# Service difficulty reports: N68061

A list on [N68061](https://openairdocs.org/aircraft/N68061.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 95 reports

- [SDR CALA2026100620138](https://openairdocs.org/sdr/CALA2026100620138.md): Light · damaged · Oct 3, 2026 · N68061 · Boeing 767424ER · Emergency Lighting
  > GENERAL VISUAL INSPECTION OF THE BE PINNACLE TOURIST SEAT PROCEDURE - SEAT MONTED - EMERGENCY LIGHTS #32F AND #44F DAMAGED REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHTS #32F AND 44F. AS REFERENCE AMM TASK 33-51-10-962-104. ITEM GOOD FOR SERVICE.
- [SDR CALA2026100620136](https://openairdocs.org/sdr/CALA2026100620136.md): First Aid Kit · open · Oct 3, 2026 · N68061 · Boeing 767424ER · Emergency Equipment
  > FIRST RESPONSE KIT (FRK) WITH MISSING SEAL REMOVED AND REPLACED FRK AS REF AMM TASK 03-25-64-210-803,ITEM GOOD FOR SERVICE.PARTS USED: 29-2560-3-0125,QTY:1
- [SDR CALA2026092919955](https://openairdocs.org/sdr/CALA2026092919955.md): Panel · missing · Sep 27, 2026 · N68061 · Boeing 767424ER · Nacelle/Pylon, Plate/Skin
  > NR 2 ENGINE HAS PYLON ACCESS PANEL 446AR MISSING. INSPECTED THE AREA FOR DAMAGE IAW AMM 05-51-59, NO DAMAGE FOUND. CDL 54BE REJECTION REPLACED THE MISSING PANEL IAW AMM 54-53-01-404-007. OK FOR SERVICE.
- [SDR CALA2026080518290](https://openairdocs.org/sdr/CALA2026080518290.md): Rib · cracked · Aug 4, 2026 · N68061 · Boeing 767424ER · Leading Edge Devices
  > LEFT WING, DURING OK TO CLOSE OF ACCESS PANEL 524AT, OBSERVED THE END RIB CRACKED AT NR 3 SLAT. OSS 684 - 043 (INBD END OF SLAT 3). REMOVED, FABRICATED, & INSTALLED THE RIB, WAS ACCOMPLISHED IAW NR 3601211.
- [SDR CALA2026080218175](https://openairdocs.org/sdr/CALA2026080218175.md): Skin · contaminated · Jul 31, 2026 · N68061 · Boeing 767424ER · Ailerons
  > DURING THERMOGRAPHIC INSPECTION AT LEFT OUTBOARD AILERON IT WAS FOUND MOISTURE INGRESSION INDICATION WS 1046.2, REMOVED THE LIQUID INGRESS ON THE LOWER SKIN OF THE OTBD AILERON RT AND REPAIRED IAW SRM 57-60-02-2R-1, FIGURE 201, DETAIL II, AND SRM 51-70-05-0G-
- [SDR CALA2026080218168](https://openairdocs.org/sdr/CALA2026080218168.md): Skin · contaminated · Jul 31, 2026 · N68061 · Boeing 767424ER · Ailerons
  > RII INSPECTION REQUIRED DURING THERMOGRAFIC INSPECTION OF AILERON RH WAS FOUND MOISTURE INGRESSION INDICATION ON WS 1075.2. REMOVED THE LIQUID INGRESS ON THE LOWER SKIN OF THE OTBD AILERON RT AND REPAIRED IAW SRM 57-60-02-2R-1, FIGURE 201, DETAIL II, AND SRM
- [SDR CALA2026080218165](https://openairdocs.org/sdr/CALA2026080218165.md): Skin · contaminated · Jul 31, 2026 · N68061 · Boeing 767424ER · Ailerons
  > DURING THERMOGRAFIC INSPECTION OF OTBD AILERON RT WAS FOUND MOISTURE INGRESSION INDICATION CLOSE TO WS 1075.2. REMOVED THE WATER INGRESS LIQUID ON THE RT OTBD AILERON AT WS 906.2, LOWER SKIN AND REPAIRED IAW SRM 57-60-02-2R-1, FIGURE 201, DETAIL II, AND SRM
- [SDR CALA2026080218163](https://openairdocs.org/sdr/CALA2026080218163.md): Skin · contaminated · Jul 31, 2026 · N68061 · Boeing 767424ER · Ailerons
  > DURING THERMOGRAFIC INSPECTION OF AILERON RH WAS FOUND MOISTURE INGRESSION INDICATION ON WS 906.2. REMOVED THE WATER INGRESS LIQUID ON THE RT OTBD AILERON AT STATION WS 906.2, LOWER SKIN AND REPAIRED IAW SRM 57-60-02-2R-1, FIGURE 201, DETAIL II, AND SRM 51-70
- [SDR CALA2026080218159](https://openairdocs.org/sdr/CALA2026080218159.md): Skin · contaminated · Jul 31, 2026 · N68061 · Boeing 767424ER · Ailerons
  > DURING THERMOGRAPHIC INSPECTION AT LEFT OUTBOARD AILERON IT WAS FOUND MOISTURE INGRESSION INDICATION AT WS 934.2. IT WAS REMOVED THE LIQUID INGRESS ON THE LOWER SKIN OF THE OUTBOARD AILERON LH AND REPAIRED AS PER SRM 57-60-02-2R-1 FIGURE 201 DETAIL II AND SRM
- [SDR CALA2026051116162](https://openairdocs.org/sdr/CALA2026051116162.md): Engine · vibration · May 7, 2026 · N68061 · Boeing 767424ER · Engine Vibration Analyzer
  > FAN VIBRATION 4.1 AT CLB THRST TO FL270. AT CRUISE VIB IS 1.0. NO AIR FRM VIB FELT. OIL TEMP AND PRESS PER CREW DEBRIEF: ALL OTHER ENGINE INDICATIONS WERE NORMAL DUE TO PILOT REPORT OF VIBRATION NOT FELT IN FLIGHT DECK, PERFORMED FIM 77-31 FAULT TREE 808. SWI
- [SDR CALA2026030214210](https://openairdocs.org/sdr/CALA2026030214210.md): Door · inflt separation · Feb 26, 2026 · N68061 · Boeing 767424ER · Cabin Cooling System
  > LEFT RAM AIR INLET DOOR ASSY FWD PIECE DEPARTED A/C. COMPOSITE PIECE MORE 15 SQUARE INCHES BUT NOT MORE THAN 150 SQUARE INCHES. PART IS ROUGHLY 17 INCH X 12 INCH.
- [SDR CALA2026020613622](https://openairdocs.org/sdr/CALA2026020613622.md): Controller · faulted · Feb 4, 2026 · N68061 · Boeing 767424ER · Pneumatic Distribution System
  > ON DESCENT, RECIEVED LT & RT PACK OFF LIGHT. ATTEMPT TO RESET FAILED. DESCENDED TO 9000 FT, DEBRIEF FROM PILOTS. DURING OCCURANCE, RT COND TEMP CONT & R SEC HX SENSOR DISPLAYED AT TOC FL320, ACCOMP SYS TEST ON RT CTC.. TEST PASSED. RT RAM INLET ACTUATOR
- [SDR CALA2025102710588](https://openairdocs.org/sdr/CALA2025102710588.md): Wire · broken · Oct 24, 2025 · N68061 · Boeing 767424ER · Hydraulic Power System Wiring
  > RIGHT ELEC HYD PUMP INOP.AS PER FIM 29-11- FAULT TREE 891, FOUND PHASE B MISSING ON CONNECTOR D486 (RT ELEC PUMP). M896. REMOVED & CHECKED FOR 115 VAC ON CONTACTS A1/B1/C1 OK. CONTINUITY FROM M896 B2 TO D486/B SHOWS OPEN CIRCUIT (NO SHORT TO GROUND). FURTH
- [SDR CALA2025082108009](https://openairdocs.org/sdr/CALA2025082108009.md): Skin · cracked · Aug 20, 2025 · N68061 · Boeing 767424ER · Leading Edge Devices
  > DURING INSPECTION AT RIGHT WING OTBD SLAT NR 11 FOUND CRACKED ON SKIN INBD NEAR ACCESS PANEL 625AT. PERFORMED PERMANENT REPAIR IAW EC/RA 5743-02012.
- [SDR CALA2025011601924](https://openairdocs.org/sdr/CALA2025011601924.md): Track · fod · Jan 13, 2025 · N68061 · Boeing 767424ER · Service Doors
  > 4R DOOR SLIDE WILL NOT ARM. INSPECTED SLIDE TRACKS AND FOUND DEBRIS. CLEANED DEBRIS AND OPS CHECK 4R DOOR. REF AMM 52-11-00. ADD 381101, U380359 AND REF AMM 25-66-01 FOR ARMING 4R DOOR SLIDE.
- [SDR CALA2024120603026](https://openairdocs.org/sdr/CALA2024120603026.md): Transducer · faulted · Dec 4, 2024 · N68061 · Boeing 767424ER · Brake Anti-Skid Section
  > ANTISKID CAUTION MSG. ANTISKID CONTROLLER, BIT TEST PASS. #7 ANTISKID XDCR SPIN TEST ROTABLE PARTS CHANGE WAS INDICATED - TT # 1527113 SN OFF 0572 STILL NEEDED FOR REPLACEMENT OF TRANSDUCER. AFTER TAKE-OFF, ANTISKID CAUTION MSG BITE CHKD ANTISKID AUTO BRAKE C
- [SDR CALA2024060701728](https://openairdocs.org/sdr/CALA2024060701728.md): Electronic Unit · intermittent · Jun 2, 2024 · N68061 · Boeing 767424ER · Trailing Edge Flap Control System
  > ON SHORT FINAL GOT A TE FLAPS ASYM EICAS TOMC LOCKS FOR REPAIR, TOMC UNLOCKS FOR UPDATING ABOVE UPDATE APPLIES TO FLAPS AT 20 DEGREES PER FIM 27-51 TASK 811, ARMED AND DEARMED ALT TE SWITCH TWICE. MOVED FLAPS FROM 30 DEGREES TO 0 DEGREES WITH C2 HYDRAULICS ONL
- [SDR CALA2023081602537](https://openairdocs.org/sdr/CALA2023081602537.md): Battery Pack · discharged · Aug 15, 2023 · N68061 · Boeing 767424ER · Emergency Lighting
  > EMER LT SYSTEM DEEP CYCLE CHECK FOUND BAT PACK EQ NO.M739 (LH STA 1360) TEST FAIL TRANSFER REF. NON-ROUTINE HX NRC WO.2019164. EMER LT BAT PACK EQ NO. M739 REPLACED AND TEST RESULT NORMAL AS PER AMM 33-51-07.
- [SDR CALA2023081602536](https://openairdocs.org/sdr/CALA2023081602536.md): Battery Pack · discharged · Aug 15, 2023 · N68061 · Boeing 767424ER · Emergency Lighting
  > EMER LT SYSTEM DEEP CYCLE CHECK FOUND BAT PACK EQ NO.M734 (RH STA 1380) TEST FAIL TRANSFER REF. NON-ROUTINE HX NRC WO.2019172 EMER LT BAT PACK EQ NO. M734 REPLACED AND TEST RESULT NORMAL AS PER AMM 33-51-07.
- [SDR CALA2023081602535](https://openairdocs.org/sdr/CALA2023081602535.md): Battery Pack · discharged · Aug 15, 2023 · N68061 · Boeing 767424ER · Emergency Lighting
  > EMER LT SYSTEM DEEP CYCLE CHECK FOUND BAT PACK EQ NO.M7236 (LH STA 1190+70) TEST FAIL TRANSFER REF. NON-ROUTINE HX NRC WO.2019143. EMER LT BAT PACK EQ NO. M7236 REPLACED AND TEST RESULT NORMAL AS PER AMM 33-51-07
- [SDR CALA2023081602534](https://openairdocs.org/sdr/CALA2023081602534.md): Battery Pack · discharged · Aug 15, 2023 · N68061 · Boeing 767424ER · Emergency Lighting
  > EMER LT SYSTEM DEEP CYCLE CHECK FOUND BAT PACK EQ NO.M737 (LH STA 980) TEST FAIL TRANSFER REF. NON-ROUTINE HX NRC WO.2019120 AND ORIGINATED BY EMP V897815 EMER LT BAT PACK EQ NO. M737 REPLACED AND TEST RESULT NORMAL AS PER AMM 33-51-07
- [SDR CALA2023081602533](https://openairdocs.org/sdr/CALA2023081602533.md): Battery Pack · discharged · Aug 15, 2023 · N68061 · Boeing 767424ER · Emergency Lighting
  > EMER LT SYSTEM DEEP CYCLE CHECK FOUND BAT PACK EQ NO.M6760 (RH STA 1190+70) TEST FAIL TRANSFER REF. NON-ROUTINE HX NRC WO.2019135 AND ORIGINATED BY EMP V897815 EMER LT BAT PACK EQ NO. M6760 REPLACED AND TEST RESULT NORMAL AS PER AMM 33-51-07 WORK ACCOMPLISHED
- [SDR CALA2023080202406](https://openairdocs.org/sdr/CALA2023080202406.md): Spar Web · cracked · Aug 2, 2023 · N68061 · Boeing 767424ER · Nacelle/Pylon, Main Frame
  > B767-06-3-7294 NO.2 PYLON MID SPAR WEB AT DISCONNECT BOX CUTOUT FOUND CRACK TRANSFER REF. NON-ROUTINE HX NRC WO.2012233 AND ORIGINATED BY EMP NO. V925649 NO.2 PYLON MID SPAR WEB REPAIRED AS PER SRM 54-55-01-2R-2 REPAIR 2 FIG 203 AND REPAIR 2 IS A CATEGORY A RE
- [SDR CALA2023080202405](https://openairdocs.org/sdr/CALA2023080202405.md): Failsafe · cracked · Aug 2, 2023 · N68061 · Boeing 767424ER · Fuselage Main, Structure
  > 1EA HOLE FOUND CRACK AT LH STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP TRANSFER REF. NON-ROUTINE HX NRC WO.2023425 AND ORIGINATED EMP V906014 LH STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP REPAIRED AS PER EA5340-01385 REV ORIG OP003 WORK ACCOMPLISHED BY MECHANIC V
- [SDR CALA2023080202403](https://openairdocs.org/sdr/CALA2023080202403.md): Tee Fitting · corroded · Aug 1, 2023 · N68061 · Boeing 767424ER · Fuselage Main, Attach Fittings
  > EA 5340-01385 REV ORIG OP 003 LH SIDE STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP T-FITTING FOUND CORROSION TRANSFER REF. NON-ROUTINE HX NRC WO.2029686 AND ORIGINATED BY EMP V906449 EA5340-01385 REV ORIG OP003 LHS STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP T-FITT
- [SDR CALA2023080202402](https://openairdocs.org/sdr/CALA2023080202402.md): Tee Fitting · corroded · Aug 1, 2023 · N68061 · Boeing 767424ER · Fuselage Main, Attach Fittings
  > EA 5340-01385 REV ORIG OP 004 RH SIDE STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP T-FITTING FOUND CORROSION TRANSFER REF. NON-ROUTINE HX NRC WO.2029680 AND ORIGINATED BY EMP V906449 EA5340-01385 REV ORIG OP 004 RHS STA955 REAR SPAR BULKHEAD FAILSAFE STRAP T-FTG
- [SDR CALA2023080202401](https://openairdocs.org/sdr/CALA2023080202401.md): Failsafe · cracked · Aug 1, 2023 · N68061 · Boeing 767424ER · Fuselage Main, Structure
  > 1EA HOLE FOUND CRACK AT RH STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP TRANSFER REF. NON-ROUTINE HX NRC WO.2023412 AND ORIGINATED EMP V906014 RH STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP REPLACED AS PER EA5340-01385 REV ORIG OP 004 WORK ACCOMPLISHED BY MECHANIC
- [SDR CALA2023073102377](https://openairdocs.org/sdr/CALA2023073102377.md): Shear Tie · corroded · Jul 29, 2023 · N68061 · Boeing 767424ER · Fuselage Internal Mounting Structure
  > BULK CARGO COMPT - BELOW FLOOR SHEAR TIE FOUND CORROSION AT STA 1417 BTN S37R-S38R (AS MARK) TRANSFER REF. NON-ROUTINE HX NRC WO.2005165 AND ORIGINATED BY EMP NO. V896820 BULK CARGO COMPT BELOW FLOOR AT STA 1417 BTN STR 37R-38R SHEAR TIE REPLACED AS PER SRM 51
- [SDR CALA2023061601874](https://openairdocs.org/sdr/CALA2023061601874.md): Filter · failed · Jun 15, 2023 · N68061 · Boeing 767424ER · Engine Fuel and Control
  > L ENG FUEL FILTER ON BOTH EICAS AND STATUS PAGE.
- [SDR CALA2023021600443](https://openairdocs.org/sdr/CALA2023021600443.md): Rvdt · none · Feb 15, 2023 · N68061 · Boeing 767* · Flight Control System
  > ON APPROACH GOT TE FLAP DISAGREE WHEN ATTEPTING TO MOVE FLAPS F ROM 1 TO 5 PERFORMED BITE OF FSEU GOT MESSAGE NUMBER27-81041 L/E OUTBD PDU RVDT REQUIRES MORE T/S PARTS USED: 64-2781-3-0320,QTY:1 76-2781-3-0173,QTY:1 T/S IRW FIM 27-51 TASK 809. FOUND FAULT
- [SDR CALA2023021400441](https://openairdocs.org/sdr/CALA2023021400441.md): Flap System · none · Feb 14, 2023 · N68061 · Boeing 767* · Trailing Flap Position Indicating System
  > TE DISAGREE EICAS FLAPS 1 HAD TO EXTEND ELECTRICALLY UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V123456 83, FAULT TREE 82 AND 809...TOMC MO PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC RELATED WORK ORDER 00000000
- [SDR CALA2022121403370](https://openairdocs.org/sdr/CALA2022121403370.md): Fseu · faulted · Dec 12, 2022 · N68061 · Boeing 767424ER · Trailing Flap Position Indicating System
  > L/E SLAT DISAGEE EICAS AND 6, LEFT INBOARD AND RIGHT INBOARD WERE NOT FULLY EXTENDED. FURTHER INSPECTION REQUIRED. REFER TO FAULT TASK 27-51 FAULT TREE 809 AND 27-51 FAULT TREE 815. FSEU BITE REQUIRED. UPON ARRIVAL DEBRIEF CREW. NO OVERSPEED OCCURRED. ISS
- [SDR CALA2022113003260](https://openairdocs.org/sdr/CALA2022113003260.md): Line · blocked · Nov 30, 2022 · N68061 · Boeing 767424ER · Waste Disposal System
  > LEFT SIDE LAVATORIES INOPERATIVE DURING FLIGHT ABOVE 16K, LAVATORY TANK FULL LIGHT ILLUMINATED. FWD WASTE SYS INOPERATIVE LIGHT ILLUMINATED, AND FWD WASTE TANK SHOWS MORE THAN 3/4 FULL. UNABLE TO DUMP FWD WASTE TANK SYS, MAY HAVE A BLOCKAGE IN DUMP LINE. REM
- [SDR CALA2022091202330](https://openairdocs.org/sdr/CALA2022091202330.md): None · corroded · Sep 9, 2022 · N68061 · Boeing 767 · Cabin Equipment/Furnishings
  > EA 2500-12538 OP 2 DURING ACCESS G2 GALLEY FLOOR SUPPORT REWORK, STA 325 LBL 22 - 44 FLOOR BEAM UPR SURFACE FOUND CORROSION. REF HX NR WO. 968113, ORIG BY V898556 CABIN FLOOR BEAM STA 325 UPPER CHORD REPAIRED AS PER ECRA 5315-0 1179 REV- BTN LBL 22" AND LBL 44
- [SDR CALA2022090902313](https://openairdocs.org/sdr/CALA2022090902313.md): None · none · Sep 9, 2022 · N68061 · Boeing 767 · Cabin Equipment/Furnishings
  > EA 2500-12538 OP 2 DURING ACCESS G2 GALLEY FLOOR SUPPORT REWORK, STA 325 LBL 22 - 44 FLOOR BEAM UPR SURFACE FOUND CORROSION. REF HX NR WO. 968113, ORIG BY V898556 CABIN FLOOR BEAM STA 325 UPPER CHORD REPAIRED AS PER ECRA 5315-0 1179 REV- BTN LBL 22" AND LBL 44
- [SDR CALA2022052301318](https://openairdocs.org/sdr/CALA2022052301318.md): Manifold · unserviceable · May 23, 2022 · N68061 · Boeing 767424ER · Smoke Detection
  > L ENG OVHT CAUTION AT CRUISE FL310 CONTACT TOMC EMC DESK WITH FINDINGS PRIOR TO CLEARING ITEM.. TOM EMC R. TOTH DOWN WIRING AND DETECTORS. UNABLE TO GENERATE ANY FAULTS. VISUALLY CHECKED ALL DETECTOR CONNECTIONS, NO SIGNS OF DEFECTS REF WDM26-11-12-2. L/P UNL
- [SDR CALA2021102902004](https://openairdocs.org/sdr/CALA2021102902004.md): None · missing · Oct 28, 2021 · N68061 · Boeing 767424ER · Leading Edge Slat Position Indicating System
  > #4 INBD LEADING EDGE SLAT IS MISSING A BLOWOUT PANEL AND SUSPECT INTERSTITIAL DUCT SEPARATED FROM LEADING EDGE TAI DUCT, REF IPC30-11-02-01, ITEM 365 ID,ITEM 355 DUCT NOTED IN #3 SLAT INTERSTITIAL DUCT. REMOVED SLAT PANELS 522DT, 523AT,523FT, 524AT. REMOVED IN
- [SDR CALA2021090801528](https://openairdocs.org/sdr/CALA2021090801528.md): Skin · dented · Sep 7, 2021 · N68061 · Boeing 767424ER · Trailing Edge Flaps
  > RIGHT INBOARD AFT FLAP HAS NUMEROUS DENTS FROM HAIL, THE LARGEST IS 1.25 INCH DIAMETER,.093 INCH DEEP, TAP TESTED AND NO DELAMINATION NOTED. REVIEWED AND LOCKED FOR MAINT FERRY UNLOCK RHW I/B AFT FLAP IN DENT LOCATIONS LISHED IN RI PAR4 PERFORMED REPAIR AS PE
- [SDR CALA2021090801527](https://openairdocs.org/sdr/CALA2021090801527.md): Panel · dented · Sep 7, 2021 · N68061 · Boeing 767424ER · Trailing Edge Flaps
  > LEFT OUTBOARD AFT FLAP HAS NUMEROUS DENTS, WORST BEING 35.5 INCHES OUTBOARD OF INBOARD EDGE 45 1/2 INCHES FROM TRAILING EDGE, 1.5 " DIAMETER,.040" DEEP. NO HOLES, TAP TESTED AND FOUND NO DELAMINATION. CORRECTION TO ORIGINAL WRITE UP: SHOULD READ LEFT OUTBOARD
- [SDR CALA2021090801524](https://openairdocs.org/sdr/CALA2021090801524.md): Skin · damaged · Sep 6, 2021 · N68061 · Boeing 767424ER · Elevator, Plate/Skin
  > LOG# 6677208 LEFT OUTBOARD ELEVATOR HAS EIGHT PUNCTURES FROM HAIL DAMAGE. 1. 23.5 INCHES IN BOARD FROM OUTBOARD EDGE, 3.5 INCHES FROM TRAILING EDGE, 1 INCH DIAMETER. 2. 35.5 INCHES INBOARD FROM OUTBOARD EDGE, 20" FROM TRAILING EDGE, 1 INCH DIAMETER. 3. 55.5 IN
- [SDR CALA2021090801523](https://openairdocs.org/sdr/CALA2021090801523.md): Skin · dented · Sep 6, 2021 · N68061 · Boeing 767424ER · Trailing Edge Flaps
  > LEFT INBOARD AFT FLAP UPPER SURFACE HAS 3 HOLES AND NUMEROUS DENTS. HOLES: 1. 64 INCHES INBOARD FROM OUTBOARD EDGE, 14.75 INCHES FROM TRAILING EDGE, THREE-QUARTER INCH DIAMETER. 2. 65.25 INCHES INBOARD FROM OUTBOARD EDGE, 5.5 INCHES FROM TRAILING EDGE, 5/8" DI
- [SDR CALA2021090301492](https://openairdocs.org/sdr/CALA2021090301492.md): Charger · failed · Sep 1, 2021 · N68061 · Boeing 767424ER · Emergency Lighting
  > MULT-33-3-0004 EMER LT PWR SUPPLY M6758 FAILED FUNCTIONAL TEST. EMER LT PWR SUPPLY M6758 CHARGER REPLACED & TESTED NORMAL AS PER AMM 33-51-07.
- [SDR CALA2021090301491](https://openairdocs.org/sdr/CALA2021090301491.md): Charger · failed · Sep 1, 2021 · N68061 · Boeing 767424ER · Emergency Lighting
  > MULT-33-3-0004 EMER LT PWR SUPPLY M7236 FAILED FUNCTIONAL TEST TRANSFER REF. EMER LT PWR SUPPLY M7236 CHARGER REPLACED & TESTED NORMAL AS PER AMM 33-51-07.
- [SDR CALA2021090301490](https://openairdocs.org/sdr/CALA2021090301490.md): Stiffener · cracked · Sep 1, 2021 · N68061 · Boeing 767424ER · Fuselage Miscellaneous Structure
  > AD2017-17-16 SUPPORT TASK EA 5310-07143 OP2 - RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL 159-185 FOUND 1EA CRACK RUNNING VERTICALLY APPROX 7/8" IN LENGTH.PLS PRINT AND ACCOMPLISH REPAIR PER OP4 TRANSFER REF. EA 5310-07143 REV D OP2 R/H NOSE W
- [SDR CALA2021090301489](https://openairdocs.org/sdr/CALA2021090301489.md): Stiffener · cracked · Sep 1, 2021 · N68061 · Boeing 767424ER · Fuselage Miscellaneous Structure
  > AD 2017-17-16 SUPPORT TASK - EA 5310-07143 OP1 - LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL159 TO 185 FOUND 1EA CRACK RUNNING VERTICALLY APPROX 7/8 " IN LENGTH.PLS PRINT AND AC COMPLISHED REPAIR PER OP3. TRANSFER REF. NON-ROUTINE LP 9130629 AND
- [SDR CALA2021090101485](https://openairdocs.org/sdr/CALA2021090101485.md): Stiffener · cracked · Sep 1, 2021 · N68061 · Boeing 767424ER · Fuselage Miscellaneous Structure
  > AD2017-17-16 SUPPORT TASK EA 5310-07143 OP2 - RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL 159-185 FOUND 1EA CRACK RUNNING VERTICALLY APPROX 7/8" IN LENGTH.PLS PRINT AND ACCOMPLISH REPAIR PER OP4 EA 5310-07143 REV D OP2. R/H NOSE WHEEL WELL VER
- [SDR CALA2021090101484](https://openairdocs.org/sdr/CALA2021090101484.md): Stiffener · cracked · Sep 1, 2021 · N68061 · Boeing 767424ER · Fuselage Miscellaneous Structure
  > AD 2017-17-16 SUPPORT TASK - EA 5310-07143 OP1 - LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL159 TO 185 FOUND 1EA CRACK RUNNING VERTICALLY APPROX 7/8 " IN LENGTH.PLS PRINT AND AC COMPLISHED REPAIR PER OP3. TRANSFER REF. EA 5310-07143 REV D OP1
- [SDR CALA2020012600230](https://openairdocs.org/sdr/CALA2020012600230.md): Skin · cracked · Jan 21, 2020 · N68061 · Boeing 767424ER · Fuselage Main, Plate/Skin
  > DOUBLER REPAIR INSTALL BTWN STA 1654.5 AND STA 1678 ALONG STR 13 R, REF SRM 53-80-01 REPAIR 7 DETAIL 7. THIS REPAIR NEEDS REPEAT INSPECTIONS EVERY 7500 FLIGHT CYCLES EITHER 30,000 CYCLES AFTER AC DELIVERY OR 7500 CYCLES FROM REPAIR INSTALLION, WHICHEVER COM ES
- [SDR CALA2019060700900](https://openairdocs.org/sdr/CALA2019060700900.md): Bottle · empty · Jun 5, 2019 · N68061 · Boeing 767424ER · Crew Oxygen System
  > DURING FLIGHT, CREW EMERGENCY O2 LEVEL FOUND DEPLETED TO 11 LBS. CREW O2 BOTTLE REPLACED ACC AMM12-15-08-603-001. P/N42365-1 S/N ON:R08-000164 S/N OFF:R14-000449. PERFORMED FURTHER T/S, FOUND F/O O2 MASK REPLACED IN MARCH BEFORE SEVERAL O2 SERVICES OCCURED. FO
- [SDR CALA2019032200454](https://openairdocs.org/sdr/CALA2019032200454.md): Socket · burned · Mar 22, 2019 · N68061 · Boeing 767424ER · Passenger Compartment Lighting
  > READING LIGHT ASSY AT 16L SMOKED UPON PAX TURNING LIGHT ON. F/A SHUT LIGHT OFF AND SMOKE DISSAPATED. PANEL WAS WARM/HOT TO THE TOUCH. LOCKING LOG TO ENSURE PSU IS DROPPED AND AN INSPECTION OF WIRING AND COMPONENTS ON BACK SIDE OF PANEL IS ACCOMPLISHED. SMOKE

Next page: https://openairdocs.org/aircraft/N68061/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 n_number = 'N68061' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N68061/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.