# Service difficulty reports: N76062

A list on [N76062](https://openairdocs.org/aircraft/N76062.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 · 66 reports

- [SDR CALA2026082618928](https://openairdocs.org/sdr/CALA2026082618928.md): Modulating Valve · faulty · Aug 24, 2026 · N76062 · Boeing 767424ER · Cabin Cooling System
  > DIVERSION IN TO LHR FROM VCE. CREW VERBAL: AFT CABIN TEMP UNCONTROLLABLE, VERY COLD STS MSG AND AUTO SNAPSHOT PHOTO UPDATE. L TRIM AIR CONT, AFT TEMP CONT STS. AFT CABIN TRIM VLV IND BLANK, IND CAME BACK WITH RESEATING THE CONNECTOR REF AMM 21-61-07-401. REP
- [SDR CALA2026060416830](https://openairdocs.org/sdr/CALA2026060416830.md): Light · inoperative · Jun 3, 2026 · N76062 · Boeing 767424ER · Emergency Lighting
  > 30D SEAT-MOUNTED EMERGENCY ESCAPE PATH LIGHT DOES NOT COMES ON. REMOVED AND REPLACED 30D SEAT-MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY REF AMM TASK 33-51-10-962-104. OPS CHECK GOOD. ITEM OK FOR SVC.
- [SDR CALA2026031714621](https://openairdocs.org/sdr/CALA2026031714621.md): Skin · dented · Feb 25, 2026 · N76062 · Boeing 767424ER · Fuselage Main, Plate/Skin
  > SECTION 46 AT LOWER SKIN BETWEEN STA 1439 / STA1461 AND STR 38R HAS DENT & CREASE CREATED THE SFR AND IT IS NECESSARY TO QC CHECK AND APPROVAL THE SFR THE SFR #3048 WAS REVIEWED BY QC. DENT/CREASE IN THE FUSELAGE SKIN BETWEEN STA 1439/1461 AND STGR - 38R WAS R
- [SDR CALA2025121912259](https://openairdocs.org/sdr/CALA2025121912259.md): Seal · missing · Dec 18, 2025 · N76062 · Boeing 767424ER · Wing Main, Frame Structure
  > RIGHT WING INBD AILERON BOTTOM SEAL MISSING.
- [SDR CALA2025080807495](https://openairdocs.org/sdr/CALA2025080807495.md): Light · broken · Aug 7, 2025 · N76062 · Boeing 767424ER · Emergency Lighting
  > SEATS 39D AND 40D WITH ESCAPE PATH LIGHTS BROKEN. CONFIRMED. REPLACED ESCAPE PATH LIGHT OF THE SEATS 39D AND 40D, IN REF AMM 33-51-10-962-104 ITEM OKAY FOR SERVICE.
- [SDR CALA2025050704514](https://openairdocs.org/sdr/CALA2025050704514.md): Light · unknown · May 4, 2025 · N76062 · Boeing 767424ER · Emergency Lighting
  > AFT RIGHT SERVICE DOOR EMERGENCY LIGHT FOUND INOP. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS IN REF TO TASK AMM 33-51-00-715-001, OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR CALA2025030702621](https://openairdocs.org/sdr/CALA2025030702621.md): Switch · detached · Mar 5, 2025 · N76062 · Boeing 767424ER · Light System Wiring
  > WIRE BALE FOR OVERHEAD EMERG EXIT LIGHT SW FELL OFF. PLACED IN C A/S PEN POCKET BTW L1+L2 WINDOWS REMOVED AND REPLACED SWITCH GUARD OVERHEAD PANEL.PARTS USED: 19-3351-3-0093,QTY:1
- [SDR CALA2024112801345](https://openairdocs.org/sdr/CALA2024112801345.md): Panel · missing · Nov 25, 2024 · N76062 · Boeing 767424ER · Wing, Plate/Skin
  > PDA 2 RH WING LE TAI PANEL 623AT MISSING ON INBOARD SIDE OF #9 SLAT SDR FLAGGED BLOW OUT PANEL ON PANEL 623AT MISSING. PANEL 623AT TEMPORAILY FITTED TO PREVENT FOD INCRESS. REPAIR OR REPLACE WHOLE PANEL AND REFIT ON COMPLETION OF WORK. REMOVED DUCT CONNECTOR A
- [SDR CALA2024112501262](https://openairdocs.org/sdr/CALA2024112501262.md): Oxygen Gen · faulty · Nov 25, 2024 · N76062 · Boeing 767424ER · Passenger Oxygen System
  > FLT ATTENDANT OXYGEN GENERATOR ACTIVATED AT EMERGENCY EXIT FWD OF PAX SEAT 38KL. REMOVED OXYGEN GENERATOR PER AMM 35-21-10-002-017 AND REPLACED WITH SERVICEABLE UNIT PER AMM 35-21-10-402-102.PARTS USED: 25-3511-3-0008,QTY:1
- [SDR CALA2024082000469](https://openairdocs.org/sdr/CALA2024082000469.md): Clamp · loose · Aug 20, 2024 · N76062 · Boeing 767424ER · Air Distribution System
  > R DUCT LEAK EICAS. RAN CHECKLIST TO COMPLETION. PERFOMED FIM 26-18 FAULT TREE 804. TEST PASSED. VISUALLY CHECKED R PACK BAY FOR LEAKS. FOUND LEAKS FROM FCV/SOV CLAMP LEADING TO HEAT XCHANGER. FURTHER T/S REQUIRED. SOURCE OF AIR IS APU BLEED. FOUND GAP AT CLA
- [SDR CALA2024062100048](https://openairdocs.org/sdr/CALA2024062100048.md): Pcb · faulted · Jun 21, 2024 · N76062 · Boeing 767424ER · Hydraulic Power System Wiring
  > C HYD DEM PUMP CAUTION MSG ILLUMINATED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 8089386 SN OFF 0122 CORRECT TRACKING TAG # IS 1952038 FIM 29-11 FAULT TREE 896 PERFORMED, FOUND ADP OVERSPEED/ELECTRONIC CARD M11291FAULTY, REPLACED IAW AMM 29-11-69 PB 401 OK
- [SDR CALA2024011500105](https://openairdocs.org/sdr/CALA2024011500105.md): Control Panel · broken · Jan 14, 2024 · N76062 · Boeing 767424ER · Autopilot System
  > ATL SELECT WINDOW DIALED TO ZERO WHEN WE TRIED TO SELECT A HIGHER ALT. REMOVED AND REPLACED MODE CONTROLL PANEL PER AMM 22-11-02. PERFORMED TEST 04 AND TEST 30. OPS CHECKS GOOD. A/C REMAINS FULLY CAT CAPABLE. OK FOR SERVICE.
- [SDR CALA2023072102303](https://openairdocs.org/sdr/CALA2023072102303.md): Pitot Tube · blocked · Jul 20, 2023 · N76062 · Boeing 767424ER · Pitot/Static System
  > JUST AFTER ROTATION BOTH FLIGHT DIRECTORS FAILED EICAS CAUTION I AS DISAGREE AIRSPEED DISAGREE, CAPTAINS AIRSPEED ROLLED BACK, 30-50 KNOTS LOWER THAN F/O IDT INSPECTED PITOT QUICK DISCONNECTS. DUE TO CAPT AIRSPEED LOSS, T/S BY INVESTIGATING CAPT PITOT STATIC P
- [SDR CALA2023072102300](https://openairdocs.org/sdr/CALA2023072102300.md): Indicator · faulty · Jul 19, 2023 · N76062 · Boeing 767424ER · Aircraft Fuel System
  > 800LB DIFFERENTIAL IN LT & RT MAIN TANKS ON DEPARTURE 2.1 DIFFERENTIAL WITH FUEL CONFIG LIGHT. CENTER TANK FUEL. RAN FUEL CONFIG BUT WAS UNABLE TO COMPLETE DUE TO CENTER TANK FUEL. RT NOTE: FUEL TANKS HAVE BEEN SUMPED & LT & RT TANK QTY CHECKED WITH DRIP STICK
- [SDR CALA2023042401230](https://openairdocs.org/sdr/CALA2023042401230.md): Bulb · inoperative · Apr 22, 2023 · N76062 · Boeing 767 · Emergency Lighting
  > EMERGENCY LIGHTS OPS CHECK {B767-33-3-7000} - DOOR 2R EXTERIOR EMERGENCY LIGHT WILL NOT COME ON RELAMPED IN REFERENCE AMM 33-51-06-902-082. OPSCHECK GOOD.
- [SDR CALA2023032400850](https://openairdocs.org/sdr/CALA2023032400850.md): Beam · corroded · Mar 22, 2023 · N76062 · Boeing 767 · Fuselage Structure (General)
  > CABIN - STA 303 LBL 20-55 FLOOR SUPPORT FOUND CORRODED TRANSFER REF. NON-ROUTINE HX NRC WO.1458064 AND ORIGINATED BY EMP NO. V897979 CABIN STA 303 BETWEEN LBL 20 AND LBL 55 FLOOR BEAM UPPER CHORD REPAIRED AS PER EC/RA 5310-08125 REV -. ATTACHED FORM 44-0008 IT
- [SDR CALA2023031500744](https://openairdocs.org/sdr/CALA2023031500744.md): Beam · corroded · Mar 13, 2023 · N76062 · Boeing 767* · Fuselage Structure (General)
  > CABIN - STA 325 LBL 20-36 FLOOR SUPPORT FOUND CORRODED TRANSFER REF. NON-ROUTINE HX NRC WO.1458070 AND ORIGINATED BY EMP NO. V897979 CABIN STA 325 LBL 20-36 FLOOR SUPPORT REPAIRED AS PER EC/RA 5310-08126 REV-. ATTACHED FORM 44-0008 ITEM 1 TO ITEM 36 ACCOMPLISH
- [SDR CALA2023030100588](https://openairdocs.org/sdr/CALA2023030100588.md): None · corroded · Feb 28, 2023 · N76062 · Boeing 767* · Fuselage Structure (General)
  > BULK CGO COMPT BILGE STA 1540 S38L -S39L SHEAR TIE FOUND CORROSION TRANSFER REF. NON-ROUTINE HX NRC WO.1469539 AND ORIGINATED BY EMP NO. V896810 BULK CARGO COMPT BILGE STA 1540 BETWEEN STR 38L AND STR 39 SHEAR TIE REPLACED AS PER SRM 51-10-02. ATTACHED FORM 44
- [SDR CALA2023021600453](https://openairdocs.org/sdr/CALA2023021600453.md): None · cracked · Feb 15, 2023 · N76062 · Boeing 767* · Fuselage Structure (General)
  > EA 5310-07143 REV D OP 001 AD2017-17-16 LH NOSE W/W VERT. STIFFENER ON STA 287 BETWEEN WL 159 AND 185 FOUND 1EA SUBSURFACE CRACK AS MARKED. PLEASE ACCOMPLISH REPAIR EA 5310-07143 OP 003 BEFORE FURTHER FLIGHT TRANSFER REF. NON-ROUTINE HX NRC WO.1443421 AND ORIG
- [SDR CALA2023021600452](https://openairdocs.org/sdr/CALA2023021600452.md): None · cracked · Feb 15, 2023 · N76062 · Boeing 767* · Fuselage Structure (General)
  > EA 5310-07143 REV D OP 002 AD2017-17-16 RH NOSE W/W VERT. STIFFENER ON STA 287 BETWEEN WL 159 AND 185 FOUND 1EA SUBSURFACE CRACK AS MARKED. PLEASE ACCOMPLISH REPAIR EA 5310-07143 OP 004 BEFORE FURTHER FLIGHT TRANSFER REF. NON-ROUTINE HX NRC WO.1443433 AND ORIG
- [SDR CALA2022102802989](https://openairdocs.org/sdr/CALA2022102802989.md): Feeder Cable · burned · Oct 28, 2022 · N76062 · Boeing 767424ER · Electrical Power System Wiring
  > ON TAKEOFF RT GEN OFF THROUGH 85KTS. FOUND #2 ENGINE IDG FEEDER CABLES AT UPPER PYLON JUNCTION FIRE BOX(INBOARD SIDE)MISSING INSULATION, BURNT & ARCING. IDENTIFIED WIRES DAMAGED. WIRES W208-001-3/0 AND W208-002-3/0 REMOVED DAMAGED WIRES W208-001-3/0 AND W208-
- [SDR CALA2022102402932](https://openairdocs.org/sdr/CALA2022102402932.md): Gcu · failed · Oct 24, 2022 · N76062 · Boeing 767 · AC Inverter
  > RT GEN OFF AFTER TAKE OFF. REMOVED AND REPLACED RIGHT ENG GCU, AFTER IDG REPLACED. ONLINE POWERING BUSSES. BPCU BITE TEST PASSED WITH NO FAULTS ALL THREE FEEDERS CHECK GOOD.4 OHMS TO GROUND. CHECKED ALL CT''S RECORDED AT THIS TIME. REF TASK 24-22-00-745-051-
- [SDR CALA2022092802524](https://openairdocs.org/sdr/CALA2022092802524.md): None · inoperative · Sep 28, 2022 · N76062 · Boeing 767 · Electrical Power System
  > RT GEN INOP. REF L/P 9615248 FOR PRIOR MX ACTION, ALSO C/W RIGHT ENG IDG MEL. ALL MX REQUIREMENTS VERIFIED FOR MEL 2400P ITEM PLACED ON MEL 2400P. ANDMX ACTION CW. DISCONNECT AS REQUIRED PER MEL 2400P, PLACING RIGHT ENG IDG ON DISPATCH DESK: 22 NAME: BB DATE
- [SDR CALA2022091902409](https://openairdocs.org/sdr/CALA2022091902409.md): Fmc · none · Sep 19, 2022 · N76062 · Boeing 767 · Flight Management Computing Software System
  > L FMC FAIL. REMOVED AND REPLACED LEFT FMC COMPUTER.
- [SDR CALA2022051801275](https://openairdocs.org/sdr/CALA2022051801275.md): Valve · stuck · May 17, 2022 · N76062 · Boeing 767424ER · Pneumatic Indicating System
  > RT ENG BLEED OFF AFTER TO. UNABLE TO RESTORE AIRCRAFT WILL REQUIRE #2 ENGINE HIGH POWER RUN AND BLEED AIR IADMM WORKING ITEM OPERATIONAL CHECK REF AMMT ASK 71-00-00-862-053-H03 AND TASK 36-00-00-862-047 AFTER AHM LOG PAGE 8577396 AND LP 8604759 HAVE BEEN CLEAR
- [SDR CALA2022022100464](https://openairdocs.org/sdr/CALA2022022100464.md): Skin · damaged · Feb 19, 2022 · N76062 · Boeing 767424ER · Fuselage Structure (General)
  > AIRCRAFR DAMAGE,LEFT SIDE, BELOW THE 14TH WINDOW, 7:00 POSITION, DAMAGE OUTER SKIN 10 INCH BY 4 INCH VERIFIED PER AVO 5900 PART A. STEPS 1 THRU 6. OK TO CONTINUE. PER AVO 5900 COMPLIED WITH PART A. STEPS 1 THRU 6. PER AVO9500 PART A STEP 7 HFEC CW ON CUTOUT R
- [SDR CALA2022021400382](https://openairdocs.org/sdr/CALA2022021400382.md): Skin · damaged · Feb 14, 2022 · N76062 · Boeing 767424ER · Fuselage Structure (General)
  > AIRCRAFR DAMAGE,LEFT SIDE, BELOW THE 14TH WINDOW, 7:00 POSITION, DAMAGE OUTER SKIN 10 INCH BY 4 INCH VERIFIED PER AVO 5900 PART A. STEPS 1 THRU 6. OK TO CONTINUE. PER AVO 5900 COMPLIED WITH PART A. STEPS 1 THRU 6. PER AVO9500 PART A STEP 7 HFEC CW ON CUTOUT R
- [SDR CALA2021100401773](https://openairdocs.org/sdr/CALA2021100401773.md): Fairing · missing · Oct 3, 2021 · N76062 · Boeing 767* · Nacelle/Pylon, Main Frame
  > PDA 3 #2 ENGINE INBD PYLON AFT FAIRING 447DB MISSING 1EA SCREW IN METAL PAN. INSTALLED SCREW AT #2 PYLON INBD AFT FAIRING PAN.
- [SDR CALA2021072101141](https://openairdocs.org/sdr/CALA2021072101141.md): Frame · cracked · Jul 19, 2021 · N76062 · Boeing 767424ER · Nacelle/Pylon, Main Frame
  > B767-06-3-0012 - NO.2 PYLON NAC STA 258 I/B FRAME FOUND CRACK. R EF N/R L/P 9130908. NO.2 PYLON NAC STA 285 I/B FRAME REPLACED AS PER SRM 51-10-02 AND NEW FRAME INSTALLED AS PER SRM 51-40-02 AND BOEING DWG 311T2350 & DWG 311T2400 FOR ATT FASTENER DETAILS. ADD
- [SDR CALA2020030700584](https://openairdocs.org/sdr/CALA2020030700584.md): Skin · cracked · Mar 4, 2020 · N76062 · Boeing 767424ER · Fuselage Main, Plate/Skin
  > B767-53-3-0076 - EMP STA 1645-1678 LH STA 4-5 SKIN FOUND CRACKED REF NR L/P 9130519 DOUBLER REPAIR PERFORMED PER SRM53-00-01 REPAIR 1 FIG 201 AS CAT B REPAIR. REPEAT INSP REQUIRED PER REPAIR 1 ZONE A R EPAIR INSP TABLE V. CURRENT PTT77487, PTC11675 12,000C INT
- [SDR CALA2019112702102](https://openairdocs.org/sdr/CALA2019112702102.md): Ecu · malfunctioned · Nov 26, 2019 · N76062 · Boeing 767424ER · Engine (Turbine/Turboprop)
  > L ENG COMPRESSOR STALL W/ VISIBLE TORCHING EICAS L ENG CONT STAT US NOW L ENG EEC C1 ACCOMPLISH FIM TASK 71-05-00-815-848-N01 AND AMM 72-00-00/601 UNUSUAL CONDITION INSPECTION. CARRIED OUT FIM TASK PER 71-05-00-815-848-H01 AND UNUSUAL CONDITION INSPECTION AS P
- [SDR CALA2019042200632](https://openairdocs.org/sdr/CALA2019042200632.md): Nut Plate · missing · Apr 22, 2019 · N76062 · Boeing 767424ER · Nacelle/Pylon, Main Frame
  > #2 ENG INBD PYLON PANEL 446CL HAS 1 MISSING NUTPLATE. REPLACED NUTPLATE REF SRM 51-40-02
- [SDR CALA2018022700826](https://openairdocs.org/sdr/CALA2018022700826.md): Power Supply · no test · Feb 27, 2018 · N76062 · Boeing 767424ER · Emergency Lighting
  > EMERGENCY LIGHTS POWER SUPPLY AT ROW 1LK AND 24AB NOT TESTING INDIVIDUALLY IAW TASK CARD 64-3351-1-3800, STEP B. SLAVED GOOD KNOWN BATTERY STILL NO GOOD, SUSPECT POWER SUPPLY. REPLACED THE POWER SUPPLIES AT SEATS 1KL AND 24AB, OPS CHECKED OK.
- [SDR CALA2017050101205](https://openairdocs.org/sdr/CALA2017050101205.md): Control Module · faulty · May 1, 2017 · N76062 · Boeing 767424ER · Buffet/Galleys
  > OVEN 607 SMOKE WHILE USING. COOKS TOO HOT. REPLACED THE OVEN 607 CONTROL MODULE ASSY.
- [SDR CALA2017050101204](https://openairdocs.org/sdr/CALA2017050101204.md): Heater · odor · May 1, 2017 · N76062 · Boeing 767424ER · Air Distribution System
  > FLIGHT CREW REPORTED HEATER AT THE L1 DOOR HAD A BURNED ODOR, SHUT OFF AND ODOR WENT AWAY. IT HAS PREVIOUS HISTORY. REPLACED THE HEATER IAW AMM 21-45-23-404-002, OPS CHECKED GOOD.
- [SDR CALA2017041400983](https://openairdocs.org/sdr/CALA2017041400983.md): Unknown · odor · Apr 14, 2017 · N76062 · Boeing 767424ER · Air Distribution System
  > 1R DOOR HAD BURNING PLASTIC SMELL AFTER TAKEOFF BUT THEN DISSIPATED. CREW REPORT SMELL COMING MORE LIKELY FROM GALLEY AND DISAPPEAR ITSELF AREA INSPECTED IAW AMM 05-51-58-200-801C1. NIL FINDING.
- [SDR CALA2017033100767](https://openairdocs.org/sdr/CALA2017033100767.md): Web · cracked · Mar 29, 2017 · N76062 · Boeing 767424ER · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON MID SPAR IDG FEED CABLE THROUGH CUTOUT SKIN FOUND CRACKED. CUTOUT THE CRACKED AREA AND REPAIRED IAW SRM 54-55-01, REPAIR 2, FIG 202, DETAIL I.
- [SDR CALA2017033100765](https://openairdocs.org/sdr/CALA2017033100765.md): Web · cracked · Mar 28, 2017 · N76062 · Boeing 767424ER · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON MID SPAR IDG FEEDER CABLE THROUGH CUTOUT SKIN FOUND CRACKED AT NAC STA 222.25 FORWARD MID SPAR WEB CRACKEDREPAIRED AS PER SRM 54-55-01, REPAIR 2, FIG 203, DETAIL I.
- [SDR CALA2017031200581](https://openairdocs.org/sdr/CALA2017031200581.md): Floorbeam · corroded · Mar 11, 2017 · N76062 · Boeing 767424ER · Fuselage Main, Floor Beam
  > CABIN - STA 325 LBL 35-57 FLOORBEAM FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-10-02, CORROSION REMOVED AREA MEASURED DEPTH 0.035" (ORG THK: 0.100") X WIDTH 2" X LENGTH 3" OUT OF SRM 53-00 -51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT. CORRODED FLOORBEAM UPP CHORD
- [SDR CALA2017012000144](https://openairdocs.org/sdr/CALA2017012000144.md): Pump · faulty · Jan 20, 2017 · N76062 · Boeing 767424ER · Engine Fuel Pump
  > R N1 3 PCT LESS THAN L N1 AT TAKEOFF PWR. ALL OTHER INDICATIONS IN NORMAL RANGE. OK INFLT PER INBOUND CREW, SHOULD READ LEFT ENGINE WAS 3% LOWER N1 THAN RIGHT ENGINE. REPLACED NR 1 ENG FUEL PUMP DUE TO FAILED PRESSURE TEST PER AMM 73-11-01-705-001-H00. PER AMM
- [SDR CALA2017011600110](https://openairdocs.org/sdr/CALA2017011600110.md): Unknown · malfunctioned · Jan 16, 2017 · N76062 · Boeing 767424ER · Powerplant System
  > LEFT ENGINE INDICATION WOULD NOT REACH COMMANDED POWER ON THE TAKEOFF ROLL CARRIED OUT CHECK AND SECURITY OFF EEC CONNECTIONS NO DEFECTS NOTED. REMOVED N1FAN SPEED SENSOR REF AMM 77-12-01-004-007-H00 CARRIED OUT INSPECTION OF INTEGRITY NO DEFECTS NOTED. CARRIE
- [SDR CALA2016080100478](https://openairdocs.org/sdr/CALA2016080100478.md): Switch · cracked · Jul 31, 2016 · N76062 · Boeing 767424ER · Hydraulic Pump (Electric/Engine), Main
  > LOW RIGHT HYD QTY, FOLLOWED QRH AND RETURNED TO DEPARTURE. FOUND DIFFENTIAL INDICATOR ON RT EDP PRESSURE MODULE BROKEN AND LEAKING. REPLACED IAW AMM 29-11-17 AND SERVICED RT HYDRAULIC SYS AS REQUIRED. NO FURTHER LEAKS NOTED. ACFT OK FOR CONTINUED SERVICE
- [SDR CALA2016062700387](https://openairdocs.org/sdr/CALA2016062700387.md): Shutoff Valve · damaged · Jun 26, 2016 · N76062 · Boeing 767424ER · Pneumatic Distribution System
  > ON TAKEOFF ROLL ABOVE 100 KTS LT ENGINE BLEED OFF EICAS MSG FOLLOWED BY LT PARK OFF. FOUND LT HPSOV DAMAGED. REPLACED SAME. RAN NR 1 ENGINE. CHECKS NORMAL.
- [SDR CALA2015021200100](https://openairdocs.org/sdr/CALA2015021200100.md): Gcu · malfunctioned · Feb 11, 2015 · N76062 · Boeing 767424ER · AC Regulator
  > INBOARD FLIGHT CREW DID NOT GENERATE ITEM FOR DIVERSION FROM TOMC LOG. AFTER TAKEOFF RT GEN TRIPPED IAW QRH APU IS RUNNING. CREW & DISPATCH IN AGREEMENT & WILL CONTINUE FLIGHT. TROUBLE SHOT IAW FIM 24-22-00-745-051 & 24-20-00-815-821. BPCU CONFIRMED RIGHT
- [SDR CALA2015010600001](https://openairdocs.org/sdr/CALA2015010600001.md): Battery Pack · discharged · Dec 30, 2014 · N76062 · Boeing 767424ER · Emergency Lighting
  > MULT-33-3-0001 VCC CLOSET G4 LT FLOOR PROXIMITY EMER LIGHT FOUND 2 EA DO NOT LIGHT UP. BATTERY PACK M7235 REPLACED & LAMP TEST RESULTED NORMAL IAW AMM 33-51-10.
- [SDR CALA2014123001548](https://openairdocs.org/sdr/CALA2014123001548.md): Skin · damaged · Dec 29, 2014 · N76062 · Boeing 767424ER · Fuselage Main, Plate/Skin
  > FOUND DAMAGE TO BE 2 INCHES LONG BY 1.5 INCHES WIDE BY.094 INCHES DEEP AT STATION 400 BETWEEN STRINGER 31L & 32L. PLACED DENT ON DIP IAW SRM 53-00-01 ALLOWABLE 1. MAKE A DETAIL INSPECTION EVERY 300 FLIGHT CYCLES. HEFC INSPECTION EVERY 3000 FIGHT CYCLES OR
- [SDR CALA2014051200578](https://openairdocs.org/sdr/CALA2014051200578.md): Control Panel · faulty · May 9, 2014 · N76062 · Boeing 767424ER · Weather Radar System
  > WEATHER RADAR FAIL AFTER TAKEOFF, ENTERED FOR B6989. REPLACED RADAR CONTROL PANEL IAW MM 34-43-02, OPERATIONS CHECKED GOOD. ROTABLE PARTS CHANGE WAS INDICATED TT 1398533, SN OFF 09011, PANEL CONTROL, OFF 64-3443-9-0001 9011 & ON 64-3443-9-0001 3158.
- [SDR CALA2012042600300](https://openairdocs.org/sdr/CALA2012042600300.md): Tie Down · corroded · Apr 26, 2012 · N76062 · Boeing 767424ER · Fuselage, Seat/Cargo Attach Fittings
  > BS 1615, RBL 44.5 TIE DOWN SUPPORT FITTING CORRODED. TIE DOWN SUPPORT FITTING REPLACED IAW 20-11-00 AND SRM 51-40-04.
- [SDR CALA2012042000280](https://openairdocs.org/sdr/CALA2012042000280.md): Floorbeam · corroded · Apr 20, 2012 · N76062 · Boeing 767424ER · Fuselage Main, Floor Beam
  > CABIN BS 303 LBL 21 TO 55 FLOORBEAM CORRODED. CABIN BS 303 LBL 6" TO LBL 64" FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-00-51 REPAIR FIG 201 AND AFEC NIL CRACK FOUND ATTACH MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1 TO ITEM 26 ACCOMPLISHED.
- [SDR CALA2012042000279](https://openairdocs.org/sdr/CALA2012042000279.md): Floorbeam · corroded · Apr 20, 2012 · N76062 · Boeing 767424ER · Fuselage Main, Floor Beam
  > CABIN BS 325 LBL 21 TO 55 FLOORBEAM CORRODED. CABIN BS 325 LBL 15" TO LBL 63" FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND AFEC NIL CRACK FOUND ATTACH MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1 TO ITEM 30 ACCOMPLISHED.

Next page: https://openairdocs.org/aircraft/N76062/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 = 'N76062' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N76062/reports

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