBD PANE PANEL. STA835 RBL85. ACCOMPLISHED MAJOR REPAIR IAW EO B767-5320-9693-G, REF N/R 398499.Nov 21, 2009 · N317UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659478Floor Panel · damagedREF D413410, .5 IN X .5 IN IN MAIN CARGO FLOOR PANEL AT POSITION 7R STA 650, RBL 63. ACCOMPLISHED MAJOR REPAIR IAW EO B767-5320-9693-G, REF NR 398499.Nov 21, 2009 · N317UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659477Floor Panel · damagedREF D413409, 2 EA 1 IN X 1 IN HOLES IN MAIN CARGO FLOOR PANEL AT POSITION 7R. STA 840 RBL 85 AND STA 870 RBL 85. PERFORMED MAJOR REPAIR IAW EO B767-5320-9693-G. REF NR 398500.Nov 21, 2009 · N317UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657947Floor Panel · damagedMCD FLOOR PANEL DAMAGED. REPAIRED PER EO B767-53200-9693-F.Nov 17, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657953Panel · delaminatedVERTICAL STAB AREA OF DELAMINATION, LEFT SIDE, FSS 195.39. REMOVED, REPAIRED AND INSTALLED PER SRM 51-40-02-OG, AND BOEING DWG 175T0000.Nov 11, 2009 · N320UP · Boeing 76734AF · Vertical Stabilizer, Plate/SkinSDR IPXA09657910Wedge · damagedLEFT O/B FLAP T/E WEDGE DAMAGED. REPAIRED PER EO B767-5750-35546-A.Nov 9, 2009 · N311UP · Boeing 76734AF · Trailing Edge Flaps
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