# Service difficulty reports: N66056

A list on [N66056](https://openairdocs.org/aircraft/N66056.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 · 73 reports

- [SDR CALA2026101920475](https://openairdocs.org/sdr/CALA2026101920475.md): Aileron · contaminated · Oct 16, 2026 · N66056 · Boeing 767424ER · Ailerons
  > DURING LT OTBD AILERON THERMOGRAFIC INSPECTION WAS NOTICED ONE POINT OF MOISTURE INGRESS ABOUT 25 INCHES FROM INBOARD EDGE LOWER SURFACE, ON A PREVIOUS REPAIR, WS 934.2 DAMAGE B# UPGRADE THE ATTRIBUTES TO MAJOR, PERFORMED THE SFR AND QC CHECK. ALL THE STEPS
- [SDR CALA2026101920473](https://openairdocs.org/sdr/CALA2026101920473.md): Aileron · contaminated · Oct 16, 2026 · N66056 · Boeing 767424ER · Ailerons
  > DURING LH OUTBOARD AILERON THERMOGRAFIC INSPECTION WAS NOTICED ONE POINT OF MOISTURE INGRESS ON INBOARD EDGE LOWER SURFACE STA 910.45 DAMAGE C# UPGRADE THE ATTRIBUTES TO MAJOR, PERFORMED THE SFR AND A QC CHECK. ALL THE STEPS OF THE EC/RA:5760-01129 WERE ACCO
- [SDR CALA2026081818717](https://openairdocs.org/sdr/CALA2026081818717.md): Bulb · inoperative · Aug 17, 2026 · N66056 · Boeing 767424ER · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT OVER SEAT 1L DOESN'T WORK PROPERLY. REPLACED LANP BULB IN REF AMM AISLE LIGHT - LAMP REPLACEMENT IN REFERENCE AMM TASK 33-51-05-002-039, ITEM OK PARTS USED: 00-0596-3-2874,QTY:1
- [SDR CALA2026041515388](https://openairdocs.org/sdr/CALA2026041515388.md): Control Panel · odor · Apr 14, 2026 · N66056 · Boeing 767424ER · Indicating/Recording System
  > ELECTRICAL ODOR COMING FROM OVERHEAD ANNUN PANEL FLAGGED SDR AND FILLED IN REMOVED PART INFO UPDATED PART INFO FOR SDR REMOVED AND REPLACED OVERHEAD MISCELLANEOUS ANNUCIATOR PANEL PER CMM 33-16-52. ALL LIGHT TEST PASSED. PANEL SECURED. COMPLIED WITH SMOKE/ODOR
- [SDR CALA2026041515379](https://openairdocs.org/sdr/CALA2026041515379.md): Unknown · odor · Apr 14, 2026 · N66056 · Boeing 767424ER · Air Distribution System
  > ELECYRICAL BURNING ODOR IN THE COCKPIT CAN SMELL AT THE MAIN DO OR AIRCRAFT HAS BEEN ON THE GROUND 24 HOURS WITH NO AIRCONDITIONING HOOKED UP. TEMPERATURES TODAY WERE IN HIGHS 80F. STARTED APU WITH PACKS ON. NO ELECTRICAL ODOR. INSPECTED COCKPIT ALL DISPLAYS
- [SDR CALA2026012613299](https://openairdocs.org/sdr/CALA2026012613299.md): None · none · Jan 26, 2026 · N66056 · Boeing 767424ER · Standard Practices/Structures
  > REMOVED DOOR 1L BUSSEL AND PINNED SLIDE TO FOM. REMOVED SAFETY PIN AND INSTALLED BUSTLE REF AMM TASK 25-66-01-404-072 C/W RII FOR THE REACTIVATION OF THE L1 ESCAPE SLIDE PER THE GMM
- [SDR CALA2026012613276](https://openairdocs.org/sdr/CALA2026012613276.md): Plunger · out of adjust · Jan 26, 2026 · N66056 · Boeing 767424ER · Service Doors
  > DOOR 1R TOOK 3X TO DISARM. REMOVED BUSTLE, PINNED SLIDE AND REMOVED GIRT BAR TO FOM REF AMM TASK 25-66-01-004-001. ADJUSTED FWD R1 PLUNGER SPRING REF IPC 52-11-01-06D FIGURE NUMBER 715 PERFOMED OPS CHECK GOOD REF AMM TASK 52-11-00-715-128 NO BINDING AT THIS T
- [SDR CALA2026012613241](https://openairdocs.org/sdr/CALA2026012613241.md): Module · faulted · Jan 26, 2026 · N66056 · Boeing 767424ER · AC Power Distribution System
  > ON TAKEOFF HIGH SPEED AND LOW SPEED STALL SPEED TAPES OVERLAPPED ON FO SIDE W LOW AS EICAS. FO SIDE BITE YSM LRU PER FIM 27-09 FT 815. FOUND MX MSG 27-41076. R & R RT FSPM IAW AMM 27-58-01. OPS CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME.
- [SDR CALA2026010612694](https://openairdocs.org/sdr/CALA2026010612694.md): Door · fod · Jan 3, 2026 · N66056 · Boeing 767424ER · Service Doors
  > 1R DOOR DIFFICULT TO ARM/DISARM REMOVED DEBRIS FROM 1R ENTRY/SERVICE DOOR AND PERFORMED OPERATIONAL TEST REF AMM TASK 52-11-00-715-128 WITH GOOD RESULTS. OK FOR FURTHER SERVICE.
- [SDR CALA2025122912501](https://openairdocs.org/sdr/CALA2025122912501.md): Module · faulty · Dec 26, 2025 · N66056 · Boeing 767424ER · Trailing Edge Flap Control System
  > UNSCHEDUALED STAB TRIM EICAS 7 TIMES DURING FLIGHT WITH AUTOPILOT ON & OFF. FOUND R FSPM FAULT MSG. 27-41076 ON YAW DAMP/STAB TRIM MODULE RIGHT. R & R FLAP/STABILIZER POSITION MODULE IAW AMM 27-58-01-904-001. PERFORMED FSPM TEST, BITE CHECKED GOOD. PERFORME
- [SDR CALA2025102010309](https://openairdocs.org/sdr/CALA2025102010309.md): Fitting · fod · Oct 20, 2025 · N66056 · Boeing 767424ER · Service Doors
  > DOOR 1R DOES NOT ARM. REMOVED DEBRIS FROM FLOOR FITTING, DOOR ARMS NORMALLY.
- [SDR CALA2025101610159](https://openairdocs.org/sdr/CALA2025101610159.md): Bottle · low pressure · Oct 15, 2025 · N66056 · Boeing 767424ER · Escape Slide
  > EMERGENCY ESCAPE SLIDE PRESSURE LOW 1L PERFORMED VISUAL INSPECTION OF L1 DOOR SLIDE CYLINDER REF AMM 25-66-02, NEEDLE ON GREEN BAND OK TO CONTINUE.
- [SDR CALA2025101610165](https://openairdocs.org/sdr/CALA2025101610165.md): O-Ring · leaking · Oct 14, 2025 · N66056 · Boeing 767424ER · APU Engine Fuel and Control
  > FUEL FUMES IN THE CABIN AND COCKPIT CONFIRMED FUEL ODOR COMING FROM BOTH PACKS. T/S TO APU FUEL LEAKING FUEL. APU FIRE HANDLE PULLED. INSPECTED APU, FOUND LEAK AT FUEL LINE. REMOVED AND REPLACED RECIRCULATION AIR FILTERS IAW AMM 21-25-02 AS PRECAUTION IAW AMM
- [SDR CALA2025101009905](https://openairdocs.org/sdr/CALA2025101009905.md): Pressure Switch · faulted · Oct 8, 2025 · N66056 · Boeing 767424ER · Fuel Controlling System
  > R ENG FUEL FILT MSG AFTER LEVEL OFF... ALL OTHER ENG INDICATION NORMAL REF FIM 73-11 FAULT TREE 803 T/SHOOTING, R/H FUEL FILTER REPLACED AS PER AMM 73-11-02 NIL FINDINGS, REPLACEMENT OF FUEL FILTER DIFFERENTIAL TRANSMITTER REQUIRED. FUEL PX SWITCH R & R IAW
- [SDR CALA2025070806313](https://openairdocs.org/sdr/CALA2025070806313.md): Fuel Sys · leaking · Jul 6, 2025 · N66056 · Boeing 767424ER · APU Engine Fuel and Control
  > TOXIC FUMES IN CABIN. APU FUEL LEAK. RAN BOTH PACKS, INSPECTED THE CABIN AND PERFORMED INSPECTION IAW AMM 05-54-56. NO SIGN OF ODOR FUMES THROUGHOUT THE CABIN.
- [SDR CALA2025061105465](https://openairdocs.org/sdr/CALA2025061105465.md): Pca · leaking · Jun 10, 2025 · N66056 · Boeing 767424ER · Hydraulic System, Main
  > RIGHT HYD QTY LOW PER CREW DEBRIEF, APPEOX 2 HRS INTO FLT, HYD QTY STARTED TO DECREASE & NOT FLUCTUATE ON ARRIVAL QTY IND SHOWS.39 WITH BRAKES SET MATCHING HYD SERVICE PANAL GAUGE. ON ARRIVAL PERFORMED GVI OF RT MLG, WINGS, & BELLY OF A/C WITH NO NOTIABLE LEA
- [SDR CALA2025042504243](https://openairdocs.org/sdr/CALA2025042504243.md): Lamp · inoperative · Apr 24, 2025 · N66056 · Boeing 767424ER · Emergency Lighting
  > EMERGENCY LIGHTS OPERATIONAL CHECK FOUND SLIDE AND OVERWING ESCAPE LIGHT EMERGENCY INOPERATIVE NEAR DOOR 4L/H. REMOVED AND REPLACED LAMP FROM SLIDE AND OVERWING ESCAPE LOGHT EMERGENCY NEAR DOOR 4L/H AS PER AMM TASK 33-51-06-902-082. GOOD FOR SERVICE.
- [SDR CALA2025041703956](https://openairdocs.org/sdr/CALA2025041703956.md): Idg · faulted · Apr 16, 2025 · N66056 · Boeing 767424ER · AC Generator-Alternator
  > RT GEN OFF. RESET ONCE. FAILED A SECOND TIME. PERFORMED BPCU BITE PER MM 24-11- 00. FOUND MM 24-35002 FOR RIDG PHASE A CURRENT DISAGREE. PERFORMED BPCU BITE PER MM 24-11-00. FOUND R IDG PHASE A CURRENT DISAGREE, MM 24-35002. PERFORMED BPCU BITE PER MM 24-11-00
- [SDR CALA2024012900249](https://openairdocs.org/sdr/CALA2024012900249.md): Pump · faulted · Jan 26, 2024 · N66056 · Boeing 767424ER · Fuel Boost Pump
  > RIGHT AFT FUEL PUMP FAILED IN FLIGHT DEFECTS NOTED. REF FIM 28-22 FAULT TREE 819. ACCOMPLISHED IDT REQUIREMENTS OF CDCCL BONDING JUMPER SAFETY AND SECURITY. ELECTRICAL BONDING RESISTANCE CHECK WITHIN LIMITS IAW AMM TASK 28-22-03-404-074, AMM TASK 28-22-03-706-
- [SDR CALA2023122603738](https://openairdocs.org/sdr/CALA2023122603738.md): Stiffener · cracked · Dec 18, 2023 · N66056 · Boeing 767424ER · Fuselage Miscellaneous Structure
  > LHW L/E STA 665 FRONT SPAR ATTACH STIFFENER FOUND CRACKED TRANSFER REF. NON-ROUTINE HX NRC WO.2487576. LHW L/E STA 665 FRONT SPAR STIFFENER FABRICATED AND INSTALLED ATTACHED FORM 44-0008 ITEM 1-17 ACCOMPLISHED. IAW RI NO. RI-57-00-16577 (FINAL NO DEVIATION WI
- [SDR CALA2023122003677](https://openairdocs.org/sdr/CALA2023122003677.md): Stiffener · cracked · Dec 18, 2023 · N66056 · Boeing 767424ER · Fuselage Miscellaneous Structure
  > CABIN PRESSURE DECK PNL STA 971 BTN LBL 85.9 AND LBL 97.42 STIFFENER AND L ANGLE FOUND CRACKED TRANSFER REF. NON-ROUTINE HX NRC WO.2534260. CABIN PRESSURE DECK PANEL STA 971 BTN LBL859 TO LBL97.42 STIFFENER AND ANGLE REPLACED AS PER SRM 51-10-02 AND EC/RA NO.
- [SDR CALA2023122003693](https://openairdocs.org/sdr/CALA2023122003693.md): Stiffener · cracked · Dec 13, 2023 · N66056 · Boeing 767424ER · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 1 PYLON NACELLE STRUT AFT TORQUB BOX (INT) O/B STIFFENER AT NAC. WL 1436 AND NAC STA 265.4-295 FOUND DAMAGE. REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02
- [SDR CALA2023122003691](https://openairdocs.org/sdr/CALA2023122003691.md): Tee Fitting · corroded · Dec 11, 2023 · N66056 · Boeing 767424ER · Fuselage Main, Attach Fittings
  > RH BS955 T-FITTING FOUND CORRODED TRANSFER REF. RH STA 955 T FITTING REPLACED AS PER EC/RA NO.5340-02175 REV-.
- [SDR CALA2023122003679](https://openairdocs.org/sdr/CALA2023122003679.md): Tee Fitting · corroded · Dec 11, 2023 · N66056 · Boeing 767424ER · Fuselage Miscellaneous Structure
  > TEE FITTING FOUND CORRODED TRANSFER REF. NON-ROUTINE HX NRC WO.2533217. LH BS 955 T FITTING REPLACED AS PER EC/RA NO.5340-02174 REV-. ATTACHED FORM 44-0008 ITEM 1-8 ACCOMPLISHED.
- [SDR CALA2023120803591](https://openairdocs.org/sdr/CALA2023120803591.md): Shear Tie · corroded · Dec 5, 2023 · N66056 · Boeing 767424ER · Fuselage Internal Mounting Structure
  > BULK CARGO COMPT - BELOW FLOOR SHEAR TIE FOUND CORROSION AT STA 1540 BTN S38L-S39L (AS MARK) TRANSFER REF. NON-ROUTINE HX NRC WO.2494482 AND BULK CARGO COMPT BELOW FLOOR SHEAR TIE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 AT STA 1540 BTN S
- [SDR CALA2023071202215](https://openairdocs.org/sdr/CALA2023071202215.md): Beam · corroded · Jul 10, 2023 · N66056 · Boeing 767424ER · Fuselage Main, Structure
  > CABIN FWD WET AREA FOUND CORROSION ON THE TEE CHORD UPPER SURFACE OF PREVIOUS FLOOR BEAM REPAIR AT STA303 LBL46.5 REFER TO BSH N 0329 PERFORMED FLOOR BEAM REPAIR AT STA303 AS PER ECRA5310-08166 DETA IL STEPS REF TO ATTACHED 44-0008 FORM WORK ACCOMPLISHED BY V9
- [SDR CALA2023071202214](https://openairdocs.org/sdr/CALA2023071202214.md): Beam · corroded · Jul 10, 2023 · N66056 · Boeing 767424ER · Fuselage Main, Structure
  > CABIN FWD WET AREA FOUND CORROSION ON THE TEE CHORD UPPER SURFACE OF PREVIOUS FLOOR BEAM REPAIR AT STA325 LBL55 REFER TO BSH N03 30 PERFORMED FLOOR BEAM REPAIR AT STA325 AS PER ECRA5310-08167 DETA IL STEPS REF TO ATTACHED 44-0008 FORM WORK ACCOMPLISHED BY V914
- [SDR CALA2023013000268](https://openairdocs.org/sdr/CALA2023013000268.md): Seal · missing · Jan 30, 2023 · N66056 · Boeing 767424ER · Fuselage Structure (General)
  > LH MAIN FUEL QTY HARNESS NEEDS SEALING AT BUSSING PLUG AND 2 EACH INTERNAL GROMETS AT RIB FEED THROUGH. REF AMM 28-41-09 INSTALLED BUSSING PLUG AND SEALED GROMET AT PANEL 541JB/HB COMPLETED SEALING GROMETS.
- [SDR CALA2022051301224](https://openairdocs.org/sdr/CALA2022051301224.md): Hydraulic Line · leaking · May 13, 2022 · N66056 · Boeing 767424ER · Hydraulic Power Accumulator, Main
  > CENTER HYD QTY DROPPED TO.46RF TWO HOURS INTO FLT WHILE AT CRUISE...C HYD PRESS NORMAL ON INITIAL WALK AROUND FOUND HYDRAULIC FLUID LEAK, RIGHT WING FOUND CROSS UNION LEAKING REF LPC 32-32-56-03 ITEM 520. REMOVED TRAILING EDGE JUST OUTBOARD OF RIGHT LANDIN
- [SDR CALA2022030300552](https://openairdocs.org/sdr/CALA2022030300552.md): Control Panel · unserviceable · Mar 3, 2022 · N66056 · Boeing 767* · Autopilot Computer
  > MCP ALTITUDE WINDOW CANT BE CHANGED WITH A/P ON HAVEE TO CLICK O FF A/P AND FD TO CHANGE ALT REPLACED MODE CONTROL PANEL IAW AMM INSTALLATION REFERENCE: TASK 22-11-02-402-008 PERFORMED TEST 04 AND TEST 30 REFERENCE: TASK 22-00-02-742-006-001 OPS CK GOOD ACFT
- [SDR CALA2021092701685](https://openairdocs.org/sdr/CALA2021092701685.md): Drain Line · cracked · Sep 24, 2021 · N66056 · Boeing 767424ER · Wash Water System
  > B767-25-3-0068 - FWD CARGO L/H STA 480 TO STA 500 SIDE WALL INSI DE, A GALLEY DRAIN LINE, CONNECT RUBBER HOSE FOUND TORN. REF N/R L/P 9130151 AND ORIGINATED BY EMP V896834. FWD CARGO L/H STA 480 TO 500 SIDE WALL AREA GALLEY DRAIN LINE RE PLACED AS PER AMM 20-1
- [SDR CALA2021091701591](https://openairdocs.org/sdr/CALA2021091701591.md): Shear Tie · corroded · Sep 15, 2021 · N66056 · Boeing 767424ER · Fuselage Internal Mounting Structure
  > SUPPORT TASK - BULK CGO COMPT BELOW FLOOR STA 1417 S39L - S39R P OS SHEAR TIE FOUND CORROSION. REF N/R L/P 9131333 AND ORIGINATED BY EMP V896810 BULK CARGO COMPT BELOW FLOOR (STA 1417 S39L-39R SHEAR TIE REPLAC ED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS P
- [SDR CALA2021091701590](https://openairdocs.org/sdr/CALA2021091701590.md): Shear Tie · corroded · Sep 15, 2021 · N66056 · Boeing 767424ER · Fuselage Internal Mounting Structure
  > SUPPORT TASK - BULK CARGO BELOW FLOOR STA 1417 S37L - S38L SHEAR TIE FOUND CORROSION. RER N/R L/P 9131332 AND ORIGINATED BY EMP V896810 BULK CARGO BELOW FLOOR STA 1417 S3TL-38L SHEAR TIE REPLACED AS P ER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02,
- [SDR CALA2021091701592](https://openairdocs.org/sdr/CALA2021091701592.md): Shear Tie · corroded · Sep 15, 2021 · N66056 · Boeing 767424ER · Fuselage Internal Mounting Structure
  > SUPPORT TASK - BULK CARGO STA 1417 S38L - S39L POSITION SHEAR TI E FOUND CORROSION. REF N/R L/P 9131387 AND ORIGINATED BY EMP V89 6810. BULK CARGO STA 1417 S38L-39L SHEAR TIE REPLACED AS PER SMR 51-10 -02 AND FASTENER INSTALLED AS PER SRM 51-40-02, DWG 146T121
- [SDR CALA2021091501581](https://openairdocs.org/sdr/CALA2021091501581.md): Shear Tie · corroded · Sep 15, 2021 · N66056 · Boeing 767424ER · Fuselage Internal Mounting Structure
  > SUPPORT TASK - BULK CARGO BELOW FLOOR STA 1417 S37L - S38L SHEAR TIE FOUND CORROSION. RER N/R L/P 9131332 AND ORIGINATED BY EMP V896810 BULK CARGO BELOW FLOOR STA 1417 S3TL-38L SHEAR TIE REPLACED AS P ER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02,
- [SDR CALA2021091501576](https://openairdocs.org/sdr/CALA2021091501576.md): Shear Tie · corroded · Sep 15, 2021 · N66056 · Boeing 767424ER · Fuselage Internal Mounting Structure
  > SUPPORT TASK - BULK CARGO STA 1417 S38L - S39L POSITION SHEAR TI E FOUND CORROSION. REF N/R L/P 9131387 AND ORIGINATED BY EMP V89 6810. BULK CARGO STA 1417 S38L-39L SHEAR TIE REPLACED AS PER SMR 51-10 -02 AND FASTENER INSTALLED AS PER SRM 51-40-02, DWG 146T121
- [SDR CALA2021090801530](https://openairdocs.org/sdr/CALA2021090801530.md): Stiffener · cracked · Sep 7, 2021 · N66056 · Boeing 767424ER · Fuselage Miscellaneous Structure
  > SUPPORT TASK - EA5310-07143 REV.D OP 002, AD 2017-17-16 RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BETWEEN WL 159 AND 185. FOUND CRACK GENERATED AND ACCOMPLISH OP 004. REF N/R L/P 913051 8. RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BETWEEN WL 15
- [SDR CALA2021090801529](https://openairdocs.org/sdr/CALA2021090801529.md): Skin · cracked · Sep 7, 2021 · N66056 · Boeing 767424ER · Fuselage Main, Plate/Skin
  > SUPPORT TASK - EA 5380-01178 REV A OP 003 L/H FUSELAGE SKIN BETW EEN 1654 TO 1678 FOUND 2EA CRACK AT STR 13AL APPROX 3/8" AND 5/8 " IN LENGTH. N/R L/P 9130401 AND ORIGINATED BY EMP V924736 CREATE REPEAT INSPECTION AS PER SRM 53-80-01-2R-7 REPAIRT TABLE 202 DET
- [SDR CALA2021083001456](https://openairdocs.org/sdr/CALA2021083001456.md): Panel · missing · Aug 30, 2021 · N66056 · Boeing 767424ER · Wing, Plate/Skin
  > PDA 3 UPON ARRIVIAL FOUND PANEL 621FB ON RIGHT WING MISSING. FURTHER DETAILS AWAITED
- [SDR CALA2020030700583](https://openairdocs.org/sdr/CALA2020030700583.md): Bracket · missing · Mar 4, 2020 · N66056 · Boeing 767424ER · Main Landing Gear
  > FOUND AT RH MLG ABOVE TIRE #7 BRACKET LOOSE AND MISSING 1 BLOCK AT ELETRICAL CONDUIT. REF. IPC 32-10-50-01E ITEM 205. PART NEEDED P/N 287T6138-9 ACCOMPLSHED VISUAL INSPECTION AT WIRE CONDUIT, NO DAMAGE FOUND. FABRICATED A CLAMP BLOCK WITH RUBBER MOUNT AS REQUI
- [SDR CALA2018022100734](https://openairdocs.org/sdr/CALA2018022100734.md): Web · cracked · Feb 21, 2018 · N66056 · Boeing 767424ER · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON MID SPAR WEB FOUND CRACKED. REPAIRED IAW SRM 54-55-01, REPAIR 2, FIG 202, DETAIL I.
- [SDR CALA2018022100733](https://openairdocs.org/sdr/CALA2018022100733.md): Floorbeam · corroded · Feb 21, 2018 · N66056 · Boeing 767424ER · Fuselage Main, Floor Beam
  > FLOORBEAM BS 324, LBL 55 FOUND CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-02. REPAIRED IAW ECRA 5310-07355, REV.
- [SDR CALA2018022100732](https://openairdocs.org/sdr/CALA2018022100732.md): Web · cracked · Feb 21, 2018 · N66056 · Boeing 767424ER · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON NAC STA 223, MID SPAR WEB FOUND CRACKED. REPAIRED IAW SRM 54-55-01, REPAIR 2, FIG 202, DETAIL I.
- [SDR CALA2018022100715](https://openairdocs.org/sdr/CALA2018022100715.md): Light · dim · Feb 21, 2018 · N66056 · Boeing 767424ER · Emergency Equipment
  > COCKPIT OVERHEAD PORTABLE EMERGENCY EXIT LIGHT FOUND DIM. REPLACED THE LIGHT AND TEST NORMAL IAW AMM 33-51-01
- [SDR CALA2018021600630](https://openairdocs.org/sdr/CALA2018021600630.md): Floorbeam · corroded · Feb 9, 2018 · N66056 · Boeing 767424ER · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM BS 347, RBL 32 TO 41 FOUND CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-02, AND FOUND OUT LIMITS IAW SRM 53-00-51 ALLOWABLE DAMAGE 1, FIG 101. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201, DETAIL I.
- [SDR CALA2017120804327](https://openairdocs.org/sdr/CALA2017120804327.md): Altimeter · stuck · Dec 8, 2017 · N66056 · Boeing 767424ER · Altimeter, Barometric/Encoder
  > STBY ALTIMETER HANGS UP THEN JUMPS 250 FT DURING CLIMB. STBY ALTIMETER REPLACED PER AMM 34-13-06-344-031. ALL INDICATION S NOW NORMAL
- [SDR CALA2017120104264](https://openairdocs.org/sdr/CALA2017120104264.md): Battery Pack · inoperative · Dec 1, 2017 · N66056 · Boeing 767424ER · Emergency Lighting
  > FOUND L4 EXTERIOR EMERGENCY LIGHT NOT OPERATING. REMOVED AND REPLACED L4 EXTERIOR EMERGENCY LIGHT BULB AND M739 BATTERY PACK IAW WDM 33-512-15.L4 EXTERIOR EMERGENCY LIGHT VISUALLY OPS CHECK OK, A/C OK TO CONTIN UE.
- [SDR CALA2017120104263](https://openairdocs.org/sdr/CALA2017120104263.md): Bulb · inoperative · Dec 1, 2017 · N66056 · Boeing 767424ER · Emergency Lighting
  > L2 EXTERIOR EMERGENCY LIGHT INOP. R&R L2 EXTERIOR LIGHT BULB AND SECURED LIGHT ASSEMBLY. VISUAL OPS CHECK OF L2 EXTERIOR LIGHT, CHECKS GOOD. A/C O.K. TO CONTINUE.
- [SDR CALA2017042301120](https://openairdocs.org/sdr/CALA2017042301120.md): Flashlight · inoperative · Apr 23, 2017 · N66056 · Boeing 767424ER · Emergency Equipment
  > 2L FWD FACING FLASHLIGHT NOT CHARGING. REPLACED EMERG FLASHLIGHT AT 2L.
- [SDR CALA2015111300928](https://openairdocs.org/sdr/CALA2015111300928.md): Monitor · faulty · Nov 13, 2015 · N66056 · Boeing 767424ER · Hydraulic Quantity Indicator
  > LOST RT HYD FLUID SYS, QTY READS ZERO. NOTE TWO HOURS INTO FLIGHT QTY RETURNED TO NORMAL 1.10. PLACED ON MEL RT HYD QTY INDICATION INOPERATIVE. TROUBLESHOOTING REQUIRED. COMPLIED WITH DDP CHECK BEFORE EACH DEPARTURE FLIGHT IAW FIM 29-11-00-815-899-0-01. R

Next page: https://openairdocs.org/aircraft/N66056/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 = 'N66056' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N66056/reports

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